# Service difficulty reports: N497WN

A list on [N497WN](https://openairdocs.org/aircraft/N497WN.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 · 310 reports

- [SDR SWAA2026101656650](https://openairdocs.org/sdr/SWAA2026101656650.md): Lens · missing · Oct 12, 2026 · N497WN · Boeing 7377H4 · Emergency Lighting
  > MID CABIN OVHD EXIT SIGN MISSING REAR COVER. REPLACED THE LENS COVER AMM 33-25-0.
- [SDR SWAA2026082063813](https://openairdocs.org/sdr/SWAA2026082063813.md): Slide · out of position · Aug 16, 2026 · N497WN · Boeing 7377H4 · Escape Slide
  > FORWARD GALLEY SERVICE DOOR SLIDE DRAGS EXCESSIVELY WHEN OPENING DOOR. REPOSITIONED EXISTING SLIDE SO IT WOULD NOT DRAG WHEN OPENED PER 725-61-06-FS
- [SDR SWAA2026081044408](https://openairdocs.org/sdr/SWAA2026081044408.md): Panel · elongated · Aug 1, 2026 · N497WN · Boeing 7377H4 · Wing, Plate/Skin
  > LEFT LOWER WING PANEL 551GB HAD LOOSE AND WORKING FASTENERS AT BEAM ATTACHMENT. LT LOWER WING PANEL 551GB WAS REPAIRED ON FAULT TTG8Q01DGTG5. REMOVED AND REINSTALLED THE BEAM ATTACHMENT IAW SRM 51-40-02-0G AND DWG 115A2714 REV-.
- [SDR SWAA2026081077485](https://openairdocs.org/sdr/SWAA2026081077485.md): Floorbeam · cracked · Jul 22, 2026 · N497WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > FLOORBEAM CRACKED AT BS 540, BL 0, WL 208. LOCATED AND DRILLED NEW FLOORBEAM IAW SRM 51-40-05-0G-0, AND DWG 143A0060, REV A. R & R THE FLOORBEAM IAW SRM 51-40-02-0G-0, AND DWG 143A0060, REV A
- [SDR SWAA2026081083067](https://openairdocs.org/sdr/SWAA2026081083067.md): Plate · damaged · Jul 22, 2026 · N497WN · Boeing 7377H4 · Wing Main, Frame Structure
  > RIGHT WING REAR SPAR WIGGLE PLATE HAS OVERSIZED ATTACHMENT HOLES AT ORSS 259. R & R RT WING REAR SPAR WIGGLE PLATE ORSS 259 AT SMRO IAW SRM 51-40-02-0G, AND DWG 115A2001, REV-.
- [SDR SWAA2026081099954](https://openairdocs.org/sdr/SWAA2026081099954.md): Plate · damaged · Jul 22, 2026 · N497WN · Boeing 7377H4 · Wing Main, Frame Structure
  > LEFT WING REAR SPAR WIGGLE PLATE HAS OVERSIZED ATTACHMENT HOLES AT ORSS 259 REF TO FAULT TTG8Q01DAC7Z, WHERE EA 26-157-02020 ADDED AS A SUBTASK. THE FAULT WILL BE REPAIRED ON TTG8Q01DAC7Z WHERE EA 26-157-02020 WAS ADDED AS A SUBTASK.
- [SDR SWAA2026081038759](https://openairdocs.org/sdr/SWAA2026081038759.md): Shield · corroded · Jul 22, 2026 · N497WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO BAY FWD SHIELD, BS 767+10, RBL 20, WL 156. RECEIVED NEW SHIELD. LOCATED AND DRILLED IAW SRM 51-40-05-0G, & DWG 146A0081, REV A. R & R FWD SHIELD BS 767+10, RBL 20 IAW SRM 51-40-02, & DWG 146A0081, REV A.
