22-11-01
 ú ú 07 Page 564 ú Nov 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 Test 55.04 PCWS FORCE (LBS) Limits: 2.5 to 7.0 Test 55.05 PCWS FORCE (LBS) Limits: 17 to 25 Test 55.06 PCWS SENSOR (LBS) Limits: 21 to 29 Test 55.07 PCWS FORCE (LBS) Limits: 2.5 to 7.0 Test 55.08 PCWS FORCE (LBS) Limits: 17 to 25 Test 55.09 PCWS SENSOR (LBS) Limits: 21 to 29 Test 55.10 PCWS FORCE (LBS) Limits: 2.5 to 7.0 Test 55.11 PCWS FORCE (LBS) Limits: 17 to 25 Test 55.12 PCWS SENSOR (LBS) Limits: 21 to 29 Test 55.13 PCWS FORCE (LBS) Limits: 2.5 to 7.0 Test 55.14 PCWS FORCE (LBS) Limits: 17 to 25 Test 55.15 PCWS SENSOR (LBS) Limits: 21 to 29
 S 745-144
 (6)  Push the LSK adjacent to <CONTINUE to go back to the Rigging Tests Index.
 J.  Roll Control Wheel Steering Rigging Test
 S 865-035 WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
_______ SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER. AILERONS, RUDDER, ELEVATORS, FLAPS, SLATS, SPOILERS, LANDING GEAR, AND THRUST REVERSERS CAN MOVE QUICKLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (1)  
Supply hydraulic power (AMM 29-15-00/201).
 S 745-145

 (2)  
Push the LSK adjacent to <CWS from the Rigging Tests Index. S 745-189

 (3)  
Push the LSK adjacent to <CONTINUE.
 S 745-146

 (4)  
Push the LSK adjacent to <ROLL CWS.
 S 485-151

 (5)  
Install the control wheel steering torque wrench adaptor.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú

 22-11-01
 ú ú 09 Page 565 ú Nov 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 S 745-147
 (6)  
During this test, follow the instructions and push the LSK adjacent to <CONTINUE as shown on the CDU display.

 S 745-148

 (7)  
Make sure that the values for the A and B sides are in the limits shown on the CDU or in this section.

 Test 55.30 RCWS SENSOR (VAC) Limits: -0.15 to 0.15
 NOTE: Do not apply force to the torque wrench for the Test 55.30.
____
 Test 55.31 RCWS FORCE (IN-LBS) Limits: 12 to 24
 Test 55.32 RCWS FORCE (IN-LBS) Limits: 60 to 100
 Test 55.33 RCWS FORCE (IN-LBS) Limits: 12 to 24
 Test 55.34 RCWS FORCE (IN-LBS) Limits: 60 to 100
 S 745-149
 (8)  Push the LSK adjacent to <CONTINUE to go back to the Rigging Tests Index.
 K. Mach Trim Rigging Test
 S 865-039
 WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
_______ SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER. AILERONS, RUDDER, ELEVATORS, FLAPS, SLATS, SPOILERS, LANDING GEAR, AND THRUST REVERSERS CAN MOVE QUICKLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (1)  
Supply hydraulic power (AMM 29-15-00/201).

 S 745-178

 (2)
Push the LSK adjacent to MACH TRIM> from the Rigging Tests Index.

 S 745-115

 (3)  
During this test, follow the instructions and push the LSK adjacent to <CONTINUE as shown on the CDU display.

 S 745-116

 (4)  
Make sure that the values for the A and B sides are in the limits shown on the CDU or in this section.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú

 22-11-01
 ú ú 08 Page 566 ú Nov 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
 Test 57.01 Test 57.02 Test 57.03 Test 57.04 Test 57.05 Test 57.06 Test 57.07
S 745-194
A 737-300/400/500MAINTENANCE MANUAL
STAB POS (VAC)  Limits:  -0.07 to 0.07
MT ACT POS (VAC)  Limits:  -0.10 to 0.10
ELEV POS (VAC)  Limits:  -0.54 to -0.42
RETRACTION (SEC)  Limits:  10 to 25
-SURF DELTA (DEG)  Limits:  3.81 to 4.65
EXTENTION (SEC)  Limits:  10 to 25
ELEV POS (VAC)  Limits:  -0.54 to -0.42
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 自動飛行 AUTOFLIGHT 1(145)