20001209031529I

Incident · Minor damage

FAA incident report · Amtr LANCAIR 235 · Wendover, UT · December 9, 2000

Date
December 9, 2000 · 15:30 local
Place
Wendover, UT
Airport
Wendover Airport
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N417EM
Reported as
Amtr LANCAIR235
People aboard
2
Fatal injuries
0
Pilot’s flight hours
2,521 total300 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) On approach at Wendover, UT airport the pilot noticed a flickering down/lock light for the a/c righ main landing gear after the landing gear was extended. The pilot recycled the gear and got a steady green light indicating the landing gear was down and locked. During the landing rollout the right main landing gear collapsed. The a/c suffered minor damage. The right gear collapsed because the downlock overcenter link was out of adjustment causing inadequate overcenter force. Rod end bearing, p/n HM-6M, for the side strut link assembly was broken after the landing gear collapsed. The broken rod end was welded back together in order to move the a/c from the active runway.

As the FAA filed it

(-23) ON APPROACH AT WENDOVER, UT AIRPORT THE PILOT NOTICED A FLICKERING DOWN/LOCK LIGHT FOR THE A/C RIGH MAIN LANDING GEAR AFTER THE LANDING GEAR WAS EXTENDED. THE PILOT RECYCLED THE GEAR AND GOT A STEADY GREEN LIGHT INDICATING THE LANDING GEAR WAS DOWN AND LOCKED. DURING THE LANDING ROLLOUT THE RIGHT MAIN LANDING GEAR COLLAPSED. THE A/C SUFFERED MINOR DAMAGE. THE RIGHT GEAR COLLAPSED BECAUSE THE DOWNLOCK OVERCENTER LINK WAS OUT OF ADJUSTMENT CAUSING INADEQUATE OVERCENTER FORCE. ROD END BEARING, P/N HM-6M, FOR THE SIDE STRUT LINK ASSEMBLY WAS BROKEN AFTER THE LANDING GEAR COLLAPSED. THE BROKEN ROD END WAS WELDED BACK TOGETHER IN ORDER TO MOVE THE A/C FROM THE ACTIVE RUNWAY.

Other reports on N417EM · 1

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