# N558WN: 2002 Boeing 737-73V

- Status: Valid registration
- Airframe: [Boeing 737-73V](https://openairdocs.org/model/boeing-737-73v) (registry code 1384540, 149 seats)
- Engine: [CFM International CFM56-7B24 series](https://openairdocs.org/engine/cfm-international-cfm56-7b24-series) (registry code 13044)
- Serial number: 30248
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 28, 2015
- Certificate issued: July 15, 2024
- Expires: July 31, 2031
- Mode S code: A71F24
- 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=558WN
- Page: https://openairdocs.org/aircraft/N558WN

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 737-73V)

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 N558WN.

## FAA accident and incident reports

None matched to N558WN.

## Service difficulty reports (243, 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 SWAA2024110857947](https://openairdocs.org/sdr/SWAA2024110857947), Nov 7, 2024: ESCAPE ROPE. DETACHED. F/O EMERGENCY ESCAPE ROPE DOOR DETACHED DURING PRE-FIGHT<[01] RESECURED DOOR IAW M/M 25-00-00.
- [SDR SWAA2024110154812](https://openairdocs.org/sdr/SWAA2024110154812), Oct 30, 2024: LIGHT. LOOSE. THE VERY AFT SMALL PORTION OF THE PHOTOLUMINESCENT STRIP BEHIND ROW 24ABC IS LOOSE.<[01] SECURED PHOTOLUMINESCENT STRIP PER M/M 33-51-15.
- [SDR SWAA2024110154814](https://openairdocs.org/sdr/SWAA2024110154814), Oct 30, 2024: BATTERY PACK. NO TEST. R/H AFT EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.
- [SDR SWAA2024081324965](https://openairdocs.org/sdr/SWAA2024081324965), Aug 12, 2024: PANEL. DELAMINATED. WING TO BODY FAIRING PANEL 193B IS DELAMINATED AT ONE FASTENER HOLE ON FWD EDGE OF PANEL.<[01] REMOVED AND REPLACED WING TO BODY PANEL 193B IAW AMM 53-51-21.
- [SDR SWAA2024071008794](https://openairdocs.org/sdr/SWAA2024071008794), Jul 3, 2024: BATTERY PACK. INOPERATIVE. FWD RIGHT EMERGENCY BATTERY PACK M1674 WILL NOT CHARGE FWD RIGHT EMERGENCY BATTERY PACK WILL NOT CHARGE<[01] REMOVED AND REPLACED FWD RIGHT EMERGENCY PACK M1674
- [SDR SWAA2024070908653](https://openairdocs.org/sdr/SWAA2024070908653), Jul 3, 2024: HANDLE. LOOSE. L-2 DOOR LINER ASSIST HANDLE IS LOOSE.<[01] SECURED L-2 DOOR LINER ASSIST HANDLE I/A/W AMM 52-13-31-400-802 STEP 3.G.(2);[02] VERIFIED ITEM 1<BR>AUDIT C/W
- [SDR SWAA2024070908655](https://openairdocs.org/sdr/SWAA2024070908655), Jul 3, 2024: HANDLE. LOOSE. ASSIST HANDLES AT G-1 GALLEY AND R-1 DOOR LINER ARE LOOSE.<[01] SECURED ASSIST HANDLES AT G-1 GALLEY AND R-1 DOOR LINER I/A/W AMM 52-41-31-400-802 STEP 3.F.(2) 
- [SDR SWAA2024071006860](https://openairdocs.org/sdr/SWAA2024071006860), Jun 28, 2024: BATTERY PACK. INOPERATIVE. RIGHT SIDE EMERGENCY LIGHTS INOP FROM OVERWING EMERGENCY EXIT FWD<[01] REMOVED AND REPLACED RH BATTERY PACK AT RH OVERWING EXIT IAW AMM 33-51-06-960-805. OPS CH
