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ANC11CA013

2011-02-23 · Sterling, Alaska, United States · None · 1 aircraft · Status: Completed

Airport 40AK

Current FAA registration · N623MP

Make / Model
PIPER PA-18
Year of manufacture
1964 · 47 years old at event
Engine
LYCOMING 0-320 SERIES (180 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19960703
ADS-B equipped
Yes — Mode-S A82283

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The airplane owner improper fabrication of a fuel line, and subsequent inadequate inspection by an aviation mechanic, resulting in a loss of engine power.

Factual narrative

According to the pilot's statement, the accident flight was the first flight after a major rebuild of the airplane. After completing ground runs on the engine, the pilot and passenger departed the airport for a test flight. During the initial climb, approximately 600 feet above the ground, the engine lost power. The pilot elected to land in a snow covered field, and during the landing the airplane nosed over. Substantial damage was sustained to both the front and rear lift struts on the right wing. A postaccident inspection of the fuel system by the pilot, who is also the mechanic that oversaw the rebuild of the airplane, revealed a flap of rubber inside a flexible fuel hose that was of significant size to restrict fuel flow to the engine. The fuel hose was fabricated by the airplane owner, under the supervision of the mechanic. The fuel hose was fabricated out of flexible automotive hydraulic line, not approved aircraft-grade fuel hose. According to the pilot, the accident flight was the first flight after a major rebuild of the airplane. After completing ground runs on the engine, he and a passenger departed for a test flight. During the initial climb, approximately 600 feet above the ground, the engine lost power. He elected to land in a snow-covered field and during the landing the airplane nosed over. Substantial damage was sustained to both the front and rear lift struts on the right wing. A postaccident inspection of the fuel system by the pilot revealed a flap of rubber inside a flexible fuel hose that was of significant size to restrict fuel flow to the engine. The fuel hose was fabricated by the airplane owner, under the supervision of the mechanic. The fuel hose which was fabricated out of flexible automotive hydraulic line was not an approved aircraft-grade fuel hose. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

FAA avdata. C = Cause, F = Factor.

  • C Aircraft-Fluids/misc hardware-Misc hardware-Hoses and tubes-Inadequate inspection - C
  • C Personnel issues-Task performance-Maintenance-Fabrication-Owner/builder - C
  • C Aircraft-Aircraft power plant-Engine fuel and control-Fuel distribution-Damaged/degraded - C

Verbatim from NTSB's published report. Source file NTSB_2011_ANC11CA013.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.