19980629015269A

Accident · Substantial damage

FAA accident report · Trytek 65-CA · Phoenix, AZ · June 29, 1998

Date
June 29, 1998 · 10:05 local
Place
Phoenix, AZ
Airport
Phoenix-Deer Valley Municipal Airport
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N34482
NTSB investigation
NTSBLAX98LA217
Reported as
Trytek 65CA
Reported engine
Continental A658
People aboard
2
Fatal injuries
0
Pilot’s flight hours
152 total145 in this make and model19 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.

(.19) On June 29, 1998, at 1005 hours mountain standard time, an Aeronca chief 65-CA, N34482, struck the lights at the end of the runway at the Deer valley airport, Phoenix, Arizona. The aircraft sustained substantial damage, and the private pilot and passenger, the sole occupants, were not injured. The local personal flight was terminating at the time of the accident. Visual meteorological conditions prevailed and no flight plan was filed. The pilot reported that he performed a full-stall landing on runway 25R. During the rollout, the aircraft veered to the left. The pilot stated that he applied aileron to try to keep the plane level, but the airplane continued to pull to the left. He reported that to avoid having the right wing contact the ground, he decided to roll off the runway. The aircraft contacted the visual approach slope indicator (VASI) lights causing damage to the horizontal stabilizer. The pilot reported that he had not noticed any crosswind component on the final approach. The wind was from 220 degrees at 10 knots. The pilot reported no mechanical malfunction with the aircraft prior to the accident. (.4) the pilot performed a full-stall landing and, during the landing rollout, the airplane veered to the left. He stated that he applied aileron to keep the aircraft level, but the airplane continued to pull to the left. He decided to roll off the runway in order to avoid having the right wing contact the ground. The aircraft struck the visual approach slope indicator lights. The pilot reported that he had not noted any crosswind component noticed on the final approach. He further reported that he had not experienced any mechanical malfunction with the aircraft prior to the accident. (-23) pilot reported normal landing. On rollout speed was estimated to be approximately 30 mph. The plane pulled severely to the left. Aileron was applied to keep the plane level. The wheels squealed and the plane continued to pull hard to the left. In order to avoid contacting the right wing with the ground, the pilot opted to leave the runway. Speed departing the runway was approximately 20 mph. Contact was made with the vertical approach slope indicator (VASI). Plane was taxied back to hangar.

As the FAA filed it

(.19) ON JUNE 29, 1998, AT 1005 HOURS MOUNTAIN STANDARD TIME, AN AERONCA CHIEF 65-CA, N34482, STRUCK THE LIGHTS AT THE END OF THE RUNWAY AT THE DEER VALLEY AIRPORT, PHOENIX, ARIZONA. THE AIRCRAFT SUSTAINED SUBSTANTIAL DAMAGE, AND THE PRIVATE PILOT AND PASSENGER, THE SOLE OCCUPANTS, WERE NOT INJURED. THE LOCAL PERSONAL FLIGHT WAS TERMINATING AT THE TIME OF THE ACCIDENT. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AND NO FLIGHT PLAN WAS FILED. THE PILOT REPORTED THAT HE PERFORMED A FULL-STALL LANDING ON RUNWAY 25R. DURING THE ROLLOUT, THE AIRCRAFT VEERED TO THE LEFT. THE PILOT STATED THAT HE APPLIED AILERON TO TRY TO KEEP THE PLANE LEVEL, BUT THE AIRPLANE CONTINUED TO PULL TO THE LEFT. HE REPORTED THAT TO AVOID HAVING THE RIGHT WING CONTACT THE GROUND, HE DECIDED TO ROLL OFF THE RUNWAY. THE AIRCRAFT CONTACTED THE VISUAL APPROACH SLOPE INDICATOR (VASI) LIGHTS CAUSING DAMAGE TO THE HORIZONTAL STABILIZER. THE PILOT REPORTED THAT HE HAD NOT NOTICED ANY CROSSWIND COMPONENT ON THE FINAL APPROACH. THE WIND WAS FROM 220 DEGREES AT 10 KNOTS. THE PILOT REPORTED NO MECHANICAL MALFUNCTION WITH THE AIRCRAFT PRIOR TO THE ACCIDENT. (.4) THE PILOT PERFORMED A FULL-STALL LANDING AND, DURING THE LANDING ROLLOUT, THE AIRPLANE VEERED TO THE LEFT. HE STATED THAT HE APPLIED AILERON TO KEEP THE AIRCRAFT LEVEL, BUT THE AIRPLANE CONTINUED TO PULL TO THE LEFT. HE DECIDED TO ROLL OFF THE RUNWAY IN ORDER TO AVOID HAVING THE RIGHT WING CONTACT THE GROUND. THE AIRCRAFT STRUCK THE VISUAL APPROACH SLOPE INDICATOR LIGHTS. THE PILOT REPORTED THAT HE HAD NOT NOTED ANY CROSSWIND COMPONENT NOTICED ON THE FINAL APPROACH. HE FURTHER REPORTED THAT HE HAD NOT EXPERIENCED ANY MECHANICAL MALFUNCTION WITH THE AIRCRAFT PRIOR TO THE ACCIDENT. (-23) PILOT REPORTED NORMAL LANDING. ON ROLLOUT SPEED WAS ESTIMATED TO BE APPROXIMATELY 30 MPH. THE PLANE PULLED SEVERELY TO THE LEFT. AILERON WAS APPLIED TO KEEP THE PLANE LEVEL. THE WHEELS SQUEALED AND THE PLANE CONTINUED TO PULL HARD TO THE LEFT. IN ORDER TO AVOID CONTACTING THE RIGHT WING WITH THE GROUND, THE PILOT OPTED TO LEAVE THE RUNWAY. SPEED DEPARTING THE RUNWAY WAS APPROXIMATELY 20 MPH. CONTACT WAS MADE WITH THE VERTICAL APPROACH SLOPE INDICATOR (VASI). PLANE WAS TAXIED BACK TO HANGAR.

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 N34482 · 1

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