# N217JC: 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: 34232 - Year built: 2005 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 29, 2005 - Certificate issued: July 20, 2005 - Expires: October 31, 2027 - Mode S code: A1D44E - 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=217JC - Page: https://openairdocs.org/aircraft/N217JC 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/N217JC/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 N217JC. ## FAA accident and incident reports None matched to N217JC. ## Service difficulty reports (266, 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 SWAA2026101201027](https://openairdocs.org/sdr/SWAA2026101201027), Oct 6, 2026: LAVATORY. DIRTY. FORWARD LAV HAD A HORRIBLE ODOR. FWD LAV CLEANED IAW TTG8Q01FSWJ9. - [SDR SWAA2026042492106](https://openairdocs.org/sdr/SWAA2026042492106), Apr 23, 2026: GIRT BAR. LOOSE. L1 DOOR GIRT BAR BRACKET LOOSE<[01] RE-SECURED L1 DOOR GIRT BAR BRACKET. NO OTHER DEFECTS NOTED AT THIS TIME. REF AMM 25-66-01 - [SDR SWAA2026040381804](https://openairdocs.org/sdr/SWAA2026040381804), Mar 21, 2026: PRESSURE BLKHD. CRACKED. DURING INSPECTION OF BS 1016 AFT PRESSURE BULKHEAD CENTER DOME APEX - GROUP 2; INDICATION OF A CRACK AT BL0 FASTENER DURING HFEC INSPECTION. CRACK VERIFIED POST - [SDR SWAA2026010858254](https://openairdocs.org/sdr/SWAA2026010858254), Jan 4, 2026: OIL SYSTEM. LEAKING. LOST OIL QUANTITY THEN WE LOST OIL PRESSURE ON NR 1 ENG. SHUTDOWN AND LANDED WHITE BOX CAME ON FOR THE OIL QTY AND 20 MINS LATER WENT YELLOW THEN RED ON THE OIL - [SDR SWAA2025120240639](https://openairdocs.org/sdr/SWAA2025120240639), Nov 29, 2025: PUMP. FAILED. AFTER EXITING RUNWAY (AFTER LANDING), NR 1 ENGINE FAILED. FAIL ON ENGINE INSTRUMENTS. NR 1 GEN OFF LINE AT SAME TIME. NR 1 ENGINE SPOOLS UP MUCH SLOWER ON TAKEO - [SDR SWAA2025120241853](https://openairdocs.org/sdr/SWAA2025120241853), Nov 29, 2025: HMU. FAILED. AFTER EXITING RUNWAY (AFTER LANDING) NR 1 ENGINE FAILED. FAIL ON ENGINE INSTRUMENTS. NR 1 GEN OFF LINE AT SAME TIME. NR 1 ENGINE SPOOLS UP MUCH SLOWER ON TAKEOF - [SDR SWAA2025120241854](https://openairdocs.org/sdr/SWAA2025120241854), Nov 29, 2025: ELEC CONNECTOR. DISCONNECTED. AFTER EXITING RUNWAY, AFTER LANDING. NR 1 ENGINE FAILED. FAIL ON ENGINE INSTRUMENTS.NR 1 GEN OFF LINE AT SAME TIME. NR 1 ENGINE SPOOLS UP MUCH SLOWER ON TAKEOFF - [SDR SWAA2025102828365](https://openairdocs.org/sdr/SWAA2025102828365), Oct 24, 2025: GIRT BAR. JAMMED. FWD SERVICE DOOR GIRT BAR JAMMED. FREED THE GIRT BAR FROM SLIDE COVER RETAINER IAW MM 25-66-02, OPS NORMAL. - [SDR SWAA2025090511358](https://openairdocs.org/sdr/SWAA2025090511358), Sep 4, 2025: LENS. DETACHED. ROW 11F SIDEWALL LIGHT LENS FELL OFF. ATTACHED