# N263WN: 2007 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: 32520
- Year built: 2007
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: January 17, 2007
- Certificate issued: February 22, 2007
- Expires: September 30, 2029
- Mode S code: A28C23
- 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=263WN
- Page: https://openairdocs.org/aircraft/N263WN

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 CFM56-7B24 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 (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA15CA025](https://openairdocs.org/ntsb/DCA15CA025), Nov 21, 2014: Boeing 737 7H4 (N263WN), Dallas, TX, minor damage. Probable cause: N263WN captain's failure to maintain a safe clearance from the parked N8314L resulting in a ground collision.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Accident 20141120021422A](https://openairdocs.org/incident/20141120021422A), Nov 20, 2014: Boeing 737-7H4 (N263WN), Dallas, TX, Substantial damage. Preliminary report. Additional information is required At approximately 2000C on November 20, 2014, at Dallas Love Field (dal), N263WN was taxiing from gate 3…

## Service difficulty reports (288, 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 SWAA2026072007194](https://openairdocs.org/sdr/SWAA2026072007194), Jul 14, 2026: LAMP. INOPERATIVE. EXTERNAL EMERGENCY LIGHT RIGHT SIDE FWD OF AFT CARGO DOO INOPERATIVE. REMOVED AND REPLACED EXTERNAL EMERGENCY LIGHT LAMP AT RIGHT SIDE FWD OF AFT CARGO DOOR IAW
- [SDR SWAA2026072045852](https://openairdocs.org/sdr/SWAA2026072045852), Jul 14, 2026: LIGHT. INOPERATIVE. LEFT SIDE CABIN AFT MOST OVERHEAD BIN EMERGENCY LIGHT IN OPERATIVE. REMOVED AND REPLACED IAW AMM 33-51-01-201-NG.
- [SDR SWAA2026063016096](https://openairdocs.org/sdr/SWAA2026063016096), Jun 26, 2026: WEB. CRACKED. NR 1 ENGINE INBD COWL WEB CRACKED AFT OF OIL SERVICE DOOR. REMOVED AND REPLACED NR 1 ENGINE INBD COWL WEB AFT OF OIL SERVICE DOOR PER SRM 51-40-02. REMOVED AND 
- [SDR SWAA2025121043821](https://openairdocs.org/sdr/SWAA2025121043821), Dec 7, 2025: MEGAPHONE. NO DISCREPANCY. MEGAPHONE IN AFT GALLEY INOPERATIVE. MEGAPHONE OPS CHECK GOOD IAW AMM 25-64-00
- [SDR SWAA2025102727936](https://openairdocs.org/sdr/SWAA2025102727936), Oct 23, 2025: SENSOR. FAULTY. LE FLAPS TRANSIT AT FLAPS 10 AND BEYOND. ALL LE DEVICES APPEARED EXTENDED; NO ASYMMETRY WAS DETECTED NOR ANY SKEW. PERFORMED BYTE CHECK, FOUND FAULT 27-81215. S
- [SDR SWAA2025040721822](https://openairdocs.org/sdr/SWAA2025040721822), Apr 4, 2025: TRANSMITTER. MALFUNCTIONED. ON APPROACH FLAP WOULD NOT GO BEYOND FLAPS 5 THE LEFT FLAP POSITION TRANSMITTER LAGGED THEN ASYMMETRY BYPASS INITIATED BUT LOOKS LIKE IT MIRROR UP AFTER. I WOUL
- [SDR SWAA2025033119766](https://openairdocs.org/sdr/SWAA2025033119766), Mar 30, 2025: CONNECTOR. LOOSE. FLAPS FAILED BETWEEN 1 AND 2; EXTENDED FLAPS TO 15 USING ALT FLAP EXTENSION. RNO MX FOUND LEFT POSITION TRANSMITTER CONNECTOR LOOSE BARELY FINGER TIGHT. CLEANED
- [SDR SWAA2025011384855](https://openairdocs.org/sdr/SWAA2025011384855), Jan 10, 2025: SIGN. OUT OF ADJUST. OVERWING EMERGENCY EXIT SIGN LOOSE / DANGLING<[01] REINSTALLED EMERGENCY EXIT SIGN PER AMM 33-51-02
- [SDR SWAA2025011384744](https://openairdocs.org/sdr/SWAA2025011384744), Jan 10, 2025: HANDLE. BROKEN. AFT PASSENGER DOOR R2 DOOR HANDLE CAM SAFETY WIRE BROKEN.<[01] RE-SECURED AFT GALLEY SVC DOOR HANDLE CAM BOLTS AND SAFETY WIRE REF AMM 20-50-11.<BR>CORRECTION A
- [SDR SWAA2025011384740](https://openairdocs.org/sdr/SWAA2025011384740), Jan 10, 2025: SEAL. CRACKED. R/H HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED FWD EDGE<[01] R&R RH HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL REF. AMM 53-31-31.
