B.
Access
(1)
Location Zone
101, 102 Control Cabin
C.
Procedure
S 226-002
(1)
Examine the latch lug on the speed brake lever (Fig. 601):
(a)
Lift the speed brake lever out of the detent.
(b)
Measure the detent latch lug.
(c)
Repair or replace the speed brake lever if the latch lug is not in the tolerance shown in Fig. 601.
(d)
Put the speed brake lever in the detent.
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A
737-300/400/500MAINTENANCE MANUAL
PILOTS'
SPEED CONTROL STAND
SEE
LATCH LUG
NO. INDEX PART NAME DIM. DESIGN LIMITS WEAR LIMITS WORN PART REPLACE PART WORN REPAIR INSTR. REPAIR
DIAMETER MITTED PER-DIM. WEAR DIA. MAX ANCE CLEAR-
MIN MAX
1 DETENT LATCH LUG OD 0.235 0.265 0.210 X 1
THE MAXIMUM PERMITTED WEAR IS 0.04 INCH. REFER TO THE OVERHAUL MANUAL FOR REPAIR INFORMATION.
Speed Brake Lever Wear Limits
Figure 601
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A
737-300/400/500MAINTENANCE MANUAL
ENGINE THROTTLE SWITCHES - REMOVAL/INSTALLATION
_______________________________________________
1. General_______
A. There are two tasks in this procedure. There is a task for the removal and a task for the installation of the engine throttle switches. The engine throttle switches are installed on the autothrottle clutch supports in the ceiling of the electronic compartment.
B. The M1639 (Engine 1) and M1640 (Engine 2) engine throttle switches are S1 through S5.
C. You use the angular dimensions at the thrust levers to adjust the engine throttle switches.
TASK 27-62-04-004-001
2. Engine Throttle Switch Removal______________________________
A. Access
(1)
Location Zone
205 Electronic Compartment
B.
Procedure
S 864-002
(1)
Open these circuit breakers and attach DO-NOT-CLOSE tags:
(a)
P6 Panel
1) AUTO SPEED BRAKE
2) AURAL WARN
3) AUTO BRAKES CONT
4) ENGINE 1 SYNC LOCK
S 024-003
(2)
Remove the applicable engine throttle switch:
(a)
Disconnect the electrical wires from the terminals on the switch.
(b)
Remove the S1 - S4 switches (Fig. 401): 1) Remove the cotter pin from the drilled straight pin. 2) Remove the drilled straight pin. 3) Remove the switch.
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A 737-300/400/500MAINTENANCE MANUAL
S5 JAMNUTS
S5 ADJUSTMENT BOLTS
S1-S4 ADJUSTMENT BOLTS
S1-S4 JAMNUTS
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本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 飛行操縱 FLIGHT CONTROLS 5(100)
