# Service difficulty reports: N494WN

A list on [N494WN](https://openairdocs.org/aircraft/N494WN.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 · 335 reports

- [SDR SWAA2026072999375](https://openairdocs.org/sdr/SWAA2026072999375.md): Seal · out of adjust · Jul 24, 2026 · N494WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > LEFT UPPER STAB PANEL 333AT SLIDING SEAL NOT IN GUIDE. INSTALLED 333AT IAW SRM 51-40-02, REF IPC 55-10-52.
- [SDR SWAA2026072878794](https://openairdocs.org/sdr/SWAA2026072878794.md): Battery Pack · faulted · Jul 7, 2026 · N494WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHTS RUN OFF OF BATTERY PACK M1673, DID NOT TURN ON. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-06-960-805.
- [SDR SWAA2026072859606](https://openairdocs.org/sdr/SWAA2026072859606.md): Seal · cracked · Jul 7, 2026 · N494WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > RIGHT UPPER HORIZONAL STAB SLIDING SEAL CRACKED. REMOVED AND REPLACED SLIDING PLATE IAW AMM 53-31-31-000-802.
- [SDR SWAA2026072944661](https://openairdocs.org/sdr/SWAA2026072944661.md): Lug · corroded · Jun 25, 2026 · N494WN · Boeing 7377H4 · Fuselage, Stabilizer Attach Fittings
  > FOUND SURFACE CORROSION ON AFT FACE OF RT HORIZONTAL STAB CENTER SECTION LOWER LUG, AS PER EA 26-155-01728 THE CONFIGURATION IS ACCEPTABLE.
- [SDR SWAA2026072944812](https://openairdocs.org/sdr/SWAA2026072944812.md): Lug · corroded · Jun 23, 2026 · N494WN · Boeing 7377H4 · Fuselage, Stabilizer Attach Fittings
  > FOUND SURFACE CORROSION ON AFT FACE OF LT HORIZONTAL STAB CENTER SECTION LOWER LUG. AS PER EA 26-155-01709 THE CONFIGURATION IS ACCEPTABLE.
- [SDR SWAA2026072829856](https://openairdocs.org/sdr/SWAA2026072829856.md): Scuff Plate · cracked · Jun 22, 2026 · N494WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO DOOR FWD CORNER SCUFF PLATE CRACKED. ACCOMPLISHED WELD REPAIR IAW SRM 53-30-15-2R-1, REPAIR 1. RII BLOCK SELECTED TO ANSWER STEP 7 NOT RII IAW MPM 10.3.4;
- [SDR SWAA2026072835627](https://openairdocs.org/sdr/SWAA2026072835627.md): Strap · cracked · Jun 22, 2026 · N494WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK INDICATION NOTED AT RH BS 639 RBL 47.0 WL 206.6 AFT LOWER FASTENER. REMOVED AND REPLACED STRAPS IAW SRM 51-40-02 AND DWG 111A6504, REV B.
- [SDR SWAA2026072874342](https://openairdocs.org/sdr/SWAA2026072874342.md): Strap · cracked · Jun 22, 2026 · N494WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK INDICATION NOTED AT LT BS 616, LBL 47, WL 206.6 AFT INBD UPPER FASTENER. REMOVED AND REPLACED THE STRAPS IAW SRM 51-40-02, AND DWG 111A6504, REV B.
- [SDR SWAA2026072878390](https://openairdocs.org/sdr/SWAA2026072878390.md): Strap · cracked · Jun 22, 2026 · N494WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK INDICATION NOTED AT BS 597, LBL 47, WL 206.6. MAIN CABIN OVERWING BOX FWD OTBD LOWER FASTENER LOCATION. R & R STRAP IAW AMM 20-50-11 AND DWG 111A6504, SHEET 3, REV-.
