# Service difficulty reports: N444WN

A list on [N444WN](https://openairdocs.org/aircraft/N444WN.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 7 · 336 reports

- [SDR SWAA2026092247064](https://openairdocs.org/sdr/SWAA2026092247064.md): Sleeve · missing · Sep 21, 2026 · N444WN · Boeing 7377H4 · Emergency Equipment
  > LEFT SIDE AFT SERVICE DOOR GIRT BAR LOCKING SLEEVE MISSING. CONFIRMED REAR RELEASE STOP AY WAS MISSING. INSTALLED LT AFT SERVICE DOOR GIRT BAR LOCKING SLEEVE IAW AMM 25-66-00.
- [SDR SWAA2026070618708](https://openairdocs.org/sdr/SWAA2026070618708.md): Sensor · faulted · Jul 4, 2026 · N444WN · Boeing 7377H4 · Trailing Flap Position Indicating System
  > ON APPROACH FLAPS STUCK AT THE 10 POSITION. R & R T/E SKEW SENSOR NR 5 IAW AMM 27-59-01. OPS CHECKED GOOD. REF AHM - FLAP SKEW POSITION MARGINS TTG8Q01D16AS.
- [SDR SWAA2026060808495](https://openairdocs.org/sdr/SWAA2026060808495.md): Isolation Mount · cracked · Jun 2, 2026 · N444WN · Boeing 7377H4 · Escape Slide
  > PASSENGER CABIN AFT ENTRY DOOR FORWARD LOWER SLIDE MOUNT ISOLATOR CRACKED. R & R AFT ENTRY DOOR FORWARD LOWER SLIDE MOUNT ISOLATOR IAW AMM 51-40-02.
- [SDR SWAA2026060308507](https://openairdocs.org/sdr/SWAA2026060308507.md): Battery Pack · failed · Jun 2, 2026 · N444WN · Boeing 7377H4 · Emergency Lighting
  > AFT RT EMERGENCY BATTERY PACK M1672 FAILED CAPACITY CHECK. R&R CABIN EMERGENCY BATTERY PACK PER AMM 33-51-06.
- [SDR SWAA2026060308506](https://openairdocs.org/sdr/SWAA2026060308506.md): Battery Pack · failed · Jun 2, 2026 · N444WN · Boeing 7377H4 · Emergency Lighting
  > AFT LT EMERGENCY BATTERY PACK M1673 FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK PER AMM 33-51-06.
- [SDR SWAA2026060308493](https://openairdocs.org/sdr/SWAA2026060308493.md): Lens · out of adjust · Jun 2, 2026 · N444WN · Boeing 7377H4 · Emergency Lighting
  > FWD ENTRY DOOR SIDEWALL EMERGENCY LIGHT LENS NOT ATTACHED<[01] REMOVED AND REPLACED FWD ENTRY DOOR SIDEWALL EMERGENCY EXIT LIGHT ASSY IAW AMM 33-51-01.;[02] INSPECTION VERIFIED CORRECTIVE ACTION TAKEN IN STEP 1.
- [SDR SWAA2026040886783](https://openairdocs.org/sdr/SWAA2026040886783.md): Lamp · inoperative · Apr 6, 2026 · N444WN · Boeing 7377H4 · Emergency Lighting
  > SIDE WALL LIGHT AT RT OVERWING EXIT ROW INOPERATIVE. RELAMPED RH OVERWING EXIT LIGHT IAW AMM 33-21-00. OPS CHECK GOOD
- [SDR SWAA2026030976238](https://openairdocs.org/sdr/SWAA2026030976238.md): Bulkhead Web · cracked · Mar 3, 2026 · N444WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > CRACK INDICATION ON STRINGER 7L OF AFT PRESSURE BULKHEAD CENTER WEB.
