# Service difficulty reports: N481WN

A list on [N481WN](https://openairdocs.org/aircraft/N481WN.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 · 317 reports

- [SDR SWAA2026101391729](https://openairdocs.org/sdr/SWAA2026101391729.md): Slide · dislodged · Oct 9, 2026 · N481WN · Boeing 7377H4 · Escape Slide
  > OPS REPORTS FWD SERVICE DOOR SLIDE FELL OUT REINSTALLED FWD SERVICE DOOR SLIDE IAW MT 725-61-06.
- [SDR SWAA2026080344267](https://openairdocs.org/sdr/SWAA2026080344267.md): Slide · low pressure · Aug 2, 2026 · N481WN · Boeing 7377H4 · Escape Slide
  > AFT ENTRY SLIDE PRESSURE GAUGE SHOWING LOW. REMOVED AND REPLACED AFT ENTRY DOOR SLIDE PACK IAW AMM 25-66-00 AND MT 725-61-06.
- [SDR SWAA2026070115636](https://openairdocs.org/sdr/SWAA2026070115636.md): Battery Pack · inoperative · Jun 25, 2026 · N481WN · Boeing 7377H4 · Emergency Lighting
  > MUTIPLE EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED; INSTALLED SERVICEABLE, AND PERFORMED OPS CHECK OF EMERGENCY LIGHT BATTERY PACKS M1672, M1673, AND M1675 IAW AMM 33-51-06-960-805. OPS CHECK GOOD. PERFOMED OPS CHECK OF EMERGENCY LIGHT BATTERY PACKS IAW AM
- [SDR SWAA2026070111069](https://openairdocs.org/sdr/SWAA2026070111069.md): Attach Angle · cracked · Jun 11, 2026 · N481WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > RIGHT VAPOR BARRIER ATTACH ANGLE CRACKED AT BS 663, RBL 25. REMOVED AND REPLACED RH VAPOR BARRIER UPPER ATTACH ANGLE AT BS 663 IAW SRM 51-40-02 AND BOEING DWG 111A1000 SHEET 45 REV:A AND BOEING DWG 111A1000 SHEET 153 REV-.
- [SDR SWAA2026070117650](https://openairdocs.org/sdr/SWAA2026070117650.md): Support Beam · damaged · Jun 10, 2026 · N481WN · Boeing 7377H4 · Wing Main, Frame Structure
  > RIGHT WING TRAILING EDGE STRUCTURE; DEFLECTION CONTROL RIB AND SUPPORT BEAM ATTACHMENT. ELONGATED FASTENER HOLES NOTED. REPAIRED RIGHT WING TRAILING EDGE STRUCTURE; DEFLECTION CONTROL RIB AND SUPPORT BEAM ATTACHMENT ELONGATED FASTENER HOLES IAW SRM 57-51-02-2
- [SDR SWAA2026070111065](https://openairdocs.org/sdr/SWAA2026070111065.md): Rib · damaged · Jun 10, 2026 · N481WN · Boeing 7377H4 · Wing, Rib/Bulkhead
  > RIGHT WING TRAILING EDGE STRUCTURE; DEFLECTION CONTROL RIB AND SUPPORT BEAM ATTACHMENT. ELONGATED FASTENER HOLES NOTED. REPAIRED RIGHT WING TRAILING EDGE STRUCTURE; DEFLECTION CONTROL RIB AND SUPPORT BEAM ATTACHMENT ELONGATED FASTENER HOLES PER B737 SRM 57-51
- [SDR SWAA2026033083879](https://openairdocs.org/sdr/SWAA2026033083879.md): Lens · missing · Mar 27, 2026 · N481WN · Boeing 7377H4 · Emergency Lighting
  > EXIT SIGN LENS AT EXIT ROW RIGHT MISSING. INSTALLED A NEW EXIT SIGN LENS IAW AMM 33-51-01.
- [SDR SWAA2026020668358](https://openairdocs.org/sdr/SWAA2026020668358.md): Slide · loose · Feb 5, 2026 · N481WN · Boeing 7377H4 · Escape Slide
  > ESCAPE SLIDE FRONT GALLEY DOOR LOOSE. REPACKED FWD SERVICE DOOR SLIDE IAW MT 725-61-06.
