20000902026719I

Incident · Substantial damage

FAA incident report · Hughes 269C · St. Francis, MO · September 2, 2000

Date
September 2, 2000 · 19:10 local
Place
St. Francis, MO
Phase of flight
Autorot Descent (Rotorcraft)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N24TP
Reported as
Hughes 269C
Reported engine
Continental IO360*
People aboard
2
Fatal injuries
0
Pilot’s flight hours
4,600 total150 in this make and model90 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)On takeoff field location at approximately seventy feet, pilot heard "metal on metal" sound from rear of helicopter immediately followed by an aircraft right yaw of approximately thirty degrees. Pilot entered autorotation and landed on a slope resulting in the tail rotor blades, tail skid, and lower vertical fin on the tail boom striking the ground. Additionally, aircraft aft landing gear cross tube and structural support were spread/bent respectively. Initial discussion of aircraft damage with NTSB investigator privacy data omitted (chicago) resulted in an aircraft damage assessment of an incident. Suspect loss or control of tail rotor authority. Investigation is continuing into determining the cause of the aircraft incident.

As the FAA filed it

(-23)ON TAKEOFF FIELD LOCATION AT APPROXIMATELY SEVENTY FEET, PILOT HEARD "METAL ON METAL" SOUND FROM REAR OF HELICOPTER IMMEDIATELY FOLLOWED BY AN AIRCRAFT RIGHT YAW OF APPROXIMATELY THIRTY DEGREES. PILOT ENTERED AUTOROTATION AND LANDED ON A SLOPE RESULTING IN THE TAIL ROTOR BLADES, TAIL SKID, AND LOWER VERTICAL FIN ON THE TAIL BOOM STRIKING THE GROUND. ADDITIONALLY, AIRCRAFT AFT LANDING GEAR CROSS TUBE AND STRUCTURAL SUPPORT WERE SPREAD/BENT RESPECTIVELY. INITIAL DISCUSSION OF AIRCRAFT DAMAGE WITH NTSB INVESTIGATOR ^PRIVACY DATA^ (CHICAGO) RESULTED IN AN AIRCRAFT DAMAGE ASSESSMENT OF AN INCIDENT. SUSPECT LOSS OR CONTROL OF TAIL ROTOR AUTHORITY. INVESTIGATION IS CONTINUING INTO DETERMINING THE CAUSE OF THE AIRCRAFT INCIDENT.

Other reports on N24TP · 1

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