20001129024739A

Accident · Substantial damage

FAA accident report · Piper PA-32-260 · Florence, SC · November 29, 2000

Date
November 29, 2000 · 09:11 local
Place
Florence, SC
Airport
Florence Regional Airport
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
Air taxi and commuter (Part 135)
Operator
SX0A
Damage
Substantial damage
Aircraft
N6YB
NTSB investigation
NTSBATL01LA012
Reported as
Piper PA32260
Reported engine
Lycoming O540E4B5
People aboard
1
Fatal injuries
0
Pilot’s flight hours
3,400 total400 in this make and model300 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 November 29, 2000, at 0911 EST, a Piper cherokee six (PA-320-260), N6YB, registered to corporate air fleet, crashed at the Florence Regional Airport, Florence, SC. The a/c impacted the earth in a nearly level attitude. During the impact sequence, the landing gear was separated, and the propeller was bent. Visual meteorological conditions prevailed, and an instrument flight rules flight plan was filed for the business flight conducted under title 14 code of federal regulations part 135. The a/c was substantially damaged. The pilot was the sole occupant aboard and was not injured. (.4) on November 29, 2000, at 0907 eastern standard time, a Piper PA-32-260, N6YB, registered to and operated by corporate air fleet inc., was substantially damaged when it impacted the ground following a loss of engine power during initial climb following takeoff from Florence Regional Airport in Florence, south carolina. The commercial pilot, the sole occupant aboard, was not injured. Visual meteorological conditions prevailed, and an instrument flight rules flight plan was filed for the business flight being conducted under title 14 code of federal regulations part 135. The intended des tination was fayetteville regional/grannis airport in fayetteville, north carolina. The flight was originating at the time of the accident. According to the pilot, shortly after departure from runway 19, with a load of cargo on board, the engine lost power. The pilot executed a forced landing, impacting hard into a grassy area adjacent to the departure end of runway 19. During the impact sequence, the landing gear was separated and the propeller was bent. Examination of the engine showed no defects that would have prevented it from producing power. Conditions conductive to carburetor icing existed at the time of the accident. Temp was 48 degrees and the dewpoint was 39 degrees.

As the FAA filed it

(-23) ON NOVEMBER 29, 2000, AT 0911 EST, A PIPER CHEROKEE SIX (PA-320-260), N6YB, REGISTERED TO CORPORATE AIR FLEET, CRASHED AT THE FLORENCE REGIONAL AIRPORT, FLORENCE, SC. THE A/C IMPACTED THE EARTH IN A NEARLY LEVEL ATTITUDE. DURING THE IMPACT SEQUENCE, THE LANDING GEAR WAS SEPARATED, AND THE PROPELLER WAS BENT. VISUAL METEOROLOGICAL CONDITIONS PREVAILED, AND AN INSTRUMENT FLIGHT RULES FLIGHT PLAN WAS FILED FOR THE BUSINESS FLIGHT CONDUCTED UNDER TITLE 14 CODE OF FEDERAL REGULATIONS PART 135. THE A/C WAS SUBSTANTIALLY DAMAGED. THE PILOT WAS THE SOLE OCCUPANT ABOARD AND WAS NOT INJURED. (.4) ON NOVEMBER 29, 2000, AT 0907 EASTERN STANDARD TIME, A PIPER PA-32-260, N6YB, REGISTERED TO AND OPERATED BY CORPORATE AIR FLEET INC., WAS SUBSTANTIALLY DAMAGED WHEN IT IMPACTED THE GROUND FOLLOWING A LOSS OF ENGINE POWER DURING INITIAL CLIMB FOLLOWING TAKEOFF FROM FLORENCE REGIONAL AIRPORT IN FLORENCE, SOUTH CAROLINA. THE COMMERCIAL PILOT, THE SOLE OCCUPANT ABOARD, WAS NOT INJURED. VISUAL METEOROLOGICAL CONDITIONS PREVAILED, AND AN INSTRUMENT FLIGHT RULES FLIGHT PLAN WAS FILED FOR THE BUSINESS FLIGHT BEING CONDUCTED UNDER TITLE 14 CODE OF FEDERAL REGULATIONS PART 135. THE INTENDED DES TINATION WAS FAYETTEVILLE REGIONAL/GRANNIS AIRPORT IN FAYETTEVILLE, NORTH CAROLINA. THE FLIGHT WAS ORIGINATING AT THE TIME OF THE ACCIDENT. ACCORDING TO THE PILOT, SHORTLY AFTER DEPARTURE FROM RUNWAY 19, WITH A LOAD OF CARGO ON BOARD, THE ENGINE LOST POWER. THE PILOT EXECUTED A FORCED LANDING, IMPACTING HARD INTO A GRASSY AREA ADJACENT TO THE DEPARTURE END OF RUNWAY 19. DURING THE IMPACT SEQUENCE, THE LANDING GEAR WAS SEPARATED AND THE PROPELLER WAS BENT. EXAMINATION OF THE ENGINE SHOWED NO DEFECTS THAT WOULD HAVE PREVENTED IT FROM PRODUCING POWER. CONDITIONS CONDUCTIVE TO CARBURETOR ICING EXISTED AT THE TIME OF THE ACCIDENT. TEMP WAS 48 DEGREES AND THE DEWPOINT WAS 39 DEGREES.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.