22-11-00
ú ú 08 Page 565 ú Mar 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 865-031
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 745-094
(2)
Push the LSK adjacent to <CWS from the Rigging Tests Index.
S 745-095
(3)
Push the LSK adjacent to <PITCH CWS.
S 745-096
(4)
During this test, follow the instructions and push the LSK adjacent to <CONTINUE as shown on the CDU display.
S 745-057
(5)
Make sure that the values for the A and B side are in the limits shown below or in the CDU display.
NOTE: Do not apply force to column for the Tests 55.01 thru 55.03.
____
Test 55.01 PCWS SENSORS RIGGING Limits: -0.20 to 0.20
(VAC)
Test 55.02 PCWS SENSOR (VAC) Limits: -0.20 to 0.20
Test 55.03 PCWS SENSOR (VAC) Limits: -0.20 to 0.20
NOTE: Apply force at the center of the control wheel hub,
____ perpendicular to the axis of the control column. Apply force to the NOM value as shown on the CDU display.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITHOUT EFIS ú
22-11-00
ú ú 11 Page 566 ú Mar 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 745-103
(6) Push the LSK adjacent to <CONTINUE to go back to the Rigging Tests Index.
J. Roll Control Wheel Steering Test
S 865-058 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).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITHOUT EFIS ú
22-11-00
ú ú 12 Page 567 ú Mar 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
S 745-059
(2)
Push the LSK adjacent to <CWS from the Rigging Tests Index.
S 745-060
(3)
Push the LSK adjacent to <ROLL CWS.
S 745-061
(4)
During this test, follow the instructions and push the LSK adjacent to <CONTINUE as shown on the CDU display.
S 745-065
(5)
Make sure that the values for the A and B sides are in the limits shown on below or on the CDU display.
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 745-063
(6) 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.
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