EVALUATION SECTION - 1 JANUARY 1958 TO 31 DECEMBER 1958

• Document Type: CREST
• Collection: General CIA Records
• Document Number (FOIA) /ESDN (CREST): CIA-RDP74B00752R000100050001-0
• Release Decision: RIPPUB
• Original Classification: K
• Document Page Count: 43
• Document Creation Date: December 22, 2016
• Document Release Date: December 13, 2010
• Sequence Number: 1
• Publication Date: January 1, 1958
• Content Type: REPORT

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Section VI
Evaluation Section - 1 January 1958 to 31 December 1958
1. Evaluation and Analysis of'the following test missions-
a.
73
- "B" Missions
b.
11
- "C" Missions
c.
2
- A-2 Missions
d.
1
- A-1 Mission
Approximately 650, 0.00 feet of.film'was viewed in.making the' evaluations
on the'above missions.
the viewing of an.additibnal.60,.000:,to 75, 000 feet of material....
2. Evaluation of about 25 missions at?Proj:ect. Hqs. and E., K. which included
2. I' The majority. of these 'were "B" missions which, in'most cases,
showed a marked increase in quality over that which had Been obtained
in.previous seasons. Several of these were of even better quality
than.. that obtained'in locaLtest missions-under more or less ideal
operation conditions. . Some of the problem areas detected by viewing
this material were a light leak and the slipping of a:frame (thought
to.be.a- shutter. malfunction) both of which were evidenced only in the
on-off operation duzi ng operational missions and not in test missions
where the unit was run continuously. Both of these conditions have
since been corrected. Another area of concern, a loss of quality
during the'initial portion of these missions, is being investigated.
It is suspected the cause may be due to the rapid temperature change
in the equipment bay causing increased distortion in the lens system.
Verification of this hypothesis and consequent remedial actions are
being sought through a series of test flights to be flown early in 1959
so that maximum quality may be obtained through all of each mission
in the 1959 season.
The quality of the A-2 take viewed remained up to the same high
standard established during the-previous seasons.
3. An S-Curve analysis was established to record progress made during
product improvement program on the "B". Also, this was used to establish
minimum acceptability standards of quality prior to shipment of each unit.
3. 1 The product improvement program entered into at the beginning
of the year resulted in the average quality on the "B" being increased
from approximately 25 1/mm.to 35-40 1/mm or an increase of about
10- 15 1/mm. This increase is being noted throughout as the minimum
quality obtained was raised from 10 to 25 I/mm and the maximum
changed from 35 to 40 up to 45 to 50,1. Therefore, a mean' of 35 1/mm
was established as minimum quality on all units before acceptance
for shipment.
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Spares and Supply
Delivery of all items was completed on Contracts .SC-21-54-(Work'Order.
32) and BC-200 (Work Orders 44 and 322) during the 1958 season.. Call-,
a
Contract HF-CT-696 (Work Order 325) was started,1 July 1958, with.
total of four Calls to each Customer submitted through 31 December 0 58.,
This contract is 98% on schedule.
P. ardin Contract BC-450 items . returned by Depots to'* M & O` f6r',re-
g
work, the 1958 season started with a relatively large back H
in September 1958, a complete. review of ,the backlog was made and a'
semi-monthly list of all items on work order for each customer':wae
7.- 7_77
ancies and established `a record control system which should'
discre
man
p
y
enable faster turnaround time for items requiring, rework. In August-1.958;
a complete inventory of M & 0 stores was conducted. The'inventbrj~ wag:,
.
split into- sections for, Customers A and B. Maximum and minimum supply.:
levels were established on all items..
A close liaison was maintained with both Depots an d ?Del Rio through,:
periodic visits. The contacts have eliminated many discrepancies before
they developed into major problems. Hycon Spares.Coordinator; .M.r..,
R. Keppler, at the request of the PE Corp. and FOG, made, several trips
to Norwalk to assist in establishing a supply system at that location.
In-plant, Stock Record Cards have been made covering all tooling on
Contracts SC-21-54 and BC-200 to facilitate transfer to M & O. A review''.:
and disposition report of all GFE for both contracts was made to insure
proper control. A procedure was established for obtaining disposition of
all scrap and obsolete materials on hand.
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4. Tests were outlined for verification of suspected causes of degradation
in quality, such as vibration, aircraft motion,, temperature changes, star-
light and filter characteristics.
4. 1 All areas of possible improvement to the quality of the "B"
take are being investigated such as the exclusion of much "stray
light" through a series of baffles. Baffle tests to date indicate
an improvement in the quality, mainly by increasing the contrast
and by permitting easier recognition of detail. Filter tests are
being planned with additional optical glass filters to determine if
ground haze can be more satisfactorily penetrated than with just
the present coatings. Tests to date in this area have been' ,.
unsatisfactory owing to the effects 'of temperature, humidity and
air movement on. the gelatin . type filters used on'the' tests,, these.
being the only ones.. then available.
5. A special "B" Fault Book was assembled and,distributed to all parties,
concerned.
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Section VII
Future activities during the 1959 season will include continuation of the
following:
a. Vibration Studies.
b. Infligh.t Quality Change
c. Stray Light Control and Haze Penetration,
d. S-Curve Standardizat
e. Temperature Studies
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To:
From
Date: 10 February 1959
Subject: Annual Report of Project Activities for Period 1 January, 1958
;:.through 31. December 1958
-r 7
. ' ' Service :Bulletin Summary
::Configuration Status
Manning:,Chart's;
Mission Summary 1958
Section 2 - ,Equipment Effectivity
Section 1 --Maintenance and, Overhaul
Section 3 - Field Service. Department
Section 4 = Test Site Activities'
Section 5 - Spares and Supply
Section 6 - Evaluation Section
Section 7 - Future Activities
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STAT
STAT
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Engineering Department
are the major areas of endeavor;
The main concern and effort has been directed to produce improvement
of the 73-B Configurations. The end result of this effort has been marked
improvement in both equipment reliability and product quality. Following
1. Two-Speed. Film- Drive Motor- (73-B). Provides"-reliable two-
speed motors to replace one.-speed units which necessitated manual'
changeover. This new unit provides in-flight 'selection' of`coverage
2.'- Film Drive Assembly. Redesigned' shuffle cam providing'.
sImoother_IMC and relocated. guide roller for more accurate,film
sensing.
