19990925032309A

Accident · Substantial damage

FAA accident report · Beech C35BEECH · Lone Grove, OK · September 25, 1999

Date
September 25, 1999 · 16:30 local
Place
Lone Grove, OK
Phase of flight
Takeoff Ground Roll
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N5818C
NTSB investigation
NTSBFTW99LA266
Reported as
Beech C35BEECH
Reported engine
Continental E2258
People aboard
1
Fatal injuries
0
Pilot’s flight hours
240 total240 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.

(.19) On September 25, 1999, at 1719 central daylight time, a Beech C35 airplane, N5818C, owned and operated by the pilot, was substantially damaged during takeoff roll from a field near Lone Grove, Oklahoma. The private pilot was not injured, and his three passengers sustained minor injuries. Visual meteorological conditions prevailed, and a flight plan was not filed for the 14 code of federal regulations (CFR) part 91 personal cross-country flight. The flight originated from the mcgehee catfish restaurant airport, marietta, Oklahoma, at 1700, with the halliburton field airport near duncan, Oklahoma, as its intended destination. The pilot reported to the FAA inspector that during cruise flight, while en route to duncan, with the fuel selector positioned to the left fuel tank, the engine lost power. An attempt to select the right fuel tank and restart the engine was unsuccessful, and a successful forced landing to a field was accomplished. The pilot further reported that after selecting the right fuel tank and starting the engine, he attempted a short field takeoff. According to the FAA inspector, the pilot had attempted an uphill takeoff on a heading of 030 degrees with weeds approximately 18 inches tall. The airplane traveled uphill 165 yards through the weeds, struck a barbed wire fence, continued 70 yards and struck another fence. The airplane then traveled 35 yards to a ravine, crossed over the 45-foot wide ravine and continued for another 35 yards before coming to rest upright on a heading of 330 degrees. Examination of the airplane by the FAA inspector revealed that the left wing was structurally damaged, the fuselage was buckled just aft of the wings, and both propeller blades were damaged. The nose landing gear was folded aft, the right main landing gear was twisted outward, and the left main landing gear collapsed. An examination of the fuel system revealed that both wing fuel tanks were empty, and the fuel selector was found positioned on the right fuel tank. At 1650, 29 minutes prior to the accident, the wind at the ardmore municipal airport, located about 8 miles east of the accident site, was from 130 degrees at 10 knots. (-23)FTW99LA266 (.4)during cruise flight, with the fuel selector positioned to the left fuel tank, the engine lost power. An attempt to select the right fuel tank and restart the engine was unsuccessful, and a successful forced landing to a field was accomplished. After the pilot selected the right fuel tank and started the engine, he attempted a short field downwind takeoff uphill in 18-inch tall weeds; however, the airplane 'could not gain enough speed to keep flying.' The airplane traveled uphill 165 yards, struck a barbed wire fence, continued 70 yards and struck another fence. The airplane then traveled 35 yards to a ravine, crossed over the 45-foot wide ravine and continued for another 25 yards before coming to a stop upright. The pilot's takeoff heading was 030 degrees, and the wind was from 130 degrees at 10 knots.

