# Service difficulty reports: N455WN

A list on [N455WN](https://openairdocs.org/aircraft/N455WN.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 8 · 352 reports

- [SDR SWAA2026082139058](https://openairdocs.org/sdr/SWAA2026082139058.md): Handle · broken · Aug 17, 2026 · N455WN · Boeing 7377H4 · Emergency Equipment
  > CAPTAINS GRAB HAMDLE BROKEN. R & R HANDLE IAW SIP. NO DEFECTS NOTED.
- [SDR SWAA2026050194336](https://openairdocs.org/sdr/SWAA2026050194336.md): Slide · dislodged · Apr 30, 2026 · N455WN · Boeing 7377H4 · Escape Slide
  > L1 DOOR SLIDE FELL OUT. REINSTALLED SLIDE IAW 26-66-01.
- [SDR SWAA2026041789660](https://openairdocs.org/sdr/SWAA2026041789660.md): Door · cracked · Apr 16, 2026 · N455WN · Boeing 7377H4 · Landing Gear Doors
  > LEFT MLG STRUT GEAR DOOR IS CRACKED AT FWD LOWER ATTACH POINT INNER DOOR REMOVED SERVICEABLE PER CDL REQUIREMENT. REMOVED CENTER AND INNER GEAR DOOR REF MM 32-13-11 OK TO CONT REF AUTH 315248;[02] REMOVED CENTER AND INNER GEAR DOOR REF MM 32-10-03 OK TO CONT
- [SDR SWAA2026041789707](https://openairdocs.org/sdr/SWAA2026041789707.md): Battery Pack · no test · Apr 16, 2026 · N455WN · Boeing 7377H4 · Emergency Lighting
  > AFT LEFTT EMERGECY BATTERY PACK M01673 FAILED A CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06.
- [SDR SWAA2026041689705](https://openairdocs.org/sdr/SWAA2026041689705.md): Light · loose · Apr 16, 2026 · N455WN · Boeing 7377H4 · Emergency Lighting
  > PASSENGER CABIN SEAT ROW 1 ABC PHOTOLUMINESCENT STRIP LOOSE AND MOISTURE UNDER COVER. REMOVED AND REPLACED PER AMM 33-51-15;[02] INSPECTION C/W REMOVED AND REPLACED PER AMM 33-51-15
- [SDR SWAA2026020567513](https://openairdocs.org/sdr/SWAA2026020567513.md): Bracket · loose · Feb 4, 2026 · N455WN · Boeing 7377H4 · Emergency Equipment
  > THE GIRT BAR BRACKET ON THE LT SIDE, FORWARD ENTRY, IS LOOSE. SECURED THE GIRT BAR IAW AMM 25-66-00. OPS CHECK GOOD.
- [SDR SWAA2025111434447](https://openairdocs.org/sdr/SWAA2025111434447.md): Data Plate · loose · Nov 12, 2025 · N455WN · Boeing 7377H4 · Placards and Markings
  > CUSTOMER REQUEST LOOSE RIVETS AT PLACARD DATA ON OUTBOARD SIDE ENGINE 2<2025-671319
- [SDR SWAA2025111830618](https://openairdocs.org/sdr/SWAA2025111830618.md): Angle · cracked · Oct 31, 2025 · N455WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK ANGLE TRAILING EDGE LOCATED ORSS 276 AT RT WING. REPLACED ANGLE TRAILING EDGE LOCATED ORSS 276 AT RT WING IAW SRM 51-40-02. MEASURE CRACK IS:0.996.
- [SDR SWAA2025111830620](https://openairdocs.org/sdr/SWAA2025111830620.md): Angle · cracked · Oct 31, 2025 · N455WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK ANGLE TRAILING EDGE LOCATED ORSS 271 LT WING. REPLACED ANGLE AND FASTENERS TRAILING EDGE LOCATED ORSS 271 LT WING IAW SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A2930 SHEET 7, REV -.
- [SDR SWAA2025111830409](https://openairdocs.org/sdr/SWAA2025111830409.md): Panel · debonded · Oct 31, 2025 · N455WN · Boeing 7377H4 · Trailing Edge Flaps
  > DEBONDED EXTERNAL SKIN UPPER AREA OF WEDGE PANEL LOC ON INBD MAIN FLAP, LT WING. REPAIRED WEDGE PANEL LOC ON INB MAIN FLAP LT WING IAW B737-700 SRM 57-53-01-2R-7 REPAIR 7.
