20010127000839A

Accident · Substantial damage

FAA accident report · Piper PA-22-160 · Camarillo, CA · January 27, 2001

Date
January 27, 2001 · 11:11 local
Place
Camarillo, CA
Airport
Camarillo Airport
Phase of flight
Takeoff Ground Roll
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N9411D
NTSB investigation
NTSBLAX01LA081
Reported as
Piper PA22160
Reported engine
Lycoming O320B2A
People aboard
1
Fatal injuries
0
Pilot’s flight hours
180 total31 in this make and model18 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) The pilot in command lost control of the a/c on takeoff resulting in a ground loop. Damage consisted of this: left wing including both spars, left airleron, left elevator, both main gear, and possibly fuselage, this a/c is a PA-22-S160, converted to a tailwheel configuration. (.4) on January 27, 2001, at 1111 hours pacific standard time, a Piper PA-22, N9411D, was substantially damaged when the aircraft ground looped during takeoff at Camarillo, California. The private pilot, the sole occupant, was not injured. The local area personal flight was operated by the owner under 14 CFR part 91. Visual meteorological conditions prevailed and no flight plan was filed. The pilot reported that the purpose of the flight was to practice touch-and-go landings at another nearby airport. The airplane had been converted from tricycle to conventional landing gear and the pilot had received a tailwheel aircraft logbook endorsement. The pilot applied about 1/2 of the engine power and intended to perform a "slow takeoff." Runway 26 is 6,010 feet long and 150 feet wide. During the early part of the takeoff roll, when the pilot applied forward pressure on the controls to lift the tail from the runway, the aircraft started to veer to the left. He corrected with right rudder and the airplane entered a skid to the right and ground looped. The airplane came to rest off the right-hand edge of the runway with damage to the left wing, left horizontal stabilizer, and left landing gear. The surface wind was from 020 degrees at 3 knots.

As the FAA filed it

(-23) THE PILOT IN COMMAND LOST CONTROL OF THE A/C ON TAKEOFF RESULTING IN A GROUND LOOP. DAMAGE CONSISTED OF THIS: LEFT WING INCLUDING BOTH SPARS, LEFT AIRLERON, LEFT ELEVATOR, BOTH MAIN GEAR, AND POSSIBLY FUSELAGE, THIS A/C IS A PA-22-S160, CONVERTED TO A TAILWHEEL CONFIGURATION. (.4) ON JANUARY 27, 2001, AT 1111 HOURS PACIFIC STANDARD TIME, A PIPER PA-22, N9411D, WAS SUBSTANTIALLY DAMAGED WHEN THE AIRCRAFT GROUND LOOPED DURING TAKEOFF AT CAMARILLO, CALIFORNIA. THE PRIVATE PILOT, THE SOLE OCCUPANT, WAS NOT INJURED. THE LOCAL AREA PERSONAL FLIGHT WAS OPERATED BY THE OWNER UNDER 14 CFR PART 91. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AND NO FLIGHT PLAN WAS FILED. THE PILOT REPORTED THAT THE PURPOSE OF THE FLIGHT WAS TO PRACTICE TOUCH-AND-GO LANDINGS AT ANOTHER NEARBY AIRPORT. THE AIRPLANE HAD BEEN CONVERTED FROM TRICYCLE TO CONVENTIONAL LANDING GEAR AND THE PILOT HAD RECEIVED A TAILWHEEL AIRCRAFT LOGBOOK ENDORSEMENT. THE PILOT APPLIED ABOUT 1/2 OF THE ENGINE POWER AND INTENDED TO PERFORM A "SLOW TAKEOFF." RUNWAY 26 IS 6,010 FEET LONG AND 150 FEET WIDE. DURING THE EARLY PART OF THE TAKEOFF ROLL, WHEN THE PILOT APPLIED FORWARD PRESSURE ON THE CONTROLS TO LIFT THE TAIL FROM THE RUNWAY, THE AIRCRAFT STARTED TO VEER TO THE LEFT. HE CORRECTED WITH RIGHT RUDDER AND THE AIRPLANE ENTERED A SKID TO THE RIGHT AND GROUND LOOPED. THE AIRPLANE CAME TO REST OFF THE RIGHT-HAND EDGE OF THE RUNWAY WITH DAMAGE TO THE LEFT WING, LEFT HORIZONTAL STABILIZER, AND LEFT LANDING GEAR. THE SURFACE WIND WAS FROM 020 DEGREES AT 3 KNOTS.

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 N9411D · 1

Matched to the same aircraft by N-number and date.