FTW90LA102

NTSB accident investigation · Piper PA-32-260 · Tulsa, OK · April 27, 1990

Accident · Minor injuriesLimited investigationFinal report
Date
April 27, 1990, 09:27 local (14:27 UTC)
Place
Tulsa, OK
Injuries
1 minor
Damage
Destroyed
Phase of flight
Approach
Aircraft
N7732JPiper PA-32-260
Weather
Visual (VMC) · Day
Status
Completed · report January 23, 1992
Report
Approved by Office Director
FAA report
19900427016659A
Case key
23126

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

An engine failure due to a disconnect in the magneto drive train caused by the crankshaft gear not being properly installed and secured during a recent engine overhaul.

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(total) - mech failure/malfApproach - faf/outer marker to threshold (ifr)
Ignition system,magneto - disconnectedCause
Accessory drive assy,drive gear - not securedCause
Maintenance,overhaul - improperOther maintenance personnelCause
Forced landingApproach - faf/outer marker to threshold (ifr)
In flight collision with objectApproach - faf/outer marker to threshold (ifr)
Terrain condition - none suitableFactor
Object - tree(s)

Analysis

While on final, the engine quit without warning and the pilot was forced to execute a forced landing into a heavily wooded bird sanctuary. Examination of the engine revealed that the crankshaft gear attachment bolt was loose with 0.196 inches of play and the dowel pin was sheared. Gear installation instructions called for the gear to be seated with a drift and hammer with no more than 0.001 inches of clearance. Otherwise, the dowel pin would be offset and work. Both the bolt and the dowel pin showed evidence of working. Shearing of the crankshaft dowel pin would have released the gear to rotate about the bolt, thus disconnecting the gear and the idler gears which transmitted torque to the magnetos. Secondary damage was observed in the left magneto. Maintenance records indicated that the engine had been overhauled 88.7 hours prior to the accident.

Aircraft

Registration
N7732J
Reported as
Piper PA-32-260
Category
Airplane
Serial number
32-1135
Airframe hours
6,106
Engine
Lycoming O-540-E4B5, 260 horsepower, reciprocating
Damage
Destroyed
Flight
Part 135
Operator
Martinaire
Registered owner
Galhoun, John L
Airworthiness certificate
Standard, Utility; Standard, Normal
Last inspection
AAIP · April 23, 1990 · 18 hours before
Departed
DAL · Dallas, TX
Flight plan
IFR
Airport
TWL · Tulsa Int., runway 17R, 6,101 × 150 ft, concrete

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
68
Certificates
Flight instructor, Commercial
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Invalid Medical for flight
Seat
Left
Flight hours
18,000 total · 3,000 in this make and model · 6,000 as pilot in command · 210 in the last 90 days · 70 in the last 30 days · 4 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
180° at 8 knots
Visibility
10 statute miles
Lowest ceiling
2,000 ft broken
Temperature
64 °F, dew point 59 °F
Altimeter
29.00 inHg
Observed at
TUL

FAA reports on this event · 1

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