# N814SY: 2001 Boeing 737-8BK

- Status: Valid registration
- Airframe: [Boeing 737-8BK](https://openairdocs.org/model/boeing-737-8bk) (registry code 13844FG, 149 seats)
- Engine: [CFM International CFM56-7B24 series](https://openairdocs.org/engine/cfm-international-cfm56-7b24-series) (registry code 13044)
- Serial number: 30620
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 8, 2011
- Certificate issued: February 20, 2020
- Expires: February 28, 2027
- Mode S code: AB19DF
- 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=814SY
- Page: https://openairdocs.org/aircraft/N814SY

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 CFM56-7B24 model are included.

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

### Matched by airframe (Boeing 737-8BK)

None in force.

### Matched by engine (CFM International CFM56-7B24 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 N814SY.

## 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 20110904019659I](https://openairdocs.org/incident/20110904019659I), Sep 4, 2011: Boeing 737-8BK (N814SY), Mendota, MN, Minor damage. On decent into sea at about 12000 feet the aircraft encounter a bird strike. The pilot did not declare an emergency and the aircraft was vectored for visual…

## Service difficulty reports (174, 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 SCNA20261009418](https://openairdocs.org/sdr/SCNA20261009418), Oct 7, 2026: LIGHT. INOPERATIVE. AFT LEFT AND RIGHT EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED SLIDE/OVERWING LIGHT PER AMM 33-51-04. OPS CHECK GOOD.
- [SDR SCNA20260702279](https://openairdocs.org/sdr/SCNA20260702279), Jul 2, 2026: MODULE. FAULTED. CARGO FIRE TEST NOT TESTING PROPERLY. REMOVED AND REPLACED CARGO SMOKE MODULE ASSY, OPS CK GOOD. IAW AMM 26-16-00
- [SDR SCNA20260616249](https://openairdocs.org/sdr/SCNA20260616249), Jun 16, 2026: BRACKET. LOOSE. FWD ENTRY LEFT SIDE GIRT BAR BRACKET IS LOOSE. ADJUSTED FWD PAX DOOR GIRT BAR BRACKETS REF AMM 25-66-01. OK FOR SERVICE.
- [SDR SCNA20260420160](https://openairdocs.org/sdr/SCNA20260420160), Apr 18, 2026: GIRT BAR. OUT OF ADJUST. R1 GIRT BAR BRACKET IS TOO TIGHT. ADJUSTED GIRT BAR TENSION ON R1 DOOR RE. AMM 25-66-00.
- [SDR SCNA20260216084](https://openairdocs.org/sdr/SCNA20260216084), Feb 14, 2026: LIGHT. INOPERATIVE. CENTER LIGHT DOES NOT TURN ON IN UPPER AREA OF RH AFT EMERGENCY EXIT. BALLAST OF THE EMERGENCY EXIT RH AFT WAS REPLACED PER B737-800 SRM 51-40-02-0G-0 AND PER B
- [SDR SCNA20260219089](https://openairdocs.org/sdr/SCNA20260219089), Jan 31, 2026: FRAME ANGLE. CORRODED. AFTER REMOVAL, CORROSION WAS FOUND ON THE FRAME ANGLE, S28R, BS 500G. THE FRAME ANGLE WAS REPLACE IAW SRM 51-40-02-0G-0.
