Service difficulty report · Spar Cap · Cndair CL2151A10

Difficulty date
October 15, 2003
Submitted
November 21, 2003
Operation
General aviation
Make and model
Cndair CL2151A10
Aircraft time
3,329 hours
Engine
Pwa CWASP
Propeller
Hamstd 43E60
System (JASC)
5711 · Wing Spar
Part
Spar Cap
Condition
Cracked
Location
Lt Wing
Stage of operation
IN
How discovered
9
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

(CAN) DURING ACCOMPLISHMENT OF AD CF-92-26R1, THE ULTRASONIC INSPECTION WAS BEING COMPLETED IAW SB 215-A454. CRACKS WERE DETECTED ON THE LOWER RT AND LOWER LT SPAR CAPS. THE AIRCRAFT WILL BE REPAIRED IAW MFG REO PRIOR TO BEING TO RETURNED TO SERVICE.