# N214WN: 2005 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 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (The Boeing Company) (OpenAirDocs) - Serial number: 32486 - Year built: 2005 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 6, 2005 - Certificate issued: June 22, 2005 - Expires: August 31, 2027 - Mode S code: A1CA5F - 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=214WN - Page: https://openairdocs.org/aircraft/N214WN 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 model are included. ## ADs that may apply (OpenAirDocs): 55 in force ### Matched by airframe (Boeing 737-7H4) None in force. ### Matched by engine (CFM International CFM56 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 2017-14-08](https://openairdocs.org/ad/2017-14-08): Turbine Engine Compressor Section · CFM International CFM56-3, CFM56-3B and CFM56-3C. Effective Aug 18, 2017 - [AD 2017-05-09](https://openairdocs.org/ad/2017-05-09): Accessory Gearboxes · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 33 more. Effective Apr 13, 2017 - [AD 2016-14-10](https://openairdocs.org/ad/2016-14-10): High-pressure turbine (HPT) disks · CFM International CFM56-3, CFM56-3B and CFM56-3C with STC SE00034EN. Effective Aug 9, 2016 - [AD 2016-02-04](https://openairdocs.org/ad/2016-02-04): Turbine rear frames (TRFs) · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 33 more. Effective Mar 1, 2016 - [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 2013-14-06](https://openairdocs.org/ad/2013-14-06): Hydro-mechanical unit (HMU) fuel control · CFM International CFM56-5, CFM56-5B1, CFM56-5B1/2P and 34 more. Effective Sep 3, 2013 - [AD 2012-02-03](https://openairdocs.org/ad/2012-02-03): Engine · CFM International CFM56-5B1/3, CFM56-5B2/3, CFM56-5B3/3 and 8 more. Effective Mar 15, 2012 - [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 2010-12-03](https://openairdocs.org/ad/2010-12-03): Fan blades · CFM International CFM56-3 and CFM56-3B. Effective Jul 13, 2010 - [AD 2010-09-14](https://openairdocs.org/ad/2010-09-14): Exhaust gas temperature (EGT) · CFM International CFM56-5B1/2P, CFM56-5B1/P, CFM56-5B2/2P and 16 more. Effective Jun 8, 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 2009-18-01](https://openairdocs.org/ad/2009-18-01): LP turbine rear frames · CFM International CFM56-5B1/3, CFM56-5B1/P, CFM56-5B2/3 and 19 more. Effective Oct 1, 2009 - [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 2007-24-04](https://openairdocs.org/ad/2007-24-04): Low pressure turbine (LPT) · CFM International CFM56-5C4/1. Effective Dec 6, 2007 - [AD 2007-03-15](https://openairdocs.org/ad/2007-03-15): Exhaust gas temperature (EGT) harness · CFM International CFM56-5, CFM56-5B1, CFM56-5B1/2P and 34 more. Effective Mar 19, 2007 - [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 2005-10-05](https://openairdocs.org/ad/2005-10-05): Air turbine starters · CFM International