Service difficulty report · Cable · Beech 400A

Difficulty date
June 22, 2021
Submitted
June 23, 2021
Operation
Air carrier
Filed by
IZ2R916K
Intercontinental Jet Service Corporation
Aircraft
N484TP
Make and model
Beech 400A
Aircraft serial
RK195
Aircraft time
10,606 hours, 8,307 cycles
Part
Cable
Part number
45A103511
Condition
Broken
Location
Rt Flap
Part time
10,606 hours, 8,307 cycles
Stage of operation
NR
How discovered
9
Nature of condition
O
Precautionary procedure
O

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

What was found

DURING A SCHEDULED MAINTENANCE INSPECTION, IT WAS NOTICED THAT THE RIGHT FLAP OUTBOARD CABLE DID NOT HAVE TENSION AND THE FLAP FORWARD CABLE WAS TOUCHING THE RIGHT-WING REAR SPAR. FURTHER INVESTIGATION REVEALED THAT THE CABLE WAS BROKEN FROM THE SWAGED FITTING DUE TO CORROSION. WHILE THIS HAPPENED ONLY IN THE RIGHT WING, BOTH (LEFT AND RIGHT) CABLES WILL BE REPLACED AT THIS VISIT. POSSIBLE REASON: THE FRONT CABLES RUN BELOW THE SPOILERS SURFACES AND THEREFORE ARE SUBJECT TO RAINWATER. THE CURRENT 400/400A MAINTENANCE MANUAL CALLS FOR LUBRICATING THE LEVER ASSEMBLIES, RAILS AND ROLLERS BUT NOT THE FLAP CABLES SWAGED FITTING. SUGGESTIONS (FOR ADDING TO THE MAINTENANCE MANUALS): INSPECT FOR CONDITION AND APPLY WATER RESISTANT SEALANT TO BELLCRANK DRIVER CAVITY TO PREVENT WATER ACCUMULATION AND INSPECT CONDITION EVERY B CHECK. OR FILL BELLCRANK DRIVER CAVITY WITH GREASE AND INSPECT CONDITION EVERY B CHECK. OR ADD AN INSPECTION/REPLACEMENT SCHEDULE TO THE INSPECTION PROGRAM.

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