(2)
The A/T BITE test will make sure the PLA synchro rigging is correctly done.
B. References
(1)
AIRPLANES WITHOUT EFIS; AMM 22-04-00/101, Autothrottle System - Built-In Test
(2)
AIRPLANES WITH EFIS; AMM 22-04-10/101, Autothrottle System - Built-In Test
(3)
AMM 24-22-00/201, Manual Control
(4)
AMM 32-00-01/201, Ground Lock Assemblies
(5)
AIRPLANES WITHOUT EFIS;
AMM 34-28-00/201, Inertial Reference System
(6)
AIRPLANES WITH EFIS;
AMM 34-28-01/201, Inertial Reference System
(7)
AMM 71-11-02/201, Fan Cowl Panels
C. Access
(1)
Location Zone
502 Engine No. 1 - 7:00 o'clock position
602 Engine No. 2 - 7:00 o'clock position
(2)
Access
5746L Engine No. 1 - Left Fan Cowl Panel
5846R Engine No. 2 - Left Fan Cowl Panel
D. Prepare for The Autothrottle BITE test
S 865-002
(1)
Make sure the engines are off.
(2)
Make sure the landing gear lever is in the DOWN position.
S 865-003
S 865-036
WARNING: YOU MUST CAREFULLY INSTALL THE GROUND LOCKS IN ALL LANDING
_______ GEAR. AN ACCIDENTAL RETRACTION OF THE LANDING GEAR CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(3)
Install the ground locks in all landing gear (AMM 32-00-01/201).
S 865-004
(4)
Make sure that you turn the BAT switch on the Pilots' forward overhead panel to ON.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
22-31-11
ALL ú ú 02 Page 501 ú Nov 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
POWER LEVER ANGLE SYNCHROS (LEFT SIDE OF ENGINES)
SEE A
THRUST
CONTROL
RIG CABLE
SEE B PIN
1
A PART POWER
RIG HOLE MEC FUEL CONTROL BOX
RP
PLA SYNCHRO MOUNTING BOLTS
1 737-300 AIRPLANES WITH A/T CMPTR 10-62017-1 THRU 10-62017-5;ONE RIG PIN IS REQUIRED: F70207-23, POWER LEVEROR MS20392-3C, OR EQUIVALENT ANGLE SYNCHRO0.248 (+0.000/-0.002)-INCH DIAMETER, 3 INCH LONG ROD OR BOLT. 737-300 AIRPLANES WITH A/T CMPTR 10-62017-11 AND SUBSEQUENT, B 737-400, AND 737-500; RIG PIN IS NOT REQUIRED FOR ADJUSTMENT.
Autothrottle Power Lever Angle Synchro Adjustment Figure 501
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22-31-11
ALL ú ú 01 Page 502 ú Nov 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
S 865-005
(5) Make sure the STANDBY POWER switch on the Pilots' forward overhead panel is in the AUTO position.
S 865-006
(6) Supply the electrical power (AMM 24-22-00/201).
S 865-009
(7) Push and hold the master dim and test switch on pilots' center instrument panel to the TEST position to make sure these lights work properly: (a) Pilots Panel Lights (b) Indicator lights (c) Annunciator lights
S 865-030
(8) Close these circuits breakers on the P6-1 circuit breaker panel: (a) NO. 2 AIR DATA - COMPUTER-2 - 26VAC (b) NO. 2 AIR DATA - COMPUTER-2 - AC (c) NO. 2 INSTRUMENTS - DAA NO. 2 - FMC AC (d) NO. 2 INSTRUMENTS - DAA NO. 2 - IRS AC (e) NO. 2 INSTRUMENTS - DAA NO. 2 - DC (f) NO. 2 INSTRUMENTS - IRS NO. 2 - AC (g) NO. 2 INSTRUMENTS - IRS NO. 2 - DC (h) NO. 2 INSTRUMENTS - DAA FMC NO. 2 (i) AIRPLANES WITH EFIS; NO. 2 INSTRUMENTS - EFIS - SYM GEN R
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