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NTSB Report

May 6, 2019 · Bell 47G 2 · N5990

Denton, TX

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
May 6, 2019
Injury Outcomes
No injuries (2 uninjured)
Location
Denton, TX
Aircraft
Bell 47G 2 (1992)
Tail Number
N5990
Injuries
None
Aircraft Damage
Substantial
NTSB Number
GAA19CA250

The student pilot reported that he hovered the helicopter to the parking pad and landed with the helicopter's nose facing north. The skid placement on the parking pad was incorrect, and the flight instructor directed the student to reposition the helicopter about 3 ft to the left. The student brought the helicopter to a hover and repositioned it 3 ft to the left. However, before the student established a descent and landed, the helicopter encountered a tailwind gust. The nose pitched down, the rotor rpm decreased, and the helicopter traveled about 75 ft forward. The skids contacted the ground hard, and the helicopter came to an abrupt stop, upright and facing downslope. The main rotor blades struck the tail rotor drive shaft and the tailboom. The tail rotor gear box and the tail rotor separated from the helicopter. The helicopter sustained substantial damage to the tail rotor drive system, the tailboom, and the main rotor blades. The pilot reported that there were no mechanical malfunctions or failures with the helicopter that would have precluded normal operation. The airport's METAR reported that, about the time of the accident, the wind was from 180° at 15 knots and that the cloud layer was broken at 800 ft.

NTSB Probable Cause

The flight instructor's improper decision to instruct the student pilot to establish a hover and reposition the helicopter with a tailwind, which resulted in the student pilot's loss of pitch control.

Full Narrative

The student helicopter pilot reported that he hovered to the parking pad and landed with the nose of the helicopter facing north. The skid placement on the parking pad was incorrect, and the instructor directed the student to reposition the helicopter about 3ft to the left. The student brought the helicopter to a hover and repositioned the helicopter 3ft to the left. However, before the student established a descent and landed, the helicopter encountered a tailwind gust. The nose pitched down, the rotor rpm decreased, and the helicopter traveled about 75ft forward. The skids contacted the ground hard, and the helicopter came to an abrupt stop, upright and facing downslope. The main rotor blades struck the tail rotor drive shaft and the tailboom. The tail rotor gear box and the tail rotor separated from the helicopter. The helicopter sustained substantial damage to the tail rotor drive system, the tailboom, and the main rotor blades. The airport's Meteorological Aerodrome Report, about the time of the accident, reported that the wind was from 180° at 15 knots, and the cloud layer was broken at 800ft. The predominant wind about 30 minutes prior to the accident was from 170° at 13 knots. One-hour prior, the wind was from 160 at 09 knots. The pilot reported that there were no mechanical malfunctions or failures with the helicopter that would have precluded normal operation.

Flight

Event TypeAccident
Event Time10:20 CDT
Nearest AirportDenton Enterprise (0nm NW)
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBell 47G 2
Tail NumberN5990
Aircraft CategoryHeli
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · VO-435-A1 · Reciprocating · 270
Seats3

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 54 · Third Class · None
Crew 2Age 61 · First Class · None

Conditions

ConditionsVMC
LightDaylight
Wind180° @ 15 kt
Visibility10 sm
CeilingBroken clouds 8000 ft
Temperature / Dew Point63 F
Altimeter29.95 inHg
Observation Time15:28
Weather SourceWFAC

Appendix: Source Data