# N7833A: 2003 Boeing 737-79P - Status: Valid registration - Airframe: [Boeing 737-79P](https://openairdocs.org/model/boeing-737-79p) (registry code 13844JA, 149 seats) - Engine: [CFM International CFM56-7B24 series](https://openairdocs.org/engine/cfm-international-cfm56-7b24-series) (registry code 13044) - Serial number: 30036 - Year built: 2003 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 22, 2015 - Certificate issued: December 20, 2022 - Expires: December 31, 2029 - Mode S code: AA9E6D - 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=7833A - Page: https://openairdocs.org/aircraft/N7833A From the FAA registry file of October 27, 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 737-79P) 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 N7833A. ## FAA accident and incident reports None matched to N7833A. ## Service difficulty reports (250, 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 SWAA2026042491970](https://openairdocs.org/sdr/SWAA2026042491970), Apr 23, 2026: MOUNT. CRACKED. PASSENGER CABIN FORWARD SERVICE DOOR AFT SLIDE MOUNT ISOLATOR IS CRACKED. REPLACED PASSENGER CABIN FORWARD SERVICE DOOR AFT SLIDE MOUNT ISOLATOR. IAW SRM 51-40- - [SDR SWAA2026042491982](https://openairdocs.org/sdr/SWAA2026042491982), Apr 23, 2026: BATTERY PACK. FAILED. AFTER LT EMERGENCY BATTERY PACK M1672 FAILED CAPACITY CHECK. R&R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06 - [SDR SWAA2025093018958](https://openairdocs.org/sdr/SWAA2025093018958), Sep 28, 2025: HANDLE. LOOSE. PAX CABIN AFT LEFT DOOR ASSISTANT HANDLE LOOSE. TIGHTENED AFT LEFT DOOR ASSISTANT HANDLE IAW B737-700 AMM 52-13-31-400-802 STEP 3.G(2). - [SDR SWAA2025093018959](https://openairdocs.org/sdr/SWAA2025093018959), Sep 28, 2025: GIRT BAR. BINDING. PAX CABIN FWD SERVICE DOOR SLIDE GIRT BAR IS HARD TO CONNECT TO THE FLOOR SUPPORT FITTINGS. PERFORMED OPERATIONAL TEST ON SLIDE GIRT BAR FWD SERVICE DOOR IAW AM - [SDR SWAA2025093018611](https://openairdocs.org/sdr/SWAA2025093018611), Sep 26, 2025: LIGHT. BURNED. BURNED EMERGENCY LIGHT (1 EA) LOCATED BEHIND ACCESS PANEL 194FR AT LOWER FUSELAG. REPLACED EMERGENCY LIGHT (1 EA) LOCATED BEHIND ACCESS PANEL 194FR AT LOWER FUS - [SDR SWAA2025093018610](https://openairdocs.org/sdr/SWAA2025093018610), Sep 26, 2025: LIGHT. BURNED. BURNED EMERGENCY LIGHTS (2EA) LOCATED BEHIND ACCESS PANEL 194FL AT LOWER FUSELAGE AND LOCATED AT AFT ENTRY DOOR. REPLACED EMERGENCY LIGHTS (2EA) LOCATED BEHIND - [SDR SWAA2025093014344](https://openairdocs.org/sdr/SWAA2025093014344), Sep 14, 2025: LIGHT. DETERIORATED. DETERIORATE PHOTOLUMINESCENT AT PASSENGER CABIN RH SIDE (7EA). THE REPLACEMENT PHOTOLUMINESCENT STRIP RH SIDE AT PASSENGER CABIN (7 EA) WILL BE ACCOMPLISHED IN - [SDR SWAA2025093014343](https://openairdocs.org/sdr/SWAA2025093014343), Sep 14, 2025: LIGHT. DETERIORATED. DETERIORATE PHOTOLUMINESCENT STRIP AT PASSENGER CABIN LH SIDE (7EA). THE REPLACEMENT PHOTOLUMINESCENT STRIP AT PASSENGER