CHI89FA128 · Beech 58
Beech 58 · Accident: total loss of engine power (non-mechanical) during initial climb
From Battle Creek Executive Airport at Kellogg Field (BTL) to New York Stewart International Airport (SWF)
Event
- NTSB case
- CHI89FA128
- 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
- 3 · all aircraft and ground
- Ground fatalities
- 0
- 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
Beech 58
- Aircraft type
- Beechcraft 58
- 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
- N9253A
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From Battle Creek Executive Airport at Kellogg Field (BTL)To New York Stewart International Airport (SWF), Newburgh, 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
- 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 starvation
- DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
- Destroyed
Cause areas
- Copilot/second pilot › Aircraft control, not maintained
- Emergency procedure › Improper
- Wrong engine shutdown
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
DURING THE INITIAL CLIMB AFTER TAKEOFF, ONE OF THE CREW MEMBERS REPORTED THAT THE RIGHT ENGINE LOST POWER & THAT THEY WOULD RETURN FOR A LANDING. THE AIRCRAFT WAS OBSERVED TO CIRCLE TO THE LEFT WITH THE RIGHT PROP FEATHERED. DURING THE TURN TO THE AIRPORT, THE AIRCRAFT DESCENDED & CRASHED IN A SWAMPY AREA THAT WAS SURROUNDED BY TREES. A POST IMPACT FIRE ERUPTED & DESTROYED THE AIRCRAFT. SUBSEQUENT INVESTIGATION VERIFIED THAT THE RIGHT ENGINE PROPELLER HAD BEEN FEATHERED. THE FUEL SELECTOR FOR THE RIGHT ENGINE WAS FOUND POSITIONED BETWEEN 'OFF' & 'ON.' THE MAGNETO SWITCH FOR THE LEFT ENGINE WAS FOUND IN THE 'OFF' POSITION, WHILE THE MAGNETO SWITCH FOR THE RIGHT ENGINE WAS IN THE 'BOTH' POSITION. REMNANTS OF THE THROW-OVER YOKE SHOWED THAT IT WAS POSITIONED TO THE COPILOT'S SIDE. THE COPILOT'S FLIGHT TIME IN THE BEECH 58 WAS NOT VERIFIED. BOTH ENGS WERE REMOVED & PREPARED FOR OPERATIONAL CHECKS. AFTER WATER CONTAMINATION WAS CLEANED FROM THE ENGINES, BOTH WERE STARTED & RAN SUCCESSFULLY.
Probable cause
THE FLIGHT CREW INADVERTENTLY SHUT DOWN THE LEFT ENGINE AFTER THE RIGHT ENGINE LOST POWER, AND THE COPILOT FAILED TO MAINTAIN CONTROL OF THE AIRCRAFT WHILE MANEUVERING THE AIRCRAFT BACK TOWARD THE RUNWAY. FACTORS RELATED TO THE ACCIDENT WERE: IMPROPER POSITIONING OF THE FUEL SELECTOR (PROBABLY) BY THE COPILOT AND IMPROPER MONITORING BY THE OTHER PILOT, WHICH RESULTED IN FUEL STARVATION TO THE RIGHT ENGINE.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record CHI89FA128
- Event ID
- 20001213X28755
- Case number
- CHI89FA128
- 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. 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: e4e7659d102e5f1ad413c7e0b5aff3fc8fd32d2901a7b51a739c382a750352b1; retrieved 2026-09-21T03:14:54.246Z.