GAA20CA089
2019-11-17 · DuBois, Pennsylvania, United States · None · 1 aircraft · Status: Completed
Airport DUJ
Current FAA registration · N683SP
- Make / Model
- CESSNA 172S
- Year of manufacture
- 1999 · 20 years old at event
- Engine
- LYCOMING I0360 SER (180 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19990201
- ADS-B equipped
- Yes — Mode-S A90FFA
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's improper fuel management, which resulted in fuel starvation and a total loss of engine power, and his subsequent improper landing flare, which resulted in a hard, bounced landing. Contributing to the accident were the pilot's improper preflight inspection during which he failed to see that the right fuel cap was not secured.
Factual narrative
The pilot reported that the airplane was refueled while he performed the pre-flight inspection at night, but the right fuel tank fuel cap was not secured. He recalled that the fuel selector had been set to Both, and about halfway through the flight, he noticed that the right fuel tank appeared full, but the left fuel gauge indicated that fuel was being consumed from the left tank. He decided that he would, "check the situation out" when he reached his destination. About 5 miles from his destination, he noticed that the left wing tank fuel quantity indicator showed that the left tank had 5-gallons remaining, and that the right tank was still full. During approach, the airplane became, "very unstable and seemed to be uncoordinated." The stall warning horn sounded, and he applied left aileron and left rudder to align the airplane's heading with the runway heading but was unsuccessful. He aborted the landing, established a climb and retracted the flaps. The Low Fuel warning light illuminated, and he switched the fuel selector to the right tank. The engine lost power, and he made a right tear drop turn back to the runway. The airplane was about 1,000ft above ground level, and he pitched for best glide airspeed about 70 knots, and he attempted to restart the engine, but the engine did not start. He lowered the nose, the airspeed increased to 85 knots and he put in 20° of flaps and landed on the runway. The airplane bounced hard and returned to the runway before coming to a stop. The airplane sustained substantial damage to the lower fuselage longerons. The pilot reported that there were no mechanical malfunctions or failures with the airplane that would have precluded normal operation. The pilot reported that the airplane was refueled while he performed the preflight inspection at night. He recalled that the fuel selector had been set to "both," and about halfway through the flight, he noticed that the right fuel tank appeared full but that the left fuel gauge indicated that fuel was being consumed from the left tank. He decided that he would "check the situation " when he reached his destination. About 5 miles from his destination, he noticed that the left-wing tank fuel quantity indicator showed that the left tank had 5 gallons remaining and that the right tank was still full. The pilot stated that, during the approach, the airplane became "very unstable and seemed to be uncoordinated." The stall warning horn sounded, and he applied left aileron and left rudder to align the airplane's heading with the runway heading but was unsuccessful. He aborted the landing, established a climb, and retracted the flaps. The Low Fuel warning light illuminated, and he switched the fuel selector to the right tank. The engine lost power, and he made a right tear drop turn back to the runway. When the airplane was about 1,000 ft above ground level, he pitched for best glide airspeed, about 70 knots, and he attempted to restart the engine to no avail. He lowered the nose, the airspeed increased to 85 knots, and he added 20° of flaps and landed on the runway. The airplane bounced hard and then came to a stop. After the accident, it was determined that the right fuel cap was not secured and had fallen off the airplane onto the runway during takeoff. The airplane sustained substantial damage to the lower fuselage longerons. The pilot reported that there were no preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Aircraft-Fluids/misc hardware-Fluids-Fuel-Fluid management - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Landing flare-Not attained/maintained - C
- C Personnel issues-Task performance-Use of equip/info-Use of equip/system-Pilot - C
- F Personnel issues-Task performance-Inspection-Preflight inspection-Pilot - F
- F Personnel issues-Action/decision-Action-Lack of action-Pilot - F
- — Personnel issues-Task performance-Use of equip/info-Use of checklist-Pilot
Verbatim from NTSB's published report. Source file
NTSB_2019_GAA20CA089.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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During the summer of 2015, a series of three full-scale crash tests were performed at the Landing and Impact Research Facility located at NASA Langley Research Center of Cessna 172 aircraft.
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