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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

March 20, 1997 · North American NA-265-40 · N123CD

Hailey, ID

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
March 20, 1997
Injury Outcomes
No injuries (3 uninjured)
Location
Hailey, ID
Aircraft
North American NA-265-40
Tail Number
N123CD
Operator
Southwest Jet
Injuries
None
Aircraft Damage
Substantial
NTSB Number
SEA97LA081

The pilot reported that during the landing roll, the thrust reversers were deployed, and the airplane began to slowly veer to the left. The pilot applied rudder control to correct the situation; however, the airplane continued to the left. The pilot stated that he then applied hard right braking action. When the airplane slowed to below 60 knots, the pilot centered the rudder and tried twice to engage the nosewheel steering and then the standby steering system. Neither system seemed to engage, and the airplane continued off the side of the runway and collided with a runway marker and a snowbank. The nose gear collapsed, and the airplane came to rest off the runway. Postaccident investigation of the electrical system revealed a short to the command potentiometer, which affected the primary and standby nosewheel steering systems.

NTSB Probable Cause

an electrical short in the electrical system, which resulted in a malfunction of the nosewheel steering system and loss of directional control.

Full Narrative

On March 20, 1997, at 0716 mountain standard time, the pilot of a North American NA-265-40, N123CD, operated by Southwest Jet as a 14 CFR Part 91 business flight, was unable to maintain directional control of the airplane during the landing roll at the Friedman Memorial airport, Hailey, Idaho. The airplane swerved to the left and collided with a snowbank off the side of the runway. Visual meteorological conditions prevailed at the time and an instrument flight rules flight plan was filed. The airplane was substantially damaged; both airline transport pilots and their one passenger were not injured. The flight had originated from Kansas City, MO, about two hours and thirty minutes before the accident. In a written statement, the pilot-in-command reported that the approach for landing was normal. The airplane touched down approximately 1,000 feet down the runway on the centerline. The pilot stated that during the landing roll, the thrust reversers were deployed and the airplane began to slowly veer to the left. The pilot applied right rudder control and right braking action, however, the airplane continued to the left. The pilot applied "hard" right braking action which had no effect. The pilot stated that he re-stowed the thrust reversers and continued to apply right braking action which seemed to have some affect. The speed had decreased to 60 knots at this time and the pilot centered the rudder and tried two times to engage the nosewheel steering. The nosewheel steering would not engage, so the pilot selected standby steering, it did not automatically "fall down" like it should, and the airplane continued to travel off the side of the runway, colliding with a runway marker and subsequently a snowbank. The nose gear collapsed and the airplane came to rest off the west side of the runway. Inspection of the nose wheel steering system identified a short in the wiring to the command potentiometer, which affected the primary and standby nose wheel steering systems. The National Transportation Safety Board was not notified of the structural damage to the airplane until March 31, 1997.

Flight

Event TypeAccident
Event Time07:16 MST
Nearest AirportFriedman Memorial (0nm)
Runway31
Runway Length6602 ft
Runway Width100 ft
Flight Plan FiledIFR
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftNorth American NA-265-40
Tail NumberN123CD
Aircraft CategoryAir
DamageSubstantial
OperatorSouthwest Jet
Operating RulePart 91
Engines2
Engine TypeTurbojet
Engine DetailsP&W · JT12A-8 · Turbojet · 3300
Seats9

People & Injuries

Injury SummaryNo injuries (3 uninjured)
Fatal0
Serious0
Minor0
Uninjured3
Total3
Crew 1Age 43 · First Class

Conditions

ConditionsVMC
LightDaylight
Wind340° @ 8 kt
Visibility30 sm
CeilingBroken clouds 9000 ft
Temperature / Dew Point28 C / 16 C
Altimeter30.00 inHg
Observation Time13:55
Weather SourceWFAC

Appendix: Source Data