LAX84FA046

NTSB accident investigation · Piper PA38-112 · Corona, CA · November 5, 1983

Accident · No injuriesField investigationFinal report
Date
November 4, 1983, 16:25 local (Nov 5, 1983, 00:25 UTC)
Place
Corona, CA
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N2556DPiper PA38-112
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
FAA report
19831104057839A
Case key
23901

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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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) - nonmechanicalTakeoff - initial climb
Fuel system,carburetor - improperCause
Maintenance,annual inspection - inadequatePilot in commandCause
Fuel system,pump - contaminationFactor
Fuel system,tank - contaminationFactor
Forced landingLanding - flare/touchdown
Complete gear collapsedLanding - flare/touchdown
Landing gear,main gear - overloadFactor
Landing gear,nose gear - overloadFactor

Analysis

The acft landing gear collapsed during an off rwy but on arpt forced landing. The pilot had just completed the annual inspection and was testing the acft. At 150 ft AGL during takeoff the engine quit. The plt landed on rough terrain ABOUT1/4 mile west of the departure end of the rwy. The post accident investigation revealed minor foreign contaminates in both fuel tanks. The main fuel line to the carburetor inlet union did not contain any fuel. Fuel however was found in the gascolator bowl. The electric fuel boost pump filter contained extensive foreign contaminates. The carburetor and fuel pump were bench tested and the carburetor bowl flooded at an input pressure of 3.8 # PSI. At 5# PSI the fuel level in the bowl should be about 1/2 inch from the bowl top when the float shuts off the fuel. The float assembly did not submerge when placed in fuel. The float level was set at 8/32 inch. The service limit is 7/32 inch. According to a testing technician the failure of the float was probably due to contamination in the float valve seat.

Aircraft

Registration
N2556D
Reported as
Piper PA38-112
Category
Airplane
Serial number
38-79A0371
Airframe hours
1,350
Engine
Lycoming O-235-L2C, 112 horsepower, reciprocating
Damage
Substantial damage
Flight
Other work use · Part 91
Operator
Omni Aviation
Registered owner
Kenneth I. Crowder
Airworthiness certificate
Standard, Normal
Last inspection
Annual · November 3, 1983 · 1 hours before
Airport
L66 · Corona Municipal, runway 25, 3,200 × 60 ft, asphalt

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
Private
Airplane ratings
Single-engine land
Medical
Class 3, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
145 total · 2 in this make and model · 107 as pilot in command · 16 in the last 90 days · 3 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
240° at 10 knots
Visibility
6 statute miles
Lowest ceiling
None
Altimeter
29.00 inHg
Observed at
CNO, 5 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.