19990706043389A

Accident · Substantial damage

FAA accident report · Bell 206L3 · Wood Bridge, NJ · July 6, 1999

Date
July 6, 1999 · 16:45 local
Place
Wood Bridge, NJ
Phase of flight
Power On Descent (Rotorcraft)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N4NJ
NTSB investigation
NTSBNYC99FA169
Reported as
Bell 206L3
Reported engine
Allison 250C30P
Fatal injuries
0
Pilot’s flight hours
2,250 total500 in this make and model45 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.

(.4)The pilot took off into the wind to conduct a high orbit, and as the pilot 'gently and smoothly' started a right turn, an uncommanded right yaw, along with a 'high engine whine sound,' was experienced. At that time the pilot estimated the wind was at his 10 o'clock position. The pilot immediately applied left pedal to compensate for the right yaw, but it did not arrest the rotation. The collective was then lowered, and in an attempt to fly out of the ensuing condition, the helicopter was turned into the direction of rotation. After the helicopter made three complete 360-degree turns to the right, the PIC closed the throttle to idle, and performed an autorotation to a dry lakebed. FAA advisory circular 90-95 stated that 'any maneuver which requires the pilot to operate in a high-power, low airspeed environment with a left crosswind or tailwind creates an environment where unanticipated right yaw may occur.' The ac also advised of greater susceptibility for lte in right turns and the phenomena may occur in varying degrees in all single main rotor helicopters at airspeeds less than 30 knots. (-23)n.j. state police helicopter was involved in search for escaped prison er, when it experienced loss of tail rotor authority and impacted with ground.

As the FAA filed it

(.4)THE PILOT TOOK OFF INTO THE WIND TO CONDUCT A HIGH ORBIT, AND AS THE PILOT 'GENTLY AND SMOOTHLY' STARTED A RIGHT TURN, AN UNCOMMANDED RIGHT YAW, ALONG WITH A 'HIGH ENGINE WHINE SOUND,' WAS EXPERIENCED. AT THAT TIME THE PILOT ESTIMATED THE WIND WAS AT HIS 10 O'CLOCK POSITION. THE PILOT IMMEDIATELY APPLIED LEFT PEDAL TO COMPENSATE FOR THE RIGHT YAW, BUT IT DID NOT ARREST THE ROTATION. THE COLLECTIVE WAS THEN LOWERED, AND IN AN ATTEMPT TO FLY OUT OF THE ENSUING CONDITION, THE HELICOPTER WAS TURNED INTO THE DIRECTION OF ROTATION. AFTER THE HELICOPTER MADE THREE COMPLETE 360-DEGREE TURNS TO THE RIGHT, THE PIC CLOSED THE THROTTLE TO IDLE, AND PERFORMED AN AUTOROTATION TO A DRY LAKEBED. FAA ADVISORY CIRCULAR 90-95 STATED THAT 'ANY MANEUVER WHICH REQUIRES THE PILOT TO OPERATE IN A HIGH-POWER, LOW AIRSPEED ENVIRONMENT WITH A LEFT CROSSWIND OR TAILWIND CREATES AN ENVIRONMENT WHERE UNANTICIPATED RIGHT YAW MAY OCCUR.' THE AC ALSO ADVISED OF GREATER SUSCEPTIBILITY FOR LTE IN RIGHT TURNS AND THE PHENOMENA MAY OCCUR IN VARYING DEGREES IN ALL SINGLE MAIN ROTOR HELICOPTERS AT AIRSPEEDS LESS THAN 30 KNOTS. (-23)N.J. STATE POLICE HELICOPTER WAS INVOLVED IN SEARCH FOR ESCAPED PRISON ER, WHEN IT EXPERIENCED LOSS OF TAIL ROTOR AUTHORITY AND IMPACTED WITH GROUND.

NTSB investigation

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