Service difficulty report · Nut Plate · Bell 407

Difficulty date
August 16, 2011
Submitted
August 25, 2011
Operation
General aviation
Aircraft
N911VS
Make and model
Bell 407
Aircraft serial
53650Q
Aircraft time
3,947 hours, 4,113 cycles
Part
Nut Plate
Part number
NAS577B4A
Condition
Loose
Location
Zone 300
Part time
3,947 hours, 4,113 cycles
Stage of operation
IN
How discovered
V
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

UPON PRE-FLIGHT, FOUND 1 OF 4 BOLTS THAT HOLD THE VERTICAL STABILIZER, TO BE STICKING OUT APPROX 2 INCHES. THIS BOLT WAS THE AFT UPPER BOLT. UPON EXAMINATION OF THE REMAINING BOLTS, AFT LOWER BOLT HAD POSSIBLY ONLY 1 THREAD ENGAGED AND WAS STICKING OUT APPROX .2500", FWD UPPER WAS ONLY FINGER TIGHT, AND THE FWD LOWER DID NOT HAVE SPECIFIED TORQUE. ACFT WAS INSPECTED 2 DAYS PRIOR AND PRE-FLIGHT/POST FLIGHT WAS ACCOMPLISHED THE DAY BEFORE. HELICOPTER IS PARKED AND MAINTAINED WITHIN PRIVATE HANGAR. AFTER REMOVAL OF 2 EA BOLTS, PN NAS6604-36 (FWD), 2 EA BOLTS PN NAS6604-28 (AFT) AND 4 EA NUTPLATE PN NAS577B4A, ALL 4 BOLTS WERE ABLE TO BE SCREWED IN BY HAND TO FULL THREAD ENGAGEMENT. THERE IS NO LOCTITE OR SAFETIES UTILIZED FOR THIS INSTALLATION.

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