- [SDR SWAA2024071006857](https://openairdocs.org/sdr/SWAA2024071006857), Jun 28, 2024: BATTERY PACK. INOPERATIVE. LEFT SIDE EMERGENCY LIGHTS INOP FROM SEAT 6ABC FWD<[01] REMOVED AND REPLACED FWD CABIN LEFT SIDE BATTERY PACK IAW 33-51-06-960-805. ALL CHECKS GOOD<BR>A TAG#WN4
- [SDR SWAA2024071006278](https://openairdocs.org/sdr/SWAA2024071006278), Jun 26, 2024: SPAR. CORRODED. FOUND CORROSSION ON RIGHT WING; FORWARD SPAR; LOWER CHORD AT WS 290. REF. TTG8Q00U749A.<[01] FAULT RESOLVED ON EA 24-157-01775-WIP1 AND WIP2;[02] AUDIT C/W
- [SDR SWAA2024062705817](https://openairdocs.org/sdr/SWAA2024062705817), Jun 26, 2024: BATTERY PACK. FAILED. BOTH FWD ENTRY AND SERVICE DOOR EMERGENCY EXIT LIGHTS SHUTOFF WITHIN SECONDS AFTER TURNING ON FLIGHT DECK EMERGENCY LIGHT SWITCH.<[01] C/W BATTERY PACK DEEP CYC
- [SDR SWAA2024061401799](https://openairdocs.org/sdr/SWAA2024061401799), Jun 14, 2024: LAMP. INOPERATIVE. LH AFT BOTTOM EMERGENCY LIGHT OUT<[01] RE-LAMPED LH AFT BOTTOM EMERGENCY LIGHT REF AMM 33-51-04. OPS CHECK GOOD.
- [SDR SWAA2024050181244](https://openairdocs.org/sdr/SWAA2024050181244), May 1, 2024: LAMP. FAILED. FORWARD SERVICE DOOR EMERGENCY ESCAPE SLIDE EMERGENCY LIGHT WILL NOT ILLUMINATE. RELAMPED FORWARD SERVICE DOOR EMERGENCY ESCAPE SLIDE EMERGENCY LIGHT; OPS CHECK
- [SDR SWAA2024012944807](https://openairdocs.org/sdr/SWAA2024012944807), Jan 26, 2024: SKIN. DELAMINATED. LEFT WING OUTBOARD TRAILING EDGE FLAP DELAMINATED ON INBOARD EDGE.<[01] C/W EA 24-127-00235
- [SDR SWAA2023031616736](https://openairdocs.org/sdr/SWAA2023031616736), Mar 14, 2023: SLIDE. OUT OF ADJUST. ENTRY DOOR SLIDE APPEARS TO HAVE INADVERTENTLY MOVED OUT OF PLACE<[01] INSPECTED FORWARD ENTERY DOOR SLIDE PER AMM 25-66-01; ARMED AND UNARMED SLIDE PACK SEVERA
- [SDR SWAA2023022805047](https://openairdocs.org/sdr/SWAA2023022805047), Feb 20, 2023: BATTERY PACK. DEFECTIVE. DURING EMERGENCY LIGHT TEST FOUND BATTERY PACK POS M1670 DEFECTIVE.<[01] REPLACED BATTERY PACK POS M1670 S/N 1536 OFF WITH BATTERY PACK S/N WN1766 ON AS PER REF
- [SDR SWAA2023022804529](https://openairdocs.org/sdr/SWAA2023022804529), Feb 17, 2023: BATTERY PACK. INOPERATIVE. LEFT OVERWING EXIT EMERGENCY EXIT SIGNS LIGHTS INOP.<[01] REMOVED AND REPLACE POWER SUPPLY BATTERY PACK PER REFERENCE AMM 33-51-06-960-805. PERFORMED OPERATION 
- [SDR SWAA2023022804530](https://openairdocs.org/sdr/SWAA2023022804530), Feb 17, 2023: COVER. MISSING. AFT ENTRY AND SERVICE DOORS EXIT EMERGENCY SINGS LENS COVER MISSING.<[01] INSTALLED AFT ENTRY SERVICE DOORS EXIT EMERGENCY SINGS LENS COVER AS PER B737 AMM 33-5
- [SDR SWAA2023022899099](https://openairdocs.org/sdr/SWAA2023022899099), Feb 4, 2023: PLATE. CRACKED. PNL 651GB HAS CRACKER WOBBLE PLATE.<[01] REMOVED AND REPLACED WOBBLE PLATE AT R/W T/E IAW B-737-700 SRM-51-40-02-0G-0;[02] VERIFIED STEP 1
