# N819SY: 2006 Boeing 737-86N

- Status: Valid registration
- Airframe: [Boeing 737-86N](https://openairdocs.org/model/boeing-737-86n) (registry code 13844CD, 149 seats)
- Engine: [CFM International CFM56-7B26 series](https://openairdocs.org/engine/cfm-international-cfm56-7b26-series) (registry code 13045)
- Serial number: 34254
- Year built: 2006
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 10, 2014
- Certificate issued: January 7, 2020
- Expires: January 31, 2030
- Mode S code: AB2C72
- Registered owner: [Sun Country Inc](https://openairdocs.org/faa-owner/SUN%20COUNTRY%20INC)
- 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 is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=819SY
- Page: https://openairdocs.org/aircraft/N819SY

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 CFM International CFM56-7B26 model are included.

## ADs that may apply (OpenAirDocs): 19 in force

### Matched by airframe (Boeing 737-86N)

None in force.

### Matched by engine (CFM International CFM56-7B26 series)

- [AD 2023-05-05](https://openairdocs.org/ad/2023-05-05): Turbine Engine Compressor Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 98 more. Effective May 10, 2023
- [AD 2022-02-03](https://openairdocs.org/ad/2022-02-03): Turbine Engine Accessory Drive · CFM International CFM56-3, CFM56-3B, CFM56-3C and 34 more. Effective Mar 22, 2022
- [AD 2021-16-08](https://openairdocs.org/ad/2021-16-08): Turbine Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 55 more. Effective Sep 28, 2021
- [AD 2018-26-01](https://openairdocs.org/ad/2018-26-01): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jan 10, 2019
- [AD 2018-09-51](https://openairdocs.org/ad/2018-09-51): Engine · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jun 7, 2018
- [AD 2015-18-04](https://openairdocs.org/ad/2015-18-04): 73-tooth gearshaft located in the engine accessory gearbox (AGB) · CFM International CFM56-3, CFM56-7B20, CFM56-7B20/2 and 47 more. Effective Oct 20, 2015
- [AD 2015-04-02](https://openairdocs.org/ad/2015-04-02): Dual engine thrust instability event · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Mar 31, 2015
- [AD 2010-13-09](https://openairdocs.org/ad/2010-13-09): Stage 3 low-pressure turbine (LPT) · CFM International CFM56-5, CFM56-5-A1/F, CFM56-5A4 and 88 more. Effective Jul 26, 2010
- [AD 2010-01-05](https://openairdocs.org/ad/2010-01-05): LP turbine rear frames · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 25 more. Effective Feb 18, 2010
- [AD 2009-11-02](https://openairdocs.org/ad/2009-11-02): HPC 4-9 spools · CFM International CFM56-2, CFM56-2A, CFM56-2B and 109 more. Effective Jun 23, 2009
- [AD 2008-03-09](https://openairdocs.org/ad/2008-03-09): Low pressure turbine rear frames (TRFs) · CFM International CFM56-7B18, CFM56-7B20, CFM56-7B22 and 10 more. Effective Mar 10, 2008
- [AD 2006-26-01](https://openairdocs.org/ad/2006-26-01): Fuel filters · CFM International CFM56-2, CFM56-2A, CFM56-2B and 93 more. Effective Jan 3, 2007
- [AD 2002-16-18](https://openairdocs.org/ad/2002-16-18): Low pressure turbine (LPT) nozzle segments · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 33 more. Effective Sep 18, 2002
- [AD 2002-13-03](https://openairdocs.org/ad/2002-13-03): Turbofan Engines · CFM International CFM56-2, CFM56-2A, CFM56-2B and 55 more. Effective Aug 1, 2002
- [AD 2001-11-05](https://openairdocs.org/ad/2001-11-05): No. 4 Bearings · CFM International CFM56-2, CFM56-2B, CFM56-3 and 45 more. Effective Jun 11, 2001
- [AD 2001-02-12](https://openairdocs.org/ad/2001-02-12): On-Wing Torque Inspection · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 11 more. Effective Feb 14, 2001
- [AD 98-21-23](https://openairdocs.org/ad/98-21-23): Electronic Engine Control · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 10 more. Effective Nov 2, 1998
- [AD 98-19-20](https://openairdocs.org/ad/98-19-20): Hydromechanical Unit · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 7 more. Effective Oct 7, 1998
- [AD 98-14-51](https://openairdocs.org/ad/98-14-51): Accessory Gearbox · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 10 more. Effective Oct 1, 1998

