FTW86FA085

NTSB accident investigation · Bell 206B · Pine Spring, TX · May 12, 1986

Accident · FatalField investigationFinal report
Date
May 12, 1986, 17:45 local (23:45 UTC)
Place
Pine Spring, TX
Injuries
2 fatal
Damage
Destroyed
Phase of flight
Approach
Aircraft
N27785Bell 206B
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
FAA report
19860512082049A
Case key
21903

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.

Airframe/component/system failure/malfunctionApproach - vfr pattern - downwind
Rotor drive system,engine to transmission drive - disconnectedCause
Maintenance,installation - improperOther maintenance personnelCause
Improper use of procedureOther maintenance personnelCause
Forced landingManeuvering - turn to landing area (emergency)
Autorotation - initiated
In flight collision with terrain/waterLanding
Weather condition - turbulenceFactor
Weather condition - gustsFactor
Weather condition - high density altitudeFactor
Rotor rpm - not maintained
Flare - not possible

Analysis

The helicopter was on a flt to a site nr guadalupe pass, an area known for erratic & gusty wnds. As the plt was on an apch to a hi meadow (elev aprx 5460'), the helicopter entered a dscnt & crashed well short of the intended lndg area. A witness rprtd the main rotor RPM slowed & the rotor blades coned prior to impact. There was evidence the helicopter impacted in a lvl attitude & at a high rate of dscnt. An inv revealed that a coupling on the eng-to-main transmission drive shaft had become disconnected. There was evidence that the male driveshaft coupling was not properly secured to the flange on the main rotor driveshaft's eng end. Eight days prior to the acdnt, an air cond sys was installed on the helicopter. This would have reqd that a drive shaft coupling be disconnected. There was evidence that the self locking nuts were reused when the coupling was reconnected.

Aircraft

Registration
N27785
Reported as
Bell 206B
Category
Helicopter
Serial number
2800
Airframe hours
2,415
Engine
Allison 250-C20B, 317 horsepower, turbo shaft
Damage
Destroyed
Flight
Part 135
Registered owner
Lone Star Helicopters Inc
Airworthiness certificate
Standard, Normal
Last inspection
Continuous airworthiness · April 28, 1986 · 11 hours before
Departed
Pecos, TX

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
54
Certificates
Commercial, Airline transport, Flight instructor
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane, Helicopter
Medical
Class 1, Valid Medical--w/ waivers/lim
Seat
Right
Toxicology
Performed
Flight hours
5,400 total · 1,100 in this make and model · 5,230 as pilot in command · 8 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
0° at 16 knots, gusting 34
Visibility
50 statute miles
Lowest ceiling
None
Temperature
81 °F

FAA reports on this event · 1

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