TACAN INSTALLATION IN AIRCRAFT 124

• Document Type: CREST
• Collection: General CIA Records
• Document Number (FOIA) /ESDN (CREST): CIA-RDP69B00279R000100110001-2
• Release Decision: RIPPUB
• Original Classification: S
• Document Page Count: 133
• Document Creation Date: December 9, 2016
• Document Release Date: April 21, 2001
• Sequence Number: 1
• Publication Date: July 11, 1966
• Content Type: MF

Approved For Release 20/06/09 : CIA-RDP69B00279R0001001r10001-2
1 i July 1966
25X1A
Director Of Materiel, t
TACT t installation in Aircraft 124
(A) DIS Won* -'1*$"-66 dated 23 Juno 66.
(C) - 2142
1. raf*rence (A) requested that an agenda ite n for the
Est a ch*du ed Configuration control Board meting co
is accordance with the request of reference (B). Refer+ence (C)
which i lk the Installation of TLCI3 in aircraft 124
to reference {H} for later installation.
overall a roval gives to reference (C) via
d and approved providing for the transfer of
affected .
2. it is rocomended that, coatingeett upon the aaai.lsbil i
of a TACAX systes, authority for installation in air rar
be gra*t as requested in refereace tai.
25X1A
F gp (11 July 66)
2-D/M .
4 -
8 - chrono
6 -
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 ApprOved For-Release 200110
- 0100
10001-2
ENGINEERING STUDY ^
LOCK -CALIF'ORIlIA COMPA_ '
22 -31-1
CHANGE PROPOSAL
DATE 14 JAl'
TfJAIiY 3g6.t ~
AFFECTS : WSPO PROJECT
NAME OF MAJOR COMPONENT
PART OR LOWEST SUBASSEMBLY
PART NO. & MODEL OR TYPE
SR-3
TITLE OF PROPOSAL
INSTALL IY ROV ) GYRO REFERENCE HT ADDIG SYSTEM
NATURE Of PROPOSAL :This ECP covers the development and manufacture of kits req-aired to
install the SR-3 Reference System in all A-12 ships except S/N 124. The SR-3 System
will replace the MA-1 and MD-1 Reference System. Flight Testing of the SR-3 System
will be accomplished on Contract JET-250.
REASON FOR PROPOSAL PEA-i and MD-1 Reference Heading System is used as a back-up for
the INS. This system has a total drift rate of approximately fops' (4) degrees ~ per
hour. The SR-3 system has a total drift rate of one (1) degree per hour. In addi-
'tion, the SR-3 system is lighter and occupies less space.
Use of the SR-3 system should provide the program with a highly reliable method of
carrying out a mission if the INS fails during the flight.
Reason for Revision: To submit Proposed Target Price. This price reflects the trans-i
fer of ship 124 to ECP 22-74.
This ECP was approved by Headquarters Message 2401, dated 19 August 1964.
ESTIMATED COST AND TIME INVOLVED
ES
ADDITIONAL FUNDING REQUIRED :
ESTIMATED COST FOR KITS OR PARTS :
C P
(See Page 2.)
ADDITIONAL FUNDING REQUIRED
ITEMS AFFECTED BY PROPOSAL
SAFETY
MISSION
EFFEC?
PERFORM.
ANCE
OPERATING
PROCEDURE
INTER-
CHANGE.
WEIGHT OR
WEIGHT
TOOLS i
SUPPORT
MNNTE.
NANCE
SERVICE FLIGHT
LIPS MANUAL
MAINTE?
NANCE
MANUAL
TIVENESS
ABILITY
BALANCE
EQUIPMENT
PROCEDURE
^
^
^
^
^
^
^
^
^ ^.
^
EST. MAN/HRS. REQ'D. TO ACCOMPLISH CHANGE IN FIELD
SOURCE OF PARTS FOR KIT ADP will furnish
AVAILABILITY WEEKS AFTER APPROVAL
under Service Bulletins 726,735 and 940
DISPOSITION OF SPARES AFFECTED
i
MA.1 XM M0-1 COMPONENTS 4IOULD BE SENT TO THE DEPOT. ILLEGIB (j
INITIATED BY :
APPROVED :
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9B00279R0001lI=lJ J01-2
PAGE 1 OF 2.
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 Approved For Release 2001/0
/09 : CIA-RDP69B00279
010 110001-2
JI.
R
ENGINEERING STUDY
CHANGE PROPOSAL i
DATE
1!I .T1~ UA Y 1~3~~i
AFFECTS : WSPO [j PROJECT Y
NAME OF MAJOR COMPONENT
PART OR LOWEST SUBASSEMBLY
PART NO. & MODEL OR TYPE
If,g
j14-X-1
TITLE OF PROPOSAL :1 PLACE APX-1?r.:, ZF'F' 7'L ViIL- COX 914X-1 AJ. L AS0CIAT~~ C0r TR0L TJ:tI.T
NATURE OF PROPOSAL : This ECP covers the desigm, development and rmnufacture of kits
required to reple.ce the APX-4 6 IFF with the 'hilco~: 914X-1 IFF, in A-12 Article:: 122,
125-127, 130 and 132. Also included is the associated control units for all A-12,
Aircraft.
ECP 22-68 will provide Wilcox IFF for aircraft 134 and 135 and FCP 22-76 for serials
129 and 131.
124
,
REASON FOR PROPOSAL' The retrofit of the ADP AIC in?A-12 Articles requires the use of
space currently occupied by the APX-!}6. The customized Wilcox IF'? will replace the
APX-46. It is smaller, lighter and technically superior to the APX-1+6. The new con-
trol panel incorporates all the necessary operating functions in a single unit. All
codes can be set during preflight checkout and an emergency bar is provided so that
Fri! Emergency Code is generated by actuating a switch. We have demonstrated our En-
gineering model to the pilots and they have expressed their satisfaction.
Reason for Revision: To submit Proposed Target Price. This price reflects the break-,
out of the five (5) aircraft, (Ref. ECP 2:_1-68 and 22-76), noted above and increased
equipment costs.
This ECP was approved by Headquarters Message 2341, dated 10 February 1965.
ESTIMATED COST AND TIME INVOLVED
E S
N/A
ADDITIONAL FUNDING REQUIRED :
ESTIMATED COST FOR KITS OR PARTS
)
2
(`g
P
C
ee
.
age
ADDITIONAL FUNDING REQUIRED
ITEMS AFFECTED BY PROPOSAL
SAFETY
MISSION
EFFEC-
PERFORM-
ANCE
OPERATING
PROCEDURE
INTER.
CHANGE.
WEIGHT Olt
WEIGHT L
TOOLS L
SUPPORT
MAINTE-
NANCE
SERVICE
UPI
FLIGHT
MANUAL
MAINTE-
AN N CE
TIVENESS
ABILITY
BALANCE
EQUIPMENT
PROCIDURI
^
^
El
El
0
El
ED
E]
^
El
El
EST. MAN/HRS. REQ'D. TO ACCOMPLISH CHANGE IN FIELD
SOURCE OF PARTS FOR KIT ADP will furnish
AVAILABILITY WEEKS AFTER APPROVAL
under Service Bulletins 734, 750, 770,
778,829 and 843.
DISPOSITION OF SPARES AFFECTED ILLEGIB
M-46 units will be returned to the Depot for disposition.
INITIATED BY :
APPROVED : -
P
P ECT
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-12 _j
69
10=1 -
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 Approved For Release. 2001/06
/09 : CIA-RDP69B00279RpAQ100
10001-2
IF0FM1A COMI'kNY -
ENGINEERING STUDY
r 22-35-1
LOCKII! )-CAL
~
CHANGE PROPOSAL 1XI
DATE 14 JAZy[TARY 1966
AFFECTS : WSPO ^ PROJECT
NAME OF MAJOR COMPONENT
PART OR LOWEST SUBASSEMBLY
PART NO. & MODEL OR TYPE
TITLE OF PROPOSAL
ALL ATTITUDE FUEL QUAflTITY SYSTEM
NATURE OF PROPOSAL :This ECP covers (1) design and development of new probes for all
fuel tanks. (2) design and tooling for changes required to the vehicles as result of
the new probes. (3) fabrication, assembly and procurement of all parts necessary to in
124-
122
121
l
12 S
i
,
.,
s
er
a
stall the new probes. The new probes will be incorporated in A-
1329 134 and 135.
Reason for Revision: To submit Proposed Target Price.
This RCP was approved by Headquarters Message 2341, dated 10 February 1965.
REASON FOR PROPOSAL .The present fuel quantity was designed to be light, simple and
as reliable as possible. This resulted in a single capacitance probe in each tank whic
is accurate for the design cruise condition (i.e., 7- degrees nose up). We have re-
ceived complaints from the pilots about the accuracy of the system during non-design
l
,
cruise conditions, especially during letdown. During letdown the fuel quantity is low,
the nose is down and the aircraft is decelerating. Under these conditions the probes
can be completely uncovered, resulting in a zero quantity reading while several thous-
and pounds may remain. To correct these conditions it is proposed that two probes be
installed in each tank. The resultant fuel quantity system will be accurate over a
range of 15 degrees nose up to 15 degrees nose down. These probes will. have the same
overall capacitance as the present probes so the present selector switch, fuel addih?
tive compensator and cabling need not be changed.
ESTIMATED COST AND TIME INVOLVED L1/A
ES
ADDITIONAL FUNDING REQUIRED
ESTIMATED COST FOR KITS OR PARTS
C P
(See Page 2.)
ADDITIONAL FUNDING REQUIRED
ITEMS AFFECTED BY PROPOSAL :
SAFETY
MISSION
EFFEC-
PERFORM.
ANCE
OPERATING
PROCEDURE
INTER.
CHANGE.
WEIGHT OR
WEIGHT IL
TOOLS ?
SUPPORT
EQUIPMENT
MAINTE?
NANCE
PROCEDURE
SERVICE FLIGHT
LIFE MANUAL
MAINTE-
MApNCE
^
TIVENESS
^
^
^
ABILITY
Cl
BALANCE
^
^
^
^ ^
EST. MAN/HRS. REQ'D. TO ACCOMPLISH CHANGE IN FIELD
SOURCE OF PARTS FOR KIT ADP will furnish AVAILABILITY WEEKS AFTER APPROVAL
under Service Bulletins 826, 844 and 922.
DISPOSITION OF SPARES AFFECTED Existing probes removed from Articles will be sent to
ILLEGIB I -/
the Depot.
INITIATED BY :
APPROVED :
C/
AD
P
CT
1E
P
01
Approved Fo
r Release 2001/06/09: CIA-RDE1
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Approved For Release 2001/06/09 : CIA-RDP69B00279R000100110001-2
Approved For Release 2001/06/09 : CIA-RDP69B00279R000100110001-2
 Approved For Release 2001/06/09 : CIA-RDP69B00279R000100110001-2
ROUTINE
TOR: 2 ti3SL 22 JAN 65
THE ~~ EL QUAN 'I SYSTEM ON TT'ti OXCART AND KEDLOCK
AtTEI T ID Fm O N ?AR'1NOcSKY FROM Ca, L JO HMSO
SUBJECTS ALL ATTITUDE FUEL p UANTI .," S;STET
AXRPLANES HAS B';EEN DESIGNED TO SE' AS LIGHT. SII'agLE AND
RELIABLE AS P?`we,S AT THE TIME THIS DESIGN WAS MADE.
THE PROBESg COAX PLUGS MtD THE COAX. CABLES WERE NEW
R y,
r L OF
*
hYom{ t~f NUM
!I"'1.4 ! ft!i pt THE !ia~R t~P
PROBES t1 D L S9 W 4S F'.iRFtOSEL? KEPT TO A MINIMUM.
t? Uu1. Q0.5?r,]TITY SYSTEN ON THE OXCART AIRFL, fRE
4F` dl*'E risrO F P; ' .f `ti'y `.'7~, 4:[~ S COI FE.F h{..:.LY,F'?. ACsCeL !h'iE OFti'1,
t'' ...O..: t,. Lk 1isC 'J 4 S SYSL Fi V..i5.>ES y`ROK JR._
C"T
rtt. .. E4 J ..T '1M ` ~, Y+ .t DE
;
t n,Q 3, i H x.. t~ p A T 1 1 ~ ~~ :'..-
.~~ +%..C~.!Jii :~'.A? ',.'a S M
~ 4?r .
.fi ~; b:.
A 17 I.S w F_4 t~?ir N ED i r1AT WE INSTALL. TWO
ROBES IN ALL TABtIKS. HEAD VOLUME DATA AND PROBE LOCATIONS
. CROUP f.
R3:CLNP40 FROM AUTO
tATtC VOW'NCRADINO
y~{{ I.Nb VtC!fs;IefGTiCN
Approved For Release 2601/06/01 :F,Id("'-RDX-69 00279R 00100'fiT.O,'1-2'
7 NEPTHAN Ti E ISSUING'OFFICE'S PROHIBITED, Con
z
I IN 65.44 11
 Approved For Release 2001/06/09 : CIA-RDP69B00279R000100110001-2
15X1A
111.
`a,;~ak9, S E C R E T
H/1VE BEEN GIVEN "J"O M-H ON ALL TANKS ALTHOUGH THEY HAVE
NOT BEEN GIVEN A GO='AHE AD FOR PROBES ON ANY TANK EXCEPT 4c
5. THE TWO PROBE PER TANK, ALL ATTITUDE SYSTEM INSTALLED
IN THE AIRPLANE HAS PROVEN STABLE IN PITCH, ROLL
AND YAW MANEUVERS IN FLIGHT TESTS TO DATE.
