N56755

Substantial
None

PIPER PA 34-200S/N: 34-7450029

Accident Details

Date
Friday, April 25, 2014
NTSB Number
CEN14LA220
Location
Spring, TX
Event ID
20140428X24336
Coordinates
30.063333, -95.553054
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
4
Total Aboard
4

Probable Cause and Findings

The loss of right brake effectiveness during landing for reasons that could not be determined based on the available evidence, which resulted in a loss of directional control.

Aircraft Information

Registration
Make
PIPER
Serial Number
34-7450029
Engine Type
Reciprocating
Year Built
1973
Model / ICAO
PA 34-200M600
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2
Seats
7
FAA Model
PA-34-200

Registered Owner (Current)

Name
PEA-WAYMAN FLIGHT LLC
Address
561 PEARL HARBOR DR
City
DAYTONA BEACH
State / Zip Code
FL 32114-3845
Country
United States

Analysis

On April 25, 2014, about 1825 central daylight time, a Piper PA-34-200 multi-engine airplane, N56755, was substantially damaged during landing at David Wayne Hooks Airport (DWH), Spring, Texas. The three occupants were not injured. The airplane was registered to BAT Aviation, Inc.; Spring, Texas, and was being operated by United Flight Systems, Inc.; Spring, Texas. Day visual meteorological conditions (VMC) prevailed at the time of the accident and a flight plan had not been filed for the 14 Code of Federal Regulations Part 91 instructional flight.The flight instructor was manipulating the flight controls and demonstrating a short-field landing. After the airplane touched down at about 90 mph, the flight instructor retracted the flaps and then discovered the right brake pedal went full forward and was not slowing the airplane. He proceeded to pump the brake several times to try and build pressure in the lines, but was not successful. The pilot receiving instruction checked his brake pedals and confirmed the right brake failure. The flight instructor reported that he then shut down both engines when the airplane's speed was about 60 mph. Directional control was lost and the airplane drifted off the left side of the runway and impacted a ditch at an estimated impact speed of about 20 mph resulting in substantial damage to the lower aft fuselage and lower forward empennage.

A photograph of skid marks of the main gear tires over the asphalt pavement showed that the skid marks for the left main gear tire seemed to be darker than the skid marks for the right main gear tire which were lighter in intensity. An examination of the brakes on the following day by a Federal Aviation Administration Inspector did not disclose a problem with the right brake, however it was unclear whether the brake system had been serviced or repaired following the accident.

At 1753, the official surface weather observation site at DWH, reported wind from 120 degrees at 5 knots, visibility of 10 miles, and few clouds at 6,500 feet. Data from the National Oceanic and Atmospheric Administration showed that, at the accident location, at 1825, the altitude of the sun was about 18 degrees above the horizon and the azimuth of the sun was about 275 degrees. Apparent sunset occurred at 1956.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN14LA220