# Service difficulty reports: N465WN

A list on [N465WN](https://openairdocs.org/aircraft/N465WN.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 · 285 reports

- [SDR SWAA2026101274296](https://openairdocs.org/sdr/SWAA2026101274296.md): Assist Handle · broken · Oct 7, 2026 · N465WN · Boeing 7377H4 · Emergency Exits
  > PASSENGER ENTRY DOOR ASSIST HANDLE BROKEN. REMOVED AND REPLACED IAW AMM INTRODUCTION-NG (USE OF STANDARD INDUSTRY PRACTICES - SIP - PERMANENT)]
- [SDR SWAA2026031678273](https://openairdocs.org/sdr/SWAA2026031678273.md): Engine · power loss · Mar 10, 2026 · N465WN · Boeing 7377H4 · Engine (Turbine/Turboprop)
  > AT TOP OF CLIMB NR 1 ENGINE REDUCED TO 60% N1 UN-COMMANDED WITH NO THRUST LEVER SPLIT, NR 2 ENGINE REDUCED TO 85% N1 AS EXPECTED. AUTO-THROTTLES WERE ON. ALL OTHER INDICATIONS NORMAL. AND ENGINE OPS NORMALLY FOR REMAINDER OF FLIGHT. PERFORMED NR 1 ENGINE AC
- [SDR SWAA2026012859175](https://openairdocs.org/sdr/SWAA2026012859175.md): Plate · cracked · Jan 7, 2026 · N465WN · Boeing 7377H4 · Wing Main, Frame Structure
  > CRACKED CORRUGATED PLATE ORSS 261, RT WING T/E. REPLACED THE CORRUGATED PLATE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 115A2001, SHEET 29, REV -.
- [SDR SWAA2026012859177](https://openairdocs.org/sdr/SWAA2026012859177.md): Angle · cracked · Jan 7, 2026 · N465WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACKED ANGLE, ORSS 271, RT WING T/E. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, & DWG 115A2900, SHEET 2, REV E. MEASUREMENT OF CRACK: L= 0.320.
- [SDR SWAA2026012859176](https://openairdocs.org/sdr/SWAA2026012859176.md): Plate · cracked · Jan 7, 2026 · N465WN · Boeing 7377H4 · Wing Main, Frame Structure
  > CRACKED CORRUGATED PLATE ORSS 241, RT WING T/E. REPLACED THE CORRUGATED PLATE IAW SRM 51-40-02-0G, & DWG 115A2001, SHEET 30, REV A.
- [SDR SWAA2026012858919](https://openairdocs.org/sdr/SWAA2026012858919.md): Support Bracket · cracked · Jan 6, 2026 · N465WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT BRACKET ON THE VAPOR BARRIER, RBL 15.54 - RBL 25. REPLACED THE SUPPORT BRACKET IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 111A1000, SHEET 141, REV -.
- [SDR SWAA2026012858801](https://openairdocs.org/sdr/SWAA2026012858801.md): Vapor Barrier · cracked · Jan 6, 2026 · N465WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > CRACKED VAPOR BARRIER RT SIDE BETWEEN RBL 15 & 25. REPAIRED THE VAPOR BARRIER IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2026012858916](https://openairdocs.org/sdr/SWAA2026012858916.md): Rib · cracked · Jan 6, 2026 · N465WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > CRACKED RIB, LE STA 142.45 ACCESS PANEL 341B, RT HORIZONTAL STAB REPLACED THE RIB IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 186A1001, SHEET 10, REV A.
- [SDR SWAA2026012858310](https://openairdocs.org/sdr/SWAA2026012858310.md): Landing · cracked · Jan 5, 2026 · N465WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACKED ACCESS PANEL 343AT LANDING AT RT HORIZONTAL STAB. REPLACED THE LANDING AND FASTENER IAW SRM 51-40-02, & 51-10-02 ITEM 9. MEASURE OF CRACK IS L: 0.249?.<BR>TOOL USED: DIGITAL CALIPER P/N: 500-197-30 S/N: B23316868 DUE DATE 17/APR/26.;[02] CERTIFIED
- [SDR SWAA2026012857873](https://openairdocs.org/sdr/SWAA2026012857873.md): Crossbeam · cracked · Jan 3, 2026 · N465WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACKED CROSSBEAM, BS 540, BL 0 - RBL 24.75. REPLACED CROSSBEAM IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A0060, SHEET 36, REV A.