CABIN LH SIDE (7EA) WILL BE ACCOMPLISHE - [SDR SWAA2025100213378](https://openairdocs.org/sdr/SWAA2025100213378), Sep 10, 2025: ANGLE. CRACKED. CRACK ON ANGLE LOCATED ON ACCESS PANEL 651FB TRAILING EDGE AT RT WING. REPLACED ANGLE IAW SRM 51-10-02 ITEM 9, SRM 51-40-05, AND DWG#115A2710 SHEET 6 REV B DUE - [SDR SWAA2025100213158](https://openairdocs.org/sdr/SWAA2025100213158), Sep 9, 2025: PAINT. PEELING. CORROSION SUPPORT STRUCTURE ACCESS PANEL 551FB TRAILING EDGE AT LT WING. PERFORMED DETAIL VISUAL INSPECTION ON SUPPORT STRUCTURE ACCESS PANEL 551FB TRAILING EDG - [SDR SWAA2025100213026](https://openairdocs.org/sdr/SWAA2025100213026), Sep 9, 2025: FAIRING. CRACKED. CRACKED FAIRING 644BB AT RT WING. PERFORMED PERMANENT REPAIR ON FAIRING PANEL 644BB AT RT WING IAW EA 25-157-02530-WIP1 AND STEPS ARE DOCUMENTED ON FAULT TTG8Q0 - [SDR SWAA2025100113159](https://openairdocs.org/sdr/SWAA2025100113159), Sep 9, 2025: WEB. CORRODED. CORROSION DOOR CUTOUT LOWER SILL BETWEEN BS 794 TO BS 847 AND STRINGER 25R AFT CARGO COMPARTMENT. REPLACED LOWER SILL LOCATED ON DOOR CUTOUT LOWER SILL BETWEEN - [SDR SWAA2025100113020](https://openairdocs.org/sdr/SWAA2025100113020), Sep 9, 2025: PLATE. CRACKED. CRACK CORRUGATED PLATE TRAILING EDGE ORSS 243, LT WING. REPLACED CORRUGATED PLATE TRAILING EDGE ORSS 243, LT WING IAW SRM 51-40-02-0G-0; DWG 115A2781 SHEET: 7 R - [SDR SWAA2025100212827](https://openairdocs.org/sdr/SWAA2025100212827), Sep 8, 2025: SUPPORT BRACKET. CRACKED. CRACK TRAILING EDGE SUPPORT BRACKET ORSS 271 AT RT WING. REPLACED TRAILING EDGE SUPPORT BRACKET ORSS 271 AT RT WING IAW SRM 51-40-02; SRM 51-40-05 AND DWG 115A2 - [SDR SWAA2025100112632](https://openairdocs.org/sdr/SWAA2025100112632), Sep 8, 2025: ANGLE. CRACKED. CRACK ANGLE, TRAILING EDGE ORSS 271 AT LT WING. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, STEP 9, AND DWG 115A2930, SHEET 7, REV-. DUE TO - [SDR SWAA2025100112828](https://openairdocs.org/sdr/SWAA2025100112828), Sep 8, 2025: PLATE. CRACKED. CRACK CORRUGATED PLATE TRAILING EDGE ORSS 261 RT WING. REPLACED CORRUGATED PLATE AND FASTENERS LOCATED ORSS 261 AT RT WING IAW SRM 51-40-02, & DWG 115A2714, SHE - [SDR SWAA2025100112633](https://openairdocs.org/sdr/SWAA2025100112633), Sep 8, 2025: BRACKET. CRACKED. CRACK TRAILING EDGE SUPPORT BRACKET ORSS 297 AT LT WING. REPLACED TRAILING EDGE SUPPORT BRACKET AND FILLER ORSS 297, LT WING IAW SRM 51-40-02, SRM 51-10-02, ITE - [SDR SWAA2025100112130](https://openairdocs.org/sdr/SWAA2025100112130), Sep 6, 2025: FLOORBEAM. CRACKED. CRACK BRAKE PANEL FLOOR STRUCTURE LOCATED BETWEEN BS540 AND BL0 TO LBL24.75 AT PASSENGER CABIN 2025-549876<[01] REPLACED BRAKE PANEL FLOOR STRUCTURE LOCATED BET - [SDR SWAA2025100112132](https://openairdocs.org/sdr/SWAA2025100112132), Sep 6, 2025: FLOOR SUPPORT. CRACKED. CRACK ANGLE FLOOR STRUCTURE, BS 695, BL 0. REPLACED THE FLOOR SUPPORT ANGLE AND FASTENERS IAW SRM 51-40-02-0G-0, AND DWG 273A9110, SHEET 6, REV A. - [SDR