FTW94LA215

NTSB accident investigation · Piper J4A · Granite Shoals, TX · June 30, 1994

Accident · No injuriesLimited investigationFinal report
Date
June 30, 1994, 12:20 local (17:20 UTC)
Place
Granite Shoals, TX
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N30342Piper J4A
Weather
Visual (VMC) · Day
Status
Completed · report January 26, 1995
Report
Approved by Office Director
FAA report
19940630020279A
Case key
19099

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

Fuel system starvation due to the pilot's failure to secure the engine fuel primer. A factor was the lack of suitable terrain for the forced landing.

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 - starvationCause
Fuel system,primer system - not securedCause
Aircraft preflight - inadequatePilot in commandCause
Forced landingDescent - emergency
On ground/water collision with objectLanding - roll
Terrain condition - none suitableFactor
Object - tree(s)

Analysis

The number two and four cylinders were changed on the engine. A ground test run and preflight did not reveal any discrepancies. During the takeoff initial climb, a total loss of engine power occurred. The airplane was approximately 1/4 mile beyond the departure end of the runway where the land merged with water. The forced landing was made on a street where the left wing struck a tree during the landing roll. Examination revealed the fuel primer control was unlocked and the primer was out 1/2 inch. A test run of the engine with the primer in did not disclose any discrepancies.

Factual narrative

On June 30, 1994, at 1220 central daylight time, a Piper J4A, N30342, was substantially damaged during a forced landing. The commercial pilot was not injured. Visual meteorological conditions prevailed for the local maintenance test flight.

The pilot reported that the number two and four cylinders were changed on the engine. Prior to flight no discrepancies were found during a ground operational test run of the engine. During the takeoff initial climb 300 feet above the ground, a total loss of engine power occurred. The airplane was approximately 1/4 mile beyond the departure end of the runway where the land merged with water. A street was selected for the landing. During the landing roll the left wing struck a tree.

The Federal Aviation Administration inspectors' examination of the airplane at the accident site revealed the fuel primer control was unlocked and out one half inch. A test run of the engine with the primer in did not disclose any discrepancies.

Aircraft

Registration
N30342
Reported as
Piper J4A
Category
Airplane
Serial number
4-1170
Airframe hours
1,292
Engine
Continental A-65-8, 65 horsepower, reciprocating
Damage
Substantial damage
Flight
Part 91
Registered owner
Yeilding, Brooks
Airworthiness certificate
Standard, Normal
Last inspection
Annual · June 8, 1994 · 2 hours before
Departed
2KL · Sunrise Beach, TX

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
65
Certificate
Commercial
Airplane ratings
Single-engine land, Multi-engine land
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
1,780 total · 1 in this make and model · 1,684 as pilot in command

Weather

Conditions
Visual (VMC) · Day
Wind
120° at 7 knots
Visibility
12 statute miles
Lowest ceiling
None
Temperature
88 °F

FAA reports on this event · 1

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