Service difficulty report · Longeron · Piper PA18150

Difficulty date
February 22, 2004
Submitted
June 4, 2004
Operation
General aviation
Make and model
Piper PA18150
Engine
Lyc O320A2B
Propeller
Snsnch M74DM
Part
Longeron
Condition
Cracked
Location
Fuselage
Part time
4,349 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) UPPER LT LONGERON TUBE CRACKED IN AREA BETWEEN FORWARD WELD OF LT REAR STABILIZER SUPPORT AND FORWARD WELD OF CROSS BRACE TUBE.

More about the Piper PA-18-150