- [SDR SWAA2026081037916](https://openairdocs.org/sdr/SWAA2026081037916.md): Battery Pack · inoperative · Jul 18, 2026 · N497WN · Boeing 7377H4 · Emergency Lighting
  > R1 DOOR LOWER FWD EMERGENCY EXIT LIGHT INOPERATIVE. FOUND ISSUE WITH BATTERY PACK M1674. WORK PERFORMED ON CARD 803827 AVIONICS 5001, TTG8Q01D8NMM.
- [SDR SWAA2026081070662](https://openairdocs.org/sdr/SWAA2026081070662.md): Battery Pack · inoperative · Jul 18, 2026 · N497WN · Boeing 7377H4 · Emergency Lighting
  > ROW 3DEF AND 5DEF EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED M1674 IAW AMM 33-51-06-960-805. OPS TESTED GOOD.
- [SDR SWAA2026081009390](https://openairdocs.org/sdr/SWAA2026081009390.md): Battery Pack · inoperative · Jul 18, 2026 · N497WN · Boeing 7377H4 · Emergency Lighting
  > L1 DOOR UPPER EMERGENCY EXIT LIGHT INOP FOUND BATTERY PACK M1674, WORK PERFORMED ON CARD 803827 AVIONICS 5001 (TTG8Q01D8NMM) FOUND ISSUE WITH BATTERY PACK M1674, WORK PERFORMED ON CARD 803827 AVIONICS 5001 (TTG8Q01D8NMM).
- [SDR SWAA2026042190196](https://openairdocs.org/sdr/SWAA2026042190196.md): Seal · cracked · Apr 17, 2026 · N497WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED. R & R LT HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL IAW AMM 53-31-31.
- [SDR SWAA2025102727922](https://openairdocs.org/sdr/SWAA2025102727922.md): Tire · damaged · Oct 23, 2025 · N497WN · Boeing 7377H4 · Tire
  > NORMAL LANDING. EXITING RUNWAY ( 25-35 KTS) FELT ANTI-SKID KICK IN. TWR ADVISED US SMOKE FROM NR 2 TIRE ON TAXI-IN FELT A/C WOBBLE WHILE TAXING. INSPECTED BRAKE SYSTEM FOR NORMAL OPERATION; FOUND BRAKE DISK TO BE LOCKING UP IAW AMM 32-41-00. PERFORMED BITE CH
- [SDR SWAA2025102728792](https://openairdocs.org/sdr/SWAA2025102728792.md): Brake · locked · Oct 23, 2025 · N497WN · Boeing 7377H4 · Landing Gear Brake System
  > NORMAL LANDING. EXITING RUNWAY ( 25-35 KTS) FELT ANTI-SKID KICK IN. TWR ADVISED US SMOKE FROM NR 2 TIRE. ON TAXI-IN FELT A/C WOBBLE WHILE TAXING. INSPECTED BRAKE SYSTEM FOR NORMAL OPS. FOUND BRAKE DISK TO BE LOCKING UP IAW AMM 32-41-00. PERFORMED BITE C
- [SDR SWAA2025092216581](https://openairdocs.org/sdr/SWAA2025092216581.md): Drain · misinstalled · Sep 19, 2025 · N497WN · Boeing 7377H4 · Fuselage Main, Structure
  > CLIMBING OUT OF 12000 WE HEARD A LOUD SCREECHING NOISE.(NOISE SO LOUD HARD TO COMMUNICATE WITH HEADSETS ON) NOTED AIRCRAFT WAS NOT PRESSURIZING. NO OTHER INDICATIONS OBSERVED. THE NOISE WENT AWAY @3000 AND AIRSPEED OF 220KTS. NOTE THE SOUND DID NOT RETURN. F
- [SDR SWAA2025072192498](https://openairdocs.org/sdr/SWAA2025072192498.md): Isolator · cracked · Jul 18, 2025 · N497WN · Boeing 7377H4 · Emergency Equipment
  > AFT ENTRY DOOR FWD UPPER SLIDE ISOLATOR IS CRACKED. R&R AFT ENTRY DOOR FWD UPPER SLIDE ISOLATOR IAW SRM 51-40-02.
