CHI01LA278 · Gremminger 532 Commander
Gremminger 532 Commander · Accident: total loss of engine power (non-mechanical) on approach
From Sainte Genevieve Flying Club Airport (6MO2) to an unrecorded destination
Event
- NTSB case
- CHI01LA278
- 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
Gremminger 532 Commander
- Aircraft type
- Gremminger 532
- Category
- Gyroplane
- 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
- N609CE
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From Sainte Genevieve Flying Club Airport (6MO2), Ste. Genevieve, MOTo not recorded
- 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
- Approach · VFR pattern downwind
- 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
- Total 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
- Fuel exhaustion
- 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 › Exhaustion
- Pilot in command › Fuel supply, inadequate
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
The gyrocopter nosed over during a forced landing following a loss of engine power while on downwind to land. The pilot reported he had made several flights during the day which included practicing forced landings. The pilot reported that he took off and stayed in the traffic pattern to land. He reported, "Turning onto the crosswind leg I noted the fuel level indication at one eighth of a tank and decided that this will be my last circuit for the day." The pilot reported he turned onto downwind and leveled off at an altitude of 200 feet above the ground. He reported that after 3 - 5 seconds the engine lost power. The pilot reported that due to the low altitude and the high sink rate, he was committed to an off airport landing. The pilot reported there was a bean field near the downwind leg which contained a barren area. He reported the barren area was wet with an area which looked dry. He made the landing on the section which looked dry. The pilot reported, "As the nose landing gear touched down there was a sensation of the aircraft's nose continuing down below normal ground roll attitude. At this point it became obvious that the aircraft was tipping over forward and to the left." The pilot reported that after the landing he discovered that there was damp mud under a thin layer of dry terrain. The pilot reported that two cups of fuel were drained from the fuel tank following the forced landing.
Probable cause
The inadequate fuel supply for the flight which resulted in fuel exhaustion. A factor associated with the accident was the low altitude and the soft terrain on which the forced landing was made.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record CHI01LA278
- Event ID
- 20010814X01680
- Case number
- CHI01LA278
- 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. Values present in the bulk record are kept.
- The date is the local date; the NTSB stores the UTC date 2001-08-12.
- API snapshot SHA-256: d273dce3857035c1da9248b5e07c69a27d0d50687989f0015d1e5fe2c7a57f42; retrieved 2026-09-22T11:39:37.770Z.