20061214029119I

Incident · Minor damage

FAA incident report · Amtr LC41-550FG · Van Nuys, CA · December 14, 2006

Date
December 14, 2006 · 20:41 local
Place
Van Nuys, CA
Airport
Van Nuys Airport
Phase of flight
Level Off Touchdown
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N626ER
Reported as
Amtr LC41550FG
People aboard
2
Fatal injuries
0
Pilot’s flight hours
106 total45 in this make and model50 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) While on approach the aircraft was about 10 KTS high. The aircraft touched down after the numbers on 16L. On landing the aircraft bounced once causing the wheel pant assemblies on both main gears to break off the aircraft. As the wheel pant assemblies came off the aircraft, they caused damage to the wing and fuselage. The nose wheel was rotated 90 degrees to the starboard when aircraft came to a stop. Vibration from the landing caused an improperly installed rear seat to break free causing damage to the interior. The vibration also caused a crease in the paint about 4 inches forward of the port horizontal stabilizer. All three tires had wear marks on the left side walls. The port main tire had a bald spot on it caused by part of the wheel pant being stuck in front of it.

As the FAA filed it

(-23) WHILE ON APPROACH THE AIRCRAFT WAS ABOUT 10 KTS HIGH. THE AIRCRAFT TOUCHED DOWN AFTER THE NUMBERS ON 16L. ON LANDING THE AIRCRAFT BOUNCED ONCE CAUSING THE WHEEL PANT ASSEMBLIES ON BOTH MAIN GEARS TO BREAK OFF THE AIRCRAFT. AS THE WHEEL PANT ASSEMBLIES CAME OFF THE AIRCRAFT, THEY CAUSED DAMAGE TO THE WING AND FUSELAGE. THE NOSE WHEEL WAS ROTATED 90 DEGREES TO THE STARBOARD WHEN AIRCRAFT CAME TO A STOP. VIBRATION FROM THE LANDING CAUSED AN IMPROPERLY INSTALLED REAR SEAT TO BREAK FREE CAUSING DAMAGE TO THE INTERIOR. THE VIBRATION ALSO CAUSED A CREASE IN THE PAINT ABOUT 4 INCHES FORWARD OF THE PORT HORIZONTAL STABILIZER. ALL THREE TIRES HAD WEAR MARKS ON THE LEFT SIDE WALLS. THE PORT MAIN TIRE HAD A BALD SPOT ON IT CAUSED BY PART OF THE WHEEL PANT BEING STUCK IN FRONT OF IT.