# Service difficulty reports: N224WN

A list on [N224WN](https://openairdocs.org/aircraft/N224WN.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 6 · 281 reports

- [SDR SWAA2026062415073](https://openairdocs.org/sdr/SWAA2026062415073.md): Fuse · inoperative · Jun 23, 2026 · N224WN · Boeing 7377H4 · Emergency Lighting
  > RIGHT OVERWING EMERGENCY LIGHT COVER MISSING ON BOTTOM RIGHT DOOR AND LIGHT INOPERATIVE. CENTER TOP EMERGENCY LIGHT INOP AS WELL. REMOVED AND REPLACED M1669 POWER SUPPLY FUSES IAW AMM 33-51-06. OPS CHECKED GOOD. INSTALLED NEW EMERGENCY LIGHT COVER ON BOTTOM
- [SDR SWAA2025103130480](https://openairdocs.org/sdr/SWAA2025103130480.md): Sign · out of adjust · Oct 30, 2025 · N224WN · Boeing 7377H4 · Emergency Lighting
  > FORWARD EXIT SIGN BY L1 DOOR FELL OFF. SECURED FWD EMERGENCY EXIT SIGN COVER BY L1 DOOR PER AMM 33-51-01.
- [SDR SWAA2025102928779](https://openairdocs.org/sdr/SWAA2025102928779.md): Strap · broken · Oct 26, 2025 · N224WN · Boeing 7377H4 · Emergency Equipment
  > R2 SAFETY STRAP BROKEN. REPLACED R 2 DOOR SAFETY STRAP PER SIP AND AMM 52-41-31
- [SDR SWAA2025102726133](https://openairdocs.org/sdr/SWAA2025102726133.md): Charger · inoperative · Oct 21, 2025 · N224WN · Boeing 7377H4 · Emergency Lighting
  > RIGHT FWD OVER DOOR EMERGENCY SIGN INOP<[01] R&R CHARGER ASSEMBLY FOR RIGHT FWD OVER DOOR EMERGENCY SIGN PER AMM 33-51-06. OPS CHECK GOOD
- [SDR SWAA2025091212848](https://openairdocs.org/sdr/SWAA2025091212848.md): Fuse · inoperative · Sep 9, 2025 · N224WN · Boeing 7377H4 · Emergency Lighting
  > FED EMERGENCY EXIT LIGHT ON AFT FACE OF LAV-A INOP<[01] OK TO CLOSE STEP 1. REPLACED FUSE OF M1675 BATTERY POWER SUPPLY AND PERFORMED GOOD OPERATIONAL TEST OF FED EMERGENCY EXIT LIGHT ON AFT OF LAV-A IAW B737 AMM 33-51-06-960-804 AND AMM 33-51-00-710-801.
- [SDR SWAA2025091208093](https://openairdocs.org/sdr/SWAA2025091208093.md): Bulkhead · cracked · Aug 25, 2025 · N224WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > B.S. 663 LOWER COMPOSITE BULKHEAD IS CRACKED AT LBL 15; WL 167. BS 663 LOWER COMPOSITE BULKHEAD IS CRACKED AT LBL 15; WL 167; WAS REPAIRED IAW SRM 51-70-04-2R-10.
