# N293WN: 2007 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: 36612 - Year built: 2007 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 18, 2007 - Certificate issued: October 9, 2007 - Expires: August 31, 2028 - Mode S code: A302A0 - 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=293WN - Page: https://openairdocs.org/aircraft/N293WN From the FAA registry file of October 21, 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 (1) From the NTSB's public API. Aircraft 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. - [NTSB OPS11IA428](https://openairdocs.org/ntsb/OPS11IA428), Mar 27, 2011: Boeing 737-7H4 (N293WN), Orlando, FL, incident, no damage. Probable cause: The air traffic controllers’ application of inappropriate separation between the B737 and the Cirrus and their inappropriate use of airborne civilian aircraft for observation of other airborne… ## FAA accident and incident reports None matched to N293WN. ## Service difficulty reports (269, newest 50) As reported by operators and repair stations. - [SDR SWAA2026051904055](https://openairdocs.org/sdr/SWAA2026051904055), May 17, 2026: GIRT BAR. UNSECURE. FWD SERVICE DOOR SLIDE WILL NOT STAY IN THE STOWED POSITION. RESECURED FWD SERVICE DOOR SLIDE GIRT BAR IN THE STOWED POSITION. REF AMM 25-66-01. OK FOR SERVICE. - [SDR SWAA2026021971705](https://openairdocs.org/sdr/SWAA2026021971705), Feb 18, 2026: BATTERY PACK. NO TEST. EMERGENCY BATTERY PACK FAILED TIMED CHECK AT 14 ABC. R & R THE BATTERY PACK IAW AMM 33-51-06. - [SDR SWAA2025052072088](https://openairdocs.org/sdr/SWAA2025052072088), May 17, 2025: HOOK. OUT OF ADJUST. FWD SERVICE DOOR FORWARD GIRT BAR STOWAGE HOOK DOES NOT STOW GIRT BAR SECURELY <[01]. ADJUSTED FORWARD SERVICE DOOR; FORWARD GIRT BAR STOWAGE HOOK PER SIP. OPS - [SDR SWAA2025051467110](https://openairdocs.org/sdr/SWAA2025051467110), May 4, 2025: LIGHT. DAMAGED. FWD LAV EMERGENCY EXIT LIGHT DAMAGED<[01] REPLACED FWD LAVATORY 'A' EXIT LIGHT WITH NEW ASSEMBLY IAW AMM 33-51-01-960-802.;[02] ADDITION: SATISFACTORY OPERATION - [SDR SWAA2025051366262](https://openairdocs.org/sdr/SWAA2025051366262), May 1, 2025: FLOOR SUPPORT. CORRODED. CORROSION ON ACB FLOOR SUPPORT INTERCOSTAL STA 767+5; RBL 25<[01] REMOVED AND REPLACED ACB FLOOR SUPPORT INTERCOSTAL AT STA 767 TO STA 787; RBL 25 LOT 1602576-1 - [SDR SWAA2025051465016](https://openairdocs.org/sdr/SWAA2025051465016), Apr 28, 2025: SCUFF PLATE. CRACKED. FWD CAREGO BAY FWD CORNER SCUFF PLATE IS CRACKED<[01] JOB CARD COMPLETED AND INSTALLED ON CUSTOMER CARD TTG8Q00ZSUFL;[02] REPAIRED FCB FWD CORNER SCUFF PLATE IA - [SDR SWAA2025051464309](https://openairdocs.org/sdr/SWAA2025051464309), Apr 25, 2025: PLATE. CORRODED. LWR FUSELAGE - ANTENNA COVER PLATE AREA HAS EVIDENCE OF CORROSION AND FILLET SEAL DETERIORATED AT STA 410; STR 27L.<[01] REMOVED AND REPLACED THE LWR FUSELAGE - - [SDR SWAA2025051456877](https://openairdocs.org/sdr/SWAA2025051456877), Apr 25, 2025: FLOORBEAM. CRACKED. MAIN CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO RBL 24.75.<[01] REMOVED AND REPLACED NEW PANEL BREAK ASSY P/N 143A5240-64 LOT 1601361-1 AT STA - [SDR SWAA2025051456875](https://openairdocs.org/sdr/SWAA2025051456875), Apr 25, 2025: FLOORBEAM. CRACKED. MAIN CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO LBL 24.75.