# N815SY: 2002 Boeing 737-8BK, registration cancelled 2026-01-19

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 19, 2026
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-8BK](https://openairdocs.org/model/boeing-737-8bk) (registry code 13844FG)
- Engine: [CFM International CFM56-7B24 series](https://openairdocs.org/engine/cfm-international-cfm56-7b24-series) (registry code 13044)
- Serial number: 30623
- Year built: 2002
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 21, 2011
- Certificate issued: May 8, 2024
- Last registry action: May 8, 2024
- Mode S code: AB1D96
- Owners when cancelled: [Sun Country Inc DBA](https://openairdocs.org/faa-owner/SUN%20COUNTRY%20INC%20DBA), [Sun Country Airlines](https://openairdocs.org/faa-owner/SUN%20COUNTRY%20AIRLINES)
- Location: [Minneapolis, MN](https://openairdocs.org/faa-place/MN/Minneapolis)
- Owner type: Corporation
- Owner's area on the map: 44.8723° N, 93.2328° W: Placed by OpenAirDocs at the center of ZIP code 55450, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N815SY
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=815SY
- Page: https://openairdocs.org/deregistered/N815SY-2026-01-19

From the FAA registry file of November 3, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Boeing 737-8BK: https://openairdocs.org/model/boeing-737-8bk.md

## Service difficulty reports (183, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR SCNA20250408106](https://openairdocs.org/sdr/SCNA20250408106), Apr 7, 2025: SIGHT GLASS. CRACKED. DEFECT 730825: DOOR 1R SLIDE WINDOW CRACKED. R&R R1 DOOR SLIDE WINDOW IAW AMM 25-66-01 THIS CLEARS MEL.
- [SDR SCNA20241230408](https://openairdocs.org/sdr/SCNA20241230408), Dec 24, 2024: FLAP SYSTEM. STUCK. DEFECT 794276: FLAPS STUCK AT 5 ON APPROACH RAN QRH AND USED ALTERNATE FLAPS. RESOLUTION: PERFORMED FSEU BITE CHECK REF AMM 27-51-00 NO FAULTS NOTED, INSPECTED 
- [SDR SCN2024F00003](https://openairdocs.org/sdr/SCN2024F00003), Dec 24, 2024: FLAP SYSTEM. STUCK. DEFECT 794276: FLAPS STUCK AT 5 ON APPROACH RAN QRH AND USED ALTERNATE FLAPS. RESOLUTION: PERFORMED FSEU BITE CHECK REF AMM 27-51-00 NO FAULTS NOTED, INSPECTED 
- [SDR SCNA20241209395](https://openairdocs.org/sdr/SCNA20241209395), Dec 7, 2024: GIRT BAR. ABNORMAL. DEFECT 781145: 1L GIRT BAR SLID OUT OF HOLDER ON THE LEFT SIDE AS THE DOOR WAS OPENED. RESOLUTION: VERIFIED INSTALLATION OF L1 GIRTBAR REF AMM 25-66-01. NO DEFE
- [SDR SCNA20240807292](https://openairdocs.org/sdr/SCNA20240807292), Aug 5, 2024: WEB. CRACKED. DURING SCHEDULED MAINTENANCE, TWO CRACKS WERE FOUND ON THE WEB AT THE FORWARD INBOARD CORNER OF THE LEFT MAIN LANDING GEAR CENTER DOOR (P/N 113A8232-1), SEE FIG
- [SDR SCNA20240708267](https://openairdocs.org/sdr/SCNA20240708267), Jul 7, 2024: LAMP. INOPERATIVE. EMERGENCY AREA LIGHT OUT AT 25 DEF. RELAMPED EMERGENCY AREA LIGHT AT 25 DEF IAW AMM 33-51-03-960-801. OPS CHECK GOOD.
- [SDR SCNA20240429221](https://openairdocs.org/sdr/SCNA20240429221), Apr 25, 2024: BRACKET. LOOSE. 2L GIRT BAR BRACKETS ARE VERY LOOSE. ADJUSTED GIRT BAR STOWAGE CLIPS REF AMM 25-66-00 OK FOR SERVICE
- [SDR SCNA20240312155](https://openairdocs.org/sdr/SCNA20240312155), Mar 10, 2024: WINDOW. CRACKED. AT FL 360 L1 WINDOW MADE LOUD POP AND APPROX 27 SPIDER WEB CRACKS PROPOGATED, ASSOCIATED WINDOW OVERHEAT SIMULTANEOUSLY ILLUMINATED. REMOVED L1 WINDOW IAW AMM 5
- [SDR SCNA20240206027](https://openairdocs.org/sdr/SCNA20240206027), Feb 1, 2024: SLIDE. FAULTED. DEFECT 754996: - - L1 DOOR SLIDE WAS ARMED AND DOOR WAS OPEN SLIDE DID NOT OPEN. REISTALLED ESCAPE SLIDE PER AMM 25-66-01,RII COMPLETED.
