EPJ55B/S 75-122
o^v
I
INFORM1TION ON FU
CERTIFIC1TION OF IIICRIFT
JINUKRY 1975
U.S. ENVIRONMENUL PROTECTION I6ENCV
Washington, o.c. 20460
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EPH-550/8-75-022
IFIClTili OF
JifW 197S
by
Carl Modig
U.S. ENVIRONMENTAL PROTECTION AGENCY
Office of Noise Abatement and Control
Washington, D.C. 20460
Under contract No. 68-01 -3115
This report has been approved for general availability. The contents of this
report reflect the views of the contractor, who is responsible for the facts and
the accuracy of the data presented herein, and do not necessarily reflect the
official views or policy of EPA. This report does not constitute a standard,
specification, or regulation.
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EPH-550/S-75-022
Flfi
1IICRAF7
JI1IRY 1975
by
Carl Modig
U.S. ENVIRONMENTAL PROTECTION AGENCY
Office of Noise Abatement and Control
Washington, D.C. 20460
Under contract No. 68-01-3115
This report has been approved for general availability. The contents of this
report reflect the views of the contractor, who is responsible for the facts and
the accuracy of the data presenter! herein, and do not necessarily reflect the
official views or policy of EPA. This report does not constitute a standard,
specification, or regulation.
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PREFACE
Under Section 7 of the Noise Control Act of 1972 (Public
Law 92-574), the Environmental Protection Agency (EPA) is authorized
to propose to the Federal Aviation Administration, aircraft noise
regulations, including the application of §uch regulations in the issuance,
amendment, modification, suspension or revocation of any .certificate
authorized by the Federal Aviation Act of 1958 (49 U.S. C. 1431).
This study was undertaken to furnish EPA with an overview
of aircraft type certification regulations (e.g., original type, supplemental,
airworthiness, etc.) through which aviation noise regulations are or
i
could be implemented.
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TABLE OF CQNTENTS
(
Page
1. Introduction j
2. Certification process 3
2. 1 Requirements and procedures for certificates 3
2. 1. 1 The various kinds of certificates 3
2. 1. 2 New Type Certificates (TC's) 5
2. 1. 3 Amendments to Type Certificates 10
2.1.4 Supplemental Type Certificates (STC's) 19
2. 1. 5 Other kinds of type certificates 21
2. 1.6 Airworthiness Certificates (AC's) 22
2.2 How certificates are conveyed 23
2. 3 Periods for which certificates are effective 24
3. Specific types and models certificated since 1969 25
3. 1 Listing of Types/Models complying with; FAR 36 25
noise limits in Appendix C of.FAR 36.
3.2 Turboprop aircraft in the Transport category 28
4. Sources of information 29
5. List of references 37
Appendix A:
Sample sheets from "Type Certification
Project Status" Log . A-l
Appendix B:
Extent of Changes in Aircraft Modified by
Amendment to Type Certificate B-l
Appendix C:
Annual Production (or Sales) of Selected
Transport or Turbojet Aircraft. C-l
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1. INTRODUCTION
As requested by EPA/ONAC a literature search and study
has been made on the following; with special reference to transport
category aircraft..
(1) Certification proce ss. Information on what requirements
and procedures must be met (from application to award)
to obtain "original type,' certificates," "amended type
certificates," "supplemental type certificate s, " .etc .
How are these certificates conveyed and for what periods
of time are they effective?
!
(2) Specific types and models certificated since 1969. Since
December 1, 1969 to date, what transport category
aircraft models (including business jets) have been
certificated in accordance with FAR Part 36, compared
to a listing of all transport category aircraft models.
t
The listed aircraft are'to be grouped according to the
various types of certificates granted. For aircraft other
than those for which an "original type certificate" was
granted, major airframe and/or engine changes which
were made from the original model are: to be indicated.
(3) Recent annual production statistics or estimates.
The certification process is complex. One expert consulted
called it "a bag of worms. " Parts of it .are more clearly documented
and clearly explained than others, and other parts are ambiguous
unless the actual practice is examined case by case. One reason for
this is that the FAA documentation of 'the process is itself complex
i
(FAR. Part 21; Part 25, since we are talking chiefly about transport
aircraft; plus handbook on Typ<=- riprti firatiori} No 8110.4, issued to
FAA personnel). A second reason is that the process is decentralized
to the FAA regions, with only summary reporting to FAA headquarters
in Washington. Details of the process, may vary from region to region.
Furthermore, in the region controlling a particular ce.rti tication
i
process, large portions of the work may be delegated to an FAA
Designated Engineering Representative (DER), who is frequently an
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employee of the applicant manufacturer. The amount delegated
cannot easily be described, for it depends on the judgment of
regional FAA officials, the complexity and scope of the case, and
the reputation and integrity of the manufacturer.
On the other hand, parts of the process are documented
in such detail that it is not possible to summarize all of the fine
points iti this overview. For this reason, the reader is urged to
consult FAR 21 and the Type Certification Handbook 8110. 4 if he
has detailed questions about a particular aspect of the process
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2. CERTIFICATION PROCESS
2. 1 Requirements and Procedures for Certificates
2.1.1 The Various Kinds of Certificates
FAA issues two main types o± certificates on aircraft:
those on types and those on individual aircraft. Certification actions
on types include:
/ '
New Type Certificates (TC's)
/ '
Amendments to Type Certificates
! '
Supplemental Type Certificates (STC's)
Amendments to Supplemental Type Certificates
Restricted TC's
Provisional Certificates:
Clas.s I Provisional Type Certificates .
Class II Provisional Type Certificates
Provisional Amendments to Type Certificates
In addition to type certificates, the FAA, when requested,
certifies each U.S. registered aircraft to be air-worthy.* There are
standard and special airworthiness certificates (AC's)
Standard: (for aircraft type certificated in the normal,
utility, acrobatic, or transport categories)
Special: restricted airworthiness certificates;
limited airworthiness certificates';
provisional airworthine ss certificates;
special flight permits ;
experimental.
All aircraft should be registered. All registered aircraft are
not airworthy.
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There arc other types of FAA certificates thai arc related
!
to type re rtificates and airworthiness certificates bul do not certify
aircraft. There is the Production Certificate (PC), awarded to certain
manufacturing facilities for particular aircraft types. The manufacture
of an aircraft at a Production Certificated location facilitates the award
of airworthiness certificates. There is the Delegation Option Authorization,
allowing the holder of TC's and a PC for helicopters and small aircraft
to award themselves other TC's, PC's and AC's. This power does not
evidently extend to cover any transport and/or business jet aircraft,
since the only turbojet engines eligible are of not more than 1000 Ibs.
thrust. Finally, there is the Designated Alteration Station (DAS), by
which the FAA delegates the power to issue STC's, and certain air-
worthiness certificates, to the aviation industry.
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2.1.2 New Type Certificates
Type Certificates are issued for aircraft engines and
propellers as well as for aircraft. Since recently added revisions to
the Federal Aviation Regulations have various dates of effectiveness,
the date of application for a type certificate determines which require-
ments of the FAR must be met. An application for the transport
t
i
category is effective for five years; for the other ordinary categories
(normal, utility, acrobatic) it is three years unless an exception is
granted. Besides new aircraft designs, existing designs also undergo
the new type certificate process if prpposed design changes are "so
extensive that a substantially complete investigation of compliance
with the applicable regulations is required" ( 21.19)*; For transport
category aircraft, Part 21 spells this out further as a change in the
number of engines or in the method of propulsion (e.g. propeller to
jet).
Formerly, the definition pf "transport aircraft" included
aircraft over 12, 500 Ibs. ( Handbook., Appendix 1, Page 2), but it has
recently been changed to cover any airplanes carrying at least 10
passengers, regardless of weight.**
Anyone may apply for a type certificate. The application
is made using FAA form 312, "Application for Type .Certificate,
Production Certificate, or Supplemental Type Certificate." It is
made to the. region in which the applicant is located and is accompanied
by a three view drawing of the aircraft plus available preliminary
All references are to the FAR 21 as of November 1, 1974 ("21. --"
or to the last version available (''Handbook /-"), of FAA Handbook
8110.4, Type Certification.
See FAR Section 23. 1 and 135. 144.
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basic data. The region then becomes the controlling region; the
.Engineering and Manufacturing Branch/Aircraft Certification Staff/
Aircraft Engineering Division of that region processes the application
and issues the certificate, in accordance with policy set by the Engineer-
ing and Manufacturing Division of the Washington office. There is one
exception to regional independence: special conditions. If it is found
per FAR 21. 101(b) that the airworthiness regulations of FAR 21 do
not contain adequate or appropriate safety standards because of a
novel or unusual design feature, special conditions must be issued
with the TC. Proposed special conditions are developed by the region,
giving the applicant and other interested parties opportunity to par^
ticipate, but they are issued by the Engineering and Manufacturing
Division, Washington, with the assistance of the Office of the General
,j
Counsel. The detailed procedures are to be found in the Handbook,
pp. 3 to 4-3..
Under FAR 21.21 the applicant is entitled to a TC in the
! -
normal, utility, acrobatic or transport categories if he "submits the
I ype design, test reports and computations" necessary to show that
it meets:
o the airworthiness requirements of the FAR
° the aircraft noise requirements of the FAR
o and any special conditions prescribed.
In addition,the type certificate data sheet must be prepared
and, for transport category aircraft, the airplane flight manual
must be FAA-approved. Specific requirements for transport category
aircraft are to be found in FAR 25.
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Steps -- The region sets up a Type Certificatioa Board
(TCB) with prescribed FAA membership (Handbook, p. 6-7,) and
chaired by the Region Chief, Engineering and Manufacturing Branch.
During its lifetime, the TCB holds at least three meetings: preliminary,
preflight and final. At the preliminary meeting a first draft of th^
FAA Type Inspection Authorization (TIA, Form 8110-1) should be
prepared as far as possible; special compliance teams should be formed
for probable problem areas (e. g., cockpit visibility). Also, the TCB
must determine whether the special conditions process, involving
Washington, must be initiated. Then manufacturing inspection by FAA
inspectors continues to determine that the prototype aircraft conforms
with drawings and specifications, and to evaluate special manufacturing
processes. The degree to which FAA inspectors spot check or inspect
intensively is partly determined by the 'manufacturer's experience
(Handbook, p. 39), but at any rate, much of the inspecting must be
done by the applicant's own staff. Conformity check results are
reported on Conformity Inspection Report forms (CIR's , Form 8100-1).
Processes and fabrication methods must be specified by process
drawings and specifications, which also become part of the Type Design.
If there are any particularly "complex, controversial, or
troublesome" design features, the Chairman of the TGB may* appoint a
Critical Design Review (CDR) team, to work concurrently with the
standard regional type certification program. Technical assistance
from Washington usually is included on the CDR team.
When the documentation forming the Type Design is
i
complete, and the prototype aircraft is ready, the final TIA is issued
authorizing ground and flight inspections. The TCB holds its pre-flight
meeting.
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The ground inspection physically determines that "the
aircraft submitted for FAA flight test meets the minimum requirements
for quality, conforms with the technical data, " and is safe to fly.
The ground inspection proceed, in three phases: (1) preliminary, -
including inspections that had been made during the course of development
and construction; (2) official, which the FAA performs just prior
to the FAA flight test; (3) coordinated ground-flight inspection,
to determine that the aircraft is airworthy and all deficiencies so
far uncovered are corrected before FAA flight testing. The second
phase is performed only after the manufacturer has submitted a
Statement of Conformity (FAA Form 317), which is his committment
that the prototype aircraft is ready for FAA final inspection and
flight test. At the conclusion pf the ground inspection the ground
portion of the Type Inspection Report (TIR, Form 8110-5 for air-
planes) must be prepared in time for review by the final TCB meeting.
The flight tests follow. (An experimental certificate pf
airworthiness must be obtained before any flight testing).
The final TCB is then held to review outstanding questions
and establish the TC data sheet items. The TC is issued upon
resolution of all outstanding items.
i
Within 90 days of TC issuance, the flight inspection
portion of the Type Inspection Report (TIR) should be completed,
completing the TIR. The TIR now contains results of all official
TC inspections, and is retained by the certificating region for refer-
ence purposes. It is an in-house FAA document; the applicant may
get a copy only after all internal FAA and proprietary information
is removed.
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Form -- the TC includes the Type Design (Z1.31), the
operating limitations, the TC data sheet, and the "certification basis":
the applicable regulations and special conditions (often issued by FAA
letter) with which the Administrator records compliance. The TC
data sheet is distributed to all regions and the Washington office, and
is available to the public. The complete TC. since it includes the
r
Type Design, is not available to the public but may be seen by the
National Transportation Safety Board. Special conditions are filed
as dated material in the FAA General Counsel's office.
TC's are transferable to other persons and can also be
made available by licensing agreements.
TC's are issued for foreign-manufactured aircraft from
countries with which the U. S. has an agreement for acceptance, pro-
vided, inter alia, that the civil air authority of the other country signs
a Certificate of Airworthiness for Export and technical data are sub-
mitted, including data on aircraft noise airworthiness showing noise
levels no greater than that under FAR 36. (21. 29)
The holder of a TC becomes eligible to receive a Produc-
tion Certificate. Almost all holders of TC's for transport category
aircraft get them, judging by all recent TC's for jet transport aircraft.
(The number of the PC is listed on the TC data sheet. ) The reason
is simple: aircraft manufactured under a PC become eligible for a ,
standard Airworthiness Certificate (AC) without further showing.
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2.1.3 Amendments to TC's
Amendments to TC's and Supplemental TC's (STC'sj are very
similar in form, requirements and purpose, and compared to TC's,
form the vast bulk of FAA type certificating activity. They differ
from each other in the following way: anyone may apply for a
STC, but only the holder of a TC may apply for an amendment to
the TC. (21. 113) Application is made to the FAA region where the
Type Design is filed.
Requirements -- Alterations introducing a major change
in a product require an amendment of the TC, or an STC. The
language of 21.93 implies that a major change is one having ah
"appreciable effect on the weight, balance, structural strength,
reliability, operational characteristics, or other characteristics
affecting the airworthiness of the product."
The following charts (Tables IA & IB) list certificated
jet transports together with data about the TC and amendment-to-TC
processes. It -will help to clarify how the processes have worked
in practice for this type of aircraft. The information is excerpted from
the TC data sheets.
In general, the applicant need satisfy only the require-
ments of the regulations incorporated in the original TC.*
However, under 21.101(a), an exception is made for the pro-
visions of FAR 36, including amendment 2, which must be met
irrespective of the date of the original TC.
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TABLES IA S; IB (following pages)
INFORMATION ON CERTIFICATION OF AIRCRAFT
LA: at least some models of the aircraft were approved on or
after December 1, 1969
IB: All models of the aircraft approved before December 1 , 1969
Notes to Tables
1) Source of all data columns 114: FAA Aircraft Type Certification
Data Sheets and Specifications updated to include all revisions
issued through October 1974.
2) Source of all data columns 15 17: FAA Summary of Supplemental
Type Certificates. Includes all issued through September .1974. '
3) For the group of IB, there may have been revision in the data
sheets after December 1, 1969, but no approvals of new.models
or serie s of models .
4) With one exception, no STC has been issued for transport category
jet aircraft for changes to engines or major changes to airframes.
Such changes otherwise have always been covered by an amendment
to the TC, as shown in the tables. However, in the last few years,
some applications have been made to re-engine business jets using
an STC, although no STC has yet been issued by the FAA. See
footnote, page 20. .
5) In cases where no "date of application" is given, it is because it
was not given on the TC data sheet.
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TABLE IA
Approved Before! December 1P(J£
Approved Cn Or After 1 December 1S'69
HI (2) (3) (4) |5) (6) (7)
TCHo.'Jer Basic Mode! TC FAA Date Dale Latert
Region of Approved Revision
Application (and date
of)
U.S. Airlines
Fleirt - 4 cnplne
EoeLrg V47, -100, -2008, A20WE North- 12/30/69 Rev. 6
-200r, 747SR western (5/1/74)
f
U.S. Airlines
1 Fleet - 3 engine
1 LocUsced L-10i:-3SS-l A23WE Western 4/14/72 Rev. 9
(9/1S/74)
McDonnell DC-10-10, -30, A22WE Western 7/29/71 Rev. 1
Doujlai -30F, -40 (6/S/73)
l
(8) !9) CO)
Models Date Engine
Approved Ty^ic(s)
(11) (12) (13) (14) l
Models Dale Engine N'nMire of ?
Approved Tyyc(s) Ch».".ge;.'Notcj !
I. 747-100 12/30/69 4 PCW
JT9D-3,
-3A.-7,
or 7A
II. 747-200D 12/23/70 same Extended range version.
Stren^tliened corroon-
ents. Increased grrsa
weight.
III. 747-200F 3/7/72 JT9D-3A, Freighter version of
-7, or-7A 747-2003, Cargo doer,
mod* to interior, rtrength
IV. 747-200C 4/17/73 tanie "Convert-liJc-vcrslon of
747-200B icrics
I. U1011 4/14/72 3 Rolls Noie: Special contiitionj
385-1 - P.oycc, on alrframe, H25-17-WE
RB21 ^-22 6 amendment ao. 1 of
C-02, RB 12/3/71.
211-22CA,
RB211-22B
U DC-10- 7/29/71 3 Cu CF6- For all models, special
-10 6DorCF conditions No. 25- '.5-
6-6D1 W^7of 25-17-V.'E-7
of 1 of 7/9/7:, and
2S-46-V/E-4 o! 10/26/72
IL DC-10-40 10/20/72 3 PCW JT Engines with water
9D-20 Injection.
IlL DC-10-30 11/21/72 3 CE CF6-
50A
IV. DC. 1 0-30 3/30/73 3 CE CF6- Freighter version of
T ---50A -JI1.
.5) (16) (17)
o. Approx. T>",i:c.". !
sued N*. Oi.:v -. ;
cf Hcldert
54 20 Irjta'.'atloa of a^o-ics,
~>-dor: picrur- r,.v.e=i:.
ci:j;o con:ai=ers VS^ASC
co.-rt7.-.rt7=an-2. :'vj ^e-.'.'.rc
e-r u;';:r:»^ etc.
9 8 Interior pisenger coic^amaect
rnodiScaticMii.
19 12 I=r^Ilaio^ of nods :o ps^tcqer
com pa meet
ro
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TABLE IA
Approved Before 1 December 1969
Approved On Or After December 1?69
n on STCi
'!! (?) (3) (4) (5) (6) (7)
'.'C Holder Basic Model TC 'FAA Date Date latest
Region of Approved Revision
Controlling Application (and date
of)
U.S. Alr'iric
Heel - 2 engine
5oci.-.r. 737-100 series A16WE North- 10/9/64 . 12/15/67 Rev. 6
-200 scries western . (757-112) (5/1/73)
-2CCC series
British BAG 1-11 A5EU European 10/4/61 4/15/65 Rev. 14
Aircraft Corp. 200 series (2/4/74)
1-11 400
serirs
1
.
(8) (?) (10)
Date Engine
Approved Typets)
L 737-100 series various: 2 PSW jf
12/15/67 8D-7, -9.
