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Aviation safety reports, made easier to study

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February 2, 1997 · Beech N35 · N61DE

Payson, AZ

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
February 2, 1997
Injury Outcomes
2 injuries (2 minor injuries)
Location
Payson, AZ
Aircraft
Beech N35
Tail Number
N61DE
Operator
Robert W Glenn
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
LAX97LA096

The pilot departed for a 20-minute-long flight with nearly full fuel tanks. During the flight, no unusual sounds or vibrations were noted. The pilot arrived at the destination airport, entered the downwind leg, lowered the landing gear, and went through the 'GUMP' check list. According to the pilot, when he attempted to increase engine power the engine did not respond, and the airplane continued descending. The pilot turned on the fuel boost pump and attempted to restart the engine; however, he was not successful. Unable to glide to the runway, the pilot made a forced landing in trees and brush. An examination of the airplane revealed both fuel tanks had ruptured. The left fuel tank was found ripped open and was dry; the right tank contained about 10 gallons of fuel. The FAA coordinator reported that he examined the recovered airframe wreckage and the engine. The engine was started and it functioned. Normal operation of both magnetos was noted, and no abnormal conditions were found. The reason for the engine power loss was not determined.

NTSB Probable Cause

a loss of engine power for undetermined reasons.

Full Narrative

On February 2, 1997, at 0950 hours mountain standard time, a Beech N35, N61DE, operated by Diamond Eagle Inc., Carefree, Arizona, experienced a total loss of engine power while in the traffic pattern at the Payson, Arizona, airport. The pilot made a forced landing into trees and brush short of runway 24. The airplane was substantially damaged, and the private pilot and passenger received minor injuries. Visual meteorological conditions prevailed, and no flight plan was filed. The flight originated from Carefree at 0930. On February 5, 1997, the pilot verbally reported that the engine power loss had not been preceded by any unusual vibrations, smoke, or sounds. He stated that the engine lost power after he had lowered the landing gear and went through the "GUMP" check list. He first detected the power loss when he attempted to increase engine power on the extended downwind leg. Turning on the electric boost fuel pump had no effect. When the pilot began the flight the left and right fuel tanks contained approximately 37 and 32 gallons of fuel, respectively. The pilot subsequently made the following written statement about the sequence of events: "I tried the to restart the engine. No response. I turned toward the airport and again attempted to restart. No response. I lost altitude fast. No hope of making the airport." The pilot further reported that as the airplane came to rest it collided with 10- to 15-foot high trees and brush. Immediately after stopping the odor of fuel was noted. An examination of the airplane revealed both fuel tanks had ruptured. The left fuel tank was found ripped open and was dry; the right tank contained about 10 gallons of fuel. The Federal Aviation Administration (FAA) coordinator reported that he examined the recovered airframe wreckage and the engine. According to the FAA, the engine was started and it functioned. Normal operation of both magnetos was noted. No abnormal conditions were found. The reason for the power loss was not determined.

Flight

Event TypeAccident
Event Time09:50 MST
Nearest AirportPAYSON (1nm)
Runway24
Runway Length5500 ft
Runway Width75 ft
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBeech N35
Tail NumberN61DE
Aircraft CategoryAir
DamageSubstantial
OperatorRobert W Glenn
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsContinental · IO-470-N-1-B · Reciprocating · 260
Seats4

People & Injuries

Injury Summary2 injuries (2 minor injuries)
Fatal0
Serious0
Minor2
Uninjured0
Total2
Crew 1Age 55 · Third Class

Conditions

ConditionsVMC
LightDaylight
WindCalm
Visibility40 sm
CeilingNone
Temperature / Dew Point64 F / 0 C
Altimeter30.00 inHg
Weather SourcePILO

Appendix: Source Data