- [SDR SWAA2025111830014](https://openairdocs.org/sdr/SWAA2025111830014.md): Scuff Plate · cracked · Oct 30, 2025 · N455WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK FWD POSITION CORNER SCUFF PLATE CUT OUT DOOR AT FWD CARGO BAY. REPAIRED FWD POSITION CORNER SCUFF PLATE CUT OUT DOOR IAW SRM 53-30-15-2R-1, REPAIR 1, & BAC 5975.
- [SDR SWAA2025111830197](https://openairdocs.org/sdr/SWAA2025111830197.md): Floorbeam · cracked · Oct 30, 2025 · N455WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CRACKED PLATE ON FLOORBEAM LOCATED BS 540 BETWEEN BL 0 TO RBL 24.75. REPLACED PLATE ON THE FLOORBEAM IAW SRM 51-40-02 AND DRAWING 143A0060, SHEET 36, REV A.
- [SDR SWAA2025111830200](https://openairdocs.org/sdr/SWAA2025111830200.md): Stiffener · cracked · Oct 30, 2025 · N455WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CRACKED FLOORBEAM LOCATED BS540 BETWEEN BL 0 TO LBL 24.75. REPLACED THE FLOORBEAM IAW SRM 51-40-02 AND DRAWING 143A0060, SHEET 36, REV A.
- [SDR SWAA2025111830407](https://openairdocs.org/sdr/SWAA2025111830407.md): Lens · broken · Oct 30, 2025 · N455WN · Boeing 7377H4 · Emergency Lighting
  > BROKEN EMERGENCY LIGHT LENS ON SIDEWALL PANEL 242YAW AT PASSENGER CABIN. REPLACED EMERGENCY LIGHT LENS ON SIDEWALL PANEL 242YAW AT PASSENGER CABIN IAW AMM 33-51-01-960-802 OPS TESTED OK.
- [SDR SWAA2025111829679](https://openairdocs.org/sdr/SWAA2025111829679.md): Rib · cracked · Oct 28, 2025 · N455WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > CRACK LEADING EDGE RIB LOCATED LE STA 95.96 RT HORIZONTAL STAB. REPLACED RIB AND FASTENERS LOCATED ON LEADING EDGE LE STA 95.96 AT RT HORIZONTAL STABILIZER IAW SRM 51-40-02-0G-0 AND DRAWING 186A1001, SHEET 10, REV A.
- [SDR SWAA2025111829417](https://openairdocs.org/sdr/SWAA2025111829417.md): Doubler · cracked · Oct 28, 2025 · N455WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK ON EXISTING DOUBLER REPAIR LOCATED ON BS 235.5 AFT POSITION ELECTRICAL GROUND POWER ACCESS. PERFORMED PERMANENT REPAIR LOCATED ON BS 235.5 AFT POSITION ELECTRICAL GROUND POWER ACCESS IAW SRM 51-40-02 AND SRM 53-10-15-2R-4 REPAIR 4 IAW SRM 51-40-02 AND 5
- [SDR SWAA2025111829041](https://openairdocs.org/sdr/SWAA2025111829041.md): Pressure Web · cracked · Oct 27, 2025 · N455WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK INDICATION FOUND (2EA) ON HORIZONTAL PRESSURE WEB AT LBL 31 BETWEEN STA 663 TO STA 675 IN MAIN WHEEL WELL. CRACK LENGTHS: 0.250 IN. & 0.187 IN. PERFORMED A PERMANENT REPAIR ON HORIZONTAL PRESSURE WEB IAW SRM 53-40-51-2R-2, REPAIR 2, AND EA 25-153-03006
- [SDR SWAA2025111829040](https://openairdocs.org/sdr/SWAA2025111829040.md): Pressure Web · cracked · Oct 27, 2025 · N455WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK INDICATION FOUND ON HORIZONTAL PRESSURE DECK WEB AT RBL 41 BETWEEN STA 663 TO STA 675 IN THE MAIN WHEEL WELL CRACK LENGTH: 0.312 IN. PERFORMED PERMANENT REPAIR ON THE PRESSURE WEB IAW SRM 53-40-51-2R-2, REPAIR 2.
