19950128000919I

Incident · Minor damage

FAA incident report · Bell 206B3 · Perry, FL · January 28, 1995

Date
January 28, 1995 · 18:00 local
Place
Perry, FL
Airport
Perry-Foley Airport
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
Air taxi and commuter (Part 135)
Operator
HXCA
Damage
Minor damage
Aircraft
N5008N
NTSB investigation
NTSBMIA95LA065
Reported as
Bell 206B3
People aboard
3
Fatal injuries
0
Pilot’s flight hours
3,600 total

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

Narrative: while observing engine being removed from aircraft, it was discovered that the p/c (pneumatic) stainless steel line had come loose from engine. Evidence showed black streaks originating at b nut sleeve and covering line adjacent to "b" nut. There was wear marks on the outboard threads of fitting indicating that the line had not been fully seated. When it finally backed off, the engine spooled down and finally failed. (The p/c line connects to the fuel control and the engine gear box) it came loose at the engine end. This case is forwarded to FSDO 17, the chdo for the operator for further investigation.

As the FAA filed it

NARRATIVE: WHILE OBSERVING ENGINE BEING REMOVED FROM AIRCRAFT, IT WAS DISCOVERED THAT THE P/C (PNEUMATIC) STAINLESS STEEL LINE HAD COME LOOSE FROM ENGINE. EVIDENCE SHOWED BLACK STREAKS ORIGINATING AT B NUT SLEEVE AND COVERING LINE ADJACENT TO "B" NUT. THERE WAS WEAR MARKS ON THE OUTBOARD THREADS OF FITTING INDICATING THAT THE LINE HAD NOT BEEN FULLY SEATED. WHEN IT FINALLY BACKED OFF, THE ENGINE SPOOLED DOWN AND FINALLY FAILED. (THE P/C LINE CONNECTS TO THE FUEL CONTROL AND THE ENGINE GEAR BOX) IT CAME LOOSE AT THE ENGINE END. THIS CASE IS FORWARDED TO FSDO 17, THE CHDO FOR THE OPERATOR FOR FURTHER INVESTIGATION.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.