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RUD ON’ LIGHT ON THE P5-3 PANEL (Continued)
TASK 27-00-00-040-811
19. MMEL 27-21 (DDPG) Restoration - STBY RUD ON Light Inoperative
A. General
(1) This task puts the airplane back to its usual condition after operation with the STBY RUD ON
indicator light inoperative (illuminated).
(2) The STBY RUD ON indicator light is located on the P5-3 overhead panel.
B. References
Reference Title
27-21-00-840-801 Put the Rudder Hydraulic systems A, B, and Standby Back to the
Condition Before the Pressurization (P/B 201)
27-62-00-800-801 Speed Brake Hydraulic Systems A and B Pressurization (P/B 201)
32-09-00-860-801 Put the Airplane in the Air Mode (P/B 201)
32-09-00-860-802 Return the Airplane to the Ground Mode (P/B 201)
C. Location Zones
Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
325 Vertical Fin - Rudder
D. Procedure
SUBTASK 27-00-00-860-040
(1) Remove the safety tag and close this circuit breaker:
F/O Electrical System Panel, P6-2
Row Col Number Name
D 15 C01628 FLIGHT CONTROL FORCE FIGHT MONITOR
SUBTASK 27-00-00-860-041
WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER. AILERONS, RUDDERS,
ELEVATORS, FLAPS, SLATS, SPOILERS, LANDING GEAR, AND THRUST REVERSERS
CAN MOVE QUICKLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE
INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(2) Pressurize the speed brake hydraulic systems A and B. To pressurize them, do this task: Speed
Brake Hydraulic Systems A and B Pressurization, TASK 27-62-00-800-801.
SUBTASK 27-00-00-810-007
(3) Do a check of the STBY RUD ON light:
(a) Set the FLT CONTROL A and B switches on the P5-3 panel to the ON positions.
(b) Do this task: Put the Airplane in the Air Mode, TASK 32-09-00-860-801.
(c) Move the flap control lever to the 1-unit detent position.
(d) Make sure that the STBY RUD ON light is not illuminated.
(e) Set the FLT CONTROL A switch on the P5-3 panel to the STDBY RUD position.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-00-00
Page 926
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
GUN 006-099, 101-122; GUN 001-005, 155-157, 201-999 POST SB 737-27-1253; AIRPLANES WITH ’STBY
RUD ON’ LIGHT ON THE P5-3 PANEL (Continued)
(f) Make sure that the STBY RUD ON light is illuminated.
(g) Set the FLT CONTROL A switch on the P5-3 panel to the OFF position.
(h) Make sure that the STBY RUD ON light is not illuminated.
(i) Set the FLT CONTROL B switch on the P5-3 panel to the STDBY RUD position.
(j) Make sure that the STBY RUD ON light is illuminated.
(k) Set the FLT CONTROL B switch on the P5-3 panel to the OFF position.
(l) Make sure that the STBY RUD ON light is not illuminated.
(m) Set the FLT CONTROL A and B switches on the P5-3 panel to the ON positions.
(n) Make sure that the STBY RUD ON light is not illuminated.
(o) Move the flap control lever to the UP detent position.
(p) Do this task: Return the Airplane to the Ground Mode, TASK 32-09-00-860-802.
(q) Do this task: Put the Rudder Hydraulic systems A, B, and Standby Back to the Condition
Before the Pressurization, TASK 27-21-00-840-801.
SUBTASK 27-00-00-930-021
(4) Remove the INDICATOR INOP placard from the STBY RUD ON indicator on the P5-3 panel.
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-00-00
Page 927
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
FLIGHT CONTROLS CABLES - MAINTENANCE PRACTICES
1. General
A. This procedure has these tasks:
(1) The identification and assembly specifications of the control cable
(2) The rigging of the control cables.
TASK 27-09-14-860-801
2. Control Cables Identification and Assembly Specifications
A. References
Reference Title
20-10-91-000-801 Control Cables Removal (P/B 401)
20-10-91-400-801 Control Cables Installation (P/B 401)
27-11-00-700-804 Control Wheel Centering Check (P/B 501)
27-11-00-700-805 Aileron Control Wheel Force Test (P/B 501)
27-11-00-700-809 Aileron Travel Test (P/B 501)
27-11-00-730-801 Aileron Trim Response Test (P/B 501)
27-11-00-820-801 Aileron Cables Adjustment (P/B 501)
27-21-00-700-815-001 Rudder Centering Test (P/B 501)
27-21-00-700-815-002 Rudder Centering Test (P/B 501)
27-21-00-700-816-001 Rudder Pedal Forces Test (P/B 501)
27-21-00-700-816-002 Rudder Pedal Forces Test (P/B 501)
　
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