# Service difficulty reports: N464WN

A list on [N464WN](https://openairdocs.org/aircraft/N464WN.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 · 318 reports

- [SDR SWAA2026092253284](https://openairdocs.org/sdr/SWAA2026092253284.md): Comms Unit · malfunctioned · Sep 14, 2026 · N464WN · Boeing 7377H4 · VHF Communications System
  > LOSS OF COMMS 1/2 AND ACARS, FLYING THROUGH WEATHER. PERFORMED STATIC DISCHARGER INSPECTION IAW AMM 23-61-00, NO DEFECTS NOTED. PERFORMED VHF COMMS SYSTEM OPS CHK IAW AMM 23-12-00 NO DEFECTS NOTED. ACFT OK FOR SERVICE.
- [SDR SWAA2026071420043](https://openairdocs.org/sdr/SWAA2026071420043.md): Isolator · cracked · Jul 10, 2026 · N464WN · Boeing 7377H4 · Escape Slide
  > FWD SERVICE DOOR ESCAPE SLIDE AFT ISOLATOR CRACKED. R & R FWD SERVICE DOOR ESCAPE SLIDE AFT ISOLATOR IAW SRM 51-40-02.
- [SDR SWAA2026071320046](https://openairdocs.org/sdr/SWAA2026071320046.md): Battery Pack · failed · Jul 10, 2026 · N464WN · Boeing 7377H4 · Emergency Lighting
  > AFT RT EMERGENCY BATTERY PACK M1672 FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06.
- [SDR SWAA2026071320045](https://openairdocs.org/sdr/SWAA2026071320045.md): Battery Pack · failed · Jul 10, 2026 · N464WN · Boeing 7377H4 · Emergency Lighting
  > AFT LEFT EMERGENCY BATTERY PACK M1673 FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06
- [SDR SWAA2026041383872](https://openairdocs.org/sdr/SWAA2026041383872.md): Strap · cracked · Mar 27, 2026 · N464WN · Boeing 7377H4 · Leading Edge Devices
  > FOUND CRACK ON LEFT HAND WING LEADING EDGE TO WING LWR ATTACHMENT AT 452.75 WING STATION<[01] UPON FURTHER INVESTIGATION NO CRACK WAS FOUND. DAMAGE FOUND TO BE CORROSION ONLY. ALL CORROSION MAINTENANCE WILL BE ACCOMPLISHED ON FAULT TTG8Q01B6MKV;[02] VERIFIED:
- [SDR SWAA2026040982147](https://openairdocs.org/sdr/SWAA2026040982147.md): Scuff Plate · cracked · Mar 22, 2026 · N464WN · Boeing 7377H4 · Cargo Compartments
  > FWD CARGO FWD CORNER SCUFF PLATE CRACKED<[01] LOCATED AND DRILLED REPLACEMENT FWD CARGO FWD CORNER SCUFF PLATE P/N 654A0004-337 LOT# 7530406 IAW SRM 51-40-05-0G-0 AND BOEING DWG# 143A8330 REV:-;[02] FWD CARGO; FWD CORNER SCUFF PLATE WILL BE INSTALLED ON TTG8Q0
- [SDR SWAA2026040982251](https://openairdocs.org/sdr/SWAA2026040982251.md): Scuff Plate · cracked · Mar 22, 2026 · N464WN · Boeing 7377H4 · Cargo Compartments
  > AFT CARGO FWD CORNER SCUFF PLATE CRACKED<[01] LOCATED AND DRILLED AFT CARGO FWD CORNER SCUFF PLATE IAW B737 SRM 51-40-05-0G AND DRAWING 146A8340 REV - SCUFF PLATE TO BE INSTALLED ON FAULT TTG8Q01B8N46;[02] VERIFIED: LOCATED AND DRILLED AFT CARGO FWD CORNER SCU
- [SDR SWAA2026040982252](https://openairdocs.org/sdr/SWAA2026040982252.md): Web · corroded · Mar 22, 2026 · N464WN · Boeing 7377H4 · Cargo Compartments
  > CORROSION ALONG FWD CARGO DOOR TRHESHHOLD<[01] REMOVED AND REPLACED FWD CARGO THRESHOLD WEB IAW SRM 51-40-02-0G-0 AND BOEING DWG# 143A8330 REV:-;[02] VERIFIED COMPLETE.
