19990805010839A

Accident · Substantial damage

FAA accident report · Robsin R22 ALPHA · Shirley, NY · August 5, 1999

Date
August 5, 1999 · 17:30 local
Place
Shirley, NY
Airport
Brookhaven Airport
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N8561K
NTSB investigation
NTSBNYC99LA190
Reported as
Robsin R22ALPHA
Fatal injuries
0

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.

1985 Roginson R-22 helicopter was demonstrating a 180 degree rotation when it experienced low RPM and landed hard from 50 feet AGL. (-23)at time and place of occurrence, instructor pilot (hugh paul covopoulo) was demonstrating a 180 degree autorotation maneuver to his student (guy raoul rosenschein). During final approach segment of the maneuver, the instructor pilot demonstrated an extended glide. During the extended glide procedure, the aircraft lost rotor RPM at approximately 50 feet AGL and subsequently imapcted the ground area approximately 50 feet suth of the approach end of runway 6 (hwv). The aricraft came to rest on its left side 20 feet south of the initial area, resulting in substantial damage to the aircraft and causing an injury to the instructor pilot.

As the FAA filed it

1985 ROGINSON R-22 HELICOPTER WAS DEMONSTRATING A 180 DEGREE ROTATION WHEN IT EXPERIENCED LOW RPM AND LANDED HARD FROM 50 FEET AGL. (-23)AT TIME AND PLACE OF OCCURRENCE, INSTRUCTOR PILOT (HUGH PAUL COVOPOULO) WAS DEMONSTRATING A 180 DEGREE AUTOROTATION MANEUVER TO HIS STUDENT (GUY RAOUL ROSENSCHEIN). DURING FINAL APPROACH SEGMENT OF THE MANEUVER, THE INSTRUCTOR PILOT DEMONSTRATED AN EXTENDED GLIDE. DURING THE EXTENDED GLIDE PROCEDURE, THE AIRCRAFT LOST ROTOR RPM AT APPROXIMATELY 50 FEET AGL AND SUBSEQUENTLY IMAPCTED THE GROUND AREA APPROXIMATELY 50 FEET SUTH OF THE APPROACH END OF RUNWAY 6 (HWV). THE ARICRAFT CAME TO REST ON ITS LEFT SIDE 20 FEET SOUTH OF THE INITIAL AREA, RESULTING IN SUBSTANTIAL DAMAGE TO THE AIRCRAFT AND CAUSING AN INJURY TO THE INSTRUCTOR PILOT.

NTSB investigation

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