Service difficulty report · Attach Angle · Cndair CL2151A10

Difficulty date
July 12, 2002
Submitted
August 7, 2002
Operation
General aviation
Make and model
Cndair CL2151A10
Aircraft time
3,415 hours
Part
Attach Angle
Condition
Cracked
Location
Wing To Body
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

(CAN) CRACK FOUND AT ATTACH FASTENER HOLE AT LOWER SPAR LOCATION DURING NDT REQUIRED BY AD 1997-07R2 WHOSE REQUIREMENTS ARE EVERY 415 FLIGHT HOURS OR 1500 WATER DROPS, WHICHEVER COMES FIRST. THIS AIRCRAFT HAD 1250 WATER DROPS SINCE THE LAST COMPLIANCE OF THIS AD.