- [SDR SCNA20240116012](https://openairdocs.org/sdr/SCNA20240116012), Jan 12, 2024: BATTERY PACK. NO TEST. DEFECT W/O 84272 NRC00005: - - PERFORMED EMERGENCY LIGHT CHECK .FOUND RH FWD DOOR #1 EXTERIOR LIGHT,INTERIOR LWR AND UPPER EXIT LIGHTS INOP.NEEDS BATTERY PACK. 
- [SDR SCNA20240116011](https://openairdocs.org/sdr/SCNA20240116011), Jan 12, 2024: BATTERY PACK. NO TEST. DEFECT W/O 84272 NRC 00006: - - PERFORMED EMERGENCY BATTERY PACK FUNCTION CHECK.FOUND ROW 14DEF,15DEF UPPER EXIT SIGNS INOP.NEEDS BATTERY PACK. - - RESOLUTION: 
- [SDR SCNA20230921228](https://openairdocs.org/sdr/SCNA20230921228), Sep 6, 2023: SUPPORT. CORRODED. DEFECT J/C 802778_NR 00067: PANEL FAIRING SUPPORT STRUCTURE ON AFT SIDE WHERE PANEL 193 D IS LOCATED HAS DAMAGED AND CORRODED HOLES WHERE NUTPLATES WERE REMOVED
- [SDR SCNA20230921227](https://openairdocs.org/sdr/SCNA20230921227), Sep 6, 2023: UNKNOWN. UNKNOWN. DEFECT JC 802778 NR 00066: PANEL FAIRING SUPPORT STRUCTURE ON FWD SIDE WHERE PANEL 193 D IS LOCATED HAS DAMAGED AND CORRODED HOLES WHERE NUTPLATES WERE REMOVED.
- [SDR SCNA20240310117](https://openairdocs.org/sdr/SCNA20240310117), Jun 8, 2023: FLOOR SUPPORT. CORRODED. CORROSION ON G4 GALLEY FLOOR SUPPORT STABILIZER FITTING APROX’ BS.995 RBL. 7.00. - - RESOLUTION: REMOVED AND REPLACED G4 GALLEY FLOOR SUPPORT STABILIZER FITTING
- [SDR SCNA20221118145](https://openairdocs.org/sdr/SCNA20221118145), Nov 16, 2022: INDICATOR. FAULTED. DEFECT 713571: ON APPROACH FLAPS STUCK AT JUST UNDER 1 WITH THE FLAPS HANDLE IN 5. ORH RUN FLAPS EXTENDED TO 15. NO OTHER ISSUES. RESOLUTION: OPERATIONAL CHECK 
- [SDR SCNA20221020135](https://openairdocs.org/sdr/SCNA20221020135), Oct 18, 2022: BRACKET. STICKING. DEFECT 700882: 1R DOOR GIRT BAR BRACKET STICKING. RESOLUTION: CLEANED GIRT BAR BRACKETS AS REQUIRED. OK FOR SERVICE.
