ATL89LA100

NTSB accident investigation · Hughes 269C · Bexley, OH · March 13, 1989

Accident · No injuriesLimited investigationFinal report
Date
March 13, 1989, 07:20 local (12:20 UTC)
Place
Bexley, OH
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N300PPHughes 269C
Weather
Visual (VMC) · Day
Status
Completed · report August 2, 1990
Report
Approved by Office Director
FAA report
19890313003519A
Case key
7995

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

The inadequate maintenance inspection of the engine following evidence of previous damage which led to the failure of the no. 1 cylinder exhaust valve.

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.

Loss of engine power(partial) - mech failure/malfCruise - normal
Engine assembly,valve,exhaust - failure,totalCause
Engine assembly - overspeedCause
Engine assembly - previous damageCause
Maintenance,inspection - inadequateCompany maintenance personnelCause
Forced landingDescent - emergency
Hard landingLanding

Analysis

The helicopter was in cruise flight at 500 feet AGL when the engine quit without warning. An autorotation was executed to an open field. The tailboom was severed by the main rotor blades. Post accident examination of the engine revealed the no. 1 cylinder exhaust valve failed. Further investigation revealed the engine had been damaged previously oversped about 60 hours prior the exhaust valve failure. Engine maintenance records contained no evidence of an overspeed inspection but did reveal that the no. 2 cylinder was removed because of oil fouling. The engine was operated two tenths of an hour after replacement of the cylinder and suffered failure of the no. 1 cylinder exhaust valve.

Aircraft

Registration
N300PP
Reported as
Hughes 269C
Category
Helicopter
Serial number
900958
Airframe hours
1,951
Engine
Lycoming HIO-360-D1A, 200 horsepower, reciprocating
Damage
Substantial damage
Flight
Other work use · Part 91
Registered owner
Baumberger, Terry F.
Airworthiness certificate
Standard, Normal
Last inspection
Annual · February 1, 1989 · 75 hours before
Departed
2I4 · Columbus, OH
Destination
2I4

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
29
Certificates
Commercial, Flight instructor
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Helicopter, Airplane
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
4,360 total · 250 in this make and model · 3,000 as pilot in command · 150 in the last 90 days · 25 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
110° at 5 knots
Visibility
7 statute miles
Lowest ceiling
25,000 ft broken
Temperature
28 °F, dew point 25 °F
Altimeter
30.00 inHg
Observed at
CMH, 14 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.