# N783SW: 2000 Boeing 737-7H4 - Status: Valid registration - Airframe: [Boeing 737-7H4](https://openairdocs.org/model/boeing-737-7h4) (registry code 1384404, 143 seats) - Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (The Boeing Company) (OpenAirDocs) - Serial number: 29809 - Year built: 2000 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 3, 2000 - Certificate issued: October 26, 2000 - Expires: August 31, 2028 - Mode S code: AA9D50 - Registered owner: [Southwest Airlines Co](https://openairdocs.org/faa-owner/SOUTHWEST%20AIRLINES%20CO) - Location: [Dallas, TX](https://openairdocs.org/faa-place/TX/Dallas) - Owner type: Corporation - Owner's area on the map: 32.8326° N, 96.8491° W: Placed by OpenAirDocs at the center of ZIP code 75235, 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=783SW - Page: https://openairdocs.org/aircraft/N783SW From the FAA registry file of October 20, 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 737-7H4) 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/N783SW/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 N783SW. ## 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; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20090717014579I](https://openairdocs.org/incident/20090717014579I), Jul 17, 2009: Boeing 7377H4 (N783SW), Omaha, NE, No damage. (-23) N783SW, B737-7H4 being operated by southwest airlines as flight 209 performed a go around after approach to Omaha Eppley Airfield, due to a flap issue.… ## Service difficulty reports (364, newest 50) As reported by operators and repair stations. - [SDR SWAA2023091901688](https://openairdocs.org/sdr/SWAA2023091901688), Sep 16, 2023: FLOOR PANEL. CRACKED. FWD CARGO COMPARTMENT FLOOR PANEL IS CRACKED<[01] OKAY TO CONTINUE PER MEL 25-16-01 SP1B FWD BIN TO REMAIN EMPTY;[02] REMOVED AND REPLACED CRACKED FLOOR PANEL F - [SDR SWAA2023061959937](https://openairdocs.org/sdr/SWAA2023061959937), Jun 16, 2023: GIRT BAR. OUT OF POSITION. GIRT BART LOCATED AT THE R2 AFT GALLEY DOOR IS HANGING OUT OF POSITION<[01] REPOSITIONED GIRT BAR AS REQD. AMM 25-66-01
R2 DOOR - [SDR SWAA2023061658972](https://openairdocs.org/sdr/SWAA2023061658972), Jun 14, 2023: HANDLE. LOOSE. FWD ENTRY DOOR UPPER ASSIST HANDLE LOOSE<[01] ADJUSTED FWD ENTRY DOOR ASSIST HANDLE PER AMM 52-11-31-000-802 - [SDR SWAA2023060956455](https://openairdocs.org/sdr/SWAA2023060956455), Jun 6, 2023: BATTERY PACK. INOPERATIVE. FWD LH EMERGENCY LIGHT BATTERY INOP.<[01] REMOVED AND REPLACED FWD LH EMERGENCY LIGHT BATTERY PACK REF: AMM 33-51-06. - [SDR SWAA2023042730410](https://openairdocs.org/sdr/SWAA2023042730410), Apr 23, 2023: FLOOR PANEL. CRACKED. FWD CARGO AFT FLOOR PANEL HAS A CRACK 9.5 INCHES IN LENGTH<[01] REMOVED AND REPLACED FWD CARGO AFT FLOOR PANEL IAW AMM 25-52-10. - [SDR SWAA2023021502479](https://openairdocs.org/sdr/SWAA2023021502479), Feb 13, 2023: TAILPIPE. FIRE. ENGINE TAILPIPE FIRE @ 75KTS DURING T/O ON NO 1 ENG REJECTED T/O ; PERFORMED QRH PROCEDURES .FLAMES WERE REPORTED FROM ANOTHER A/C AND TOWER RAN BRAKE COOLING O - [SDR SWAA2022120979977](https://openairdocs.org/sdr/SWAA2022120979977), Dec 8, 2022: SLIDE. OUT OF POSITION. STBD AFT A/C SERVICE DOOR SLIDE PULL HANDLE VISIBLE AND EXPOSED WHEN DOOR IS ARMED. REPOSITIONED MANUAL HANDLE COVER FOR AFT SERVICE DOOR ESCAPE SLIDE IAW AMM 2 - [SDR SWAA2022102765082](https://openairdocs.org/sdr/SWAA2022102765082), Oct 26, 2022: FLASHLIGHT. INOPERATIVE. FA FOUND FWD GALLEY UPPPER EMER FLASHLIGHT NOT BLINKING / [01] R&R EMER FLASHLIGHT PER AMM 25-64-00 - [SDR SWAA2022090649795](https://openairdocs.org/sdr/SWAA2022090649795), Sep 2, 2022: SLIDE. LOW. FORWARD RIGHT SERVICE DOOR SLIDE INDICATOR GAUGE SHOWING LOW. SLIDE PART REQUEST IS BUILT INTO THE SUBTASK / [01] R&R?D FWD SERVICE (R1)DOOR EMERGENCY ESCAPE SL - [SDR SWAA2022060111139](https://openairdocs.org/sdr/SWAA2022060111139), May 24, 2022: WEB. CRACKED. RIGHT WING TRAILING EDGE DEFLECTION CONTROL RIB PANEL SUPPORT WEB CRACKED AT OUTBOARD ATTACH FASTENER HOLE. REMOVED DAMAGE WEB ANGLE AT R/H WING TRAILING EDGE D - [SDR SWAA2022060111136](https://openairdocs.org/sdr/SWAA2022060111136), May 24, 2022: SUPPORT ANGLE. CRACKED. RIGHT WING TRAILING EDGE DEFLECTION CONTROL RIB PANEL SEAL SUPPORT ANGLE CRACKED AT WEB ATTACH POINT. REMOVED DAMAGE SEAL SUPPORT ANGLE AT R/H WING TRAILING EDG - [SDR SWAA2022060111137](https://openairdocs.org/sdr/SWAA2022060111137), May 24, 2022: SUPPORT ANGLE. CRACKED. LEFT WING DEFLECTION CONTROL RIB PANEL VERTICAL SEAL SUPPORT ANGLE CRACKED AT THE FORWARD SIDE OF WEB. / [01] REMOVED AND REPLACED SEAL SUPPORT ANGLE AT FWD SID - [SDR SWAA2022030279163](https://openairdocs.org/sdr/SWAA2022030279163), Mar 2, 2022: LIGHT. MISSING. EMERGENCY EXIT LIGHT LENS NOT INSTALLED AT R2 DOOR / [01] REMOVED & REPLACED EMERGENCY EXIT LIGHT ASSY; AT R2 DOOR; PER AMM 33-51-01. - [SDR SWAA2022021472148](https://openairdocs.org/sdr/SWAA2022021472148), Feb 11, 2022: SENSOR. FAULTY. CREW REPORTED FLAP LOCK OUT ON LANDING ; / [01] REPLACED SLAT #1 INBOARD PROXIMITY SENSOR PER AMM 27-88-11; OPS CHECK GOOD. - [SDR SWAA2021110832157](https://openairdocs.org/sdr/SWAA2021110832157), Oct 20, 2021: GIRT BAR. OUT OF POSITION. L-1 DOOR GIRT BAR HITTING AFT DOOR CUTOUT (WHEN OPENING DOOR) ; / [01] REMOVED R1 DOOR SLIDE REF MT 725-61-06; [02] REPOSITIONED GIRT BAR FOR L1 DOOR REF B737 M - [SDR SWAA2021110832154](https://openairdocs.org/sdr/SWAA2021110832154), Oct 20, 2021: GIRT BAR. OUT OF POSITION. R-1 DOOR GIRT BAR HITTING DOOR CUTOUT WHEN CLOSING ON AFT CORNER ; / [01] REMOVED R1 DOOR SLIDE REF MT 725-61-06; [02] REPOSITIONED GIRT BAR FOR R1 DOOR REF B73 - [SDR SWAA2021102832155](https://openairdocs.org/sdr/SWAA2021102832155), Oct 20, 2021: BULB. INOPERATIVE. L-1 DOOR UPPER EMERGENCY LIGHT WITH 2EA BULBS INOP ; / [01] RECITED BULBS (2EA) AT L-1 DOOR UPPER EMERGENCY LIGHT AS PER REF B737 AMM 33-51-01-960-801 PERFORMED - [SDR