20170908015939A

Accident · Destroyed

FAA accident report · Schweizer 269C-1 · Medford, NJ · September 8, 2017

Date
September 8, 2017 · 13:00 local
Place
Medford, NJ
Airport
Flying W
Phase of flight
Landing: Approach
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N204HF
NTSB investigation
NTSBERA17FA317
Reported as
Schweizer 269C-1
Reported engine
Lycoming HO-360
People aboard
2
Fatal injuries
2
Other injuries
0
Pilot’s certificates
Commercial pilot, flight instructor, private pilot
Pilot’s flight hours
480 total376 in this make and model164 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

While conducting a part 91 ride with one passenger the pilot notified Flying W UNICOM of throttle failure and that the RPM was stuck at a high power setting. For approximately 15 minutes 3 other qualified helicopter pilots rendered assistance, advice and suggestions over the UNICOM frequency. The local police, fire and EMS was alerted and was in position adjacent to the intended runway for landing. The pilot elected to perform an autorotation from approximately 1000' AGL to runway 1. The initial segment of the autorotation appeared normal to aviation witnesses. At approximately 500' AGL however the helicopter descended vertically at a high rate with noticeably low rotor RPM and impacted trees and brush in a ravine approximately 200' short of the intended runway.

As the FAA filed it

WHILE CONDUCTING A PART 91 RIDE WITH ONE PASSENGER THE PILOT NOTIFIED FLYING W UNICOM OF THROTTLE FAILURE AND THAT THE RPM WAS STUCK AT A HIGH POWER SETTING. FOR APPROXIMATELY 15 MINUTES 3 OTHER QUALIFIED HELICOPTER PILOTS RENDERED ASSISTANCE, ADVICE AND SUGGESTIONS OVER THE UNICOM FREQUENCY. THE LOCAL POLICE, FIRE AND EMS WAS ALERTED AND WAS IN POSITION ADJACENT TO THE INTENDED RUNWAY FOR LANDING. THE PILOT ELECTED TO PERFORM AN AUTOROTATION FROM APPROXIMATELY 1000' AGL TO RUNWAY 1. THE INITIAL SEGMENT OF THE AUTOROTATION APPEARED NORMAL TO AVIATION WITNESSES. AT APPROXIMATELY 500' AGL HOWEVER THE HELICOPTER DESCENDED VERTICALLY AT A HIGH RATE WITH NOTICEABLY LOW ROTOR RPM AND IMPACTED TREES AND BRUSH IN A RAVINE APPROXIMATELY 200' SHORT OF THE INTENDED RUNWAY.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.