20000517022179I

Incident · Minor damage

FAA incident report · Amtr LANCAIR 4P · Palo Alto, CA · May 17, 2000

Date
May 17, 2000 · 14:06 local
Place
Palo Alto, CA
Airport
Palo Alto Airport-Santa Clara Cou
Phase of flight
Level Off Touchdown
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N114L
Reported as
Amtr LANCAIR4P
Reported engine
Lycoming TIO540*
People aboard
3
Fatal injuries
0
Pilot’s flight hours
3,000 total470 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)Airplane nose gear failed to extend when gear handle moved to down position during approach to the Palo Alto airport. Alternate gear extension method also failed. The tower was advised a accordingly and equipment was standing by. The landing was made made with little damage to the aircraft, some skin damage and bending of propeller blades. There were no injuries to the pilot and his two passengers. Upon further examination of the nose gear assembly and the gear retraction mechanism, it was determined that the nose wheel was offset 10 degrees from center due to a centering cam failure and that this caused the wheel to jam in the up position.

As the FAA filed it

(-23)AIRPLANE NOSE GEAR FAILED TO EXTEND WHEN GEAR HANDLE MOVED TO DOWN POSITION DURING APPROACH TO THE PALO ALTO AIRPORT. ALTERNATE GEAR EXTENSION METHOD ALSO FAILED. THE TOWER WAS ADVISED A ACCORDINGLY AND EQUIPMENT WAS STANDING BY. THE LANDING WAS MADE MADE WITH LITTLE DAMAGE TO THE AIRCRAFT, SOME SKIN DAMAGE AND BENDING OF PROPELLER BLADES. THERE WERE NO INJURIES TO THE PILOT AND HIS TWO PASSENGERS. UPON FURTHER EXAMINATION OF THE NOSE GEAR ASSEMBLY AND THE GEAR RETRACTION MECHANISM, IT WAS DETERMINED THAT THE NOSE WHEEL WAS OFFSET 10 DEGREES FROM CENTER DUE TO A CENTERING CAM FAILURE AND THAT THIS CAUSED THE WHEEL TO JAM IN THE UP POSITION.

Other reports on N114L · 3

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