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Aviation safety reports, made easier to study

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April 27, 2004 · Bell 407 · N407BP

Hurst, TX

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
April 27, 2004
Injury Outcomes
No injuries (2 uninjured)
Location
Hurst, TX
Aircraft
Bell 407
Tail Number
N407BP
Operator
Bell Training Academy
Injuries
None
Aircraft Damage
Substantial
NTSB Number
FTW04LA117

During a recurrent training flight, the 1,413-hour commercial pilot who was receiving the training, and was at the controls, initiated a full-touchdown practice autorotation in the single engine helicopter. During the landing "flare," just prior to touchdown, the helicopter’s pitch attitude became "excessively" nose high. Subsequently, the tailboom stinger struck the ground, which resulted in structural damage to the tailboom. The 13,200-hour CFI stated that he was "unable to correct the aircraft attitude" before the stinger struck the ground. The helicopter was operating normally during the flight, and post-accident examination of the flight controls did not reveal anomalies that could have contributed to the accident.

NTSB Probable Cause

The student pilot's excessive flare prior to touchdown during the practice autorotation which resulted in the tailboom stinger striking the ground. A contributing factor was the flight instructor's delay to take remedial action.

Full Narrative

On April 27, 2004, at 1130 central daylight time, a Bell 407 helicopter, N407BP, registered to Textron Financial Corp, of Wichita, Kansas, and operated by the Bell Training Academy, of Hurst, Texas, was substantially damaged during a practice autorotation at the Bell Helicopter Flight Training Facility (OTE2), near Hurst, Texas. The flight instructor (CFI) and the commercial pilot who was receiving recurrent training were not injured. Visual meteorological conditions prevailed, and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 instructional flight. The local flight originated from OTE2 at 1030. The 13,200-hour CFI reported on the Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2) that during the flight, the 1,413-hour pilot who was receiving instruction and was at the controls, initiated a practice, full-touchdown autorotation. During the cyclic "flare," just prior to touchdown, the helicopter’s pitch attitude became "excessively" nose high. Subsequently, the tailboom stinger struck the ground. The CFI stated that he was "unable to correct the aircraft attitude" before the stinger struck the ground. Examination of the helicopter by a Federal Aviation Administration inspector, who responded to the site of the accident, revealed that three of the five Thomas couplings on the tail-rotor drive shaft were compressed. Multiple wrinkles were observed along the length of the tail boom. The tail stinger was bent upward. The helicopter was operating normally during the flight, and post-accident examination of the flight controls did not reveal anamalies that could have contributed to the accident.

Flight

Event TypeAccident
Event Time11:30 CDT
Nearest AirportBell Hurst Training Facility (0nm)
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBell 407
Tail NumberN407BP
Aircraft CategoryHeli
DamageSubstantial
OperatorBell Training Academy
Operating RulePart 91
Engines1
Engine TypeTurboshaft
Engine DetailsRolls Royce · 250C47B · Turboshaft · 650
Seats2

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 53 · Second Class · None
Crew 2Age 50 · Second Class · None

Conditions

ConditionsVMC
LightDaylight
Wind250° @ 5 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point52
Altimeter30.27 inHg
Observation Time15:53
Weather SourceWFAC

Appendix: Source Data