- [SDR SCNA20260219090](https://openairdocs.org/sdr/SCNA20260219090), Jan 28, 2026: FITTING. DAMAGED. TWO ELONGATED HOLES ON THE NR 1 COWLING HINGE FITTING INBD & OTBD, NAC STA 158.1230 REPAIRED IAW ECTC ENG-54SCA-11809, & ETI-737-26-025, REV 6.
- [SDR SCNA20260217087](https://openairdocs.org/sdr/SCNA20260217087), Jan 13, 2026: DOOR SILL. CORRODED. CORROSION ON WEB LOWER MAIN SILL AT FWD CARGO DOOR CUTOUT BTW STA 440 TO STA 492
- [SDR SCNA20260113026](https://openairdocs.org/sdr/SCNA20260113026), Jan 11, 2026: ANCHOR NUT. DAMAGED. DAMAGE ANCHOR NUT 1EA OF SUPPORT OF SLIDE ON INTERNAL STRUCTURE OF AFT ENTRY DOOR . NUT 1EA OF SUPPORT OF SLIDE ON INTERNAL STRUCTURE OF AFT ENTRY DOOR WAS REPL
- [SDR SCNA20251202456](https://openairdocs.org/sdr/SCNA20251202456), Nov 29, 2025: LAMP. INOPERATIVE. DURING L/O CHK FOUND RIGHT AFT OVERWING DOOR EMERGENGY LIGHT INOP. RELAMPED RT AFT OVERWING EMERGENCY LIGHT IAW AMM 33-51-04-960-801. NO HELP. RELAMPED RT AFT O
- [SDR SCNA20251111435](https://openairdocs.org/sdr/SCNA20251111435), Nov 10, 2025: OVEN. DIRTY. AFT GALLEY OVEN OVERLY DIRTY CREATTTES FUMES WHEN COOKING - CATERING NOTIFIED TO CHANGE OUT INSERS
- [SDR SCNA20251104430](https://openairdocs.org/sdr/SCNA20251104430), Nov 4, 2025: VIEW PORT. UNSECURE. 2R DOOR SLIDE COMPARTMENT WINDOW IS BROKEN. R2 SLIDE WINDOW NO DEFECTS. R1 SLIDE WINDOW UNSECURE. READHEARED R1 SLIDE WINDOW REF AMM 20-30-11
- [SDR SCNA20251103428](https://openairdocs.org/sdr/SCNA20251103428), Nov 2, 2025: GLOWSTRIP. DAMAGED. SELF ILLUMINATING FLOOR PATH AT 20 DEF DAMAGED REMOVED AND REPLACED SELF ILLUMINATING FLOOR PATH AT 20 DEF REF AMM 33-51-16
- [SDR SCNA20250918380](https://openairdocs.org/sdr/SCNA20250918380), Sep 15, 2025: WIRE. DETACHED. CABIN SEAT 13D SEAT BACK HAS SHARP WIRE POCKING OUT BEHIND. REATTACHED WIRE TO SEAT POCKET BRACKET. REF AMM 25-22-00.
- [SDR SCNA20250619220](https://openairdocs.org/sdr/SCNA20250619220), Jun 18, 2025: BUTTON. INOPERATIVE. DEFECT 788705: LEFT REAR LAV EMERGENCY CALL BUTTON INOP. - - RESOLUTION: RELAMPED LEFT REAR LAV CALL LIGHT.REF AMM 33-27-00. OK FOR SERVICE.
- [SDR SCNA20250612207](https://openairdocs.org/sdr/SCNA20250612207), Jun 12, 2025: BOLT. LOOSE. 2L DOOR BOLTS ON BOTH SIDES OF SLIDE APPEAR LOOSE. - RESOLUTION: CHECKED TORQUE ON AFT SLIDES (MOUNT BOLTS) OK FOR SERVICE AMM REF: 25-66-21.
- [SDR SCNA20250414111](https://openairdocs.org/sdr/SCNA20250414111), Apr 11, 2025: SLIDE. DISLODGED. R1 DOOR SLIDE PACK FALLING OUT. - REPACKED 1R DOOR SLIDE PER AMM 25-66-00.
- [SDR SCNA20250410109](https://openairdocs.org/sdr/SCNA20250410109), Apr 9, 2025: WIRE HARNESS. CROSSED. WORK ORDER 94469, NR00004: 15 ABC EMERGENCY EXIT LIGHT INOP. - RESOLUTION: REMOVED AND REPLACED 15 ABC EMERGENCY EXIT LIGHT AND FOUND THE WIRING HARNESS CROSSED