3. Light Baffles (73-B). Eliminates extraneous internal light
reflections which insures low level of base-fog on results.
4. Take-Up and Film Drive Clutches (73-B). Provides smoother
operation of take-up and film drive. Also reduces field maintenance
to a minimum on these components.
5. Programmer-Junction Box (73-B). Completely redesigned for
in-flight mode selection. Programmer and junction box are enclosed
within one box to simplify wiring and maintenance.
6. Shock Mounting (73-B). IMC Follower Cam Optical Structure,
Take-up assy. oblique drive assy, and shutter were shock mounted
to reduce vibration and consequent degradation of the photo results.
7. Shutter HS-732. Increased reliability through refinement of detail
design in the mechanical and electrical system.
8. Remote Control of Configuration. Enables pilot to select different
modes of operation during flight.
9. Supply Spool Brake. Provides smoother supply film feed which
affects and improves film transport.
? 10. Tension'Sensing Assy. Increased reliability through refinement
of detail design in the mechanical and electrical system.
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11. Platen. Improved and more positive vacuum application to
platens.
12. Vacuum Valve. Improved design utilizing rubber piston
which replaces previous metal piston. -This eliminated need for
critical adjustment and eliminates previous trouble area.
quality of image.
13. Data Recorder. Improved installation, ldendab'ili.ty and;'.
Maintenance Order,' Authorization Requests, S-Curves,. Fault Book 'and
major breakdown of 'activity: Shop Work Orders, S.ervice'Bulletin's~,
ment and/or quality improvement. This section-contains the following;
calendar year. 1.958 emphasizes, the work completed for product irriprove-
The activities report of the Maintenance: and Overhaul'section for
A. Work Shop Orders:,. The following 'number 'of. ma jor components
and units were overhauled ' and' returned to service:
L- 18 Configurations 73.-B
2. 4 Configurations A:-Z'--
3. 3 Configurations A-1
4. 101 Shutters HS-732
5. 135 Shutters HS-731
6. 31 Shutters HS-730
7. 51 Magazines HM-732
8. 13 Magazines HM-730
9. 28 Film.Drive As s y. 73-B
R. Service Bulletins. Equipment improvements generated and
initiated by in-plant engineering are furnished directly to the field
for immediate use on equipment by means of the service bulletin
system. A total of 31 service bulletins:were initiated and delivered
during this period. The complete list is submitted as enclosure (2).
C. Maintenance Orders (MOE's). The MOE system furnishes the.
detachment teams with the latest preventative maintenance proce-
dure and provides an interim introduction to new equipment and/or
techniques. A total of three MOE's were initiated and delivered
during this period.
1. Moe #17 - Preliminary Manual, Shutter HS-732 (Revision 1)
2. Moe #18 - 73-B Configuration (Revisions 1 &2)
3. Moe #19 - Shutter Speed Testing and Reporting.
D. Authorization Requests (A. R. 's). A total of 239 A. R. 's were ?
processed during this period. The following breakdown indicates
the general distribution of activity.
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15 A- 1 Configuration
39 A-2 Configuration.
152 73-B Configuration
33 Ground Support Equipment
E. S-Curves. , A system for standardizing and controlling the
quality of each configuration was introduced into operation during
this period. ` This system. enables each detachment to check the .
quality output of each configuration-prior ?tothe next missi.on'.. This
information is fed back to the-plant and consolidated for. continual
F. Fault Books. ? Six fault books were fabricated. to{assist,in
detecting areas of trouble. within the Configuration:" T. hes?e
were-delive?red to "Det; .."B" Det. Hge: P. I,, EAFB, FOG:;
'
and
Plant. Graphic illustrattong and' explanations ..were furnished
on the following, subjects::
Image.Motion.
Shutter
3. Focus
4. Vacuum Loss
is tracking.
6. Fogging
7. Static
8. Obstructions
9. Condensation
10. Overlay Tool for P. I. Use
G. Unsatisfactory Reports. A total of 20 U. R. 's were received
from FOG and acted upon during this period. The majority of these
U. R. 's were concerned with relatively minor discrepancies.
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Equipment Effectivity
Enclosure (1) summarizes equipment effectivity for the 1958,operational
season based on Headquarters Directed and Test Missions of DetachmentsB and. C. The box scores for:. Headquarters. Directed Missions. utilizing.
Configurations A- l, A-2.and B are as follows: B Detachment, 95. 1% . acid .
uipment effectivity of 94. 0%.
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STAT
Field Service Department
Personnel at Detachments- B and C. To bring the number of-personnel up
to a complement of eight (8) men at each- Detachment for the 1959 season,
During the later part of 1958, was assigned to the position _ -STAT
of Field Service Manager replacing On 1 December 1958, 'STAT
new Agreements of Erimp1oyment were signed by thirteen (13) Field Service
additional new personnel will sign contracts in January and February.'