- [SDR SWAA2024121777620](https://openairdocs.org/sdr/SWAA2024121777620), Dec 15, 2024: LAMP. INOPERATIVE. RIGHT AFT EMERGENCY LIGHT INOP<[01] REMOVED AND REPLACED LAMP IN REF TO AMM 33-51-00
- [SDR SWAA2024101547585](https://openairdocs.org/sdr/SWAA2024101547585), Oct 12, 2024: LIGHT. INOPERATIVE. FORWARD SERVICE DOOR FWD LOWER EXIT LIGHT BULB OUT<[01] RELAMPED FORWARD SERVICE DOOR FWD LOWER EXIT LIGHT AND PERFORMED GOD OPERATIONAL CHECK PER AMM 33-51-01-
- [SDR SWAA2024101547587](https://openairdocs.org/sdr/SWAA2024101547587), Oct 12, 2024: BULB. INOPERATIVE. RH EMERGENCY EXIT DORR LOWER EXIT LIGHT BULB OUT<[01] RELAMPED RH EMERGENCY EXIT DOOR LOWER EXIT LIGHT AND PERFORMED GOOD OPERATIONAL CHECK PER AMM 33-51-01-960
- [SDR SWAA2024101646714](https://openairdocs.org/sdr/SWAA2024101646714), Oct 9, 2024: BATTERY PACK. NO TEST. EMERGENCY BATTRIES PACK (M1672; M1673; N1668; M1670; 1675; M1674) FAIL TEST; DO NOT HOLD CHARGE EMERGENCY BATTRIES PACK (M1672 M1673 M1668 M1670 M1675 M1674) FA
- [SDR SWAA2024101642801](https://openairdocs.org/sdr/SWAA2024101642801), Sep 27, 2024: INSERT. OUT OF POSITION. FLOOR PANEL 241AF HAS NUMEROUS THROUGH INSERTS THAT DO NOT ALIGN WITH THE UNDERLYING STRUCTURE.<[01] NEW 241AF FLOOR PANEL FABRICATION HAS BEEN COMPLETED PER [S
- [SDR SWAA2024101639184](https://openairdocs.org/sdr/SWAA2024101639184), Sep 18, 2024: STUB FRAME. CRACKED. CRACK FOUND AT R1 DOOR ON STUB FRAME ABOVE SEAL DEPRESSOR BS 294+5 WL274<[01] REMOVED AND REPLACED STUB FRAME UPPER AREA R1 DOOR FWD SIDE PER SRM 51-40-02 AND D
- [SDR SWAA2024101637738](https://openairdocs.org/sdr/SWAA2024101637738), Sep 14, 2024: WEB. CORRODED. SHEAR WEB AT BS 1016 RBL 36 WL 208 HAS CORROSION AROUND FASTENER HOLES ON UPPER SURFACE<[01] REMOVED AND REPLACED NEW SHEAR WEB PN#147A5744-14 FROM BS986-BS1016
- [SDR SWAA2024101637286](https://openairdocs.org/sdr/SWAA2024101637286), Sep 13, 2024: INTERCOSTAL. CRACKED. FORWARD CABIN COMPARTMENT STRUCTURE AREA; AT BS294.5 TO BS303.9 L/H SIDE STRINGER 15; INTERCOSTAL WITH CRACK MARKED.<[01] REMOVED AND REPLACED INTERCOSTAL AT FW
- [SDR SWAA2024101637293](https://openairdocs.org/sdr/SWAA2024101637293), Sep 13, 2024: WEB. CORRODED. CORROSION ON AFT CARGO COMPARTMENT DOOR CUT-OUT SUB-TRHESHOLD WEB FROM STA 807 TO STA 827+8 RBL 27; WL 158.<[01] REMOVED AND REPLACED SUB-THRESHOLD WEB P/N 146A
- [SDR SWAA2024101637294](https://openairdocs.org/sdr/SWAA2024101637294), Sep 13, 2024: SHIELD. CORRODED. CORROSION ON AFT CARGO DOOR CUT-OUT FWD SHIELD AT STA 767+2 & 767+15; WL 158; RBL 22.<[01] REMOVED AND REPLACED AFT CARGO DOOR CUT-OUT FWD SHIELD BS 767 TO BS29
