# N218WN: 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: 32489
- Year built: 2005
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 30, 2005
- Certificate issued: July 20, 2005
- Expires: October 31, 2027
- Mode S code: A1D93B
- 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=218WN
- Page: https://openairdocs.org/aircraft/N218WN

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/N218WN/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 N218WN.

## FAA accident and incident reports

None matched to N218WN.

## Service difficulty reports (281, 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 SWAA2026102116002](https://openairdocs.org/sdr/SWAA2026102116002), Oct 17, 2026: LAMP. INOPERATIVE. RIGHT FWD EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. R & R THE LAMP IAW AMM 33-51-04. OPS CHKD SATISFACTORY.
- [SDR SWAA2026100556763](https://openairdocs.org/sdr/SWAA2026100556763), Oct 3, 2026: COLLECTOR. ABNORMAL. NR 1 ENGINE CANDLING AFTER SHUT DOWN FOR ABOUT 5-7 MINUTES. REMOVED AND REPLACED IAW AMM 71-00-00-800-803-F00, INSPECTION AFTER AN ENGINE FIRE USE OF FIRE EXTIN
- [SDR SWAA2026092906455](https://openairdocs.org/sdr/SWAA2026092906455), Sep 25, 2026: LAMP. INOPERATIVE. EMERGENCY EXIT LIGHT AT R1 DOOR WAS INOPERATIVE. REMOVED AND REPLACED THE LAMPS IAW AMM 33-51-04-960-801.
- [SDR SWAA2026090301846](https://openairdocs.org/sdr/SWAA2026090301846), Aug 30, 2026: STRUT. CRACKED. NR 1 ENGINE TURBINE REAR FRAME HAD A CRACK ON STRUT NR 15 AT C2, LOCATION MEASURING 0.0895" CW EA M-21-172-00808 NR 1 ENG TURBINE REAR FRAME TO REINSP EVERY 470
- [SDR SWAA2026081077807](https://openairdocs.org/sdr/SWAA2026081077807), Aug 5, 2026: LIGHT. INOPERATIVE. FO EMERGENCY EXIT DOOR INTERNAL EMERGENCY LIGHT INOPERATIVE. R & R IAW AMM 33-51-04-960-801.
- [SDR SWAA2026062314655](https://openairdocs.org/sdr/SWAA2026062314655), Jun 21, 2026: SEAT. FAULTED. SEAT 15 DEF WONT STAY UP. TIGHTENED AFFECTED SEAT ROW AS REQUIRED IAW CMM 25-21-45.
- [SDR SWAA2026061511252](https://openairdocs.org/sdr/SWAA2026061511252), Jun 10, 2026: SIGN. BROKEN. MID-CABIN CEILING EXIT SIGN BROKEN. REMOVED AND REPLACED OVERWING CEILING EMERGENCY EXIT SIGN IAW AMM 33-51-01.
- [SDR SWAA2025091113796](https://openairdocs.org/sdr/SWAA2025091113796), Sep 11, 2025: BATTERY. NO TEST. FA REPORTS AFT EMERGENCY FLASH LIGHT WONT TEST. REPLACED AFT INBOARD FLASHLIGHT BATTERY. OPS CHECK OKAY. REF AMM 25-64-00
- [SDR SWAA2025082206432](https://openairdocs.org/sdr/SWAA2025082206432), Aug 19, 2025: ACM. SEIZED. WITH MAX COOLING FROM THE APU; AFTER ABOUT 10 MINUTES; SMOKE FILLED THE CABIN AND AN ACRID SMELL WAS NOTICED. THE PACKS AND RECIRC FAN WERE TURNED OFF AND THE S
- [SDR SWAA2025051670801](https://openairdocs.org/sdr/SWAA2025051670801), May 13, 2025: FLASHLIGHT. INOPERATIVE. FWD FLASHLIGHT (FA) INOP<[01] R+R FWD FA FLASHLIGHT PER AMM 33-55-00.<BR>OPS CHECKS GOOD.