- [SDR SWAA2026070714489](https://openairdocs.org/sdr/SWAA2026070714489.md): Floor Panel · delaminated · Jun 21, 2026 · N494WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 231 VF IS DELAMANITED. FABRICATED FLOORPANEL USING BMS4-17 TY VI IAW SRM 53-00-50-2R-0. VERIFIED FABRICATED FLOORPANEL USING BMS4-17 TY VI IAW SRM 53-00-50-2R-0
- [SDR SWAA2026070714610](https://openairdocs.org/sdr/SWAA2026070714610.md): Floor Panel · delaminated · Jun 21, 2026 · N494WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 231 XF IS DELAMINATED AT SCREW HOLES. FABRICATED NEW FLOORBOARD PN 114A5810-126 IAW BAC DWG 114A5810-126 REV J, SRM 53-00-50-2R-0; INSPECTED IAW SRM 53-00-50-2R-0-A00938 AND BAC DWG 114A5810 REV J
- [SDR SWAA2026070714611](https://openairdocs.org/sdr/SWAA2026070714611.md): Floor Panel · delaminated · Jun 21, 2026 · N494WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 231 YF IS DELAMINATED AND HAS EDGE DAMAGE. AFTER EVALUATION; FOUND FLOOR PANEL 231YF TO BE OUT OF REPAIRABLE LIMITS AND REQUIRES FABRICATION. FABRICATED FLOOR PANEL USING BMS4-17 TY VI IAW SRM 53-00-50-2R-0, DWG 144A5810-189. INSPECTED IAW SRM
- [SDR SWAA2026072890712](https://openairdocs.org/sdr/SWAA2026072890712.md): Support Bracket · corroded · Jun 19, 2026 · N494WN · Boeing 7377H4 · Trailing Edge Flaps
  > RIGHT WING TRAILING EDGE LOWER PANEL SUPPORT BRACKET CORRODED AT FASTENER LOCATIONS. (LOCATED BETWEEN FLAP TRACKS 6 AND 7). REMOVED AND REPLACED SOPPORT BRACKET AT R/W T/EDGE LOWER PNL IAW SRM 51-40-05 AND 51-40-02 REF AIPC 57-50-00-20.
- [SDR SWAA2026072832274](https://openairdocs.org/sdr/SWAA2026072832274.md): Web · cracked · Jun 19, 2026 · N494WN · Boeing 7377H4 · Fuselage Main, Structure
  > HORIZONTAL PRESSURE DECK WEB STA 663 RBL 40 FORWARD OUTBOARD EDGE OF STIFFENING BEAD HAS CRACK INDICATION. ACCOMPLISHED REPAIR OF BEADED PRESSURE DECK WEB AT STA.663.75 RBL 40 IAW SRM 53-40-51-2R-2.
- [SDR SWAA2026072896972](https://openairdocs.org/sdr/SWAA2026072896972.md): Web · corroded · Jun 19, 2026 · N494WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR SURROUND LOWER WEB AT SCUFF PLATE NUMEROUS CORRODED AREAS AROUNG BLIND RIVETS AND FASTNER HOLES REMOVED AND REPLACED AFT CARGO DOOR SURROUND LOWER WEB IAW B737-700 SRM 51-40-02 AND; BOEING DWG# 146A8340 REV: -.
- [SDR SWAA2026072875377](https://openairdocs.org/sdr/SWAA2026072875377.md): Support Bracket · corroded · Jun 19, 2026 · N494WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > RIGHT WING, TRAILING EDGE LOWER PANEL SUPPORT BRACKET CORRODED AT FASTENER HOLES. LOCATED BETWEEN FLAP TRACKS 7 AND 8. INSTALLED RT WING TRAILING EDGE LOWER PANEL SUPPORT BRACKET IAW SRM 51-40-02, AND DWG 115A3758, REV A.
- [SDR SWAA2026072850933](https://openairdocs.org/sdr/SWAA2026072850933.md): Panel · cracked · Jun 18, 2026 · N494WN · Boeing 7377H4 · Wing, Plate/Skin
  > RIGHT WING TRAILING EDGE PANEL 661BB HAS CRACKS AROUND FASTENER HOLES. REPAIRED R/H WING TAILING EDGE PANEL 661BB IAW B737-700 SRM 57-51-01-2R-1 REPAIR 1 AND 51-70-05-2R-6 REPAIR 6 AND 51-70-05-2R-0
- [SDR SWAA2026072865570](https://openairdocs.org/sdr/SWAA2026072865570.md): Panel · cracked · Jun 18, 2026 · N494WN · Boeing 7377H4 · Wing Main, Frame Structure
  > RIGHT WING T/E PANEL 661AB HAD CRACKS AROUND FASTENER HOLES. REPAIRED IAW SRM 57-51-01-2R-1-A01282, REPAIR 1.
