WPR14LA315 · Ercoupe 415 C
Ercoupe 415 C · Accident: loss of engine power (partial) en route
From Rogers Field (O05) to Rogers Field (O05)
Event
- NTSB case
- WPR14LA315
- 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
Ercoupe 415 C
- Aircraft type
- Ercoupe 415
- 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
- N2013H
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From Rogers Field (O05), Chester, CATo Rogers Field (O05), Chester, CA
- Aircraft age
- About 68 years (built 1946)
- 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
- En route · cruise
- 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 (partial)
- 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
- Environmental issues › Conditions/weather/phenomena
- Personnel issues › Task performance
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
The commercial pilot reported that, before the first flight leg of the day, he used the engine primer during a cold engine start. He did not use the primer before he departed for the accident flight leg. He stated that, during cruise flight, he began to slowly climb the airplane to cross a ridgeline, and, as he pushed the throttle up, the engine did not respond. He pumped the throttle numerous times, and the engine finally responded; however, the airplane had lost altitude and airspeed, and he was forced to land the airplane in a wooded area.
Examination of the wreckage revealed that the spark plugs' electrode areas were dark and sooty, indicative of a rich-mixture condition. The engine primer plunger was found in the unlocked-and-extended position, and it was undamaged and would lock when the lugs were engaged. The primer position and the condition of the spark plugs indicated that the engine power loss was likely due to an overly rich mixture, which resulted from excess fuel being pulled through the primer into the engine's intake system when power was applied.
The Starting checklist procedures indicated that, after using the primer, the primer plunger should be locked. An unsecured primer plunger can cause the engine to run richer than normal and result in a rough-running engine, loss of power, and blackened spark plugs. It is likely that, when the pilot used the primer while starting the engine before the first flight leg, he did not ensure that it was locked before initiating the accident flight in accordance with the Starting checklist and that this led to the subsequent in-flight loss of engine power. The calculated density altitude at cruise altitude at the time of the flight was about 9,240 ft, which would have further degraded the engine's performance.
Probable cause
The pilot’s failure to follow the checklist while starting the engine and to lock the engine primer plunger, which resulted in the partial loss of engine power during cruise flight in high density altitude conditions.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record WPR14LA315
- Event ID
- 20140729X95232
- Case number
- WPR14LA315
- 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. 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: d1f3283652a3f0ecc9e056fd170d6ba060d31f7793a0e13b7c7adfc17ec92b0b; retrieved 2026-09-16T01:01:59.945Z.