# N243WN: 2006 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 CFM56-7B24 series](https://openairdocs.org/engine/cfm-international-cfm56-7b24-series) (registry code 13044) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (The Boeing Company) (OpenAirDocs) - Serial number: 34863 - Year built: 2006 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 17, 2006 - Certificate issued: July 27, 2006 - Expires: October 31, 2027 - Mode S code: A23D25 - 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=243WN - Page: https://openairdocs.org/aircraft/N243WN From the FAA registry file of October 22, 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 737-7H4) 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 N243WN. ## 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 20190720023852I](https://openairdocs.org/incident/20190720023852I), Jul 20, 2019: Boeing 737-7H4 (N243WN), Nashville, TN, Minor damage. Related report A-SW-29-19-007; The captain stated; ""the airplane of gate 13 had stopped for a while and there was no indication from any ground personnel that… ## Service difficulty reports (293, 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 SWAA2026100296033](https://openairdocs.org/sdr/SWAA2026100296033), Sep 28, 2026: LAMP. INOPERATIVE. AFT LT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS AFT LEFT EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-04. - [SDR SWAA2026080326308](https://openairdocs.org/sdr/SWAA2026080326308), Jul 28, 2026: LOCK. OUT OF ADJUST. AFT ENTRY DOOR GIRT BAR WILL NOT STAY CLIPPED IN. ADJUSTED LOCK CLIP IAW SIP. - [SDR SWAA2026072106685](https://openairdocs.org/sdr/SWAA2026072106685), Jul 18, 2026: LAMP. INOPERATIVE. EXTERIOR EMERGENCY LIGHT INOP AT R-2 DOOR. REMOVED AND REPLACED SLIDE LAMP AT DOOR R2 IAW AMM 33-51-04. OPS CHECK GOOD. - [SDR SWAA2026030375699](https://openairdocs.org/sdr/SWAA2026030375699), Mar 2, 2026: BULB. INOPERATIVE. EXTERIOR EMERGENCY LIGHT BY THE AFT ENTRY DOOR WAS INOPERATIVE. R & R THE BULB IAW AMM 33-51-04. - [SDR SWAA2026020366140](https://openairdocs.org/sdr/SWAA2026020366140), Jan 30, 2026: LAMP. INOPERATIVE. R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED THE LAMP AND PERFORMED A GOOD TEST IAW AMM 33-51-04-960-801. - [SDR SWAA2026020366139](https://openairdocs.org/sdr/SWAA2026020366139), Jan 30, 2026: LAMP. INOPERATIVE. L1 DOOR EMERGENCY EXIT LIGHT PEANUT LIGHT INOPERATIVE. REPLACED THE LAMP AND TESTED GOOD IAW AMM 33-51-01-960-801. - [SDR SWAA2026020364934](https://openairdocs.org/sdr/SWAA2026020364934), Jan 27, 2026: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1670 DID NOT ILLUMINATE. REMOVED & REPLACED THE BATTERY PACK (M1670) IAW AMM 33-51-06-960-805, AND PERFORMED A GO - [SDR SWAA2026020364935](https://openairdocs.org/sdr/SWAA2026020364935), Jan 27, 2026: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1672 DID NOT ILLUMINATE. REMOVED & REPLACED BATTERY PACK M1672 AND PERFORMED A GOOD TEST IAW AMM 33-51-06-960-805 - [SDR SWAA2026020364936](https://openairdocs.org/sdr/SWAA2026020364936), Jan 27, 2026: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1673 DID NOT ILLUMINATE. REMOVED & REPLACED THE BATTERY PACK (M1673) AND PERFORMED A