CFM56-5, CFM56-5B1, CFM56-5B1/2P and 50 more. Effective Jun 14, 2005 - [AD 97-09-02 R3](https://openairdocs.org/ad/97-09-02-R3): High pressure turbine rotor (HPTR) front shafts · CFM International CFM56-5C2, CFM56-5C3/G and CFM56-5C4. Effective Oct 14, 2004 - [AD 2004-10-13](https://openairdocs.org/ad/2004-10-13): Service main fuel pumps · CFM International CFM56-3, CFM56-5, CFM56-5-A1/F and 4 more. Effective Jun 24, 2004 - [AD 2002-22-12](https://openairdocs.org/ad/2002-22-12): Titeflex hoses · BAE Systems ATP, Avro 146-RJ100A, Avro 146-RJ70A and 122 more. Effective Dec 13, 2002 - [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 2002-02-13](https://openairdocs.org/ad/2002-02-13): Magnetic Drain Plug · CFM International CFM56-5, CFM56-5-A1/F, CFM56-5A4 and 33 more. Effective Mar 21, 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 2001-09-17](https://openairdocs.org/ad/2001-09-17): Fuel Manifold and CJ9L Harness · CFM International CFM56-5C2, CFM56-5C2/4, CFM56-5C2/F and 13 more. Effective May 14, 2001 - [AD 2001-04-06](https://openairdocs.org/ad/2001-04-06): Fan Disk · CFM International CFM56-3, CFM56-3B and CFM56-3C. Effective Apr 4, 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 2000-15-01](https://openairdocs.org/ad/2000-15-01): Fuel Leakage · CFM International CFM56-2, CFM56-2A, CFM56-2B and 39 more. Effective Oct 2, 2000 - [AD 2000-05-22](https://openairdocs.org/ad/2000-05-22): CFM International CFM56-2, CFM56-2A, CFM56-2B and 3 more. Effective May 2, 2000 - [AD 99-06-16](https://openairdocs.org/ad/99-06-16): High Pressure Turbine Rotor (HPTR) Front Air Seal · CFM International CFM56-5, CFM56-5-A1/F, CFM56-5A4 and 3 more. Effective Apr 21, 1999 - [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 - [AD 98-19-10](https://openairdocs.org/ad/98-19-10): Accessory Gearbox · CFM International CFM56-3, CFM56-3B and CFM56-3C. Effective Sep 28, 1998 - [AD 98-12-32](https://openairdocs.org/ad/98-12-32): High Pressure Turbine Rotor Disks · CFM International CFM56-2, CFM56-2A, CFM56-2B and 3 more. Effective Jul 20, 1998 - [AD 98-10-11](https://openairdocs.org/ad/98-10-11): Accessory Gearbox · CFM International CFM56-3, CFM56-3B, CFM56-3C and 31 more. Effective Jun 3, 1998 - [AD 98-07-02](https://openairdocs.org/ad/98-07-02): Air/oil Seal · CFM International CFM56-3, CFM56-3B and CFM56-3C. Effective Mar 30, 1998 - [AD 98-02-04](https://openairdocs.org/ad/98-02-04): Low Pressure Turbine Case · CFM International CFM56-5B1/2P, CFM56-5B2/2P, CFM56-5B3/2P and 1 more. Effective Mar 23, 1998 - [AD 89-23-06 R1](https://openairdocs.org/ad/89-23-06-R1): Magnetic Chip Detector · CFM International CFM56-2, CFM56-2A, CFM56-3 and 8 more. Effective Jan 28, 1998 - [AD 97-08-01](https://openairdocs.org/ad/97-08-01): Fan Disks · CFM International CFM56-3, CFM56-3B and CFM56-3C. Effective Jun 23, 1997 - [AD 97-06-01](https://openairdocs.org/ad/97-06-01): High Pressure Compressor Rotor (HPCR) Stage 1-2 Spool · CFM International CFM56-5, CFM56-5B1, CFM56-5B1/2P and 28 more. Effective Jun 3, 1997 - [AD 97-05-13](https://openairdocs.org/ad/97-05-13): Air Turbine Engine Starter · CFM International CFM56-5, CFM56-5-A1/F, CFM56-5A4 and 3 more. Effective Jun 3, 1997 - [AD 96-25-11](https://openairdocs.org/ad/96-25-11): Redesigned Fan Blades · CFM International CFM56-3B and CFM56-3C. Effective Jan 29, 1997 ### 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 2013-02-02](https://openairdocs.org/ad/2013-02-02) (historical): High-pressure turbine (HPT) disks · CFM International CFM56-3, CFM56-3B and CFM56-3C with STC SE00034EN. Effective Jan 28, 2013 - [AD 2009-01-01](https://openairdocs.org/ad/2009-01-01) (historical): Exhaust gas temperature (EGT) · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 22 more. Effective Dec 31, 2008 - [AD 97-09-02 R2](https://openairdocs.org/ad/97-09-02-R2) (historical): Low pressure turbine rotor (LPTR) · CFM International CFM56-5C2, CFM56-5C2/4, CFM56-5C2/F and 9 more. Effective Apr 29, 2003 - [AD 2003-02-04](https://openairdocs.org/ad/2003-02-04) (historical): Exhaust gas temperature (EGT) · CFM International CFM56-5 Series (all). Effective Feb 27, 2003 - [AD 97-09-02 R1](https://openairdocs.org/ad/97-09-02-R1) (historical): High Pressure Turbine rotor (HPTR) front shaft · CFM International CFM56-5C2/G, CFM56-5C2/G4, CFM56-5C3/G and 3 more. Effective Sep 24, 2002 - [AD 2001-17-14](https://openairdocs.org/ad/2001-17-14) (historical): LPT Conical Supports · CFM International CFM56-5C4/1. Effective Sep 7, 2001 - [AD 2001-08-51](https://openairdocs.org/ad/2001-08-51) (historical): Fuel leakage · CFM International CFM56-5 Series (all) - [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 - [AD 99-08-16](https://openairdocs.org/ad/99-08-16) (historical): CFM International CFM56-2, CFM56-2A, CFM56-2B and 3 more. Effective May 13, 1999 - [AD 97-09-02](https://openairdocs.org/ad/97-09-02) (historical): High/Low Pressure Turbine Rotor · CFM International CFM56-5C2/G, CFM56-5C2/G4, CFM56-5C3/G and 3 more. Effective Jun 30, 1997 All 71: https://openairdocs.org/aircraft/N214WN/ads.md ## Information bulletins (advisory) (4 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-13-33R2](https://openairdocs.org/saib/NE-13-33R2): Turbine Engine Air Inlet Section - LP Turbine, Stage 1 Nozzle Vanes. Issued Jan 28, 2014 - [SAIB NE-12-29](https://openairdocs.org/saib/NE-12-29): Engine Fuel Distribution CFM56-5B LPTACC Fuel Manifold. Issued Apr 27, 2012 - [SAIB NE-06-02](https://openairdocs.org/saib/NE-06-02): . Issued Oct 18, 2005 - [SAIB NE-13-33R1](https://openairdocs.org/saib/NE-13-33R1) (historical): Turbine Engine Air Inlet Section - LP Turbine, Stage 1 Nozzle Vanes. Issued Jun 24, 2013 - [SAIB NE-13-33](https://openairdocs.org/saib/NE-13-33) (historical): Turbine Engine Air Inlet Section - LP Turbine, Stage 1 Nozzle Vanes. Issued May 