6. WY WOULD LIKE TO GO AHEAD ON ECP 22-35 PREVIOUSLY
SUBMITTED TO YOU IN ORDER TO PROVIDE THIS ALL ATTITUDE
SYSTEM FOR ALL AIRPLANES. WE WILL MAKE THE PROBES
MATCH THE PRESENT FUEL TANK OR THE ADDITIONAL FUEL
CONFIGURATION AS REQUIRED.
Approved For Release 2001/06/09 CEIA-RD RP69 E B00279R000100110001-2
 lkpproved Fo lease 200 - 10 10001-2
ENGINEERING STUDY ^
LOCh`_; D-C 1LIFOR '_1A COI?PA~I Y gyp"" 22-gib-1
CHANGE PROPOSAL na
14 JA'NAN.Y 1966
NAME OF MAJOR COMPONENT
AFFECTS : WSPO (0 PROJECT
AIRPLAITF COr TROL SYSTEM CI-LECKOUT CART
NATURE OF PROPOSAL : Design, develop and manufacture four carts to aid in the complete
checkout of the airplane control system. Three of these carts will be stationed at
or use on the A-12 Articles and the other cart will be stationed at EAF..B for use
on the AF-12's. STATI TL
STATINTL 1
ESTIMATED COST AND TIME INVOLVED :
REASON FOR PROPOSAL: The Contractor has thus far used various pieces of his own in-
strumentation and a ui at to check out problems. This equipment has thur far been
hand carried to of need each time a problem has arisen. This ECP will pro-
vide the program with new checkout equipment in a suitable form and Sufficient quanti.
ty.
Supplying a cart for each airplane location will greatly reduce the amount of time
used for the operational checkout of all servos and hydraulic actuators used in the
control system. The addition of this piece of equipment should greatly enhance the
efficiency of pre-flight and post-flight trouble shooting.
This ECP was approved by Headquarters Message 2341, dated, 10 February 1965.
Reatoi for Revision: To submit osed Target Price. This price reflects increased
ES
CP
ADDITIONAL FUNDING REQUIRED :
ESTIMATED COST FOR KITS OR PARTS
ennITlnNeI FUNfINC; RFOUIRED
(: ee Page 2.)
SAFETY
^
MISSION
EFFEC-
T IVENESS
^
PERFORM.
ANCE
El
OPERATING
PROCEDURE
1:1
INTER-
CAS HANGE
ABILITY
11
WEIGIII oft
WEIGHT L
BALANCE
^
TOOLS &
SUPPORT
EQUIPMENT
^
MAINT!-
PROCEDURE
^
SERVICI
Elf!
FLIGHT
MANUMI
^
MAINTE
NAN(E
MANUAL
^
EST, MAN/HRS. RFQ'D. TO ACCOMPLISH CHANGE IN FIELD
INITIATED BY : APPROVED :
1y/
LDP ?e 001/06/09: CIA-RDP 9B00279R00010M1Ek001-2
-
PAG
1 3~7
AVAILABILITY WEEKS AFTER APPROVAL
E
`'
 STATINTL
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 -Rclea 2
001
-
i
ENGINEERING STUDY D
LOCKtiM,, -CALIFORTETIA COMPATTY
22-58-1 i
CHANGE PROPOSAL y,
DATE
14 JANUARY 1966
AFFECTS : WSPO ? PROJECT ? `
;
NAME OF MAJOR COMPONENT
PART OR LOWEST SUBASSEMBLY
PART NO. & MODEL OR TYPE I
OIL PR 'SSURE TRANS TTER
_,
TITLE OF PROPOSAL
r, _. r
UOiGITTF, OIL PRs.. ~,( n'~ TRI~iTSMITTEM Dr,al l%T I..TFROVI1P ::T T ;: ,.~i,:: I
NATURE OF PROPOSAL : This r CP covers the prototype dc~rclo :lent of" an irtpro~: ed r:n;zine
Oil Pressure Transmitter t:'lrouk-li Sept,::mber 1965. Further t: stirs - of t:^e prototype
units -trill coIltinue r, ayond t. is; time and this eiiort is beinL- ecconrnlished. u"ider
Contract `.JM-66 Category II.
I
REASON FOR PROPOSAL : To improve the service liz e of the nGine Oil Pressure Trans-
mitter. Reference letter Kelly to John, dated 27 October 1964 and APP ,less4je 4667
dated 1 October 1965.
i
Reason for Revision: To submit Proposed Target Price. This price reflect: the cost !
of Phase I prototype testin and the deletion of Phase II, Production Incorporation.
Phase I of ECP 22-58 was approved by Headquarters Message 2341, dated 10 February 1965a
I
i
ESTIMATED COST AND TIME INVOLVED
E S
N/A i
ADDITIONAL FUNDING REQUIRED
ESTIMATED COST FOR KITS OR PARTS :
C[~
(See Page 2.) !
ADDITIONAL FUNDING REQUIRED :
ITEMS AFFECTED BY PROPOSAL
I
SAFETY MISSION PERFORM- OPERATING INTER- WEIGHT OR TOOLS & MAINTE- SERVICE FLIGHT MAINTE.
EFFEC. ANCE PROCEDURE CHANGE- WEIGHT & SUPPORT NANCE LIFE MANUAL NANCE
TIVENESS ABILITY BALANCE EQUIPMENT PROCEDURE MANUAL
^ ^ ^ ^ o ^ ^ ^ a ^
EST. MAN/HRS. REQ'D. TO ACCOMPLISH CHANGE IN FIELD {
SOURCE OF PARTS FOR KIT
AVAILABILITY WEEKS AFTER APPROVAL
t3/A
~
DISPOSITION OF SPARES AFFECTED ,~ 2
N/A ~L~E~oz7'gRIIO~o~r
ENGINEERING STUDY Q
IACKF~-CALTFOitId'.CA C4NtPANY
~
01
-
22-57-1
CHANGE PROPOSAI
DATE ~~ JANJUARY 1866
AFFECTS : W5P0 ? PROJECT ~X
NAME OF MAJOR COMPONENT
PART OR LOWEST SUBASSEMBLY
PART NO. d MODEL OR TYPE
TITLE OF PROPOSAL : HYDRALIISC RE'~IORK - TFB CAPd
NATURE OF PROPOSAL: This ECP prcyvides kits necess#~y to re-route outboard elevan hy-
draulic lines on a1.1 A-12 and YF-1?.A Aircraft. '.Phis Change is raquir::d due to c~~anged
location of the TL'R CAIV by the Engine Contractor.
i
S
I
- - - --~
REASON FOR PROPOSAL :Interference Cif hydraulic lines w1.th TEH C/u~1.
Engineering required w331 be s,ccamglished under Contract I'T-21. Installation of kits
wilt be accompLtshed under Contracts FT-23. ax~d~Qr 3G 23 a.s applicable.
Reason for Rcvisislax: To submit Proposed Target Price.
.This ECP was appxoved by HeadgT~rters Message 2256, dated 26 July 1965.
ESTIMATED COST AND TIME INVOLVED
E ~
NA
ADDITIONAL FUNDING REQUIRED
ESTIMATED COST FOR KITS OR PARTS
(See Pa
e 2
)
g
.
f
ADDITIONAL FUNDING REQUIRED : t
ITEMS AFFECTED BY PROPOSAL
SAFETY
MISSION
EfFEG
PERFORM?
ANCE
OPERATING
PROCEDURE
INTER?
CHANGE?
WEIGHT OR
WEIGHT L
TOOlS i
SUPPORT
MAINTE?
NANCE
SERVICE
llf!
FIiflNT
MANUAL
MAINTE?
NANCf I
itVEN#SS
AsIl1TY
BALANCE
EDUIPMENT
-ROCEDURE
MANUAL
a
a
o
0
o
a
o
0
0
0
0~
EST. MAN/HRS. REQ'D. TO ACCOMPLISH CHANGE IN FIELD I
SOURCE OF PARTS FOR KIT
AVAILABILITY _ WEEKS AFTER APPROVAL F
SERVIr,'F', }3iTI.I,~'TI~d 262 - YF'-12A
SERVICE RLTt~LF,TIiI 673 - A-12
_~/
DISPOSITION OF SPARES AFFECTED ~ ~ 'V
r~oT ICASZE ~~ ~ ._..
INITIATED BY APPROVED :
'
_
A.,DP Approved For Release 2001/06/09 :CIA-RDP 9B00279R0001~r~10~@@p1-2 ILLEGIB
137 PACE i.nF "'
 STATINTL
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:CIA-RDP69B00279R0001 011
0 -
ENGINEERING STUDY D ~
L4C3SEiEErD-GALZFORNIA COME~A~tY
.
~ ,~ 22?50-1
CHANGE PROPOSAL
DATE
. l~+ JANiJAI3y ]~.,
AFFECTS : WSPO ~ PROJECT
NAME OF MAJOR COMPONENT
PART OR LOWEST SUBASSEMBLY
PART NO. 6 MODEL OR TYPE
TITLE OF PROPOSAL
sc-13o car~~~.;~ TRA)!~MIT'1.r~ Arm ~.r~cav~~ ~a~naf-~~ s~.~TEr~ - T.~r$o,~ ~
NATURE OF PROPOSAL: j
. f}
f
f
f
i
r
(See Pale :~~~.)
i
r
i
~
_
REASON FOR PROPOSAL ~tLis revision to this ECP provides the Proposed Target Price for
this woxk. The wtlrk described herein was orfgina,L1y authorized under Contract DK-366g 1
Aiiscell-aneous A~rrnral Na. 1. .Approval far this work under CT-22 was provided is Head
quarters Message 6786, plated b October 1965. The difference between the original Bud-~
getasy Estimate atnd the Pxvposed Target Price is the result of the following scope
changesi
a. Fvaty-nine (~~) ea. six pack up Chutes were added;
b.. Eleven (1,3,j ala. replacement chute systems were e,dded;
c. Fifty (50) Qa. stabilization chutes were deleted;
d.. Fifteea (15) each air pick ~ chutes to be prarured with replacement systems
yrexe deleted, rand
~. 4 & R .was reduced.
EST{MATED COST AND TIME INVOlVEO
E S
ADDITIONAL FUNDING REQUIRED
C ~
ESTIMATED COST FOR KITS OR PARTS
(See Ptage 3 . )
ADDITIONAL FUNDING REQUIRED ;
ITEMS AFFECTED BY PROPOSAL
SAFEri
MISSION
EfFEC?
pER/ORM?
ANC!
OPERATING
PpOCEDUR!
INTER?
CHANGE-
WEIGHT OR
WEIGHT \
TOOLS L
SIMpORT
MAINTE?
NANCE
flRVIC~
LIP!
Ft1G1lT
MANUAL
MAINT!? j
NANCE
TIVENE53
ABILITY
MLANCE
EQUIPMENT
MIOClOURE
MANUAL t
~ t
EST. MAN/HRS. REQ'D. TO ACCOMPLISH CHANGE IN FIELD
SOURCE OF PARTS FOR KIT
AVAILABILITY WEEKS AFTER APPROVAL
NOT Ak'PL+xCABL,E
DISPOSITION OF SPARES AFFECTED ' \ y ~
NoT APFZZCABLk; ~, ~
INITIATED BY ;
---,
APPROVED
ILLEGIB
idle Approved For Release 2001/06/09 :CIA-RD
69B00279R000~6~01-2
1337
 Approved~For Releas~~'001/06/09 :CIA-RDP69B00279R0001(00110001-2 LAC_22_50-1
Fage 2 of 3.
NATLTI~ OF F'R?PO"AS,:
This ECP coves the activities required to furnish the- follocairrg systems:
A. JC-130 Cor~ttm.ncl. Tzxansmitter Kit
1. ?'rototy~~~ Kit
Thia inclu~.en ttcsi~;n, manufacf ure anc~ incts.ll?stion oP one (1)
kit in JC-130 F.
~. K.its (~))
Covers manufacture an3 asUer~ly of nine (~) lcit.~.
3. rurnish ten (10) sets of transmitter:,, a,~alifi~~r , coax ~,aitchc.~,
c:~bling, etc .
~. Furnish five (:) sets (approximately 50;~ Sparc , } for Item 3 above .
13. ~t`~ainirrg Hatches
1. r;anufacture and deliver t:~n (l0) traininu hatr_hes.
C. Recovery Parach~xtes
1. a. Procure fifty (,e?) training parachute eystems (14' airpickup,
main and stabilization), and reefir~ cutters.
b. Procure forty nine (1F9) 16' airpickup chutes to modify the
e}.fisting parachute systems.
2. Procure fifty (50) additions]. pickup.
3. Replacement of expended chutes.
Provide approximately twenty-six (26) additional traini.*~ parachute
systems, (less air pickup chutes), u3ed for ri~in~; tests grid training.
4. Limited repair and overhaul of chutes used Burin; training fznd/or
riggir~x tests.
Approved For Release 2001/06/09 :CIA-RDP69B00279R000100110001-2
 STATINTL
Approved For Release 2001/06/09 :CIA-RDP69B00279R000100110001-2
Approved For Release 2001/06/09 :CIA-RDP69B00279R000100110001-2
 pprove or a ease
8z3':~DT~' 0 798000100
10001-2 ~~
ENGINEERING STUDY ^
LOCt~~-Cr~I,IFflFiTdXA G?~'A1V'Y
2?_-37-1 ~
,
CHANGE PROPOSAL
;
DATE
l~+ J/'~tiJ11RY 196
AFFECTS : WSPO PROJECT
^
NAME OF MAJOR COMPONENT
PART OR LOWEST SUBASSEMBLY
PART NO. b. MC+DEL OR TYPE
TITLE OF PROPOSAL
~IORLJ)-~v'?DE CAPA~II,TTY k'LTGHT TFfiTS
NATURE OF PROPOSAL: Th~.s ECP covers the activities necessary to conduct y7orld-Wide
C.a~ability flight tests of TNS eq~iipmexrt in one (1} C-5~F aircraft. -.