- [SDR SWAA2025040721696](https://openairdocs.org/sdr/SWAA2025040721696), Apr 4, 2025: LENS. OUT OF ADJUST. R1 OVERDOOR EXIT SIGN LENS FALLING<[01] R&R OVERDOOR EXIT SIGN ASSY PER AMM 33-51-01
- [SDR SWAA2025032608223](https://openairdocs.org/sdr/SWAA2025032608223), Mar 22, 2025: HANDLE. BROKEN. L-2 DOOR ASSIST HANDLE IS BROKEN IN TWO HALVES. REPLACED L-2 DOOR ASSIST HANDLE IAW AMM-52-13-31-400-802 ITEM G STEP 2.
- [SDR SWAA2025032607422](https://openairdocs.org/sdr/SWAA2025032607422), Mar 19, 2025: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT BATTERY PACK M1668 WILL NOT CHARGE<[01] REMOVED AND REPLACED EMERGENCY EXIT BATTERY M1668 IAW AMM 33-51-06-960-805.<BR>OPS CHECK GOOD.<BR>WN50148
- [SDR SWAA2025032601595](https://openairdocs.org/sdr/SWAA2025032601595), Mar 3, 2025: FLOOR PANEL. PULLED. PASSENGER CABIN FLOOR PANEL 231UF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE<[01] REFER TO FAULT TTG8Q00YYRBQ WHERE EA 25-153-00560 WAS ADDED AS A SUBTASK.;[0
- [SDR SWAA2025032601596](https://openairdocs.org/sdr/SWAA2025032601596), Mar 3, 2025: FLOOR PANEL. PULLED. PASSENGER CABIN FLOOR PANEL 231LF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE<[01] REFER TO FAULT TTG8Q00YYRBQ WHERE EA 25-153-00560 WAS ADDED AS A SUBTASK.;[0
- [SDR SWAA2025032601597](https://openairdocs.org/sdr/SWAA2025032601597), Mar 3, 2025: FLOOR PANEL. PULLED. PASSENGER CABIN FLOOR PANEL 231KF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE<[01] REFER TO FAULT TTG8Q00YYRBQ WHERE EA 25-153-00560 WAS ADDED AS A SUBTASK.;[0
- [SDR SWAA2025032601326](https://openairdocs.org/sdr/SWAA2025032601326), Mar 2, 2025: ATTACH ANGLE. CRACKED. CENTER TANK REAR SPAR LEFT HAND LOWER ATTACH ANGLE COMMON TO STA663 VAPOR BARRIER WEB IS CRACKED AT FASTENER HOLE OUTBOARD OF LBL 6.13; WL 169<[01] REMOVED AND 
- [SDR SWAA2025032601193](https://openairdocs.org/sdr/SWAA2025032601193), Mar 1, 2025: SKIN. CRACKED. #2 TANK UPPER SKIN (INTERNAL) BETWEEN RIB 21 AND RIB 22; AFT UPPER STRINGER END IS CRACKED.<[01] CRACK ON #2 FUEL TANK (INTERNAL). AFT UPPER STRINGER; BETWEEN R
- [SDR SWAA2025032600387](https://openairdocs.org/sdr/SWAA2025032600387), Feb 27, 2025: FLOOR PANEL. PULLED. DOT A24-12 AFT CABIN FLOOR PANEL 241ADF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] REFER TO FAULT TTG8Q00YYRBQ WHERE EA 25-153-00560 WAS ADDED AS A SUBT
- [SDR SWAA2025032600477](https://openairdocs.org/sdr/SWAA2025032600477), Feb 27, 2025: FLOOR PANEL. PULLED. DOT A24-12 FORWARD CABIN FLOOR PANEL 222DF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] REFER TO FAULT TTG8Q00YYRBQ WHERE EA 25-153-00560 WAS ADDED AS A S
- [SDR SWAA2025032600043](https://openairdocs.org/sdr/SWAA2025032600043), Feb 26, 2025: SUPPORT ANGLE. CORRODED. (147-91) R1 DOOR CREASE BEAM SUPPORT ANGLE HAS CORROSION AT STA 332.1-10' TOP SIDE (MARKED)<[01] REMOVED DAMAGE IAW SRM 53-10-15-1A-2 STEP: 4.C<BR>01 - REMOVED 
- [SDR SWAA2025032600040](https://openairdocs.org/sdr/SWAA2025032600040), Feb 26, 2025: FLOOR PANEL. PULLED. (151- DOT 015) PULLED FIBERS ON TOP SIDE OF CABIN FLOOR PANEL 241DF.<[01] ALL STEPS EA 25-153-00560; WORK ACCOMPLISHED IAW B737 SRM 53-00-50-2R-1.;[02] COMPLETE