GOOD TEST IAW AMM 33-51 - [SDR SWAA2026020359539](https://openairdocs.org/sdr/SWAA2026020359539), Jan 8, 2026: SEAT TRACK. CORRODED. FIRST OFFICER'S FWD SEAT TRACK CORRODED ON BOTTOM SURFACE. REPLACED THE FIRST OFFICER'S SEAT TRACK IAW AMM 25-11-11-400-801. - [SDR SWAA2026020359541](https://openairdocs.org/sdr/SWAA2026020359541), Jan 8, 2026: SEAT TRACK. CORRODED. CAPT'S FWD SEAT TRACK CORRODED ON LOWER SURFACE. REPLACED THE CAPT'S FWD SEAT TRACK IAW AMM 25-11-11-400-801. - [SDR SWAA2026020359350](https://openairdocs.org/sdr/SWAA2026020359350), Jan 7, 2026: SUPPORT. CORRODED. CORROSION ON THE AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT PLATE AROUND MULTIPLE NUT PLATE HOLES, BS 727B - 767, LBL 22, WL 156. REMOVED & REPLACED THE FLOOR T - [SDR SWAA2026020359351](https://openairdocs.org/sdr/SWAA2026020359351), Jan 7, 2026: SUPPORT. CORRODED. CORROSION ON THE AFT CARGO BAY, RT FLOOR TO SIDEWALL SUPPORT PLATE AROUND MULTIPLE NUT PLATE HOLES, BS 727B - 767, RBL 22, WL 156. REMOVED & REPLACED THE FLOOR - [SDR SWAA2026020359184](https://openairdocs.org/sdr/SWAA2026020359184), Jan 7, 2026: STRINGER CLIP. CRACKED. CRACKED STRINGER CLIP, BS 727B, S7L. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02-0G-0, & DWG 146A1102, SHEET 15, REV -. - [SDR SWAA2026020359185](https://openairdocs.org/sdr/SWAA2026020359185), Jan 7, 2026: STRINGER CLIP. CRACKED. CRACKED STRINGER CLIP, BS 727C, S6L. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02-0G-0, AND DWG 146A1103, SHEET 11, REV -. - [SDR SWAA2026020359186](https://openairdocs.org/sdr/SWAA2026020359186), Jan 7, 2026: STRINGER CLIP. CRACKED. CRACKED STRINGER CLIP, BS 727E, S6L. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02-0G-0, AND DWG 146A1112, SHEET 09, REV -. - [SDR SWAA2026020358812](https://openairdocs.org/sdr/SWAA2026020358812), Jan 6, 2026: FRAME. CRACKED. CRACK FOUND IN THE E/E BAY, BS 328, 4 INCHES ABOVE STRINGER 21R. REMOVED & REPLACED THE FRAME, AND STRAP IAW EA 26-153-00075. - [SDR SWAA2026020357494](https://openairdocs.org/sdr/SWAA2026020357494), Jan 1, 2026: FLOOR PANEL. PULLED. FLOOR PANEL 241FF HAD AREAS OF PULLED STRANDS. DUE TO EXTENT OF THE DAMAGE, FABRICATED A NEW 241FF FLOOR PANEL IAW SRM 53-00-50-2R-0. - [SDR SWAA2026020357482](https://openairdocs.org/sdr/SWAA2026020357482), Jan 1, 2026: FLOOR PANEL. PULLED. FLOOR PANEL 232RF HAD AREAS OF PULLED STRANDS. A REPLACEMENT FLOOR PANEL 232RF FABRICATED IAW SRM 53-00-50-2R-0. - [SDR SWAA2026020357483](https://openairdocs.org/sdr/SWAA2026020357483), Jan 1, 2026: FLOOR PANEL. DELAMINATED. FLOOR PANEL 241AF HAS DELAMINATED PREVIOUS REPAIR. A REPLACEMENT FLOOR PANEL 241AF HAS BEEN FABRICATED IAW SRM 53-00-50-2R-0. - [SDR SWAA2026020357484](https://openairdocs.org/sdr/SWAA2026020357484), Jan 1, 2026: FLOOR PANEL. PULLED. FLOOR PANEL 241DF HAD AREAS OF PULLED STRANDS. FABRICATION OF A NEW 241DF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0. - [SDR SWAA2026020357485](https://openairdocs.org/sdr/SWAA2026020357485), Jan 1, 2026: FLOOR PANEL. PULLED. FLOOR PANEL 241EF HAS AREAS OF PULLED STRANDS. DUE TO EXTENT OF THE DAMAGE, FABRICATED A NEW 241EF FLOOR PANEL IAW SRM 53-00-50-2R-0. - [SDR