SWAA2025100112133](https://openairdocs.org/sdr/SWAA2025100112133), Sep 6, 2025: FLOOR SUPPORT. CRACKED. CRACK ANGLE FLOOR SUPPORT, BS 695, RBL 24.75. REPLACED THE FLOOR SUPPORT AND FASTENERS IAW SRM 51-40-02-0G-0, AND DWG 273A9110, SHEET 6, REV A. - [SDR SWAA2025100111977](https://openairdocs.org/sdr/SWAA2025100111977), Sep 5, 2025: STOP FITTING. CRACKED. CRACK AFT LOWER STOP FITTING SERVICE DOOR AT FWD GALLEY AND LAV . REPLACED STOP FITTING DOOR AND FASTENERS LOCATED ON AFT LOWER SERVICE DOOR AT FWD GALLEY AND L - [SDR SWAA2025100111639](https://openairdocs.org/sdr/SWAA2025100111639), Sep 5, 2025: SCUFF PLATE. CRACKED. CRACK FWD SCUFF PLATE LOCATED ON FWD CARGO DOOR CUT-OUT. REPAIRED AT CORNER FWD SCUFF PLATE LOCATED ON FWD CARGO DOOR CUT-OUT I. A.W. B737-700 SRM 53-30-15-2R-1 - [SDR SWAA2025093011643](https://openairdocs.org/sdr/SWAA2025093011643), Sep 5, 2025: FLOOR PANEL. DELAMINATED. DELAMINATED FLOOR PANEL 242AF AT PASSENGER CABIN. REPAIRED THE FLOOR PANEL 242AF IAW SRM 53-00-50-2R-1, REPAIR 1, AND SRM 53-00-50-2R-0, REPAIR GENERAL. - [SDR SWAA2025100111617](https://openairdocs.org/sdr/SWAA2025100111617), Sep 4, 2025: SCUFF PLATE. CRACKED. CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT. REPAIRED AT FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT I. A.W. B737-700 SRM 53-60-15-2R-1; REPAIR 1. - [SDR SWAA2025020392336](https://openairdocs.org/sdr/SWAA2025020392336), Feb 2, 2025: LIGHT. INOPERATIVE. L/H SLIDE EMERGENCY LIGHT INOP<[01] RE-LAMPED L/H SLIDE EMERGENCY LIGHT PER AMM 33-51-04. - [SDR SWAA2024102250274](https://openairdocs.org/sdr/SWAA2024102250274), Oct 18, 2024: SEAL. CRACKED. RT HORIZONTAL STABILIZER UPPER FWD SLIDER SEAL CRACKED 4 INCHES ON THE FWD SIDE.<[01] REMOVED AND REPLACED SLIDER SEAL PER AMM 53-31-31.;[02] INSPECTED WORK PER - [SDR SWAA2024102250275](https://openairdocs.org/sdr/SWAA2024102250275), Oct 18, 2024: SEAL. CRACKED. RT HORIZONTAL STABILIZER LOWER FWD SLIDER SEAL ATTACHMENT BRACKET BENT INWARDS AT A 45 DEGREE ANGLE AND IS CRACKING.<[01] REMOVED AND REPLACED SLIDER SEAL PER A - [SDR SWAA2024090433088](https://openairdocs.org/sdr/SWAA2024090433088), Sep 2, 2024: CONNECTOR. DISCONNECTED. DURING MV2 FOUND ROW 20ABC EMERGENCY LIGHT WONT TURN ON<[01] PERFORMED T/S IAW WDM 33-51-13-11 FOUND PLUG D11344 WAS DISCONNECTED. RECONNECTED PLUG D11344 EMERG - [SDR SWAA2024072616856](https://openairdocs.org/sdr/SWAA2024072616856), May 30, 2024: SKIN. CRACKED. DID UPPER R/H WING POST DOCK AND FOUND R/H LEADING EDGE #5 SLAT CRACK. CRACK IS 0.800 IN LENGTH LATERALLY. CRACK IS AT #5 SLAT STATION 89.69 (17.75 FROM TRAILIN - [SDR SWAA2023101608720](https://openairdocs.org/sdr/SWAA2023101608720), Oct 6, 2023: BATTERY. INOPERATIVE. AFT FLIGHT ATTENDANT STATION EMERGENCY FLASHLIGHTS ARE NOT FLASHING. ( 2 EA. REQUIRED)<[01] REPLACED BATTERY'S AT AFT FLIGHT ATTENDANT STATION EMERGENCY FLASHLI - [SDR SWAA2023101707853](https://openairdocs.org/sdr/SWAA2023101707853), Oct 5, 2023: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHT INOP FOR POWER SUPPLY/BATTERY PACK M1673<[01] REMOVE & REPLACE BATTERY PACK M1673 PER B737 AMM 33-51-06-960-805. PERFORM TEST OF BATTERY PACK OE - [SDR SWAA2023101704639](https://openairdocs.org/sdr/SWAA2023101704639), Sep 26, 2023: FLAP. DELAMINATED. LEFT WING O/B AFT FLAP I/B UPPER TRAILING EDGE TIP DELAMINATED DOT 223-LWAF2.