Personnel who did'not` renew-their contracts were either reassigned to
awaiting' overseas deployment. Effective 1 January 1959, however, Test
by a permanent Field Service-crew supplemented by back up personnel
meets -B-and C.'.,Stipport of Test. Site activities- during, 1958 was accomplished
'closure; (1) outlines the .. current manning. charts covering-'Detach--
available and on contract for' deployment when and where required.. En
back up support-level'of from three (3) to five (5) men is-plannedto'.be-`'
with the transfer of only one man from-Detachment B to Detacbment'C'.. _A
February; 1959 ,- Rotation. of personnel. between detachments=was.'minimized,.
in-plant activities or . terminated. Annual' vacations for overs.ea.s,pe'r.'sonnef.
commenced in November-:and for the rriost part ,will have been completed by
Site activities will. be supported by personnel assigned to the.M &' O Section
and will be dispatched to the Site .only for Headquarters authorized .tests-:
A team of three (3) Field Service Re resentatives was maintained at Del Rio
to support FOG operations, as assigned in June 1958, to .STAT
assist Messrs In August, was reassi nSTAT
as Senior Engineer at Detachment B and was replaced b
For personal reasons, returned to take another company STAT
assignment at the end o the year an was, therefore, re laced b STAT.
It is anticipated that the services of Messrs. STAT
L
and will continue through the year 1959. STAT
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During the 1958 season, a total of 146 missions were flown at the Test
Site with A-1, A-2, B and C Configurations plus Triple Tracker. 75 of
these flights were optical-and reliability acceptance tests with the 73-B
Configuration, 18 for Project and 57 for FOG. One optical and reliability
feet of 9- 1/2 inch film and 20, 000`fe'et;of' 6-3/4 inch film:was processed:
test flight was made with an A- 1 Configuration and two.flights with A-2
Configurations for the Project. Eleven (11) test flights were' flown with
the .'C Configuration. ? Film from one side of all missions and all film
from some missions was processed at..the test site. A .total of 350,
on the A-9- Film Processor.
processing combination would: provide'. the best photographic results.
photographic emulsions to determine which film-filter-camera s"etting-
Fifty-one Red Dot missions were flown for.E: K.using the A-?Z?and B
Configurations and the, Tracking Cameras, .for the purpose of testing
The tollowing tests were.accomplisnea:
.11 Series D Triple Tracker Missions
11 Series E A-2 Missions (3-V Mount)
6 Series F A-Z Missions (3-V Mount)
4 Series G A-Z Missions. (3-V Mount)
4 Series H A-Z Missions (3-V Mount)
8 Series J Triple Tracker Missions
7 Series K B Configuration
With the exception of.film clips, all Red Dot material. was shipped. to E: K.
for processing.
Headquarters Directed Missions for 1958 included one flight with B
Configuration Serial #13, and one flight with A-2 Configuration, Serial
#8. All material from these two missions was forwarded to E. K. for
processing.
To provide E. K. with rolls of 70rrim film for processing, four special.
missions were flown using four Trackers mounted in a single hatch. .
Installation, maintenance and repair of Tracking Cameras, Hand Controls,
Drift,Sights and Sextants were also supported by Hycon Field Service
personnel at the Test Site.
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ENCLOSURE -----_1_---_-_--
MWO* T s ZDN
' !'festivity" is interp amen, to s,eaa the ov*rsU efteotiv*n ss
or ability of a .Dstsaloeat to obtsls1Qg the ead result of vssable a posed
file for all types of Missions (?riming-Test, Eq. Directed, vz) vith
& specified photopsphie eonfLg retina. DgvipwrAt etteetivity is based
i .ril1 oa the eat pssto a of the ccntigmrstiona
to hAdetiaa Orly eat re]aabtf. O ratica of the skdtes, film traas-
yoar~ dytfrss-, obliq~ai po ii~ioaing, 0, yat"ograoaiug, vae~oosi~ axr "Sol rsd
ds iii "septabU p s. Xqui s efteetivity is slso
'tb ibiuty of tbs. piste at" at ts, to yrosr]4r srsitasa,.
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IIDZVIM l 'AQA CPZRATIOI AID 8lMTIv1?Y
9'1'Aa!' I
A?1
NO -
l~lf .
1 1000
25
B. 28
Tota3 54
A-1
A?a
92.5%
93.0%
`X' MILdz . sst
NO. 8ff.
2 . 90
30
43
1.00%
81.8%
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3,922 REM= R
! Hew ruts Bireet?d Xtssioas
Dot - B
Qonftg ttion A?1
1
3
Configuration A.2
25
13
.Oonfigmration B
g8
20
48
s$
38
Cvsrau Aquilawt it f tir'ity
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 BaaBo 33c1~C
6.#3 al s
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!. ',(1 JamaaiO 1959-to 33 December 1958)
L8 BK J23
mutari i stuck to
MW ]bII
1. LBO{ 37-
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6-41 Vay
T. 21-0 or-$541
R-6 B5#9W6
]b )Well III an I&
1. I
2. PACO-wommer
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4g
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(I Jy 1938 to 31 Deear 1958)
113.79a aura
1. 3-26
2. 5-2
3. 5-10
4. 5-12
5. 516
6. 5-23
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Bff 5&63
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2.
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1. 3-18 T 58-38
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1. 4-30 BT 58-61
2. 8-19 3-1461
ss 61
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'ion
1. 5 i8. BwlAo9 e 6
2. 5..26 C-1763 H-S![ 8
3. u-6 B?-58-91 B-88 2
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11.29 B-1493 SN76-8-9-68
run j" (No amply break. )
;. 7-23 B-IA3 i R-Ss 6
n2ft JJ (Bo apparent caeae)
1. 4-21 0-1734 B-8N 10
Filmm Sem (Caao lan)
1. 4-5 0-1722 8-8810
smfte Itty e ) terial
1. T-Lp BT 58-83 B-S 9
Vbewn Solenoid Stuck
1. 5-24 0-1762 B-S8 10
NO MALFUWr3M
1. Pralpeoamer
2. Cbliqm VrIvO
ks
'5
17
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EQUIPMENT OPERATION &EFFECTIVITY. FOR 1958
HEADQUARTERS DIRECTED MISSIONS.
