# N298WN: 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 CFM56-7B24/3 series](https://openairdocs.org/engine/cfm-international-cfm56-7b24-3-series) (registry code 13074) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (The Boeing Company) (OpenAirDocs) - Serial number: 32543 - Year built: 2007 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 28, 2007 - Certificate issued: December 12, 2007 - Expires: March 31, 2029 - Mode S code: A31533 - 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=298WN - Page: https://openairdocs.org/aircraft/N298WN From the FAA registry file of October 24, 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 CFM56-7B24/3 model are included. ## ADs that may apply (OpenAirDocs): 10 in force ### Matched by airframe (Boeing 737-7H4) None in force. ### Matched by engine (CFM International CFM56-7B24/3 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 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 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 ### 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 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 ## 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 N298WN. ## FAA accident and incident reports None matched to N298WN. ## Service difficulty reports (268, 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 SWAA2026092845005](https://openairdocs.org/sdr/SWAA2026092845005), Sep 22, 2026: SWITCH. DAMAGED. EMERGENCY LIGHTS GUARD ON SWITCH DAMAGED (FLIGHT DECK). REMOVED AND REPLACED THE FLIGHT DECK EMERGENCY LIGHT SWITCH GUARD PER SIP. PERFORMED OPERATIONAL TEST OF - [SDR SWAA2026061110081](https://openairdocs.org/sdr/SWAA2026061110081), Jun 7, 2026: DOOR. OPEN. ON CLIMB OUT VIBRATION NOTED CLIMBING ABOVE FL260, ON POST FLIGHT WALKAROUND NOTICED GROUND POWER DOOR OPEN. PERFORMED AIRFRAME CONDITION INSPECTION IAW AMM 05- - [SDR SWAA2026040385368](https://openairdocs.org/sdr/SWAA2026040385368), Apr 1, 2026: HANDLE. BROKEN. FWD ENTRY DOOR ASSIST HANDLE BROKE OFF. INSTALLED L1 DOOR HANDLE IAW AMM 52-11-31. OK TO CONTINUE ON MEL 25-10-01; SP1B C/W. - [SDR SWAA2026031980273](https://openairdocs.org/sdr/SWAA2026031980273), Mar 16, 2026: SIGN. BROKEN. EMERGENCY EXIT ROW SIGN MID CABIN ATTACHED TO THE CEILING IS BROKEN. REMOVED AND REPLACED MID CABIN CEILING EMERGENCY LIGHT IAW AMM 33-51-01. OPS CHECK GOOD. - [SDR SWAA2026022573948](https://openairdocs.org/sdr/SWAA2026022573948), Feb 24, 2026: COUNTER. ODOR. ELECTRICAL ODOR COMING FROM FO YOKE TRIP COUNTER. REMOVED AND REPLACED FO'S TRIP COUNTER IAW MM 33-11-00. - [SDR SWAA2026012965750](https://openairdocs.org/sdr/SWAA2026012965750), Jan 29, 2026: LAMP. DAMAGED. FWD ENTRY EMERGENCY EXIT LENS HOUSING & LAMP ASSY FOUND DAMAGED. REMOVED & REPLACED IAW AMM 33-51-01-960-802-NG. OPS TESTED GOOD. - [SDR SWAA2026012764351](https://openairdocs.org/sdr/SWAA2026012764351), Jan 24, 2026: SIGN. DETACHED. FWD GALLEY EXIT SIGN FELL DOWN. COMPLIED WITH EA 26-133-00249, REV A. - [SDR SWAA2025101624569](https://openairdocs.org/sdr/SWAA2025101624569), Oct 15, 2025: COVER. BROKEN. EMERGENCY EXIT LIGHT COVER BROKEN FWD OF LH OVERWING EXIT DOOR. R & R EMERGENCY EXIT LIGHT COVER FWD OF LH OVERWING EXIT DOOR IAW AMM 33-51-01. - [SDR SWAA2025092918436](https://openairdocs.org/sdr/SWAA2025092918436), Sep 26, 2025: GIRT BAR. OUT OF POSITION. R1 FWD SERVICE DOOR GIRT BAR HANGS LOW. REPACKED CABIN R1 FWD SERVICE DOOR GIRT BAR IAW AMM 25-66-01. - [SDR SWAA2025092918437](https://openairdocs.org/sdr/SWAA2025092918437), Sep 26, 2025: GIRT BAR. OUT OF POSITION. CABIN - L1 FWD ENTRY DOOR GIRT BAR HANGS LOW. REPACKED L-1 DOOR SLIDE GIRT BAR IAW AMM 25-66-01-000-804-NG. - [SDR SWAA2025090209200](https://openairdocs.org/sdr/SWAA2025090209200), Aug 27, 2025: TAILPIPE. FIRE. RAMP TOWER REPORTED POSSIBLE TAIL PIPE FIRE LT ENGINE. NO ABNORMAL INDICATION IN COCKPIT, ON TAXI OUT WITH BOTH ENGINES RUNNING GROUND CONTROL REPORTS TAIL PIPE - [SDR SWAA2025062081444](https://openairdocs.org/sdr/SWAA2025062081444), Jun 13, 2025: FLASHLIGHT. INOPERATIVE. FWD L/H WINDSCREEN LOWER FLASHLIGHT INOP <[01]. REMOVED AND REPLACED FWD L/H WINDSCREEN LOWER FLASHLIGHT BATTERY IAW AMM 25-64-00-900-806. OPERATIONAL CHECK WAS - [SDR SWAA2025061781447](https://openairdocs.org/sdr/SWAA2025061781447), Jun 13, 2025: FUSE. OPEN. EMERGENCY EXIT LIGHTS L1365; L751 ASSOCIATED WITH BATTERY PACK M1668 ARE INOPERATIVE. REPLACED FUSE AT POWER SUPPLY M1668 AND PERFORMED GOOD TEST IAW AMM 33-51- - [SDR SWAA2025061781446](https://openairdocs.org/sdr/SWAA2025061781446), Jun 13, 2025: BATTERY PACK. INOPERATIVE. ALL EMERGENCY EXIT LIGHTS ASSOCIATED WITH M1670 BATTERY PACK ARE INOP. REMOVED AND REPLACED BATTERY PACK M1670 AND PERFORMED GOOD INSTALLATION TEST; PER AMM 33- - [SDR SWAA2025061781445](https://openairdocs.org/sdr/SWAA2025061781445), Jun 13, 2025: FUSE. OPEN. EMERGENCY LIGHT L1365; L751 & L1605 ASSOCIATED WITH M1669 BATTERY PACK ARE INOPERATIVE. REPLACED FUSE AT POWER SUPPLY M1669 AND PERFORMED GOOD TEST IAW AMM 33-5 - [SDR SWAA2025061781240](https://openairdocs.org/sdr/SWAA2025061781240), Jun 13, 2025: BATTERY PACK. INOPERATIVE. ALL ASSOCIATED LIGHTS INOP WITH M1674 EMERGENCY BATTERY PACK. REMOVED AND REPLACED M1674 EMERGENCY BATTERY PACK AND PERFORMED GOOD OPERATIONAL TEST IAW AMM 33-5 - [SDR SWAA2025062078296](https://openairdocs.org/sdr/SWAA2025062078296), Jun 4, 2025: RIB. CRACKED. CRACKED ON LOWER AREA OF STIFFENER 2 INSPAR RIB 6, STAB STA 120.30. REPAIRED AT LOWER AREA OF STIFFENER 2 INSPAR RIB 6 STAB STA 120.30 PER SRM 55-10-09-2R-4 REP - [SDR SWAA2025062078297](https://openairdocs.org/sdr/SWAA2025062078297), Jun 4, 2025: RIB. CRACKED. CRACKED ON LOWER AREA OF STIFFENER 4 INSPAR RIB 6, STAB STA 120.30. REPAIRED AT LOWER AREA OF STIFFENER 4 INSPAR RIB 6 STAB STA 120.30 PER SRM 