### Historical (superseded or no longer in force)

- [AD 2021-10-09](https://openairdocs.org/ad/2021-10-09) (historical): Turbine Engine Compressor Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 82 more. Effective Jun 24, 2021
- [AD 2019-12-05](https://openairdocs.org/ad/2019-12-05) (historical): Turbine Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 39 more. Effective Jul 5, 2019
- [AD 2018-18-01](https://openairdocs.org/ad/2018-18-01) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Oct 16, 2018
- [AD 2018-10-11](https://openairdocs.org/ad/2018-10-11) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jun 1, 2018
- [AD 2018-09-10](https://openairdocs.org/ad/2018-09-10) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective May 14, 2018
- [AD 2013-26-01](https://openairdocs.org/ad/2013-26-01) (historical): Oil dynamic seal assembly · CFM International CFM56-3, CFM56-3B, CFM56-3C and 52 more. Effective Feb 3, 2014
- [AD 2000-12-01](https://openairdocs.org/ad/2000-12-01) (historical): Critical Life-Limited Parts · CFM International CFM56-2, CFM56-2A, CFM56-2B and 54 more. Effective Dec 11, 2000

## Information bulletins (advisory) (1 in force)

- [SAIB NE-08-17R3](https://openairdocs.org/saib/NE-08-17R3): Turbine Section - Propulsion Technology LLC Unapproved Repair. Issued May 28, 2014
- [SAIB NE-08-17R2](https://openairdocs.org/saib/NE-08-17R2) (historical): Turbine Section - Propulsion Technology LLC Unapproved Repair. Issued Mar 7, 2011
- [SAIB NE-08-17R1](https://openairdocs.org/saib/NE-08-17R1) (historical): Propulsion Technology LLC Unapproved Repair. Issued May 22, 2008
- [SAIB NE-08-17](https://openairdocs.org/saib/NE-08-17) (historical): Propulsion Technologies International Unapproved Repair. Issued May 14, 2008

## NTSB investigations

None matched to N819SY.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20240804011789I](https://openairdocs.org/incident/20240804011789I), Aug 4, 2024: Boeing 737-86N (N819SY), Los Angeles, CA, Substantial damage. On 08/03/2024 at 1730 local time at Los Angeles International Airport (lax), California, aircraft [privacy data omitted], serial number 34254, a Boeing 737-800…

