19961125045949A

Accident · Substantial damage

FAA accident report · Cessna 172P · Van Nuys, CA · November 25, 1996

Date
November 25, 1996 · 13:35 local
Place
Van Nuys, CA
Airport
Van Nuys Airport
Phase of flight
Go Round (Aborted VFR)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N54686
NTSB investigation
NTSBLAX97LA053
Reported as
Cessna 172P
Reported engine
Lycoming O320D2J
People aboard
2
Fatal injuries
0
Pilot’s flight hours
69 total69 in this make and model32 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.

(.4) During a private pilot practical flight test, the applicant (a student pilot) made a simulated soft field approach, and the aircraft bounced 5 to 6 feet in the air after touchdown. The student decided to go-around and applied full power, but the aircraft rolled left and drug its left wing tip. The flight examiner attempted to take control of the aircraft, but was unable to prevent it from again colliding with the runway. At the time of the accident, a 5-knot/80-degree left crosswind was reported. According to the aircraft manufacturer, the crosswind component was within the aircraft performance parameters.

As the FAA filed it

(.4) DURING A PRIVATE PILOT PRACTICAL FLIGHT TEST, THE APPLICANT (A STUDENT PILOT) MADE A SIMULATED SOFT FIELD APPROACH, AND THE AIRCRAFT BOUNCED 5 TO 6 FEET IN THE AIR AFTER TOUCHDOWN. THE STUDENT DECIDED TO GO-AROUND AND APPLIED FULL POWER, BUT THE AIRCRAFT ROLLED LEFT AND DRUG ITS LEFT WING TIP. THE FLIGHT EXAMINER ATTEMPTED TO TAKE CONTROL OF THE AIRCRAFT, BUT WAS UNABLE TO PREVENT IT FROM AGAIN COLLIDING WITH THE RUNWAY. AT THE TIME OF THE ACCIDENT, A 5-KNOT/80-DEGREE LEFT CROSSWIND WAS REPORTED. ACCORDING TO THE AIRCRAFT MANUFACTURER, THE CROSSWIND COMPONENT WAS WITHIN THE AIRCRAFT PERFORMANCE PARAMETERS.

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 N54686 · 1

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