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Atlas / NTSB / CEN11CA136

NTSB CAROL · Event

Event CEN11CA136

2010-12-28 Columbus, Ohio, United States Minor 1 aircraft Status: Completed

Registry · N888CA

FAA Aircraft Registry record.

Make / Model

PIPER PA-46-310P

Year of manufacture

1984 · 26 years old at event

Engine

CONT MOTOR TSIO-520 SER (300 hp)

Seats / Engines

6 seats · 1 engine

Last airworthiness date

20250715

ADS-B equipped

Yes — Mode-S AC3BC0

Registrant of record

INTERNATIONAL AIR SERVICES INC TRUSTEE

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot’s improper fuel management which resulted in a loss of engine power due to fuel exhaustion.

Factual narrative

Prior to the flight, the pilot preflighted the airplane and recalled observing the fuel gauge indicating full; however, he did not visually check the fuel tanks. The airplane departed and the en route portion of the flight was uneventful. During the downwind leg of the circling approach, the engines began to surge and the pilot added full power and turned on the fuel boost pumps which "seemed to resolve the problem..." While abeam the approach end of the runway on the downwind leg, the engines again started to surge and subsequently lost power. The pilot executed a forced landing and the airplane impacted terrain short of the runway. Examination of the airplane by Federal Aviation Administration inspectors revealed the fuselage was buckled in several areas, and the left wing was crushed and bent upward. The fuel tanks were intact and approximately one cup of fuel was drained from the single fuel sump. Fueling records indicated the airplane was fueled 3 days prior with 135 gallons of fuel or approximately 4 hours of operational time. Flight records indicated the airplane had flown approximately 4 hours since refueling when the engines lost power. Prior to the flight, the pilot preflighted the airplane and recalled observing the fuel gauge indicating full; however, he did not visually check the fuel tanks. The airplane departed and the en route portion of the flight was uneventful. During the downwind leg of the circling approach, the engines began to surge and the pilot added full power and turned on the fuel boost pumps. While abeam the approach end of the runway on the downwind leg, the engines again started to surge and subsequently lost power. He executed a forced landing and the airplane impacted terrain short of the runway. A postaccident examination by Federal Aviation Administration inspectors revealed the fuselage was buckled in several areas, and the left wing was crushed and bent upward. The fuel tanks were intact and approximately one cup of fuel was drained from the single fuel sump. Fueling records indicated the airplane was fueled 3 days prior to the accident with 135 gallons of fuel or approximately 4 hours of operational time. Flight records indicated the airplane had flown approximately 4 hours since refueling when the engines lost power. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).

  • C Personnel issues-Task performance-Planning/preparation-Fuel planning-Pilot - C
  • C Aircraft-Fluids/misc hardware-Fluids-Fuel-Fluid level - C

Verbatim from NTSB's published report. Source file NTSB_2010_CEN11CA136.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.