13, 2013 - [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 N214WN. ## FAA accident and incident reports None matched to N214WN. ## Service difficulty reports (305, 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 SWAA2026082509906](https://openairdocs.org/sdr/SWAA2026082509906), Aug 21, 2026: LAMP. INOPERATIVE. EXTERIOR EMERGENCY LIGHT ON WING EXIT DOOR RIGHT SIDE WILL NOT ILLUMINATE. R & R THE LAMP ON EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-04. - [SDR SWAA2026081478569](https://openairdocs.org/sdr/SWAA2026081478569), Aug 10, 2026: SCUFF PLATE. PEELING. FWD CARGO DOOR CENTER SCUFF PLATE. MEL_WORKING WITH ENGINEERING, R & R FWD CARGO CENTER SCUFF PLATE IAW AMM 53-11-02. - [SDR SWAA2026080372800](https://openairdocs.org/sdr/SWAA2026080372800), Jul 31, 2026: BRACKET. LOOSE. FORWARD ENTRY DOOR GIRT BAR BRACKET LOOSE. SECURED THE FWD ENTRY DOOR SLIDE GIRT BAR RETAINER CLIPS IAW AMM 25-66-01. - [SDR SWAA2026073134647](https://openairdocs.org/sdr/SWAA2026073134647), Jul 27, 2026: STRUT. CRACKED. LPT REAR FRAME HAD 2 ADDITIONAL CRACKS FOUND TOTALING 5 WHEN PERFORMING 7256-I-11716-NG. FRAME ASSEMBLY, TURBINE REAR FRAME MOUNT STRUT INSPECTION) [TTG8Q01BASK - [SDR SWAA2026073160152](https://openairdocs.org/sdr/SWAA2026073160152), Jul 27, 2026: STRUT. CRACKED. NR 2 ENG, LPT REAR FRAME, TRF STRUT NR 15 LOCATION C2 LARGEST CUMULATIVE CRACK LENGTH OF 0.170 INCH. TRANSFERRED TO [TTG8Q01DDT54] FOR M-21-172-00810 [TTG8Q01DD - [SDR SWAA2026043093586](https://openairdocs.org/sdr/SWAA2026043093586), Apr 27, 2026: RIVET. LOOSE. GIRT BAR LOOSE ON AFT ENTRY DOOR SLIDE. REPLACED GIRT BAR RIVET PER SIP. - [SDR SWAA2026022372610](https://openairdocs.org/sdr/SWAA2026022372610), Feb 19, 2026: LENS. DETACHED. OVERHEAD EXIT SIGN MID CABIN FELL OFF. SECURED OVERHEAD EXIT SIGN LENS IAW AMM INTRO SIP. - [SDR SWAA2025103130085](https://openairdocs.org/sdr/SWAA2025103130085), Oct 30, 2025: GIRT BAR. OUT OF ADJUST. AFT R2 DOOR SLIDE GIRT HANGING DOWN EXCESSIVELY. AFT SIDE HOOK AND LOOP STRIP EXPOSED. SECURED AFT R2 DOOR EMERGENCY SLIDE GIRT IN REF TO SIP. - [SDR SWAA2025100620872](https://openairdocs.org/sdr/SWAA2025100620872), Oct 3, 2025: COVER. DETACHED. MID CABIN EXIT SIGN COVER FELL DOWN. SECURED EXIT SIGN COVER IAW SIP. - [SDR SWAA2025063085513](https://openairdocs.org/sdr/SWAA2025063085513), Jun 26, 2025: SEAL. CRACKED. RIGHT HORIZONTAL STABILIZER UPPER FORWARD SLIDER SEAL CRACKED. REMOVED AND REPLACED RIGHT HORIZONTAL STABILIZER UPPER SLIDER SEAL IAW AMM 53-31-31 - [SDR SWAA2025042226087](https://openairdocs.org/sdr/SWAA2025042226087), Apr 18, 2025: LAMP. INOPERATIVE. L2 EXTERIOR EMERGENCY LIGHT INOP<[01] REPLACED L2 EXTERIOR EMERGENCY LAMP REF AMM 33-51-04. OPS CHECK GOOD. - [SDR SWAA2025021094181](https://openairdocs.org/sdr/SWAA2025021094181), Feb 8, 2025: BULB. BURNED OUT. BURNED ENTRY DOOR EMERGENCY LIGHT BULB ON EXTERIOR FUSELAGE AT AFT GALLEY AREA 2024-780560<[01] REPLACED