SDR 99ZZZX431

Service difficulty report · Wheel · Cessna 210L

Difficulty date
November 1, 1998
Submitted
March 26, 2000
Operation
General aviation
Aircraft
N444CL
Make and model
Cessna 210L
Aircraft serial
21060910
Part
Wheel
Condition
Cracked
Location
Mlg
Part time
2,669 hours
Component
Mcauly
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

MAIN WHEELS REMOVED DURING ANNUAL INSPECTION, FOUND ALL BOLT HOLES IN HUBS CRACKED. PREVIOUS WHEELS HAVE AD 74-13 6 ASSOC WITH THEM. AD REQUIRES THE SERIES OF ATTACH HOLES IN THE HUBS ENLARGED FROM .25 INCH FASTENER TO .3125 INCH FASTENER BY OVERSIZING THE HOLES AND TAPING. WHEELS ADDRESSED IN THIS REPORT ARE NOT SUBJECT IN THE BODY OF THIS AD, YET HAVE BEEN MODIFIED TO THE LARGER BOLT HOLES. MODIFICATION LEAVES MINIMAL WALL THICKNESS BETWEEN THE HOLE AND OUTER DIA OF HUB EDGE. SUBMITTER STATED MINIMAL THICKNESS COMBINED WITH NUMEROUS CYCLES OF BOLT REMOVAL AND INSTALLATION INITIATED THESE CRACKS. RECOMMEND ALL MCCAULEY WHEELS OF THIS SERIES MODIFIED TO .3125 INCH BOLT STYLE BE INSPECTED FOR CRACKS.

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