LAX98LA181

NTSB accident investigation · Piper J3C-65 · Mesa, AZ · May 9, 1998

Accident · No injuriesLimited investigationFinal report
Date
May 9, 1998, 10:45 local (17:45 UTC)
Place
Mesa, AZ
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N7447HPiper J3C-65
Weather
Visual (VMC) · Day
Status
Completed · report August 3, 1999
Report
Approved by Office Director
FAA report
19980509008609A
Case key
30106

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

Failure of a weld in the engine's throttle control support assembly due to inadequate maintenance which was the ultimate responsibility of the owner-pilot. Contributing factors were the presence of rough terrain, the lack of a suitable forced landing site, and the pilot's inadequate in-flight planning.

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/malfDescent
Throttle/power lever,linkage - disconnectedCause
Throttle/power lever,linkage - failureCause
Maintenance - inadequatePilot in commandFactor
Forced landingEmergency descent/landing
On ground/water encounter with terrain/waterLanding - flare/touchdown
Terrain condition - none suitableFactor
In-flight planning/decision - inadequatePilot in commandFactor
Terrain condition - rough/unevenFactor

Analysis

The airplane, which the pilot owned and operated, experienced a total loss of engine power while descending for a practice forced landing. The pilot indicated that no adequate landing site was available within gliding distance, so he landed in the rough terrain of a dry wash shearing off both main landing gear. The airplane was recovered and examined. A clamp that had been welded onto a bracket which was secured to the engine case was found broken. The clamp/bracket assembly supported the throttle cable. When the weld broke subsequent movement of the cockpit throttle control had no effect upon the engine's rpm. The pilot described the weld as having been 'bad,' and it was not a Piper manufactured component.

Factual narrative

On May 9, 1998, at 1045 hours mountain standard time, a Piper J3C-65, N7447H, owned and operated by the pilot, experienced a total loss of engine power while descending. The private pilot made a forced landing on rough terrain, and the airplane was substantially damaged. Neither the private pilot nor the passenger was injured. Visual meteorological conditions prevailed during the personal flight which originated from Mesa, Arizona, about 1030.

According to the pilot, the mishap occurred while he was practicing a simulated forced landing over desert terrain. When he pushed the throttle forward to restore engine power, the engine did not respond. No adequate landing sites existed within gliding distance, so he landed in a dry wash. During rollout, both main landing gear were sheared off.

The pilot initially reported that damage to his airplane was minor. The Federal Aviation Administration coordinator subsequently examined the airplane and observed that the airplane's fuselage was buckled aft of the wings.

Additional examination of the airplane revealed that a clamp, which had been welded onto an engine case mounted bracket, was broken at its attachment weld. The clamp was identified as Continental Engine Part number 70801-00. The clamp/bracket assembly supported the throttle cable. The pilot indicated that evidently, when the weld broke, alignment of the throttle cable with the carburetor was lost. Subsequent movement of the cockpit throttle control produced no corresponding effect upon the engine's rpm, which was thereby reduced to idle. The pilot further indicated that the malfunction had resulted from the "bad weld" which was not a Piper component.

Aircraft

Registration
N7447H
Reported as
Piper J3C-65
Category
Airplane
Serial number
20712
Airframe hours
5,800
Engine
Continental C85-12, 85 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
James D. Bullard
Airworthiness certificate
Standard, Normal
Last inspection
Annual · July 15, 1997 · 100 hours before
Departed
FFZ · Falcon Field, AZ
Destination
E14 · Tucson, AZ

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
51
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Valid Medical--w/ waivers/lim
Seat
Rear
Flight hours
1,200 total · 417 in this make and model · 1,050 as pilot in command · 22 in the last 90 days

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.