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NYC91LA224 · Cessna 337

27 Aug 1991 · Urbana, OH, United States

Cessna 337 · Accident: partial loss of engine power (non-mechanical) during initial climb

From VFY · London, OH to an unrecorded destination

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Event

NTSB case
NYC91LA224
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
0
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 337

Aircraft type
Cessna 337
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
N6304F
Operator
Martin J. Cook · private individual
Onboard fatalities
Unknown
Route
From VFY · London, OHTo not recorded
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
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
Partial loss of engine power (non-mechanical)
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
Stall/mush
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

  • Pilot in command › Lack of total experience in type of aircraft
  • Pilot in command › Procedures/directives, not followed
  • Pilot in command › Stall/mush, encountered
  • Powerplant › Failure, total
  • Terrain condition › Water

Approximate · Estimated position: the centre of Urbana, OH, the place the record names. Not the accident site.

NTSB narrative

THE PILOT'S PREFLIGHT CONSISTED OF CHECKING THE FUEL TANKS WITH A STICK, AND FINDING ABOUT 2 INCHES OF FUEL IN THE RIGHT MAIN FUEL TANK. THE AIRPLANE HAD JUST COME OUT OF MAINTENANCE BECAUSE OF INOPERATIVE FUEL GAUGES. THE PILOT WAS RETURNING TO HIS HOME AIRPORT, LANDED AND INTENDED TO TAKEOFF AGAIN. BECAUSE OF WINDS HE HAD TO TAXI TO A DIFFERENT RUNWAY. JUST AFTER TAKEOFF AND AT A LOW ALTITUDE THE PILOT REALIZED THE REAR ENGINE HAD FAILED. THE AIRPLANE STARTED TO STALL, HOWEVER THE PILOT SAID THERE WAS NOT ENOUGH RUNWAY REMAINING TO ABORT THE TAKE OFF. HE ELECTED TO MAKE A FORCED LANDING AND CAME TO REST IN A POND. THE FUEL SELECTOR FOR THE REAR ENGINE WAS FOUND ON THE RIGHT MAIN TANK. A CESSNA SERVICE LETTER AND AD HAD BEEN ISSUED FOR THIS TYPE AIRPLANE CALLING FOR AN OPERATIONAL PROCEDURE; TO LEAD WITH THE REAR ENGINE WHILE TAXIING, AND DURING TAKE OFF, IN ORDER TO MORE CLEARLY RECOGNIZE A REAR ENGINE FAILURE. THE PILOT'S STATEMENT DID NOT INDICATE THAT HE HAD COMPLIED WITH EITHER THE SERVICE LETTER OR THE AD.

Probable cause

THE PILOT'S FAILURE TO FOLLOW PROCEDURES AND DIRECTIVES WHICH RESULTED IN THE FAILURE OF THE PILOT TO RECOGNIZE THE STOPPAGE OF THE REAR ENGINE PRIOR TO TAKE OFF. ADDITIONALLY THE LACK OF TOTAL ENGINE POWER RESULTED IN THE INABILITY OF THE PILOT TO MAINTAIN THE PROPER CLIMB SPEED, AND RESULTED IN A SUBSEQUENT FORCED LANDING IN WATER. FACTORS RELATED TO THE ACCIDENT WERE THE PILOT'S FAILURE TO COMPLY WITH THE MANUFACTURER'S SERVICE LETTER PERTAINING TO THE OPERATIONAL PROCEDURES TO PREVENT A REAR ENGINE POWER LOSS, AND THE PILOT'S TOTAL LACK OF FLYING EXPERIENCE IN THIS TYPE OF AIRPLANE.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record NYC91LA224
Event ID
20001212X17969
Case number
NYC91LA224
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. 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: 665c1389acce2e6e6492f0a2c933919cc43cae80033a3e7ab423cdc82aabc92d; retrieved 2026-09-21T23:27:55.520Z.