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Aviation safety reports, made easier to study

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November 18, 2010 · Beech 35-33 · N5481

Roanoke, TX

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
November 18, 2010
Injury Outcomes
No injuries (1 uninjured)
Location
Roanoke, TX
Aircraft
Beech 35-33
Tail Number
N5481
Injuries
None
Aircraft Damage
Substantial
NTSB Number
CEN11LA076

While on base leg of the traffic pattern at the destination airport, the airplane lost engine power. The pilot completed the emergency checklist but was unable to restore engine power. During the forced landing near the airport, the airplane collided with several trees resulting in substantial damage. An engine test run was conducted while the motor was still attached to the airframe, utilizing an external fuel source attached to the left side fuel system. The engine started and accelerated to 2,400 rpm. Dark black smoke was observed from the exhaust system and the engine ran rough at full mixture. The engine ran smooth when leaned, and the leak rate on the metering unit return to the fuel pump was higher than normal. The exact cause of the loss of engine power could not be determined.

NTSB Probable Cause

Environmental issues-Physical environment-Terrain-(general)-Effect on operation - F

Full Narrative

On November 17, 2010, approximately 1940 central standard time, a Beech 35-33, N5481, was substantially damaged when it impacted trees following a loss of engine power near Roanoke, Texas. Night visual meteorological conditions prevailed at the time of the accident. The personal flight was being conducted under the provisions of 14 Code of Federal Regulations Part 91 without a flight plan. The pilot was not injured. The cross-country flight departed Jackson, Mississippi, and was en route to Roanoke, Texas. According to a written statement submitted by the pilot, while on base leg for runway 35 the engine "went to idle power". The pilot performed the emergency checklist but was unable to restore engine power. During the forced landing the airplane impacted several trees. The airplane's right wing separated from the fuselage, and the left wing was crushed aft and embedded into an adjacent tree. The airplane's salvage recovery team reported that the right main fuel tank contained 8 gallons of fuel and the right auxiliary fuel tank contained 1/2 gallon of fuel. The left main fuel tank contained 15 gallons of fuel and the left auxiliary fuel tank contained 1 quart of fuel. An engine test run was conducted while the motor was still attached to the airframe, utilizing an external fuel source attached to the left side fuel system. The engine started and accelerated to 2,400 rpm. A dark black smoke was observed from the exhaust system and the engine ran rough at full mixture. The engine ran smooth when leaned. Further examination of the engine's fuel delivery system revealed that the number five fuel nozzle, main filter screen, and fuel screen were full of contaminants. The source of the contaminants was not determined. The fuel system was placed on a test bench and the unit operated as designed. The leak rate on the metering unit return to the fuel pump was higher than normal. Additional examination revealed that the diaphragm on the manifold was not as pliable as a newer diaphragm; however, there were no cracks and no leaks noted.

Flight

Event TypeAccident
Event Time19:40 CST
Nearest AirportNorthwest Regional Airport (0nm)
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBeech 35-33
Tail NumberN5481
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsContinental · IO-470 · Reciprocating · 225
Seats4

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 28 · First Class · None

Conditions

ConditionsVMC
LightNight
Wind330° @ 13 kt, gusting 24 kt
Visibility10 sm
CeilingOvercast 3800 ft
Temperature / Dew Point54 / 39 C
Altimeter30.18 inHg
Observation Time00:53
Weather SourceWFAC

Appendix: Source Data