Service difficulty report · Elec Connector · Boeing 737824

Difficulty date
May 10, 2025
Submitted
May 13, 2025
Operation
Air carrier
Aircraft
N26208
Make and model
Boeing 737824
Aircraft serial
30580
Aircraft time
75,048 hours, 27,885 cycles
Part
Elec Connector
Condition
Damaged
Location
Flap Sys
Stage of operation
AP
How discovered
O
Nature of condition
F
Precautionary procedure
O

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

What was found

SPLIT FLAP ON ARRIVAL. LEFT FLAP LESS THAN ONE RIGHT FLAP STUCK AT ZERO. PILOT INFOMED THAT THEY SELECTED FLAPS ONE THE RH SIDE FLAPS DROPPED AND THE LH FLAPS STAYED THE SAME THE SAW SPLIT FLAPS AND DID THE SPILT FLAPS PROCEDURE. THEY ARMED ALTERNATE FLAPS AND FLAPS INHIBIT SWITCHES AND PERFORMED A NO FLAPS LANDING AT 182 KNOTS WHEN THEY PULLED INTO GATE THE SPILT FLAPS DISAPPEARED FOUND PSEU LIGHT ILLUMINATED UPDATED SCREENSHOTS OF FSEU BITE TEST. FOUND MAINTENANCE MSG 27-53250 ON FSEU LAST LEG FAULTS LEG 1. REMOVED CONNECTOR FROM FLAP SCEW SENSOR 8. FOUND PUSHED BACK SOCKETS ON CONNECTORS. SECURED SOCKETS. ALL SOCKETS ARE NOW LOCKED IN. RESECURED CONNECTOR. FOUND MAINT MSG 27-53250 ON FSEU LAST LEG FAULTS LEG 1. REMOVED CONNECTOR FROM FLAP SCEW SENSOR 1. FOUND PUSH BACK SOCKETS ON CONNECTORS.SECURED SOCKETS. ALL SOCKETS ARE NOW LOCKED IN. RESECURED CONNECTOR.RAN FLAPS SEVERAL TIMES, NO FAULT NOTED. REF FIM 27-59 TASK 801. ACOMPLISHED FLAP SKEW DETECTION SYSTEM FUNCTION CHECK IAW AMM 27-59-00-730-801. SYTEM TEST OK.