20060108000209A

Accident · Substantial damage

FAA accident report · Piper PA-34-200 · Van Nuys, CA · January 8, 2006

Date
January 8, 2006 · 16:53 local
Place
Van Nuys, CA
Airport
Van Nuys Airport
Phase of flight
Sfl Final Approach
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N4459T
Reported as
Piper PA34200
Reported engine
Continental IO360CONT
People aboard
2
Fatal injuries
0
Pilot’s flight hours
1,750 total120 in this make and model40 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 purpose of the flight was an aircraft checkout for the pilot, who was at the controls at the time of the accident. On the downwind leg for runway 34 right, the CFI sumulated a right engine failure by closing the right throttle. According to the pilot, CFI and witnesses on the ground, everything was normal up to the point of the landing flare. Both pilots stated that during the flare, the airplane rotated rapidly to the right, striking the right wing on the runway. The airplane veered to the right and departed the runway surface. At that point, the airplane pitched up. The CFI took control, leveled the wings and pitched the nose down. The airplane hit the taxiway and slid sideways, right wing first, into a hangar, substantially damaging the airplane. The wind was reported to be 330 at 9 knots during the time of the accident. The CFI recalled a wind report of 330 at 12 prior to landing. Both pilots recalled that the winds were gusting at the time. This would have resulted in a 10 degree crosswind from the left. The right engine was simulated failed, and the throttle was closed. The pilot was using only the left throttle.y

As the FAA filed it

(-23) THE PURPOSE OF THE FLIGHT WAS AN AIRCRAFT CHECKOUT FOR THE PILOT, WHO WAS AT THE CONTROLS AT THE TIME OF THE ACCIDENT. ON THE DOWNWIND LEG FOR RUNWAY 34 RIGHT, THE CFI SUMULATED A RIGHT ENGINE FAILURE BY CLOSING THE RIGHT THROTTLE. ACCORDING TO THE PILOT, CFI AND WITNESSES ON THE GROUND, EVERYTHING WAS NORMAL UP TO THE POINT OF THE LANDING FLARE. BOTH PILOTS STATED THAT DURING THE FLARE, THE AIRPLANE ROTATED RAPIDLY TO THE RIGHT, STRIKING THE RIGHT WING ON THE RUNWAY. THE AIRPLANE VEERED TO THE RIGHT AND DEPARTED THE RUNWAY SURFACE. AT THAT POINT, THE AIRPLANE PITCHED UP. THE CFI TOOK CONTROL, LEVELED THE WINGS AND PITCHED THE NOSE DOWN. THE AIRPLANE HIT THE TAXIWAY AND SLID SIDEWAYS, RIGHT WING FIRST, INTO A HANGAR, SUBSTANTIALLY DAMAGING THE AIRPLANE. THE WIND WAS REPORTED TO BE 330 AT 9 KNOTS DURING THE TIME OF THE ACCIDENT. THE CFI RECALLED A WIND REPORT OF 330 AT 12 PRIOR TO LANDING. BOTH PILOTS RECALLED THAT THE WINDS WERE GUSTING AT THE TIME. THIS WOULD HAVE RESULTED IN A 10 DEGREE CROSSWIND FROM THE LEFT. THE RIGHT ENGINE WAS SIMULATED FAILED, AND THE THROTTLE WAS CLOSED. THE PILOT WAS USING ONLY THE LEFT THROTTLE.Y

Other reports on N4459T · 2

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