19961014031959A

Accident · Substantial damage

FAA accident report · Bell 206L-3 · Venice, LA · October 14, 1996

Date
October 14, 1996 · 07:20 local
Place
Venice, LA
Airport
Shell Airport
Phase of flight
Forced/Precautionary Landing
Operating rules
Air taxi and commuter (Part 135)
Operator
HEEA
Damage
Substantial damage
Aircraft
N21497
NTSB investigation
NTSBFTW97LA016
Reported as
Bell 206L3
Reported engine
Allison 250C30P
People aboard
4
Fatal injuries
0
Pilot’s flight hours
13,967 total10,807 in this make and model198 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.

Helicopter hovering when pilot heard loud pop, executed autorotation, main rotor flexed, cut off tail boom. (.4)during takeoff, approximately 50 feet AGL, the pilot heard a 'big pop and the helicopter was shaky and noisy.' He initiated a deceleration due to the wires in front of the helicopter. During the landing, 'a main rotor blade flexed down and severed the tailboom.' Throughout the forced landing the pilot had tail rotor pedal control. An examination of the engine by the operator revealed that frogs had been ingested. (-23) on October 14, 1996, at 7:20 am, central daylight time, pilot nien v. phan was attempting to take off from the Shell heliport located at Venice, Louisiana, in a Bell, model 206-L3, N21497, owned by petroleum helicopters, inc. the aircraft was approximately 50 feet in the air when the engine sounded like it was backfiring. Pilot phan entered into an emergency autorotation, landing long on the helipad in order to avoid striking high tension power lines located directly in front of the flight path. The aircraft's main rotor blade struck the tail boom, severing approximately a two-foot secti on of the tail boom to include the vertical fin and tail rotor gear box. Subsequent investigation and tear down of the engine revealed that the engine had ingested several green tree frogs, resulting in loss of power.

As the FAA filed it

HELICOPTER HOVERING WHEN PILOT HEARD LOUD POP, EXECUTED AUTOROTATION, MAIN ROTOR FLEXED, CUT OFF TAIL BOOM. (.4)DURING TAKEOFF, APPROXIMATELY 50 FEET AGL, THE PILOT HEARD A 'BIG POP AND THE HELICOPTER WAS SHAKY AND NOISY.' HE INITIATED A DECELERATION DUE TO THE WIRES IN FRONT OF THE HELICOPTER. DURING THE LANDING, 'A MAIN ROTOR BLADE FLEXED DOWN AND SEVERED THE TAILBOOM.' THROUGHOUT THE FORCED LANDING THE PILOT HAD TAIL ROTOR PEDAL CONTROL. AN EXAMINATION OF THE ENGINE BY THE OPERATOR REVEALED THAT FROGS HAD BEEN INGESTED. (-23) ON OCTOBER 14, 1996, AT 7:20 AM, CENTRAL DAYLIGHT TIME, PILOT NIEN V. PHAN WAS ATTEMPTING TO TAKE OFF FROM THE SHELL HELIPORT LOCATED AT VENICE, LOUISIANA, IN A BELL, MODEL 206-L3, N21497, OWNED BY PETROLEUM HELICOPTERS, INC. THE AIRCRAFT WAS APPROXIMATELY 50 FEET IN THE AIR WHEN THE ENGINE SOUNDED LIKE IT WAS BACKFIRING. PILOT PHAN ENTERED INTO AN EMERGENCY AUTOROTATION, LANDING LONG ON THE HELIPAD IN ORDER TO AVOID STRIKING HIGH TENSION POWER LINES LOCATED DIRECTLY IN FRONT OF THE FLIGHT PATH. THE AIRCRAFT'S MAIN ROTOR BLADE STRUCK THE TAIL BOOM, SEVERING APPROXIMATELY A TWO-FOOT SECTI ON OF THE TAIL BOOM TO INCLUDE THE VERTICAL FIN AND TAIL ROTOR GEAR BOX. SUBSEQUENT INVESTIGATION AND TEAR DOWN OF THE ENGINE REVEALED THAT THE ENGINE HAD INGESTED SEVERAL GREEN TREE FROGS, RESULTING IN LOSS OF POWER.

NTSB investigation

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