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ú ú 08 Page 558 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
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: 4.80 to 5.00 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: -5.00 to -4.80
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.
S 745-141
(6) Do the aileron authority check:
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú
22-11-01
ú ú 08 Page 559 ú Nov 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
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 745-085
(7) Push the LSK adjacent to <CONTINUE to get out of the Rigging Tests Index.
G. Flaps Rigging Test
S 865-029 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 745-086
(2)
Push the LSK adjacent to <FLAPS from the Rigging Tests Index.
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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737-300/400/500MAINTENANCE MANUAL
S 745-171
(3)
During this test, follow the instructions and push the LSK adjacent to <CONTINUE as shown on the CDU display.
S 745-172
(4)
Make sure that the values for the A and B sides are in the limits shown on the CDU or in this section.
Test 53.01 FLAP POS (DEG) Limits: 315 (-45) to 8 degrees (0 units)
Test 53.02 FLAP POS (DEG) Limits: 26 to 42 degrees (1 unit)
Test 53.03 FLAP POS (DEG) Limits: 71 to 84 degrees (2 units)
Test 53.04 FLAP POS (DEG) Limits: 105 to 122 degrees (5 units)
Test 53.05 FLAP POS (DEG) Limits: 146 to 159 degrees (10 units)
Test 53.06 FLAP POS (DEG) Limits: 171 to 193 degrees (15 units)
Test 53.07 FLAP POS (DEG) Limits: 199 to 219 degrees (25 units)
Test 53.08 FLAP POS (DEG) Limits: 234 to 246 degrees (30 units)
Test 53.09 FLAP POS (DEG) Limits: 266 to 315 degrees (40 units)
S 745-089
(5) Push the LSK adjacent to <CONTINUE to go back to the Rigging Tests Index.
H. Stabilizer Rigging Test
S 865-030
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