Activities include:
1. Install.atian design, liaison e~rtd moxiitar the results erP the flight test pra-
gra3a;
2. Fabrictatian and subsequent instarll.stian of ,kit in the C-$~ aircraft;
3. Restaraticm a~ C-~~ to original configuration after- cam~aletia-iwl of testing.
will. cT~.tralert for the conduction cf fLight testy data reduction and
~Y' blssaciated work. d3r ectly with ~Iieadquarters. Dio ~ effort is included in
this ECP. STATINTL
REA50N FOR PROPOSAL : L~tter~ Xe11y t4 Sohn, same sub~eCtf dated ~+-29-&g.
Ressos: for R~.sion; Ta submit Proposed Target Frice. This price reflects a reduc-
tian in engis3eering and manufacturing effort.
This ECP u+as approved b3' Headquarters :~essage $O$, dated 1 Suly 1965.
ESTIMATED COST ANO TIME INVOLVED
E S
Pd~A
ADDITIONAL FUNDING REQUIRED : F
ESTIMATED COST FOR KITS OR PARTS : ~
A
C 4-
J ~+~ ~ }
~ ee x e ~~
ADDITIONAL FUNDING REQUIRED :
ITEMS, AFFECTED BY PROPOSAL : I
SAFETY
MISSION
EFFEG
PERFCMM-
ANC!
OPERATING
PRCKECIURE
INTER-
CHANGE?
WEIC+Hf OR
WEIGHT L
TOOLS L
SUPPOIIi
MAINTE-
NANCE
SERVICE
LIFt
FLIOFlT
MANUAL
MAINTE~
NANCE ~
TIVENfSS
AGILITY
BALANCE
EQUIPMENT
PROCEI>3 sh
AVAILABILITY WEEKS AFTER APPROVAL
under Service Pu1l.etix>, !sF'-386.
v
DISPOSITION OF SPARES AFFECTED ~("
N~A C/
INtTiATED f3Y ;
APPROVED : WSPO
Approved' Release 2001/06/09 :CIA-R
6960027 ILLEGIB
1337 PAGE 1 OF3.
 ,~.
_.
~.._..
Approved For Release 2001/g~/~;I,~~>N SY~TEMS 9R0001 0110001-2
LIST OF MAIrd DIFFERENCES
TEB
Pyrophoric Ignition
Essentially a chemical system with
electric current to dump solenoid only.
Electric current (1 amp only) required
at dump. _
Remaining TEB may be dumped after
touchdown fox safety.
4 1 f 2 amps (D. C.) steady state
currexit at each glow plug. (Total
starting amps = 66; total steady amps=
Dump of remaining H2 not r.equired.:
H2 IGNITIC7N SYSTEM
______y_.~ A_D VAN TA GES __ _, . _.. _
More ignition firings (20+).
Less hazardous..
Uses CIS system except for plug and
new wiring.
Doesn't need special ground support
equipment,
Cheaper,
Cleaner combustion.
Pdo tube plugging problem.
Better air $ttrte.
Pale ~ 03 3
H2
Electrical Ignition
H2 gas-D. C. electric system.
Requires continuous D, C. current.
Requires 3 glow plugs in each engine:
Left main engine plug on ~ Es s ential
D. C. bus (This is only plug in each
engine that remai~,zs on battery if both
engines are aut) ,right main engine
plug on monitor bus, and afterburner
plug on monitor bus,
1 I amps (D. C.) starting current and
. ~- ... L ~,,.,.-~ivr~~r..,~.1.~r w..i14, ~..
Potential electric failure.
High current load (surge) to iniate
system.
Ability of current equipment to contain
H2 under pressure must be determineda
System mu-st be on continually in oxderf
#o avoid warmup period.
Dual flameout case may not, have
sufficient battery capacity for relight
if below generator cut out RPM.
Weight penalty =Approximately 3 to 5
pounds.
Approved For Release 2001/06/09 :CIA-RDP69B00279R000100110001-2
 STATINTL
Approved For Release 2001/06/09 :CIA-RDP69B00279R000100110001-2
Approved For Release 2001/06/09 :CIA-RDP69B00279R000100110001-2
 REASON FOR PROPOSAL:
3TAT1 NT
Re~uirPment established by
~Thia ECP is in accordance t~ith letter Mck to Teap, dated #C ~~
STAT{~JV - r u ~ '`~'r
T 1961+ and
3TAT1 ~j
?1eBSOn Yor Revision: To submit Target~Ceiling trice. ~... 4?
r..
~~~~~~~D - c;Al:~axrrT~~ CO~pAfl'Y
_~ ,, x.
CHANGE PROPOSAL
.mDATE~__ ._ ~~t l~(~ ~._._.._
AFFECTS : WSPO ~ PiROJEGT ~.
TAME OF MAJOR COMPONENT
PART OR LOWEST SUBASSEMBLY
ARC-50 AY
3?1TLE OF PROPOSAL = ~r_ ap AY IN T.~LZATION KITS FOR FIVE (5) KC-1.35 `s
NATURE OF PROPOSAL:
Existing ,spare ARC-50 AY Equl.pment will be used to outfit the KC-135'x. T'i~4is
equiptt~ent is reWOrked (OFF AxQ-23 nets procured on Purchase Request ~u8.
,- -r ,,
,~ ~i, .-~ $
ESTIMATED COST AND TIME 1NVOlVED :
ADDITIONAL FUNDING REQUIRED
ESTIMATED COST FOR KITS OR PARTS
ADDITIONAL FUNDING REQUIRED ~e Page 2.
ITEMS AFFECTED BY PROPOSAL
SAFELY MISSION PERFORM- OPERATING INTER- WE16HT OR TOOIb L MAINi!? SE#VICE FF.. tiHT
EFEEG ANC! PRCKEDVRE CNANGE? WEIGNi ~ SiJPPOfI NANCE IIPE MAJ~RIA&
TIVENESS ADIIITY SAEANCE EQUIPMENT PROCIDURI
n
,9
EST, MAN/HRS. REQ'D. TO ACCOMPLISH CHANGE IN FIELD
SOURCE OF PARTS FOR KIT
AVAILABILITY WEEKS AFTER ~,PPi7
~a?E~?.VI(~ BULTETI1ti1 678
DISPOSITION OF SPARES AFFECTED
INITIATED BY ;
APPROVED WSPO
~1 Approved For Release 2001/06/09 :CIA-RD
69B00279R0
~~zua~~.
 STATINTL
Approved For Release 2001/06/09 :CIA-RDP69B00279R000100110001-2
Approved For Release 2001/06/09 :CIA-RDP69B00279R000100110001-2
 Approved For Release 2001/06/09 :CIA-RDP69B00279R000100110001-2
TORS
ro -
25X1~ ATT~1t
DIRECTQ~
183?Z R9 FES 65
SUBJECTa ARC~S? AftaGRAN! STATUS 0F' GROUND STATIONS
OXCART
1. AT !'RE5ENT TIi~E THERE ARE TW4 ARCQSfl tGY) GROUND
25X1A STATIONS AT
2. CLAN YO DELI4JER TWO ADDI'fIOiVAL ARC~S~ ~GY) Gl~OUND
STATIONS DURING WEEK f3F ~#ARLH S, 19b5; At~D O~tE DURING
' ~,
WEEK OF MARCH a5Q 1565. tLEASE ADVISE DISPOSITION.
3.. GRDmI d GROUND UHF=DF EQUIP~9ENT IS JOT PART OE ARC~S16 ~GY)
GROUND ST ATIO~i E.QUIPP~ENTm I~' DF' CAPABILIT'~ IS DESIKED~
THIS EQUIF'@lEI~T BUST BE U5ED IN GOAt~1U~dCTI(~N WITH ARC~Sf fGY) a
PROCUREi~ENT THRQUGH G~'E.
4. CONSIDERAELE CONFUSION I~AS ARISEPJ REGA~tI~ING AI~C~S~ tGY)
DESIGNATION, SONETIl4E a ERRONEOUSLY RE~`ERREI} TO P.S
GRCd 1 t5. GRC~g 15 IS ARR?23 GROUND ST~?IIOI~, EdOT GO:~PAT ISLE
WITH ARC~S~? S. USE OF ARC FOR GR4UAD ST~,TION DESIGNATION
IS ALSO ERRONEOUS. ~lE SUGGES? ESTABLISNINti ANEW
aRaw s
axewoco ~.wr euro.
-uv+a oowNOa~a~.
t.9 DtC1.MlYI/iCNTIQN
REPE~pp~~~~FQeI~ 2f!(()"TT/~~~~~~~J~9~~~1~~~F00~'~~2 ~0.
SECRET
 STAN
N ~s grev5,e>usly ree,~ated by tl>9r~ed Ztj Jane ~.~DS.
The Sena a~ ret3clee tri11 be inate~3.].ed 3>:t the i'iald by thle '~~a1.~a1. se~a?
STATI N
tativ~:s as a part of their xtorma~. duties tus+dsr Contre+ct ?
~~proved For Release
? cio_rznpFgFtnn~~a~,pp01
_
"
ENGiNEER1NG STUDY ^
22~-711
iA. C0~'A~IY
ZACKC~
~
CHANGE PROPOSAL
DATE
29 Roves, 1g65
AFFECTS : WSPO ~ PROJECT
NAME Of MAJOR COMPONENT
PART OR LOWEST SUBASSEMBLY
PART NO. 6 MODEL OR TYPE
~tZ500PE
TITLE OF PROPOSAL : ~~ ~C~ ~l~ ~~
NATURE OF PROPOSAL:
This ~ is for the mattuPactture crf' ~Yteen {?-g) lens reed to vtitri$ t~11 p+~x~~FRs
th the d 3.oo~c c~pebil3ty. The lesaR ass dl~v+el.trped wader ~'2-3.~ ` '~- +'
~
.
tional. le~et ~r'e presently sv~c3.].able t~sd utltd~ t?T~22 $'a11 ~ 6~~tf~96~ i~ tt~].1
'
?
bectRne aces. This MCP e1g+o oavesa the del~i8zy devr~].vpme~.t u~d a~tur~e tit f3.t
'
frhe
teen {I.~ rte reticles required due to tb~ chaa8ed I~~ ~.eP~` Pz'el~~site~l lxy ~
~oxat~rc]. loe~k letna. .
,-
- :
~
?
. ::~..
;.,
- ~t. { '
ate aa.'e peeling with this fob as d3.reeted.
yv
~
~~
ESTIMATED COST AND TIME INVOLVED
E S
ADDITIONAL 1`UNDING REQUIRED
ESTIMATED COST FOR KITS OR PARTS : ~'mrBet Pr3.ce55,122
n
C `-
Caz3.13'~ Fz~`ce ~6~~
ADDITIONAL FUNDING REQUIRED :
ITEMS AFFECTED BY PROPOSAL : _
SAFETY
MISSION
EFFEG
PlRFORM?
AHC!
OPERATIFId
PROCE[11ME
IMER?
C-lANX~ $10,500
NAME OF MAJOR COMPONENT
PART OR LOWEST SUBASSEMBLY
PART NO. 6 MC-DEL OR TYPE
HYDROGEN IGNITIOP~ SYST'r.M FOR YF-12A' S
NATURE OF PROPOSAL:
This HCP consists of engineering, production of hits, E>" ' ~ '
ESTIMATED COST AND TIME INVOLVED
E S
ADDITIONAL FUNDING REQUIRED
ESTIMATED COST FOR KITS OR PARTS : Budgetary Estimate for Total Program
n
C `-
STATI NTL
ADDITIONAL FUNDING REQUIRED :
ITEMS AFFECTED BY PROPOSAL
SAFETY
MISSION
EifEC?
PERFORM.
ANCE
OPERATING
PROCEDURE
INTER.
CHANGE-
WEIOMT OR
1A1EICi/lT L
TOOLS i
61~POfT
MAINT6
NANCE
i!R'VtU FIIOM
UK MANUAL
MAtME?
NANCE
TIVENESS
1
AlItITY
RALAfKE
EOUI/MpiT
PROCEDURE
MANUAL
a
o
a'
o
0
o
a
o
o?
o
EST. MAN/HRS. REQ'D. TO ACCOMPLISH CHANGE IN FIELD
SOURCE OF PARTS FOR KIT
AVAfIABIUTY ~_ WEEKS AFTER APPROVAL
~CS17~E BD~+IIR'SIN TO BE WRITTLH ~?
t. 3
.
DISPOSITION OF SPARES AFFECTED - ~ "
INIjiATEO.: BY ' g
' Ac~pirovedFQr"F2e'lease 2001/060''9 ; CIA=FAD
APPROVED : .
~~? ` ? rx ~ ' ICCEGIB
9B0027~R0
i33?
PAGE ~ OF ~
TINTL
 r~t,r cc- ~ c
Page2of2
Approved For Release 2001/06/09 :CIA-RDP69B00279R000100110001-2
LOCHIiEED IRLET COT~ROLS
LIST OF MAIN DIFF~ES
HAM-STD SYSTII+I ADP Ai SYSTEM
Essentially non-electronic except for
Electronics essential and integrated in
a few ewitcYyes) mechanical, hydraulic,,
electronic, mechanical, hydraulic, pneumatic
pneumatic-mechanical computer.
system-electronic computer. Computer located
Computer located in nacelle-aub~ect to
in E-bay air conditioned environment (or
300o heat in oil cooled encloc~ure.
missile bay on Y'1~`12A).
Probe is near inlet-M Ss picked up off
Probe is on nose of fuselage for M,o(& ~.
nacelle;o( &~ are picked up off inbd
Manual backup provided to offset computer
leading edge half way between nacelle
failure.
cad Fuselage.
Increased spike actuator diameter.
Ito manual backup for confuter.
Uses Separate and fixeda(8~~sensore.
Moderate spike actuator diameter.
