19971101047989A

Accident · Substantial damage

FAA accident report · Cessna 172P · Tooele, UT · November 1, 1997

Date
November 1, 1997 · 10:55 local
Place
Tooele, UT
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N96575
NTSB investigation
NTSBFTW98LA041
Reported as
Cessna 172P

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.

(-16) Airman competency - the student pilot failed to maintain control of the aircraft during the landing phase of a touch-and-go landing. The aircraft touched down first on the right landing gear and was not aligned with the runway. The student pilot failed to maintain directional control of the aircraft which exited the runway to the left, struck a runway distance marker, and subsequently stopped after impacting a wire fence. The aircraft's left wing was buckled, its left main landing gear and propeller were damaged. A light quartering headwind existed. The aircraft's fuel load was unbalanced (right wing heavy). The student pilot was on second solo and had made approximately 7 solo landings prior to the accident. The student pilot had logged a total of 29 flight hours prior to this flight with .6 hours total solo flight time.

As the FAA filed it

(-16) AIRMAN COMPETENCY - THE STUDENT PILOT FAILED TO MAINTAIN CONTROL OF THE AIRCRAFT DURING THE LANDING PHASE OF A TOUCH-AND-GO LANDING. THE AIRCRAFT TOUCHED DOWN FIRST ON THE RIGHT LANDING GEAR AND WAS NOT ALIGNED WITH THE RUNWAY. THE STUDENT PILOT FAILED TO MAINTAIN DIRECTIONAL CONTROL OF THE AIRCRAFT WHICH EXITED THE RUNWAY TO THE LEFT, STRUCK A RUNWAY DISTANCE MARKER, AND SUBSEQUENTLY STOPPED AFTER IMPACTING A WIRE FENCE. THE AIRCRAFT'S LEFT WING WAS BUCKLED, ITS LEFT MAIN LANDING GEAR AND PROPELLER WERE DAMAGED. A LIGHT QUARTERING HEADWIND EXISTED. THE AIRCRAFT'S FUEL LOAD WAS UNBALANCED (RIGHT WING HEAVY). THE STUDENT PILOT WAS ON SECOND SOLO AND HAD MADE APPROXIMATELY 7 SOLO LANDINGS PRIOR TO THE ACCIDENT. THE STUDENT PILOT HAD LOGGED A TOTAL OF 29 FLIGHT HOURS PRIOR TO THIS FLIGHT WITH .6 HOURS TOTAL SOLO FLIGHT TIME.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.