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(h) Installation of replacement bushings on the aileron balance tab front spar hinge nearest the
tab control rods.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-11-00
Page 573
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(i) Installation of replacement tab control rods.
NOTE: For each aileron tab, if both control rods are adjusted, then flight test is
necessary.
If only one rod is adjusted, and you can verify that the remaining rod had not been
replaced or adjusted since the last flight test, then flight test is not necessary.
If only one rod is adjusted, and you can not verify that the remaining rod had not
been replaced or adjusted since the last flight test, then flight test is necessary.
(j) Installation of the original tab control rods if you changed the adjusted lengths of the tab
control rods.
(k) Installation of the original tab control rods if you also removed the aileron and/or aileron
balance tab from the airplane.
B. References
Reference Title
27-09-71-820-802 Aileron Balance Tab Adjustment to Equalize Lateral Manual
Reversion Forces (P/B 501)
27-21-00-820-810-001 Control Rod for Standby Rudder Power Control Unit Adjustment
(P/B 501)
27-21-00-820-810-002 Control Rod for Standby Rudder Power Control Unit Adjustment
(P/B 501)
C. Tools/Equipment
NOTE: When more than one tool part number is listed under the same "Reference" number, the
tools shown are alternates to each other within the same airplane series. Tool part numbers
that are replaced or non-procurable are preceded by "Opt:", which stands for Optional.
Reference Description
COM-1557 Gauge - Force
(Part #: DG-200, Supplier: 92456, A/P Effectivity: 737-ALL)
(Part #: DPP-500G, Supplier: 92456, A/P Effectivity: 737-ALL)
(Part #: DPPH-150, Supplier: 92456, A/P Effectivity: 737-ALL)
(Part #: DPPH-50, Supplier: 92456, A/P Effectivity: 737-ALL)
(Part #: FDIX 100, Supplier: 0BFD9, A/P Effectivity: 737-ALL)
(Part #: FDIX 50, Supplier: 0BFD9, A/P Effectivity: 737-ALL)
(Part #: FDV 50, Supplier: 0BFD9, A/P Effectivity: 737-ALL)
(Opt Part #: FDI 100, Supplier: 0BFD9, A/P Effectivity: 737-ALL)
D. Location Zones
Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
572 Left Wing - Aileron
672 Right Wing - Aileron
E. Prepare for the Test
SUBTASK 27-11-00-820-019
(1) Adjust the applicable system or systems before the flight test if you get these conditions:
(a) The aileron trim is more than 3/4 unit at cruise, 3/4 unit at 250 knots, or more than 1 unit
other than cruise flight configuration.
(b) The rudder trim is more than 1/2 unit at cruise, 3/4 units at 250 knots, or 1 unit other than
cruise configuration.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-11-00
Page 574
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
SUBTASK 27-11-00-210-006
(2) Make sure the airspeed is 250 knots.
SUBTASK 27-11-00-860-070
(3) Make sure the flight altitude is 10,000 to 17,000 feet.
SUBTASK 27-11-00-860-071
(4) Make sure the aileron trim is not more than 3/4 unit at cruise or 3/4 unit at 250 knots.
SUBTASK 27-11-00-860-072
(5) Make sure the rudder trim is not more than 1/2 unit at cruise or 3/4 unit at 250 knots.
SUBTASK 27-11-00-860-073
(6) Make sure the flaps are up.
SUBTASK 27-11-00-860-074
(7) Make sure all persons are seated.
F. Procedure
SUBTASK 27-11-00-860-075
(1) Move the control wheel to the neutral position.
SUBTASK 27-11-00-860-076
(2) Set the SPOILER A and B switches to OFF.
SUBTASK 27-11-00-860-077
(3) Make sure that the FLT CONTROL A and FLT CONTROL B switches are ON.
SUBTASK 27-11-00-860-078
(4) Set the FLT CONTROL A switch to OFF.
NOTE: The airplane may pitch up or down during transition.
SUBTASK 27-11-00-860-079
(5) Carefully move the elevators, ailerons, and rudder.
(a) Make sure that the control forces and operation do not change.
SUBTASK 27-11-00-860-080
(6) Set the FLT CONTROL A switch to ON.
SUBTASK 27-11-00-860-081
(7) Set the FLT CONTROL B switch to OFF.
NOTE: The airplane may pitch up or down during transition.
SUBTASK 27-11-00-860-082
(8) Carefully move the elevators, ailerons, and rudder.
(a) Make sure that the control forces and operation do not change.
SUBTASK 27-11-00-860-083
(9) Set the FLT CONTROL B switch to STBY RUD.
SUBTASK 27-11-00-860-084
(10) Set the FLT CONTROL A switch to OFF.
　
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