20021101030259A

Accident · Destroyed

FAA accident report · Hughes 269A · Fortgibson, OK · November 1, 2002

Date
November 1, 2002 · 11:50 local
Place
Fortgibson, OK
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N8885F
NTSB investigation
NTSBFTW03FA028
Reported as
Hughes 269A
People aboard
1
Fatal injuries
1

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.

(.19) On November 01, 2002, approximately 1150 central standard time, a Hughes 269A helicopter, N8885F, impacted the terrain following a loss of control during cruise flight near fort gibson, Oklahoma. The helicopter was owned and operated by tundra resources corporation of tulsa, Oklahoma. The private pilot, sole occupant, received fatal injuries, and the helicopter was destroyed during the impact sequence and post-crash fire. Visual meteorological conditions prevailed for the planned cross-country flight, and a flight plan was not filed. The 14 code of federal regulations part 91 flight originated from cookson, Oklahoma, at an unknown time, with a planned destination of tulsa, Oklahoma. One witness, who observed the helicopter flying to the west for about 8 seconds, reported a piece of the tail rotor separated. Subsequently, the helicopter pitched to the right, the main rotor separated, the helicopter started spinning, and descending toward the ground. A second witness reported that he heard a "pop." Subsequently, he observed the main rotor slowing, wobbling, stop turning, break away from the helicopter and travel forward of the helicopter. The helicopter pitched "nose forward and then fell almost vertical." This witness found one tail rotor blade, the left tailboom strut (GPS latitude 35 degrees 46.50 minutes north; 095 degrees 08.19 west), the right stabilator, and the main rotor (GPS latitude 35 degrees 47.00 minutes north; longitude 095 degrees 08.20 minutes west). Local authorities and the NTSB investigation team, who responded to the accident site, found the helicopter (GPS latitude 35 degrees 46.59 minutes north; longitude 095 degrees 08.19 minutes west) in an inverted attitude at the base of a tree in the wooded wildlife management area. (-23) investigation, by inspectors of the Oklahoma city flight standards district office, shows that on 11/01/02 at approximately 11:50 CST, Mr. Fred I. Barrs was piloting a Hughes 269A, N8885F from cookson, OK to tulsa r.l. jones airport (rvs). Mr. Barrs lost control of the helicopter and impacted terrain approximately 6.5 miles southeast of of fort gibson, OK. Evidence from the accident scene shows that an in-flight break up occurred. Components of the aircraft have been gathered and will be analyzed to determine the cause of the break up.

As the FAA filed it

(.19) ON NOVEMBER 01, 2002, APPROXIMATELY 1150 CENTRAL STANDARD TIME, A HUGHES 269A HELICOPTER, N8885F, IMPACTED THE TERRAIN FOLLOWING A LOSS OF CONTROL DURING CRUISE FLIGHT NEAR FORT GIBSON, OKLAHOMA. THE HELICOPTER WAS OWNED AND OPERATED BY TUNDRA RESOURCES CORPORATION OF TULSA, OKLAHOMA. THE PRIVATE PILOT, SOLE OCCUPANT, RECEIVED FATAL INJURIES, AND THE HELICOPTER WAS DESTROYED DURING THE IMPACT SEQUENCE AND POST-CRASH FIRE. VISUAL METEOROLOGICAL CONDITIONS PREVAILED FOR THE PLANNED CROSS-COUNTRY FLIGHT, AND A FLIGHT PLAN WAS NOT FILED. THE 14 CODE OF FEDERAL REGULATIONS PART 91 FLIGHT ORIGINATED FROM COOKSON, OKLAHOMA, AT AN UNKNOWN TIME, WITH A PLANNED DESTINATION OF TULSA, OKLAHOMA. ONE WITNESS, WHO OBSERVED THE HELICOPTER FLYING TO THE WEST FOR ABOUT 8 SECONDS, REPORTED A PIECE OF THE TAIL ROTOR SEPARATED. SUBSEQUENTLY, THE HELICOPTER PITCHED TO THE RIGHT, THE MAIN ROTOR SEPARATED, THE HELICOPTER STARTED SPINNING, AND DESCENDING TOWARD THE GROUND. A SECOND WITNESS REPORTED THAT HE HEARD A "POP." SUBSEQUENTLY, HE OBSERVED THE MAIN ROTOR SLOWING, WOBBLING, STOP TURNING, BREAK AWAY FROM THE HELICOPTER AND TRAVEL FORWARD OF THE HELICOPTER. THE HELICOPTER PITCHED "NOSE FORWARD AND THEN FELL ALMOST VERTICAL." THIS WITNESS FOUND ONE TAIL ROTOR BLADE, THE LEFT TAILBOOM STRUT (GPS LATITUDE 35 DEGREES 46.50 MINUTES NORTH; 095 DEGREES 08.19 WEST), THE RIGHT STABILATOR, AND THE MAIN ROTOR (GPS LATITUDE 35 DEGREES 47.00 MINUTES NORTH; LONGITUDE 095 DEGREES 08.20 MINUTES WEST). LOCAL AUTHORITIES AND THE NTSB INVESTIGATION TEAM, WHO RESPONDED TO THE ACCIDENT SITE, FOUND THE HELICOPTER (GPS LATITUDE 35 DEGREES 46.59 MINUTES NORTH; LONGITUDE 095 DEGREES 08.19 MINUTES WEST) IN AN INVERTED ATTITUDE AT THE BASE OF A TREE IN THE WOODED WILDLIFE MANAGEMENT AREA. (-23) INVESTIGATION, BY INSPECTORS OF THE OKLAHOMA CITY FLIGHT STANDARDS DISTRICT OFFICE, SHOWS THAT ON 11/01/02 AT APPROXIMATELY 11:50 CST, MR. FRED I. BARRS WAS PILOTING A HUGHES 269A, N8885F FROM COOKSON, OK TO TULSA R.L. JONES AIRPORT (RVS). MR. BARRS LOST CONTROL OF THE HELICOPTER AND IMPACTED TERRAIN APPROXIMATELY 6.5 MILES SOUTHEAST OF OF FORT GIBSON, OK. EVIDENCE FROM THE ACCIDENT SCENE SHOWS THAT AN IN-FLIGHT BREAK UP OCCURRED. COMPONENTS OF THE AIRCRAFT HAVE BEEN GATHERED AND WILL BE ANALYZED TO DETERMINE THE CAUSE OF THE BREAK UP.

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 N8885F · 2

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