# N967WN: 2011 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 CFM56-7B24E series](https://openairdocs.org/engine/cfm-international-cfm56-7b24e-series) (registry code 13804) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (The Boeing Company) (OpenAirDocs) - Serial number: 36967 - Year built: 2011 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 1, 2011 - Certificate issued: October 24, 2011 - Expires: October 31, 2027 - Mode S code: AD7828 - 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=967WN - Page: https://openairdocs.org/aircraft/N967WN 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 CFM56-7B24E model are included. ## ADs that may apply (OpenAirDocs): 6 in force ### Matched by airframe (Boeing 737-7H4) None in force. ### Matched by engine (CFM International CFM56-7B24E 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 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 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 ### 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 ## NTSB investigations None matched to N967WN. ## FAA accident and incident reports None matched to N967WN. ## Service difficulty reports (184, 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 SWAA2026083151036](https://openairdocs.org/sdr/SWAA2026083151036), Aug 26, 2026: ENGINE. FIRE. UPON POST FLIGHT WALK AROUND, 5 MINUTES AFTER SHUTDOWN, FLAMES WERE OBSERVED INSIDE ENG#2 EXHAUST NOZZLE. EVENTUALLY, FLAMES WENT OUT BY THEMSELVES._ 02 - INSPE - [SDR SWAA2026030976137](https://openairdocs.org/sdr/SWAA2026030976137), Mar 3, 2026: ACCESS PANEL. DAMAGED. ACCESS PANEL 194BL HAS ELONGATED FASTENER HOLE. PREPPED AND PAINTED ACCESS PANEL 194BL REF M/M 51-21-99. PANEL READY FOR INSTALLATION. REF TTG8Q01ARDBG FOR PANE - [SDR SWAA2025102024311](https://openairdocs.org/sdr/SWAA2025102024311), Oct 14, 2025: COVER. DETACHED. EXIT LIGHT COVER CAME OFF. REPLACED FO SIDE EXIT WINDOW EXIT SIGN LIGHT COVER PER AMM 33-51-01. - [SDR SWAA2025101423667](https://openairdocs.org/sdr/SWAA2025101423667), Oct 11, 2025: SLIDE. PARTIAL DEPLOY. FWD ENTRY DOOR SLIDE PARTIALLY DEPLOYED. REINSTALLED FWD ENTRY DOOR SLIDE IAW MT 725-61-06. AC OK FOR SERVICE. - [SDR SWAA2025100319840](https://openairdocs.org/sdr/SWAA2025100319840), Oct 1, 2025: LIGHT. INOPERATIVE. AFT LAV EMERGENCY EXIT LIGHT HAS INOP SEGMENTS. RELAMPED INOP SEGMENTS ON AFT LAV EMERGENCY EXIT LIGHT AND PERFORMED GOOD INSTALLATION TEST IAW AMM 33-51-01-960 - [SDR SWAA2025100319839](https://openairdocs.org/sdr/SWAA2025100319839), Oct 1, 2025: LAMP. INOPERATIVE. L/H OVER WING EXIT EMERGENCY LIGHTS HAVE INOP SEGMENTS. REPLACED THE LAMPS IN THE SEGMENTS ON L/H OWE EMERGENCY EXIT LIGHT AND PERFORMED GOOD INSTALLATION TEST - [SDR SWAA2025100319843](https://openairdocs.org/sdr/SWAA2025100319843), Oct 1, 2025: LIGHT. INOPERATIVE. R/H OVER WING EXIT EMERGENCY LIGHT HAS INOP SEGMENTS. RELAMPED INOP SEGMENTS ON R/H OWE EMERGENCY EXIT LIGHTS AND PERFORMED GOOD INSTALLATION TEST IAW AMM 33-51 - [SDR