# N7826B: 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: 30035 - Year built: 2003 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 25, 2015 - Certificate issued: January 9, 2023 - Expires: January 31, 2030 - Mode S code: AA9B20 - 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=7826B - Page: https://openairdocs.org/aircraft/N7826B 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. ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB ENG24WA013](https://openairdocs.org/ntsb/ENG24WA013), Apr 27, 2024: Boeing 737-79P (N7826B), San Miguel de Cozumel, Mexico, incident, no damage ## NTSB investigations on N7826B not matched to an aircraft (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB DEN66A0040](https://openairdocs.org/ntsb/DEN66A0040), Nov 22, 1965: Beech T-34A (N7826B), Kamas, UT, destroyed, 1 fatal ## FAA accident and incident reports None matched to N7826B. ## 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 ## Service difficulty reports (256, 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 SWAA2026102046931](https://openairdocs.org/sdr/SWAA2026102046931), Oct 16, 2026: HANDLE. LOOSE. FWD L1 PAX DOOR INNER HANDLE LOOSE. SECURED THE FWD ENTRY DOOR HANDLE HARDWARE IAW AMM 52-11-31, & OPS CHKD GOOD. - [SDR SWAA2026100849482](https://openairdocs.org/sdr/SWAA2026100849482), Oct 4, 2026: HANDLE. BROKEN. FIRE EXTINGUISHER HANDLE BROKEN IN THE FLIGHT DECK. R & R THE FIRE EXTINGUISHER IAW AMM. 26-26-01. - [SDR SWAA2025122354471](https://openairdocs.org/sdr/SWAA2025122354471), Dec 20, 2025: HANDLE. LOOSE. R2 DOOR GRAB HANDLE IS LOOSE. ADJUSTED R2 DOOR GRAB HANDLE IAW SOPM 20-50-01. - [SDR SWAA2025111735581](https://openairdocs.org/sdr/SWAA2025111735581), Nov 15, 2025: PANEL. CRACKED. WHEN REMOVING SEAL FOUND CRACK ON COVE PANEL. PERMANENT REPAIR ACCOMPLISHED PER SRM 55-40-30-1A-1. - [SDR SWAA2025110731515](https://openairdocs.org/sdr/SWAA2025110731515), Nov 4, 2025: GIRT BAR. OUT OF ADJUST. AFT GALLEY L2 DOOR GIRT BAR HANGS LOW. SECURED L2 DOOR EMERGENCY SLIDE GIRT BAR IAW SIP. - [SDR SWAA2025081300006](https://openairdocs.org/sdr/SWAA2025081300006), Aug 9, 2025: LIGHT. BURNED. PAX CABIN 2 EA EMERGENCY LIGHT BURNED AT 11R AND 16R SEATS POSITIONS. REPLACED PAX CABIN 2 EA EMERGENCY LIGHT AT 11R AND 16R SEATS POSITIONS. I.A.W B737-700 AMM - [SDR SWAA2025081493375](https://openairdocs.org/sdr/SWAA2025081493375), Jul 20, 2025: WEB. CORRODED. CORROSION WEB LOWER SILL LOCATED BETWEEN BS 440 - 492.4 AND RBL 26, WL 156 AT FWD CARGO COMPARTMENT. REPLACED WEB LOWER SILL AND FASTENERS LOCATED BETWEEN STA44 - [SDR SWAA2025081493373](https://openairdocs.org/sdr/SWAA2025081493373), Jul 20, 2025: ANGLE. CRACKED. CRACK ANGLE TRAILING EDGE LOCATED IRSS 141 AT RT WING. REPLACED ANGLE TRAILING