- [SDR SWAA2026030973931](https://openairdocs.org/sdr/SWAA2026030973931.md): Stringer · cracked · Feb 24, 2026 · N444WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK INDICATION ON STRINGER 7L OF AFT PRESSURE BULKHEAD CENTER WEB. REPAIRED THE STRINGER IAW EA 26-153-00539.
- [SDR SWAA2026030973417](https://openairdocs.org/sdr/SWAA2026030973417.md): Stringer · cracked · Feb 23, 2026 · N444WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > POSSIBLE CRACK INDICATION ON STRINGER 7L OF AFT PRESSURE BULKHEAD CENTER WEB. REMOVED PRIMER IAW AMM 51-21-11, VERIFIED CRACK IAW NDT MANUAL 51-00-00, PROCEDURE 23, STEP 7.D. (2) DYE PENETRANT. MEASURES.0973,
- [SDR SWAA2025063083931](https://openairdocs.org/sdr/SWAA2025063083931.md): Battery Pack · inoperative · Jun 22, 2025 · N444WN · Boeing 7377H4 · Emergency Lighting
  > ALL LIGHTS ASSOCIATED WITH EMERGENCY BATTERY PACK M1669 ARE INOP.<[01] REMOVED; REPLACED; AND PERFORMED GOOD FUNCTIONAL TEST OF EMERGENCY LIGHTS BATTERY PACK M1669 PER AMM 33-51-06-960-805;[02] VERIFIED CORRECTIVE ACTION COMPLETE
- [SDR SWAA2025063083930](https://openairdocs.org/sdr/SWAA2025063083930.md): Battery Pack · inoperative · Jun 22, 2025 · N444WN · Boeing 7377H4 · Emergency Lighting
  > ALL LIGHTS ASSOCIATED WITH EMERGENCY BATTERY PACK M1674 ARE INOP<[01] REMOVED REPLACED AND PERFORMED GOOD FUNCTIONAL TEST OF EMERGENCY LIGHT BATTERY PACK M1674 PER AMM 33-51-06-960-805;[02] VERIFIED ACTION 1
- [SDR SWAA2025063082311](https://openairdocs.org/sdr/SWAA2025063082311.md): Frame · cracked · Jun 16, 2025 · N444WN · Boeing 7377H4 · Fuselage Main, Frame
  > FORWARD ENTRY DOOR CUTOUT CRACK IN FRAME I/B RADIUS AT BS312 STR 5L (MARKED)<[01] REPAIR ACCOMPLISHED AT M-22-153-01244 (737-NG - SWA - BS 312 FRAME UPPER CHORD CRACK DAMAGE AT LBL 33 BETWEEN S-5L AND S-6L)<BR>'EA-GENERAL' REPAIR REFERENCE IS SELECTED.;[02] VE
- [SDR SWAA2025063082147](https://openairdocs.org/sdr/SWAA2025063082147.md): Rib · cracked · Jun 15, 2025 · N444WN · Boeing 7377H4 · Wing, Rib/Bulkhead
  > RIGHT WING DEFLECTION RIB TO WEB; OB CLIP IS CRACKED<[01] REMOVED AND REPLACED RIGHT WING DEFLECTION RIB TO WEB; OB CLIP IAW SRM 51-40-02<BR>DESC: CLIP<BR>P/N: 115A6260-2;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2025063080934](https://openairdocs.org/sdr/SWAA2025063080934.md): Stringer Clip · cracked · Jun 12, 2025 · N444WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > FUSELAGE STATION PSX STRINGER CLIP STA 727C; S-5L HAS CRACKED<[01] REMOVED AND INSTALLED STR CLIP AT PAX CABIN STA 727C; S-5L IAW SRM 51-40-02. AND DWG NBR 146A1103;[02] CORRECTION ACTION ITEM 1: DWG NBR 146A1103 REV -;[03] VERIFIED CORRECTIVE ACTIONS 1 AND 2
- [SDR SWAA2025063080933](https://openairdocs.org/sdr/SWAA2025063080933.md): Stringer Clip · cracked · Jun 12, 2025 · N444WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > FUSELAGE STATION PSX STRINGER CLIP STA 727B; S-6L HAS CRACKED<[01] REMOVED AND INSTALLED STR CLIP AT PAX CABIN STA 727B; S-6L IAW SRM 51-40-02 AND DWG NBR 146A1102;[02] CORRECTION ACTION ITEM 1: DWG NBR 146A1102 REV. -;[03] VERIFIED CORRECTIVE ACTIONS 1 AND 2
