# N809SY: 2005 Boeing 737-8Q8

- Status: Valid registration
- Airframe: [Boeing 737-8Q8](https://openairdocs.org/model/boeing-737-8q8) (registry code 13844BX, 189 seats)
- Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802)
- Serial number: 30683
- Year built: 2005
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 22, 2005
- Certificate issued: January 28, 2020
- Expires: January 31, 2030
- Mode S code: AB04F3
- 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=809SY
- Page: https://openairdocs.org/aircraft/N809SY

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 model are included.

## ADs that may apply (OpenAirDocs): 55 in force

### Matched by airframe (Boeing 737-8Q8)

None in force.

### Matched by engine (CFM International CFM56 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 2017-14-08](https://openairdocs.org/ad/2017-14-08): Turbine Engine Compressor Section · CFM International CFM56-3, CFM56-3B and CFM56-3C. Effective Aug 18, 2017
- [AD 2017-05-09](https://openairdocs.org/ad/2017-05-09): Accessory Gearboxes · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 33 more. Effective Apr 13, 2017
- [AD 2016-14-10](https://openairdocs.org/ad/2016-14-10): High-pressure turbine (HPT) disks · CFM International CFM56-3, CFM56-3B and CFM56-3C with STC SE00034EN. Effective Aug 9, 2016
- [AD 2016-02-04](https://openairdocs.org/ad/2016-02-04): Turbine rear frames (TRFs) · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 33 more. Effective Mar 1, 2016
- [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 2013-14-06](https://openairdocs.org/ad/2013-14-06): Hydro-mechanical unit (HMU) fuel control · CFM International CFM56-5, CFM56-5B1, CFM56-5B1/2P and 34 more. Effective Sep 3, 2013
- [AD 2012-02-03](https://openairdocs.org/ad/2012-02-03): Engine · CFM International CFM56-5B1/3, CFM56-5B2/3, CFM56-5B3/3 and 8 more. Effective Mar 15, 2012
- [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 2010-12-03](https://openairdocs.org/ad/2010-12-03): Fan blades · CFM International CFM56-3 and CFM56-3B. Effective Jul 13, 2010
- [AD 2010-09-14](https://openairdocs.org/ad/2010-09-14): Exhaust gas temperature (EGT) · CFM International CFM56-5B1/2P, CFM56-5B1/P, CFM56-5B2/2P and 16 more. Effective Jun 8, 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 2009-18-01](https://openairdocs.org/ad/2009-18-01): LP turbine rear frames · CFM International CFM56-5B1/3, CFM56-5B1/P, CFM56-5B2/3 and 19 more. Effective Oct 1, 2009
- [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 2007-24-04](https://openairdocs.org/ad/2007-24-04): Low pressure turbine (LPT) · CFM International CFM56-5C4/1. Effective Dec 6, 2007
- [AD 2007-03-15](https://openairdocs.org/ad/2007-03-15): Exhaust gas temperature (EGT) harness · CFM International CFM56-5, CFM56-5B1, CFM56-5B1/2P and 34 more. Effective Mar 19, 2007
- [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 2005-10-05](https://openairdocs.org/ad/2005-10-05): Air turbine starters · CFM International CFM56-5, CFM56-5B1, CFM56-5B1/2P and 50 more. Effective Jun 14, 2005
- [AD 97-09-02 R3](https://openairdocs.org/ad/97-09-02-R3): High pressure turbine rotor (HPTR) front shafts · CFM International CFM56-5C2, CFM56-5C3/G and CFM56-5C4. Effective Oct 14, 2004
- [AD 2004-10-13](https://openairdocs.org/ad/2004-10-13): Service main fuel pumps · CFM International CFM56-3, CFM56-5, CFM56-5-A1/F and 4 more. Effective Jun 24, 2004
- [AD 2002-22-12](https://openairdocs.org/ad/2002-22-12): Titeflex hoses · BAE Systems ATP, Avro 146-RJ100A, Avro 146-RJ70A and 122 more. Effective Dec 13, 2002
- [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 2002-02-13](https://openairdocs.org/ad/2002-02-13): Magnetic Drain Plug · CFM International CFM56-5, CFM56-5-A1/F, CFM56-5A4 and 33 more. Effective Mar 21, 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 2001-09-17](https://openairdocs.org/ad/2001-09-17): Fuel Manifold and CJ9L Harness · CFM International CFM56-5C2, CFM56-5C2/4, CFM56-5C2/F and 13 more. Effective May 14, 2001
- [AD 2001-04-06](https://openairdocs.org/ad/2001-04-06): Fan Disk · CFM International CFM56-3, CFM56-3B and CFM56-3C. Effective Apr 4, 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 2000-15-01](https://openairdocs.org/ad/2000-15-01): Fuel Leakage · CFM International CFM56-2, CFM56-2A, CFM56-2B and 39 more. Effective Oct 2, 2000
- [AD 2000-05-22](https://openairdocs.org/ad/2000-05-22): CFM International CFM56-2, CFM56-2A, CFM56-2B and 3 more. Effective May 2, 2000
- [AD 99-06-16](https://openairdocs.org/ad/99-06-16): High Pressure Turbine Rotor (HPTR) Front Air Seal · CFM International CFM56-5, CFM56-5-A1/F, CFM56-5A4 and 3 more. Effective Apr 21, 1999
- [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
- [AD 98-19-10](https://openairdocs.org/ad/98-19-10): Accessory Gearbox · CFM International CFM56-3, CFM56-3B and CFM56-3C. Effective Sep 28, 1998
- [AD 98-12-32](https://openairdocs.org/ad/98-12-32): High Pressure Turbine Rotor Disks · CFM International CFM56-2, CFM56-2A, CFM56-2B and 3 more. Effective Jul 20, 1998
- [AD 98-10-11](https://openairdocs.org/ad/98-10-11): Accessory Gearbox · CFM International CFM56-3, CFM56-3B, CFM56-3C and 31 more. Effective Jun 3, 1998
- [AD 98-07-02](https://openairdocs.org/ad/98-07-02): Air/oil Seal · CFM International CFM56-3, CFM56-3B and CFM56-3C. Effective Mar 30, 1998
- [AD 98-02-04](https://openairdocs.org/ad/98-02-04): Low Pressure Turbine Case · CFM International CFM56-5B1/2P, CFM56-5B2/2P, CFM56-5B3/2P and 1 more. Effective Mar 23, 1998
- [AD 89-23-06 R1](https://openairdocs.org/ad/89-23-06-R1): Magnetic Chip Detector · CFM International CFM56-2, CFM56-2A, CFM56-3 and 8 more. Effective Jan 28, 1998
- [AD 97-08-01](https://openairdocs.org/ad/97-08-01): Fan Disks · CFM International CFM56-3, CFM56-3B and CFM56-3C. Effective Jun 23, 1997
- [AD 97-06-01](https://openairdocs.org/ad/97-06-01): High Pressure Compressor Rotor (HPCR) Stage 1-2 Spool · CFM International CFM56-5, CFM56-5B1, CFM56-5B1/2P and 28 more. Effective Jun 3, 1997
- [AD 97-05-13](https://openairdocs.org/ad/97-05-13): Air Turbine Engine Starter · CFM International CFM56-5, CFM56-5-A1/F, CFM56-5A4 and 3 more. Effective Jun 3, 1997
- [AD 96-25-11](https://openairdocs.org/ad/96-25-11): Redesigned Fan Blades · CFM International CFM56-3B and CFM56-3C. Effective Jan 29, 1997

