CEN21LA194 · Cessna A185F
Echelon Right Cessna A185F · Accident: fuel starvation during initial climb
From North Vernon Airport (OVO) to an unrecorded destination
Event
- NTSB case
- CEN21LA194
- 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
- Event fatalities
- Unknown
- 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
Cessna A185F
- Aircraft type
- Cessna 185
- 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
- N19D
- Operator
- Echelon Right
- Onboard fatalities
- Unknown
- Route
- From North Vernon Airport (OVO), North Vernon, INTo not recorded
- Aircraft age
- About 41 years (built 1980)
- 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
- Fuel starvation
- 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 › Fluids/miscellaneous hardware
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
After a 100-hour inspection, which the pilot assisted with, he conducted an operational check of the airplane, which included a run-up of the airplane. The mechanic had to leave before the inspection was complete, and the pilot installed portions of the interior which included the fuel selector handle. He then departed the airport and after retracting the landing gear and flaps, the engine lost power. During the forced landing the airplane sustained substantial damage to the empennage and aft section of the fuselage.
Examination of the airplane revealed that fuel was available in the left and right fuel tanks. The examination also found that the fuel selector handle had been installed incorrectly by 90° on the fuel selector shaft. The position of the shaft as found would have restricted all fuel flow from the left and right fuel tanks. The shaft was “keyed” such that the fuel selector handle should only be installed one way; however, the handle partially fit over the stem when not aligned with the key on the shaft and allowed the attaching screw to partially engage on the stem.
An engine test run was conducted; the engine started normally and with the engine at full throttle, the fuel selector was placed in the left, right, and both positions. The engine continued to run with no anomalies noted. The airplane was factory equipped with a small header tank that fuel accumulated in before being fed to the engine. The accident is consistent with the fuel selector shaft being in the off position while the selector handle pointed to the left fuel tank. Once the fuel in the airplane’s header tank was exhausted, the engine lost power due to fuel starvation.
Probable cause
The pilot’s improper installation of the fuel selector handle, which resulted in a total loss of engine power due to fuel starvation.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record CEN21LA194
- Event ID
- 20210419102937
- Case number
- CEN21LA194
- 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: local date, investigation status, cause areas. Values present in the bulk record are kept.
- The date is the local date; the NTSB stores the UTC date 2021-04-17.
- API snapshot SHA-256: 4823f883f254b50130c53a70725d67615ad2fee409178467c784b250da15207b; retrieved 2026-09-16T13:57:52.006Z.