# N216WR: 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: 32488 - Year built: 2005 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 25, 2005 - Certificate issued: July 13, 2005 - Expires: October 31, 2027 - Mode S code: A1D1D0 - 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=216WR - Page: https://openairdocs.org/aircraft/N216WR 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/N216WR/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 N216WR. ## FAA accident and incident reports None matched to N216WR. ## Service difficulty reports (301, 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 SWAA2026090819670](https://openairdocs.org/sdr/SWAA2026090819670), Sep 4, 2026: LIGHT. CONTAMINATED. CABIN SEAT ROW 1ABC PHOTOLUMINESCENT STRIP HAS MOISTURE UNDER LENS. R & R THE PHOTOLUMINESCENT STRIP IAW AMM 33-51-15. - [SDR SWAA2026070216762](https://openairdocs.org/sdr/SWAA2026070216762), Jun 28, 2026: LAMP. INOPERATIVE. RIGHT FO SIDE EXIT LIGHT INOPERATIVE. RELAMPED RIGHT SIDE OVER WING EMERGENCY EXIT WINDOW LIGHT IAW AMM 33-51-04 - [SDR SWAA2026051296950](https://openairdocs.org/sdr/SWAA2026051296950), May 9, 2026: BATTERY PACK. INOPERATIVE. RIGHT AFT EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED RIGHT AFTER BATTERY PACK ON EMERGENCY LIGHTS PER AMM 33-51-06 OPS CHECK GOOD AT THIS TIME - [SDR SWAA2026050594499](https://openairdocs.org/sdr/SWAA2026050594499), May 1, 2026: BATTERY PACK. INOPERATIVE. LEFT FORWARD EMERGENCY LIGHTS NOT CHARGING. REMOVED AND REPLACED CHARGER AND BATTERY PACK IAW M/M 33-51-06. - [SDR SWAA2026041387346](https://openairdocs.org/sdr/SWAA2026041387346), Apr 8, 2026: SUPPORT BRACKET. CRACKED. R/H WING UPPER TRAILING PANEL SUPPORT BRACKET CRACKED BETWEEN #7 GROUND SPOILER AND DEFLECTION RIB (SEE ATTACHED PICS)<[01] R&R R/H WING UPPER TRAILING PANEL SU - [SDR SWAA2026041087348](https://openairdocs.org/sdr/SWAA2026041087348), Apr 8, 2026: COVER. MISSING. RH OVERWING EMERGENCY LIGHT FLOOR COVER MISSING<[01] INSTALLED RH OVERWING FLOOR LIGHT COVER PER AMM 33-51-01 - [SDR SWAA2026040987557](https://openairdocs.org/sdr/SWAA2026040987557), Apr 8, 2026: GIRT BAR. OUT OF ADJUST. AFT PASSENGER DOOR GIRT CONTACTING DOOR JAM WHILE CLOSING DOOR<[01] SECURED AFT PASSENGER DOOR GIRT PER AMM 25-66-01 - [SDR SWAA2026032682416](https://openairdocs.org/sdr/SWAA2026032682416), Mar 23, 2026: COVER. MISSING. ROW 1; ABOVE SEAT C; LIGHT COVER MISSING.<[01] REINSTALLED MISSING ROW 1CBA EMERGENCY AREA LIGHT COVER IAW AMM 33-51-03. - [SDR SWAA2026021971479](https://openairdocs.org/sdr/SWAA2026021971479), Feb 17, 2026: LENS. MISSING. ROW 22 DEF BULL NOSE EMERGENCY LIGHT LENS MISSING. INSTALLED THE LENS IAW AMM 33-51-03. - [SDR SWAA2025122254060](https://openairdocs.org/sdr/SWAA2025122254060), Dec 19, 2025: SLIDE. DISLODGED. R 2 DOOR EVAC. SLIDE FELL OUT OF HOLDER.