## Service difficulty reports (55, newest 50)

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

- [SDR SCNA20260720319](https://openairdocs.org/sdr/SCNA20260720319), Jul 18, 2026: POWER SUPPLY. INOPERATIVE. RIGHT AFT CABIN EMERGENCY EXIT LIGHTS FAIL TO ILLUMINATE. REMOVED AND REPLACED THE POWER SUPPLY M1672 IAW AMM 33-51-06. OPS CHKD GOOD.
- [SDR SCNA20260720318](https://openairdocs.org/sdr/SCNA20260720318), Jul 18, 2026: POWER SUPPLY. INOPERATIVE. LEFT OVER WING EXIT EMERGENCY EXIT LIGHT LIGHTS FAILED TO ILLUMATED. REMOVED AND REPLACED THE POWER SUPPLY M1694 IAW AMM 35-51-06. OPS CHKD GOOD.
- [SDR SCNA20260720317](https://openairdocs.org/sdr/SCNA20260720317), Jul 18, 2026: POWER SUPPLY. INOPERATIVE. COCKPIT OVERHEAD ENTRY, L1 DOOR EMERGENCY EXIT LIGHT FAILS ILLUMINATED. REMOVED AND PLACED THE POWER SUPPLY M1675 IAW AMM 33-51-06. OPS CHKD GOOD.
- [SDR SCNA20260630274](https://openairdocs.org/sdr/SCNA20260630274), Jun 29, 2026: GIRT BAR. FOD. L1 GIRT BAR NOT STAYING IN LOCKED POSITION ON LEFT SIDE. CLEANED DEBRIS ON L1 GIRT BAR LATCH, ATTACHED LATCH TO GIRT BAR AND BAR STAYED IN PLACE IN REF TO AMM 2
- [SDR SCNA20260605239](https://openairdocs.org/sdr/SCNA20260605239), Jun 4, 2026: UNKNOWN. ODOR. PASSENGER AND AGENT IN PHL REPORTED A BURING PLASTIC SMELL IN THE CABIN - - PERFORMED FIM 21-00 TASK 806 NO DEFECTS NOTED A/C FOR SERVICE
- [SDR SCNA20260427170](https://openairdocs.org/sdr/SCNA20260427170), Apr 24, 2026: LIGHT. INOPERATIVE. RIGHT EMERGENCY LIGHTS ROW 25 AND ROW 27 INOPERATIVE. OPEN
- [SDR SCNA20260427169](https://openairdocs.org/sdr/SCNA20260427169), Apr 24, 2026: ELEC CONNECTOR. DISCONNECTED. EMERGENCY LIGHT R2 OUTSIDE INOPERATIVE. PERFORMED T/S AT R2 OUTSIDE IAW B737 WDM 33-51-13 FWD EMERGENCY LIGHT L733 DISCONNECTED AT THE REAR AND RE CONNECTED IT 
- [SDR SCNA20260427168](https://openairdocs.org/sdr/SCNA20260427168), Apr 24, 2026: LAMP. INOPERATIVE. R/H AFT SLIDE EMERGENCY LIGHT INOP. R/H AFT SIDE EMERGENCY OVERWING LIGHT LAMP REPLACED IAW B737 AMM 33-51-04 OPS CHECK SATISFACTORY REV 89.
- [SDR SCNA20260223099](https://openairdocs.org/sdr/SCNA20260223099), Feb 23, 2026: STRIP. CRACKED. FORWARD GALLEY RUBBER STRIP BETWEEN GALLEY AND CARPET IS CRACKED AND POSES A TRIPPING HAZARD. REMOVED AND REPLACED RUBBER STRIP AMM 25-27-31-00-804.
- [SDR SCNA20260209060](https://openairdocs.org/sdr/SCNA20260209060), Feb 8, 2026: LIGHT. UNSECURE. EXIT PATH LIGHTS RAISED OFF FLOOR AT ROW 11 SIDE ABC. INSPECTED FLOOR ILLUMINATION PATH IAW AMM 25-27-21, NO ISSUE FOUND. OK FOR SERVICE.
- [SDR SCNA20260105007](https://openairdocs.org/sdr/SCNA20260105007), Jan 4, 2026: WINDOW. LEAKING. LOUD NOISE ,AIR RUSHING ON THE CA SIDE WINDOW. AIRPLANE PRESSURIZATION NOT ASSURED. REMOVED & REPLACED L2 WINDOW ASSY IAW AMM 56-12-11. OPS & LEAK CHECKED GOOD.
