20220507006709I

Incident · Minor damage

FAA incident report · Cessna 210 · Greenville, TX · May 7, 2022

Date
May 7, 2022 · 12:20 local
Place
Greenville, TX
Airport
Majors Airport
Phase of flight
Landing: Approach
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N7411E
Reported as
Cessna 210
Reported engine
Continental I0-470 series
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Private pilot, student
Pilot’s flight hours
70 total40 in this make and model30 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

Aircraft lost engine power contacted terrain 0.2 NM short of runway 17 and came to rest approximately 0.17 NM short of the runway.

Trace amounts of fuel were found in right wing tank. Right wing tank bladder had several creases longitudinally. However, this did not contribute to the fuel starvation. Approximately 25 gallons of fuel found in the left wing tank. Throttle and mixture were moved forward and the electric boost pump was turned on. When the fuel selector was switched to the left tank, sufficient fuel flow was noted on the cockpit instrument panel.

As the FAA filed it

AIRCRAFT LOST ENGINE POWER CONTACTED TERRAIN 0.2 NM SHORT OF RUNWAY 17 AND CAME TO REST APPROXIMATELY 0.17 NM SHORT OF THE RUNWAY.

TRACE AMOUNTS OF FUEL WERE FOUND IN RIGHT WING TANK. RIGHT WING TANK BLADDER HAD SEVERAL CREASES LONGITUDINALLY. HOWEVER, THIS DID NOT CONTRIBUTE TO THE FUEL STARVATION. APPROXIMATELY 25 GALLONS OF FUEL FOUND IN THE LEFT WING TANK. THROTTLE AND MIXTURE WERE MOVED FORWARD AND THE ELECTRIC BOOST PUMP WAS TURNED ON. WHEN THE FUEL SELECTOR WAS SWITCHED TO THE LEFT TANK, SUFFICIENT FUEL FLOW WAS NOTED ON THE COCKPIT INSTRUMENT PANEL.