<[01] REINSTALLED R2 ESCAPE SLIDE PER MT 725-61-06. OK FOR SERVICE. - [SDR SWAA2025071791668](https://openairdocs.org/sdr/SWAA2025071791668), Jul 16, 2025: ISOLATION MOUNT. BROKEN. AFT ENTRY DOOR FORWARD SLIDE ATTACH BRACKET HAS TWO BROKEN MOUNT ISOLATORS. R & R IAW SRM 51-40-02. - [SDR SWAA2025062384193](https://openairdocs.org/sdr/SWAA2025062384193), Jun 20, 2025: GIRT BAR. OUT OF ADJUST. FWD ENTRY GIRT BAR IS OUT OF ALIGNMENT. <[01] REPOSITIONED THE FWD ENTRY GIRT BAR AS REQUIRED. REF. AMM 25-66-01. OPS CHECK GOOD. - [SDR SWAA2025040821715](https://openairdocs.org/sdr/SWAA2025040821715), Apr 5, 2025: FUSE. INOPERATIVE. AFT ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOP<[01] SLAVED IN NEW LAMP AND BATTERY PACK. NO HELP. OK TO CONTINUE PER MEL 33-14-01. SP.1 AUTH #245726;[02] REPLACED - [SDR SWAA2025032408168](https://openairdocs.org/sdr/SWAA2025032408168), Mar 20, 2025: SIGN. OUT OF ADJUST. FWD SERVICE DOOR EXIT LIGHT COVER FELL OFF <[01]. R&R?D FWD SERVICE OVER DOOR EMERGENCY EXIT SIGN ASSY. IAW MM 33-51-01. OPS CK?D OK. - [SDR SWAA2025031798935](https://openairdocs.org/sdr/SWAA2025031798935), Feb 23, 2025: THRESHOLD. CORRODED. CORROSION ON THRESHOLD PLATE AT COCKPIT 2025-112784<[01] FAULT RESOLVED ON OTHER FAULT SEE TTG8Q00YW6S7;[02] FAULT RESOLVED ON OTHER FAULT SEE TTG8Q00YW6S7 - [SDR SWAA2025031498524](https://openairdocs.org/sdr/SWAA2025031498524), Feb 23, 2025: PLATE. CORRODED. CORROSION ON THRESHOLD PLATE AT COCKPIT 2025-112784 <[01]. REPLACED THRESHOLD PLATE AT COCKPIT IAW B737-700 SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9.; [02] REPLAC - [SDR SWAA2025031295686](https://openairdocs.org/sdr/SWAA2025031295686), Feb 13, 2025: STRIP. DETERIORATED. DETERIORATED PHOTOLUMINESCENT STRIP LH (5EA) AND RH (5EA) AT FWD GALLEY AREA 2025-113163 <[01]. REPLACED PHOTOLUMINESCENT STRIP LH (5EA) AND RH (5EA) AT FWD GAL - [SDR SWAA2025031395328](https://openairdocs.org/sdr/SWAA2025031395328), Feb 12, 2025: SUPPORT ANGLE. CRACKED. CRACK ANGLE - SUPPORT LOCATED BS807 LBL47 AT AFT CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR ON ANGLE - SUPPORT LOCATED BETWEEN BS787+15 TO BS 807+5, LBL47 AT - [SDR SWAA2025031494855](https://openairdocs.org/sdr/SWAA2025031494855), Feb 10, 2025: FRAME. CRACKED. CRACK WEB FRAME LOCATED BS 259 AND BTW STR 8R TO STR 9R AT PASSENGER CABIN 2025-113077 <[01]. PERFORMED PERMANENT REPAIR LOCATED BS259 AND BTW STR6R TO STR11R A - [SDR SWAA2025031794500](https://openairdocs.org/sdr/SWAA2025031794500), Feb 9, 2025: STRINGER. CRACKED. CRACK ON STRINGER 8 INTERNAL AREA FUEL TANK LOCATED BTW RIB 19 AND RIB 20 UPPER SKIN