# N200WN: 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: 32482
- Year built: 2005
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: January 24, 2005
- Certificate issued: February 17, 2005
- Expires: September 30, 2029
- Mode S code: A19404
- 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=200WN
- Page: https://openairdocs.org/aircraft/N200WN

From the FAA registry file of October 22, 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/N200WN/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 N200WN.

## FAA accident and incident reports

None matched to N200WN.

## Service difficulty reports (337, 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 SWAA2026100237102](https://openairdocs.org/sdr/SWAA2026100237102), Sep 28, 2026: FIRE WARNING. ILLUMINATED. CARGO FIRE DISCH IN FLIGHT. VERIFIED NO LEAKS IN BOTTLE COMPARTMEN. DISCHARGE SWITCH VERIFIED OPEN. IAW WDG 26-23-11. REPLACED CARGO FIRE PANEL IAW AMM 26-00-02
- [SDR SWAA2026042791649](https://openairdocs.org/sdr/SWAA2026042791649), Apr 22, 2026: BATTERY PACK. NO TEST. FWD ENTRY LEFT EMERGENCY BATTERY PACK M1675 FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06.
- [SDR SWAA2026042791650](https://openairdocs.org/sdr/SWAA2026042791650), Apr 22, 2026: BATTERY PACK. NO TEST. AFT LEFT EMERGENCY BATTERY PACK M1673 FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06.
- [SDR SWAA2026042791648](https://openairdocs.org/sdr/SWAA2026042791648), Apr 22, 2026: BATTERY PACK. NO TEST. AFT RT EMERGENCY BATTERY PACK M1672 FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06.
- [SDR SWAA2026041387852](https://openairdocs.org/sdr/SWAA2026041387852), Apr 8, 2026: HEADS-UP DISPLAY. LOOSE. HGS COMBINER FELL DOWN ON CAPTS HEAD<[01] FOUND COMBINER TO HAVE A SOFT LATCH.SECURED COMBINER UP WITH ZIP TIE.OK TO CONT ON MEL 34-44-02.SP1 & 1 A C/W.?A/C DOW
- [SDR SWAA2025112638664](https://openairdocs.org/sdr/SWAA2025112638664), Nov 22, 2025: BUSHING. WORN. NUMBER 2 ENGINE VERY SLOW TO SPOOL UP BOTH ON TAKEOFF AND ON LANDING WHEN THRUST REV ENGAGE. PERFORMED TEST 8 ACCELERATION CHECK ON NR 2 ENGINE ACCELERATION TIM
- [SDR SWAA2025111234401](https://openairdocs.org/sdr/SWAA2025111234401), Nov 8, 2025: ENGINE. ABNORMAL. NR 2 ENGINE GREATELY LAGS #1 ENGINE IN SPOOL UP CAUSING YAW WHEN USING REVERSE IN LANDING. PERFORMED ACCEL CHECK TEST 8 IAW AMM 73-21-00 OPS CHECK GOOD .PERFORM
- [SDR SWAA2025061681776](https://openairdocs.org/sdr/SWAA2025061681776), Jun 14, 2025: SIGN. DETACHED. EXIT SIGN MID CABIN FELL OFF. INSTALLED COVER PER AMM CH 33-51-00.