- [SDR SWAA2025091104028](https://openairdocs.org/sdr/SWAA2025091104028.md): Support Plate · corroded · Aug 13, 2025 · N224WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION FWD CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS500A+1' TO BS500C+10' LBL22 WL156. EVALUATED; LOCATED AND DRILLED; REMOVED AND REPLACED FWD CARGO BAY L/H NEW SECTION FLOOR SIDEWALL SUPPORT PLATE BS480+10 TO
- [SDR SWAA2025091104029](https://openairdocs.org/sdr/SWAA2025091104029.md): Support Plate · corroded · Aug 13, 2025 · N224WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 LBL22 WL156. CORROSION EVALUATION ON ACB L/H FLOOR TO SIDEWALL SUPPORT BS727B TO BS767 LBL22 WL156 WAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-5
- [SDR SWAA2025091104351](https://openairdocs.org/sdr/SWAA2025091104351.md): Strap · corroded · Aug 13, 2025 · N224WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS727D+6' RBL11.5 WL156. EVALUATED CORROSION ON AFT CARGO BAY FLOOR STRAP BS 727D+6 RBL 11.5 WL 156; FOUND TO BE OUT OF LIMITS; RECEIVED NEW STRAP AND APPLIED ENAMEL; ALL PER SRM 51-10-02-0G-0;
- [SDR SWAA2025091503810](https://openairdocs.org/sdr/SWAA2025091503810.md): Skin · delaminated · Aug 12, 2025 · N224WN · Boeing 7377H4 · Trailing Edge Flaps
  > LEFT WING OTBD AFT FLAP INBD UPPER SURFACE DELAMINATED. REMOVED AND REPLACED THE LT WING OTBD AFT FLAP IAW AMM 27-51-22-000-801, AND AMM 27-51-22-400-801.
- [SDR SWAA2025091203774](https://openairdocs.org/sdr/SWAA2025091203774.md): Floorbeam · cracked · Aug 12, 2025 · N224WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CRACKED PANEL BREAK AT PASSENGER COMPARTMENT BS 540; RBL 2; WL 208. REMOVED PANEL BREAK ASSY AT STA 520; RBL 1-24 PER SRM 51-40-02-0G-0. REMOVED AND REPLACED PANEL BREAK AT PASSENGER COMPARTMENT BS 540; RBL 2; WL 208 IAW SRM 51-40-02-0G-0.
- [SDR SWAA2025091203119](https://openairdocs.org/sdr/SWAA2025091203119.md): Attach Angle · cracked · Aug 11, 2025 · N224WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > B.S. 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT L.B.L. 45; W.L. 167.<[01] REMOVED AND INSTALLED NEW UPPER ATTACH ANGLE AT BS 663 L.B.L. 45; W.L. 167 PER SRM 51-40-02-0G-0; DWG 111A1000 REV. B AND DWG 111A700 REV.A.
- [SDR SWAA2025091103388](https://openairdocs.org/sdr/SWAA2025091103388.md): Handle · damaged · Aug 11, 2025 · N224WN · Boeing 7377H4 · Passenger Compartment Equipment
  > FED AFT SURROUND SIDEWALL LINING PANEL ASSIST HANDLE ASSY AND YELLOW SAFETY STRAP DAMAGED. REMOVED AND REPLACED ASSIST HANDLE ASSY AND YELLOW SAFETY ON THE FED AFT SURROUND SIDEWALL LINING PANEL IAW IPC 25-21-25-22 ITEM 20;25-66-10-02 ITEM 30;25-21-25-22 ITE
- [SDR SWAA2025091200092](https://openairdocs.org/sdr/SWAA2025091200092.md): Panel · debonded · Aug 10, 2025 · N224WN · Boeing 7377H4 · Aerodynamic Fairings
  > PANEL 193CL HAS LARGE DISBONDS ON BOTH SKINS. DUE TO THE EXTENT OF DAMAGE; REPLACED PANEL 193CL WITH NEW PANEL IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-14-00-03A ITEM 290.;
- [SDR SWAA2025091200093](https://openairdocs.org/sdr/SWAA2025091200093.md): Panel · debonded · Aug 10, 2025 · N224WN · Boeing 7377H4 · Aerodynamic Fairings
  > PANEL 193CR INNER SKIN IS DISBONDED. REPAIRED IAW SRM 51-70-05-2R-2-A00733, REPAIR 2. REPAIR OF DAMAGE THAT IS MORE THAN 0.50 INCH (12.70 MM) IN DIAMETER TO ONE SKIN AND THE HONEYCOMB CORE.