- [SDR SCNA20250116015S](https://openairdocs.org/sdr/SCNA20250116015S), Jan 13, 2025: LIGHT. NOT REPORTED. REPLACED PAX CABIN OVERHEAD BIN EMERGENCY LIGHTS IAW B737-8 AMM TASK, 33-51-03-960-802 PAR 3.D STEP (1) THRU (5) AND STEP (7) REV 85 DATED 10-15-2024.
- [SDR SCNA20250116015](https://openairdocs.org/sdr/SCNA20250116015), Jan 13, 2025: LIGHT. BROKEN. WORK ORDER 88096, NR00114: PAX CABIN OVERHEAD BIN WITH EMERGENCY LIGHTS BROKEN AT BIN POSITION 4R,6L,5L. RESOLUTION: (IN PROGRESS)
- [SDR SCNA20250131040](https://openairdocs.org/sdr/SCNA20250131040), Jan 7, 2025: SKIN. WORN. RH WING, SLAT #7 ACTUATOR AREA, FIXED LEADING EDGE WITH WEAR. RESOLUTION: PERFORMED PERMANENT REPAIR AT RH WING SLAT #7 ACTUATOR AREA FIXED L/E IAW B737-800 SRM
- [SDR SCNA20250131039](https://openairdocs.org/sdr/SCNA20250131039), Jan 7, 2025: STRUCTURE. WORN. RH WING, SLAT #4 ACTUATOR AREA, FIXED LEADING EDGE WITH WEAR. PERFORMED PERMANENT REPAIR AT R/H WING SLAT #8 ACTUATOR AREA FIXED L/E IAW B737-800 SRM 57-41-01-2
- [SDR SCNA20250108008](https://openairdocs.org/sdr/SCNA20250108008), Jan 7, 2025: LIGHT. BROKEN. UPPER SIDE, PAX CABIN GENERAL PHOTOLUMINESCENT FLOOR PATH MARKING BROKEN IN SEVERAL PLACE (10EA). RESOLUTOIN:
- [SDR SCNA20241230407](https://openairdocs.org/sdr/SCNA20241230407), Dec 25, 2024: SLIDE. UNPACKED. DEFECT 798889: GIRT BAR NOT DISARMED PRIOR TO FWD DOOR OPENING . SLIDE FELL OUT OF PACK HALF WAY BUT DID NOT DEPLOY. RESOLUTION: REINSTALLED SLIDE REF AMM 25-66
- [SDR SCNA20241202379](https://openairdocs.org/sdr/SCNA20241202379), Nov 27, 2024: GIRT BAR. LOOSE. L1 GIRT BAR IS LOOSE IN HOLDER. ADJUSTED CLAMP ON GIRT BAR ON L1 DOOR SLIDE RED AMM 25-66-02 OK FOR SERVICE.
- [SDR SCNA20241028346](https://openairdocs.org/sdr/SCNA20241028346), Oct 27, 2024: INDICATION SYS. MALFUNCTIONED. DEFECT 778180: FA REPORTS R2 LAV EMERGANCY RETURN LIGHT INOP ( PASSENGER LIGHTED INFORMATION SIGNS AND NOTICE SYSTEM; “NO SMOKING/FASTEN SEAT BELT/RETURN TO SEA
- [SDR SCNA20240716273](https://openairdocs.org/sdr/SCNA20240716273), Jul 12, 2024: CONTROLLER. FAILED. PRESSURIZATION AUTO FAIL AT 50KTS ( CABIN PRESSURE CONTROL SYSTEM; AUTOMATIC MODES. (PRESSURIZED) ). R/R #1 CABIN PRESS CONTROLLER REF AMM 21-31-11, OPS CHECKS 
- [SDR SCNA20240702262](https://openairdocs.org/sdr/SCNA20240702262), Jun 29, 2024: CHARGER. FAILED. EMERGENCY INTERIOR LIGHTS (6,9,11) FAILED OPERATION. R&R BATTERY PACK AT ROW 8ABC REF AMM 33-51-06. NO HELP. SUSPECT POWER SUPPLY. REPLACED CHARGER AND BATTERY 
- [SDR SCNA202405170243](https://openairdocs.org/sdr/SCNA202405170243), May 21, 2024: SLIDE. DISLODGED. DURING OPENING OF L1 DOOR L1 SLIDE FELL PARTLY OUT OF CONTAINER. REMOVED, REPLACED, AND REINSTALLED L1 DOOR SLIDE IAW AMM 25-66-01
- [SDR SCNA20240424196](https://openairdocs.org/sdr/SCNA20240424196), Apr 22, 2024: IDG. FAULTED. DRIVE LIGHT ILLUMINATED ON #2 ENGINE- FOUND IDG FAULT ON #2 GCU REMOVED AND REPLACED #2 ENG IDG IAW AMM 24-11-11 OPS CHECKED GOOD. APU AUTO SHUTDOWN IN FLIGHT (
