19960706016339I

Incident · Minor damage

FAA incident report · Robsin R22 BETA · Littleton, NC · July 6, 1996

Date
July 6, 1996 · 18:40 local
Place
Littleton, NC
Phase of flight
Forced/Precautionary Landing
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N23428
Reported as
Robsin R22BETA
Reported engine
Lycoming O320B2C
People aboard
2
Fatal injuries
0
Pilot’s flight hours
1,000 total80 in this make and model25 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.

Narrative: pilot stated in phone interview that after refueling helicopter with a total of 30 gallons, he and his passenger departed a backyard located in the fox hollow subdivision. Departure time was approximately 1800 to 1815 EDT. Fuel was purchased from an amoco and 93 octane automotive fuel was used. Shortly after clearing some high tension power lines at approximately 200 feet AGL, the helicopter entered a slight r/h turn, descending. At that point, the low rotor RPM light and horn activated. The pilot stated that he lowered the collective and attempted to add power. A vibration began to occur "like it lost a jug". The helicopter continued to lose altitude and rotor RPM. Pilot reported that the throttle felt stiff. Pilot notified passenger that "we're going down". Helicopter landed in the water and rolled onto its left side. Both occupants had seat belts and shoulder harnesses on. Both occupants safety exited the right side of the helicopter and swam fifty to sixty feet to shore. Pilot reported approximately 20 gallons of fuel remaining at time of incident. Unable to verify this due to water contamination. Pilot weighs approximately 235 to 240 pounds. Passenge r weighs approximately 190 pounds.

As the FAA filed it

NARRATIVE: PILOT STATED IN PHONE INTERVIEW THAT AFTER REFUELING HELICOPTER WITH A TOTAL OF 30 GALLONS, HE AND HIS PASSENGER DEPARTED A BACKYARD LOCATED IN THE FOX HOLLOW SUBDIVISION. DEPARTURE TIME WAS APPROXIMATELY 1800 TO 1815 EDT. FUEL WAS PURCHASED FROM AN AMOCO AND 93 OCTANE AUTOMOTIVE FUEL WAS USED. SHORTLY AFTER CLEARING SOME HIGH TENSION POWER LINES AT APPROXIMATELY 200 FEET AGL, THE HELICOPTER ENTERED A SLIGHT R/H TURN, DESCENDING. AT THAT POINT, THE LOW ROTOR RPM LIGHT AND HORN ACTIVATED. THE PILOT STATED THAT HE LOWERED THE COLLECTIVE AND ATTEMPTED TO ADD POWER. A VIBRATION BEGAN TO OCCUR "LIKE IT LOST A JUG". THE HELICOPTER CONTINUED TO LOSE ALTITUDE AND ROTOR RPM. PILOT REPORTED THAT THE THROTTLE FELT STIFF. PILOT NOTIFIED PASSENGER THAT "WE'RE GOING DOWN". HELICOPTER LANDED IN THE WATER AND ROLLED ONTO ITS LEFT SIDE. BOTH OCCUPANTS HAD SEAT BELTS AND SHOULDER HARNESSES ON. BOTH OCCUPANTS SAFETY EXITED THE RIGHT SIDE OF THE HELICOPTER AND SWAM FIFTY TO SIXTY FEET TO SHORE. PILOT REPORTED APPROXIMATELY 20 GALLONS OF FUEL REMAINING AT TIME OF INCIDENT. UNABLE TO VERIFY THIS DUE TO WATER CONTAMINATION. PILOT WEIGHS APPROXIMATELY 235 TO 240 POUNDS. PASSENGE R WEIGHS APPROXIMATELY 190 POUNDS.

Other reports on N23428 · 1

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