- Date
- November 17, 2019, 17:30 local (22:30 UTC)
- Place
- DuBois, PA
- Injuries
- 2 uninjured
- Damage
- Substantial damage
- Phase of flight
- Landing
- Aircraft
- N683SPCessna 172
- Defining event
- Landing-aborted after touchdown: Loss of engine power (total)
- Weather
- Visual (VMC) · Day
- Status
- Completed · report May 21, 2020
- Report
- Approved by Office Director
- NTSB office
- General Aviation Accidents
- Parties
- FAA
- FAA report
- 20191117018489A
- Case key
- 100607
From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.
On this page
Probable cause
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.
Findings · 6
NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.
Sequence of events
The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.
Analysis
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.
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.
Aircraft
- Registration
- N683SP
- Reported as
- Cessna 172 (S)
- Category
- Airplane
- Serial number
- 172S8094
- Built
- 1999
- Airframe hours
- 6,938.8
- Engine
- Lycoming IO-360-L2A, 180 horsepower, reciprocating
- Damage
- Substantial damage
- Flight
- Personal · Part 91
- Operator
- Hobart Aviation Inc
- Registered owner
- Hobart Aviation Inc
- Airworthiness certificate
- Standard, Normal
- Last inspection
- 100 hour · October 29, 2019
- Departed
- AKR · Akron, OH
- Destination
- AKR · Akron, OH
- Airport
- DUJ · Dubois Rgnl, runway 25, 5,503 × 100 ft, asphalt
- Equipment
- Stall warning system, Electronic flight bag or handheld device, Auto-pilot, ADS-B
Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.
Flight crew
As NTSB recorded them. NTSB leaves out names.
- Role
- Pilot
- Age
- 20
- Injuries
- None
- Certificate
- Private
- Airplane ratings
- Single-engine land
- Medical
- Class 1, Without waivers/limitations
- Last flight review
- October 5, 2019
- Seat
- Left
- Restraint
- 3-point
- Flight hours
- 103 total · 48 in this make and model · 18 as pilot in command · 13 in the last 90 days · 7 in the last 30 days
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- 130° at 10 knots
- Visibility
- 10 statute miles
- Lowest ceiling
- None
- Temperature
- 36 °F, dew point 25 °F
- Altimeter
- 30.01 inHg
- Observed at
- KDUJ
Docket · 2
The files NTSB released with the investigation on February 7, 2020, on NTSB’s docket system: statements, records, photos and specialists’ reports. 4.9 MB in all.
FAA reports on this event · 1
The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.