20210826015039A

Accident · Substantial damage

FAA accident report · Cessna 172M · Olive Branch, MS · August 26, 2021

Date
August 26, 2021 · 19:31 local
Place
Olive Branch, MS
Phase of flight
Landing: Touchdown
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N12573
NTSB investigation
NTSBCEN21LA392
Reported as
Cessna 172M
Reported engine
Lycoming 0-320 series
People aboard
1
Fatal injuries
0
Other injuries
1
Pilot’s certificate
Student
Pilot’s flight hours
16 total16 in this make and model8 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.

Student pilot on long solo cross country flight departed on 08/26/2021 runway 18, olv, en route to crx, tup, and then return for final stop in olv. On final approach and stop to olv, runway 18L, pilot was notified there was an 8 knot crosswind from the east. Upon landing the aircraft bounced after initial landing. The pilot mismanaged controls applying opposite directional control to the ailerons and rudder pedals causing the aircraft to veer off the runway into a ditch. The aircraft received substantial damage from the impact to the engine mounts and forward lower fuselage structure.

As the FAA filed it

STUDENT PILOT ON LONG SOLO CROSS COUNTRY FLIGHT DEPARTED ON 08/26/2021 RUNWAY 18, OLV, EN ROUTE TO CRX, TUP, AND THEN RETURN FOR FINAL STOP IN OLV. ON FINAL APPROACH AND STOP TO OLV, RUNWAY 18L, PILOT WAS NOTIFIED THERE WAS AN 8 KNOT CROSSWIND FROM THE EAST. UPON LANDING THE AIRCRAFT BOUNCED AFTER INITIAL LANDING. THE PILOT MISMANAGED CONTROLS APPLYING OPPOSITE DIRECTIONAL CONTROL TO THE AILERONS AND RUDDER PEDALS CAUSING THE AIRCRAFT TO VEER OFF THE RUNWAY INTO A DITCH. THE AIRCRAFT RECEIVED SUBSTANTIAL DAMAGE FROM THE IMPACT TO THE ENGINE MOUNTS AND FORWARD LOWER FUSELAGE STRUCTURE.

NTSB investigation

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