<[01] REMOVED AND REPLACED NEW PANEL BREAK ASSY P/N 143A5240-63 LOT 1602100-2 AT STA - [SDR SWAA2025051456870](https://openairdocs.org/sdr/SWAA2025051456870), Apr 24, 2025: PANEL. DELAMINATED. PANEL 193D HAS DELAMINATION ON INNER SURFACE CORE<[01] DELAMINATION TO INNER SURFACE CORE OF PANEL 193D WAS REPAIRED IAW SRM 51-70-05-2R-2.;[02] VERIFIED CORREC - [SDR SWAA2025051356866](https://openairdocs.org/sdr/SWAA2025051356866), Apr 21, 2025: SUPPORT ANGLE. CORRODED. CORROSION ON SUPPORT ANGLE ACB STA-767 TO 790 RBL-25 COMMON TO FWD SHIELD.<[01] REMOVED AND REPLACED NEW ON SUPPORT ANGLE ACB BS767 TO BS 787 RBL 25 IAW SRM 51- - [SDR SWAA2025051456818](https://openairdocs.org/sdr/SWAA2025051456818), Apr 16, 2025: FLOORBEAM. CORRODED. CORROSION ON BS986 FLOOR BEAM AT NUTPLATE HOLES AT RBL 27.5; RBL31.5; RBL35.5 AND RBL 43 WL208.1<[01] REPAIRED PASSENGER CABIN FLOOR BEAM BS 986 IAW SRM 53-70-5 - [SDR SWAA2025051441158](https://openairdocs.org/sdr/SWAA2025051441158), Apr 16, 2025: VAPOR BARRIER. CRACKED. R/H VAPOR BARRIER CRACKED AT BS 663<[01] R/H VAPOR BARRIER CRACK AT BS 663 WAS REPAIRED IAW SRM 51-70-04-2R-10;[02] VERIFIED CORRECTIVE ACTION ITEM 1. - [SDR SWAA2025051441159](https://openairdocs.org/sdr/SWAA2025051441159), Apr 16, 2025: VAPOR BARRIER. CRACKED. L/H VAPOR BARRIER CRACKED AT BS 663<[01] L/H VAPOR BARRIER CRACK AT BS663 WAS REPAIRED IAW SRM 51-70-04-2R-10.;[02] VERIFIED CORRECTIVE ACTION ITEM 1. - [SDR SWAA2025051456819](https://openairdocs.org/sdr/SWAA2025051456819), Apr 16, 2025: SEAL. CRACKED. RT. HORIZONTAL STAB FWD UPPER SLIDE SEAL CRACKED.<[01] REMOVED AND REPLACED RT. HORIZONTAL STAB FWD UPPER SLIDE SEAL IAW AMM 53-31-31-000-802 AND AMM 53-31-31-4 - [SDR SWAA2025051456782](https://openairdocs.org/sdr/SWAA2025051456782), Apr 15, 2025: SUPPORT ANGLE. CRACKED. WATER SERVICE PAN AFT SUPPORT ANGLE CRACKED AT APPROX. STA 907+15 (MARKED)<[01] REMOVED AND REPLACED WATER SERVICE PAN AFT SUPPORT ANGLE AT APPROX. STA 907+15 P - [SDR SWAA2025051456786](https://openairdocs.org/sdr/SWAA2025051456786), Apr 15, 2025: WEB. CANNING. CORROSION ON ACB SUB THRESHOLD WEB AT MULTIPLE AREAS<[01] REMOVED AND REPLACED ACB THRESHOLD WEB IAW SRM 51-40-02-0G-0 AND DWG 146A8340; ID: 0024 REV: A.;[02] V - [SDR SWAA2025051456780](https://openairdocs.org/sdr/SWAA2025051456780), Apr 15, 2025: SUPPORT. CORRODED. CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT STA 747+10; LBL 25<[01] THIS CARD WILL BE ACCOMPLISHED ON TASK CARD # TTG8Q00ZV5YL
FOR REPLACEMENT PART.;[02] VERI - [SDR SWAA2025051456791](https://openairdocs.org/sdr/SWAA2025051456791), Apr 15, 2025: SHIELD. CORRODED. CORROSION ON FWD CARGO BAY DOOR CUT-OUT FWD SHIELD AT STA 420+2; 420+9; 420+17; WL 156; RBL 24.<[01] REMOVED AND REPLACED NEW ON FWD CARGO BAY DOOR CUT-OUT FWD - [SDR SWAA2025051456783](https://openairdocs.org/sdr/SWAA2025051456783), Apr 15, 2025: SHIELD. CORRODED. CORROSION ON FWD CARGO BAY DOOR CUT-OUT AFT SHIELD AT STA 500+12 AND 500+16; WL 156; RBL 24.<[01] REMOVED AND REPLACED NEW ON FWD CARGO BAY DOOR CUT-OUT AFT SHI - [SDR SWAA2025051456800](https://openairdocs.org/sdr/SWAA2025051456800), Apr 15, 2025: WEB. CORRODED. CORROSION ON FWD CARGO SUB-THRESHOLD WEB FROM STA 440+6 TO 480+9 RBL 25 TO RBL 28; WL 156.<[01] REMOVED AND REPLACED NEW ON FWD CARGO SUB-THRESHOLD WEB BS440 TO - [SDR SWAA2025051456766](https://openairdocs.org/sdr/SWAA2025051456766), Apr 15, 2025: FLOOR SUPPORT. CRACKED. CRACKED INTERCOSTAL AT STA 324; RBL 30; WL 208.1<[01] REMOVED AND INSTALLED AT DISCREPANCY AREA NEW INTERCOSTAL PN:141A5410U140ATSMRO; LOT#1598453-1 PER DWG#141 - [SDR SWAA2025051456815](https://openairdocs.org/sdr/SWAA2025051456815), Apr 15, 2025: SEAL. CRACKED. LT HORIZONTAL STAB FWD UPPER SLIDE SEAL CRACKED.<[01] REMOVED AND REPLACED LT HORIZONTAL STAB FWD UPPER SLIDE SEAL
PER AMM 53-31-31-000-802. (REMOVAL)