EDGE LOCATED IRSS 141 AT RT WING IAW SRM 51-40-02 AND SRM 51-10-02 PARAGRAPH 9. M - [SDR SWAA2025081493143](https://openairdocs.org/sdr/SWAA2025081493143), Jul 19, 2025: ANGLE. CRACKED. CRACK ANGLE TRAILING EDGE LOCATED IRSS 141 AT LT WING. REPLACED ANGLE TRAILING EDGE LOCATED IRSS 141 AT LT WING IAW SRM 51-40-02, AND SRM 51-10-02, PARAGRAPH 9, - [SDR SWAA2025081493140](https://openairdocs.org/sdr/SWAA2025081493140), Jul 19, 2025: PLATE. CRACKED. CRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 217 AT LT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 217 AT LT WING IAW SRM 51-40-02; SRM 51-1 - [SDR SWAA2025081393153](https://openairdocs.org/sdr/SWAA2025081393153), Jul 19, 2025: LIGHT. BROKEN. BROKEN GALLEY 1 EMERGENCY EXIT BASE AT FWD GALLEY AREA . REPLACED GALLEY 1 EMERGENCY EXIT BASE AT FWD GALLEY AREAI.A.W. BOEING 737-700 AMM 33-51-01-960-802. TES - [SDR SWAA2025081492540](https://openairdocs.org/sdr/SWAA2025081492540), Jul 18, 2025: PRESSURE WEB. CRACKED. CRACK INDICATION FOUND AT HORIZONTAL PRESSURE DECK WEB BETWEEN STA 663 TO STA 675 AT LBL 31 AT MAIN WHEEL WELL COMPARTMENT CRACK LENGTH: 0.500 INCHES APPROX. RE - [SDR SWAA2025081392833](https://openairdocs.org/sdr/SWAA2025081392833), Jul 18, 2025: HANDLE. DETERIORATED. DETERIORATED ASSIST HANDLE NUT ON FORWARD ENTRY DOOR LINING AT FORWARD GALLEY AREA (4EA). REPLACED ASSIST HANDLE NUT ON FORWARD ENTRY DOOR LINING AT FORWARD GAL - [SDR SWAA2025081492536](https://openairdocs.org/sdr/SWAA2025081492536), Jul 17, 2025: FLOORBEAM. CRACKED. CRACK FLOOR STRUCTURE BRAKE PANEL BS 540 AND RBL 1 AT PASSENGER CABIN. REPLACED FLOOR STRUCTURE BRAKE PANEL BS 540 AND BTW RBL 0 TO RBL 24.75 PASSENGER CABIN IA - [SDR SWAA2025081492537](https://openairdocs.org/sdr/SWAA2025081492537), Jul 17, 2025: FLOORBEAM. CRACKED. CRACK FLOOR STRUCTURE BRAKE PANEL BS 540 AND LBL 1 AT PASSENGER CABIN. REPLACED FLOOR STRUCTURE BRAKE PANEL LOCATED ON BS 540 AND LBL 1 AT PASSENGER CABIN IAW S - [SDR SWAA2025081492290](https://openairdocs.org/sdr/SWAA2025081492290), Jul 17, 2025: RIB. CRACKED. CRACK ON INSPAR RIB 3 HSS 111.10 AT 38 INCHES FROM FRONT SPAR (STIFFENER 4) RT HORIZONTAL STAB. PERFORMED REPAIRED ON INSPAR RIB 3(STAB STA 111.10) AT 38 INCHES - [SDR SWAA2025081491965](https://openairdocs.org/sdr/SWAA2025081491965), Jul 16, 2025: PANEL. ELONGATED. ELONGATED HOLES ON ACCESS PANEL 561BB TRAILING EDGE AT LT WING. REPAIRED ACCESS PANEL 561BB TRAILING EDGE AT LT WIN IAW SRM 51-70-04-2R-10 REPAIR 10. - [SDR SWAA2025081491720](https://openairdocs.org/sdr/SWAA2025081491720), Jul 15, 2025: ANGLE. CRACKED. CRACK ANGLE TRAILING EDGE ORSS 271 RT WING. REPLACED ANGLE TRAILING EDGE ORSS 271, RT WING IAW SRM 51-10-02-0G-0 ITEM 9, SRM 51-40-02-0G-0, AND DWG 115A2930, SH - [SDR