<[01] FINAL STATEMENT: ACCOMPLISHED UT DISBOND INSP. ON UPPER SKIN AT LEFT WING O/B - [SDR SWAA2023101704304](https://openairdocs.org/sdr/SWAA2023101704304), Sep 25, 2023: FLAP. DELAMINATED. LEFT WING OUB AFT FLAP INB END LOWER TRAILING EDGE TIP DELAMINATED MKD DOT<[01] FINAL STATEMENT: REMOVED AND REPLACED L/H O/B AFT FLAP REF AMM 27-51-22-000-81 A - [SDR SWAA2023101602510](https://openairdocs.org/sdr/SWAA2023101602510), Sep 19, 2023: FLOOR PANEL. CRACKED. AFT CARGO COMPARTMENT PANEL 142KW IS CRACKED AT EDGE(MARKED)<[01] RECIEVED NEW AFT CARGO PANEL # 142KW; WILL BE INSTALLED ON TASK CARD# TTG8Q00MVWFY.;[02] FINAL - [SDR SWAA2023101700420](https://openairdocs.org/sdr/SWAA2023101700420), Sep 13, 2023: PANEL. ELONGATED. LEADING EDGE PANEL 521CB HAS MULTIPLE ELONGATED FASTENER HOLES<[01] APPLIED PERMANENT REPAIR ON DAMAGE AREA ON PANEL #521CB AS MARKED AS PER B737 SRM 57-41-01-2 - [SDR SWAA2023101700424](https://openairdocs.org/sdr/SWAA2023101700424), Sep 13, 2023: PANEL. ELONGATED. LEADING EDGE PANEL 511AT HAS ELONGATED FASTENER HOLES<[01] APPLIED PERMANENT REPAIR ON DAMAGE AREA ON PANEL #511AT AS MARKED AS PER B737 SRM 57-41-01-2R-1; B737 - [SDR SWAA2023101700425](https://openairdocs.org/sdr/SWAA2023101700425), Sep 13, 2023: PANEL. ELONGATED. LEADING EDGE PANEL 521FB HAS ELONGATED FASTENER HOLES<[01] APPLIED PERMANENT REPAIR ON DAMAGE AREA ON PANEL #521FB AS MARKED AS PER B737 SRM 57-41-01-2R-1; B737 - [SDR SWAA2023101798941](https://openairdocs.org/sdr/SWAA2023101798941), Sep 11, 2023: SLIDE. OUT OF ADJUST. FWD ENTRY DOOR. L1. SLIDE PRESSURE VISOR IS TORN.<[01] RECEIVED PART AND INSTALLATION WILL BE ACCOMPLISHED ON T/C MT 725-61-06;
SLIDE REM/INSTL TTG8Q00NC3V2; - [SDR SWAA2023101799116](https://openairdocs.org/sdr/SWAA2023101799116), Sep 11, 2023: SIDEWALL SUPPORT. ELONGATED. FWD CABIN WET AREA L/H SIDE WALL SUPPORT CLIP HOLE ELONGATED @ S-10L STA 270 MKD DOT<[01] REMOVED AND REPLACED SUPPORT CLIP AT FWD CABIN WET AREA L/H SIDE WALL; - [SDR SWAA2023101799112](https://openairdocs.org/sdr/SWAA2023101799112), Sep 11, 2023: FLOOR SUPPORT. CRACKED. MAIN CABIN CENTER WING BOX FLOOR SUPPORT BREAK CRACKED AT FASTENER'S TAIL RBL 1 STA 540<[01] REMOVED AND REPLACED SUPPORT BREAK ASSY AT MAIN CABIN STA 540 BETWE - [SDR SWAA2023101799114](https://openairdocs.org/sdr/SWAA2023101799114), Sep 11, 2023: ANGLE. CORRODED. CORROSION AT RIVETS TAILS 4EA ATTACHED ANGLE ABOVE L-1 DOOR STA 328<[01] REMOVED AND REPLACED 4EA RIVETS AT UPPER FUSELAGE SKIN ATTACHED ANGLE ABOVE L-1 DOOR ST - [SDR SWAA2023101799115](https://openairdocs.org/sdr/SWAA2023101799115), Sep 