SWAA2026020357486](https://openairdocs.org/sdr/SWAA2026020357486), Jan 1, 2026: FLOOR PANEL. PULLED. FLOOR PANEL 242CF HAS AREAS OF PULLED STRANDS. FABRICATION OF A NEW 242CF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0. - [SDR SWAA2026020357487](https://openairdocs.org/sdr/SWAA2026020357487), Jan 1, 2026: FLOOR PANEL. PULLED. FLOOR PANEL 242DF HAS AREAS OF PULLED STRANDS. FABRICATION OF NEW 242DF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0. - [SDR SWAA2026020357480](https://openairdocs.org/sdr/SWAA2026020357480), Jan 1, 2026: ACCESS PANEL. DELAMINATED. ACCESS PANEL 194AL LOWER CORNER IS DELAMINATED. REPAIRED IAW SRM 51-70-05-2R-6-A00737, REPAIR 6. - [SDR SWAA2026020356939](https://openairdocs.org/sdr/SWAA2026020356939), Dec 30, 2025: SKIN. CRACKED. CRACK AROUND THE FASTENER AT NR 2 SLAT, LOWER SURFACE OF THE L/E SLAT NOSE SKIN AT ACTUATOR RIBS. REPAIRED THE NR 2 SLAT LOWER SURFACE NOSE SKIN IAW SRM 57-42-0 - [SDR SWAA2025080597352](https://openairdocs.org/sdr/SWAA2025080597352), Aug 1, 2025: BATTERY PACK. FAILED. EMERGENCY LIGHTS AT ROWS 1CBA THROUGH 4CBA WILL NOT COME ON<[01] REPLACED EMERGENCY ROW POWER SUPPLY AND BATTERY AT M1675 REF AMM 33-51-06. - [SDR SWAA2025073096386](https://openairdocs.org/sdr/SWAA2025073096386), Jul 29, 2025: HANDLE. BROKEN. AFT RIGHT SERVICE DOOR HANDLE DETACHED DOOR ASSIST HANDLE BROKE OFF OF THE MOUNTS. SWAPPED ASSIST HANDLE FROM AFT LAV TO AFT SERVICE DOOR. OPS CHECK GOOD IAW AM - [SDR SWAA2025042827412](https://openairdocs.org/sdr/SWAA2025042827412), Apr 23, 2025: GIRT BAR. OUT OF ADJUST. L2 DOOR SLIDE GIRT DRAGS. REPACKED L2 DOOR SLIDE GIRT PER AMM 25-66-01. - [SDR SWAA2024022347264](https://openairdocs.org/sdr/SWAA2024022347264), Jan 31, 2024: RIB. CRACKED. CRACK ACCESS PANEL 331B RIB LOCATED LE STA95.96 AT LT HORIZONTAL STABILIZER 2024-68301<[01] REPLACED RIB (ASSY) ON ACCESS PANEL LOCATED LE STA95.96 AT LT HORIZO - [SDR SWAA2024022347265](https://openairdocs.org/sdr/SWAA2024022347265), Jan 31, 2024: RIB. CRACKED. CRACK ACCESS PANEL 331B RIB LOCATED LE STA105.26 AT LT HORIZONTAL STABILIZER 2024-68302<[01] REPLACED RIB (CHORD) ON ACCESS PANEL 331B LOCATED LE STA105.26 AT L - [SDR SWAA2024022347266](https://openairdocs.org/sdr/SWAA2024022347266), Jan 31, 2024: RIB. CRACKED. CRACK ACCESS PANEL 331B RIB LE STA133.15 AT LT HORIZONTAL STABILIZER 2024-68303<[01] REPLACED RIB (ASSY) AND FASTENERS ON ACCESS PANEL 331B LOCATE STA133.15 AT - [SDR SWAA2024022346610](https://openairdocs.org/sdr/SWAA2024022346610), Jan 30, 2024: ACCESS PANEL. CRACKED. CRACK ACCESS PANEL 642BB AT RT WING 2024-68291<[01] TOOL USED HOTBONDER P/N: HCS9200B-AV S/N: 18185761 DUE DATE: 24-JAN-25.;[02] TOOL USED SCALE P/N:CR5200 S/N: - [SDR SWAA2024022345860](https://openairdocs.org/sdr/SWAA2024022345860), Jan 28, 2024: NUT PLATE. CORRODED. CORROSION LEADING EDGE ON RAIL NUT PLATES LOCATED OFSS305 AT LT WING 2024-68280<[01] REPLACED RAIL NUT PLATES LOCATED OFSS305 AT LT WING I.A.W B737-700 SRM 51-4 - [SDR SWAA2024022345861](https://openairdocs.org/sdr/SWAA2024022345861), Jan 28, 2024: NUT PLATE. CORRODED. CORROSION LEADING EDGE RAIL NUT PLATES LOCATED OFSS291 AT LT WING 2024-68281<[01] REPLACED RAIL NUT PLATES LOCATED OFSS291 AT LT WING I.A.W B737-700 SRM 51-40-0 - [SDR SWAA2024022345865](https://openairdocs.org/sdr/SWAA2024022345865), Jan 28, 2024: SUPPORT BRACKET. CRACKED. CRACK SUPPORT BRACKET TRAILING EDGE LOCATED ORSS270 LT WING 2024-68267<[01] REPLACED SUPPORT BRACKET LOCATED ON TRAILING EDGE ORSS270 LT WING IAW B737-700 SRM 5 - [SDR SWAA2024022345866](https://openairdocs.org/sdr/SWAA2024022345866), Jan 28, 2024: ANGLE. CRACKED. CRACK ANGLE TRAILING EDGE LOCATED ORSS279 LT WING 2024-68268<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS279 LT WING
IAW B737-700 SRM 51-40-02 AND 51-10-0 - [SDR SWAA2024022345864](https://openairdocs.org/sdr/SWAA2024022345864), Jan 28, 2024: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE LOCATED TRAILING EDGE ORSS270 AT LT WING 2024-68269<[01] REPLACED SUPPORT ANGLE LOCATED ON TRAILING EDGE ORSS270 AT LT WING IAW B737-700 SRM - [SDR SWAA2024022345858](https://openairdocs.org/sdr/SWAA2024022345858), Jan 28, 2024: ANGLE. CRACKED. CRACK ON ANGLE LOCATED AUXILIARY TRACK INBOARD POSITION SLAT8 RT WING 2024-68276<[01] REPLACED ANGLE LOCATED AUXILIARY TRACK INBOARD POSITION SLAT8 RT WING IAW - [SDR SWAA2024022345859](https://openairdocs.org/sdr/SWAA2024022345859), Jan 28, 2024: ANGLE. CRACKED. CRACK ANGLE ON AUXILIARY TRACK INBOARD POSITION SLAT1 AT LT WING 2024-68278<[01] REPLACED ANGLE ON AUXILIARY TRACK INBOARD POSITION SLAT1 AT LT WING IAW B737-70 - [SDR SWAA2024022345163](https://openairdocs.org/sdr/SWAA2024022345163), Jan 26, 2024: STRAP. CORRODED. CORROSION STRAP LOCATED BTW BS767 TO BS787 AND STR25L TO STR25R WL156 AFT CARGO COMPARTMENT 2024-68235<[01] REPLACED STRAP LOCATED BTW BS767 TO BS787 AND STR25L - [SDR SWAA2024022345294](https://openairdocs.org/sdr/SWAA2024022345294), Jan 26, 2024: PLATE. CRACKED. CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS261 AT RT WING 2024-68238<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS261 AT RT WING IAW B737-700 - [SDR SWAA2024022345295](https://openairdocs.org/sdr/SWAA2024022345295), Jan 26, 2024: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE LOCATED ORSS268 TRAILING EDGE AT RT WING 2024-68240<[01] REPLACED SUPPORT ANGLE LOCATED ORSS268 TRAILING EDGE AT RT WING IAW B737-700 SRM 51 - [SDR SWAA2024022345296](https://openairdocs.org/sdr/SWAA2024022345296), Jan 26, 2024: SUPPORT BRACKET. CRACKED. CRACK SUPPORT BRACKET TRAILING EDGE LOCATED ORSS268 RT WING 2024-68241<[01] REPLACED SUPPORT BRACKET TRAILING EDGE LOCATED ORSS268 RT WING IAW B737-700 SRM 51-4 - [SDR SWAA2024022345297](https://openairdocs.org/sdr/SWAA2024022345297), Jan 26, 2024: ANGLE. CRACKED. CRACK ANGLE TRAILING EDGE LOCATED ORSS274 RT WING 2024-68242<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS274 RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM - [SDR SWAA2024022245162](https://openairdocs.org/sdr/SWAA2024022245162), Jan 26, 2024: SUPPORT ANGLE. CRACKED. CRACK ANGLE - SUPPORT LOCATED BTW BS907 TO BS927 AND STR26R AT AFT CARGO COMPARTMENT 2024-68227<[01] REPLACED ANGLE - SUPPORT LOCATED BTW BS907 TO BS927 AND STR - [SDR SWAA2024022344603](https://openairdocs.org/sdr/SWAA2024022344603), Jan 24, 2024: FLOOR SUPPORT. ELONGATED. CUSTOMER REQUEST AAI AFT CARGO COMPARTMENT; FLOOR SUPPORT CHANNEL SHIELD HAS ELONGATED