GAA19CA216

NTSB accident investigation · Bell 47G · Donna, TX · April 17, 2019

Accident · No injuriesData collectionFinal report
Date
April 17, 2019, 11:08 local (16:08 UTC)
Place
Donna, TX
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N96671Bell 47G
Defining event
Maneuvering-low-alt flying: Low altitude operation/event
Weather
Visual (VMC) · Day
Status
Completed · report November 6, 2019
Report
Approved by Office Director
NTSB office
General Aviation Accidents
Parties
FAA
FAA report
20190417010829A
Case key
99288

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

On this page

Probable cause

The pilot's failure to maintain altitude during an agricultural application flight.

Findings · 3

NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.

Performance/control parameters: altitudeAircraft › Aircraft oper/perf/capability · Not attained/maintainedBell 47G-3B-1: 2 casesAll aircraft: 1,310 casesProbable cause
Use of equip/info: aircraft controlPersonnel issues › Task performance · PilotBell 47G-3B-1: 6 casesAll aircraft: 9,295 casesProbable cause
Wind: gustsEnvironmental issues › Conditions/weather/phenomena · Effect on operationBell 47G-3B-1: 1 caseAll aircraft: 1,199 casesProbable cause

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

Analysis

The helicopter pilot reported that, during an agricultural application flight and while heading east about 3 ft above ground level, the "wind suddenly shifted, a gust of wind [came] from the west," and the helicopter "settled." The pilot increased power and raised the collective, but the helicopter impacted terrain. The helicopter sustained substantial damage to the fuselage and tailboom. The pilot reported that there were no preaccident mechanical malfunctions or failures with the helicopter that would have precluded normal operation. The pilot further reported that the helicopter was equipped with a muffler, which he believed adversely affected the engine's performance. However, correspondence with the helicopter's certificate holder stated that there would "be no reduction of horsepower with the muffler installed if done as per the instructions per the STC [supplemental type certificate]." An automated weather observation station located 5 nautical miles east of the accident site reported that, about 8 minutes before the accident, the wind was from 180° at 16 knots, gusting to 25 knots and that, about 32 minutes after the accident, the wind was from 180° at 16 knots, gusting to 26 knots.

Factual narrative

The helicopter pilot reported that, during an aerial application flight with an easterly heading, about 3 feet above ground level, the "wind suddenly shifted, a gust of wind [came] from the west" and the helicopter "settled." The pilot increased power and raised the collective but the helicopter impacted the terrain. The helicopter sustained substantial damage to the fuselage and tail boom. The pilot reported that there were no preaccident mechanical malfunctions or failures with the helicopter that would have precluded normal operation. The pilot further reported that the helicopter was equipped with a muffler, which he believed adversely affected engine's performance. Correspondence with the certificate holder of the helicopter, "determined to be no reduction of horsepower with the muffler installed if done as per the instructions per the STC." The automated weather observation station located 5 NM east of the accident, reported that, about 8 minutes before the accident, the wind was from 180° at 16 knots, gusting to 25 knots. The same automated station reported that, about 32 minutes after the accident, the wind was from 180° at 16 knots, gusting to 26 knots.

Aircraft

Registration
N96671
Reported as
Bell 47G (3B1)
Category
Helicopter
Serial number
3539
Built
1967
Engine
Lycoming VO-435-A1F, 265 horsepower, reciprocating
Damage
Substantial damage
Flight
Aerial application · Part 137
Operator
Hendrickson Flying Service
Registered owner
Turnquist Lee W
Airworthiness certificate
Standard, Normal; Special, Restricted (Special)
Departed
TXW · Weslaco, TX
Destination
TXW · Weslaco, TX
Equipment
ADS-B

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
55
Injuries
None
Certificate
Commercial
Medical
Class 2, With waivers/limitations
Last flight review
June 14, 2017
Seat
Left
Flight hours
12,500 total · 6,000 in this make and model · 12,100 as pilot in command · 5 in the last 90 days · 5 in the last 30 days · 3 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
180° at 16 knots, gusting 25
Visibility
7 statute miles
Lowest ceiling
1,900 ft broken
Temperature
82 °F, dew point 72 °F
Altimeter
29.80 inHg
Observed at
KTXW, 5 nm away

Docket · 3

The files NTSB released with the investigation on May 15, 2019, on NTSB’s docket system: statements, records, photos and specialists’ reports. 953 KB in all.

FAA reports on this event · 1

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

Other investigations on N96671 · 1

Matched to the same aircraft by N-number and date.