SWAA2021110831031](https://openairdocs.org/sdr/SWAA2021110831031), Oct 17, 2021: NONE. POPPED. PASSENGER CABIN LIGHTING EMERGENCY CHARGER FWD C/B POPPING AT P18. ; PASSENGER CAIN LIGHTING EMERGENCY CHARGER FWD CB POPPING AT P18. / [01] PERFORMED TROUBLESH - [SDR SWAA2021110831030](https://openairdocs.org/sdr/SWAA2021110831030), Oct 17, 2021: LIGHT. INOPERATIVE. OVERHEAD BIN EMERGENCY LIGHT INOP BY ROW 4 LH ; OVERHEAD IN EMERGENCY LIGHT INOP Y ROW 4 LH / [01] RE-SECURED CONNECTOR D11090 IN AISLE LIGHT L1065; AS PER REFE - [SDR SWAA2021110929830](https://openairdocs.org/sdr/SWAA2021110929830), Oct 14, 2021: SCUFF PLATE. CRACKED. FWD CARGO FWD SCUFF PLATE CRACKED ; / [01] RECEIVED WELDED SCUFF PLATE ON TAG #397070; ISSUE TAG #HZ896; P.O.#1734696. WILL BE INSTALLED ON CARD 3 # TTG8Q004G7H - [SDR SWAA2021110826978](https://openairdocs.org/sdr/SWAA2021110826978), Oct 5, 2021: FLOOR PANEL. DELAMINATED. FOUND PANEL 212DC DELAMONATE AT CORNER ; / [01] PREPARED FOR REPAIR AT PANEL 212 DC AS PER B737-700-SRM 51-70-06-2R-6; [02] VERIFIED STEP 1. OK TO INSTALL REPAI - [SDR SWAA2021110826221](https://openairdocs.org/sdr/SWAA2021110826221), Oct 4, 2021: SEAT TRACK. CORRODED. FOUND FIRST OFFICER FWD I/B AND O/B SEAT TRACKS WITH CORROSION ; / [01] 1ST OFFICER FWD I/B AND O/B SEAT TRACKS WERE REMOVED ON TASKCARD TTG8Q0036K60.; [02] VER - [SDR SWAA2021110826222](https://openairdocs.org/sdr/SWAA2021110826222), Oct 4, 2021: SEAT TRACK. CORRODED. FOUND CAPTAIN FWD I/B AND O/B SEAT TRACKS WITH CORROSION ; / [01] RECEIVED CAPTAIN FWD I/B AND O/B SET TRACKS TO BE INSTALLED ON CARD TTG8Q0036K4C; [02] RECEIVE - [SDR SWAA2021110924748](https://openairdocs.org/sdr/SWAA2021110924748), Sep 29, 2021: NONE. CORRODED. CORROSION.>>>>>VERTICAL FIN FWD R/H ATTACHMENT FITTING LUGS STA 1016 INNER BORE EVIDENCE OF PITTI CORROSION. ; / [01] REMOVED CORROSION ON VERTICAL FIN FWD R/H - [SDR SWAA2021110924747](https://openairdocs.org/sdr/SWAA2021110924747), Sep 29, 2021: NONE. CORRODED. CORROSION >>>>>>>VERTICAL FIN FRONT SPAR R/H FITTING LUG HAVE SIGN OF PITTI CORROSION AT INNER BORE. ; / [01] REMOVED CORROSION ON VERTICAL FIN FRONT SPAR R/H F - [SDR SWAA2021110924746](https://openairdocs.org/sdr/SWAA2021110924746), Sep 29, 2021: NONE. CORRODED. CORROSION >>>>>>>VERTICAL FIN FRONT SPAR L/H FITTING LUG HAVE SIGN OF PITTI CORROSION AT INNER BORE. ; / [01] REMOVED CORROSION ON VERTICAL FIN FRONT SPAR L/H F - [SDR SWAA2021110919709](https://openairdocs.org/sdr/SWAA2021110919709), Sep 17, 2021: SKIN. CORRODED. AFT UPPER FUSELAGE AT STA 1016 - STA 1088 STR 3L - STR 3R WL 308.5 HAS SURFACE CORROSION. REMOVED CORROSION ON UPPER FUSELAGE FROM BS 1016 TO 1088, BETWEEN STRI - [SDR SWAA2021110820614](https://openairdocs.org/sdr/SWAA2021110820614), Sep 17, 2021: ANGLE. CRACKED. CABIN PASSENGER STATION 616 LBL 60 CRACK AT FASTENER HOLE ; / [01] INSTALLED EWIS PROTECTION AT LT SIDE BETWEDN STA 540 TO 639 REF B737-7 AMM 20-60-07-913-801; - [SDR