Service difficulty report · Igniter

Difficulty date
January 10, 2005
Submitted
May 11, 2005
Operation
General aviation
Engine
Ge CF7002D2
Part
Igniter
Condition
Damaged
Location
Engine
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

IGNITER WOULD NOT THREAD INTO ENGINE LOSS DURING O/H ASSEMBLY. 1ST THREAD SHOWS DAMAGE AND FURTHER EXAMINATION SHOWS THREAD DIAMETER IS .003 INCH-.004 INCH LARGER THAN THE OTHER NEW IGNITER INSTALLED ON THIS ENGINE. THE UNDAMAGED IGNITER WAS CHECK-THREADED INTO BOTH ENGINE BOSSES WITH NO PROBLEMS. RECOMMMEND CAREFUL CONDITION CHECKS. (K)