- [SDR SCNA20220822097](https://openairdocs.org/sdr/SCNA20220822097), Aug 18, 2022: SLIDE. OUT OF POSITION. WORK ORDER: 72798: DOOR R 1 ESCAPE SLIDE NEEDS THE LOWER FLAP REPOSITIONED , TUCKE AND SECURED TO VELCRO. RESOLUTION: DOOR R1 ESCAPE SLIDE LOWER FLAP VELCRO RES
- [SDR SCNA20220426032](https://openairdocs.org/sdr/SCNA20220426032), Apr 26, 2022: SLIDE. LOOSE. DOOR 2R SLIDE LOOSE. RESOLUTION: REPLACED DOOR SLIDE AT 2R WITH NEW SERVICEABLE UNIT REF AMM 25-66-1
- [SDR SCNA20210514028](https://openairdocs.org/sdr/SCNA20210514028), May 9, 2021: LAMP. INOPERATIVE. R2 DOOR HEADER PANEL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LAMPS FOR R2 DOOR HEADER PANEL EMERGENCY LIGHT. OPS CHECK GOOD I.A.W. B7-737. 33-51-01-960-
- [SDR SCNA20210514020](https://openairdocs.org/sdr/SCNA20210514020), May 8, 2021: LAMP. NO TEST. FLIGHT DECK DOME LIGHT DOES NOT ILLUMINATE DURING EMERGENCY LIGHT OPS CHECK AMM 33-55-00-720-801 STEP 1 .B. 4) (D). RELAMPED EMERGENCY LIGHT BULB IN FLIGHT DECK
- [SDR SCNA20210514027](https://openairdocs.org/sdr/SCNA20210514027), May 7, 2021: FRAME. CRACKED. CRACK AT FASTENER HOLE STA 727B S8L. REPAIRED CRACK IN FRAME AT FASTENER HOLE @ STA. 727B, STR 8L PER ER # 21-01759 REV IR AND ENG-53SCA-10739 REV 00
- [SDR SCNA20210514026](https://openairdocs.org/sdr/SCNA20210514026), May 7, 2021: FRAME. CRACKED. CRACK IN FRAME AT FASTENER HOLE STA 360 S-8L. REPAIRED CRACK IN FRAME AT FASTENER HOLE @ STA. 360, STR. 8L PER ER # 21-01759 IR AND ENG-53SCA-10739 REV. 00
- [SDR SCNA20210514025](https://openairdocs.org/sdr/SCNA20210514025), May 7, 2021: FRAME. CRACKED. CRACK IN FRAME AT FASTENER HOLE STA 400 S-8L. REPAIRED CRACK IN FRAME AT FASTENER HOLE @ STA. 400, STR 8L PER ER # 21-01759 REV IR AND ENG-53SCA-10739 REV. 00
- [SDR SCNA20210514024](https://openairdocs.org/sdr/SCNA20210514024), May 7, 2021: FRAME. CRACKED. CRACK IN FRAME AT FASTENER HOLE STA 400 S8R. REPAIRED CRACK IN FRAME AT FASTENER HOLE @ STA. 400, STR 8R PER # 21-01759 REV. IR AND ENG-53SCA-10739 REV 00
- [SDR SCNA20210514023](https://openairdocs.org/sdr/SCNA20210514023), May 7, 2021: FRAME. CRACKED. CRACK IN FRAME AT FASTENER HOLE STA 867 S-8R. REPAIRED CRACK IN FRAME AT FASTENER HOLE @ STA. 867, STR 8R PER ER # 21-01759, REV IR AND ENG-53SCA-10739 REV 00
- [SDR SCNA20210514022](https://openairdocs.org/sdr/SCNA20210514022), May 7, 2021: FRAME. CRACKED. CRACK IN FRAME AT FASTENER HOLE STA 500A S-8R. REPAIRED CRACK IN FRAME AT FASTENER HOLE @ STA 500A, STR 8R PER ER # 21-01759 REV IR AND ENG-53SCA-10739 REV 00
- [SDR SCNA20210514021](https://openairdocs.org/sdr/SCNA20210514021), May 7, 2021: FRAME. CRACKED. 2 CRACKS IN FRAME AT FASTENER HOLES STA 440 S8R. REPAIRED 2 EA CRACKS IN FRAME AT FASTENER HOLES @ STA. 440, STR 8R PER ER # 21-01759 REV. IR AND ENG-53SCA-1073
- [SDR SCNA20210514033](https://openairdocs.org/sdr/SCNA20210514033), May 6, 2021: STRAP. BROKEN. PANEL 191D ACCESS DOOR GROUND STRAP BROKEN. REMOVED AND REPLACE BROKEN GROUND STRAP ON PANEL 191D ACCESS DOOR IAW SRM 51-40-02-0G-0.