- [SDR SWAA2025091100083](https://openairdocs.org/sdr/SWAA2025091100083.md): Cradle · broken · Aug 9, 2025 · N224WN · Boeing 7377H4 · Emergency Equipment
  > 1EA AFT EMERGENCY FLASHLIGHT HOLDER ASSY BROKEN. REMOVED AND REPLACED 1EA AFT EMERGENCY FLASHLIGHT HOLDER PER SOPM 20-50-01.
- [SDR SWAA2025091299693](https://openairdocs.org/sdr/SWAA2025091299693.md): Scuff Plate · cracked · Aug 8, 2025 · N224WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD SERVICE DOOR SCUFF PLATE IS CRACKED AT AFT EDGE. REMOVED ALL THE COATINGS AND OTHER UNWANTED FROM THE SCUFF PLATE BEFORE WELDING PER SRM 53-10-15-2R-1 STEP 4.B.(3). WELDED THE DAMAGED AREA ON SCUFF PLATE IAW SRM 53-10-15-2R-1 STEP 4.B.(4). INSPECTED
- [SDR SWAA2025072192774](https://openairdocs.org/sdr/SWAA2025072192774.md): Slide · dislodged · Jul 18, 2025 · N224WN · Boeing 7377H4 · Escape Slide
  > FWD SERVICE DOOR SLIDE FELL OUT OF HOLDER. REINSTALLED FWD SERVICE DOOR SLIDE.
- [SDR SWAA2025050165462](https://openairdocs.org/sdr/SWAA2025050165462.md): Handle · loose · Apr 28, 2025 · N224WN · Boeing 7377H4 · Passenger/Crew Doors
  > FWD ENTRY DOOR ASSIST HANDLE LOOSE<[01] RESECURED FWD ENTRY DOOR ASSIST HANDLE PER AMM 52-11-31.
- [SDR SWAA2025042864023](https://openairdocs.org/sdr/SWAA2025042864023.md): Wedge · debonded · Apr 23, 2025 · N224WN · Boeing 7377H4 · Trailing Edge Flaps
  > LH IB MAIN FLAP TE WEDGE ASSY ADDITIONAL DISBOND UPPER AND LOWER SKINS WHILE PERFORMING TAP TEST FOUND ADDITIONAL AREAS OF DISBOND TO UPPER AND LOWER SKINS OF TE WEDGE. FOUND LOWER SKIN DISBOND 30 IN. L X 12 IN. W. FOUND UPPER SKIN DISBOND OF 27.5 IN. L X 6 IN
- [SDR SWAA2024051384116](https://openairdocs.org/sdr/SWAA2024051384116.md): Light · failed · May 10, 2024 · N224WN · Boeing 7377H4 · Emergency Lighting
  > SIDEWALL LIGHT OUT AT L/H OVERWING EXIT DOOR.<[01] R/R SIDEWALL LIGHT AT L/H OVERWING LIGHT PER AMM 33-51-04
- [SDR SWAA2024042377338](https://openairdocs.org/sdr/SWAA2024042377338.md): Circuit Breaker · tripped · Apr 19, 2024 · N224WN · Boeing 7377H4 · Light System Wiring
  > INFO ONLY FOUND EMERGENCY PANEL LIGHT BREAKER POPPED CONTACTED DAVE IN MOC -NO 10 DAY HISTORY - PERFORMED ONE TIME RESET BREAKER REMAINED CLOSED <BR>P6-3 BREAKER D8<[01] 02 - INSPECTED PER [GENERAL MPM 52.06.05 (INFO ONLY ITEM; NOTED BY MX)]<BR>NOTED BY MX REF
- [SDR SWAA2024041774900](https://openairdocs.org/sdr/SWAA2024041774900.md): Cover · out of adjust · Apr 15, 2024 · N224WN · Boeing 7377H4 · Emergency Lighting
  > LOWER EMER EXIT LIGHT @ 11BC EMER EXIT ROW COVER BROKEN<[01] C/W EA M-21-133-00720; LENS COVER SECURED W/ CLEAR TAPE.
