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August 5, 2017 · Beech 19A A · N6523T

Palmer, AK

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
August 5, 2017
Injury Outcomes
No injuries (2 uninjured)
Location
Palmer, AK
Aircraft
Beech 19A A (1968)
Tail Number
N6523T
Injuries
None
Aircraft Damage
Substantial
NTSB Number
ANC17LA042

According to the private pilot, while landing at a remote, unimproved airstrip, the right main landing (MLG) tire impacted a rock. The airplane then began to veer right, and the MLG collapsed, which resulted in substantial damage to the empennage and horizontal stabilizer. Postaccident examination of the airplane revealed that the right MLG separated near its attachment point. Visual and magnified optical examinations of the fractured surfaces revealed features consistent with a bending overstress fracture. Due to the pilot's selection of unsuitable terrain to land, the right main tire impacted a rock, which resulted in the subsequent loss of directional control and collapse of the right MLG.

NTSB Probable Cause

The pilot's selection of unsuitable terrain for landing, which resulted in the right main landing (MLG) tire impacting a rock and the subsequent loss of directional control and collapse of the right MLG.

Full Narrative

On August 4, 2017, about 1900 Alaska daylight time, a tricycle gear equipped Beech BE19 airplane, N6523T, sustained substantial damage while landing at a remote unimproved airstrip, about 25 miles southeast of Palmer, Alaska. The airplane was being operated by the pilot as a 14 Code of Federal Regulations Part 91 visual flight rules flight. The private pilot and passenger were not injured. Visual meteorological conditions prevailed, and no flight plan had been filed. The flight departed Merrill Field Airport (PAMR), Anchorage, Alaska at about 1745. According to the pilot, while landing at a remote unimproved airstrip, the right main tire impacted a rock. The airplane began to veer to the right, and the right main gear collapsed, which resulted in substantial damage to the empennage and horizontal stabilizer. A National Transportation Safety Board (NTSB) Senior Metallurgist reported that visual and magnified optical examination of the fractured surfaces revealed features consistent with a bending overstress separation. No indications of preexisting fatigue, corrosion or significant porosity were detected. (A synopsis of the NTSB Metallurgist's case review is included in the public docket for this accident.) In the recommendation section of the NTSB Accident/Incident Reporting Form 6120.1, the pilot stated that the accident may have been avoided if the Federal Aviation Administration or Alaska Department of Transportation would have provided minimal funding to local pilot groups to provide minimal maintenance of routinely used backcountry airstrips.

Flight

Event TypeAccident
Event Time19:00 AKDT
Nearest Airport0nm
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBeech 19A A
Tail NumberN6523T
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · O-320 SERIES · Reciprocating · 160
Seats4

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 33 · Second Class · None

Conditions

ConditionsVMC
LightDaylight
Wind190° @ 3 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point55
Altimeter30.19 inHg
Observation Time02:53

Appendix: Source Data