- [SDR SCNA20260105005](https://openairdocs.org/sdr/SCNA20260105005), Dec 24, 2025: SKIN. GROUND DAMAGE. CATERING TRUCK RAILING MADE CONTACT AFT OF L2 DOOR. REPAIR DAMAGE ON FUSELAGE SKIN AT FS 1006 TO FS 1016 BETWEEN STR 14L TO 15L IAW SRM 53-70-01-2R-5, REPAIR 5,
- [SDR SCNA20251231514](https://openairdocs.org/sdr/SCNA20251231514), Dec 24, 2025: SKIN. GROUND DAMAGE. CATERING TRUCK RAILING MADE CONTACT AFT OF L2 DOOR. REPAIR THE DAMAGE ON FUSELAGE SKIN AT BS 1006 TO 1016 BETWEEN STR 14L TO 15L IAW SRM 53-70-01-2R-5, REPAIR 5
- [SDR SCNA20251215486](https://openairdocs.org/sdr/SCNA20251215486), Dec 14, 2025: BULB. INOPERATIVE. 14ABC AND 15ABC EMERGENCY WINDOW FWD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT BULB ON 14ABC AND 15ABC EMERGENCY WINDOW FWD EMERGENCY LIGHT REF AM
- [SDR SCNA20251117440](https://openairdocs.org/sdr/SCNA20251117440), Nov 15, 2025: LIGHT. DETACHED. ROW 11 ABC SIDE EMERGENCY LIGHT STRIP COMING OFF THE FLOOR. SECURED THE PATH LIGHT STRIP NEAR ROW 11ABC IAW AMM 33-51-15. OPS CHECKED GOOD.
- [SDR SCNA20251117439](https://openairdocs.org/sdr/SCNA20251117439), Nov 15, 2025: RETAINER. LOOSE. L1 DOOR LEFT BRACKET FOR GIRT BAR IS LOOSE. ADJUSTED FORWARD GIRT BAR RETAINER CLIP ON L1 DOOR REF. AMM 25-66-01. OPS CHECKED GOOD.
- [SDR SCNA20250905360](https://openairdocs.org/sdr/SCNA20250905360), Sep 5, 2025: THRESHOLD. UNSECURE. FWD GALLEY FLOOR RUBBER FLOOR TRIM IS RIPPED UP AND A TRIPPING HAZARD. REMOVED AND REPLACED THE CARPET TO MAT THRESHOLD IAW AMM 25-27-21.
- [SDR SCNA20250902348](https://openairdocs.org/sdr/SCNA20250902348), Sep 2, 2025: COFFEEMAKER. DAMAGED. PLACARD ON FORWARD GALLEY COFFEE MAKER IS BENT AND SHARP. SECURED FWD. GALLEY PLACARD AT COFFEE MAKER PER AMM 11-32-00
- [SDR SCNA20250429135](https://openairdocs.org/sdr/SCNA20250429135), Apr 29, 2025: WINDOW. OVERTEMP. WINDOW R3 OVERHEAT. SLIGHT ELECTRICAL WIRING SMELL WHEN SWITCH STAYS ON. REPLACED RCPT FOR R2 SLIDING WINDOW. REPLACED R2 WINDOW COIL CHORD. REF: WDM 30-41-11 A
- [SDR SCNA20241217399](https://openairdocs.org/sdr/SCNA20241217399), Dec 17, 2024: SEAT. DAMAGED. WORK ORDER 911123, NR00010 THROUGH NR00029: 4C SEAT CUSHION OUT OF POSITION - NOTED VELCRO MISSING AND FIREBLOCKING DAMAGED. REMOVED AND REPLACED SEAT CUSHIONS 
- [SDR SCNA20241114369](https://openairdocs.org/sdr/SCNA20241114369), Oct 31, 2024: COVER. CRACKED. DEFECT 71919: 1L DOOR FLOOR LIGHT COVER CRACKED. RESOLUTION: INSTALLED NEW COVER ON THE L1 FLOOR PROXIMITY LIGHT REF AMM 33-51-14. THIS CLEARS MEL 25-10
