19990415003569A

Accident · Substantial damage

FAA accident report · Robsin R22 · Port Jefferson, NY · April 15, 1999

Date
April 15, 1999 · 14:45 local
Place
Port Jefferson, NY
Phase of flight
Pwr On Vertical Ldng/Rtrcrft
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N151RM
NTSB investigation
NTSBNYC99LA090
Reported as
Robsin R22
Reported engine
Lycoming O320*
People aboard
2
Fatal injuries
0
Pilot’s flight hours
750 total550 in this make and model176 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.

Pilot was practicing landing the Robinson R-22 helicopter on the beach when the acft lost engine power at 10 feet AGL, landed hard on the sand, and rolled over, other circumstances are unknown. (-23) flight instructor and his student were practicing normal approaches to a hover at a beach in Port Jefferson, nu. The flight instructor indicates that as he pulled collective pitch to bring helicopter into a hover, the aircraft engine did not produce enough power to allow aircraft to hover. Helicopter hit the sand left skid first and rolled over. Flight instructor further states that he did hear low rotor horn sound prior to touch down. (.4) the private pilot was receiving rotorcraft instruction and was on approach to land. As the helicopter passed through about 15 feet, the flight instructor was also on the flight controls. The airspeed was about 20 mph, with a descent of 200-300 fpm. When the collective was raised the helicopter continued to descend, landed hard, and rolled over. When interviewed the flight instructor remembered the low rotor warning horn had sounded. Post accident examination of the engine and mechanical throttle compensator found n o evidence of a mechanical failure. The helicopter manufacturer had published a safety notice which cautioned against airspeed of less than 30 knots until the descent rates were less than 300 fpm.

As the FAA filed it

PILOT WAS PRACTICING LANDING THE ROBINSON R-22 HELICOPTER ON THE BEACH WHEN THE ACFT LOST ENGINE POWER AT 10 FEET AGL, LANDED HARD ON THE SAND, AND ROLLED OVER, OTHER CIRCUMSTANCES ARE UNKNOWN. (-23) FLIGHT INSTRUCTOR AND HIS STUDENT WERE PRACTICING NORMAL APPROACHES TO A HOVER AT A BEACH IN PORT JEFFERSON, NU. THE FLIGHT INSTRUCTOR INDICATES THAT AS HE PULLED COLLECTIVE PITCH TO BRING HELICOPTER INTO A HOVER, THE AIRCRAFT ENGINE DID NOT PRODUCE ENOUGH POWER TO ALLOW AIRCRAFT TO HOVER. HELICOPTER HIT THE SAND LEFT SKID FIRST AND ROLLED OVER. FLIGHT INSTRUCTOR FURTHER STATES THAT HE DID HEAR LOW ROTOR HORN SOUND PRIOR TO TOUCH DOWN. (.4) THE PRIVATE PILOT WAS RECEIVING ROTORCRAFT INSTRUCTION AND WAS ON APPROACH TO LAND. AS THE HELICOPTER PASSED THROUGH ABOUT 15 FEET, THE FLIGHT INSTRUCTOR WAS ALSO ON THE FLIGHT CONTROLS. THE AIRSPEED WAS ABOUT 20 MPH, WITH A DESCENT OF 200-300 FPM. WHEN THE COLLECTIVE WAS RAISED THE HELICOPTER CONTINUED TO DESCEND, LANDED HARD, AND ROLLED OVER. WHEN INTERVIEWED THE FLIGHT INSTRUCTOR REMEMBERED THE LOW ROTOR WARNING HORN HAD SOUNDED. POST ACCIDENT EXAMINATION OF THE ENGINE AND MECHANICAL THROTTLE COMPENSATOR FOUND N O EVIDENCE OF A MECHANICAL FAILURE. THE HELICOPTER MANUFACTURER HAD PUBLISHED A SAFETY NOTICE WHICH CAUTIONED AGAINST AIRSPEED OF LESS THAN 30 KNOTS UNTIL THE DESCENT RATES WERE LESS THAN 300 FPM.

NTSB investigation

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