### 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 2013-02-02](https://openairdocs.org/ad/2013-02-02) (historical): High-pressure turbine (HPT) disks · CFM International CFM56-3, CFM56-3B and CFM56-3C with STC SE00034EN. Effective Jan 28, 2013
- [AD 2009-01-01](https://openairdocs.org/ad/2009-01-01) (historical): Exhaust gas temperature (EGT) · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 22 more. Effective Dec 31, 2008
- [AD 97-09-02 R2](https://openairdocs.org/ad/97-09-02-R2) (historical): Low pressure turbine rotor (LPTR) · CFM International CFM56-5C2, CFM56-5C2/4, CFM56-5C2/F and 9 more. Effective Apr 29, 2003
- [AD 2003-02-04](https://openairdocs.org/ad/2003-02-04) (historical): Exhaust gas temperature (EGT) · CFM International CFM56-5 Series (all). Effective Feb 27, 2003
- [AD 97-09-02 R1](https://openairdocs.org/ad/97-09-02-R1) (historical): High Pressure Turbine rotor (HPTR) front shaft · CFM International CFM56-5C2/G, CFM56-5C2/G4, CFM56-5C3/G and 3 more. Effective Sep 24, 2002
- [AD 2001-17-14](https://openairdocs.org/ad/2001-17-14) (historical): LPT Conical Supports · CFM International CFM56-5C4/1. Effective Sep 7, 2001
- [AD 2001-08-51](https://openairdocs.org/ad/2001-08-51) (historical): Fuel leakage · CFM International CFM56-5 Series (all)
- [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
- [AD 99-08-16](https://openairdocs.org/ad/99-08-16) (historical): CFM International CFM56-2, CFM56-2A, CFM56-2B and 3 more. Effective May 13, 1999
- [AD 97-09-02](https://openairdocs.org/ad/97-09-02) (historical): High/Low Pressure Turbine Rotor · CFM International CFM56-5C2/G, CFM56-5C2/G4, CFM56-5C3/G and 3 more. Effective Jun 30, 1997

All 71: https://openairdocs.org/aircraft/N809SY/ads.md

## Information bulletins (advisory) (4 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-13-33R2](https://openairdocs.org/saib/NE-13-33R2): Turbine Engine Air Inlet Section - LP Turbine, Stage 1 Nozzle Vanes. Issued Jan 28, 2014
- [SAIB NE-12-29](https://openairdocs.org/saib/NE-12-29): Engine Fuel Distribution  CFM56-5B LPTACC Fuel Manifold. Issued Apr 27, 2012
- [SAIB NE-06-02](https://openairdocs.org/saib/NE-06-02): . Issued Oct 18, 2005
- [SAIB NE-13-33R1](https://openairdocs.org/saib/NE-13-33R1) (historical): Turbine Engine Air Inlet Section - LP Turbine, Stage 1 Nozzle Vanes. Issued Jun 24, 2013
- [SAIB NE-13-33](https://openairdocs.org/saib/NE-13-33) (historical): Turbine Engine Air Inlet Section - LP Turbine, Stage 1 Nozzle Vanes. Issued May 13, 2013
- [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 N809SY.

## 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 20130406004239I](https://openairdocs.org/incident/20130406004239I), Apr 6, 2013: Boeing 737-8Q8 (N809SY), Minneapolis, MN, Minor damage. Aircraft struck 2 or 3 ducks on climb out from msp. Crew did not declare an emergency. Flight returned to msp without any further incident. Number 2 engine was…

