What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(.4) On September 3, 2001, at 1701 eastern daylight time, a Piper PA-22-160, N3516Z, owned and operated by an individual, operating as a title 14 CFR part 91 personal flight impacted the ground during a forced landing near the Spruce Creek Airport, Daytona Beach, Florida. Visual meteorological conditions prevailed. No flight plan was filed. The airplane was substantially damaged. The private-rated pilot and one passenger reported no injuries. The flight departed vandenberg airport, tampa, Florida, at 1600. The pilot stated that while on a "gradual descent" at an altitude of about 900 feet MSL, and in preparation for entry into the traffic pattern at the airport, "...the aircraft commenced an abrupt, uncommanded roll to the right." The pilot corrected the situation and regained level flight by applying "full left aileron and full left rudder," however the airplane remained in a "right wing" low attitude and "gradual right turn." The pilot stated that she realized that "directional control was compromised," and that due to the "high density" of housing in the area of the airport, she elected to attempt a forced landing in the "only" area that was clear of houses trees and cattle. After landing the airplane impacted an "overgrown" drainage ditch not visible from the air. According to the FAA inspector's statement, the pilot said the right wing suddenly dropped (lost lift), and the engine was at 2100 RPM. The landing was made in a cow pasture west of the airport. In addition, the passenger told the FAA inspector he turned off the ignition just prior to impact with the ground. The airplane came to rest in a "shallow" drainage ditch about 50 feet from initial touchdown. Examination of the airplane's fuel system revealed that the forward fuel filter bowl was slightly displaced from the top of the filter assembly. The fuel tanks were not breached, and the left fuel tank was full of fuel. A rubber hose had to be inserted into the lowest point of the right fuel tank in an attempt to recover fuel from the tank. No fuel was found in the right fuel tank. Examination of the fuel selector handle in the cockpit revealed that the fuel selector was positioned on the "right tank." About "1 ounce" of fuel was drained from the forward fuel filter, and about "1/3 of a pint" of fuel was drained from the aft fuel filter. Examination of the flight controls revealed that they "...operated normally and found to be in serviceable condition." Examination of the propeller revealed that one propeller blade was bent aft 30 degrees and scratched, the other blade was straight and clean. (-23) inspector's statement: the pilot said she was returning to Spruce Creek from vandenberg airport. While in straight and level flight, approximately two miles west of Spruce Creek Airport, the right wind suddenly dropped (lost lift). She said the engine was at 2100 RPM. She said she used all her strength to turn the control wheel full left and use full left rudder to maintain level flight. She said she thought about adjusting the nose trim but didn't dare take her hands off the control wheel. The pilot said she didn't want to risk landing at the airport because of the houses, so she elected to land in the cow pasture west of hwy 415. She said she pulled back the power and set the mixture to full rich. privacy data omitted The passenger said she lowered the flaps to fifteen degrees and he immediately told her to go back to zero to preserve airspeed. privacy data omitted Said he turned off the ignition just prior to impact with the ground. The aircraft came to rest in a s hallow drainage ditch approximately 50 feet from initial touchdown. The aircraft nose pointed wnw with the nose ten degrees down and left wing twenty degrees down in the shallow two-foot ditch. The nose and left main landing gear were broken off. Four feet of the left wing tip was bent upward resulting in damage to the spar. The bottom of the engine impacted the ground resulting in damage to the carburetor, engine mounts and forward fuel filter. One propeller blade was bent aft 30 degrees and scratched, the other was straight and clean. The forward fuel filter bowl was slightly displaced from the top of the filter assembly. The left fuel tank was full, a rubber hose was inserted into the lowest part of the right fuel tank and no fuel was detected. Examination of the interior revealed the ignition switch in the off position, the fuel selector on the right tank, flaps up, throttle back (idle), mixture forward (rich), and attitude indicator glass broken. The elevator trim indicator was two notches (seven total) from "dn". The compass read 17.5 degrees. The tachometer hour meter read 297.98 hrs. All gauges read zero. The aircraft was moved to a hangar at Spruce Creek Airport. The flight controls were inspected, operated normally and found to be in serviceable condition. Approximately one ounce of fuel was drained from the forward fuel filter. Approximately one third of a pint of fuel was drained from the aft fuel filter.