- [SDR SWAA2025032600041](https://openairdocs.org/sdr/SWAA2025032600041), Feb 26, 2025: FLOOR PANEL. PULLED. (151- DOT 016) PULLED FIBERS ON TOP SIDE OF CABIN FLOOR PANEL 242DF.<[01] REFER TO FAULT TTG8Q00YYRBQ WHERE EA 25-153-00560 WAS ADDED AS A SUBTASK.;[02] COMPLET
- [SDR SWAA2025032600045](https://openairdocs.org/sdr/SWAA2025032600045), Feb 26, 2025: FLOOR PANEL. PULLED. (151- DOT 017) PULLED FIBERS ON TOP SIDE OF CABIN FLOOR PANEL 241EF.<[01] REFER TO FAULT TTG8Q00YYRBQ WHERE EA 25-153-00560 WAS ADDED AS A SUBTASK.;[02] COMPLET
- [SDR SWAA2025032600042](https://openairdocs.org/sdr/SWAA2025032600042), Feb 26, 2025: FLOOR PANEL. PULLED. (151- DOT 018) PULLED FIBERS ON TOP SIDE OF CABIN FLOOR PANEL 242CF.<[01] REFER TO FAULT TTG8Q00YYRBQ WHERE EA 25-153-00560 WAS ADDED AS A SUBTASK.;[02] COMPLET
- [SDR SWAA2025032699636](https://openairdocs.org/sdr/SWAA2025032699636), Feb 25, 2025: PANEL. CRACKED. (147-80) L/H HORZ PANEL 333AT GAP COVER FIN HAS CRACK<[01] REMOVED AND REINSTALLED GAP COVER SEAL TO F.O.M ON PANEL 333AT; THEN THE GAP COVER FIN WAS REMOVED DU
- [SDR SWAA2025032699171](https://openairdocs.org/sdr/SWAA2025032699171), Feb 24, 2025: STRAP. CORRODED. DOT#07 A-043 AFT CARGO COMPARTMENT FLOORBOARD STRAP CORRODED AT STA 887 RBL 20 TO LBL 10 WL 156<[01] REMOVED AND REPLACED ON SHELF AFT CARGO COMPARTMENT FLOORBO
- [SDR SWAA2025032698984](https://openairdocs.org/sdr/SWAA2025032698984), Feb 24, 2025: PRESSURE DECK. CRACKED. A177-001 HORIZONTAL PRESSURE DECK WEB STA 665; RBL 43; WL 202 HAS A .50' CRACK IN WEB. VERIFIED WITH HFEC AND MARKED ENDS IN BLACK.<[01] 04 - REPAIRED HORIZONTA
- [SDR SWAA2025032699172](https://openairdocs.org/sdr/SWAA2025032699172), Feb 24, 2025: ANGLE. CORRODED. DOT#08 A-043 AFT CARGO COMPARTMENT AFT BKHD LOWER STAINTION ANGLE CORRODED AT STA 947.5 RBL 20 TO LBL 10 WL 156<[01] REMOVED CORROSION AFT CARGO COMPARTMENT AFT
- [SDR SWAA2025032699175](https://openairdocs.org/sdr/SWAA2025032699175), Feb 24, 2025: ESCAPE ROPE. FRAYED. RIGHT EMERGENCY ESCAPE HATCH ESCAPE ROPE STARTING TO FRAY<[01] REPLACED RIGHT EMERGENCY ESCAPE HATCH ESCAPE ROPE I/A/W AMM 25-61-10-400-802 STEP 6;[02] REMOVED 
- [SDR SWAA2025032699174](https://openairdocs.org/sdr/SWAA2025032699174), Feb 24, 2025: SKIN. DELAMINATED. DOT#09 A-043 LH WING; OTBD AFT FLAP INBD LOWER CORNER DELAMINATED<[01] REPAIRED LH WING OUTBD AFT FLAP INBD CORNER IAW B737 SRM 57-53-01-2R-1 AND SRM 51-70-10-2
- [SDR SWAA2025033198409](https://openairdocs.org/sdr/SWAA2025033198409), Feb 23, 2025: SUPPORT BRACKET. CRACKED. (A125-13) AFT CARGO BAY; PANEL SUPPORT BRACKET ATTACHED TO FWD BULKHEAD CRACKED; BS727; RBL04; WL162<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A0072
- [SDR SWAA2025032698397](https://openairdocs.org/sdr/SWAA2025032698397), Feb 23, 2025: THRESHOLD. CORRODED. (A125-01) AFT CARGO BAY; DOOR LOWER THRESHOLD CORRODED; BS787+8' - BS847; RBL21-RBL29; WL156<[01] REMOVED CORROSION AND EVALUATED .045 ORIG 'T' .033 REMAINING .
