Service difficulty report · Connector · Boeing 737277

Difficulty date
November 5, 2001
Submitted
November 20, 2001
Operation
Air carrier
Aircraft
N184AW
Make and model
Boeing 737277
Aircraft serial
22651
Aircraft time
58,279 hours, 47,663 cycles
Part
Connector
Part number
BACC63BN18C14S8
Condition
Worn
Location
Autopilot Sys
Stage of operation
CL
How discovered
O
Nature of condition
F, E
Precautionary procedure
A

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

AFTER T/O, HEARD LOUD THUMP DURING GEAR RETRACTION, INDICATIONS NORM. IN FLT W/AP ENGAGED ACFT STARTED PORPOISING. AP WAS DISENGAGED, DIFFICULTY CONTROLLING PITCH ATTITUDE. DIVERTED. ON APPROACH 165 KTS BUFFETING FELT, FLAPS 15, 170 KTS. FERRIED, A COMPLETE VERT STAB & ELEV CHECK INCLUDING CABLES, PULLEYS, BEARINGS, SURFACES & ELECT CONTROL SYS PERFORMED. AUTO PILOT STAB TRIM SERVO CONNECTOR (D381) PIN NR 3 FOUND LOOSE & WORN THRU INSULATION. REPLACED CONNECTOR, STAB TRIM BRAKE, AUTO PILOT STAB TRIM SERVO MOTOR, FLAPS UP LIMIT SWITCH (S245), STAB TRIM CUTOUT SWITCH (S272) & STAB ELEC ACT LIMIT & TAKEOFF WARNING SWITCH (S546). LOUD THUMP DETERMINED TO BE NOSE GEAR LOCK ACTUATOR, WHICH WAS REPLACED.