FTW85FA188

NTSB accident investigation · Bell UH-1B · Boutte, LA · April 15, 1985

Accident · Serious injuriesField investigationFinal report
Date
April 15, 1985, 08:30 local (14:30 UTC)
Place
Boutte, LA
Injuries
1 serious
Damage
Destroyed
Phase of flight
Maneuvering
Aircraft
N2252ABell UH-1B
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
FAA report
19850415014959A
Case key
21541

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

On this page

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 power(partial) - mech failure/malfHover
Fuel system,fuel control - incorrectCause
Maintenance,adjustment - improperCompany maintenance personnelCause
Turboshaft engine,gas generator - dirty(foggy)Cause
Bleed air system,actuator - loss,partialCause
Maintenance,inspection - poorCompany maintenance personnelCause
Turboshaft engine,free turbine governor - incorrectCause
Maintenance,adjustment - improperCompany maintenance personnelCause
Forced landingDescent - emergency
In flight collision with objectDescent - emergency
Object - tree(s)Cause
Terrain condition - none suitableCause
In flight collision with terrain/waterDescent - emergency
Terrain condition - high vegetationFactor
Terrain condition - softFactor

Analysis

The plt had stabilized acft in a 125' hover, prior to picking up a load, when the eng spooled down and acft entered talltrees with low rotor RPM and pitched nose down as it descended thru the trees. Ground witnesses heard 2 loud 'bangs' prior to the acft entering the trees. Investigation of the eng revealed that the fuel control and pwr governor schedules were set above the specified limits. These settings would increase fuel flow and eng pwr available while decreasing operating temperatures; however, it also reduces the eng surge margin and increases the possibility of eng surge (comressor stall) and pwr drop. In addition, the compression was found dirty and the bleed air line was loose, which would have further reduced the surge margin. The nature of the long line operation and the surrounding tall trees precluded the successful completion of the eng out emergency procedure.

Aircraft

Registration
N2252A
Reported as
Bell UH-1B
Category
Helicopter
Serial number
378
Airframe hours
8,696
Engine
Lycoming T-53-L-11D, 1,100 horsepower, turbo shaft
Damage
Destroyed
Flight
Other work use · Part 133
Registered owner
J. Jaws Helicopter Service
Airworthiness certificate
Special, Restricted (Special)
Last inspection
100 hour · March 31, 1985 · 29 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
42
Certificate
Commercial
Airplane ratings
Single-engine sea, Single-engine land
Instrument ratings
Helicopter, Airplane
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Right
Flight hours
6,317 total · 1,200 in this make and model · 158 in the last 90 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Visibility
5 statute miles
Lowest ceiling
None

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 N2252A · 1

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