What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) Student pilot was taking off to the south on runway 18. A witness stated at approximately 0920, AWOS reported winds 270 @ 8 g 14. The student pilot was limited to making solo flights in a Cessna 172 with 5 knots or less crosswind component. Witness reported seeing the aircraft in a pitch attitude, rolling to the left. The aircraft impacted the ground at a 20-30 degree angle. Damage to the aircraft indicated the left wing struck first, followed by a simultaneous impact of the left main and nose landing gears. The propeller/engine area struck, breaking the crankshaft just aft of the propeller. The right wing hit next, the aircraft then went inverted, struck the ground again, and slid approximately 80 feet. Unable to determine at what point the tail section of the aircraft was broken at the rear window frame. A post accident measurement was taken by a Cessna representative at the flap jackscrew assembly, which he extrapolated to a 20 degree flap setting. No significant mechanical findings were noted.
As the FAA filed it
(-23) STUDENT PILOT WAS TAKING OFF TO THE SOUTH ON RUNWAY 18. A WITNESS STATED AT APPROXIMATELY 0920, AWOS REPORTED WINDS 270 @ 8 G 14. THE STUDENT PILOT WAS LIMITED TO MAKING SOLO FLIGHTS IN A CESSNA 172 WITH 5 KNOTS OR LESS CROSSWIND COMPONENT. WITNESS REPORTED SEEING THE AIRCRAFT IN A PITCH ATTITUDE, ROLLING TO THE LEFT. THE AIRCRAFT IMPACTED THE GROUND AT A 20-30 DEGREE ANGLE. DAMAGE TO THE AIRCRAFT INDICATED THE LEFT WING STRUCK FIRST, FOLLOWED BY A SIMULTANEOUS IMPACT OF THE LEFT MAIN AND NOSE LANDING GEARS. THE PROPELLER/ENGINE AREA STRUCK, BREAKING THE CRANKSHAFT JUST AFT OF THE PROPELLER. THE RIGHT WING HIT NEXT, THE AIRCRAFT THEN WENT INVERTED, STRUCK THE GROUND AGAIN, AND SLID APPROXIMATELY 80 FEET. UNABLE TO DETERMINE AT WHAT POINT THE TAIL SECTION OF THE AIRCRAFT WAS BROKEN AT THE REAR WINDOW FRAME. A POST ACCIDENT MEASUREMENT WAS TAKEN BY A CESSNA REPRESENTATIVE AT THE FLAP JACKSCREW ASSEMBLY, WHICH HE EXTRAPOLATED TO A 20 DEGREE FLAP SETTING. NO SIGNIFICANT MECHANICAL FINDINGS WERE NOTED.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.
Other reports on N75510 · 2
Matched to the same aircraft by N-number and date.