FTW92LA040

NTSB accident investigation · Bell 206L-3+ · Arlington, TX · December 10, 1991

Accident · No injuriesLimited investigationFinal report
Date
December 10, 1991, 08:55 local (14:55 UTC)
Place
Arlington, TX
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N2770XBell 206L-3+
Weather
Visual (VMC) · Day
Status
Completed · report June 30, 1993
Report
Approved by Office Director
FAA report
19911210063059A
Case key
18420

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

The helicopter's autorotational landing performance capability was exceeded. Factors were the proper descent rate was not possible for the PIC and sufficient information from the manufacturer was not provided.

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.

Hard landingLanding - flare/touchdown
Emergency procedure - simulatedPilot in command
Autorotation - performedPilot in command
Aircraft performance,landing capability - exceededCause
Proper descent rate - not possiblePilot in commandFactor
Information insufficientManufacturerFactor
Misc rotorcraft,tail boom - buckled
Rotor drive system,tail rotor drive shaft - separation

Analysis

The experimental certificated helicopter was being test flown as part of the height velocity diagram development for the 206L4 certification program. The test pilot was conducting aborted takeoffs when at 30 feet and 50 knots he initiated an autorotation. The collective was lowered slightly and a high descent rate occurred. During the descent the main rotor RPM decreased and the helicopter landed hard resulting in tailboom buckling and separation of the tail rotor drive shaft. The pilot's application of collective before touchdown did not arrest the descent rate.

Aircraft

Registration
N2770X
Reported as
Bell 206L-3+
Category
Helicopter
Serial number
51022
Airframe hours
3,577
Engine
Allison 250C-30P, 650 horsepower, turbo shaft
Damage
Substantial damage
Flight
Part 91
Operator
Bell Helicopter Textron
Registered owner
Bell Helicopter Textron
Airworthiness certificate
Special, Experimental (Special)
Last inspection
100 hour · August 14, 1991 · 53 hours before
Airport
F54 · Arlington Municipal, runway 16, 4,000 × 100 ft, asphalt

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
53
Certificates
Commercial, Flight instructor
Airplane ratings
Single-engine land
Instrument ratings
Helicopter, Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Right
Flight hours
8,200 total · 100 in this make and model · 8,000 as pilot in command · 50 in the last 90 days · 20 in the last 30 days · 2 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
12 statute miles
Lowest ceiling
None
Temperature
52 °F, dew point 46 °F
Altimeter
30.00 inHg
Observed at
DFW, 10 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.