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ENCLOSURE Enclosure (2)
.SUMMARY.OF SIGNIFICANT SERVICE BULLETINS
"B" Configuration'
HC-73B-SB6
HC-73B-SB5
HC-73B-SB7
HC-73B-SB8
.'HC-73B-SB9 'Film Drive 'Pressure. Roller Remove interference.`. in film drive'
and, Servo Motor-. and protect servo motor radio noise;
HC-73B-SB14
FOR 1958
Purpose
To replace 2-wire solenoids with
3-wire solenoids.
Oblique Position Lamp Block To eliminate loosening of Position
Indicator Lamp.
Oblique Position Resistor To give better control of lamp
intensity and prevent lamp. burnout
of bulbs by turning potentiometer
to extreme position.
IMC--Cam- Follower Vibtra= A Title Self-Explanatory
. Takeup and 'Film Drive,-
Mod. (Clutch)"
filter from lens' cone.
assure .sufficient tension.-on- fi]
supply spool from full spool to
pty spool condition
o ^replace original 1-.speed motor.;arid,
irst.design of `2-speed rno,tors
o (eliminate =extraneous :light from'
outside of'format area. reflecting
'?froin'inside'of 'structure to'~
.To eliminate exc.essive',field main=
.tenance previously required on film
drive and takeup drive clutches; to
provide smoother slippage and reduce
possibility of binding under extreme
emergency conditions' of operation.
HC-73B-SB15 - Standby Holding Circuit To,eliminate extra data chamber
Mod.- counter pulse when camera is shut
off and restarted during mission.
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Enclosure (2)
Page 2
Nut Spring Pivot on Film
Drive
HC-73B-SB16 ' Clip Assy, Sensor Roller
HC-73B-SB17
HC-73B-SB18
HC-7313-SB19
HC-73B-SB20
Shutter' Shock Mount
Installation
Field Replacement of Platen
Purpose
Replacement of Ground Desig- To provide a good exposure of the
nator Letters "L" & "R" .letters "L" and "R" on the- film.
HC-73B-SB21 Replace Rt. Tension Sensor To replace "2-piece assembly with
HP-8191-SB1-
HP-8191-SB2
Arm
Mod. Mark I, II, &' III
Controls
Replacement of_2-amp-fuses
with Circuit Breakers
Title
Capacitor &' Diode. Change,
K-2"Relay
Platen Measurement HM-732
Magazine
To eliminate inisadjustment of
tension sensing device during shipping
and ground handling of camera.
To replace Hex. Nut with Slotted Nut
to eliminate film interference.
To establish proper dimensions be-
tween shock mounts for shutter.
To improve operation of camera by
installation of improved platen assy.
improved 1-piece arm,
To allow pilot selection of all,four
modes of 73-B Camera
operation.,
.1. 0 mfd capacitor'.in.place.'of .; 1 mfd capacitor reduces arcing, also removal
o provide ' ,voltage protection'fo.r. -arc.
auppression'capacitoracross 'relay. `..:.
ccontacts and provide =field".personne
-with oscil1oscope.check to, determine
.
serviceability'of -filter- suppres sor fly {
To supply depth=gauge for periodic
inspection of platen surface to camera
mating surface for assurance of proper
focus.
a) HR-731 Manual.Trip
Lockout
a).
b) Mode 2 Lock-up Pro-
tection
b)
To prevent camera HR-731 from
tripping when HC-730. camera trip
is depressed.
To prevent relay lock-up when
.switching from Mode 1 to Mode 2.
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III. Ground Support and Related Equipment
HG- SB 10
HG-SB 10A
HG- SB 11
HG-SB 12
Modification of Electrical .'.
Test Set
Elec. Test Set Cables
Elec. Test Set .Cables
Power and Vacuum Cart
Mod.
Znclosure(2)
Page 3 - ' _
Purpose
To bring Electrical Test Setup to
date to test latest modification of
73B Camera with 4-mode selection.
To add 3 new cables to test set
cable list.
To furnish Programmer test cables
for Elec. Test Set.
To remove wet cell acid batteries
and replace with 115 V A. C. 50-601?'
cycle to 28 VDC Rectifier Power
'Pack.
To add primary transformer to
Sensitometer in order to reduce
fluctuation due to line voltage
HG-SB13-
HSOP-SB7
Cart Parking_Brake
Filing and. Disposition o
o
e
l
Obs
te Prints
variations'.
To .provide a safe-parking method.
To insure that_field"group is keyed
for latest revisions of drawings .as
-they 'are released
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12 January 1959
Customer Remarks
B Complete with 8R-731STAT
A
~hri,aksg~
avaibing disposition. by Spares Coordinator. 8/N 10 is on loam to Customer A project
o0Na ON STATUS
are being',hold ijr-M a' 0 new .stores on.Voucher #9015215. as spares for Customer D
-Complete with HR.731
Complete Vith -M -T31
WO AR-731, W/3 NC-730
d W43D. (~C 8/x 18,19,25)
to Cust~ A. with eamere T'A/a '18, .. 19 6'051. BIN 12. b"
Gemara tor ooistiguretion 8/A. 8 iii! "ie b.fng held ,in N d 0 r sv.:.
g'3.ie per reQussti; or. Spsri i :0ooraiuutOr. came ra .8/g 14 and 84
No cameras (disassembled)
W/0 ER-731
B No cameras (disassembled)
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 Sanitized Copy Approved for Release 2010/12/13: CIA-RDP74B00752R000100050001-0
12 January 1959
A-8 Configurations
It is Of a$van to K&..0 andl.tho`aastdmer.'to keep this Configuration sv
on short.notice and in addition,, provides a complete configuration for rotation to
STAT '
installation. This in-no var. affects the readiness capability for immediate shipment
M &',0 for working`.out - andtesting minor component; improvements; suol data
detachments to permit in* ion of desirable improvenente in field units,. besides:.
