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CEN11LA552 · Cessna T210N

5 Aug 2011 · Amarillo, TX, United States

Muy Flying Cessna T210N · Accident: loss of engine power (total) on approach

From Moore County Airport (DUX) to Rick Husband Amarillo International Airport (AMA)

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Event

NTSB case
CEN11LA552
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 T210N

Aircraft type
Cessna 210
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
N829MB
Operator
Muy Flying
Onboard fatalities
Unknown
Route
From Moore County Airport (DUX), Dumas, TXTo Rick Husband Amarillo International Airport (AMA), Amarillo, TX
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
Approach
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

  • Not determined › Not determined

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 noticed a loss of engine power while descending to land, and he made several unsuccessful attempts to restart the engine. The pilot was unable to maintain altitude and made a forced landing to rugged, uneven terrain north of the runway. During the landing roll, the airplane struck a gully and flipped over. The pilot said he did not observe any fuel leaking from the airplane after the accident, and a postaccident inspection of the grassy area around and under the airplane revealed no discoloration from fuel exposure. Examination of the fuel system revealed no mechanical anomalies or blockages, and the fuel selector was set to the right fuel tank. A review of fuel receipts and data downloaded from the engine analyzer revealed there should have been about 58 gallons of fuel on board at the time of the accident. However, only 20 gallons of fuel (15 gallons from the right tank and 5 gallons from the left tank) were drained from the airplane. The missing 38 gallons could not be accounted for.

Data from the engine analyzer was downloaded and confirmed a loss of engine power, but it did not identify the cause of the loss of engine power. About 1 minute later, both values dropped to zero. When the engine was test run, it started immediately and ran through its full power band without interruption. No mechanical anomalies were noted that would have precluded the engine from operating normally. Even with a discrepancy of 38 gallons, there was still adequate fuel available for the engine to continue operating. It could not be determined what caused the loss of engine power.

Probable cause

A loss of engine power for reasons that could not be determined because postaccident examination of the engine did not reveal any anomalies that would have precluded normal operation.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record CEN11LA552
Event ID
20110808X02225
Case number
CEN11LA552
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: 02cfb481cc7d11800d78dcf714da4204f152824c95d1d617733ac10a2cabda4a; retrieved 2026-09-15T16:34:49.043Z.