MIA92LA111

NTSB accident investigation · Bell UH-1B · La Belle, FL · April 22, 1992

Accident · Serious injuriesLimited investigationFinal report
Date
April 22, 1992, 07:10 local (11:10 UTC)
Place
La Belle, FL
Injuries
1 serious
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N4028FBell UH-1B
Weather
Visual (VMC) · Day
Status
Completed · report August 26, 1993
Report
Approved by Office Director
FAA report
19920422015369A
Case key
33085

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

Improper preflight by the pilot-in-command, in his failure to identify a crack in a brazed area surrounding an attach point on the air diffuser. Contributing to the accident following the loss of engine power was obstacles that were ahead of the flight path.

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/malfManeuvering - aerial application
Bleed air system,fittings - fatigue
Aircraft preflight - inadequatePilot in commandCause
Bleed air system,fittings - failure,total
Hard landingLanding - flare/touchdown
Unsuitable terrain or takeoff/landing/taxi area - encounteredPilot in commandFactor
Roll overOther
Nose overOther

Analysis

The plt stated that the flt path of the helicopter was perpendicular to power lines that were ahead. The flight continued and he further stated that he heard a loud explosion & the eng quit. He pulled the collective control & cleared the power lines then lowered it, & prior to impact with the ground, pulled the collective control to cushion the impact. The helicopter landed hard, bounced, touched down, rolled over on the lt side, then nosed over & came to rest inverted. A small fire was extinguished by several individuals who responded to the accident site. The eng was removed & sent to the manufacturer's facility for examination. Exam of the eng revealed that a mounting boss on the air diffuser failed due to fatigue. The line attached to the boss was the interstage bleed air line. Also, a power turbine blade failed due to fatigue. Review of the eng logbooks revealed that this eng was removed from another helicopter & installed in this helicopter 6 days prior to the accident. The eng had accumulated about 10 hrs since then & 703 hrs since major overhaul. According to the eng daily inspection checklist, the air diffuser external vane brazements should be checked for cracks.

Aircraft

Registration
N4028F
Reported as
Bell UH-1B
Category
Helicopter
Serial number
62-1948HC
Airframe hours
6,979
Engine
Lycoming TH53-L110, 1,100 horsepower, turbo shaft
Damage
Substantial damage
Fire
On-Ground
Flight
Aerial application · Part 137
Operator
Colony Services, Inc.
Registered owner
Helicorp, Inc.
Airworthiness certificate
Special, Restricted (Special)
Last inspection
Annual · March 27, 1992 · 31 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
47
Certificates
Commercial, Private
Airplane ratings
Multi-engine land, Single-engine land
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
17,000 total · 7,500 in this make and model · 16,800 as pilot in command · 75 in the last 90 days · 25 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Visibility
10 statute miles
Lowest ceiling
None
Temperature
70 °F

FAA reports on this event · 1

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