# N569WN: 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: 33656
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 28, 2015
- Certificate issued: November 3, 2014
- Expires: November 30, 2027
- Mode S code: A74A5A
- 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=569WN
- Page: https://openairdocs.org/aircraft/N569WN

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

None matched to N569WN.

## FAA accident and incident reports

None matched to N569WN.

## Service difficulty reports (253, 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 SWAA2026061509885](https://openairdocs.org/sdr/SWAA2026061509885), Jun 6, 2026: STIFFENER. CRACKED. CENTER FUEL TANK VERTICAL STIFFENER IS CRACKED. BS 540, LBL 24 ON THE TOP 6 INCHES BELOW THE BOTTOM OF THE CABIN FLOOR PANEL. REF TTG8Q01CKAZ4. REMOVED AND REPL
- [SDR SWAA2026061009723](https://openairdocs.org/sdr/SWAA2026061009723), Jun 6, 2026: STIFFENER. CRACKED. CENTER FUEL TANK VERTICAL STIFFENER IS CRACKED. STA 540, LBL 24 ON THE TOP 6 INCHES BELOW THE BOTTOM OF THE CABIN FLOOR PANEL. AIRCRAFT TO BE FERRIED TO PAE FOR
- [SDR SWAA2026060909230](https://openairdocs.org/sdr/SWAA2026060909230), Jun 5, 2026: DOOR. CRACKED. RIGHT MLG CENTER DOOR CRACKED. REMOVED RT CTR & INNER DOOR ASSY IAW AMM 32-13-11, OK TO CONTINUE SERVICE PER CDL 32-10-3XD AUTHORIZATION 322696. REPLACED RT GEA
- [SDR SWAA2026060909228](https://openairdocs.org/sdr/SWAA2026060909228), Jun 5, 2026: DOOR. CRACKED. LEFT MLG CENTER DOOR CRACKED.<[01] REMOVER LT MLG CENTER AND INNER DOOR PER AMM 32-13-11. OK TO CONTINUE PER CDL 32-10-3XC. AUTHORIZATION NR 322695. REPLACED LT
- [SDR SWAA2026060909265](https://openairdocs.org/sdr/SWAA2026060909265), Jun 5, 2026: LIGHT. DAMAGED. PASSENGER CABIN SEAT ROW 1DEF PHOTOLUMINESCENT STRIP HAS MOISTURE UNDER CLEAR LENS. REMOVED AND REPLACED PHOTO STRIP PER AMM 33-51-15.
- [SDR SWAA2026060809275](https://openairdocs.org/sdr/SWAA2026060809275), Jun 5, 2026: STIFFENER. CRACKED. CENTER FUEL TANK VERTICAL STIFFENER IS CRACKED. STA 540; LBL 24 ON THE TOP 6 INCHES BELOW THE BOTTOM OF THE CABIN FLOOR PANEL. AIRCRAFT TO BE FERRIED TO PAE FOR
- [SDR SWAA2026060207887](https://openairdocs.org/sdr/SWAA2026060207887), May 30, 2026: SCREW. WORN. RH OVERWING ESCAPE SLIDE LIGHT LENS HAS 1 SCREW THAT SPINS AND WILL NOT COME OUT SUSPECT BAD NUT PLATE. UPON FURTHER INVESTIGATION FOUND SCREW TO BE WORN. SCREW
- [SDR SWAA2026060207758](https://openairdocs.org/sdr/SWAA2026060207758), May 30, 2026: WIRE. DAMAGED. OVERWING ESCAPE LIGHT AT RT WAS INOPERATIVE. REMOVED DAMAGED WIRING BETWEEN OVERWING EXIT LIGHT ASSEMBLY L7 AND D11076 AND INSTALLED NEW WIRING PER WDM 33-51-13
- [SDR SWAA2026060207757](https://openairdocs.org/sdr/SWAA2026060207757), May 30, 2026: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS ASSOCIATED WITH EMERGENCY LIGHTS BATTERY PACK M2335 ARE INOPERATIVE. REMOVED AND REPLACED M2335 EMERGENCY LIGHTS BATTERY PACK AND CHARGER AND P
- [SDR SWAA2026060208281](https://openairdocs.org/sdr/SWAA2026060208281), May 30, 2026: CHARGER. INOPERATIVE. EMERGENCY LIGHTS ASSOCIATED WITH EMERGENCY LIGHTS BATTERY PACK M2335 ARE INOPERATIVE. REMOVED AND REPLACED M2335 EMERGENCY LIGHTS BATTERY PACK AND CHARGER AND P
