19981210044229A

Accident · Substantial damage

FAA accident report · Robsin R22 BETA · West Palm Beach, FL · December 10, 1998

Date
December 10, 1998 · 14:00 local
Place
West Palm Beach, FL
Airport
Palm Beach County Park Airport
Phase of flight
Level Off Touchdown
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N2321X
NTSB investigation
NTSBATL99LA033
Reported as
Robsin R22BETA
Reported engine
Lycoming O320B2C
People aboard
2
Fatal injuries
0
Pilot’s flight hours
320 total260 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.

(.19)On December 10, 1998, at 1400 eastern standard time, a Robinson R-22, helicopter, N2321X, collided with the ground, according to the flight instructor, during a practice autorotation, at the lantana airport, in lantana, Florida. The instructional flight operated under the provisions of title 14 CFR part 91 with no flight plan filed. A review of weather data from the nearest reporting facility revealed that, visual weather conditions prevailed at the time of the accident. According to the director of maintenance for the operator, the helicopter sustained substantial structural damage to the airframe. The flight instructor and the dual student were not injured. The initial departure time of the flight from lantana, Florida, was not determined. The flight instructor reported that he and the dual student were conducting autorotation training. The dual student had completed several power recovery autorotations, and the session had progressed to the point where the dual student was ready for a 180-degree autorotation. The flight instuctor was demonstrating a 180-degree autorotation, with power recovery, when the accident occurred. The flight instructor stated that he did no t believe that the engine responded when the power was applied for the recovery. (.4) the flight instructor was demonstrating a 180-degree autorotation, with power recovery, when the accident occurred. As the helicopter descended through 200 feet the low rotor RPM horn sounded. The tachometer was at about 92 percent. The flight instructor then rolled on the throttle and went down on the collective simultaneously. The helicopter contacted the ground in a level attitude. The instructor attempted a shallow flare, and cushioned with collective. The aircraft slid in grass, the right skid dug into the ground and the helicopter rolled over. No mechanical problems with the airplane were discovered during the wreckage examination.

As the FAA filed it

(.19)ON DECEMBER 10, 1998, AT 1400 EASTERN STANDARD TIME, A ROBINSON R-22, HELICOPTER, N2321X, COLLIDED WITH THE GROUND, ACCORDING TO THE FLIGHT INSTRUCTOR, DURING A PRACTICE AUTOROTATION, AT THE LANTANA AIRPORT, IN LANTANA, FLORIDA. THE INSTRUCTIONAL FLIGHT OPERATED UNDER THE PROVISIONS OF TITLE 14 CFR PART 91 WITH NO FLIGHT PLAN FILED. A REVIEW OF WEATHER DATA FROM THE NEAREST REPORTING FACILITY REVEALED THAT, VISUAL WEATHER CONDITIONS PREVAILED AT THE TIME OF THE ACCIDENT. ACCORDING TO THE DIRECTOR OF MAINTENANCE FOR THE OPERATOR, THE HELICOPTER SUSTAINED SUBSTANTIAL STRUCTURAL DAMAGE TO THE AIRFRAME. THE FLIGHT INSTRUCTOR AND THE DUAL STUDENT WERE NOT INJURED. THE INITIAL DEPARTURE TIME OF THE FLIGHT FROM LANTANA, FLORIDA, WAS NOT DETERMINED. THE FLIGHT INSTRUCTOR REPORTED THAT HE AND THE DUAL STUDENT WERE CONDUCTING AUTOROTATION TRAINING. THE DUAL STUDENT HAD COMPLETED SEVERAL POWER RECOVERY AUTOROTATIONS, AND THE SESSION HAD PROGRESSED TO THE POINT WHERE THE DUAL STUDENT WAS READY FOR A 180-DEGREE AUTOROTATION. THE FLIGHT INSTUCTOR WAS DEMONSTRATING A 180-DEGREE AUTOROTATION, WITH POWER RECOVERY, WHEN THE ACCIDENT OCCURRED. THE FLIGHT INSTRUCTOR STATED THAT HE DID NO T BELIEVE THAT THE ENGINE RESPONDED WHEN THE POWER WAS APPLIED FOR THE RECOVERY. (.4) THE FLIGHT INSTRUCTOR WAS DEMONSTRATING A 180-DEGREE AUTOROTATION, WITH POWER RECOVERY, WHEN THE ACCIDENT OCCURRED. AS THE HELICOPTER DESCENDED THROUGH 200 FEET THE LOW ROTOR RPM HORN SOUNDED. THE TACHOMETER WAS AT ABOUT 92 PERCENT. THE FLIGHT INSTRUCTOR THEN ROLLED ON THE THROTTLE AND WENT DOWN ON THE COLLECTIVE SIMULTANEOUSLY. THE HELICOPTER CONTACTED THE GROUND IN A LEVEL ATTITUDE. THE INSTRUCTOR ATTEMPTED A SHALLOW FLARE, AND CUSHIONED WITH COLLECTIVE. THE AIRCRAFT SLID IN GRASS, THE RIGHT SKID DUG INTO THE GROUND AND THE HELICOPTER ROLLED OVER. NO MECHANICAL PROBLEMS WITH THE AIRPLANE WERE DISCOVERED DURING THE WRECKAGE EXAMINATION.

NTSB investigation

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

Other reports on N2321X · 2

Matched to the same aircraft by N-number and date.