19990504004559A

Accident · Substantial damage

FAA accident report · Bbavia 7AC · Lancaster, CA · May 4, 1999

Date
May 4, 1999 · 10:42 local
Place
Lancaster, CA
Airport
Gen Wm J Fox Airfield Airport
Phase of flight
Ground Taxi, Other Airplane
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N2403E
NTSB investigation
NTSBLAX99LA169
Reported as
Bbavia 7AC
Reported engine
Continental C858
People aboard
1
Fatal injuries
0
Pilot’s flight hours
1,733 total962 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.

Acft ground looped and flipped over while taxiing to the rwy in preparation for departure, other circumstances are unknown. (.19) on may 4, 1999, at 1045 hours pacific daylight time, an Aeronca 7AC, N2403E, ground looped and came to rest inverted on a taxiway while preparing for an intersection departure on runway 24 at the general fox field airport, Lancaster, California. The aircraft, owned and operated by the pilot under 14 CFR part 91, sustained substantial damage. The private pilot, the sole occupant, was not injured. Visual meteorological conditions existed for the personal flight and no flight plan was filed. The flight was originating at the time and scheduled to terminate at the whiteman airport, los angeles, California, on the day of the accident. The pilot stated that he had been cleared to taxi to runway 24 for takeoff. In order to position the aircraft on the runway, the pilot conducted a 360-degree turn. The pilot stated that during the turn he lost control of the aircraft after it was struck by a gust of wind that elevated the tail. The pilot reported gusty wind conditions existed and there were no mechanical anomalies with the aircraft. (.4)the pilot had been cleared for an intersection takeoff and was attempting a 360-degree turn to realign the airplane with the taxiway. The winds at the time the pilot attempted the maneuver were from 270 degrees at 20 knots, with higher gusts to 26 knots. As the tail turned into the wind during the turn, the tail lifted and the airplane nosed over. The pilot reported that there were no mechanical abnormalities with the conventional gear airplane.

As the FAA filed it

ACFT GROUND LOOPED AND FLIPPED OVER WHILE TAXIING TO THE RWY IN PREPARATION FOR DEPARTURE, OTHER CIRCUMSTANCES ARE UNKNOWN. (.19) ON MAY 4, 1999, AT 1045 HOURS PACIFIC DAYLIGHT TIME, AN AERONCA 7AC, N2403E, GROUND LOOPED AND CAME TO REST INVERTED ON A TAXIWAY WHILE PREPARING FOR AN INTERSECTION DEPARTURE ON RUNWAY 24 AT THE GENERAL FOX FIELD AIRPORT, LANCASTER, CALIFORNIA. THE AIRCRAFT, OWNED AND OPERATED BY THE PILOT UNDER 14 CFR PART 91, SUSTAINED SUBSTANTIAL DAMAGE. THE PRIVATE PILOT, THE SOLE OCCUPANT, WAS NOT INJURED. VISUAL METEOROLOGICAL CONDITIONS EXISTED FOR THE PERSONAL FLIGHT AND NO FLIGHT PLAN WAS FILED. THE FLIGHT WAS ORIGINATING AT THE TIME AND SCHEDULED TO TERMINATE AT THE WHITEMAN AIRPORT, LOS ANGELES, CALIFORNIA, ON THE DAY OF THE ACCIDENT. THE PILOT STATED THAT HE HAD BEEN CLEARED TO TAXI TO RUNWAY 24 FOR TAKEOFF. IN ORDER TO POSITION THE AIRCRAFT ON THE RUNWAY, THE PILOT CONDUCTED A 360-DEGREE TURN. THE PILOT STATED THAT DURING THE TURN HE LOST CONTROL OF THE AIRCRAFT AFTER IT WAS STRUCK BY A GUST OF WIND THAT ELEVATED THE TAIL. THE PILOT REPORTED GUSTY WIND CONDITIONS EXISTED AND THERE WERE NO MECHANICAL ANOMALIES WITH THE AIRCRAFT. (.4)THE PILOT HAD BEEN CLEARED FOR AN INTERSECTION TAKEOFF AND WAS ATTEMPTING A 360-DEGREE TURN TO REALIGN THE AIRPLANE WITH THE TAXIWAY. THE WINDS AT THE TIME THE PILOT ATTEMPTED THE MANEUVER WERE FROM 270 DEGREES AT 20 KNOTS, WITH HIGHER GUSTS TO 26 KNOTS. AS THE TAIL TURNED INTO THE WIND DURING THE TURN, THE TAIL LIFTED AND THE AIRPLANE NOSED OVER. THE PILOT REPORTED THAT THERE WERE NO MECHANICAL ABNORMALITIES WITH THE CONVENTIONAL GEAR AIRPLANE.

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 N2403E · 2

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