- [SDR SWAA2025100922969](https://openairdocs.org/sdr/SWAA2025100922969.md): Fastener · loose · Oct 9, 2025 · N455WN · Boeing 7377H4 · Wing Main, Frame Structure
  > NUMBER 6 TRAILING EDGE AFT FLAP FAIRING HAS 3 LOOSE AND/OR PULLED THRU FASTENERS FWD OF PREVIOUS REPAIR. REPAIRED NR 6 INBD TE FLAP FAIRING ATTACH FASTENER HOLES IAW SRM 57-53-70-2R-2, ALTERNATIVE 1.
- [SDR SWAA2025100620748](https://openairdocs.org/sdr/SWAA2025100620748.md): Stiffener · damaged · Oct 3, 2025 · N455WN · Boeing 7377H4 · Nacelle/Pylon Miscellaneous Structure
  > NR 2 ENGINE AFT STRUT FAIRING STIFFENER HAS 4 EACH ELONGATED HOLES FORWARD SIDE. REAMED HOLES TO.328 AND INSTALLED OVERSIZED FATSENERS IAW EA 25-154-02693 REFERENCE TASK TTG8Q015HNDM.
- [SDR SWAA2025071791246](https://openairdocs.org/sdr/SWAA2025071791246.md): Seat · out of adjust · Jul 15, 2025 · N455WN · Boeing 7377H4 · Passenger Compartment Equipment
  > PASSENGER SEAT RECLINES INTO AN EXIT ROW 11F. READJUSTED HYDRO LOCK PER AMM 25-22-00. INSPECTION C/W READJUSTED HYDRO LOCK PER AMM 25-22-00.
- [SDR SWAA2025071791255](https://openairdocs.org/sdr/SWAA2025071791255.md): Slide · debonded · Jul 15, 2025 · N455WN · Boeing 7377H4 · Escape Slide
  > AFT SERVICE DOOR ESCAPE SLIDE SKIRT RUBBER DISBONDED. R&R AFT SERVICE DOOR ESCAPE SLIDE IAW AMM 25-66-01. INSPECTION C/W R&R AFT SERVICE DOOR ESCAPE SLIDE IAW AMM 25-66-01.
- [SDR SWAA2025071791257](https://openairdocs.org/sdr/SWAA2025071791257.md): Plate · loose · Jul 15, 2025 · N455WN · Boeing 7377H4 · Service Doors
  > FWD SERVICE DOOR HANDLE CAM PLATE IS LOOSE. SECURED FWD SERVICE DOOR HANDLE CAM PLATE IAW AMM 20-50-11.
- [SDR SWAA2025071490353](https://openairdocs.org/sdr/SWAA2025071490353.md): Switch · out of adjust · Jul 10, 2025 · N455WN · Boeing 7377H4 · Door Warning System
  > DURING DESCENT; LEFT OVERWING LIGHT. FLIGHT DIRECTORS BLANKED ON APPROACH; PSEU LIGHT ON LANDING ROLL OUT. FOR LEFT OVERWING LIGHT AND PSEU LIGHT ON LANDING ROLL OUT; PERFORMED PSEU BITE TEST. FOUND FAULTS 52-72020 AND 52-72010. PERFORMED FIM TASKS 52-20 #80
- [SDR SWAA2025022097522](https://openairdocs.org/sdr/SWAA2025022097522.md): Seat · unlocked · Feb 19, 2025 · N455WN · Boeing 7377H4 · Passenger Compartment Equipment
  > *SEAT 11F RECLINES @ EMERGENCY EXIT ROW.<[01] LOCKED OUT 11F SEAT RECLINE PER CMM 25-21-42
- [SDR SWAA2025021997513](https://openairdocs.org/sdr/SWAA2025021997513.md): Handle · loose · Feb 19, 2025 · N455WN · Boeing 7377H4 · Service Doors
  > R1 DOOR INTERIOR HANDLE LOOSE<[01] TIGHTENED R1 DOOR INTERIOR HANDLE CAM PER AMM 52-41-11.