- [SDR SWAA2026072851106](https://openairdocs.org/sdr/SWAA2026072851106.md): Panel · cracked · Jun 18, 2026 · N494WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > RIGHT WING TRAILING EDGE PANEL 661CB HAS CRACKS AROUND FASTENER HOLES. REPAIRED RT WING T/E PANEL 661CB IAW SRM 57-51-01-2R-1 & 51-70-05-2R-0. INSPECTED PER [SRM 57-51-01-2R-1-A01282 (REPAIR 1 - WING FIXED TRAILING EDGE SKIN PANELS MADE OF COMPOSITE MATERIA
- [SDR SWAA2026072830472](https://openairdocs.org/sdr/SWAA2026072830472.md): Bracket · cracked · Jun 17, 2026 · N494WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > RIGHT WING TRAILING EDGE AT DEFLECTION CONTROL RIB. DEFLECTION CONTROL RIB WEB RIGHT SIDE BRACKET, AS VIEWED LOOKING FORWARD, CRACKED. R & R THE BRACKET ON RT WING TRAILING EDGE AT DEFLECTION CONTROL RIB IAW SRM 51-40-02. REF AIPC 57-42-51-02. R
- [SDR SWAA2026072839387](https://openairdocs.org/sdr/SWAA2026072839387.md): Bracket · cracked · Jun 17, 2026 · N494WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > LEFT WING TRAILING EDGE DEFLECTION CONTROL RIB WEB CENTER BRACKET CRACKED. R & R LT WING TRAILING EDGE DEFLECTION CONTROL RIB WEB CENTER BRACKET IAW SRM 51-40-02 AND REF IPC 57-50-00.
- [SDR SWAA2026072841428](https://openairdocs.org/sdr/SWAA2026072841428.md): Bracket · cracked · Jun 17, 2026 · N494WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > RIGHT WING TRAILING EDGE AT DEFLECTION CONTROL RIB. CONTROL RIB WEB CENTER BRACKET CRACKED. REMOVED AND REPLACED R/W T/E DEFLECTION CONTROL RIB WEB BRACKET FITTING IAW SRM 51-40-02 AND AMM 20-50-11-910-801.
- [SDR SWAA2026041689943](https://openairdocs.org/sdr/SWAA2026041689943.md): Latch · broken · Apr 15, 2026 · N494WN · Boeing 7377H4 · Emergency Equipment
  > AFT GALLEY FLASHLIGHT UPPER LATCH BROKEN. REMOVED AND REPLACED AFT GALLEY FLASHLIGHT DOOR UPPER LATCH IAW CMM 25-31-05
- [SDR SWAA2026033083503](https://openairdocs.org/sdr/SWAA2026033083503.md): Battery Pack · inoperative · Mar 26, 2026 · N494WN · Boeing 7377H4 · Emergency Lighting
  > C/B P-18-3 B10 EMERGENCY CHARGER RIGHT AFT IS OPENED AND WILL NOT RESET. EMERGENCY LIGHTS IN AFT CABIN ARE ON<[01] 01 - REMOVED AND REPLACED AFT R/H EMERGENCY POWER PACK AND CHARGER PER PER [AMM 33-51-06-201-NG (POWER SUPPLIES - MAINTENANCE PRACTICES - PERMANE
- [SDR SWAA2026033084433](https://openairdocs.org/sdr/SWAA2026033084433.md): Charger · inoperative · Mar 26, 2026 · N494WN · Boeing 7377H4 · Emergency Lighting
  > C/B P-18-3 B10 EMERGENCY CHARGER RIGHT AFT IS OPENED AND WILL NOT RESET. EMERGENCY LIGHTS IN AFT CABIN ARE ON<[01] 01 - REMOVED AND REPLACED AFT R/H EMERGENCY POWER PACK AND CHARGER PER PER [AMM 33-51-06-201-NG (POWER SUPPLIES - MAINTENANCE PRACTICES - PERMANE
- [SDR SWAA2026033083504](https://openairdocs.org/sdr/SWAA2026033083504.md): Battery Pack · damaged · Mar 26, 2026 · N494WN · Boeing 7377H4 · Emergency Lighting
  > REF L/P 3089074 EMERGENCY C/B POPPED<[01] FOUND BATTERY PACK M1672 DAMAGED; DISCONNECTED PACK AND C/B STAYS IN. REF AMM 33-20-00. SEE LOGPAGE 3089074 FOR FINAL CORRECTIVE ACTION
- [SDR SWAA2026021671086](https://openairdocs.org/sdr/SWAA2026021671086.md): Sign · broken · Feb 14, 2026 · N494WN · Boeing 7377H4 · Emergency Lighting
  > L2 DOOR EMER LT SIGN LENS BROKEN OFF AND ONE WIRE OF LIGHT ASSY MISSING. RECONNECTED WIRES & R & R L2 DOOR LOWER SIGN ASSY IAW AMM 33-51-01.