- [SDR SWAA2025110330366](https://openairdocs.org/sdr/SWAA2025110330366.md): Light · dim · Oct 31, 2025 · N481WN · Boeing 7377H4 · Emergency Lighting
  > LEFT EMERGENCY EXIT LIGHT IS DIM ABOVE HATCH. R & R THE OVERWING SIDEWALL LIGHT AND LENS PER AMM 33-51-03.
- [SDR SWAA2025110331272](https://openairdocs.org/sdr/SWAA2025110331272.md): Light · dim · Oct 31, 2025 · N481WN · Boeing 7377H4 · Emergency Lighting
  > LEFT EMERGENCY EXIT LIGHT IS DIM ABOVE HATCH. R & R THE OVERWING SIDEWALL LIGHT AND LENS PER AMM 33-51-03.
- [SDR SWAA2025110330365](https://openairdocs.org/sdr/SWAA2025110330365.md): Light · inoperative · Oct 31, 2025 · N481WN · Boeing 7377H4 · Emergency Lighting
  > RIGHT EMERGENCY EXIT LIGHT IS INOP ABOVE HATCH. R & R THE OVERWING SIDEWALL LIGHT AND LENS IAW AMM 33-51-03.
- [SDR SWAA2025110331273](https://openairdocs.org/sdr/SWAA2025110331273.md): Light · inoperative · Oct 31, 2025 · N481WN · Boeing 7377H4 · Emergency Lighting
  > RIGHT EMERGENCY EXIT LIGHT IS INOP ABOVE HATCH. R & R OVERWING SIDEWALL LIGHT AND LENS IAW AMM 33-51-03.
- [SDR SWAA2025102025214](https://openairdocs.org/sdr/SWAA2025102025214.md): Trim Motor · inoperative · Oct 16, 2025 · N481WN · Boeing 7377H4 · Stabilizer Control System
  > ELECTRIC STABILIZER TRIM INOPERATIVE. ] R & R STAB TRIM MOTOR PER AMM 27-41-71 OPS CHECK GOOD.
- [SDR SWAA2025030602135](https://openairdocs.org/sdr/SWAA2025030602135.md): Handle · cracked · Mar 5, 2025 · N481WN · Boeing 7377H4 · Passenger/Crew Doors
  > AFT ENTRY DOOR ASSIST HANDLE IS CRACKED.<[01] R&R AFT ENTRY DOOR ASSIST HANDLE ATTACH FITTING IAW AMM 52-13-31.;[02] INSP IAW AMM 52-13-31
- [SDR SWAA2024080923909](https://openairdocs.org/sdr/SWAA2024080923909.md): Element · arced · Aug 8, 2024 · N481WN · Boeing 7377H4 · Window System Wiring
  > LEFT SIDE SLIDING WINDOW HEATING ELEMENT ARC-ED. LASTED A FEW SECONDS WITH A STRONG SMELL. TURNED WINDOW HEAT OFF; NO CBS POPPED.<[01] REPLACED LT. NO. 2 OPENABLE WINDOW IAW AMM 56-12-11 AND MT 756-12-02. REPLACED LT. SIDE WHCU BECAUSE OF ARCING WHICH OCCURRED
- [SDR SWAA2024080220366](https://openairdocs.org/sdr/SWAA2024080220366.md): Skirt · out of adjust · Jul 31, 2024 · N481WN · Boeing 7377H4 · Escape Slide
  > CUSTOMER WALK ITEMS / R2DOOR SLIDE SKIRT HANGS ON THRESHOLD WHEN DOOR OPERATED<[01] REPOSITION R2 DOOR ESCAPE SLIDE SKIRT AS PER WORK INSTRUCTIONS 725-61-06;[02] VERIFIED STEP 1.
