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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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NTSB Report

August 29, 2002 · Beech 1900D · N81533

Tampa, FL

Overview

Report Status
Final with probable cause
Event Type
Incident
Date
August 29, 2002
Injury Outcomes
No injuries (15 uninjured)
Location
Tampa, FL
Aircraft
Beech 1900D
Tail Number
N81533
Operator
Continental Connection
Injuries
None
NTSB Number
ATL02IA165

According to the pilot, as the airplane decelerated to 40 knots during the landing rollout he felt a vibration in the airframe. As the airplane continued to slow down the airplane began to pull to the left. The flight crew stopped the airplane on the runway. During the post-flight examination of the airplane the pilot discovered that the left main landing gear had turned 90 degrees to the left. The examination also revealed a fatigue fracture in the left main landing gear socket assembly. Examination of the socket assembly fracture revealed two fatigue regions initiated from the lower corner lug base radii and along the left and right base radii with multiple origins. Both the lower lug corner radii were confirmed to show marks consistent with repair blending. According to the blend repair procedure the surface is to be blended to surface finish comparable to that produced by 250 grit sand paper. A comparison was made between the surface finish in the repair area, and the surface produce by 240 grit sand paper on the part, which is slightly coarser than the 250 grit required. The surface finish in the repair region was much rougher than that produced by 240 grit sand paper.

NTSB Probable Cause

The improper service of the left main landing gear socket, resulting in fatigue failure of the left main landing gear socket assembly at the lower scissor attachment point.

Full Narrative

On August 29, 2002, at 1730 eastern daylight time, a Beech 1900B, N81533, registered to Gulfstream International Aviation and operated by Continental Connection, main landing gear failed during landing roll at Tampa International Airport, Tampa. The scheduled flight was operated under the provisions of Title 14 CFR part 121 with an instrument flight plan filed. Visual meteorological conditions prevailed at the time of the accident. The airplane sustained minor damage; the air transport pilots were not injured nor were the thirteen passengers. The flight departed Ft. Lauderdale Airport, Ft. Lauderdale, Florida, at 1445. According to the pilot, as the airplane decelerated to 40 knots during the landing rollout he felt a vibration in the airframe. As the airplane continued to slow down the airplane began to pull to the left. The pilot stopped the airplane on the runway. During the post-flight examination of the airplane the pilot discovered that the left main landing gear had turned 90 degrees to the left. The examination also revealed a fracture in the left main landing gear socket. Examination of the left main landing gear socket assembly fracture revealed, two fatigue regions initiated from the lower corner lug base radii and along the left and right base radii with multiple origins. The fatigue failure occurred at the lower torque knee attach point on the main landing gear socket assembly. Between the two fatigue regions, features consistent with overstress were observed. The lug was stripped of paint to reveal the underlying surface features. Both the lower lug corner radii were confirmed to show marks consistent with repair blending. According to the Raytheon component maintenance manual 32-10-00, pages 18-19 the blend is an allowed repair procedure. According to the blend repair procedure the surface is to be blended to surface finish comparable to that produced by 250 grit sand paper. A comparison was made between the surface finish in the repair area, and the surface produce by 240 grit sand paper on the part, which is slightly coarser than the 250 grit required. The surface finish in the repair region was much rougher than that produced by 240 grit sand paper.

Flight

Event TypeIncident
Event Time17:30 EDT
Nearest AirportTampa Intl (0nm N)
Runway18
Runway Length8300 ft
Runway Width150 ft
Flight Plan FiledIFR
Flight Plan ActivatedYes
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBeech 1900D
Tail NumberN81533
Aircraft CategoryAir
OperatorContinental Connection
Operating RulePart 121
Engines2
Engine TypeTurboprop
Engine DetailsPratt & Whitney · PT6A SER · Turboprop · 750 | Pratt & Whitney · PT6A SER · Turboprop · 750
Seats13

People & Injuries

Injury SummaryNo injuries (15 uninjured)
Fatal0
Serious0
Minor0
Uninjured15
Total15
Crew 1Age 26 · First Class · None
Crew 2Age 24 · First Class · None

Conditions

ConditionsVMC
LightDaylight
Wind190° @ 7 kt
Visibility10 sm
CeilingBroken clouds 25000 ft
Altimeter29.87 inHg
Observation Time00:53
Weather SourceWFAC

Appendix: Source Data