- [SDR SWAA2023022897766](https://openairdocs.org/sdr/SWAA2023022897766), Feb 1, 2023: SHIELD. CRACKED. NO-1 ENG I/B FAN COWL INTERNAL INTERCOSTAL CRACKED @ UPPER EDGE AFT OF ENG SERVICE OIL ACCESS DOOR MKD DOT<[01] REMOVED 1EA DAMAGED SHIELD FROM NO-1 ENG I/B FAN
- [SDR SWAA2023022897765](https://openairdocs.org/sdr/SWAA2023022897765), Feb 1, 2023: SHIELD. CRACKED. NO 2 ENG O/B FAN COWL INTERNALINTERCOSTAL CRACKED @ UPPER EDGE AFT ENG SERVICE OIL ACCESS DOOR MKD DOT<[01] REMOVED 1 OFF E/A DAMAGED SHIEL FROM NO2ENG O/B FAN 
- [SDR SWAA2023022897312](https://openairdocs.org/sdr/SWAA2023022897312), Jan 31, 2023: DOOR. OUT OF ADJUST. ACCOMPLISH FORWARD SERVICE DOOR ADJUSTMENT<[01] PARTIAL ADJUSTED FORWARD SERVICE DOOR IN REF . B737 AMM 52-41-00-820-801 STEPS 2A TO 2Q;[02] ADJUSTED FORWARD SE
- [SDR SWAA2023022800443](https://openairdocs.org/sdr/SWAA2023022800443), Jan 31, 2023: PANEL. CRACKED. RIGHT WING LOWER T/E ACCESS PANEL # 661BB HAS BULGING/CRACKED FASTENER HOLES<[01] PREPARED FOR REPAIR PANEL 661 BB; AS PER B737 SRM 51-70-04-2R-9;[02] OK TO ACC
- [SDR SWAA2023022796654](https://openairdocs.org/sdr/SWAA2023022796654), Jan 29, 2023: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL #241DF DELAMINATED.<[01] RECEIVED NEW PANEL #241DF. PANEL WILL BE INSTALLED ON CLOSING CARD # TTG8Q00GK96W;[02] VERIFIED STEP 1.
- [SDR SWAA2023022796656](https://openairdocs.org/sdr/SWAA2023022796656), Jan 29, 2023: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL #231XF DELAMINATED.<[01] RECEIVED NEW FLOOR PANEL. INSTALLATION WILL BE ACCOMPLISHED ON ITEM TTG8Q00GK97E.;[02] RECEIVED NEW FLOOR PANEL 231XF
- [SDR SWAA2023022796657](https://openairdocs.org/sdr/SWAA2023022796657), Jan 29, 2023: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL #241AF DELAMINATED.<[01] RECEIVED NEW FLOOR PANEL 241AF. INSTALLATION WILL BE ACCOMPLISHED ON ITEM TTG8Q00GK972.;[02] VERIFIED STEP #1.
- [SDR SWAA2023022896434](https://openairdocs.org/sdr/SWAA2023022896434), Jan 28, 2023: HANDLE. LOCKED. L1 DOOR ASSIST HANDLE LOOSE.<[01] IN REFERENCE TTG8Q00HKJT7;[02] VERIFIED STEP 1
- [SDR SWAA2022111068837](https://openairdocs.org/sdr/SWAA2022111068837), Nov 8, 2022: LIGHT. INOPERATIVE. LEFT FWD EMERGENCY EXIT LIGHT LEFT OF FWD F/A SEAT INOP / [01] REMOVED AND REPLACED LEFT FWD EXIT SIGN LEFT OF FWD FA SEAT REF AMM 33-51-01. OPS CHECK GOOD
- [SDR SWAA2022081540960](https://openairdocs.org/sdr/SWAA2022081540960), Aug 11, 2022: LIGHT. INOPERATIVE. OVERWING EMERGENCY EXIT SIDEWALL LIGHT INOP CAPT SIDE. OVERWING EMERGENCY EXIT SIDEWALL LIGHT INOP CAPT SIDE.DAL MX STATES IT NEED A BALLAST. SIDEWALLS NEED REM
- [SDR SWAA2022052510612](https://openairdocs.org/sdr/SWAA2022052510612), May 24, 2022: LIGHT. INOPERATIVE. AFT RH EXTERIOR EMERGENCY LIGHT OUT / [01] RELAMPED AFT RH EXTERIOR EMERGENCY LIGHT PER AMM 33-51-04
- [SDR SWAA2022022172577](https://openairdocs.org/sdr/SWAA2022022172577), Feb 15, 2022: BRACKET. BROKEN. KEEL BEAM PANEL 192E FOWARD L/H SUPPORT BRACKET BROKEN / [01] REMOVE AND REPLACED KEEL BEAM PANEL 192E FWD L/H SUPPORT BRACKET IAW SRM 51-40-02.
