FTW94LA005

NTSB accident investigation · Piper PA-28-180C · Albuquerque, NM · October 5, 1993

Accident · Serious injuriesLimited investigationFinal report
Date
October 5, 1993, 12:30 local (18:30 UTC)
Place
Albuquerque, NM
Injuries
1 serious, 3 minor
Damage
Destroyed
Phase of flight
Initial climb
Aircraft
N9317JPiper PA-28-180C
Weather
Visual (VMC) · Day
Status
Completed · report November 18, 1994
Report
Approved by Office Director
FAA report
19931005037729A
Case key
18948

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 pilot's failure to maintain adequate airspeed. The high density altitude was a factor.

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 control - in flightTakeoff - initial climb
Weather condition - high density altitudeFactor
Airspeed - not maintainedPilot in commandCause
Stall - inadvertentPilot in command
In flight collision with terrain/waterTakeoff - initial climb

Analysis

The pilot stated that he leaned the mixture for high altitude just prior to the takeoff roll. Shortly after takeoff the engine started running very rough. After advancing the mixture to full rich the engine lost all power, and he made a forced landing in an open field. After all the occupants exited the airplane, there was an explosion and the airplane burned. One witness said he saw the airplane make a left turn, stall, and impact the ground. Another witness, an active pilot with a commercial certificate, said that he first observed the airplane at a low airspeed, high angle-of-attack, climbing at about the same rate as the up-slope of the ground. It then pitched up and down, and rolled into a sharply descending left turn; it appeared to him that it had stalled. As the airplane then approached the witness's location, he heard the engine operating & developing power just before it crashed. The pilot had originally told the FAA inspector that '...the aircraft stalled.' Post-accident engine examination did not disclose any anomalies.

Factual narrative

On October 5, 1993, at 1230 mountain daylight time, N9317J, a Piper PA-28-180C, collided with terrain shortly after taking off from Coronado Airport, Albuquerque, New Mexico. One passenger was seriously injured, but the private pilot and two other passengers received only injuries. The airplane was destroyed. Visual meteorological conditions prevailed at the time; no flight plan had been filed for the personal flight.

The following is based on the submitted Pilot/Operator Report (6120.1/2). The airplane was fueled to capacity, and three passengers and baggage were loaded for a planned flight to Altus, Oklahoma. Because the wind was from the southwest at seven knots, the pilot took off on runway 17. The engine began running rough at an altitude of approximately 400 feet, so he adjusted the mixture slightly to the rich position, and the engine ran smoother. He turned crosswind and at an altitude of about 600 to 700 feet, the engine began to run rough again so he adjusted the mixture control to full rich. A check of the magnetos, fuel selector, fuel pressure, and oil pressure revealed everything was normal; however the engine lost power and he made a forced landing to an open field. Following the landing the airplane began to burn so all the occupants evacuated the airplane. The airplane was consumed by fire.

One witness at the airport told the Federal Aviation Administration (FAA) inspector they saw the "airplane make a left turn, stall, and impact the ground." Another witness, who is a commercial and instrument rated pilot, submitted a detailed statement in which he noted "the aircraft pitched up and down and rolled into a sharply descending left turn. It appeared that it had stalled...The engine was operating as I could hear it developing power." The pilot originally told the FAA inspector that "the nose pitched up, the wings wiggled, and the aircraft stalled." When questioned later about the engine roughness, the pilot stated he could "feel the roughness through the rudder pedals."

Post-accident engine examination by FAA inspectors failed to disclose any anomalies. According to the pilot, fuel samples taken from three sump drains on the airplane 30 minutes after it was refueled contained no contaminants.

Aircraft

Registration
N9317J
Reported as
Piper PA-28-180C
Category
Airplane
Serial number
28-3426
Airframe hours
5,130
Engine
Lycoming O-360-A3A, 180 horsepower, reciprocating
Damage
Destroyed
Fire
On-Ground
Flight
Personal · Part 91
Registered owner
Castillo, James & Gilbert
Airworthiness certificate
Standard, Normal
Last inspection
Annual · April 24, 1993 · 11 hours before
Destination
AXS · Altus, OK
Airport
4AC · Coronado

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
62
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
233 total · 233 in this make and model · 195 as pilot in command · 5 in the last 90 days · 4 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
210° at 7 knots
Visibility
50 statute miles
Lowest ceiling
0 ft
Temperature
77 °F, dew point 30 °F
Altimeter
30.00 inHg
Observed at
ABQ, 9 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.

Other investigations on N9317J · 2

Matched to the same aircraft by N-number and date.