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Aviation safety reports, made easier to study

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July 1, 1999 · Piper PA-22 · N3513A

Billings, MT

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
July 1, 1999
Injury Outcomes
No injuries (2 uninjured)
Location
Billings, MT
Aircraft
Piper PA-22
Tail Number
N3513A
Injuries
None
Aircraft Damage
Substantial
NTSB Number
SEA99LA103

The pilot reported that upon touchdown the aircraft began to drift left, and right rudder was applied to correct with no effect. As the drift continued, the pilot applied right brake, increasing brake pressure until he 'was pushing against the seat.' The aircraft continued to veer left, tightening its turn radius until it had rotated more than 180 degrees counter-clockwise. During the rotation, the aircraft settled to the left in line with the runway lights and came to a stop. Post-crash examination by a certified mechanic revealed that the left main landing gear shock strut tube had separated at its attach point to the left main wheel assembly. This would have allowed the release of the left main landing gear, permitting it to pivot into a flat (collapsed) position.

NTSB Probable Cause

The separation of the left main landing gear shock strut for undetermined reasons.

Full Narrative

On July 1, 1999, approximately 1445 mountain daylight time, a tailwheel equipped Piper PA-22, N3513A, registered to and being flown by a private pilot, was substantially damaged during the collapse of the left main landing gear on landing rollout at the Billings International Airport, Billings, Montana. The pilot and passenger were uninjured. Visual meteorological conditions existed, and no flight plan had been filed. The flight, which was personal, was to have been operated under 14CFR91, and originated from Helena, Montana, at 1234. The pilot reported that upon touchdown on runway 28R the aircraft began to drift left, and right rudder was applied to correct with no effect. As the drift continued, the pilot applied right brake, increasing brake pressure until he "was pushing against the seat." The aircraft continued to veer left, tightening its turn radius until it had rotated more than 180 degrees counter-clockwise. During the rotation, the aircraft settled to the left in line with the runway lights and came to a stop. The pilot and passenger exited and noted the left main landing gear separated from its bungee (shock strut,) but still attached to the airframe. Post-crash examination by an IA certified mechanic revealed that the left main landing gear shock strut tube had separated at its attach point to the left main wheel assembly (refer to DIAGRAM I). This would have allowed the release of the left main landing gear, permitting it to pivot into a flat (collapsed) position.

Flight

Event TypeAccident
Event Time14:45 MDT
Nearest AirportBillings Logan Internatio (0nm)
Runway28R
Runway Length10528 ft
Runway Width150 ft
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftPiper PA-22
Tail NumberN3513A
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · O-290-D2 · Reciprocating · 135
Seats4

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 49 · First Class

Conditions

ConditionsVMC
LightDaylight
Wind180° @ 8 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point39 C
Altimeter29.00 inHg
Observation Time20:56
Weather SourceWFAC

Appendix: Source Data