# N2758N: 2005 Phoenix X-TREME

- Status: Valid registration
- Airframe: [Phoenix X-TREME](https://openairdocs.org/model/phoenix-x-treme) (registry code 05903Q1, 2 seats)
- Engine: [Rotax 582SER](https://openairdocs.org/engine/rotax-582ser) (registry code 55556)
- Serial number: 0524
- Year built: 2005
- Type: Powered parachute
- Engine type: 2 cycle
- Airworthiness: Experimental, registered before 01/31/08
- Airworthiness date: September 27, 2007
- Certificate issued: August 29, 2007
- Expires: March 31, 2028
- Mode S code: A2BC8C
- Registered owner: [Lowe Jerry W](https://openairdocs.org/faa-owner/LOWE%20JERRY%20W)
- Location: [Danville, VA](https://openairdocs.org/faa-place/VA/Danville)
- Owner type: Individual
- Owner's area on the map: 36.5895° N, 79.5155° W: Placed by OpenAirDocs at the center of ZIP code 24541, within about 5 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=2758N
- Page: https://openairdocs.org/aircraft/N2758N

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 0 in force

### Matched by airframe (Phoenix X-TREME)

None in force.

### Matched by engine (Rotax 582SER)

None in force.

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N2758N.

## FAA accident and incident reports

None matched to N2758N.

