20011125031789A

Accident · Substantial damage

FAA accident report · Hughes OH-6A · Hernando, MS · November 25, 2001

Date
November 25, 2001 · 16:00 local
Place
Hernando, MS
Airport
Private
Phase of flight
Sfl Autorotation
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N129BC
NTSB investigation
NTSBMIA02LA029
Reported as
Hughes OH6A
Reported engine
Allison 250C10D
People aboard
2
Fatal injuries
0
Pilot’s flight hours
11,000 total1,200 in this make and model95 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) During auto rotation to ground, instructor pilot noticed aircraft descending too rapidly but could not recover in time. (.4) on November 25, 2001, about 1600 central standard time, a Hughes OH-6A helicopter, N129BC, registered to, and operated by the desoto county sheriff's office, as title 14 CFR part 91 instructional flight, made a hard landing at a Private field in Hernando, Mississippi. Visual meteorological conditions prevailed, and no flight plan was filed. The student pilot, and the airline transport-rated flight instructor were not injured, and the helicopter incurred substantial damage. The flight originated from Hernando, Mississippi, the same day, about 1610. The flight instructor stated that they had been practicing autorotations and during the last autorotation the student was flying the helicopter. The instructor said that the airspeed on final was 70 knots, and that the student flared the helicopter at an altitude of about 65 feet, and applied initial collective pitch control input at about 10 feet, leveling the helicopter. He said that the helicopter was about 2 feet high, and still moving forward, and at that point the student did not let the helicopter settle to the ground, but continued to apply collective pitch control input. The instructor said he stopped the student from applying collective pitch control input, and the helicopter started to descend, but the student applied aft cyclic control input, and the helicopter contacted the ground on the heels of the skids, while main rotor rpms were low. He said the main rotor blades contacted the tail boom, severing the tail just forward of the tail rotor gear box. According to the flight instructor, prior to the accident, there were no failures or malfunctions to the helicopter, or any of its systems.

As the FAA filed it

(-23) DURING AUTO ROTATION TO GROUND, INSTRUCTOR PILOT NOTICED AIRCRAFT DESCENDING TOO RAPIDLY BUT COULD NOT RECOVER IN TIME. (.4) ON NOVEMBER 25, 2001, ABOUT 1600 CENTRAL STANDARD TIME, A HUGHES OH-6A HELICOPTER, N129BC, REGISTERED TO, AND OPERATED BY THE DESOTO COUNTY SHERIFF'S OFFICE, AS TITLE 14 CFR PART 91 INSTRUCTIONAL FLIGHT, MADE A HARD LANDING AT A PRIVATE FIELD IN HERNANDO, MISSISSIPPI. VISUAL METEOROLOGICAL CONDITIONS PREVAILED, AND NO FLIGHT PLAN WAS FILED. THE STUDENT PILOT, AND THE AIRLINE TRANSPORT-RATED FLIGHT INSTRUCTOR WERE NOT INJURED, AND THE HELICOPTER INCURRED SUBSTANTIAL DAMAGE. THE FLIGHT ORIGINATED FROM HERNANDO, MISSISSIPPI, THE SAME DAY, ABOUT 1610. THE FLIGHT INSTRUCTOR STATED THAT THEY HAD BEEN PRACTICING AUTOROTATIONS AND DURING THE LAST AUTOROTATION THE STUDENT WAS FLYING THE HELICOPTER. THE INSTRUCTOR SAID THAT THE AIRSPEED ON FINAL WAS 70 KNOTS, AND THAT THE STUDENT FLARED THE HELICOPTER AT AN ALTITUDE OF ABOUT 65 FEET, AND APPLIED INITIAL COLLECTIVE PITCH CONTROL INPUT AT ABOUT 10 FEET, LEVELING THE HELICOPTER. HE SAID THAT THE HELICOPTER WAS ABOUT 2 FEET HIGH, AND STILL MOVING FORWARD, AND AT THAT POINT THE STUDENT DID NOT LET THE HELICOPTER SETTLE TO THE GROUND, BUT CONTINUED TO APPLY COLLECTIVE PITCH CONTROL INPUT. THE INSTRUCTOR SAID HE STOPPED THE STUDENT FROM APPLYING COLLECTIVE PITCH CONTROL INPUT, AND THE HELICOPTER STARTED TO DESCEND, BUT THE STUDENT APPLIED AFT CYCLIC CONTROL INPUT, AND THE HELICOPTER CONTACTED THE GROUND ON THE HEELS OF THE SKIDS, WHILE MAIN ROTOR RPMS WERE LOW. HE SAID THE MAIN ROTOR BLADES CONTACTED THE TAIL BOOM, SEVERING THE TAIL JUST FORWARD OF THE TAIL ROTOR GEAR BOX. ACCORDING TO THE FLIGHT INSTRUCTOR, PRIOR TO THE ACCIDENT, THERE WERE NO FAILURES OR MALFUNCTIONS TO THE HELICOPTER, OR ANY OF ITS SYSTEMS.

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 N129BC · 1

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