Service difficulty report · Blade · Cessna T207A

Difficulty date
April 15, 2009
Submitted
April 21, 2009
Operation
General aviation
Aircraft
N803AN
Make and model
Cessna T207A
Aircraft serial
20700570
Engine
Cont TSIO520M
Propeller
Mcauly D3A34C401
Part
Blade
Part number
D3A34C401
Part serial
765815
Condition
Cracked
Location
Propeller
Stage of operation
NR
How discovered
9
Nature of condition
O
Precautionary procedure
O

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

What was found

THE ACFT WAS TAKEN OUT OF SERVICE DUE TO A BLADE THAT ROTATED FREELY IN THE HUB AND WAS NOT CONNECTED TO THE PITCH CHANGE MECHANISM. THE PROPELLER WAS DISASSEMBLED AND THE RETENTION AREA OF ONE BLADE WAS FOUND TO BE CRACKED APPROX 3 INCHES ACROSS THE RETENTION AREA OF ONE BLADE WAS FOUND TO BE STAMPED ON THE BLADE BUTT SHOWED THE BLADE MODEL TO BE A 90DFA-12, THE TIP AREA OF THE BLADE WAS FOUND TO HAVE BEEN RESHAPED TO AN INCORRECT BLADE PLATFORM FOR THE BLADE MODEL NR. THE PROPELLER IS SUSPECTED TO HAVE BEEN IN A MAJOR GROUND STRIKE AND THE BLADES WERE RESHAPED, REMOVING ANY EVIDENCE OF GROUND STRIKE DAMAGE AND REINSTALLED INTO A PROPELLER ASSY. THE PROP WAS ALSO FOUND UNDER THE MINIMUM DIAMETER FOR THIS APPLICATION BY .5 INCH. THE BLADES SHOULD HAVE BEEN REJECTED DUE TO THE STRIKE DAMAGE AND NOT MEETING THE MINIMUM WIDTH, THICKNESS AND BLADE PLATFORM SPECIFICATIONS. (K)

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