- [SDR SWAA2026060202871](https://openairdocs.org/sdr/SWAA2026060202871), May 13, 2026: INTERCOSTAL. CRACKED. FOUND CRACKED FASTENER HOLE DURING NDI ON AFT INTERCOSTAL CLIP AT BS 663 STR 15R. NEW CLIP WAS FABRICATED PER SWA EA 26-153-01321 AND INSTALLED PER EA 26-153-01
- [SDR SWAA2026060202869](https://openairdocs.org/sdr/SWAA2026060202869), May 13, 2026: BRACKET. CORRODED. CORROSION ON AFT DOG BONE BRACKET BS 663.75, STR 18 R/H. AFT DOG BONE BRACKET BS 663.75, STR 18R WAS FOUND TO HAVE CORROSION. AFT DOG BONE BRACKET AT BS 663.75 
- [SDR SWAA2026060202870](https://openairdocs.org/sdr/SWAA2026060202870), May 13, 2026: FITTING. CORRODED. CORROSION WAS FOUND ON RT KICK FITTING. CUSTOMER CARD TTG8Q01C1KDT WIP 1 STEP 26 ACCOMPLISHES SB 737-53-1397 FIGURE 173 INSPECTIONS AND DOES NOT ALLOW ANY CORRO
- [SDR SWAA2026060293856](https://openairdocs.org/sdr/SWAA2026060293856), Apr 29, 2026: FITTING. CRACKED. RH PICKLEFORK FRAME FITTING AT S-18A IS CRACKED FROM FASTENER TO EDGE OF FITTING (SECOND FASTENER DOWN ON AFT SIDE OF FITTING. REMOVED AND REPLACED RT PICKLE FO
- [SDR SWAA2026010557151](https://openairdocs.org/sdr/SWAA2026010557151), Dec 31, 2025: TRIM MOTOR. FAILED. MAIN STAB TRIM FAIL AFTER DEPARTURE. R & R STAB TRIM MOTOR IAW AMM 27-41-71. PERFORMED STAB TRIM MOTOR TEST IAW AMM 27-41-71, TESTED GOOD. PERFORMED STAB TRIM M
- [SDR SWAA2025080697686](https://openairdocs.org/sdr/SWAA2025080697686), Aug 2, 2025: HANDLE. BROKEN. FWD SERVICE DOOR BULKHEAD ASSISST HANDLE BROKEN. TIGHTENED ASSISST HANDLE PER CMM 25-21-71.
- [SDR SWAA2025072895258](https://openairdocs.org/sdr/SWAA2025072895258), Jul 24, 2025: SLIDE. OUT OF POSITION. AFT ENTRY DOOR SLIDE PARTIALLY PULLED OUT<[01] REPOSITIONED AFT ENTRY DOOR SLIDE PER AMM 25-66-01 AND MT 725-61-06 WITH NO DEFECTS NOTED. AC OK FOR SERVICE
- [SDR SWAA2024120271900](https://openairdocs.org/sdr/SWAA2024120271900), Nov 26, 2024: SEAL. CRACKED. LEFT HORIZONTAL UPPER FORWARD SLIDER SEAL AND TRACK IS CRACKED; BUCKLED.<[01] OK TO CONTINUE PER CDL 55-10-1. AUTHORIZATION # 225145.;[02] REMOVED AND REPLACED 
- [SDR SWAA2024120273333](https://openairdocs.org/sdr/SWAA2024120273333), Nov 26, 2024: TRACK. BUCKLED. LEFT HORIZONTAL UPPER FORWARD SLIDER SEAL AND TRACK IS CRACKED; BUCKLED.<[01] OK TO CONTINUE PER CDL 55-10-1. AUTHORIZATION # 225145.;[02] REMOVED AND REPLACED 
- [SDR SWAA2024112771594](https://openairdocs.org/sdr/SWAA2024112771594), Nov 26, 2024: SEAL. CRACKED. RIGHT HORIZONTAL LOWER FORWARD SLIDER SEAL IS CRACKED; BUCKLED.<[01] REPLACED RH HORIZONTAL STAB LOWER FWD SLIDER SEAL PER AMM 53-31-31.;[02] VERIFIED REPLACED 
- [SDR SWAA2024112161314](https://openairdocs.org/sdr/SWAA2024112161314), Nov 15, 2024: PANEL. CRACKED. FED UPPER FWD COVE PANEL IS CRACKED<[01] REMOVED AND REPLACED FED REVEAL PANEL PER SOPM 20-50-01; SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 AND DWG:141A8220.;[02] RE
- [SDR SWAA2024112559994](https://openairdocs.org/sdr/SWAA2024112559994), Nov 14, 2024: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT LIGHTS ASSOCIATED WITH M1670 BATTERY PACK ARE INOP.<[01] REMOVE AND REPLACED BATTERY PACK M1670 AND PERFORMED GOOD TEST IAW AMM 33-51-06-960-805.
