ERA10FA202 · Cessna 172E
Cessna 172E · Accident: loss of engine power (total) during initial climb
From Greenwood Lake Airport (4N1) to Lincoln Park Airport (N07)
Event
- NTSB case
- ERA10FA202
- 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
- 1 · 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
Cessna 172E
- 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
- N5528T
- Operator
- Arthur Leidenfrost
- Onboard fatalities
- Unknown
- Route
- From Greenwood Lake Airport (4N1), West Milford, NJTo Lincoln Park Airport (N07), Lincoln Park, NJ
- 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
- 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 › Fluids/miscellaneous hardware
- Personnel issues › Action/decision
- Personnel issues › Task performance
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
The airplane had remained outside and unused for several years before it was purchased by two co-owners, through an individual acting as an aircraft broker, about 4 weeks prior the accident. One co-owner held a private pilot certificate, and the other held a student pilot certificate; neither held an aircraft mechanic's certificate. About 2 weeks after the purchase, the co-owners and a mechanic drove to the airport to examine the airplane, with the reported intent to fly it about 75 miles back to the home airport of the pilot-rated co-owner. Some maintenance activity and a brief test flight were conducted, but mechanical and weather difficulties prevented the relocation of the airplane that day. The following week the three returned to the airplane, and the pilot and mechanic flew it to the pilot's home airport. The next week, the pilot flew the airplane to the student pilot's home airport, and the two then departed, with the student pilot in the left seat. It could not be determined what roles or actions were conducted by either of the individuals during the flight. That flight ended several minutes later, when the airplane impacted a wooded area in a residential neighborhood.
First responders noticed a slight odor of fuel; one fuel tank was breached and contained no fuel, and the other, intact tank contained only a trace amount of fuel. Examination of the wreckage revealed that the fuel strainer contained cloudy fuel contaminated by water and other unidentified contaminants and that the carburetor accelerator pump gasket was deformed. The general overall appearance of the airplane was consistent with it not being well-maintained, but no evidence of any preimpact airframe discrepancies that would have precluded normal flight was observed. The only fuel purchase that could positively be associated with the airplane indicated that 17 gallons were added on the day of the test flight, 2 weeks before the accident. Calculations that used the manufacturer's fuel consumption rates indicated that the total fuel consumption for the period between that last verified fueling and the accident flight ranged from a low of 13 gallons to a high of 32 gallons. The manufacturer specified a total usable fuel quantity of 39 gallons, but the total fuel on board after the last verified fueling could not be determined.
Probable cause
The complete loss of engine power due to fuel starvation.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record ERA10FA202
- Event ID
- 20100403X24937
- Case number
- ERA10FA202
- 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: 287a159016440b587b8d8b0715172d979ff4aa1576b7a8e1171dcc09ffa1d837; retrieved 2026-09-13T20:44:37.301Z.