- [SDR SWAA2025063080398](https://openairdocs.org/sdr/SWAA2025063080398.md): Floor Panel · pulled · Jun 10, 2025 · N444WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231XF WITH AREAS OF PULLED STRANDS ON UPPER SKIN WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810 ID:0007;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2025063080399](https://openairdocs.org/sdr/SWAA2025063080399.md): Floor Panel · pulled · Jun 10, 2025 · N444WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241AF WITH AREAS OF PULLED UPPER STRANDS WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810 ID:0008;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2025063080400](https://openairdocs.org/sdr/SWAA2025063080400.md): Floor Panel · pulled · Jun 10, 2025 · N444WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241BF WITH AREAS OF PULLED STRANDS WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810 ID:0132;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2025063080401](https://openairdocs.org/sdr/SWAA2025063080401.md): Floor Panel · pulled · Jun 10, 2025 · N444WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 242AF UPPER SKINHAS AREAS OF PULLED STRANDS.<[01] PANEL 242AF WITH AREAS OF PULLED STRANDS WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810 ID:0132;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2025063080182](https://openairdocs.org/sdr/SWAA2025063080182.md): Attach Angle · cracked · Jun 10, 2025 · N444WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED ATTACH ANGLE AT PASSENGER COMPARTMENT BS 706; LBL 1; WL 208. MARKED<[01] REMOVED AND REPLACED NEW ATTACH ANGLE ON PASSENGER COMPARTMENT BS706 LBL1 IAW SRM 51-40-02 AND DWG 273A9110 ID: 0002 REV: A;[02] VERIFIED CORRECTIVE ACTION 1.
- [SDR SWAA2025040922278](https://openairdocs.org/sdr/SWAA2025040922278.md): Flap · delaminated · Apr 7, 2025 · N444WN · Boeing 7377H4 · Trailing Edge Flaps
  > RH OUTBOARD AFT FLAP (PN: 113A3700-20; SN: 997) UPPER SKIN DELAMINATION AT INBOARD EDGE <[01]. REMOVED R/H O/B AFT. FLAP PER AMM 27-51-22; [02] OK TO INSTALL NEW FLAP; [03] INSTALLED RH OB AFT FLAP PER AMM 27-51-22.; [04] INSTALLED RH OB AFT FLAP PER AMM 27-5
- [SDR SWAA2025040821719](https://openairdocs.org/sdr/SWAA2025040821719.md): Skin · debonded · Apr 5, 2025 · N444WN · Boeing 7377H4 · Trailing Edge Flaps
  > RIGHT OUTBOARD AFT FLAP UPPER SKIN DISBONDED AT INBOARD EDGE; 10 INCHES FROM AFT EDGE (NOT DELAMINATED)<[01] REPAIRED PER EA 25-157-00897.
- [SDR SWAA2025031906544](https://openairdocs.org/sdr/SWAA2025031906544.md): Girt Bar · loose · Mar 18, 2025 · N444WN · Boeing 7377H4 · Emergency Equipment
  > FWD R/H SERVICE DOOR ESCAPE SLIDE GIRT BAR NEEDS TO BE RE SECURED.<[01] RE SECURED FWD R/H SERVICE DOOR ESCAPE SLIDE GIRT BAR PER MM 25-66-01
- [SDR SWAA2024082227511](https://openairdocs.org/sdr/SWAA2024082227511.md): Mount · broken · Aug 19, 2024 · N444WN · Boeing 7377H4 · Emergency Lighting
  > CENTER AISLE OVERWING EXIT LIGHT ASSY HAS BROKEN MOUNTING BRACKETS<[01] R/R CENTER AISLE OVERWING EXIT LIGHT ASSY REF AMM 33-51-01. OPS CHECKS GOOD AT THIS TIME.