ROW 11F SIDEWALL LIGHT LENS IAW AMM 33-51-00 - [SDR SWAA2025072992996](https://openairdocs.org/sdr/SWAA2025072992996), Jul 19, 2025: HINGE. CRACKED. WATER SERVICE DOOR; AFT HINGE CRACKED. REMOVED AND REPLACED WATER SERVICE DOOR; AFT HINGE IAW SRM 51-40-02-0G-0 AND IPC 52-49-00-02. - [SDR SWAA2025071690904](https://openairdocs.org/sdr/SWAA2025071690904), Jul 13, 2025: GIRT BAR. OUT OF ADJUST. CHECK R1 GIRT BAR PROPER FUNCTION FA REPORTS LOOSE IN HOLDER. REPAIRED PER [UNLISTED MANUAL NOT LISTED (NO REFERENCE FOUND)] TIGHTENED GIRT BAR HOLDING BRACKET - [SDR SWAA2025070788698](https://openairdocs.org/sdr/SWAA2025070788698), Jul 6, 2025: SLIDE. OUT OF LIMITS. AFTER SERVICE. DOOR SLIDE IS INDICATING IN RED. REMOVED AND REPLACED SLIDE ASSY PER M/M 25-66-01 AND MT 725-61-06. - [SDR SWAA2025032406906](https://openairdocs.org/sdr/SWAA2025032406906), Mar 19, 2025: HANDLE. LOOSE. PAX CABIN FWD ENTRY DOOR INTERNAL HANDLE WITH LOOSE PLATE 2025-137106 <[01]. INSTALLED CORRECTLY PAX CABIN FWD ENTRY DOOR INTERNAL HANDLE PLATE IAW B737-700 AMM - [SDR SWAA2025032404186](https://openairdocs.org/sdr/SWAA2025032404186), Mar 11, 2025: SLAT TRACK. CORRODED. CORROSION ON SLAT 5 OUTBOARD MAIN TRACK ON UPPER ROLLER SURFACE AT RT WING 2025-137044 <[01]. REPLACED LEADING EDGE SLAT 5 OUTBOARD MAIN TRACK IAW B737-700 AMM - [SDR SWAA2025032198532](https://openairdocs.org/sdr/SWAA2025032198532), Feb 22, 2025: SLAT. CRACKED. REPLACE SLAT 5 DUE TO CRACK ON FITTING WAS FOUND AT RT WING 2025-137023<[01] REPLACED SLAT 5 IAW B737-700 AMM 27-81-21-401-NG
SEE INDIVIDUAL SIGN OFF BELLOW; - [SDR SWAA2025032498190](https://openairdocs.org/sdr/SWAA2025032498190), Feb 20, 2025: SUPPORT BRACKET. DAMAGED. ELONGATED HOLES ON SUPPORT BRACKETS OF BRACE SUPPORT AT RT MLG WHEEL WELL RING 2025-136995<[01] REPLACED SUPPORT BRACKETS OF BRACE SUPPORT AT RT MLG WHEEL WELL - [SDR SWAA2025032497763](https://openairdocs.org/sdr/SWAA2025032497763), Feb 19, 2025: SUPPORT BRACKET. CRACKED. CRACK SUPPORT BRACKET ON BULKHEAD BS 727 AT LEVEL STRINGER 27R AFT CARGO COMPARTMENT 2025-136984 <[01]. REPLACED SUPPORT BRACKET ON BULKHEAD BS 727 AT LEVEL STR - [SDR SWAA2025032497125](https://openairdocs.org/sdr/SWAA2025032497125), Feb 17, 2025: GUSSET. CRACKED. CRACK ON GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT 2025-136939 <[01]. REPLACED NEW GUSSET AND FASTENERS LOCATED ON BS500D AND STR19L FWD CARGO COMP - [SDR SWAA2025032497128](https://openairdocs.org/sdr/SWAA2025032497128), Feb 17, 2025: LIGHT. BROKEN. BROKEN HOUSING ASSY EMERGENCY LIGHT OVERHEAD BIN BULLNOSE ROW 6 DEF AND 14 DEF 2025-136949 <[01]. REPLACED HOUSING ASSY EMERGENCY LIGHT OVERHEAD BIN BULLNOSE RO - [SDR SWAA2025032497124](https://openairdocs.org/sdr/SWAA2025032497124), Feb 