# N119DL: 2016 Case Grant SPORTSMAN GS-2 - Status: Valid registration - Airframe: [Case Grant SPORTSMAN GS-2](https://openairdocs.org/model/case-grant-sportsman-gs-2) (registry code 05634Y7, 4 seats) - Engine: [Amateur-built UNKNOWN ENG](https://openairdocs.org/engine/amateur-built-unknown-eng) (registry code 99999) - Serial number: 7436 - Year built: 2016 - Type: Fixed wing single engine - Engine type: Reciprocating - Kit: Glasair Aviation USA LLC SPORTSMAN GS-2 - Airworthiness: Experimental, amateur built - Airworthiness date: April 6, 2016 - Certificate issued: July 20, 2023 - Expires: July 31, 2030 - Mode S code: A04DF8 - Registered owner: [Sunset Air LLC](https://openairdocs.org/faa-owner/SUNSET%20AIR%20LLC) - Location: [Caledonia, MI](https://openairdocs.org/faa-place/MI/Caledonia) - Owner type: LLC - Owner's area on the map: 42.7938° N, 85.5505° W: Placed by OpenAirDocs at the center of ZIP code 49316, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=119DL - Page: https://openairdocs.org/aircraft/N119DL 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 (Case Grant SPORTSMAN GS-2) None in force. ### Matched by engine (Amateur-built UNKNOWN ENG) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N119DL. ## FAA accident and incident reports None matched to N119DL. ## Reports on N119DL not matched to an aircraft (5) They name N119DL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [Incident 19950903037069I](https://openairdocs.org/incident/19950903037069I), Sep 3, 1995: Boeing 767 (N119DL), Nassau, Bahamas. Encounted cat en route to jnu. Flight attendants and passengers injured. Diverted to Nassau. - [Incident 19910310015789I](https://openairdocs.org/incident/19910310015789I), Mar 10, 1991: Boeing 767332 (N119DL), West Palm Beach, FL. Smoke in galley on climb. Returned. Found NR3 galley oven fan circuit breaker popped. Oven deactivated. - [Incident 19900930063059I](https://openairdocs.org/incident/19900930063059I), Sep 30, 1990: Boeing 767332 (N119DL), Atlanta, GA, Minor damage. Panel from leading edge of wing departed over city. Discovered loss on arrival. - [Incident 19900621032759I](https://openairdocs.org/incident/19900621032759I), Jun 21, 1990: Boeing 767232 (N119DL), Ft Lauderdale, FL. Leading edge slat light on during descent. Declared emegency. Landed safely. Adjusted NR6 slat. - [Incident 19881124067629I](https://openairdocs.org/incident/19881124067629I), Nov 24, 1988: Boeing 767332 (N119DL), Boston, MA, Minor damage. While being marshalled to gate left wing contacted wingtip of a parked aircraft. Marshallers direction disregarded. ## 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 N119DL not