# N567WN: 2002 Boeing 737-7CT

- Status: Valid registration
- Airframe: [Boeing 737-7CT](https://openairdocs.org/model/boeing-737-7ct) (registry code 13844NE, 149 seats)
- Engine: [CFM International CFM56-7B24 series](https://openairdocs.org/engine/cfm-international-cfm56-7b24-series) (registry code 13044)
- Serial number: 32747
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 16, 2015
- Certificate issued: October 14, 2014
- Expires: October 31, 2027
- Mode S code: A742EC
- 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=567WN
- Page: https://openairdocs.org/aircraft/N567WN

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 737-7CT)

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 DCA24FA143](https://openairdocs.org/ntsb/DCA24FA143), Apr 3, 2024: Boeing 737-7CT (N567WN), Gulf of America (Gulf of Mexico), no damage. Probable cause: The pilot’s inadvertent encounter with convectively induced turbulence from a broken line of embedded thunderstorms moving across the region. Contributing to the accident was the failure of the air…

## 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 20240403003199A](https://openairdocs.org/incident/20240403003199A), Apr 3, 2024: Boeing 737-7CT (N567WN), Tampa, FL, No damage. NTSB took investigation iic ntsb- [privacy data omitted], upgraded it to a class 3 accident and will be launching an air traffic team. The accident # is:…