7/14/69 or-I5
11/12/63
Ha. 737-200 scries models same
201 serial nos. except
20632 C 20633, 205
except serial 8/3/71,
serial 20344, 222
except serials 20529-
331, 247, 248, 275
except seiials 2C5S8
C 20670, 2S1 except
serials 20413,20414,
20449-452, 20506-503,
291, 297, 271 except
. serial 20589, 2A3, 2/6,
2E1 except serial 20?00,
2CO, 2B2, except Z0680,
except serial '.ii758, 244
!"a". 1-11 200 series 4/15/65 .2 Rolls
except amended as follows: Royce
Model 204/AF 5/13/6S Spey
212/AR 3/29/66 506-14.
215/AM 4/13/66 -I4A, 14C,
or 14O
11" a". 1-11 400ierle9
except amended as
follows:
Model 410/AQ 9/1/66 2 Rolls
Spey
511-14, or
-14W
(11) (12) ;13) (14)
Models Drtte Engine Nature cf
Approved Typefs) Changes/ N'otes
Ib. 737-200 series various same Note: Various speciSc
All other models mode's la a series Here
C serial numbers . approved on different
except those dates. Thus, there are
listed under Ilu. 3 dates of approval for
the 1 model series, 47
dates for !», ap.d If dates
.'or HI type aircr.ifi.
n. 737-200C series, various same
All models except
-202C/210C serial
nos. 1D426, 19594,
which were approved
.before 12/l/6a
f'b". 1-11 200 series. 3/26/70 same as la. Note: Special conditions a
model 201/7/ AC recorded in (British) Air
Registration Board X'alida-
tion Arrangements Note 1
Issue 1.
Exemptions to FAR 25:
553A fue! Jedsoning
5-i9 max. passen.;?rj.
»"b". 1-1! 400 S/14V73 511-14W
seriefmodelT412A/
EB
151 (16) (ir;
^'o. Approx, Typical
ssued No. of Charges
Holder!
3 20 Installs doc of nods to
passe=s*: Cibio, avicclcs
li^is, cat JO Laadllni
pallers. e*.c.
29 16 InstallJtlca of tvlo^ics, mods
to passeEjw cabir^ aux. fuel
tarJcs ' c asjo cerEparjnenS,
etc.
I
r-1
to
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TABLE IA
Aopr-vccl Before 1 December 1969 '
_Apnroved_gr__'rT_After 1 DecemberJT69
m:1 f.:.on t-n S'VC'i
i" 0 (3) (4) (S) . (6) . (7)
TC:-!o!^fr i;;ric Moiiel TC FAA Date Date Latest
Region of Approved Revision
Controlling Application (and date
j c-f)
i
Orh.T- 2 ermine
;
j l»r.ii:l Ai:vr.ift "Aero Comman- A2S\Sr Soutli- S.':l/61 11/4/64 Rev.ll
L-.lu-tri« der": H21, 112IA, wcrtem, (reissued (7/27/73)
!!21B,1123 Technical IAI7/19/
data now 69)
fi!<-d with
: Ew;-^aji
region.
I
i
j
Ce»nJ Air- "Citation": 500 A22CE Central 7/16/68 9/9/71 Rev. 4
crjftCi-., . (PTC issued 7/15/74
Wlchiu per FAR
121. sr
6/29/71)
Avlalion !»:., -A/522, -1A/R- (11/26/73
Er-sljaJ 522,-3A/RA,
-400A, Secch-
r.'fl Ell :2S-400.-\
i -600A
/ivicvu Falcon Series A7EU European 9/13/62 6/9/65 . Rev. 7
! M-ireci C, D, E, F (6/13/72)
IA.M.D. )
1
,
'
(S) (9) (10)
Models Date Engine
Approved Tp*e(s)
L 1121 11/4/64 2 CE
II. 1I21A 9/19/67 CJ610-1,
or 610-5
HI. 11218 4/23/68 CJ610-1,
CJ610-5
L DM. 12S-1A 9/25/64 2 Bristol
II. DH. I2S-1A/522 2/3/66 Siddeley Viper
III. DH. 12S-3A 11/7/66 .522
FV. DH. 125-1A/R-522 8/9/67 same as II
VI. DH. 12S-1A/S-S22 8/9/67 " "
VII. DH. 125-3A/RA 2/15/68 " "
VIII. DH. I25-400A 2/15/68 " "
11/15/68 " "
I. Kan Jet Falcon 6/9/65 2 CE CF-700-
2C
II!. Series D 6/20/6S CF-700-2D
(H! (12) (13)
Models Date Engine
Approved Typc(s)
IV Cancelled
V 1123 12/8/71. 2 CE
CJ610-9
I. 500 9/9/71 2PCWJTI5D-
1, OT United
Aircraft of
Canada JT15D-
1
IX. Becchcraft 7/14/70 Viper 522
Hawker EH. 125-
4OOA
>L BH. 125-600A 8/17/72 2 R.oHs Roycc
(1971) Bristol
Engine C-iv.
Viper 601- 22
II, Series C 2/24/70 CF-700-2C
IV, Series E 2/24/70 CF-700-2D-2
V. Series F 2/24/70 CF-700-2D-2
(14)
Nature of
Charges/ Notes
'
Increased weight, htgh-
lift wing, greater -ensLne
thrust C fuel capacity,
fuselage length. Note:
Special conditions: FAA
letters of 12/13/63,
6/2/64 Exemptions: S44
f. 660. Complies with
FAR 36 (I)(c)(2)
Note: Special con-
ditions: 25-25-
CE-4.
Same as VHI exception
for name plates and
data plates.
Increased fuselage length,
weights, speeds. Com-
plies with FAR 36(1}
(c)(2)
3 -disc brahfls C increased
fuel capacity
3-dJscbrakes G increased
fuel capacity
Installation of high lift
devices on wing leading
edges.
15) (16) -(17)
N'o. .-'.;.::-rox. Typical
Lssix^l N >. OiiTiijes
of Ho Men
'
40 24 Avion!?:. :r.o
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TABLE IA
Approved BcforeAJPecembfr 1969e
^Approved On Or After 1 December 1969
Information on STCs
(!) (=) (3) (4) (5) (6) (7)
TC Holder Hasic Model TC FAA Date Date Latest
Region of Approved Revision
Controlling Application (and date
of)
.
fli-l_-..2-en^i.-_conifluid
c-«" Learlct 24.24A, A10CE Central 5/13/65 3/17/66 Rev. 12
Uarjct Cor,'. 24B, :4B-A, 24C, . ' . (8/1/74)
(V.lchlra) T-1D, 24D-A, 25,
23A, :5B, 2SC,
35, 16
.
_
i .
| Roc!-.-.>eU "Sabrelinei" A2WE Western 3/23/62 Rev. 10
lntcm-t!,?njl Roc^-eU Inter- 4/1/74)
C.-rp. (Vibre- ration.-!! NA-
llner Kv. ) 265, 265-20, -30,
-40, -60, -70, -SO
!
i
i
f
Dausali Falcon 10 A33£'J European 6/8/69 9/20/73
(S) ' (9) (10)
Models Date Engine
Approved Typefs)
I. .-24 3/17/66 2CECJ-610-
4, or -6
24A 4/5/66
ITo" 25 10/10/67 CJ-610-6
IIT'b" 24B 12/17/68 CJ-610-6
24B-A 4/24/69
I NA-265 3/23/62 2PGWJT12
A-6A
NA-26S-2C 8/31/62
-30 12/20/62
11 . -40 4/17/S3 JT12A-6A, or
8
in -60 4/28/67 JT12A-8
-
C-l) (12) (13)
Models Date Engine
Approved Type(s)
If'b" 25A 5/19/70 2 GE
.256 8/19/70 CJ-610-6
25C 8/19/70,
IH"b" 24C 6/30/70 CJ-610-6
24D 6/30/70
24D-A 7/31/70
IV 35 6/28/74 2 Ai Re-
search
36 6/28/74 TFE 731-
....,,,2-23
IVNA-26S-70 6/17/70 2 PCW
JT12A-8
V -80 11/30/73 2 CE
CF-700-2D
-2 "B"
(14)
Nature of
_ Chrises/Notes
Note: Special Conditions:
24 G 24A: FAA letters of
8/5/55 G 11/19/65
24B G other 24' s: FAA letters
of 3/1/67
25's FAA letters of 3/1/67,
35 G 36: FAA letters of
3/1/67, plus *25-50-CE-6
of 4/1S/73 and amendment
1 of 9/18/73
Rencngined; increased engine
pmver, weight.
Increased weights
Re-engined; increased weights
Notes: Special Conditions:
02S-11-WF, and FAR 36. 1(C)
and 36.2 anply to NA-26S
-70 and -SO
Exemptions: FAA »26, 270,
SS8, 709, 709A
(IS) (16) (17)
Xo. Approx. Tyy-ical
Issued Xo. of O.aages
Holders
26 16 Avionics, mods tc cahln
interior. Installa-no" of
camera tloorl
Note: SA2675"At
Anicncied 11,- 13;" 73- l^sta
of sou;:d suppressors.
Ui
I
-------
TABLE IB
mcde'.J o.' i-Se bi«lc aircraft cerMf'.cated l»forc 1 D«c. 1?*9. Crlglail Typo Certificates
Models approved be.'ore 1 Dec. 1969
:;i (2) (3) (4) (5) (6) (7) (8)
TC Hz'.ifr Qii-ic Model TC FAA Region Date of Date Latest Revision Models
Co-tro't-n" Application Approved (and Date of)
'.'5 A;T::-C r'.-.-c: - -^-erci-r
r^cir...: 707-100. -200. 4A:i N,',r:h*est 18 Sop 58 Rev. 8 (1 May 73) - 7C7. 100 long body
-IPOH Lor.-.: Fodv , -_
-lOOUShor! llo-fy ''" 7°'-«°
HI. 707-1POU long body
IV. 7'.-7.10CIi short body
Soci^c 707-300, --100. -300D, -300C. 4A26 Northwest ' .~15 Ju!.59 .-Rey.9 (1 May 73) ' 707-300
11. 707-^OD
111. 707-300D
IV. 707-300C
Boei.-s 720 4A28 Northvest - 30 Jun 60 Rev.8 (1 May 73) 1. 720
720D " 72° u
Coavai" C2 4A27 Wes'ern 1 May 60 Rev.8 (15 Apr 73) - 22
,,., II. 22M
(?)
approved
IB Scp W
5 Nov 59
1 Mar 61
24 J-.il 41
15 Jul 59
12 Feb 60
21 V.ay 62
30 Apr 63
30 Jun 60
3 M.r 61
! May 60
24 Jul 61
(10)
i Ti'A' JTIC-'j
-'T4A-3/5 or J74A-V/1C
JT3D-1. -_'.: C6. -3. IS, or LVC7
JT3O-1. -L-.IC-^. LV.C7
JT4A-9. -1. -11, -12
4 Rolls R-jyce Turbojet Conway Mart
50d !H. Co-I2|
JT3IJ-}, -3f, -:. -IMC. -IVCt, -:i£C
all uf I.'I «b'.i-e plus J73D-7
4 PtW .'T3C-7
JT5U-!, -:-.'.^CX,, -1-.VC-7
4CEC.'--"5-3 or-3A
4 CK C:t'Jl-3D
DC-8-U tSrouRh
2C-S-63T
)1 Aug 59 Rev 27 (20 Teh 72) I through XX In the T. C. latemt
model (XX
OC-3-657:
7 Jun Ifc
J F<.W JT4 or JT3 -type enriaeo,
::c-i.-4i.
; ''-.;' F'-jce Turbojet O/rway ^i
-------
TABLE IB
All models of the basic aircraft certificated before 1. Dec. 69 Origins! Type Certificates
Models approved before 1 Dec. 1969
i"! (2) (3) ( DC-9. -11, -12. -13. -14. A6WE Western' 28Feb63
-32F. -33F. -41
C-.-ier - 4-enjine
Convalr
Ce.-.en: r>yna~ics 30. 30A 4A30 Western
Convalr
Gc--.er.i! r>.T.a.-rucs 22, Z2N' . 4A27 Western
(6) (7) (8!
Date Latest Revision Models
. p o e (a e )
24 Dec 63 Rov. 11 (1 Jul 74) 1. 727. 727-KO,
727C, 727-100C
II. 727-200
23 Nov 65 Rev. 13 (15 Sep 74) ! DC-9-11. -12,
-DC-9-1-5
. II. DC-9-31
HI. DC-9-i5F
IV. DC-9-32
V. DC-9-32 F
VI. DC-9--11
VII. UC-9-33 r
Vlll. DC-9-21
Note: -TC with spot
exemptions:
15 Dec 61 . Rev. 4 (14 Nov 69) I. 30
30A
1 May 60 Rev. 8 (15 Apr 71) 1. 22
22 M
O)
Date
anproved
24 Dec (.3
1 3 Jan 66
29 N'ov 67
-13, 23 N'>v 65
19 Dec 66
1 Mar ',!
1 Mar 67
4 Oct 67
21 Feb 68
5 Apr 68
25 N'.v 68
415D and 424 (on i
15 O*c 4!
10 Oct 42
1 Msy 00
24 Jul ',1
(10) ' ' |
Er.jir-.e type's) ;
3 r-t,W JTSD-l. -1A, -7, -7A. -?,
or -9A
AH o.' above piai -11, -15. or -17
2 M-A- 3':-.li-'.. -1A, 5, 7. or -7A
same as ai-ove pj-js -9, -9A. -11, or|
Sarr.s as I
Sa.-,,. a.'ui
Sa--r.e as ^:
JT>.D-9. -11, or -!5
JT.O-1, 'iA or -11
Sa/r.e «s V.'U
uel ;e:'.is--.'.:r.j a-d e:T-.erger;cy exits;
4 CE
C:-.-.:.-2!. -23E
4 OE. C; £05-3, or -3A
C; *Oi-3B
1329-23A, -23D.>2JE
4 Sep 58
28Aug61 Rev. 8 (1 May 73) I. 1329-23A. -23D
II. 1329-2JE
28 yay 41 4 P4W. JI12A-4. er -6A
. C Jun 67 J712A-6
-------
CO
TABLE IB
IS/3 AU_ models of the basic aircraft certificated before 1 Dec. 1969 Original Type Certificate
Modeli approved before 1 Dec. 196?
(1!
TC Holder
Da sic Model
(3) (4) (5) (6) (7) (8)
TC FAJV Region Date of Date Latest Revision Model!
Controlling Application Approved (and Date of)
approve-i
r.rlne Mrpe(i)
Cti-cr . i e-^ine
Gr-.i"i:--.an-American Aviation G-M59
A12EA Last cm. 24 Jun 64 19 Oct 67 Rev. 7 (I May 7 Z\ j. C -1 1 59
Tncli. dnra now
Tiled with Southern
19 Oct '.7 Z I<<.]I> P.iyce
L-.«> Rb .'lU-Z
HFD 320 Hansa
A14EU EuropeaJi 6 Feb 63 7 Apr 67 Rev. 4 (19 Aug 71) j. uj-g 325
? Apr 67 2 CE
c.' tic-:
Fcsker-VFV N. V.
N>l!'. orlands
Fokker Fellowship
F. 28 Mark 1000
A20EU European 20 Oct 66 24 M«r 69 Hev. 2 (14 Apr 721 j. F28 v.srk 1000 24 M»r 69 2 P^llf Royce
Spey .VKi:j-:j
Gates Learjet. Lnc. (WlcKUa) Lear Jet 23 ' A5CE
(Note: Normal category, not
transport category)
Central
31 Jul 64 Rev. 7 (15 Jul 74) I. 23
31 Jul 64 2 CE
C.'-'. 13-1 or
Morine-Sav.'nler
Paris
V.. S. 760 (Note: utility category) 7A3 European
7oOA.
76011
!'.' Jul 55 3Jul 58
(Rev. 2 (22 Drc 65 1. 700
.'I. 7'.,OA
3 Jul 56 I ~ jrbcm«ca
22 Dec 65 .v.«rbor» L' C
Wart-.r. VI C
22 3-c 65 Var'.-.r- VI C
-------
If he also elects to meet any regulation in effect on the date of the
application, he must then also meet any other existing regulations
that the Administrator finda to be directly related (21. 101).
The amendment-to-TC process follows the general steps of the
i '
TC process, except that the documentation and flight testing is
usually not so exhaustive. When a number of proposed amendments
together form a new variant to the basic model of the type, a new
section is made in the TC, designated by a roman numeral.
Section I contains .the characteristics and specifications of the original,
basic model, while successive sections each cover a new model or
series of models. In the case where a series of models is covered
under one Roman .numeral section of the TC data sheet (e.g., Boeing
737-200 series), the dates of approval of each model in the 200 series
(e.g., models, -205, -214, etc. ) were once all given on
the TC data sheet. Now, the date of approval is listed on the TC
data sheet only for the first modql of the series that is approved. For
examples of the extent of changes between models, see Appendix B.
2.1.4 Supplemental Type Certificates (STC's)
Supplemental type certificates may be applied for by anyone. While
amendments to TC's, applications are processed by the FAA region
where the applicant resides. In practice, for transport category
aircraft, most are applied for by owners and operators of aircraft
and firms modifying interiors of such aircraft or installing equipment
such as avionics. Although STC's have been used to re-engine small
piston aircraft, they have rarely been used to re-engine transport
-19-
-------
aircraft, or make major changes to their airf rames . * The FAA
caseload of STC's has been estimated to be about 1300 per year.
The large number of STC actions is confirmed by an estimate of
360 cases pending in the Western region during a typical quarter
in 1974; the majority of these action's were STC's.
Under an arrangement spelled out in 21.431 to .493 and
Handbook p. 171, manufacturers, domestic repair station operators,
air carriers and others may issue STC's independently and report
the action to the FAA later (within 30 days). To do this, they must
!
qualify as a Designated Alteration Station (DAS). The DAS may also
issue and amend airworthiness certificates. This arrangement
enables the FAA, with limited personnel, to continue to handle the
STC caseload.
In order to get a clearer idea of the type of actions covered
by STC's the reader should examine the sample sheets from, the Type
Certification Projects Status Log. T These applications are currently
active, and the pages have been chosen because of interesting transport
category items. Those project numbers beginning with CT designate
complete type certification of a transport; those beginning with T,
partial certification (STC's and Amendments to TC's). The project
numbers ending with D, DO, DM, DS, or DT are ones where the Desig-
nated Engineering Representative (Handbook, pp. 151-164) at the DAS
is playing the major role in the approval process. The STC consists
of the FAA approval of the STC certificate and the related TC. STC
holders may obtain airworthiness certificates, and also production
certificates for changes in type design approved by the STC. STC's may
be amended in the same way as TC's.
* One past exception: STC SA1096 WE, amended 7/27/66, issued ^o
General Dynamics to re-engine the Convair 340 with Rolls Royce
Dart 542-4 turboprop engines.
Two pending applications for STC's;
(a) Change engines on Lear j?;t 24 & 25 from CJ610-6 to CJ610-8;
(b) Change engines on the Lockheed 1329 (Jetstar) from F&W JT12A
series to AiResearch TFE 731-3 engines.