- [SDR SWAA2025032698398](https://openairdocs.org/sdr/SWAA2025032698398), Feb 23, 2025: SHIELD. CORRODED. (A125-02) AFT CARGO BAY; DOOR FWD SHIELD CORRODED; BS767 - BS787+8'; RBL21; WL156<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTEN
- [SDR SWAA2025032698399](https://openairdocs.org/sdr/SWAA2025032698399), Feb 23, 2025: FLOOR SUPPORT. CORRODED. (A125-03) AFT CARGO BAY; FLOOR LATERAL UNION CORRODED; BS767+5'; RBL22-LBL22; WL156<[01] REMOVED AND REPLACED ON SHELF AFT CARGO BAY; FLOOR LATERAL UNION P/N 14
- [SDR SWAA2025032698405](https://openairdocs.org/sdr/SWAA2025032698405), Feb 23, 2025: ANGLE. CORRODED. (A125-04) AFT CARGO BAY; DOOR FWD SHIELD; UNDERLYING STRUCTURE - ANGLE CORRODED; BS767 - BS787+8'; RBL22; WL156<[01] VERIFIED 100% MATERIAL LOSS FOUND OUT OF LI
- [SDR SWAA2025032698925](https://openairdocs.org/sdr/SWAA2025032698925), Feb 23, 2025: SKIN. PULLED. (147-73 ) R/H WING L/E INBOARD OF THE NACELLE STRUT SKIN HAS PULLED FASTENERS (MARKED) AFT END<[01] 04 - REPAIRED PER [SRM 57-41-01-2R-7-A01177 (REPAIR 7 - WING
- [SDR SWAA2025032698926](https://openairdocs.org/sdr/SWAA2025032698926), Feb 23, 2025: SKIN. PULLED. (147-74) R/H WING L/E SKIN INBOARD OF THE NACELLE STRUT HAS PULLED FASTENER (MARKED) AFT AND I/B END<[01] 01 - REMOVED AND REPLACED PER [SRM 57-41-01-2R-7-A0117
- [SDR SWAA2025032698406](https://openairdocs.org/sdr/SWAA2025032698406), Feb 23, 2025: ANGLE. CORRODED. (A125-07) AFT CARGO BAY; Z-ANGLE CORRODED; BS727 - BS767; RBL22; WL156<[01] BLENDED CORROSION ON AFT CARGO Z-ANGLE BS727 - BS767; RBL22 ACCOMPLISHED 10X MAG IAW
- [SDR SWAA2025032698407](https://openairdocs.org/sdr/SWAA2025032698407), Feb 23, 2025: ANGLE. CORRODED. (A125-08) AFT CARGO BAY; Z-ANGLE CORRODED; BS727 - BS847; LBL22; WL156<[01] BLENDED CORROSION ON AFT CARGO Z-ANGLE BS727 - BS847; LBL22 VERIFIED TO 100% MATERIA
- [SDR SWAA2025032698383](https://openairdocs.org/sdr/SWAA2025032698383), Feb 22, 2025: BAFFLE. CRACKED. (A204 DOT 45) FORWARD CARGO STA 500 TO 500A; STR 26L; Z-ANGLE BAFFLE PLATE IS CRACKED IN 2EA PLACES.<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A0072
- [SDR SWAA2025032698384](https://openairdocs.org/sdr/SWAA2025032698384), Feb 22, 2025: BAFFLE. CRACKED. (A204 DOT 46) FORWARD CARGO. STA 440+10; STR 26L; Z-ANGLE BAFFLE PLATE IS CRACKED AT FASTNER HOLE.<[01] REMOVED BAFFLE IAW SRM 51-40-02-0G-0 RECEIVED REPLACEMEN