LOWER SURFACE AT RT WING 2025-113037<[01] PERFORMED PERMANENT REPAIR ON LOC - [SDR SWAA2025031794502](https://openairdocs.org/sdr/SWAA2025031794502), Feb 9, 2025: STRINGER. CRACKED. CRACK ON STRINGER 9 INTERNAL AREA FUEL TANK LOCATED BTW RIB 21 AND RIB 22 UPPER SKIN LOWER SURFACE AT RT WING 2025-113040<[01] TOOL USED: TEMPERATURE CONTROLLER - [SDR SWAA2025031494503](https://openairdocs.org/sdr/SWAA2025031494503), Feb 9, 2025: PANEL. CRACKED. CRACK BLADE ACCESS PANEL 333AT AT LT HORIZONTAL STAB 2025-113042 <[01]. REPLACED BLADE ACCESS PANEL 333AT AT LT HORIZONTAL STAB IAW B737-700 SRM 51-10-02 PARAGR - [SDR SWAA2025031494560](https://openairdocs.org/sdr/SWAA2025031494560), Feb 9, 2025: SUPPORT ANGLE. CRACKED. CRACK ANGLE - SUPPORT LOCATED BS867 AT LEVEL STR27L AT AFT CARGO COMPARTMENT 2025-113049 <[01]. REPLACED ANGLE-SUPPORT LOCATED BS 867 AT LEVEL STRINGER 27L AT A - [SDR SWAA2025031294436](https://openairdocs.org/sdr/SWAA2025031294436), Feb 9, 2025: BATTERY PACK. INOPERATIVE. INOP BATTERY PACK ON LOWER CEILING PANEL LH SIDE AT AFT AREA GALLEY 2025-113017 <[01]. REPLACED BATTERY PACK ON LOWER CEILING PANEL LH SIDE AT AFT AREA GALLEY I - [SDR SWAA2025031294437](https://openairdocs.org/sdr/SWAA2025031294437), Feb 9, 2025: BATTERY PACK. INOPERATIVE. INOP BATTERY PACK ON LOWER CEILING PANEL RH SIDE AT AFT AREA GALLEY 1EA 2025-113018 <[01]. REPLACED BATTERY PACK ON LOWER CEILING PANEL RH SIDE AT AFT AREA GALL - [SDR SWAA2025031294438](https://openairdocs.org/sdr/SWAA2025031294438), Feb 9, 2025: POWER SUPPLY. INOPERATIVE. INOP EMERGENCY POWER SUPPLY ON LOWER CEILING PANEL LH SIDE AT AFT AREA GALLEY 1EA 2025-113019 <[01]. REPLACED EMERGENCY POWER SUPPLY ON LOWER CEILING PANEL LH S - [SDR SWAA2025031294439](https://openairdocs.org/sdr/SWAA2025031294439), Feb 9, 2025: POWER SUPPLY. INOPERATIVE. INOP EMERGENCY POWER SUPPLY ON LOWER CEILING PANEL RH SIDE AT AFT AREA GALLEY 1EA 2025-113020 <[01]. REPLACED EMERGENCY POWER SUPPLY ON LOWER CEILING PANEL RH S - [SDR SWAA2025031794432](https://openairdocs.org/sdr/SWAA2025031794432), Feb 8, 2025: STRINGER. CRACKED. CRACK STRINGER 23L LOCATED BS540 AT FWD CARGO COMPARTMENT 2025-113006<[01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29- - [SDR SWAA2025031794433](https://openairdocs.org/sdr/SWAA2025031794433), Feb 8, 2025: STRINGER. CORRODED. CORROSION STRINGER 26L LOCATED BS540 WL156.5 AT FWD CARGO COMPARTMENT 2025-113004<[01] STEP 2. ULTRASONIC EQUIPMENT USED P/N: 45MG; S/N: 130066401 AND DUE DATE: - [SDR SWAA2025031794270](https://openairdocs.org/sdr/SWAA2025031794270), Feb 8, 2025: PANEL. CRACKED. CRACK LOWER EDGE ACCESS PANEL 211B AT CONTROL CABIN 2025-112959. - [SDR SWAA2025031494434](https://openairdocs.org/sdr/SWAA2025031494434), Feb 