.providing the opportunity for complete factory K A 0.
cation custmor
Aemazts~
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 Sanitized Copy Approved for Release 2010/12/13: CIA-RDP74B00752R000100050001-0
2
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 Sanitized Copy Approved for Release 2010/12/13: CIA-RDP74B00752R000100050001-0
4. C Configurations
Camera No. Location
] Plan'.
2 EAFB
3 Plant
EAFB
5 PE
6 Plant
Customer
t M:
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 Sanitized Copy Approved for Release 2010/12/13: CIA-RDP74B00752R000100050001-0
12 January 19;9
S~m!mar,~.
Physical ConfCoru%g.A-? con-rig. 3 Config.C
Location 'u.-t.A Cust.! Cu.$t.A Cun",.B i=Ust.A i.c .3 Ct1st.A Cuat.B
M & 0
EAFB
PECo
Salvage
0 0 0
Total Serial Nos. 9
3
14
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1 0 0 3
0 3
0 1
0 6'
 Sanitized Copy Approved for Release 2010/12/13: CIA-RDP74B00752R000100050001-0
6, Status Summary
12 January 1959
A-1 Configuration at M & 0
A-1 #1 Projected delivery 15 March 1959.
a. This configuration shipped from
to be returned tq
and flight test.
b. Is presently in M&O,
on completion 'of overhaul
c. - HC-730 cameras and magazines are being readied for
shipment Bu. Stds. for calibration.
A-2 #8 This configuration is being held in M&O for storage only, and
is ready for delivery upon direction.
STAT
STAT,
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 Sanitized Copy Approved for Release 2010/12/13: CIA-RDP74B00752R000100050001-0
6. Status Summary
B Configurations at M & 0 and. EAFB
B #11 Projected delivery undetermined, pending lens delivery.
a. This configuration shipped from
rorM&0. It is to be
STAT
returned to via wRAMA on completion of overhaul and flight STAT
b. It presently in M & 0 having completed a series of Red Dot Tests.
with special.non-coated lens.
c. B'Lens sent.to PE'for.overhaul.. Not yet received for installation
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 Sanitized Copy Approved for Release 2010/12/13: CIA-RDP74B00752R000100050001-0
6. Status Summary, Contd.
B #17 . Projected delivery undetermined, pending lens delivery.
a. This configuration shipped from
for M&O. It is to be' ' STAT
on completion of overhaul and flightSTAT
b. Is presently in factory M&O and has had no flight tests since
STAT it was received from
c. B Lens sent to PE for overhaul.
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 Sanitized Copy Approved for Release 2010/12/13: CIA-RDP74B00752R000100050001-0
Iq
Next 2 Page(s) In Document Denied
ILLEGIB
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 Sanitized Copy Approved for Release 2010/12/13: CIA-RDP74B00752R000100050001-0
Date
TWX
Mission Number
A/C
Config.
& S/N
Trac
S/N
Config.
Footage
Tracker
Footage
Configuration Operation
Tracker Operation
Drift Sight Operation
3-5-58
BT-58-29
3
210
Successful. Quality good.
Clear.
MK
3 6-78
BT-58 30
~
353
7
475
~
'
Successful, Qua'yiry good.
Cl. ean
.
MK2
37-58
BT-58-31
351.
12
3 hr.,
500'
Successful. Quality
Successful.
Cear.
43 mi:..
undetermir.t-d due weather.
3 11-58
BT-58-33
35?
~
A ? 1
13
250'
'd nn due wcat.iter.
Met.~. s''.tch
~ri ng cycle
Clear.
Malfunction after 250'.
3-12-58
BT 58 31
351
B 9
17
3 hr.,
240'
Successful. Quaff t} fair.
Malfunction after 240' - cause
Fooled for 1 hour, then
2.4 min.
undetermined.
cleared.
1800
3-13-58
BT-58-35
352
A-2 #4
1
120'
450'
Successful. Quality fair.
Successful.
Clear.
Weather poor.
3-15-58
BT-58-37
352
B #2
12
3600'
126'
Successful. Quality fair.
Malfunction after 126'. Cause
Clear.
Weather poor.
undetermined.
3-15-58
4078
351
13
600'
Successful. Quality excellent.
Clear.
3-18-58
BT-58-38
352
B #9
7
1914 cy
250'
HS-7.2 Manfunction #61.
Malfunction after 250' - cycle
Clear.
K-2;ReLay - transport okay.
switch.
Undezcast - no quality,
rAl
3-19-58
BT-58-39
351
13
11'
4
Malfunction after 11' -cycle
Fogging throughout flight.
switch'.
Checked for leaks.
3-20-58
BT-58-40
352
A-2 #3
7
1800'
550'
Successful - V-7 counter failure -
Successful.
Clear.
Quality excellent.
3-21-58
BR-58-41
351
B #9
7
?
450'
100'%.'successful. Vib on ,
Successful.
Clear.
obliges - no quality due poor
weather.
3-25-58
BT-58-42
352
A-2 #5
17
11'
Not fUrned on due weather.
Malfunction after 11' - spool
Fogging for first 1 1/2 hrs,
latch interference,
then cleared. Driftsight
pulled and found to be
leaking at numerous places.
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 Sanitized Copy Approved for Release 2010/12/13: CIA-RDP74B00752R000100050001-0
Date TWX
Mission Number
A/C
Config.
& S/N
rac
S/N
Config.