SWAA2025100318855](https://openairdocs.org/sdr/SWAA2025100318855), Sep 27, 2025: BATTERY PACK. NO TEST. EMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1675 FAIL TEST. REMOVED AND REPLACED POWER SUPPLY - BATTERY PACK M1675 AND PERFORMED GOOD OPERATIONAL TEST PER AM - [SDR SWAA2025100216902](https://openairdocs.org/sdr/SWAA2025100216902), Sep 21, 2025: LATCH. DAMAGED. FSD SLIDE COVER ASSY CLOSE-OUT LATCH (BLOCK ASSY) DAMAGED WILL NOT RE-ENGAGE. REMOVED AND REPLACED WITH NEW FSD SLIDE COVER ASSY CLOSE-OUT LATCH (BLOCK ASSY) IA - [SDR SWAA2025100615793](https://openairdocs.org/sdr/SWAA2025100615793), Sep 17, 2025: STRINGER CLIP. NO DISCREPANCY. FUSELAGE STATION PSX STRINGER CLIP STA 727D; S-7R HAS CRACKED. UPON FURTHER INVESTIGATION FOUND FUSELAGE STATION PSX STRINGER CLIP NOT CRACKED, NDI VERIFIED. - [SDR SWAA2025100215791](https://openairdocs.org/sdr/SWAA2025100215791), Sep 17, 2025: STRINGER CLIP. CRACKED. FUSELAGE STATION PSX STRINGER CLIP STA 727D; S-6L HAS CRACKED. REMOVED AND REPLACED STRINGER CLIP STA 727D; S-6L PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 AND DW - [SDR SWAA2025100215790](https://openairdocs.org/sdr/SWAA2025100215790), Sep 17, 2025: STRINGER CLIP. CRACKED. FUSELAGE STATION PSX STRINGER CLIP STA 706; S-4L HAS CRACKED. FABRICATED; REMOVED AND REPLACED STRINGER CLIP STA 706; S-4L PER SRM 51-40-02-0G-0; SRM 51-40-05-0 - [SDR SWAA2025100215792](https://openairdocs.org/sdr/SWAA2025100215792), Sep 17, 2025: STRINGER CLIP. CRACKED. FUSELAGE STATION PSX STRINGER CLIP STA 747; S-5L HAS CRACKED.<[01] REMOVED AND REPLACED STRINGER CLIP STA 747; S-5L PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 AND - [SDR SWAA2025100215786](https://openairdocs.org/sdr/SWAA2025100215786), Sep 17, 2025: STRINGER CLIP. CRACKED. STRINGER CLIP STA 727E, S-6L HAS CRACKED. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-05-0G-0, SRM 51-40-02-0G-0, AND DWG 146A1112, REV -. - [SDR SWAA2025100215785](https://openairdocs.org/sdr/SWAA2025100215785), Sep 17, 2025: STRINGER CLIP. CRACKED. STRINGER CLIP STA 727C; S-6L HAS CRACKED. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-05-0G-0, SRM 51-40-02-0G-0, AND DWG 146A1103, REV -. - [SDR SWAA2025100215787](https://openairdocs.org/sdr/SWAA2025100215787), Sep 17, 2025: STRINGER CLIP. CRACKED. FUSELAGE STATION PSX STRINGER CLIP STA 767; S-5L CRACKED. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0, AND DWG 146A1132, REV - [SDR SWAA2025100215788](https://openairdocs.org/sdr/SWAA2025100215788), Sep 17, 2025: STRINGER CLIP. CRACKED. FUSELAGE STATION PSX STRINGER CLIP STA 727E, S-6R CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-0G-0, SRM 51-40-05-0G-0, AND DWG 146A1112, REV -. - [SDR SWAA2025100614961](https://openairdocs.org/sdr/SWAA2025100614961), Sep 15, 2025: SEAT TRACK. CORRODED. CORROSION ON TOP AND IN WELL OF PAX CABIN SEAT TRACK AT BS 687 LBL 45 WL 208. REMOVED PASSENGER CABIN SEAT TRACK AT BS 540-727B LBL 45 WL 208. INSTALLED NEW SER - [SDR