Uses rotating probe frith evanbined
a( Eo ~ si gna1.
'
"basic system tolerance dons not
ash reliable operation".
ADP/AIRESEARCH 3Y8'!~I
ADVA1QTAiGE$ DISAUVAI~ITAQSS
d System Pex~'axmence"
mprav
"7
High degree of electronic caa~etence needed
.
e
Higher degree of accuracy and rate -~+?~
from service personnel.
Sec yaw and '7? sideslip (H/S good to
Probe on fuselage measures fuselage deflection
3 1/2 see lox, and only 2?/sec at high
as well as ~. However, this error has proven
.alt.),
fairly predictable for known flight patterns.
Sideslip angle measurement now prac-
Requires higher premium, air conditioned space
tical (off nose boom) ,
in "E" bay; or use of rlissile bay apace on
Clear cut mach number off nos baor~
prototypes. Layup time iS six weeks and
(M at nacelle varies witho(& and
requires approximately 2000 man hours.
introduces co~plexity into scheduling
Weight penalty ~ approximately 10 lbs.
rind dynamic response. ;,ess compli-
cated flow field at nose.)
More occur `te measurement of 0(&
(Loca1G~ & ~ at nacelle vary from true
o f Ee ~ in a complex way making accurate
programming difficult] Independent p~
8a~'pickups contributes to more accurate
Scheduling than combined contrnl.
More reliable switches. Less dynamic
difficulties. Less oscillation. No
noticeable limit cycle (This has been
noticeable in H/S system) Better
control of servo loops. dreater
system flexibility due to separation
of0(8o pickup and use of electronics.
.Large diameter spike actuator more
'
rugged. Manual backup improves re-
liability. Local flow caused by
misaile?firinge less disturbing on
?
ike siti frith pitat at nose
~n
ce~e
a
a
.
 pproved o~F-'r T~eTease
- 1
000 -2
ENGINEERING STUDY ^
LOCKSEED-CALIFORY7:A COA4PANY
~ 22-70
CHANGE PROPOSAL 0
DATE 27 April 1~v5
AFFKTS : WSPO ~ PROJECT ~X
NAME OF MAJOR COMPONENT
PART OR LOWEST SUBASSEMBLY
PART NO. 6 MODEL C!R TYPE
TITLE OF PROPOSAL
IMPROVED WHEE'GS AP? BRAKE$ FOR A-12
roPosgcl is for the replacement of all wheels acid brakes us
NATURE OF PROPOSAL: This p
t
on A-]2' s 6~W' s 121,722, ].2~h - 132. The proposed new brakes E~tld rrheela are of the eon-
figuration developed for aria to be used by S~~'e 13~ and 135?
Thirty wheels and brakes were previously procured under DK-3665 fox 13~+ ~ 135. ~Te
propose to provide an additional 125 wheels and brakes under this ECP. This would
bring the total w"nee:]. and. brake asset? to 155 for tl.irteen (13) airplanes, resczlting
in lOO~i Spaxeg. Suuu'aaz'y: S~PI Installed .eras Total
o Dx
'~ 1
~5)
1
3
135
-3
~
Thi a F7GP)
12~F-132 b6 ~ ~
721
L?2
,
,
Total 78 77 155
REASON FOR PROPOSAL
1. Headquarters I~G$. E~ requests eu LCP. Please, al BO, refer to letter, :Kelly
to John, dated 9 .April 1~5 on the same subject.
2. We request that tyre Depot, be authorized to issue s; Purchase Request under
Contract CT-22 as follow>;t
a. P~N AA3199'+7 Brake Asay Qty. 125 (Budgetary Price $1,034 ea.)
b. P~:d 219A't7.9 Wheel Qty. 125 {Budgetary Price $b35 ea.)
ESTIMATED COST AND TIME INVOLVED
E S
ADDITIONAL FUNDING REQUIRED
ESTIMATED COST FOR KITS OR PARTS : Budgetax~,~ Esti^~ate for CT-22 Call $2~, E~25
C ~
ADDITIONAL FUNDING REQUIRED ;
ITEMS AFFKTED BY PROPOSAL
SAFETY
MISSION
EFFEC?
PlRFORM-
ANC!
OPERATINQ
PROCEDURE
INTER-
tHAN(iE?
WEIGHT CM
WEIGHT L
TOOL,{ i
t11P-ORT
MAINTE?
NANCE
iERVIC,! FlIC3/fT
UFE MANUAL
MAINT!?
NANCE
11VFNE55
AsIIITY
MLANCE
EQUIPMENT
MOCEDURE
MANUAL
^
^
^
^
a
^
^
^
^ o
a
EST. MAN/HRS. RE?'D. TO ACCOMPLISH CHANGE IN FIELD
SOURCE OF PARTS FOR KIT (SERVICE SULI,ETI.N
AVAILABILITY 12-14 WEEKS AFTER APPROVAL
TO RE ISSUED FOR INSTRUCTIONS OI~TLY)
COMPT~TE DELIVERY 18-21 WEEKS
DISPOSITION OF SPARES AFFECTED
BALVA4E WF +' ~ BEARII~3 ILLEGIB
SCRAP ( ) STATINTL
INITIATED BY ; APPROVED
Approv~.>~ ~A~10~~31A~R 69B00279R00 ~?O~QbOa
1337
 Approved For Release 2001/06/09 :CIA-RDP69B00279R000100110001-2
25X1A
O"t :1G
It`1
i
1
o at'iguratiaa~ preeent3.y on oz~.~r
Wider IIT~ oars to be cancele8.. We h+~ve p3.a.eed. n "step warms"
order on these t~ra {~} uaita and. are waiting for ~ foxmal re~~uest
cancel.
pi~:ld maintece eh~l.]. be iis~ited to the repl~aceaent Qf l~idtil.+~r
n=ants (With minor exeeptiane s3a1r).
Cp' ~?-~; ~rould be revised to providr~ the KC-1.35 ARe..54 Bits, less
the five ~S} sate ~t# ARC-S(? AY Ec~uint.
.~. ~ :d stetious {5= above} w~+src~ p3.t~need on ord+cr if
~,~ ,~ .
1 ~ an estisaated prise o~ ~1~K3:~ ce. Brtimated ee2lertic~n
~~~ .$ be ~tit~telY 5: 3P ga-tahead W~ n gi.v~ ~ o~ this
,~~;~ ce-tim~te~t deliv~r?~ ~.-r~u3.d. be in July 1;~5. intended 2aanti.an fbr theta~t
t~ ~-5C ~' $ ie art Qi,scayatian.
Approved For Release 2001/06/09 :CIA-RDP69B00279R000100110001-2
 Approved For Rele~e 2001/06/09 :CIA-RDP69B00279R00(~100110001-2
~'e ~`+~ praceed ~t3th ~~P 22-65 (lase ~c.54 i~quip~nt) and: EGP 22w~ (as
st~amitte~ to ~ in t~* leterest of a~voidia~ any possib~.e delays.
~e reeve ~e~uested to initiate ps^ocuremeat action va the attached ~vantities
arith fsasm~ approval. to bE din t;pon receipt of this ~. ~s a perk of
yx faxaat apprc-v$1' xe re~xest the~t the L~epct ism Rtrchase 1"tern~:st~ for
the tlvntxact -22 ~a~ntitiee iadieated in the attadm~ut.
Also attached is a edgy` of the:- ~raz~k sheets v.sed as a gu3.de dwrit~ ~,ax prate
~wisioa~.ng ec>n:`erettce (+as rev3.sed ~~ ~anua~ry 1}65 ~ ?
'lours trulyt
STATINTL cc:
Approved For Release 2001/06/09 :CIA-RDP69B00279R000100110001-2
 Approved For Rele 20
9 : CIA-RDP69B0029R10d1000,1-2
oa3x;
AdO a
'oa~x
ARC-50 EQUIPMENT TO BE PROCURED BY ADP
AS A RESULT OF THE
18 AND lg JANUARY lg 5 CONFERENCE
Part Number
Nomenclature
CT-22
Qty.
HA-3666
~ty?
Budgetary
Unit Price
1
71+295-$O1
Oscillator
6
6
2
71+221-802
Receiver
6
6
3
71+222-802
Programmer
6
6
~+
71+223-801
Generator
6
6
5
71~+22~+-802
Modem
1
5
6
71+016-801
Power Supply
3
0
7
71+220-801
Madule - Range
6
6
8
71+219-802
Chassis
1
1
g
71:408-801
Power Supply
3
S
10
71+001-802
. Transceiver (R-T)
~+
0
11
71.3953-801
Power supply
5
9
12
713950-802
oscillator
9
27
13
713961-802
Synthesizer
7
8
1~+
713854-802
Multiplier
7
17
15
713956-802
Receiver - Main
7
17
16
713852-802
Converter
7
17
17
713851-802
Receiver - Guard
7
11.-
18
713957-802
Modem
7
17
19
714850-801
Transmitter
7
i7
STATINTL
20
713822-$02
Chassis
2
2
21
713965-804
Translator
~+
0
22
713997-801
Relay
1
0
23
713996-801
Relay
1
0
24
714004-801
Control - Gnd. Sta.
$
0
25
71?+686-801
Amplifier
1
0
26
71~g6g-801
Selector.
1
0
27
708662-801
Cantrol - Transceiver
7
' 0
28 .
708663-841
Cantrol - Transceiver
0
7
2g
708665-841
Indicator - Range
0
8
30
708946-801
Control - Translator
0
9
31
708829-$01
Cantrol - Translator
7
0
32
708977-801
Indicator -Frequency
0
6
33
708810-801
Tester - Transmitter
1
0
34
715094-801
Test Set - Transceiver
6
~+
35
708808-802
Test Set - Translator
l
0
36
708808-802
Test Set - Transceiver
1
0
37
70$928-801
Test Set -Elect. Cable
2
~+
2-3-65
Approved For Release 2001/06/09: CIA-RDP69B00279R000100110001-2
 AdOJ ~'-~
OLI3X i
ARC-50 EQUIPMENT TO BE PROCURED BY ADP
AS A RESULT OF THE
1$ AND 19 JANUARY 19.5 CONFERENCE
Part Number
Nomenclature
CT-22
Qty.
HA-3666
RtY~
Budgetary
Unit Price
1
714295-801
Oscillator
6
,,,
6
2
714221-802
Receiver
6
6
3
714222_802
Programmer
6
6
~+
714223-801
Generator
6
6
5
714224_802
Modem
1
6
714016-801
Power Supply
3
0
7
714220-801
Module - Range
6
6
$
714219-802
Chassis
1
1
9
714008-801
Power Supply
3
5
10
714001-802
Transceiver (R-T~
~.
p
11
713953-801
Power Supply
5
9
12
713950-$02
Oscillator
9
27
13
713961-802
Synthesizer
7
g
14
713954-802
Multiplier
7
17
1S
713956-802
Receiver - Main ~
7
17
16
713952-802
Converter
7
17
17
713851-802
Receiver - Guard
7
11
18
713957-802
Modem
7
17'
19
71~-850-801
Transmitter
7
17
2O
713922-802
Chassis
2
2
~-
713965-~4
Translator
4
p
22
713997-801
Relay
1
0
23
713996-801
Relay
1
0
24
714004-801
Control - Gnd. Sta.
5
p
25
714686-801
Amplifier
1
0
26
713968-801
..Selector.
1
0
27
708662-$O1
Control - Transceiver
7
~ p
28
708663-801
Control - Transceiver
0
7
29
708665-801
Indicator _ Rare
0
$
30
708946-801
Control - Translator
p
g
31
708828-801
Control - Translator
7
p
32
708977-801
Indicator - Frequency
0
6
33
708810-801
Tester - Transmitter
1
0
34
715094-801
Test Set - Transceiver
6
4
35
70$80q-802
Test Set - Translator
1
0
36 .
708808-802
Test Set - Transceiver
1
.
0
37
70$928-$Ol
Test Set - Elect. Cable
2
4
2-3-65
Approved For Release 2001/06/09: CIA-RDP69B00279R000100110001-2
CIA-RDP~9B00279OQ01'~Q001-2
 Approve or a ease 00
-
1 -
ENGINEERING STUDY
LOCKfiF~D -CALIFORNIA CCU~lF'ANY
~ 22-32-1
CHANGE PROPOSAL
BATE ~~ ~ l~~
AFFECTS : WSPO ~ PROJECT
NAME OF MAJOR COMPONENT
PART OR LOWEST SUBASSEMBLY
PART NO. 6 MODEL OR TYPE
TITLE OF PROPOSAL : IASPROVED FIR$ WAR3~ING BYSTlI;M ~ - ?
NATURE OF PROPOSAL : '
,Install n~r.Fenwall Fire Weacniz>sg System to replace Edison Temperature System.
=Fernwall Sgstmm mill be incorporated'ia.all A?12 Article~.-
v
,.~ , .
i.. `~
' ~"w'~yr r Vin _- _
n
_
_
..
_ .. ,
ThiQ'~t~.l'L rn'vide a reliable s ?tem xith~~an e~ ~ y. ,
P Y xpe cted 20, 000 hours P]. iglu time
.', per: false wr~rnirr~. - -
:
,
.. .
s a
.., ..
.> .. -
,.
REASON FOR PROPOSALS =~ .,~ Y~
a
? ~4~
-
~
?
.
k.
:t :
'l.: The Fezi~r~].~.~ Fire;Y Warning Sensing Loop is sensitive to localized high tempera-
-t~re conditionr~,' Edison system eras based upon average temperature conditions.
2... Fenwa.ll.system. is composed of two (2)-.s~n,3ing loops; placed side by side.
Both loops mu>;t indicate that a high nacelle temperature exists before the
pilot is notified hf a high temperature condition.
'3. Reason for Revision. To submit Target~Cei].ing Price.
