Service difficulty report · Fitting · Piper PA36375

Difficulty date
January 16, 2002
Submitted
February 5, 2002
Operation
General aviation
Make and model
Piper PA36375
Engine
Lyc IO720D1C
Part
Fitting
Part number
97101301
Condition
Cracked
Location
Fuselage
Part time
5,517 cycles
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

(AUS) RT FRONT SPAR ATTACHMENT FITTING ON FUSELAGE LOCATED AT RT STN 124.250 CRACKED IN REAR LAMINATE. CRACK LENGTH 10MM (0.39IN).

More about the Piper PA-36-375