## Service difficulty reports (219, 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 SCNA20260713295](https://openairdocs.org/sdr/SCNA20260713295), Jul 12, 2026: A/C PACK. ODOR. FLIGHT ATTENDANTS REPORT STRONG BURNING ELECTRICAL ON THE GROUND AFTER LANDING IN AFT GALLEY. FOUND RIGHT PACK INOP TURNED PACK OFF SMELL DISAPATED ACFT OK FOR 
- [SDR SCNA20260316122](https://openairdocs.org/sdr/SCNA20260316122), Mar 13, 2026: SIGN. DETACHED. EMERGENCY EXIT SIGN FELL OFF. ATTACHED THE DISLOCATED EXIT SIGN IAW AMM 33-51-01.
- [SDR SCNA20260306110](https://openairdocs.org/sdr/SCNA20260306110), Mar 5, 2026: BATTERY PACK. NO TEST. EMERGENCY LIGHTS FAILED AFTER 6MIN OPERATION IN ROWS 15 THROUGH 22 AND EMERGENCY DOOR R2.. REPLACED EMERGENCY BATTERY PACK M1671 REF AMM 33-51-06
- [SDR SCNA20251215491](https://openairdocs.org/sdr/SCNA20251215491), Nov 21, 2025: FRAME. CRACKED. CRACK ON FRAME STA 312 & S-6L AT PASSENGER CABIN FWD ENTRY DOOR. EMP 201533743 - CRACK ON FRAME STA 312 & S-6L AT PASSENGER CABIN FWD ENTRY DOOR WAS REPAIRED PE
- [SDR SCNA20251215490](https://openairdocs.org/sdr/SCNA20251215490), Nov 21, 2025: ANGLE. CRACKED. CRACKED ANGLE OF INTERCOSTAL STA 500H+1 BTW STRG 25R /26R AT FWD CARGO COMPARMENT. EMP 201954011 - ANGLE OF INTERCOSTAL STA 500H+1 BTW STRG 25R /26R AT FWD CARG
- [SDR SCNA20251215489](https://openairdocs.org/sdr/SCNA20251215489), Nov 21, 2025: ANGLE. CRACKED. CRACKED ANGLE OF INTERCOSTAL BS 500G -1 BTW S25 - 26R IN FWD CARGO. THE ANGLE OF INTERCOSTAL WAS REPLACED IAW SRM 51-40-02-0G-0.
- [SDR SCNA20251215488](https://openairdocs.org/sdr/SCNA20251215488), Nov 21, 2025: ANGLE. CRACKED. CRACKED ANGLE OF INTERCOSTAL BS 500G BTW S25-26L AT FWD CARGO. THE ANGLE OF INTERCOSTAL WAS REPLACED IAW SRM 51-40-02-0G-0.
- [SDR SCNA20251215487](https://openairdocs.org/sdr/SCNA20251215487), Nov 21, 2025: ANGLE. CRACKED. CRACKED ANGLE OF INTERCOSTAL BS 500F BTW S25-26L AT FWD CARGO COMPARMENT. ANGLE OF INTERCOSTAL BS 500F BTW S25-26L AT FWD CARGO WAS REPLACED IAW SRM 51--40-02-0
- [SDR SCNA20251210476](https://openairdocs.org/sdr/SCNA20251210476), Nov 21, 2025: INTERCOSTAL. CRACKED. CRACKED ANGLE OF INTERCOSTAL STA 500I LBL 3 AT ZONE OF AIR CONDITIONING DISTRIBUTION BAY. ANGLE OF INTERCOSTAL STA 500I LBL 3 AT ZONE OF AIR CONDITIONING WAS RE
- [SDR SCNA20251210475](https://openairdocs.org/sdr/SCNA20251210475), Nov 21, 2025: INTERCOSTAL. CRACKED. CRACKED ANGLE OF INTERCOSTAL STA 500I RBL 3 AT ZONE OF AIR CONDITIONING DISTRIBUTION BAY - EMP 200001336 - ANGLE OF INTERCOSTAL STA 500I RBL 3 AT ZONE OF AIR CO
