LAX88FA140

NTSB accident investigation · Enstrom 280C · Fremont, CA · March 27, 1988

Accident · No injuriesField investigationFinal report
Date
March 27, 1988, 15:45 local (23:45 UTC)
Place
Fremont, CA
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Approach
Aircraft
N5692PEnstrom 280C
Weather
Visual (VMC) · Day
Status
Completed · report July 9, 1990
Report
Approved by Office Director
FAA report
19880327008969A
Case key
25818

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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Probable cause

Failure of the engine to main rotor drive system due to a drive belt slippage caused by a drive pulley worn beyond its service limit. Contributing to the accident was the inadequate factory maintenance manuals which did not provide the serviceable limits for the drive belt pulleys.

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,main rotor driving pulley - wornCause
Maintenance,inspection - information insufficientManufacturerFactor
Rotor system - underspeedCause
Forced landingDescent - emergency
Autorotation - delayedPilot in command
In flight collision with terrain/waterLanding - flare/touchdown
Rotor system - underspeedCause
Proper descent rate - not possible

Analysis

While working in the traffic pattern on a local instructional flight, the CFI noticed the main rotor RPM was below the green arc. He entered an autorotation and tried unsuccessfully to get the rotor RPM back into the green arc. The helicopter collided with the ground during the attempted autorotation with a low main rotor speed. Investigation revealed that the engine drive pulley was worn beyond the factory established limit, which allowed the drive belt to slip. The minimum serviceable wear limit for the drive pulley was not published in the factory maintenance procedures.

Aircraft

Registration
N5692P
Reported as
Enstrom 280C
Category
Helicopter
Serial number
1185
Airframe hours
1,673
Engine
Lycoming HIO-360-E1BD, 205 horsepower, reciprocating
Damage
Substantial damage
Flight
Instructional · Part 91
Operator
Pegasus Aviation Corporation
Registered owner
Joseph R. Reinhard
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · February 29, 1988 · 20 hours before
Departed
PAO · Palo Alto, CA
Destination
PAO

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
31
Certificates
Commercial, Flight instructor
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 1, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
1,701 total · 18 in this make and model · 1,494 as pilot in command · 273 in the last 90 days · 99 in the last 30 days · 3 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
330° at 15 knots, gusting 20
Visibility
50 statute miles
Lowest ceiling
None
Temperature
75 °F, dew point -0 °F
Altimeter
30.00 inHg

FAA reports on this event · 1

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

Other investigations on N5692P · 1

Matched to the same aircraft by N-number and date.