MIA99LA107

NTSB accident investigation · Fairchild Hiller FH-1100 · Opp, AL · March 16, 1999

Accident · No injuriesLimited investigationFinal report
Date
March 16, 1999, 10:01 local (16:01 UTC)
Place
Opp, AL
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N547FHFairchild Hiller FH-1100
Weather
Visual (VMC) · Day
Status
Completed · report June 23, 2000
Report
Approved by Office Director
FAA report
19990316002459A
Case key
45941

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

a loss of engine power due to the failure of the engine to transmission drive shaft flex coupling, resulting in an in-flight collision with a vehicle.

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 engine powerHover - in ground effect
Rotor drive system,engine to transmission drive - failure,totalCause
Rotor drive system,engine to transmission drive - corroded
In flight collision with objectHover - in ground effect
Object - vehicle

Analysis

The helicopter had completed a 2-hour aerial application flight and returned to the helipad to refuel and reload. The helipad was a flat bed trailer attached to a truck. After refueling and taking on more chemicals, the pilot reported that when he lifted off the trailer, the helicopter's engine lost power, causing the helicopter to settle downward, resulting in the main rotor blades striking the cab of the truck. Examination of the helicopter revealed the engine to transmission drive shaft flex coupling had failed. Corrosion was found on both flex coupling components.

Factual narrative

On March 16, 1999, about 1001 central standard time, a Fairchild Hiller FH-1100 helicopter, N547FH, operated by Ward Aviation Inc., lost power during liftoff and collided with the cab of a truck near Opp, Alabama. Visual meteorological conditions prevailed at the time, and no flight plan was filed for the 14 CFR Part 137 aerial application flight. The helicopter was substantially damaged. The commercial-rated pilot reported no injuries. The flight was originating at the time.

The helicopter had completed a 2-hour aerial application flight and returned to the helipad to refuel and reload. The helipad was a flatbed trailer attached to a truck. After refueling and taking on more chemicals, the pilot reported that when he lifted off the trailer, the helicopter's engine lost power, causing the helicopter to settle downward, resulting in the main rotor blades striking the cab of the truck.

According to the FAA inspector's statement, "...inspection of the helicopter...revealed failure of the engine to transmission drive shaft flex coupling...physical breakup of the flex coupling with metal particles present. Both flex coupling components were covered with rust. Failure prior to ground impact was evident due to the extensive surface abrasions caused by the failure of the coupling and countinued operation of the engine."

Aircraft

Registration
N547FH
Reported as
Fairchild Hiller FH-1100
Category
Helicopter
Serial number
47
Engine
Allison C-18-250, 317 horsepower, turbo shaft
Damage
Substantial damage
Flight
Aerial application · Part 137
Registered owner
Darrel Ward
Airworthiness certificate
Special, Restricted (Special)
Last inspection
Annual · March 15, 1999 · 10 hours before

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
54
Certificates
Flight instructor, Commercial
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Right
Flight hours
26,000 total · 2,100 in this make and model · 25,000 as pilot in command · 50 in the last 90 days · 40 in the last 30 days · 10 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
0° at 4 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
55 °F, dew point 36 °F
Altimeter
30.00 inHg
Observed at
OZR, 15 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.