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Aviation safety reports, made easier to study

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July 2, 2011 · Temco GC-1B · N106S

Sparta, TN

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
July 2, 2011
Injury Outcomes
No injuries (1 uninjured)
Location
Sparta, TN
Aircraft
Temco GC-1B
Tail Number
N106S
Injuries
None
Aircraft Damage
Substantial
NTSB Number
ERA11CA375

The pilot reported that, during the takeoff roll, he was unable to correct an uncommanded left yaw with control inputs, so he elected to abort the takeoff. During rollout, the airplane departed the left side of the runway and the landing gear collapsed, which resulted in substantial damage to the right wing spar. A postaccident examination revealed that a "nicopress" fitting on the left rudder cable had failed and disconnected from its bell-crank. The cable fitting had been pressed with an improper tool or technique at installation. The airplane's entire flight control system had been refitted and re-rigged approximately 9 years prior to the accident.

NTSB Probable Cause

The improper installation of the right rudder control cable by maintenance personnel, which resulted in the pilot's inability to maintain directional control during takeoff.

Full Narrative

During the takeoff roll, an uncommanded left yaw could not be corrected with control inputs, so the pilot elected to abort the takeoff. During rollout, the airplane departed the left side of the runway, and the landing gear collapsed, which resulted in substantial damage to the left wing spar. Examination by a Federal Aviation Administration inspector revealed that a "nicopress" fitting on the right rudder cable had failed, and disconnected from its bell-crank. According to the Inspector, the cable fitting had been pressed with an improper tool or technique at installation. The airplane's entire flight control system was refitted and re-rigged approximately 9 years prior to the accident.

Flight

Event TypeAccident
Event Time10:10 CDT
Nearest AirportUpper Cumberland Regional (0nm)
Runway22
Runway Length6005 ft
Runway Width100 ft
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftTemco GC-1B
Tail NumberN106S
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsCont Motor · C145 SERIES · Reciprocating · 145
Seats2

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 41 · Third Class · None

Conditions

ConditionsVMC
LightDaylight
Wind360° @ 3 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point66 F
Altimeter30.15 inHg
Observation Time14:53
Weather SourceWFAC

Appendix: Source Data