- [SDR SCNA20210514050](https://openairdocs.org/sdr/SCNA20210514050), May 5, 2021: SKIN. DELAMINATED. LEFT HAND OUTBOARD AFT FLAP INBOARD LOWER CORNER DELAMINATED. REPAIRED DELAMINATION AT INBOARD LOWER CORNER ON LEFT HAND OUTBOARD AFT FLAP PER 737-800 SRM 57-53
- [SDR SCNA20210514041](https://openairdocs.org/sdr/SCNA20210514041), May 5, 2021: SKIN. DAMAGED. PANEL 521NB SCREW HOLES DAMAGED. REPAIRED DAMAGED SCREW HOLES ON PANEL 521NB IAW SRM 57-41-01-2R-1, SRM 51-70-04-2R-9 AND SRM 51-70-14-2R-3
- [SDR SCNA20210514036](https://openairdocs.org/sdr/SCNA20210514036), May 5, 2021: SKIN. DAMAGED. WING PANEL 621QB SCREW HOLE CRACKED. CRACKED SCREW HOLE ON WING PANEL 621QB REPAIRED IAW B737 SRM 57-41-01-2R-1 TABLE 202 AND IAW B737 SRM 51-70-05-2R-10.
- [SDR SCNA20210514029](https://openairdocs.org/sdr/SCNA20210514029), May 5, 2021: RUB STRIP. MISSING. LH O/B FWD FLAP WORN WHERE I/B EDGE OF AFT FLAP MAKES CONTACT, AND RUB STRIP MISSING. REPAIRED WORN AREA ON L/H O/B FWD FLAP AT I/B EDGE OF LOWER SURFACE AND RE
- [SDR SCNA20210514055](https://openairdocs.org/sdr/SCNA20210514055), May 3, 2021: MOUNT. CRACKED. PSU MOUNT CRACKED AT ATTACH POINTS TO FRAME BRACKET STA 727D S8L. REMOVED AND REPLACED PSU MOUNT AT ATTACH POINTS TO FRAME BRACKET STA 727D S8L PO # 822467 IAW 
- [SDR SCNA20210514054](https://openairdocs.org/sdr/SCNA20210514054), May 3, 2021: FLOOR PANEL. CORRODED. LOOR PANEL 211AF HAS LIGHT SURFACE CORROSION AT FASTENER HOLES. LOCATED AND DRILLED NEW REPLACEMENT PANEL 211AF (141A5133U15) IAW-B-737-SRM-51-40-05-0G-0, APPLI
- [SDR SCNA20210514038](https://openairdocs.org/sdr/SCNA20210514038), Apr 29, 2021: SKIN. DAMAGED. WING PANEL 621LB SCREW HOLE DAMAGED. REPAIRED DAMAGED SCREW HOLE ON WING PANEL 621LB IAW SRM 57-41-01-2R-1, SRM 51-70-04-2R-9 AND SRM 51-70-14-2R-3
- [SDR SCNA20210514044](https://openairdocs.org/sdr/SCNA20210514044), Apr 27, 2021: SKIN. DAMAGED. PANEL 521WB LEADING EDGE DELAMINATED. DELAMINATED LEADING EDGE ON PANEL 521WB REPAIRED IAW B737 SRM 57-41-01-2R-1 TABLE 202 AND IAW B737 SRM 51-70-04-2R-9.
- [SDR SCNA20210514051](https://openairdocs.org/sdr/SCNA20210514051), Apr 21, 2021: ANGLE. DAMAGED. AUXILIARY ANGLE ATTACHED TO FRAME @STA. 500D R/H HAS DAMAGE AROUND MULTIPLE NUTPLATE LOCATIONS. DUE TO NO ALLOWABLE DAMAGE IN THE SRM. FRAME ATTACH ANGLE AT STA
- [SDR SCNA20210514048](https://openairdocs.org/sdr/SCNA20210514048), Apr 20, 2021: FRAME. CORRODED. CORROSION FOUND ON FRAME @STA. 727I, STR. 24R-25R. REMOVED AND REPLACED CORRODED ANGLE ASSY P/N 146A9403-84 WITH NEW IAW DWG 146A1243 AND SRM 51-40-02-0G
- [SDR SCNA20210514040](https://openairdocs.org/sdr/SCNA20210514040), Apr 20, 2021: SKIN. DAMAGED. PANEL 521MB SCREW HOLES DAMAGED. REPAIRED DAMAGED SCREW HOLES ON PANEL 521MB IAW B737 SRM 51-70-04-2R-9
- [SDR SCNA20210514039](https://openairdocs.org/sdr/SCNA20210514039), Apr 19, 2021: SKIN. DAMAGED. PANEL 521TB FORWARD EDGE DELAMINATING. DELAMINATED FORWARD EDGE OF PANEL 521TB REPAIRED IAW B737 SRM 57-41-01-2R-1 TABLE 202 AND IAW B737 SRM 51-70-04-2R-9.