- [SDR SWAA2026012857874](https://openairdocs.org/sdr/SWAA2026012857874.md): Crossbeam · cracked · Jan 3, 2026 · N465WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACKED CROSSBEAM BS 540, BL 0 - LBL 24.75. REPLACED CROSSBEAM IAW SRM 51-40-02, AND DWG 143A0060, SHEET 36, REV A.
- [SDR SWAA2026012857876](https://openairdocs.org/sdr/SWAA2026012857876.md): Support Angle · cracked · Jan 3, 2026 · N465WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT ANGLE BS 695, RBL 24.75. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 273A9110, SHEET 6, REV A.
- [SDR SWAA2026012857983](https://openairdocs.org/sdr/SWAA2026012857983.md): Access Panel · elongated · Jan 3, 2026 · N465WN · Boeing 7377H4 · Wing, Plate/Skin
  > ELONGATED HOLES ON ACCESS PANEL 561CB, T/E, LT WING. REPAIRED THE ACCESS PANEL 561CB IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2026012757877](https://openairdocs.org/sdr/SWAA2026012757877.md): Floor Support · cracked · Jan 3, 2026 · N465WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED FLOOR SUPPORT, OTBD SIDE, BS 695 BL 0. REPLACED FLOOR SUPPORT AND FASTENERS IAW SRM 51-40-02-0G-0, AND DWG 273A9110, SHEET 6, REV A.
- [SDR SWAA2026012757879](https://openairdocs.org/sdr/SWAA2026012757879.md): Floor Support · cracked · Jan 3, 2026 · N465WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED FLOOR SUPPORT, BS 695, BL 0. REPLACED THE FLOOR SUPPORT AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 273A9110, SHEET 6, REV A.
- [SDR SWAA2026012757880](https://openairdocs.org/sdr/SWAA2026012757880.md): Floor Support · cracked · Jan 3, 2026 · N465WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED FLOOR SUPPORT OTBD SIDE, BS 695, BL 0. REPLACED FLOOR SUPPORT IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DRAWING 273A9110, SHEET 6, REV A.
- [SDR SWAA2026012757741](https://openairdocs.org/sdr/SWAA2026012757741.md): Skin · cracked · Jan 2, 2026 · N465WN · Boeing 7377H4 · Leading Edge Devices
  > CRACKED SLAT 2, SS 322.71, LT WING. PERFORMED PERMANENT REPAIR IAW SRM 57-42-01-2R-8, REPAIR 8.
- [SDR SWAA2025123156725](https://openairdocs.org/sdr/SWAA2025123156725.md): Slide · out of adjust · Dec 29, 2025 · N465WN · Boeing 7377H4 · Escape Slide
  > FWD GALLEY DOOR SLIDE PARTIALLY OUT OF BOX. INSTALLED THE FWD SERVICE DOOR SLIDE ASSEMBLY IAW MT 725-61-06.
- [SDR SWAA2025121953161](https://openairdocs.org/sdr/SWAA2025121953161.md): Battery Pack · inoperative · Dec 17, 2025 · N465WN · Boeing 7377H4 · Emergency Lighting
  > FOUND ROW 6 ABC EMERGENCY LIGHT INOPERATIVE. R & R THE BATTERY PACK IAW AMM 33-51-06. OPS CHECKED GOOD.
- [SDR SWAA2025121651934](https://openairdocs.org/sdr/SWAA2025121651934.md): Handle · broken · Dec 13, 2025 · N465WN · Boeing 7377H4 · Service Doors
  > R1 DOOR ASSIST HANDLE BROKEN. INSTALLED A SERVICEABLE ASSIST HANDLE ONTO THE R1 DOOR FROM FWD LAVATORY IAW AMM 52-11-31. OK TO CONTINUE IAW MEL 25-10-01, SP1B AUTH 297294. R&R DOOR ASSIST HANDLE PER SIP.
