20250326002499A

Accident · Substantial damage

FAA accident report · Cessna 180 · San Carlos, CA · March 26, 2025

Date
March 26, 2025 · 11:50 local
Place
San Carlos, CA
Airport
San Carlos Airport
Phase of flight
Landing: Rollout
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N180ZR
NTSB investigation
NTSBWPR25LA119
Reported as
Cessna 180
Reported engine
Continental O-470 series
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Commercial pilot, flight instructor
Pilot’s flight hours
7,242 total1,297 in this make and model181 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.

In a training flight for the commercial certificate, a Cessna 180 performed a three-point landing on runway 12 at San Carlos Airport. Rolling out after landing, the pilot and instructor encountered a crosswind gust from the right and did not provide enough aileron and rudder control input soon enough to prevent a ground loop which was confined within the runway width. Left wing, left horizontal stabilizer, and hub of left main wheel all contacted the surface. The changing wind was directly from the plane's right at 10 knots with gusts to 18 KTS.

(Ksql 261856Z 20010G18KT 10SM SCT022 17/10 A3000

Ksql 261850Z 17013KT 10SM SCT022 17/10 A3000)

As the FAA filed it

IN A TRAINING FLIGHT FOR THE COMMERCIAL CERTIFICATE, A CESSNA 180 PERFORMED A THREE-POINT LANDING ON RUNWAY 12 AT SAN CARLOS AIRPORT. ROLLING OUT AFTER LANDING, THE PILOT AND INSTRUCTOR ENCOUNTERED A CROSSWIND GUST FROM THE RIGHT AND DID NOT PROVIDE ENOUGH AILERON AND RUDDER CONTROL INPUT SOON ENOUGH TO PREVENT A GROUND LOOP WHICH WAS CONFINED WITHIN THE RUNWAY WIDTH. LEFT WING, LEFT HORIZONTAL STABILIZER, AND HUB OF LEFT MAIN WHEEL ALL CONTACTED THE SURFACE. THE CHANGING WIND WAS DIRECTLY FROM THE PLANE'S RIGHT AT 10 KNOTS WITH GUSTS TO 18 KTS.

(KSQL 261856Z 20010G18KT 10SM SCT022 17/10 A3000

KSQL 261850Z 17013KT 10SM SCT022 17/10 A3000)

NTSB investigation

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