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ERA10FA202 · Cessna 172E

3 Apr 2010 · West Milford, NJ, United States

Cessna 172E · Accident: loss of engine power (total) during initial climb

From Greenwood Lake Airport (4N1) to Lincoln Park Airport (N07)

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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
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.