WPR15LA234

NTSB accident investigation · Cessna 180J · Dixie, ID · July 26, 2015

Accident · No injuriesLimited investigationFinal report
Date
July 26, 2015, 08:30 local (14:30 UTC)
Place
Dixie, ID
Injuries
4 uninjured
Damage
Substantial damage
Phase of flight
Taxi
Aircraft
N52095Cessna 180J
Defining event
Taxi-into takeoff position: Sys/Comp malf/fail (non-power)
Weather
Visual (VMC) · Day
Status
Completed · report May 16, 2016
Report
Approved by Office Director
NTSB office
Western Pacific Region
Parties
Federal Aviation Administration
FAA report
20150726011279A
Case key
91724

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

The failure of the right brake hydraulic line during taxi due to fatigue, which caused a loss of hydraulic fluid and rendered the brake inoperative.

Findings · 3

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: brakeAircraft › Aircraft systems · FailureCessna 180J: 2 casesAll aircraft: 297 casesProbable cause
Hydraulic power systemAircraft › Aircraft systems · Fatigue/wear/corrosionCessna 180J: 1 caseAll aircraft: 22 casesProbable cause
TerrainEnvironmental issues › Physical environment · Decision related to conditionCessna 180J: 2 casesAll aircraft: 267 cases

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

The commercial pilot was conducting a nonscheduled passenger flight. The pilot reported that, while he was turning the airplane to align it with the runway for takeoff, the right brake failed. The pilot subsequently intentionally ground looped the airplane to avoid elevated terrain near the runway, during which the right wing struck terrain. Postaccident examination of the right brake hydraulic line revealed that it was cracked where the line bends between the fuselage and main landing gear leg. It is likely that the crack caused a hydraulic fluid leak, which rendered the brake inoperative. Metallurgical examination of the fracture surface revealed fatigue striations and ratchet mark formations, consistent with a fatigue fracture.

Factual narrative

On July 26, 2015, about 0830 mountain daylight time, a Cessna 180J, N52095, sustained substantial damage while taxiing for takeoff following a reported loss of the right brake control at the Wilson Bar USFS Airport (C48) Dixie, Idaho. The airplane was registered to a private individual and operated by SP Aircraft under the provisions of Title 14 Code of Federal Regulations Part 135. The commercial pilot and three passengers were not injured. Visual meteorological conditions prevailed and no flight plan was filed for the non-scheduled passenger flight. The flight was originating at the time with a planned destination of Boise Air Terminal/Gowen Field, Boise, Idaho. The pilot reported that the right brake failed while performing a 180 degree turn to align the airplane with the runway. As a result, the pilot stated that he intentionally ground looped the airplane, in order to avoid elevated terrain near the runway. Subsequently, the right wing struck terrain. Postaccident examination of the damaged airplane by a Federal Aviation Administration inspector revealed that substantial damage was sustained to the right wing and aileron. The right brake hydraulic line was observed to be cracked at a bend between the fuselage and the main landing gear leg. The airplane is equipped with a hydraulically actuated disc brake on each wheel. Each brake is connected by a hydraulic line to a master cylinder attached to each side of the pilot's rudder pedals. The appropriate section of the brake hydraulic line was removed and sent to the National Transportation Safety Board, Materials Laboratory Division, for a detailed examination. Electron microscope images revealed that the brake line fracture surface was consistent with a fatigue fracture. Fatigue striations and ratchet mark formations were observed.

Aircraft

Registration
N52095
Reported as
Cessna 180J (J)
Category
Airplane
Serial number
18052496
Built
1974
Airframe hours
6,547.6
Engine
Cont Motor O-470 SERIES, 230 horsepower, reciprocating
Damage
Substantial damage
Flight
Part 135
Operator
Patrick, Scott, doing business as SP Aircraft
Registered owner
Patrick Bonnie
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · June 29, 2015
Departed
C48 · Dixie, ID
Destination
BOI · Boise, ID
Flight plan
Company VFR
Airport
C48 · Wilson Bar Usfs, runway 06, 1,500 × 50 ft, dirt

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
43
Injuries
None
Certificate
Commercial
Airplane ratings
Single-engine land, Single-engine sea
Instrument ratings
Airplane
Medical
Class 2, With waivers/limitations
Last flight review
August 28, 2015
Seat
Left
Restraint
3-point
Flight hours
2,900 total · 2,800 as pilot in command · 120 in the last 90 days · 60 in the last 30 days · 3 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
10 statute miles
Lowest ceiling
None
Temperature
64 °F, dew point 55 °F
Altimeter
29.96 inHg
Observed at
KP69, 53 nm away

Docket · 2

The files NTSB released with the investigation on April 4, 2016, on NTSB’s docket system: statements, records, photos and specialists’ reports. 3.4 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.

Other investigations on N52095 · 2

Matched to the same aircraft by N-number and date.