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May 1, 2000 · Hughes 269C · N5395S

Rialto, CA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
May 1, 2000
Injury Outcomes
2 injuries (2 minor injuries)
Location
Rialto, CA
Aircraft
Hughes 269C
Tail Number
N5395S
Operator
Western Operations
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
LAX00LA181

The helicopter landed hard and rolled over during a practice autorotation. The CFI was providing dual instruction to his student, a CFI candidate. The student was handling all of the controls, and he intended to perform a 180-degree full touchdown autorotation. During the maneuver, the CFI observed that his student had allowed the airspeed to decrease and the main rotor rpm to become low. The CFI called the low rotor rpm situation to his student's attention. However, the student did not take decisive corrective action by initiating a power recovery in sufficient time to avoid the resultant low rotor rpm flare and hard touchdown. No mechanical malfunctions were noted.

NTSB Probable Cause

The student's misjudged altitude and failure to maintain rotor rpm while practicing an autorotation, and, the instructor's delayed remedial corrective action and inadequate supervision of the flight.

Full Narrative

On May 1, 2000, about 1645 hours Pacific daylight time, a Hughes 269C, N5395S, operated by Western Operations, Inc., landed hard at the (uncontrolled) Rialto Municipal Airport, Rialto, California. The helicopter was substantially damaged, and the commercial certificated flight instructor (CFI) and the student sustained minor injuries. Visual meteorological conditions prevailed, and no flight plan was filed. The instructional flight was performed under 14 CFR Part 91, and it originated from Rialto about 1600. The CFI indicated to the National Transportation Safety Board investigator that he was providing dual instruction to the student, and the student was handling all of the engine and flight controls. The CFI was providing training to the student who was a CFI candidate. The accident occurred during a practice, 180-degree full touchdown autorotation, when the helicopter's airspeed decreased and the main rotor rpm became too low. The CFI indicated that he observed the low rpm indication and called it to the attention of his student, but the student did not take decisive corrective action by promptly initiating a power recovery to avoid the resultant low rotor rpm flare and hard touchdown. No mechanical malfunctions were noted. The student reported to the Safety Board investigator that he holds an airline transport pilot certificate with both airplane and rotorcraft ratings. He also holds a CFI certificate for airplanes. The purpose of the flight was to receive instruction in furtherance of a rotorcraft instructor's certificate. The student indicated that he commenced the practice full touchdown autorotation from 2,000 feet mean sea level (about 545 above ground level), and abeam the desired taxiway touchdown point. He stated that, "As I rolled out on final at 300 feet (agl) I was low." The student indicated that although he had initiated a power recovery, the helicopter impacted the ground hard. He also stated that no mechanical malfunctions occurred during the flight.

Flight

Event TypeAccident
Event Time16:45 PDT
Nearest AirportRialto Municipal (0nm)
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftHughes 269C
Tail NumberN5395S
Aircraft CategoryHeli
DamageSubstantial
OperatorWestern Operations
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · HIO-360-D1A · Reciprocating · 190
Seats3

People & Injuries

Injury Summary2 injuries (2 minor injuries)
Fatal0
Serious0
Minor2
Uninjured0
Total2
Crew 1Age 67 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind240° @ 13 kt
Visibility10 sm
CeilingBroken clouds 25000 ft
Temperature / Dew Point19 C / 14 C
Altimeter29.00 inHg
Observation Time23:53
Weather SourceWFAC

Appendix: Source Data