- [SDR SWAA2024112556238](https://openairdocs.org/sdr/SWAA2024112556238), Nov 3, 2024: STIFFENER. CRACKED. RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB AT STABILIZER STATION 111.10 3RD VERTICAL STIFFENER IS CRACKED.<[01] REMOVED DAMAGE FROM 3RD VERTICAL STIFFENER AND 
- [SDR SWAA2024112555555](https://openairdocs.org/sdr/SWAA2024112555555), Oct 31, 2024: RADOME. DELAMINATED. PER CUSTOMER REQUEST; FOUND NOSE RADOME DELAMINATED AT THE VERY TIP MARKED<[01] REMOVED DAMAGED RADOME BOOT AND FOUND A DELAMINATION IN THE COMPOSITE AT THE DIS
- [SDR SWAA2024112555322](https://openairdocs.org/sdr/SWAA2024112555322), Oct 31, 2024: SKIN. CORRODED. CORROSION ON EXTERNAL LOWER FUSELAGE SKIN COMMON TO ATC ANTENNA STA 351.50-357.50; BLO; WL 149.<[01] REPAIRED LWR SKIN COMMON TO ATC ANTENNA IAW EA 24-153-03031
- [SDR SWAA2024112554736](https://openairdocs.org/sdr/SWAA2024112554736), Oct 30, 2024: PANEL. CRACKED. CRACKED PANEL BREAK AT BS540; LBL25-LBL45; WL208.<[01] REMOVED DAMAGED PANEL; BRAKE ASSY IAW SRM 51-40-02.<BR>INSTALLED NEW PANEL; BRAKE ASSY IAW SRM 51-40-02 A
- [SDR SWAA2024112554362](https://openairdocs.org/sdr/SWAA2024112554362), Oct 28, 2024: ATTACH ANGLE. CRACKED. CRACKED ATTACH ANGLE AT MID CABIN BS690 RBL1 WL206. MARKED<[01] REMOVED AND REPLACED ATTACH ANGLE (BRACKET) AT BS BS690 RBL 1 WL 206 PER SRM 51-40-02-0G-0 AND B
- [SDR SWAA2024112554176](https://openairdocs.org/sdr/SWAA2024112554176), Oct 28, 2024: SEAT TRACK. CORRODED. CORROSION ON PAX CABIN SEAT TRACK RBL25 BS554; BS562; BS661; BS712CROWN. WL208. MARKED<[01] REMOVED CORROSION FROM CABIN SEAT TRACK ON RBL25 BS552.5 3'X.70'X.01
- [SDR SWAA2024112554363](https://openairdocs.org/sdr/SWAA2024112554363), Oct 28, 2024: STIFFENER. CRACKED. RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 111.10; 4TH VERTICAL STIFFENER IS CRACKED.<[01] REMOVED DAMAGE FROM 4TH VERTICAL STIFFENER AN
- [SDR SWAA2024112554360](https://openairdocs.org/sdr/SWAA2024112554360), Oct 28, 2024: PANEL. CRACKED. CRACKED PANEL BREAK AT MID CABIN BS540 RBL1 WL208.<[01] REMOVED AND REPLACED PANEL BREAK AT BS540 RBL1 TO RBL24 WL 208 PER SRM 51-40-02-0G-0 AND BOEING DWG 143A
