Service difficulty report · Angle · Beech A100

Difficulty date
March 18, 1998
Submitted
March 26, 2000
Operation
General aviation
Make and model
Beech A100
Engine
Pwa PT6A34
Part
Angle
Condition
Cracked
Location
Wing
Component
50160018
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

(CAN) ON ROUTINE WING INSPECTION, THE RT OUTBOARD FLAP INBOARD FLAP HANGER, LOWER CLIPS P/N 35-115 396-1 AND -3 WERE FOUND TO BE TORN AT HANGER RIVET ATTACHMENTS AND THE LOWER PORTION OF THE HANGER TO SPAR ATTACHMENT ANGLES P/N 35-115398-1 AND -3 WERE TORN AWAY FROM THE SPAR. ANGLES AND CLIPS REPLACED. ON FURTHER INVESTIGATION, THE LT OUTBOARD FLAP INBOARD HANGER HAD SIMILAR DAMAGE AND ANOTHER A100 IN THE FLEET ALSO REQUIRED REPAIRS TO SAME COMPONENTS.

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