20170502005009A

Accident · Substantial damage

FAA accident report · Bell 407 · Boothville, LA · May 2, 2017

Date
May 2, 2017 · 06:30 local
Place
Boothville, LA
Airport
Boothville
Phase of flight
Cruise/Level Flight
Operating rules
Air taxi and commuter (Part 135)
Operator
HEEA
Damage
Substantial damage
Aircraft
N457PH
NTSB investigation
NTSBCEN17LA174
Reported as
Bell 407
People aboard
6
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
3,272 total1,938 in this make and model190 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.

A Bell 407 helicopter was enroute to an offshore location . At approximately three (3) minutes after takeoff on the first flight of the day, the pilot heard a "pop" which was followed by a vibration he diagnosed as emanating from the tail section of the aircraft. The pilot began a descent from cruise altitude of 1,750 and headed toward a helideck that was in the immediate vicinity. After landing and reducing the rotor RPM to idle, the pilot noted an increase in vibration, at which time he secured the engine and stopped the rotor system using the aircraft's rotor brake. Post-flight inspection revealed a missing tail rotor blade tip cap and weights associated with one tail rotor blade and damage to the tail rotor gearbox fairing.

As the FAA filed it

A BELL 407 HELICOPTER WAS ENROUTE TO AN OFFSHORE LOCATION . AT APPROXIMATELY THREE (3) MINUTES AFTER TAKEOFF ON THE FIRST FLIGHT OF THE DAY, THE PILOT HEARD A "POP" WHICH WAS FOLLOWED BY A VIBRATION HE DIAGNOSED AS EMANATING FROM THE TAIL SECTION OF THE AIRCRAFT. THE PILOT BEGAN A DESCENT FROM CRUISE ALTITUDE OF 1,750 AND HEADED TOWARD A HELIDECK THAT WAS IN THE IMMEDIATE VICINITY. AFTER LANDING AND REDUCING THE ROTOR RPM TO IDLE, THE PILOT NOTED AN INCREASE IN VIBRATION, AT WHICH TIME HE SECURED THE ENGINE AND STOPPED THE ROTOR SYSTEM USING THE AIRCRAFT'S ROTOR BRAKE. POST-FLIGHT INSPECTION REVEALED A MISSING TAIL ROTOR BLADE TIP CAP AND WEIGHTS ASSOCIATED WITH ONE TAIL ROTOR BLADE AND DAMAGE TO THE TAIL ROTOR GEARBOX FAIRING.

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 N457PH · 1

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