- [SDR SWAA2024112554366](https://openairdocs.org/sdr/SWAA2024112554366), Oct 28, 2024: SKIN. CORRODED. CORROSION ON EXTERNAL FUSELAGE SKIN UNDER VERTICAL STAB BS1016 - BS1033 LBL12 TO RBL12 WL308. MARKED<[01] COMPLETED CARD;[02] ACCOMPLISHED PER EA 24-153-03047-;
- [SDR SWAA2024112553950](https://openairdocs.org/sdr/SWAA2024112553950), Oct 27, 2024: RIB. CRACKED. LEFT HORIZONTAL STAB REMOVABLE L/E 331B RIB #4 CRACKED<[01] TASK COMPLETE:<BR>REMOVED CRACKED #4 RIB ON L/E 331B AND REPLACED WITH NEW (PN: 186A1304-1 LOT: 1582
- [SDR SWAA2024112553951](https://openairdocs.org/sdr/SWAA2024112553951), Oct 27, 2024: RIB. CRACKED. RIGHT HORIZONTAL STAB REMOVABLE L/E 341B RIB #5 CRACKED<[01] TASK COMPLETE:<BR>REMOVED CRACKED #5 RIB ON L/E 341B AND REPLACED WITH NEW (PN: 186A1305-2 LOT: 158
- [SDR SWAA2024092039256](https://openairdocs.org/sdr/SWAA2024092039256), Sep 19, 2024: BATTERY PACK. INOPERATIVE. LH EMERGENCY EXIT OVERWING LIGHTS INOP<[01] R&R EMERGENCY LIGHT BATTERY PACK FOR OVERWING EXIT DOOR PER AMM 33-51-06. OPS CHECK GOOD.
- [SDR SWAA2024082227525](https://openairdocs.org/sdr/SWAA2024082227525), Aug 19, 2024: LAMP. INOPERATIVE. LH OVERWING EMERGENCY EXIT LIGHT INOPERATIVE.<[01] RELAMPED LH OVERWING EMERGENCY EXIT LIGHT IAW AMM 33-51-04.
- [SDR SWAA2024070507848](https://openairdocs.org/sdr/SWAA2024070507848), Jul 2, 2024: BATTERY PACK. NO TEST. EMX LIGHT BATT/POWER SUPPLY M01673 FAILS TO ILLUMINATE LIGHTS<[01] 01 - REMOVED AND REPLACED EMX BATTERY PACK AND POWER SUPPLY M01673 PER [AMM 33-51-06-960-805-
- [SDR SWAA2024070507844](https://openairdocs.org/sdr/SWAA2024070507844), Jul 2, 2024: HANDLE. LOOSE. AFT SERVICE DOOR ASSIST HANDLE A/C SIDE IS LOOSE<[01] TIGHTENED AFT SERVICE DOOR ASSIST HANDLE A/C SIDE PER AMM 20-50-11
- [SDR SWAA2024062705429](https://openairdocs.org/sdr/SWAA2024062705429), Jun 25, 2024: LAMP. INOPERATIVE. AFT ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOP<[01] RE LAMPED SLIDE LIGHT IAW AMM 33-51-04. OPS CHECK GOOD
- [SDR SWAA2024061903258](https://openairdocs.org/sdr/SWAA2024061903258), Jun 19, 2024: BRACKET. LOOSE. FORWARD ENTRY DOOR GIRT BAR STOWAGE BRACKET LOOSE<[01] RESECURED FWD ENTRY DOOR FWDGIRT BAR BRACKET REF AMM 25-66-02.