- [SDR SWAA2026040982253](https://openairdocs.org/sdr/SWAA2026040982253.md): Threshold · corroded · Mar 22, 2026 · N464WN · Boeing 7377H4 · Cargo Compartments
  > CORROSION ALONG AFT CARGO DOOR TRHESHOLD<[01] REMOVED AND REPLACED TRHESHOLD ON FWD CARGO; IAW B737 SRM 51-40-02-0G STEP 5; AND DWG 146A8340 R -;[02] CORRECTION TO CORRECTIVE ACTION: REMOVED AND REPLACED THRESHOLD ON AFT CARGO; IAW B737 SRM 51-40-02-0G STEP 5;
- [SDR SWAA2026040980898](https://openairdocs.org/sdr/SWAA2026040980898.md): Strap · cracked · Mar 18, 2026 · N464WN · Boeing 7377H4 · Leading Edge Devices
  > FOUND CRACK AND CORROSION ON LEFT HAND WING LEADING EDGE TO WING LWR ATTACHMENT AT 452.75 WING STATION.<[01] REPAIRED LEFT HAND WING LEADING EDGE TO WING LWR ATTACH STRAP AT WSTA 452.75 (OSS 227.95) PER EA 26-157-00825 TTG8Q01BKAXB;[02] VERIFIED: REPAIRED LEFT
- [SDR SWAA2026022473875](https://openairdocs.org/sdr/SWAA2026022473875.md): Quick Disconnect · leaking · Feb 23, 2026 · N464WN · Boeing 7377H4 · Landing Gear Brake System
  > BRAKE SEVERELY SHUDDERING WHEN ATTEMPTING TO STOP AT THE GATE. COMING TO A STOP WAS VERY DIFFICULT. R & R NR 4 MLG BRAKE IAW AMM 32-41-41, FOUND NR 4 MLG BRAKE DISCONNECT TO BE LEAKING. R & R BRAKE DISCONNECT IAW AMM 32-42-11, PERFORMED BRAKE BLEEDING IAW AM
- [SDR SWAA2026012864353](https://openairdocs.org/sdr/SWAA2026012864353.md): Valve · failed · Jan 24, 2026 · N464WN · Boeing 7377H4 · Hydraulic System, Main
  > HYDRAULIC B SYSTEM FAILURE. IF IT IS A PRIORITY VALVE THERE IS A DEVIATION ALL EA FOR THE CHECK OUT M-25-127-00862. R & R T/E FLAP FLOW LIMITER VALVE IAW AMM 27-51-67. OPS CHECKED. NO LEAKS DETECTED.
- [SDR SWAA2025010682785](https://openairdocs.org/sdr/SWAA2025010682785.md): Lamp · inoperative · Jan 3, 2025 · N464WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHT - ABOVE F/O SIDE - EMERGENCY EXIT OUT<[01] RELAMPED F/O SIDE EMERGENCY EXIT LIGHT REF AMM 33-51-01. OPS CHK GOOD.
- [SDR SWAA2024091135054](https://openairdocs.org/sdr/SWAA2024091135054.md): Tail Cone · delaminated · Sep 7, 2024 · N464WN · Boeing 7377H4 · Aerodynamic Fairings
  > FUSELAGE SECTION 48 DELAMINATION COMMON TO TAIL CONE<[01] PERFORMED PERMANENT REPAIR OF THE TAIL CONE IAW SRM 51-70-04
- [SDR SWAA2024080722685](https://openairdocs.org/sdr/SWAA2024080722685.md): Lens · broken · Aug 4, 2024 · N464WN · Boeing 7377H4 · Emergency Lighting
  > FO SIDE EMERGENCY EXIT LENS INDICATOR BROKEN<[01] REMOVE AND REPLACE FO SIDE EXIT LENS INDICATOR PER AMM 33-51-01. OPS CHECK GOOD.
