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Aviation safety reports, made easier to study

NTSB Reports is an independent research and search tool for public aviation accident and incident records. It brings NTSB aviation reports, structured fields, docket files, extracted figures, photos, videos, and update history into one searchable interface.

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May 16, 2000 · Beech H35 · N5477D

Show Low, AZ

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
May 16, 2000
Injury Outcomes
1 injury (1 minor injury), 1 uninjured
Location
Show Low, AZ
Aircraft
Beech H35
Tail Number
N5477D
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
LAX00LA197

While on short final the airplane drifted below the glide slope. The pilot advanced the throttle to find that the airplane had lost power. An attempt was made to restart the engine and the fuel tanks were switched, but the airplane was already at a low altitude. The airplane impacted the ground short of the runway. The auxiliary tanks were damaged from the impact and found dry, according to the recovery person. Friends of the pilot reportedly moved the wreckage and drained the fuel in the airplane before authorized inspection. Twenty-six gallons of fuel was removed from the left main. In a post crash examination, the engine tested successfully after an adjustment was made to a fuel line separation that had been damaged from impact. The pilot bought 35.5 gallons of fuel before the flight and by his own account filled the tanks.

NTSB Probable Cause

The pilot's failure to properly position the fuel selector to a tank with fuel resulting in fuel starvation, a loss of engine power, and subsequent collision with the ground during the final landing approach.

Full Narrative

On May 15, 2000, at 2145 hours mountain standard time, a Beech H35, N5477D, lost power, landed short, and collided with ground obstructions while on approach to Show Low Municipal Airport, Show Low, Arizona. The aircraft sustained substantial damage. The certificated private pilot was not injured and his passenger received minor injuries. The airplane was being operated as a personal flight by a private owner under 14 CFR Part 91 when the accident occurred. The flight originated from Falcon Field in Mesa, Arizona, at 2045. Visual meteorological conditions prevailed at the time and no flight plan was filed. According to the pilot, while about 0.25 miles from the runway on final approach, the aircraft drifted below the pilot's desired approach angle. He attempted to correct the condition by advancing the throttle but the engine did not respond. The aircraft landed about 120 feet short of the runway threshold and collided with ground obstructions. The engine was tested on May 19, 2000, and did not start initially. The fuel line was found separated at the selector. The aircraft recovery company representative observed impact damage on the underside of the airplane that extended to the fuel selector area. On May 22, 2000, the engine was retested. No further malfunctions were reported. The Beech has multiple fuel selector positions for the H35 model equipped with auxiliary fuel tanks such as this one. Extended range tanks are selected separately on the fuel selector switch. Both auxiliary tip-tanks were damaged from impact. The pilot stated having switched tanks after the power failure but as the airplane drifted below the glide slope, impact was imminent. The switch was found on the left main where 26 gallons of fuel was reportedly removed. Friends of the pilot reportedly had moved the wreckage and drained the fuel tanks before investigators could examine the airplane. There was fuel on the ground around the airplane wreckage. An investigation record found that the pilot bought 35.5 gallons of fuel before the flight. The pilot reported the tanks were filled before departure.

Flight

Event TypeAccident
Event Time21:45 MST
Nearest AirportShow Low Municipal (0nm ENE)
Runway24
Runway Length7200 ft
Runway Width75 ft
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBeech H35
Tail NumberN5477D
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsContinental · IO-520 BA2 · Reciprocating · 285
Seats4

People & Injuries

Injury Summary1 injury (1 minor injury), 1 uninjured
Fatal0
Serious0
Minor1
Uninjured1
Total2
Crew 1Age 41 · Third Class · Minor

Conditions

ConditionsVMC
LightNight
Wind180° @ 12 kt
Visibility30 sm
CeilingBroken clouds 20000 ft
Temperature / Dew Point64 F / 16 C
Altimeter30.00 inHg
Observation Time05:10
Weather SourceWFAC

Appendix: Source Data