- [SDR SWAA2024072617582](https://openairdocs.org/sdr/SWAA2024072617582.md): Seat · loose · Jul 26, 2024 · N444WN · Boeing 7377H4 · Passenger Compartment Equipment
  > CABIN SEAT ROWS LOOSE IN TRACK AT 21ABC;20ABC;17ABC AND 11ABC<[01] SECURED CABIN SEATS TO FLOOR TRACK AT ROWS 21ABC; 20ABC; 17ABC AND 11ABC IN REF AMM 25-22-00.
- [SDR SWAA2024050181299](https://openairdocs.org/sdr/SWAA2024050181299.md): Lens · out of adjust · Apr 30, 2024 · N444WN · Boeing 7377H4 · Emergency Lighting
  > CREW REPORTED CEILING EXIT LIGHT LENS CAME OFF<[01] REINSTALLED LENS I/A/W 33-51-01
- [SDR SWAA2024021952547](https://openairdocs.org/sdr/SWAA2024021952547.md): Sensor · faulty · Feb 14, 2024 · N444WN · Boeing 7377H4 · Landing Gear Position and Warning
  > FWD NOSE GEAR INDICATED RED; UPPER NOSE GEAR INDICATED GREEN. AIRSPEED WAS 250K; LOWERED GEAR BELOW 230K.<[01] PERFORMED FIM 32-61013 NOSE DOWN DISAGREE; R&R NOSE GEAR DOWN SENSOR S835 PER AMM 32-61-51. SYSTEM OPS CHECK GOOD PER AMM 32-61-51 PERFORMED FIM 32-
- [SDR SWAA2023081484695](https://openairdocs.org/sdr/SWAA2023081484695.md): Angle · cracked · Aug 1, 2023 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK FOUND AT I/B FASTENER HOLE OF LOWER SUPPORT ANGLE FOR APU REMOTE CONTROL PANEL P-28. CRACK EXTENDS I/B AND O/B FROM BOTH SIDES OF THE HOLE.<[01] CERTIFIED WORK STEPS. APU REMOTE CONTROL PANEL LWR SUPPORT ANGLE REMOVED - FABRICATED NEW - INSTALLED.
- [SDR SWAA2023081480555](https://openairdocs.org/sdr/SWAA2023081480555.md): Light · disconnected · Jul 19, 2023 · N444WN · Boeing 7377H4 · Emergency Lighting
  > EXTERIOR AFT RIGHT OVERWING SLIDE EMERGENCY LIGHT INOP. T/S AND REPAIR<[01] RESECURED CONNECTOR AT EXTERIOR AFT RIGHT OVERWING SLIDE EMERGENCY LIGHT; TEST FOUND OK; AS PER REF B737 AMM 33-51-04-960-801; WDM 33-51-12.;[02] VERIFIED SECURED AND TESTED; OK.
- [SDR SWAA2023081479311](https://openairdocs.org/sdr/SWAA2023081479311.md): Battery Pack · inoperative · Jul 16, 2023 · N444WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHTS ARE INOPERATIVE AT 11CB;9 CBA; 4 CBA; AND R-1 DOOR<[01] REMOVED AND REPLACED POWER SUPPLY - BATTERY PACK M1675 AND M1670 AS PER REF AMM 33-51-06-960-805. TEST FOUND NORMAL.;[02] INSP. VERIFIED ENTRY #1 WAS WORK ACCOMPLISHED.