## Service difficulty reports

None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

## Service difficulty reports on N2758N not matched to an aircraft (27)

They name N2758N, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR HEEA063219](https://openairdocs.org/sdr/HEEA063219), Aug 9, 1999: VOLT REGULATOR. FAILED. GENERATOR WILL NOT COME ON-LINE.
- [SDR HEEA063216](https://openairdocs.org/sdr/HEEA063216), Aug 9, 1999: INDICATOR. INOPERATIVE. TOT INDICATOR INOPERATIVE.
- [SDR HEEA061586](https://openairdocs.org/sdr/HEEA061586), Apr 2, 1999: INDICATOR. INOPERATIVE. INDICATOR'S PRESSURE NEEDLE INOPERATIVE.
- [SDR HEEA061584](https://openairdocs.org/sdr/HEEA061584), Apr 2, 1999: VOLT REGULATOR. MALFUNCTIONED. AMMETER SPIKES WHEN RADIO MIKE KEYED ON VOLTAGE REGULATOR.
- [SDR HEEA060817](https://openairdocs.org/sdr/HEEA060817), Feb 22, 1999: INDICATOR. READS LOW. FUEL QUANTITY INDICATOR HAS A CRACKED GLASS AND READS LOW AT 400 POUNDS AND ABOVE.
- [SDR HEEA060665](https://openairdocs.org/sdr/HEEA060665), Feb 16, 1999: FITTING. WRONG PART. WRONG TYPE FITTING INSTALLED ON HOSE ASSEMBLY.
- [SDR HEEA060212](https://openairdocs.org/sdr/HEEA060212), Jan 22, 1999: SKIN. DENTED. FIN ASSEMBLY HAS HOLE IN LEADING EDGE, DENTED, AND SEPARATED.
- [SDR HEEA0015912](https://openairdocs.org/sdr/HEEA0015912), Aug 28, 1998: INDICATOR. READS HIGH. TOT INDICATOR READS 10 PERCENT HIGH ABOVE 500 AFTER UNIT IS WARM.
- [SDR HEEA0015911](https://openairdocs.org/sdr/HEEA0015911), Aug 28, 1998: INDICATOR. MALFUNCTIONED. TOT NEEDLE STICKS ON START-UP.
- [SDR HEEA0015750](https://openairdocs.org/sdr/HEEA0015750), Aug 25, 1998: IMPELLER. CORRODED. BLOWER IMPELLER EXCESSIVELY CORRODED. SCRAPPED ASSY AND REPLACED WITH NEW ASSY.
- [SDR HEEA0015742](https://openairdocs.org/sdr/HEEA0015742), Aug 25, 1998: PANEL. MISMANUFACTURED. PANEL ASSEMBLY MISMANUFACTURED. PANEL WAS TRIMMED .1250 INCH TOO SMALL, COULD NOT GET GOOD EDGE DISTANCE FOR SCREW HOLES.
- [SDR HEEA0015721](https://openairdocs.org/sdr/HEEA0015721), Aug 20, 1998: DOOR. CORRODED. DOOR ASSEMBLY CORRODED AND SEPARATED BEYOND REPAIR AT THIS STATION.
- [SDR HEEA0015540](https://openairdocs.org/sdr/HEEA0015540), Aug 13, 1998: BELLCRANK. CHAFED. BELLCRANK CHAFED BEYOND LIMITS. SCRAPPED BELLCRANK AND REPLACED WITH SERVICEABLE PART.
- [SDR HEEA0015539](https://openairdocs.org/sdr/HEEA0015539), Aug 13, 1998: SUPPORT. CORRODED. SUPPORT HAS CORROSION AND PITTED BEYOND LIMITS. REPLACED WITH SERVICEABLE SUPPORT.
- [SDR HEEA0015538](https://openairdocs.org/sdr/HEEA0015538), Aug 13, 1998: CROSSTUBE. CORRODED. CORROSION AND PITTING DAMAGE AT SKID TUBE MOUNTING POINT EXCEEDING LIMITS. SCRAPPED CROSSTUBE.
- [SDR HEEA0015537](https://openairdocs.org/sdr/HEEA0015537), Aug 13, 1998: DISC SET. CORRODED. DISC CORRODED AND PITTED. REPLACED WITH SERVICEABLE PARTS.
- [SDR HEEA0015397](https://openairdocs.org/sdr/HEEA0015397), Jul 29, 1998: INDICATOR. CRACKED. TOT INDICATOR INTERMITTENT AND GLASS FACE CRACKED.
- [SDR HEEA0015394](https://openairdocs.org/sdr/HEEA0015394), Jul 29, 1998: INDICATOR. INTERMITTENT. TOT INDICATOR INTERMITTENT.
- [SDR HEEA0015241](https://openairdocs.org/sdr/HEEA0015241), Jul 27, 1998: COOLER. FAILED. INSTALLED OIL COOLER FROM STOCK AND RAN AIRCRAFT. ENGINE OIL TEMP WAS HIGH.
- [SDR HEEA0013778](https://openairdocs.org/sdr/HEEA0013778), Apr 2, 1998: ACTUATOR. FAILED. ACTUATOR INOPERATIVE.
- [SDR HEEA0012223](https://openairdocs.org/sdr/HEEA0012223), Dec 3, 1997: TRANS RESTRAINT. WORN. WORN BEARINGS AND UNSTAKED.
- [SDR HEEA0011895](https://openairdocs.org/sdr/HEEA0011895), Nov 10, 1997: INDICATOR. FAILED. INDICATOR WAS REMOVED FROM BOWL AND CLEANED. INSTALLED INDICATOR BACK ON BOWL, TESTED AND INDICATOR STILL DID NOT WORK. SCRAPPED INDICATOR AND REPLACED WITH SER
- [SDR HEEA0011190](https://openairdocs.org/sdr/HEEA0011190), Oct 2, 1997: ELT. MALFUNCTION. ELT STAYS ON AND WILL NOT SHUT OFF.
- [SDR HEEA0010483](https://openairdocs.org/sdr/HEEA0010483), Jul 16, 1997: NOZZLE. CRACKED. ENGINE REMOVED DUE TO HIGH T.O.T. UPON INSPECTION OF TURBINE PARTS NOTED: CRACKED BEYOND SERVICEABLE LIMITS ON #2 NOZZLE FWD INNER BAND, AFT INNER BAND WELDMENT
- [SDR HEEA979136](https://openairdocs.org/sdr/HEEA979136), Feb 21, 1997: SHROUD HOUSING. OVER SPECS. RECEIVING INSPECTION REVEALED: MEASURED .005 TO .007 OVER SPECS (10.199 - 10.200) ON SHROUD HOUSING AFT PILOT. INSTALLED A DALLAS AIRMOTIVE OVERHAULED SHROUD HO
- [SDR HEEA955791](https://openairdocs.org/sdr/HEEA955791), Sep 21, 1995: BATTERY. WEAK. BATTERY HOT LIGHT. INSPECTED BY ACCESSORY SHOP: VOLTAGE READING TAKEN AS RECEIVED. FOUND BATTERY WEAK.
- [SDR HEEA955072](https://openairdocs.org/sdr/HEEA955072), May 24, 1995: WHEEL. SULFIDATION. ENGINE REMOVED DUE TO TURBINE OVERHAUL. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: SULFIDATION ON ALL 1ST STAGE WHEEL BLADES. SCRAPPED 1ST STAGE WHEE

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Earlier aircraft with N2758N

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N2758N before.

- [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N2758N-undated): Cessna 120, S/N 13016, built 1947

## Related

- Other Phoenix X-TREME aircraft: https://openairdocs.org/model/phoenix-x-treme/aircraft.md
- The Rotax 582SER engine: https://openairdocs.org/engine/rotax-582ser.md

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