- [SDR SWAA2024121676518](https://openairdocs.org/sdr/SWAA2024121676518.md): Seat Back · out of adjust · Dec 11, 2024 · N455WN · Boeing 7377H4 · Passenger Compartment Equipment
  > SEAT 12F RECLINE INOP - SEAT LOCKED UPRIGHT ROW 12DEF DOES NOT RECLINE LOCATED IN EXIT ROW.<[01] SEAT LOCKED UPRIGHT<BR>OK TO CONT PER MEL 25-6-02 SP#1B;[02] INSPECTED SEAT 12F; FOUND TO BE IN EMERGENCY EXIT ROW. NO DEFECTS OR DAMAGE NOTED IN REF TO AMM 25-22-
- [SDR SWAA2024090333186](https://openairdocs.org/sdr/SWAA2024090333186.md): Retainer · loose · Aug 31, 2024 · N455WN · Boeing 7377H4 · Emergency Equipment
  > FWD ENTRY DOOR GIRT BAR RETAINING CLIP IS LOOSE<[01] TIGHTEN FWD ENTRY DOOR GIRT BAR CLIP PER SIP.
- [SDR SWAA2024011639529](https://openairdocs.org/sdr/SWAA2024011639529.md): Light · inoperative · Jan 10, 2024 · N455WN · Boeing 7377H4 · Emergency Lighting
  > FWD ENTRY OVERHEAD EMERGENCY EXIT LIGHTS INOP SUSPECTED FUSE IN BATTERY CHARGER NEEDS REPLACEMENT<[01] RE-LAMPED AND REPLACED FUSES OF FWD ENTRY OVERHEAD EMERGENCY EXIT LIGHTS PER AMM 33-51-01-960-801. OPS CHECK GOOD.;[02] UPDATED FOR MEASUREMENTS;[03] VERIFIE
- [SDR SWAA2024011639528](https://openairdocs.org/sdr/SWAA2024011639528.md): Bulb · inoperative · Jan 10, 2024 · N455WN · Boeing 7377H4 · Emergency Lighting
  > L/H OVERWING EMERGENCY EXIT SIGN HAS INOP BULB IN AFT SIDEWALL ASSY<[01] RE-LAMPED L/H OVERWING EMERGENCY EXIT SIGN; AFT SIDEWALL ASSY<BR>PER AMM 33-51-01-960-802; OPS CHECK GOOD.;[02] UPDATED FOR MEASUREMENTS.;[03] VERIFIED CORRECTIVE ACTION ENTRY 1. AND MEAS
- [SDR SWAA2024011637442](https://openairdocs.org/sdr/SWAA2024011637442.md): Floor Panel · delaminated · Jan 3, 2024 · N455WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 231XF HAS DELAMINATION.<[01] PARTIAL STEP 1;[02] REMOVED PASSENGER CABIN FLOOR PANEL 231XF PER AMM 53-21-00-000-801.<BR><BR>IDENTIFIED FLOOR PANEL MATERIAL IAW SRM 53-00-50-0I-1 SHEET 1; FIGURE 4; TABLE 4.<BR><BR>UPON INVESTIGATION
- [SDR SWAA2024011637443](https://openairdocs.org/sdr/SWAA2024011637443.md): Floor Panel · delaminated · Jan 3, 2024 · N455WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 241AF HAS DELAMINATION.<[01] PARTIAL STEP 1;[02] REMOVED PASSENGER CABIN FLOOR PANEL 241AF PER AMM 53-21-00-000-801. IDENTIFIED FLOOR PANEL MATERIAL IAW SRM 53-00-50-0I-1 SHEET 1; FIGURE 4; TABLE 4.<BR><BR>UPON INVESTIGATION FOUND D
- [SDR SWAA2024011637444](https://openairdocs.org/sdr/SWAA2024011637444.md): Floor Panel · delaminated · Jan 3, 2024 · N455WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 241DF HAS DELAMINATION.<[01] PARTIAL STEP 1;[02] REMOVED PASSENGER CABIN FLOOR PANEL 241DF PER AMM 53-21-00-000-801.<BR>IDENTIFIED FLOOR PANEL MATERIAL IAW SRM 53-00-50-0I-1 SHEET 1; FIGURE 4; TABLE 4.<BR><BR>UPON INVESTIGATION FOUN
- [SDR SWAA2024011637104](https://openairdocs.org/sdr/SWAA2024011637104.md): Light · broken · Jan 2, 2024 · N455WN · Boeing 7377H4 · Emergency Lighting
  > AFT ENTRYWAY CENTER DROP DOWN PANEL EMERGENCY EXIT LIGHT IS BROKEN.<[01] UPDATED TABLE; SIGNED PART;[02] COMPLETED STEP 1;[03] COMPLETED STEP 2; REPLACED AFT ENTRYWAY CENTER DROP DOWN PANEL EMERGENCY EXIT LIGHT PER AMM 33-51-01-960-802; OPS CHECK IS GOOD.;[04]
- [SDR SWAA2024011636649](https://openairdocs.org/sdr/SWAA2024011636649.md): Floor Panel · cracked · Dec 31, 2023 · N455WN · Boeing 7377H4 · Fuselage Floor Panel