## Service difficulty reports (225, 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 SWAA2026092324437](https://openairdocs.org/sdr/SWAA2026092324437), Sep 19, 2026: ASSIST HANDLE. LOOSE. FORWARD GALLEY R1 DOOR ASSIST HANDLE LOOSE. SECURED THE ASSIST HANDLE IAW CMM 25-31-03.
- [SDR SWAA2026042792357](https://openairdocs.org/sdr/SWAA2026042792357), Apr 24, 2026: BATTERY PACK. NO TEST. EMERGENCY BATTERY PACK AT 14 DEF M1669 FAILED CAPACITY CHECK. R&R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06.
- [SDR SWAA2026040987817](https://openairdocs.org/sdr/SWAA2026040987817), Apr 9, 2026: LAMP. INOPERATIVE. AFT. OF L2 DOOR EXTERIOR EMERGENCY LIGHTS INOP<[01] RELAMPED L2 EXTERIOR EMERGENCY LIGHT AND CHECK GROUND WIRES. PER AMM 33-51-04. REMOVED AND REPLACED L2 DOOR 
- [SDR SWAA2025121652036](https://openairdocs.org/sdr/SWAA2025121652036), Dec 13, 2025: GIRT BAR. OUT OF ADJUST. FWD SERVICE DOOR GIRT HANGING LOW. SECURED THE GIRT BAR IAW AMM 25-66-01.
- [SDR SWAA2025051268286](https://openairdocs.org/sdr/SWAA2025051268286), May 7, 2025: LAMP. INOPERATIVE. EMERGENCY LIGHT AT SEAT ROW 14ABC INOPERATIVE.<[01] REMOVED AND REPLACED EMERGENCY LIGHT LAMP AT SEAT ROW 14ABC. REF AMM 33-51-01. OPERATIONAL CHECK GOOD.
- [SDR SWAA2025051268285](https://openairdocs.org/sdr/SWAA2025051268285), May 7, 2025: LAMP. INOPERATIVE. EMERGENCY LIGHT AT SEAT ROW 6DEF INOPERATIVE.<[01] REMOVED AND REPLACED EMERGENCY LIGHT LAMP AT SEAT ROW 6DEF. REF AMM 33-51-01. OPERATIONAL CHECK GOOD.
- [SDR SWAA2025031304356](https://openairdocs.org/sdr/SWAA2025031304356), Mar 12, 2025: SEAT BACK. OUT OF ADJUST. SEATS RECLINING AT EMERGENCY EXIT ROW 12D; 12F. ADJUSTED 12D; 12F SEAT RECLINE REF AMM 25-22-00
- [SDR SWAA2025021094370](https://openairdocs.org/sdr/SWAA2025021094370), Feb 9, 2025: SLIDE. OUT OF POSITION. R2 DOOR ESCAPE SLIDE DRAGS ON THE FLOOR<[01]. PROPERLY INSTALLED R2 DOOR ESCAPE SLIDE IAW AMM 25-66-01-400-801;[02] VERIFIED CORRETIVE ACTION ENTRY 1.
- [SDR SWAA2025021093811](https://openairdocs.org/sdr/SWAA2025021093811), Feb 6, 2025: BATTERY PACK. NO TEST. EMERGENCY LIGHTS RELATED TO BATTERY PACK M2355 FAIL TEST<[01] REPLACED EMERGENCY BATTERY PACK M2335; PERFORMED GOOD EMEREGENCY LIGHT TEST PER AMM 33-51-06-960-8
- [SDR SWAA2025021093812](https://openairdocs.org/sdr/SWAA2025021093812), Feb 6, 2025: LIGHT. INOPERATIVE. FWD ESCAPE EMEREGENCY LIGHT OUTSIDE FWD MAIN ENTRY DOOR INOP (L731)<[01] INSTALLED NEW LIGHT AT FWD ESCAPE EMEREGENCY OUTSIDE FWD MAIN ENTRY DOOR; PERFORMED GOO
- [SDR SWAA2025021091146](https://openairdocs.org/sdr/SWAA2025021091146), Jan 29, 2025: SCUFF PLATE. MISSING. AFT AND FWD SCUFF PLATES (CORNERS) MISSING AT FWD CARGO BAY<[01] 01 - REMOVED AND REPLACED PER [AMM 53-11-02-420-801-NG (CARGO DOOR SCUFF PLATE - INSTALLATION -
- [SDR SWAA2025021088431](https://openairdocs.org/sdr/SWAA2025021088431), Jan 22, 2025: FLOORBEAM. CRACKED. CRACKED PANEL BREAK BS 540 BL 0 - RBL 25 WL 207 (MARKED)<[01] REMOVED AND REPLACED PANEL BREAK AT BS540 BL0-RBL25 WL207 PER SRM 51-40-02 AND DWG:143A0060 REV:A;
- [SDR SWAA2025021088432](https://openairdocs.org/sdr/SWAA2025021088432), Jan 22, 2025: FLOORBEAM. CANNING. CRACKED PANEL BREAK BS 540 BL 0 - LBL 25 WL 207 (MARKED)<[01] REMOVED AND REPLACED PANEL BREAK AT BS540 BL0-LBL25 WL207 PER SRM 51-40-02 AND DWG:143A0060 REV:A;