55-10-09-2R-4 REP - [SDR SWAA2025061777526](https://openairdocs.org/sdr/SWAA2025061777526), Jun 2, 2025: PANEL. DEBONDED. PANEL 193AR INNER SURFACE HAS MULTIPLE DISBONDS. PANEL 193AR WAS REPLACED ON CUSTOMER FAULT TTG8Q010RK8D. - [SDR SWAA2025062075888](https://openairdocs.org/sdr/SWAA2025062075888), May 28, 2025: FITTING. CRACKED. WHILE REMOVING LT STAB INSPAR RIB AT STAB STA 111.10 FOUND CRACK IN #3 ELEVATOR HINGE RIB FITTING AT FWD FLANGE. <[01] 04 - REPAIRED PER [EA EA-COMPONENT (EA AT - [SDR SWAA2025061775508](https://openairdocs.org/sdr/SWAA2025061775508), May 27, 2025: STRINGER. CRACKED. CRACKED STRINGER AT FWD CABIN BS297 S-7L WL275. THE DAMAGE WAS REPAIRED PER 737-700 SRM 53-00-03-2R-1 REPAIR 1 AND EA 25-153-01407 WITH AN INSPECTION PROGRAM DE - [SDR SWAA2025061775509](https://openairdocs.org/sdr/SWAA2025061775509), May 27, 2025: FRAME. CRACKED. PASSENGER CABIN FED UPPER FRAME BS 312 STR 5L CRACKED. REMOVED DAMAGE ON PASSENGER CABIN FED UPPER FRAME BS 312 STR 5L I.A.W SRM 51-10-02-0G-0 AND M-22-153-0124 - [SDR SWAA2025062075339](https://openairdocs.org/sdr/SWAA2025062075339), May 26, 2025: INTERCOSTAL. CRACKED. FED INTERCOSTAL CRACKED AT BS295.5 STR16L; WL216. REMOVED AND REPLACED INTERCOSTAL BS 294-BS 303 S16L WL216 PER SRM 51-40-02 AND DWG 141A8180 REV: C. REJECT COR - [SDR SWAA2025062074866](https://openairdocs.org/sdr/SWAA2025062074866), May 24, 2025: SIDEWALL SUPPORT. CORRODED. MULTIPLE SPOTS OF CORROSION ON FCB RH SIDE FLOOR TO SIDEWALL SUPPORT NUTPLATES BS500A TO BS500D; RBL22;WL156. REMOVED AND REPLACED FCB SIDEWALL SUPPORT
BS 50 - [SDR SWAA2025062074867](https://openairdocs.org/sdr/SWAA2025062074867), May 24, 2025: SIDEWALL SUPPORT. CORRODED. MULTIPLE SPOTS OF CORROSION ON FCB LH SIDE FLOOR TO SIDEWALL SUPPORT NUTPLATES BS460 TO BS500D; RBL22;WL156. MULTIPLE SPOTS OF CORROSION ON FCB LH SIDE FLOOR TO - [SDR SWAA2025062074868](https://openairdocs.org/sdr/SWAA2025062074868), May 24, 2025: SUPPORT. CORRODED. CORROSION ON FCB FLOOR TO AFT BULKHEAD SUPPORT BS500D FROM RBL22 TO LBL22 WL156. REMOVED AND REPLACED FCB FLOOR TO AFT BULKHEAD SUPPORT BS500D RBL22 TO LBL22 WL - [SDR SWAA2025062074873](https://openairdocs.org/sdr/SWAA2025062074873), May 24, 2025: SIDEWALL SUPPORT. CORRODED. CORROSION ON ACB RH SIDE FLOOR TO SIDEWALL SUPPORT AT BS927+3 RBL16 WL156. REMOVED AND REPLACED ON ACB RH FLOOR TO SIDEWALL SUPPORT FROM BS 887 TO BS 947 RBL16 - [SDR SWAA2025062075333](https://openairdocs.org/sdr/SWAA2025062075333), May 24, 2025: SHIELD. CORRODED. CORROSION ON ACB FWD SHIELD NUTPLATES B767 TO BS787 RBL22 WL156. REMOVED AND REPLACED NEW ON ACB FWD SHIELD BS767 TO BS794 RBL22 IAW SRM 51-40-02 AND DWG 146A00 - [SDR SWAA2025061774864](https://openairdocs.org/sdr/SWAA2025061774864), May 24, 2025: WEB. CORRODED. MULTIPLE SPOT WITH CORROSION ON FCB DOOR CUTOUT SURROUND THRESHOLD BS440+15; 460+3;460+6;BS460+17; RBL29, WL156. REMOVED AND