- [SDR SCNA20241028333](https://openairdocs.org/sdr/SCNA20241028333), Oct 17, 2024: COVER. DETACHED. DEFECT 777247: ESCAPE SLIDE PACK BUSTLE COVER FELL. RESOLUTION: SECURED SLIDE PACK PRESSURE SIGHT WINDOW REF AMM 25-66-01.
- [SDR SCNA20240920320](https://openairdocs.org/sdr/SCNA20240920320), Aug 25, 2024: SKIN. DAMAGED. WORK ORDER A1P190 JOB 2 ITEM 70: PERFORMED FUSELAGE SKIN REPAIR BETWEEN STA 440 AND STA480, S-4R AND S-6R DUE TO LIGHTNING STRIKE IAW COOPESA EO# C00-EO-2024-20
- [SDR SCNA20240920319](https://openairdocs.org/sdr/SCNA20240920319), Aug 25, 2024: SKIN. DAMAGED. WORK ORDER A1P190 JOB 2: UPPER FUSELAGE, EXTERNAL SKIN SECTION AT STA 500+3 AND 1.5 INCH BELOW STR-4R SKIN LAP JOINT WITH LIGHTNING STRIKE. PERFORMED FUSELAGE S
- [SDR SCNA20240920318](https://openairdocs.org/sdr/SCNA20240920318), Aug 25, 2024: SKIN. DAMAGED. WORK ORDER A1P190 JOB 2 ITEM 71: UPPER FUESLAGE, EXTERNAL SKIN SECTION AT STA 481 AND 1.750 INCH BELOW STR-4R SKIN WITH LIGHTNING STRIKE. - - - WORK PERFORMED: 
- [SDR SCNA20240920317](https://openairdocs.org/sdr/SCNA20240920317), Aug 25, 2024: SKIN. DAMAGED. WORK ORDER A1P190 JOB 2 ITEM 73: UPPER FUSELAGE, EXTERNAL SKIN SECTION AT STA 500 + 12 AND 1.5 INCH BELOW STR-4R SKIN LAP JOINT WITH LIGHTNING STRIKE. - - WORK 
- [SDR SCNA20240920316](https://openairdocs.org/sdr/SCNA20240920316), Aug 25, 2024: SKIN. DAMAGED. UPPER FUSELAGE EXTERNAL SKIN SECTION AT STA 203 AND WL243 SKIN WITH LIGHTNING STRIKE (RHS) - - WORK PERFORMED: PERFORMED FUSELAGE SKIN FREEZE PLUG REPAIR BETWEE
- [SDR SCNA20240920315](https://openairdocs.org/sdr/SCNA20240920315), Aug 25, 2024: SKIN. DAMAGED. UPPER FUSELAGE, EXTERNAL SKIN SECTION AT STA 233 AND WL 265 (RBL 40) SKIN WITH LIGHTNING STRIKE. - - WORK PERFORMED: PERFORMED FUSELAGE SKIN FREEZE PLUG REPAIR 
- [SDR SCNA20240820305](https://openairdocs.org/sdr/SCNA20240820305), Aug 8, 2024: SKIN. DENTED. WORK ORDER FS240105 NR002: POSSIBLE DENT WITH 2 BLIND FASTENERS INSTALLED THRU SKIN AND STRINGER STA 440 STR 28R. - - RESOLUTION: DENT WITH CREASE ON SKIN AT ST
- [SDR SCNA20240820304](https://openairdocs.org/sdr/SCNA20240820304), Aug 8, 2024: RIB. CRACKED. WORK ORDER FS240105 NR001: LH WING OUTER RIB P/N 737-5274-1 #18 HOLE AS A CRACK INDICATION. - - RESOLUTION: LH WING OUT RIB P/N 737-5274-1 #18 CRAKCED HOLE WAS 
- [SDR SCNA20240206028](https://openairdocs.org/sdr/SCNA20240206028), Feb 3, 2024: BRACKET. LOOSE. 1R GIRT BAR DOOR BRACKET TOO LOOSE GIRT BAR FALLS OFF. ADJUSTED GRIT BAR HANGER REF AMM 25-66-01.
- [SDR SCNA20230809207](https://openairdocs.org/sdr/SCNA20230809207), Aug 8, 2023: UNKNOWN. UNKNOWN. DEFECT 770498: AFT LEFT OVEN 410 DEGREES SMOKING WHEN USED. - - - RESOLUTION: REMOVED AND REPLACED AFT L/H OVEN REF AMM 25-31-01, OPS CHECK GOOD.