17, 2025: ANGLE. CRACKED. CRACK ON ANGLE LOCATED BS663 UPPER POSITION RBL39 AT CENTER WING BOX 2025-136945 <[01]. TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; - [SDR SWAA2025032497118](https://openairdocs.org/sdr/SWAA2025032497118), Feb 17, 2025: SUPPORT ANGLE. CRACKED. CRACK ANGLE - SUPPORT LOCATED BS500D STR28R AFT POSITION FWD CARGO COMPARTMENT 2025-136936 <[01]. REPLACED ANGLE-SUPPORT LOCATED BS500D STR28R AFT POSITION FWD - [SDR SWAA2025032497123](https://openairdocs.org/sdr/SWAA2025032497123), Feb 17, 2025: GUSSET. CRACKED. CRACK ON GUSSET LOCATED BS500D AND STR21L FWD CARGO COMPARTMENT 2025-136940 <[01]. REPLACED GUSSET LOCATED BS500D AND STR21L FWD CARGO COMPARTMENT AND FASTENERS - [SDR SWAA2025032497126](https://openairdocs.org/sdr/SWAA2025032497126), Feb 17, 2025: GUSSET. CRACKED. CRACK ON GUSSET LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT 2025-136938 <[01]. REPLACED GUSSET AND FASTENERS LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT - [SDR SWAA2025032497120](https://openairdocs.org/sdr/SWAA2025032497120), Feb 17, 2025: STRINGER. CRACKED. CRACK ON STRINGER 25L LOCATED BTW BS520 TO BS540 AT FWD CARGO COMPARTMENT 2025-136937<[01] ON STEP 2: TOOL USED ULTRASONIC EQUIPMENT PN: 45MG; SN: 221859911; DU - [SDR SWAA2025032497127](https://openairdocs.org/sdr/SWAA2025032497127), Feb 17, 2025: SKIN. CRACKED. CRACK FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 9.5 INCHES FROM FRONT SPAR; INB SIDE OF RIB LENGTH APPROX= 0.845 INCHES. 2025- - [SDR SWAA2025032497121](https://openairdocs.org/sdr/SWAA2025032497121), Feb 17, 2025: ACCESS PANEL. CRACKED. CRACK ACCESS PANEL 667BT OB FOREFLAP AT RT WING 2025-136944<[01] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29-JAN-26.;[02 - [SDR SWAA2025032097122](https://openairdocs.org/sdr/SWAA2025032097122), Feb 17, 2025: TIE CLIP. CRACKED. CRACK ON TIE CLIP LOCATED BS500C AND STR19L AT FWD CARGO COMPARTMENT 2025-136941 <[01]. REPLACED TIE CLIP LOCATED BS500C AND STR19L AT FWD CARGO COMPARTMENT IAW - [SDR SWAA2025031997117](https://openairdocs.org/sdr/SWAA2025031997117), Feb 17, 2025: INTERCOSTAL. CRACKED. CRACK WEB - INTERCOSTAL LOCATED BTW BS500D TO BS520 STR28L FWD CARGO COMPARTMENT 2025-136935 <[01]. REPLACED WEB-INTERCOSTAL AND FASTENERS LOCATED BTW BS500D TO - [SDR SWAA2025032496586](https://openairdocs.org/sdr/SWAA2025032496586), Feb 16, 2025: LENS. BROKEN. BROKEN EMERGENCY EXIT LIGHT LENS LAVATORY A AT FWD GALLEY AREA (1 EA) 2025-136886 <[01]. REPLACED EMERGENCY EXIT LIGHT LENS LAVATORY A AT FWD GALLEY AREA (1 EA) - [SDR SWAA2025032496597](https://openairdocs.org/sdr/SWAA2025032496597), Feb 16, 2025: LENS. BROKEN. BROKEN EMERGENCY EXIT LIGHT LENS LAVATORY B AT AFT GALLEY AREA (1 EA) 