# N244WN: 2006 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 CFM56-7B24 series](https://openairdocs.org/engine/cfm-international-cfm56-7b24-series) (registry code 13044)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (The Boeing Company) (OpenAirDocs)
- Serial number: 34864
- Year built: 2006
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 24, 2006
- Certificate issued: August 3, 2006
- Expires: February 29, 2028
- Mode S code: A240DC
- 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=244WN
- Page: https://openairdocs.org/aircraft/N244WN

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 CFM56-7B24 model are included.

## ADs that may apply (OpenAirDocs): 19 in force

### Matched by airframe (Boeing 737-7H4)

None in force.

### Matched by engine (CFM International CFM56-7B24 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 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 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 2010-01-05](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 2009-11-02](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 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 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 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 2001-02-12](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 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

### 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 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

## Information bulletins (advisory) (1 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-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 N244WN.

## FAA accident and incident reports

None matched to N244WN.

## Service difficulty reports (297, 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 SWAA2026072756058](https://openairdocs.org/sdr/SWAA2026072756058), Jul 22, 2026: LAMP. INOPERATIVE. COCKPIT DOME EMERGENCY EXIT LIGHT IS INOPERATIVE. REPLACED THE LAMPS AND PERFORMED GOOD. INSTALLATION TEST IAW AMM 33-14-00-960-804.
- [SDR SWAA2026043093145](https://openairdocs.org/sdr/SWAA2026043093145), Apr 26, 2026: LIGHT. INOPERATIVE. PAX CABIN SEAT ROW 15 FED SIDEWALL MIDDLE EMERGENCY LIGHT IS INOPERATIVE. REPLACED THE LAMP PAX CABIN SEAT ROW 15 FED SIDEWALL MIDDLE EMERGENCY LIGHT IAW AMM 33
- [SDR SWAA2026043093144](https://openairdocs.org/sdr/SWAA2026043093144), Apr 26, 2026: HANDLE. LOOSE. PAX CABIN FWD ENTRY DOOR ASSISTANT HANDLES LOOSE (2 EA). TIGHTENED THE TWO DOOR ASSISTANT HANDLES IAW AMM 25-21-31-420-802, STEP 3.B, ITEM (6).
- [SDR SWAA2026043093146](https://openairdocs.org/sdr/SWAA2026043093146), Apr 26, 2026: HANDLE. LOOSE. PAX CABIN AFT RIGHT DOOR ASSISTANT HANDLE LOOSE. TIGHTENED THE DOOR ASSISTANT HANDLE IAW AMM 25-21-25-420-801, STEP 3.B, ITEM (5).
- [SDR SWAA2026043086229](https://openairdocs.org/sdr/SWAA2026043086229), Apr 4, 2026: SHIELD. CORRODED. CORROSION ON SHIELD WEB LOCATED BTW BS 767 - 794.3, WL 156, AND RBL 21 IN THE AFT CARGO BAY. REPLACED SHIELD WEB IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG
- [SDR SWAA2026043086226](https://openairdocs.org/sdr/SWAA2026043086226), Apr 4, 2026: SUPPORT. CORRODED. CORRODED SUPPORT ZEE, BS 727C - 767, WL 156, RBL 21 IN THE AFT CARGO BAY. REPLACED THE SUPPORT ZEE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 146A7500, SHE
- [SDR SWAA2026043086230](https://openairdocs.org/sdr/SWAA2026043086230), Apr 4, 2026: SUPPORT ANGLE. CORRODED. CORRODED SUPPORT ANGLE, BTW BS 767 - 787, WL 156, RBL21, IN THE AFT CARGO BAY. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, SRM 51-40-02, 51-10-02, ITEM 9, AND 
- [SDR SWAA2026043086221](https://openairdocs.org/sdr/SWAA2026043086221), Apr 3, 2026: STRINGER. CRACKED. CRACKED STRINGER 23L, BS 540 IN THE FWD CARGO BAY. REPLACED REPAIR PARTS [7] STRINGER SECTION (1E/A); [2] CHANNEL (1E/A); [3] ANGLE (2E/A) AND FASTENERS LOC. BT
- [SDR SWAA2026043086223](https://openairdocs.org/sdr/SWAA2026043086223), Apr 3, 2026: STRINGER. CRACKED. CRACKED STRINGER 27L, BS 540 IN THE FWD CARGO BAY. REPLACED REPAIR PARTS [7] STRINGER SECTION (1E/A); [2] CHANNEL (1E/A) AND [3] ANGLE (2E/A) ON STRINGER 27L LO
- [SDR SWAA2026043086222](https://openairdocs.org/sdr/SWAA2026043086222), Apr 3, 2026: STRINGER. CRACKED. CRACKED STRINGER 26L, BS 540, IN THE FWD CARGO BAY. REPLACED THE STRINGER WITH REPAIR PARTS [7] STRINGER SECTION, [2] CHANNELS, [2] ANGLES IAW SRM 53-00-03-2R-1
- [SDR SWAA2026043086220](https://openairdocs.org/sdr/SWAA2026043086220), Apr 3, 2026: WEB. CORRODED. CORRODED UPPER SILL WEB, CUTOUT DOOR BS 460 + 6 INCHES, WL 195, RBL 68 IN THE FWD CARGO BAY. REPLACED UPPER SILL WEB CUTOUT DOOR IAW SRM 51-10-02, ITEM 9, SRM 5
- [SDR SWAA2026043086225](https://openairdocs.org/sdr/SWAA2026043086225), Apr 3, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 907 + 7 INCHES, RBL 14 IN THE AFT CARGO BAY. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 147A7221, SHEET 28, REV-.
- [SDR SWAA2026043086224](https://openairdocs.org/sdr/SWAA2026043086224), Apr 3, 2026: FITTING. CRACKED. CRACKED FITTING, FLOOR STRUCTURE BS 947, LBL 10 IN THE AFT CARGO BAY. REPLACED THE FITTING IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 149A8103, SHEET 7, RE
- [SDR SWAA2026042986227](https://openairdocs.org/sdr/SWAA2026042986227), Apr 3, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE FLOOR STRUCTURE BS 867, LBL 11 IN THE AFT CARGO BAY. REPLACED SUPPORT ANGLE LOCATED FLOOR STRUCTURE IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G
- [SDR SWAA2026043085948](https://openairdocs.org/sdr/SWAA2026043085948), Apr 2, 2026: SUPPORT BRACKET. CRACKED. CRACKED SUPPORT BRACKET ON THE PNEUMATIC DUCT, BS 540, RBL 6 IN THE AIR CONDITIONING BAY. REPLACED THE SUPPORT BRACKET IAW SRM 51-10-02, ITEM 9, AND SRM 51-40-0
- [SDR SWAA2026043085949](https://openairdocs.org/sdr/SWAA2026043085949), Apr 2, 2026: SUPPORT BRACKET. CRACKED. CRACKED SUPPORT BRACKET, ON PNEUMATIC DUCT, BS 540, LBL 6 IN THE AIR CONDITIONING BAY. REPLACED THE SUPPORT BRACKET IAW SRM 51-10-02, ITEM 9, AND SRM 51-40-02.
