ATL02IA065

NTSB incident investigation · Beech C24R · Greenville, MS · March 14, 2002

Incident · No injuriesIncident investigationFinal report
Date
March 14, 2002, 16:58 local (22:58 UTC)
Place
Greenville, MS
Injuries
1 uninjured
Damage
Minor damage
Phase of flight
Takeoff
Aircraft
N6753LBeech C24R
Weather
Visual (VMC) · Day
Status
Completed · report July 23, 2003
Report
Approved by Office Director
Parties
FAA Jackson FSDO - 07
FAA report
20020314003569I
Case key
54376

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the incident.

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Probable cause

An overload failure of the nose gear assembly for undetermined reasons.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Airframe/component/system failure/malfunctionTakeoff
Reason for occurrence undetermined
Landing gear,nose gear assembly - overloadCause
Wheels up landingEmergency landing
Terrain condition - runway
Terrain condition - foamed

Analysis

The airplane's nose wheel and nose gear housing fell onto the runway during takeoff. The pilot returned to the airport and executed an emergency gear-up landing on a foamed runway. Examination of the outboard nose gear housing flange revealed it was completely fractured approximately 300 degrees in the area where the nose gear yoke assembly connects to the housing. The left and right tow-limit stop bolts for the nose gear were bent. There was no record of previous damage or a known overstress event involving the nose gear assembly. Scanning electron microscope examination of the fractures revealed no evidence of fatigue. Laboratory-induced overstress of the component produced a fracture surface similar in morphology to the examined fractures.

Factual narrative

On March 14, 2002, at 1658 central standard time, a Beech C24R, N6753L, registered to and operated by the private pilot, landed gear-up during an emergency landing following a separation of the nose gear assembly at Mid Delta Regional Airport in Greenville, Mississippi. The personal flight was operated under the provisions of Title 14 CFR Part 91 with a VFR flight plan filed. Visual meteorological conditions prevailed. The pilot was not injured, and the airplane sustained minor damage. The flight departed Mid Delta Regional Airport in Greenville, Mississippi, about 1220.

The airplane's nose wheel and nose gear housing fell onto the runway during takeoff and were retrieved by persons on the ground. The pilot maneuvered in the area for hours to burn off fuel, then returned to the airport and executed an emergency gear-up landing on a foamed runway.

Examination of the airplane revealed minor damage to the lower fuselage skin. The nose wheel and nose gear housing were separated, and the nose gear yoke assembly was fractured. The left and right tow-limit stop bolts for the nose gear was bent, and the rod end attached to the nose gear collar was bent. There was no record of previous damage or a known overstress event involving the nose gear assembly.

Metallurgical examination of the nose gear assembly was performed by the National Transportation Safety Board, Office of Research and Engineering, Materials Laboratory Division, Washington, D.C. Examination of the outboard flange of the nose gear housing revealed the flange was completely fractured approximately 300 degrees in the area where the nose gear yoke assembly connects to the housing. Examination of the fracture surface revealed the crack initiated from one of three equally spaced bolt holes in the outboard flange. The fracture propagated in both directions circumferentially from one hole and terminated at the outboard surface of the flange. A longitudinal fracture propagated from another of the three bolt holes and terminated at the circumferential fracture.

Scanning electron microscope examination of the circumferential fracture and the longitudinal fracture revealed no evidence of fatigue. Laboratory-induced overstress of the component produced a fracture surface similar in morphology to the circumferential and longitudinal fractures.

Aircraft

Registration
N6753L
Reported as
Beech C24R
Category
Airplane
Serial number
MC-740
Airframe hours
3,213
Engine
Lycoming IO-360, 200 horsepower, reciprocating
Damage
Minor damage
Flight
Personal · Part 91
Operator
Earnest Doyle Mosley
Registered owner
Doyle E Mosley
Airworthiness certificate
Standard, Normal
Last inspection
Annual · February 1, 2001
Departed
GLH · Greenville, MS
Destination
DHN · Dothan, AL
Flight plan
VFR
Airport
GLH · Mid Delta Regional, runway 18R, 7,019 × 150 ft, asphalt

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
61
Injuries
None
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Valid Medical--w/ waivers/lim
Last flight review
October 1, 2001
Seat
Left
Flight hours
3,800 total · 3,000 in this make and model · 12 in the last 90 days

Weather

Conditions
Visual (VMC) · Day
Wind
150° at 15 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
75 °F
Altimeter
29.73 inHg
Observed at
GLH

Docket · 2

The files NTSB released with the investigation on May 21, 2003, on NTSB’s docket system: statements, records, photos and specialists’ reports. 1.7 MB in all.

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.