- [SDR SWAA2025072192496](https://openairdocs.org/sdr/SWAA2025072192496.md): Bracket · cracked · Jul 18, 2025 · N497WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > VERTICAL BRACKET CRACKED UNDER FWD INBD CORNER OF PANEL 551AT. REMOVED & REPLACED VERTICAL BRACKET UNDER FWD INBD CORNER OF PANEL 551AT. I.A.W. SRM 51-40-02.
- [SDR SWAA2024112561461](https://openairdocs.org/sdr/SWAA2024112561461.md): Cover · missing · Nov 19, 2024 · N497WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHT ON OVERHEAD BIN AT ROW 6 ABC MISSING COVER<[01] INSTALLED NEW COVER ON EMERGENCY EXIT LIGHT AT ROW 6ABC PER B737 AMM 33-51-03. OPS CHECK GOOD.
- [SDR SWAA2024100442780](https://openairdocs.org/sdr/SWAA2024100442780.md): Lamp · inoperative · Sep 28, 2024 · N497WN · Boeing 7377H4 · Emergency Lighting
  > R/H SIDE EXTERIOR; AFT OVERWING; EMERGENCY EXIT LIGHT INOP<[01] RE-LAMPED R/H SIDE EXTERIOR; AFT OVERWING; EMERGENCY EXIT LIGHT AS PER AMM REF 33-51-04-960-801. TEST PASS;[02] VERIFIED STEP 1.
- [SDR SWAA2024100442389](https://openairdocs.org/sdr/SWAA2024100442389.md): Lens · misinstalled · Sep 26, 2024 · N497WN · Boeing 7377H4 · Emergency Lighting
  > G1 GALLEY EMERGENCY EXIT SIGN ARROW IS POINTING TOWARDS THE COCKPIT.<[01] REMOVED AND REPLACED G1 GALLEY EXIT SIGN LENS IN REF WITH AMM 33-51-01-960-802.;[02] VERIFIED CORRECTIVE ACTION.
- [SDR SWAA2024100441432](https://openairdocs.org/sdr/SWAA2024100441432.md): Housing · defective · Sep 25, 2024 · N497WN · Boeing 7377H4 · Emergency Lighting
  > OVHD BIN EMERGENCY LIGHT ROW 11-12 ABC LEFT HAND SIDE HOUSING FOUND DEFECTIVE<[01] REMOVED AND REPLACED EMERGENCY AREA LIGHT ASSEMBLY ON ROWS 11-12 ABC AS PER B737 AMM 33-51-03-960-802. INSTALLATION TEST PASSED.;[02] VERIFIED CORRECTIVE ACTION STEP 1
- [SDR SWAA2024100335272](https://openairdocs.org/sdr/SWAA2024100335272.md): Cargo Track · corroded · Sep 9, 2024 · N497WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SPOT AT AFT CARGO FLOOR STRUCTURE RAIL (LBL 13) STA 767 + 5'.<
- [SDR SWAA2024100432795](https://openairdocs.org/sdr/SWAA2024100432795.md): Fastener · missing · Aug 30, 2024 · N497WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CABIN FLR INTERCOSTAL TO FRAME ATTACH ANGLE AT STA 312 AND RBL 31 MISSING FASTENERS<[01] INSTALLED (6) EACH FASTENERS AT CABIN FLOOR INTERCOASTAL TO FRAME ATTACH ANGLE AT STA 312 AND RBL 31 REF SRM 51-40-02-0G-0 AND DWG <BR>141A5400;[02] VERIFIED STEP 1
- [SDR SWAA2024100435149](https://openairdocs.org/sdr/SWAA2024100435149.md): Support · corroded · Aug 29, 2024 · N497WN · Boeing 7377H4 · Fuel Storage