- [SDR SWAA2026043084628](https://openairdocs.org/sdr/SWAA2026043084628), Mar 30, 2026: SCUFF PLATE. CRACKED. CRACKED SCUFF PLATE OF SERVICE DOOR IN THE FWD GALLEY AREA. REPAIRED THE SCUFF PLATE IAW SRM 53-10-15-2R-2, REPAIR 2, AND BAC 5975.
- [SDR SWAA2026043084387](https://openairdocs.org/sdr/SWAA2026043084387), Mar 29, 2026: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON ACCESS PANEL 661BB AT RT WING. REPAIRED ACCESS PANEL 661BB AT RT WING IAW SRM 51-70-04-2R-10 REPAIR 10. REFER TO INDIVIDUAL SIGNOFFS BELOW. R
- [SDR SWAA2026043083952](https://openairdocs.org/sdr/SWAA2026043083952), Mar 27, 2026: STRINGER. CRACKED. CRACKED STRINGER 8 INTERNAL AREA FUEL TANK LOC. BTW RIB 19 AND RIB 20 UPPER SKIN LOWER SURFACE AFT AREA AT RT WING. REPAIRED STRINGER 8 INTERNAL AREA FUEL TANK 
- [SDR SWAA2026043083953](https://openairdocs.org/sdr/SWAA2026043083953), Mar 27, 2026: STRINGER CLIP. CRACKED. CRACKED STRINGER CLIP BS 277, STR 10R IN THE PASSENGER CABIN. REPLACED TIE CLIP IAW SRM 51-10-02 ITEM 9, SRM 51-40-02, DWG 141A1110, SHEET 18, REV -, AND DWG 14
- [SDR SWAA2026043083752](https://openairdocs.org/sdr/SWAA2026043083752), Mar 26, 2026: ANGLE. CRACKED. CRACKED ANGLE, INTERNAL STRUCTURE FRONT SPAR SUPPORT FITTING RT AREA APPROX AT BS 1016 IN THE VERTICAL STAB. REPLACED THE ANGLE IAW SRM 51-40-02, AND DWG 176A31
- [SDR SWAA2026043083756](https://openairdocs.org/sdr/SWAA2026043083756), Mar 26, 2026: CROSSBEAM. CRACKED. CRACKED FLOOR STRUCTURE BRAKE PANEL BS 540 AND LBL 1 IN PASSENGER CABIN. REPLACED BREAK PANEL LOCATED BS 540 AND LBL 1 IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, A
- [SDR SWAA2026043083753](https://openairdocs.org/sdr/SWAA2026043083753), Mar 26, 2026: CROSSBEAM. CRACKED. CRACK FLOOR STRUCTURE BRAKE PANEL BS 540 AND RBL 1 AT PASSENGER CABIN. REPLACED BREAK PANEL LOCATED BS 540, RBL 1 IAW SRM 51-40-02; SRM 51-10-02, ITEM 9, AND DW
- [SDR SWAA2026043083754](https://openairdocs.org/sdr/SWAA2026043083754), Mar 26, 2026: FLOOR SUPPORT. CRACKED. CRACKED FLOOR ANGLE, BS 695, RBL 24.75, WL 204. REPLACED FLOOR ANGLE IAW SRM 51-40-02, AND DWG 273A9110, SHEET 6, REV A.
- [SDR SWAA2026043083755](https://openairdocs.org/sdr/SWAA2026043083755), Mar 26, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BS 695, BL 0, WL 208.1. REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM 51-40-02, AND DWG 273A9110, SHEET 6, REV A.
- [SDR SWAA2026043083475](https://openairdocs.org/sdr/SWAA2026043083475), Mar 26, 2026: RIB. CRACKED. CRACKED RIB LOCATED LE HSS 95.96 ACCESS PANEL 341B AT RT HORIZONTAL STAB. REPLACED RIB LOCATED LE HSS 95.96 ACCESS PANEL 341B IAW SRM 51-10-02, ITEM 9, AND DWG 
- [SDR SWAA2026043083161](https://openairdocs.org/sdr/SWAA2026043083161), Mar 25, 2026: DRAIN MAST. CRACKED. CRACKED ACCESS PANEL 194FL BODY FAIRING, APU SHROUD AND HYDRAULIC DRAIN. REPLACED APU SHROUD AND HYDRAULIC DRAIN MAST FUSELAGE EXTERIOR ON ACCESS PANEL 194FL IA
- [SDR SWAA2026043082774](https://openairdocs.org/sdr/SWAA2026043082774), Mar 24, 2026: BEAR STRAP. CRACKED. CRACKED R1 DOOR BEAR STRAP; BTWN BS 291.5 - 298, S8-9R. PERFORMED PERMANENT REPAIR ON FUSELAGE BEAR STRAP BS 277 - 320, S6-11R IAW SRM 53-10-01-2R-6, REPAIR 6, 