- [SDR SWAA2024010937896](https://openairdocs.org/sdr/SWAA2024010937896.md): Battery Pack · failed · Jan 5, 2024 · N224WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACKS FAILED CAPACITY TEST AT LOCATIONS M1673;M1675;M1669;M1668;M1670 EMERGENCY LIGHT BATTERY PACKS FAILED CAPACITY TEST AT LOCATIONS M1673M1675M1669M1668M1670<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AT LOCATIONS M1673;M
- [SDR SWAA2023091499348](https://openairdocs.org/sdr/SWAA2023091499348.md): Girt Bar · out of adjust · Sep 12, 2023 · N224WN · Boeing 7377H4 · Emergency Equipment
  > AFT ENTRY DOOR SLIDE GIRT REQUIRES ADJUSTMENT<[01] ADJUSTED AFT ENTRY DOOR SLIDE GIRT PER AMM 25-66-01
- [SDR SWAA2023091499340](https://openairdocs.org/sdr/SWAA2023091499340.md): Light · inoperative · Sep 12, 2023 · N224WN · Boeing 7377H4 · Emergency Lighting
  > PASSENGER CABIN OWE SIDEWALL LIGHT IS INOP<[01] RE LAMPED OWE EMERGENCY LIGHT REF AMM 33-51-01.
- [SDR SWAA2023091198597](https://openairdocs.org/sdr/SWAA2023091198597.md): Battery · inoperative · Sep 8, 2023 · N224WN · Boeing 7377H4 · Emergency Equipment
  > AFT MEGAPHONE INOPERATIVE<[01] R/R BATTERIES IAWMM 25-64-00
- [SDR SWAA2023082890342](https://openairdocs.org/sdr/SWAA2023082890342.md): Door · cracked · Aug 17, 2023 · N224WN · Boeing 7377H4 · Galley Doors
  > R1 SERVICE DOOR SLIDE AFT SHOCK MOUNT CRACKED. (51-011)<[01] FWD GALLEY DOOR WAS REPLACED ON TASK CARD TTG8Q00MWSPU;[02] CORRECTION TO STEP 1 SHOULD READ FWD GALLEY DOOR WAS REPLACED ON TASK CARD TTG8Q00MS4S4;[03] VERIFIED 2.
- [SDR SWAA2023082890341](https://openairdocs.org/sdr/SWAA2023082890341.md): Door · cracked · Aug 17, 2023 · N224WN · Boeing 7377H4 · Service Doors
  > R1 SERVICE DOOR HANDLE TORQUE BOX UPPER BEAM CRACKED NEAR TORQUE BOX FORWARD ATTACH BOLT. (51-012)<[01] REPLACED FWD GALLEY SERVICE DOOR PER B737 AMM 52-41-00-400-801-NG INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q00MS4S4;[02] VERIFIED 1.
- [SDR SWAA2023082389891](https://openairdocs.org/sdr/SWAA2023082389891.md): Battery Pack · inoperative · Aug 16, 2023 · N224WN · Boeing 7377H4 · Emergency Lighting
  > LH SIDE OVER WING EXIT EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED BATTERY POWER SUPPLY; PERFORMED OPERATIONAL TEST; TEST PASSED;[02] VERIFIED CORRECTIVE ACTION.
- [SDR SWAA2023082389892](https://openairdocs.org/sdr/SWAA2023082389892.md): Battery Pack · inoperative · Aug 16, 2023 · N224WN · Boeing 7377H4 · Emergency Lighting
  > RH SIDE OVERHEAD BIN ROW 8 AREA EMERGENCY LIGHT INOP.<[01] PERFORMED T/S AND REMOVED BATTERY PACK FOUND FUSE LOOSE; REPOSITIONED FUSE; REINSTALLED BATTERY PACK AND PERFORMED TEST; TEST PASSED.;[02] VERIFIED CORRECTIVE ACTION.
