Service difficulty report · Bolt · Cessna U206F

Difficulty date
October 29, 2009
Submitted
December 1, 2009
Operation
General aviation
Make and model
Cessna U206F
Aircraft time
10,750 hours
Engine
Cont IO550F
Propeller
Hartzl PHCC3YF1
Part
Bolt
Condition
Loose
Location
Alternator
Part time
91 hours
Component
Alternator
Component part number
DOFF10300JR
Stage of operation
IN
How discovered
9
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) ALTERNATOR WAS RETURNED DUE TO FAILURE TO CHARGE BATTERY AND HAD BEEN O/H. UPON INSP THE THROUGH BOLTS WERE FOUND LOOSE. THE STATOR HAD BECOME LOOSE BETWEEN THE HSG AND HAD BEEN SPUN BY THE ROTOR, BREAKING THE STATOR WIRES. A PLACARD ON ALTERNATORS STATING THAT THE THROUGH BOLTS SHOULD BE RETORQUED AT 10 HOURS OF OPERATION AND EVERY 100 HRS AFTERWARD. THIS PLACARD GAVE A TORQUE VALUE OF 30-35 IN. LBS. WHICH IS THE TORQUE FOR THE 10-24 BOLTS USED IN OLDER HSGS. THIS ALTERNATOR HAD THE NEWER STYLE 1/4"-20 BOLTS, WHICH HAVE A PLACARD THAT GIVES A TORQUE VALUE OF 75-85 IN. LBS. IF CUSTOMER HAD RETORQUED AT THE LWR VALUE INDICATED IT WOULD HAVE CAUSED THE FAILURE OF THE ALTERNATOR. AN EXCHANGE ALTERNATOR WAS SENT TO THE CUSTOMER.

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