- [SDR SWAA2024101637291](https://openairdocs.org/sdr/SWAA2024101637291), Sep 13, 2024: SIDEWALL SUPPORT. CORRODED. CORROSION ON AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT ANGLEE FROM STA 727B+6 TO STA 767; RBL 22; WL 158.<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL BS72
- [SDR SWAA2024101637292](https://openairdocs.org/sdr/SWAA2024101637292), Sep 13, 2024: SIDEWALL SUPPORT. CORRODED. CORROSION ON AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT ANGLEE FROM STA 727C+5 TO STA 787+2 LBL 22; WL 158.<[01] REMOVED AND REPLACED AFT CARGO COMPARTMENT
- [SDR SWAA2024101637295](https://openairdocs.org/sdr/SWAA2024101637295), Sep 13, 2024: SUPPORT. CORRODED. REJECT: CORROSION NOT REMOVED ON FCB AFT BULKHEAD RH SIDE SUPPORT TOP CORNER AT BS 500D; WL194<[01] REPAIRED PER EA 24-153-02618;[02] VERIFIED CORRECTIVE ACTION
- [SDR SWAA2024101637280](https://openairdocs.org/sdr/SWAA2024101637280), Sep 12, 2024: ATTACH ANGLE. CRACKED. FCB ATTACH ANGLE CRACKED AT BS 500C LBL 26 WL 156.<[01] REMOVED AND REPLACE FCB ATTACH ANGLE BS 500C LBL 26 WL 156 P/N 143A7502-157 IAW SRM 51-40-02-0G-0 AND DW
- [SDR SWAA2024101637261](https://openairdocs.org/sdr/SWAA2024101637261), Sep 12, 2024: WEB. CORRODED. PASSENGER CABIN AFT WET AREA; FOUND CORROSION AT FLOOR WEB STA 1016; WL 208.1 & LBL 38 APPROX.<[01] ?REFER TO FAULT TTG8Q00VTXK7 WHERE EA 24-153-02532 WAS ADDED
- [SDR SWAA2024101637043](https://openairdocs.org/sdr/SWAA2024101637043), Sep 12, 2024: SILL DRAIN. CORRODED. PASSENGER CABIN WET AREA; AFT RH DOOR MOPSILL FOUND CORROSION AROUND SEVERAL FASTENER HOLES BTWN STA 967 TO 985; WL 208.1 APPROX.<[01] REMOVED AND REPLACED RH M
- [SDR SWAA2024101637038](https://openairdocs.org/sdr/SWAA2024101637038), Sep 12, 2024: STRAP. CORRODED. PASSENGER CABIN AFT WET AREA; FOUND CORROSION AT TENSION STRAP STA 1027; WL 208.1 & RBL 18 APPROX.<[01] REMOVED AND REPLACED NEW PASSENGER CABIN AFT WET AREA TE
- [SDR SWAA2024101637041](https://openairdocs.org/sdr/SWAA2024101637041), Sep 12, 2024: STRAP. CORRODED. PASSENGER CABIN AFT WET AREA; FOUND CORROSION AT TENSION STRAP STA 1028; WL 208.1 & LBL 3 APPROX.<[01] REMOVED AND REPLACED PASSENGER CABIN AFT WET AREA TENSION
- [SDR SWAA2024101637282](https://openairdocs.org/sdr/SWAA2024101637282), Sep 12, 2024: FLOOR SUPPORT. CRACKED. FORWARD WET AREA FLOOR STRUCTURE INTERCOSTAL FOUND WITH CRACK AT BS312 TO BS328 WL 208 RBL30 MARKED.<[01] REMOVED AND REPLACED INTERCOSTAL P/N 141A5410-140. LOT
- [SDR SWAA2024101637279](https://openairdocs.org/sdr/SWAA2024101637279), Sep 12, 2024: FLOOR SUPPORT. CRACKED. FORWARD CABIN PASSENGER COMPARTMENT FLOOR STRUCTURE; INTERCOSTAL BS 380 TO BS 400 WL 208 RBL 10 FOUND WITH CRACK (R/H) MARKED.<[01] REMOVED AND REPLACED (1EA.) 