Footage
Tracker
Footage
3-26-58
BT-58-43
355
B #9 7
2276 cyc
500'
2
3-27-58
BT-58-44
351
A-1 #5 13
R2-V3-L4
1
11'
167'
V5
126'
3-28-58
BT-58-45
352
A-2 #5 112
158' per
475'
camera
4-1-58
BT-58-46
352
A-1 12
425'
4-2.58
BT-58-47
351
B 17
400'
4-3-58
BT-58-48 1
355
A-1 17
475'
4-8-58
BT-58-50
355
B #2 13
4320'
450'
4-9-58
BT-58-51
351
13
450'
4-10-58
BT-5 8-52
355
B 7
375'
4-11-58
BT-58-53
351
B #9 7
6386'
475'
4_15-58
BT-58-54
355
12
475'
4-16-58
BT-58-55
351
7
450'
4-17-58
BT-58-56
355
12
400'
4-18-58
BT-58-57
351
B #9 17
3, 750'
320'
4-23-58
BA-58-02
355
19
400'
4-23-58
BT-58-58
351
18
400'
4-24-58
BW-58-08
355
18
27.5'
4-25-58
BT-58-59
351
1 13
300'
1
I
Configuration Operation
HS-73 #61. Malfunctioned after
276 out of sched. 2350.
Faulty latching - Xport okay.
Quality good. 97 ?1c
00 % successful. Weather
undercast.
100 % successful. Weather
undercast.
Tracker Operation
Malfunction after 11'. Spool
latch interference.
Drift Sight Operation
Cancelled due weather..
Successful.
Clear.
Cancelled due weather.
Successful.
Clear.
Cancelled due weather.
Succe ssf ul.
Mirror fogged and face
glass scratched.
Successful 100 %. Quality poor
Fogging of D/S - (Leaks). ,
due weather.
Successful.
Clear.
Cancelled due weather.
Successful.
Fogging of D/S.
100 %. uccessful. Weather
Successful.
Clear.
undeaast. Quality indeterminate
HS-732 #61 failed to auto-wind.
'Y 7 ?10
Successful.
Successful.
Successful.
Successful.
Succe ssf ul.
S uccessful.
Fogging after going through
clouds at 26, 000.; Disappears
after 2 or 3 hours.
Fogging after going through
clouds. Clears after.
Clear.
Fogged.
Clear.
Fogged.
Clear.
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 5-9-58
5-13-58
5-15-58
16-58
5-17-58
5-18.58
Mission Number
BT-58-61 1352
BT-58-62 1 355
BT-58-63 352
BT-58-65 352
BT-58-66 352
BT-58-68
BT-58-69
BT-58-70
B-1406
B-1407
B-1409
A/C
Config.
& S/N
352
1355
355 B #9
1352 B #9
352 B #6
352 B #9
355 B #2
B #6
351
352
355 A-2 #3 Sanitized Copy Approved for Release 2010/12/13: CIA-RDP74B00752R000100050001-0
Track
S/N
Config.
Footage
12 1 336 cyc
">0 nuaotu:', SUMMARY DETACHMENT
940 cyc I ?No report
5, 826' 400'
4,830' 418'
7, 038' 500'
8,110' 658'
6,000, 931'
Tracker
Footage
Configuration Operation
100 ?Josuccessful. Weather
scattered - broken. 10 %a to
take quality good.
115-732 jam (#12). Blade #1
Undetermi-ned. // o;4
Successful 100 %.
HS-732 (#56) Malfunction
mislatching. 2 s-
100 % successful.
100 % successful.
100 %''euccessful. Mode 1.
100 To..successful. Mode 2.
100 % ,ccessful, Mode 1.
100 uccessful, Mode 1.
100 ?f e ccessful, Mode 2.
Model Film wrapping on
meter roller due failure
tensio ensing switch. S-0 qp'o
100 % successful.
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? No report.
Successful.
Successful.
Successful.
Successful.
Successful.
Successful.
Tracker Operation Drift Sight
Operation
Successful.
S uccessful.
Successful.
Failed to latch after 3861.
Fogging.
Slight fogging.
Clear. (1st flight no fog
this A/C).
Clear.
Clear.
Clear.
Clear.
Clear.
Clear.
Clear.
Clear.
Clear.
Clear.
 5-28-58
5-29-58
5-30-58
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i yjo nun-)iuw Z)U MMARy llr.1AGHMENT .1-..J
Config.
& S/N
Trac;
S/N
Config.
Footage
Tracker Operation
Successful. I Slight frost - upper rim.
Manfunction - Prism cycle switch, Clear.
maladjusted.
Successful. 1 Motor burnedout after 4 1/2 k
loose'f4'iling to take up, causing
film wrap, (Tension Servo).
62 ?
HS-7311
MecM
Failed to operate during portion I Clear.
of flight. No reason found.
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Tracker
Footage
509' ManfujCtion - Spool Gear came
 Sanitized Copy Approved for Release 2010/12/13: CIA-RDP74B00752R000100050001-0
Date
TWX
Mission Number
A/C
Config.
& S/N
Tra d
S/N
Config.
Footage
Tracker
Footage
Conf iguration Operation
Tracker Operation
Drift Sight Operation
6-25-58
2695
B-1419
355
A-2 #4
one
R 1629'
100 % guccessful. Mode I.
No report.
V 1629'
L 1629'
6-27-58
B-1420
355
A-2 #3
None
1500' ea
100 % satisfactory . Condensation
Clear.
V-7 window. Data exposures
poor.
6-29-58
BM-58-13
355
B #6
None
2816'
100 % satisfactory. Quality good.
Clear.
Total
943 cyc.
6-29-58
IB-1421
351
A-2 #4
None
1459' ea
100 % satisfactory
Slight fog top front of bub'
camera
- 3 times.