- [SDR SCNA20210514034](https://openairdocs.org/sdr/SCNA20210514034), Apr 19, 2021: SKIN. DAMAGED. WING PANEL 621DB COMPOSITE DAMAGED MULTIPLE SPOTS ON THE FORWARD EDGE. REPAIRED DAMAGED COMPOSITE IN MULTIPLE SPOTS ON THE FORWAARD EDGE OF WING PANEL 621DB IAW
- [SDR SCNA20210514047](https://openairdocs.org/sdr/SCNA20210514047), Apr 16, 2021: FRAME SPLICE. CORRODED. CORROSION FOUND ON STA. 787 FRAME SPLICE @ STR. 25R. DUE TO NO ALLOWABLE DAMAGE IN THE SRM, FRAME SPLICE AT STA. 787 S25R FOUND TO BE OUT OF LIMITS. REMOVED AND
- [SDR SCNA20210514043](https://openairdocs.org/sdr/SCNA20210514043), Apr 16, 2021: SKIN. DAMAGED. PANEL 521FB SCREW HOLES DAMAGED. REPAIRED DAMAGED SCREW HOLES ON PANEL 521FB IAW B737 SRM 57-41-01-2R-1 TABLE 202 AND IAW B767 SRM 51-70-04-2R-9.
- [SDR SCNA20210514042](https://openairdocs.org/sdr/SCNA20210514042), Apr 16, 2021: SKIN. DAMAGED. PANEL 521UB SCREW HOLES DAMAGED. REPAIRED DAMAGED SCREW HOLES ON PANEL 521UB IAW B737 SRM 57-41-01-2R-1 TABLE 202 AND IAW B737 SRM 51-70-04-2R-9.
- [SDR SCNA20210514037](https://openairdocs.org/sdr/SCNA20210514037), Apr 16, 2021: SKIN. DAMAGED. WING PANEL 621PB SCREW HOLE DAMAGED. REPAIRED DAMAGED SCREW HOLE ON WING PANEL 621PB IAW B737 SRM 51-70-04-2R-9
- [SDR SCNA20210514035](https://openairdocs.org/sdr/SCNA20210514035), Apr 16, 2021: SKIN. DAMAGED. WING PANEL 621FB MULTIPLE SCREW HOLES DAMAGED. REPAIRED MULTIPLE DAMAGED SCREW HOLES ON WING PANEL 621FB IAW B737 SRM 51-70-04-2R-9
- [SDR SCNA20210514053](https://openairdocs.org/sdr/SCNA20210514053), Apr 15, 2021: SKIN. WORN. RH HORIZONTAL STAB PANEL 343AB SHARK FIN WORN. REMOVED AND REPLACED RH HORIZ. STAB PANEL 343AB BLADE ASSY (SHARK FIN) PER SRM 51-40-02 AND DRAWING 186A3101
- [SDR SCNA20210514052](https://openairdocs.org/sdr/SCNA20210514052), Apr 15, 2021: SKIN. WORN. RH HORIZONTAL STAB PANEL 343AT SHARK FIN WORN. REMOVED AND REPLACED RH HORIZ. STAB PANEL 343AT BLADE ASSY (SHARK FIN) PER SRM 51-40-02 AND DRAWING 186A3101.
- [SDR SCNA20210514049](https://openairdocs.org/sdr/SCNA20210514049), Apr 15, 2021: TIE DOWN. CORRODED. CORROSION FOUND ON NET TIE DOWN @STA. 792, STR. 23L. DUE TO NO ALLOWABLE LIMITS IN THE SRM, TIE DOWN PLATE AT STA. 792 S23L FOUND TO BE OUT OF LIMITS, FABRICATE
- [SDR SCNA20210514045](https://openairdocs.org/sdr/SCNA20210514045), Apr 15, 2021: FAIRING. ERODED. #1 FWD FLAP FAIRING 544AB, EROSION AT AFT MOUNT HOLES. REPAIRED EROSION AT AFT MOUNT HOLES ON #1 FWD FLAP FAIRING 544AB PER 737-800 SRM 57-53-70-2R-3 TABLE 203 

All 183: https://openairdocs.org/deregistered/N815SY-2026-01-19/reports.md

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