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NTSB Report

March 27, 2005 · Cessna 182 · N5748B

Sacramento, CA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
March 27, 2005
Injury Outcomes
No injuries (3 uninjured)
Location
Sacramento, CA
Aircraft
Cessna 182
Tail Number
N5748B
Operator
Donald D Ridenour
Injuries
None
Aircraft Damage
Substantial
NTSB Number
LAX05LA125

During the landing rollout, the airplane veered sharply left and nosed down until the right wing impacted the runway. During the subsequent airframe examination, a component of the nose gear steering system was observed broken. The component was the right side steering link rod. It had failed in fatigue, separated from the steering assembly, then the corresponding left side rod end failed in overload, and all steering control was lost.

NTSB Probable Cause

a fatigue failure of the right side steering link rod for the nose landing gear steering system.

Full Narrative

On March 26, 2005, about 1700 Pacific standard time, a Cessna 182, N5748B, operated by its owner-pilot, experienced a mechanical malfunction during takeoff roll at the McClellan Airfield, Sacramento, California. The pilot immediately reversed course and returned for a landing on runway 34. According to the pilot, during rollout the airplane shook and he lost directional control. The airplane veered sharply left, and it nosed down until the right wing impacted the runway. The airplane was substantially damaged. Neither the private pilot nor the two passengers were injured during the personal flight. Visual meteorological conditions prevailed. The flight was performed under the provisions of 14 CFR Part 91, and it originated about 1630. The pilot indicated that although runway 34 is 10,600 feet long by 200 feet wide, he was not able to control the airplane's course during landing rollout because of the mechanical problem related to his lack of nose gear steering control. During the subsequent airframe examination, a nose gear steering linkage component was observed broken. A Federal Aviation Administration (FAA) inspector subsequently examined the damaged airplane and reported his findings. The FAA inspector stated that the right side steering link assembly rod end appeared to have fractured in fatigue. The fracture occurred outboard of the link's jam nut at its hard point casting on the nose gear assembly. Following the link's separation, the left side steering link rod end failed in overload, and the dampener internal static stop limit was exceeded, resulting in the dampener shearing off at its attachment point.

Flight

Event TypeAccident
Event Time17:00 PST
Nearest AirportMcclellan Airfield (0nm)
Runway34
Runway Length10600 ft
Runway Width200 ft
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftCessna 182
Tail NumberN5748B
Aircraft CategoryAir
DamageSubstantial
OperatorDonald D Ridenour
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsContinental · O-470 · Reciprocating · 230
Seats4

People & Injuries

Injury SummaryNo injuries (3 uninjured)
Fatal0
Serious0
Minor0
Uninjured3
Total3
Crew 1Age 54 · Third Class · None

Conditions

ConditionsVMC
LightDaylight
Wind180° @ 8 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point64 F / 48
Altimeter30.15 inHg
Observation Time00:53
Weather SourceWFAC

Appendix: Source Data