- [SDR SWAA2022020265510](https://openairdocs.org/sdr/SWAA2022020265510), Jan 29, 2022: PANEL. CRACKED. 193D PANEL HAS TWO FASTENER HOLE WITH CRACKS EMANATING FROM HOLES.(MARKED) / [01] REPLACED PANEL 193D; REF AMM 53-51-21; TSR 202200756
- [SDR SWAA2022020265511](https://openairdocs.org/sdr/SWAA2022020265511), Jan 29, 2022: PANEL. CRACKED. 194E PANEL HAS TWO FASTENER HOLES WITH CRACKS EMANATING FROM HOLES. (MARKED) / [01] INSTALLED NEW PANEL IAW 53-51-21. REF TSR 202200756
- [SDR SWAA2022012562831](https://openairdocs.org/sdr/SWAA2022012562831), Jan 21, 2022: FLAP SYSTEM. FAILED. ON APPROCH FLAPS STOPPED AT 25 NO ASSYBELLY BRAKE FLAG / [01] CHECKED FSEU FOR FAULTS NO CURRENT FAULTS NOTED PERFORMED AMM 27-51-00 AND FIM 27-51 TASK 836 AS R
- [SDR SWAA2021081605794](https://openairdocs.org/sdr/SWAA2021081605794), Aug 10, 2021: RETAINER. OUT OF ADJUST. FWD SERVICE GIRT BAR FALLS OUT OF CLIPS ; / [01] INSPECTED BAR CLIPS & NO DAMAGE NOTED. ADJUSTED CLIPS PER SIP
- [SDR SWAA2021052776182](https://openairdocs.org/sdr/SWAA2021052776182), May 23, 2021: SUPPORT BEAM. CRACKED. L/H WING LINK ASSY - LWR STAB CRACKED. R & R SUPPORT BEAM IAW AMM 57-15-00. R/R SUPPORT BEAM AS PER AMM 57-15-00. VERIFIED R/R SUPPORT BEAM AS PER AMM 57-15-00.
- [SDR SWAA2021052575720](https://openairdocs.org/sdr/SWAA2021052575720), May 21, 2021: TIRE. BLOWN. ABORTED T/O AT 100K DUE TO BOTH LEFT MAIN TIRES BLOWN. NO ABNORMALITIES NOTED BEFORE THE EVENT. / R&R BOTH #1 AND #2 MLG TIRES PER AMM 32-4511
- [SDR SWAA2021052576315](https://openairdocs.org/sdr/SWAA2021052576315), May 21, 2021: TIRE. FAILED. ABORTED T/O AT 100K DUE TO BOTH LEFT MAIN TIRES BLOWN. NO ABNORMALITIES NOTED BEFORE THE EVENT. / R&R BOTH #1 AND #2 MLG TIRES PER AMM 32-4511
- [SDR SWAA2021022246358](https://openairdocs.org/sdr/SWAA2021022246358), Jan 30, 2021: STIFFENER. CRACKED. CRACK STRUCTURE STIFFENER LOCATED FRONT INSPAR RIB 120.30 AT RT HORIZONTAL STABILIZER / REPLACED STIFFENER LOC FRONT INSPAR RIB 120.30 AT RT HORIZONTAL STABILIZ
- [SDR SWAA2021022245661](https://openairdocs.org/sdr/SWAA2021022245661), Jan 28, 2021: BRACKET. CRACKED. CRACK BRACKET LOCATED BS867 AT LEVEL STR26L AT AFT CARGO COMPARTMENT / REPLACED BRACKET LOCATED BS 867 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT IAW B737-700 SR
- [SDR SWAA2021022244716](https://openairdocs.org/sdr/SWAA2021022244716), Jan 25, 2021: NUT PLATE. BROKEN. BROKEN FASTENER NUTPLATE ADF 1 ANTENNA INTERNAL AREA BTW BS685 TO BS706 AND BTW S-1 TO STR 2R AT PASSENGER CABIN (REPAIR FOR SRM 53-40-01-2R-1 IAW WORK INSTRUCT
- [SDR SWAA2021022244715](https://openairdocs.org/sdr/SWAA2021022244715), Jan 22, 2021: BRACKET. CRACKED. CRACK BRACKET LOCATED BS 986 BETWEEN S-26R AND S-26L AT AFT CARGO COMPARTMENT / REPLACED BRACKET LOC BS 986 BETWEEN S-26R TO S-26L AT CARGO COMPARTMENT IAW SRM 