- [SDR SWAA2023081476248](https://openairdocs.org/sdr/SWAA2023081476248.md): Scuff Plate · cracked · Jul 7, 2023 · N444WN · Boeing 7377H4 · Passenger Compartment Equipment
  > R-1 DOOR CENTER SCUFF PLATE CRACKED AT AFT EDGE<[01] R 1 DOOR CENTER SCUFF PLATE; WELDING REPAIR WAS ACCOMPLISH BY OUTSIDE VENDOR JDL WELDING UNDER PO414104;[02] VERIFIED WELDING REPAIR BY JDL WELDING UNDER PO414104
- [SDR SWAA2023081475666](https://openairdocs.org/sdr/SWAA2023081475666.md): Panel · corroded · Jul 5, 2023 · N444WN · Boeing 7377H4 · Accessory Compartment Doors
  > CORROSION: NOSE WHEEL WELL PANEL #114AC INB SIDE ALL AROUND. CORRECTION TO FAULT DESCRIPTION. CORROSION: NOSE WHEEL WELL PANEL #113AC INB SIDE ALL AROUND.<[01] REPLACED NOSE WHEEL WELL ACCESS PANEL 113AC REF. B737-700 AMM 53-14-01-420-801. ACCESS PANEL 113AC W
- [SDR SWAA2023081475667](https://openairdocs.org/sdr/SWAA2023081475667.md): Panel · corroded · Jul 5, 2023 · N444WN · Boeing 7377H4 · Accessory Compartment Doors
  > CORROSION: NOSE WHEEL WELL ACESS PANEL # 114AC INTERNAL SIDE; CORROSION ALL AROUND.<[01] AFTER REMOVED CORROSION ON SOME AREAS FOUND CORROSION GOING THRU GASKET - O - SEAL CAVITY REF. B737-700 SRM 53-10-14-1A. DOOR WILL BE REPLACE;[02] REPLACED NOSE WHEEL WELL
- [SDR SWAA2023081474578](https://openairdocs.org/sdr/SWAA2023081474578.md): Pan · cracked · Jul 3, 2023 · N444WN · Boeing 7377H4 · Passenger/Crew Doors
  > AFT ENTRY DOOR (L 2) INNER LOWER PAN ASSY AFT AND FWD BRACKET ARE CRACKED<[01] REMOVED AND REPLACED NEW AFT ENTRY L-2 DOOR INNER LOWER PAN ASSY AFT AND FWD BRACKETS REF USED B737-7 SRM 51-40-02-0G-0;[02] VERIFIED STEP 1.
- [SDR SWAA2023081474235](https://openairdocs.org/sdr/SWAA2023081474235.md): Baffle · cracked · Jul 2, 2023 · N444WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > FWD CARGO LEFT SIDE BAFFLE IS CRACKER AT 440 BELOW 'Z' CHANNEL STRINGER 25 L<[01] REMOVED AND REPLACED SIDE BAFFLE AT FWD CARGO STA 440 STRINGER 25L PER B737-700 SRM 51-40-02-0G-0 & DRWN# 143A7505.;[02] CERTIFIED WORK PERFOMED SIDE BAFFLE AT FWD CARGO STA 440
- [SDR SWAA2023081473555](https://openairdocs.org/sdr/SWAA2023081473555.md): Door · corroded · Jun 30, 2023 · N444WN · Boeing 7377H4 · Cargo/Baggage Doors
  > CORROSION FOUND AFT CARGO DOOR INTERNAL LOWER FWD AREA HAS SPOTS OF CORROSION.<[01] FOUND CORROSION EXFOLIATION OUT OF LIMITS AS PER SRM 52-30-01-1A-1 AND REMOVED AND REPLACED AFT CARGO DOOR IN REFERENCE AMM 52-31-00-000-801 AND AMM 52-31-00-400-801.;[02] RII
- [SDR SWAA2023081471799](https://openairdocs.org/sdr/SWAA2023081471799.md): Baffle · cracked · Jun 26, 2023 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMP. L/H SIDE BELOW SIDEPLATE STA 500 THRU 500A BAFFLE ASSY WITH CRACK AT LBL 23<[01] REMOVED AND REPLACED FWD CARGO COMP. BAFFLE ASSY L/H SIDE BELOW SIDEPLATE STA 500 THRU 500A PER B737-700 SRM 51-40-02-0G-0 AND DRAW. 143A7505;[02] CERTIFIED WORK S
- [SDR SWAA2023081471798](https://openairdocs.org/sdr/SWAA2023081471798.md): Baffle · cracked · Jun 26, 2023 · N444WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > FWD CARGO COMP. L/H SIDE BELOW SIDEPLATE STA 500A THRU 500B BAFFLE ASSY WITH CRACKAT LBL 23<[01] REMOVED AND REPLACED BAFFLE ASSY AT FWD CARGO COMP. L/H SIDE BELOW SIDEPLATE STA 500A THRU 500B;PER B 737-700 SRM 51-40-02-0G-0;[02] VERIFIED STEP 1.