!'~
Gfi
ESTIMATED COST AND TIME INVOLVED
ADDITIONAL FUNDING REQUIRED
ESTIMATED COST FOR KITS OR PARTS
See Page 20 ..
ADDITIONAL FUNDING REQUIRED ;
ITEMS AFFECTED BY PROPOSAL :
SAFETY
MI5510N
EiFEC?
PERfORM?
ANC!
OPERATINd
PROCEIXIR!
INTER?
CNANOf?
WEIpHT OR
WlIGNT i
TOC+LS ?
SU-PdfT
MAINT!?
NANCE
SERVICE
tiff
ill(t11t
MANUAL
MAIfYIE?
NANCE
TIVENE55
AeIIITY
fAIANCE
EOtJIPMlNT
-IIOClDURE
MANUAL
?
?
^
^
a
^
^
^
^
?
^
EST, MAN/HR5. REQ'0. TO ACCOMPLISH CHANGE IN f1ElD
SOURCE OF PARTS FOR KIT
AVAILABILITY WEEKS AFTER APPROVAL
SERVICE BULLETIN 611
`
015POSITIOht OF SPARES AFFECTEO
ILLEGIB
KILL BR ~~ D~ETERhQNBD BY CDSTt~R IJEPOT
INITIATED. BY ;
APPROVED ; ~
LA,C . Approved For Release 2001/06/09: CIA-R
~
P69B00279R00~'It~0EQD0 ~- (L/J.c~~~, I
U 1337, ~,. ,.. _ ,. ''' ~ ... ~ .. r PAGE 1 OF2+
 STATINTL
Approved For Release 2001/06/09 :CIA-RDP69B00279R000100110001-2
Approved For Release 2001/06/09 :CIA-RDP69B00279R000100110001-2
 STATI NTL
t
ST.ATfNT~~
a ~ ~
' ~ -`' ,.,
. 1/0~/r1~ ~'`in-~~~6JB00279ROOD10011,0001`2
LOGU ,- CALIFaRII~IA 117MPANY
29 ~~t 1865
ENGINEERING STUDY
CHANGE PROPOSAL
AFFECTS : WSPO ~ PROJECT
NAME OF MAJOR COMPONENT PART OR LOWEST SU9ASSEMBLY PART NO. ~ MODEL OR TYPE
TITLE OF PROPOSAL :MEASUREI~NT ~ ~~' ~~ AND YAW
NATURE OF PROPOSAL:
This $CP will provide a method of accurately determining airplane roll, pitch and
yaw. A 7pmm camera, will be fixed to the structure of the airplane~ and will be run
at the same time as the Type I or Type II system.
This ECP includes the design and, manufacture of one comparator system, development
of the computer pxogram required to analyze comparator data and .five (5) data runs
with 'I~rpe T or 2~rpe II .~rstem.
REASON FOR PROPOSAL:
his ECP provides a method for checking the performance and quality of the airplane
~~ systems. For a mare comprehensive description of this ro m
to the letter to John Para osy,~ p ,please refer
of A-12 o i ng .?V, dated 3 September 196+ an the subject
pt provisions
.
Budgetary ECP approvie~l Tf'TX
Reason for Revision:. 3b submit Target/Ceiling~Price.
ESTIMATED COST .FOR KITS OR PAR
TS
.
C i
z
P
ESTIMATED ,COST AND TIME INVOLVED
~ ADDiTIOI+1Al' fttNDING REQUIREd
ITEMS AFFECTED BY ~PROPOSAI~
-~
SOURCE OF PARTS FOR KIT
NOT APPLICABLE
MIS610N /LRIClA14
EFtEG ANC!
TIVENE53
01lMATIMG
i'ROCEOIIRE
INTEII.
AeC IHA`~-
WEIGHT OR
WEIGHT ~
lALANCE
TSUIIOfT
E4UNMENi
iMA1NTE-
PROC~lOURE E
u~lw~u {~ WIGHT
u AAAWUI~IL
PLAINT!.
IMAt WEt
EST, MANfHRS. REQ'D: TO ACCOMPLISH. CHANGE iN FIELD
DISPOSITION OF SPARES AFFECTED
NOT APPLICABLE
AVAILAHIIITY WEEKS AFTER APPROVAL
STATIN INITIATED 9Y ; APPROoVF~
ved For Release 2001/06/09 :CIA-RD 69B0027912~0 1:2
PROJECT ~'~" - ~ Z /,~ ~/(o J
 STATINTL
Approved For Release 2001/06/09 :CIA-RDP69B00279R000100110001-2
Approved For Release 2001/06/09 :CIA-RDP69B00279R000100110001-2
 a~-~~oo~~os/~? ~ -~A-R~RS~9$o?~~~Raoo10O~10~,a~o1'-2..'.._. --
FNGiI`:i.Cidlt3C Sy i f-']!' ~ '1 !
_..J - I
CI1!`.raGl: PRCr't)~!`.l ~'~
p Ai`FEC:~:i : 1.'~I~i'rJ ~~~ P't3t7.FFCT ~' ~
NAME OF MAJOR COMPONENT ~ PART OR i.OVVE ? `aUi~A.;5Et+1'3i.Y a !'~~4iT P'~?. t~~ ;~!C)UCt OR TYPE
TITLE OF PROPOSAL ~ 470RL,D-WIDE C,,f1P/'~ILT7.'Y ~'L.TGIIT T+~STS ~
!
NATURE OF PROPt)SAI.:
'Ihi3 FCi' covc~r3 the ~.ctivttics necessary to concT.uc?t Woxl.d-Wide Capability flight i:estc~
of :[PI:~ equip~~m~: in one (1 J C- jI~ airl:xta..;'t .
t
Activitie:J, inclt,tde: ~
1. Tnct~~tll.a.tion cir,cil;n, ~.iai,.on axia rioni~;~~r thc; reault~ of tlic fli~~ht t~-:.t pro~;ra:n
2. I~:~brication and crib ~equJ~nt inctal7~it9.on Uf kit in thy: C-Si. n~.rci~~.t't.
~ U,...~r,-.,...,+i.,., "i` J`_r:)L i-.~ nrdrvi?nl rr,nP?frterai-_inn nt~h_.~r rnmt'~lr+i'.inn nf' t.nr:'f:inU_ .
will c:onLr~.ct for thc~ conduc;tian of flil7ht Lest, cl,.ita r~~dt.tc~tion t3.nc1
arty asca\:ir~.tt~d wort c~iixeetly with II~ad~Iu~rte~r:. No - :fiOrt ir; included in
thi . >?;CI~. STATINTL
Leti;c:r, Kelly to ~7UIin~ :~,mc sub~T.?rt, d~ttc~ci ZI-~~-65.
E CJ
C
ESTIMATED CO51' AND TIME INVOl.VFU :
ADDITIONAL FUNDING itEOUlRED
ESTIMATED COST FUR KITS OI: PARTS
ADDITIONAL FUNDING REC~UIl2ED ,
Uud~etary Ec~tim~~te ,t~0,CU0
PERiORM ~ QPtRApfNli ~ INifR? ~ :~lru,ilT i?It ~ ti~r7t5 d ~ At.hl71;'.? R Slrv~t.# ~ ;IC ~ >~Qp
1337 V ~ ~ PAG~/1 OF 2
 Approved For Release 2001/06/09: CIA-RDP69B00279R0001001102~-~9
Page 2 of 2,
NATURE OF PROPOSAL (Continued from page 1)
1. The drag chute hook lock support will be revised to reduce friction and im-
prove ,jettisoning capability at higYter speeds. The drag chute hook and link
will be changed to a "roller" configuration; the roller configuration elim-
inates the spherical contact which presently exists between the ball and the
hack. This spherical surface has, proved to be difficult to inspect arid.
maintain. An external indicator system will be adopted in order to provide
a visual assurance that the hook and ball are in the proper position after
the chute packing operation is cou~leted.
2. The actuator will be revised from a single electrical screw hack with a
stall load of 300 - X00 lbs. to a 8ua1 electrical. actuator with an "impact
wrench" mode so as to have e~.peak capability of approximately 2,000 lbs.
This load is more than enough:ta operate the system even when the forces
are unu3ually highly, either in~the deployment or jettison mode. Each elec-
txic mentor is energized by a 'separate electrical, circuit which extends all -
the way to the cockpit, and each half of the dual actuator has. the ability .
to perform X11 required functions in case of me.lfunction of the other. A
single handle is used to energize both halves of the dual actuator. Both
circuits will be individuallyy checked as a part of the pre-flight check-out.
The drag chute door mechanism .will. .be revised to minimize friction by install-
ing~bronze guide rollers bushed licks. We will also shorten the main actu-
ating rod to minimize the effects of bending due to heat.- We will reverse
the direction of the door~ywing to prevent any aerodynamic scooping effect
in the event that it may not be rigged in a completely closed position.
*(This refers to t'_~~e "latching" door - not the drag chute door).
Approved For Release 2001/06/09: CIA-RDP69B00279R000100110001-2
 Approved For Release 2001/06/09 :CIA-RDP69B00279R00010011~01-2
OSA ~ "/~(4~ 5 = (v S
A~~ ~9~5
ub~e~
_'~s ~~r ~ ;,:daa~che-~t It~tet Cor~tx~~ ~~
~~,mit.~.t~n ~y~ster~s fog ~* YF-1~i, C,~+ntrae~fi~ ~T.~2.2
~~ a~ s3d~r~.xi~ the ~ta3,l.atior~ of tl-~ I,o~kha~sd ~I.e~
~~n~l ~,n ~.i+~ ~~ ~ ~~ail.r~ eta in ~ Y'F'~?~ZA ~ir~r~~'1:.
~~3ct~t'~33.ri~3.~: request that A~ ~~ ~s~~ Chan~a ~=~ai
~~r ~~,1x~t~t ^T-~2 tv prct~lc~a th~.s ~~rature #.n aEl3. tae ~'~`?i2A's +~~ are
e~it~! b~as#.s. ~ri actdit~.er~ the r~z-ns1 ?~ ia~af4raa~~~, ohs P
aht~t a~~ ~.ne].ude the ~fnllc.n~t
a.. t tsY :n~1ln d~~tere~es bee ~ t~+c- av~ta~al
~`~ ~ ~.th y~ux ec3,onts an the a~taa ~r disatas et f~tn~
that ate t+z~ the Y~'-# ~A .
'b. Cost ~alcd~a she3w~.n~; e3ig~ie8r~.1't~# kit, grad
~'t~.'! st~,?~n e~osts patc~~y~
~. ~~lu].ea ~r ~ti.t s~a3~,'t~",~' ~ttad ix~L7~.ati~n hss
~ ~,~p~va1 of the LC'~ ~ (Ase~ae -~ahea~ ~r~,car - ~ ~~aly 19~5~
d, Ins~tc~n ~a~ Furs ~2e~d~ day's dc~mtS.-~~a
requ~ r ir~sta~.lati~n ~`ar eassh airt3ra~~.
Yeu ~thari. to suh~it i'~r 3.~s~tten
den i~3,tie~ ~3y'at, on all three Y:~-1 ~A ~ s. The ~s a~
atio~ des~.r~ c~t~ this ~C~' alb.
'T`heater ~Gf'' a eheuls~ i~r F~Pa ~nr the s~pext ern
?~rt'. '~T~,~ 3.atter drams rat ~tth~ret axty e~~fert Y,~ry`enc3 tfhat ratqu'~d
+ t tk~ ~~' ~~ a~ prQV~.da the i.x~F~r~a.t~.ex~ requested. Your
~+asa is r~aestad,
STATINTL ~~ ~*
Approved For Release 2001/06/09 :CIA-RDP69B00279R000100110001-2
 P r
- 00 11 01-2
ENGINEERING STUDY
IAC~4~F~D-CAL3.~URft
A Ca~II'ANY
22^~3-1
~
I
CHANGE PROPOSAL
.
k.
GATE 2~ ~
Aril 1965
AFFECTS : WSPO ^
PROJECT
NAME OF MAJOR COMPONENT
PART OR LOWEST SUBASSEMBLY
PART NO. 6 MODEL OR TYPE
TITLE OF PROPOSAL
FUEL COOLING SY t
NATURE OF PROPOSAL:
SEE PACE 2
NOTE: TMU-~+lE; s, F-G' s, and GId2 Trt~ilers Wvi.>r7.d :~c GFP
'cn ADP.
REASON FOR PROPOSAL
Z. PROVIDE AD~ITIO~YAL RAs~GE CAPABILITY FOR THE A-12
2. THIS REVTSI01~ REPftEBE~TB A DIFP'ERE7!1T A~'PltOACH THAN PREf3E.~ Ll~ THE
SIC ECP P2-63 AND ~S IT IN ENTIRETY.
~ ~
y
ESTIMATED COST AND TIME INVOLVED
E S
ADDITIONAL FUNDING REQUIRED
C ~
ESTIMATED COST FOR KITS OR PARTS : Budgeter Estic~.te Item 1. ~10~0p0
ADDITIONAL FUNDING REQUIRED ;
2. $~.35~400
ITEMS AFFECTED BY PROPOSAL
SAFETY
MISSION
EFFEC-
-[RFORM-
ANCE
OPERATING
PROCEDURE
INTEN-
CHANGE?