- [SDR SWAA2026021670775](https://openairdocs.org/sdr/SWAA2026021670775.md): Wire · disconnected · Feb 14, 2026 · N494WN · Boeing 7377H4 · Light System Wiring
  > L2 DOOR EMERGENCY LIGHT SIGN LENS BROKEN OFF AND ONE WIRE OF LT ASSY MISSING. CONNECTED WIRES & R & R THE L2 DOOR LOWER EMERGENCY SIGN ASSY IAW AMM 33-51-01.
- [SDR SWAA2026021670760](https://openairdocs.org/sdr/SWAA2026021670760.md): Lens · broken · Feb 13, 2026 · N494WN · Boeing 7377H4 · Emergency Lighting
  > AFT GALLEY EXIT LIGHT MARKER BROKEN LENS NEAR FLIGHT ATTENDANT SEAT. SECURED THE LIGHT LENS IAW EA M-21-133-00720.
- [SDR SWAA2025110631577](https://openairdocs.org/sdr/SWAA2025110631577.md): Girt Bar · out of adjust · Nov 3, 2025 · N494WN · Boeing 7377H4 · Emergency Equipment
  > FWD SERVICE DOOR SLIDE CLIPS NEED ADJUSTMENT. ADJUSTED GIRT BAR SPRING CLIPS PER MM 25-66-01.
- [SDR SWAA2024121776621](https://openairdocs.org/sdr/SWAA2024121776621.md): Skin · cracked · Dec 13, 2024 · N494WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > DURING ACCOMPLISHMENT OF 5331-I-16838-NG [TTG8Q00VM3PM]; FOUND INDICATION OF POSSIBLE CRACK AT FUSELAGE SKIN LAP SPLICE LOWER SKIN AT S-14R STA 787+6.5'. PERFORMED EA 24-153-03454 REF TTG8Q00XLL2C FOR MAINTENANCE ACCOMPLISHED.
- [SDR SWAA2024121776620](https://openairdocs.org/sdr/SWAA2024121776620.md): Skin · cracked · Dec 13, 2024 · N494WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > DURING ACCOMPLISHMENT OF 5331-I-16838-NG [TTG8Q00VM3PM]; FOUND INDICATION OF POSSIBLE CRACK AT FUSELAGE SKIN LAP SPLICE LOWER SKIN AT S-14R STA 787+5'. PERFORMED EA 24-153-03454 FOR REPAIR.