- [SDR SWAA2025021088206](https://openairdocs.org/sdr/SWAA2025021088206), Jan 21, 2025: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK LBL 24.75 BS500A+8; BS500A+11; BS500A+14.5; BS500A+17; BS500D+9.5; BS 520+5.5 TO BS520+11 WL 208 (MARKED)<[01] BS 480 TO BS 520 LBL25 SE
- [SDR SWAA2025021088212](https://openairdocs.org/sdr/SWAA2025021088212), Jan 21, 2025: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK LBL 45.5 BS480+16.5; BS500A+5; BS500A+8; BS500B+16; BS500B+18.5; BS00D+9.5 WL 208 (MARKED)<[01] SEAT TRACK WILL REPLACE DUE TO MECHANICA
- [SDR SWAA2025021087806](https://openairdocs.org/sdr/SWAA2025021087806), Jan 20, 2025: SKIN. CRACKED. CRACK ON RH LOWER HORIZONTAL STABILIZER SKIN AT STAB STA 193.90; 18.5' FROM FWD EDGE; .35' IN LENGTH (MARKED) <[01]. REPAIRED R/H HORIZONTAL STAB LOWER SKIN AT 
- [SDR SWAA2025021087557](https://openairdocs.org/sdr/SWAA2025021087557), Jan 19, 2025: WEB. CRACKED. RIGHT WING T/E UPPER SURFACE PANEL AT ORSS 276; TRANSVERSE WEB IS CRACKED AT O/B UPPER FASTENER<[01] REMOVED R/W T/E UPPER SURFCE PANEL TRANSVERSE WEB AT ORSS 2
- [SDR SWAA2025021087563](https://openairdocs.org/sdr/SWAA2025021087563), Jan 19, 2025: RIB. CRACKED. L-CLIP COMMON TO L/W I/B SIDE OF DEFLECTION CONTROL RIB AND UPPER SURFACE PANEL ORSS 271 IS CRACKED <[01]. REMOVED AND REPLACED L- CLIP COMMON TO L/W I/B SIDE O
- [SDR SWAA2025021187233](https://openairdocs.org/sdr/SWAA2025021187233), Jan 18, 2025: PANEL. DEBONDED. RIGHT WING L/E PANEL 621HB HAS DISBOND AT I/B FWD CORNER<[01] 04 - REPAIRED PER [SRM 51-70-05-2R-6-A00737 (REPAIR 6 - REPAIR OF DAMAGE TO THE EDGEBAND OF A HONE
- [SDR SWAA2025021087434](https://openairdocs.org/sdr/SWAA2025021087434), Jan 18, 2025: RIB. CRACKED. LEFT HORIZONTAL STAB REMOVABLE L/E 331B RIB #3 IS CRACKED<[01] 1. KENNETH RUDIO (TECHNICIAN); 24-JAN-2025 22:07 UTC<BR>REMOVED AND REPLACED L/H HORIZONTAL STAB.
- [SDR SWAA2025021087435](https://openairdocs.org/sdr/SWAA2025021087435), Jan 18, 2025: RIB. CRACKED. LEFT HORIZONTAL STAB REMOVABLE L/E 331B RIB #5 IS CRACKED<[01] REMOVED AND REPLACED L/H HORIZONTAL STAB. L/E #5 RIB IAW SRM 51-40-02-0G-0 PARA. 4.;[02] VERIFIED
- [SDR SWAA2025021087226](https://openairdocs.org/sdr/SWAA2025021087226), Jan 18, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231XF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR P
- [SDR SWAA2025021087227](https://openairdocs.org/sdr/SWAA2025021087227), Jan 18, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 231YF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231YF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR P
- [SDR SWAA2025021087224](https://openairdocs.org/sdr/SWAA2025021087224), Jan 18, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 231ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231ZF; WITH UPPER SKIN AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED F
- [SDR SWAA2025021087228](https://openairdocs.org/sdr/SWAA2025021087228), Jan 18, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241AF UPPER SKIN; WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED F
- [SDR SWAA2025021087230](https://openairdocs.org/sdr/SWAA2025021087230), Jan 18, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 242AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 242AF; UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED F
