DFW08IA045

NTSB incident investigation · Bell 407 · Hig Island A595 · December 15, 2007

Incident · No injuriesIncident investigationFinal report
Date
December 15, 2007, 14:58 local (20:58 UTC)
Place
Hig Island A595
Injuries
2 uninjured
Damage
No damage
Phase of flight
Enroute
Aircraft
N407AKBell 407
Weather
Visual (VMC) · Day
Status
Completed · report March 31, 2008
Report
Approved by Office Director
Parties
Baton Rouge, Lousiana
FAA report
20071215829179I
Case key
67261

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the incident.

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Probable cause

The NTSB’s determination of the probable cause, and any contributing factors.

The loss of tail rotor effectiveness for undetermined reasons.

Analysis

During cruise flight, the commercial pilot experienced a violent vibration in the airframe followed by a loud "pop" and the helicopter began to yaw to the right. The pilot attempted to correct the adverse yaw but could not regain tail rotor control. The pilot deployed the floatation system and performed an autorotation onto the water. Both pilot and passenger were able to egress the helicopter without incident and entered a life raft. While awaiting rescue the pilot visually inspected the helicopter and could observe no damage or malfunction. A US Coast Guard helicopter crew rescued the pilot and passenger from the water. Prior to recovery, the helicopter capsized due to the rough seas, sank and was not recovered.

Factual narrative

On December 15, 2007, approximately 1458 central standard time, a single-engine Bell 407 helicopter, N407AK, registered to and operated by Rotorcraft Leasing Company LLC, lost tail rotor control while in cruise flight over the Gulf of Mexico approximately 98-nautical miles off the coast of Texas. The commercial pilot successfully autorotated the helicopter to the ocean. The pilot and his passenger were able to enter a life raft and were not injured. A visual flight rules flight plan was filed and visual meteorological conditions prevailed for the 14 Code of Federal Regulations Part 135 on-demand air taxi flight. The flight originated at 1453 from offshore platform High Island A573A, and was bound for offshore platform High Island A376, in the Gulf of Mexico.

On a NTSB Form 6120, the 2,075-hour pilot stated that during cruise flight, he experienced a violent vibration in the airframe. Within a few seconds a noise similar to a loud "pop" was heard and the helicopter began to yaw to the right. The pilot attempted to correct the adverse yaw but could not regain control of the helicopter. Rather than continue flight or attempt a platform landing with a loss of tail rotor effectiveness, the pilot elected to perform an autorotation in the Gulf of Mexico. A distress message was transmitted and the emergency floatation system was activated prior to landing. Once successfully landed, the pilot radioed a position report and shutdown the helicopter. The life raft was deployed and both pilot and passenger successfully egressed the helicopter. While waiting for the US Coast Guard, the pilot visually inspected the helicopter and could observe no damage or malfunction. A Coast Guard helicopter crew recovered both personnel.

The helicopter was capsized due to swells in excess of 15 feet, sank and was not recovered.

At 1452 weather reported at Scholes International Airport, Galveston, Texas, approximately 105 nm northeast was winds from 320 degrees at 21 knots gusting to 27 knots, temperature 63 degrees Fahrenheit, and a barometric pressure of 29.98 inches of Mercury.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Airframe/component/system failure/malfunctionCruise
Rotorcraft flight control,tail rotor control - malfunctionCause
Loss of tail rotor effectiveness - encounteredPilot in command
Forced landingDescent - emergency
Terrain condition - water
Emergency floats - activatedPilot in command
On ground/water encounter with weatherLanding
Weather condition - other

Aircraft

Registration
N407AK
Reported as
Bell 407
Category
Helicopter
Serial number
53269
Airframe hours
3,972
Engine
Rolls-Royce 250-C47B, 650 horsepower, turbo shaft
Damage
No damage
Flight
Part 135
Registered owner
Rotorcraft Leasing Compnay, LLC
Airworthiness certificate
Standard, Normal
Last inspection
AAIP · December 1, 2007
Departed
A573 · Hi A573a, GM
Destination
A376 · Hi A376, GM
Flight plan
VFR

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
28
Injuries
None
Certificates
Flight instructor, Commercial
Instrument ratings
Helicopter
Medical
Class 2, With waivers/limitations
Last flight review
October 1, 2007
Seat
Right
Flight hours
2,075 total · 84 in this make and model · 1,991 as pilot in command · 179 in the last 90 days · 54 in the last 30 days · 6 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
320° at 21 knots, gusting 27
Visibility
10 statute miles
Lowest ceiling
None
Temperature
63 °F, dew point 43 °F
Altimeter
29.97 inHg
Observed at
KGLS, 105 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.