19960416007549A

Accident · Substantial damage

FAA accident report · Bell 206B · San Diego, CA · April 16, 1996

Date
April 16, 1996 · 16:00 local
Place
San Diego, CA
Airport
Montgomery Field Airport
Phase of flight
Autorot Descent (Rotorcraft)
Operating rules
General operating rules (Part 91)
Operator
IVSA
Damage
Substantial damage
Aircraft
N2750F
NTSB investigation
NTSBLAX96LA172
Reported as
Bell 206B
Reported engine
Allison 250C20B
People aboard
2
Fatal injuries
0
Pilot’s flight hours
3,300 total1,250 in this make and model120 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)While practicing touchdown autorotations, the helicopter landed hard on uneven terrain short of the intended touchdown point. The commercial pilot-rated student was demonstrating a autorotation with a turn to the runway. As he completed the turn and was aligning with the runway, the helicopter rotor RPM dropped to 70 percent. Halfway into the maneuver the flight instructor realized the helicopter was too low and slow to accomplish a power recovery and took control. The helicopter landed short of the runway in rough terrain. A postflight inspection of the helicopter revealed wrinkles in the tail boom. The pilot under instruction held a rotorcraft helicopter rating.

As the FAA filed it

(.4)WHILE PRACTICING TOUCHDOWN AUTOROTATIONS, THE HELICOPTER LANDED HARD ON UNEVEN TERRAIN SHORT OF THE INTENDED TOUCHDOWN POINT. THE COMMERCIAL PILOT-RATED STUDENT WAS DEMONSTRATING A AUTOROTATION WITH A TURN TO THE RUNWAY. AS HE COMPLETED THE TURN AND WAS ALIGNING WITH THE RUNWAY, THE HELICOPTER ROTOR RPM DROPPED TO 70 PERCENT. HALFWAY INTO THE MANEUVER THE FLIGHT INSTRUCTOR REALIZED THE HELICOPTER WAS TOO LOW AND SLOW TO ACCOMPLISH A POWER RECOVERY AND TOOK CONTROL. THE HELICOPTER LANDED SHORT OF THE RUNWAY IN ROUGH TERRAIN. A POSTFLIGHT INSPECTION OF THE HELICOPTER REVEALED WRINKLES IN THE TAIL BOOM. THE PILOT UNDER INSTRUCTION HELD A ROTORCRAFT HELICOPTER RATING.

NTSB investigation

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