SWAA2025100214965](https://openairdocs.org/sdr/SWAA2025100214965), Sep 15, 2025: FLOORBOARD. DELAMINATED. PASSENGER CABIN FLOORBOARD 241RF TOP SURFACE DELAMINATED.. REMOVED PASSENGER CABIN FLOORBOARD 241RF IAW AMM 53-21-00-000-801;IDENTIFIED FLOOR PANEL 241RF MATERI - [SDR SWAA2025100314368](https://openairdocs.org/sdr/SWAA2025100314368), Sep 13, 2025: BULKHEAD WEB. CRACKED. RH VAPOR BARRIER BULKHEAD WEB HAS CRACKED AT BS 663 RBL 26 WL 161 - 176. FAULT WILL BE RESOLVED ON ANOTHER FAULT; REFER TO TTG8Q0155JAJ. - [SDR SWAA2025100314370](https://openairdocs.org/sdr/SWAA2025100314370), Sep 13, 2025: ATTACH ANGLE. CRACKED. RH VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT BS 663 RBL 33 WL 176. INVESTIGATED FOR POSSIBLE CRACK AS PER SRM 51-10-02; UPON FURTHER INVESTIGATION AND ACCO - [SDR SWAA2025100314373](https://openairdocs.org/sdr/SWAA2025100314373), Sep 13, 2025: VAPOR BARRIER. CRACKED. R/H BS663 VAPOR BARRIER IS CRACKED RBL35 WL156. RIGHT BS663 VAPOR BARRIER WITH A CRACK AT RBL35 AND WL156 WAS REPAIRED IAW SRM 51-70-04-2R-10. - [SDR SWAA2025090811838](https://openairdocs.org/sdr/SWAA2025090811838), Sep 6, 2025: HANDLE. LOOSE. L1 DOOR; UPPER ASSIST HANDLE LOOSE. SECURED L1 DOOR UPPER ASSIST HANDLE. REF AMM 52-11-41. - [SDR SWAA2025081198812](https://openairdocs.org/sdr/SWAA2025081198812), Aug 6, 2025: MEGAPHONE. DAMAGED. AFT. MEGAPHONE HANDLE IS DAMAGED.<[01] R/R THE AFT. MEGAPHONE; OP?S CHECKS IAW AMM 25-64-00. - [SDR SWAA2025060275765](https://openairdocs.org/sdr/SWAA2025060275765), May 28, 2025: VAPOR BARRIER. CRACKED. RIGHT WHEEL WELL FIBERGLASS VAPOR BARRIER HAS APPROXIMATELY 17' CRACK BETWEEN RBL 28 AND RBL 36 <[01]. C/W EA ON ATTACHED FAULT; [02] C/W EA 25-157-01402 ON ATT - [SDR SWAA2025021997631](https://openairdocs.org/sdr/SWAA2025021997631), Feb 19, 2025: BATTERY PACK. INOPERATIVE. FWD CABIN LT SIDE EMERGENCY LIGHTS INOP<[01] 01 - REMOVED AND REPLACED L/H FWD PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT - [SDR SWAA2024102953971](https://openairdocs.org/sdr/SWAA2024102953971), Oct 27, 2024: BRACKET. BROKEN. FWD SERVICE DOOR REAR GIRT BAR BRACKET BKN<[01] FOUND ONE RIVET ON AFT GIRT BAR BRAKET MISSING. INSTALLED NEW RIVET REF SRM 51-40-02. - [SDR SWAA2024031261693](https://openairdocs.org/sdr/SWAA2024031261693), Mar 10, 2024: VALVE. FLUCTUATES. NUMBER 2 ENGINE FLUCTUATING INFLIGHT 50-65 % N1 WHILE IN SHALLOW DESCENT ;PULLED THRUST TO IDLE AND RECEIVED ENG FAIL INDICATION ON NUMBER 2 ENGINE ; THRUST LEV - [SDR SWAA2023100204692](https://openairdocs.org/sdr/SWAA2023100204692), Sep 27, 2023: BATTERY PACK. INOPERATIVE. L/H EMERGENCY OVERWING EXIT SIGN AND DOOR LINING LIGHTS INOP<[01] BY REPLACING THE BATTERY PACK AT LOCATION M1668 ON CUSTOMER CARD TTG8Q00NNRKS ALSO FIX L/H EME - [SDR SWAA2023100204691](https://openairdocs.org/sdr/SWAA2023100204691), Sep 27, 2023: BATTERY PACK. INOPERATIVE. L/H OVERHEAD BIN ROW 6ABC EMERGENCY LIGHT INOP<[01] REMOVED AND REPLACED BATTERY PACK AT POSITION M1668 P/N AD-D717-01-100WA S/N WN2756 PERFORMED OPERATIONAL TE - [SDR SWAA2023092899974](https://openairdocs.org/sdr/SWAA2023092899974), Sep 13, 2023: FLOOR PANEL. DETERIORATED. MAIN CABIN FWD WET AREA CENTER FLOOR PANEL 221CF HAS 2 PREVIOUS REPAIR<[01] PANEL ASSY FABRICATED; AS PER DRAWING 141A5810 -9 DATE SEP 14; 2023; AND SRM 50-00-5 - [SDR SWAA2023092899973](https://openairdocs.org/sdr/SWAA2023092899973), Sep 13, 2023: FLOOR PANEL. PEELING. MAIN CABIN FWD WET AREA CENTER FLOOR PANEL 221EF TOP SKIN PEELING OFF<[01] REPLACED MAIN CABIN FWD CENTER FLOOR PANEL # 221EF REF. B737-700 AMM 53-21-00-400-801 - [SDR SWAA2023092897826](https://openairdocs.org/sdr/SWAA2023092897826), Sep 7, 2023: FLOOR PANEL. CRACKED. MAIN CABIN AFT WET AREA RT SIDE FLOOR PANEL 242XF CRACKED CENTER AREA<[01] REPLACED MAIN CABIN AFT WET AREA FLOOR PANEL 242XF REF. B737-700 AMM 53-21-00-400-801 - [SDR SWAA2023092897391](https://openairdocs.org/sdr/SWAA2023092897391), Sep 6, 2023: STIFFENER. CRACKED. RT VAPOR BARRIER ANGLE STIFFENER CRACKED I/B OF RT ECS EXHAUST. CORRECTING DESCRIPTION: RT VAPOR BARRIER ANGLE STIFFENER CRACKED O/B OF RT ECS EXHAUST. [TTG8Q00 - [SDR SWAA2023092896641](https://openairdocs.org/sdr/SWAA2023092896641), Sep 3, 2023: RIB. CRACKED. LEFT HORIZONTAL STABILIZER FRONT SPAR FAIRING 331B CRACKED @ INTERNAL RIB # 4<[01] REMOVED AND INSTALLED NEW LEFT HORIZONTAL STABILIZER FRONT SPAR FAIRING INTER - [SDR SWAA2023092896383](https://openairdocs.org/sdr/SWAA2023092896383), Sep 2, 2023: INTERCOSTAL. CRACKED. AFT CARGO COMPARTMENT INTERCOSTAL WEB AT STA 947.5 RBL 21 CRACK.<[01] REMOVED AND REPLACED AFT CARGO COMPARTMENT INTERCOSTAL WEB AT STA 947.5 RBL 21 REF B737 SR - [SDR SWAA2023092896265](https://openairdocs.org/sdr/SWAA2023092896265), Sep 1, 2023: FLOOR PANEL. DETERIORATED. MAIN CABIN FWD WET AREA FLOOR PANEL 222BF HAS 2EACH PREVIOUS REPAIR<[01] REPLACED MAIN CABIN FWD WET AREA RT SIDE FLOOR PANEL 222BF REF. B737-700 AMM 53-21-00-4 - [SDR SWAA2023092894695](https://openairdocs.org/sdr/SWAA2023092894695), Aug 28, 2023: CAP. DAMAGED. LEFT HORIZONTAL STAB. TIP FWD CAP WITH ELONGATED HOLES (MKD)<[01] REPLACED LEFT HORIZONTAL STAB. TIP. AND WILL BE INSTALLED ON ITEM TTG8Q002QRY2;[02] VERIFIED S - [SDR SWAA2023092894272](https://openairdocs.org/sdr/SWAA2023092894272), Aug 27, 2023: FLOOR PANEL. PEELING. MAIN CABIN FWD WET AREA L/H SIDE FLOOR PANEL 221DF TOP SKIN SOME AREAS PEELING OFF MATERIAL<[01] FABRICATED MAIN CABIN FLOOR FWD WET AREA FLOOR PANEL 221DF BY O - [SDR SWAA2023092894273](https://openairdocs.org/sdr/SWAA2023092894273), Aug 27, 2023: FLOOR PANEL. PEELING. MAIN CABIN FWD WET AREA L/H SIDE FLOOR PANEL 221BF TOP SKIN SOME AREAS PEELING OFF MATERIAL<[01] FABRICATED MAIN CABIN FWD WET AREA FLOOR PANEL 221BF BY OUTSIDE - [SDR SWAA2023092893979](https://openairdocs.org/sdr/SWAA2023092893979), Aug 27, 2023: FLOOR SUPPORT. CORRODED. CORROSION FOUND AFT CARGO FLOOR SUPPORT AT STA 947.5 FROM LBL 6 TO RBL 20 WL 155.5 HAS MULTIPLE SPOTS OF CORROSION.