SWAA2025081491722](https://openairdocs.org/sdr/SWAA2025081491722), Jul 15, 2025: SUPPORT BRACKET. CRACKED. CRACK SUPPORT BRACKET TRAILING EDGE ORSS 271 AT LT WING. REPLACED SUPPORT BRACKET TRAILING EDGE ORSS 271 AT LT WING IAW SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 A - [SDR SWAA2025081491393](https://openairdocs.org/sdr/SWAA2025081491393), Jul 14, 2025: ACCESS PANEL. DAMAGED. ELONGATED HOLE ON ACCESS PANEL 193B, BODY FAIRING AT LOWER FUSELAGE. REPAIRED THE ACCESS PANEL 193B, BODY FAIRING AT LOWER FUSELAGE IAW SRM 51-70-04-2R-9 REPAIR - [SDR SWAA2024080722092](https://openairdocs.org/sdr/SWAA2024080722092), Aug 3, 2024: LIGHT. INOPERATIVE. FWD SERVICE DOOR ESCAPE SLIDE LIGHT INOP<[01] REPLACED FWD SERVICE DOOR SLIDE LIGHT REF AMM 33-51-04 - [SDR SWAA2024052387943](https://openairdocs.org/sdr/SWAA2024052387943), May 20, 2024: LANDING GEAR. FAILED. AFTER T/O AND AIRCRAFT IN CLEAN CONFIGURATION FO PUT THE GEAR HANDLE IN 'OFF' POSITION. NOSE GEAR EXTENED; MAIN DID NOT.<[01] 02 - INSPECTED PER [AMM 32-33-00-7 - [SDR SWAA2023092101771](https://openairdocs.org/sdr/SWAA2023092101771), Sep 18, 2023: LIGHT. INOPERATIVE. EMERGENCY EXIT AREA LIGHT IN RIGHT OVERWING ESCAPE HATCH INOP<[01] RELAMPED EMERGENCY EXIT AREA LIGHT IN RIGHT OVERWING ESCAPE HATCH AND TESTED GOOD IAW AMM 33- - [SDR SWAA2023092199509](https://openairdocs.org/sdr/SWAA2023092199509), Sep 12, 2023: SCUFF PLATE. CRACKED. AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED<[01] WELDED AFT CARGO BAY AFT CORNER SCUFF PLATE PER SRM 53-60-15-2R-1 PARAGRAPH 4.B. (2); (4); (5) USING ER4043 - [SDR SWAA2023092199508](https://openairdocs.org/sdr/SWAA2023092199508), Sep 12, 2023: SCUFF PLATE. CRACKED. AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED< - [SDR SWAA2023092195952](https://openairdocs.org/sdr/SWAA2023092195952), Sep 1, 2023: BAFFLE. CRACKED. FCB BAFFLE IS CRACKED BETWEEN BS 400 TO BS 420 LBL 24 WL 156<[01] REMOVED AND REPLACED FCB BAFFLE BETWEEN BS400 TO BS420;LBL24;WL156.IAW SRM 51-40-02 AND DWG#14 - [SDR SWAA2023092195951](https://openairdocs.org/sdr/SWAA2023092195951), Sep 1, 2023: BAFFLE. CRACKED. FCB BAFFLE IS CRACKED BETWEEN BS 400 TO BS 420 LBL 24 WL 156< - [SDR SWAA2023092593244](https://openairdocs.org/sdr/SWAA2023092593244), Aug 24, 2023: SKIN. CORRODED. SURFACE CORROSION ON UPPER CROWN SKIN UNDER VERT STAB FUSELAGE STA 1016 TO STA 1040 AND FROM STRINGERS S-2AR TO S-2AL.<[01] REMOVED FASTENERS BETWEEN BS1016- BS - [SDR SWAA2023092592616](https://openairdocs.org/sdr/SWAA2023092592616), Aug 22, 2023: SEAL. CRACKED. RT HORIZONTAL STAB FWD UPPER SLIDE SEAL CRACKED.<[01] REMOVED AND INSTALLED NEW RT HORIZONTAL STAB FWD UPPER SLIDE SEAL PER AMM 53-31-31.;[02] FINAL INSPECTION. - [SDR SWAA2023092592618](https://openairdocs.org/sdr/SWAA2023092592618), Aug 22, 2023: TRACK. CRACKED. RT HORIZONTAL STAB UPPER FWD TRACK FOR PANEL 343AT CRACKED.