N3331V

Substantial
None

BEECH 35 S/N: D-792

Accident Details

Date
Sunday, December 26, 1993
NTSB Number
FTW94LA056
Location
CRYSTAL BEACH, TX
Event ID
20001211X13863
Coordinates
29.480354, -94.570358
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
4
Total Aboard
4

Probable Cause and Findings

WAS A TOTAL LOSS OF ENGINE POWER FOR UNDETERMINED REASONS. FACTORS WERE A PASSENGER DOOR INADVERTENTLY OPENING IN FLIGHT DUE TO INADEQUATE PREFLIGHT BY THE PILOT, UNSUITABLE TERRAIN FOR THE FORCED LANDING, AND CARBURETOR ICING CONDITIONS.

Aircraft Information

Registration
N3331V
Make
BEECH
Serial Number
D-792
Engine Type
Reciprocating
Year Built
1947
Model / ICAO
35 BE35
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
ALOOF PINCUS
Address
2407 AVEUNE O
Status
Deregistered
City
GALVESTON
State / Zip Code
TX 77550
Country
United States

Analysis

On December 26, 1993, approximately 1230 central standard time a Beech BE35, N3331V, sustained substantial damage during a forced landing near Crystal Beach, Texas. The private pilot and the three passengers were not injured. Visual meteorological conditions prevailed for the local personal flight.

A witness stated to the Federal Aviation Administration (FAA) inspectors that the airplane had departed the private grass airstrip to the south. The witness said that he observed the airplane climbing approximately 800 feet above the ground and then enter the pattern for an approach to the runway. On site examination by the inspectors revealed the airplane landed short of the runway, hit a fence, and came to rest nose down. Examination of the airplane by the inspectors (enclosed statement) indicated damage to the propeller, gear, fuselage, and wing structures.

The pilot reported that he "felt like he did not have full power and RPM" during the climb. About 200 feet above the ground, the door inadvertently opened and the pilot decided to return for landing and secure the door. During final approach approximately 300 feet above the ground, the pilot reported a total loss of engine power to the passengers. The pilot reported that he could "only assume the cause of the power loss can be attributed to carburetor ice." The pilot reported a temperature dewpoint spread of 3 degrees Fahrenheit. The Federal Aviation Administration carburetor icing probability chart (copy enclosed) indicates serious icing at glide power.

During a telephone interview conducted by the investigator in charge, the pilot said that he had "throttled back during the approach and at 300 feet above the ground as he increased the throttle there was no power increase." He described the engine "as sputtering and coughing." He said the propeller was "turning slightly."

A representative of the manufacturer (report enclosed) examined the engine. No anomalies that would have contributed to the power loss were reported.

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Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW94LA056