- [SDR SCNA20251210474](https://openairdocs.org/sdr/SCNA20251210474), Nov 21, 2025: INTERCOSTAL. CRACKED. CRACKED ANGLE OF INTERCOSTAL STA 500G +1 BTW STRG 25R /26R AT FWD CARGO COMPARMENT. - EMP 200001336 - ANGLE OF INTERCOSTAL STA 500G +1 BTW STRG 25R/26R AT FWD C
- [SDR SCNA20251210473](https://openairdocs.org/sdr/SCNA20251210473), Nov 21, 2025: ANGLE. CRACKED. CRACKED ANGLE OF INTERCOSTAL STA 500H -1 BTW STRG 25RL/26L AT FWD CARGO COMPARMENT. CRACKED ANGLE OF INTERCOSTAL STA 500H -1 BTW STRG 25L/26L AT FWD CARGO COMPA
- [SDR SCNA20251210472](https://openairdocs.org/sdr/SCNA20251210472), Nov 21, 2025: ANGLE. CRACKED. CRACKED ANGLE OF INTERCOSTAL STA 500H+1 BTW STRG 25L /26L AT FWD CARGO COMPARMENT. CRACKED ANGLE OF INTERCOSTAL STA 500H+1 BTW STRG 25L /26L AT FWD CARGO COMPAR
- [SDR SCNA20251119445S](https://openairdocs.org/sdr/SCNA20251119445S), Nov 18, 2025: RETAINER. LOOSE. LOOSE FASTENERS ON GIRT BAR RETAINER CLIPS OF EMERGENCY ESCAPE SLIDE AT FWD PASSENGER L1. FASTENERS ON GIRT BAR RETAINER CLIPS OF EMERGENCY ESCAPE SLIDE AT FWD 
- [SDR SCNA20251119446](https://openairdocs.org/sdr/SCNA20251119446), Nov 18, 2025: GLOWSTRIP. DIRTY. REMOVE & INSTALL AND CLEAN PHOTOLUMINESCENT FLOOR PROXIMITY STRIPS AND REPLACE AS REQUIRED. OPEN
- [SDR SCNA20251119445](https://openairdocs.org/sdr/SCNA20251119445), Nov 18, 2025: RETAINER. LOOSE. LOOSE FASTENERS ON GIRT BAR RETAINER CLIPS OF EMERGENCY ESCAPE SLIDE AT FWD PASSENGER L1. OPEN
- [SDR SCNA20251023405](https://openairdocs.org/sdr/SCNA20251023405), Oct 21, 2025: FUSE. INOPERATIVE. FWD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE LT SIDE. REMOVED AND REPLACED POWER SUPPLY FUSE FOR L/H FORWARD EXIT DOOR EMERGENCY LIGHT. OPS CHECKS GOOD. REF AM
- [SDR SCNA20250701238](https://openairdocs.org/sdr/SCNA20250701238), Jun 29, 2025: LIGHT. INOPERATIVE. RIGHT BULLNOSE EMERGENCY LIGHTS 1, 2, AND 4 INOPERATIVE. INTERIOR EMERGENCY EXIT LIGHTING SYSTEM; EMERGENCY AISLE LIGHTS. REMOVED AND REPLACED RH BULLNOSE LIGHT
- [SDR SCNA20250623223](https://openairdocs.org/sdr/SCNA20250623223), Jun 22, 2025: LIGHT. INOPERATIVE. DEFECT 701451: R/H BULLNOSE EMER LIGHTS 1, 2, AND 4 INOP ( INTERIOR EMERGENCY EXIT LIGHTING SYSTEM; EMERGENCY AISLE LIGHTS ) . REMOVED AND REPLACED RH BULLNOSE 
- [SDR SCNA20250623222](https://openairdocs.org/sdr/SCNA20250623222), Jun 21, 2025: WIRE. BROKEN. DEFECT 796449: FOUND SEVERAL EMER LIGHTS INOP WHILE PERFORMING TASK CARD 330100000 - -RESOLUTION: REPAIRED BROKEN WIRE AND REINSERTED WIRE INTO GROUND BLOCK GD0