- [SDR SWAA2023082888399](https://openairdocs.org/sdr/SWAA2023082888399.md): Door · out of adjust · Aug 11, 2023 · N224WN · Boeing 7377H4 · Galley Doors
  > R-1 DOOR VERTICAL ADJUSTMENT OUT OF LIMITS AT.020-.024 IN; MIN.060 IN; R-1 DOOR MECHANICAL ADJUSTMENT AT DOOR TORQUE TUBE IS AT MAX VERTICAL ADJUSTMENT.<[01] FWD GALLEY SERVICE DOOR ADJUSTMENT WILL BE ACCOMPLISHED ON TASK CARD TTG8Q00MS4S4;[02] VERIFIED CORR
- [SDR SWAA2023082491380](https://openairdocs.org/sdr/SWAA2023082491380.md): Plate · corroded · Aug 2, 2023 · N224WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CUSTOMER REQUEST AAI INSPECTION; - FUSELAGE LOWER LOBE- AFT ANTENNA AT STA 450; STR 27L APPROX. HAS EVIDENCE OF CORROSION FUSELAGE LOWER LOBE- AFT COVER PLATE AT STA 450 STR 27L APPROX. HAS EVIDENCE OF CORROSION<[01] REMOVED AND INSTALLED NEW AFT ALTIMETER FAI
- [SDR SWAA2023082490333](https://openairdocs.org/sdr/SWAA2023082490333.md): Plate · corroded · Aug 2, 2023 · N224WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CUSTOMER REQUEST AAI INSPECTION; - FUSELAGE LOWER LOBE - FWD ANTENNA AT STA 410; STR 27L APPROX. HAS EVIDENCE OF CORROSION FUSELAGE LOWER LOBE - FWD COVER PLATE AT STA 410 STR 27L APPROX. HAS EVIDENCE OF CORROSION<[01] REMOVED AND INSTALLED NEW AFT ALTIMETER F
- [SDR SWAA2023082383807](https://openairdocs.org/sdr/SWAA2023082383807.md): Floor Panel · damaged · Jul 30, 2023 · N224WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD CABIN FLOOR PANEL 231CF UPPER SKIN SURFACE CHIPPING AT EDGE.<[01] REMOVED AND REPLACED FWD CABIN FLOOR PANEL 231CF UPPER SKIN ASPER AMM 53-21-000-801 AND 53-21-00-400-801;[02] VERIFIED REMOVED AND REPLACED FWD CABIN FLOOR PANEL 231CF.
- [SDR SWAA2023082383806](https://openairdocs.org/sdr/SWAA2023082383806.md): Floor Panel · peeling · Jul 30, 2023 · N224WN · Boeing 7377H4 · Fuselage Floor Panel
  > R/H FWD CABIN FLOOR 232AF UPPER SKIN SURFACE PEELING.<[01] RECEIVED R/H FWD CABIN FLOOR 232AF UPPER SKIN SURFACE WILL BE CLOSED ON TTG8Q00LYLAQ ASPER DWG#141A5810;[02] VERIFIED 1.
- [SDR SWAA2023082483507](https://openairdocs.org/sdr/SWAA2023082483507.md): Skin · corroded · Jul 29, 2023 · N224WN · Boeing 7377H4 · Nacelle/Pylon, Plate/Skin
  > L/H AFT STRUT FAIRING I/B SIDE AFT LOWER SKIN SURFACE HAS CORROSION.<[01] REMOVED AND REPLACED #1 PYLON STRUT AFT LOWER EDGE SKIN IN REF B737-700 SRM 51-40-02-0G-0 AND BOEING DRAWING #313A2750.;[02] VERIFIED CORRECTIVE ACTION.