- [SDR SWAA2023081471511](https://openairdocs.org/sdr/SWAA2023081471511.md): Scuff Plate · cracked · Jun 25, 2023 · N444WN · Boeing 7377H4 · Fuselage Main, Structure
  > FOUND AFT CARGO COMPARTMENT CENTER SCUFF PLATE CRACKED AT FORWARD EDGE<[01] ACCOMPLISHED WELDING AT AFT CARGO DOOR CENTER SCUFF PLATE OUTSIDE BY J.L WELDNG VENDOR FAA REPAIR STATION # JLWR146K AS PER SRM 53-60-15-2R-1 AND BAC5975;[02] VERIFIED STEP 1.
- [SDR SWAA2023081460727](https://openairdocs.org/sdr/SWAA2023081460727.md): Bracket · cracked · Jun 19, 2023 · N444WN · Boeing 7377H4 · Passenger/Crew Doors
  > AFT ENTRY DOOR SLIDE FWD BRACKET SHOCK MOUNT CRACKED<[01] ENTER IN ERROR - DUPLICATE ITEM - THIS FAULT WILL BE ACCOMPLISHED ON FAULT # TTG8Q00L61Y;[02] VERIFIED TTG8Q00L61Y
- [SDR SWAA2023081460415](https://openairdocs.org/sdr/SWAA2023081460415.md): Stringer · cracked · Jun 18, 2023 · N444WN · Boeing 7377H4 · Fuselage Main, Structure
  > FWD CABIN WET AREA STRINGER CRACKED @ STA 294.5 S-8L MKD DOT<[01] ACCOMPLISHED STRINGER REPAIR AT LT FUSELAGE STRINGER 8-L FROM STA 286 TO STA 300 REF USED B737-7 SRM 53-00-03-2R-1 FIG 205 DETAIL A-A;[02] VERIFIED WORK STEPS ACCOMPLISHED FOR STRINGER REPAIR AT
- [SDR SWAA2023081460412](https://openairdocs.org/sdr/SWAA2023081460412.md): Support · cracked · Jun 18, 2023 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR CENTER AISLE SUPPORT BREAK CRACKED @ RBL 1 STA 540 WL 208.1<[01] REMOVED FLOOR SUPPORT BREAK ASSY AT STA 540 BTW RBL 1 TO RBL 20 AS PER B737-700 SRM 51-40-02.;[02] LOCATED AND DRILLED NEW FLOOR SUPPORT BREAK ASSY PN 143A5240-36 AT STA 540 BTW
- [SDR SWAA2023081460413](https://openairdocs.org/sdr/SWAA2023081460413.md): Support · cracked · Jun 18, 2023 · N444WN · Boeing 7377H4 · Wing Main, Frame Structure
  > MAIN CABI CENTER WING BOX FLOOR SUPPORT INNER CHORD CRACKED AT STA 520 LBL 64 WL 208.1<[01] VERIFIED / INSPECTED REPAIR ACCOMPLISHED AT CABIN FLOOR STRUCTURE STA 520 LBL 64 WL 208.1. FABRICATED PARTS REPAIR DOUBLERS. INSTALLED. REF. FABRICATED INNER CHORD CREA
- [SDR SWAA2023081459853](https://openairdocs.org/sdr/SWAA2023081459853.md): Slide · damaged · Jun 16, 2023 · N444WN · Boeing 7377H4 · Escape Slide
  > R-1 DOOR ESCAPE SLIDE GIRT FABRIC FRAYED AT BOTTOM.<[01] REMOVED AND REPLACED FWD SERVICE DOOR MOUNTED SLIDE. REF B 737 AMM 25-66-01-401;[02] VERIFIED SLIDE REPLACEMENT.
