19990608006659A

Accident · Substantial damage

FAA accident report · Hughes 369D · South Bend, WA · June 8, 1999

Date
June 8, 1999 · 09:20 local
Place
South Bend, WA
Operating rules
Rotorcraft external load (Part 133)
Damage
Substantial damage
Aircraft
N8306F
NTSB investigation
NTSBSEA99LA082
Reported as
Hughes 369D
Fatal injuries
0

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.

1978 Hughes 369D helicopter was involved in an external load operation when the acft engine failed, the pilot autorotated the acft, and the acft made a hard landing and sustained substantial damage, other circumstances are unknown. (-23) helicopter released external load at 100 foot hover and experienced power loss. Executed autorotation and experienced hard landing and power off rotor sudden stoppage. Helicopter rolled on right side. Substantial damage to rigth side of fuselage. Tail boom seperated mid span, with detached portion of boom laying approximately 30 feet from aircraft. Engine exmaination found air transfer tube damage, and mounting bolts for compressor to gearbox attachment sheared. Aircraft released to owner for transportation to base for further examination. On 6-10-99, inspection helicopter at owners main base. Found #1 bearing housing seperated from front compressor housing. N1 and N2 gear train of engine found seized.

As the FAA filed it

1978 HUGHES 369D HELICOPTER WAS INVOLVED IN AN EXTERNAL LOAD OPERATION WHEN THE ACFT ENGINE FAILED, THE PILOT AUTOROTATED THE ACFT, AND THE ACFT MADE A HARD LANDING AND SUSTAINED SUBSTANTIAL DAMAGE, OTHER CIRCUMSTANCES ARE UNKNOWN. (-23) HELICOPTER RELEASED EXTERNAL LOAD AT 100 FOOT HOVER AND EXPERIENCED POWER LOSS. EXECUTED AUTOROTATION AND EXPERIENCED HARD LANDING AND POWER OFF ROTOR SUDDEN STOPPAGE. HELICOPTER ROLLED ON RIGHT SIDE. SUBSTANTIAL DAMAGE TO RIGTH SIDE OF FUSELAGE. TAIL BOOM SEPERATED MID SPAN, WITH DETACHED PORTION OF BOOM LAYING APPROXIMATELY 30 FEET FROM AIRCRAFT. ENGINE EXMAINATION FOUND AIR TRANSFER TUBE DAMAGE, AND MOUNTING BOLTS FOR COMPRESSOR TO GEARBOX ATTACHMENT SHEARED. AIRCRAFT RELEASED TO OWNER FOR TRANSPORTATION TO BASE FOR FURTHER EXAMINATION. ON 6-10-99, INSPECTION HELICOPTER AT OWNERS MAIN BASE. FOUND #1 BEARING HOUSING SEPERATED FROM FRONT COMPRESSOR HOUSING. N1 AND N2 GEAR TRAIN OF ENGINE FOUND SEIZED.

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 N8306F · 4

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