:* Appendix A
-20- !
-------
2. 1. 5
Other kinds of Type Certificates
Provisional (PTC's) -- These certificates make it possible
for an aircraft in the certification process to obtain a "temporary"
i
type certificate in advance of the award of the actual TC, Amendment
to TC, or STC -- provided it has finished a substantial part of its
flight testing under an experimental certificate.
There are Class I and Class II Provisional Certificates.
Differences between them include:
Class I
Aircraft manufacturer or
engine manufacturer may
apply. ;
Applicant must apply for
a TC or STC for the air-
craft.
Class II
Aircraft manufacturer may
apply.
Applicant must apply for a
TC in the transport category
for the aircraft. !
At Least 50 hours flown on
the experimental certif-
icate
At least 100 hours flown.
There is also the "Provisional Amendment to a TC", quite
similar to the two PTC's mentioned above. None of these three
certificates of provisional character are transferable; The 'reader
is referred to 21. 71-85 for details.
-21-
-------
Restricted -- Restricted TC's are granted for special-
use aircraft for such operations as crop dusting, wildlife conservation,
i
aei'ial surveying, cLoud seeding, skywriting, etc. (21.25). This kind
of certificate is not germane to the transport category.
2.1.6 Airworthiness Certificates (AC's)
AC's permit the operation of individual aircraft. Any
registered owner of a U. S.-registered aircraft may apply to any;FAA
office. AC's are explained in detail in 21.171-. 225. Germane to
transport-category aircraft are the standard AC and the following
kinds of special AC's: "provisional" and "experimental."
Standard transport tategory AC. - - For new aircraft,
this is issued without further showing if the aircraft was manufac-
tured under a Production Certificate, except that the FAA Adminis-
trator may inspect the aircraft for conformity to type design. The
vast majority of transport category aircraft are manufactured under
such production certificates; hence, the issuance of AC's is almost .
automatic for transport and/or subsonic turbojet powered airplanes.
However, under 21.183(e), no standard airworthiness certificate
is originally issued (to a new aircraft) unless the FAA has found
that the Type Design meets FAR 36.
Import aircraft, including transport category aircraft,
are issued the AC if the country of manufacture certifies,
and the FAA finds, that the aircraft conforms to its type design and
is in condition for safe operation (21.183(c). However, import
aircraft equally fall under the nqise -requirement of 21. 183(e). They
-22-
-------
must meet FAR 36. l(d) or otherwise provide noise levels no greater
than those specified in FAR 36. l(d).
Experimental Certificate (EC's) -- In general, EC's are
a form of AC issued to aircraft for flight testing purposes,. Aircraft
i - ' '
with an EC may al:6o be u'sed for market^&efVeys, sales d«mons"t rations, and
customer crew training if they have undergone at least 50 hours of
flight testing, or at least 5 hours if the aircraft is a type-certificated
aircraft that has been modified. (21 . 193;21 . 195)
Provisional Airworthiness Certificate -- These are the
AC's issued to aircraft conforming to Provisional Type Certificates to
enable them to be operated. Thus, they conform to the types of
t
provisional type certificates:
Class I .Provisional AC
Class II Provisional
Provisional .AC for aircraft conforming to Provisional
Amendment to a TC.
2.2 How certificates are conveyed.
TC's and PTC's are conveyed in writing on FAA Form
8110-2 by the issuing FAA region (Handbook, p 13). They are signed
by or for the FAA Regional Chief, Engineering and Manufacturing
i
Branch. Concurrently, telegraphic notification is made to the FAA
Chief, Engineering and Manufacturing Division, FS-100, Washington.
The TC or PTC data sheet should be sent to Washington (FS-100)
within 48 hours after issuance of the T C or PTC. (Handbook, pp.
14-15. ) STC's, also conveyed on Form 8110-2, may be limited
to one aircraft serial number of a model. When necessary the FAA
-23-
-------
may originally convey the STC approval by telephone, transmitting
the final approval notice and STC number to the holder, and then
confirm it in writing. The actual STC form will then be processed
as soon as all -written internal documents have been received by the
FAA project engineer and will be back-dated to the same date as the
written communication that confirmed the STC.
2.3 Periods for which certificates are effective.
Type Certificates: TC's, STC's and Amendments to
TC's are effective until surrendered by the holder. Provisional type
certificates are effective as follows:
Class I PTC FO.J 24 months after the date of issue;
Class II PTC . For 12 ". " " '"! " "
Provisional Amendment For 6 " " " " " "
to a TC
Airworthiness Certificates:
Standard AC's, including transport category:
Indefinitely, as long as maintenance and alterations
are performed per FAR 43 and 91.
i
Experimental Certificates:
One year from the date of issue, or less as prescribed
by FAA Administrator.
Provisional AC's:
For the life of the corresponding PTC.
-24-
-------
3. SPECIFIC TYPES AND MODELS CERTIFICATED SINCE 1969
3. 1 Listing of Jet Aircraft Types /Models Complying with FAR 36
Noise Limits
;|'
All aircraft of the following types or models of types are
certificated as complying with FAR 36. They are on the list only if
FAR 36 is specifically listed in the ^certification basis" portion of the
latest revision of the TC data sheet, and only if it is clear that the limits
of Appendix C are meant rather than merely the "no acoustical change"
provision of 36. 1 (c)(2). Although the way FAR 36 is listed varies from
TC to TC, it may be presumed that FiAR 36 including amendment 1 is
meant in all cases, since that amendment dates from the same time
period as the original FAR 36.
Some aircraft TCed before 1 Dec 1969 are included--
for example, the Dassault Fan Jet Falcon, TC approved >9 Jun 1965.
Obviously the original version of the TC made no mention of FAR 36.
But evidently, in the course of later revisions, not only was the TC
amended to approve new series of models, but also the TC data sheet
was revised to declare compliance of all models to FAR 36.
New Type Certificate
TC/Date of Approval for model, or
if model series, first model of series
747-100 series*
L-1011-385-1
Boeing
Lockheed
McDonnel'-
Douglas DC-10-10 series
Dassault-Brequet Falcon-10
Cessna 500
Groupement
(airbusj d'Interet
Economique A300-B2-1A
Fokker F28 Mark 1000
Dassault Fan Jet Falcon
A20WE/30 Dec 69
A23WE/14Apr 69
A22WE/29 Jul 71
A33EU/20 Sep 73
A22CE/ 9 Sep 71
TC approved but data sheet
not yet issu ^d.
A20EU/
A7EU/9 Jun 65
*Except for those produced before 12/1/71 (approx. 127 aircraft).
-25-
-------
Amendment to TC
TC/Date of Approval for model, or
if model series, first model of series
Boeing
McDonnell-
Douglas
747 -200B series*
-200F
-SR
-200C
DC-10-30
" "-30F
" " -40
Dassault Fan Jet
Falcon series C
D
E
" F
A20WE/23 Dec 70
7 Mar 72
13 Apr 73
17 Apr 73
A22WE/21 Nov 72
30 Mar 73
20 Oct 72
A7EU/24 Feb 70
20 Jun 68
24 Feb 70
24 Feb 70
Gates Learjet 35
36
Rockwell Sabre-
liner 70
80
A10CE/28 Jun 74
28 Jun 74
A2WE/17 Jun 70
30 Nov 73
For the major airframe and/or engine changes between models, see Tables
IA and IB and Appendix B.
In addition, notation is made in two other TC's that some
aircraft of the type (i. e. , those first flown on or after 1 Dec 1973) will
comply with the noise limits in Appendix C of FAR 36. ** These are:
^Except for the 33 747-200B aircraft produced before 12/1/71.
**If flown according to the-operating specifications in the revised TC data
sheet and referenced flight manuals.
-26-
-------
TG
A3WE
A6WE
Type
Boeing 727,
all models
McDonnell-
Douglas DC9,
all models
Wording in TC data sheet
. . .all aircraft issued original
standard airworthiness certifi-
cates after I'Dec. 1973.
. . . all aircraft not flown before
1 Dec 1973.
A16WE Boeing 737 [* ]
Although there appears to be lack of uniformity in the
wording, it is clear that FAR 36 Amendment 2 is referred to. The only
i
other reference to noise compliance that was encountered in TC data
sheets was for the Lockheed 382-G Turboprop (T.C: A150). '-BniReVision
No. 8 of 1 Jun 1971, it was stated that the 382 model G only com-
plied with FAR 21. 93 (b) and" 36. 1 (c)(2), effective 1 Dec 69. in~that
noise levels had not been increased over those of the basic model" (the
"no acoustical change" provision). The IAI 1123 and the BH 125-600A
i
also comply with the acoustical change provisions of FAR 36. 1 (c) (2).
*The latest available revision of the TC data sheet for the 737 aircraft
does not contain the notation. Nevertheless, all Boeing 737 aircraft first
flown on or after 1 December 1973 must comply with the noise limits in
Appendix C, per FAR 36 Amendments.
-27-
-------
3. .1 Turboprop Aircraft in the Transport Category
From 1 July 1969 to 1 December 1974, only one of the
turboprop aircraft certificated referenced FAR 36 in the "certification
basis" section of the TC data sheet, except as noted for the Lockheed
382G in section 3. 1 above. The reference to FAR 36 for the 382G
was not one of compliance to the FAR 36 noise limits, but rather to
the "acoustic change" portion of FAR 36, section 36. 1 (c)(2). The
following turboprop aircraft models were certificated during this period:
o Complies with FAR 36 noise limits:
Hawker Siddeley HS 748 Series 2A
o No mention of FAR 36 in TC data sheet:
Lockheed 382F
Nihon YS-11A-500
Nihon YS-llAr600
Nihon YS-11 A.600
Ae rospacelines Boeing 377SGT
Aerospatiale Nord 262A Series
o Only complies with "no acoustical'change" provision of FAR 36:
Lockheed 382G
-28-
-------
4. SOURCES OF INFORMATION
The basic authority for certification Is Part 21 of the
Federal Aviation Regulations. FAA has also published a handbook,
Type Certification, for the guidance of FAA Washington and Field
personnel. The discussion above is drawn brLJefly from these two
sources. Sources of information oh certificates granted exist for
TC's, .amendments to TC's and ST^'s.
i
A ring binder of TC data sheets issued is kept in th'e \FAA
library and elsewhere, and is periodically updated in the same
fashion as the FAR's. Data sheets are arranged within it by the
region that issued them. Each data sheet runs from one or two to
several dozen pages and contains all the specifications of the aircraft.
As the data sheet is amended to include new models of the aircraft
(e.g. , the 200 series of the 727) the old copy of the data sheet is
removed and a new version including the latest revision (amendment)
is added. The specifications for each series are given separately in
separate sections each assigned a roman rvmneral. The specifications
include engine types that may be used. It is often permissible to
intermix several different similar engines (e.g. JT8D-9, -9A, -11,
and -15 engines on DC9-40 aircraft). Not every revision means a
new series. For example, for DC-9's, the latest model approved was
the DC9-21 in 1968, while the latest revision to the TC occurred
September 15, 1974.
The data sheets are accessed by an "index to data sheets"
in the same ring binder. This index is by TC holder (the manufacturer)
and lists only the TC's awarded to each manufacturer. It is issued
yearly, and is updated monthly by the use of supplem.en1i.ry 1-page
sheets.
-29-
-------
FAA Flight Standards Service keeps a ringbinder by
region of the status of all pending actions, including applications
for TC's, amendments .toTC's, andSTC's. This "Type Certification
Projects Status" log uses a standard reporting form (see sample,
next page) and is the device by which FAA regions report quarterly
to FAA headquarters in Washington. Not all regions report alike.
For example, on the sample sheet for the Western Region, the "%
complete" space is filled in, whereas some other regions do not use
this space. The same form is used to list actions completed during
the quarter. (See samples on following pages and also Appendix A).
-30-
\
-------
(Jj
*I
I
TYPE CERTIFICATION PROJECTS STATUS
PROJECT
NUMBER
A5348WE-S
A53*<9WE-S
-A5350WE-.DS
CT5352WE-D
T5353WE-D
MAKE AND MODEL
AND DATE
OF APPLICATION
Bellanca 1*1-13-2
6/25/73
St. rickfaden 1.10
PIPLR APACHE PA-23
6/3/73
Krueger 110
.-Ld-s combe -8A .;; -:-
V30/7.3
Krueger 110
.Douglas DC-9-51F
6/29/73
Irwin 120
(amends CT53I»2WE-D)
Locknee'4 L-1011
Rammel.sberg 1^0
DESCRIPTION
ROBIN HARRISON, San Dimas, Calif.
Install Lycoming 04-35-A engine, HarCzeli HC
12x20-8 propeller, Bellanca 1^-19 engine mount,
cowlings, and hardware on Bellanca 1^-13-2.
DENVER L. VAN HOUTEN, Norco, Ca.
Install 150 HP Lycoming engines and install 180 H
Lycoming engines.
, A:LRCEAF.T..MaD l,FJ=GATaLON=:E.Jsl.G,l.-N.E£-W!Nfi.-S.EIl!._:1-«takewood ,
Calif. Installation of fuel tank in each wing,
.replacing original tank in fuselage.
MCDONNELL DOUGLAS, Long Beach, Ca.
Certifiction of DC-9-51F tseries 50 aircraft)
(l) Increase series *»0 length by 76 inches.
(2) 130 passengers.:
(3) 120,000 Ibs. G.T.O.W.
CO JT8D-15 and -17 engines.
LOCKHEED-CALIFORNIA CO.^ Burbank^ Ca
Approval of a modified start fuel schedule on
Rolls Royce RB.211-22B engines as installed on
L-1011. Data obtained during tests Will be used
for adjusting fuel regulators on specific engines
as requi red.
KIS: FS 8HO-2
REGION
WESTERN REGION
PACE
32.
TYPE REPORT
CXJ QUARTERLY [^j SUPPLEMENTAL
PERIC
June 30, i97/*
u
X
u
*-
MEND
<
X
u
at
X
X
-X
TMER
O
X
O
t-
S~ t- i j
0<0
K S I
7o COMPLETE
ESTIMATED
DATE OF
COMPLETION
902;
9/7^
0%
9/7A
30°/
10/7^
105
1971*
50*
9/7^
DATE OF
APPROVAL
FAA form ( >-l3 (j.70, SUPERSEDES LOCAL FORMS
MS- 487
-------
1
w
1 *
TYPE CERTIFICATION PROJECTS STATUS
^
PROJECT
KUM8r.PI
T5i06V2lD
AH/J49V3-S
T5U55W2-D
CA5U62VE-D
T5U72VS-D
HI!
T^i^vP-S
T>$lt9',v"2-Di
3^6 TVE- s
T5570nl'E-D
T5576V2-D3
7S;?91'7l49:,v7J-3
A£750''"3-s
K AKE AND «OCE:-
ASO D* rE
0* APOLIC AT:ON
Douglas EC-10-10
Globe GC-1B
Convjiir 22H
Ted Smith 601P
Doubles DC-10
Lockheed L-188
-Douglas DC-10
Piper P/.-23
Lockheed L-1011-385
LiGcLhoeel L163A
'Hughes 269C
Douglas DC-9-32
Fair-child C-119C
Lockheea L-1011
Bee ins 707-3200
I*.'U£las I--0-9-32
Dou.:,lss DC-10-10
Lockheed L-1011
Dout ie-o DC-9-32
pougias DC-1C-30
Lockheed L-3Q2C
T.ockheed-Boeiiig-
.-Cus-ias:7l|7;BC-10;L-
Dou.c;la3 DC-1C-30
.-iSrO sGO«.^2wlvl2JL"';
roech
L't-.ec:-:.
i -. !. J ^ .J'.\ CCMr'-UjPSD'
A1^-
120 Sharp, ac
110 Davis
120 Patschke
120 Brandt
130 Maxwell
120 Davis
120 Sharman
120 'Brandt '
120 Vasley
120 Davis
120 Astorga
120 Ii-win
120 Willou^iby
120 Vasley .
120 Davis.
120 Irwin
120 Shaman
120 Vasley
120 Irwin
120 Sharmar.
130 Mulby
120 Wood
1011
120 Sharman
~ «: 4 w I-B
IJ fT .£ ni >-~t'
~~ SJ (9 P P
K 01 W Wl H-
£'S- o » en
(5 H- H en
3 c+ P
7 <*} H- to S
' H- 3 "J" QJ
° 6 PC c
J5- h -r- ^ ^ *
^" ^ t- "t» 0
r 'H o M
J? » H) O
T
'" ^ " -T
"^ OU*«Tt"LY ] S'jPP^ £ MS < T AL
PER1°° SEPT2M3SR 197U
K
B
2
"
O
^~
O
w
4
u
^
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kJ
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3,
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HI
>-
a < 2
^ 1- X 3
y> O ^ O
»J t- 1 I
2929V:
- -
-. .
ST.^
Number:
Field
Approval
SA2889WS
SA268!;'rfE
"^^'-J^Q..^ '
7^^p1',^
sni^vs^
_^
SA2915VB
SA2607VE
SA28L3VE
_
SA2$S3'rfS
^
1 ^ A ? Q T y^T"""
SA2893WE
SA660V/S
SA-290-T-r:
3A2908V,'E '
OATt or
APPROVAL
9/'7a
9/71;
lf
n
it
M
It
II j
'
,,
n
rt
11
n
tt
tt
n
it
ii
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ji
i»
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SS>0 8M-M7
-------
;r
^ &
TYPE CERTIFICATION PROJECTS STATUS
-
PROJECT
NUMBER
A5751WE-S
A5752WE-S
T5759WE-D
TS781WS-S
AS812WE
T5861WE-D
Tij570WE-S
TU692WE-DS
~E-l4977W2-S
E5018WE-5
T$C8lWE-D
H5123WE-D
H5300V/S-D
T535oWE-D
H56U5WE-S
A5672WE-S
T572SWE-&
HAKE AND MODEL
AND DATE
Of APPLICATION
Swearingen SA226T
Swearingen SA226T
Douglas DC-10-^0
Boeing 7U7-123
Vfcatherly 201B
Douglas DC-9-31
Lear 23, 21*, 2$
Boeing 727-100
Continental 0-U70
Continertal IO-360A
Douglas DC-8
Ku^nes 369
Hughes 3^9
Lockheed L-1011
Aerospatiale 315B
Bellanca 17-30'
Douglas DC-8/8F
Piper PA-12
. , m PROJECT 3 C OMPL2TED
ll^O Mason .
' lljO Mason
120 Shaman
120 Wood
120 Brandt
120 Villoughby
PROJECTS CANCELLED
120 Barnett - Req. of applicant
120 Wood - Req., of applicant
1'ljO "~"""'MGsiiul"ain - Inactive
lijO Acampora - Inactive
120 Keelaghan - Inactive
120 Astorga - Req. of applicant
120 Aetorga - Req. of applicant
120 Vasley - Inactive
120 Soderquist - fiaq. of applicant
110 Kruegsr - Not required - See
. Proj.A5802WE-S
130 Grieco - See Proj.#T5839WB-S
110 Strickfaden - See Proj.#A5907WE-S
. «.> t> :. .
to-o*.