REPLACED SUBTHRESHOLD WEB AT BS440 - [SDR SWAA2025061774865](https://openairdocs.org/sdr/SWAA2025061774865), May 24, 2025: SHIELD. CORRODED. MULTIPLE SPOTS OF CORROSION ON FCB FWD SHIELD NUT PLATES BS420 TO BS440 RBL24 WL156. REMOVED AND INSTALLED NEW FCB FWD SHIELD BS420 TO BS440 RBL24 WL156 P/N 143 - [SDR SWAA2025061776458](https://openairdocs.org/sdr/SWAA2025061776458), May 24, 2025: SHIELD. CORRODED. MULTIPLE SPOTS OF CORROSION ON FCB AFT SHIELD NUTPLATES BS480+13 TO BS500A; RBL22;WL156. REMOVED AND REPLACED FCB AFT SHIELD P/N 143A8126-31 LOT: 1594230-1 BS49 - [SDR SWAA2025061775702](https://openairdocs.org/sdr/SWAA2025061775702), May 24, 2025: SUPPORT. CORRODED. MULTIPLE SPOTS OF CORROSION ON FCB FWD SHIELD NUTPLATES BS 400 TO BS 420, RBL24, WL156. REMOVED AND REPLACED FCB FLOOR TO SIDEWALL SUPPORT BS 400 TO BS 420, RBL - [SDR SWAA2025061774566](https://openairdocs.org/sdr/SWAA2025061774566), May 23, 2025: SEAT TRACK. CRACKED. F/O'S FWD I/B SEAT TRACK CRACKED. REMOVED AND REPLACED F/O'S FWD I/B SEAT TRACK PER AMM 25-11-11-400-801. - [SDR SWAA2025062073749](https://openairdocs.org/sdr/SWAA2025062073749), May 21, 2025: RIB. CRACKED. SUSPECT CRACK ON UPPER AREA OF STIFFENER 2 INSPAR RIB 5 (STAB STA 110). REPAIRED THE UPPER AREA OF STIFFENER 2 IN SPAR RIB 5 (STAB STA 110) APPLIED A FILLET SEA - [SDR SWAA2025062073750](https://openairdocs.org/sdr/SWAA2025062073750), May 21, 2025: RIB. CRACKED. CRACKED ON LOWER AREA OF STIFFENER 3 INSPAR RIB 6. STAB STA 120, LT HORIZONTAL STAB. REPAIRED AT LOWER AREA OF STIFFENER 3 INSPAR RIB 6 STAB STA 120.30 PER SRM - [SDR SWAA2025061773751](https://openairdocs.org/sdr/SWAA2025061773751), May 21, 2025: SUPPORT ANGLE. CRACKED. CRACKED ON UPPER FLOOR SUPPORT ANGLE AT BS927+4; BL0; WL 208. REMOVED AND REPLACED UPPER SUPPORT ANGLE BETWEEN BS 927 TO BS 947 BL 0 PER SRM 51-40-02-0G-0 AND D - [SDR SWAA2025061773518](https://openairdocs.org/sdr/SWAA2025061773518), May 21, 2025: INTERCOSTAL. CRACKED. CRACKED INTERCOSTAL AT FWD WET AREA BS390 RBL41 WL208. REMOVED AND REPLACED ANGLE AT FLOOR STRUCTURE RBL 41 WL 208 BETWEEN BS 380 TO BS 400 PER SRM 51-40-02 AND - [SDR SWAA2025061773519](https://openairdocs.org/sdr/SWAA2025061773519), May 21, 2025: INTERCOSTAL. CRACKED. CRACKED INTERCOSTAL AT FWD WET AREA BS394 LBL13 WL208. REMOVED AND REPLACED THE CRACKED INTERCOSTAL UPPER ANGLE FROM BS-380 TO BS-400; LBL13; WL208 IAW SRM 51-4 - [SDR SWAA2025061773517](https://openairdocs.org/sdr/SWAA2025061773517), May 21, 2025: ATTACH ANGLE. CRACKED. CRACKED ATTACH ANGLE AT FWD CABIN BS294 RBL54 WL208. REMOVED AND REPLACED ATTACH ANGLE BS 291.5 TO 294 WL 208 RBL 54 PER SRM 51-40-02 AND DWG 141A8310 REV D. - [SDR SWAA2025061773490](https://openairdocs.org/sdr/SWAA2025061773490), May 21, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 241UF UPPER SURFACE HAS AREAS OF PULLED STRANDS. FLOOR PANEL 241UF UPPER SURFACE; WITH AREAS