DCA92MA048 · Beech C-45H
Exa Beech C-45H · Accident: total loss of engine power (mechanical failure) during initial climb
From OC2 to OC2
Event
- NTSB case
- DCA92MA048
- 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
- 12 · 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 C-45H
- Aircraft type
- Beechcraft C-45
- 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
- N3657G
- Operator
- Exa
- Onboard fatalities
- Unknown
- Route
- From OC2To OC2
- 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 (mechanical failure)
- 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
- Company/operator management › Maintenance, 100-hour inspection, not performed
- Company/operator management › Maintenance, inadequate
- Eng assembly, blower/impeller/integral supercharger › Failure, total
- Propeller feathering › Not attained
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
AFTER TAKEOFF, THE AIRPLANE WAS SEEN AT LOW ALTITUDE TRAILING SMOKE FROM THE LEFT ENGINE. WITNESSES SAW THE WINGS 'TIPPING' BACK AND FORTH, THEN A WING DROPPED AND HIT THE GROUND. EXAMINATION REVEALED THAT A SUPERCHARGER BEARING HAD FAILED IN THE LEFT ENGINE. THE LEFT ENGINE HAD BEEN RECENTLY INSTALLED BY NON-CERTIFICATED PERSONNEL AFTER BEING INACTIVE FOR 18 YRS WITHOUT PRESERVATION. THE AIRPLANE HAD FLOWN ABOUT 184 HRS SINCE THE LAST ANNUAL INSPECTION; NO RECORD OF SUBSEQUENT 100-HR INSPECTION. THE LEFT PROP BLADES WERE FOUND IN AN INTERMEDIATE POSITION BETWEEN THE OPERATING RANGE AND THE FEATHERED POSITION. THE LEFT PROP WAS CHANGED SEVERAL WEEKS PRIOR TO THE ACCIDENT. THERE IS NO EVIDENCE THAT THE LEFT PROP HAD EVER BEEN SUCCESSFULLY CYCLED TO THE FULL FEATHER POSITION. THE OPERATOR AND PILOTS WERE NOT AWARE OF HAMILTON STANDARD SB 657 RECOMMENDING FULL-FEATHER CHECKS EVERY 30 DAYS. LEFT PROP FEATHERING MOTOR RELAYS NOT RECOVERED. ALL 11 PARACHUTISTS WERE FOUND IN CENTER PART OF FUSELAGE; NO EVIDENCE OF RESTRAINT USEAGE.
Probable cause
INADEQUATE MAINTENANCE AND INSPECTION BY THE OPERATOR WHICH RESULTED IN AN ENGINE POWER LOSS DURING THE CRITICAL TAKEOFF PHASE OF FLIGHT. IN ADDITION, THE PILOT DID NOT, OR WAS UNABLE TO, ATTAIN A FULL-FEATHER POSITION ON THE LEFT ENGINE PROPELLER, WHICH WOULD HAVE MOST LIKELY ENABLED THE AIRPLANE TO SUSTAIN MINIMUM CONTROL AIRSPEED.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record DCA92MA048
- Event ID
- 20001211X15678
- Case number
- DCA92MA048
- 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: 725232eaff0dd5ee33ade6f9f23fd2ce3942d2e33c0c10c6d9598f12797f6d07; retrieved 2026-09-21T00:57:38.223Z.