N5406C

Substantial
None

CESSNA 170AS/N: 19440

Accident Details

Date
Monday, September 5, 2011
NTSB Number
ANC11CA095
Location
Anchorage, AK
Event ID
20110905X01931
Coordinates
61.186668, -149.965270
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The fracture of a hydraulic brake line fitting due to incorrect installation of the brake line by the pilot/owner, which resulted in a loss of brake pressure and subsequent loss of directional control during the landing roll.

Aircraft Information

Registration
Make
CESSNA
Serial Number
19440
Engine Type
Reciprocating
Year Built
1950
Model / ICAO
170AC170
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
170A

Registered Owner (Current)

Name
GUGEL JOSEPH J
Address
4788 E CRANE RD
City
WASILLA
State / Zip Code
AK 99654-0935
Country
United States

Analysis

The pilot was landing his tailwheel-equipped airplane on a dry, gravel runway at the conclusion of a local area flight. After landing, the pilot applied the brakes to slow the landing roll, and while depressing both brake pedals, the left brake pedal unexpectedly went to the floor, and the airplane swerved to the right. The airplane subsequently went off the right side of the runway and nosed over in an area of soft, marshy, wet tundra, sustaining substantial damage to the rudder, left wing, and left aileron. A Federal Aviation Administration (FAA) airworthiness inspector's postaccident inspection revealed that a hydraulic brake supply line fitting, near the airplane's fuselage, had broken. The FAA inspector noted that the hydraulic brake line was not secured to the landing gear strut as required, which allowed the line to flex and bend at the fitting during flight. The pilot reported the he recently rebuilt the airplane himself.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC11CA095