- [SDR SWAA2024101637040](https://openairdocs.org/sdr/SWAA2024101637040), Sep 12, 2024: STRAP. CORRODED. PASSENGER CABIN AFT WET AREA; FOUND CORROSION AT TENSION STRAP STA 1028; WL 208.1 & RBL 3 APPROX.<[01] REMOVED AND REPLACED PASSENGER CABIN AFT WET AREA TENSION
- [SDR SWAA2024101637263](https://openairdocs.org/sdr/SWAA2024101637263), Sep 12, 2024: NUT PLATE. CORRODED. MULTIPLE SPOT WITH CORROSION ON FCB FWD BULKHEAD CENTER SUPPORT NUTPLATE (6 EACH).<[01] REMOVED AND INSTALLED NEW 6EA RECEPTACLES<BR>IAW SRM 51-40-02 AND DWG 45
- [SDR SWAA2024101637265](https://openairdocs.org/sdr/SWAA2024101637265), Sep 12, 2024: SUPPORT. CORRODED. CORROSION ON FCB AFT BULKHEAD RH SIDE SUPPORT TOP CORNER AT BS 500D; WL194.<[01] FAULT RESOLVED ON FAULT TTG8Q00VUEL8;[02] REPAIRED ON TTG8Q00VUEL8 PER EA 24-15
- [SDR SWAA2024101639183](https://openairdocs.org/sdr/SWAA2024101639183), Sep 12, 2024: SHIELD. CORRODED. CORROSION ON FCB AFT SHIELD AT BS 500+24 RBL 25 WL 156.<[01] REMOVED AND REPLACED FCB AFT SHIELD <BR>IAW SRM 51-40-02 <BR>AND DWG # 143A0080 REV: -;[02] VERIFIE
- [SDR SWAA2024101637281](https://openairdocs.org/sdr/SWAA2024101637281), Sep 12, 2024: FLOOR SUPPORT. CRACKED. FORWARD CABIN COMPARTMENT FLOOR STRUCTURE; INTERCOSTAL FOUND WITH CRACK AT BS 277 TO BS 294.5 WL 208 BL 0 MARKED.<[01] REMOVED AND REPLACED INTERCOSTAL BS 277 T
- [SDR SWAA2024101637283](https://openairdocs.org/sdr/SWAA2024101637283), Sep 12, 2024: FLOOR SUPPORT. CORRODED. FORWARD CABIN COMPARTMENT FLOOR STRUCTURE; BRACKET FOUND WITH CORROSION AT BS312 LBL55 WL208 MARKED.<[01] REMOVED AND REPLACED BRACKET AT BS 312 LBL 55 WL 208.1
- [SDR SWAA2024101637289](https://openairdocs.org/sdr/SWAA2024101637289), Sep 12, 2024: SILL DRAIN. CORRODED. FORWARD CABIN COMPARTMENT ON FLOOR WET AREA MOP SILL WITH CORROSION; BS294 TO BS312 WL208 LBL55 (MARKED).<[01] REMOVED AND REPLACED FORWARD CABIN COMPARTMENT ON
- [SDR SWAA2024101537277](https://openairdocs.org/sdr/SWAA2024101537277), Sep 12, 2024: FLOOR SUPPORT. CRACKED. FORWARD CABIN PASSENGER COMPARTMENT FLOOR STRUCTURE INTERCOSTAL BS 380 TO BS 400 WL 208 LBL 13 FOUND WITH CRACK (L/H) MARKED.<[01] REMOVED AND REPLACED (1EA.) U
- [SDR SWAA2024101537039](https://openairdocs.org/sdr/SWAA2024101537039), Sep 12, 2024: WEB. CORRODED. PASSENGER CABIN AFT WET AREA; FOUND CORROSION AT FLOOR WEB STA 1030; WL 208.1 & RBL 5 APPROX.<[01] REMOVED CORROSION AND REWORKED AFFECTED AREA AT PASSENGER CAB
- [SDR SWAA2024101636350](https://openairdocs.org/sdr/SWAA2024101636350), Sep 11, 2024: FLOOR PANEL. PULLED. AFT FLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 241UF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[0