  > CORROSION CENTER TANK ACCESS PLATE 531BB SUPPORT RING. 124-039<[01] REMOVED DAMAGE AT CENTER TANK ACCESS PLATE 531BB SUPPORT RING PER REF SRM 51-10-02-0G-0 FOUND OUT OF LIMITS PER REF SRM 57-20-01-2R-1;[02] RECEIVED NEW FUEL PLATE 531BB SUPPORT RING; PANEL WIL
- [SDR SWAA2024100435148](https://openairdocs.org/sdr/SWAA2024100435148.md): Shim · corroded · Aug 29, 2024 · N497WN · Boeing 7377H4 · Fuel Storage
  > *CORROSION* CENTER TANK ACCESS PLATE 531AB SUPPORT RING. 124-038<[01] REMOVED DAMAGE AT CENTER TANK ACCESS PLATE 531AB SUPPORT RING REF SRM 51-10-02-0G-0 FOUND OUT OF LIMITS PER REF SRM 57-20-01-2R-1;[02] RECEIVED NEW FUEL PLATE 531AB SUPPORT RING; PANEL WILL
- [SDR SWAA2024100434877](https://openairdocs.org/sdr/SWAA2024100434877.md): Shim · debonded · Aug 29, 2024 · N497WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > LT WING TANK PLATE 532BB SUPPORT RING SHIM DEBONDED. 124-043<[01] RECEIVED NEW LT.WING TANK PLATE 532BB RING; PLATE AND RING WILL BE INSTALL ON TTG8Q00UX02X;[02] VERIFIED STEP 1
- [SDR SWAA2024100331503](https://openairdocs.org/sdr/SWAA2024100331503.md): Floor Panel · peeling · Aug 28, 2024 · N497WN · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 231HF HAS PEELED UPPER SURFACE LAYER FIBERS.<[01] FLOOR PANEL 231HF WAS RECEIVED AND WILL BE INSTALLED ON TASK CARD TTG8Q00VHX9H.;[02] ENTRY ON ERROR STEP 1 SHOULD READ: FLOOR PANEL 231HF WAS RECEIVED AND WILL BE INSTALLED ON TASK CARD TTG8Q0
- [SDR SWAA2024100331504](https://openairdocs.org/sdr/SWAA2024100331504.md): Floor Panel · peeling · Aug 28, 2024 · N497WN · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 231GF HAS PEELED UPPER SURFACE LAYER FIBERS.<[01] FLOOR PANEL 231GF WAS RECEIVED AND WILL BE INSTALLED ON TASK CARD TTG8Q00VHX9M.;[02] ENTR ON ERROR STEP 1 SHOULD READ: FLOOR PANEL 231GF WAS RECEIVED AND WILL BE INSTALLED ON TASK CARD TTG8Q00
- [SDR SWAA2024100331505](https://openairdocs.org/sdr/SWAA2024100331505.md): Floor Panel · peeling · Aug 28, 2024 · N497WN · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 231UF HAS PEELED UPPER SURFACE LAYER FIBERS.<[01] FLOOR PANEL 231UF WAS RECEIVED AND WILL BE INSTALLED ON TASK CARD TTG8Q00VHX9S.;[02] ENTRY ON ERROR STEP 1 SHOULD READ: FLOOR PANEL 231UF WAS RECEIVED AND WILL BE INSTALLED ON TASK CARD TTG8Q0
- [SDR SWAA2024100331506](https://openairdocs.org/sdr/SWAA2024100331506.md): Floor Panel · peeling · Aug 28, 2024 · N497WN · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 231KF HAS PEELED UPPER SURFACE LAYER FIBERS.<[01] RECEIVED FLOOR PANEL 231KF WILL BE INSTALLED ON TTG8Q00VG21D AS PER AMM 53-21-00-400-801;[02] VERIFIED CORRECTIVE ACTION.