ENTRY DOOR EMERGENCY LIGHT BULB ON EXTERIOR FUSELAGE AT - [SDR SWAA2025021093069](https://openairdocs.org/sdr/SWAA2025021093069), Feb 5, 2025: LIGHT. DETACHED. MISSING EMERGENCY EXIT LIGHT (2EA) FOUND DISCONNECTED AND REMOVED FROM EYE END TERMINALS BY UNDOCUMENTED MAINTENANCE ON ROW 12ABC AND 9ABC AT PASSENGER CABIN 20 - [SDR SWAA2025021092660](https://openairdocs.org/sdr/SWAA2025021092660), Feb 3, 2025: PLATE. CRACKED. CRACK CORRUGATED PLATE AT OFS 353 BTW SPOILER 3 AND 4 LT WING 2024-780547<[01] REPLACED CURRUGATED PLATE LOC OFS 353 BTW SPOILER 3 AND 4 LT WING IAW B737-700 SR - [SDR SWAA2025021086354](https://openairdocs.org/sdr/SWAA2025021086354), Jan 15, 2025: BEAM. CRACKED. CRACK INDICATION FOUND LOC. STA 663.75 LBL 45.5 I/B SIDE LOWER CHORD LONGITUDINAL BEAM AT 10 OCLOCK. 2024-780492 <[01]. TOOL USED ON STEP 2. ET EQUIPMENT: P/N: - [SDR SWAA2025021089099](https://openairdocs.org/sdr/SWAA2025021089099), Jan 12, 2025: SUPPORT. CRACKED. CRACK ANGLE WEATHER RADAR SUPPORT STRUCTURE LOCATED BETWEEN STA188 TO STA203.8 AND RBL5 AT FWD OF NOSE WHEEL WELL 2024-780466<[01] REPLACED NEW ANGLE WEATHER RA - [SDR SWAA2025020585210](https://openairdocs.org/sdr/SWAA2025020585210), Jan 12, 2025: STRINGER. CRACKED. CRACK STRINGER 26L LOCATED STA540 FWD CARGO COMPARTMENT 2024-780464 <[01] TOOL USED P/N: 45MG; S/N: 130066401; CAL DUE: 21-OCT-25.;[02] TOOL USED EDDY CURRENT E - [SDR SWAA2025020585211](https://openairdocs.org/sdr/SWAA2025020585211), Jan 12, 2025: STRINGER. CRACKED. CRACK STRINGER 25L LOCATED STA540 FWD CARGO COMPARTMENT 2024-780465 <[01] TOOL USED P/N: 45MG; S/N: 130066401; CAL DUE: 21-OCT-25.;[02] TOOL USED ON STEP 8: ET - [SDR SWAA2025021084900](https://openairdocs.org/sdr/SWAA2025021084900), Jan 10, 2025: SUPPORT BRACKET. CRACKED. CRACK SUPPORT BRACKET ON PNEUMATIC DUCT BS 540 AND LBL 6 AT AIR CONDITIONING BAY 2024-780405<[01] REPLACED SUPPORT BRACKET ON PNEUMATIC DUCT BS 540 AND LBL 6 AT - [SDR SWAA2025021085018](https://openairdocs.org/sdr/SWAA2025021085018), Jan 10, 2025: RIB. CRACKED. CRACK LEADING EDGE RIB ACCESS PANEL 331B LE STA 151.75 AT LT HORIZONTAL STABILIZER 2024-780411<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142 - [SDR SWAA2025021085019](https://openairdocs.org/sdr/SWAA2025021085019), Jan 10, 2025: RIB. CRACKED. CRACK LEADING EDGE RIB ACCESS PANEL 331B LE STA 161.04 AT LT HORIZONTAL STABILIZER 2024-780414<[01] REPLACED LEADING EDGE RIB ACCESS PANEL 331B LE STA 161.04 AT - [SDR SWAA2025021084899](https://openairdocs.org/sdr/SWAA2025021084899), Jan 10, 2025: BRACKET. CRACKED. CRACK SUPPORT BRACKET INBOARD FRONT SPAR IFSS 151 AT RT WING 2024-780410<[01] REPLACED SUPPORT BRACKET LOCATED INBOARD FRONT SPAR IFSS 151 AT RT WING IAW B737-7 - [SDR SWAA2025020584898](https://openairdocs.org/sdr/SWAA2025020584898), Jan 10, 2025: STRINGER. CRACKED. CRACK STRINGER 8 INTERNAL AREA FUEL TANK LOC. BTW RIB 19 AND RIB 20 UPPER SKIN LOWER SURFACE AFT AREA AT RT