FTW85FA265

NTSB accident investigation · Aerospatiale AS35OD · Dallas, TX · June 26, 1985

Accident · FatalField investigationFinal report
Date
June 26, 1985, 11:40 local (16:40 UTC)
Place
Dallas, TX
Injuries
1 fatal
Damage
Destroyed
Phase of flight
Enroute
Aircraft
N148BHAerospatiale AS35OD
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
FAA report
19850626027969A
Case key
21560

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,engine to transmission drive - failure,totalCause
Maintenance,inspection - inadequateCompany maintenance personnelCause
Forced landingDescent - emergency
Loss of control - in flightManeuvering
Emergency procedure - not possiblePilot in commandFactor
In flight collision with objectManeuvering
Object - tree(s)Factor

Analysis

The eng to transmission short shaft became disconnected in flt. This resulted in complete loss of pwr to the main rotor assembly. However, the tail rotor assembly was still being powered by the eng. Upon collective pitch application to stop the descent the acft yawed about 90 degs to the right and also rolled about 70 degs to the right and impacted the trunk of a large tree. This impact resulted in disintegration of the helicopter. Investigation revealed that cotter pins had not been installed in the bolts which connect the forward end of the short shaft to the flexible coupling at the transmission. It also revealed that a required 30 hr recurring inspection had not been completed and was 15.9 hrs overdue. The completion of this required inspection would have revealed that the cotter pins were missing.

Aircraft

Registration
N148BH
Reported as
Aerospatiale AS35OD
Category
Helicopter
Serial number
1274
Airframe hours
1,256
Engine
Lycoming LTS-101-600A2, 531 horsepower, turbo shaft
Damage
Destroyed
Flight
Positioning · Part 91
Registered owner
Cia Machinery, Inc.
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · May 25, 1985 · 55 hours before
Departed
DAL · Dallas, TX
Destination
Lancaster, TX

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
41
Certificates
Flight instructor, Commercial
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Helicopter
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Right
Toxicology
Performed
Flight hours
7,044 total · 166 in this make and model

Weather

Conditions
Visual (VMC) · Day
Wind
180° at 14 knots
Visibility
15 statute miles
Lowest ceiling
3,000 ft broken
Temperature
86 °F, dew point 68 °F
Altimeter
29.00 inHg
Observed at
DAL, 16 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.