- [SDR SCNA20231129241](https://openairdocs.org/sdr/SCNA20231129241), Nov 28, 2023: UNKNOWN. UNKNOWN. DEFECT - W/O 83388 NRC-10: L-1 DOOR SLIDE NOT INSTALLED PROPERLY, LOWER SUPORT PIN NOT ENGAGED. - RESOLUTION: REMOVED AND REINSTALLED SLIDE BUSSEL ASSY. REF AMM
- [SDR SCNA20231011233](https://openairdocs.org/sdr/SCNA20231011233), Oct 8, 2023: UNKNOWN. UNKNOWN. TRAILING EDGE FLAP ASYMMETRY. NEEDLE POSITION L=1/ R=2. POSITION AT LOCKOUT WAS 1. NO ROLL WAS FELT. NO LAGGING. SPLIT WAS MINOR FLAPS WERE MOVED TO 5. NEEDLES 
- [SDR SCNA202310112321](https://openairdocs.org/sdr/SCNA202310112321), Oct 8, 2023: UNKNOWN. UNKNOWN. TRAILING EDGE FLAP ASYMMETRY. NEEDLE POSITION L=1/ R=2. POSITION AT LOCKOUT WAS 1. NO ROLL WAS FELT. NO LAGGING. SPLIT WAS MINOR FLAPS WERE MOVED TO 5. NEEDLES 
- [SDR SCNA20230718203](https://openairdocs.org/sdr/SCNA20230718203), Jul 16, 2023: UNKNOWN. UNKNOWN. DEFECT 702131: DOOR 2L PARTIALLY OPENED WITH SLIDE ARMED. - - - RESOLUTION: PERFORMED ESCAPE SLIDE PACK CHECK ON 2L DOOR SLIDE. REF AMM 25-66-02. NO DEFECTS NOT
- [SDR SCNA20230627196](https://openairdocs.org/sdr/SCNA20230627196), Jun 26, 2023: UNKNOWN. UNKNOWN. DEFECT 702104: ALL FA INTERPHONES SHOCKED FA'S WHILE IN USE. - - - RESOLUTION: PERFORMED OPS CHECK IAW AMM 23-31-00. OPS CHECK NORMAL. OK TO CONTINUE SVC.
- [SDR SCNA20230606176](https://openairdocs.org/sdr/SCNA20230606176), May 31, 2023: WEB. WORN. DEFECT NR00129: E&E COMPARTMENT DOOR CUTOUT FRAME LH WEB HAS WEAR MARKS. - - - RESOLUTION: REMOVED AND REPLACED E&E BAY DOOR CUTOUT LH WEB WITH NEW LOT # 504774
- [SDR SCNA20230606175](https://openairdocs.org/sdr/SCNA20230606175), May 29, 2023: FRAME. UNKNOWN. DEFECT NR00065: E&E COMPARTMENT DOOR CUTOUT FRAME RH HAVE MARKS, (MARKED). - - - RESOLUTION: REMOVED AND REPLACED RH E&E COMPARTMENT DOOR CUTOUT FRAME WITH NEW 
- [SDR SCNA20230412121](https://openairdocs.org/sdr/SCNA20230412121), Apr 10, 2023: UNKNOWN. UNKNOWN. DEFECT 742110: L1 DOOR SLIDE GIRT BAR RETAINING LOOP LOOSE. REMOVED AND REPLACED RETAINING LOOP FASTENER REF SRM 51-40-00 REMOVED AND REPLACED L1 SLIDE REF AMM 
- [SDR SCNA20230404119](https://openairdocs.org/sdr/SCNA20230404119), Mar 28, 2023: UNKNOWN. UNKNOWN. DEFECT 700991: ASSSEMETRYTRAILING EDGE FLAPS AT LESS THAN 2 DEGREES ON APPROCH TO MSP RAN QRH LANDED NORMALLY. - - - RESOLUTION: TRANSFERRED TO W/O 77861 N/R000
- [SDR SCNA20230103002](https://openairdocs.org/sdr/SCNA20230103002), Dec 30, 2022: SEAL. OUT OF ADJUST. CREW UNABLE TO PRESSURIZE CABIN AFTER TAKEOFF. EMERGENCY DECLARED. OVERWEIGHT LANDING WITH SMOOTH TOUCHDOWN AT 161.4. ADJUSTED L1 DOOR LWR FLAPPER SEAL IAW AMM 
- [SDR SCNA20220802088](https://openairdocs.org/sdr/SCNA20220802088), Jul 29, 2022: SLIDE. INOPERATIVE. DEFECT: L1 DOOR SLIDE FELL OUT OF CASE RESOLUTION: RE-INSTALLED L1 SLIDE IN ACCORDANCE WITH AMM 25-66-00.
