Service difficulty report · Plate · Cessna R182

Difficulty date
June 1, 2001
Submitted
July 11, 2001
Operation
General aviation
Make and model
Cessna R182
Propeller
Mcauly B2D34C218
Part
Plate
Part number
C5046
Condition
Cracked
Location
Aft Blkhd Attach
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

THIS PROPELLER INSTALLATION UTILIZES 2 SPINNER AFT BULKHEAD ATTACH PLATES, PN A1639-9. BOTH PLATES WERE FOUND TO BE CRACKED WITHIN 50 HR OF INSTALLATION OF PROP AFTER OVERHAUL. BECAUSE BULKHEAD ATTACHMENT PLATES ARE INSTALLED UNDER ATTACHMENT NUTS, PN A1639-9, THAT HOLDS THE PROP TO THE ENGINE IS SUBJECTED TO VERY HIGH CONTACT FORCES DUE TO THE SMALL SHOULDER ON THE NUT(A1639-9). THE LIKELIHOOD OF THIS FAILURE WILL INCREASE WITH THE NUMBER OF TIMES THESE FASTENERS ARE TORQUED. IPC CALLS FOR THE INSTALLATION OF A WASHER BETWEEN ATTACHMENT PLATE AND NUT, EXCEPT THERE IS NOT SUFFICIENT CLEARANCE TO ALLOW THE INSTALLATION OF THE WASHER.

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