- [SDR SWAA2024101635741](https://openairdocs.org/sdr/SWAA2024101635741), Sep 10, 2024: SCUFF PLATE. CRACKED. AFT CARGO COMPARTMENT FORWARD SCUFF PLATE IS CRACKED.<[01] ALL STEPS COMPLETED;[02] AFT CARGO BAY FWD SCUFF PLATE REPAIRED PER SRM 53-60-15-2R-1;[03] CORRECTED 
- [SDR SWAA2024101635740](https://openairdocs.org/sdr/SWAA2024101635740), Sep 10, 2024: SCUFF PLATE. CRACKED. FORWARD CARGO COMPARTMENT AFT CORNER SCUFF PLATE IS CRACKED.<[01] ALL STEPS COMPLETED;[02] REPAIRED FCB AFT CORNER SCUFF PLATE IAW SRM 53-30-15-2R-1.<BR>WILL BE
- [SDR SWAA2024101635950](https://openairdocs.org/sdr/SWAA2024101635950), Sep 10, 2024: FLOOR PANEL. PULLED. FLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE; FABRICATED NEW FLOOR PANEL 231XF IAW SRM 53-00-50-2R-0 AND BOEING DWG 14
- [SDR SWAA2024101635951](https://openairdocs.org/sdr/SWAA2024101635951), Sep 10, 2024: FLOOR PANEL. DEBONDED. FLOOR PANEL 231ZF LOWER SKIN HAS AREAS OF DISBONDS. (MARKED)<[01] FLOOR PANEL 231ZF LOWER SKIN WITH AREAS OF DISBONDS AS MARKED WAS REPLACED WITH A SERVICEABLE 
- [SDR SWAA2024101635965](https://openairdocs.org/sdr/SWAA2024101635965), Sep 10, 2024: FLOOR PANEL. DAMAGED. AFT FLOOR PANEL 242XF CENTER AREA OF PANEL IS SOFT.<[01] AFT FLOOR PANEL 242XF WITH CENTER AREA OF PANEL BEING SOFT WAS REPLACED WITH A SERVICEABLE FLOOR PANEL 
- [SDR SWAA2024101635953](https://openairdocs.org/sdr/SWAA2024101635953), Sep 10, 2024: FLOOR PANEL. PULLED. FLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241DF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR P
- [SDR SWAA2024101635955](https://openairdocs.org/sdr/SWAA2024101635955), Sep 10, 2024: FLOOR PANEL. PULLED. AFT FLOOR PANEL 241YF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241YF WITH AREAS OF PULLED STRANDS ON UPPER SKIN WAS REPAIRED IAW SRM 53-00-5
- [SDR SWAA2024101635957](https://openairdocs.org/sdr/SWAA2024101635957), Sep 10, 2024: FLOOR PANEL. PULLED. AFT FLOOR PANEL 241ABF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] 241ABF FLOOR PANEL UPPER SKIN DAMAGE HAS BEEN REPAIRED PER [SRM 53-00-50-2R-1-A00939 (REPAIR
- [SDR SWAA2024101635961](https://openairdocs.org/sdr/SWAA2024101635961), Sep 10, 2024: FLOOR PANEL. PULLED. AFT FLOOR PANEL 241AEF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241AEF; UPPER SKIN; AREAS OF PULLED STRANDS WERE REPAIRED IAW SRM 53-00-50-2
- [SDR SWAA2024101635963](https://openairdocs.org/sdr/SWAA2024101635963), Sep 10, 2024: FLOOR PANEL. PULLED. AFT FLOOR PANEL 242VF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242VF WITH PULLED STRANDS ON UPPER SKIN WAS REPAIRED IAW SRM 53-00-50-2R-1.;[

All 288: https://openairdocs.org/aircraft/N263WN/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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