WEIGHT OR
WEIGHT ~
TOOLS ~
SlM-ORT
AAAINTE-
NANCE
tERVIGE FLIGHT
LIFE MANUAL
MAINit-
NANCE
71VENESS
Aslllry
lAIANCE
EOUN'MENT
-110CEDURE
MANUAL
^
^
^
^
a
^
^
^
^ ^
^
EST. MAN/HRS. REQ'D. TO ACCOMPLISH CHANGE IN FIELD
SOURCE OF PARTS FOR KIT
AVAIIABiLITY
WEEKS AFTER APPROVAL
N/A
DISPOSITION OF SPARES AFFECTED
NSA STATINTL
INITIATED BY :
App qc~y p
~
Approved For Release 2001/06/09 :CIA-RD
69B002
9F700 1-2
LAC
PROJE
CT
 r. ..^
'~ Approved For Release 2001/06/09 :CIA-RDP69B00279R0~01001100F ~ of 2
(~ ~A$ bF ~OPOSAL:
STATINTL 1. Fuel Cooling System for
This system consists of a mobile fLiel chil]:er capable of coolir~ 25,000
gallons of fuel f'rc~ 84oF to 15aF in txenty-Pour hauxs, used in coii~unction
with four TMU-4,/E insulated tanks. The '~J-4/E's are GFP and must be
mods-Pied to provide Par oa.?e bottom loading. We will also provide the
necessary ~la.el and nitrogen manifbld$, as indicated. on block diagram ~1
of TAG 1212 drawing, to couple the chiller P~.eel tares and nttragen tank. .
The '1''[~J-}+~E; s are semi-mobile in that the ones prevently availcible do not.
have w}ieels mounted on the*.n. These tanks do not }~avc~ their afrn pun ~s,
Filters, etc., and must be located near such Facilities. Each TMU-~/E
has a c~aeity of x,$00 gallana.
2 . Fuel Coo11.n~ 3ys~teM far Deployment Base (s)
This system consists of a F, Levelopznent and Froduc~ticn of two ('') :~,:.~1 ;ool.r:. ~'~:~, j
Cooler will be a TrailLr ~~unt~:>~l 2 to :, FrL02"1, Fiefs i~;~;r:~tian ay~te~~. _"iii. is suffi-
ci~nt coolir~ capacity to lo:~er th~. te>;r~~ratur~: of ~i 25,000 z alla:i fug-1 ts..LC f'rorr! ~~~?r'~
to ~5o~' in a 2~+ hour period cz.uring ti.c ~tL^.u~ier ninths xheii atirer:~?-e air tc~rpc nature is
100 F.
i
fief: wetter, C. L. Jahnsan to J. Ps.razu;osl~y, dated > Octoher 1~6~+. ~ ~
t
I
;'
1
REASON FOR PROPOSAL:
The cooler fuel temperrr~.?ture will slow th.e .Article to carry approxizrmtnly 2,000 powids
acl.ditiorial fuel .and gain an increased heat sink capability.
ESTIMATED COST ANO TIME INVOLVED : .
E ~
-
ADDITIONAL.. FUNDING REQUIRED :
ESTIMATED COST FOR KITS OR PARTS ' Bu.igetary Target Price X53, 931
C ~
(See Page 2~ i
ADDITIONAL fUNDING REQUIRED ;
ITEMS AFFECTED BY PROPOSAL : ,
1
SAfE1V
MISSION
EFFEG
PERfORM-
ANCE
OPERAi1N6
PROCEDURE
INTER
CNANGE-
WEIGHT OR
WEIGNi ~
TdOl3 i
SU-PGR1
MAINTE?
NANCE
SERVICt
UFt
FLIGHT
MANUAL
MAINTE-
NANCE
i1VENESS
AEtIITY
MLANCE
EQUIPMENT
/ROCEDURE
MANUAL s
^
^
^
^
a
^
^
^
^
^
^
EST. MAN/HRS. REQ'D. TO ACCOMPLISH CHANGE IN FIELD
SOURCE OF PARTS FOR KIT
AVAILABILITY
NO'" AP:ZICA~LE
DISPOSITION OF SPARES AFFECTED
i~OT APPLICAzLE
STATINTL
INITIATEDpprOi~ed E,~'~ Release 2001/06/09 :CIA-RD ~~~~
~ /~~i
RO
PROJECT
1-2
 STATINTL
Approved For Release 2001/06/09 :CIA-RDP69B00279R000100110001-2
Approved For Release 2001/06/09 :CIA-RDP69B00279R000100110001-2
 25X1A ~~~~ ;
~Sk~~
'9C~ld 1~3C.~ ~7 i;L'T ~~
~.~~~~
THE NEVI VENT r~RAC~E,T AND DENT DISCpr1NECT SHCIULD FsE INCLtiDF;D Dl1RI~iG
~.Er.~Lacx
S(1D~JECT~ ECP LAC '~2~s2 SEAT ~ t'ARAC~~d~iTE rE~tORK
l e SUt~UECT ECP HAS DEF;N :~EVIE4lI:D Ar~D I5 APi'F?pVED. SEAT
r94DIFICATIpN AID Tt4E ~lEid SINaLE PARA'TihbER ~~ILL SL COVERED UNDE3't
CONTRACT FT~~1 PRESEriT FUNDINU AND THG I~F:~ CATAIP~JLTS Ar6D DUAL
PF,RAT$MERS i~riDER CpNTkACT CT~2~ PRESENT Fl~~4DINGa SEJ~3UECT ECP IS
NOT SPECIFIC AS Tn GNAT COUERED IN SEAT iBQD OThtER Tr~AN NEB' CATAPULT.
THIS ~7QD TURt~t~ARp+JND. ^
25X1A ~? COFiTRACT NEG~7TIATION SCHEDUL~.D AT 12 ~ 13 rj+~V sa
FOR 24 NE~d PARAC-{(~TES? PROPOSED t)ELIVEi~~ SCt{ED~ILES pF T~iI:SE NEB
CHUTES MILL PROVIDE SUFFICIENT FOit Gp~~lF:RAGF. wFtILF: TriE NIr3F: CH(~TE,S
INVOLUEp HERO ARE Tt~RNED AR4i!-~JD. THE NIivE GriUTFr TURea F~RO(9ND COl1~.D
F3E HAi~DLEi~ AS Ait ADD ITIpNAi. ITE-~i Tu THIS COC~TkACT. ACTt~AL TU(,CN
AriptJi~D 4~p'ttLD r'spT f~F: SCr1F.DJLF:D l~ivT IL: ~1PPR01L~ dYi~aR s5 s
3Q FOft _ ABODE CH6~rbGE CAUSED ~Y NEsa HI Er~ERGY C.~TAPULT
Ari~7 r3prl Caf?ipATI3iI.ITY +1~IT~t Ti1F. a~LD CHUTEm ~ Ts~E NF;~3 ~CATE~F'U:..T REQUIRES
3;~.;~~ ! ddx~
:D E L ~ ~ T
~~ 25X1A ~~~~
i~amuP ~ "~'~
>ereaaoan ranee nuiax~ 3
beh:'10 6C1a0/071~n1k-6
A~YJ eYdCR.l:7SHt~:AT?04
Appr~t~~~~.~~~0~ e~.a ~'}~ ~,~~uvjsg'3'G"~1~~1~~~'~~i ~:D, ~?~ ray.
.ii~a ~455~
 ,APpr`o~ec~ fir i~eleatse 2001 /Ofr/09 : CfA=R[7P69B0~0?798000100110001-2
25X1A
~~ ~b .? ~
' ~ "!'
~`
J
(IN 54552) ~ FAGE T~C3
A C~Qd SH]:FT qFT '~I'~K OLD Cf~~{'?Ee isALLRST COiJLD t3,E USFfl TO S}IIFT
~J'T SPl~CE LI~IITATiONS WOULt~ ~1~4S,1r THIS 1~lF~RGIN~i.~ #~'ROt~ ~ S~rEiY
ST?~~DPOIt~T. TUr~N ARtiUI+ID F'(3~i "f,'~IS ~IOD ~ILI.. SE ~3FL~'~~E1J TLL~, R;I'I3i~tG
65 ~HEI~ OLD CAT~Pt,~LTS DUE 1+4ft 'i' i.t`lE CHF~N4E~
4a 1~4~i _ PL1r4SE FURNiSN SCHLDL'1.E I",~H 'T'l9; I~ ~ROIi"1D t~,'~SEO
?!~ OLD CATP.P~IL~' REPI..F1C:Ei~IEdJT Dr~TI?.S l~PF'R:aX S~'RiNG 554
EIwiD OF c~k:SSAGE
Approved For Release 2001/06/09 :CIA-RDP69B00279R000100110001-2
 Approved For Release X01106/09:CIA-RDPS9B00279R000100110001-2
4 r ~_
~,_,
ENGINEERING STUDY ^
C~1'~
~-~2
{!?
CHANGE PROPOSAL ?
~
~
DATE 2~ ~~ 19~
AFFECTS : WSPO ? PROJECT
NAME OF MAJOR COMPONENT
PART OR LOWEST SUBASSEM9LY :
PART NO. 6 MODEL OR TYPE
SEAT AIQD PAAAt;HUTE
TITLE OF PROPOSAL
AF-l2 ~ A1',ID PARACIiL?TE REWORK PROGRAP~4
NATURE OF PROPOSAL:
1. Bxix~ a.11 AF-12 S2Eits back to LAC far Rework to Etccept the ~-ore poWerftzl. Catapult,
developed undex ECP 22-12-]., and other changes resulting from tree Collins El Centro
Test Program. 1
2. Send all AB'-12 Parac.~utes b$ek to P`Sre~re]. for Rewflrk to the liEhter, tl~3.nner versio{
developed under the Collins El Centro Test Pmgxart. `I~Y:e timers wi1.l be sent to LAST. `
I,rA~C wi11 scrap the timers saving all parts useable in the manufacture of i;he new timers;
s
REASON FOR PROPOSAL
The abov~a Td+ork wi1.1 bring the AF-12 Seat and ParEtchute Equipment up to the latest
GanfYguration. {P1E:arae refer to letter, Rus to TemT~. dated 2 Uctober 1~) i
i
1
i
9
11
ESTIMATED COST AND TIME INVOLVED
E S
_
ADDITIONAL FUNDING REQUIRED : I
w
.ESTIMATED COST FOR KITS OR PARTS : NO COST APi'LZCABLE TO 7~iIS RCP
ADDITIONAL FUNDING REQUIRED ; SEE PAGE 2 Eut.cf ~latcd :'ragrs.m ~v~t~ ~~3,1`~0 j
ITEMS AFFECTED BY PROPOSAL : I
SAfETV
MISSION
PERiCMMt~
OPERATING
INTER?
WEIGF/T OR
TOOl1 ?
MAINTE?
SERVICE i11G1(T
MAINTE-
EfFEG
ANCE
PRCICEOURE
CHANGE-
WEIpHT ~
SUPfOfT
NANCE
Uft MANUAL
NANCE
TIVENESS
A81t1TY
MIANCE
EQUIPMENT
-ROCEdURE
MANUAL
^~
^
^
^
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^
^
^
^ ^
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EST. MAN/HRS. REQ'D. TO AGCOMPLI5H CHANGE tN FIELD
SOURCE OF PARTS FOR KIT
AVAtLABIUTY WEEKS AFTER APPROVAL
E EUW[1~I'ItV'S T(? BE ~T
~
SPARES 1~Id, RE F>T:WflI[~I~:A IP1 SO FAR AS - -
IN171ATED 9Y
Approved For Release 2001/06/09 :CIA-RDP6
APPROVED ;
B00279R0001
 Approved For Rele~f~e-2001/06/09 :CIA-RDP69B00279R00~100110001-2
>,.~ -
ECP 22-62
Page 2 of 2
Seat modii"icatfon wi11 be acecm~plished under Contract FT-21, Repair
and Overhaul Section. Budgetary estimate is $1,500 per Seat or
$9,000 total.
New Catapults Por tire seat: ere being provided under Contrrjet C~'-22,
Call Section, FY '6~. Purcrase RAquest 355. l3udE~etRxy es+.i;aftte is
$x,100 per Catapult or ,600 total.
The Parachute Rework will be aceor~plished by Fire~~el under t'~eir
own Pr3.m~ Contract.
The new 8iugle Timer ~rtll 6e provided under Contract F1'-21, Repair
and Overhaul Section. Budgetary estimate is ~70Q per 21~mer or
$6, 300 tote]..
The new Dual Timers w1.11 be procured Under Cantre+ct CT-2~ , CaJ.l
Section. Paxts salvageable t"rorn old single timers wilt be used to
,every extent possible in reducing the pxice of these timers.
Budgetary estimate is $1,250 per Dus.7. Timer, or $11,250 total.
Approved For Release 2001/06/09 :CIA-RDP69B00279R000100110001=2
 Approved For Release 200'I'/06/09 :CIA-RDP69B00279R00010011Q001-2
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Approved For Release 2001/06/09:CIA-RDP69B00279R000100110001-2
 Approved For Release 20'0"1/06/09 :CIA-RDP69B00279R0001001~Q001-2
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Approved For Release 2001/06/09 :CIA-RDP 8000100110001-2
 Approved For Release 2001/06/09 :CIA-RDP69B00279R000100110001-2
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t+~i ~s #+i~ ~.~.. aa:#.~- t~~ ! s.~tteddlg
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kid srti+~ be ~i fir a a~sime Q~te~~la~t~a
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Approved For Release 2001/06/09 :CIA-RDP69B00279R000100110001-2
 Approved For Release 200"1/06/09 :CIA-RDP69B00279R0001001~,p001-2
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Approved For Release 2001/06/09 :CIA-RDP69B00279R000100110001-2
 Approved For Release 20'01/06/09 :CIA-RDP69B00279R0001001.1~0001-2
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Approved For Release 2001/06/09 :CIA-RDP69B00279R000100110001-2
 Approved For Release 2001/06/09 :CIA-RDP69B00279R000100110001-2
23:7 w ~~ ~if2~2 65
.
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.. T O P S E C Ft E T ~ ;~ ' '~
ro DIRECTOR
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~raRg 2~b2~ ~~ MAR 6S ~ ~ ~ ~, aSA 1-E5
~tlo~~TY
OXCART ~ ~ . ~ .
