(10) Push the LSK adjacent to <CONTINUE to get back to the Rigging Tests Index.
F. Aileron Rigging Tests
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITHOUT EFIS ú
22-11-00
ú ú 12 Page 560 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 865-028 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 745-079
(2)
Push the LSK adjacent to AILERON> from the Rigging Tests Index. S 745-078
(3)
During this test, follow the instructions and push the LSK adjacent to <CONTINUE as shown on the CDU display.
S 745-080
(4)
Make sure that the values for the A and B sides are in the limits shown below or on the CDU display.
S 745-081
(5)
Do the aileron sensors check: Test 52.01 AIL LVDT (VAC) Limits: -0.08 to 0.08 Test 52.02 AIL POS (VAC) Limits: -0.06 to 0.06 The Aileron Index Mark must align with the wing index in
|0.06 inch. Test 52.03 AIL LVDT (VAC) Limits: 4.90 to 5.10 Test 52.04 AIL POS (VAC) Limits: 1.60 to 2.25 The RIGHT Aileron Index Mark must be 1.00 |0.10 inches above
the wing index. The LEFT Aileron Index Mark must be 1.00 |0.10 below the wing index. Test 52.05 AIL LVDT (VAC) Limits: -5.10 to -4.90
Test 52.06 AIL POS (VAC) Limits: -2.25 to -1.60 Multiply the A and B Aileron positon shown on the CDU display by 2.716. Record the results.
The LEFT Aileron Index Mark must be 1.00 |0.10 inches above the the wing index. The RIGHT Aileron Index Mark must be 1.00 |0.10 below the wing index.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITHOUT EFIS ú
22-11-00
ú ú 13 Page 561 ú Mar 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 745-125
(6) Do the aileron authority check: Test 52.07 AIL POS (DEG) Add the A and B Aileron position from the Test 52.07 to the
recorded values of the Test 52.06. Record the results.
The limit of the results must be between 0 and 1 degree.
Test 52.08 AIL POS (DEG) Limits: -1.15 to 1.15
Test 52.09 AIL POS (DEG)
Add the A and B Aileron position from the Test 52.09 to the
recorded values of the Test 52.06. Record the results.
The limit of the results must be between 0 and 1 degree.
Test 52.10 AIL POS (DEG) Limits: -1.15 to 1.15 Test 52.11 AIL LVDT (VAC) Limits: -0.08 to 0.08 Test 52.12 AIL POS (VAC) Limits: -0.06 to 0.06 Test 52.13 AIL POS (VAC) Limits: -0.06 to 0.06 Test 52.14 AIL POS (VAC) Limits: -0.06 to 0.06 Test 52.15 AIL POS (VAC) Limits: -0.06 to 0.06 Test 52.16 AIL POS (DEG) Limits: -1.00 to 1.00 Test 52.17 AIL POS (DEG) Limits: -1.00 to 1.00
S 745-083
(7)
Do the aileron force limiter check: Test 52.18 AIL POS (VAC) Limits: -2.03 to -1.42 Test 52.19 AIL POS (VAC) Limits: -2.82 to -2.23 Test 52.20 AIL POS (VAC) Limits: -0.20 to 0.20
S 745-085
(8)
Push the LSK adjacent to <CONTINUE to get out of the Rigging Tests Index.
G. Flaps Rigging Test
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITHOUT EFIS ú
22-11-00
ú ú 09 Page 562 ú Nov 15/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
S 865-029
WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：737-300 400 500 AMM 飞机维护手册 自动飞行 AUTOFLIGHT 1(71)