- [SDR SWAA2024090632657](https://openairdocs.org/sdr/SWAA2024090632657.md): Battery Pack · inoperative · Aug 31, 2024 · N494WN · Boeing 7377H4 · Emergency Lighting
  > INOP BATTERY PACK IN LOWERED CEILING PANEL AT FWD GALLEY AREA (2 EA) 2024-473281<[01] REPLACED BATTERY PACK IN LOWERED CEILING PANEL AT FWD GALLEY AREA (2 EA) IAW B737-700 AMM 33-51-06-960-805 SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED BATTERY PACK IN LOWERED
- [SDR SWAA2024090632656](https://openairdocs.org/sdr/SWAA2024090632656.md): Battery Pack · inoperative · Aug 31, 2024 · N494WN · Boeing 7377H4 · Emergency Lighting
  > INOP BATTERY PACK OF THE STA 603 RT SIDE AT PASSENGER CABIN 2024-473282<[01] REPLACED BATTERY PACK OF THE STA 603 RT SIDE AT PASSENGER CABIN IAW B737-700 AMM 33-51-06-960-805 SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED BATTERY PACK OF THE STA 603 RT SIDE AT PA
- [SDR SWAA2024090632655](https://openairdocs.org/sdr/SWAA2024090632655.md): Battery Pack · inoperative · Aug 31, 2024 · N494WN · Boeing 7377H4 · Emergency Lighting
  > INOP BATTERY PACK IN LOWERED CEILING PANEL AT AFT GALLEY AREA 2024-473280<[01] REPLACED BATTERY PACK IN LOWERED CEILING PANEL AT AFT GALLEY AREA IAW B737-700 AMM 33-51-06-960-805 SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED BATTERY PACK IN LOWERED CEILING PANEL
- [SDR SWAA2024090530738](https://openairdocs.org/sdr/SWAA2024090530738.md): Stringer · corroded · Aug 20, 2024 · N494WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > REJECT-REPAIR PARTS BETWEEN BS807-BS847; STRINGER 19L; DUE TO NO MEET 20 INCHES BETWEEN STRINGER REPAIR SPLICES AT AFT CARGO COMPARTMENT 2024-473249<[01] TOOL USED ON STEP 3: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 220272712; DUE DATE: 28-NOV-24.;[02] MA
- [SDR SWAA2024090624621](https://openairdocs.org/sdr/SWAA2024090624621.md): Stringer · cracked · Aug 12, 2024 · N494WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK TIE CLIP LOC. BS 259 STRINGER 6L AT PASSENGER CABIN 2024-473243<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112820025 DUE DATE: 22?JAN-25;[02] REPLACED TIE CLIP LOC. BS 259 STRINGER 6L AT PASSENGER CABIN LOC. BS 259 STRINGER 6L AT PASSE
- [SDR SWAA2024090922307](https://openairdocs.org/sdr/SWAA2024090922307.md): Access Panel · cracked · Aug 3, 2024 · N494WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK ON PLATE LOCATED ACCESS PANEL 341B OUTBOARD EDGE AT HORIZONTAL STABILIZER RT 2024-473223<[01] REPLACED PLATE LOCATED ACCESS PANEL 341B OUTBOARD EDGE AT HORIZONTAL STABILIZER RT IAW B737-700 #DWG: 186A120 SHEET: 3 REV: B AND SRM 51-10-02 ITEM 9 AND SRM 51
- [SDR SWAA2024090622303](https://openairdocs.org/sdr/SWAA2024090622303.md): Access Panel · delaminated · Aug 3, 2024 · N494WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > DELAMINATED ACCESS PANEL 193CL AT LOWER FUSELAGE 2024-473211<[01] TOOL USED: CALIPER P/N:500-464 S/N:B17030933 DUE DATE:07-NOV-24.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18175478 DUE DATE: 25/JAN/25;[03] TOOL USED: SCALE: P/N:CR5200 S/N:8343110809 DU
- [SDR SWAA2024090921996](https://openairdocs.org/sdr/SWAA2024090921996.md): Angle · cracked · Aug 2, 2024 · N494WN · Boeing 7377H4 · Horizontal Stabilizer Structure
  > CRACK ACCESS PANEL 333AT ANGLE AT LT HORIZONTAL STABILIZER 2024-473197<[01] REPLACED ANGLE LOCATED ON ACCESS PANEL 333AT AT LH HORIZONTAL STABILIZER I.A.W. B737-700 SRM 51-40-02. SEE INDIVIDUAL SIGN-OFFS BELOW.;[02] CORRECTED CORRECTIVE ACTION 1: <BR>REPLACED
- [SDR SWAA2024090621995](https://openairdocs.org/sdr/SWAA2024090621995.md): Access Panel · cracked · Aug 2, 2024 · N494WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK ACCESS PANEL 343AT ANGLE AT RT HORIZONTAL STABILIZER 2024-473196<[01] REPLACED ACCESS PANEL 343AT ANGLE AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02.;[02] REPLACED ACCESS PANEL 343AT ANGLE AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02.