- [SDR SWAA2024121774916](https://openairdocs.org/sdr/SWAA2024121774916), Dec 7, 2024: SIGN. BROKEN. AFT LOWERED CEILING EXIT SIGN ASSY BROKEN.<[01] REMOVED AND REPLACED AFT LOWERED CEILING EMERGENCY EXIT SIGN ASSY AS PER B737 AMM 33-51-01-960-802. PERFORMED IN
- [SDR SWAA2024121774308](https://openairdocs.org/sdr/SWAA2024121774308), Dec 5, 2024: SIGN. DAMAGED. G-1 GALLEY EXIT SIGN DAMAGED.<[01] REMOVED AND REPLACED G-1 GALLEY EXIT SIGN AS PER AMM 33-51-01-960-802.;[02] VERIFIED REMOVED AND REPLACED
- [SDR SWAA2024121773972](https://openairdocs.org/sdr/SWAA2024121773972), Dec 4, 2024: SCUFF PLATE. CRACKED. ACCOMPLISH WELD REPAIR OF AFT CARGO DOOR AREA AFT SCUFF PLATE<[01] RECEIVED WELDED AFT SCUFF PLATE OF AFT CARGO REF INSTALLATION TO TASK CARD TTG8Q003DUDR;[02] 
- [SDR SWAA2024121772279](https://openairdocs.org/sdr/SWAA2024121772279), Nov 27, 2024: SCUFF PLATE. CRACKED. FWD CORNER SCUFF PLATE AT AFT CARGO CRACKED<[01] RECEIVED FWD CORNER SCUFF PLATE AT AFT CARGO REF INSTALLATION TO TASK CARD TTG8Q003DUDR;[02] VERIFIED RECEIVED 
- [SDR SWAA2024121772280](https://openairdocs.org/sdr/SWAA2024121772280), Nov 27, 2024: SCUFF PLATE. CRACKED. AFT CORNER SCUFF PLATE AT AFT CARGO CRACKED<[01] RECEIVED AFT CORNER SCUFF PLATE AT AFT CARGO REF INSTALLATION TO TASK CARD TTG8Q003DUDR;[02] VERIFIED STEP 1
- [SDR SWAA2024121772281](https://openairdocs.org/sdr/SWAA2024121772281), Nov 27, 2024: SCUFF PLATE. CRACKED. AFT CORNER SCUFF PLATE AT FWD CARGO CRACKED<[01] RECEIVED AFT CORNER SCUFF PLATE AT FWD CARGO REF INSTALLATION TO TASK CARD TTG8Q003DUEY;[02] VERIFIED STEP 1
- [SDR SWAA2024121769906](https://openairdocs.org/sdr/SWAA2024121769906), Nov 20, 2024: GALLEY. CORRODED. G-4 GALLEY COUNTERTOP HAS CORROSION.<[01] PART TRANSACTION ONLY; G-4 GALLEY INSTALLATION REF TASK CARD FOR JOB ACCOMPLISHMENT TTG8Q003E0PW;[02] VERIFIED PART TR
- [SDR SWAA2024121760342](https://openairdocs.org/sdr/SWAA2024121760342), Nov 15, 2024: FAIRING. ELONGATED. FUSELAGE CENTER LOWER AFT FAIRING 194E HAS SEVERAL OVERSIZED AND ELONGATED HOLES.<[01] INSTALLED A PERMANENT REPAIR TO DAMAGE FASTENERS HOLES AS MARKED ON LOWER
- [SDR SWAA2024121759717](https://openairdocs.org/sdr/SWAA2024121759717), Nov 13, 2024: STRUCTURE. ELONGATED. AFT CABIN WET AREA R-2 DOOR LOWER SILL INNER SUPPORT O/B HAS 3EA ELONGATED HOLES MKD DOTS<[01] SUMMARY=INSTALLED EWIS PROTECTION DURING MAINTENANCE AS PER REF B
- [SDR SWAA2024121759705](https://openairdocs.org/sdr/SWAA2024121759705), Nov 13, 2024: SUPPORT. CRACKED. MAIN CABIN CENTER SECTION FLOOR SUPPORT BREAK CRACKED @ FWD FACE STA 540 LBL-1<[01] REMOVED AND REPLACED FLOOR SUPPORT BREAK AT MAIN CABIN CENTER SECTION STA 54
