SDR 95ZZZX2035

Service difficulty report · Web · Cessna 441

Difficulty date
March 27, 1995
Submitted
March 26, 2000
Operation
General aviation
Aircraft
N441K
Make and model
Cessna 441
Aircraft serial
4410093
Part
Web
Part number
521304027
Condition
Holes Elongated
Location
Nlg Wheelwell
Part time
4,442 hours
Stage of operation
IN
Nature of condition
O
Precautionary procedure
K

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

What was found

THE NOSE GEAR DRAG BRACE ATTACH BRACKET ATTACH BOLTS WORK LOOSE WITH TIME DUE TO FORE AND AFT LOADS PLACED ON NOSE GEAR DURING TOWING. AFTER BOLTS WORK LOOSE, THEY ELONGATE THE WHEELWELL ATTACH AREAS WHERE THE BOLTS GO THROUGH THE SKIN OF THE WHEELWELL. THE WHEELWELL SKIN IS ONLY .040 INCH THICK. SUBMITTER RECOMMENDS A .063 INCH DOUBLER INSTALLED TO STIFFENER AREA AND PREVENT BOLT HOLE ELONGATION. THIS CONDITION HAS BEEN FOUND ON NUMEROUS 441 CONQUEST II AIRCRAFT.

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