- [SDR SCNA20230307092](https://openairdocs.org/sdr/SCNA20230307092), Mar 6, 2023: NONE. NONE. DEFECT W/O 77392: CABIN EMERGENCY LIGHTS AT RH EXIT ROW 14 UPPER AND AFT LOWER RIGHT AND LEFT LOWER ROW 14 NOT ILLUMINATING. RESOLUTION: REPLACED ALL LAMPS FIXT
- [SDR SCNA20221121146S](https://openairdocs.org/sdr/SCNA20221121146S), Nov 20, 2022: SENSOR. FAULTED. FLAP ASYMMETRY AFTER T/O ON CLEAN UP. BITE CK. OF FSEU REPORTED FAULT 27-53251 FLAP 2 SKEW. FOUND SKEW SENSOR 2 OUT OF RANGE . REMOVED AND REPLACED #2 FLAP SKEW
- [SDR SCNA20221121146I](https://openairdocs.org/sdr/SCNA20221121146I), Nov 20, 2022: FLAP. ASYMETRIC. DEFECT 713770: FLAP ASYMMETRY AFTER T/O ON CLEAN UP. RESOLUTION: (IN PROGRESS)
- [SDR SCNA20220815096SU](https://openairdocs.org/sdr/SCNA20220815096SU), Aug 12, 2022: FASTENER. MISSING. SUPPLEMENTAL. DEFECT 705390: 2L AFT DOOR MISSING SCREW ON GIRT PLATE. RESOLUTION: REF MDDR# 113587 LOG # 705202 ITEM#1 2L THRESHOLD FASTENERS THIS CLEARS GMM/MT
- [SDR SCNA20220815096](https://openairdocs.org/sdr/SCNA20220815096), Aug 12, 2022: SCREW. MISSING. DEFECT 705390: 2L AFT DOOR MISSING SCREW ON GIRT PLATE.
- [SDR SCNA20220616069](https://openairdocs.org/sdr/SCNA20220616069), Jun 5, 2022: ROPE. LOOSE. DEFECT: F.O. EMERGENCY ESCAPE ROPE NOT SECURED TO A/C. MXC NOTIFIED RESOLUTION: SECURED F/O EMERGENCY ESCAPR ROPE TO AIRCRAFT REF AMM 25-61-10.
- [SDR SCNA20220523051](https://openairdocs.org/sdr/SCNA20220523051), May 11, 2022: FLOOR SUPPORT. CRACKED. DEFECT: FOUND DAMAGE TO FRAME, AFT CARGO @STA. 807, STR. 24L TO 22L. RESOULTION: REPAIRED FRAME @ STA 807 STR 24L - 22L IN ACCORDANCE WITH SCA ENG-53SCA-10965 R
- [SDR SCNA20220523056](https://openairdocs.org/sdr/SCNA20220523056), May 10, 2022: STRINGER. CRACKED. DEFECT: DAMAGE FOUND ON STRINGER 23L AT STA 727A. RESOLUTION: REPAIRED STRINGER @ STA 727A 23L IAW B737 SRM 53-00-03-2R-1 REV 75 THIS IS A CATEGORTY "A". NO FUR
- [SDR SCNA20220523054](https://openairdocs.org/sdr/SCNA20220523054), Apr 18, 2022: FLOOR SKIN. CRACKED. DEFECT: FOUND DAMAGE TO FRAME, AFT CARGO @STA 727E, STR 24L TO 25L. RESOLUTION: REPAIRED FRAME @STA 727E STR 24L - 25L IAW SCA ENG-53SCA-10964 REV 00 AND ATS ER
- [SDR SCNA20220523053](https://openairdocs.org/sdr/SCNA20220523053), Apr 18, 2022: FRAME ANGLE. CRACKED. DEFECT: FOUND DAMAGE TO FRAME, AFT CARGO @STA 727B, STR 24L. RESOLUTION: REPAIRED DAMAGED FRAME @STA 727B STR 24L IN ACCORDANCE WITH B737 SRM 53-60-70-2R-3 REV 
- [SDR SCNA20220520049](https://openairdocs.org/sdr/SCNA20220520049), Apr 18, 2022: FLOORBEAM. CRACKED. DEFECT: FOUND DAMGE TO FRAME, AFT CARGO @STA. 727B, STR. 3R RESOLUTION: REPAIRED FRAME AFT CARGO @STA 727B, STR 23R PER SRM 53-60-07-2R-3 REV 75 REPAIR IS CAT B