WING 2024-780408 <[01]. TOOL USED: TEMPERATURE CONTR - [SDR SWAA2025021084797](https://openairdocs.org/sdr/SWAA2025021084797), Jan 9, 2025: SKIN PANEL. CRACKED. CRACK INDICATION FOUND ON RT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 RIB AND 16 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK LENG - [SDR SWAA2025020584460](https://openairdocs.org/sdr/SWAA2025020584460), Jan 8, 2025: INTERCOSTAL. CRACKED. CRACK WEB INTERCOSTAL LOCATED BETWEEN BS 294.5 AND BS 303.9 AND STRINGER 16L AT FWD GALLEY AREA 2024-780350<[01]. INSTALLED NEW WEB INTERCOSTAL; STRAP 1(E/A) AN - [SDR SWAA2025020584458](https://openairdocs.org/sdr/SWAA2025020584458), Jan 8, 2025: ANGLE. CRACKED. CRACK ANGLE LOCATED STA294.5 AND STR13L AT PASSENGER CABIN 2024-780338 <[01]. REPLACED ANGLE AND FASTENERS LOCATED STA294.5 AND STR13L AT PASSENGER CABIN I.A.W - [SDR SWAA2025020584461](https://openairdocs.org/sdr/SWAA2025020584461), Jan 8, 2025: ANGLE. CRACKED. CRACK ANGLE LOCATED STA294.5 AND STR17R AT FWD GALLEY AREA 2024-780353 <[01] REPLACED ANGLE AND FASTENERS LOCATED STA294.5 AND STR17R AT FWD GALLEY AREA IAW B73 - [SDR SWAA2025020584462](https://openairdocs.org/sdr/SWAA2025020584462), Jan 8, 2025: TIE CLIP. COLLAPSED. CRACK TIE CLIP LOCATED STA277 AND STR10R PASSENGER CABIN 2024-780336 <[01]. REPLACED TIE CLIP LOCATED STA277 AND STR10R PASSENGER CABIN IAW B737-700 SRM: 51-40- - [SDR SWAA2025020583804](https://openairdocs.org/sdr/SWAA2025020583804), Jan 7, 2025: SUPPORT ANGLE. CRACKED. CRACK ANGLE - SUPPORT BETWEEN BS 907 TO BS 927 STRINGER 25R AND STRNGER 27R AFT CARGO COMPARTMENT 2024-780306 <[01] REPLACED ANGLE - SUPPORT LOCATED BETWEEN BS - [SDR SWAA2025020483803](https://openairdocs.org/sdr/SWAA2025020483803), Jan 7, 2025: INTERCOSTAL. CRACKED. CRACK WEB - INTERCOSTAL BETWEEN BS 927 TO BS 947.5 AND STRINGER 25R AFT CARGO COMPARTMENT 2024-780305<[01]. REPLACED WEB INTERCOSTAL AND FASTENERS LOCATED BETWE - [SDR SWAA2025021083466](https://openairdocs.org/sdr/SWAA2025021083466), Jan 6, 2025: ANGLE. CRACKED. CRACK ANGLE - CLIP LOCATED STA400 AND STR26R FWD CARGO COMPARTMENT 2024-780271<[01] REPLACED ANGLE-CLIP AND FASTENERS LOC ON STA400 AND STR26R FWD CARGO COMPART - [SDR SWAA2025021083472](https://openairdocs.org/sdr/SWAA2025021083472), Jan 6, 2025: PRESSURE WEB. CRACKED. CRACK INDICATION FOUND ON HORIZONTAL PRESSURE WEB UPPER SURFACE BTW STA 663 TO STA 675; AT LEVEL LBL 30. CRACK LENGTH = 0.695 INCHES APPROX. 2024-780281<[01] ON - [SDR SWAA2025020483469](https://openairdocs.org/sdr/SWAA2025020483469), Jan 6, 2025: SUPPORT. ELONGATED. ELONGATED HOLE ON SUPPORT ZEE LOCATED BETWEEN STA500 TO STA500A AFT CARGO COMPARTMENT 2024-780276 ELONGATED HOLE ON SUPPORT ZEE LOCATED BETWEEN STA500 TO STA500 - [SDR SWAA2025020483470](https://openairdocs.org/sdr/SWAA2025020483470), Jan 6, 2025: INTERCOSTAL. CRACKED. CRACK WEB - INTERCOSTAL LOCATED BETWEEN STA500 TO STA500A AND LBL22 FWD CARGO COMPARTMENT 