SWAA2021110819715](https://openairdocs.org/sdr/SWAA2021110819715), Sep 17, 2021: ANGLE. CRACKED. CABIN PASSENGER STATION 616 LBL 60 CRACK AT FASTENER HOLE ; / [01] INSTALLED EWIS PROTECTION AT LT SIDE BETWEDN STA 540 TO 639 REF B737-7 AMM 20-60-07-913-801; - [SDR SWAA2021110920599](https://openairdocs.org/sdr/SWAA2021110920599), Sep 16, 2021: NONE. CORRODED. >>> CORROSION >> VERTICAL STABILIZER; RIGHT FRON SPAR FITTING PITTING CORROSION ; / [01] REMOVED BUSHING AT VERTICAL STABILIZER RIGHT FRONT SPAT FITTING AS PER - [SDR SWAA2021110920598](https://openairdocs.org/sdr/SWAA2021110920598), Sep 16, 2021: NONE. CORRODED. >>> CORROSION >> VERTICAL STABILIZER ; LEFT FRON SPAR FITTING CORROSION ; / [01] REMOVED BUSHING AT VERTICAL STABILIZER LEFT FRONT SPAR FITTING AS PER B737-700 - [SDR SWAA2021110920597](https://openairdocs.org/sdr/SWAA2021110920597), Sep 16, 2021: NONE. CORRODED. >>> CORROSION >> VERTICAL STABILIZER CENTER SECTION; LEFT FRON SPAR FITTINGS CORROSION ; / [01] REMOVED BUSHINGS AT VERTICAL STABILIZER CENTER SECTION LEFT FRON - [SDR SWAA2021110919708](https://openairdocs.org/sdr/SWAA2021110919708), Sep 16, 2021: FITTING. CORRODED. >>> CORROSION >> VERTICAL STABILIZER CENTER SECTION; RIGHT O/B REAR SPAR FITTINGS PITTING CORROSION ; / - [SDR SWAA2021110919702](https://openairdocs.org/sdr/SWAA2021110919702), Sep 16, 2021: FITTING. CORRODED. >>> CORROSION >> VERTICAL STABILIZER CENTER SECTION; LEFT O/B REAR SPAR FITTINGS CORROSION ; / - [SDR SWAA2021110919701](https://openairdocs.org/sdr/SWAA2021110919701), Sep 16, 2021: FITTING. CORRODED. >>> CORROSION >> VERTICAL STABILIZER CENTER SECTION; LEFT I/B REAR SPAR FITTINGS CORROSION ; / - [SDR SWAA2021110919700](https://openairdocs.org/sdr/SWAA2021110919700), Sep 16, 2021: FITTING. CORRODED. >>> CORROSION >> VERTICAL STABILIZER; RIGHT FRON SPAR FITTING PITTING CORROSION ; / - [SDR SWAA2021110919699](https://openairdocs.org/sdr/SWAA2021110919699), Sep 16, 2021: FITTING. CORRODED. >>> CORROSION >> VERTICAL STABILIZER ; LEFT FRON SPAR FITTING CORROSION ; / - [SDR SWAA2021110919698](https://openairdocs.org/sdr/SWAA2021110919698), Sep 16, 2021: FITTING. CORRODED. >>> CORROSION >> VERTICAL STABILIZER CENTER SECTION; LEFT FRON SPAR FITTINGS CORROSION ; / - [SDR SWAA2021110920602](https://openairdocs.org/sdr/SWAA2021110920602), Sep 16, 2021: FITTING. CORRODED. >>> CORROSION >> VERTICAL STABILIZER ; RIGHT I/B REAR SPAR FITTINGS PITTING CORROSION ; / [01] REMOVED BUSHINGS AT RIGHT VERTICAL STABILIZER I/B REAR SPAR AS P[ - [SDR SWAA2021110920607](https://openairdocs.org/sdr/SWAA2021110920607), Sep 16, 2021: FITTING. CORRODED. >>> CORROSION >> VERTICAL STABILIZER CENTER SECTION; RIGHT I/B REAR SPAR FITTINGS PITTING CORROSION ; / [01] EA EA-GENERAL (EA ATTACHED TO AN AIRCRAFT FAULT); [ - [SDR SWAA2021110920604](https://openairdocs.org/sdr/SWAA2021110920604), Sep 16, 2021: FITTING. CORRODED. VERTICAL STABILIZER LEFT I/B REAR SPAR FITTINGS CORRODED. REMOVED BUSHINGS AT LEFT