- [SDR SWAA2025032698389](https://openairdocs.org/sdr/SWAA2025032698389), Feb 22, 2025: STRINGER CLIP. CRACKED. (A204 DOT 54) FORWARD CARGO. STA 500D; STR 19L; STRINGER CLIP GUSSET IS CRACKED IN RADIUS COMMON TO BULKHEAD SUPPORT.<[01] REMOVED AND REPLACED STA 500D; STR 19
- [SDR SWAA2025032698394](https://openairdocs.org/sdr/SWAA2025032698394), Feb 22, 2025: STRINGER CLIP. CRACKED. (A204 DOT 55) FORWARD CARGO; STA 500D; STR 21L; STRINGER CLIP GUSSET CRACKED COMMON TO BULKHEAD SUPPORT.<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A
- [SDR SWAA2025032698385](https://openairdocs.org/sdr/SWAA2025032698385), Feb 22, 2025: ANGLE. CORRODED. (A204 DOT 47) FORWARD CARGO STA 500A TO 500D; LBL 21; WL 159; Z-ANGLE HAS CORROSION AROUND NUTPLATE HOLES.<[01] 04 - REPAIRED PER [SRM 53-00-53-2R-5-A00957 (REP
- [SDR SWAA2024111858841](https://openairdocs.org/sdr/SWAA2024111858841), Nov 12, 2024: BATTERY PACK. FAILED. PASSENGER CABIN EMERGENCY EXIT LIGHT BATTERY PACK M1675 FAILED CAPACITY TEST.<[01] R&R PASSENGER CABIN EMERGENCY EXIT LIGHT BATTERY PACK M1675 IAW AMM 33-51-06.
- [SDR SWAA2024111858820](https://openairdocs.org/sdr/SWAA2024111858820), Nov 12, 2024: PANEL. CRACKED. -CABIN FLOORBOARD PNL BREAKS CRACKED STA. 540 BETWEEN FLOORBOARDS 231XF AND 231UF BOTH SIDES LEFT AND RIGHT.<[01] R&R CABIN FLOORBOARD PANEL BREAKS/INTERCOSTALS
- [SDR SWAA2024111858821](https://openairdocs.org/sdr/SWAA2024111858821), Nov 12, 2024: GIRT BAR. LOOSE. R1 DOOR SLIDE AFT GIRT BAR BRACKET RIVET LOOSE<[01] REMOVED AND REPLACED RIVETS FOR R1 DOOR SLIDE AFT GIRT BAR BRACKET PER SRM 51-40-02.
- [SDR SWAA2024111858822](https://openairdocs.org/sdr/SWAA2024111858822), Nov 12, 2024: GIRT BAR. OUT OF ADJUST. L1 DOOR SLIDE GIRT NOT SECURED WITH VELCRO<[01] RE-SECURED L1 DOOR SLIDE GIRT WITH VELCRO PER AMM 25-66-01.
- [SDR SWAA2024111858835](https://openairdocs.org/sdr/SWAA2024111858835), Nov 12, 2024: SEAL. CRACKED. R/H HORIZONTAL STABILIZER UPPER FORWARD SLIDING SEAL IS CRACKED 4 PARALLEL TO SLIDING SEAL LEADING EDGE.<[01] R&R RH HORIZONTAL STABILIZER FRONT UPPER SLIDING S

All 281: https://openairdocs.org/aircraft/N218WN/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

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