- [SDR SCNA20250619219](https://openairdocs.org/sdr/SCNA20250619219), Jun 18, 2025: COVER. BROKEN. DEFECT 796445: EMERGENCY LIGHT COVER SIGN BROKEN AND FALLING OUT OF MOUNT. MC NOTIFIED DG 6199. - - RESOLUTION: REPLACED EMERGENCY LIGHT ASSY IAW AMM 33-51-01-9
- [SDR SCNA20250312071](https://openairdocs.org/sdr/SCNA20250312071), Mar 10, 2025: BATTERY PACK. NO TEST. WORK ORDER 93714 N/R-00006: EMERGENCY LIGHTS AT AFT EXIT DOORS & OVERWING EXIT DOORS FAILED CAPACITY CHECK. RETEST AFTER 3/10 1730 AMM 33-51-06-200-801 STEP 5. 
- [SDR SCNA20250309069](https://openairdocs.org/sdr/SCNA20250309069), Mar 9, 2025: LAMP. OUT OF ADJUST. DEFECT 734633: OUTSIDE EMERGENCY LIGHTS AT FWD SERVICE DOOR & FWD LEFT OVERWING EXIT INOP. - - RESOLUTION: ADJUSTED LAMP IAW AMM 33-51-04 AT FWD SERVICE DOOR & 
- [SDR SCNA20241203391](https://openairdocs.org/sdr/SCNA20241203391), Nov 20, 2024: FLOORBEAM. CORRODED. UPPER FUSELAGE PASSENGER CABIN AREA, W/L 207, AT FLOOR BEAM ON STA 947.5 AND LBL 49, WITH CORROSION. FOUND DURING WORK PROCESS WITH N.R.I 2-14. PERFORMED PERMAN
- [SDR SCNA20241206393](https://openairdocs.org/sdr/SCNA20241206393), Nov 7, 2024: BAFFLE. CRACKED. LOWER FUSELAGE FWD CARGO COMPARTMENT BETWEEN STA 500B-500C, RBL 24" INTERCOSTAL WITH CRACK. NOTE: IT WAS FOUND DURING THE REMOVAL OF FLOOR CHANNEL WITH NRI 1-34
- [SDR SCNA20241203387](https://openairdocs.org/sdr/SCNA20241203387), Nov 6, 2024: BAFFLE. CRACKED. LOWER FUSELAGE FWD CARGO COMPARTMENT BETWEEN STA 500B-500C, RBL 24" INTERCOSTAL WITH CRACK. NOTE: IT WAS FOUND DURING THE REMOVAL OF FLOOR CHANNEL WITH NRI 1-34
- [SDR SCNA20241203386](https://openairdocs.org/sdr/SCNA20241203386), Nov 6, 2024: BAFFLE. CRACKED. LOWER FUSELAGE FWD CARGO COMPARTMENT BETWEEN STA 500A-500B, RBL 24" INTERCOSTAL WITH CRACK. NOTE: IT WAS FOUND DURING THE REMOVAL OF FLOOR CHANNEL WITH NRI 1-34
- [SDR SCNA20241202384](https://openairdocs.org/sdr/SCNA20241202384), Nov 6, 2024: INTERCOSTAL. CRACKED. LOWER FUSELAGE FWD CARGO COMPARTMENT BETWEEN STA 500A-500B, RBL 24" INTERCOSTAL WITH CRACK. NOTE: IT WAS FOUND DURING THE REMOVAL OF FLOOR CHANNEL WITH NRI 1-34
- [SDR SCNA20241202383](https://openairdocs.org/sdr/SCNA20241202383), Nov 6, 2024: INTERCOSTAL. CRACKED. WORK ORDER 80719, N/R00114: EMP# 9892 LOWER FUSELAGE FWD CARGO COMPARTMENT BETWEEN STA 500A-500B, RBL 24" INTERCOSTAL WITH CRACK. NOTE: IT WAS FOUND DURING THE 