- [SDR SWAA2024080220362](https://openairdocs.org/sdr/SWAA2024080220362.md): Bulb · inoperative · Jul 31, 2024 · N481WN · Boeing 7377H4 · Emergency Lighting
  > CUSTOMER WALK ITEMS/ 1 EA BULB BURNED OUT ON EMER EXIT SIGN ABOVE R2 DOOR<[01] RE-LAMPED 1 LAMP ON EMERGENCY EXIT SIGN ABOVE R2 DOOR AS PER AMM REF 33-51-01-960-801. INSTALLATION TEST FOUND NORMAL.;[02] VERIFIED STEP 1.
- [SDR SWAA2024080220363](https://openairdocs.org/sdr/SWAA2024080220363.md): Slide · out of adjust · Jul 31, 2024 · N481WN · Boeing 7377H4 · Escape Slide
  > CUSTOMER WALK ITEMS / L2 DOOR SLIDE SKIRT HANGS ON THRESHOLD WHEN DOOR OPERATED<[01] REPOSITION L2 DOOR ESCAPE SLIDE SKIRT AS PER WORK INSTRUCTIONS 725-61-06;[02] VERIFIED STEP 1.
- [SDR SWAA2024080518605](https://openairdocs.org/sdr/SWAA2024080518605.md): Skin · cracked · Jul 29, 2024 · N481WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > R1 DOOR FWD CUTOUT PANEL CRACKED AT LOWER SECTION<[01] REPAIRED R1 DOOR FWD CUTOUT PANEL AT LOWER SECTION AS PER B737 AMM 25-00-00-300-802.;[02] VERIFIED STEP 1<BR>AUDIT C/W REF MPM 52.02.02
- [SDR SWAA2024080217837](https://openairdocs.org/sdr/SWAA2024080217837.md): Light · inoperative · Jul 27, 2024 · N481WN · Boeing 7377H4 · Emergency Lighting
  > L/H AFTER WING EXTERIOR EMERGENCY LIGHT INOPERATIVE.<[01] TROUBLESHOT INOPERATIVE L/H AFT WING EMERGENCY LIGHT (L547) REF B737 FIM 33-50 TASK 801; REMOVED AND REPLACED CONNECTOR D11082 AT EMERGENCY LIGHT L547 REF B737 SWPM 20-61-28; PERFORMED EMERGENCY LIGHT L
- [SDR SWAA2024080217840](https://openairdocs.org/sdr/SWAA2024080217840.md): Light · inoperative · Jul 27, 2024 · N481WN · Boeing 7377H4 · Emergency Lighting
  > L2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE.<[01] REPLACED LAMP AT L2 DOOR EXTERIOR EMERGENCY LIGHT (L732) IN REF WITH B737 AMM 33-51-04-960-801.LAMP TEST NORMAL.;[02] VERIFIED STEP 1
- [SDR SWAA2024080217116](https://openairdocs.org/sdr/SWAA2024080217116.md): Sign · inoperative · Jul 26, 2024 · N481WN · Boeing 7377H4 · Emergency Lighting
  > L1 DOOR LINER EMERGENCY EXIT SIGN INOP<[01] FOUND CONNECTOR D2972 FOR EXIT LIGHT NOT PROPERLY SEATED; RESEAT I/A/W BOEING WDM 33-51-12; PERFORMED OPS CHECK OF EMERGENCY LIGHTS I/A/W BOEING AMM 33-51-00-710-801; OPS CHECK NORMAL;[02] VERIFIED STEP 1<BR>AUDIT C/
- [SDR SWAA2024080515287](https://openairdocs.org/sdr/SWAA2024080515287.md): Scuff Plate · cracked · Jul 22, 2024 · N481WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > **REJECTION** DURING OK TO CLOSE FOUND AFT CARGO SCUFF PLATE AFT CORNER CRACKED MKD (107-001)<[01] RECEIVED AFT CARGO SCUFF PLATE AFT CORNER P;O 2074280 WILL BE INSTALL ON THIS CARD TTG80022CD3;[02] RECEIVED AFT CARGO SCUFF PLATE AFT CORNER P;O 2074280 WILL BE
- [SDR SWAA2024080514751](https://openairdocs.org/sdr/SWAA2024080514751.md): Cover · cracked · Jul 20, 2024 · N481WN · Boeing 7377H4 · Trailing Edge Flaps
