Service difficulty report · Frame · Dhav DH82A

Difficulty date
February 21, 2013
Submitted
March 1, 2013
Operation
Air carrier
Aircraft
N5300
Make and model
Dhav DH82A
Aircraft serial
T5703
Aircraft time
10,385 hours, 11,359 cycles
Part
Frame
Condition
Corroded
Location
Fuselage
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

FRAME FLANGES AT FR 176 STR 32-30P HAVE CORROSION. REMOVED 1 EA RIVET TO FOM AND REMOVED CORROSION IAW SRM 51-42-05-02-01, 53-00-00-02-09 REV 12 AND DISPLACED WIRES IAW AMM 20-30-26-910-801, REV 40. PRIOR TO CORROSION REMOVAL REMOVED AN ADDITIONAL 6 RIVETS IAW SRM 51-42-05-02-01, REV 12. VERIFIED AFFECTED AREAS TO BE CRACK FREE REF NDTM PART 6 TASK 51-00-01-250-801, REV 8. MIN THICKNESS NOTED .045" REF NDTM PART 1 TASK 51-00-04-910-801 REV 8. NOMINAL THICKNESS .040" REF DWG 85328142 FOUND TO BE WITHIN LIMITS IAW SRM 53-20-15-00-01, REV 12. ALODINE AND PRIMED REWORKED AREA IAW SRM 51-21-10-02-01, 51-25-10-02-01 REV1 2. INSTALLED RIVETS IAW SRM 51-42-05-02-01, REV 12. APPLIED TOP COAT IAW SRM 51-25-15-02-01 REV 12. APPLIED CPC IAW AMM 51-25-01-390-801, REV 40. RESECURED WIRES IAW WM 20-12-10-201, REV 39.