# Accident 20000712006879A: Piper PA38112, Selma, CA, July 12, 2000

- Type: FAA accident report (Accident/Incident Data System), as reported
- Date: July 12, 2000, 11:30 local time
- Place: Selma, CA
- Damage: Substantial damage
- Phase of flight: Forced/Precautionary Landing
- Operating rules: General operating rules (Part 91)
- Location: 36.5296° N, 119.6403° W: From the FAA, an estimate near the named town, within about 3 miles
- Nearby events: https://openairdocs.org/map.md?lat=36.5296&lon=-119.6403&mi=10
- Aircraft: N2466D, a cancelled registration (https://openairdocs.org/deregistered/N2466D-2012-06-28) (OpenAirDocs)
- Registry model: Piper PA-38-112 (registry code 7103812, https://openairdocs.org/model/piper-pa-38-112) (OpenAirDocs)
- Registry engine: Lycoming 0-235 series (registry code 41505, https://openairdocs.org/engine/lycoming-0-235-series) (OpenAirDocs)
- Reported make and model: PIPER PA38112
- Reported engine: LYC O235L2C
- People aboard: 2
- Fatal injuries: 0
- Pilot flight hours: 295 total, 224 in this make and model, 85 in the last 90 days
- NTSB investigation: [NTSB LAX00LA264](https://openairdocs.org/ntsb/LAX00LA264) (OpenAirDocs)
- FAA source: FAA Aviation Safety Information Portal (https://asip.faa.gov/)
- Page: https://openairdocs.org/incident/20000712006879A

## Narrative

As the FAA filed it, in capitals; the FAA replaces private details with ^PRIVACY DATA OMITTED^.

