20150525007719I

Incident · Minor damage

FAA incident report · Hillard Charlie R HAWKER FB60 · Englewood, CO · May 25, 2015

Date
May 25, 2015 · 11:30 local
Place
Englewood, CO
Airport
Centennial
Phase of flight
Landing: Rollout
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N254SF
Reported as
Hillard Charlie R Hawker FB60
Reported engine
Amateur-built UNKNOWN ENG
People aboard
2
Fatal injuries
0
Other injuries
0

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.

The aircraft landed safely at approximately 1130 hours local time on runway 35R at Centennial Airport (kapa). On deceleration rollout the aircraft veered off the runway west side into the median between the runway and taxiway bravo. Both main landing gears collapsed the right main landing gear failed outward and the left main landing gear folded inward. The right main landing gear part lower stay failed by a threaded stem being stripped by its? Attaching nut. The left main landing gear drag link failed due to ductile overload fracturing at the end nearest its attachment to the lower stay. The propeller contacted the ground and the engine stopped. The pilot and one passenger exited the aircraft without incident.

As the FAA filed it

THE AIRCRAFT LANDED SAFELY AT APPROXIMATELY 1130 HOURS LOCAL TIME ON RUNWAY 35R AT CENTENNIAL AIRPORT (KAPA). ON DECELERATION ROLLOUT THE AIRCRAFT VEERED OFF THE RUNWAY WEST SIDE INTO THE MEDIAN BETWEEN THE RUNWAY AND TAXIWAY BRAVO. BOTH MAIN LANDING GEARS COLLAPSED THE RIGHT MAIN LANDING GEAR FAILED OUTWARD AND THE LEFT MAIN LANDING GEAR FOLDED INWARD. THE RIGHT MAIN LANDING GEAR PART LOWER STAY FAILED BY A THREADED STEM BEING STRIPPED BY ITS? ATTACHING NUT. THE LEFT MAIN LANDING GEAR DRAG LINK FAILED DUE TO DUCTILE OVERLOAD FRACTURING AT THE END NEAREST ITS ATTACHMENT TO THE LOWER STAY. THE PROPELLER CONTACTED THE GROUND AND THE ENGINE STOPPED. THE PILOT AND ONE PASSENGER EXITED THE AIRCRAFT WITHOUT INCIDENT.

Other reports on N254SF · 2

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