7-2-58
BT-58-81
351
A-I #5
None
R-2/V-3
Tri Cameras 100 %. Rocker -
Clear.
L-4
film wrap on metering roller -
ea 224 cyc
sheaved pin.
Rocker
I
I
938 cyc
7-8-58
B-1424
352
A-2 #3
12
R-6/V -7
725'
100 % successful.
Successful.
Clear.
L-8
ea 1600'
7-10-58
BT-58-83
355
B #9
7
960' ea
629'
Failur after 960'. Folds and
Successful but double pulse.
Clear.
cassette
tears material. /7 q'
7-10-58
BT-58-84
351
13
566'
Double pulsed Quality good.
Clear.
7-11-58
BT-58-85
355
B #2
7
4934'
490'
100 % uccessful. Modes 1, 2,
Successful.
No report.
1645."cyc
3, 4` }
7-15-58
B-1426
355
B #6
18
67201,
Of
100 % uccessful. Mode 2.
Malfunction. Cause undetermined
No report.
2232 cyc
Quaff fair - weather.
7-16-58
B-1427
355
A-2 #5
19
R-6/1043
731'
V-7 -731 failure blade link
Successful.
No report.
V-7/368
to sht' trip cam pin frozen.
L-8/1043
R-6 -8 okay. 77 z
cycles
7-17-58
B-1428
355
B #6
19
3875/3875
935'
100 % successful. Baffling
Successful.
No report.
feet.
installed. Mode 2.
2590 cyc
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 Sanitized Copy Approved for Release 2010/12/13: CIA-RDP74B00752R000100050001-0
11 .
Configuration Operation
100,uccessful, Mode
(Afirxcr frosted on post flight,
100 % successful, Mode 2.
Best"ireSUlts to date at "BHH -
Bafflee installed.
9L 100'%? 9R failure last 300'
due nt' supply brake kit installed.
9z
Drift Sight Operation
Malfunction , Cause undetermined
Slight fogging, Cleared 2 h
Successful. (Vibration),
100 % successful.
100 % successful.
Successful,
Clear. (power changer
inoperative - loose set screw
on drive gear.
Malfunction. Scan motor
out. No report,
ut,
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 8-7-58 2895 B-1451
8-9-58 2946 BT-58-87
8-11-58 2950 B-1453
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P sg- e A/C overload,
Failure after 50'. Blown fuse - Cloudy driftsite.
o bi
R & L 100 % successful. V-7 Successful.
c
ase drive taper pin in pinion gea
loose.'` Jamming latching arm -
Pop out. c/c
No onerat;nn
PAGE
Failure after 300'. Broken wire I Oily appearance due
in T/TT 1l,...._
% successful, V-7 0 % - I Successful
rive zailure. S/N 98 gear
L-8 48 % mistracked S/N
y9 Vo
7 100 %successful. Successfu
t. stuck metering roller
film wrap. e
HS-732 K-3 Delay. Failure
inter'tJ(?ttent, SIN 16 - failed
Autow nd. Mode 1. 73 54e
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720
R & V 100 % successful.
L- 8 10.,731 failure Cj %
(Lind-N/S 54-2124
 8-20-58 3176 B-1462
8-21-58 3176 B-1464
8-26-58 3269 B-1466
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f V-7 1400, 1
(74%)
L-8 1400'
4681'/4681 1000'
3983'/3983 1000'
4698'/4698 900'
34131/3413'1 200,
2275cyc
177' Trig= 1 750'
ea camera
1800' Roc.
Tracker Operation
V-7 8 100 R-6 Magazine 100 % successful
fled and Ge
neva gear
Jammed; Life cycles 4000'.
R-6 & L-8 100 % successful.
" HS-731 SN 54-2075. Rewind
Sping failed. Life cycles 780
E? C) 71C,
R-6 & t-8 100 % suc
c
essful
Successful.
V-7 HS-
731 SN 54
.
-2708.
Shtr.
trip sp" ring failed. 9/ as
HS-732-',$N 16.
Failed after 3. 3
hrs. 1 Successful.
blade
100 %. ccessful.
100 %` ccessf?t I'Lx
d
o
e
100 %pa tccessful, Mode'2
Excellept to good.
90% HS 732. Lat ch f
a
ajiure alter 200' - Metering
solenoid,
i ure
(#51) (Test n? d 100 % successful.
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t
l R-6 1100' 1000'
V-7 740'
L-8 1100'
PAGE
Frosti:nz on right portion of
bubble. Evidence of windo,
frost on V-7.
Vibration in Drift Sight.
Slight frosting at 36. 5 alt.
Clear.
Heavy oil on windows. Drift!
clear.
No report.
 Date
19-3-58
10-3-58 3907 B-1478 367
10-7-58 3952 B-1480 367
10-23-58 4220 BT-58-89 352
10-24-58 4221 B-1486 352
10-31-58 4324 BT-58-90 349
B-1493
B-1494
B-1495
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12 f
1 ? 12500, 1 425'
L-8 1405'
V-7 1610'
1.) 7622' 1000'
2541 cyc
18 R-61610' 900'
1 7 1 5755'total 1 935'
3837 cyc
tJ
(18 369 r' 1000'
2465 cyc
ched. take - Diode on
100 % successful.
100 % successful. I & 2 Modes.
shorted causing Ckt Bi(r
5reaking pwr to shtr.
ilm wrap on metering
'rh side.' Occurred during
tom Mode 2 to 1. Long
sensing arm.
43 %x4' ode 2- Film wrap meterin
rolls h side. Supply spool
SN 73 .' 80-0-6-6000, 76-8-9-68.
Beari Ys out of alignment.
1100 % successful.
100 %
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Configuration Operation
100 % iccessful. Mode 2 -
Qualityffair. (Pinhole) (Fuzzy).