- [SDR SWAA2026043082955](https://openairdocs.org/sdr/SWAA2026043082955), Mar 24, 2026: INTERCOSTAL. CRACKED. CRACKED INTERCOSTAL, BTWN BS 927 - 947.5, STR 25R IN THE AFT CARGO BAY. REPLACED INTERCOSTAL AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 147A750
- [SDR SWAA2026043082956](https://openairdocs.org/sdr/SWAA2026043082956), Mar 24, 2026: LIGHT. DETERIORATED. TEN DETERIORATED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN. REPLACED PHOTOLUMINESCENT STRIP IAW AMM 33-51-15-400-802.
- [SDR SWAA2026043082783](https://openairdocs.org/sdr/SWAA2026043082783), Mar 24, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 440, STR 26L IN THE FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-40-02, AND DWG 143A7505, SHEET 82, REV-.
- [SDR SWAA2026043082789](https://openairdocs.org/sdr/SWAA2026043082789), Mar 24, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500C, STR 26R IN THE FWD CARGO BAY. REPLACED ANGLE IAW SRM 51-40-02, AND DWG 143A7505, SHEET 82, REV-.
- [SDR SWAA2026043082775](https://openairdocs.org/sdr/SWAA2026043082775), Mar 24, 2026: STUB FRAME. CRACKED. CRACKED R1 DOOR STUB FRAME, BETWEEN BS 291.5 - 303, S7 - 9R, REPLACED THE STUB FRAME IAW SRM 53-10-01-2R-6, REPAIR 6, PARAGRAPH 4.N, & DWG 141A8370, SHEET 10, R
- [SDR SWAA2026043082776](https://openairdocs.org/sdr/SWAA2026043082776), Mar 24, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 400, STR 26L IN THE FWD CARGO BAY. REPLACED THE ANGLE, IAW SRM 51-40-02, AND DWG 143A7505, SHEET 81, REV-.
- [SDR SWAA2026043082785](https://openairdocs.org/sdr/SWAA2026043082785), Mar 24, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500C, STR 26L IN THE FWD CARGO BAY. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02, AND DWG 143A7505, SHEET 82, REV-.
- [SDR SWAA2026043082787](https://openairdocs.org/sdr/SWAA2026043082787), Mar 24, 2026: GUSSET. CRACKED. CRACKED GUSSET, BS 500D, STR 19R IN THE FWD CARGO BAY. REPLACED THE GUSSET IAW SRM 51-40-02, AND DWG 143A7902, SHEET 174, REV -.
- [SDR SWAA2026043082784](https://openairdocs.org/sdr/SWAA2026043082784), Mar 24, 2026: GUSSET. CRACKED. CRACKED GUSSET, BS 500D, STR 19L IN THE FWD CARGO BAY. REPLACED THE GUSSET IAW SRM 51-40-02, AND DWG 143A7902, SHEET 174, REV -.
- [SDR SWAA2026043082788](https://openairdocs.org/sdr/SWAA2026043082788), Mar 24, 2026: GUSSET. CRACKED. CRACKED GUSSET, BS 500D, STR 21R FWD CARGO BAY. REPLACED GUSSET AND FASTENERS LOCATED BS 500D, STR 21R IAW SRM 51-40-02, 51-10-02, ITEM 9, AND DWG 143A7902, SHE
- [SDR SWAA2026043094258](https://openairdocs.org/sdr/SWAA2026043094258), Mar 24, 2026: GUSSET. CRACKED. CRACKED GUSSET BS 500D AND STR 21R FWD CARGO BAY. REPLACED GUSSET AND FASTENERS LOCATED BS 500D AND STR 21R FWD CARGO BAY IAW SRM 51-40-02; 51-10-02, ITEM 9, & 
- [SDR SWAA2026043082085](https://openairdocs.org/sdr/SWAA2026043082085), Mar 22, 2026: SCUFF PLATE. CRACKED. CRACKED FWD CORNER SCUFF PLATE IN THE AFT CARGO BAY. REPAIRED FWD CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, AND BAC 5975.