- [SDR SCNA202205170SUPP](https://openairdocs.org/sdr/SCNA202205170SUPP), Apr 18, 2022: FRAME ANGLE. CRACKED. DEFECT: FOUND DAMAGE TO FRAME, AFT CARGO @STA 727C, STR 23L
- [SDR SCNA20220517048](https://openairdocs.org/sdr/SCNA20220517048), Apr 18, 2022: STABILATOR. CRACKED. DEFECT: FOUND DAMAGE TO FRAME, AFT CARGO @STA 727C, STR. 23L RESOLUTION: REPAIRED FRAME AFT CARGO @ STA 727C, STR 23L PER SRM 53-60-07-2R-3 REV 75 REPAIR IS CAT
- [SDR SCNA22020516047](https://openairdocs.org/sdr/SCNA22020516047), Apr 18, 2022: FLOOR SUPPORT. CRACKED. DEFECT: FOUND DAMAGE TO FRAME, AFT CARGO @STA. 727F, STR. 24L. RESOLUTION: AFT CARGO FRAME @ STA 727F, STR 24L REPAIRED PER SRM 53-60-07-2R-3 REV 75. REPAIR IS 
- [SDR SCNA20220523052](https://openairdocs.org/sdr/SCNA20220523052), Apr 15, 2022: STRINGER. CRACKED. DEFECT: FOUND DAMAGE TO STA 727A, STR 24L FRAMES, AFT CARGO IN AREA OF FWD FLOOR PANEL. RESOLUTION: REPAIRED FRAME @ STA 727A STR 24L IAW SCA ENG-53SCA-10962 RE
- [SDR SCNA20220523055](https://openairdocs.org/sdr/SCNA20220523055), Apr 13, 2022: FLOOR SUPPORT. CRACKED. DEFECT: DAMAGED BEAM FOUND ON FORWARD CARGO DOOR, BEAM "B" (2ND INTERNAL BEAM FROM TOP). RESOLUTION: REPAIRED DAMAGED BEAM ON FWD CARGO DOOR PER ATS ER 2201541 
- [SDR SCNA20200929052](https://openairdocs.org/sdr/SCNA20200929052), Sep 4, 2020: BULKHEAD WEB. DAMAGED. TOOL MARK FOUND C/T AFT PRESSURE WEB AT W/L 207 RT WEB JUST BELOW THE PRESSURE WEB. REMOVED .006" MATERIAL FROM .040" NOMINAL .034" REMAINING, IAW B737 SRM 53-8
- [SDR SCNA20190627073](https://openairdocs.org/sdr/SCNA20190627073), Jun 27, 2019: BATTERY PACK. INOPERATIVE. MULTIPLE EMERGENCY LIGHTS OUT ON RH SIDE. REMOVED AND REPLACED 4 EA EMERLIGHT BATTERY PACKS. OPS CHECKS GOOD.

All 55: https://openairdocs.org/aircraft/N819SY/reports.md

## STCs that may be installed (OpenAirDocs) (2)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the engine (CFM International CFM56-7B26 series)

- [STC SE04840NY](https://openairdocs.org/stc/SE04840NY): Installation of HarcoSemco Exhaust Gas Temperature (EGT) Electrical Harnesses in CFM56-7 engine. Kilroy Aviation LLC
- [STC SE03036CH](https://openairdocs.org/stc/SE03036CH): Application of a deep compressive stress layer using a Low Plasticity Burnishing (LPB) process on CFM56-7 Series Engines Stage 1 High Pressure Compressor (HPC) Blade Dovetails in accordance with Delta Air Lines Inc. Drawing No. 72-0396, Revision B, dated November 3, 2011, or later FAA Approved revision. Delta Air Lines Inc

## Related

- Other Boeing 737-86N aircraft: https://openairdocs.org/model/boeing-737-86n/aircraft.md
- The CFM International CFM56-7B26 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b26-series.md

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