matched to an aircraft (33) They name N119DL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DL76S050813](https://openairdocs.org/sdr/DL76S050813), Dec 20, 2005: BOWL. STRIPPED. LOST CENTER SYSTEM HYD. FOUND ADP FILTER MODULE BOWL STRIPPED OFF THE HOUSING. REPLACED MODULE. - [SDR DL76S041062](https://openairdocs.org/sdr/DL76S041062), Nov 25, 2004: CAP. CRACKED. CENTER HYDRAULIC SYSTEM DUMPED ALL FLUID WHILE MOVING FLAPS TO 15 DEGREES ON TAXI OUT SLC. FOUND CAP CRACKED AND SEPARATED FROM MODULE ON UPPER PART ABOVE HANDL - [SDR DL76S040425](https://openairdocs.org/sdr/DL76S040425), May 8, 2004: SKIN. CRACKED. THE LOWER AFT CORNER OF THE L1 DOOR CUTOUT WAS FOUND WITH A CRACK IN THE SKIN AND UNDERLYING BEARSTRAP AT FS 340. THE CRACK WAS REMOVED WITH A 4 X 5 INCHES CUTO - [SDR DL76S040408](https://openairdocs.org/sdr/DL76S040408), May 6, 2004: SKIN. CRACKED. CRACK REPAIR THE LOWER AFT CORNER OF THE L1 DOOR CUTOUT WAS FOUND WITH A CRACK IN THE SKIN AND UNDERLYING BEARSTRAP. THE CRACK WAS REMOVED WITH A 5 X 4 INCHES C - [SDR DL76S031113](https://openairdocs.org/sdr/DL76S031113), Dec 18, 2003: BULKHEAD. BIRD STRIKE. THE WEB OF THE FWD PRESSURE BULKHEAD AT FS 132.5 WAS PUNCTURED AS A RESULT OF A BIRD STRIKE BETWEEN LBL 10.6 & 16. THE VERTICAL BEAMS AT LBL 10.6 & 16 WERE DENT - [SDR DL76S030650](https://openairdocs.org/sdr/DL76S030650), Jul 12, 2003: SUPPORT BEAM. CORRODED. WING LT INBD FLAP OUTBD SUPPORT BEAM NR 3 SUPPORT : CORROSION IN AFT ATTACH HOLE BORES. THE AFT 4 ATTACH HOLES FOR THE OUTBD SUPPORT BEAM AT THE INBD FLAP ATTAC - [SDR DL76S030649](https://openairdocs.org/sdr/DL76S030649), Jul 12, 2003: SUPPORT BEAM. CORRODED. WING LT INBD FLAP OUTBD SUPPORT BEAM NR 3 SUPPORT : FWD FLAP ATTACH HOLE CORROSION, THE 2 FWD FLAP ATTACH HOLES ON THE OUTBD SUPPORT BEAM NR 3 SUPPORT FOR THE I - [SDR DL76S030648](https://openairdocs.org/sdr/DL76S030648), Jul 12, 2003: SUPPORT BEAM. CORRODED. WING / LT / INBD FLAP / INBD SUPPORT BEAM / SUPPORT NR 4 : FLAP ATTACH HOLE CORROSION THE LT INBD FLAP INBD SUPPORT BEAM WAS FOUND WITH CORROSION IN THE AFT INB - [SDR DL76S020671](https://openairdocs.org/sdr/DL76S020671), Jun 15, 2002: SMOKE. DETECTED. AFTER T/O SMOKE IN MID CABIN WITH SMOKE DETECTOR GOING OFF IN MID CABIN. RETURNED TO LAND. LT PACK TRIPPED AND LT ENG BLEED LIGHT ILLUMINATED. ON GROUND SMOKE D - [SDR DL76S020257](https://openairdocs.org/sdr/DL76S020257), Mar 4, 2002: BEAM. CRACKED. NR 5 LEADING EDGE SLAT NOSE BEAM WAS FOUND DAMAGED AT STA 439. REPAIR PER ER/A 402159-14. - [SDR DL76S020060](https://openairdocs.org/sdr/DL76S020060), Jan 18, 2002: SWITCH. MALFUNCTIONED. DURING THE BOARDING OF FLIGHT 706 FROM SEA/ATL CREW REPORTED SMOKE