- [SDR SWAA2024100331346](https://openairdocs.org/sdr/SWAA2024100331346.md): Cargo Track · corroded · Aug 27, 2024 · N497WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SPOT AT AFT CARGO FLOOR STRUCTURE RAIL (RBL 13) STA 767 + 5'.<[01] REMOVED AND REPLACED EXISTING REPAIR AND RAIL FROM STA 727 TO STA 887 PER SRM 51-40-02-0G-0; SRM 53-00-53-2R-3 AND DRG #146A7500
- [SDR SWAA2024100331341](https://openairdocs.org/sdr/SWAA2024100331341.md): Splice · corroded · Aug 27, 2024 · N497WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SPOT AT AFT CARGO FLOOR STRUCTURE WEB INTERCOSTAL SPLICE (RBL 20) STA 787 + 5'. CORROSION SPOT AT AFT CARGO FLOOR STRUCTURE WEB STRAP (RBL 20) STA 787 + 5' STR25R WL 156.4.<[01] REMOVED CORROSION ON WEB STRAP STA 787+5 RBL 20; FOUND EXFOLIATED CORROS
- [SDR SWAA2024100331123](https://openairdocs.org/sdr/SWAA2024100331123.md): Floor Panel · corroded · Aug 27, 2024 · N497WN · Boeing 7377H4 · Fuselage Floor Panel
  > *CORROSION* FLT. COMPARTMENT FLOOR PANEL 211AF HAS CORRROSION AS MARKED ON UNDER SIDE OF PANEL BOARDER. 124-029<[01] FOUND PANEL 211AF OUT OF LIMITS PER SRM 53-10-51-1A-1; RECEIVED NEW PANEL 211AF; PANEL WILL BE INSTALL ON (TTG8Q00UX018);[02] VERIFIED STEP 1<B
- [SDR SWAA2024100331335](https://openairdocs.org/sdr/SWAA2024100331335.md): Support Bracket · cracked · Aug 27, 2024 · N497WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO FWD BULKHEAD SUPPORT 144A9401-20 CRACKED.<[01] REMOVED AND REPLACED SUPPORT BRACKET AT AFT CARGO FWD BULKHEAD SRM 51-40-02-0G-0 AND DWG:144A9401;[02] VERIFIED STEP# 1
- [SDR SWAA2024100331345](https://openairdocs.org/sdr/SWAA2024100331345.md): Floor Support · corroded · Aug 27, 2024 · N497WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AT AFT CARGO FLOOR STRUCTURE INTERCOSTAL (BETWEEN STA 747-767) RH UNDER Z CHANNEL MULTIPLE AREAS. CORROSION AT AFT CARGO FLOOR STRUCTURE INTERCOSTAL (BETWEEN STA 747-767 RBL 21 WL 156.3) RH UNDER Z CHANNEL MULTIPLE AREAS.<[01] REMOVED AND REPLACED AF
- [SDR SWAA2024100331338](https://openairdocs.org/sdr/SWAA2024100331338.md): Cargo Track · corroded · Aug 27, 2024 · N497WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SPOT AT AFT CARGO FLOOR STRUCTURE RAIL (RBL 8) STA 767 + 5'.<[01] FOUND CORROSION DAMAGE ON PREVIOUS REPAIR AT STA. 767+5'; RBL 8; WL 156.4; NO ALLOWABLE DAMAGED; REMOVED PREVIOUS REPAIR AT STA. 767+5'; RBL 8; WL 156.4 PER REF. SRM 51-40-02-0G-0 AND
- [SDR SWAA2024100331347](https://openairdocs.org/sdr/SWAA2024100331347.md): Cargo Track · corroded · Aug 27, 2024 · N497WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SPOT AT AFT CARGO FLOOR STRUCTURE RAIL (RBL 3) STA 767 + 5'.<[01] FOUND CORROSION DAMAGE ON PREVIOUS REPAIR AT STA. 767+5'; RBL 3; WL 156.4; NO ALLOWABLE DAMAGED; REMOVED PREVIOUS REPAIR AT STA. 767+5'; RBL 3; WL 156.4 PER REF. SRM 51-40-02-0G-0 AND