2024-780277<[01]. REPLACED WEB - INTERCOSTAL LOCATED BETWEEN STA500 TO - [SDR SWAA2025020583158](https://openairdocs.org/sdr/SWAA2025020583158), Jan 5, 2025: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE FLOOR STRUCTURE BS 695 AND BL 0 AT PASSENGER CABIN 2024-780190<[01]. STEP 1. EDDY CURRENT EQUIPMENT USED P/N: NORTEC 600D; S/N: 240494307 AN - [SDR SWAA2025020583159](https://openairdocs.org/sdr/SWAA2025020583159), Jan 5, 2025: PANEL. CRACKED. CRACK BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN BL 0 AND RBL 24.75 AT PASSENGER CABIN 2024-780232 <[01]. REPLACED BRAKE PANEL (INTERCOSTAL) AND FASTENERS LOCAT - [SDR SWAA2025020583164](https://openairdocs.org/sdr/SWAA2025020583164), Jan 5, 2025: PANEL. CRACKED. CRACK BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN BL 0 AND LBL 24.75 AT PASSENGER CABIN 2024-780225<[01] REPLACED BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN BL 0 - [SDR SWAA2025020583163](https://openairdocs.org/sdr/SWAA2025020583163), Jan 5, 2025: SUPPORT ANGLE. CRACKED. CRACK LOWER SUPPORT ANGLE FLOOR STRUCTURE BS 695 AND LBL 24.75 AT PASSENGER CABIN 2024-780204 <[01]. TOOL USED: TEMPE CONTROLLER P/N P3015GOES00000 S/N 14281102 - [SDR SWAA2025020583347](https://openairdocs.org/sdr/SWAA2025020583347), Jan 5, 2025: PANEL. CRACKED. CRACK ON HOLES ACCESS PANEL 191CL BODY FAIRING AT FUSELAGE EXTERIOR 2024-780250 <[01] TOOL USED: HOT BONDER P/N: HCS9200B S/N: 16122983 DUE DATE: 15-FEB-25;[02] - [SDR SWAA2025020483344](https://openairdocs.org/sdr/SWAA2025020483344), Jan 5, 2025: LIGHT. BROKEN. BROKEN FLOOR PROXIMITY LIGHTING PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10 EA) 2024-780243<[01] INSTALLED FLOOR PROXIMITY LIGHTING PHOTOLUMINESCENT STRIP AT - [SDR SWAA2025020483161](https://openairdocs.org/sdr/SWAA2025020483161), Jan 5, 2025: GUSSET. CRACKED. CRACK GUSSET LOCATED STA500D AND STR19R FWD CARGO COMPARTMENT 2024-780157 <[01]. REPLACED NEW GUSSET AND FASTENERS LOCATED STA500D AND STR19R FWD CARGO COMPARTM - [SDR SWAA2025020483160](https://openairdocs.org/sdr/SWAA2025020483160), Jan 5, 2025: GUSSET. CRACKED. CRACK GUSSET LOCATED STA500D AND STR19L FWD CARGO COMPARTMENT 2024-780148<[01] REPLACED GUSSET AND FASTENER LOCATED STA500D AND STR19L FWD CARGO COMPARTMENT IAW - [SDR SWAA2025020483153](https://openairdocs.org/sdr/SWAA2025020483153), Jan 5, 2025: ANGLE. CRACKED. CRACK ANGLE - CLIP LOCATED STA400 AND STR26L FWD CARGO COMPARTMENT 2024-780136<[01] REPLACED ANGLE - CLIP LOCATED STA400 AND STR26L FWD CARGO COMPARTMENT IAW B7 - [SDR SWAA2025020483162](https://openairdocs.org/sdr/SWAA2025020483162), Jan 5, 2025: ANGLE. CRACKED. CRACK ANGLE - CLIP LOCATED STA500C AND STR26R FWD CARGO COMPARTMENT 2024-780168<[01] REPLACED ANGLE - CLIP LOCATED ON STA500C AND STR26R FWD CARGO COMPARTMENT I - [SDR SWAA2025021083142](https://openairdocs.org/sdr/SWAA2025021083142), Jan 4, 2025: ACCESS PANEL. CRACKED. CRACK ON HOLES ACCESS PANEL 661BB