IN THE COCKPIT. CAUSE OF SMOKE WAS FOUND TO BE THE RT AFT FUEL PUMP SWITCH IN P5 PANEL. REPLA - [SDR DL76S020919](https://openairdocs.org/sdr/DL76S020919), Aug 7, 2001: LIGHT. INOPERATIVE. FOUND ON L/O CHECK, DOOR R1 EXT EMERGENCY SLIDE LIGHT INOP. REPLACED LIGHT ASSY, CHECK GOOD. - [SDR DL76S002047](https://openairdocs.org/sdr/DL76S002047), Oct 17, 2000: BOTTLE. DISCHARGED. ON LAYOVER FOUND RT WING OVERWING SLIDE BOTTLE PRESS LOW. REPLACED BOTTLE. - [SDR DL76S000211](https://openairdocs.org/sdr/DL76S000211), Jan 21, 2000: SKIN. CRACKED. SKIN CRACKED AT VHF ANTENNA CUTOUT AT STA 1197 + 99 AND BL 0. DAMAGE REMOVAL RESULTED IN A RECTANGULAR CUTOUT MEASURING 3 I/B-O/B BY 14 FWD/AFT. ER/A 334036-14 - [SDR DL76S992707](https://openairdocs.org/sdr/DL76S992707), Dec 10, 1999: MEGAPHONE. BROKEN. ON L/O, FOUND FWD CLOSET MEGAPHONE BROKEN. REPLACED MEGAPHONE. - [SDR DL76S991504](https://openairdocs.org/sdr/DL76S991504), Jul 3, 1999: OVEN. DIRTY. ACRID FUMES IN COCKPIT AND CABIN COULD NOT ISOLATE. POSSIBLY STRONGER IN FWD GALLEY AND FC AREA. INSPECTED E & E, ALL CARGO COMPARTMENTS, NOTHING FOUND. REMOVED - [SDR DL76S991075](https://openairdocs.org/sdr/DL76S991075), May 16, 1999: RETRACT MECH. MALFUNCTIONED. RT MAIN GEAR REMAINED EXTENDED AFTER T/O, ALT GEAR EXTENSION WORKED OK. MTC IN WORK ON GEAR RETRACTION AT TOC. NO NOTICEABLE DAMAGE TO GEAR. GEAR PINS INSTALLED - [SDR DL76S981272](https://openairdocs.org/sdr/DL76S981272), Jun 16, 1998: SKIN. DELAMINATED. UPPER SKINS ON THE TRAILING EDGE WEDGES OF THE NR 9, 10, AND 12 SLATS WERE FOUND WITH DELAMINATED AREAS. REPAIRED PER ERA 365048-14AD. - [SDR DL76S980069](https://openairdocs.org/sdr/DL76S980069), Jan 10, 1998: LIGHT. INOPERATIVE. FOUND ON LAYOVER, LT OVERWING EMERGENCY LIGHTS INOP. RELAMPED, CHECKS GOOD. - [SDR DL76S972328](https://openairdocs.org/sdr/DL76S972328), Nov 11, 1997: FLOORBEAM. CORROSION. CORROSION WAS FOUND ON THE UPPER CAP AT FS 1480 AT LBL 30 AND ENTIRE RT SIDE. REPAIRED PER ERA330975-14. - [SDR DL76S972327](https://openairdocs.org/sdr/DL76S972327), Nov 11, 1997: FLOORBEAM. PUNCTURED. A NEW UPPER TEE CHORD WAS ADDED TO THE BEAM EXTRUSION PER SRM. DURING ACCOMPLISHMENT THE FLOORBEAM WEB WAS PUNCTURED. REPAIRED PER ERA 330971-14. - [SDR DL76S972326](https://openairdocs.org/sdr/DL76S972326), Nov 11, 1997: SEAT TRACKS. CRACKED. SEAT TRACKS AT LBL AND RBL 54 WERE FOUND CRACKED IN THE VERTICAL WEB OF THE UPPER CHORD AT FS 786. REPAIRED PER ERA330946-14. - [SDR DL76S972325](https://openairdocs.org/sdr/DL76S972325), Nov 11, 1997: KEEL BEAM. CORRODED. LT KEEL BEAM HAD CORROSION AT STA 917. REPAIRED PER ERA 330983-14. - [SDR DL76S972324](https://openairdocs.org/sdr/DL76S972324), Nov 