- [SDR SWAA2021051344604](https://openairdocs.org/sdr/SWAA2021051344604), Jan 21, 2021: WEB. DAMAGED. ELONGATED HOLE ANGLE - SUPPORT WEB LOC BTW BS 927 TO BS 947.5 AND BL0 AT AFT GALLEY AREA / REPLACED ANGLE -SUPPORT WEB LOCATED BTW BS927 AND BS947.5 AND BL 0 AT
- [SDR SWAA2021022244713](https://openairdocs.org/sdr/SWAA2021022244713), Jan 21, 2021: LIGHT. BROKEN. BROKEN STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT AT PASSENGER CABIN (10 EA) / REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CAB
- [SDR SWAA2021022244609](https://openairdocs.org/sdr/SWAA2021022244609), Jan 21, 2021: SUPPORT. CORRODED. CORROSION SUPPORT ZEE LOCATED BETWEEN BS 747 TO BS 787; AT LEVEL STRINGER 25L; LBL 21 AFT CARGO COMPARTMENT AT WL 156.1 / REPLACED SECTION SUPPORT ZEE LOCATED B
- [SDR SWAA2021022244611](https://openairdocs.org/sdr/SWAA2021022244611), Jan 21, 2021: FASTENER. WORN. WEAR ON GIRT BAR FITTING HARDWARE (SCREW AND WASHER) AT FWD GALLEY AREA / REPLACED ON GIRT BAR FITTING HARDWARE (SCREW AND WASHER ) AT FED GALLEY AREA IAW AMM 2
- [SDR SWAA2021022244610](https://openairdocs.org/sdr/SWAA2021022244610), Jan 21, 2021: PLATE. WORN. WEAR ON GIRT BAR FITTING ADAPTER PLATE(4EA) AND ALL HARDWARE AT AFT GALLEY AREA / REPLACED GIRT BART FITTING ADAPTER PLATE(4EA) AND ALL HARDWARE AT AFT GALLEY A
- [SDR SWAA2021022249721](https://openairdocs.org/sdr/SWAA2021022249721), Jan 20, 2021: WEB. GOUGED. GOUGE WEB LOCATED BETWEEN BS 328 TO BS 344 AND STR 5R AT FWD GALLEY AREA / PERFORMED REPAIR FWD GALLEY DOOR SURROUND STRUCTURE UPPER AUXILIARY SILL WEB LOC BTW 
- [SDR SWAA2021022244599](https://openairdocs.org/sdr/SWAA2021022244599), Jan 20, 2021: FLOORBEAM. CRACKED. CRACK FLOOR BEAM BS 328 RBL 24 AT FWD GALLEY AREA / PERFORMED REPAIR ON BS 328 LOC. BTW RBL 65 TO LBL 12 IAW B737-700 53-10-51-2R-7 FIG 205 ALTERNATIVE 2; DUE T
- [SDR SWAA2021022244600](https://openairdocs.org/sdr/SWAA2021022244600), Jan 20, 2021: FLOORBEAM. CRACKED. CRACK FLOOR BEAM LOCATED BS 294.5 AND RBL 54 AT FWD GALLEY AREA / PERFORMED PERMANENT REPAIR ON FLOOR BEAM BS 294.5 RBL 17 AND RBL 60 IAW B737-700 SRM 53-10-51-

All 243: https://openairdocs.org/aircraft/N558WN/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

## Earlier aircraft with N558WN

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N558WN before.

- [Cancelled 1971-12-01](https://openairdocs.org/deregistered/N558WN-1971-12-01): Beech C-45H, S/N AF-489. Exported to Panama. Owner: [Trans-Airborne Inc](https://openairdocs.org/faa-owner/TRANS-AIRBORNE%20INC), [Miami, FL](https://openairdocs.org/faa-place/FL/Miami)

## Related

- Other Boeing 737-73V aircraft: https://openairdocs.org/model/boeing-737-73v/aircraft.md
- The CFM International CFM56-7B24 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b24-series.md

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