FTW88FA131

NTSB accident investigation · Aerospatiale SA330J · Gulf-Of-Mexico · July 14, 1988

Accident · FatalField investigationFinal report
Date
July 14, 1988, 07:25 local (12:25 UTC)
Place
Gulf-Of-Mexico
Injuries
1 fatal, 1 serious, 14 uninjured
Damage
Destroyed
Phase of flight
Takeoff
Aircraft
N47307Aerospatiale SA330J
Weather
Visual (VMC) · Day
Status
Completed · report January 16, 1990
Report
Approved by Office Director
FAA report
19880714026579A
Case key
22557

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

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Probable cause

None submitted

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.

Loss of control - in flightTakeoff
Rotorcraft flight control,tail rotor control - incorrectFactor
Maintenance,adjustment - improperCompany maintenance personnelFactor
Preflight planning/preparation - inadequatePilot in commandFactor
Directional control - not maintainedPilot in commandCause
In flight collision with terrain/waterTakeoff
Emergency procedure - improperPilot in commandFactor
Terrain condition - waterFactor

Analysis

Drg lift-off from an oil platform in the Gulf of Mexico, the helicopter bgn a slow uncommanded left turn. The plt tried to fly it by lowering the nose & increasing collective. After 2 turns, the helicopter settled & impacted the water in a left bank, nose down attitude. The auto-plt was not disconnected, nor were the floats inflated. No preimpact mech failure was found. Interviews revealed the helicopter was not stabilized in a hover before initiating a takeoff. There was a previous write-up which stated 'a/c requires more right pedal than usual in hover and forward flight.' In responseto this write-up, a mechanic had adjusted a tube which ran rearward from the pedal assembly to the lower portion of the auto-pilot system. The maintenance manual described this tube as being one of the 'semi-fixed' rods. Referring to these rods, the manual cautioned, 'they are adjusted once for all when they are fitted to the aircraft. They must not be adjusted subsequently.'

Aircraft

Registration
N47307
Reported as
Aerospatiale SA330J
Category
Helicopter
Serial number
1402
Airframe hours
4,727
Engine
Turbomeca TURMO IVC, 1,495 horsepower, turbo shaft
Damage
Destroyed
Flight
Part 135
Operator
Petroleum Helicopters
Registered owner
Topspin Data Corp.
Airworthiness certificate
Standard, Normal
Last inspection
Continuous airworthiness · July 9, 1988 · 5 hours before
Destination
Eugene Island, OF

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
47
Certificate
Airline transport
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane, Helicopter
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Right
Flight hours
11,687 total · 2,075 in this make and model · 8,044 as pilot in command · 204 in the last 90 days · 88 in the last 30 days · 3 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
150° at 10 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
84 °F, dew point 75 °F
Altimeter
30.00 inHg

FAA reports on this event · 1

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