FASTENER HOLES (2EA) AT STA 847 STA 867; STR 25R. 2024-68214<[01] REPLACE - [SDR SWAA2024022244594](https://openairdocs.org/sdr/SWAA2024022244594), Jan 24, 2024: INTERCOSTAL. CRACKED. CRACK WEB INTERCOSTAL LOCATED BTW BS294.5 TO BS303.9 AND STR16L AT PASSENGER CABIN 2024-68192<[01] REPLACED WEB INTERCOSTAL LOCATED BTW BS294.5 TO BS303.9 AND S - [SDR SWAA2024022244595](https://openairdocs.org/sdr/SWAA2024022244595), Jan 24, 2024: TIE CLIP. CRACKED. CRACK TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN 2024-68193<[01] REPLACED TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN IAW B737-700 SRM 51-10- - [SDR SWAA2024022244596](https://openairdocs.org/sdr/SWAA2024022244596), Jan 24, 2024: ANGLE. CRACKED. CRACK ANGLE FLOOR STRUCTURE LOCATED BTW BS291.5 TO BS294.5 AND STR17R AT PASSENGER CABIN 2024-68194<[01] REPLACED ANGLE AND FASTENERS LOC. BTW BS291.5 TO BS294. All 293: https://openairdocs.org/aircraft/N243WN/reports.md ## STCs that may be installed (OpenAirDocs) (32) 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 airframe (Boeing 737-7H4) - [STC ST00555AT](https://openairdocs.org/stc/ST00555AT): Installation of Airshow 210 system. AIRCRAFT RECONFIG TECHNOLOGIES, LLC. Lists 737 Series - [STC SA4842SW](https://openairdocs.org/stc/SA4842SW): Modification of air to air heat exchanger (P/N 182820-2 Series 2). Honeywell International Inc. Lists 737 Series - [STC SA270NW](https://openairdocs.org/stc/SA270NW): Installation of modified seat. Aviation Technical Services. Lists 737 Series - [STC ST01162NY](https://openairdocs.org/stc/ST01162NY): Installation of Literature Pockets. Magee Plastics Company. Lists 737 Series - [STC SA2607SO](https://openairdocs.org/stc/SA2607SO): Installation of coffee maker P/N 416-1001-29. B/E Aerospace Inc. Lists 737 Series - [STC SA2608SO](https://openairdocs.org/stc/SA2608SO): Installation of rail assembly, P/N 416-0201-15. B/E Aerospace Inc. Lists 737 Series - [STC SA3058SO](https://openairdocs.org/stc/SA3058SO): Installation of coffee maker 416-0001-23 and rail assembly 416-0201-5. B/E Aerospace Inc. Lists 737 Series - [STC ST01476AT](https://openairdocs.org/stc/ST01476AT): Installation of coffee maker. B/E Aerospace Inc. Lists 737 Series - [STC ST01778AT](https://openairdocs.org/stc/ST01778AT): Installation of espresso maker p/n 3510-0066-01. B/E Aerospace Inc. Lists 737 Series - [STC SA629GL](https://openairdocs.org/stc/SA629GL): Installation of Grimes galley, Model 1545LW unit 2 and unit 4. B/E Aerospace. Lists 737 Series - [STC ST01332AT](https://openairdocs.org/stc/ST01332AT): Installation of Galley Service Carts. Champ International, Inc. Lists 737 Series - [STC ST09870SC](https://openairdocs.org/stc/ST09870SC): Installation of Mechanical Window Shades. Lou Martin & Associates. Lists 737 Series - [STC ST00033AT](https://openairdocs.org/stc/ST00033AT): Installation of a single Mode S system and provisions for a TCAS II system. General Aerospace, Inc. Lists 737 Series - [STC SA4532NM](https://openairdocs.org/stc/SA4532NM): Installation of Coltech, CTD-80 ATSCALL, enabling company calling of selected aircraft via company selected radio. Avtech Corporation. Lists 737 Series - [STC