  > RIGHT WING O/B AFT FLAP AT #6 CUT OUT EDGE COVER CRACKED<[01] REMOVED AND REPLACED RIGHT WING O/B AFT FLAP AT #6 CUT OUT EDGE COVER B737 SRM-51-40-02-0G-0 DWG#113A3700 AND AICP-27-51-22-01.;[02] VERIFIED STEP 1<BR>AUDIT C/W REF MPM 52.02.02
- [SDR SWAA2024080511465](https://openairdocs.org/sdr/SWAA2024080511465.md): Channel · corroded · Jul 11, 2024 · N481WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FOUND CHANNEL TIE WITH PITTING CORROSION AT E&E COMP INTERNAL SIDE STA 351.2+8 BL0<[01] REMOVED; FABRICATED AND INSTALLED NEW CHANNEL TIE AT SKIN BS 351.2+8 BL 0 PER REF SRM 51-40-02-0G-0 AND DWG 141A1160;[02] VERIFIED STEP 1<BR>AUDIT C/W REF MPM 52.02.02
- [SDR SWAA2024080511464](https://openairdocs.org/sdr/SWAA2024080511464.md): Support · worn · Jul 11, 2024 · N481WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > KEEL BEAM UNDER WING-TO-BODY FAIRING PANEL 192E HAS SUPPORT WITH FRETTING AT STA 600. 8-48<[01] REMOVED AND INSTALLED NEW SUPPORT AT KEEL BEAM UNDER WING-TO-BODY FAIRING PANEL 192E AS PER SRM-51-40-02-0G-0;[02] VERIFIED STEP:1
- [SDR SWAA2024080510312](https://openairdocs.org/sdr/SWAA2024080510312.md): Panel · cracked · Jun 29, 2024 · N481WN · Boeing 7377H4 · Wing, Plate/Skin
  > L/W LOWER LEADING-EDGE PANEL#521XB HAS SCREW HOLE CRACKED. 8-46<[01] APPLIED PERMANENT REPAIR ON DAMAGE AREA AS MARKED ON PANEL #521XB AS PER B737 SRM 51-70-04-2R-9; MATERIAL USED; PO#1791128; PO#1473815; TOOL USED; TEMP CONTROLLER ID 160354; CALIBRATION DUE 0
- [SDR SWAA2024080505912](https://openairdocs.org/sdr/SWAA2024080505912.md): Channel · corroded · Jun 26, 2024 · N481WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SPOT IN E&E AT SKIN BS 351.2+6 BL O. 8-25<[01] REMOVED; FABRICATED AND INSTALLED NEW CHANNEL AT SKIN BS 351.2+6 BL 0 PER REF SRM 51-40-02-0G-0 AND DWG 141A3502;[02] VERIFIED STEP 1<BR>ATC ANTENNA WILL BE INSTALL ON T/C TTG8Q00UT1KC<BR>AUDIT C/W REF M
- [SDR SWAA2024080505749](https://openairdocs.org/sdr/SWAA2024080505749.md): Rib · cracked · Jun 26, 2024 · N481WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > LEFT HORIZONTAL STABILIZER L/E PANEL RIB # 2 CRACK.<[01] REMOVED CRACKED RIB #2 AT LEFT HORIZONTAL STABILIZER L/E PER B737-700 SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW RIB #2 AT LEFT HORIZONTAL STABILIZER L/E PANEL PER B737-700 SRM 51-40-05-0G-0 AND DWG#: 18
- [SDR SWAA2024080505750](https://openairdocs.org/sdr/SWAA2024080505750.md): Rib · cracked · Jun 26, 2024 · N481WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > LEFT HORIZONTAL STABILIZER L/E PANEL RIB # 3 CRACK.<[01] LOCATED AND DRILLED NEW RIB #3 AT LEFT HORIZONTAL STABILIZER L/E PER B737-700 SRM 51-40-05-0G-0 AND DWG#:186A1303.<BR>OK TO INSTALL NEW RIB #3 AT LEFT HORIZONTAL STABILIZER L/E PANEL.<BR>INSTALLED NEW RI
