PREFLIGHT INSPECTION

• Document Type: CREST
• Collection: General CIA Records
• Document Number (FOIA) /ESDN (CREST): CIA-RDP89B00551R000200080033-5
• Release Decision: RIPPUB
• Original Classification: K
• Document Page Count: 12
• Document Creation Date: November 17, 2016
• Document Release Date: December 13, 1999
• Sequence Number: 33
• Publication Date: February 10, 1957
• Content Type: FORM

Approved -For Relee 2000/04/18: CIA-RDP89B001 R02M80033-5
Plastic nose & windc-!Ts i're', o cracks & secure,
fy
2. ARK/6 boot for cor.r'_it. on &. cl o~,nd, ARN/6 and compass secure.G
Brake fluid for pNopev l(,trel Ri -a.p scc~~._ e,
Pitot clean & secure, c.'i ck A r.,._'P"w:).
.5'2
? ,`CH ? 114,-
Nose section clean & OK to ul Est pana:i.n
8, All items cleared
open,
1,.'Static holes all,
C opZ external handle secure.
.;3
Lower antenna secure,
Windshield & canopy glass cleanliness & condition.
5, All items cleared.
COCKPIT,
CREW CHIC :
9-1
I '
'A 020
2, . Canopy emerency release handle locked & safe tie
- capper wire .
Caoyforproper latching with aft hatch installed
Cano ,,Yseal & connection for. condition "
Brakes for solid feel.
Rudder pedals for freedom & operation of ad:iustmen
7. elevator for operation &f reedom.
W1O ~ ~-' aA- ~JP89Bd05 04A A8A~0
C Aileron for operation &P reedom,
Js El$vator tab for operation & direct. on, " Tlo
is Canopy antenna: connection secure
 Approved For Re se, 2000/04/18 CIA-RDP89B0 1.R000200080033-5
l ottae'for operation & fricticn look,
COCKP T IIiTZ'~RNM.: (Continu'xi)
-i~ri IYI I~i~l!
1.2. tf.H,F.
rag in map case,
14. Tnstruinents for condition & clocza:ness.
15. Autopilot:
a,- Power one
b, Inverter ono
After 3 minutes turn autopilot on. (Stick should not
'move f ore or aft.)
'.~CH~ I..,;cF e
Check roll trim knob $or operation. vvnt e.. 011VU-L%A ~
, ? -3- A4 -+A^" l
.
Check yaw trim knob for operation.
f. Check pitch trim knob for operation.
Check turn knob for operation.
Overpower autopilot in all three axes. (Stick arx
1P J7
21. Seat for condition & operation.
22, Interior iignts
'24. All items cleared. CF.. ~~ s . ,+`=f
pedals sh
Center yaw and`roll trim knobs.
Inverter off.
Power off.
16,LLCircuit breakers set or into white line.
17. Seat bolt & shoulder straps for condition & operation.
1$. Oxygen system checked out., system pressure 1300-2000# cap
installed, check out face heat.
19, Warning lights .for operation.
2O, Emergency battery for operation) check voltage with
precision meter,
Approved or release 2000/04/18: C1A-RDP89B00551 R000200080033-5
 Approved For Rele 2000/04/18 CIA-RDP89B00 R0'00200080033-5.
QUI NT DAY
. Peacan drained, flushed & valve closed.
2R Cockpit regulato'rs' fore cleanliness & condition.
3. Control cables for freedom, operation & turnbarrels safetie
. 2
_
~. E ui ent f or security in hatch & ba
~. Lower hatch & seal for operation & condition of latching
-m - h .ni.sm,
6. 'OIL to install lower hatch.
7. Lower hatch installed, latched and safetied,
8. Check HF radio equipment for* security.
,, Upper hatch latching mechanism for opeittions.
10. Pressure regulator safetied in fli ht position.
to install upper hatch
ll. OK
..w. .A-YM~?W`- ?ri~?YWM
IP
. User hatch installed, latched & safetied.
13, All items cleared.
1, Heat exch anger duct connections for security'.
Zz Check for ~lumbin g or anything ridi structure
.
OK to close acces door
Access door closed & secure,
4.
-
All items cleared. CHftEGT CHIT :
'ENG AIR DUCTS ?
------ -
1 R/H &L/H main ducts for cracks & cleanliness,
2 R oil cooler duct for cracks & cleanliness.
Check inlet aide vanes compressor rotor & stator blades
-
'
`
evidence that the engine has in
other
for, dents, nicks or
Bested foreign material.
screens removed.
4- Run UP
cleared. C MIT j C' Tr'; ;
All items c
Approved For Release .2000/04/18 CIA-RDP89B00551 R000200080033-5
 Approved For Redse -2000/04/18 : CIA-RDP89B01 R000200080033-5
"~ R/H wanor coin tyo.z & co_rPr__p;~'.t.~.~
R aileron & tab for securit & cm4J.t nn,,_--~~~
Fr
3. t/H fl