What was found
INSPECTION FOUND A 2 CRACK IN NR 1 ENGINE NOSE COWL AFT BULKHEAD AND ANGLE SUPPORT. THE ANGLE WAS REMOVED. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 54-11-01, FIGURE 1 AND 51-31-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2 CRACK IN NR 1 ENGINE NOSE COWL AFT BULKHEAD AND ANGLE SUPPORT. THE ANGLE WAS REMOVED. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 54-11-01, FIGURE 1 AND 51-31-01.