SEA83FA135

NTSB accident investigation · Enstrom 280C · Kent, WA · June 28, 1983

Accident · Minor injuriesField investigationFinal report
Date
June 27, 1983, 17:44 local (Jun 28, 1983, 00:44 UTC)
Place
Kent, WA
Injuries
1 minor, 1 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N652HEnstrom 280C
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
FAA report
19830627027169A
Case key
39619

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/malfunctionCruise - normal
Rotor drive system,tail rotor gearbox(90 deg) - wornCause
Maintenance,lubrication - inadequateOther maintenance personnelCause
Rotor drive system,tail rotor gearbox(90 deg) - otherCause
Loss of control - in flightCruise
Directional control - not possiblePilot in commandFactor
Forced landingLanding - flare/touchdown
Autorotation - performedPilot in commandFactor
In flight collision with terrain/waterLanding - flare/touchdown

Analysis

During a traffic reporting flt for a radio station, the plt noted the onset of a severe vibration which he felt through the antitorque pedals. He stated that within seconds, the helicopter lost directional control & began a rapid, uncontrolled spin to the right. Reportedly, the helicopter tumbled out of control for a time. However, the plt was able to regain partial control as it rolled thru a relatively upright attitude. Before crashing, the rate of descent was slowed with full collective & a rotating impact occurred in a horizontal attitude. An investigation revealed the tail rotor drive shaft spline coupling, pn 28-13609, had become worn. The teeth of the coupling were worn away & there was iron oxide & carbonized lubricant within the coupling. The splined male end of the coupling would rotate within the splined female housing. It had accumulated 149.1 hrs since lubricated. The lubrication chart & check sheet (pages MM-3-5 & MM-3-6 of the maintenance manual) show that the coupling should be lubed at 100 hr intervals

Aircraft

Registration
N652H
Reported as
Enstrom 280C
Category
Helicopter
Serial number
1102
Airframe hours
3,362
Engine
Lycoming HIO-360-E1BD, 205 horsepower, reciprocating
Damage
Substantial damage
Flight
Aerial observation · Part 91
Registered owner
Paul W. Brendle, II
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · May 27, 1983 · 96 hours before
Departed
BFI · Seattle, WA

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
36
Certificate
Commercial
Airplane ratings
Single-engine land
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
7,176 total · 5,740 in this make and model · 6,025 as pilot in command · 375 in the last 90 days · 5 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
310° at 10 knots
Visibility
20 statute miles
Lowest ceiling
None
Altimeter
30.00 inHg
Observed at
RNT, 7 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.