- [SDR SWAA2025091715500](https://openairdocs.org/sdr/SWAA2025091715500.md): Transfer Sys · no discrepancy · Sep 16, 2025 · N465WN · Boeing 7377H4 · Aircraft Fuel Distribution System
  > AFTER LEVEL OFF AT 10;000 ABOUT 12 MINUTES INTO FLIGHT WE RECEIVED A MASTER CAUTION FOR FUEL W/FUEL IMBALANCE ON NR 1 TANK. COMPLIED WITH QRH TO BALANCE FUEL. FUEL WAS WITHIN LIMITS ON LANDING. NO OVERWEIGHT LANDING. NO ABNORMAL ENGINE INDICATIONS OBSERVED. E
- [SDR SWAA2025091513812](https://openairdocs.org/sdr/SWAA2025091513812.md): Engine · failed · Sep 11, 2025 · N465WN · Boeing 7377H4 · Engine (Turbine/Turboprop)
  > NUMBER 1 ENGINE FAILED AFTER TAKEOFF, LOUD BANG, N1 DROPPED TO APPROX 16%, EGT REMAINED IN THE YELLOW. NO NOTICEABLE SMELL OF SMOKE R & R NR 1 ENGINE IAW MT 771-00-01.
- [SDR SWAA2025090811786](https://openairdocs.org/sdr/SWAA2025090811786.md): Charger · inoperative · Sep 5, 2025 · N465WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHT OVERHEAD AILSE AT MID CABIN AND LIGHT ON OVERWING EXIT CAPT SIDE WILL NOT ILLUMINATE. REMOVED AND REPLACED BATTERY CHARGER AND BATTERY AMM 33-51-06
- [SDR SWAA2025090812316](https://openairdocs.org/sdr/SWAA2025090812316.md): Battery · inoperative · Sep 5, 2025 · N465WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHT OVERHEAD AILSE AT MID CABIN AND LIGHT ON OVERWING EXIT CAPT SIDE WILL NOT ILLUMINATE. REMOVED AND REPLACED BATTERY CHARGER AND BATTERY AMM 33-51-06.
- [SDR SWAA2025061079046](https://openairdocs.org/sdr/SWAA2025061079046.md): Cover · missing · Jun 7, 2025 · N465WN · Boeing 7377H4 · Emergency Lighting
  > CABIN R/H EMERGENCY EXIT DOOR FWD EMERGENCY LIGHT COVER IS MISSING.<[01] INSTALLED NEW LIGHT COVER ON EXIT SIGN FOR R/H EMERGENCY EXIT DOOR FWD LIGHT PER AMM 33-51-01.
- [SDR SWAA2025021795502](https://openairdocs.org/sdr/SWAA2025021795502.md): Girt Bar · unpacked · Feb 13, 2025 · N465WN · Boeing 7377H4 · Emergency Equipment
  > L1 DOOR ESCAPE SLIDE GIRT REPACKED REQUIRED.<[01] REPACKED L1 DOOR SLIDE GIRT PER AMM 25-66-01.
- [SDR SWAA2025021395501](https://openairdocs.org/sdr/SWAA2025021395501.md): Girt Bar · debonded · Feb 13, 2025 · N465WN · Boeing 7377H4 · Emergency Equipment
  > AFT SERVICE DOOR R2 DOOR SLIDE GIRT BONDED BLACK LINER DISBONDED & SEPERATED.<[01] REMOVED AND REPLACED R2 DOOR SLIDE PER AMM 25-66-01. REF BARCODE TTG8Q004QAHQ FOR R/I.
- [SDR SWAA2025012388881](https://openairdocs.org/sdr/SWAA2025012388881.md): Bushing · loose · Jan 23, 2025 · N465WN · Boeing 7377H4 · Emergency Equipment
  > PLASTIC BUSHING FELL OFF FWD SERVICE DOOR GIRT BAR<[01] REPLACED BUSHING IAW MM 25-66-01.