- [SDR SWAA2024052387864](https://openairdocs.org/sdr/SWAA2024052387864), May 20, 2024: SLIDE. PARTIAL DEPLOY. FORWARD SERVICE DOOR SLIDE PARTIALLY DEPLOYED/UNPACKED<[01] REINSTALLED FWD SERVICE DOOR SLIDE; FOUND IT NOT PARTIALLY DEPLOYED AND FOUND NO DAMAGE INSTALLED PE
- [SDR SWAA2023121830941](https://openairdocs.org/sdr/SWAA2023121830941), Dec 11, 2023: SKIN. HANDLER ERROR. PROVO TRUCK COLLIDED WITH CAPT SIDE ENTRY AFT DOOR<[01] REPAIRED ON EA 23-153-03617 (N569WN - SWA - REPAIR - SECTION 47 FUSELAGE SKIN DAMAGE BETWEEN STA 914 - 9
- [SDR SWAA2023121830942](https://openairdocs.org/sdr/SWAA2023121830942), Dec 11, 2023: STRINGER. CRACKED. REF TO LP 2398631 FOUND DAMAGE CAUSED BY PROVO TRUCK IN BETWEEN STATIONS 914-937 AND STRINGERS S-20L & S-21L LENGTH OF 7-12/32 AND WIDTH OF 15-8/32 13/64TH DEEP
- [SDR SWAA2023101710911](https://openairdocs.org/sdr/SWAA2023101710911), Oct 15, 2023: LIGHT. INOPERATIVE. AREA EMERGENCY LIGHT AT ROW 6FED INOP<[01] RELAMPED AREA EMERGENCY LIGHT AT ROW 6FED REF AMM 33-51-03. OPS CHK GOOD.
- [SDR SWAA2023072481094](https://openairdocs.org/sdr/SWAA2023072481094), Jul 20, 2023: LENS. BROKEN. FWD ENTRY DOOR LOWER EXIT SIGN LENS BROKEN.<[01] R+R FWD ENTRY DOOR LOWER EXIT SIGN LENS PER AMM 33-51-01.
- [SDR SWAA2023052450847](https://openairdocs.org/sdr/SWAA2023052450847), May 21, 2023: LIGHT. INOPERATIVE. AFT R/H SIDE EMERGENCY SLIDE LIGHT INOP<[01] RELAMPED AFT R/H SIDE EMERGENCY SLIDE LIGHT PER AMM 33-51-04.
- [SDR SWAA2023051749156](https://openairdocs.org/sdr/SWAA2023051749156), May 15, 2023: LIGHT. OUT OF ADJUST. FWD RIGHT SIDE ILLUMINATION STRIP LIFTING.<[01] APPLIED DOUBLE SIDE TAPE TO ILLUMINATES STRIP PER SIP.
- [SDR SWAA2023051548481](https://openairdocs.org/sdr/SWAA2023051548481), May 13, 2023: BATTERY PACK. INOPERATIVE. FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP<[01] REMOVED AND REPLACED FWD ENTRY DOOR BATTERY PACK IAW AMM 33-51-06 OPS CHECK GOOD AT THIS TIME
- [SDR SWAA2023031515943](https://openairdocs.org/sdr/SWAA2023031515943), Mar 11, 2023: STRIP. LOOSE. FLOOR LIGHTING PHOTOLUMENESCENT STRIP AT FWD CABIN COMING LOOSE.<[01] RESECURED STRIP PER AMM 33-51-15
- [SDR SWAA2022120277578](https://openairdocs.org/sdr/SWAA2022120277578), Dec 2, 2022: BATTERY PACK. INOPERATIVE. ENEMERGENCY LIGHTS AT SEAT 6C; 8D; 9A AND 12A INOPERATIVE. REPLACED BATTERY PACK AND CHARGER ASSEMBLY IAW AMM 33-51-06, OPS CHECKED GOOD.
- [SDR SWAA2022120277656](https://openairdocs.org/sdr/SWAA2022120277656), Dec 2, 2022: CHARGER. INOPERATIVE. ENEMERGENCY LIGHTS AT SEAT 6C; 8D; 9A AND 12A INOPERATIVE. REPLACED BATTERY PACK AND CHARGER ASSEMBLY PER AMM 33-51-06;OPS CHECK GOOD

All 253: https://openairdocs.org/aircraft/N569WN/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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