8, 2025: SUPPORT ANGLE. CRACKED. CRACK ANGLE - SUPPORT LOCATED BS500D AT LEVEL STR28R FWD CARGO COMPARTMENT 2025-113009 <[01]. REPLACED ANGLE - SUPPORT AND FASTENERS LOCATED BS500D AT LEVEL STR - [SDR SWAA2025031494271](https://openairdocs.org/sdr/SWAA2025031494271), Feb 8, 2025: SHIELD. CORRODED. CORROSION ON SHIELD LOCATED BTW BS492.4 TO BS500A AT LEVEL STR26R WL156.5 AT FWD CARGO COMPARTMENT 2025-112979 <[01]. REPLACED SHIELD AND FASTENERS LOCATED BTW - [SDR SWAA2025031494272](https://openairdocs.org/sdr/SWAA2025031494272), Feb 8, 2025: PRESSURE DECK. CRACKED. CRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB BETWEEN STA. 663 TO STA. 675 RBL 42. CRACK LENGTH 0.625 IN. PASSENGER CABIN 2025-112981 <[01]. TOOL USED: EDDY - [SDR SWAA2025031794244](https://openairdocs.org/sdr/SWAA2025031794244), Feb 7, 2025: SUPPORT BRACKET. CRACKED. CRACK SUPPORT BRACKET BS 663.75 AND RBL 54 AT LOWER FUSELAGE 2025-112923<[01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811019; DUE DATE: - [SDR SWAA2025031794245](https://openairdocs.org/sdr/SWAA2025031794245), Feb 7, 2025: INTERCOSTAL. CRACKED. CRACK ON INTERCOSTAL LOCATED BTW BS 685 TO BS 707 AT LEVEL STR 14R AT PASSENGER CABIN 2025-112924<[01] REPLACED WEB INTERCOSTAL
LOCATED BTW BS 685 TO BS 707 - [SDR SWAA2025031794115](https://openairdocs.org/sdr/SWAA2025031794115), Feb 7, 2025: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED AT LEVEL STR 17R BTW BS 291.5 TO 294.5 AT PASSENGER CABIN 2025-112898 <[01]. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED AT LEVE - [SDR SWAA2025031794123](https://openairdocs.org/sdr/SWAA2025031794123), Feb 7, 2025: ANGLE. CRACKED. CRACK SLAT 8 ANGLE ON INBOARD AUXILIARY TRACK AT RT WING 2025-112907 <[01]. REPLACED ANGLE LOCATED ON SLAT 8 INBOARD AUXILIARY TRACK AT RT WING.
IAW B737-700 - [SDR SWAA2025031494113](https://openairdocs.org/sdr/SWAA2025031494113), Feb 7, 2025: PANEL. DELAMINATED. DELAMINATE ON ACCESS PANEL 333CB AT LT HORIZONTAL STABILIZER 2025-112894 <[01]. TOOL USED P/N: EPOCH 600; S/N: 120357005; CAL DUE: 10-JUN-25.;[02] REPAIRED ACCE - [SDR SWAA2025031494114](https://openairdocs.org/sdr/SWAA2025031494114), Feb 7, 2025: SUPPORT ANGLE. CRACKED. CRACK SEAL - PLATE ACCESS PANEL 333AB SUPPORT ANGLE LT HORIZONTAL STAB 2025-112897 <[01]. REPLACED PLATE ACCESS PANEL 333AB SUPPORT ANGLE LT HORIZONTAL STAB IAW - [SDR SWAA2025031494120](https://openairdocs.org/sdr/SWAA2025031494120), Feb 7, 2025: SUPPORT ANGLE. CRACKED. CRACK SEAL - PLATE ACCESS PANEL 343AB SUPPORT ANGLE RT HORIZONTAL STAB 2025-112899 <[01]. REPLACED PLATE ACCESS PANEL 343AB SUPPORT ANGLE RT HORIZONTAL STAB IAW - [SDR SWAA2025031494241](https://openairdocs.org/sdr/SWAA2025031494241), Feb 7, 2025: RAIL. CRACKED. CRACK O/B FIXED LEADING EDGE RAIL NUT PLATE OFSS 449 AT RT WING 2025-112911<[01]. REPLACED O/B FIXED LEADING EDGE RAIL NUT PLATE (GANG CHANNEL) OFSS 449 AT RT W - [SDR SWAA2025031494118](https://openairdocs.org/sdr/SWAA2025031494118), Feb 7, 2025: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE WING BODY FAIRING STRUCTURE BS 500D AT LEVEL STRINGER 19R LOWER FUSELAGE 2025-112895 <[01]. REPLACED SUPPORT ANGLE LOC. WING BODY FAIRING ST - [SDR SWAA2025031494252](https://openairdocs.org/sdr/SWAA2025031494252), Feb 7, 2025: GIRT BAR. DETERIORATED. DETERIORATED GIRT BAR FLOOR BRACKETS HARDWARE AND PLATE AFT ENTRY DOOR AT AFT GALLEY AREA 2025-112910 <[01]. REPLACED GIRT BAR FLOOR BRACKETS HARDWARE AND PLATE - [SDR SWAA2025031494253](https://openairdocs.org/sdr/SWAA2025031494253), Feb 7, 2025: GIRT BAR. DETERIORATED. DETERIORATED GIRT BAR FLOOR BRACKETS HARDWARE AND PLATE AFT SERVICE DOOR AT AFT GALLEY AREA 2025-112909 <[01]. REPLACED GIRT BAR FLOOR BRACKETS HARDWARE AND PLA - [SDR SWAA2025031494247](https://openairdocs.org/sdr/SWAA2025031494247), Feb 7, 2025: INTERCOSTAL. CRACKED. CRACK ON INTERCOSTAL LOCATED BTW BS 685 TO BS 707 AT LEVEL STR 14L AT PASSENGER CABIN 2025- 112927 <[01]. REPLACED WEB INTERCOSTAL LOCATED BTW BS 685 TO BS 707 - [SDR SWAA2025031494122](https://openairdocs.org/sdr/SWAA2025031494122), Feb 7, 2025: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED BS 294.5 AT LEVEL STR 13L AT FWD GALLEY AREA 2025-112904 <[01]. REPLACED SUPPORT ANGLE LOCATED BS 294.5 AT LEVEL STR 13L AT FWD G - [SDR SWAA2025031494248](https://openairdocs.org/sdr/SWAA2025031494248), Feb 7, 2025: SUPPORT BRACKET. CRACKED. CRACK ON SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN 2025-112932 <[01]. REPLACED SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R - [SDR SWAA2025031793990](https://openairdocs.org/sdr/SWAA2025031793990), Feb 6, 2025: SCUFF PLATE. CRACKED. CRACK FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT 2025-112830<[01] TOOL USED DIGITAL CALIPER P/N: 500-196-30; S/N: B23399190; DUE DATE: 04/MAR/25.;[02] EQUI - [SDR SWAA2025031793770](https://openairdocs.org/sdr/SWAA2025031793770), Feb 6, 2025: INTERCOSTAL. CRACKED. CRACK INTERCOSTAL - WEB FLOOR STRUCTURE LOCATED BS540 BTW BL0 TO LBL24.75 AT PASSENGER CABIN 2025-112771<[01] REPLACED INTERCOSTAL - WEB FLOOR STRUCTURE LOCATED - [SDR SWAA2025031793763](https://openairdocs.org/sdr/SWAA2025031793763), Feb 6, 2025: INTERCOSTAL. CRACKED. CRACK INTERCOSTAL - WEB FLOOR STRUCTURE LOCATED AT BS540 BTW BL0 TO RBL24.75 AT PASSENGER CABIN. 2025-112772 CRACK INTERCOSTAL - WEB FLOOR STRUCTURE LOCATED BS5 All 301: https://openairdocs.org/aircraft/N216WR/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.