S 034-008
(8)
Remove the transducer from the bracket.
TASK 31-31-09-404-009
3. Install the Control Wheel Position Transducer (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
(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 AlliedSignal Inc., DBA AlliedSignal 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-0005-001, Adapter Cable - MADU
B. References
(1)
AMM 20-10-23/401, Lockwires
(2)
AMM 24-22-00/201, Electrical Power Control
GUN 001-008, 010, 101 POST-EO B531006; ú 31-31-09
GUN 051, 102-999 ú ú 10 Page 403 ú Jan 28/02
A
757 MAINTENANCE MANUAL
C. Procedure
S 434-010
(1)
Install the transducer into the bracket with the EZ mark on the transducer housing aligned with mark on the bracket.
S 434-011
(2)
Install and tighten the mounting screw to the bracket.
S 434-012
(3)
Install the crank arm into the transducer shaft.
S 864-013
(4)
Align the crank arm slot with the index mark on the transducer's serrated shaft.
S 434-014
(5)
Install and tighten the mounting screw to the crank arm.
S 434-015
(6)
Connect the electrical connector to the transducer.
S 034-016
(7)
Remove the rig beam from the control wheel.
