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Aviation safety reports, made easier to study

NTSB Reports is an independent research and search tool for public aviation accident and incident records. It brings NTSB aviation reports, structured fields, docket files, extracted figures, photos, videos, and update history into one searchable interface.

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July 24, 1995 · Gulfstream GV-1 · N480UP

Englewood, CO

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
July 24, 1995
Injury Outcomes
No injuries (9 uninjured)
Location
Englewood, CO
Aircraft
Gulfstream GV-1
Tail Number
N480UP
Injuries
None
Aircraft Damage
Substantial
NTSB Number
FTW95LA316

DURING LANDING ROLL/TAXI, FOLLOWING A NORMAL FLIGHT AND LANDING, THE LEFT MAIN LANDING GEAR STRUT DISCONNECTED AND THE STRUT PENETRATED THE LANDING GEAR FAIRING BOX.

NTSB Probable Cause

FAILURE OF THE LEFT MAIN LANDING GEAR STRUT ATTACHMENT FOR UNDETERMINED REASONS.

Full Narrative

On July 24, 1995, at 1336 mountain daylight time, a Gulfstream Aerospace GV-1, N480UP, sustained substantial damage on landing at Centennial Airport, Englewood, Colorado, when part of the left main landing gear penetrated the wing during landing/taxi. 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 (PA). According to the crew, the flight from Allentown, PA to their destination was uneventful. They were given a visual approach to runway 33 at Centennial Airport and the landing and taxi appeared normal; however, they noted a slight list to the left during taxi. The aircraft was parked at the AMR Combs passenger facility and the passengers disembarked normally. During post flight, the crew found damage to the left main landing gear assembly. Items incurring damage were the tires, shock strut, cables/wiring, left gear fairing box, and door fairing. It was found that the left shock strut had penetrated the gear fairing box aft of the gear well. The left strut and right knuckle and pins were tested at the facilities of Applied Technical Services, Incorporated, Marietta, Georgia. Their report is attached and states that the most likely failure scenario is that the through bolt loosened and the pin fell out allowing the strut to move abnormal to its design function. The left knuckle and pins were not recovered. A copy of the Applied Technical Services report was forwarded to the Board's Materials Laboratory for review. The review concurred with the report.

Flight

Event TypeAccident
Event Time13:36 MDT
Nearest AirportCentennial Airport (0nm)
Runway33
Runway Length10002 ft
Runway Width101 ft
Flight Plan FiledIFR
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftGulfstream GV-1
Tail NumberN480UP
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines2
Engine TypeTurbojet
Engine DetailsRolls-Royce · TAY 611-8 · Turbojet · 14000
Seats18

People & Injuries

Injury SummaryNo injuries (9 uninjured)
Fatal0
Serious0
Minor0
Uninjured9
Total9
Crew 1Age 54 · First Class

Conditions

ConditionsVMC
LightDaylight
Wind360° @ 5 kt
Visibility30 sm
CeilingNone
Temperature / Dew Point39 C
Altimeter30.00 inHg
Observation Time19:47
Weather SourceWFAC

Appendix: Source Data