.
REFi
WE WILL BE UNABLE TU (1BTAIN A TITa~N II ~'1lEL `tRUCK, THEREFORE
IT WILL BE NECESSARY TO i~UY ANU INSTALL AiV ALUMINl1M TANit FOR Tt~r
f~2E?~CAOLED FUEL T~:STo 7ANit AN4 X~tSTtALLATT4N COSTS WA~.L BE
,rU'PR4XIMATELY 10,Ot~0 DOLL~,RS FLUS THE' S~, t~OGJ DCLI:.AR~ FOR ECP 22~&3.
xF YOU TKYNK THE SMALL FLANGE INCREASE t~ldlCN MAY BE OBTAI~iED BY
USYNG pRE~COOLED FUEL IS ~iORI'H THE CCiS~'9 l~LEASE XNFORM US Sfl TKAT
WE CAN TAKE AGTI4N 74 OBTAIN Ti~E ALUMINl9M TANK.
END OF MESSAGE
T O P S E C R E x
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OXC-R490-65
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REF:
t. WE THINK. PR~mcoc~t.ED FUEL t~PEeIFIC ti,JETGH'f o.& ?oUNDS PE~i
GALLt7N~ ~IAY INCREASE C2ANGE' A~'F'R07~It~lA1'ELY 6!~ NAU1'CCAL MILLS RA'33i~~'
THAN Aoo To C2~ AS I.NDICATEi~ r.N YOUR MF.SSAt~E. out Fa.cuRE ~s f3(~SED oN
CARRYING TFtE ADD"tTIONAL 2pf~00 POl1NDS OF FUEL FROM TA~~"~0~"i~ 7`D END
OF NORMAL C62UISE, RATHER THAfd ADDIP96 THE FUEL INCREASE, A'C' THE t~:iJD
UE' NORMAL GRUISE. 4JE THINK YOUR FIGUi~CS t~;aY REPRESENT THE 3~AT'~F.R
SITUATION. ACIDITIptdALLYfl WC DO NOT KNOW HDW MUCH 'fFll~: 294101 POUND
WEIGHT INCREASE WILL DEGRADE TRANSd)NIC ACC{?LERA7'ION ANU THERF.6Y 7HE
E!;'~'EGTIVE C~ANUE INCREASE ATTRIBUTABLE TO PRE?COpLED t' UEL. SINGE
THE RANGE INCREASE WILL. BE SMALL NQ MAT?E,R Wi{O5E FIGURES ARE USEDp
IT WILL 6E NECESSARY TO PRE~CpOL KC-135 TANI(ER OFF~~LOAD FUEL IF
THIS PROGRAM IS TO MAVE ANY OPERATIONAL SI(aNIFTCANCE.
Z. WE AGtiEE THAT LACpS PR4POSA1? FOR PC~2E~~?Ct~OLING FU1~L SIrCI' 22~63g
IS SATISFACTORY; HOWEVER, WE DO NOT 4JANT TO USE OUR UNDERGROUND
STORAGE TANKS AS TtIEY SUGGE5T. TH3S PARTICULAR AREA IS NOW USED
..,..~..,..~.,..,......~...,~....v~,,~.....~,...,e....,..y...z~ ,.
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Approved For Release 20 1/06/09 : ~~R~~~~~y0279R0 0100 -
..~.,..~a.r.,...~.~..~,,.,.,..._
REPRODUCTION BY 4it-lER THAid THE ISSlJ11(G OFFICE gS PRO}~1a11`Ep. cpnY ~a?
 Approved For Release X001/06/09: CIA-RDP69B00279R000~9'b110001-2
TOP SECRET
25X1A
SIN 773G59 PAGE TWO
FOR AIRCRAFT ENGINE CHECKOUTS AND IS OVER A MILE FROM OUR HANGAR.
WE ARE DETERMINING AVAILABILITY OF 15,010 GALLON TANKER TRAILER
VEHICLES USED TO FUEL TITAN II MISSILES. THESE VEHICLES WOULD
BE IDEALLY SUITED FOR OUR TEST SINCE THEY ARE INSULATED AND HAVE A
NITROGEN PURGE SYSTEM, IF WE CANNOT OBTAIN THESE VEHICLES, WE WILL
BUILD A SMALL. STORAGE TANK CAPPROX 20,000 GALS ADJACENT TO OUR HANGARS.
WE RECOMMEND THAT YOU HAVE LAC PROCEED WITH CONSTRUCTION OF THE FUEL
COOLER QECP 22Q63~` ANA WE WILL CONNECT THESE UNITS Tp OUR VEHICLE/
STORAGE TANK. WE RECOMMEND THAT LAC CONSTRUCT THE FUEL COOLERS SINCE
THEIR PRICE ESTIMATE IS LESS THAN OURS IF WE WERE TO CONSTRUCT THEM
3. WE RECOMMEND THAT YOU CHECK WITH USAF AND DETERl~1.INE WHETHER
FUEL TEMPERATURE INFORMATION IS AVAILABLE FOR KC~~35 BODY TANKS. THIS
FUEL MUST REMAIN COLD UP TO OFF LOAD TIME IF WE ARE TO DERIVE ANY
`BENEFIT FROt~1 THIS PROGRAM. A SECOND APPROACH TO THE TANKER PROBLEM
COULD BE?TO REmEXAMINE~USE OF KC~135 WING TANK FUEL FOR OFFFLOAD.
IN ANY EVENT, WE WOULD WANT TO CONDUCT KC~~1~~5 TE5T5 HERE TO DETERMINE
FUEL TEMPERATURE AT OFF LOAD TIME. THE MINKMUM TIME BETWEEN KC~13S
PFaI FUEL GROUND SERVICING TO OFF LOAD TIME VARIED BETWEEN ONE AND
ONE HALF HOURS TO FOUR AND ONE HALF HOURS FOR THE SKYLARK OPERATION.
WE THINK THESE TIME ESTIMATES ARE REASONABLI: FOR ANY FORESEEABLE
OPERATIONAL COMMITMENT, THEREFORE THE FUEL. t1UST REMAIN COLD UP TO
FOUR AND ONE HALF HOURS.
xOP S E C R+E T
Approved For Release 2001/06/09: CIA-RDP69B00279R000100110001-2
 Approved For Relea e`2001/06/09: CIA-RDP69B00279R0001~90~10001-2
TOP SECRET
25X1A
25X1A
eIN 77365I PAGE THREE
A. REFERENCE QUESTIONS IN PARAGRAPH 2 OF YOUR MESSAGES
A. USE LAC CONSTRUCTED FUEL COOLERS ATTACHED TO OUR VEHICLE
OR TANK TO PRECOOL FUEL.
B. PRE COOLED FUEL WOULD BE REQUIRED FAT A?12 AND TANKER
LOCATIONS AND IN SUFFICIENT QUANTITY ~'0 SERVICE ALL AIRCRAFT
IMMEDIATELY PRIOR TO FLIGHT.
C, LAC ECP 2253 COST ESTIMATE IS 530931 DOLLARS AND A
20,000 GALLON STORAGE TANK ~ I.~ 10,0fd?~ DOLLARS. 1'HE
10,000 DOLLAR EXPENDITURE WILL NOT BE NECESSARY IF WE ARE
SUCCESSFUL IN OBTAINING THE TITAL II ~~UEL SERVICING VEHICLES.
5. LAC ESTI-MATED 3 MONTHS, FOR CONSTRUCTION OF THE FUEL COOLERS.
M
THIS IS SUFFICIENT TIME FOR US TO SET UP A STORAGE TANK
END OF MESSAGE
TOP SECRET
Approved For Release 2001/06/09: CIA-RDP69B00279R000100110001-2
 25X1A
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OXC-$490-65
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~?R~~~'!?OLYi~XG ~?-l:; ~~Ri~ '1PQ ~IS~7$ FI.~'x.~~I~:u~1 ?~I;GI~~"~$ I
ESTIMATED COST FOR KITS OR PARTS ' ECP ?sudgetary Target 't'rice
C ~]
3ee Page 2. Est imste of fir.,l . F'ra;z?au, ;;o t s I ~, GGO
ADDITIONAL FUNDING REQUIRED : Estimated ibts.l F'roJ:,ram Casty .zllr,?7j ".
ITEMS AFFECTED BY PROPOSAL
SAfETV
MISSION
EfPEt~
PERECtRM?
ANCC
OPERATING
PRC>CEDURE
INTER.
CHANGE-
WEIGHT CMI
WEIGHT ?
TOOLS ?
SUPPORT
MAIHT!?
NANCE
SERVIC!
IIFR
illf3Hi
MANUAL
MA,NTE?
NANrE
TIVENESS
ABILITY
BALANCE
EQUIPMENT
-ROClDURE
MANUAL
D
D
^
D
D
D
D
D
^
~
Q
EST, MAN/HRS. REQ'D. TO ACCOMPLISH CHANGE IN FIELD
SOURCE OF PARTS FOR KIT
AVAILABILITY WEEKS AFTER APPROVAL '
NOT APPLICABLE
'
DISPOSITION OF SPARES AFFECTED
NOT APPLICABLE ~ `
INITIATED BY :
APPROVED : WSPO
'LAC _ -terse 2001/06/09 :CIA-R
P69B00279ROOQ~89~0001-2
INTL
INTL
 STATINTL
Approved For Release 2001/06/09 :CIA-RDP69B00279R000100110001-2
Approved For Release 2001/06/09 :CIA-RDP69B00279R000100110001-2
 ;.
Approved For Release 2~Qy/06/09 : CIA-RDP69B00279Rg00100'F41~~~-~
necember 2, 196+
To: Leo .Geary ~
cc: Contracting Officer -
In response to your request for a price proposal for (1) Conanand Transmitter
Systems for the JC-130 B airplanes and (2) for Recovery Parachute Systems,
z~re submit the following:
It should be Dept in mind that there are some unknowns related to these
systems and we would propose to firm these prices up as soon as these
unknowns can be determined.
I Command Transmitter Systems - JC-130 B's
A. Prototype Kit -
This includes design, tooling, fabrication,
assembly and installation of one lcit in a
JC-130 B at Edwards.
fi7, 000
Note: The equipment casts are included in
Ttem C beloz?r.
B. Provide 9 each Kits :~1~+,000
This includes in-plant fabrication and
assembly.
Note: Installation of these kits to be
performed by the customer.
C. 10 Sets of Transmitters, Amplifiers, Coax
Stritches, Cabling, etr,. ~~+0,000
This includes the cost of qualification tests
by the supplier. It is possible that these
tests may not be necessary; therefore, the
price would be reduced accordingly.
D. Provide 5 Sets (50~ Spares) for Item C above. "12 00
Total Estimated Price s~7 ,500
E. Schedule: Approximate7.y two weelcs time span
is required for us to tool for, mock-up,
fabricate and assemble the prototype kit.
tiTe trill require five days to install this
prototype kit in a C-130 at Edwards.
Approved For Release 2001/06/09: CIA-RDP69B00279R000100110001-2
 Approved For Release 2f~Q,y/06/09 : CIA-RDP69B00279R000100101-2
~;. Schedule: (Cont'd)
2t will require ninety days to obtain the
transmitters and amplifiers; however, there
is a spare transmi~~ter and amplifier avail-
able which could be used for the
prototype installation..
II Recovery Parachute Systems
A. Procure 50 Parachutes, including reef cutters
I3. Provide 10 Test Hatches
This includes tooling, fabrications assembly
and packa~in~.
Note: The above does not include AGN to
handle the hatches. Ere assume that
tl~is is available.
C. Schedule: As of 10-21-6~- t~re authorized our vendor to
obtain long lead. time material and parts for 5d
parachutes and reef cutters. They will require
approfir~lately 30 days after go ahead to furnish the
first chute and can deliver 2~week thereafter.
We can provide the first hatches in 90 days.
Sincerely,
Approved For Release 2001/06/09: CIA-RDP69B00279R000100110001-2
 pprove or a ease 2 /09 : CIA-RDP69B00279ROr0~010 110001-2
ENGINEERING STUDY LL..~~.. ~?
&40~;~'~;D-C~T.~~~`r:"r'~~ ~Di'~'~~"'?~ CHANGE PROPOSAL
DATE ~~, 1Tbti'T~"'l?'~: '_?'}.:~-
AFFECTS : WSPO ~ PROJECT
NAME OF MAJOR COMPONENT PART OR LOWEST SUBASSEMBLY
T1TlE OF PROPOSAL
9~~'. STA~INTL
NATURE OF PROPOSAL : ~L~~? 5 l~CP C'?V~:PE (1~ dr 5;.x;17 Lttd. ra.e,~lc7rr,~te~:t O" iieSl 1;?"aJeS ~Q2? 2.l].
~'t;e? t?n}~s. (?_~ dFSi;~.~ a;~u toolirir_; fox c}~anres r~.qu3xecl L?o tie yc:}::isles ^.s result oz'
the riew probes. (,;;, :s'abr~~cat~.on~ asser7bly and pracure~lsrat of all T+~..--t?,s ~
a_;:it:i,:'~Et;t~ m0~~. ~~:Z . (i:~f.'t6
EST. MAN/HRS. REQ'D. TO ACCOMPLISH CHANGE IN FIELD
AVAILABILITY WEEKS AFTER APPROVAL
Sex^~xe~; ?ullet3lx ~~~ '~~ Y:r:Lttc:z ( --
DISPOSITION OF SPARES AFFECTED i?,.Y.%st3.ytg l:ro'~f.:s senrov~d ~'roa.~ Axticle?.: ^ari.ll. ue sent to
t,~E Dex>ot to }~~c)~-lru S/I~ l~%~ - -
INITIATED BY : APPROVED : -
Appro d Release 2001/06/09 :CIA-RD 69B00279R000'~'~~b01-2
1337
6'l~ ~'T'~i'T't'IiI~ ~l73s'I+ ~AII?ts
TITIE OF PROPOSAL : ~,Eh MANI~CEP~NT xEVISI~N
i
NATURE OF PROPOSAL:
This ECP covers the engineering design and fabrication of kits required to change
the fuel tank se uencing of tanks ~3 and ~+. '.Phis change will be accampli:;hed on
q
all A-12 T s except #12~+ (12 ships) . STA
~.