«^3:...-j.
^
3-
T YPt P»t POPT
3cUAWTtB,Y ::^.^e«^
PERIOD
sa?raG2K 197;.
o
t-
9
I
O
*"
O
01
a
o
n
Id
Z
H
o
u
K
>< .8
H - * 3
3O < O
K a i
t -
T-.'.Iv
' ^e"
SA2909'«E
SA2910'*"2
_
SA2926WE
_
- -'
DATE Of
APPRCVA
9/71;
it
11
n
ti
1
?\4A
SUPERSEDES LOCAL FORMS
-------
TYPE CERTIFICATION PROJECTS STATUS
! PROJECT
NU MB ER
1
| CT2859WS-.D
! CTj369".v£-D
; CT3555'^2
j TM409WE-D
Tii/.,22V,;E-D
Tlu*91Vr3-L
TioU r/Z-D
> T^Sj'.-VZ-i)
! i'^OWE-D
| Tii666VE
5 AV/22V3-S
TU750VT5-DS
Ti;787v/E-DS
T-.567VS-D
] Ti.;873*'r2-D
| T^yObVS-DS
! H!49l;6W3-D
Ti;95^"f^-ES
{ T$C2Uv.'2-DS
j A5C29VE-S
! E50U3WE-S
! FSOiiitVE-S
A5050VE--DS-
T507SVE-D
T5092VE-S
Tpl 30'rfE-D
T;>'13Th'E-D
^ '' * "*
i ^ bl ^ '"Vn\l~^)
HAKE Ar:L UC DF.L
ASD C*T£
OF APPLICATION
No. At;crlc2^ 265
Dc-j^laa 20-10-30
Douglas LG-10-3CF
No. ijaerican 26^-70
Douglas DC-10-10
!-!o. Aoiflrican 265-70
Ko. ArjoricsLn 265-1^0
Dowlas LC-1C-10
Douglas LC-10-10
Do^-189 E-C-10
Dougls-j PC -6
Boeing 727-1H2
Eou^lac EC-"6B
I^ujlas I.J-^3
Tcu^-las DC-10-10
Douglas DC-8-62
^Tii;^*^ ^4 '?^O(^
*J '-^i^* i -» O '*. \J j \j
l:.o . iaericc^ 26$-i|.0
Fokior F--27
Etoch H-18
Sikorsky S-^5>
Air Borne Electron.
Swearing-cr. SA226T
Dox^las EC-10-10
~^f-ung 7u7-12
Ko . A.M 2 r i c -^n 26^-60
Douglas DC-10-30
Douglas 1X3-10-30
lushes 2 c;iC
PBOJ327S NErDIXG T.T.-.
(See - AWE-110 List)
AWE- 120 Fatschke
120 Sharaan
120 Shaxaan
120 Patechke .
120 Shancan
120 Fatschke
120 Fatschke
120 Sharaian
130 Treacy
120 Sharuan
#[46 Hart (SEA)
130 Treacy
#Lj6 Hart "(SEA) ." -
120 Kselaghan
lilO Vatt
130 Treacy
120 Astorga
130 Thompson
120 Barnett
130 Thompson
120 Haynes
lliO Heahulam
1>40 Killion
130 Treacy
130 . Wells
130 Bulmer
lliO Vatt
130 Kackal
120 Astorga _continued
T~T^;
1 ,
v-:-:; ]'^t
TYPE BE.PO«
-------
"p-r' - :^J
\ ~
TYPE CERTIFICATION PROJECTS STATUS
\
v
PROJECT
NUMBER
A2978W3-S
A3231WE-S
A373UWB-3
A3826WB-S
A3835W3-3
A3876WS-S
AJ4026WE-S
AI480WE-S
AI|222W3~S
Al*303WE-S
A1>313WE-S
AU371WE-S
A1&60W-S
AUU97WS-S
Al£l2WE-S
A1£7UW3-S
Al*$S6WE-S
Al»587WE-s
A5607WE-S
Al;609WE-S
Al|6U8WB-S
AU676W3-S
Al»712WE-S
Al|725'.73-S
Ai4765T^E-D3
MAKE AND MODEL
AND DATE
OF APPLICATION
Cessna 195A
Taylorcraft BL-65
Universal GC-13
Navion A
Bellanca lh-9
Taylorcraft BC-12D
Piper PA- 15
Champion 7GC
Gruncaan G-l6i^
Ryan -11*5
_MbT.ane-Sauliiier'"760
Spartan TV
Beech D95A
Universal GC-13
Co^aor.wealth-Reawin
Cessna 132H
Cessna 190
Piper PA-18-125
iv.-'^n (Navion)
Piper ^-20
Cessna ISO
FurJ: B75L
Taylorcraft BL65
Piper PA-12
Eeech 95 Series
- '
AW3-110
PROJECTS COi'IPLETE EXCEPT FOR T.I.R.
AWB-110 Erdaan
Strickfaden
Srdnan
VE-102(GRJ)
Krueger
Krueger
Davis
WE-102(GRJ)
Krueger
^WE-102(GRJ)
Strickfaden .
Strickfaden
WE-102fGRj)
Krueger
Strickfaden
Brdman
Strickfaden
Strickfaden
Krueger
WE-102(GRJ)
WB-102(GRJ)
Krueger
Davis
Davis
Krueger
- cwtinued
*IS: FS «;;.-. (1 '
REilON - r~t
WSSTES!: H3CDS |
T
TYP£ REPORT
l_XJ QUARTERLY ; ?J»PLE:MEHTAL
PERIOD , .,_r,^_^.. _
- i-i i i?iji.-i _ - i _
fi
>-
«
u
z
O
t-
Q
^
U
I
<
u
«1
a
kJ
i
^~
o
a
u
f-
< j w
3 < i - a i
-
% COUPLE ~E
AND
ESTIMATED
DATE CF
COMPLETION
:- "- - "'
OATE OF
APPROVAL
FAA Form 8110-13
!3-70)
SUPERSEDES LOCAL FORMS
-------
The FAA Office of Management Systems gets information
on registered aircraft from the Oklahoma City Aeronautical Center
Thse data form the basis for Census of U.S. Civil Aircraft, CY72
published in 1974 by that office. The office has data available in
unpublished form as of December 31, 1973 (microfiche of computer
printouts). Data for December 31, 19,74 will not be available until
mid-year 1975. The data are ordered in various ways; most useful
for purposes of this report was aircraft type by manufacturer by
model. Unfortunately, data was not available,on new registrations
only, from that office.
FAA Advisory Circular AC No. 36-1 provides noise
level data for turbine-powered aircraft. It was published in May 1973,
but a revised version is in preparation for issue by the FAA by the
end of February, 1975. One listing identifies aircraft certificated as
meeting the FAR 36 noise limits, and the other listing gives reported
levels of aircraft not yet noise certificated.
-36-
-------
5. LIST OF REFERENCES
1. Dept. of Transportation, Federal Aviation Administration.
Type Certification. No. ll-YZ". ~December~28, 1967.
2. Federal Aviation Regulations. Part 21 Excerpts: Preambles
21-7. 21-12, 21-21, 21-24, 21-15, 21-39, and all subparts
of Part 21 (A-N). (As updated through December 1974.)
3. Dept. of Transportation. Second Annual Report, Fiscal Year
1968. Excerpt: pp. 60-61."
4. Dept. of Transportation. Third Annual Report, Fiscal Year
1969. Excerpt: pp. 62-64.1
5. Dept. of Transportation. Fourth Annual Report. Fiscal Year
1970. Excerpt: pp. 124-126.
6. Dept. of Transportation. Fifth Annual Report, Fiscal Year
1971. Excerpt: pp. 165-166.
7. Dept. of Transportation, Federal Aviation Administration.
Unpublished data prepared for input into the DOT Sixth
Annual Report, Fiscal Year 1972.
8. Dept. of Transportation. Seventh Annual Report, Fiscal Year
1973. Excerpt: pp. 147-148.
9. Dept. of Transportation, Federal Aviation Administration.
Unpublished data prepared for input into the DOT Eighth
Annual Report, Fiscal Year 1974.
10. fljisL Census of U.S. Civil Aircraft. CY1972.
April 1974. j
11. Dept. of Transportation, Federal Aviation Administration,
AEQ-20. Advisory Circular 36-1 of 5/31/73: "Airp'ane N,oise
; Levels. " ' .'
-37-
-------
APPENDIX A
]
The sheets from the "Type Certification Projects Status"
Log were selected because they contained major projects concerning
transport category aircraft. It is believed that they represent most
oi~ such projects active in the various regiohTs"as of March 31, 1975.
-------
TYPE CERTIFICATION PROJECTS STATUS
PROJECT
NUMBER
CA1177CE
CT2762CE-0
A2952CE-S
A3351CE-S
A3384CE-S
T3475CE-D
'CA3T8TCE-DO
A3487CE-DO
MAKE AND VOOEL
AND DATE
OF APPLICATION
lerkle Mark II
12/15/65(212)
Deactivated
12/3/71
.ear 35/36
5/30/70(212)
>iper PA1S-150
2/15/70(214)
laval Aircraft
N3N-3
3/21/72(212)
Reopened 3/5//(
iavion
5/6/72(213)
:essna 500
(212)
JecCP.TD :261 ' -
l/l/7c (212)
ii'tch PC 234-
12-Vl
11, '22/72 (21 2}
DESCRIPTION
CENTRAL REGION PROJECTS
Ed Merkle, Wichita
New Model, 1500s* GW Biplane, 2 seat tandem, Lycoming
IO-360-BIB 180 HP
Gates l.earjet Corp_.
.^ew Mode"! "35/36 to A10CE
Central States Air-craft, inc.
Installation of Ly^or.iing U-J60-C2A engine and Sensem'ch .
Fred Niedner S Thomas Ahlcrs
Single step central float, one cut-rigger float under
each lower wing
r.rr-:. A. Evenson
ilTstli'l raTfo"n~bT Federal ITiT Model F-200 autopilot
Cessna Aircraft Co.
French Certification
Vcec ;i "Arrcr c! f~t- ?0'r_p_.
','ew i-ioJei - TV; in engine, pressurized
'eecli Aircraft Corp.
New Model siniiidr to AGO
R1S: rS 8110-3
RICION I PAGE
'CEN1RAL 1 3 '
TYPE REPORT
[3 QUARTERLY T j r,U P P U EM E S T A L
PERIOD
3rd Quarter - FY 7"
u
t-
»
u;
z
X
X
;l
X
AMEND TC
U
h-
ft
y.
Y
X
OTHER
X
ESTIMATED
TOTAL
MAN-
HOURS
1650
2550
300
175
150
500
500
% COMIV re
AND /
ESTIMATED
DATE OF
COMPL ETION
60;^
10/31/75
95%
6/30/75
70;::
'5/31/75
75?i
6/30/75
i o:;
5/1 5/7 5
Indefinite
]?,
9/30/76
5%
11/30/75
DATE OF
APPROVAL
TVoprove'd
6/28/74
FAA Form 8110-13 (j-?o)
LOCAL
a>o tit-tt:
-------
J
TYPE
PROJECT
NUMBER
T3982CE-D
A3983CE-DS
T3984CE-DS
"T3990CE-DS
A3993CE-D
A3996CE-DS
T3997CE-D
. J.3999.C&-D =
MAKE AND MODEL
AND DATE
OF APPLICATION
Lear 35/36
7/9/74 (;214)
Lear 23
7/16/74(212)
Lear 24/25
7/16/74(212,}
Sabreliner
NA265-80
7/25/74 (213)
Great Lakes
2T-1A-1
8/1/74 (212)
Beech A36
0/2.1/74 (213)
Revised 10/24//
Lear 23/24/25''
8/9/74(212)
tear' 35/36
8/1974 (212)
CERTIFICATION PROJECTS STATUS
DESCRIPTION
Gates Learjet Corp.
Installation of Grumman thrust reversers as
.optional equipment
Avcon Industries, Inc.
Removal of toilet seat for installation of navigation
sight
Avcon Industries, Inc.
Removal of Lo.i.Let--sea-t ,:f-or i-ns,ta-l-lation -o f -TO vrga t ion
sight
Aviation Services Div., .Rockwell Int'l
Installation of RNAV-VNAV system
Great Lakes Aircraft Co.
Amend TC to add optional Hartzell HC-C2YK-4F/FC 7666A-2
prop and Lyconn'ng 10-360-B1F6 180 HP engine
Collins Radio Group
Installation of AP-107 auto pilot, 2 Axis .
74
Gates Learjet Corp.
Cert, to operate to 50,000 ft. with all models
Gates Learjet Corp.
French TC (Export)
RIS: FS 0)10-3
REGION (PACE
CENTRAL 1 10
TYPE REPORT '
fjr) QUARTERLY fj^l SUPPLEMENTAL
PERIOD
3rd Quarter - FY 75
u
1-
s
Ul
2
I
AMEND TC
X
X
X
U
t-
U)
X
X
X
X
OTHER
J
ESTIMATED
TOTAL
MAN-
HOURS .
200
LT100
LT100
60
LT100
60
500
% COMPLETE
AND
ESTIMATED
DATE OF
COMPLETION
25%
6/30/75
95%
6/30/75
95%
10%
5/30/75
90%
6/30/75
80%
8/31/75
1%.
6/30/75
Indefinit
DATE OF
APPROVAL
FAA Form 8110-13 (3-701 SUPERSEDES LOCAL FOWMS «re §«»?
'- . . i
-------
1
TYPE CERTIFICATION PROJECTS STATUS
PROJECT
NUMBER
DS74-10CEW
DE75-27CE
DT75-32CE
T3648CE-D
A3889CE-S
A3906CE-S
Z3927CE
Z-VJ23CE-T
2454SrE-r
MAKE AND MODEL
AND DATE
OF APPLICA rio;<
(213)
(213A.218)
Cessna A188A
Lear 24/25
7/9/73(214)
Monocoupe 90A'.
3/25/74(214A)
Beech 18
3/7/74(212)
5/14/74
(213)
9/13/74 .
(213)
DESCRIPTION
-Terminated Projects
Recommendation to Wash, on a requested change on TS078
Crew Oxygen Masks (Requested by l-,;ash.)
Collins Radio Co.
Application for designated alteration station
Evaluation of A188B for export to Canada
Assisting MOT - Canada
Gates Lear jet Corp.
Installation of noise suppressor exhaust system -
conduct of FAR 36 test.
P'ijrlin G. Smith, Topoka, Kansas
Re-move Lycoming 235C1 engine end install A10 320E1A
engine complete with prop and accessories
Aeronautical Engineers, Inc., M-;o-!'.i, l-'Kvdi:;
Installation of spar strops (forwarded oy Southern RO)
Collins Radio
Design approval for Collins MS-CMA Area, Nayiqafign
Syste:n-A:-;S-/'OA ' "
Co'i 1 ii;s Rridio Group
ViT-;-351 uav. Receiver (TSO)
10/16/74 r.ol iiiv. iJ.idio Corn.
.'i'-; I:;D-JJ-J, lNJ-3ji i.<..'j liiO.-J'jIC deviation :; Jv: Ljrs
RIS: FS 811Q-3
REGION
CENTRAL
PAGE
23
TYPE RGPCnT
(v vl 1 1
l\Aj QUANTERtY 1 | SUPPLHUENTAL
PEHiOD
:i»..i f>.;,;r:or- !-Y 75
»-
u
z
u
(-
MEN D
<
X
«.
u
m
X
v
1
K
l-J
1.
1-
O
X
X
X-
X
X
X
75
u
1-
< -J V,
a < . a.
r t- 2 3
\n o < o
% COMPLETE
AND
ESTIMATED
DATE OF
W i- a u CGMPLLTION
1 1
DATE OF
APPROVAL
ompleted
3/17/75 ,
Completed
3/1/75
Completec
3/15/75
t
Co:r:p' eted
^ /*"'' 7 -
w' / -» / / J
Completed
3/1/75
CarctlUc
3/3/75 ,
Completed
1/2-/7S-
\
ii
Co;:::;1et.c-J
3/19/75!
I
jCor.i'lcteri
. .-' .' j '
= 1 - ;
FAA Form 8110-13 (3-721 SUPERSEDES LOCAL r
cro
-------
TYPE CERTIFICATION PROJECTS STATUS
PROJECT
NUMBER
ZL116SO
Z2049SO
(O'Brien)
Z2066SO
(Goodblood)
OTHER REGIONS
A3635EA-S
(Wilson)
C.H2592SW-D
(MIA EMDO)
CT2L9EU
(MIA EMDO)
T102RM-DS
(Bentley)
A2063SO-S
A2209SW-S
MAKE AND MODEL
AND DATE
OF APPLICATION
DAS
Batteries
for ELT
11/11/74
Aircraft
parts
T2731774
PROJECTS
Piper
PA- 28- 140
10/29/74
Bell 206L
1/21/75
Westwind
112''j
12/17/72
Boeing 737
2/14/75
DESCRIPTION
Pan American World Airways, Miami, Fla.
Surveillance of DAS.
B&K Electronics, Palm Harbor, Fla. PMA application
to manufacture replacement batteries for Larago ELT.
Airline Training, Inc., Ft. Lauderdale, Fla.
Request for PMA approval to produce parts in
connection wi't"H"STC "SA814SO.
Alpha Airways, Brooklyn, N.Y. Installation of
Sensenich Model M74DM-0-54 propeller and oil cooler.
(Ground inspections and flight test). (Airplane
located at Arden, N.C.)
Bell Helicopter Company, Ft. Worth, Texas. Request
for conformity inspection of prototype and/or test
parts manufactured by Patten/Pan Avion Div. ,
Miami, Fla.
Israel Aircraf.t Industries, Israel. Request for FAA
conformity inspection and 3130-3 tags.
Frontier Airlines, Inc., Denver, Colo. Installation
of tray carrier cart. Conformity inspection and
witness static tests, Aerospace Div. of UOP, Jacksonvil
Fla.
CANCELLED PROJECTS
CANCELLED 3/6/75
CANCELLED 3/6/75
RIS: FS 8110-3
REGION
SOUTHERN
PACE
13
TYPE REPORT
Q3 QUARTERLY {^1} SUPPLEMENTAL
PERIOD
Januarv 1 - March 31. 1975
u
1-
*
u
z
X
X
e
AMEND TC
U
t-
1/1
X
X
OTHER
X
X
X
ESTIMATED
TOTAL
MAN-
HOURS
120
80
56
12
135
80
% COMPLETE
AND
ESTIMATED
DATE OF
COMPLETION
Continui;
107,
757,
6/30/75
07.
6/30/75
707,
5/31/75
257.
6/30/75
07.
5/1/75
O»TE OF
APPROVAL
g
FA-A Form 8110-13 (3-701 SUPERSEDES LOCAL FORMS
CPO ess- 487
-------
TYPE CERTIFICATION PROJECTS STATUS
PROJECT
NUMBER
CT24EU
(MEG)
CE26EU
(REF)
'
CT45EU
(REF)
MAKE AND MO3EL
AND DATE
OF APPLICATION
BAC/Aerosp;
Concorde
Filton, Engl.
Toulouse, Fr .
