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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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September 25, 2000 · North American T-28D · N28YF

Heber City, UT

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
September 25, 2000
Injury Outcomes
No injuries (1 uninjured)
Location
Heber City, UT
Aircraft
North American T-28D
Tail Number
N28YF
Injuries
None
Aircraft Damage
Substantial
NTSB Number
DEN01LA006

The pilot said that during the landing roll, the nose wheel began to shimmy. As the airplane slowed down, the shimmying became worse. As the airplane approached 40 knots, the nose landing gear collapsed, and the propeller began striking the runway. Postaccident examination by Engineering Systems, Inc., Aurora, Illinois, determined that the nose wheel shimmy damper had malfuctioned. They determined that there was grit behind both cylinder end caps, and there was evidence of a slow hydraulic leak from the damper.

NTSB Probable Cause

the failure of the nose wheel landing gear shimmy damper, which resulted in failure and collapse of the nose wheel landing gear during landing roll.

Full Narrative

On September 25, 2000, at approximately 1015 mountain daylight time, a North American T-28D, N28YF, was substantially damaged when the nose gear collapsed during landing roll at Russ McDonald Airfield, Heber City, Utah. The airline transport pilot, the sole occupant aboard the airplane, was not injured. The pilot was operating the airplane under Title 14 CFR Part 91. Visual meteorological conditions prevailed for the local flight that originated approximately 20 minutes prior to the accident. No flight plan had been filed. The pilot said that during the landing roll the nose wheel began to shimmy. As the airplane slowed down, the shimmying became worse. He said that as the airplane approached 40 knots, the nose landing gear collapsed, and the propeller began striking the runway. The airplane sustained structural damage to the firewall and its bulkhead. Postaccident examination by Engineering Systems, Inc., Aurora, Illinois, determined that the nose wheel shimmy damper had malfuctioned. They determined that there was grit behind both cylinder end caps, and there was evidence of a slow hydraulic leak from the damper.

Flight

Event TypeAccident
Event Time10:15 MDT
Nearest AirportHeber City Municipal (0nm)
Runway21
Runway Length6900 ft
Runway Width75 ft
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftNorth American T-28D
Tail NumberN28YF
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsWright · 1820-86B · Reciprocating · 1425
Seats2

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 63 · First Class

Conditions

ConditionsVMC
LightDaylight
Wind210° @ 5 kt
Visibility15 sm
CeilingNone
Temperature / Dew Point14 C / 12 C
Altimeter30.00 inHg
Weather SourcePILO

Appendix: Source Data