- [SDR SWAA2024100745252](https://openairdocs.org/sdr/SWAA2024100745252.md): Cover · missing · Oct 4, 2024 · N465WN · Boeing 7377H4 · Emergency Lighting
  > L1 DOOR EMERG EXIT SING COVER MISSING<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-01-960-802-NG (EXIT SIGN - LIGHT ASSEMBLY REPLACEMENT - PERMANENT)]
- [SDR SWAA2024091638147](https://openairdocs.org/sdr/SWAA2024091638147.md): Slide · detached · Sep 16, 2024 · N465WN · Boeing 7377H4 · Escape Slide
  > FWD ENTRY DOOR SLIDE PARTIALLY FELL OUT OF COVER<[01] REINSTALLED SLIDE IN COVER PER MT 725-61-06. A/C OK FOR SERVICE.
- [SDR SWAA2024030753243](https://openairdocs.org/sdr/SWAA2024030753243.md): Scuff Plate · cracked · Feb 17, 2024 · N465WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > REJECT: CRACK FOUND AT FWD CORNER SCUFF PLATE ACB<[01] UPDATED MEASUREMENT TABLE;[02] IT WAS REMOVED AND WELDED FWD CORNER SCUFF PLATE;APPLIED CHEMICAL CONVERSION AND PRIMER.;[03] VERIFIED CORRECTIVE ACTION 2 AND MEASUREMENT TABLE
- [SDR SWAA2024030652468](https://openairdocs.org/sdr/SWAA2024030652468.md): Fairing · delaminated · Feb 14, 2024 · N465WN · Boeing 7377H4 · Trailing Edge Flaps
  > #1 CANOE FAIRING AFT FAIRING HAS DELAMINATION ON AFT END.<[01] REMOVED AND REPLACED #1 CANOE FAIRING AFT FAIRING IAW AIPC 27-51-28-01 AND AMM 20-50-11-910-801<BR><BR> SCREW GUN ID PER2216 CAL DUE 11/2024;[02] UPDATED PARTS FIELD;[03] VERIFIED CORRECTIVE ACTION
- [SDR SWAA2024030850539](https://openairdocs.org/sdr/SWAA2024030850539.md): Skin · corroded · Feb 9, 2024 · N465WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > REJECT: CORROSION AT FUSELAGE SKIN AROUND RADIO ALTIMETER ANTENNA STA-450 BTW STR-27L TO STR-28L<[01] REMOVED CORROSION AND REWORKED AREA AROUND RADIO ALTIMETER ANTENNA STA-450 BTW STR-27L TO STR-28L IAW EA 24-153-00438.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1
- [SDR SWAA2024030850538](https://openairdocs.org/sdr/SWAA2024030850538.md): Skin · corroded · Feb 9, 2024 · N465WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > REJECT: CORROSION AT FUSELAGE SKIN AROUND RADIO ALTIMETER ANTENNA STA-410 BTW STR-27L TO STR-28L<[01] VERIFIED STEP 3 COMPLETED;[02] 'REFER TO FAULT TTG8Q00RFUS3 FOR REPAIR RESOLUTION'.;[03] VERIFIED CORRECTIVE ACTION ENTRY 2.