  > REJECT: CRACK FOUND ON PASSENGER CABIN FLOOR SUPPORT PANEL STA-540 BL-0 TO BL-25R FLOOR PANEL 231UF.<[01] PARTIAL STEP 1;[02] COMPLETED STEP 1; REINSTALLED PASSENGER CABIN FLOOR PANEL 231UF PER AMM 53-21-00-400-801. USED SCREWGUN ID PER1811; S/N A5792887; DUE
- [SDR SWAA2024011634859](https://openairdocs.org/sdr/SWAA2024011634859.md): Frame · cracked · Dec 22, 2023 · N455WN · Boeing 7377H4 · Fuselage Main, Frame
  > LH NUMBER ONE FLIGHT DECK WINDOW AFT FRAME; CRACK DETECTED AT THE UPPER IB FASTENER HOLE; MARKED. (ENGINEERING DISPOSITION REQUIRED)<[01] NDT HFEC INSPECTED THE CRACKED HOLE IAW 737 NDTM PART 6 51-00-00 PROC 16. MARKED THE DIRECTION OF THE CRACK; GOES IB APPRO
- [SDR SWAA2024011634699](https://openairdocs.org/sdr/SWAA2024011634699.md): Floor Support · cracked · Dec 22, 2023 · N455WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > BS 500D-520; BL0; WL208; INTERCOSTAL ANGLE IS CRACKED.<[01] VERIFIED;[02] REMOVED AND REPLACED INTERCOSTAL ANGLE AT BS 500D-520; BL0; WL208 PER SRM 51-40-05-0G-0 AND PER DRAWING 143A5400.;[03] VERIFIED CORRECTIVE ACTION 2.;[04] REMOVED AND REPLACED BS 500D-520
- [SDR SWAA2024011634269](https://openairdocs.org/sdr/SWAA2024011634269.md): Strap · corroded · Dec 21, 2023 · N455WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS727D+6' RBL13 WL156<[01] CORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS727D+6' RBL13 WL156; FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE DAMAGE; REPLACEMENT OF PART RE
- [SDR SWAA2024011634270](https://openairdocs.org/sdr/SWAA2024011634270.md): Strap · corroded · Dec 21, 2023 · N455WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS767+6' RBL11 WL156<[01] CORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS767+6' RBL11 WL156 FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE LIMITS; REPLACEMENT OF PART REQUI
- [SDR SWAA2024011633719](https://openairdocs.org/sdr/SWAA2024011633719.md): Window Frame · cracked · Dec 19, 2023 · N455WN · Boeing 7377H4 · Flight Compartment Windows
  > CAPTAIN'S NO1 WINDOW FRAME HAS CRACK AT UPPER O/B CORNER<[01] REMOVED CRACK AND REPAIRED CAPTAIN'S NO.1 WINDOW FRAME AT UPPER O/B CORNER AND REPAIR WAS ACCOMPLISHED PER WIP1 AND WIP 2 FAULT# TTG8Q00QFTN9 AND FAULT# TTG8Q00QKS7K;[02] PARTIAL WORK STEP 1;[0
- [SDR SWAA2024011632047](https://openairdocs.org/sdr/SWAA2024011632047.md): Flap · debonded · Dec 14, 2023 · N455WN · Boeing 7377H4 · Trailing Edge Flaps
  > LT WING O/B AFT FLAP I/B END LOWER SKIN AT T/E IS DISBONDED.<[01] REMOVED AND REPLACED LT. WING O/B AFT FLAP IAW AMM 27-51-22-000-801 & AMM 27-51-22-400-801 STEPS 3F(4). TORQUES AND SAFETIES VERIFIED.<BR><BR>CAL TOOLING:<BR> ID DD<BR>ATS2327 10/2024<BR>E11413
- [SDR SWAA2024011630883](https://openairdocs.org/sdr/SWAA2024011630883.md): Support Fitting · corroded · Dec 11, 2023 · N455WN · Boeing 7377H4 · Emergency Equipment
  > CORROSION ON FWD ENTRYWAY; FWD GIRT BAR FITTING SUPPORT STA 312; LBL 54; WL 208.<[01] REMOVED AND REPLACED FWD ENTRYWAY; FWD GIRT BAR FITTING SUPPORT STA 312; LBL 54; WL 208 DUE TO NO ALLOWABLE LIMITS IN THE SRM FOR THIS PART IAW SRM 51-10-02; SOPM 20-50-01 A
- [SDR SWAA2024011630881](https://openairdocs.org/sdr/SWAA2024011630881.md): Seat Track · corroded · Dec 11, 2023 · N455WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK HAS CORROSION IN WELL OF CROWN AT BS 480+15; LBL 45; WL 208<[01] PASSENGER CABIN SEAT TRACK STA 480-520; LBL 45; WL 208 WILL BE REPLACED ON CUSTOMER CARD# TTG8Q00Q3RA0;[02] VERIFIED.<BR>VERIFIED MEASUREMENTS.
