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Aviation safety reports, made easier to study

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January 15, 2022 · Bell 205A-1 · N502HQ

El Cajon, CA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
January 15, 2022
Injury Outcomes
No injuries (2 uninjured)
Location
El Cajon, CA
Aircraft
Bell 205A-1 (1974)
Tail Number
N502HQ
Injuries
None
Aircraft Damage
Substantial
NTSB Number
ANC22LA014

The flight instructor stated that he was demonstrating an autorotation to the pilot receiving instruction as part of the company’s flight training program. The flight instructor entered the autorotation at an altitude of about 1,500 to 2,000 ft above ground level and reduced the engine’s power to flight idle during the descent. When the helicopter reached its power recovery altitude, the instructor attempted to increase the engine’s power; however, the engine did not respond. Subsequently, he attempted to recover engine power three times but was unsuccessful. The pilot committed to a touchdown autorotation. On touchdown, the helicopter rocked forward then aft on its skids, and the main rotor blades struck the tailboom, which sustained substantial damage. A postaccident examination of the engine, governor, and fuel control revealed no preaccident mechanical malfunctions or failures that would have precluded normal operation. As a result, the reason for the partial loss of engine power could not be determined from the available evidence for this investigation.

NTSB Probable Cause

A partial loss of engine power for reasons that could not be determined based on the available evidence.

Full Narrative

On January 15, 2022, about 1230 Pacific standard time, a Bell 205A-1 helicopter, N502HQ, sustained substantial damage when it was involved in an accident near El Cajon, California. The flight instructor and the pilot receiving instruction were not injured. The helicopter was operated as a Title 14 Code of Federal Regulations Part 91 instructional flight. The flight instructor stated that he was demonstrating an autorotation to the pilot receiving instruction as part of the company’s flight training program. The flight instructor entered the autorotation at an altitude of about 1,500 to 2,000 ft above ground level and reduced the engine’s power to flight idle during the descent. When the helicopter reached its power recovery altitude, the instructor attempted to increase the engine’s power, but the engine did not respond. Subsequently, he attempted to recover engine power three times but was unable to do so. The pilot then committed to a touchdown autorotation. On touchdown, the helicopter rocked forward and then aft on its skids, and the main rotor blades struck the tailboom, which sustained substantial damage. A postaccident examination of the engine, governor, and fuel control (which included a full engine run in accordance with the engine manufacturer’s overhaul manual, full vibration analysis with all parameters within limits. Functional test on the governor to check flow rates and reaction time moving from each parameter to another. Functional test of fuel regulator emergency solenoid, acceleration flow rates were checked, main components of the computer assembly were checked, and borescope inspection) revealed no preaccident mechanical malfunctions or failures that would have precluded normal operation.

Flight

Event TypeAccident
Event Time12:30 PST
Nearest Airport0nm
Flight Plan FiledCvfr
Flight Plan ActivatedYes
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBell 205A-1
Tail NumberN502HQ
Aircraft CategoryHeli
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeTurboshaft
Engine DetailsHoneywell · T-53-17A · Turboshaft · 1500
Seats11

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 47 · First Class · None
Crew 2Age 39 · Second Class · None

Conditions

ConditionsVMC
LightDaylight
WindCalm
Visibility10 sm
CeilingNone
Temperature / Dew Point52 F / 43 F
Altimeter30.11 inHg
Observation Time01:55
Weather SourceWFAC

Appendix: Source Data