19980503008229A

Accident · Substantial damage

FAA accident report · Bell 47G3B2A · Stanwood, WA · May 3, 1998

Date
May 3, 1998 · 12:00 local
Place
Stanwood, WA
Phase of flight
Pwr Off Vert Land/Autorotate
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N7965J
NTSB investigation
NTSBSEA98LA069
Reported as
Bell 47G3B2A
Reported engine
Lycoming TVO435F1A
People aboard
3
Fatal injuries
0
Pilot’s flight hours
5,300 total900 in this make and model62 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.

Sightseeing tours from Stanwood fairgrounds when the engine caught fire and the acft made an emerg landing. (.4)while reducing power in the initial climb in order to establish cruise flight, the pilot of the helicopter experienced a partial engine power loss, followed by a complete loss of power about 15 seconds later. The pilot executed an autorotation to an emergency landing in a freshly plowed field, whereupon the main rotor flexed downward and contacted the tail boom during the touchdown. A post-accident inspection of the engine revealed that the number two connecting rod had failed near where it attaches to the crankshaft, ultimately leading to a total engine failure. Because both relevant fracture surfaces of the connecting rod were severely damaged and disfigured by repeated rotational impact pounding, the rod was not submitted for metallurgical failure mode examination.

As the FAA filed it

SIGHTSEEING TOURS FROM STANWOOD FAIRGROUNDS WHEN THE ENGINE CAUGHT FIRE AND THE ACFT MADE AN EMERG LANDING. (.4)WHILE REDUCING POWER IN THE INITIAL CLIMB IN ORDER TO ESTABLISH CRUISE FLIGHT, THE PILOT OF THE HELICOPTER EXPERIENCED A PARTIAL ENGINE POWER LOSS, FOLLOWED BY A COMPLETE LOSS OF POWER ABOUT 15 SECONDS LATER. THE PILOT EXECUTED AN AUTOROTATION TO AN EMERGENCY LANDING IN A FRESHLY PLOWED FIELD, WHEREUPON THE MAIN ROTOR FLEXED DOWNWARD AND CONTACTED THE TAIL BOOM DURING THE TOUCHDOWN. A POST-ACCIDENT INSPECTION OF THE ENGINE REVEALED THAT THE NUMBER TWO CONNECTING ROD HAD FAILED NEAR WHERE IT ATTACHES TO THE CRANKSHAFT, ULTIMATELY LEADING TO A TOTAL ENGINE FAILURE. BECAUSE BOTH RELEVANT FRACTURE SURFACES OF THE CONNECTING ROD WERE SEVERELY DAMAGED AND DISFIGURED BY REPEATED ROTATIONAL IMPACT POUNDING, THE ROD WAS NOT SUBMITTED FOR METALLURGICAL FAILURE MODE EXAMINATION.

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 N7965J · 2

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