- [SDR SWAA2024062404772](https://openairdocs.org/sdr/SWAA2024062404772.md): Slide · out of position · Jun 22, 2024 · N464WN · Boeing 7377H4 · Escape Slide
  > L2 DOOR SLIDE CATCHES ON THRESHOLD<[01] CORRECTED THE Z-FOLD ON L2 DOOR SLIDE AND TUCKED EXCESS GIRT MATERIAL IN REF WORK INSTRUCTIONS 725-61-06;[02] VERIFIED STEP 1.
- [SDR SWAA2024062401925](https://openairdocs.org/sdr/SWAA2024062401925.md): Sign · broken · Jun 14, 2024 · N464WN · Boeing 7377H4 · Emergency Lighting
  > AFT LOWERED CEILING PANEL EXIT SIGN BROKEN<[01] REMOVED AND REPLACED AFT CEILING PANEL EXIT SIGN ASSEMBLY AS PER B737 AMM 33-51-01-960-802. OPS CHECK PASSED.;[02] VERIFIED STEP 1.
- [SDR SWAA2024062599500](https://openairdocs.org/sdr/SWAA2024062599500.md): Light · glazed · Jun 8, 2024 · N464WN · Boeing 7377H4 · Emergency Lighting
  > MAIN CABIN PHOTOLUMINESCENT ARE GLAZED/SCRATCHED<[01] REMOVED AND REPLACED MAIN CABIN PHOTOLUMINESCENT IN REF AMM-33-51-15-000-802; 33-51-15-400-802;[02] CORRECTION: REMOVED AND REPLACED MAIN CABIN PHOTOLUMINESCENT IN REF AMM-33-51-15-000-802; 33-51-15-400-802
- [SDR SWAA2024062597847](https://openairdocs.org/sdr/SWAA2024062597847.md): Battery Pack · no test · Jun 3, 2024 · N464WN · Boeing 7377H4 · Emergency Lighting
  > SEVERAL PAX CABIN EMERGENCY LIGHT BATTERIES WILL NOT HOLD CHARGE<[01] REMOVED AND REPLACED PAX EMERGENCY LIGHT BATTERY PACK M1675 I/A/W BOEING AMM 33-51-06-960-805; OPS CHECK NORMAL;[02] VERIFIED STEP 1<BR>AUDIT C/W PER MPM 52.02.02
- [SDR SWAA2024062691159](https://openairdocs.org/sdr/SWAA2024062691159.md): Skin · delaminated · May 29, 2024 · N464WN · Boeing 7377H4 · Trailing Edge Flaps
  > L/WING O/B AFT FLAP I/B LOWER T/EDGE SKIN AREA DELAMINATED FOUND OUT-LIMIT<[01] REMOVED & INSTALLED LEFT WING O/B AFT FLAP AS PER AMM 27-51-22-400-801. ACCOMPLISHED ADJUSTMENT FOUND TO BE WITHIN LIMITS. <BR>DIGITAL CALIPER USED BC 175307 DUE DATE 05-DEC-24<BR>
- [SDR SWAA2024062590273](https://openairdocs.org/sdr/SWAA2024062590273.md): Seal · cracked · May 26, 2024 · N464WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > R/H HOR. STAB FWD UPPER SLIDER SEAL CRACKED.<[01] REMOVED STABILIZER TO BODY UPPER FRONT SPAR SLIDING SEAL AS PER AMM 53-31-31-000-802; TRANSFERED TIE-BAR AND CORNER PLATES FROM OLD SEAL PLATE TO NEW SEAL PLATE REF SRM 51-40-02-0G-0; AND INSTALLED STABILIZER T
- [SDR SWAA2024062589194](https://openairdocs.org/sdr/SWAA2024062589194.md): Plate · damaged · May 23, 2024 · N464WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > LH WING DEFLECTOR RIB ATTACH SERRATED PLATE HOLES ELONGATED<[01] REMOVED BOLTS AT L/H WING DEFLECTOR CONTROL RIB UPPER TAB IN REF B737-700 SRM 51-40-02-0G-0; AFTER FURTHER INSPECTION FOUND NO ENLONGATED HOLES; AND NO SERRATED PLATES DAMAGE; REPLACED BOLTS IN R