- [SDR SWAA2024121759706](https://openairdocs.org/sdr/SWAA2024121759706), Nov 13, 2024: SUPPORT. CRACKED. MAIN CABIN CENTER SECTION FLOOR SUPPORT BREAK CRACKED @ FWD FACE STA 540 RBL-1 MKD DOT<[01] REMOVED AND REPLACED FLOOR SUPPORT BREAK AT MAIN CABIN CENTER SECTIO
- [SDR SWAA2024121759025](https://openairdocs.org/sdr/SWAA2024121759025), Nov 12, 2024: SCUFF PLATE. CRACKED. FWD CABIN GALLEY R-1 DOOR FUS CUTOUT LOWER SILL SCUFF PLATE EDGE CRACKED 2EA PLACES<[01] SUMMARY=LOCATED DRILLED AND COUNTERSANK NEW SCUFF PLATE AS PER B 737 SR
- [SDR SWAA2024121759026](https://openairdocs.org/sdr/SWAA2024121759026), Nov 12, 2024: SUPPORT ANGLE. CORRODED. FWD CABIN R-1 DOOR CUTOUT LOWER SILL SCUFF PLATE SUPPORT ANGLE FWD SPOTS SURFACE CORR MKD DOTS<[01] REMOVED CORROSION AT FWD CABIN R-1 DOOR CUTOUT LOWER SILL SC
- [SDR SWAA2024121758500](https://openairdocs.org/sdr/SWAA2024121758500), Nov 11, 2024: STRINGER. CRACKED. FWD MAIN CABIN WET AREA SIDEWALL S-16L CRACKED BETWEEN STA 294 & 303.9<[01] ACCOMPLISHED REPAIR PER EA 24-153-03228 REF: TTG8Q00X5QPQ<BR>& TTG8Q00XDWZU;[02] VER
- [SDR SWAA2024121758752](https://openairdocs.org/sdr/SWAA2024121758752), Nov 11, 2024: STIFFENER. CRACKED. STIFFENER CRACKED AT STA 663; RBL 25; WL 148<[01] SUMMARY :REMOVED AND REPLACED NEW STIFFENER ON STA 663 ;RBL 25 WL 148 AS PER B/737 SRM 51-40-02-0G-0 AND DW 11
- [SDR SWAA2024121758750](https://openairdocs.org/sdr/SWAA2024121758750), Nov 11, 2024: GUIDE ARM. CORRODED. R1 DOOR GUIDE ARM CORRODED<[01] REMOVED AND REPLACED R1 DOOR GUIDE ARM PER B737 AMM 52-41-21-400-801-NG FINAL INSTALLATION AND ADJUSTMENT REF TTG8Q00X0R56<BR>TO
- [SDR SWAA2024101447698](https://openairdocs.org/sdr/SWAA2024101447698), Oct 12, 2024: TRANSMITTER. FAULTY. FLAPS WOULD NOT EXTEND PAST 5 WITH 15 SELECTED. FLAPS MOVED TO 15 MANUALLY NO NEEDLE SPLIT NOTED<[01] TROUBLESHOT PER FIM 27-51 TASK 801 & 820; FSEU BITE SHOWS 
- [SDR SWAA2024080221719](https://openairdocs.org/sdr/SWAA2024080221719), Aug 1, 2024: SLIDE. OUT OF ADJUST. AFT SLIDE CAPT SIDE NOT PACKED CORRECTLY REF: BAR CODE ID TTG8Q00UYJU5<[01] RE-PACKED CAPTAINS SIDE AFT ESCAPE SLIDE IAW MT 725-61-06.
- [SDR SWAA2024080221387](https://openairdocs.org/sdr/SWAA2024080221387), Aug 1, 2024: SLIDE. OUT OF ADJUST. AFT SLIDE CAPT SIDE NOT PACKED CORRECTLY<[01] RE-PACKED CAPTAINS SIDE AFT ESCAPE SLIDE IAW AMM 25-66-01. OK FOR SERVICE.
- [SDR SWAA2024072516672](https://openairdocs.org/sdr/SWAA2024072516672), Jul 24, 2024: SEAT. OUT OF ADJUST. CAPTAINS SIDE EXIT ROW 12A SEAT STAYS RECLINED.<[01] ADJUSTED PAX SEAT IN 12A PER MM 25-22-00 OPS CHECK GOOD;[02] FAULT RAISED IN ERROR.
