Service difficulty report · Stud · Beech B200C

Difficulty date
July 9, 2002
Submitted
August 7, 2002
Operation
General aviation
Make and model
Beech B200C
Engine
Pwa PT6A42
Propeller
Hartzl HCD4N3A
Part
Stud
Part number
AN2278B
Condition
Fractured
Location
Control Column S
Component
Control Column S
Stage of operation
IN
Nature of condition
O, F
Precautionary procedure
K

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

What was found

(AUS) AILERON CONTROL SYSTEM STUD FRACTURED. CLAMP PNO AN737TW56-66 LOOSE AT BOTTOM OF CONTROL COLUMN ALLOWING THE CONTROL COLUMN BOOT PNO 101-54149-37 TO MOVE UNSECURED AROUND THE CONTROLCOLUMN. LH AILERON CONTROL CABLE TURNBUCKLE LOCKWIRE CAUGHT ONBRACKET PNO 50-524466-7 WHEN THE CONTROL WHEEL WAS MOVED TO THE RIGHT.

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