- [SDR SCNA20210205041](https://openairdocs.org/sdr/SCNA20210205041), Feb 2, 2021: FAIRING. DAMAGED. NUMBER 6 AFT FLAP FAIRING LEADING EDGE IS DAMAGED. REPAIRED NR 6 AFT FLAP FAIRING LEADING EDGE IAW SCA EA 57-0059 AND ATS ER 21-01119 REV IR.
- [SDR SCNA20210205037](https://openairdocs.org/sdr/SCNA20210205037), Feb 1, 2021: TORQUE TUBE. WORN. RIGHT INBOARD MAIN FLAP HAS WEAR ON UPPER AND LOWER SURFACES OF TORQUE TUBE ABOUT 3" OUTBOARD OF INBOARD CARRIAGE. REPAIRED RT IB MAIN FLAP TORQUE TUBE UPPER AN
- [SDR SCNA20210205043](https://openairdocs.org/sdr/SCNA20210205043), Jan 30, 2021: PANEL. ERODED. LH AFT MODULATION PANEL HAS WIND EROSION. REPAIRED WIND EROSION ON LH AFT MODULATION PANEL IAW SRM 51-70-05-2R-6
- [SDR SCNA20210205042](https://openairdocs.org/sdr/SCNA20210205042), Jan 28, 2021: FAIRING. DAMAGED. RIGHT WING FLAP TRACK FAIRING NR 6 HAS BULB SEAL RETAINER FASTENERS PULLING THOUGH SKIN. REPAIRED SKIN AT BULB SEAL RETAINER FASTENERS ON RT WING FLAP TRACK FAI
- [SDR SCNA20210205039](https://openairdocs.org/sdr/SCNA20210205039), Jan 28, 2021: PANEL. DELAMINATED. WTB PANEL 193AR HAS DELAMINATION AT UPPER AFT EXTERIOR SURFACE. REPAIRED DELAMINATION AREA AT UPPER AFT EXTERIOR SURFACE OF WTB PANEL 193AR PER SRM 53-40-70-2R-
- [SDR SCNA20210205040](https://openairdocs.org/sdr/SCNA20210205040), Jan 26, 2021: FAIRING. ERODED. LEFT WING FLAP TRACK FWD FAIRING 543AB HAS WIND EROSION AROUND AFT ATTACH HOLES. REPAIRED WIND EROSION AROUND AFT ATTACH HOLES ON LT WING FLAP TRACK FWD FAIRING
- [SDR SCNA20210205035](https://openairdocs.org/sdr/SCNA20210205035), Jan 26, 2021: SKIN PANEL. WORN. NUMBER 2 ENGINE PYLON PANEL 441ER OUTER SURFACE HEAVILY WORN. BLENDED NR 2 ENGINE PYLON PANEL 441ER OUTER SURFACE MIN. REMAINING THICKNESS IS .090 FOLLOWED INST
- [SDR SCNA20210205038](https://openairdocs.org/sdr/SCNA20210205038), Jan 22, 2021: FLAP. DELAMINATED. RIGHT INBOARD MAIN FLAP DELAMINATED AT TRAILING EDGE NEAR OUTBOARD END. REPAIRED DELAMINATION AT TRAILING EDGE NEAR OUTBOARD END ON RT INBOARD MAIN FLAP IAW SRM
- [SDR SCNA20210205036](https://openairdocs.org/sdr/SCNA20210205036), Jan 22, 2021: BELLCRANK. WORN. LEFT INBD FLAP CABLE OUTBOARD BELL CRANK WORN AT CABLE ATTACH POINTS. REPAIRED LT IB FLAP OB BELLCRANK AT CABLE ATTACH POINT PER SCA EA 57-0058 REV 00 AND ATS E

All 174: https://openairdocs.org/aircraft/N814SY/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 CFM56-7B24 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 737-8BK aircraft: https://openairdocs.org/model/boeing-737-8bk/aircraft.md
- The CFM International CFM56-7B24 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b24-series.md

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