2025-136900<[01] REPLACED EMERGENCY EXIT LIGHT LENS LAVATORY B AT AFT GALLEY AREA (1 EA) I - [SDR SWAA2025032496584](https://openairdocs.org/sdr/SWAA2025032496584), Feb 15, 2025: LIGHT. BROKEN. BROKEN FLOOR PROXIMITY LIGHTING PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10 EA) 2025-136877 <[01]. REPLACED FLOOR PROXIMITY LIGHTING PHOTOLUMINESCENT STRIP AT - [SDR SWAA2025032496581](https://openairdocs.org/sdr/SWAA2025032496581), Feb 15, 2025: RIB. CRACKED. CRACK FRONT SPAR INSPAR RIB 4 AT RT HORIZONTAL STABILIZER 2025-136863<[01] TOOL USED ON STEP 3: ET EQUIPMENT; P/N: NORTEC 600D; S/N: 210138503 ; DUE DATE: 05-AU - [SDR SWAA2025032496430](https://openairdocs.org/sdr/SWAA2025032496430), Feb 15, 2025: RIB. CRACKED. CRACK RIB ON ACCESS PANEL 331B LEADING EDGE STA 105.26 LT HORIZONTAL STAB 2025-136851<[01] REPLACED RIB LOCATED ON ACCESS PANEL 331B LEADING EDGE STA 105.26 LT - [SDR SWAA2025032496433](https://openairdocs.org/sdr/SWAA2025032496433), Feb 15, 2025: RIB. CRACKED. CRACK RIB ON ACCESS PANEL 341B LE STA95.96 AT RT HORIZONTAL STABILIZER 2025-136853 <[01]. REPLACED RIB ON ACCESS PANEL 341B LE STA95.96 AT RT HORIZONTAL STABILI - [SDR SWAA2025032496208](https://openairdocs.org/sdr/SWAA2025032496208), Feb 14, 2025: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE FWD BODY FAIRING STRUCTURE BS 500D AT LEVEL STRINGER 19R LOWER FUSELAGE 2025-136785<[01] REPLACED SUPPORT ANGLE LOCATED AT FWD BODY FAIRI - [SDR SWAA2025032495999](https://openairdocs.org/sdr/SWAA2025032495999), Feb 13, 2025: FAIRING. DAMAGED. ELONGATED HOLE ACCESS PANEL 544CL FLAP SUPPORT FAIRING 1 AT LT WING 2025-136774<[01] REPLACED ACCESS PANEL 544CL FLAP SUPPORT FAIRING 1 AT LT WING I.A.W. B737-8 - [SDR SWAA2025032495332](https://openairdocs.org/sdr/SWAA2025032495332), Feb 12, 2025: PRESSURE DECK. CRACKED. CRACK ON HORIZONTAL PRESSURE DECK WEB BS 665 AND LBL 33 AT CENTER SECTION 2025-136659 <[01]. TOOL USED ON STEP 5 EDDY CURRENT EQUIPMENT P/N: NORTEC 600D S:N 600 - [SDR SWAA2025032495545](https://openairdocs.org/sdr/SWAA2025032495545), Feb 12, 2025: FRAME. CRACKED. CRACK ON FRAME BS 259.5 BETWEEN STRINGER 8R AND STRINGER 9R AT PASSENGER CABIN 2025-136683 <[01]. TOOL USED ON STEP 4 EDDY CURRENT EQUIPMENT P/N: NORTEC 600D S: - [SDR SWAA2025032495546](https://openairdocs.org/sdr/SWAA2025032495546), Feb 12, 2025: FRAME. CRACKED. CRACK FRAME BS 259.5 BETWEEN STRINGER 8L TO STRINGER 9L AT PASSENGER CABIN 2025-136687 <[01] .TOOL USED ON STEP 4 ET EQUIPMENT: P/N: NORTEC 600D; S/N: 600071614 - [SDR SWAA2025032495330](https://openairdocs.org/sdr/SWAA2025032495330), Feb 12, 2025: FLOORBEAM. CRACKED. CRACK BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN BL 0 TO LBL 24.75 AT PASSENGER CABIN 2025-136657<[01] REPLACED