ATL92LA003
1991-10-06 · GADSDEN, Alabama, United States · Minor · 1 aircraft · Status: Completed
Airport GAD
Current FAA registration · N4726X
- Make / Model
- CESSNA 150G
- Year of manufacture
- 1966 · 25 years old at event
- Engine
- CONT MOTOR 0-200 SERIES (100 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19660805
- ADS-B equipped
- Yes — Mode-S A5CBC8
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
FUEL STARVATION DUE TO INCORRECT FUEL LINE INSTALLATIONS, AN INOPERATIVE FUEL BOOST PUMP, AND INCORRECT PILOT PROCEDURE. A FACTOR IN THIS ACCIDENT WAS THE PILOT'S INTENTIONAL OPERATION WITH A KNOWN FUEL SYSTEM DEFICIENCY.
Factual narrative
THE PLT WAS AWARE OF A PROBLEM WITH THE AIRCRAFT FUEL SYSTEM, SINCE FUEL FROM THE RIGHT MAIN TANK WOULD FEED QUICKER THAN FROM THE LEFT MAIN TANK. RATHER THAN HAVE THE A/C REPAIRED IN FLORIDA, HE ELECTED TO FLY THE A/C TO HIS HOME IN INDIANA TO HAVE THE REPAIRS DONE THERE. WHILE ON APPROACH TO A REFUELING STOP, HE REPORTED THAT BOTH ENGINES QUIT SIMULTANEOUSLY. A FORCED LANDING WAS MADE IN A NEARBY FIELD. THE INVESTIGATION REVEALED THAT THE LT TANK BOOST PUMP WAS INOP, AND THE FUEL SYSTEM CROSSFEED LINES WERE INCORRECTLY INSTALLED (NORMAL X-FEED WAS DISABLED). THUS, FUEL FROM THE RT, MAIN TANK WAS PRESSURE FED TO THE LT, MAIN TANK, AND THEN OVERBOARD, UNTIL THE RT TANK WAS EMPTIED, AND THE RT ENGINE QUIT. HOWEVER, FUEL WAS STILL AVAILABLE TO THE LT ENGINE. THEREFORE THE SAFETY BOARD BELIEVES THAT THE PILOT SELECTED X-FEED ON THE LT FUEL SELECTOR AFTER THE RT ENGINE QUIT; THIS SUBSEQUENTLY SHUT OFF FUEL TO THE LT ENGINE. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1991_ATL92LA003.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
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Related research
Matched on aircraft type or causal vocabulary (stall, fuel starvation). All research papers
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- Embry-Riddle Scholarly Commons 2015 · Journal article (JAAER) Is “Green Dot” Always the Optimum Engines-Out Glide Speed on the Airbus A320 Aircraft?
The dual-engine failure checklist of the Airbus A320 states that the optimum airspeed at which the aircraft can be flown is the “green dot” speed when an engine restart is considered impossible.
- NASA NTRS 2026 · Conference Paper Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
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