- [SDR SWAA2023082483506](https://openairdocs.org/sdr/SWAA2023082483506.md): Skin · corroded · Jul 29, 2023 · N224WN · Boeing 7377H4 · Nacelle/Pylon, Plate/Skin
  > R/H AFT STRUT FAIRING I/B SIDE AFT LOWER SKIN SURFACE HAS CORROSION.<[01] REMOVED AND REPLACED R/H LOWER STRUT FAIRING EDGE IN REF B737-700 SRM 51-40-02-0G-0 AND BOEING DRAWING # 313A2750.;[02] VERIFIED STEP 1 COMPLETE.
- [SDR SWAA2023082883505](https://openairdocs.org/sdr/SWAA2023082883505.md): Access Panel · cracked · Jul 28, 2023 · N224WN · Boeing 7377H4 · Wing, Plate/Skin
  > L/H WING T/E ACCESS PANEL 561AB LOWER SKIN SURFACE AROUND FASTENER HOLES CRACKS.<[01] APPLIED TOPCOAT ON L/H WING T/E ACCESS PANEL 561AB LOWER SKIN SURFACE REF B 737 AMM 51-21-73-370-803;[02] APPLIED REPAIR IN DAMAGE AREA AROUND FASTENER HOLES ON PANEL #561AB
- [SDR SWAA2023082888996](https://openairdocs.org/sdr/SWAA2023082888996.md): Access Panel · cracked · Jul 28, 2023 · N224WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CENTER WHEEL WELL ACCESS PANEL # 193D HAS BULGING/CRACKED FASTENER HOLES<[01] APPLIED A PERMANENT REPAIR ON DAMAGED FASTENER HOLES AS MARKED ON PANEL #193D AS PER B737 SRM 51-70-04-2R-9 PARA 4.L-M-N; MATERIAL USED PO#2011230; PO#1775890 AND PO#1690463;[02
- [SDR SWAA2023082483246](https://openairdocs.org/sdr/SWAA2023082483246.md): Shield · corroded · Jul 28, 2023 · N224WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO R/H FWD SHIELD FROM ST 767 TO 787; RBL 20 AROUND THE 4 FASTENER HOLE HAVE COROCION. (228-008) AFT CARGO R/H FWD SHIELD FROM ST 767 TO 787 RBL 21 AROUND THE 4 FASTENER HOLE HAVE CORROSION. (228-008) [TTG8Q00MGCG3]<[01] REMOVED CORROSION AT R/H FWD SH
- [SDR SWAA2023082483245](https://openairdocs.org/sdr/SWAA2023082483245.md): Channel · corroded · Jul 28, 2023 · N224WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO R/H Z CHANNE AT ST 747 + 18.5'; RBL 20 HAS CORROCION ATROUND THE HOLE FASTENER (228-007) AFT CARGO R/H CHANNE AT ST 747 + 18.5' RBL 21 HAS CORROCION ATROUND THE HOLE FASTENER (228-007) [TTG8Q00MGCEU]<[01] AFT CARGO R/H Z CHANNE AT ST 747 + 18.5'; R
- [SDR SWAA2023082483243](https://openairdocs.org/sdr/SWAA2023082483243.md): Channel · corroded · Jul 28, 2023 · N224WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO R/H Z CHANNE AT ST 747 + 10'; RBL 21 HAS CORROCION ATROUND THE HOLE FASTENER (228-005)<[01] AFT CARGO R/H Z CHANNE AT ST 747 + 10'; RBL 21; TO BE REPLACED ON CUSTOMER BAR CODE TTG8Q00MGCKT.;[02] VERIFIED STEP # 1.
- [SDR SWAA2023082483242](https://openairdocs.org/sdr/SWAA2023082483242.md): Channel · corroded · Jul 28, 2023 · N224WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO R/H Z CHANNE AT ST 747 + 6'; RBL 21 HAS CORROCION ATROUND THE HOLE FASTENER (228-004)<[01] AFT CARGO R/H Z CHANNE AT ST 747 + 6'; RBL 21; TO BE REPLACED ON CUSTOMER BAR CODE TTG8Q00MGCKT;[02] VERIFIED STEP # 1.