- [SDR SWAA2023081459854](https://openairdocs.org/sdr/SWAA2023081459854.md): Slide · out of adjust · Jun 16, 2023 · N444WN · Boeing 7377H4 · Escape Slide
  > R-1 DOOR ESCAPE SLIDEGIRT BAR; BOTH RETAINER CLIPS HAVE LOOSE RIVETS.<[01] REMOVED AND REPLACED FASTENER. AT R-1 DOOR ESCAPE SLIDEGIRT BAR USED REFERENCE B-737.SRM- 51-40-05-0G-0;[02] TO CORRECT REFERENCE ON STEP 1 SHOULD BE SRM 51-40-02-0G-0;[03] VERIFIED STE
- [SDR SWAA2023081460389](https://openairdocs.org/sdr/SWAA2023081460389.md): Slide · out of adjust · Jun 16, 2023 · N444WN · Boeing 7377H4 · Escape Slide
  > L-1 DOOR ESCAPE SLIDE GIRT BAR BOTH RETAINER CLIPS HAVE LOOSE RIVETS.<[01] REMOVED AND REPLACED FASTENER. USED REFERENCE B-737.SRM- 51-40-05-0G-0;[02] TO CORRECT REFERENCE ON STEP 1 SHOULD BE SRM 51-40-02-0G-0;[03] VERIFIED STEP 1 AND 2.
- [SDR SWAA2023081459844](https://openairdocs.org/sdr/SWAA2023081459844.md): Bracket · cracked · Jun 16, 2023 · N444WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > AFT CARGO AT STA 867 LBL 10 WL 155.5 BRACKET CRACK.<[01] REMOVED AND REPLACED AFT CARGO BRACKET AT STA 867; LBL 10; WL 155.5 AS PER SRM 51-40-02-0G-0 AND DWG 149A8102;[02] VERIFIED STEP 1.
- [SDR SWAA2023081459840](https://openairdocs.org/sdr/SWAA2023081459840.md): Channel · corroded · Jun 16, 2023 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION FOUND AFT CARGO RH 'Z' CHANNEL FROM STA 727D TO STA 727E RBL 21 WL 155.5 HAS SPOTS OF CORROSION.<[01] REMOVED CORROSION AT AFT CARGO RH 'Z' CHANNEL FROM STA 727D TO STA 727E RBL 21 WL 155.5.ORIGINAL MATERIAL 0.040'; MATERIAL LOST 0.012'; MATERIAL RE
- [SDR SWAA2023081459841](https://openairdocs.org/sdr/SWAA2023081459841.md): Channel · corroded · Jun 16, 2023 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION FOUND AFT CARGO RH 'Z' CHANNEL FROM STA 727E TO STA 747 RBL 21 WL 155.5 HAS SPOTS OF CORROSION.<[01] REPAIR WAS ACCOMPLISHED IN THE ITEM TTG8Q00LP0BE;[02] VERIFIED ENTRY #1 AS WORK ACCOMPLISHED & WORK REMAINING WILL BE ON ' TTG8Q00LP0BE ' UNTIL APPLI

Next page: https://openairdocs.org/aircraft/N444WN/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N444WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N444WN/reports

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