- [SDR SWAA2025021087229](https://openairdocs.org/sdr/SWAA2025021087229), Jan 18, 2025: FLOOR PANEL. PULLED. PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 241DF WITH UPPER SKIN HAS AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANE
- [SDR SWAA2025021086864](https://openairdocs.org/sdr/SWAA2025021086864), Jan 17, 2025: THRESHOLD. CORRODED. FWD CARGO SUBTHRESHOLD HAS CORROSION IN MULTIPLE AREAS<[01] UPON FURTHER INVESTIGATION; FOUND TO BE OUT OF LIMIT AS PER SRM 53-30-15-1A-1. REPAIR BY REPLACEMENT
- [SDR SWAA2025021086866](https://openairdocs.org/sdr/SWAA2025021086866), Jan 17, 2025: PRESSURE DECK. CRACKED. CRACK IN LH HORIZONTAL PRESSURE DECK BS 672 WL 202 LBL35. CRACK IS .650 INCHES IN LENGTH. MARKED IN RED INK.<[01] REPAIRED LH HORIZONTAL PRESSURE DECK WEB AT BS
- [SDR SWAA2025021086867](https://openairdocs.org/sdr/SWAA2025021086867), Jan 17, 2025: PRESSURE DECK. CRACKED. CRACK IN RH HORIZONTAL PRESSURE DECK BS 664.5 WL 202 RBL 43. CRACK IS .250 INCHES LONG AND MARKED IN RED INK.<[01] REMOVED THE DAMAGE PART OF THE WEB AT BS 663.
- [SDR SWAA2025021086862](https://openairdocs.org/sdr/SWAA2025021086862), Jan 17, 2025: WEB. CORRODED. AFT CARGO SUBTHRESHOLD WEB HAVE CORROSION MULTIPLE AREAS.<[01] REMOVE AND REMPLACE AFT CARGO SUBTHRESHOLD WEB SRM 51-40-02 DWG 146A8340 ID:0024 REV: A;[02] REMO
- [SDR SWAA2025021086863](https://openairdocs.org/sdr/SWAA2025021086863), Jan 17, 2025: STRAP. CORRODED. AFT CARGO BAY TENSION STRAP HAS CORROSION APPROX BS802; RBL25.<[01] CORROSION ON TENSION STRAP AT ACB BS 806 ; RBL 25 IN L=2' X W=1' X D=0.030' FROM ORIGINAL TH
- [SDR SWAA2025021086500](https://openairdocs.org/sdr/SWAA2025021086500), Jan 16, 2025: SCUFF PLATE. CRACKED. AFT CARGO FWD SCUFF PLATE IS CRACKED <[01]. WELDED THE CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-60-15-2R-1 PARA 4.B.(4). REFERRE
- [SDR SWAA2025021086861](https://openairdocs.org/sdr/SWAA2025021086861), Jan 16, 2025: VAPOR BARRIER. CRACKED. CRACKED VAPOR BARRIER IN THE MAIN WHEEL WELL BS663 LBL15 WL147. MARKED <[01]. CRACKED VAPOR BARRIER BS663 LBL15 WL147 WAS REPAIRED IAW SRM 51-70-04-2R-10;[02] V
- [SDR SWAA2025021086319](https://openairdocs.org/sdr/SWAA2025021086319), Jan 15, 2025: DOUBLER. DAMAGED. CUSTOMER REQUEST: DOUBLER AT BS 407 BETWEEN S-1 AND S-2L REQUIRES REMOVAL AND REPAIR DOUBLER AT BS 407 STR 1 - STR 2L/H <[01]. `THE DAMAGE WAS REPAIRED PER EA 2
- [SDR SWAA2024102148684](https://openairdocs.org/sdr/SWAA2024102148684), Oct 15, 2024: GIRT BAR. UNSECURE. R1 DOOR SLIDE GIRT IS NOT SECURED WITH VELCRO<[01] RE-SECURED R1 DOOR SLIDE GIRT WITH VELCRO PER AMM 25-66-01.
- [SDR SWAA2024102148674](https://openairdocs.org/sdr/SWAA2024102148674), Oct 15, 2024: BRACKET. CRACKED. KEEL BEAM ACCESS PANEL 192E FWD RH ATTACH HANGAR BRACKET IS CRACKED.<[01] REMOVED AND REPLACED KEEL BEAM ACCESS PANEL 192E FWD R/H ATTACH HANGER BRACKET PER SRM
- [SDR SWAA2024081926753](https://openairdocs.org/sdr/SWAA2024081926753), Aug 16, 2024: BATTERY PACK. INOPERATIVE. LEFT OVERWING EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED LEFT OVERWING EMERGENCY LIGHTS PSU BATTERY PACK. TEST OK. REF AMM. 33-51-06.
