SDR 98ZZZX1910

Service difficulty report · Bolt · Beech 77

Difficulty date
May 12, 1998
Submitted
March 26, 2000
Operation
General aviation
Aircraft
N3818D
Make and model
Beech 77
Aircraft serial
WA221
Part
Bolt
Condition
Failed
Location
Wing
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

DURING THE 7,000 HOUR WING CARRY-THROUGH STRUCTURE INSPECTION AND WING BOLT REPLACEMENT, FOUND BOLT HEAD, WASHER, AND SPACER LYING IN BOTTOM OF SPAR. NOTED CORROSION BETWEEN PARTED SURFACES OF BOLT AND HEAD - SUSPECT CAUSE OF BOLT FAILURE. NOTE: AIRCRAFT EXCEEDED 7,000-HOUR INSPECTION. RECOMMEND AT LEAST PERIODICALLY REMOVING WING TIP CAPS AND LOOKING DOWN SPAR FOR DEFECTS. ACTT: 7,785.7 HOURS.

More about the Beech 77