- [SDR SWAA2026043082086](https://openairdocs.org/sdr/SWAA2026043082086), Mar 22, 2026: SCUFF PLATE. CRACKED. CRACKED CORNER SCUFF PLATE IN THE AFT CARGO BAY. REPAIRED AFT CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, AND BAC 5975.
- [SDR SWAA2025122254275](https://openairdocs.org/sdr/SWAA2025122254275), Dec 19, 2025: GIRT BAR. FOD. AFT ENTRY ESCAPE SLIDE GIRT BAR WOULD NOT ENGAGE IN SLIDE BRACKET. DEBRIS WAS BLOCKING BRACKET FROM ENGAGING THE BAR. REMOVED DEBRI AND PERFORMED INSTALL TEST A
- [SDR SWAA2025110330712](https://openairdocs.org/sdr/SWAA2025110330712), Oct 31, 2025: SLIDE. OUT OF ADJUST. R1 SLIDE STICKING OUT. ADJUSTED THE R1 SLIDE IAW AMM 25-66-00.
- [SDR SWAA2025101424004](https://openairdocs.org/sdr/SWAA2025101424004), Oct 12, 2025: SLIDE. DETACHED. R1 SLIDE PARTLY DETACH FROM HOUSING. RE ATTACHED R1 SLIDE BAYONET TO DOOR HOUSING. IAW AMM 25-66-01
- [SDR SWAA2025022699016](https://openairdocs.org/sdr/SWAA2025022699016), Feb 24, 2025: BATTERY PACK. INOPERATIVE. L/H OVERWING EMERGENCY EXIT LIGHT BATTERY PACK INOP<[01] REPLACED L/H OVERWING EMERGENCY LIGHT BATTERY PACK M1668 IAW AMM 33-51-06. OP CHECK GOOD.
- [SDR SWAA2025021896632](https://openairdocs.org/sdr/SWAA2025021896632), Feb 16, 2025: CHARGER. INOPERATIVE. FWD RH SECTION OF CABIN EMERGENCY EXIT LIGHTS INOP<[01] REPLACED M1674 EMERGENCY CHARGER ASSEMBLY AND BATTERY PACK REF AMM 33-51-06. OPS CHECK GOOD.
- [SDR SWAA2025021897345](https://openairdocs.org/sdr/SWAA2025021897345), Feb 16, 2025: BATTERY PACK. INOPERATIVE. FWD RH SECTION OF CABIN EMERGENCY EXIT LIGHTS INOP<[01] REPLACED M1674 EMERGENCY CHARGER ASSEMBLY AND BATTERY PACK REF AMM 33-51-06. OPS CHECK GOOD.
- [SDR SWAA2024122780811](https://openairdocs.org/sdr/SWAA2024122780811), Dec 26, 2024: GIRT BAR. CRACKED. AFT ENTRY DOOR GIRT BAR PLASTIC CLIP CRACKED.<[01] R & R AFT ENTRY DOOR GIRT BAR PLASTIC CLIP PER MM 25-66-01
- [SDR SWAA2024122780810](https://openairdocs.org/sdr/SWAA2024122780810), Dec 26, 2024: GIRT BAR. CRACKED. FWD ENTRY DOOR GIRT BAR PLASTIC CLIP CRACKED.<[01] R & R FWD ENTRY DOOR GIRT BAR PLASTIC CLIP PER MM 25-66-01
- [SDR SWAA2024122780812](https://openairdocs.org/sdr/SWAA2024122780812), Dec 26, 2024: GIRT BAR. CRACKED. AFT SERVICE DOOR GIRT BAR PLASTIC CLIP CRACKED.<[01] R & R AFT SERVICE DOOR GIRT BAR PLASTIC CLIP PER MM 25-66-01

All 297: https://openairdocs.org/aircraft/N244WN/reports.md

## STCs that may be installed (OpenAirDocs) (32)

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 CFM56-7B24 series)

- [STC SE04840NY](https://openairdocs.org/stc/SE04840NY): Installation of HarcoSemco Exhaust Gas Temperature (EGT) Electrical Harnesses in CFM56-7 engine. Kilroy Aviation LLC
- [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

## Related

- Other Boeing 737-7H4 aircraft: https://openairdocs.org/model/boeing-737-7h4/aircraft.md
- The CFM International CFM56-7B24 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b24-series.md

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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.
