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NTSB Report

March 8, 2000 · Arrow Aircraft OH-58A · N39FA

Calipatria, CA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
March 8, 2000
Injury Outcomes
1 injury (1 serious injury)
Location
Calipatria, CA
Aircraft
Arrow Aircraft OH-58A
Tail Number
N39FA
Operator
Farm Air Services
Injuries
Serious
Aircraft Damage
Substantial
NTSB Number
LAX00LA118

The helicopter took off to the south and began a climb. Upon reaching about 60 feet above the ground, the helicopter lost power. At this time the helicopter was approaching power lines and the pilot used cyclic to climb over them. After clearing the wires, the pilot attempted an autorotative landing but there was insufficient main rotor speed to cushion the landing. The helicopter impacted the ground and the main rotor flexed severing the tail boom.

NTSB Probable Cause

The pilot's inadequate checklist procedure prior to departure, which did not verify the fuel selector was in the proper position for flight, and the pilot's failure to maintain adequate main rotor speed for an autorotative landing.

Full Narrative

On March 8, 2000, at 1215 hours Pacific standard time, an Arrow Falcon OH-58A, N39FA, experienced a power loss and made a forced landing while taking off at Calipatria, California. The helicopter sustained substantial damage and the certificated commercial pilot, the sole occupant, received serious injuries. The aircraft was being operated as an agricultural flight by Farm Air Services, Inc., under 14 CFR Part 137 when the accident occurred. The flight was originating from the Cliff Hatfield Memorial Airport at the time of the accident. Visual meteorological conditions prevailed at the time and no flight plan was filed. Witnesses said the pilot was taking off to the south from the operator's ramp and had reached an altitude of about 60 feet agl when the power loss occurred. At the time, he was approaching utility lines at the field boundary and chose to make a cyclic climb in order to clear them. After clearing the lines, he attempted to make an autorotative landing but lacked sufficient main rotor rpm to decelerate and cushion the landing. The aircraft landed hard, bounced, and spun laterally. In the process, the main rotor blades flexed down and severed the tailboom. The postcrash inspection revealed that the fuel selector had been in the off position. The fuel filter was opened and only about 4 ounces of fuel was found in the bowl, which normally holds about 20 ounces. There were no traces of fuel found in the high pressure fuel filter. Both the N1 and N2 turbines rotated freely. The pilot did not recall moving any switches or levers before exiting the helicopter. A pilot/operator report of the accident on NTSB Form 6120.1/2 was not received.

Flight

Event TypeAccident
Event Time12:15 PST
Nearest AirportCliff Hatfield Memorial (0nm S)
Runway8
Runway Length3440 ft
Runway Width50 ft
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftArrow Aircraft OH-58A
Tail NumberN39FA
Aircraft CategoryHeli
DamageSubstantial
OperatorFarm Air Services
Operating RulePart 137
Engines1
Engine TypeTurboshaft
Engine DetailsRolls-Royce · T63A720 · Turboshaft · 317
Seats4

People & Injuries

Injury Summary1 injury (1 serious injury)
Fatal0
Serious1
Minor0
Uninjured0
Total1
Crew 1Age 45 · Unknown · Minor

Conditions

ConditionsVMC
LightDaylight
Wind150° @ 11 kt
Visibility30 sm
CeilingBroken clouds 20000 ft
Temperature / Dew Point66 F / 41 C
Altimeter30.14 inHg
Observation Time19:50
Weather SourceWFAC

Appendix: Source Data