LAX91LA382

NTSB accident investigation · Piper PA-28R-200 · Redwood City, CA · September 4, 1991

Accident · Serious injuriesLimited investigationFinal report
Date
September 3, 1991, 19:15 local (Sep 4, 1991, 02:15 UTC)
Place
Redwood City, CA
Injuries
1 serious
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N2080TPiper PA-28R-200
Weather
Visual (VMC) · Day
Status
Completed · report May 3, 1993
Report
Approved by Office Director
FAA report
19910903038419A
Case key
27349

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 fatigue failure of the number two connecting rod and rod cap due to an engine overspeed condition which the rods and rod caps were exposed at some undetermined historical point.

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/malfCruise - normal
Engine assembly,connecting rod cap - fatigueCause
Engine assembly,connecting rod cap - failure,totalCause
Powerplant - overspeedCause
Reason for occurrence undeterminedUnknownCause
Forced landingDescent - emergency
Terrain condition - none suitable
In flight collision with terrain/waterDescent - emergency
Terrain condition - rough/unevenFactor
Visual lookout - not possiblePilot in commandFactor

Analysis

The 400 hour since factory remanufactured engine began to run rough, then it quit with a loud 'bang.' The pilot was attempting to complete a forced landing in a pasture area when the aircraft collided with the ground. Disassembly of the engine revealed that the number two cylinder connecting rod and its associated rod cap had failed. Metallurgical examination of all connecting rods and caps was performed. The #2 rod and cap failed due to a fatigue fracture with an origin on the bore surface. Areas of galling were found on both the rod cap and the connecting rod bore. Cracks were identified within the galled area on the number two connecting rod bore. Examination of the three remaining connecting rods and their caps revealed galled areas within the bores. The metallurgists stated that he had observed similar failures on helicopter piston engines which were known to have had an overspeed.

Aircraft

Registration
N2080T
Reported as
Piper PA-28R-200
Category
Airplane
Serial number
28R-7135024
Airframe hours
3,646
Engine
Lycoming IO-360-CIC, 200 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Crawford, Jeffrey C.
Registered owner
Crawford, Jeffrey C.
Airworthiness certificate
Standard, Normal
Last inspection
Annual · June 21, 1991 · 26 hours before
Departed
SQL · San Carlos, CA
Destination
SNS · Salinas, 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
29
Certificate
Commercial
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
492 total · 393 in this make and model · 307 as pilot in command · 30 in the last 90 days · 7 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
30 statute miles
Lowest ceiling
None
Temperature
70 °F

FAA reports on this event · 1

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