19950724048879A

Accident · Substantial damage

FAA accident report · Aircraft · Englewood, CO · July 24, 1995

Date
July 24, 1995 · 13:36 local
Place
Englewood, CO
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N480UP
NTSB investigation
NTSBFTW95LA316

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.

(-16) On July 24, 1995, at 1336 MDT, a Gulfstream aerospace G-1V, N480UP, sustained substantial damage on landing at centennial airport, Englewood, Colorado, when part of the left main landing gear failed and penetrated the wing shortly after touchdown. The two crew members and seven passengers were not injured. Visual meteorological conditions prevailed and an IFR flight plan was filed for this business flight which originated in allentown, Pennsylvania. According to the flight crew, they heard a load "clunk" when the landing gear was lowered. All indications were normal and upon touchdown the left shock absorber assy., which had become detached at the upper fitting, penetrated the wing.

As the FAA filed it

(-16) ON JULY 24, 1995, AT 1336 MDT, A GULFSTREAM AEROSPACE G-1V, N480UP, SUSTAINED SUBSTANTIAL DAMAGE ON LANDING AT CENTENNIAL AIRPORT, ENGLEWOOD, COLORADO, WHEN PART OF THE LEFT MAIN LANDING GEAR FAILED AND PENETRATED THE WING SHORTLY AFTER TOUCHDOWN. THE TWO CREW MEMBERS AND SEVEN PASSENGERS WERE NOT INJURED. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AND AN IFR FLIGHT PLAN WAS FILED FOR THIS BUSINESS FLIGHT WHICH ORIGINATED IN ALLENTOWN, PENNSYLVANIA. ACCORDING TO THE FLIGHT CREW, THEY HEARD A LOAD "CLUNK" WHEN THE LANDING GEAR WAS LOWERED. ALL INDICATIONS WERE NORMAL AND UPON TOUCHDOWN THE LEFT SHOCK ABSORBER ASSY., WHICH HAD BECOME DETACHED AT THE UPPER FITTING, PENETRATED THE WING.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.