ST4532NM](https://openairdocs.org/stc/ST4532NM): Installation of Coltech CTD-80 ATSCALL, enabling company calling of selected aircraft via company selected radio. Avtech Corporation. Lists 737 Series - [STC ST00774NY](https://openairdocs.org/stc/ST00774NY): Installation of a passenger cabin Liquor/beverage service cart P/N E500170. (757-222) (767-222) (727-222) (737 SERIES 222, 291, 322, 522) (747-100 SERIES 238B). Driessen Aircraft Interior Systems USA, Inc. Lists 737 Series - [STC ST02052AT](https://openairdocs.org/stc/ST02052AT): Installation of a single Collins GNLU910A flight management system, along with global navigation satellite system sensor. General Aerospace, Inc. Lists 737 Series - [STC SA02034AT](https://openairdocs.org/stc/SA02034AT): Manufacture of tray carrier, P/N 2282-506. BFE Services. Lists 737 Series - [STC ST01968AT](https://openairdocs.org/stc/ST01968AT): Manufacture of inserts for galley stowage. JK Aerospace, Inc. Lists 737 Series - [STC SA01916AT](https://openairdocs.org/stc/SA01916AT): Manufacture of Tray Carrier P/N 1839-501. BFE Services. Lists 737 Series - [STC SA2534SO](https://openairdocs.org/stc/SA2534SO): Installation of window shades, acoustic panes and reveals. Magee Plastics Company. Lists 737 Series - [STC ST179CH](https://openairdocs.org/stc/ST179CH): Installation of cargo container curtain. Plastic Composites Corp. Lists 737 Series - [STC SA00056LA](https://openairdocs.org/stc/SA00056LA): Installation of Weber Coffeemaker, P/N 870130-415. Monogram Systems. Lists 737 Series - [STC SA6090NM](https://openairdocs.org/stc/SA6090NM): Installation of emergency vision assurance system (EVAS). VisionSafe Corporation. Lists 737 Series - [STC SA370NW](https://openairdocs.org/stc/SA370NW): Removal of passenger interior, installation of cargo compartment liners and cargo tie down equipment. Western Metal Products. Lists 737 Series - [STC SA2589CE](https://openairdocs.org/stc/SA2589CE): Install Bennetts Seat Converter Stowage Compartment on passenger seat(s). John's Aircraft and Upholstery. Lists 737 Series - [STC SA1029NW](https://openairdocs.org/stc/SA1029NW): Installation of a cargo system. Western Metal Products. Lists 737 Series - [STC SA1258EA](https://openairdocs.org/stc/SA1258EA): Installation of Cosco model78-( ) child restraint system. (172M S/N 17263459 - 17267584). Miller Stuart R. Lists 737 Series - [STC SA1052SO](https://openairdocs.org/stc/SA1052SO): Installation of GE battery P/N43B022RB36 in place of Marathon P/N CA-727-7, CA-727-20, or CA-27-20 batteries or SAFT P/N23180 batteries; or installation of GE battery P/N 43B020RB10 replacing Marathon P/N CA-727-7, CA-727-20 or CA-27-20 or SAFT P/N 23186 or 23180 batteries. General Electric Company. Lists 737 Series - [STC SA1082NW](https://openairdocs.org/stc/SA1082NW) (historical): Installation of auxiliary fuel tanks in the aft cargo compartment. (737 series -2K9A). Rogerson ATS. Lists 737 Series ### 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 737-7H4 aircraft: https://openairdocs.org/model/boeing-737-7h4/aircraft.md - The CFM International CFM56-7B24 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b24-series.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.