WPR11LA370

NTSB accident investigation · Piper J5A · Biddle, MT · July 24, 2011

Accident · No injuriesLimited investigationFinal report
Date
July 23, 2011, 20:40 local (Jul 24, 2011, 02:40 UTC)
Place
Biddle, MT
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N38AWPiper J5A
Defining event
Landing-landing roll: Landing gear collapse
Weather
Visual (VMC) · Day
Status
Completed · report May 15, 2012
Report
Approved by Office Director
NTSB office
Western Pacific Region
Parties
Federal Aviation Adminstration FSDO
FAA report
20110723015839A
Case key
81394

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

On this page

Probable cause

Failure of the left main landing gear strut during the landing roll due to a preexisting crack.

Findings · 1

NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.

Landing gear system: main landing gearAircraft › Aircraft systems · FailureAll aircraft: 241 casesProbable cause

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

Analysis

During the landing roll on the grass airstrip, the nose of the airplane began to drop, and the pilot confirmed that he was not applying excessive brake pressure. The nose continued to descend, then the airplane dropped back onto the tailwheel and onto its left wing. Examination revealed that the left main landing gear aft strut failed, and signatures consistent with a preexisting crack in the aft landing gear strut at the axle knuckle were observed. The area of failure was obscured by fabric covering material, thereby limiting the pilot’s ability to observe the crack during a preflight check.

Factual narrative

HISTORY OF FLIGHT On July 23, 2011, about 2040 mountain daylight time, a Piper J5A, N38AW, experienced a left main landing gear collapse during the landing roll near Biddle, Montana. The pilot was operating the airplane under the provisions of Title 14 Code of Federal Regulations Part 91. The private pilot and passenger were not injured. The airplane sustained substantial damage to the left side of the fuselage during the accident sequence. The local flight departed from a private airstrip near Biddle about 2000. Visual meteorological conditions prevailed, and no flight plan had been filed. The pilot reported a normal takeoff and flight, with a subsequent uneventful landing on the grass airstrip. During the landing roll, the nose of the airplane began to drop, and the pilot confirmed that he was not applying excessive brake pressure. The nose continued to descend, and the airplane then dropped back onto the tailwheel, and then onto its left wing. Subsequent examination revealed that both of the upper landing gear struts had separated at the axle knuckle. Black dust and residue was present around the fracture surface of the aft strut. Examination of the corresponding right landing gear struts revealed that the area of failure was obscured by fabric covering material.

Aircraft

Registration
N38AW
Reported as
Piper J5A
Category
Airplane
Serial number
5-218
Airframe hours
2,717
Engine
Lycoming O-290 SERIES, 125 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Airworthiness certificate
Standard, Normal
Last inspection
Annual · June 1, 2011 · 7 hours before
Departed
PVT · Biddle, MT
Destination
PVT · Biddle, MT
Airport
PVT · Mader Ranch Private, runway 30, 1,400 × 100 ft, grass/turf

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
56
Injuries
None
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, With waivers/limitations
Last flight review
June 25, 2010
Seat
Front
Flight hours
1,400 total · 900 in this make and model · 1,300 as pilot in command · 20 in the last 90 days · 5 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
100° at 5 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
70 °F, dew point 52 °F
Altimeter
30.12 inHg
Observed at
GCC, 57 nm away

Docket · 5

The files NTSB released with the investigation on April 6, 2012, on NTSB’s docket system: statements, records, photos and specialists’ reports. 5.2 MB in all.

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.