<[01] REMOVED AND REPLACED RT HORIZONTAL STAB UPPER FWD TRACK FOR PANEL 343AT PER AMM 20-50-11-910-80 - [SDR SWAA2023092592598](https://openairdocs.org/sdr/SWAA2023092592598), Aug 22, 2023: SUPPORT. CORRODED. AFT CARGO FLOOR TO SIDE WALL SUPPORT HAS CORROSION AT BS 727+7 - 747+2; RBL 21; WL 156<[01] EFFECTIVITY SRM 53-60-53-0I-2 IDENTIFICATION 2 AND SRM 53-00-53-1A-2 - [SDR SWAA2023092192080](https://openairdocs.org/sdr/SWAA2023092192080), Aug 22, 2023: SHIELD. CORRODED. CORROSION ON FORWARD CARGO COMPARTMENT DOOR CUT-OUT AFT SHIELD FROM STA 500 TO 500A; RBL 24; WL 156.<[01] THE STRUCTURAL ITEM DOES NOT HAVE ALLOWABLE DAMAGE ENT - [SDR SWAA2023092192081](https://openairdocs.org/sdr/SWAA2023092192081), Aug 22, 2023: WEB. CORRODED. CORROSION ON FORWARD CARGO BAY DOOR CUT-OUT SUB-THRESHOLD WEB FROM STA 440+11 TO 460+10; RBL 28 TO 30; WL 156.<[01] VERIFIED APLICABILITY SRM 53-30-53-0I-2 FOR - [SDR SWAA2023092192077](https://openairdocs.org/sdr/SWAA2023092192077), Aug 22, 2023: SIDEWALL SUPPORT. CORRODED. CORROSION ON FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT STA 500A+2; +6; +10; +14; +18; 500B+2; +6; +18; RBL 24; WL 158.<[01] REPLACED ON FWD CARGO BAY FLOOR - [SDR SWAA2023092192078](https://openairdocs.org/sdr/SWAA2023092192078), Aug 22, 2023: SIDEWALL SUPPORT. CORRODED. CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT ANGLE AT STA 500C+2; +16; +18; RBL 24; WL 156.<[01] CORROSION AT SUPPORT ANGLE OF FWD CARGO BAY FLOOR SIDEW - [SDR SWAA2023092192079](https://openairdocs.org/sdr/SWAA2023092192079), Aug 22, 2023: SHIELD. CORRODED. CORROSION ON FWD CARGO DOOR CUT-OUT FWD SHIELD AT STA 420+6 & 420+9; WL 156; RBL 24.<[01] THE STRUCTURAL ITEM DOES NOT HAVE ALLOWABLE DAMAGE ENTRIES. THEREFORE; - [SDR SWAA2023092192082](https://openairdocs.org/sdr/SWAA2023092192082), Aug 22, 2023: SIDEWALL SUPPORT. CORRODED. CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT ANGLE AT STA 460+18; 480+6; +10; 500A+14; 500B+17; 500C+13; LBL 24; WL 156.<[01] VERIFIED APPLICABILITY SRM - [SDR SWAA2023092192594](https://openairdocs.org/sdr/SWAA2023092192594), Aug 22, 2023: SUPPORT. CORRODED. AFT CARGO HAS CORROSION ON FWD BULKHEAD SUPPORT AT BS 727+4; LBL 22; WL 155<[01] REMOVED AND REPLACED AFT CARGO FWD BULKHEAD SUPPORT AT BS727+4 PER SRM 51-40-02 - [SDR SWAA2023092192596](https://openairdocs.org/sdr/SWAA2023092192596), Aug 22, 2023: SIDEWALL SUPPORT. CORRODED. AFT CARGO FLOOR TO SIDE WALL SUPPORT HAS CORROSION AT BS 727B+4 - 727E+10; LBL 21; WL 156<[01] REMOVED AND REPLACED AFT CARGO FLOOR TO SIDEWALL SUPPORT FROM BS - [SDR SWAA2023092192602](https://openairdocs.org/sdr/SWAA2023092192602), Aug 