WPR13LA322

NTSB accident investigation · Piper PA-28-235 · Albany, OR · July 7, 2013

Accident · No injuriesLimited investigationFinal report
Date
July 7, 2013, 13:30 local (20:30 UTC)
Place
Albany, OR
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N8606WPiper PA-28-235
Defining event
Landing-landing roll: Sys/Comp malf/fail (non-power)
Weather
Visual (VMC) · Day
Status
Completed · report October 19, 2015
Report
Approved by Office Director
NTSB office
Western Pacific Region
Parties
Federal Aviation Administration
FAA report
20130707011599A
Case key
87438

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 loss of hydraulic fluid, which rendered the brakes ineffective. The reason for the loss of hydraulic fluid could not be determined based on the available evidence.

Findings · 2

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.

AircraftAircraft › Aircraft systems · FailurePiper PA-28-235: 1 caseAll aircraft: 63 casesProbable cause
Fluids: hydraulic fluidAircraft › Fluids/misc hardware · Fluid levelPiper PA-28-235: 1 caseAll aircraft: 33 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

The pilot reported that, during the landing rollout, he applied the brakes but that the airplane failed to stop. The airplane continued about 2,600 ft down the runway, departed the runway surface, and impacted a chain link fence. Postaccident examination of the airplane revealed that the brake hydraulic fluid reservoir was empty, and an elbow fitting on the right main landing gear brake assembly hydraulic line was found broken; it could not be determined when the elbow fitting broke. The lack of hydraulic fluid rendered the brakes ineffective.

Factual narrative

On July 7, 2013, at 1330 Pacific daylight time, a Piper PA 28-235, N8606W, overran the runway on the landing rollout on runway 34 at the Albany Municipal Airport (S12), Albany, Oregon. The pilot/owner operated the airplane under the provisions of 14 Code of Federal Regulations Part 91 as a personal flight. The pilot and passenger were not injured, and the airplane sustained substantial damage to the wings. Visual meteorological conditions prevailed for the flight, and no flight plan had been filed. The flight departed Lake County Airport (LKV), Lakeview, Oregon, at 1200, with a planned destination to S12. According to the pilot, during the landing rollout he applied the brakes, but the airplane did not stop. The airplane continued down the runway about 2,600 feet, departed the runway surface, and impacted a chain link fence. Postaccident examination by the Federal Aviation Administration (FAA) revealed that the brake fluid reservoir was empty. Further examination revealed a broken elbow fitting on the right landing gear brake assembly hydraulic line. The pilot did not complete or turn in the National Transportation Safety Board Pilot Operator/Aircraft Accident/Incident Report, Form 6120.1.

Aircraft

Registration
N8606W
Reported as
Piper PA-28-235
Category
Airplane
Serial number
28-10121
Built
1963
Airframe hours
3,827
Engine
Lycoming O-540 SERIES, 250 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Airworthiness certificate
Standard, Normal
Departed
LVK · Lakeview, OR
Destination
S12 · Albany, OR
Flight plan
Unknown
Airport
S12 · Albany Municipal Airport, runway 34, 3,004 × 75 ft, asphalt

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
76
Injuries
None
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, With waivers/limitations
Last flight review
September 15, 2012
Seat
Left
Flight hours
1,200 total · 300 in this make and model · 5 in the last 90 days

Weather

Conditions
Visual (VMC) · Day
Wind
360° at 9 knots, gusting 14
Visibility
10 statute miles
Lowest ceiling
None
Temperature
88 °F, dew point 54 °F
Altimeter
30.04 inHg
Turbulence
Unknown
Observed at
CVO, 13 nm away

Docket · 4

The files NTSB released with the investigation on September 15, 2015, on NTSB’s docket system: statements, records, photos and specialists’ reports. 3.1 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 N8606W · 3

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