19980519010199A

Accident · Substantial damage

FAA accident report · Bell UH-1H · Hope, ID · May 19, 1998

Date
May 19, 1998 · 10:15 local
Place
Hope, ID
Phase of flight
Aerial Taxi To Tkof/Rtrcrft
Operating rules
Rotorcraft external load (Part 133)
Operator
WYFL
Damage
Substantial damage
Aircraft
N98NW
NTSB investigation
NTSBSEA98FA077
Reported as
Bell UH1H
Reported engine
Lycoming T53L13B
People aboard
1
Fatal injuries
0
Pilot’s flight hours
11,700 total6,700 in this make and model160 in the last 90 days

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.

Squeal compressor stalls and smoke, flames from tail pipe. Lost all power and landed in clearing. Report to follow. (.4) the pilot reported that he had dropped off a load of chokers and was maneuvering to hook up to a load of logs when the engine began to make 'a weird squealing noise, followed by a constant series of compressor stalls, occurring about twice per second.' The airplane then lost all engine power, and the pilot performed a forced landing in a clearing. Post crash examination revealed that the no. 1 bearing (p/n:1-300-015-04; s/n:127AC) was heavily damaged. From observations of damage on the bearing raceways and the inner ring split faces, evidence indicated that both thrust and non-thrust sides of the inner ring had been misaligned, based upon ball path indications. Military records for the engine included an unserviceable tag. No evidence was found of specifics related to that failure code, nor was evidence found recording related corrective maintenance action

As the FAA filed it

SQUEAL COMPRESSOR STALLS AND SMOKE, FLAMES FROM TAIL PIPE. LOST ALL POWER AND LANDED IN CLEARING. REPORT TO FOLLOW. (.4) THE PILOT REPORTED THAT HE HAD DROPPED OFF A LOAD OF CHOKERS AND WAS MANEUVERING TO HOOK UP TO A LOAD OF LOGS WHEN THE ENGINE BEGAN TO MAKE 'A WEIRD SQUEALING NOISE, FOLLOWED BY A CONSTANT SERIES OF COMPRESSOR STALLS, OCCURRING ABOUT TWICE PER SECOND.' THE AIRPLANE THEN LOST ALL ENGINE POWER, AND THE PILOT PERFORMED A FORCED LANDING IN A CLEARING. POST CRASH EXAMINATION REVEALED THAT THE NO. 1 BEARING (P/N:1-300-015-04; S/N:127AC) WAS HEAVILY DAMAGED. FROM OBSERVATIONS OF DAMAGE ON THE BEARING RACEWAYS AND THE INNER RING SPLIT FACES, EVIDENCE INDICATED THAT BOTH THRUST AND NON-THRUST SIDES OF THE INNER RING HAD BEEN MISALIGNED, BASED UPON BALL PATH INDICATIONS. MILITARY RECORDS FOR THE ENGINE INCLUDED AN UNSERVICEABLE TAG. NO EVIDENCE WAS FOUND OF SPECIFICS RELATED TO THAT FAILURE CODE, NOR WAS EVIDENCE FOUND RECORDING RELATED CORRECTIVE MAINTENANCE ACTION

NTSB investigation

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

Other reports on N98NW · 1

Matched to the same aircraft by N-number and date.