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gear is not in the down and locked position, the landing gear
control lever is not down, and all of these conditions are true:
* TE Flaps landing warning switch A and B >10 units
* One or both SMYDs TE Flaps 15 through 25 units
* One or both thrust levers at idle or one or both engines not
running.
The horn can not be stopped with the horn reset switch when
the trailing edge flaps are in the 15 through 25 unit position.
TE Flap Position More Than 25 Units
This type of aural warning operates when one or more landing
gear is not in the down and locked position and all of these
conditions are true:
* TE Flaps landing warning switch A and B >10 units
* Both SMYDs TE Flaps > 25 units.
Also, one of these two conditions must be true:
* Landing gear control lever is in the UP position for more than
12 seconds
* Landing gear control lever is in the UP position for less than
12 seconds and one or both thrust levers at idle or one or
both engines not running.
LG POSITION INDICATING AND WARNING SYSTEM - AURAL WARNING - FUNCTIONAL DESCRIPTION
EFFECTIVITY
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The horn can not be stopped with the horn reset switch when
the trailing edge flaps are more than 25 units.
LG POSITION INDICATING AND WARNING SYSTEM - AURAL WARNING - FUNCTIONAL DESCRIPTION
EFFECTIVITY
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LG POSITION INDICATING AND WARNING SYSTEM - AURAL WARNING - FUNCTIONAL DESCRIPTION
LG POSITION INDICATING AND WARNING SYSTEM - AURAL WARNING - FUNCTIONAL DESCRIPTION
EFFECTIVITY
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737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
Purpose
The tail skid protects the stabilizer bulkhead and fuselage
structure when the main landing gear shock struts are extended
and the airplane rotates during takeoff.
General Description
The tail skid is on the bottom exterior surface of the airplane
below the horizontal stabilizer. The tail skid has a wear shoe.
The wear shoe absorbs the tail strike when the shoe rubs on the
runway. A warning placard on the aft surface of the skirt fairing
shows when you should replace the tail skid.
The forward fairing supplies an aerodynamic cover around the
tail skid skirt fairing. The forward fairing attaches to the bottom
skin of the airplane. The aft fairing continues the aerodynamic
cover aft of the skirt fairing. The aft fairing attaches to the APU
access door. A drain on the aft fairing drains moisture from the
inside the fairing.
Training Information Point
During ground maintenance, if the airplane center of gravity
exceeds the aft limit, the airplane will rest on the tail fuselage
structure and compressed landing gear struts. Damage to the
fuselage may occur.
TAIL SKID - GENERAL DESCRIPTION
EFFECTIVITY
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TAIL SKID - GENERAL DESCRIPTION
TAIL SKID - GENERAL DESCRIPTION
EFFECTIVITY
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TAIL SKID - GENERAL DESCRIPTION
TAIL SKID - GENERAL DESCRIPTION
EFFECTIVITY
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TAIL SKID - GENERAL DESCRIPTION
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737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
Components
The tail skid has these components:
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