We are proceedi.~ with this fob.
~
;~,~
~5
~
a'
REASON FOR PROPOSAL
This ECP will result in te.nk ~4 being the last tank in the fuel sequencing. Asa
result, the C.G. of the article will be moved further aft far a greater portion
of the cruise condition. Z`,oving the C.G. aft reduces trim drag, and results t
in greater range. ;
~. ~~
.~
~'..r-~'
.. ~ ~ '
~~" V i
~'
1
ESTIMATED COST AND TIME INVOLVED
c
E `~
"`
ADDITIONAL FUNDING REQUIRED : ~
ESTIMATED COST FOR KITS OR PARTS : ECP`~3u~,getary `~'hrget Price
C ~
E.-t.of `Related PraF*ram Costs
ADDITIONAL FUNDING REQUIRED : (See Page 2) Tatal Program CostSTATINTL
ITEMS AFFECTED BY PROPOSAL : s
SAFETY
M15510H
EFFEG
PERFORM-
ANCE
OPERATING
PROCEWRE
INTER?
CHANGE?
WEIGHT OR
WEIGHT i
TOCIIS ~
SUPPORT
MAIHTE-
NANCE
tERVIC!
lIF!
FllCi-fT
MANUAL
MAIHT!-
NANCE
11VENESS
As1UTY
ltAIANCE
EBUIPMEIR
PROCEDURE
MANUAL
^
^
^
^
a
^
^
^
^
^
^
EST, MANiHRS. REQ'D. TO ACCOMPLISH CHANGE IN FIELD j
SOURCE OF PARTS FOR KIT
AVAIIAB}LITY WEEKS AFTER APPROVAL
s~Exvlc~ nvr~mrN 6~+9
~
DISPOSITION OF SPARES AFFECTED
ivOT~D oN sExvlc~ B~~.E~rlri
NTL
INITIATED BY :
APPROVED
LAC
PROJECT
I NTL
PAGE l OF 2 ?
 STATINTL
Approved For Release 2001/06/09 :CIA-RDP69B00279R000100110001-2
Approved For Release 2001/06/09 :CIA-RDP69B00279R000100110001-2
 w Ann
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Approved For Release 2001/06/09 :CIA-RDP69B00279R000100110001-2
 Approved For Release 2001/ /1~~6~1~1~79F?.A~Q010 110001-2
C
HANGE PROPOSAL
NAME OF MAJOR COMPONENT PART OR `LOWEST SUBASSEMBLY PART NO. b MODEL CHt TYPE
TITLE .OF PROPOSAL
~.
ESTIMATED COST ANO TIME INVOLVED
AOOITIONAL FUNDING REQUIRED
ESTIMATED COST FOR KITS OR PARTS
ITEMS-AFFECTED BY PROPOSAL
SAfET1'
AA~SSION
EFfEC-
IIVFNES3
pE11ATIN(1
PROCEOIIR!
M~llIQ~M `R
4-LANCE
EST. MAN/HRS. REQ'0. TO ACCOMPLISH CHANGE IN FIELD
SOURCE OF PARTS FOR KIT
tae Bull,et~-n try b~ 1~~1r~n
MAINTl. .
?MAHUAI
AVAlLAB1UTY WEEKS AFTER APPROVAL
APPROVED ;
Approved For Rele~se"'2`O~Q1106f09 ; CIi4=l~E~P:69BA02"79~0100110001-2
TINTL
 STATINTL
Approved For Release 2001/06/09 :CIA-RDP69B00279R000100110001-2
Approved For Release 2001/06/09 :CIA-RDP69B00279R000100110001-2
 lease 2 OY'L'T~K[3 000100110001-2
ENGINEERING STUDY 0 22-32
IACKHEED-C 4LIFc"?~tIA COAI~'4NY ,~.`~.~~
CHANGE PROPOSAL
AFFECTS : WSPO
NAME OF MAJOR COMPONENT PART OR LOWEST SUBASSEMBLY
IMP?OVED rTRE WARNING SYSTEM
NATURE OF PROPOSAL:
Install new Fenwall Fire Warning System to r eplace Edison Temperature System.
Fenwall Syst~n wi11 be incorporated in all A-12 Articles.
This will provide a reliable eyatem with an expected 20000 hours flight time
per false warning. '_
REASON FOR PROPOSAL: _ ~ t
1. The Fenwall Fire Warning Sensing Loop is sensitive to localised hi~h.te~mper-.-
ature conditions. Edi.san systean was based upon average. temperature conditions.
2. Penwell system is compared of two (2} sensing loops,::placed side by, aide.. Both
loops must indicate that a high nacelle temperature exists befo'~e""~he pilot
is notified of a high temperature condition. w -
3. We are proceeding with this ,job.
The pCP v?~.ue wncii.catecl belc~t does not include ;~are:~ end G6E of $50~OOa apprax3.r~4ete
v~1ur}. mares End t}SE w:i.l.l be procured via Ihirchnse Ret;uest>s under C`P-?~ Call
Sactiou.
ESTIMATED COST AND TIME INVOLVED :
E ~
ADDITIONAL FUNDING REQUIRED
ESTIMATED COST FOR KITS OR PARTS
C (~
Budgetary Estimate
ADDITIONAL FUNDING REQUlREO : .
ITEMS AFFECTED BY PROPOSAL
Y
MISSION
-ERFORM-
OPERATING
INTER-
WEIGH
T OR
TOOK ?
MAINTE? iERVICE FtIGNT
A
EIN ~~~
MA1NTE-
SAFET
EFFEC
ANCE
PROCEDURE
CHANGE?
WEIGH
T L
SINPORT
N
NCE
IAANUAI
?
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AiIUTY
6AlA
NCE
EQUIPMENT
/ROCEDURE
?
a
a
o
0
0
0
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a
EST. MAN/HRS. REQ'D. TO ACCOMPLISH CHANGE IN FIELD
SOURCE OF PARTS FOR KIT .
SERVICE BULLETIN TO BE WRITTEN
DISPOSITION Of SPARES AFFECTED
WILL B E DETERMINED BY CUSTCirIER DEPOT
INITIATED BY
LAS
1337
AVAILABILITY ' WEEKS AFTER APPROVAL
PAGE 1 OF 1.
 ~ed'~ei=-Re I
0
-
ENGINEERING STUDY ^
LOCKHEED - CALIFORNIA COMPANY
CHANGE PROPOSAL
,~ 22-'31
DATE 25 July 196l~
AFFECTS : WSPO ~ PROJECT
NAME OF MAJOR COMPONENT
PART OR LOWEST 5U8ASSEMeLY
PART NO. ~ MODEL OR TYPE
SR-3
TITLE OF PROPOSAL :INSTALL IMPROVED GYRO REFERENCE HEADING SYSTEM
NATURE OF. PROPOSAL ? .,f ,_
?:, ',~
This ECP covers the entire cost of installation of the Qeneral Electric SR-3'? Reference
SysteTn.. The.compoaents of they SR-3' can'.
the MA-l and. MD-l: Reference
to replace
System
.
,,
;
beylocated im-the,same positions used for the MA-1/MD-1 Sy~tmt.`.``Engineering.:and -jam
~. installation involved are, relatively small: Sobs. ~. SR-3 System xould ba incorpora~t?d
~
a~CCOr~+13sYsed. ~~ .
in ? all A-12 Articles: F2iEht t~ati~, of :the ~-3 Byste~nl will: bps
' ~y n .k ~? { t +f~ 'r2~ x ~ ~ i r 5M uc a. JA ~ li y +y-'w
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;REASON FOR. PROPOSA~k '~ ~ `x; F _-'. ~ ~ ~T~ .~~, ~, ~ ~~~ ~ ~`? ~ ~ '"~`~~ ?' ~"`;~'',
xv r'r' .~r 'g c?. rt s.
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i. ~}, ^^~ '
,A ~ ~ ~... ."? .t. .4".'? ,dry. -. ?. ,. ?.,
~MA:1 and'MD-1 Referenc? Heading 3ystean is "used- as a back=up `for th`e INS .This s~'stem
has a total drift rate `of approximately. Your. (!t)-degree~~per: hour.~,The,.-SR-3 syeteaq~`,?` ??
f
of ones (1) .degree ?per hour. In addition,,the SR-3 system is,
''has ~a total dritt?'irate
~
- ` " : -
lighter. _and occupies less space.
Jse of'the SR-3 system should provide the program frith ahighly-reliable method of
carrying out a mission if the INS fails during the flight. '
'the PICP value indicated telow does not inclucT,e Spaz~es axrd (3~ of ~-10Q,000 apprac~icu~t
Vs7.?~. b~areo t?~d CASE wi11 be procured via Purchase Requests un~lex CT-22 Cer.l.3. Son
C
~ v
ESTIMATED COST AND TIME INVOLVED : 'S
~
?E S
1
ADDITIONAL FUNDING REQUIRED :
~
C [~
,
,.---""'
ESTIMATED COST FOR KITS OR PARTS
Budgetary Estima e - STATINTL
IkDDITIONAI FUNDING REQUIRED :
ITEMS AFFECTED BY PROPOSAL
SAFETY
MISSION
EFFEC?
PERFORM-
ANCE
OPERATINf3
PROCEDURE
INTER?
CHANGE-
WEICsHT OR
WEIGNT i
TOOIE i
SU-IORT
MAINTE?
NANCE
tERVICf F110H1
LIFE MANUAL
MAINTE?
NANCE
TtVENESS
AsIItTY
RAIAHCE
El]UI/MENT
-ROCEDURE
MANUAL
^
a
^
^
a
^
^
^
^ ^
a
EST. MAN/HRS. REQ'D. TO ACCOMPLISH CHANGE IN FIELD
SOURCE OF PARTS FOR KIT
AVAILABILITY WEEKS AFTER APPROVAL
SERVICE BULLETIN TO BE WRITTEN
DISPOSITION OF SPARES AFFECTED
ML-1 AND MD-l COMPONENTS WOULD BE SENT TO THE DEPOT . STATINTL ~_ ~ '~-'
..., ,
., x -..
. , . ,
,. , ;:. ~. ,~,
APPROVED . ` r: ,
_ _ ~-
 Approved For Release 2001/06/09 :CIA-RDP69B00279R000100110001-2
~'.^. DIRECTOR
25X1A
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25X1A nRxORI?I'Y ~~
T~
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O?~CA~iT
REF
rOR JQ Pl~1~A~JGQSXY FROM
ti 25X1A
~a flUR C',~RRE!`3T i3~JDGE'TARY ESTITMf4 E TO REfiROFIT THE ELEVEi~
~I4M1LTOt~W STA;~D4RD E'~'JI'r'i'ED l~? 12 ART CLES Ir, T'iI'S I'~tC.LUDES
MI~~IMU~f ~:.A~rI^~;EERT~G A'ui) T!~f~? ING IJECE SPRY ?"0 SAC}CF IT TIE ^,D!' R-12
PROD~JCT10~i CO~IFIG~~RAf't0~ II~JL~:T CONTR L ItiTO THE P--l2a PLUS
T'?~OG4JRE;"?w'~T Q~' E"~'.JI;':1ErJ7 A~~I} aT;TTCLE ]~~D COSTo
25X1A 2~ TI~ :~tDDITIO'.?a~ Sri", }4~'.5 i~P~,J G5E OV T~iF. Or~.DE.F? LF "rO
25X1A SH',i3>.~LD BE COtiSi'~ERrL' TO S'J~'FO
vg T%! gPRTTALLY ~OF~'SET T}-I75 COST Ti
T~f;E CU'dT 3.~IUI'~G R ~. D F1D MOi~ Er FORT DY
T THE I~~ODI~'IED fi,RTICLESe
EF.E IS A POTx.N'T IAL REDr.1CT IO'V
A;4? STD TO PftOVr AND/OR ~' 1
i }i C..L '~ JC 1r f~.-2 Croy Igo.
 Approved For Release 2001/06/09 :CIA-RDP69B00279R000100110001-2
25X1A
4 0 3 A5E D Oi~J OUR r~E ILaT~ Tfl ACGELERR3'E FRC~D1aC:~ aC~N SCf~EDULES ~'~l~Z ~iy 12
HARD'~P,RE C13rRREN~'LY G~i'~ O~~DEi~ AT ~7E~R ~Sl~~OR VE{dDORS9 ~E ~rJU1,D PLAta iO
DIt/ERT ALTERNA'~E SETS Cba T;-tE A? &~ PRGGRAM ANI~ AIt~1 TO COMPLETE 'IHF,
FiRSf CON~IERSI411g PRC~S~,~3LY 1219 BY OCTOBERa ALL, RETROFITS COULD N;~T SE
(~NIPLETEA BEFORE NE?~T SPRIt3G.
5o TIiE: ADP COd~PUTER l~l1ST IIi+STALL IN THE Si~ACE N(}~ CICCUPIED a?a' THE
APX~~6 IFFo NR OTHER E~UIVALEf~T SPRCE REMAINS I'V THE Aa 12 FOR IFF
U!dLESS R SMALLER SYSTEflI CAN HE FOUND. 1~E ARE l~OW II~VESfIGATING THISo
COST OF A ~3E~V IFF IS NOT INt~LUDED IN PARAGRAPH 1 a
END i~F ME5SA6E
S E C R E T
Approved For Release 2001/06/09 :CIA-RDP69B00279R000100110001-2