ASN Wikibase Occurrence # 365870
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Date: | Sunday 9 December 1990 |
Time: | 12:30 LT |
Type: | Bell 206B-3 |
Owner/operator: | River City Helicopters |
Registration: | N53MA |
MSN: | 2285 |
Year of manufacture: | 1977 |
Total airframe hrs: | 4020 hours |
Engine model: | Allison 250-C20B |
Fatalities: | Fatalities: 0 / Occupants: 2 |
Aircraft damage: | Substantial |
Category: | Accident |
Location: | Coeur D'alene, ID -
United States of America
|
Phase: | Landing |
Nature: | Training |
Departure airport: | (KCOE) |
Destination airport: | |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:THE PILOT (PIC) AND AN FAA INSPECTOR (CHECK PLT) WERE ON A COMBINED FLT INSTRUCTOR & FAR PART 135 CHECK FLT. THE CHECK PLT INSTRUCTED THE PIC TO EXECUTE A SIMULATED FIXED-TAIL ROTOR FAILURE; THE CHECK PLT SIMULATED THE FAILURE BY HOLDING THE RGT PEDAL SLIGHTLY IN, WHILE THE PIC REMOVED HIS FEET FROM THE PEDALS. THE PIC INITIATED A RUN-ON LANDING WITH AN ESTIMATED 10 DEG RGT YAW. HE RPRTD THAT JUST BEFORE LANDING, AT ABOUT 5 MPH & 2 FT AGL, THE HELICOPTER BEGAN TO YAW FURTHER TO THE RIGHT. HE RETARDED THE THROTTLE TO ALIGN THE HELICOPTER WITH THE GND TRACK & INCREASED THE COLLECTIVE TO CUSHION THE LANDING. THE HELICOPTER TOUCHED DOWN FIRMLY. NO PROBLEM WITH HELICOPTER WAS NOTED AT THAT TIME; HOWEVER, AFTER THE FLT, WRINKLES WERE NOTED ON THE TAIL BOOM, SIMILAR TO THOSE DEPICTED IN BELL OPNS SAFETY NOTICE (OSN) 206-84-13.
Probable Cause: FAILURE OF THE PILOT-IN-COMMAND (PIC) TO MAINTAIN ROTOR RPM, AND A DELAY BY THE FAA INSPECTOR (FLIGHT EXAMINER) IN TAKING REMEDICAL ACTION.
Accident investigation:
|
| |
Investigating agency: | NTSB |
Report number: | SEA90FA079 |
Status: | Investigation completed |
Duration: | 1 year and 10 months |
Download report: | Final report |
|
Sources:
NTSB SEA90FA079
Location
Revision history:
Date/time | Contributor | Updates |
20-Mar-2024 14:55 |
ASN Update Bot |
Added |
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