- [SDR SWAA2024100331339](https://openairdocs.org/sdr/SWAA2024100331339.md): Cargo Track · corroded · Aug 27, 2024 · N497WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SPOT AT AFT CARGO FLOOR STRUCTURE RAIL (LBL 3) STA 767 + 5'.<[01] REMOVED DAMAGED PREVIUS REPAIR FABRICATED; LOCATED AND DRILLED NEW REINFORCING CHANNEL MATERIAL BAC1510-1355 7050-T76511 PO# 2084940 AND INSTALLED REPAIR PART (REINFORCING CHANNEL) AT
- [SDR SWAA2024100331340](https://openairdocs.org/sdr/SWAA2024100331340.md): Cargo Track · corroded · Aug 27, 2024 · N497WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SPOT AT AFT CARGO FLOOR STRUCTURE RAIL (LBL 8) STA 767 + 5'.<[01] REMOVED DAMAGED PREVIUS REPAIR FABRICATED; LOCATED AND DRILLED NEW REINFORCING CHANNEL MATERIAL BAC1510-1355 7050-T76511 PO# 2084940 AND INSTALLED REPAIR PART (REINFORCING CHANNEL) AT
- [SDR SWAA2024100437195](https://openairdocs.org/sdr/SWAA2024100437195.md): Nut · corroded · Aug 26, 2024 · N497WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > LEFT HORIZONTAL STABILIZER STA 203.10 ( # 5 BAY)INSIDE CLAMP SUPPORT WIRING AND ANCHORNUT RUSTED.<[01] REMOVED AND INSTALLED NEW CLIP NUT; CLAMP AND SCREW AT LEFT HORIZONTAL STABILIZER STA 203.10(#5 BAY) PER REF. SWPM 20-10-12.<BR> TOOL USED: TORQUE WRENCH: B
- [SDR SWAA2024100430609](https://openairdocs.org/sdr/SWAA2024100430609.md): Panel · delaminated · Aug 26, 2024 · N497WN · Boeing 7377H4 · Wing, Plate/Skin
  > L/W LEADING EDGE PNL 521KB FWD EDGE DELAMINATED<[01] APPLIED PERMANENT REPAIR ON DAMAGE AREA AS MARKED ON PANEL #521KB AS PER B737 SRM 51-70-04-2R-13; TOOL USED: TEMPERATURE CONTROL ID 172858 DUE DATE 5-13-25; MATERIAL USED: PO#2061896; PO#1690463. APPLIED TOP
- [SDR SWAA2024100430940](https://openairdocs.org/sdr/SWAA2024100430940.md): Panel · delaminated · Aug 26, 2024 · N497WN · Boeing 7377H4 · Wing, Plate/Skin
  > RIGHT WING LEADING EDGE PNL 621JB DELAM AT FWD EDGE<[01] REPAIRED DAMAGE AREA AT RIGHT WING LEADING EDGE PANEL 621JB AS PER SRM 51-70-04-2R-13.MATERIAL USED EA9390 PO2061896 PLUS BMS9-3-120TYD CL7.;[02] VERIFIED CORRECTIVE ACTION.
- [SDR SWAA2024100330942](https://openairdocs.org/sdr/SWAA2024100330942.md): Panel · cracked · Aug 26, 2024 · N497WN · Boeing 7377H4 · Instrument Panel
  > FLIGHT COMPARTMENT CONSOLE PANEL 212BW COMPOSITE MATERIAL EXPOSED AND CRACKED BY MICROPHONE JACK.<[01] REPAIRED PANEL#212BW PER B737 AMM 25-00-00-300-801. MATERIAL USED RESIN 50-A PO#2073293 FIBERGLASS PO#173857.;[02] VERIFIED STEP 1.
- [SDR SWAA2024100429486](https://openairdocs.org/sdr/SWAA2024100429486.md): Rib · cracked · Aug 23, 2024 · N497WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > HORIZONTAL STABILIZER LEADING EDGE PANEL 331B 4TH RIB FROM OUTBOARD END IS CRACKED<[01] REMOVED AND REPLACED 4TH RIB AT L/HORIZONTAL STAB L/E PANEL 331B SRM 51-40-02-0G-0 AND DWG 186A1001;[02] VERIFIED AND INSPECTED.