- [SDR SWAA2024062589195](https://openairdocs.org/sdr/SWAA2024062589195.md): Bracket · damaged · May 23, 2024 · N464WN · Boeing 7377H4 · Wing, Attach Fittings
  > RIGHT WING TRAILING EDGE ACCESS PANEL 651GB ROD CONNECTED TO I/B AFT BRACKET UPPER BRACKET HOLE ELONGATED<[01] REMOVED AND INSTALLED NEW BRACKET AT PANEL # 651GB RIGHT WING TRAILING EDGE AS PER SRM 51-40-02-0G-0 AND AIPC 57-15-00-09.;[02] VERIFIED CORRECTIVE A
- [SDR SWAA2024062589199](https://openairdocs.org/sdr/SWAA2024062589199.md): Bracket · damaged · May 23, 2024 · N464WN · Boeing 7377H4 · Wing, Plate/Skin
  > RIGHT WING TRAILING EDGE ACCESS PANEL 651GB I/B AFT BRACKET HOLE ELONGATED<[01] REMOVED AND INSTALLED NEW BRACKET AT PANEL # 651GB RIGHT WING TRAILING EDGE AS PER SRM 51-40-02-0G-0 AND AIPC 57-15-00-09.;[02] VERIFIED CORRECTIVE ACTION STEP 1<BR><BR>AUDIT C/W R
- [SDR SWAA2024062589196](https://openairdocs.org/sdr/SWAA2024062589196.md): Bracket · corroded · May 23, 2024 · N464WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > EVIDENCE OF CORROSION UNDER SEALANT AT LEFT AFT BOOST PUMP BONDING STRAP<[01] REMOVED AND REPLACED BOTH UPPER AND LOWER BONDING STRAPS/BRACKETS AT LEFT WING AFT BOOST PUMP IAW SRM 51-40-02-0G-0; AIPC 28-22-41-05; AMM 20-10-44-400-801. PERFORMED ELECTRICAL RESI
- [SDR SWAA2024062401200](https://openairdocs.org/sdr/SWAA2024062401200.md): Access Panel · damaged · May 23, 2024 · N464WN · Boeing 7377H4 · Wing, Plate/Skin
  > RIGHT WING TRAILING EDGE ACCESS PANEL 651GB SECOND BRACKET FROM I/B ROD HOLE ELONGATED<[01] REMOVED AND INSTALLED NEW BRACKET AT PANEL # 651GB RIGHT WING TRAILING EDGE AS PER SRM 51-40-02-0G-0 AND AIPC 57-15-00-09.;[02] VERIFIED CORRECTIVE ACTION STEP 1<BR><BR
- [SDR SWAA2024062489490](https://openairdocs.org/sdr/SWAA2024062489490.md): Scuff Plate · cracked · May 23, 2024 · N464WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FOUND FWD CARGO COMPARTMENT FWD CORNER SCUFF PLATE CRACKED<[01] SCUFFPLATE WAS REPAIRED BY OUTSIDE VENDOR PO #414715 INSTALLATION OF SCUFFPLATE WILL BE ACCOMPLISHED ON CARD TTG8Q001TFBY;[02] VERIFIED STEP 1<BR>AUDIT C/W PER MPM 52.02.02
- [SDR SWAA2024062489201](https://openairdocs.org/sdr/SWAA2024062489201.md): Door Frame · cracked · May 23, 2024 · N464WN · Boeing 7377H4 · Fuselage Main, Structure
  > FORWARD GALLEY SERVICE DOOR (R-1) CUTOUT UPPER FWD CORNER FRAME CRACK<[01] REMOVED AND REPLACED FORWARD GALLEY SERVICE DOOR (R-1) CUTOUT UPPER FWD CORNER FRAME REF SRM 51-40-02-0G-0 AND DWG 141A8370;[02] VERIFIED STEP 1<BR>AUDIT C/W PER MPM 52.02.02
