20260901010889A

Accident · Substantial damage

FAA accident report · Boeing A75L300 · Taylor, TX · September 1, 2026

Date
September 1, 2026 · 18:00 local
Place
Taylor, TX
Airport
Taylow Municipal Airport
Phase of flight
Landing: Touchdown
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N175MD
NTSB investigation
NTSBCEN26LA305
Reported as
Boeing A75L300
Reported engine
Lycoming R680E series
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Private pilot
Pilot’s flight hours
518 total140 in this make and model94 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 was landing on runway 17 upon touchdown the aircraft began to skid/slip to the left. The pilot applied right rudder and aileron which did not have effect in controlling the skid slip. The aircraft departed the active into the sod, continuing to skid/slip. The aircraft contacted a slight embankment, coming to rest 180 degrees in the opposing direction of the landing heading. No mechanical difficulties were reported by the pilot. The pilot did report that there was a direct crosswind of 7-10 knots during the landing sequence, and that the winds were shifting regularly during the flight.

As the FAA filed it

AIRCRAFT WAS LANDING ON RUNWAY 17 UPON TOUCHDOWN THE AIRCRAFT BEGAN TO SKID/SLIP TO THE LEFT. THE PILOT APPLIED RIGHT RUDDER AND AILERON WHICH DID NOT HAVE EFFECT IN CONTROLLING THE SKID SLIP. THE AIRCRAFT DEPARTED THE ACTIVE INTO THE SOD, CONTINUING TO SKID/SLIP. THE AIRCRAFT CONTACTED A SLIGHT EMBANKMENT, COMING TO REST 180 DEGREES IN THE OPPOSING DIRECTION OF THE LANDING HEADING. NO MECHANICAL DIFFICULTIES WERE REPORTED BY THE PILOT. THE PILOT DID REPORT THAT THERE WAS A DIRECT CROSSWIND OF 7-10 KNOTS DURING THE LANDING SEQUENCE, AND THAT THE WINDS WERE SHIFTING REGULARLY DURING THE FLIGHT.

NTSB investigation

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