15 July 1965
Roils-Rovce/
Snecma
Olympus 593
(SST Eng. )
Filton, Engl.
19 Jan. 1967
Vereinige
FUigtechniscl
Werke (VFW)
VFW-614
Bremen, Gen
25 July 1969
DESCRIPTION
tiale Supersonic Jet Transport.. Cruise Mach number
between M 1. 8 and M 2. 2. Aluminum alloy construc-
tion. Four R oils -R oyce /Snecma Olympus 593 engines
of 38, 050 Ib thrust, mounted beneath the wings,
R!S: FS 811C-3
REGION
E u rop e a r
PAGE
1
TYPE REPO-.T
_3 QUARTERLY !_ J SUPPLEMENTAL
PERIOD
"': ".;'.' r \
u
u:
z
X
tricycle type landing gear. Max. takeoff v. ' '' '\
385, 000 Ib. Max. landing weight 2-10, 0(K« '.' ;
Passenger capacity : 128. ,
Basic prototype! /development powerplant for BAG/
SNIAS Concorde Olympus Model 593.
Small. 44 passenger (max. density) shorthaul jet
e transport with two Bristol/Snecrna M. 45H turbofan
engines mounted over wing. Takeoff gross weight
44, 000 Ib.
i.
X
X
1.)
t-
o
ilj
u
1-
OTHER
'
1 t'i'.rr. :.:,.. :-c !i 3 1 , 1.975
ESTIMATED
TOTAL
MAN-
HOURS
10000
.
1000
600
AS1 2
ESTIMATED
DATE Oc
92l"c
Dec.
1975
90%
Dec.
1975
90%
.V ay
1975
OATE or
APPROVAL
.
.
1
A A Fo-
10-13 (3-70) SUPERSEDES LOCAL FORMS
G?O
i 467
-------
I
-0
TYPE CERTIFICATION PROJECTS STATUS
PROJECT
NUMBER
CE100EU
(REF)
CT115EU
(RJH)
CT133EU
(FJK)
CE143EU
(REF)
- »-*r»
MAKE AND MODEL
AND DATE
OF APPLICATION
R olls-Rovce
(B.E.D.)
M-45H
Filton, Engl.
9 Mar. 1970
Avions Marc
D.as.s.ault -B,.;J
Me r cure
St. Cloud, Fr.
25 Oct. 1968
BAG
BAG. 1-11 50
series
Filton,. Engl.
Ltr of 12
' -qust 1969
Turbomeca/
Snecma
"Larzac"
Paris, Fr.
27 Mar. '1970
-' ..'. '"'- *: "
DESCRIPTION
High by-pass "advanced technology turbofan for
VFW-614 short range jet transport1'. Development
of Snecma "Mars-45" two-spool engine, tentative
takeoff rating thrust of 7,200 Ib.
;1 Twin engine turbo-jet. Max. takeoff weight 119,049
^. .Ib. -Two -P&AV- JT-8D-4 5-engines mounted under wings,
low wing, tricycle landing gear. 134 passengers.
Twin turbo-jet transport. Max. gross weight 99, 650
) Ib. Two RR 512-14DW engines (similar to 400 series
with length increased 162 inches, span increased 60
inches, passenger capacity increased to 119).
Landing weight 87, 000 Ib.
Twin spool turbo-fan engine, 2300 Ib. static thrust,
Expected application is an alternate for AMD/BA
Falcon 10 and Aerospatiale SN-600.
.^,s, -
KIS: FS 8110-3
REGION
European
PAGE
2
TYPE REPORT
G*Q QUARTERLY QD SUPPLEMENTAL
PERIOD
January 1 thru March 31, 1975
z
X
X
X
AMEND TC
-
X
u
OTHF.R
ESTIMATED
TOTAL
MAN-
HOURS
100
800
200
100
% COMPLETE
AMD
ESTIMATED
DATE OF
COMPLETION
90%
May
1975
95%
July
1975 .
75%
Dormant
0%
Dormant
DATE OF
APPROVAL
t
-
FAA For.-M ?1 10-13 (3-70) SUPERSEDES LOCAL FORMS
G?0 SS8-497
-------
TYPE CERTIFICATION PROJECTS STATUS
PROJECT
NUMBER
CT147EU
(RJH)
CG152EU
(RJH)
^
CA154EU
(RAG)
CT156EU
(RAG)
MAKE AND MOOEL
AND DATE
OF APPLICATION
A v. M. Dassai
Breguct Av.
F.J.F. 30
Paris, Fr.
19 Oct. 1970
Caproni Viz.
"Calif"A.2iJ
Italy
18 Sept. 1970
Gen. A via Coi
Slruz ioni Aer
Pe gas o F. 20
Italy
-20 Nov. 1970
Fokker
.. ?8 Mk 2001
Schipliol Zuid
The Nctherl.
'1 Jan. 1971
DESCRIPTION
It- New transport airplane derived from. Fan Jet
Falcon Series F.. Increased fuselage diameter and
length. Passenger capacity increased to 39. Primary
mission changes from executive jet to scheduled
passenger carrier. Powered by two Lycoming ALF-
502 turbo-fan engines, (Clanged, from ZOT to FJF 30.
Ref. SGAC letter 11 April, 1°72. Published as FJF
40 since 1973 Daris A :-.sh< >w) .
Two place, all metal sailplane -powered by Serrnel
TRS 18 jet engine of 225 ib. thrust.
- Light, six place, retractable gear, low wing, normal
'>. category airplane, pow.-ri-d L>v two-wimr-mour.ted
Continental IO-520-F (2o5 i!P) ongir.es. .Viax. gross
Weight 4,420 Ib.
Stretched version of M-28 ,V1k 1000 at 65, 000 Ib.
max. gross weight
RIS: PS 611C-3
REGION
European
PAGE
3
TYPE REPORT
i_;3 QUARTERLY (_J SUPPLEMENTAL
PE'-'iOO
.' .' -.". :> 1 : !: !.: M.-; vc!". 31, '. "~i '
u
t-
!
A
\
X
AMEU O TC
V
(J
S
e
tu
»~
o
>
ESTIMA TtO
TOTAL
MAN-
HOURS
400
- _ _
200
200
100
% CO'.'P'.E'E
A'O
ESTIMATED
DATE OF
COVPL.ETION
10'-;-,
Sept.
1975
10%
Dorm?,nt
90%
May
1975
10% '
Oct.
1975
CATE OF
APPROVAL
t
FAA Form fllO-13 (3-?o) SUPERSEDES LOCAL FORMS
GPO 888- 487
-------
TYPE CERTIFICATION PROJECTS STATUS
PROJECT
NUMBER
CT157EU
(MEG)
CT160EU
4ME.G)
CT161EU
(FJK)
CH168EU
(MEG)
CE169EU
(REF)
MAKE AND MODEL
AND DATE
OF APPLICATION
Fokker
F-27
Schiphol Zuid
23 Feb. 1971
Fokker
F-27
23 Feb. 1971
Hamburger
Flugzeugbau
HFB-320
Hamburg, Ge
28 Nov. 1969
Const. Aero
Giovanni
_i;~usta A 109
Cascina Cost
18 Feb. 1971
Sermcl
TRS 18
....Toulouse, FT
16,-i\la.r: 1971
DESCRIPTION
Increase of takeoff power '(approx. 90 S. HP)
Dart 532-7R engine.
Increase of zero fuel, landing and takeoff weight for
Mk 500 aircraft; T. O. 43,050 to 44, 100 Ib.
LW. 41, COO to 42, 000 Ib. .."..., -
ZFW 38, 500 to 39, 500 To.
Installation of CJ610-9 engine in lieu of '"CT6TO ^5 , ^an'd
AiResearch APU in lieu of Sauer APU; also includes
pressure refueling. FAR 36 will be met by limiting
. -9 power to -5 levels.
Normal category, twin engine tu'rboshaft helicopter.
Four blades, main rotor, two bladed tail rotors.
. Max. weight 5, 070 Ib. Allison 2 50-C20 (400 HP)
a engine.
Jet engine of 225 Ib for C.aproni sailplane, on<:.
centrifugal compressor and one axial compressor
RIS: FS 8! 10-3
REGION
European
PACE
4,
TYPE REPORT
LXj QUARTERLY |__J SUPPLEMENTAL
PERIOD
J;i.'iu.-..r\- 1 Lh;-:: March 31, 1975
u
K
=t
u;
z
X
X
AMEN D TC
X
X
JX
u
1-
UJ
U3HXO
ESTIMATED
TOTAL
MAN-
HOURS
100
100
_.1.00
500
50
% COMPLETE
AND
ESTIMATED
DATE OF
COMPLETION
20%
Oct.
1975
20%
Oct.
1975
0%
Dormant
85%
June
1975
10%
Dormant
DAT?! OF
APPROVAL -
«
FAA Forn 8110-13 (3-7Ci ". G'JPCKSEDES LOCAL FORMS
nfO 688- 4«7
-------
TYPE CERTIFICATION PROJECTS STATUS
RIS: FS 8110-3
REGION
European
PAGE _
TYPE REPORT
|_>Jj QUARTERLY [_] SUPPLEMENTAL
PERIOD
. .-.::-:a:-y 1 th
PROJECT
NUMBER
CT174EU
(FJK)
"CT18'4EU
(RAG)
CA1
-------
TYPE CERTIFICATION PROJECTS STATUS
PROJECT
NUMBER
CA202EU
(MEG)
/*" ""PO r\ L. T7^ T T
~'\^L£f\JO.JLi"\J''
(FJK)
CT.207EU
(FJK)
CT213EU
-(FJK)
MAKE AND MODEL
AND DATE
OF APPLICATION
Gazuit-
Valladeau
GV. 1020
St. Laurent, F
8 May 1972
-,1A.M. J5.inald.0-,
Piaggio
RP-196
Genoa, Italy
17 July 1972
Hawker
Siddeley
HS-146
Hatfield, Eng
8 Aug. 1972
Britten-Norrr
BN-4
Mainlander
::-Isl;c -of '-Wight
9 Jan. 1973
DESCRIPTION
Light, single engine utility and acrobatic category
airplane, 1,750 Ib. max. weight, Lycoming engine,
McCauley propeller. .
-.
Light. S-T-O.L....T.rans.p-or.tTcate.go.ry .air.plane. High wing
T-tail, 30 passengers, 7, 500 Ib. payload airplane
powered by four Garrett-AiResearch TPE 331-1
(665 SHP) turbo-prop, engines with Hartzell three-
bladed propellers (106 in. dia. ) Max. weight
21, 500 Ib.
72, 000 Ib. , 100-passenger transport category R TOL
feederliner turbojet airplane, with high wing, T-tail
and dual-wheel main gear attached to fuselage and
stowed in belly. Four wing-mounted Lycoming AFL
502 engines of 6, 500 Ib static thrust.
an Transport category, 101 passenger- airplane. Max.
takeoff weight 62, 500 Ib. Powered by two \ving-
mounted plus a vertical fin mounted RR Dart RDa7
tu r bopr op r^engine s" with^'Dow ty-"R-otol~pr ope lie r .
High wing.
RIS: FS 8110-3
REGION
European
PACE
6
TYPE REPORT
Q3 QUARTERLY P^j SUPPLEMENTAL
PERIOD
Jnn.uarv 1 tliru March 31, 1975
0
i-
s
u
z
X
X
X
X
.AMEND TC
--
U
-
U3HJLO
ESTIMATED
TOTAL
MAN-
HOURS
80
750
500
500
% COMPLETE
AND
ESTIMATED
DATE OF
COMPLETION
0%
Dormant
10%
Dormant
-
20%
Dormant
0%
Dormant
DATE OF
APPROVAL
.
'
FAA Form 8110-13 (3-70 SUPERSEDES LOCAL FORMS
see-497
-------
TYPE CERTIFICATION PROJECTS STATUS
PROJECT
NUMBER
CE214EU
(REF)
CP217EU -i
(REF)
CA21&rEU
(MEG)
CT219EU '
(MEG)
MAKE AND MODEL
AND CATi-;
OF APPLICATION
Turbomeca
Bastan V1IC
Bordes, Fr.
22 Mar. 1973
-
-R-a-t-ie r-- F-OJJ&S.
FH 206-1
Figeac, Fr.
I.A.I.
Arava 101
"Tel-Aviv, Is.
4 Feb. 1973
I.A.I.
Model 1124
Tel-Aviv, Is.
j-J Jan. 1973
DESCRIPTION
Turboprop., 2-stage axial compressor, single
stage centrifugal compressor, annular combustor,
three stage turbine. For use on Aerospatiale N26.2C
Fregate.
;: NOTE : This engine is an improved version of
Bastan VI Cl, but adds one stage to axial compressor
Need policy decision whether new T. C. required.
,. ---E.o.u.r .biad.e.d.,~-ALaT_La.bLj._pil-cli_h^d-rajali£_x:.Qi:J:jiul .i".o.r
N 262C FregaVe. 10.5 ft. dia., tractor, feathering,
reversing, flight low pitch stops, 151,7 rp::i, 1046
SHP- at T. O. /M. C.
Installation of PT6A-34 engines as optional to PT6A-
27 engines in FAR 23/FAR 135 Appendix A.
Similar to Commodore Jet 1123 except AiResearch
TFE 731-2 turbo-fan engines irstr! led. Optional
thrust rev.ersers. IAI plans to subcontract certifica-
tion work and ''certify m:\v svstvnvs anr' in;: tal la: ions
to FAR 25". IAI Technical Spec. 1650/5422, 5 June
1972 provides details.
RIS: FS S'1IO~3
REGION
European
PAGE
7
TYPE REPORT
L'J QUARTERLY [_ ^ SUPPLEMENTAL
PERIOD
J;i"v,-i i-y 1 tli-.-M N!.-' :-.-'] 3 1 , .1'-?^
u
i-
\:'
*"
.
_x
u
t-
o
1 1
<
X
X
u
>-
i,';
5
j
UJ
K
< -1 0
S < , 1
i K z n
\,i O < 0
^ H 2 ^
100
. 5.0
50
-200
:;. COMPLETE
AND
-STIMATED
DATE OF
CCV^LETICN
0%
Dormant
-07o
Dor:nant
5%
Dormant
50%
Sept.
1975
OATE'OF
APPROVAL
'
t
-
I
!
I
FAA Form 8110-13 (3-70) SUPERSEDES LOCAL FORMS
ese-457
-------
I
I'
UJ
TYPE CERTIFICATION PROJECTS STATUS
PROJECT
NUMBER
CT220EU
(MEG)
CA223EU
(RAG)
CA224EU
'
(RJH)
CE225ETT
(REF)
;-"«; -<-.
MAKE AND MODEL
AND DATE
OF APPLICATION
Aerospatiale
Nord 262C
Fregate
Toulouse, Fr.
Ltr 31 Jan. 7'.
Stil-Industri
.JS.TIL.-.BA-11
Vargarda,
Sweden
31 Aug. 1973
Socata(SNIAS
Rallye 100S
Tarbes, Fr.
7 May 1973
Turbomeoa
.--jtazou
XV1L1A
Bordes, Fr.
10 Dec. 1973
DESCRIPTION
Same as Nord 262-A12 except with crease in take-
off weight to 25, 300 Ib and installation of Tur.bomeca
Bastan VIIC engines with Ratier Forest FH-206
4-bladed propellers.
Single engine, two-place, bi-wing, acrobatic cat.
airplane, powered by 200 HP LycornintL> engine and
Hartzell propeller. 'M'ax.-"-ta1ke'off-weT«:ht-l.i--3-4.0-l.b..
Single engine, two-place, low wing, utility category
monoplane of the basic MS BOO series approved under
TC 7A14. Powered by Continental or RR 0-200-A
engine and McCaulley prop. Max. weight 1656 Ib.
Turboshaft engine rated at 1032 SHP. To be used in
Aerospatiale helicopter SA 360.
RIS: FS 8 1 20-3
REGION
Europem
PAGE
8
TYPE REPORT
I 1 I 1
[Xj QUARTERLY | | SUPPLEMENTAL
PERIOD
Jrmunry I thru March 31, 1975
H
£
UJ
z
X
.,
X
u
*-
L)
UJ
4.
s
X
u
iTi
i
0
u
(-
< -1 in
s < . a
C t- 2 D
v, O < O
u I- 2 I
200
200
40
100
% COMPLETE
AND
ESTIMATED
DATE OF
COMPLETION
0%
Dormant
0%
Aug.
1975
60%
June
1975
10%
Dec.
1975
DATE Of
APPROVAL
t
FAA Form 8110-13 0-70! SUPERSEDES LOCAL FORMS
CPO »88r
-------
TYPE CERTIFICATION PROJECTS STATUS
"
PROJECT
NUMBER
CT227EU
(FJK)
CA228EU
(RAG)
s
CA230EU
(RAG)
MAKE ASD MODEL
ANS DATE
OF APPLICATION
Poligart-Cor;:
PD-01
Zugi Rosenbe
vveg, Switzerl.
27 Nov. 1973
.
Aeronautica
Mace hi S. p. A
AM 3C
Milan, Italy
22 Feb. 1972
Scottish Av.
HP- 137
Series 200
Prestwick
Airp. Scotland
19 Nov. 1973
DESCRIPTION
Twin turboprop (UACL PT6A-45) powered, high wing,
transport category airplane intended for either short
g field length, land or water based (floatplane) opera-
tion with cargo, passenger, or mixed cargo/passen-
ger payload. Both pressurized and r.on-prcssurized
version to be offered. Mt. ;. takeoff weight is 14, 300
Ib. Approx. max. passenger configuration for 20
persons.
Single engine, high wing, three-place normal aiid
utility category airplane witii max. takeoff weight
of 3, 858 Ib. Change to baf'C Model AM 3 airplane
approved under T. C. A19EU.
Same as Jetstream HP- 137 Mk I, except more power-
ful Astazoa XIV engines in lieu of Astazou XVI, and
changes to flight .controls neces site; Led by increase in
power.
R/S: FS 8110-3
REGION
European
PAGE
9
TYPE REPORT
r~v~i ' '
L/JJ QUARTERLY :__| SUPPLEMENTAL
P E f
-------
TYPE CERTIFICATION PROJECTS STATUS
PROJECT
NUMBER
CT231EU
(RJH)
CG235EU
(RJH)
j
CG237EU
(RJH)
HAKE AND MODEL
AND DATE
OF APPLICATION
A v. M. Das sav
Breguet Av.
F.J.F. 50
St. Cloud, FT,
14 Nov. 1973
^
Schempp-
Hirth
JANUS
Kirchheim,
Germany
1 Mar. 1974
Slingsby Sail-
planes
T. 61. B
Yorkshire, Er
22 April 74
DESCRIPTION
It Three-engine, long-range development of FJF
Series F transport airplane, incorporating 100 inch
increase in fuselage length, 1000-gal. increase in
fuel capacity via fuselage tank, and 3 AiResearch
TFE 731-3 eng. in lieu of 2 GE CF 700-2D-2.
Max. takeoff weight 36, 375 Ib. (Formerly FJF 20,
Model 3)
Two-seat cantilever sailplane in fiberglass. Two
piece wing, flaps, brakes, fixed main nose gear,
and all movable tailplane. Drag chute installed in
rudder.
