Narrative:

Winds were out of the east at 10-15 kts in VFR conditions; and the aircraft was oriented directly into the wind. The helideck of the platform is located on the south side of the superstructure; with obstacles to the north. Upon departure from the platform; the aircraft began an unexpected right yaw and began to drift in a southwestern direction. Once the aircraft began to rotate; I as the first officer took control; believing the PIC (pilot in command) to be disoriented; as I had not heard a verbal acknowledgement after taking control. On the second or third spin; I was able to regain directional control through the application of left pedal and slight left cyclic while oriented to the east into the wind. I then lowered the nose in order to gain airspeed and was able to regain full control and recover the aircraft at roughly 50 feet AGL. After establishing a climb; I coupled the flight controls to the flight director; began a turn to the northwest; and relinquished controls back to the PIC.we then began an analysis of the aircraft; checking for any warning/cautions/advisories; any unusual vibrations in the flight controls; or any indications that an aircraft limit had been exceeded. None were present; and based on this information we continued our flight as planned. We made two more subsequent stops to drop off passengers and cargo; and terminated our flight. We conducted a normal shutdown; and then noticed we had used transient power; seven seconds into a two-minute power limit. Maintenance was notified; and we as a crew notified our supervisor of what had taken place.

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Original NASA ASRS Text

Title: S-76 flight crew reported loss of tail rotor effectiveness on takeoff.

Narrative: Winds were out of the east at 10-15 kts in VFR conditions; and the aircraft was oriented directly into the wind. The helideck of the platform is located on the south side of the superstructure; with obstacles to the north. Upon departure from the platform; the aircraft began an unexpected right yaw and began to drift in a southwestern direction. Once the aircraft began to rotate; I as the First Officer took control; believing the PIC (Pilot in Command) to be disoriented; as I had not heard a verbal acknowledgement after taking control. On the second or third spin; I was able to regain directional control through the application of left pedal and slight left cyclic while oriented to the east into the wind. I then lowered the nose in order to gain airspeed and was able to regain full control and recover the aircraft at roughly 50 feet AGL. After establishing a climb; I coupled the flight controls to the flight director; began a turn to the northwest; and relinquished controls back to the PIC.We then began an analysis of the aircraft; checking for any warning/cautions/advisories; any unusual vibrations in the flight controls; or any indications that an aircraft limit had been exceeded. None were present; and based on this information we continued our flight as planned. We made two more subsequent stops to drop off passengers and cargo; and terminated our flight. We conducted a normal shutdown; and then noticed we had used transient power; seven seconds into a two-minute power limit. Maintenance was notified; and we as a crew notified our Supervisor of what had taken place.

Data retrieved from NASA's ASRS site and automatically converted to unabbreviated mixed upper/lowercase text. This report is for informational purposes with no guarantee of accuracy. See NASA's ASRS site for official report.