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ERA11CA237 · Cessna 182A

10 Apr 2011 · Lesage, WV, United States

Cessna 182A · Accident: loss of engine power (total) en route

From Robert Newlon Field (I41) to Robert Newlon Field (I41)

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Event

NTSB case
ERA11CA237
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

Cessna 182A

Aircraft type
Cessna 182
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
N4810D
Operator
Paul Nadas
Onboard fatalities
Unknown
Route
From Robert Newlon Field (I41), Huntington, WVTo Robert Newlon Field (I41), Huntington, WV
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
En route · descent
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 › 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

The pilot flew four skydiving flights without refueling. On the last flight, after the skydivers exited the airplane, the pilot initiated a descent and the airplane experienced a total loss of engine power. The pilot knew he could not make it back to the airport and made a forced landing to a gravel area. The airplane collided with a gravel mound and nosed over resulting in substantial damage to the airframe. According to the pilot, the airplane owner assisted him in fueling the airplane from a local fuel truck. The pilot said he used a ladder and started refueling the right wing with the owner manning the pump. While they were refueling the airplane, the owner asked the pilot if he was getting any fuel because the fuel meter was not running. They looked at the airplane's right main fuel tank and it appeared to be full. The pilot then added what he believed to be 10 gallons of fuel to the left main fuel tank. The pilot thought he had 37.5 gallons of fuel on board when he departed. Examination of the wreckage did not reveal any preimpact mechanical malfunctions, nor did the pilot report any. The examination also did not reveal any evidence of usable fuel. Additionally, examination of the airplane rubberized bladder type fuel cells located on the inboard bay of each wing panel revealed the snap fasteners normally used to prevent the collapse of the flexible cells were not installed and wrinkling of the bladder was noted. The fuel bladders were replaced about 5 years prior to the accident. It is possible that due to the wrinkling of the right fuel bladder, the pilot may not have had the fuel that he expected when the tank was topped off.

Probable cause

A loss of engine power due to fuel exhaustion. Contributing to the accident was the improper installation of snap fasteners to the rubberized type fuel cells which resulted in wrinkling of the fuel bladders and incorrect fuel quantity for the flight.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record ERA11CA237
Event ID
20110412X02727
Case number
ERA11CA237
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. 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: 8b1bf7250beeb7ee388127971f5c8e82b094f21b3530b3f5b2dfde7e7e3d5605; retrieved 2026-09-15T16:02:38.785Z.