19990810038129I

Incident · Minor damage

FAA incident report · Skrsky S-55 · Orlando, FL · August 10, 1999

Date
August 10, 1999 · 06:55 local
Place
Orlando, FL
Airport
Orlando Sanford Airport
Phase of flight
Autorot Descent (Rotorcraft)
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N17754
Reported as
Skrsky S55
People aboard
2
Fatal injuries
0
Pilot’s flight hours
3,800 total1,200 in this make and model35 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.

(-23) Mr. James r. arnold, FAA flight test pilot, rotorcraft directorate, aircraft certification service, fort worth, Texas, 76193-0170, and captain ron mander, PIC, vice president of operations, privacy data omitted were performing flight testing, which was a type inspection authorization (certification flight tests). During this testing, the engine was cut at approximately 40-50 feet, from the runway and the aircraft descended toward the runway in a tail low altitude, resulting in a tail rotor strike. The tail motor strike, caused separation at the tail motor gearbox. No injuries to the pilots. Visual meteorological conditions existed at the time of this incident. No action required because of the certification process of additional equipment which places the helicopter in an experimental status.

As the FAA filed it

(-23) MR. JAMES R. ARNOLD, FAA FLIGHT TEST PILOT, ROTORCRAFT DIRECTORATE, AIRCRAFT CERTIFICATION SERVICE, FORT WORTH, TEXAS, 76193-0170, AND CAPTAIN RON MANDER, PIC, VICE PRESIDENT OF OPERATIONS, ^PRIVACY DATA OMITTED^ WERE PERFORMING FLIGHT TESTING, WHICH WAS A TYPE INSPECTION AUTHORIZATION (CERTIFICATION FLIGHT TESTS). DURING THIS TESTING, THE ENGINE WAS CUT AT APPROXIMATELY 40-50 FEET, FROM THE RUNWAY AND THE AIRCRAFT DESCENDED TOWARD THE RUNWAY IN A TAIL LOW ALTITUDE, RESULTING IN A TAIL ROTOR STRIKE. THE TAIL MOTOR STRIKE, CAUSED SEPARATION AT THE TAIL MOTOR GEARBOX. NO INJURIES TO THE PILOTS. VISUAL METEOROLOGICAL CONDITIONS EXISTED AT THE TIME OF THIS INCIDENT. NO ACTION REQUIRED BECAUSE OF THE CERTIFICATION PROCESS OF ADDITIONAL EQUIPMENT WHICH PLACES THE HELICOPTER IN AN EXPERIMENTAL STATUS.

Other reports on N17754 · 1

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