Service difficulty report · Fuel Nozzle

Difficulty date
March 23, 2009
Submitted
April 2, 2009
Operation
General aviation
Engine
Pwa JT8D219
Part
Fuel Nozzle
Part number
80913701
Part serial
HK18HK16
Condition
Damaged
Location
Engine
Part time
24,090 hours
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

DURING DISASSEMBLY OF THE DIFFUSER MODULE IT WAS NOTICED THAT THE FUEL NOZZLES AT NR 1 AND NR 2 POSITIONS HAD SUSTAINED DAMAGE DUE TO THE AIR SCOOP WELD FAILING, THUS ALLOWING THE AIR SCOOP TO ROTATE AND CAUSE FRETTING EROSION TO THE HEAT SHIELD AND NOZZLE BODY ASSY. EXTRA WORK COMPARING DAMAGE TO A SECTIONED NOZZLE SUPPORT SHOW’S A FURTHER 0.012 INCH (ESTIMATED) WEAR WOULD HAVE RESULTED IN A PRIMARY FUEL FLOW PASSAGE BREACH. ESTIMATED FRETTING EROSION TO NR 2 NOZZLE S/N HK18 IS APPROX 0.161 INCH. THIS IS A KNOWN PROBLEM WITH EARLY PN -200 FUEL NOZZLES. THESE NOZZLES ARE PRE 6034, 6196, 6240, 6361 AND 6405. AD 95-02-16 HAS ADDRESSED THIS ISSUE WITH THE NR 7 FUEL NOZZLE ONLY - IT DOES NOT MANDATE COMPLIANCES WITH REMAINING FUEL NOZZLES. ENG CTR RECOMMENDS FITMENT OF POST MOD 6405 NOZZLES. (K)