- [SDR SWAA2024072214652](https://openairdocs.org/sdr/SWAA2024072214652), Jul 19, 2024: BOTTLE. OUT OF LIMITS. LEFT FWD DOOR ESCAPE SLIDE PRESSURE OUT OF LIMITS<[01] 01 - REMOVED AND REPLACED FORWARD ENTRY ESCAPE SLIDE PER [AMM 25-66-01-401-NG (DOOR-MOUNTED ESCAPE SYSTEM
- [SDR SWAA2024061902297](https://openairdocs.org/sdr/SWAA2024061902297), Jun 16, 2024: FIRE LOOP. INOPERATIVE. #1 ENG B FIRE LOOP INOP #1 ENG B FIRE LOOP INOP 16-JUN-2024 06:50 UTC R&R ENGINE AND APU FIRE DETECTION MODULE IAW AMM 25-10-01 OPS CHECK GOOD.<[01] COULD NOT D
- [SDR SWAA2024022957306](https://openairdocs.org/sdr/SWAA2024022957306), Feb 29, 2024: CHARGER. INOPERATIVE. R/H EMERGENCY EXIT HATCH ( EXIT ) LIGHT INOP<[01] REPLACED BATTERY CHARGER AND EXIT SIGN ASSY PER AMM 33-51-01
- [SDR SWAA2023080885865](https://openairdocs.org/sdr/SWAA2023080885865), Aug 4, 2023: GIRT BAR. OUT OF ADJUST. R-1 SLIDE PACK GRIT BAR RIGHT. CLIP LOOSE<[01] ADJUSTED R1 SLIDE GRIT BAR RH CLIP PER AMM SIP. NO FURTHER DEFECTS NOTED AT THIS TIME
- [SDR SWAA2023071778010](https://openairdocs.org/sdr/SWAA2023071778010), Jul 13, 2023: LIGHT. INOPERATIVE. PASSENGER CABIN: RIGHT OVER WING EXIT; LIGHT IS INOPERABLE. PASSENGER CABIN: RIGHT OVER WING EXIT LIGHT IS INOPERABLE.<[01] RELAMPED EXIT LIGHT PER AMM 33-51-01
- [SDR SWAA2023071778019](https://openairdocs.org/sdr/SWAA2023071778019), Jul 13, 2023: LIGHT. DELAMINATED. PASSENGER CABIN: SECTION OF PHOTO ILLUMINATED STRIP IS DELAMINATED NEXT TO THE AFT RIGHT WINDSCREEN.<[01] REMOVED AND REPLACED PHOTO STRIP PER AMM 33-51-15;[02]
- [SDR SWAA2023041124818](https://openairdocs.org/sdr/SWAA2023041124818), Apr 7, 2023: SLIDE. OUT OF ADJUST. L2 SLIDE OUTSIDE OF CONTAINER<[01] RESECURED SLIDE CONTAINER COVER IAW AMM 25-66-01
- [SDR SWAA2022113076721](https://openairdocs.org/sdr/SWAA2022113076721), Nov 30, 2022: POWER SUPPLY. INOPERATIVE. EMERGENCY LIGHT AFT OF LEFT WING INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY IAW AMM 33-51-06. OPS CHECKED GOOD.
- [SDR SWAA2022112173210](https://openairdocs.org/sdr/SWAA2022112173210), Nov 19, 2022: LAMP. INOPERATIVE. BURNED EMERGENCY LIGHT EXTERNAL AFT LT 2022-585774 / [01] REPLACED LAMP ON EMERGENCY LIGHT EXTERNAL AFT LT IAW B737-700 AMM 33-51-04-960-801 TEST OK.;[02] REPLA
- [SDR SWAA2022112273209](https://openairdocs.org/sdr/SWAA2022112273209), Nov 18, 2022: LAMP. BURNED OUT. BURNED OUT LIGHT EMERGENCY AFT RT OVER GALLEY. REPLACED THE LAMPS IAW AMM 33-51-01-960-801.
