20031021032429A

Accident · Destroyed

FAA accident report · Cessna 172N · Olive Branch, MS · October 21, 2003

Date
October 21, 2003 · 09:15 local
Place
Olive Branch, MS
Airport
Olive Branch Airport
Phase of flight
To Init Climb(1st Pwr Reduct)
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N75510
NTSB investigation
NTSBMIA04FA007
Reported as
Cessna 172N
Reported engine
Lycoming O320H2AD
People aboard
1
Fatal injuries
1
Pilot’s certificate
Student
Pilot’s flight hours
39 total36 in this make and model17 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.

(-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.