27-51-00
ALL ú ú 01 Page 27 ú Mar 15/89
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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737-300/400/500MAINTENANCE MANUAL
Retraction of the flaps due to airloads is prevented by a no-back friction brake in the inboard transmission assembly at each flap. If a transmission assembly should fail, a torque limiter in the remaining transmission assembly on that flap will stall the flap drive system to prevent structural damage. Stopping the drive system also prevents operation of the remaining flaps, thus maintaining the airplane in a normal flight attitude.The flap segments are mechanically separated during extension. As the flaps start to extend, an actuating mechanism moves the aftflap to form a slot between the aftflap and midflap. At about 8 units of midflap extension, the foreflap sequencing toggles contact stops on the main flap tracks. The stops prevent additional aft movement of the foreflap. Continued midflap extension creates a slot between the foreflap and midflap. As the midflap approaches full travel, the aftflap again moves relative to the midflap, increasing the width of the slot between the two segments.A flap alternate drive unit is provided to operate the trailing edge flaps electrically if a failure prevents normal hydraulic operation. The flap alternate drive unit is controlled from two switches located on the overhead panel. The alternate flaps arm switch and control switch operate the system. Actuation of the alternate flaps arm switch to ARM supplies 28-volt dc power to the alternate flaps control switch. Simultaneously, 28-volt dc power is supplied to position the trailing edge flap bypass valve to BYPASS. This interconnects the flap hydraulic motor ports to allow circulation of hydraulic fluid and prevents fluid flow from the control valve to the hydraulic motor. Actuation of the alternate flaps control switch to DOWN energizes the alternate flap down relay to complete a circuit to extend the flaps. When the flaps are fully extended, a down limit switch opens to break circuit continuity. Positioning the alternate flaps control switch to UP closes the alternate flap up relay to complete a circuit to retract the flaps. When the flaps are fully retracted, an up limit switch opens to break circuit continuity. The trailing edge flaps may be stopped in any intermediate position by returning the alternate flaps control switch to OFF.An electrical asymmetry system will stop operation of the flap drive system when a certain separation of left and right indicator pointers occurs. The separation closes a comparator switch in the indicator to operate the flap asymmetry relay, causing the hydraulic bypass valve to stop operation of the flap drive hydraulic motor.
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27-51-00
ALL ú ú 01 Page 28 ú Jul 15/88
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
F. A flap control cable tension switch system is provided to stop operation of the flap drive system if a flap control cable breaks. If a cable should break, the spring loaded lever supporting the cable pulley moves the lever mounted magnet away from the switch. This activates the switch circuit. The activated switch provides 28-volt dc power to activate the flap bypass valve to BYPASS. This shuts off hydraulic power to the hydraulic motor. The flaps are prevented from extending beyond the flap control lever position.
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