OF PULLED STRANDS; WAS REPLACED WITH A NEWLY FABRICATED - [SDR SWAA2025061773509](https://openairdocs.org/sdr/SWAA2025061773509), May 21, 2025: FLOOR PANEL. PULLED. FWD FLOOR PANEL 221FF UPPER SURFACE DELAMINATED. FWD FLOOR PANEL 221FF UPPER SURFACE WITH DELAMINATIONS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-1 - [SDR SWAA2025061773500](https://openairdocs.org/sdr/SWAA2025061773500), May 21, 2025: FLOOR PANEL. DELAMINATED. AFT FLOOR PANEL 241YF UPPER SURFACE DELAMINATED. AFT FLOOR PANEL 241YF UPPER SURFACE DELAMINATED WAS REPAIRED IAW SRM 53-00-50-2R-1. - [SDR SWAA2025061773512](https://openairdocs.org/sdr/SWAA2025061773512), May 21, 2025: FLOOR PANEL. DELAMINATED. AFT FLOOR PANEL 241AAF UPPER SURFACE DELAMINATED. AFT FLOOR PANEL 241AAF; WITH UPPER SURFACE DELAMINATION; WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW - [SDR SWAA2025061773502](https://openairdocs.org/sdr/SWAA2025061773502), May 21, 2025: FLOOR PANEL. DELAMINATED. AFT FLOOR PANEL 241ABF UPPER SURFACE DELAMINATED. UPPER SURFACE DELAMINATION ON AFT FLOOR PANEL 241ABF WAS REPAIRED IAW SRM 53-00-50-2R-1. - [SDR SWAA2025061773508](https://openairdocs.org/sdr/SWAA2025061773508), May 21, 2025: FLOOR PANEL. DELAMINATED. AFT FLOOR PANEL 242VF UPPER SURFACE DELAMINATED. AFT FLOOR PANEL 242VF UPPER SURFACE DELAMINATED; WAS REPAIRED IAW SRM 53-00-50-2R-1. - [SDR SWAA2025061773496](https://openairdocs.org/sdr/SWAA2025061773496), May 21, 2025: FLOOR PANEL. DELAMINATED. FWD FLOOR PANEL 222AF UPPER SURFACE DELAMINATED. FWD FLOOR PANEL 222AF WITH UPPER SURFACE DELAMINATED WAS REPAIRED IAW SRM 53-00-50-2R-1. - [SDR SWAA2025061773511](https://openairdocs.org/sdr/SWAA2025061773511), May 21, 2025: FLOOR PANEL. DELAMINATED. AFT FLOOR PANEL 241XF UPPER SURFACE DELAMINATED. AFT FLOOR PANEL 241XF WITH UPPER SURFACE DELAMINATED WAS REPAIRED IAW SRM 53-00-50-2R-1. - [SDR SWAA2025061773501](https://openairdocs.org/sdr/SWAA2025061773501), May 21, 2025: FLOOR PANEL. DELAMINATED. AFT FLOOR PANEL 241ZF UPPER SURFACE DELAMINATED. AFT FLOOR PANEL 241ZF WITH UPPER SURFACE DELAMINATED WAS REPAIRED IAW SRM 53-00-50-2R-1. - [SDR SWAA2025061773503](https://openairdocs.org/sdr/SWAA2025061773503), May 21, 2025: FLOOR PANEL. DELAMINATED. AFT FLOOR PANEL 241ACF UPPER SURFACE DELAMINATED. REPAIRED PER SRM 53-00-50-2R-1-A00939 REPAIR 1 - REPAIR OF DAMAGE TO ONE FACESHEET IN COMPOSITE FLOOR PANELS - - [SDR SWAA2025061773506](https://openairdocs.org/sdr/SWAA2025061773506), May 21, 2025: FLOOR PANEL. DELAMINATED. AFT FLOOR PANEL 242SF UPPER SURFACE DELAMINATED. REPAIRED PER SRM 53-00-50-2R-1-A00939 REPAIR 1. All 268: https://openairdocs.org/aircraft/N298WN/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 CFM56-7B24/3 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 CFM56-7B24/3 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b24-3-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.