# N912ME: 2007 Wilson Kenneth L PREDATOR - Status: Valid registration - Airframe: [Wilson Kenneth L PREDATOR](https://openairdocs.org/model/wilson-kenneth-l-predator) (registry code 05902YJ, 2 seats) - Engine: [Rotax 582DCDI](https://openairdocs.org/engine/rotax-582dcdi) (registry code 55562) - Serial number: W403 - Year built: 2007 - Type: Powered parachute - Engine type: 2 cycle - Airworthiness: Experimental, registered before 01/31/08 - Airworthiness date: September 22, 2007 - Certificate issued: October 2, 2024 - Expires: October 31, 2031 - Mode S code: AC9F31 - Registered owner: [Bruns Darcy L](https://openairdocs.org/faa-owner/BRUNS%20DARCY%20L) - Location: [Sandia, TX](https://openairdocs.org/faa-place/TX/Sandia) - Owner type: Individual - Owner's area on the map: 28.0728° N, 97.9441° W: Placed by OpenAirDocs at the center of ZIP code 78383, within about 7 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=912ME - Page: https://openairdocs.org/aircraft/N912ME From the FAA registry file of October 27, 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 (Wilson Kenneth L PREDATOR) None in force. ### Matched by engine (Rotax 582DCDI) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N912ME. ## FAA accident and incident reports None matched to N912ME. ## 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 N912ME not matched to an aircraft (12) They name N912ME, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR HALA2012022300071](https://openairdocs.org/sdr/HALA2012022300071), Feb 23, 2012: INVERTER. INOPERATIVE. EMERGENCY INVERTER INOPERATIVE. REPLACED EMERGENCY INVERTER IAW AMM 24-24-01. OPS CHECKED OK. - [SDR MWE2008F00030](https://openairdocs.org/sdr/MWE2008F00030), Aug 10, 2008: STATIC INVERTER. INOPERATIVE. DURING INITIAL POWER UP OF AC, WHEN SELECTING EMERGENCY POWER TO ARM "BUSS AC EMERGENCY OFF" COMES ON AND BATTERY STARTS DISCHARGE. REMOVED AND REPLACED STATIC - [SDR MWEA080058](https://openairdocs.org/sdr/MWEA080058), Apr 22, 2008: PIN. PULLED. FOUND FORWARD SERVICE DOOR ESCAPE SLIDE INFLATION CABLE PINS PULLED OUT OF SLIDE. REMOVED AND REPLACED SERVICE DOOR ESCAPE SLIDE. - [SDR MWEA070269](https://openairdocs.org/sdr/MWEA070269), Nov 1, 2007: ANGLE. CRACKED. FORWARD CHANNEL AT LEFT MAIN GEAR DOOR OPENING HAS A CRACK JUST AFT OF HYDRAULIC SERVICE DOOR. FABRICATED AND INSTALLED ANGLE. - [SDR MWEA070268](https://openairdocs.org/sdr/MWEA070268), Oct 30, 2007: LONGERON. CORRODED. LONGERON 30, BETWEEN STATION 920 AND 927 HAS THREE AREAS OF EXFOLIATION CORROSION. REMOVED AREAS OF CORROSION AND INSTALLED NESTED U-CHANNEL. - [SDR MWEA070224](https://openairdocs.org/sdr/MWEA070224), Sep 20, 2007: CHANNEL. CRACKED. UPPER OUTBOARD ZEE CHANNEL AT STATION 26 IS CRACKED ON RIGHT THRUST REVERSER. REMOVED DAMAGE, FABRICATED AND INSTALLED ANGLE. - [SDR MWEA060167](https://openairdocs.org/sdr/MWEA060167), Aug 1, 2006: BATTERY PACK. DISCHARGED. OVERWING EMERGENCY LIGHTS DO NOT COME ON. REPLACED OVERWING EMERGENCY EVACUATION BATTERY POWER. - [SDR MWEA070019](https://openairdocs.org/sdr/MWEA070019), Jan 31, 2006: BATTERY PACK. DISCHARGED. LEFT FORWARD EMERGENCY EXIT OVERWING LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. - [SDR MWEA05005](https://openairdocs.org/sdr/MWEA05005), Jan 4, 2005: BATTERY PACK. INOPERATIVE. LEFT AND RIGHT EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY POWER SUPPLY. - [SDR MWEA040225](https://openairdocs.org/sdr/MWEA040225), Dec 23, 2004: CLEVIS. BINDING. CREW NOTED BINDING IN THE ELEVATOR CONTROLS. FOUND MINOR CONTACT ON ELEVATOR STANDBY LOOP CLEVIS AND TENSION CLEVIS LINKS AT CABLE RUNS 5B AND 6B. PERFORMED ENG - [SDR MWEA040219](https://openairdocs.org/sdr/MWEA040219), Dec 9, 2004: LATCH. UNLATCHED. UPON ROTATION ACCESS COMPARTMENT DOOR ALERT ILLUMINATED. VERIFIED FORWARD ACCESSORY COMPARTMENT PROXIMITY TOO FAR FROM TARGET BECAUSE THE DOOR LATCH WAS OPEN, O - [SDR MWEA040181](https://openairdocs.org/sdr/MWEA040181), Oct 1, 2004: WIRE HARNESS. CHAFED. EMERGENCY LIGHTS CHARGING CIRCUIT BREAKER TRIPPED. FOUND WIRE BUNDLE CHAFING ON CORNER OF RIGHT LAVATORY OXYGEN PNEUMATIC SYSTEM CONTROLLER, REPAIRED THREE WIRE ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Wilson Kenneth L PREDATOR aircraft: https://openairdocs.org/model/wilson-kenneth-l-predator/aircraft.md - The Rotax 582DCDI engine: https://openairdocs.org/engine/rotax-582dcdi.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.