E. Procedure
S 034-006
(1)
Disconnect the control column position transducer electrical connector.
S 034-007
(2)
Remove the screw from the crank arm assembly that holds the serrated shaft of the transducer.
S 034-008
(3)
Remove the screw from the collar bracket that holds the transducer in position.
S 024-009
(4)
Remove the transducer from the collar bracket.
TASK 31-31-08-404-034
3. Control Column Position Transducer Installation (Fig. 401)_______________________________________________
A. Equipment
(1) 981-6301-002 Data Signal Display Unit (DSDU)
Alliedsignal Air Transport Avionics
P.O. BOX 97001
15001 NE 36TH ST
Redmond, WA 98073-9701
GUN 001-008, 010, 101 POST-EO B531006; ú 31-31-08
GUN 051, 102-999 ú ú 13 Page 403 ú Sep 28/01
A
757
MAINTENANCE MANUAL
(2)
A31007-49 Adapter Cable - Tester (recommended)
A31007-30 Adapter Cable - Tester (alternative)
(3)
Portable Tester - Teledyne P/N 2222786
Teledyne Controls
12333 West Olympic Boulevard West
Los Angeles, CA 90064
(4)
A31007-1 Adapter Cable - Tester
(5)
Portable Tester - Teledyne P/N 2229738-1
Teledyne Controls
12333 West Olympic Boulevard West
Los Angeles, CA 90064
(6)
A31007-59 Adapter Cable - Tester
(7)
964-0446-001 Hand Held Download Unit (HHDLU)
27914 Allied-Signal Inc., DBA Allied-Signal Aerospace
2100 Northwest 62nd Street
Fort Lauderdale, FL 33309
(a) AIRPLANES WITH FDR P/N 980-4700-042;
The HHDLU must have mod 1 completed.
(8)
704-2567-001 Adapter Cable - Tester
(9)
Multi-Purpose AIDS Display Units - AACO Inc.
FAA-0032-001
AACO Inc.
5011 Barton Place
Seattle, WA 98118
(10)
EGA-005-001, Adapter Cable - MADU
B. References
(1)
AMM 20-10-23/401, Lockwire
(2)
AMM 20-10-24/201, Rig Pins
(3)
AMM 24-22-00/201, Eletrical Power Control
(4)
AMM 29-11-00/201, Main (Left, Right, and Center) Hydraulic Systems
C. Access
(1) Location Zone
113 Area forward of NLG wheel well (left)
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