- [SDR SWAA2022112264981](https://openairdocs.org/sdr/SWAA2022112264981), Oct 27, 2022: BEAM. CRACKED. FOUND 2 E/A CRACK O N INTERNAL BEAM 2022-585731 / [01] REMOVED AND REPLACED SLAT 7 DUE TO 2 E/A CRACK FOUND ON INTERNAL BEAM IAW B737-700 AMM 27-81-21-000-801 A
- [SDR SWAA2022112264432](https://openairdocs.org/sdr/SWAA2022112264432), Oct 25, 2022: FLOOR SUPPORT. CRACKED. CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS344 TO BS360 LBL12 WL 208.1 FWD GALLEY AND LAV. REPLACED FLOOR SUPPORT IAW SRM 51-40-02 AND DWG 141A54
- [SDR SWAA2022112163655](https://openairdocs.org/sdr/SWAA2022112163655), Oct 24, 2022: PLATE. CORRODED. CORROSION ON PLATE LOCATED BETWEEN BS 787 AND BS 807 S- 25R AND WL 156 AFT CARGO COMPARTMENT 2022-585714 / [01] REPLACED PLATE LOCATED BETWEEN BS 787 AND BS 807
- [SDR SWAA2022112263650](https://openairdocs.org/sdr/SWAA2022112263650), Oct 23, 2022: SUPPORT ANGLE. CORRODED. CORROSION SUPPORT ANGLE, BS 847, LBL 19, AFT CARGO COMPARTMENT. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02 ITEM 9, AND 51-40-02.
- [SDR SWAA2022112263651](https://openairdocs.org/sdr/SWAA2022112263651), Oct 23, 2022: SUPPORT ANGLE. CORRODED. CORRODED SUPPORT ANGLE, BS 867, LBL 10, AFT CARGO COMPARTMENT. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, AND 51-40-02.
- [SDR SWAA2022112263322](https://openairdocs.org/sdr/SWAA2022112263322), Oct 22, 2022: FLOORBEAM. CORRODED. CORROSION FLOORBEAM, BS 986.5, RBL 39.5, WL 208.1.
- [SDR SWAA2022112263323](https://openairdocs.org/sdr/SWAA2022112263323), Oct 22, 2022: FLOORBEAM. CORRODED. CORROSION FLOORBEAM, BS 986.5, RBL 35.5, WL 208.1.
- [SDR SWAA2022112263326](https://openairdocs.org/sdr/SWAA2022112263326), Oct 22, 2022: FLOORBEAM. CORRODED. CORROSION FLOORBEAM, BS 986.5, LBL38, WL 208.1.
- [SDR SWAA2022112263324](https://openairdocs.org/sdr/SWAA2022112263324), Oct 22, 2022: FLOORBEAM. CORRODED. CORROSION FLOORBEAM, BS 986.5, LBL 41, WL 208.1. REPAIRED IAW EA 22-153-03296-WIP1 AND EA 22-153-03296.
- [SDR SWAA2022112263321](https://openairdocs.org/sdr/SWAA2022112263321), Oct 22, 2022: FLOORBEAM. CORRODED. CORROSION FLOORBEAM, BS 986.5, RBL 43, WL 208.1. REPAIRED IAW EA 22-153-03281 WIP1 AND EA 22-153-03281.
- [SDR SWAA2022112263325](https://openairdocs.org/sdr/SWAA2022112263325), Oct 22, 2022: FLOORBEAM. CORRODED. CORRODED FLOORBEAM BS 312 RBL20 WL208.1.
- [SDR SWAA2022112262957](https://openairdocs.org/sdr/SWAA2022112262957), Oct 21, 2022: STUB FRAME. CRACKED. CRACKED STUB FRAME LOCATED BS294.5 RBL55 WL209 . REPLACED THE STUB FRAME IAW SRM 51-10-02 ITEM 9 AND DWG-141A8370 REV D.

All 337: https://openairdocs.org/aircraft/N200WN/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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