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CHI03LA305 · Cessna T210N

9 Sept 2003 · Pine River, MN, United States

Cessna T210N · Accident: loss of engine power en route

From Richard I Bong Memorial Airport (SUW) to Pine River Regional Airport (PWC)

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Event

NTSB case
CHI03LA305
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
N5360U
Operator
Unknown
Onboard fatalities
Unknown
Route
From Richard I Bong Memorial Airport (SUW), Superior, WITo Pine River Regional Airport (PWC), Pine River, MN
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
First occurrenceThe 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
Also codedOther events the NTSB coded in the sequence, such as a wire strike after a loss of power. Flight Findings uses them for its kinds of event. Glossary
Fuel exhaustion
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

  • Fluid, fuel › Exhaustion
  • Pilot in command › Preflight planning/preparation, inadequate

Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.

NTSB narrative

The aircraft was substantially damaged during a forced landing following a complete loss of engine power. The pilot reported that during descent he "felt the plane slow up quite quickly." He reported he verified the position of the engine controls, however he was unable to restore power. The pilot stated that he selected an emergency landing field. He noted: "After I cleared the tree line I put down my wheels and ten degrees of flaps. … I had to turn pretty sharply to avoid a large tree that was in the middle of the field. When I felt I had cleared the tree I straightened out the plane and pulled the nose up to flare. The plane did not seem to flare and hit the ground very hard. The landing gear collapsed upon impact and the plane slid on the ground." The pilot reported no malfunctions with the aircraft or engine prior to the loss of engine power. The post-accident examination of the aircraft recovered approximately 8 ounces of fuel from the fuel tanks. No fuel was present in the fuel line running from the firewall to the engine. The fuel tanks and lines appeared to be intact and no evidence of fuel leakage was observed. The pilot stated that he did not visually confirm the fuel level before flight. He reported referencing remaining fuel quantity from a fuel management computer installed in the aircraft. The operating manual for the fuel management computer stated: "[The fuel management computer] is a fuel flow measuring system and NOT a quantity-sensing device. A visual inspection and positive determination of the usable fuel in the fuel tanks is a necessity. Therefore, it is imperative that the determined available usable fuel be manually entered into the system."

Probable cause

An inadequate pre-flight inspection by the pilot due to his failure to visually confirm fuel quantity prior to flight, and the resulting fuel exhaustion. Contributing factors were the pilot's improper use of the fuel management computer installed in the aircraft, and the tree located in the middle of the emergency landing field.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record CHI03LA305
Event ID
20030911X01523
Case number
CHI03LA305
Dataset
historical-pre2008
Source SHA-256
89e2df6d848e7ab3b42e7d7c7a03ff403303057a26ca04c95b3ea67201c3ce74
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: 10ccd04bd14fdb27ab9b17802ad2ac099df2551e53185e13a1b4dcecc4a11c9a; retrieved 2026-09-21T09:23:10.812Z.