ERA10LA405 · Glines SPORTSMAN GS-2
Glines SPORTSMAN GS-2 · Accident: loss of engine power (partial) during initial climb
From Morrisville-Stowe State Airport (MVL) to Sky Acres Airport (44N)
Event
- NTSB case
- ERA10LA405
- 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
Glines SPORTSMAN GS-2
- Aircraft type
- Glines SPORTSMAN GS-2
- 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
- N546SG
- Operator
- Everett S. Glines · private individual
- Onboard fatalities
- Unknown
- Route
- From Morrisville-Stowe State Airport (MVL), Morrisville, VTTo Sky Acres Airport (44N), Millbrook, NY
- 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
- Defining eventThe 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 (partial)
- 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
- Aircraft › Aircraft oper/perf/capability
- Personnel issues › Task performance
Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.
NTSB narrative
The pilot of the experimental amateur-built airplane stated that while on the downwind leg of the traffic pattern, the annunciator system made several audible warnings stating "check fuel pressure." He noted that the fuel pressure gauge indicated low to no fuel pressure. He cycled the boost pump from the "on" position to the "off" position several times, with no effect on the fuel pressure reading. The mixture, propeller, and throttle controls appeared to be in their respective normal climb positions, but the pilot noted a decrease in engine rpm and manifold pressure. He also noticed that the rpm and manifold pressure were continuing to decline and that the engine was continuing to lose power while the annunciator continued to sound the same warning. The pilot returned to the departure airport and initiated a flare. The airplane touched down hard on the runway and veered to the left. Despite the pilot's control inputs, the airplane would not respond to rudder or brake inputs and departed off the left side of the runway, nosing over inverted.
Postaccident examination of the airframe, engine assembly and accessories did not reveal any preimpact mechanical malfunction. An engine test run and flow check was conducted with no anomalies noted. Data retrieved from the airplane's multi-function display confirmed the erratic fuel flow during the accident flight; however, the anomaly could not be duplicated during postaccident testing. The reason for the loss of fuel pressure could not be determined.
Probable cause
The pilot's improper flare during a forced landing. Contributing to the accident was a loss of fuel pressure for undetermined reasons.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record ERA10LA405
- Event ID
- 20100807X85410
- Case number
- ERA10LA405
- Dataset
- full-current
- Source SHA-256
- 5cf380f0061817c0331a6b2d8cc7e0ee3a79bea469a1001dc5c10e56f35f5ab3
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: cbc048d56f2a46520dabac43393b1f08fda10ba75d6c1fac5832076ade7136ce; retrieved 2026-09-15T14:48:27.482Z.