100 % successful.
100 % successful. I Clear.
R-6 & V-7 100 %. L-8 87 %.
Case Drive failure.
100 % euccessful. Modes 1 & 2.
Resolution fair.
100 % uccessful. Modes I R, 2
100 % successful.
100 % successful.
100 % successful.
100 % successful.
100.% successful.
100 % successful.
100% successful.
100 % successful.
 Sanitized Copy Approved for Release 2010/12/13: CIA-RDP74B00752R000100050001-0
Mission Number
A/C
Config,
& S/N
irac
SIN
Config,
Footage
Tracker
Footage
C nfiguration Operation
11-25.58
4822
BT-58-93
349
2376'
1
456'
100 1*'atisfactory
2376 cyc.
.
12-1-58
4822
BT-58-98
3551
B #6
17
1
2347'
each side
100 % satisfactory.
12-3-58
4522
BT-58-100
12-3-58
4822
B T-58-101
352
12-16-58
5081
BT-58-111
355
A-2 #4
18
1
6
7.5'
each
100 % satisfactory.
yellow f /11.
Mode I
12-23-58
5195
B-1498
352
B #6
13
!
6
954'
1
750-
100% satisfactory
Mode 2
2
385 cyc.
.
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Tracker Operation
Drift Sight Operatic
100 % satisfactory. Clear.
100 %
satisfactory. Clear.
100 % s
atisfactory. Clear.
50 %.
Maladjusted 32 sec Sli
h
g
t fogging after 2 h
;
switch on inter valorneter. from take off.
86 %.
switch.
Malfunction of scan Clear.
Had 35 firs, operation.
100% satisfactory
Poor presentation due
on inner optics.
 3-2-58
C-6011
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A/C
Conf ig.
& S/N
TracId
S/N
Config.
Footage
10
3990' total
3 cameras
44251 total
A-2 #9
10
3 cameras
4800' total
A-2 #9
10
3 cameras
147581 total
?
A-2 #9
10
3 cameras
4860' total
3 cameras
342 1A-2 #9 16 1 4680' total
3 cameras
34Z A-2 #9 10 4000' total
342
A-2 09
16
342
A-2 #9
16
3 cameras
4950' total
3 cameras
3750' total
3, cameras
3600' total
3 cameras
600
%. Quality 30-35
%. Quality 30-35
Quality 30-35
Failed immediately after takeoff.
No cause reported.
Successful 100 %. Slight bubble
fogging.
Stopped for 3 hrs; in middle o
mission, then started again -
Reason unknown,
Successful '100 %.
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Fogging during climbout -
clear after. (New purging
techniques applied on preflight).
Completely fogged for first 3
hrs. - Partially cleared
remainder of flight.
Fogged at high angles.
Slightly fogged at high angles.
Clear.
 Sanitized Copy Approved for Release 2010/12/13: CIA-RDP74B00752R000100050001-0
Mission Number
Config, rac
& SIN S/N
Conf ig.
Footage
Tracker
Footage
Tracker Operation
ter 600, No I Successful.
Fijrn
appaz
low's
V-7
cycl
R-6
1001
view
4-28-58 C-1 42 353 1 B 010
5-7-58 C-1746 342 1 B #10
5-12-58 C-1751 342 B #10
5-10-58 C-1749 342 B #10
5-13-58 C-1752 342 1 B #10
5-16-58 C-1754 342 B #10
5-14-58 -. o C-1753 343 B #10
plun 40 % loss due
HS-7 hing both
dire1
o c"c
Sanitized Copy Approved for Release 2010/12/13: CIA-RDP74B00752R000100050001-0
ul. Stopped after 5 hrs.
ul. Modes I & 2. Successful,
ttent Failure during climbout.
t
Successful.
HS -732 Successful.
9801 Vaeu roughout solenoid ' Successful.
Drift Sight Operation
Clear.
Fogged 5 0 /oat high angle.
Clear.
 Sanitized Copy Approved for Release 2010/12/13: CIA-RDP74B00752R000100050001-0
Tracker
Footage
C -1769 353 A-2 #6 16
C-1763 353 B #8 16
Successful
Successful.
Successful.
Successful.
Successful.
Successful.
Successful.
ul. Quality I Successful.
lam or better.
ul. Quality good. I Successful.
359 IA-1 04.
353 IA'-l #4'
Rocker case
r of. flight.
Superior
to date at C.
C-6013
342
CW-58-5
359
CW-58-6
)359
CT-58-24
1 359
Successful.
Upper 50% fogged.
Upper 50 % fogged.
Fogged for 1st hr., then clear.
Fogged during climbout.
Unusable throughout flight.
Clear.
Slight icing upper 100 %.
Clear.
Black smudge center . Icing~
Clear.
Clear,
I Clear.
Clear.
Minor fogging first hour..
Minor fogging first hour.
Sanitized Copy Approved for Release 2010/12/13: CIA-RDP74B00752R000100050001-0
 9-10-58
9-25-58
9-30-58
10-14-58
10-22-58
5540
C-6019
5688
C-1779
5720
CT-58-33
5873
CT-58-34
6003
C-6023
Sanitized Copy Approved for Release 2010/12/13: CIA-RDP74B00752R000100050001-0
Trac
S/N
Sanitized Copy Approved for Release 2010/12/13: CIA-RDP74B00752R000100050001-0
i racker Operation Drift Sight Operation
Successful. Minor fogging first hour.
Failure after 100' ? Minor fogging first hour.
25 % accomplished, cause Clear.
ul:known.
100 % successful.
100 % successful.
100 % successful.
For-ard 30 % iced during
climbout.
100 % successful. (Note: Abrasio Clear.
mark on back side of film entire
length - due manufacture.
Clear - R/C stiff.
qo report.
No report.