11, 1997: FLOORBEAM. CRACKED. FS 246 FLOORBEAM WEB WAS FOUND WITH VERT CRACK APPROX 3 LONG AT RBL 20. THE OVERLYING STIFFENER WAS ALSO CRACKED. REPAIRED PER ERA 330992-14. - [SDR DL76S972265](https://openairdocs.org/sdr/DL76S972265), Oct 26, 1997: FRAME. CRACKED. FORWARD CARGO COMPARTMENT STA 544 FRAME UPPER CHORD HAD AN 8 INCH CRACK IN THE RADIUS OF THE HORIZONTAL FLANGE AT RBL 16. REPLACED FLANGE. - [SDR DL76S970885](https://openairdocs.org/sdr/DL76S970885), May 8, 1997: WEDGE. DELAMINATED. THE NR 9 LEADING EDGE SLAT TRAILING EDGE WEDGE WAS FOUND TO HAVE THE UPPER SKIN DELAMINATED 4 FROM THE T/E AND 34 FROM THE INB'D END. THE DAMAGE AREA MEASURES 6 - [SDR DL76S970750](https://openairdocs.org/sdr/DL76S970750), Apr 24, 1997: SENSOR. OUT OF ADJUST. AFTER T/O OUT OF ATL, GEAR HANDLE FAILED TO COME UP. ACARS DID NOT SENSE AIRBOURN AND LATER GOT TAIL SKID LIGHT, RETURN TO ATL. SHIMMED TRUCK TILT SENSORS S245/ - [SDR DL76S970335](https://openairdocs.org/sdr/DL76S970335), Feb 24, 1997: IDG. REQD SERVICE. LOST LEFT ENG GEN AT ABOUT 200 FT AFTER T/O, LOST RT GEN AT APPROX 1,000 FT. RETURNED TO BOS. RT IDG BPCU FAULTS LOW OIL PRESS, IDG HI DELTA TEMP/IDG/PMG WIRING - [SDR DL76S962120](https://openairdocs.org/sdr/DL76S962120), Sep 16, 1996: HYD LINE. CHAFED. L HYD QTY EICAS MSG. LT ENG HYD QTY 0.46 RF. LT ENG PRIMARY AND DEMAND PUMPS OFF. REPLACED HYDRAULIC LINE AT #1 ENGINE HYDRAULIC PUMP. SYSTEM CHECKS NORMAL. - [SDR DL76S960772](https://openairdocs.org/sdr/DL76S960772), Apr 5, 1996: MEC. MALFUNCTIONED. TAKEOFF ABORTED AT 80 KTS, RT ENG ONLY 88 PERCENT, N1 ACC WAS ALSO SLOW. REPLACED RT ENG, MEC LEAK CHECKED PERFORMED, ENG RUN PER PFHB AND ALL IND NORMAL. - [SDR DL76S954306](https://openairdocs.org/sdr/DL76S954306), Nov 8, 1995: BULB. FAILED. DURING L/O, FOUND AFT RT DOOR EMERGENCY LIGHT INOP AND LT WING SLIDE LIGHT INOP. RELAMPED BOTH, CKS GOOD. - [SDR DL76S951720](https://openairdocs.org/sdr/DL76S951720), Apr 21, 1995: TRUNNION. FRACTURED. AFTER ARRIVAL AT GATE WHILE AIRCRAFT WAS MOTIONLESS, THE LEFT MAIN LANDING GEAR TRUNNION OUTER CYLINDER FRACTURED AT THE AFT TRUNNION BORE. THE LOWER 180 OF THE - [SDR DL76S950387](https://openairdocs.org/sdr/DL76S950387), Jan 26, 1995: WEDGE. DELAMINATION. FOUND DURING J-2 LETTER CHECK, DELAMINATION AREA ON LOWER SKIN OF NR 4 FLAP T/E WEDGE. REPAIRED PER SRM 51-70-07, AND PAINTED AREA. ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Case Grant SPORTSMAN GS-2 aircraft: https://openairdocs.org/model/case-grant-sportsman-gs-2/aircraft.md - The Amateur-built UNKNOWN ENG engine: https://openairdocs.org/engine/amateur-built-unknown-eng.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.