TRAILING EDGE AT RT WING 2024-780050<[01] TOOL USED: HOT BONDER P/N: HCS9200B S/N: 16122983 DUE DATE: 15-FEB-25;[02] TOOL USED - [SDR SWAA2024112161801](https://openairdocs.org/sdr/SWAA2024112161801), Nov 20, 2024: BATTERY PACK. INOPERATIVE. MID CABIN RIGHT SIDE 3 AISLE AND OVERWING EMERGENCY EXIT LIGHTS INOP<[01] T/S PER FIM 33-50 TASK 801; REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK (M1669) - [SDR SWAA2024100444540](https://openairdocs.org/sdr/SWAA2024100444540), Oct 2, 2024: COVER. DETACHED. EXIT ROW SIGN AT MID CABIN FELL OFF THE CEILING<[01] REINSTALLED COVER PER AMM 33-51-03. - [SDR SWAA2024062103854](https://openairdocs.org/sdr/SWAA2024062103854), Jun 19, 2024: HANDLE. LOOSE. CREW REPORTS MEGAPHONE HANDLE IS LOOSE<[01] R & R MEGAPHONE IAW SIP OPS CHECKS GOOD - [SDR SWAA2024030156710](https://openairdocs.org/sdr/SWAA2024030156710), Feb 26, 2024: COUNTER. SMOKE. FO TRIP COUNTER HAD SMOKE COMING FROM LIGHT<[01] INSPECTED YOKE AREA; NO DAMAGE FOUND
R/R TRIP COUNTER PER AMM 33-11-00 - [SDR SWAA2023073183551](https://openairdocs.org/sdr/SWAA2023073183551), Jul 29, 2023: FAIRING. DELAMINATED. FAIRING 194FR REQUIRE REPLACEMENT REF TTG8Q00M0SWV FOR 194FR<[01] REPLACED 194FR PANEL PER AMM 53-51-21. All 305: https://openairdocs.org/aircraft/N214WN/reports.md ## STCs that may be installed (OpenAirDocs) (37) 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 series) - [STC SE04840NY](https://openairdocs.org/stc/SE04840NY): Installation of HarcoSemco Exhaust Gas Temperature (EGT) Electrical Harnesses in CFM56-7 engine. Kilroy Aviation LLC. Lists CFM56-7B20 - [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. Lists CFM56-7B20 - [STC SE00032EN](https://openairdocs.org/stc/SE00032EN): Installation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 Fan/Booster Module. Pratt & Whitney. Lists CFM56-3 - [STC SE00033EN](https://openairdocs.org/stc/SE00033EN): Installation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 High Pressure Compressor Module. Pratt & Whitney. Lists CFM56-3 - [STC SE00034EN](https://openairdocs.org/stc/SE00034EN): Installation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 High Pressure Turbine Module. Pratt & Whitney. Lists CFM56-3 - [STC SE00035EN](https://openairdocs.org/stc/SE00035EN): Installation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 Low Pressure Turbine Module. Pratt & Whitney. Lists CFM56-3 - [STC SE00822CH](https://openairdocs.org/stc/SE00822CH): Install AeroControlex P/N 2604880-001 variable stator feedback control cable and P/N 2604880-002 variable bleed valve feedback control cable on CFM International engines. AeroControlex Group TransDigm Inc. Lists CFM56-2 ## Related - Other Boeing 737-7H4 aircraft: https://openairdocs.org/model/boeing-737-7h4/aircraft.md - The CFM International CFM56 series engine: https://openairdocs.org/engine/cfm-international-cfm56-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.