- [SDR SWAA2024080506177](https://openairdocs.org/sdr/SWAA2024080506177.md): Angle · cracked · Jun 26, 2024 · N481WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > RH HORIZONTAL STAB PANEL 343 BLADE SEAL RETAINER CRACK. RH HORIZONTAL STAB PANEL 343AB BLADE SEAL RETAINER CRACK.<[01] REMOVED AND REPLACED RH HORIZONTAL STAB PANEL 343 BLADE SEAL RETAINER ANGLE REF. SRM 51-40-02-0G-0;[02] REMOVED AND REPLACED RH HORIZONTAL ST
- [SDR SWAA2024080505743](https://openairdocs.org/sdr/SWAA2024080505743.md): Bracket · cracked · Jun 25, 2024 · N481WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT OF AFT CARGO COMPARTMENT BILGE FLOOR SUPPORT BRACKET CRACKED @ AFT END FWD OF WATER TANK STA 947.75 S-26L MKD DOT<[01] INSTALLED BRACKETED AT AFT CARGO COMPARTMENT BILGE FLOOR SUPPORT AT AFT END FORWARD OF WATER TANK STA.947.5 S-26L AS PER BOEING 737 SRM 5
- [SDR SWAA2024080505748](https://openairdocs.org/sdr/SWAA2024080505748.md): Floor Panel · peeling · Jun 25, 2024 · N481WN · Boeing 7377H4 · Fuselage Floor Panel
  > CENTER CABIN FLOOR PANEL 241BF HAS UPPER SURFACE LAYER FIBERS PEELED AND 3EA EXISTING REPAIRS. 124-002<[01] RECEIVED NEW PANEL # 241BF; INSTALLATION WILL BE ACCOMPLISH ON # TTG8Q00TNY15;[02] CORRECTED STEP 1.RECEIVED NEW PANEL # 241BF; INSTALLATION WILL BE
- [SDR SWAA2024080505746](https://openairdocs.org/sdr/SWAA2024080505746.md): Gusset · cracked · Jun 25, 2024 · N481WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT GAUSET CRACKED AT S-21R STA 500D MKD DOT<[01] REMOVED GAUSET AT S-21R STA 500D PER SRM 51-40-02-0G-0; LOCATED AND DRILLED NEW PART PER SRM 51-40-05-0G-0; TREATED AND PRIMED NEW PART PER SRM 51-20-01-0G-0; INSTALLED NEW PART PER SRM 51-40-
- [SDR SWAA2024080505742](https://openairdocs.org/sdr/SWAA2024080505742.md): Plate · cracked · Jun 25, 2024 · N481WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CABIN L-1 DOOR CUTOUT AFT JAMB LOWER INB COVER PLATE APPEARS CRACKED @ LOWER HOLE STA 348.2 MKD DOT<[01] PERFORMED HFEC INSP. ON SUSPECTED CRACK IAW B737 NDT PART 6; 51-00-00; PROCEDURE 23. CRACK CONFIRMED (LENGTH 1') <BR>TOOL: NORTEC 600 B/C: 166316 DUE:
- [SDR SWAA2024080205747](https://openairdocs.org/sdr/SWAA2024080205747.md): Floor Panel · peeling · Jun 25, 2024 · N481WN · Boeing 7377H4 · Fuselage Floor Panel
  > CENTER CABIN FLOOR PANEL 231YF HAS UPPER SURFACE LAYER FIBERS PEELED. 124-001<[01] RECEIVED NEW PANEL # 231YF INSTALLATION WILL BE ACCOMPLISH ON # TTG8Q00TNY32;[02] CORRECTED STEP 1. RECEIVED NEW PANEL # 231YF INSTALLATION WILL BE ACCOMPLISH ON #TTG8Q00TNY33;
- [SDR SWAA2024080205552](https://openairdocs.org/sdr/SWAA2024080205552.md): Shield · corroded · Jun 25, 2024 · N481WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION** FWD CARGO COMPARTMENT FLOOR SUPPORT SHIELD @ S-26R STA 500 TO 500A MKD DOT<[01] REMOVED FWD CARGO COMPARTMENT FLOOR SUPPORT SHIELD AT S-26R FROM STA 500 TO 500A PER SRM 51-40-02-0G-0; RECEIVED NEW PART; LOCATED AND DRILLED NEW PART PER SRM 51-40-05