PE - [SDR SWAA2025051356788](https://openairdocs.org/sdr/SWAA2025051356788), Apr 15, 2025: SIDEWALL SUPPORT. CORRODED. DAMAGE ON ACB FLOOR TO SIDEWALL SUPPORT STA 787; LBL 25<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT P/N 146A7502-27; LOT 1601300-2 AT ACB BS727 - BS847 - [SDR SWAA2025051356802](https://openairdocs.org/sdr/SWAA2025051356802), Apr 15, 2025: FLOOR PANEL. PULLED. FWD FLOOR PANEL 222DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] 222DF FLOOR PANEL UPPER SKIN DAMAGE HAS BEEN REPAIRED PER [SRM 53-00-50-2R-0-A00938 (REPAIR G - [SDR SWAA2025051356798](https://openairdocs.org/sdr/SWAA2025051356798), Apr 15, 2025: FLOOR PANEL. PULLED. FWD FLOOR PANEL 222CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] 222CF FLOOR PANEL UPPER SKIN DAMAGE HAS BEEN REPAIRED PER [SRM 53-00-50-2R-1-A00939 (REPAIR 1 - [SDR SWAA2025051356801](https://openairdocs.org/sdr/SWAA2025051356801), Apr 15, 2025: FLOOR PANEL. PULLED. FWD FLOOR PANEL 221CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221CF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE - [SDR SWAA2025051356781](https://openairdocs.org/sdr/SWAA2025051356781), Apr 15, 2025: SHIELD. CORRODED. CORROSION ON ACB FWD SHEILD STA 767-792; RBL 25<[01] REMOVED AND REPLACED ACB FWD SHEILD STA 767-794; RBL 25 IAW SRM 51-10-02-0G-0 AND DWG# 146A0081 ID: 0040 RE - [SDR SWAA2025051356779](https://openairdocs.org/sdr/SWAA2025051356779), Apr 15, 2025: SIDEWALL SUPPORT. CORRODED. CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT STA 727B+17; 727C+10; 727E+8; 727E+12; 727E+16; 747+7 - 767; RBL 25<[01] REMOVED AND REPLACED AT ACB FLOOR TO SIDE WA - [SDR SWAA2025051356789](https://openairdocs.org/sdr/SWAA2025051356789), Apr 15, 2025: SIDEWALL SUPPORT. CORRODED. CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT FROM STA 460 TO 500D; LBL 24; WL 156.<[01] REMOVED AND REPLACED NEW ON FWD CARGO BAY FLOOR TO SIDEWALL SUPP - [SDR SWAA2025051356771](https://openairdocs.org/sdr/SWAA2025051356771), Apr 15, 2025: FLOOR PANEL. PULLED. AFT FLOOR PANEL 241ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] 241ZF FLOOR PANEL UPPER SKIN DAMAGE HAS BEEN REPAIRED PER [SRM 53-00-50-2R-1-A00939 (REPAIR 1 - [SDR SWAA2025051356769](https://openairdocs.org/sdr/SWAA2025051356769), Apr 15, 2025: FLOOR PANEL. DEBONDED. AFT FLOOR PANEL 241XF UPPER SKIN HAS A PREVIOUS REPAIR THAT IS DISBONDED. (MARKED)<[01] 241XF FLOOR PANEL UPPER SKIN DAMAGE HAS BEEN REPAIRED PER [SRM 53-00-50- - [SDR SWAA2025051456764](https://openairdocs.org/sdr/SWAA2025051456764), Apr 14, 2025: STUB FRAME. CRACKED. CRACK FOUND ON FSD STUB FRAME AT BS 291.5+8; .2' ABOVE SEAL DEPRESSOR; 1.6' IN LENGTH<[01] EVALUATED DAMAGE; NO ALLOWABLE DAMAGE FOUND AT SRM; UPPER STUB FRAME - [SDR SWAA2025051456759](https://openairdocs.org/sdr/SWAA2025051456759), Apr 14, 2025: FLOORBEAM. CORRODED. CORROSION ON BS986 FLOOR BEAM AT NUTPLATE HOLE RBL 43; WL 208.1<[01] THE FLOOR BEAM REPAIR WILL BE COMPLETED ON COSTUMER CARD # TTG8Q00ZWBA6;[02] CORRECTIVE ACT - [SDR SWAA2025051456760](https://openairdocs.org/sdr/SWAA2025051456760), Apr 14, 2025: FLOORBEAM. CORRODED. CORROSION ON BS986 FLOOR BEAM AT BOTTOM SIDE OF NUTPLATE HOLE RBL 35.5; WL 208.1<[01] THE FLOOR BEAM REPAIR WILL BE COMPLETED ON COSTUMER CARD # TTG8Q00ZWBA6;[0 - [SDR SWAA2025051456761](https://openairdocs.org/sdr/SWAA2025051456761), Apr 14, 2025: FLOORBEAM. CORRODED. CORROSION ON BS986 FLOOR BEAM AT BOTTOM SIDE OF NUTPLATE HOLE RBL 31.5; WL 208.1<[01] THE FLOOR BEAM REPAIR WILL BE COMPLETED ON COSTUMER CARD # TTG8Q00ZWBA6;[0 - [SDR SWAA2025051456762](https://openairdocs.org/sdr/SWAA2025051456762), Apr 