22, 2023: SIDEWALL SUPPORT. CORRODED. AFT CARGO FLOOR TO SIDE WALL SUPPORT HAS CORROSION AT BS 727E+14 - 787+2; LBL 21; WL 157<[01] THIS CARD WILL BE ACCOMPLISHED ON CUSTOMER CARD NBR: TTG8Q00MZS35; - [SDR SWAA2023092192604](https://openairdocs.org/sdr/SWAA2023092192604), Aug 22, 2023: SUPPORT. CORRODED. AFT CARGO AFT BULKHEAD SUPPORT HAS CORROSION AT BS 927; RBL 13; WL 180<[01] THIS FAULT WILL BE ACCOMPLISHED ON NRC #: TTG8Q00MZT48;[02] TASK CARD COMPLETE - [SDR SWAA2023092192614](https://openairdocs.org/sdr/SWAA2023092192614), Aug 22, 2023: SUPPORT. CORRODED. AFT CARGO AFT BULKHEAD SUPPORT HAS CORROSION AT BS 927; LBL 3; WL 180<[01] OK TO INSTALL GIVEN;[02] REMOVED AND REPLACED AFT CARGO AFT BULKHEAD SUPPORT PER SRM - [SDR SWAA2023092192084](https://openairdocs.org/sdr/SWAA2023092192084), Aug 22, 2023: ATTACH ANGLE. CRACKED. CRACK ON FWD CARGO BAY BAFFLE ATTACH ANGLE AT STA 400+19.5; WL 155; RBL 24.<[01] REMOVED AND REPLACED FWD CARGO BAY BAFFLE ATTACH ANGLE AT STA 400+19.5; WL 155; - [SDR SWAA2023092190827](https://openairdocs.org/sdr/SWAA2023092190827), Aug 18, 2023: STRINGER. CRACKED. CRACKED STRINGER AT AREA AFT OF FCB BS535 S-26R WL153. MARKED<[01] REPAIRED STRINGER NBR 26RH PER REF SRM 53-00-03-2R-1;[02] VERIFIED COMPLETION OF CORRECTIVE A - [SDR SWAA2023092190828](https://openairdocs.org/sdr/SWAA2023092190828), Aug 18, 2023: STRINGER. CRACKED. CRACKED STRINGER AT AREA AFT OF FCB BS535 S-27R WL150. MARKED<[01] VERIFIED STEP 4 COMPLETE; STEP 5 IN PARTIAL OK TO INSTALL GIVEN.;[02] REPAIRED FCB STRINGER 2 - [SDR SWAA2023092190829](https://openairdocs.org/sdr/SWAA2023092190829), Aug 18, 2023: STRINGER. CRACKED. CRACKED STRINGER AT AREA AFT OF FCB BS535 S-23R WL164. MARKED<[01] VERIFIED STEPS 4 AND 5.;[02] RECEIVED NEW STRINGER SECTION FROM OSS ITEM HFAB53-STR-011 LOT N - [SDR SWAA2023092190830](https://openairdocs.org/sdr/SWAA2023092190830), Aug 18, 2023: STRINGER. CRACKED. CRACKED STRINGER AT AREA AFT OF FCB BS535 S-26L WL153. MARKED<[01] PERFOMED STRINGER REPAIR PER REF SRM 53-00-03-2R-1;[02] VERIFIED CORRECTIVE ACTION 1.;[03] VE - [SDR SWAA2023092590822](https://openairdocs.org/sdr/SWAA2023092590822), Aug 17, 2023: STIFFENER. CRACKED. RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 129.50; 3RD VERTICAL STIFFENER IS CRACKED.<[01] UPDATED MEASUREMENT CHART.;[02] REMOVED THE D - [SDR SWAA2023092590824](https://openairdocs.org/sdr/SWAA2023092590824), Aug 17, 2023: STIFFENER. CRACKED. RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 129.50; 4TH VERTICAL STIFFENER IS CRACKED.<[01] UPDATED MEASUREMENT CHART.;[02] REMOVED THE D - [SDR SWAA2023092597933](https://openairdocs.org/sdr/SWAA2023092597933), Aug 17, 2023: PANEL. ERODED. LT WING L/E PANEL 521UB HAS WIND EROSION ON CORNER (MARKED)