As the FAA filed it
(.4) ON SEPTEMBER 3, 2001, AT 1701 EASTERN DAYLIGHT TIME, A PIPER PA-22-160, N3516Z, OWNED AND OPERATED BY AN INDIVIDUAL, OPERATING AS A TITLE 14 CFR PART 91 PERSONAL FLIGHT IMPACTED THE GROUND DURING A FORCED LANDING NEAR THE SPRUCE CREEK AIRPORT, DAYTONA BEACH, FLORIDA. VISUAL METEOROLOGICAL CONDITIONS PREVAILED. NO FLIGHT PLAN WAS FILED. THE AIRPLANE WAS SUBSTANTIALLY DAMAGED. THE PRIVATE-RATED PILOT AND ONE PASSENGER REPORTED NO INJURIES. THE FLIGHT DEPARTED VANDENBERG AIRPORT, TAMPA, FLORIDA, AT 1600. THE PILOT STATED THAT WHILE ON A "GRADUAL DESCENT" AT AN ALTITUDE OF ABOUT 900 FEET MSL, AND IN PREPARATION FOR ENTRY INTO THE TRAFFIC PATTERN AT THE AIRPORT, "...THE AIRCRAFT COMMENCED AN ABRUPT, UNCOMMANDED ROLL TO THE RIGHT." THE PILOT CORRECTED THE SITUATION AND REGAINED LEVEL FLIGHT BY APPLYING "FULL LEFT AILERON AND FULL LEFT RUDDER," HOWEVER THE AIRPLANE REMAINED IN A "RIGHT WING" LOW ATTITUDE AND "GRADUAL RIGHT TURN." THE PILOT STATED THAT SHE REALIZED THAT "DIRECTIONAL CONTROL WAS COMPROMISED," AND THAT DUE TO THE "HIGH DENSITY" OF HOUSING IN THE AREA OF THE AIRPORT, SHE ELECTED TO ATTEMPT A FORCED LANDING IN THE "ONLY" AREA THAT WAS CLEAR OF HOUSES TREES AND CATTLE. AFTER LANDING THE AIRPLANE IMPACTED AN "OVERGROWN" DRAINAGE DITCH NOT VISIBLE FROM THE AIR. ACCORDING TO THE FAA INSPECTOR'S STATEMENT, THE PILOT SAID THE RIGHT WING SUDDENLY DROPPED (LOST LIFT), AND THE ENGINE WAS AT 2100 RPM. THE LANDING WAS MADE IN A COW PASTURE WEST OF THE AIRPORT. IN ADDITION, THE PASSENGER TOLD THE FAA INSPECTOR HE TURNED OFF THE IGNITION JUST PRIOR TO IMPACT WITH THE GROUND. THE AIRPLANE CAME TO REST IN A "SHALLOW" DRAINAGE DITCH ABOUT 50 FEET FROM INITIAL TOUCHDOWN. EXAMINATION OF THE AIRPLANE'S FUEL SYSTEM REVEALED THAT THE FORWARD FUEL FILTER BOWL WAS SLIGHTLY DISPLACED FROM THE TOP OF THE FILTER ASSEMBLY. THE FUEL TANKS WERE NOT BREACHED, AND THE LEFT FUEL TANK WAS FULL OF FUEL. A RUBBER HOSE HAD TO BE INSERTED INTO THE LOWEST POINT OF THE RIGHT FUEL TANK IN AN ATTEMPT TO RECOVER FUEL FROM THE TANK. NO FUEL WAS FOUND IN THE RIGHT FUEL TANK. EXAMINATION OF THE FUEL SELECTOR HANDLE IN THE COCKPIT REVEALED THAT THE FUEL SELECTOR WAS POSITIONED ON THE "RIGHT TANK." ABOUT "1 OUNCE" OF FUEL WAS DRAINED FROM THE FORWARD FUEL FILTER, AND ABOUT "1/3 OF A PINT" OF FUEL WAS DRAINED FROM THE AFT FUEL FILTER. EXAMINATION OF THE FLIGHT CONTROLS REVEALED THAT THEY "...OPERATED NORMALLY AND FOUND TO BE IN SERVICEABLE CONDITION." EXAMINATION OF THE PROPELLER REVEALED THAT ONE PROPELLER BLADE WAS