- [SDR SWAA2024073105745](https://openairdocs.org/sdr/SWAA2024073105745.md): Gusset · cracked · Jun 25, 2024 · N481WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT GUSSET CRACKED AT S-19R STA 500D MKD DOT<[01] REMOVED GUSSET AT S-19R STA 500D PER SRM 51-40-02-0G-0; LOCATED AND DRILLED NEW PART PER SRM 51-40-05-0G-0; TREATED AND PRIMED NEW PART PER SRM 51-20-01-0G-0; INSTALLED NEW PART PER SRM 51-40-
- [SDR SWAA2024073105744](https://openairdocs.org/sdr/SWAA2024073105744.md): Gasket · cracked · Jun 25, 2024 · N481WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT GAUSET CRACKED AT S-19L STA 500D MKD DOT<[01] REMOVED GAUSET AT S-19L STA 500D PER SRM 51-40-02-0G-0; LOCATED AND DRILLED NEW PART PER SRM 51-40-05-0G-0; TREATED AND PRIMED NEW PART PER SRM 51-20-01-0G-0; INSTALLED NEW GAUSET PER SRM 51-4
- [SDR SWAA2024073005544](https://openairdocs.org/sdr/SWAA2024073005544.md): Doubler · corroded · Jun 25, 2024 · N481WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CORROSION ** AFT CARGO COMPARTMENT BILGE SKIN PREVIOUS DOUBLER REPAIR @ S-26R STA 807+5' MKD DOT<[01] ACCOMPLISHED REPAIR PER EA -24-153-01888 AT AFT CARGO COMPARTMENT BILGE STR 26R STA 807'+5'.;[02] VERIFIED STEP 1; 2<BR>TREAT AND PRIME C/W ON EA 24-153-01880
- [SDR SWAA2024072911624](https://openairdocs.org/sdr/SWAA2024072911624.md): Panel · cracked · Jun 25, 2024 · N481WN · Boeing 7377H4 · Vertical Stabilizer, Plate/Skin
  > RIGHT VERTICAL FIN PANEL#323AR ASSY SUPPORT ANGLE LOWER SURFACE HAS BARE METAL. RIGHT VERTICAL FIN PANEL#323AR ASSY CRACKED AT LOWER CORNER<[01] RECEIVED NEW PART. LOCATED AND DRILLED AND COUNTERSUNK FASTENER HOLES ON NEW VERTICAL PANEL 323AR REF. SRM 51-40-05
- [SDR SWAA2024080505136](https://openairdocs.org/sdr/SWAA2024080505136.md): Linkage · corroded · Jun 24, 2024 · N481WN · Boeing 7377H4 · Nacelle/Pylon, Main Frame
  > CORROSION ** L/H RAM AIR INLET FWD DOOR ACTUATING ROD LOWER LINK MKD DOT<[01] REMOVED AND REPLACED L/H RAM AIR INLET FWD DOOR ACTUATING ROD LOWER LINK AS PER AMM 21-51-22-000-802 AND 21-51-22-400-802.;[02] VERIFIED STEP:1
- [SDR SWAA2024080505137](https://openairdocs.org/sdr/SWAA2024080505137.md): Floor Support · cracked · Jun 24, 2024 · N481WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT OF FWD CARGO COMPARTMENT INTERCOSTAL SUPPORT CRACKED @ AFT END BETWEEN STA 500D AND 520 S-25R<[01] REMOVED FWD CARGO COMPARTMENT INTERCOSTAL SUPPORT BETWEEN STA 500D AND 520 S-25R PER SRM 51-40-02-0G-0; ACCOMPLISHED HEAT TREATMENT OF FABRICATED PART PER OP
- [SDR SWAA2024080505009](https://openairdocs.org/sdr/SWAA2024080505009.md): Scuff Plate · cracked · Jun 23, 2024 · N481WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT AFT SCUFF PLATE CRACKED<[01] REPAIRED PART 'AFT CARGO AFT SCUFF PLATE' RECEIVED AND WILL BE INSTALLED ON CARD: TTG8Q00229WY;[02] VERIFIED STEP 1.