(-23) THE AIRCRAFT WAS IN THE AIRPORT TRAFFIC PATTERN ON DOWNWIND WHEN THE CFI CHANGED THE FUEL SELECTOR TO THE FULLEST TANK. THE AIRCRAFT COMPLETED A TOUCH AND GO LANDING.  APPROXIMATELY 1/4 MILE OFF THE DEPARTURE END OF RUNWAY 28, THERE WAS A COMPLETE LOSS OF ENGINE POWER AT AN ALTITUDE OF APPROXIMATELY 250 FEET AGL.  THE AIRCRAFT LANDED STRAIGHT AHEAD IN A GRAPE VINEYARD.  INVESTIGATION ON SCENE DETERMINED THAT THE FUEL SELECTOR HANDLE THAT IS MGF. FROM A PLASTIC TYPE MATERIAL WITH A BRASS INSERT HAD FAILED.  THE PLASTIC HAD CRACKED, ALLOWING THE INSERT THAT ATTCHES TO THE FUEL VALVE CONTROL ROD TO "SPIN" FREELY IN THE PLASTIC HANDLE.  THE FUEL VALVE BECAME PSOITIONED THE LEFT AND RIGHT TANK POSITION, THEREBY CLOSING OFF THE FUEL SUPPLY FROM BOTH TANKS.  THIS WAS NOT EVIDENT TO THE CFI THE HANDLE APPEARED TO  HAVE MOVED THE FUEL VALVE TO THE SELECTED TANK.                            (.4) ON JULY 12, 2000, AT 1130 HOURS PACIFIC DAYLIGHT TIME, A PIPER PA-38-112, N2466D, LOST ENGINE POWER WHILE CONDUCTING A GO-AROUND AFTER A SIMULATED ENGINE OUT PROCEDURE AT THE SELMA AIRPORT, SELMA, CALIFORNIA. THE AIRPLANE SUBSEQUENTLY TOUCHED DOWN IN A VINEYARD AND COLLIDED WITH GROUND OBSTRUCT IONS. THE AIRPLANE WAS OPERATED BY GOLDEN EAGLE ENTERPRISES, INC., D.B.A. MAZZEI FLYING SERVICE, UNDER 14 CFR PART 91 AS AN INSTRUCTIONAL FLIGHT. THE AIRPLANE SUSTAINED SUBSTANTIAL DAMAGE. THE CERTIFIED FLIGHT INSTRUCTOR (CFI) AND STUDENT PILOT WERE NOT INJURED. VISUAL METEOROLOGICAL CONDITIONS EXISTED FOR THE INSTRUCTIONAL FLIGHT, AND NO FLIGHT PLAN WAS FILED. THE FLIGHT WAS SCHEDULED TO TERMINATE AT THE FRESNO YOSEMITE INTERNATIONAL AIRPORT, FRESNO, CALIFORNIA. IN AN INTERVIEW WITH AN INVESTIGATOR FROM THE SAFETY BOARD, THE CFI STATED THAT THEY HAD BEEN PRACTICING SIMULATED ENGINE OUT PROCEDURES AT SELMA THAT CONCLUDED WITH THE STUDENT PILOT PERFORMING A TOUCH-AND-GO TAKEOFF. HE STATED THAT COMPANY PROCEDURE WAS TO SWITCH TO THE FULLEST TANK PRIOR TO TAKEOFF. HE FURTHER REPORTED THAT THE PROCESS FOR CONDUCTING THE ENGINE OUT MANEUVER WAS TO REDUCE THE THROTTLE, AND CONDUCT THE EMERGENCY CHECKLIST. NO DISCREPANCIES WERE NOTED WITH THE FIRST TWO ENGINE OUT MANEUVERS. ON THE THIRD ENGINE OUT, AT 1,700 FEET ABOVE GROUND LEVEL (AGL), THE CFI REDUCED THE THROTTLE, AND THE STUDENT DESCENDED TO THE RUNWAY. ON THE TAKEOFF, THE STUDENT PILOT SWITCHED THE FUEL SELECTOR HANDLE, AND THE ENGINE QUIT. THE CFI TOOK THE FLIGHT CONTROLS, RETRACTED THE FLAPS, SWITCHED THE FUEL SELECTOR HANDLE BACK TO ITS ORIGINAL POSITION, AND MADE AN UNSUCCESSFUL ATTEMPT TO RESTART THE ENGINE. THE CFI REPORTED THAT HE MADE AN OFF AIRPORT LANDING IN A VINEYARD AT THE DEPARTURE END OF THE RUNWAY. THE AIRPLANE WAS INSPECTED ON-SCENE BY A FEDERAL AVIATION ADMINISTRATION (FAA) INSPECTOR, AND AN FAA CERTIFIED AIRFRAME AND POWERPLANT MECHANIC. FUEL WAS FOUND IN BOTH TANKS; HOWEVER, THE FUEL SELECTOR HANDLE WAS FOUND IN THE "OFF" POSITION. THE CFI INFORMED THE INSPECTOR THAT HE HAD TURNED THE FUEL SELECTOR HANDLE TO THE "OFF" POSITION DURING THE EVACUATION. THE INSPECTOR AND MECHANIC ENGAGED THE MASTER SWITCH, AND THE ELECTRIC FUEL BOOST PUMP WAS PLACED IN THE "ON" POSITION. IT WAS NOTED THAT THE BOOST PUMP WAS WORKING, BUT THERE WAS NO FUEL PRESSURE OR FUEL PRESENT IN THE GASCOLATOR. THE FAA INSPECTOR AND MECHANIC CONDUCTED AN INSPECTION OF THE FUEL SELECTOR VALVE. THE VALVE POSITION WAS FOUND IN THE MIDDLE OF THE LEFT AND RIGHT PORT OPENINGS, AND THE FUEL VALVE CONTROL ROD WAS UNABLE TO BE TURNED MANUALLY. THE FUEL SELECTOR PLASTIC HANDLE WAS REMOVED AND FOUND CRACKED COMPLETELY THROUGH. THE INSPECTOR AND MECHANIC ALSO FOUND THAT THE BRASS INSERT HOUSED IN THE FUEL SELECTOR HANDLE THAT ATTACHES TO THE FUEL VALVE CONTROL ROD WAS "SLIPPING" IN THE PLASTIC HANDLE. THE INSPECTOR STATED THAT THE PILOTS WOULD NOT HAVE BEEN ABLE TO TELL THAT THE FUEL VALVE WAS IN AN INTERMEDIATE POSITION IN CORRELATION TO THE FUEL SELECTOR HANDLE POSITION INSIDE THE COCKPIT. HE FURTHER INDICATED THAT THERE WERE NO PREVIOUS SIGNS OF CRACKS IN THE PLASTIC FUEL SELECTOR HANDLE.

## The NTSB's investigation of this event (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB LAX00LA264](https://openairdocs.org/ntsb/LAX00LA264), Jul 12, 2000: Piper PA-38-112 (N2466D), Selma, CA, substantial damage. Probable cause: A cracked plastic fuel selector handle that precluded proper engagement of the internal mechanism to fully select a port, and left it in an intermediate position, restricting the fuel supply to the…

## Other reports on N2466D (2)

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

- [Accident 20111206027789A](https://openairdocs.org/incident/20111206027789A), Dec 6, 2011: Piper PA-38-112 (N2466D), Woodland, CA, Substantial damage. Aircraft accident preliminary notice narrative: lost engine power while on short final for runway 34 at the Yolo county airport (kdwa). Aircraft forced landed…
- [Incident 19960813026769I](https://openairdocs.org/incident/19960813026769I), Aug 13, 1996: Piper PA38112 (N2466D), Kansas City, MO, Minor damage. Narrative: 1. On 08/13/96 at 1545Z time, a Piper PA-38-112 aircraft (N2466D) departed Kansas City down town (mkc) airport, Missouri en route to return back to…

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft 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. For accidents, the NTSB's own investigation is the fuller record.

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