- [SDR SWAA2024090621561](https://openairdocs.org/sdr/SWAA2024090621561.md): Angle · cracked · Aug 1, 2024 · N494WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATED STA907 TO STA927 AND BETWEEN STR25R TO STR27R FWD POSITION AFT CARGO COMPARTMENT 2024-473168<[01] REPLACED ANGLE LOCATED STA907 TO STA927 AND BETWEEN STR25R TO STR27R FWD POSITION AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND D
- [SDR SWAA2024090621313](https://openairdocs.org/sdr/SWAA2024090621313.md): Angle · cracked · Aug 1, 2024 · N494WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATED STA500D AND LBL7 FWD CARGO COMPARTMENT 2024-473147<[01] REPLACED ANGLE LOCATED STA500D AND LBL7 FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902 SHEET 126 REV A<BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[02] REPLACED ANGLE LOCATED S
- [SDR SWAA2024090621550](https://openairdocs.org/sdr/SWAA2024090621550.md): Angle · cracked · Aug 1, 2024 · N494WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATED BS727C AT LEVEL STR18L AT AFT CARGO COMPARTMENT 2024-473155<[01] TOOL USED IN STEP 5: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631 DUE DATE: 11-MAR-25;[02] REPAIRED ANGLE LOCATED BS727A TO BS 727E AT LEVEL STR18L AT AFT CARGO C
- [SDR SWAA2024090621551](https://openairdocs.org/sdr/SWAA2024090621551.md): Angle · cracked · Aug 1, 2024 · N494WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATED BS807 AT LEVEL STR18L AT AFT CARGO COMPARTMENT 2024-473156<[01] TOOL USED IN STEP 5: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631 DUE DATE: 11-MAR-25;[02] REPAIRED ANGLE LOCATED BS727E TO BS 847 AT LEVEL<BR>STR18L AT AFT CARGO
- [SDR SWAA2024090621552](https://openairdocs.org/sdr/SWAA2024090621552.md): Angle · corroded · Aug 1, 2024 · N494WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ANGLE LOCATED BS947.5 LBL10 TO RBL21 AND WL179 AT AFT CARGO COMPARTMENT 2024-473169<[01] REPLACED ANGLE LOCATED BS947.5 LBL10 TO RBL21 AND WL179 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 <BR>SEE INDIVIDUAL SIGNOFF BELOW;[02] CORRECTED STEP 1
- [SDR SWAA2024090621557](https://openairdocs.org/sdr/SWAA2024090621557.md): Support Angle · corroded · Aug 1, 2024 · N494WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ANGLE - SUPPORT LOCATED BS767 TO BS787 RBL21 WL156 AT AFT CARGO COMPARTMENT 2024-473153<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE: 23-JAN-25. TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811019 DUE DATE: 23-
- [SDR SWAA2024090621558](https://openairdocs.org/sdr/SWAA2024090621558.md): Angle · corroded · Aug 1, 2024 · N494WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ANGLE LOCATED ON BS907 BETWEEN STR24R TO STR25R AND RBL24 WL158 AFT CARGO COMPARTMENT 2024-473164<[01] PERFORMED VISUAL INSPECTION ON ANGLE LOC. ON BS907 BETWEEN STR24R TO STR25R RBL24 WL158 AFT CARGO COMPARTMENT AND FOUND ONLY DETERIORATE MISSING PR
- [SDR SWAA2024090621563](https://openairdocs.org/sdr/SWAA2024090621563.md): Strap · corroded · Aug 1, 2024 · N494WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION STRAP LOCATED STA727D PLUS 6 INCHES AND LBL21 TO RBL21 WL156 AT AFT CARGO COMPARTMENT 2024-473175<[01] REPLACED STRAP LOCATED STA727D PLUS 6 INCHES AND LBL21 TO RBL21 WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G-0 Ï¿½TEM 9; SRM 51-40-0
- [SDR SWAA2024090521553](https://openairdocs.org/sdr/SWAA2024090521553.md): Shield · corroded · Aug 1, 2024 · N494WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SHIELD WEB LOCATED ON BS767 TO BS794 RBL21 AT AFT CARGO COMPARTMENT 2024-473150<[01] TOOL USED ON STEP 4 UT EQUIPMENT P/N: 45MG; S/N: 130064101; CAL DUE DATE: 13-DEC-24;[02] REPLACED SHIELD WEB LOCATED ON BS767 TO BS794 RBL21 AT AFT CARGO COMPARTMENT

Next page: https://openairdocs.org/aircraft/N494WN/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 = 'N494WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N494WN/reports

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