- [SDR SCNA20241202381S](https://openairdocs.org/sdr/SCNA20241202381S), Nov 6, 2024: INTERCOSTAL. CRACKED. SUPPLEMENTAL: CORRECTION: (** NOTE WEBSITE TIMED OUT **) WORK ORDER 80719, NR00116: EMP# 9892 LOWER FUSELAGE FWD CARGO COMPARTMENT BETWEEN STA 500C-500D, RBL 24
- [SDR SCNA20241202381](https://openairdocs.org/sdr/SCNA20241202381), Nov 6, 2024: INTERCOSTAL. CRACKED. LOWER FUSELAGE FWD CARGO COMPARTMENT BETWEEN STA 500C-500D, RBL 24" INTERCOSTAL WITH CRACK. NOTE: IT WAS FOUND DURING THE REMOVAL OF FLOOR CHANNEL WITH NRI 1-34
- [SDR SCNA20241107358](https://openairdocs.org/sdr/SCNA20241107358), Nov 5, 2024: SMOKE DETECTOR. BROKEN. WORK ORDER 80721 NR00020: FWD ENTRY AREA FWD LAVATORY SMOKE DETECTOR BROKEN.
- [SDR SCNA20241209396](https://openairdocs.org/sdr/SCNA20241209396), Nov 1, 2024: FLOORBEAM. CORRODED. UPPER FUSELAGE, PASSENGER CABIN WET AREA, W/L 207, AT STA 986.5, FLOOR BEAM UPPER FLANGER WITH CORROSION AT SEVERAL PLACES. PERFORMED PERMANENT RAPIR ON FLOOR B
- [SDR SCNA20241202382](https://openairdocs.org/sdr/SCNA20241202382), Nov 1, 2024: FLOOR SUPPORT. CRACKED. UPPER FUSELAGE PASSENGER CABIN AREA, W/L 207, FROM STA 277 TO STA 294, BL 0, INTERCOSTAL WITH CRACKS. REPLACED INTERCOSTAL P/N 141A5410-3 IAW B737-800 SRM 51-10
- [SDR SCNA20241114370](https://openairdocs.org/sdr/SCNA20241114370), Nov 1, 2024: LIGHT. DETERIORATED. WORK ORDER 80721 N/R00009: PAX CABIN FLOOR PANELS PHOTOLUMINISCENT LIGHTS SECTIONS (32EA) ARE DETERIORATED.
- [SDR SCNA20241203390](https://openairdocs.org/sdr/SCNA20241203390), Oct 31, 2024: DOUBLER. BENT. WHILE PERFORMING ITEM 7-13, WAS FOUND EXTERNAL POWER RECEPTACLE CUT OUT DOUBLER BENT AND BULGED. PERFORMED PERMANENT REPAIR OF THE ELECTRICAL GROUND POWER RECEP
- [SDR SCNA20241028350](https://openairdocs.org/sdr/SCNA20241028350), Oct 31, 2024: STRAP. CORRODED. WORK ORDER NR00017: PASSENGER CABIN RH EMERGENCY EXIT HATCH ESCAPE STRAP WITH END OF THE LIFE LINE CORRODED.
- [SDR SCNA20241028349](https://openairdocs.org/sdr/SCNA20241028349), Oct 31, 2024: LINE. CORRODED. WORK ORDER NON-ROUTINE00016: PASSENGER CABIN LH EMERGENCY EXIT HATCH ESCAPE WITH END OF THE LIFE LINE CORRODED.
- [SDR SCNA20241203388](https://openairdocs.org/sdr/SCNA20241203388), Oct 24, 2024: PRESSURE DECK. DAMAGED. REF W/O 87630 N/R 9 . TEMP REPAIR INSTALLED ON WING CENTER SECTION REAR SPAR VERTICAL PRESSURE DECK WEB AT STA 663 BETWEEN RBL 31.83 AND RBL 40 REQUIRES REPLACE
