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Aviation safety reports, made easier to study

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NTSB Report

July 11, 1993 · Holmes Special · N485MH

Chavies, KY

Overview

Report Status
Probable Cause
Event Type
Accident
Date
July 11, 1993
Injury Outcomes
2 injuries (1 serious injury, 1 minor injury)
Location
Chavies, KY
Aircraft
Holmes Special
Tail Number
N485MH
Operator
Stephen L Smith
Injuries
Serious
Aircraft Damage
Destroyed
NTSB Number
BFO93LA117

After takeoff, the pilot made a right turn into a hollow between rising terrain. He realized that the airplane could not attain a climb rate needed to clear the terrain, so he made a steep turn. During the turn, the airplane's engine lost partial power. During a forced landing, the airplane impacted a creek bank and was damaged. The pilot stated that there was about 6 gallons of fuel on board for the five mile flight. The fuel capacity of the airplane was 23 gallons. Post accident examination of the airframe and engine did not reveal any anomalies. The fuel tank was ruptured and empty. The fuel line from the fuel pump to the injection servo contained three to four drops of fuel. The fuel line from the servo to the flow divider contained enough fuel to fill half of the line. The pilot stated that the aircraft was modeled very closely after a 2 seat Pitts Special, which was placarded to restrict takeoffs with less than 1/4 tank of fuel due to possible fuel starvation induced by attitude.

NTSB Probable Cause

FUEL STARVATION DUE TO THE PILOT'S IMPROPER DECISION TO TAKE OFF WITH A LOW FUEL LEVEL. FACTORS RELATED TO THE ACCIDENT WERE THE LOW FUEL LEVEL, THE PILOT'S LACK OF FAMILIARITY WITH THE CHARACTERISTICS OF THE FUEL SYSTEM, AND THE UNEVEN TERRAIN IN THE EMERGENCY LANDING AREA.

Full Narrative

AFTER TAKEOFF, THE PILOT MADE A RIGHT TURN INTO A HOLLOW BETWEEN RISING TERRAIN. HE REALIZED THAT THE AIRPLANE COULD NOT ATTAIN A CLIMB RATE NEEDED TO CLEAR THE TERRAIN, SO HE MADE A STEEP TURN. DURING THE TURN, THE AIRPLANE'S ENGINE LOST PARTIAL POWER. DURING A FORCED LANDING, THE AIRPLANE IMPACTED A CREEK BANK AND WAS DAMAGED. THE PILOT STATED THAT THERE WAS ABOUT 6 GALLONS OF FUEL ON BOARD FOR THE FIVE MILE FLIGHT. THE FUEL CAPACITY OF THE AIRPLANE WAS 23 GALLONS. POST ACCIDENT EXAMINATION OF THE AIRFRAME AND ENGINE DID NOT REVEAL ANY ANOMALIES. THE FUEL TANK WAS RUPTURED AND EMPTY. THE FUEL LINE FROM THE FUEL PUMP TO THE INJECTION SERVO CONTAINED THREE TO FOUR DROPS OF FUEL. THE FUEL LINE FROM THE SERVO TO THE FLOW DIVIDER CONTAINED ENOUGH FUEL TO FILL HALF OF THE LINE. THE PILOT STATED THAT THE AIRCRAFT WAS MODELED VERY CLOSELY AFTER A 2 SEAT PITTS SPECIAL, WHICH WAS PLACARDED TO RESTRICT TAKEOFFS WITH LESS THAN 1/4 TANK OF FUEL DUE TO POSSIBLE FUEL STARVATION INDUCED BY ATTITUDE.

Flight

Event TypeAccident
Event Time17:42 EDT
Nearest Airport0nm N
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftHolmes Special
Tail NumberN485MH
Aircraft CategoryAir
DamageDestroyed
OperatorStephen L Smith
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · IO-360-A1D · Reciprocating · 180
Seats2

People & Injuries

Injury Summary2 injuries (1 serious injury, 1 minor injury)
Fatal0
Serious1
Minor1
Uninjured0
Total2
Crew 1Age 43 · First Class

Conditions

ConditionsVMC
LightDaylight
Wind180° @ 6 kt
Visibility5 sm
CeilingBroken clouds 25000 ft
Temperature / Dew Point70 F
Altimeter29.00 inHg
Observation Time21:51
Weather SourceWFAC

Appendix: Source Data