- [SDR SWAA2024030849681](https://openairdocs.org/sdr/SWAA2024030849681.md): Panel · corroded · Feb 6, 2024 · N465WN · Boeing 7377H4 · Wing Main, Frame Structure
  > RIGHT WING FUELING PANEL (621GB) FUEL GAUGE PANEL IS CORRODED<[01] REPLACED WING REFUEL PANEL (P15) PER AMM 28-21-00-000-801; INSTALLED PER AMM 28-21-00-400-801 STEP 3.A THRU 3.G. PERFORMED GOOD BONDIG CHECK RECORDING VALUE 0.7 MILLIOHMS<BR><BR>BONDING METER:<
- [SDR SWAA2024030749685](https://openairdocs.org/sdr/SWAA2024030749685.md): Drip Tray · cracked · Feb 6, 2024 · N465WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FLIGHT COMPARTMENT FLOOR STRUCTURE - CRACKED DRIPSHIELD BS 211.8 LBL 38 WL 208 (MARKED)<[01] REMOVED AND REPLACED FLIGHT COMPARTMENT FLOOR STRUCTURE DRIP SHIELD BS 211.8 LBL 38 WL 208 IAW SOPM 20-50-01;[02] VERIFIED
- [SDR SWAA2024030749684](https://openairdocs.org/sdr/SWAA2024030749684.md): Bracket · cracked · Feb 6, 2024 · N465WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > FLIGHT COMPARTMENT OVERHEAD - CRACKED BRACKET ASSY ON DRIP SHIELD OVHD BS 211.8 S-3R (MARKED)<[01] REMOVED AND REPLACED FLIGHT COMPARTMENT OVERHEAD RECEPTICLE ON DRIP SHIELD BS 211.8 S-3R IAW SRM 51-40-02-0G-0 AND BOEING DWG 232A1304.;[02] UPDATED MEASUREMENTS
- [SDR SWAA2024030749683](https://openairdocs.org/sdr/SWAA2024030749683.md): Bracket · cracked · Feb 6, 2024 · N465WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > FLIGHT COMPARTMENT OVERHEAD - CRACKED BRACKET ASSY ON DRIP SHIELD OVHD BS 211.8 S-3L (MARKED)<[01] REMOVED AND REPLACED FLIGHT COMPARTMENT OVERHEAD RECEPTICLE ON DRIP SHIELD BS 211.8 S-3L IAW SRM 51-40-02-0G-0 AND BOEING DWG 232A1304.;[02] CORRECTED MEASUREMEN
- [SDR SWAA2024030749673](https://openairdocs.org/sdr/SWAA2024030749673.md): Bracket · cracked · Feb 6, 2024 · N465WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > WING CENTER SECTION - CRACK ON SUPPORT AIR DUCT BS 540+7 RBL 6.30 WL 170.65 (MARKED)<[01] REMOVED AND REPLACED RH AIR DUCT SUPPORT BRACKET IAW SRM 51-40-02 AND AIPC 36-13-01-01A;[02] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASUREMENT TABLE.
- [SDR SWAA2024030749674](https://openairdocs.org/sdr/SWAA2024030749674.md): Bracket · cracked · Feb 6, 2024 · N465WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > WING CENTER SECTION - CRACK ON SUPPORT AIR DUCT BS 540+7 LBL 6.30 WL 170.65 (MARKED)<[01] REMOVED AND REPLACED LH AIR DUCT SUPPORT BRACKET IAW SRM 51-40-02 AND AIPC 36-13-01-01A;[02] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASUREMENT TABLE.
- [SDR SWAA2024030749416](https://openairdocs.org/sdr/SWAA2024030749416.md): Bracket · cracked · Feb 6, 2024 · N465WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > MAIN E-BAY O2 BOTTLE FWD SUPPORT BRACKET; LOWER ATTACH ANGLE IS CRACKED AT O/B FASTENER (MARKED)<[01] VERIFIED DAMAGE EVALUATION;[02] REMOVED AND INSTALLED NEW SUPPORT BRACKET LOT# 1551121-1; PER DWG 417A4121 AND SRM 51-40-02;[03] UPDATED PARTS SECTION;[04] VE
- [SDR SWAA2024030749409](https://openairdocs.org/sdr/SWAA2024030749409.md): Angle · cracked · Feb 6, 2024 · N465WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > SKIN SPLICES CRACKED AROUND HARDWARES AFT CARGO BS 907-927; WL 150; RBL 15.0.<[01] REMOVED AND REPLACED 2EA SUPPORT ANGLES FROM AFT CARGO BAY BETWEEN BS 907 TO BS 927 WL 150 RBL 15 PER SRM 51-40-02; SRM 51-40-05 AND DWG 147A7221;[02] VERIFIED CORRECTIVE ACTION
- [SDR SWAA2024030848716](https://openairdocs.org/sdr/SWAA2024030848716.md): Panel · pulled · Feb 4, 2024 · N465WN · Boeing 7377H4 · Wing, Plate/Skin