BENT AFT 30 DEGREES AND SCRATCHED, THE OTHER BLADE WAS STRAIGHT AND CLEAN. (-23) INSPECTOR'S STATEMENT: THE PILOT SAID SHE WAS RETURNING TO SPRUCE CREEK FROM VANDENBERG AIRPORT. WHILE IN STRAIGHT AND LEVEL FLIGHT, APPROXIMATELY TWO MILES WEST OF SPRUCE CREEK AIRPORT, THE RIGHT WIND SUDDENLY DROPPED (LOST LIFT). SHE SAID THE ENGINE WAS AT 2100 RPM. SHE SAID SHE USED ALL HER STRENGTH TO TURN THE CONTROL WHEEL FULL LEFT AND USE FULL LEFT RUDDER TO MAINTAIN LEVEL FLIGHT. SHE SAID SHE THOUGHT ABOUT ADJUSTING THE NOSE TRIM BUT DIDN'T DARE TAKE HER HANDS OFF THE CONTROL WHEEL. THE PILOT SAID SHE DIDN'T WANT TO RISK LANDING AT THE AIRPORT BECAUSE OF THE HOUSES, SO SHE ELECTED TO LAND IN THE COW PASTURE WEST OF HWY 415. SHE SAID SHE PULLED BACK THE POWER AND SET THE MIXTURE TO FULL RICH. ^PRIVACY DATA^ THE PASSENGER SAID SHE LOWERED THE FLAPS TO FIFTEEN DEGREES AND HE IMMEDIATELY TOLD HER TO GO BACK TO ZERO TO PRESERVE AIRSPEED. ^PRIVACY DAT^ SAID HE TURNED OFF THE IGNITION JUST PRIOR TO IMPACT WITH THE GROUND. THE AIRCRAFT CAME TO REST IN A S HALLOW DRAINAGE DITCH APPROXIMATELY 50 FEET FROM INITIAL TOUCHDOWN. THE AIRCRAFT NOSE POINTED WNW WITH THE NOSE TEN DEGREES DOWN AND LEFT WING TWENTY DEGREES DOWN IN THE SHALLOW TWO-FOOT DITCH. THE NOSE AND LEFT MAIN LANDING GEAR WERE BROKEN OFF. FOUR FEET OF THE LEFT WING TIP WAS BENT UPWARD RESULTING IN DAMAGE TO THE SPAR. THE BOTTOM OF THE ENGINE IMPACTED THE GROUND RESULTING IN DAMAGE TO THE CARBURETOR, ENGINE MOUNTS AND FORWARD FUEL FILTER. ONE PROPELLER BLADE WAS BENT AFT 30 DEGREES AND SCRATCHED, THE OTHER WAS STRAIGHT AND CLEAN. THE FORWARD FUEL FILTER BOWL WAS SLIGHTLY DISPLACED FROM THE TOP OF THE FILTER ASSEMBLY. THE LEFT FUEL TANK WAS FULL, A RUBBER HOSE WAS INSERTED INTO THE LOWEST PART OF THE RIGHT FUEL TANK AND NO FUEL WAS DETECTED. EXAMINATION OF THE INTERIOR REVEALED THE IGNITION SWITCH IN THE OFF POSITION, THE FUEL SELECTOR ON THE RIGHT TANK, FLAPS UP, THROTTLE BACK (IDLE), MIXTURE FORWARD (RICH), AND ATTITUDE INDICATOR GLASS BROKEN. THE ELEVATOR TRIM INDICATOR WAS TWO NOTCHES (SEVEN TOTAL) FROM "DN". THE COMPASS READ 17.5 DEGREES. THE TACHOMETER HOUR METER READ 297.98 HRS. ALL GAUGES READ ZERO. THE AIRCRAFT WAS MOVED TO A HANGAR AT SPRUCE CREEK AIRPORT. THE FLIGHT CONTROLS WERE INSPECTED, OPERATED NORMALLY AND FOUND TO BE IN SERVICEABLE CONDITION. APPROXIMATELY ONE OUNCE OF FUEL WAS DRAINED FROM THE FORWARD FUEL FILTER. APPROXIMATELY ONE THIRD OF A PINT OF FUEL WAS DRAINED FROM THE AFT FUEL FILTER.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.