VERTICAL STABILIZER I/B REAR SPAR AS PER B737-700 SOPM 20-50-03, AFTER BUSHIN - [SDR SWAA2021110920600](https://openairdocs.org/sdr/SWAA2021110920600), Sep 16, 2021: FITTING. CORRODED. >>> CORROSION >> VERTICAL STABILIZER CENTER SECTION; LEFT I/B REAR SPAR FITTINGS CORROSION ; / [01] PERFORMED CORRECTIVE ACTION ON BARCODE TTG8Q006LXMS. REF FAU - [SDR SWAA2021110920601](https://openairdocs.org/sdr/SWAA2021110920601), Sep 16, 2021: FITTING. CORRODED. >>> CORROSION >> VERTICAL STABILIZER CENTER SECTION; LEFT O/B REAR SPAR FITTINGS CORROSION ; / [01] PERFORMED CORRECTIVE ACTION ON BARCODE TTG8Q006LXMS. REF FAU - [SDR SWAA2021110920606](https://openairdocs.org/sdr/SWAA2021110920606), Sep 16, 2021: FITTING. CORRODED. >>> CORROSION >> VERTICAL STABILIZER CENTER SECTION; RIGHT O/B REAR SPAR FITTINGS PITTING CORROSION ; / [01] PERFORMED CORRECTIVE ACTION ON BARCODE TTG8Q006LXMS - [SDR SWAA2021110918244](https://openairdocs.org/sdr/SWAA2021110918244), Sep 15, 2021: NONE. BROKEN. FOUND RIGHT UPPER STABILIZER-TO-BODY FRONT SPAR SLIDING SEAL BROKEN ; / [01] REMOVED RIGHT UPPER STABLIZER -TO- BODY FRONT SPAR SLIDING SEAL AS PER BOEING 737 A - [SDR SWAA2021110918243](https://openairdocs.org/sdr/SWAA2021110918243), Sep 15, 2021: NONE. BROKEN. FOUND LEFT UPPER STABILIZER-TO-BODY FRONT SPAR SLIDING SEAL BROKEN ; / [01] REMOVED LEFT UPPER STABLIZER -TO- BODY FRONT SPAR SLIDING SEAL AS PER BOEING 737 AMM - [SDR SWAA2021110918242](https://openairdocs.org/sdr/SWAA2021110918242), Sep 15, 2021: ANGLE. CRACKED. VERTICAL FIN; FWD TERMINAL FITTING ASSY AFT FACE HORIZONTAL T ANGLE CRACKED 2 EA PLACES ; / [01] PERFORMED HFEC INSP ON VERTICAL FIN FWD TERMINAL FITTING ASSY A - [SDR SWAA2021110818245](https://openairdocs.org/sdr/SWAA2021110818245), Sep 15, 2021: GUSSET. CRACKED. FWD CARGO COMP GUSSET IS CRACKED BETWEEN FRAME BS 500D AND STGR 19L ; / [01] REMOVED GUSSET AT FWD CARGO COMPARTMENT AT FS 500D STRINGER 19L;FOUND OUT OF LIMITS - [SDR SWAA2021110818246](https://openairdocs.org/sdr/SWAA2021110818246), Sep 15, 2021: GUSSET. CRACKED. FWD CARGO COMP GUSSET IS CRACKED BETWEEN FRAME BS 500D AND STGR 21L ; / [01] REMOVED CRACK GUSSET IN REF B737-700 SRM 51-40-02-0G-0; [02] LOCATED AND DRILLED NE - [SDR SWAA2021110818247](https://openairdocs.org/sdr/SWAA2021110818247), Sep 15, 2021: GUSSET. CRACKED. FWD CARGO COMP GUSSET IS CRACKED BETWEEN FRAME BS 500D AND STGR 24L ; / [01] REMOVED GUSSET AT FWD CARGO COMPARTMENT FS 500D;STRINGER 24L;IN REF B737-700 SRM 51 All 364: https://openairdocs.org/aircraft/N783SW/reports.md ## Related - Other Boeing 737-7H4 aircraft: https://openairdocs.org/model/boeing-737-7h4/aircraft.md - STCs for the Boeing 737-7H4: https://openairdocs.org/model/boeing-737-7h4/stcs.md - The CFM International CFM56 series engine: https://openairdocs.org/engine/cfm-international-cfm56-series.md --- From OpenAirDocs.org, an independent open copy of FAA and NTSB data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.