- [SDR SWAA2024062588997](https://openairdocs.org/sdr/SWAA2024062588997.md): Intercostal · corroded · May 22, 2024 · N464WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > E&E COMP CORROSION ON INTERCOSTAL BS 344-360 S23L. PARTIALLY INSTALLED INTERCOSTAL IAW SRM 51-40-02 & DWG 141A8131. REMOVED AND REPLACED INTERCOSTAL BS 344-360, S23L IAW 51-40-02, & DWG 141A8131. APPLIED EWIS PROTECTION AS REQUIRED IAW AMM 20-60-07-913-80
- [SDR SWAA2024062488998](https://openairdocs.org/sdr/SWAA2024062488998.md): Intercostal · cracked · May 22, 2024 · N464WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK INDICATION OBTAINED FROM FWD FASTENER HOLE OF INTERCOSTAL AT COCKPIT FLOOR STA 250 RBL 4.<[01] ACCOMPLISHED EA 24-153-01485. REF FAULT TTG8Q00TH8E7;[02] STEP 1 IN CORRECTIVE ACTION ENTER IN ERROR;[03] ACCOMPLISHED EA 24-153-01485;[04] VERIFIED STEP 3
- [SDR SWAA2024062588645](https://openairdocs.org/sdr/SWAA2024062588645.md): Floor Support · cracked · May 21, 2024 · N464WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > MAIN CABIN WING CENTER SECTION FLOOR SUPPORT BREAK CRACKED AT STA 540 LBL 1 MKD DOT<[01] REMOVED AND REPLACED FLOOR SUPPORT BRACKET AT MAIN CABIN STA 540 LBL 1' AS PER SRM 51-40-02-0G-0 AND DWG 143A0060.;[02] VERIFIED STEP 1.;[03] AUDIT C/W PER MPM 52.02.02.
- [SDR SWAA2024062588641](https://openairdocs.org/sdr/SWAA2024062588641.md): Floorbeam · cracked · May 21, 2024 · N464WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > MAIN CABIN WING CENTER SECTION FLOOR SUPPORT BREAK CRACKED AT STA 540 RBL 1. FAULT RESOLVED ON OTHER FAULT. WORK ACCOMPLISHED ON TTG8Q00TE4QN.;[02] VERIFIED STEP 1.<BR>AUDIT C/W PER MPM 52.02.02.
- [SDR SWAA2024062588642](https://openairdocs.org/sdr/SWAA2024062588642.md): Floor Panel · cracked · May 21, 2024 · N464WN · Boeing 7377H4 · Fuselage Floor Panel
  > MAIN CABIN WING CENTER SECTION FLOOR PANEL 231YF CRACKED AT AFT END MKD DOT<[01] PERFORMED DRY OUT; PREPARED DAMAGE AREA AND APPLIED PERMANENT REPAIR ON PANEL#231YF AS PER B737 SRM 53-00-50-2R-7 MATERIAL USED PO#1690453 PO#2039827;[02] CORRECTION TO STEP 1: PE
- [SDR SWAA2024062588647](https://openairdocs.org/sdr/SWAA2024062588647.md): Floor Support · corroded · May 21, 2024 · N464WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > MAIN CABIN WING CENTER SECTION FLOOR SUPPORT INNER CHORD CORRODED FROM STA 639-5' TO STA 639+8' RBL 64. REMOVED AND REPLACED FLOOR SUPPORT INNER CHORD AT STA 639 -5 TO 639 +8 RBL 64 IN MAIN CABIN CENTER SECTION IAW SRM 51-40-02-0G-0 AND DWG 144A5901.
