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LAX01FA302 · Piper PA-23-150

9 Sept 2001 · Chico, CA, United States

Piper PA-23-150 · Accident: partial loss of engine power (non-mechanical) during initial climb

From Chico Regional Airport (CIC) to Chico Regional Airport (CIC)

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Event

NTSB case
LAX01FA302
Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
Accident
InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
Completed
API-reported fatalities
1 · all aircraft and ground
Ground fatalities
Unknown
OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
General aviation
WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
Visual Meteorological Cond

Piper PA-23-150

Aircraft type
Piper PA-23
Category
Airplane
RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
N2268P
Operator
Unknown
Onboard fatalities
Unknown
Route
From Chico Regional Airport (CIC), Chico, CATo Chico Regional Airport (CIC), Chico, CA
Aircraft age
Not recorded
Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
Part 91: General Aviation
Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
Initial climb
First occurrenceThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
Partial loss of engine power (non-mechanical)
Also codedOther events the NTSB coded in the sequence, such as a wire strike after a loss of power. Flight Findings uses them for its kinds of event. Glossary
Tree(s)
DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
Destroyed

Cause areas

  • Pilot in command › Directional control, not maintained
  • Pilot in command › Emergency procedure, improper
  • Reason for occurrence undetermined

Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.

NTSB narrative

Witnesses observed the airplane climb a maximum of 200 feet above the runway during its initial climb, and then it descended in a right wing low attitude until impacting the level ground short of the airport's perimeter fence. A fire erupted and consumed the airplane. Before the pilot succumbed to his injuries he reported to the responding medical personnel that "my engine failed and I was trying to turn around." The subsequent airframe examination revealed that the wings were fire damaged in areas corresponding to both the inboard and the outboard fuel tanks, and the fuel selectors were on the main tank positions. The landing gear was extended, and the rudder trim tab was set to a position consistent with a right engine power failure. No evidence of any internal engine mechanical malfunction was observed. The left propeller blades were torsionally twisted and gouged; the right blades sustained only minor damage. The pilot was an airframe and powerplant mechanic, had performed the maintenance on his airplane, and was its only pilot. He last flew the airplane about 3.5 months prior to the accident, and this was the first flight following maintenance. No logbook records were found that identified the maintenance performed. The cause of the right engine's nonmechanical loss of power was not determined. Given the prevailing meteorological conditions and the airplane's weight, performance data indicates that the airplane should have had a positive climb rate upon feathering the right engine's propeller blades and retraction of the landing gear.

Probable cause

The loss of right engine power for undetermined reasons, and the pilot's failure to maintain control of the aircraft due to his improper single engine emergency procedures.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record LAX01FA302
Event ID
20010920X01974
Case number
LAX01FA302
Dataset
historical-pre2008
Source SHA-256
89e2df6d848e7ab3b42e7d7c7a03ff403303057a26ca04c95b3ea67201c3ce74
Source notes (4)
  • Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
  • Filled from the NTSB case API where the bulk record had no value: local date, investigation status, coordinates. Values present in the bulk record are kept.
  • The date is the local date; the NTSB stores the UTC date 2001-09-10.
  • API snapshot SHA-256: 70183e880a0f6ac970e66efb27d3231cde4fd5b4a87eb3512746e384f0ea766a; retrieved 2026-09-20T20:21:44.366Z.