- [SDR SWAA2024100329794](https://openairdocs.org/sdr/SWAA2024100329794.md): Skin · corroded · Aug 23, 2024 · N497WN · Boeing 7377H4 · Service Doors
  > *CORROSION* TOILET SERVICE DOOR 145AL INNER SKIN AROUND BONDING JUMER AND BENEATH SEALANT OF BONDING JMPER. 124-026<[01] REPLACED TOILET SERVICE DOOR 145AL REF 51-40-02-0G-0
- [SDR SWAA2024100431977](https://openairdocs.org/sdr/SWAA2024100431977.md): Seat Track · worn · Aug 22, 2024 · N497WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > L/H O/B SEAT TRACK STA 520 SHOWS WEAR ADD TO ORIGINAL FAULT: LBL 45 AND WATERLINE 208.1<[01] ACCOMPLISHED SEAT TRACK SECTION AND SPLICE REPAIR FROM STA 500D-10' TO STA 521 LBL-45.50 REF SRM 53-00-52-2R-4 AND DWG#143A5300;[02] VERIFIED STEP 1
- [SDR SWAA2024100430259](https://openairdocs.org/sdr/SWAA2024100430259.md): Seat Track · worn · Aug 22, 2024 · N497WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > L/H I/B SEAT TRACK STA 520 SHOWS WEAR ADD TO ORIGINAL FAULT: LBL 24 AND WATERLINE 208.1<[01] REMOVED AND REPLACED SEAT TRACK SECTION BETWEEN STA 480 TO STA 520 AND LBL 24.75 IN REF BOEING DRAWING #143A5300 AND SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1
- [SDR SWAA2024100329483](https://openairdocs.org/sdr/SWAA2024100329483.md): Floor Panel · delaminated · Aug 22, 2024 · N497WN · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 242CF FWD L/E DELAMINATED<[01] ENTRY ON ERROR SHOULD READ: FLOOR PANEL 242CF WAS RECEIVED AND WILL BE INSTALLED ON TASK CARD TTG8Q00UWZHV.;[02] STEP 1 ENTRY ON ERROR SHOULD READ: FLOOR PANEL 242CF WAS RECEIVED AND WILL BE INSTALLED ON TASK CA
- [SDR SWAA2024100329485](https://openairdocs.org/sdr/SWAA2024100329485.md): Floor Panel · delaminated · Aug 22, 2024 · N497WN · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 242CF DELAM AT FWD EDGE CABIN FLOOR PANEL 242DF DELAM AT FWD EDGE<[01] FLOOR PANEL 242CF WAS RECEIVED AND WILL BE INSTALLED ON TASK CARD TTG8Q00UWZHR.;[02] ENTRY ON ERROR SHOULD READ: FLOOR PANEL 242DF WAS RECEIVED AND WILL BE INSTALLED ON TA
- [SDR SWAA2024100438739](https://openairdocs.org/sdr/SWAA2024100438739.md): Attach Bracket · cracked · Aug 21, 2024 · N497WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > LEFT AIR CONDITIONING BAY PNEUMATIC CROSS OVER DUCT ATTACH BRACKET ON KEEL BEAM CRACKED JUST AFT OF F.S. 540. (DOT 51-002)<[01] VERIFIED STEP 1.
- [SDR SWAA2024100428426](https://openairdocs.org/sdr/SWAA2024100428426.md): Fastener · pulled · Aug 20, 2024 · N497WN · Boeing 7377H4 · Leading Edge Devices
  > RIGHT WING LOWER SURFACE OF THE L/E # 7 SLAT ACTUATOR SKIN HAS FOUR FASTENERS PULLED IN.<[01] REMOVED AND REPLACED FOUR FASTENERS AT RIGHT WING LOWER SURFACE OF L/E #7 SLAT ACTUATOR FITTING TO SKIN IN REF B737-700 SRM 57-42-01-2R-8 PARAGRAPH 4.;[02] VERIFIED S

Next page: https://openairdocs.org/aircraft/N497WN/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 = 'N497WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N497WN/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.