<[01] REMOVED AND REPLACED AFT CARGO FLOOR SU - [SDR SWAA2023092694278](https://openairdocs.org/sdr/SWAA2023092694278), Aug 27, 2023: FLOOR SUPPORT. CRACKED. FWD CABIN CENTER FLOOR SUPPORT INTERCOSTAL UPPER CAP CRACKED AT BL-0 BETWEEN STA 380 AND 400 WL 208.1 MKD DOT<[01] C/W INSTRUCTIONS - [SDR SWAA2023092694277](https://openairdocs.org/sdr/SWAA2023092694277), Aug 27, 2023: FLOOR SUPPORT. CORRODED. CORROSION AND HEAVY SCRATCHES AT AFT OF AFT CARGO COMPARTMENT BULKHEAD LOWER FLOOR SUPPORT ANGLE FROM S-26L TO S-26R STA 947.75<[01] REF TASK CARD TTG8Q00N2QKZ - [SDR SWAA2023092893962](https://openairdocs.org/sdr/SWAA2023092893962), Aug 26, 2023: ATTACH ANGLE. CRACKED. R/H VAPOR BARRIER UPPER ATTACH ANGLE STA 663.75 RBL 7.5 HOLE WITH CRACK INDICATION.<[01] REPAIRED R/H VAPOR BARRIER UPPER ATTACH ANGLE STA 663.75 RBL 7.5 PER B7 - [SDR SWAA2023092893772](https://openairdocs.org/sdr/SWAA2023092893772), Aug 25, 2023: FLOOR SUPPORT. CRACKED. MAIN CABIN CENTER WING BOX FLOOR SUPPORT BREAK CRACKED AT FASTER'S TAIL @ LBL- 1 STA 540 MKD DOT<[01] REMOVED AND REPLACED MAIN CABIN CENTER WING BOX FLOOR SUPP - [SDR SWAA2023092893761](https://openairdocs.org/sdr/SWAA2023092893761), Aug 25, 2023: FLOOR PANEL. PEELING. MAIN CABIN AFT WET AREA FLOOR PANEL 242TF TOP SKIN PEELING OFF SEVERAL AREAS<[01] FABRICATED MAIN CABIN AFT WET AREA FLOOR PANEL 242TF BY OUTSIDE VENDOR (AERO M - [SDR SWAA2023092893541](https://openairdocs.org/sdr/SWAA2023092893541), Aug 25, 2023: FLOOR SUPPORT. CORRODED. CORROSION *** FWD CABIN WET AREA FLOOR SUPPORT INTERCOSTAL UPPER CAP CORRODED THRU @ LBL 11 BETWEEN STA 294.5 AND STA 312 MKD DOT<[01] REMOVED AND REPLACED INTE - [SDR SWAA2023092693768](https://openairdocs.org/sdr/SWAA2023092693768), Aug 25, 2023: SUPPORT. CRACKED. FWD CABIN L/H SIDE WALL FUSELAGE SUPPORT FRAME FLANGE CUTOUT HAS SMALL CRACK AT STA 312 ABOVE L-1 DOOR UPPER SILL CUTOUT S-6L MKD DOT<[01] ACCOMPLISHED EA M-22- - [SDR SWAA2023092693545](https://openairdocs.org/sdr/SWAA2023092693545), Aug 25, 2023: INTERCOSTAL. CRACKED. FWD CABIN WET AREA INTERCOSTAL UPPER CAP CRACKED BETWEEN STA 294.5 & STA 303.9 BL-0 MKD DOT<[01] REMOVED AND REPLACED INTERCOSTAL AT FWD CABIN WET AREA BETWEEN - [SDR SWAA2023092693766](https://openairdocs.org/sdr/SWAA2023092693766), Aug 25, 2023: INTERCOSTAL. CRACKED. FWD CABIN WET AREA INTERCOSTAL UPPER CAP CRACKED AFT END @ STA 312 & RBL 31 MKD DOT<[01] REMOVED AND REPLACED FWD CABIN WET AREA INTERCOSTAL LOCATED AT STA 312 All 184: https://openairdocs.org/aircraft/N967WN/reports.md ## STCs that may be installed (OpenAirDocs) (31) 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 CFM56-7B24E series) - [STC SE04840NY](https://openairdocs.org/stc/SE04840NY): Installation of HarcoSemco Exhaust Gas Temperature (EGT) Electrical Harnesses in CFM56-7 engine. Kilroy Aviation LLC ## Related - Other Boeing 737-7H4 aircraft: https://openairdocs.org/model/boeing-737-7h4/aircraft.md - The CFM International CFM56-7B24E series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b24e-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.