- [SDR SWAA2024062488644](https://openairdocs.org/sdr/SWAA2024062488644.md): Skin · cracked · May 21, 2024 · N464WN · Boeing 7377H4 · Trailing Edge Flaps
  > L/H WING I/B AFT FLAP LOWER SURFACE SKIN CRACK AT 28.25' O/B EDGE & 5' T/E<[01] NSTALLED REPAIR AT L/H WING I/B AFT FLAP ON LOWER SURFACE SIZE OF REPAIR 3' DIAMETER PER B737SRM 51-70-10-2R-0 PARAGRAPH(20.B) MATERIAL USED ADHESIVE AF163-2K-06 PO#2053056 AND TOO
- [SDR SWAA2024062587816](https://openairdocs.org/sdr/SWAA2024062587816.md): Gusset · cracked · May 19, 2024 · N464WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMP STA 500D STR 19L GUSSET CRACKED. REMOVED AND REPLACED GUSSET AT FWD CARGO COMP STA 500D STR 19L AS PER SRM 51-40-02-0G-0 & 143A7902.
- [SDR SWAA2024062587817](https://openairdocs.org/sdr/SWAA2024062587817.md): Gusset · cracked · May 19, 2024 · N464WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > FWD CARGO COMP STA 500D STR 19R GUSSET CRACK. REMOVED AND REPLACED GUSSET AT FWD CARGO COMP STA 500D STR 19R AS PER SRM 51-40-02-0G-0 & DWG 143A9481.
- [SDR SWAA2024062587670](https://openairdocs.org/sdr/SWAA2024062587670.md): Stringer · corroded · May 19, 2024 · N464WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > AREA AFT OF FWD CARGO STA 540 STR 26L LOWER SECTION CORROSION. ACOMPLISHED REPAIR ON STR 26L AFT OF FWD CARGO STA 540 AS PER SRM 51-40-02-0G-0 AND EA 24-153-01393.
- [SDR SWAA2024062587678](https://openairdocs.org/sdr/SWAA2024062587678.md): Skin · delaminated · May 19, 2024 · N464WN · Boeing 7377H4 · Trailing Edge Flaps
  > L/W OUB AFT FLAP INB LOWER T/E I/B TIP SKIN AREA DELAMINATED MKD DOT<[01] FLAP IS BEEING REPLACED ON WORK CARD TTG8Q00TMGD9;[02] VERIFIED STEP 1<BR>AUDIT C/W PER MPM 52.02.02
- [SDR SWAA2024062487687](https://openairdocs.org/sdr/SWAA2024062487687.md): Web · cracked · May 19, 2024 · N464WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR CUTOUT LOWER WEB CRACK AT STA 807+2'<[01] REMOVED AND REPLACED WEB AT AFT CARGO DOOR CUTOUT SRM 51-40-02-0G-0 AND DWG 146A8123;[02] VERIFIED STEP 1<BR>AUDIT C/W AS PER 52.02.02
- [SDR SWAA2024062587264](https://openairdocs.org/sdr/SWAA2024062587264.md): Panel · peeling · May 18, 2024 · N464WN · Boeing 7377H4 · Nacelle/Pylon, Main Frame
  > PANEL 431DL INNER SURFACE IS PEELING<[01] REPAIRED INNER SURFACE PANEL 431DL. AS PER; SRM 51-70-14-2R-3.;[02] VERIFIED STEP 1<BR>AUDIT C/W PER MPM 52.02.02
- [SDR SWAA2024062487276](https://openairdocs.org/sdr/SWAA2024062487276.md): Scuff Plate · cracked · May 18, 2024 · N464WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FOUND AFT CARGO AFT CORNER SCUFF PLATE CRACKED<[01] AFT CARGO AFT CORNER WAS REPAIRED BY OUTSIDE VENDOR JL WELDING UNDER PO # 414704 USING GUIDELINES ON REFERENCE SRM 53-60-15-2R-1 REPAIR 1. INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q001TFAV;[02] VERI
- [SDR SWAA2024062587249](https://openairdocs.org/sdr/SWAA2024062587249.md): Floor Panel · frayed · May 17, 2024 · N464WN · Boeing 7377H4 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 221BF UPPER SURFACE FRAYING<[01] REMOVED AND INSTALLED MAIN CABIN FWD WET AREA FLOOR PANEL 221BF IN REF 53-21-00-000-801; 53-21-00-400-801;[02] VERIFIED STEP 1<BR>AUDIT C/W PER MPM 52.02.02
