ERA21LA261 · Cessna 172 N
Aamro Aviation Cessna 172 N · Accident: loss of engine power (total) during initial climb
From North Palm Beach County General Aviation Airport (F45) to an unrecorded destination
Event
- NTSB case
- ERA21LA261
- 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 172 N
- Aircraft type
- Cessna 172
- 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
- N2797E
- Operator
- Aamro Aviation
- Onboard fatalities
- Unknown
- Route
- From North Palm Beach County General Aviation Airport (F45), West Palm Beach, FLTo not recorded
- Aircraft age
- About 43 years (built 1978)
- 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 (total)
- 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
- Aircraft › Aircraft power plant
- Personnel issues › Action/decision
- 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
During a local instructional flight, about 2,700 ft above ground level, the engine lost total power. The instructor was unable to restart the engine and attempted to land on a grass field; however, the airplane overflew the field and collided with a fence and trees before coming to rest nose-down in a creek. Review of flight track data revealed that the airplane overflew several fields, ranging in length from approximately 1,500 ft to 2,500 ft before the collision.
Examination of the wreckage revealed that the single-drive, dual output magneto had separated from the rear accessory section of the engine. The nuts, clamps, and lock washers that secured the magneto to the studs were not recovered and the studs did not exhibit any stripping or damage of the threads. Cuts in the magneto housing were consistent with the magneto vibrating over time, possibly due to tightening at an angle between the two studs. The magneto was removed and reinstalled as part of an inspection completed about 3 months (215 hours) before the accident. The mechanic who completed the inspection and reinstalled the magneto stated that the reinstallation included clamps and nuts that were used, but serviceable, and new lock washers. The mechanic added that there were no defects noted at the time of the inspection. An annual inspection of the airplane was completed about 1 month (74 flight hours) before the accident. The mechanic that completed the annual inspection stated he followed the Code of Federal Regulations Part 43 checklist, which does not specifically include magnetos; however, he checked with his hand (by trying to wiggle all the accessories) that the magneto was secure.
Probable cause
The flight instructor’s failure to obtain the proper touchdown point during a forced landing. Contributing to the accident was the improper service and subsequent inadequate inspection of the single-drive, dual magneto, which resulted in a total loss of engine power.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record ERA21LA261
- Event ID
- 20210621103301
- Case number
- ERA21LA261
- 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, cause areas. 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: ba5571353bc547bcdcdf3177d85e277ddd1c278965724b63a51b3da3c2ae1121; retrieved 2026-09-16T14:11:29.867Z.