N178DP

Substantial
Serious

Beech P35 S/N: D7090

Accident Details

Date
Thursday, February 22, 1996
NTSB Number
FTW96LA129
Location
BROWNWOOD, TX
Event ID
20001208X05257
Coordinates
31.719802, -98.970893
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

the pilot's failure to follow manufacturer's procedures and premature gear retraction.

Aircraft Information

Registration
N178DP
Make
BEECH
Serial Number
D7090
Engine Type
Reciprocating
Year Built
1962
Model / ICAO
P35 BE35
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
LEE JACK W
Address
BOX 779
Status
Deregistered
City
MASON
State / Zip Code
TX 76856
Country
United States

Analysis

On February 22, 1996, at 1030 central standard time, a Beech P35, N178DP, registered to and operated by a private owner, was substantially damaged during takeoff near Brownwood, Texas. The commercial pilot sustained serious injuries. The aircraft was being operated as a personal flight under Title 14 CFR Part 91. Visual meteorological conditions prevailed for the local flight for which a flight plan was not filed.

The airplane was departing runway 17 at Brownwood Airport. The pilot reported that the aircraft lifted off "but would not climb or accelerate." He also reported that he believed "a landing gear collapsed at or about rotation and that the propeller contacted the runway. I spent too much time trying to find the problem and ran out of runway." The airplane came to rest in an upright position less than 1/4 mile from the end of the runway. The airplane sustained damage to the wings, engine mount, firewall, propeller, and tail.

A witness to the accident reported that the airplane was about 10 to 15 feet high when he noticed the right landing gear door was partially down.

On scene inspection by the FAA inspector revealed that there were 35 propeller strikes on the runway and several imprints corresponding to the landing gear doors and belly of the airplane on the runway. Inspection of the cockpit area of the airplane revealed that the landing gear handle was in the "up" position.

The pilot's operating manual provided by the manufacturer stated that the gear should be retracted after a positive rate of climb has been established.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW96LA129