11, 2023: ANGLE. CORRODED. CORROSION AT SEVERAL RIVETS TAILS ATTACHED ANGLE ABOVE L-1 DOOR STA 328+ 10' MKD DOT<[01] REMOVED AND REPLACED RIVETS AT UPPER FUSELAGE SKIN ATTACHED ANGLE ABOV - [SDR SWAA2023101798929](https://openairdocs.org/sdr/SWAA2023101798929), Sep 10, 2023: FLOOR SUPPORT. CRACKED. BELOW CABIN FLOOR SUPPORT BREAK CRACKED AT CENTER WING BOX LBL 2 STA 540<[01] REMOVED AND REPLACED SUPPORT BREAK ASSY AT MAIN CABIN STA 540 BETWEEN BL 0 TO LBL - [SDR SWAA2023101798488](https://openairdocs.org/sdr/SWAA2023101798488), Sep 8, 2023: ACCESS PANEL. CORRODED. ***CORROSSION*** FWD CARGO COMPARTMENT FLOOR ACCESS PANEL # 120BF HAS LIGHT CORROSSION<[01] REMOVED CORROSION AT FWD CARGO COMPARTMENT FLOOR ACCESS PANEL #120BF - [SDR SWAA2023101798489](https://openairdocs.org/sdr/SWAA2023101798489), Sep 8, 2023: ACCESS PANEL. CORRODED. ***CORROSSION*** FWD CARGO COMPARTMENT FLOOR ACCESS PANEL # 120AF HAS LIGHT CORROSSION<[01] REMOVED CORROSION AT FWD CARGO COMPARTMENT FLOOR ACCESS PANEL #120AF - [SDR SWAA2023101798490](https://openairdocs.org/sdr/SWAA2023101798490), Sep 8, 2023: ACCESS PANEL. CORRODED. ***CORROSSION*** FWD CARGO COMPARTMENT FLOOR ACCESS PANEL # 120CF HAS LIGHT CORROSSION<[01] REMOVED CORROSION AT FWD CARGO COMPARTMENT FLOOR ACCESS PANEL #120CF - [SDR SWAA2023101699598](https://openairdocs.org/sdr/SWAA2023101699598), Sep 7, 2023: SUPPORT ANGLE. CRACKED. RIGHT VAPOR BARRIER UPPER SUPPORT ANGLE STA 663 FOUND CRACK AT RBL 7.<[01] REPAIRED AREA AT VAPOR BARRIER UPPER SUPPORT ANGLE STA 663 AS PER B 737-700 SRM 57-10 - [SDR SWAA2023101797257](https://openairdocs.org/sdr/SWAA2023101797257), Sep 6, 2023: SKIN. CRACKED. CRACK FOUND ON LOWER SKIN OF R/H HORIZONTAL STABILIZER AT STAB STA 193.90; 8.5' FROM FRONT SPAR; I/B ROW. CRACK LENGTH : 1'. CRACK FOUND ON LOWER SKIN OF R/H HO - [SDR SWAA2023101797421](https://openairdocs.org/sdr/SWAA2023101797421), Sep 6, 2023: SLAT. PULLED. LEFT WING # 3 SLAT ACTUATOR LOWER SURFACE OF L/E HAS SIX FASTENERS PULLED IN.<[01] CUT DAMAGED AND FABRICATE REPAIR PARTS DOUBLER AND FILLER. EVALAUTED SURFACE - [SDR SWAA2023101797427](https://openairdocs.org/sdr/SWAA2023101797427), Sep 6, 2023: SLAT. PULLED. LEFT WING # 2 SLAT ACTUATOR LOWER SURFACE OF L/E HAS SEVEN FASTENERS PULLED IN.<[01] CRACK FOUND ON #2 SLAT ACTUATOR FITTING. SLAT REPLACEMENT TO BE ACCOMPLISHE All 250: https://openairdocs.org/aircraft/N7833A/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 ## Earlier aircraft with N7833A The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N7833A before. - [Cancelled 1957-01-08](https://openairdocs.org/deregistered/N7833A-1957-01-08): Cessna 180A, S/N 32730. Owner: [Cessna Aircraft Co](https://openairdocs.org/faa-owner/CESSNA%20AIRCRAFT%20CO), [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita) ## Related - Other Boeing 737-79P aircraft: https://openairdocs.org/model/boeing-737-79p/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.