Derivative of T. 61. A which is Slinks by version of
Scheibe SF. 25. B. (LBA TC No. 653). TheT.bl.B.
has Franklin 2A-120-A engine in lion of T. 61. A
g. Stamo MS. 1 500/ 1 . Two-place, side -by- side seating,
low wing, nose engine mounted seli-iaur,c)iing powere
glider. " ' "
- ... ' ' "' -
RIB: FS 8110-3
REGION
European
PAGE
10
TYPE REPORT
Qi) QUARTERLY Q] SUPPLEMENTAL
PERIOD
January 1 Iliru March 31, 1975
u
1-
5
UJ
z
X
X
1
u
H
Q
Z
UJ
^
<
X
u
i-
1/1
OTHER
ESTIMATED
TOTAL
MAN-
HOURS
300
40
40
-
% COMPLETE
AND
ESTIMATED
DATE OF
COMPLETION
10%
Dec.
1975 '
5%
June
1975
15%
June
1975
DATE OF
APPROVAL
'iA Forr. ''0-13 (3-70) SUPERSEDES LOCAL FORMS
GfO 888-4«?
-------
TYPE CERTIFICATION PROJECTS STATUS
*
PROJECT
NUMBER
CH240EU
(MEG)
CA241EU
(RJH)
s
CG242EU
(RJH)
CT244EU
. (FJK)
MAKE AND MODEL
AND OATF.
Or APPLICATION
Aerospatiale
SA-.360
"Dauphin"
Toulouse, FT.
26 June 1974
-
N. D. Nor mar.
Esq.
NDM1
''Firecracker'
Isle of Wight
17 June 1974
Moll no Oy
PIK-20
MclsLnki, Finl
24 June 1974
Hawker-
Siclccley
I.-I S -1.2.5 -700
Hali'ield, Eng
4 Sept. 1974
DESCRIPTION
Ten-place, single engine, transport category helicopte
of 2800 kg (6180 Ib) max. wt. featuring a 13-blade
"Fenestron" type tail rotor encased in the vertical
tail surface. The 1032-SHP Astazou XVIIIA engine
(for which FAA TC application has been filed) is
derated to 782 SUP for installation m the SA-360.
Single engine, lo\v wing, tandem .2-...-S e ;Vi , 2, 300 ib.
utility category; 2,000 ib acrobatic category; 1,700
Ib acrobatic category.
Standard class sailplane, 15 meter span, single
seater, FRP sandwich structure, max. gross weight
400 kg (8S2 Ib. )
The HS- 125-700 series is derived from the series
600. The Viper 601-22 engines arc replaced by
Garrett TFE 731-3 turbo-fan engines ana the overfin
is redesi'grred.
.
RIS: h'S 8110-3
REGION
European
PAGE
11
TYPE REPORT
i | ) i
[Xj QUARTERLY | ) SUPPLEMENTAL
PER CO
. .'.'HUH-;.- 1 li.v.i A!;.rch 31, 1975
i)
t-
e
U.'
z
x
^
c
c
H
(1
z
;
X
z
l-'l
i1
r-f
o
LkJ
i-
< _l U-:
2 < . t
r >- r D
« 0 < 0
U t- 1- X
200
40
40
200
7U COMPL^ft
AMD
ESTIMATED
DATE OF
COMPLETION
10%
Mar.
1976
15%
- June
1976
80%
June
1975
5 70
July
1976
i i i
!JATE OF
APPROVAL
t
,
|
For '0-1.3 (3-70) SUPEF-.3HDES LOCAL FORMS
GPO eee-467
-------
TYPE CERTIFICATION PROJECTS STATUS
PROJECT
NUMBER
CT245EU
(FJK)
CL246EU
(RJH)
*
CE247EU
(REF)
CE248EU
(REF)
-,t
MAKE AND MODEL
AND DATE
OF APPLICATION
Cons truce ioiu
Aeronauticas
C.ASA 212C
Madrid, Spain
7 Sept. 1974
Thunder
B"alloon-S' :Ltc-.
AX5, AX6,
AX7, AX8,
AX9
.London, Engl
17 Jan. 1974
Rolls-Royce
(1971) Ltd.
RB211-524 .
Derby, Engl.
Jan. 1974
R olls-Royce
(1971.) Ltd.
..R..B21 1-22F
Derby, Engl.
Jan. 1974
DESCRIPTION
:s The' CASA VLodel 212 is a high wing, twin turbo-prop
airplane, fixed tricycle landing gear, max. gross
weight 13,230 Ib, powered by 2 Garrett TPE 331-201
turbo-prop engines and Har.tzell HC-B3TN-5D props.
18 place plus 2 crew.
Hot air balloons of bulbous 12 and 20 gore type
_iu.fciiiz.ing-_poly amide nylon with polyur ethane sealer.
The cubic volume varies from 42,009 cu. ft. to
140,000 cu. ft. and utilizes single or double liquid
propane fueled air heaters. The occupancy varies
. from 2 to 8 men.
Uprated version of RB211-22B 48, 000 Ib. thrust.
To be. used on long range- L.- 101 1 and larger version
of B747.
Uprated version of RB21 1-22B to 42,500 Ib. thrust
at ISA + 13. 9°C. Will give L-1011 longer range.
HIS: FS 8110-3
REGION
European
PAGE
12
TYPE: RCF-ORT
[_31 QUARTERLY [_]] SUPPLEMENTAL
PERIOD
L1
1-
$
til
X
\
o
i-
o
UJ
;;
<
X
X
o
i-
u>
OTHER
ESTIMATED
TOTAL
MAN-
HOURS
150
20
100
100
% COMPLETE
AND
ESTIMATED
DATE OF
COMPLETION
25%
Sept.
1975
80%
June
1-975
10%
Oct.
1975
0%
April
1976
OATE Oc
APPROVAL
t
FAA Form 8110-13 (3-701 SUPERSEDES LOCAL FORMS
888-467
-------
I
I'
oo'
TYPE CERTIFICATION PROJECTS STATUS
PROJECT
NUMBER
CE249EU
(REF)
CT250EU
(RAG)
CT251EU
(RAG)
CH252EU
(MEG)
/
MAKE AND MODEL
ANO OATE
OF APPLICATION
Rolls -Royce
Motors
Continental
IO-360A, C,
D, G & H
Crewe, EngL
29 Aug. 1974
Fukkcr-VFW
F-28, Mk
6000
Amsterdam
Ther Netherl
May 23, 1973
Fokker-VFW
F-28, MK
5000
May 23, 1973
Aerospatiale
3 A -.3.6 5
Marignane, F
Nov. 20, 1974
DESCRIPTION
.Manufacture under license agreement with Teiedyne
Continental Motors, USA. Engine currently FAA
certified. Continental is TC holder.
Same as "stretched" MK 2000, except with increase
in zero-fuel weight to 56, 000 Ib. plus full-span
wing leading edge slats, 5-foot increase in wing
span, increase in thrust rating, and engine silencing
provisions.
'
Same as basic Mk 1000, except with full-span wing
leading-edge slats, 5-foot increase in wing span,
increase in thrust rating, and engine silencing
provisions.
Same as single -engine SA-360 "Dauphin" T-Cnt.
-h.e.licopter , except with two Turb'jmrca "Arvii.'l"
. engines; same as SA-366 except lor engine -mudc-l.
RIS: FS 8110-3
REGION
European
PAGE
13
TYPE RCPORT
L^J QUARTERLY [__i SUPPLEMENTAL
PERIOD
.i';.';:i:-i:-\ 1 th:-.: V;;ir.-h 31, 1 °75
V 1
J
u:
X
*
u
f-
a
7
X
X
u
1-
Ul
OTHER
E-3TI'.'.ATED
TOTAL
MAN-
HOU PS
50
100
100
50
7o COMPLETE
ESTIMATED
DATE OF
COVPLETION
20%
July
1975
25%
April
1975
25%
April
. 1975
5%
June
... 1976
DATE OF
APPROVAL
FAA Form 8110-13 (3-701 SUPERSEDES LOCAL FORMS
CPO esi- 497
-------
[ - ' ' " :
TYPE CERTIFICATION PROJECTS STATUS
PROJECT
NUMBER
CT13liNW-S
A153NW-S
T165NW-D
CT167NV-D
....
MAKE AND MODEL
ANO OATE
OF APPLICATION
Boeing 707
5/21/73
Cook 212
Beech 65
6/30 '73
Dickson 219
Boeing 7^7
7/18/73
Nelson 212
Boeing 7U7SP
7/27/73
Connally 212
DESCRIPTION
BOEING COMMERCIAL AIRPLANE CO., SEATTLE, VA
Modernization of 707-300B/C series -airplanes to the
707-500B/C.. New model will be 200" longer (120" fwd.
of wing, 80" aft.) with quiet nacelle engines super-
jet interior, .installation of two Type II exits. Boeing
will ;as.ke this model cv:iilab]e as a ri-.'v; production
airplane cr will modify existing 3007/0 to 50CI3/C
config. There is no change in the wing structure.
p!.\sela,vo is the saiic except for inserts.
HAROLD CLARK, OLYMPIA, V/A .
Installation of individual landing gear position lights
(3) to -show when each landing gear leg is in the "safe-
for-landing" position, per Clark CTL3-1 installation
instructions.
BOEING COMMERCIAL AIRPLANE CO., CEATILE, V/A
Additional passengers on upper deck. Installation of
now exit similar to existing crew service door, to be
located on lefthand side opposite CSI).
BOEING- COMMERCIAL AIRPLANE CO., SEATTLE, V/A .
Similar to 71+7-100 except: Fua'l;8' shorter, Fin 5'
taller, new T.E. flap & system double hinged ru-'luer,
other changes as described in Boeing letter EA-6660
dated July 27, 1973-
K!S: rS 3110-3
REGION
PAG!: :
TYPE KEPORT
L j QUARTERLY [_J SUPPLEMENTAL
PERiOD
(J
t-
~f
u
z
u
H
o
2
<
X
u
Ul
X
X
IT
P
O
X
UJ
1-
< -1 10
2 < , I
~ >- 2 D
if, O < O
U (- Z I
9U66
I|0
188
1590
% COMPLETE
AMD
ESTIMATED
DATE OF
COMPLETION
5%
6/75
1056
70%
20% f
C A 7 E OF
APPROVAL
FAA Form SllO-13 (3-701 SUPCI\S!;DES LOCAL FORMS
CPC e'3
-------
*
TYPE CERTIFICATION PROJECTS STATUS
PROJECT
NUMBER
A219NW-S
A22CKW-S
A221NW-S
A222NW-S
A235NV-S
T236NW-D
MAKE AS'f MODEL
AMD "ATE
OF APPLICATIC"
Republic RC-3
10/26/73
Dicks on 219
Republic RC-3
10/26/73
Dicksori 219
Reoublic RC-3
10/26/73
Tickson 219
Republic RC-3
10/26/73
Dickson 219
Aero -Conns
11/13/73
Dickson 219
Boeing
707-300B/300C
11/7/73
Koi-eland 211;
DESCRIPTION
AERO CRAFT, INC., 33LLEVUE, WA
Installation of wide spray rails in the place of existir
rails. Multiple.
AERO CRAFT, INC., BELLEVU3, WA
Installation of a larger wind:;"-.ield (see photo). One-
AKRO CRAFT, INC . , ' lEHLSVUEy -WA
Installation of a Lyconin.^ GQ-i|30-]3ID engine" and -a
Kartell HC-83X20CL propeller in a Republic RC-3 air- .
crr-.ft. Multiple.
AERO CRAFT, INC., BELLEVUE, WA
Revised instrument parrel. in accordance with Aero Craft.
drawing. Mounted 13-5" forward. Multiple
GERALD E. GOETZ, OLYHPIA, WA
Installation of wijid collector de-vice::;, to outboard tire
wall to accomplish ":;:;!:. -\:n" .
LOSING COI-IHZfiCIAl AIRPL.I'-rE CO., SEATTLE , VA
Quiet nacelle installation' 'on 2oeii!,;i-: Mod'.'l 707-300B/
-300C equipped with Pratl: .-. V/?:itn-;.' JT3D-1 , -?. oj;d -7
ermines. Purpose of '!-.odif ication 1:-; to demonstrate com-
ulia:ice v;ith FAR ?.''>.,. A';: rnclix 0 :-yi.L:--- .li.mit.
r:
o
/.
ESTIMA TED
TOTAL
MAN-
HOURS
0-20
0-20
' 50
0-20
3C
-
'V,. COMPLETE
ESTIMATED
DATE OF
COMPLETION
60%
60%
605^
60%
3Q5S
107$
7/1/75
DATE OF '
APPROVAL
!
i
FAA Form 8110-13 (3-?o SUPERSEDES LOCAL FORMS
-------
1 - . .
TYPE CERTIFICATION PROJECTS STATUS
PROJECT
NUMBER
T237HW-D
T238NW-3
A255NW-S
T262NW-D
A282NW-S
MAKE AND MODEL
AND CATE
OF APPLICATION
Boeing
707-100B
11/7/73
I-Ioreland 211+
Boeing 720B
11/7/73
'Morelarid"<211;--
Stinson
SR-10J3
11/1/73
Dickson 219
Boeing
7U7-136
12/21/73
T-) r-T-il^rtOVl 91^
EDO Floats
2200, 2870,
2960
,.2/1.9/71+
T.rTJryjVj 9T'9
DESCRIPTION
BOEING -COMMERCIAL AIRPLANE CO., SEATTLE, WA
Qaiet nacelle installation on .Boeing Model 707-1003
equipped with Pratt &" Whitney.' JT3D-1 and -3 engines.
Purpose of modification is to demonstrate compliance
with FAR 36? Appendix C, noise limit.
BOEING COMMERCIAL AIRPLAIiE CO., SEATTLE, WA
Quiet nacelle installation on Boeing Model 7203 equippec
v.rrth"pra~tt '?-. Whitney -JT^D-l-'anc. --3" .--engines-.. -Purpose of
modification is to demonstrate compliance with FAR 36,
Aroendix C, noise ' limit.
LES R. KARES, KENT, WA
Installation of a Pratt & Whitney R935 engine, engine .
mount and a Hamilton Standard 2D30 propeller.
BOEING COMMERCIAL AIRPLANE CO., SEATTLE, WA
Follow-on airplanes with RCA weather r;:vdar in lieu of
E..K. Cc. r?.dar and Hamilton Standard flight recorder ir
lieu of the Plessey System previously installed.
ARTHUR D. INGALLS,.KIRKLAND, WA
Installation of hatch cover to provide storage within
float compartment. .
-
RIS: FS 8120-3
REGION
PAGE
TYPE. REPORT
! ) QUARTERLY i_J SUPPLEMENTAL
PERIOD
U
=:
u
2
u
t-
o
ui
0
V
y,
x
OTHER
X
:c
-*-
ESTIMATED
TOTAL
MAN-
HOI.IhS
930
650
1*0
100
60
-rc COMPLETE
AND
ESTIMATED
CATE OF
COMPLETION
7/1/75
«
20?^
80%
9056
DATE OF
APPROVAL
'
i
i
FAA Form 8110-13 C3-7O SUPERSEDES LOCAL FORMS
ere tee-487
-------
TYPE CERTIFICATION PROJECTS STATUS
RIS: FS 8110-3
REGION
NORTHWEST
PACE
TYf-£ REPORT
- QUARTERLY
SUPPLEMENTAL
PERIOD
PROJECT
NUM5ER
MAKE AND MODEL
AKT :ATE
or APPLICATION'
DESCRIPTION
H K- ^ U
i/l O < G
L) h- Z Z
"/.. COMPLETE
DATE OF
COMPLETION
OATE CF
APPROVAL
'A309NW-S
Travelair
2000
3/7/7U
Dick-sen 219
GREGG C. CALDWELL, VANCOUVER, WA
Installation of Lyc'oming R-680E3 engine, Hamilton
Standard 2B20 propeller, and governor.
X
70
Pi^er PA-26R
3/21/7U
Di.-Jk.30fi 219
SEATTLE I-L'CriTFAC TURING COR.PORATIOI:, 3ELLT".;rUE, WA
Installation cf a 3-P^1--^ -'-;i racir' in t;-/.; -bajgago
A320I-W-S
Meyers ll;5
3/25/71
Dick.-son 219
CARL lv. SCn//AR2, KENT, WA
.Installation of a Continental 10-3^0-C engine and a
KcCauley I'2A-3l)G~6T?7'6C-2 propel±er. 'Also ,-= -a--vreight
increase from 1910" to 2l50r.
!X
A3221W-S
Lusconbe 8E
3/1L/7U
Dickson 219
V7AYNE F. REAVIS, I-EDFORD, OR
Installation of Hartzell HC-32X G-2.3 vith ?636D-U "blade:
v:ith Lycorr.ir.- 0-320 engine as per STC SA173.
30
727-2003
3/29/7U
Mack 212
30E1IIG CC;C-'IEi?CIAL AIRPLAIT3 CO., SEATTLE, WA
Perivabive of Model 727-200 v/ith tr.o follov/in,^ changes:
- Increased max ta:ci c^css v/eight of 21.0,500 Ibs. (Ma:<:
brake release 209,500;^ ldgv;t., l6l,000//; zero fuel
l!.;7io'/'Vmo= 350 KEAS)' .
- Body fuel t;?jri!-:s previously approved on 727-2JU
- V/irj.3 tip extension of 3 feet
- Extended L. E.
- Variable camber L. E. flaps
- Win;; strengthening
5610
7/77
FAA Form 8110-13 (3-70) SUPERSEDES LOCAL FORMS
CfO S8S-
-------
I
.N)
'UO
-
TYPE CERTIFICATION PROJECTS STATUS
PROJECT
NUMBER
CT32ljEW-D
T3232U-S
A33MW-S
A335ir.'~s
A3U7NW-S.
.^1,9,,^
' ' j- '" - "
MAKE AND MODEL
ANO DATE
OF APPLICATION
Boeing
727-3COA
3/29/7U
Mack 212
_3ceing
737-200
UA/7U
Dickson 219
Cessna ll;0
li/l5/7U
Uln 219
Luscombe 11A
1/29/714
171 s 219
Piter J3C-65
5/2/7U
Pickron 219
.'-L-ar~J.-t;-23,
2V 25".. ,'.;,'
^7jrv;;-rc
DESCRIPTION
i .
BOEING COMMERCIAL AIRPLA1IE CO., SEATTLE, VA
Derivative of Model 727-200 with changes incorporated
on 727-200B (wing, etc.) and the following additional
changes:
- Four wheel truck-type main landing ,;7-ar
- Body length increase cf 120 inche;; forward of wir^;
and 60 inches ."ft of win/:
^ wait -;c. --tf-f.ro::" v^
Installation of modified lower interior sidewall in
accordance with Dwg, l.'o. AH-010 to increase service
life and maintain appearance of the interior of the
aircraft.
ARCKIE N. AIIDERSON, SEATTLE, V/A
Installation of an exhaupt augmented cooling system for
a C85 engine.