BRAKE PANEL FLOOR STRUCTURE LOCATED ON BS 540 BE - [SDR SWAA2025032495331](https://openairdocs.org/sdr/SWAA2025032495331), Feb 12, 2025: PANEL. CRACKED. CRACK BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN BL 0 TO RBL 24.75 AT PASSENGER CABIN 2025-136658<[01] REPLACED BRAKE PANEL FLOOR STRUCTURE AND FASTENERS LOCATE - [SDR SWAA2025032495333](https://openairdocs.org/sdr/SWAA2025032495333), Feb 12, 2025: FLOORBEAM. CRACKED. CRACK ON LOWER ANGLE FLOOR STRUCTURE BS 695 AND LBL 24.75 AT CENTER SECTION 2025-136665<[01] REPLACED ANGLE FLOOR STRUCTURE BS 695 AND LBL 24.75 AT CENTER SECTI - [SDR SWAA2025032495547](https://openairdocs.org/sdr/SWAA2025032495547), Feb 12, 2025: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE BS 294.5 AND STRINGER 13L AT PASSENGER CABIN 2025-136699<[01] REPLACED SUPPORT ANGLE BS 294.5 AND STRINGER 13L AT PASSENGER CABIN IAW B73 - [SDR SWAA2025032408753](https://openairdocs.org/sdr/SWAA2025032408753), Feb 12, 2025: STRINGER. CRACKED. CRACK ON SUPPORT ANGLE BS 294.5 AND STRINGER 13L AT PASSENGER CABIN 2025-136699<[01] REPLACED SUPPORT ANGLE BS 294.5 AND STRINGER 13L AT PASSENGER CABIN IAW B73 - [SDR SWAA2025032494666](https://openairdocs.org/sdr/SWAA2025032494666), Feb 10, 2025: SKIN. CRACKED. CRACK LEADING EDGE SLAT NOSE LOWER SKIN LOCATED SLAT 5 STATION 85.19 AT RT WING. 2025-136590<[01] TOOL USED P/N: NORTEC 500D; S/N: N500X1693P030456; CAL DUE: 14 - [SDR SWAA2024082729375](https://openairdocs.org/sdr/SWAA2024082729375), Aug 23, 2024: BATTERY PACK. NO TEST. EMX BATT PACK M01675 FAILS CAPACITANCE CHECK<[01] 01 - REMOVED AND REPLACED EMX BATT PACK M01675 PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLA - [SDR SWAA2023121330545](https://openairdocs.org/sdr/SWAA2023121330545), Dec 11, 2023: GIRT BAR. OUT OF ADJUST. FWD GALLEY SERVICE DOOR GIRT BAR WILL NOT SECURE IN THE UNARMED POSITION<[01] ADJUSTED HOOKS THAT HOLD THE FWD GALLEY SERVICE DOOR GRIT BAR AS PER AMM 25-66-02. - [SDR SWAA2023112724596](https://openairdocs.org/sdr/SWAA2023112724596), Nov 22, 2023: GIRT BAR. OUT OF ADJUST. FORWARD SERVICE DOOR GIRT BAR WILL NOT STOW.<[01] RE-ALIGN GIRT BAR PER AMM 25-66-01 ON FWD SERVICE DOOR. - [SDR SWAA2023110317240](https://openairdocs.org/sdr/SWAA2023110317240), Nov 2, 2023: SLIDE. OUT OF LIMITS. AFT SVC EVAC. SLIDE IS OVER PRESSURE.<[01] REMOVED AND REPLACED AFT SVC SLIDE PER AMM 25-66-01 AND MT 725-61-01. E34824 - [SDR SWAA2023090898240](https://openairdocs.org/sdr/SWAA2023090898240), Sep 7, 2023: NUT. BROKEN. FWD SERVICE DOOR ASSIST HANDLE BROKEN.<[01] REPLACED FWD SERVICE DOOR ASSIST HANDLE NUT IAW AMM 52-11-31.
WORK PERFORMED BY E20763. All 266: https://openairdocs.org/aircraft/N217JC/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.