14, 2025: FLOORBEAM. CORRODED. CORROSION ON BS986 FLOOR BEAM AT BOTTOM SIDE OF NUTPLATE HOLE RBL 27.5; WL 208.1<[01] THE FLOOR BEAM REPAIR WILL BE COMPLETED ON COSTUMER CARD # TTG8Q00ZWBA6;[0 - [SDR SWAA2025051456690](https://openairdocs.org/sdr/SWAA2025051456690), Apr 11, 2025: VAPOR BARRIER. CRACKED. R/H VAPOR BARRIER CRACKED AT BS 663<[01] REMOVED; REINSTALLED AND RAPAIRED VAPOR BARRIER IAW B737-7 SRM 51-40-02-0G-0 DWG 111A1000 ID: 0259 REV: A AND REINSTALL - [SDR SWAA2025051456694](https://openairdocs.org/sdr/SWAA2025051456694), Apr 11, 2025: VAPOR BARRIER. CRACKED. L/H VAPOR BARRIER CRACKED AT BS 663<[01] L/H VAPOR BARRIER BS663 REPAIRED IN TTG8Q00ZWLU7;[02] REMOVED AND REINSTALLED L/H VAPOR BARRIER AT BS 663 LBL6-LBL70 IA - [SDR SWAA2025051356692](https://openairdocs.org/sdr/SWAA2025051356692), Apr 11, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 242PF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 242PF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR P - [SDR SWAA2025051356691](https://openairdocs.org/sdr/SWAA2025051356691), Apr 11, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 241WF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241WF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR P - [SDR SWAA2025051356688](https://openairdocs.org/sdr/SWAA2025051356688), Apr 11, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 241VF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241VF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR P - [SDR SWAA2025051356687](https://openairdocs.org/sdr/SWAA2025051356687), Apr 11, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241UF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR P - [SDR SWAA2025051356682](https://openairdocs.org/sdr/SWAA2025051356682), Apr 11, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241DF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FL - [SDR SWAA2025051356681](https://openairdocs.org/sdr/SWAA2025051356681), Apr 11, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241BF WAS REPLACED. FABRICATED NEW PANEL IAW SRM 53-00-50-2R-0 & BOEING DWG 144A5810 - [SDR SWAA2025051356680](https://openairdocs.org/sdr/SWAA2025051356680), Apr 11, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 241AF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00 - [SDR SWAA2025051356679](https://openairdocs.org/sdr/SWAA2025051356679), Apr 11, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 232SF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 232SF; WITH UPPER SKIN AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED F - [SDR SWAA2025051356678](https://openairdocs.org/sdr/SWAA2025051356678), Apr 11, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 232RF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 232RF; WITH UPPER SKIN AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED F - [SDR SWAA2025051356677](https://openairdocs.org/sdr/SWAA2025051356677), Apr 11, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 231ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 231ZF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00 - [SDR SWAA2025051356684](https://openairdocs.org/sdr/SWAA2025051356684), Apr 11, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 231YF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 231YF FLOOR PANEL HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR All 269: https://openairdocs.org/aircraft/N293WN/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 CFM56-7B24 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.