20001028018779I

Incident

FAA incident report · Amtr Kitfoxii · Corona, CA · October 28, 2000

Date
October 28, 2000 · 14:30 local
Place
Corona, CA
Airport
Corona Municipal Airport
Phase of flight
Final Approach
Operating rules
General operating rules (Part 91)
Aircraft
N164JR
Reported as
Amtr Kitfoxii
People aboard
1
Fatal injuries
0
Pilot’s flight hours
400 total4 in this make and model4 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 October 28, 2000, at approximately 1430 hours PDT, experimental aircraft Kitfox 2, N164JR, made a forced landing in an open field three miles southeast of the Corona, California, airport, as a result of the total loss of engine power. The airplane which was owned and operated by the pilot sustained no damage. The private pilot, the sole occupant, sustained no injuries. Visual meteorological conditions prevailed for the personal flight operating under 14 CFR part 91 of the federal aviation regulations. The flight originated from the Corona, California, airport and no flight plan was filed. The pilot reported that he departed Corona airport at approximately 1400 hours PDT and was in the process of flying off the initial 40 hour phase one certification requirement of his amateur built aircraft. He stated that at about 28 minutes into the flight at 3500 feet AGL he noticed minor engine RPM variations and then sudden engine stoppage. After making a successful forced landing in a open field the pilot/owner stated that he inspected the aircraft fuel system. This inspection revealed that the right fuel tank and header tank were empty and the left fuel tank still had approxi mately five gallons remaining. He said that prior to departing the Corona airport, he personally verified fuel tank levels by removing the fuel filler caps. He stated that while inspecting the fuel system he noticed that the left hand fuel tank fuller cap was installed backwards. He stated that the fuel filler caps have a vent tube vacing aft. He said this explained why the left hand fuel tank still had approximately five gallons of fuel and would not feed the header tank because the tank had a vacuum effect due to the vent tube right had fuel filler cap backwards after verifying fuel quantity. The pilot/owner stated that once the left hand fuel tank filler cap was properly installed the fuel system functioned normally, the engine started immediately and no further problems were experienced.

As the FAA filed it

(-23)ON OCTOBER 28, 2000, AT APPROXIMATELY 1430 HOURS PDT, EXPERIMENTAL AIRCRAFT KITFOX 2, N164JR, MADE A FORCED LANDING IN AN OPEN FIELD THREE MILES SOUTHEAST OF THE CORONA, CALIFORNIA, AIRPORT, AS A RESULT OF THE TOTAL LOSS OF ENGINE POWER. THE AIRPLANE WHICH WAS OWNED AND OPERATED BY THE PILOT SUSTAINED NO DAMAGE. THE PRIVATE PILOT, THE SOLE OCCUPANT, SUSTAINED NO INJURIES. VISUAL METEOROLOGICAL CONDITIONS PREVAILED FOR THE PERSONAL FLIGHT OPERATING UNDER 14 CFR PART 91 OF THE FEDERAL AVIATION REGULATIONS. THE FLIGHT ORIGINATED FROM THE CORONA, CALIFORNIA, AIRPORT AND NO FLIGHT PLAN WAS FILED. THE PILOT REPORTED THAT HE DEPARTED CORONA AIRPORT AT APPROXIMATELY 1400 HOURS PDT AND WAS IN THE PROCESS OF FLYING OFF THE INITIAL 40 HOUR PHASE ONE CERTIFICATION REQUIREMENT OF HIS AMATEUR BUILT AIRCRAFT. HE STATED THAT AT ABOUT 28 MINUTES INTO THE FLIGHT AT 3500 FEET AGL HE NOTICED MINOR ENGINE RPM VARIATIONS AND THEN SUDDEN ENGINE STOPPAGE. AFTER MAKING A SUCCESSFUL FORCED LANDING IN A OPEN FIELD THE PILOT/OWNER STATED THAT HE INSPECTED THE AIRCRAFT FUEL SYSTEM. THIS INSPECTION REVEALED THAT THE RIGHT FUEL TANK AND HEADER TANK WERE EMPTY AND THE LEFT FUEL TANK STILL HAD APPROXI MATELY FIVE GALLONS REMAINING. HE SAID THAT PRIOR TO DEPARTING THE CORONA AIRPORT, HE PERSONALLY VERIFIED FUEL TANK LEVELS BY REMOVING THE FUEL FILLER CAPS. HE STATED THAT WHILE INSPECTING THE FUEL SYSTEM HE NOTICED THAT THE LEFT HAND FUEL TANK FULLER CAP WAS INSTALLED BACKWARDS. HE STATED THAT THE FUEL FILLER CAPS HAVE A VENT TUBE VACING AFT. HE SAID THIS EXPLAINED WHY THE LEFT HAND FUEL TANK STILL HAD APPROXIMATELY FIVE GALLONS OF FUEL AND WOULD NOT FEED THE HEADER TANK BECAUSE THE TANK HAD A VACUUM EFFECT DUE TO THE VENT TUBE RIGHT HAD FUEL FILLER CAP BACKWARDS AFTER VERIFYING FUEL QUANTITY. THE PILOT/OWNER STATED THAT ONCE THE LEFT HAND FUEL TANK FILLER CAP WAS PROPERLY INSTALLED THE FUEL SYSTEM FUNCTIONED NORMALLY, THE ENGINE STARTED IMMEDIATELY AND NO FURTHER PROBLEMS WERE EXPERIENCED.

Other reports on N164JR · 1

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