- [SDR SWAA2023082483244](https://openairdocs.org/sdr/SWAA2023082483244.md): Channel · corroded · Jul 28, 2023 · N224WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO R/H Z CHANNE AT ST 747 + 15'; RBL 20 HAS CORROCION ATROUND THE HOLE FASTENER (228-006) AFT CARGO R/H CHANNE AT ST 747 + 15' RBL 21 HAS CORROCION ATROUND THE HOLE FASTENER (228-006) [TTG8Q00MGCED]<[01] AFT CARGO R/H Z CHANNE AT ST 747 + 15'; RBL 21;
- [SDR SWAA2023082483241](https://openairdocs.org/sdr/SWAA2023082483241.md): Channel · corroded · Jul 28, 2023 · N224WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO R/H Z CHANNE AT ST 727E + 8.5'; RBL 20 HAS CORROCION ATROUND THE HOLE FASTENER (228-003) AFT CARGO R/H CHANNEL AT ST 727E + 8.5' RBL 21 HAS CORROSION AT ROUND THE HOLE FASTENER (228-003) [TTG8Q00MGCCH]<[01] AFT CARGO R/H Z CHANNE AT ST 727E + 8.5';
- [SDR SWAA2023082483247](https://openairdocs.org/sdr/SWAA2023082483247.md): Channel · corroded · Jul 28, 2023 · N224WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO R/H Z CHANNE AT ST 727D + 8'; RBL 20 HAS CORROCION ATROUND THE HOLE FASTENER (228-002) AFT CARGO R/H Z CHANNEL AT ST 727D + 8' RBL 21 HAS CORROSION AT ROUND THE HOLE FASTENER (228-00<[01] INSTALLED NEW FABRICATED Z CHANNEL R/H AFT CARGO; FROM STA. 7
- [SDR SWAA2023082483240](https://openairdocs.org/sdr/SWAA2023082483240.md): Channel · corroded · Jul 28, 2023 · N224WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO R/H Z CHANNE AT ST 727D + 3'; RBL 20 HAS CORROCION ATROUND THE HOLE FASTENER (228-001) AFT CARGO R/H CHANNE AT ST 727D + 3' RBL 21 HAS CORROSION AT ROUND THE HOLE FASTENER (228-001) [TTG8Q00MGCBY]<[01] FT CARGO R/H Z CHANNE AT ST 727D + 3'; RBL 21;
- [SDR SWAA2023082383417](https://openairdocs.org/sdr/SWAA2023082383417.md): Door · cracked · Jul 28, 2023 · N224WN · Boeing 7377H4 · Landing Gear Doors
  > L/H LANDING GEAR DOOR CRACKED<[01] REMOVED AND REPLACED L/H LANDING GEAR DOOR AS PER B737 AMM 32-13-11-000-803;32-13-11-420-802; 32-13-11-420-803; AND PERFORMED ADJUSTMENTS/OPS CHECK AS PER B737 AMM 32-13-11-820-801. ADJUSTMENTS WITHIN LIMITS AND OPS CHECK GOO
- [SDR SWAA2023082882998](https://openairdocs.org/sdr/SWAA2023082882998.md): Panel · cracked · Jul 27, 2023 · N224WN · Boeing 7377H4 · Wing, Control Surfaces
  > R/H WING I/B FLAP TRACK ACCESS PANEL # 194CR HAS BULGING/CRACKED FASTENER HOLES<[01] REPAIRED DAMAGE TO PANEL 194CR PER SRM 51-70-04-2R-9 PARA 4.E; SRM 51-70-04-2R-9 PRIMED AND TOP COAT PER AMM 51-21-72-370-51-21-73-370-803804. REPAIR COMPLETE.;[02] VERIFIED C

Next page: https://openairdocs.org/aircraft/N224WN/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 = 'N224WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N224WN/reports

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