- [SDR SCNA20241203389](https://openairdocs.org/sdr/SCNA20241203389), Oct 4, 2024: REPAIR. TEMP REPAIR. WORK ORDER 90721, NR00007: REF W/O 87630 N/R 11 . TEMP REPAIR INSTALLED ON WING CENTER SECTION REAR SPAR VERTICAL PRESSURE DECK WEB AT STA. 663 BETWEEN RBL 40 A
- [SDR SCNA20240729285](https://openairdocs.org/sdr/SCNA20240729285), Jul 1, 2024: LATCH. BROKEN. DURING L1 SLIDE SWAP FOR RESTORATION, FOUND BROKEN GIRT BAR LATCH. INSTALLED NEW LATCH REF AMM 25-66-01.
- [SDR SCNA20240625258](https://openairdocs.org/sdr/SCNA20240625258), Jun 19, 2024: PRESSURE WEB. CRACKED. RH MLG WHEEL WELL VERTICAL PRESSURE WEB STA. 663 RBL 31.83 TO RBL 40 CRACK APPROX. 1" LONG. STOP DRILLED 1" CRACK AND SLOTTED PER SRM 57-10-10-2R-4.
- [SDR SCNA20240625257](https://openairdocs.org/sdr/SCNA20240625257), Jun 18, 2024: BULKHEAD. CRACKED. RH MLG WHEEL WELL VERTICAL PRESSURE WEB STA. 663 RBL 40-45.64 CRACK 2.6" LONG. ACCOMPLISHED TEMP REPAIR PER SRM 57-10-10-2R-4. STOP DRILLED AND SLOTTED THE CRAC
- [SDR SCNA20240506233](https://openairdocs.org/sdr/SCNA20240506233), Apr 30, 2024: BRACKET. OUT OF ADJUST. DOOR 1R GIRT BAR BRACKET IS TOO TIGHT. ADJUSTED 1R GIRT BAR BRACKET REF AMM 25-66-00. A/C OKAY FOR SERVICE
- [SDR SCNA20240108006](https://openairdocs.org/sdr/SCNA20240108006), Jan 8, 2024: UNKNOWN. UNKNOWN. DEFECT 713317 - - 2R DOOR SLIDE PIN HANGING OUT OF COMPARTMENT - - RESOLUTION: REMOVED AND REINSTALLED SLIDE REF AMM 25-66-01. REATTACHED SLIDE PIN.
- [SDR SCNA20230921229](https://openairdocs.org/sdr/SCNA20230921229), Sep 13, 2023: UNKNOWN. UNKNOWN. DEFECT WO 81753 NR 00007: EMERGENCY LIGHTS INOP. AT LI DOOR SLIDE, R1 DOOR SLIDE, L1 DOOR FLOOR AND COCKPIT - - - RESOLUTION: REMOVED AND REPLACED EMERGENCY POW
- [SDR SCNA20230609178](https://openairdocs.org/sdr/SCNA20230609178), Jun 9, 2023: UNKNOWN. UNKNOWN. DEFECT 701157: 1L GIRT BAR BRACKET LOOSE. - - - RESOLUTION: RESECURED GIRT BAR BRACKET REF AMM 25-66-01
- [SDR SCNA20230425137](https://openairdocs.org/sdr/SCNA20230425137), Apr 24, 2023: UNKNOWN. UNKNOWN. L2 SLIDE GIRT BAR BRACKET RIVETS LOOSE. INSTALLED 2 EACH RIVETS REF. SRM 51-40-02.
- [SDR SCNA20220815095SU](https://openairdocs.org/sdr/SCNA20220815095SU), Aug 12, 2022: LIGHT. INOPERATIVE. SUPPLEMENTAL. DEFECT: 720507: FWD ENTRY LIGHT INOP. RESOUTION: RELAMPED FWD ENTRY LIGHT REF AMM 33-29-00 OPS GOOD. THIS CLEARS MEL MC NOTIFIED.
- [SDR SCNA20220815095](https://openairdocs.org/sdr/SCNA20220815095), Aug 12, 2022: LIGHT. INOPERATIVE. DEFECT 720502: FWD ENTRY LIGHT INOP

