19950504018629I

Incident · Minor damage

FAA incident report · Bell 412 · Sabine, TX · May 4, 1995

Date
May 4, 1995 · 05:41 local
Place
Sabine, TX
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
Air taxi and commuter (Part 135)
Operator
HEEA
Damage
Minor damage
Aircraft
N3893N
Reported as
Bell 412
Reported engine
Pratt & Whitney PT6T3B
People aboard
2
Fatal injuries
0
Pilot’s flight hours
10,232 total3,146 in this make and model183 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.

Narrative: on may 4, 1995, at 5:41 am, Bell helicopter, model 412, N3893N, operated by petroleum helicopters, inc. (phi), was en route to an offshore platform in the gulf of Mexico, east cameron block 195, when the pilot-in-command heard a muffled pop followed by a vibration to the aircraft and its controls. Without further incident, the pilot returned to the phi base in Sabine, Texas, where the flight had originated at 5:36 that morning. There were no injuries and no further damage to the aircraft. The flight was conducted under the provisions of visual flight rules. Inspection of the aircraft after the flight by phi maintenance personnel revealed that the stainless steel vent fitting on the no.2 engine exhaust ejector, Bell part no. 209-062-534-003, came loose during flight causing damage to two of the four main rotor blades and the tail rotor blades. Phi sent the tail rotor blades to a metallurgical testing laboratory which confirmed the fact that the material was, in fact, stainless steel.

As the FAA filed it

NARRATIVE: ON MAY 4, 1995, AT 5:41 AM, BELL HELICOPTER, MODEL 412, N3893N, OPERATED BY PETROLEUM HELICOPTERS, INC. (PHI), WAS EN ROUTE TO AN OFFSHORE PLATFORM IN THE GULF OF MEXICO, EAST CAMERON BLOCK 195, WHEN THE PILOT-IN-COMMAND HEARD A MUFFLED POP FOLLOWED BY A VIBRATION TO THE AIRCRAFT AND ITS CONTROLS. WITHOUT FURTHER INCIDENT, THE PILOT RETURNED TO THE PHI BASE IN SABINE, TEXAS, WHERE THE FLIGHT HAD ORIGINATED AT 5:36 THAT MORNING. THERE WERE NO INJURIES AND NO FURTHER DAMAGE TO THE AIRCRAFT. THE FLIGHT WAS CONDUCTED UNDER THE PROVISIONS OF VISUAL FLIGHT RULES. INSPECTION OF THE AIRCRAFT AFTER THE FLIGHT BY PHI MAINTENANCE PERSONNEL REVEALED THAT THE STAINLESS STEEL VENT FITTING ON THE NO.2 ENGINE EXHAUST EJECTOR, BELL PART NO. 209-062-534-003, CAME LOOSE DURING FLIGHT CAUSING DAMAGE TO TWO OF THE FOUR MAIN ROTOR BLADES AND THE TAIL ROTOR BLADES. PHI SENT THE TAIL ROTOR BLADES TO A METALLURGICAL TESTING LABORATORY WHICH CONFIRMED THE FACT THAT THE MATERIAL WAS, IN FACT, STAINLESS STEEL.

Other reports on N3893N · 2

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