- [SDR SWAA2024080507976](https://openairdocs.org/sdr/SWAA2024080507976.md): Support · cracked · Jun 23, 2024 · N481WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > MAIN CABIN CENTER SECTION FLOOR SUPPORT BREAK CRACKED AT LBL 1 STA 540<[01] REVOVED AND REPLACED PANEL BREAK AT MAIN CABIN CENTER SECTION; STA 540; LBL 1 AS PER B737-700 SRM 51-40-02-0G-0.;[02] ADDING DWG# 143A5240 O N STEP 1 (FINAL).;[03] VERIFIED STEP:1 AND
- [SDR SWAA2024080504869](https://openairdocs.org/sdr/SWAA2024080504869.md): Support · cracked · Jun 23, 2024 · N481WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > MAIN CABIN CENTER SECTION FLOOR SUPPORT BREAK CRACKED AT RBL 1 STA 540<[01] REMOVED AND REPLACED PANEL BREAK AT MAIN CABIN CENTER SECTION; STA 540; RBL 1 AS PER B737-700 SRM 51-40-02-0G-0.;[02] ADDING DWG#143A5240 ON STEP 1 (FINAL).;[03] VERIFIED STEP:1 AND ST
- [SDR SWAA2024080505003](https://openairdocs.org/sdr/SWAA2024080505003.md): Angle · cracked · Jun 23, 2024 · N481WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > LOWER FUS CENTER SECTION ATTACHED ANGLE CRACKED @ RAM AIR EXIT EXHAUST DUCT CUTOUT SEAL O/B LOWER CORNER MKD DOT<[01] REMOVED AND INSTALLED ANGLE AT LOWER FUS CENTER SECTION @ RAM AIR EXIT EXHAUST DUCT CUTOUT SEAL O/B LOWER CORNER AS PER SRM-51-40-02-0G-0 DWG#
- [SDR SWAA2024080504866](https://openairdocs.org/sdr/SWAA2024080504866.md): Skin · delaminated · Jun 23, 2024 · N481WN · Boeing 7377H4 · Trailing Edge Flaps
  > L/W OUB AFT FLAP INB END LOWER SURFACE DELAMINATION AROUND PREVIOUS REPAIR MKD DOT<[01] REMOVE AND REPLACED L/W OUB AFT FLAP AS PER AMM 27-51-22-000-801 AND 27-51-22-400-801.;[02] VERIFIED STEP 1
- [SDR SWAA2024080505006](https://openairdocs.org/sdr/SWAA2024080505006.md): Panel · elongated · Jun 23, 2024 · N481WN · Boeing 7377H4 · Trailing Edge Flaps
  > L/W REAR SPAR LOWER FIXED T/E PANEL 551GB INB AFT SUPPORT ROD LOWER ATTACHED FITTING ELONGATED HOLE MKD DOT<[01] REMOVED AND REPLACED L/W REAR LSPAR LOWER FIXED T/E PANEL# 551GB AFT SUPPORT ROD PER REF SRM 51-40-02-0G-0;[02] VERIFIED STEP:1
- [SDR SWAA2024080504309](https://openairdocs.org/sdr/SWAA2024080504309.md): Panel · corroded · Jun 21, 2024 · N481WN · Boeing 7377H4 · Fuselage Main, Structure
  > PANEL 192F HAS FLAME SPRAY CORRODED AT ANTENNA MOUNT AREA. 8-22<[01] RECIEVED NEW PANEL. WORK WILL BE ACCOMPLISHED ON TTG8Q00U3UBG;[02] CORRECTION TO STEP 1: <BR>RECIEVED NEW PANEL; PART NUMBER 14A7755-1 192F. WORK WILL BE ACCOMPLISHED ON TTG8Q00TNXXE;[03] VER

Next page: https://openairdocs.org/aircraft/N481WN/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 = 'N481WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N481WN/reports

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.