20091019025969A

Accident · Substantial damage

FAA accident report · Mcdonnell D 369E · Fairfield, SC · October 19, 2009

Date
October 19, 2009 · 15:15 local
Place
Fairfield, SC
Airport
Winnsboro
Phase of flight
Hover/Holding
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N502SL
NTSB investigation
NTSBERA10LA023
Reported as
Mcdonnell D 369E
Reported engine
Rolls-Royce 250
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Commercial pilot, flight instructor
Pilot’s flight hours
2,200 total600 in this make and model100 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.

On October 19, 2009, at 1515HRS, in VMC conditions, a law enforcement helicopter was conducting recurrent training of pilots using a contract flight instructor. The aircraft carried a normal catagory airworthiness certificate. The flight instructor briefed the pilot on the emergency procedures for a loss of tailrotor thrust and reviewed the corrective actions. The pilot lifted off and established the aircraft in a hover. The flight instructor initiated the maneuver by applying right pedal until a slow right yaw had occurred. The pilot reduced the throttle and stopped the rotation and the aircraft contacted the ground. The flight instructor states at the time of ground contact the pilot reintroduced the throttle and the aircraft became airborne with low RPM and the right pedal still applied. The aircraft yawed to the right for approximately 270 degrees and climbed to about 7-10 feet. The flight instructor applied left pedal and the RPM remained low and decaying. The flight instructor attempted to cushion the aircraft with remaining collective pitch. RPM remained low and was insufficient to avoid a hard landing. The left landing failed and main rotor blades made ground contact.

As the FAA filed it

ON OCTOBER 19, 2009, AT 1515HRS, IN VMC CONDITIONS, A LAW ENFORCEMENT HELICOPTER WAS CONDUCTING RECURRENT TRAINING OF PILOTS USING A CONTRACT FLIGHT INSTRUCTOR. THE AIRCRAFT CARRIED A NORMAL CATAGORY AIRWORTHINESS CERTIFICATE. THE FLIGHT INSTRUCTOR BRIEFED THE PILOT ON THE EMERGENCY PROCEDURES FOR A LOSS OF TAILROTOR THRUST AND REVIEWED THE CORRECTIVE ACTIONS. THE PILOT LIFTED OFF AND ESTABLISHED THE AIRCRAFT IN A HOVER. THE FLIGHT INSTRUCTOR INITIATED THE MANEUVER BY APPLYING RIGHT PEDAL UNTIL A SLOW RIGHT YAW HAD OCCURRED. THE PILOT REDUCED THE THROTTLE AND STOPPED THE ROTATION AND THE AIRCRAFT CONTACTED THE GROUND. THE FLIGHT INSTRUCTOR STATES AT THE TIME OF GROUND CONTACT THE PILOT REINTRODUCED THE THROTTLE AND THE AIRCRAFT BECAME AIRBORNE WITH LOW RPM AND THE RIGHT PEDAL STILL APPLIED. THE AIRCRAFT YAWED TO THE RIGHT FOR APPROXIMATELY 270 DEGREES AND CLIMBED TO ABOUT 7-10 FEET. THE FLIGHT INSTRUCTOR APPLIED LEFT PEDAL AND THE RPM REMAINED LOW AND DECAYING. THE FLIGHT INSTRUCTOR ATTEMPTED TO CUSHION THE AIRCRAFT WITH REMAINING COLLECTIVE PITCH. RPM REMAINED LOW AND WAS INSUFFICIENT TO AVOID A HARD LANDING. THE LEFT LANDING FAILED AND MAIN ROTOR BLADES MADE GROUND CONTACT.

NTSB investigation

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