- [SDR SWAA2024011629532](https://openairdocs.org/sdr/SWAA2024011629532.md): Attach Angle · corroded · Dec 8, 2023 · N455WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CORROSION ON FWD ENTRY MOP SILL ATTACH ANGLE BS 319; 338-339 LBL 59 WL 209.<[01] VERIFIED APPLICABILITY OF SRM 53-10-15-1A-1 ALLOWABLE DAMAGE 1;[02] BLENDED AND REMOVED CORROSION AT FWD ENTRY MOP SILL ATTACH ANGLE BS 319 AND BS 338-339 LBL 59 WL 208 IAW SRM 53
- [SDR SWAA2024011629531](https://openairdocs.org/sdr/SWAA2024011629531.md): Channel · cracked · Dec 8, 2023 · N455WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD ENTRY DOOR MOP SILL IS CRACKED AT BS 303 ON VERTICAL FLANGE LBL 53 WL 208.<[01] REMOVED AND REPLACED FED MOP SILL IAW SRM 51-40-02 AND DWG # 141A8110;[02] VERIFIED CORRECTIVE ACTION ITEM 1 AND MEASUREMENTS TABLE.
- [SDR SWAA2024011629535](https://openairdocs.org/sdr/SWAA2024011629535.md): Stringer Clip · cracked · Dec 8, 2023 · N455WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED STRINGER CLIP BS 277 STR 10R/H RBL 53 WL 251 FWD SIDE OF FRAME.<[01] VERIFIED STEP 1 IN PARTIAL.;[02] REMOVED DAMAGED STRINGER CLIP; LOCATED AND DRILLED NEW STRINGER CLIP AT BS 277 STRINGER 10 R/H WL 251 PER SRM 51-40-02-0G-0. APPLIED CIC TO STRINGER C
- [SDR SWAA2024011629372](https://openairdocs.org/sdr/SWAA2024011629372.md): Shield · corroded · Dec 7, 2023 · N455WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION FWD CARGO BAY AFT SHIELD BS500+1 TO BS500+19 RBL22 WL156 HAS MULTIPLE AREAS AROUND NUT PLATE HOLES<[01] CORROSION ON FWD CARGO BAY AFT SHIELD FOUND OUT OF LIMITS. REMOVED; REPLACED AND INSTALLED NEW FWD CARGO BAY AFT SHIELD PER SRM 51-40-02-0G-0 AND
- [SDR SWAA2024011629373](https://openairdocs.org/sdr/SWAA2024011629373.md): Sidewall Support · corroded · Dec 7, 2023 · N455WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION FWD CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS500A TO BS500D RBL22 WL156<[01] CORROSION ON FWD CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT FOUND OUT OF LIMITS. REMOVED; REPLACED AND INSTALLED NEW FLOOR TO SIDEW
- [SDR SWAA2024011629375](https://openairdocs.org/sdr/SWAA2024011629375.md): Support Plate · corroded · Dec 7, 2023 · N455WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 LBL22 WL156<[01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 747+12' REMOVED 0.015' IN AN AREA OF 1'X1' ORIGINAL THIC
- [SDR SWAA2024011629374](https://openairdocs.org/sdr/SWAA2024011629374.md): Support Plate · damaged · Dec 7, 2023 · N455WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 RBL22 WL156<[01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 727D-9' REMOVED 0.020' IN AN AREA OF 1'X1' ORIGINAL

Next page: https://openairdocs.org/aircraft/N455WN/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 = 'N455WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N455WN/reports

---
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.