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LAX04LA166 · Globe GC-1B

18 Mar 2004 · Placerville, CA, United States

Globe GC-1B · Accident: loss of engine power during initial climb

From Placerville Airport (PVF) to O61 · Cameron Park, CA

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Event

NTSB case
LAX04LA166
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
0 · 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

Globe GC-1B

Aircraft type
Globe GC-1
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
N369BZ
Operator
Unknown
Onboard fatalities
Unknown
Route
From Placerville Airport (PVF), Placerville, CATo O61 · Cameron Park, 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
Loss of engine power
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
Fuel starvation; 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
Substantial

Cause areas

  • Fluid, fuel › Starvation
  • Fuel system, gascolator › Leak
  • Owner/pilot mechanic › Maintenance, installation, improper

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

NTSB narrative

The airplane collided with trees and terrain following a loss of engine power in the takeoff initial climb. The pilot reported that he had just dropped off a passenger and was repositioning the airplane to another airport. At 200 to 300 feet above ground level (agl) in the takeoff initial climb the engine lost power. He attempted to turn back to the runway but did not have enough altitude. He elected to stall the airplane into the trees on the south slope of the airport boundary. The accident was witnessed by personnel at the airport. The witnesses reported that the pilot was departing using runway 23, the airplane took off and did a steep, almost vertical ascent, and banked hard to the left (south). The pilot appeared to stall the airplane, as it went into the trees on the south side of the runway. The pilot held an airframe and powerplant mechanic certificate and was the primary maintainer of the airplane. Federal Aviation Administration inspectors examined the wreckage at the accident scene and Safety Board investigators later examined the wreckage following recovery. Disassembly of the gascolator revealed that both the upper and lower gaskets in the gascolator were 1/8 to 3/16 inches smaller in diameter than the gascolator canister and the top and bottom covers. The investigators observed that in order to affect a seal, both gaskets had to be centered when installed. Both gaskets were off center. No fuel was observed in the fuel lines and the manifold valve was disassembled and found to be dry and void of any fuel. The manifold valve body and screen were clean. No other discrepancies were found during the engine examination.

Probable cause

a loss of engine power due to an improperly sized and installed set of sealing gaskets in the gascolator, which resulted in fuel starvation. A factor to the accident was the unsuitable terrain for the forced landing.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record LAX04LA166
Event ID
20040324X00361
Case number
LAX04LA166
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: investigation status, coordinates. Values present in the bulk record are kept.
  • The date is the local date, which is the same as the UTC date the NTSB stores.
  • API snapshot SHA-256: cf5615e926d4c1b2ddf6faeb7dca09bbead6f35946f86b7273a313e08cd52edd; retrieved 2026-09-21T09:18:49.072Z.