# N115US: 2009 Czech Sport Aircraft A S SPORTCRUISER - Status: Valid registration - Airframe: [Czech Sport Aircraft A S SPORTCRUISER](https://openairdocs.org/model/czech-sport-aircraft-a-s-sportcruiser) (registry code 0600066, 2 seats) - Engine: [Rotax 912ULS series](https://openairdocs.org/engine/rotax-912uls-series) (registry code 55572) - Serial number: 09SC288 - Year built: 2009 - Type: Fixed wing single engine - Engine type: 4 cycle - Airworthiness: Experimental, operating light-sport, previously under 21.190 - Airworthiness date: April 17, 2019 - Certificate issued: November 2, 2024 - Expires: November 30, 2031 - Mode S code: A04099 - Registered owner: [Adamez Benny Barrera Jr](https://openairdocs.org/faa-owner/ADAMEZ%20BENNY%20BARRERA%20JR) - Location: [Fort Worth, TX](https://openairdocs.org/faa-place/TX/Fort%20Worth) - Owner type: Individual - Owner's area on the map: 32.6490° N, 97.5147° W: Placed by OpenAirDocs at the center of ZIP code 76126, 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=115US - Page: https://openairdocs.org/aircraft/N115US 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. The registry lists only the engine series, so ADs for every Rotax 912ULS model are included. ## ADs that may apply (OpenAirDocs): 0 in force ### Matched by airframe (Czech Sport Aircraft A S SPORTCRUISER) None in force. ### Matched by engine (Rotax 912ULS series) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N115US. ## FAA accident and incident reports None matched to N115US. ## Reports on N115US not matched to an aircraft (1) They name N115US, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [Incident 19790210200189I](https://openairdocs.org/incident/19790210200189I), Feb 10, 1979: Doug DC10/ (N115US), Boston, MA. Aborted takeoff due to reverser light coming on. ## 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 N115US not matched to an aircraft (9) They name N115US, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR USAA200509007](https://openairdocs.org/sdr/USAA200509007), Sep 24, 2005: SPLICE. CORRODED. LEFT AFT ENTRY DOOR THRESHOLD CORRODED .75 X 3 X .070 INCH DEEP AT UPPER SPLICE ANGLE STATION FR 67. NO CORROSION LEVEL OR TASK. REMOVED UPPER SPLICE ANGLE, FAB - [SDR USAA200509008](https://openairdocs.org/sdr/USAA200509008), Sep 24, 2005: FLOORBEAM. CORRODED. FLOORBEAM CORRODED .5 X 7 INCH AT Y1292 BETWEEN FR 64 & FR 66. NO CORROSION LEVEL OR TASK. REMOVED CORRODED SECTION AND SPLICED IN A NEW BEAM SECTION PER SRM 51 - [SDR USAA200509006](https://openairdocs.org/sdr/USAA200509006), Sep 23, 2005: FLOORBEAM. CORRODED. FLOORBEAM AND R2 DOOR SILL CORRODED .20 X .5 X .60 INCH AT FR 67, STR 18. NO CORROSION LEVEL OR TASK. BLENDED AND TREATED CORROSION; FABRICATED AND INSTALLED RE - [SDR USAA200509005](https://openairdocs.org/sdr/USAA200509005), Sep 20, 2005: FLOORBEAM. CORRODED. 3" BY 3" CORRODED AREA AT LT CABIN FLOORBEAM Y1292 AT FS 66. REPLACED FLOORBEAM PER SRM 51-72-11. - [SDR USAA200509004](https://openairdocs.org/sdr/USAA200509004), Sep 20, 2005: FLOOR SUPPORT. CORRODED. TWO EACH 1" BY 1" CORRODED AREAS AT RT -Y1292 FLOOR SUPPORT AT FS 68 AND 10" FWD OF FS 67. REPLACED FLOOR SUPPORT PER SRM 51-72-11. - [SDR USAA200509003](https://openairdocs.org/sdr/USAA200509003), Sep 20, 2005: FLOORBEAM. CORRODED. 1 INCH BY 1 INCH CORROSION AT -Y1292 FLOORBEAM AT FS 66. REPLACED FLOORBEAM PER SRM 51-72-11. - [SDR USA2005F00001](https://openairdocs.org/sdr/USA2005F00001), Aug 1, 2005: PLACARD. LOOSE. AFTER TAKEOFF, THE NR 1 ENGINE FUEL FILTER CLOG MESSAGE ILLUMINATED ON ECAM. ENGINE FUEL FILTER SHOWED EVIDENCE OF PLACARD/LABEL MATERIAL. AIRCRAFT WAS MAINTENA - [SDR USAASA04063](https://openairdocs.org/sdr/USAASA04063), Jun 3, 2004: LANYARD. MISROUTED. PHL - FOUND DURING AN INSPECTION OF THE GIRT BAR LANYARD ROUTING, THE FORWARD LEFT ESCAPE SLIDE ELECTRICAL HARNESS, AND THE REAR RIGHT, ESCAPE LSIDE SURVIVAL KI - [SDR USAASA04031](https://openairdocs.org/sdr/USAASA04031), Mar 31, 2004: PUSH-PULL CABLE. BROKEN. THE LEFT OVERWING SLIDE CYLINDER HAS A BROKEN PUSH/PULL CABLE. MAINTENANCE REPLACED THE LEFT OVERWING SLIDE CYLINDER ASSEMBLY. OK FOR SERVICE. (M) ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Czech Sport Aircraft A S SPORTCRUISER aircraft: https://openairdocs.org/model/czech-sport-aircraft-a-s-sportcruiser/aircraft.md - The Rotax 912ULS series engine: https://openairdocs.org/engine/rotax-912uls-series.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.