As the FAA filed it

(.19) ON SEPTEMBER 25, 1999, AT 1719 CENTRAL DAYLIGHT TIME, A BEECH C35 AIRPLANE, N5818C, OWNED AND OPERATED BY THE PILOT, WAS SUBSTANTIALLY DAMAGED DURING TAKEOFF ROLL FROM A FIELD NEAR LONE GROVE, OKLAHOMA. THE PRIVATE PILOT WAS NOT INJURED, AND HIS THREE PASSENGERS SUSTAINED MINOR INJURIES. VISUAL METEOROLOGICAL CONDITIONS PREVAILED, AND A FLIGHT PLAN WAS NOT FILED FOR THE 14 CODE OF FEDERAL REGULATIONS (CFR) PART 91 PERSONAL CROSS-COUNTRY FLIGHT. THE FLIGHT ORIGINATED FROM THE MCGEHEE CATFISH RESTAURANT AIRPORT, MARIETTA, OKLAHOMA, AT 1700, WITH THE HALLIBURTON FIELD AIRPORT NEAR DUNCAN, OKLAHOMA, AS ITS INTENDED DESTINATION. THE PILOT REPORTED TO THE FAA INSPECTOR THAT DURING CRUISE FLIGHT, WHILE EN ROUTE TO DUNCAN, WITH THE FUEL SELECTOR POSITIONED TO THE LEFT FUEL TANK, THE ENGINE LOST POWER. AN ATTEMPT TO SELECT THE RIGHT FUEL TANK AND RESTART THE ENGINE WAS UNSUCCESSFUL, AND A SUCCESSFUL FORCED LANDING TO A FIELD WAS ACCOMPLISHED. THE PILOT FURTHER REPORTED THAT AFTER SELECTING THE RIGHT FUEL TANK AND STARTING THE ENGINE, HE ATTEMPTED A SHORT FIELD TAKEOFF. ACCORDING TO THE FAA INSPECTOR, THE PILOT HAD ATTEMPTED AN UPHILL TAKEOFF ON A HEADING OF 030 DEGREES WITH WEEDS APPROXIMATELY 18 INCHES TALL. THE AIRPLANE TRAVELED UPHILL 165 YARDS THROUGH THE WEEDS, STRUCK A BARBED WIRE FENCE, CONTINUED 70 YARDS AND STRUCK ANOTHER FENCE. THE AIRPLANE THEN TRAVELED 35 YARDS TO A RAVINE, CROSSED OVER THE 45-FOOT WIDE RAVINE AND CONTINUED FOR ANOTHER 35 YARDS BEFORE COMING TO REST UPRIGHT ON A HEADING OF 330 DEGREES. EXAMINATION OF THE AIRPLANE BY THE FAA INSPECTOR REVEALED THAT THE LEFT WING WAS STRUCTURALLY DAMAGED, THE FUSELAGE WAS BUCKLED JUST AFT OF THE WINGS, AND BOTH PROPELLER BLADES WERE DAMAGED. THE NOSE LANDING GEAR WAS FOLDED AFT, THE RIGHT MAIN LANDING GEAR WAS TWISTED OUTWARD, AND THE LEFT MAIN LANDING GEAR COLLAPSED. AN EXAMINATION OF THE FUEL SYSTEM REVEALED THAT BOTH WING FUEL TANKS WERE EMPTY, AND THE FUEL SELECTOR WAS FOUND POSITIONED ON THE RIGHT FUEL TANK. AT 1650, 29 MINUTES PRIOR TO THE ACCIDENT, THE WIND AT THE ARDMORE MUNICIPAL AIRPORT, LOCATED ABOUT 8 MILES EAST OF THE ACCIDENT SITE, WAS FROM 130 DEGREES AT 10 KNOTS. (-23)FTW99LA266 (.4)DURING CRUISE FLIGHT, WITH THE FUEL SELECTOR POSITIONED TO THE LEFT FUEL TANK, THE ENGINE LOST POWER. AN ATTEMPT TO SELECT THE RIGHT FUEL TANK AND RESTART THE ENGINE WAS UNSUCCESSFUL, AND A SUCCESSFUL FORCED LANDING TO A FIELD WAS ACCOMPLISHED. AFTER THE PILOT SELECTED THE RIGHT FUEL TANK AND STARTED THE ENGINE, HE ATTEMPTED A SHORT FIELD DOWNWIND TAKEOFF UPHILL IN 18-INCH TALL WEEDS; HOWEVER, THE AIRPLANE 'COULD NOT GAIN ENOUGH SPEED TO KEEP FLYING.' THE AIRPLANE TRAVELED UPHILL 165 YARDS, STRUCK A BARBED WIRE FENCE, CONTINUED 70 YARDS AND STRUCK ANOTHER FENCE. THE AIRPLANE THEN TRAVELED 35 YARDS TO A RAVINE, CROSSED OVER THE 45-FOOT WIDE RAVINE AND CONTINUED FOR ANOTHER 25 YARDS BEFORE COMING TO A STOP UPRIGHT. THE PILOT'S TAKEOFF HEADING WAS 030 DEGREES, AND THE WIND WAS FROM 130 DEGREES AT 10 KNOTS.

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 N5818C · 1

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