- [SDR SWAA2024040470177](https://openairdocs.org/sdr/SWAA2024040470177), Apr 3, 2024: SIGN. BROKEN. AFT CEILING EMERGENCY EXIT SIGN BROKEN<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-01-960-802-NG (EXIT SIGN - LIGHT ASSEMBLY REPLACEMENT - PERMANENT)]
- [SDR SWAA2023030810769](https://openairdocs.org/sdr/SWAA2023030810769), Feb 28, 2023: HANDLE. LOOSE. PER CUSTOMER WALK- L-1 DOOR AFT ASSIST HANDLE LOOSE.<[01] SECURED L-1 DOOR AFT ASSIST HANDLE AS PER AMM 25-21-31-420-802;[02] VERIFIED 1.
- [SDR SWAA2023030810774](https://openairdocs.org/sdr/SWAA2023030810774), Feb 28, 2023: FITTING. LOOSE. CUSTOMER WALK - R-2 DOOR AFT GIRT BAR FLOOR FITTING LOOSE.<[01] RESECURED R 2 DOOR AFT GIRT BAR FLOOR FITTING AS PER REF B737AMM 25-66-01-000-804;[02] VERIFIED 
- [SDR SWAA2023030810503](https://openairdocs.org/sdr/SWAA2023030810503), Feb 27, 2023: LIGHT. INOPERATIVE. R2 DOOR EXTERIOR EMERGENCY LIGHT INOP.<[01] RECONNECTED R2 DOOR EXTERIOR EMERGENCY LIGHT AS PER REF B737 AMM 33-51-04-960-801. TEST OK.;[02] VERIFIED STEP#1
- [SDR SWAA2023030809602](https://openairdocs.org/sdr/SWAA2023030809602), Feb 23, 2023: BATTERY PACK. FAILED. SEVERAL EMERGENCY LIGHTS FAILED OPERATIONAL TEST THROUGHOUT THE CABIN.<[01] REMOVED AND REPLACED AT LOCATIONS M1673; M1670 AND M1669 PERFORMED OPERATIONAL TEST 
- [SDR SWAA2023030805304](https://openairdocs.org/sdr/SWAA2023030805304), Feb 21, 2023: PANEL. CRACKED. LH HORIZONTAL STABILIZER PANEL 333AT TRACK ASSY FOUND CRACKED<[01] REMOVED PANEL 333AT AT LT HORIZONTAL STABILIZER FOR ACCESS TO DAMAGE IN AS PER B 737-700 SRM 
- [SDR SWAA2023030805302](https://openairdocs.org/sdr/SWAA2023030805302), Feb 16, 2023: SEAT. CRACKED. COCKPIT 1ST OBS SEAT BOTTOM CRACKED ON RIGHT LWR SURFACE. 8-50<[01] REMOVED FLIGHT DECK 1ST OBS. SEAT AS PER B737 AMM 25-1102-000-801;[02] ACCOMPLISHED REPAIR D
- [SDR SWAA2023030802149](https://openairdocs.org/sdr/SWAA2023030802149), Feb 11, 2023: BATTERY. INOPERATIVE. FWD LH WINDSCREEN : BATTERIES AT EMERGENCY FLASHLIGHTS DO NOT WORK (2 EACH)<[01] FLASHLIGHT BATTERIES AT FWD LH WINDSCREEN REMOVED AND REPLACED IAW CMM 25-60-02
- [SDR SWAA2023030802152](https://openairdocs.org/sdr/SWAA2023030802152), Feb 11, 2023: BATTERY. INOPERATIVE. AFT LH WINDSCREEN : BATTERIES AT EMERGENCY FLASHLIGHTS DO NOT WORK (2 EACH)<[01] FLASHLIGHT BATTERIES AT AFT LH WINDSCREEN REMOVED AND REPLACED IAW CMM 25-60-02
- [SDR SWAA2023030800909](https://openairdocs.org/sdr/SWAA2023030800909), Feb 8, 2023: TRACK. CORRODED. F/O FWD I/B SEAT TRACK HAS CORROSION ON LWR SURFACE. 8-36<[01] RECEIVED PART; NEW TRACK INSTALLED ON TASK CARD TTG8Q001YDLC.;[02] VERIFIED 1;
- [SDR SWAA2023030800907](https://openairdocs.org/sdr/SWAA2023030800907), Feb 8, 2023: TRACK. CORRODED. CAPT. FWD O/B SEAT TRACK HAS CORROSION ON LWR SURFACE. 8-35<[01] RECEIVED PART; NEW TRACK INSTALLED ON TASK CARD TTG8Q001YDLC;[02] VERIFIED 1;
- [SDR SWAA2023030800908](https://openairdocs.org/sdr/SWAA2023030800908), Feb 8, 2023: TRACK. CORRODED. F/O FWD O/B SEAT TRACK HAS CORROSION ON LWR SURFACE. 8-34<[01] RECEIVED PART; NEW SEAT TRACK INSTALLED ON TASK CARD TTG8Q001YDLC.;[02] PARTS TRANS ACTION;[03] F

All 225: https://openairdocs.org/aircraft/N567WN/reports.md

## STCs that may be installed (OpenAirDocs) (2)

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

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