FR/J-Hv R. BIORN, GLAD3TOITE, OR
Remove Continental' 185-2 v/ith metal propeller. Install
rooMild 105-3 with Hartzell IIC12 X 20-7 T
GERALD J. V.^ILSR, POST ATIG2LES , - WA '
Installation of Continental "0-200-A engine (les;.-: ^tartei'
a:vl ,s3!:c-;r'ator.) , usin,^: tho ori'.-v.lr.^l 'ir/.-JMt , OOW:;I.IT, c-c.
,,,^^1S^CK ^^ ^A^,,[A ,c;'. . ' ; .
Mpclii'i'catidn of all Lear Jet airru ?n.<- s ,by inctullation-..
of hi-lil't devices; " :' , '- - ..'"'.-. V- '-' ' '
Kit/ f'S 3! 10-3
REGION
HGRTr/'.TlST
PAGE
8
TYPE REPORT
I ' r i
1 1 QUARTERLY ! 1 SUPPLEMENTAL
PERIOD
H
*
U
2
D
1-
'.;
UJ
I
7
U
Jl
7
j-
.'
y
%
£
X
0
X
J"'l
7.
/.
Q
UJ
< -1 in
s < , a
Z t- Z D
In O < O
U 1- 2 =
2780
0-20
1;0
i;0
l£>
635
% COMPLETE
AfiO
. ESTIMATED
DATE OF
COMPLETION
5%
7/78
90°/o
10°/o
. 1095
20/D
^ -, .
OAT E OF
APPROVAL
.
FAA Form 8110-13 (3-701 SUPERSEDES LOCAL FORMS
CPO
-------
TYPE CERTIFICATION PROJECTS STATUS
PROJECT
NUMBER
E359NV.r-S
T363IIW-S
*
.369..M,
A375NV-S
T380UW-D
T383:a-s
MAKE A!i D MODEL
AND CAT:-:
Oc APPLICATION
Bell 206B
Dicks on 219
Bee in# 707
»-, ___ ___ I*"1, T "^
Boeing 7l;7? .
5/17/7U
Connally 212,
Bceirg
7U7-2COB.
6/10/7U
Bolseriga 2lh
Stinson
Vultee L-$E
6/10/7U
Dickson 219
Boeing 707
~Sl.il ei- 213
Douglas DC -7
7/9/7U
OESCHIPTION
DICKl'IAN LUMBER COMPAilY, TACOMA, WA'
Addition of Plywood Snowshoes to allow landing in. soft
snow.
SiSSo^:^o^:;^S-p^S:3' WA
Firat-of-a-Model with side cargo door and revised cargo
handling system. Installation of urroer deck aide door.
BOEING COMMERCIAL AIRPLANS CO., SEATTLE , V.'A
Installation of Pratt and VJhitney JT9D-70 engines on,
the Boeing Model 7U7-200B airplane.
DUST DEIT:L SPARING
Remove Sensonich propeller. -Install McCauley 1B200/HMX
8837 for towing gliders.'
BOEING COMMERCIAL AIRPLAME CO., SEATTLE, WA
Installation of cockpit floor grill.o cover for all cargc
conf i.gurations "'(i'l-oighttr £-. convertible).
^ '.....^^^ ro?TO..nr P,T,.:UT^. r,'->
In3taliation of auxiliary pov.'or unit.
KIB: FS 8HC-3
REGION
PACE
O
TX PE REPCST
! i QUARTERLY ' ] SUPPLEMENTAL
PERIOD
'f
UJ
U
H-
v
-
u
H
i/l
y.
:
j
'A
OTHER
X
X
'
X
« -j
5 ^ i v
r. f- z ^i
in O < O
U 1- S X
50
60
'"208
2670
30
77
5-0
Af, D
E : T '.' A T E 0
CATJ OF
CO^PL ETIOS
. 2CT/0
7*
fi«
1/36/76
2SS
80/3
ftiss
GATE O?
APPROVAL
FAA Form 8110-13 (;;:) S'jPLRiL'Oils LOCAL FORMS
Of-O 848-4*7
-------
>
1
Ln
TYPE CERTIFICATION PROJECTS STATUS
PROJECT
NUMBER
Al4i7KW-S
TU50NV-S '
"T158W-D - '
T1+60NW-D
HU62NW-S
':r- ;::.- '- :-j
MAKE AND MODEL
AND DATE
OF APPLICATION
Universal
GC-1B
10/15/71*
Lickpon 219
Douglas EC -6
10/22/7!;
Slif.ir ?.13
toeing TUT"" ' ."
10/29/7U
Bolsenga 2lU
Boeing
737-2S1
10/29/7U
Slifer 213
Boeing
Helicopter
107-ll"
.c.^ -^
':,'. :"!:; "- "';':-; >- . '
DESCRIPTION
MAC HEN, INC., SPOKANE, WA
Installation of a Franklin 6A-350.-C1 engine and a
KcCauley D2A3l|C67/3i;5?-10 propeller.
PACT7IC ALASKA AIRLINES, FAIRBAJXS , AL
Modification Divert; the tail boater air to heat the
c :. 'c-'-'/j Gc:2ri:.'.r.-t:;>;i!t d'.ri'i::,.; non-iciib-: conaitions.
-30EI-NG. C9H?-D!iaCIAL-AI-RSLAI-!3..C.O..., SEATTLE, V/A
Installation .of Pratt & Whitney JT9D-7P engines on all
models of the 7U7 airpl'ane. Initial application will
bo en the Model 7V7-200E and involve s propulsion, system
airivorthinecs and airplane .noise certification. JT9D-
7F ratings tal-:eoff v/et 50,009 pounds, takeoff dry 1^8, OOC
iDOiinds, laaxL'flum continuous L0,200 rounds.
BO"ING COI-E'ERCIAL AIRPLAY CO., SEATTLE, WA
Two Model 737-2E1 Follov:-on advancf'd pac. longer A/C.
.Identical to previously, 'c.ertificat'.-;] aircraft except
the float switch was raised .to .25 inches which
increasts tho fuel ca.Dj.city by 13 .rallonn.
COLUT'BIA HELICOPTERS, INC . , POHTLAirD, OR'
installation of Kc-v/^s^ci produced rotor blad-^a P/iT
..1Q7H1202 on 3.V. 107-II. . - V/ill re-qiiiro review of .Eoeing
Cin.i 'Kaw&3o!-:i drawing to deteriiihe aocC'ptaMlity. Con:-^
.plianuc v.-ith ".jp 7^-17-32-:rcvmii;;ed.:--.Er.c,jec-t rnr.y.be
c anc elled '.- if :, K&waar&i pa.T.e' ' a-j . Boeing.; \
fi/5; A\> SI 10-2
REGION
KP^'WEST
PACE
IP
TYPE REPORT
1 1 1 ] ' 1
( QUARTERLY : ; SUPPLEMENTAL . .
PERIOD ;"
I
K-
~f
IL-
z
o
H
o
u:
<
'
(J
f_
>:
4.
y.
THCR
O
X
-X
X
Q
UJ
r-
< -1 o-.
S < . i
~ 1- Z D
w 0 < O
U H 2 I
60
li^
,,-.260 ,
33
79
'."; COMPLETE
*r:D
ESTIMATED
DATE OF
COMPLETION
20%
icy>
6&/*
80$
5c
-------
I
t^J
o^
t
TYPE CERTIFICATION PROJECTS STATUS
PROJECT
NUMSER
TU87HW-D
Ti>91NV-D
Pfc^-S
TU931W-,
AI.9WM
CT!;97:M-D_
MAKE AKD MODEL
AN U DATtl
OF APPLICATION
Boeing
727-2LU
12/U/7U
Slifer. 213
Boeing
Haioiltcn
Standard 3DUO
12/1U/7U
VG re land 2lU
Boeing
727-200
12/17/7U
M:-ck 21?
Universal
GC-1B
I2/30/7U
L~3ra:3h 219
"727-3'C'OB
Mack 212
DESCRIPTION
BOEING COMMERCIAL AIRPLANE CO., SEATTLE,- WA
One. Model 727-2Ll| American' Capital Aviation (CM)
similar to 727-233 Air Canada airplar,ec previov.^ly
certificated except for landing- vr:-i^.t v.'hich is same as
Sterling's 727-2JU and variou/j cu^to^oi- change-::.
BOEIMG CC:-:-ERCIAL AIP-PLANE CO., S:':.M7LS, WA
Model 7a7-Elil' Co:unand Pout Phase II.
EFFICIENCY AIRCRj'JjT COMPOI^NTS, I.\"C . , T.ZITT,, V/A
Replacement of HSP Part No. 50286 and Part No. 01+98 witi
Little Giant Seal Assembly Part No. EAC UO-lOb.
BOEING COMMERCIAL MRPLANE CO., SEATTLE, WA
Pro.:rraa Lefinition -.Structural Cortification Model
727-200.
HAG MSN, INC.', IRJGH EVA1;S, SPOKAI^IE, V/A
Installation of Continental 10-3^0 ermine, HcCauley
D2A 3^;C 67/76-C2 propeller and associated char.£es to
BOEING COM-ZuOIAL ATRPTjAJ:!; CO., ^-.::^2i:-.. V/A.
Derivative cf '72'7-3'CO "(Uef . Tro-joc^t -C'lO^Lir/.'-D-V-'wi-th -£-oi-
'lov;ir.s. differences: LO" incro^.:o -in ^o::jth, 220" to^al
frc.-u 727-200 fwd; J'jSD-SU^ C:'^;.;::.,L; :-:': Lh ' uixer. .New 'S'
«/S: /'5 8110-3
REGION
PAGE
TYPE RLPORT
i | QUAF^TERLY r^j SUPPLEMENTAL
P C TV 1 O D
O
f
-
'J
\-
C
z
;v
h-
y.
V
H
o
X
X
X
CC. T IMA TED
TOTAL
MAH-
HOS'US
56
136
38
Uoo
17-80
v'o COMPLETE
ESTIMATED
DATE OF
COMPLETION
»
10^
205^
5/75
80^
7/1/75
12/77
'-*-; E o E-
APPROVAL
'
FAA Form 3110-13 (3-70) SJPERSEOES LOCAL FOKMS
90 B65- 467
-------
>
I
ro
^j
*
TYPE CERTIFICATION PROJECTS STATUS
-
PROJECT
NUMBER
T5714NW-D '
A575IIW-S
T5761W-D
CT577NW-D
T578NW-D
T579NW-D
i ,
MAKE AND MODEL
AND D'A 1 E
OF APPLICATION
Boeing
707-3L6C
3/19/75
KPerr.^pl 213
T,CM :-.P.ca
1L-13-1
3/3/75
Dickon 219
Boeing
737-200/200C
3/21/75 '
Hart 212
Boeing 7U7SP.
3/12/75
llelson, 212
iceing
7i47-238B
3/2U/75
RasrausGen 21'
Boeing
'720-025
3/?f.i/75 .;
-: >l-r. } '^\
DESCRIPTION
BOEING COMMERCIAL AIRPLANE CO., SEATTLE, V/A
One Model 707-3L6C (2li) Aviation Service & Support Corp.
(ASSCORP). Identical to 707-3L6B, except for customer
reouosts. (First-of-.vi-Hodcl airnlone)
RUSSIA 11. HILLS, FEI^rLlL WAY, V/A
Tnctailaticn of-?. Fran'-.l.iii 6A-j>'0-Cl engine, MsC today
propeller and landing gear door _cov_ar.. -
BOEING COra-ERCIAL AIRPLANE CO., SEATTLE, WA
Program Definition for increase in operating weights.
(MTGVJ= 130,000 lb.). Model 737-200/200C. Reference:
Boeing letter B-7670-HA-6156 dated M?xrch 21, 1975-
BOEING COMMERCIAL AIRPLAITS CO., SEATTLE, WA
Installation waste carts and waste containers manufac-
'turcd -by Mansfield Aircraft Procucts Company. Fire
containnent tests to be conducted at vendor plant.
Mansfield, Ohio.
BOEING COMMERCIAL AIRPLANE CO., SEATTLE, V/A
One Model 7V7-2383 Qantas Airways, S/N 2105U.
.J30EIKG--CCrc*ERClAL AIRPLAi."^ CO., SEATTLE, V/A
Altitude reporting- capability retrofit installation for
Model 720-025 Korean Airlines.
K1S: fS lliC-3
REC CN
= *GE
TYPE REFG3T
C i : 1
J QUARTERLY , ] SUPPLEMENTAL
P u r< 1 0 D
Z
X
o
t-
M t: N LI
4
x
X
X
U"
x
tr
iij
O
",r
y
X
!
o
UJ
t-
z < , c:
^ i- z n
-, o < o
w *- a -
128
60
1235
60
1045
US
"'-. COMPLETE
AND
ESTIMATED
DATE OF
COMPLETION
1055 '
6/30/76
1056
10°/D
6/30/76
DATE OF
APPROVAL
1
1
FA.\ Form 8110-13 (3-7O SUPERSEDES LOCAL FORMS
GPO
-------
I
t\)
00
PROJECT
NUMBER
(JS38WE
DS^SWE
DS50WE
D053WE
TYPE CERTIFICATION PROJECTS STATUS
MAKE AND MODEL
AND DATE
OF APPLICATION
FS-) Request
RSD DC-9 8/72 -
Noise Reduction
Acampora 1^0
Al 1 App 1 i cants for
(Audible/noise) T.C.
11/27/72
Acampora 1^0
VARIOUS Jet
(Spec. Study) Trans-
port 6/IV73
Mason 1^0
SPECIAL
:"'l/73
Ma ck 180
DESCRIPTION
DOUGLAS AIRCRAFT, Long Beach, Calif.
RtD project on DC-9 airplane consisting of a
3-phase effort which includes the design,
fabrication, ground testing, fit. testing, 6
economic analysis of a minimum cost noise
reduction nacelle configuration for the JT8R
engines installed on the DC-9.
All applicants (all aircraft) for T.C. - Sources
of audible noise. Before issuing any original
T. C. - for --.any aircraft of <-
M
OTHER 1
X
X
X
X
iSTlMATeOj
TOTAL
WAN-
MOUW5 |
% COMPLETE
AMD
' ESTIMATED
t DATE OF
COMPLETION
60%
Not Known
65^
1/75
1975
DATE OF
APPROVAL
/
FAA
8110-13 (3-70) SUPCNSCDKSLOCAL FORMS
WO 819
-------
TYPE CERTIFICATION PROJECTS STATUS
RIS: AS 8110-~3
REGION
WESTERN REGION
8.
TYPE REPORT
[_^] QUARTERLY
J SUPPLEMENTAL
CER.OO Oct. I - Dec. 31, T97*
Second Quarter - FY-1975
PROJECT
NUMBER
MAKE AND MODEL
AND DATE
OF APPLICATION
DESCRIPTION
I- Z 3
O < O
t- 3 I
V, COMPLETE
AND
ESTIMATED
DATE Of
COMPLETION
DATE OF
APPROVAL
DS83WE
Douglas DC-8-61
R&D Phase I I Noise
5/1/74
Griffith 140
R&D ON DC-8-61 AIRPLANE. Phase II "Aircraft Noise
1975
Definition". Object to improve statistical accun
of noise data and to broaden the c'ota base to
include measurc">ent s at long distance & at a thrui
required for a stceo approach.
DR84WE
~):9 74
Review Program
5/3/74
Frei 104
:FOR ..1974-1.9,7,5 AIRWORTHINESS PROGRAM. To cover
alf TDY in Washington, D. C. by "AWE-TOO pers'onnel
to assist Wash. Staff (AFS-77) in support of this
program. Also includes TOY relative to partici-
pation in the scheduled (Dec. 2-11, 1974)
conference.
12/75
DS85WE
DR87WE
DS88WE
Research & Design
(Alrspeed Celtbra-
tion) 5/6/74
Blackaller 160
RESEARCH & DESIGN - AIRSPEED CALIBRATION
iO/75
The purpose of this project is to research,
design, buy materials and construct one or more
"trailing cone static sources" for AWF.-160 to
use for airspeed calibrations.
Request by AFS-140
Rotor Fai1ures
(Inves t igat ion)
7/9/74 DuFour 140
AFS-I4Q Request - Develop criteria for approval
of aircraft engine installation design for rotor
containment and/or acceptable design criteria
for minimizing the effects of rot^r failures on
aircraft structures, systems, or orcessoriej . etc
1975
Technical Support
to: NASA/DO.T/FAA
7/19/7*
Griffi th 140
TECHNICAL SUPPORT (ACOUSTICS) TO
l\..i>k Force COI'K.:;:C'. ; .-'.1 A/C no i .-
evaluation. (AEO.-2. Was n ing ton,
FAA Form 8110-13
«r.i Dr ri LOCAI
-------
OJ
O
TYPE CERTIFICATION PROJECTS STATUS
PROJECT
NUMBER
T^550WE-D
Al»576WE-S
- A^59-2-WE-DS
AA610WE-S
M665WL-S
A^67^WE-S
AJ»688WE-S
MAKE AND MODEL
AND DATE
OF APPLICATION
DOUGLAS DC-9
H/18/71
DuFour 1'tO
PIPER PA-22-135
1 0/2:.i/7 i
Davis 110
BELANCA \k-\3
12/6/71
Strickfaden 1 10
CESSNA f207
12/15/71 AWE- 110
BELL ^7G-3B-1 , -2
2/12/72
Davis 110
CESSNA 180
1/17/72
Davis 1 10
REPUBLIC RC-3
1/1V72
Stri eki'ode" 110
DESCRIPTION
DOUGLAS AIRCRAFT, Long Beach, Calif.
Retrofitting all DC-9 model aircraft with P&W
JT8D engines modified to reduce the sound level
to thot of the DC- 10 airplane. '
WILLIAM L. SOP.NfcERGr.rtj San Diego, Calif.
Installation of PA-2G conventional landing gear,
toe brakes, ^0 amp alternator, & remove control
system bungee.
ROLAND *M."-"tJOS'E-LTN, 'Ma li bu ,"'Ca li'f .
Installation of Continental IO-470F engine.
SCENIC AIRLINES^ INC., Las Ve^a^, Nevada
Modification to doors.
A & H WELDING CO., Sun Valley, C;i.
Installation of a heat exchanger is engine tail-
pipe to augment cabin heat system.
RICHARDS S. VOROBIK, M Toro, Calif.
1 ns t:i 1 1 rit ion of Continental 0-V/O-R enqinc: and
McCuulcy l_'A3690M-8 prone 1 1 >-. r .
K RANC ! S J . MC CAR'! HY . Redwood C i ty , Calif.
1 PS t -i i 1 3 1 i on of Ci.n I. i :ien ta I IO-£'79-D cngiru' ijnd
i !...! ./(.! 1 :!-',;.-.! \-..:i..
i
R1S: FS 8UO-3
REGION
WESTERN REGION
PACE
16.