- [SDR SWAA2024062587252](https://openairdocs.org/sdr/SWAA2024062587252.md): Floor Panel · frayed · May 17, 2024 · N464WN · Boeing 7377H4 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 222BF UPPER SURFACE FRAYING<[01] REMOVED AND INSTALLED MAIN CABIN FWD WET AREA FLOOR PANELS 222BF IN REF AMM-53-21-00-000-801; 53-21-00-400-801;[02] VERIFIED STEP 1<BR>AUDIT C/W PER MPM 52.02.02
- [SDR SWAA2024062587253](https://openairdocs.org/sdr/SWAA2024062587253.md): Floor Panel · frayed · May 17, 2024 · N464WN · Boeing 7377H4 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 242VF UPPER SURFACE FRAYING<[01] REMOVED AND INSTALLED MAIN CABIN FLOOR PANEL 242VF AS PER AMM-53-21-00-000-801 AND AMM 53-21-00-400-801;[02] VERIFIED STEP 1. <BR><BR>AUDIT C/W AS PER MPM 52.02.02
- [SDR SWAA2024062587250](https://openairdocs.org/sdr/SWAA2024062587250.md): Stringer · cracked · May 17, 2024 · N464WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > AREA AFT OF FWD CARGO STA 540 STR 23R LOWER SECTION CRACK<[01] ACCOMPLISHED REPAIR PER EA 24-153-01392 AND SRM 53-00-03-2R-1;[02] VERIFIED STEP 1<BR>AUDIT C/W PER MPM 52.02.02
- [SDR SWAA2024062587251](https://openairdocs.org/sdr/SWAA2024062587251.md): Stringer · cracked · May 17, 2024 · N464WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > AREA AFT OF FWD CARGO STA 540 STR 23L LOWER SECTION CRACK<[01] THIS REPAIR WAS ACCOMPLISHED ON TASK CARDS TTG8Q00TML8P- 24-153-01394-WIP1; TTG8Q00TSFFY- 24-153-10394-WIP2; TTG8Q00TT1F1- 24-153-01394-WIP3 AND TTG8Q00TVJFV- 24-153-01394- WIP 4. STRINGER 23L REPA
- [SDR SWAA2024062587256](https://openairdocs.org/sdr/SWAA2024062587256.md): Angle · cracked · May 17, 2024 · N464WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > MAIN CABIN STA 540 RBL 1' PANEL BREAK ANGLE CRACK<[01] REMOVED AND REPLACED PANEL ANGLE AT MAIN CABIN STA 540 RBL 1' AS PER SRM 51-40-02-0G-0 AND DWG 143A0060.;[02] VERIFIED STEP 1.<BR>AUDIT C/W PER MPM 52.02.02.
- [SDR SWAA2024062587258](https://openairdocs.org/sdr/SWAA2024062587258.md): Rib · cracked · May 17, 2024 · N464WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > LH HORIZONTAL STABILIZER L/E PANEL 331B #3 RIB CRACK COUNTING FROM I/B TO O/B<[01] REMOVED AND REPLACED NEW RIB#3 AT LH HORIZONTAL STABILIZER L/E PANEL 331B REF 51-40-02-0G-0;[02] VERIFIED STEP 1<BR>AUDIT C/W PER MPM 52.02.02
- [SDR SWAA2024062587260](https://openairdocs.org/sdr/SWAA2024062587260.md): Rib · cracked · May 17, 2024 · N464WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > LH HORIZONTAL STABILIZER L/E PANEL 331B #4 RIB CRACK COUNTING FROM I/B TO O/B<[01] REMOVED AND REPLACED NEW RIB#4 AT LH HORIZONTAL STABILIZER L/E PANEL 331B REF SRM 51-40-02-0G-0;[02] VERIFIED STEP 1<BR>AUDIT C/W PER MPM 52.02.02

Next page: https://openairdocs.org/aircraft/N464WN/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 = 'N464WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N464WN/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.