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时间:2011-04-01 08:39来源:蓝天飞行翻译 作者:航空
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_______ 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.

 S 745-087

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

 S 745-088

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


 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)
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITHOUT EFIS ú

 22-11-00
 ú ú 13 Page 563 ú Mar 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 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
 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 745-090

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

 S 745-091

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

 S 745-092

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


 Test 54.01 STAB POS (VAC) Limits: -0.07 to 0.07
 Measure the stabilizer B dimension with the trammel bar or steel measurement tape (Fig. 503).
 Test 54.02 STAB POS (VAC) Limits: -1.93 to -1.43
 When the STAB is stable, measure the stabilizer B dimension with the trammel bar or steel measurement tape (Fig. 503). The limits must be between 45.39 and 45.75 inches.
 Test 54.03 STAB POS (VAC) Limits: 6.30 to 7.60
 When the STAB is stable, measure the stabilizer B dimension with the trammel bar or steel measurement tape (Fig. 503). The limits must be between 25.65 to 25.85 inches.
 S 745-093
 (5)  Push the LSK adjacent to <CONTINUE to go back to the Rigging Tests Index.
 I. Pitch Control Wheel Steering Rigging Test
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITHOUT EFIS ú

 22-11-00
 ú ú 12 Page 564 ú Mar 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
SEE A
UPPER STOP
LOWER STOP
"B" ACTUATOR DIMENSION TRAMMEL BAR
1
FWD
A
1 THE "B" DIMENSION IS MEASURED BETWEEN THE CENTER OF THE UPPER AND LOWER GIMBAL PINS
Stabilizer Trim "B" Dimension Location Figure 503
E84053
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITHOUT EFIS ú
 
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