  > R/W T/E PANEL 661BB HAS SEVERAL PULLED FASTENER HOLES UNDER THE T/E SEAL (MARKED)<[01] R/W T/ E PANEL 661BB FASTENER HOLES HAVE BEEN REPAIRED IAW SRM 51-70-04-2R-9.<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.;[03] JOB COM
- [SDR SWAA2024030748722](https://openairdocs.org/sdr/SWAA2024030748722.md): Shield · corroded · Feb 4, 2024 · N465WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD SHIELD CORRODED AROUND NUTPLATE HOLES LBL 21; 787-807; WL 150 FWD SHIELD CORRODEDN AROUND NUTE PLATES RBL 21 BS787-807 WL 150.<[01] REMOVED AND REPLACED ON AFT DOOR FWD SHIELD BS 787 TO BS 807 RBL 21 IAW SRM 51-40-02 AND DWG 146A0081;[02] VERIFIED CORRECTI
- [SDR SWAA2024030748503](https://openairdocs.org/sdr/SWAA2024030748503.md): Sidewall Support · corroded · Feb 4, 2024 · N465WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION FOUND AT SECTION 1; LBL 21; BS 440-500; WL 150 FAULT CORRECTION-CORROSION FOUND AT SECTION 1 AROUND NUTPLATE HOLES AT FLOOR TO SIDEWALL SUPPORT<[01] EVALUATED DAMAGE; WAS FOUND OUT LIMITS PER SRM 53-00-53-1A-2. STEP 4. (A) (2.A) FIG. 103.<BR> THIS CA
- [SDR SWAA2024030748720](https://openairdocs.org/sdr/SWAA2024030748720.md): Support · corroded · Feb 4, 2024 · N465WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR TO SIDEWALL SUPPORT RBL 21; BS 727 TO BS 787; WL 150<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT RBL 21; BS 727 TO BS 787; WL 150 I.A.W SRM 51-10-02-0G-0; SRM 51-40-02-0G-0 AND DWG 146A7500.;[02] VERIFIED CORRECTIVE ACTION 1.<BR>JOB
- [SDR SWAA2024030748719](https://openairdocs.org/sdr/SWAA2024030748719.md): Support · corroded · Feb 4, 2024 · N465WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR TO SIDEWALL SUPPORT LBL 21; BS 727C TO BS 807; WL 150.<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT LBL 21; BS 727C TO BS 807; WL150 I.A.W SRM 51-10-02-0G-0; SRM 51-40-02-0G-0 AND DWG 146A7500.;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2024030748717](https://openairdocs.org/sdr/SWAA2024030748717.md): Shield · corroded · Feb 4, 2024 · N465WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT DOOR SHIELD CORRODED MULTIPLE AREAS BS 867-887; RBL 21; WL 150 AFT DOOR SHIELD CORROEDED MULTIPLE AREAS BS 847-867 RBL 21 WL 150.<[01] REMOVED AND REPLACED ON AFT DOOR SHIELD BS 847 TO BS 867 RBL 21 IAW SRM 51-40-02 AND DWG 146A0081;[02] VERIFIED CORRECTIV
- [SDR SWAA2024030748509](https://openairdocs.org/sdr/SWAA2024030748509.md): Rail · corroded · Feb 4, 2024 · N465WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > CORROSION FOUND AROUND NUTPLATES AROUND NUTPLATES BS 500 D; WL 150; LBL 8.1 AND 12.5<[01] VERIFIED STEP 7 IN PARTIAL.;[02] REMOVED AND REINSTALLED AFT BULKHEAD LOWER RAIL AT BS 500 D WL 150 LBL 24.75 TO RBL 24.75 IAW SRM 51-40-02 AND DWG 143A7902.;[03] UPDATED
- [SDR SWAA2024030748507](https://openairdocs.org/sdr/SWAA2024030748507.md): Shield · corroded · Feb 4, 2024 · N465WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT FWD CARGO DOOR FLOOR SHIELD HAS CORROSION AROUND NUTPLATE HOLES FAULT CORRECTION-AFT FWD CARGO DOOR FLOOR SHIELD HAS CORROSION AROUND NUTPLATE HOLES RBL 21 WL 150 BS 500-500A.<[01] REMOVED AND REPLACED AT FWD CARGO DOOR; AFT SHIELD WITH P/N 143A8126-31 LOT

Next page: https://openairdocs.org/aircraft/N465WN/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 = 'N465WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N465WN/reports

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