All 219: https://openairdocs.org/aircraft/N809SY/reports.md

## STCs that may be installed (OpenAirDocs) (7)

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 series)

- [STC SE04840NY](https://openairdocs.org/stc/SE04840NY): Installation of HarcoSemco Exhaust Gas Temperature (EGT) Electrical Harnesses in CFM56-7 engine. Kilroy Aviation LLC. Lists CFM56-7B20
- [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. Lists CFM56-7B20
- [STC SE00032EN](https://openairdocs.org/stc/SE00032EN): Installation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 Fan/Booster Module. Pratt & Whitney. Lists CFM56-3
- [STC SE00033EN](https://openairdocs.org/stc/SE00033EN): Installation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 High Pressure Compressor Module. Pratt & Whitney. Lists CFM56-3
- [STC SE00034EN](https://openairdocs.org/stc/SE00034EN): Installation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 High Pressure Turbine Module. Pratt & Whitney. Lists CFM56-3
- [STC SE00035EN](https://openairdocs.org/stc/SE00035EN): Installation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 Low Pressure Turbine Module. Pratt & Whitney. Lists CFM56-3
- [STC SE00822CH](https://openairdocs.org/stc/SE00822CH): Install AeroControlex P/N 2604880-001 variable stator feedback control cable and P/N 2604880-002 variable bleed valve feedback control cable on CFM International engines. AeroControlex Group TransDigm Inc. Lists CFM56-2

## Related

- Other Boeing 737-8Q8 aircraft: https://openairdocs.org/model/boeing-737-8q8/aircraft.md
- The CFM International CFM56 series engine: https://openairdocs.org/engine/cfm-international-cfm56-series.md

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