LAX87FA173

NTSB accident investigation · Hughes 369E · Palm Desert, CA · April 11, 1987

Accident · Serious injuriesField investigationFinal report
Date
April 11, 1987, 07:35 local (14:35 UTC)
Place
Palm Desert, CA
Injuries
1 serious, 1 minor
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N5200WHughes 369E
Weather
Visual (VMC) · Day
Status
Completed · report June 7, 1989
Report
Approved by Office Director
FAA report
19870411009089A
Case key
25397

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/malfunctionManeuvering
Rotor drive system,tail rotor gearbox(90 deg) - incorrectCause
Maintenance,compliance with ad - improperOther maintenance personnelCause
Rotor drive system,tail rotor gearbox(90 deg) - fatigueCause
Rotor drive system,tail rotor gearbox(90 deg) - separation
Loss of control - in flightManeuvering
Forced landingDescent - emergency
Autorotation - attemptedPilot in command
Hard landingLanding

Analysis

The helicopter dscndd uncontrolled & crashed in a residential area. After the acdnt, the plt said he agreed to orbit the residence of his pax. At the aprx 135 deg point of a left orbit, he felt 'a bang & severe vibration in the tail.' The plt lost drctnl ctl & the helicopter began spinning to the right. An exam of the tail rotor gear box (t/r gb) assy revealed 3 of 4 t/r gb mounting studs had failed from cyclic fatigue due to bending which had resulted from a loss of clamp-up torque. Subsequently, the lower right ear of the t/r gb (at the lctn of the 4th stud) failed from overload & the t/r gb sepd. Further investigation revealed that 3 washers had been installed on each of the mounting studs, but only one was permitted. The washers were installed during compliance with AD 86-20-07, 78 flt hrs before the acdnt.

Aircraft

Registration
N5200W
Reported as
Hughes 369E
Category
Helicopter
Serial number
0025E
Airframe hours
333
Engine
Allison 250-C20B, 270 horsepower, turbo shaft
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Kensrue Development Corp.
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · January 9, 1987 · 35 hours before
Departed
UDD · Bermuda Dunes, CA
Destination
17L · Hemet, CA

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
65
Certificate
Commercial
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
6,000 total · 111 in this make and model · 5,075 as pilot in command · 16 in the last 90 days · 2 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
210° at 3 knots
Visibility
40 statute miles
Lowest ceiling
18,000 ft broken
Temperature
57 °F, dew point 36 °F
Altimeter
29.00 inHg
Observed at
TRM, 6 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.