TYPE REPORT
LA] OUART^nLY |_3) SUPPLEMENTAL
Ipj.-'iioo cct. 1 - Dec. 31, 1971*
Second Quarter - FY-1975
o
t-
B
bi
z
u
^-
o
z
hi
a
<
-
u
t-
it
X
X
X
x
X
X
OTHER
X
ESTIMATES
TOTAL
MAN-
HOURS
% COMPLETE
AND
ESTIM* TEO
UAT f. OF
COMPLETION
850^
1/75
15-;
6/75
15%
1975
1975
5or:
6/75
5%
6/75
20%
6/75
DATE OP
APPROVAL
FAA Form 8110-13 U-7UI SUPERSEDES LOCAL FORMS
GPO eae-
-------
I
OO
TYPE CERTIFICATION PROJECTS STATUS
PROJECT
NUMBER
CU975WE-D
A5001WE-S
,T5QOliWE-DS --
A5012WE-S
MAKE AND MODEL
AND DATE
OF APPLICATION
LOCKHEED L-1011-
385-2
2/22/72
Vasley 120
BEECHCRAFT 36 .
9/22/72 Wells 130
-GATE'S LEAR-JET
9/8/72
Presba 120
Cessna C-337
' 0/2/72
Kul ewi cz 1 ^0
-
DESCRIPTION
LOCKHEED-CALIFORNIA CO., Burbank, Ca.
Extended range derivative of the L- 10 1 1 -385- 1 ;
3 high-bypass ratio turbofan RB. 211-2^ engines;
takeoff weight = ^73,500/y; l,:i~;!inc weight -
358,000.?; zero fuel we i evil = 333,000*.
FRAf.'D DiSTEFANO, TUT, tin, Cj.
Strobe light installation.
LEAR AVIAj.Reno, Nevada Modify Learjet 2k & 25
by: 1. Revised wing: section 6 plan-form; -
2. Mod. & relocate nacelle. 3. Different engine
dash No. (CJ610-6 to CJ610-8). k. Mod. fuel sys.
- delete tip tanks. 5. Mod. fit. control sys.
spoilers, - was ailerons. Mod. stabilizer sweep,
mod. rudder sys. 6. Mod. high lift devices.
add I.E. devices, & inbd. OBD flaps. 7. Mod.
fuel vent. 8. Relocate inlet in vert. stab.
CHARLES JANISSE, Granada Hills, Calif.
Modification of rear engine exhaust stack
i ns tal 1 at ion.
.
K/S: FS 8110-3
WESTERN REGION
TVP£ REPORT
PACE
20.
[XJ QUARTERLY TJ SUPPLEMENTAL
PERIOD Oct. 1 - Dec. 31 , 197^
Second Qua-ter - FY-I97S
u
^-
9
U
Z
X
u
t-
MENO
<
u
M
X
X
X
THER
O
M
fH
U
h-
j< . S
:: h z D
30 < o
t- X I
% COMPLETE
ESTIMATES
DATE OF
COMPLETION
0%
1975
1975
1975
90%
DATE OF
APPROVAL
FAA FoirtI 8110-13 (3-70) SU'JL ffotUt. S LOCAL ('..KMj CfO 0«»- 4«7
-------
>
I
t\J
TYPE CERTIFICATION PROJECTS STATUS
PROJECT
NUMBER
T5336WE-D .
CT5342WE-D
CT53^3WE-D
CH53MWE-D
MAKE AND MODEL
AND DATE
OF APPLICATION
Rockwell NA-265-80
Tarver 130
Doucjlas DC-9
Series 50
6/29/73
Wood 120
(amended by CT5352WE
Douglas OC-10
Sharman 120
ROBINSON R-22
6/29/73
Soderquist 120
DESCRIPTION
ROCKWELL INTERNATIONAL, El Se^undo, Ca.
Installation of battery overtemperature warning
system.
MCDONNELL DOUGLAS, Long Beach, Ca.
Certification of DC-? Series 50 aircraft.
( 1 ) ;| n.cr.eai>e..:.ser i es kO -length by 76 inches
(2) 130 Passengers
(3) 120.000 Ibs. G.T.O.W.
(M JT80-I5 and - 17 engines.
DOUGLAS AIRCRAFT COMPANY, Long Beach, Ca.
Approval of supplemental fuel tank .to extend
range of DC-10 series 30 and 40 aircraft. Tank
is located in aft lower fuselage cargo compart-
ment.
ROBINSON HELICOPTER COMPANY, Palos Verdes' Penr,. ,
Calif. Certification of 2-place piston powered
he 1 i copter.
(1) rotor diameter -302" (2 blades)
(2) 1 150 Ib. gross weight
(3) Continental 0-200, 100 HP engine
CO 95 MPH cruise
'
RJS: FS 8I1Q-J
WEGIOW 1 PAGC
WESTERN RSGIDN I 33
_ ..... \ ->"
TYPE REPORT
| [>G QUARTERLY Q^j SUPPLEMENTAL
UER.OO Oct. - Dec. 3" , 1974
Second Quarter - FY-1975
u
t-
»
hi
Z
X
o
H
MEHD
<
X
o
K
M
THER
O
X
X
H
kj
a^.S
r t- Z 3
u, O < O
^ It- 2 f
% COMPLETE
AND
ESTIMATED
DATE Of
COMPLETION
30*
1975
20?
6/75
10%
1975
5*
6/76
DATE OF
APPROVAL
FAA Form 811C-13 o-
701
SUPERSEDES LOCAL FORMS
cro ess-
-------
I
to
TYPE CERTIFICATION PROJECTS STATUS
PROJECT
NUMBER
CL53/*6WE
A"5350WE-'DS '-
CTS^WE-b
Ab'J!)8Wt-:
^5365WE-S
MAKE AND MODEL
AND DATE
OF APPLICATION
Bal loon Exce 1 s ior
AX-3
6/29/73
Brand! 120
L;us-eombe .:8A
V30/73
Krueger 1 10
Douglas DC-9-51F
6/29/73
Wood 120
(amends CT53^2WE-D)
Piper PA-24-250
,/ '' '73 Meshulam 1 *»0
Boeing 727-257
7/18/73
Turner 1 30
DESCRIPTION
BALLOON EXCELSIOR, Untion City, Ca.
Type Certification of 3 one-mari hot-air balloon
with airborne neater. Envelope is of muit-
panflleJ nylon reinforced with nylon tubular load
tapes. Hooter is propane, stainless ste-..!.
Basket is stainles^ s tee 1 ' c?'.'- le reinforced rattan
;: th reinforced plywood flooring.
AIRCRAFT. MOD I.FI CAT ION..ENGJNEE RING SER. , Lakewood,
Calif. Installation of fuel tank in each w.ing,
replacing original tank in fuselage.
MCDONNELL DOUGLAS, Long Beach, Ca.
Certifiction of DC-9-51F (series 50 aircraft)
(l) Increase series 'lO length by 76 inches.
(2) 130 passengers.
(3) 120,000 Ibs. G.T.O.W.
CO JT8D-15 and:-- 17 engines.
KEITH A. FOWLED, Irvine^ Ca. Installation
of tip tanks and associated plumbing.
PACIFIC SUUTHWES'i A! R!_ 1 NES^ Gar: .Dieqo, C,-<.
Appr-cw.il of u.irci'iift interior '.:* .ir* <;-' to.
conf -rrr- to PSA Mcol con f i yuro '.. \ on .
1
RIS: FS 8110-3
REGION
WESTERN REGION
PACE
3^.
TYPE REPORT
[J< J QUARTERLf | ( SUPPLEMENTAL
PERIOD Oct. 1 - Dec. 31., 197^
Second Quarter - FY-1975
o
>-
*
Ul
z
x
'
o
t-
7
u
>
<
X
u
H
v*
X
X
x
I
L,'
X
t-
0
J
o
u
h-
3ii.»
C t- Z D
\n O < O
Ul t- X I
% COMPLETE
AND
ESTIMATED
DATE OF
COMPLETION
5£
!?/76
$6*
7/75
101
12/75
50%
5/75
1975
DATE OF
APPROVAL
P3
FAA Form 8110-13 n-701
LOCAL
-------
>
I
u>
ȣ>
TY°E CERTIFICATION PROJECTS STATUS
PROJECT
NUMBER
T5423WE-DS
H5^35WE-S
T5^36WE-D
A5H1WE-DS
-A5W6WE-S -
UASE AND MODEL
AMD DATE
OF APPL1'- »TION
BAC 1-11
9/V73
Pittman 120
Sikorsky S-61N
.9/7/7.3
Thompson 130
Douglas DC-9-30
9/73
Buell 160
Bellanca 17-30A*
9/12/73
Jenkins 130
Cessna 172K & M
8/13/73
Davis 110
LebS'na 172
8/13/73
Ddvis MO
DESCRIPTION
NATIONAL AIRCRAFT LEASING^ Encino, Ca.
Modified landing gear wing ,ind power plant.
Increased ramp wt. to 92,000 Ibs., & GTOW to
91,500 Ibs. Reduced T.O. field lengths.
KAISER AEROSPACE 5 ELECTRON! 1 CS^ Palo Alto_, Ca.
Add. of Kaiser Helicopter Flight Dirt?ctor system
1 associated peripheral sensores Co instrument
panel .
DOUGLAS AIRCRAFT, Long_ Beach, Ca. Conduct flight;
to certify DC-9~30 for grass turf, runway
operation (Norfolk Island - DER) .
AMER-ICAN SAFETY FLIGHT SYSTEMS, Glendale, Ca.
Installation of passenger/crew restraint
system.
WORLD ASSOCIATES, INC.^ Santa Hon i caj Ca.
To install observers windows in lower aft
fuselage in accordance with World Associates,
Inc. Blue Print in W.A. 101 and Engineering Data
Report' WA-3 dated Kay 1972.
-WORLD -A.SSOC-W.IE.S . 1 MC.. , ..San 1 ^ M>K; ;.-,,, Co.
KIS: FS BHO-3
REGION
WESTHRi
' REGION
PAGE
37.
TYPE ntPOST ' ~
[XJ QUART .rtL [JJ SUPPLEMENTAL
r-j?«ioD Oct. ! - Dec. 3 , 197*4
Second Quarter - FY-1975
u
B
dJ
Z
AMEND TC
U
t-
ul
X
X
X
X
X
OTH P. R
X
ESTIWATBQ
TOTAL
MAN-
HOURS |
% COMPLETE
AND
ESTIMATED
DATE OF
COMPLETION
1975
1975
1975
75%
Inactive
6/75
6/75
DATE OF
APPROVAL
FAA Form 8110-13
SUPERSEDES LOCAL
-------
PROJECT
NUMBER
E5798WE-DS
T5800WE-DS
H5805WE
-CL5-80-8WE
TYPE CERTIFICATION PROJECTS STATUS
MAKE AND MODEL
AND DATE
OF APPLICATION
AiResearch 731-2
7/23/7**
Kenv/orthy 1 ^0
Dassaul t Fa 1 con
7/23/7*« DA- 10
Mason 1 *tO
General Dynamics
7/23/7** . 3**0
Patschke 120
ARI J-2
F-a r.-.Wes.t =Ea Moon
8/8/7**
Brandt 120
DESCRIPTION
AiRESEARCH MFG. CO., OF ARIZONA, Phoenix, Ariz.
Modification of S/N P731**3 & S/N 79101 engine
to (1) replace LPC 3rd stage starter (2) replace
LPC 1st stage wheel and snaf; (3). replace LPC
2nd stoitc!' '.f.ntrol on
ART J-2 gyrocoptcr.
THE: [Af< WEST BALLOON Co., o.v<"kmd, Co.
No..' Model- FW-AX-7 '101 ,i'i r \>;\ ! ' o: -n . Tlvr-ee --bcr-ner
li'juid prn|i.-|ne he.'lfrr, Ij.-JSkOt' CT p 1 yworjd bOLtOr1
.'. I t T /IIJ! (J\: ' 1 Ot -5 i (it.'S .
R1S: FS 8110-3
RECIOM
WESTERN REGION
PAGE
63.
TYPE REPORT
QQ QUARTERLY Q^] SUPPLEMENTAL
PERIOD Oct. 1 - Dec. 31 , 197^
Second Quarter - FY-1975
o
bJ
Z
X
AMEND TC
U
t-
X
X
X
OTHER
X
ESTIMATED]
TOTAL
MAN-
HOURS ]
% COMPLETE
AND
ESTIMATED
DATE OF
COMPLETION
1975
1/75
1/75
1/75
5*
7/77
DATE Of
APPROVAL
FAA Form 8110-13 IJ-/QI 'JuiJi_pisEDti LOCAL FOHMS Cfo eoe «e?
-------
APPENDIX B
EXTENT OF CHANGES IN AIRCRAFT MODIFIED BY
AMENDMENT TO TYPE CERTIFICATE.
In this Appendix, aircraft types from Table IA are listed
that have had more than one model or model series (with at least
one approved since 1 December 1969). Additional characteristics
of the various models are listed, permitting an estimation of how
much each model has been "stretched" from the basic, or "parent!1
model. The "parent" model is always listed first.
All data except lengths is from TC data sheets.
B-l
-------
Model
Boeing 747
-100 sen e:.-;
-200 B "'
-2CO F "
-20C C "
-200 SR
DC-10
-10
-40
-30
-30F
Boeing 727
727
727-C
727-100, -100C
727-200
s
Boeing 737
-100 series
-200 series
-200C series
G fOSH
Weight ]
(1000 Ibs)
713
778 or 788
778
ii
613 or 573
443.3
558
558
558
(153,
later also
[l61 or 170.
'176, also .
183, 191,
vand 210
T97.0
up to
[l!6.
: ,
rf
Length'
(ft)
225
225
225
225
171
171
171
171
116
136
91
97
97
Engine
Thrust2
(1000 Ibs)
40.08
1 1
1 1
ii
37.5
39.2
46.3
46.0
12.6
14.2
fL2.6 (JT8
-7)
up to
1.13. 75
U suable
iM.el4
(gal)
47, 334
51, 131
1 1
1 1
47,334
178 k Ib.
243 k Ib.
243 k Ib.
243 k Ib.
N/A
N/A
N/A
Vmo3
(knots)
378
1 1
1 1
ii
j
350
350
350
350
i
'350,
later
1.380
35,0/380
350
Notes:
1. Maximum taxi -weight.
2. Maximum continuous static thrust (of most powerful engines permitted,
if intermixing allowed), standard day, sea level conditions.
3. Maximum operating speed a? sea level.
4. In U.S. gal except as otherwise noted.
N/A Data given only in flight manuals, not on TC data sheet.
5. Length of fuselage to nearest foot. Data from Janes, All The
World's Aircraft 1972-73.
B-2
-------
Model
BAG 1-11
-200 series
-400 series
-500 series
1AI Aero
Commander
model 1121
M
model 1121A
model 1121B
model 1123
Hawker Siddeley
DH. 125&BH. 125
DH. 125
-1A
-1A/522
-3A
-1A/R-522
-1A/S-522
-3A/RA
-400A
[BH. 12 5|
[-400A J
-600A
Dassault Falcon
Fan Jet Falcon
Series D
Series C
Series E
Series F
G ross
Weight
(1000 Ibs)
80. 5
87, 5
100.2
16. 8 or
17.5
17. 5
17. 5
20. 7
21.2
21.2
21. 7
22.3
21.7
23.1
23.1
23.3
25,0
26.68
27. 54
26.68
28.66
28.66
F
f.
\ Length
(ft)
84
84
97
50
50
i 52
'
47
47
47
47
47
47
47
47
50
51
51
51
51
51
B-3
Engine
Thrust
(1000 Ibs)
9. 99
12.25
2.78
2. 70
2. 78
2.925
3.12
3.10
3.10
3.10
3.10
3.10
3.10
3.10
3.68
4. 00
4.12
4. 00
4.12
4.12
u seable
Fuel
(jjal)
3726
3726
926
1090
1090
1300
1231
1231
1232
1366
1231
1366
1366
1366
1419
*
1257
1330
1330
1330
1370
Vm0
(knots)
327 to 333
345
360
360
360
360
290
285
285
260
285
260 .
26Q
260
28p or 300
350
350
350
350
350
-------
Model j
i
Gates Learjet i
'Models 24, 24A
[Models 25 ?5A
J25B, 25C
Models 24.B,
24BrA, 25C,
24D-A
Models 35, 36
1
Rockwell Sabrelim
NA-265
NA-265
-20, -30
-40
-60
-70
-80
G i' o s s
Weight
(1000 Ibs) '
12. 75 or 13. 30
12. 75 or 15. 50
12. 75 or 13. 8(
17.25
r
17. 76 or
18.65
Up to 19.92
20.37
21.20
23. 50
1
Length j
(ft) . '
41.00
45
41.0
'
44*
44
48
47
liingine
Thrust
(1000 Ibs)
2. 70
2. 78
2. 78
3. 50
2.57
3. 00
3. 00
3. 00
4.12
Useable
Fuel
(gal)
789 to 824
95!- to 1114
834
931 or 1110
6910 Ibs.
7122 Ibs.
7122
7380
7380
(
Vmo
(knots)
300
300
300
300
3.33
3.33 or 350
350
350
350
Overall length rather than fuselage length.
'- B-4
-------
APPENDIX C
ANNUAL PRODUCTION (SALES) OF
SELECTED 'TRANSPORT OR
TURBOJET AIRCRAFT
Type
Boeing 707 all models
707-320
Boeing 727 all models
727-200 (sales)
727-200
Boeing 737 all models
737-200 (sales)
737-200
Boeing 747 all models
747 (sales)
Lockheed 1011
models
models
models
els
els
les)
els
les)
els
s DC-S all
DC-9 all
DC-10 all
DC-10 (sales)
!
DC-10-30
(sales)
1
'69
59
115
114
4
_ _
85
122
'70
19
54
37
92
_ _
33
51
C-l
'71
10
33 .
29
69
_
13
43
13
Year
'72
' 3
41
22
30
17
4
24
52
'73 .
11
II1
92
861
923
17
42*
233
28
351
39;
--
21
57
221
181
Es timated
'74
182
183
962
802
753
602
553
242
351
422
-.-
502
502
'75
182
183
603
503
253
36 1
i
483 '
363;!
-------
Note: All of the following information is from DMS Civil Aircraft
Market Forecasts (3). :
Type
Fokker F-28
Gates Learjet 24
25
35/36
HS/BH-125
Lockheed 1329 Jet Star
Jet Star 2
Rockwell NA-265 Sabre series
BAG 111 series 400 & 475
Cessna Citation
Dassault Falcon 20
IAI 1123
\
Note: "--" = no production.
"Space" = no data.
C-
'69
'70
2
'71
Year
'72
--
(prodi
'73
13
21
45
2
30
7
iction
26
8
81
24
24
Estimated
'74
15
32
48
12
24
--
to sta
27
6
86
14
12
'75
11
28
44
40
20
--
t 197
22
5
135
16
12
!
i
i
i
t
-------
All data from AIAA, Aerospace Facts and Figures 1974/5, p38, unlesi
other-wise noted. These data differ from "transports" because air
craft for executive or other use are not included.
1. Woolsey, J. P., "New Airplane Sales: A Long Cold Winter? "
Air Transport World Febl'974, pp 17-23.
i
2. Av. Week & Space Technology. 11 March 1974, pp75-82.
3. DMS Civil Aircraft Market Forecasts, Updated through December
1974.
C-3
------- |