FTW85FA032

NTSB accident investigation · Bell 206B · Lane City, TX · October 30, 1984

Accident · Serious injuriesField investigationFinal report
Date
October 30, 1984, 09:45 local (15:45 UTC)
Place
Lane City, TX
Injuries
1 serious, 2 minor
Damage
Destroyed
Phase of flight
Enroute
Aircraft
N1074GBell 206B
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
FAA report
19841030060599A
Case key
21501

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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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.

Airframe/component/system failure/malfunctionCruise - normal
Rotor drive system,tail rotor gearbox(90 deg) - separationCause
Maintenance,compliance with ad - not followedCompany maintenance personnelFactor
Information unavailableCompany maintenance personnelFactor
Rotor system,tail rotor blade - corrodedCause
Loss of control - in flightManeuvering - turn to landing area (emergency)
Remedial action - attemptedPilot in command
In flight collision with terrain/waterDescent - uncontrolled
Terrain condition - none suitableFactor

Analysis

During cruise at 600 ft AGL a bang was heard & acft experienced a vibration. When turning toward a fld to land a second bang was heard & vibration ceased. However, an uncommanded rt yaw was experienced & the nose began to tuck under. Acft contacted terrain despite remedial action attempt by plt. Investigation revealed tail rotor ass'y separated from acft inflt. Lab exam revealed gear box attachment studs failed due to low cycle fatigue. Tail rotor blade, s/n TCT-7478, had aprx 60% of phenolic tip block missing & 3 aluminum rivets missing from titanium skin. No bonding material was visible on interior blade skin. Acft was operated in a salt water envir. On 4/17/82, AD 82-17-04 was issued req inspection of tail rotor ass'y specifically for tip block security, void & retention every 7 days. AD revised (AD 82-17-04,R1) req compliance not to exceed 25 hr intervals. On 9/3/84 revision 2 req inspection reverting back to 7 day interval. Operator had not received revision 2 & last inspection performed on 10/4/84 aprx 21 hrs prior to accident.

Aircraft

Registration
N1074G
Reported as
Bell 206B
Category
Helicopter
Serial number
2865
Airframe hours
3,138
Engine
Allison 250-C20, 317 horsepower, turbo shaft
Damage
Destroyed
Flight
Part 135
Registered owner
Evergreen Ventures Inc.
Airworthiness certificate
Standard, Normal
Last inspection
AAIP · September 27, 1984 · 38 hours before
Departed
5RS · Wharton, TX
Destination
B-52 · Matagorda 520, GM
Flight plan
Company VFR

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
49
Certificate
Commercial
Airplane ratings
Single-engine land
Instrument ratings
Airplane, Helicopter
Medical
Class 2, Valid Medical--w/ waivers/lim

Weather

Conditions
Visual (VMC) · Day
Wind
70° at 5 knots
Visibility
7 statute miles
Lowest ceiling
6,000 ft broken
Temperature
79 °F, dew point 75 °F
Altimeter
30.00 inHg
Observed at
PSX, 31 nm away

FAA reports on this event · 1

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