# Service difficulty reports: N475WN

A list on [N475WN](https://openairdocs.org/aircraft/N475WN.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 · 269 reports

- [SDR SWAA2026072958410](https://openairdocs.org/sdr/SWAA2026072958410.md): Handle · loose · Jul 25, 2026 · N475WN · Boeing 7377H4 · Service Doors
  > OUTSIDE FWD SERVICE DOOR HANDLE LOOSE. REPLACED FWD SERVICE DOOR HANDLE STOW SPRING IAW AMM 52-41-11.
- [SDR SWAA2026051397007](https://openairdocs.org/sdr/SWAA2026051397007.md): Battery Pack · inoperative · May 9, 2026 · N475WN · Boeing 7377H4 · Emergency Lighting
  > NUMEROUS EMERGENCY LIGHTS IN THE CABIN INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS M1673 (AFT LT GALLEY) AND M1674 (FWD RT GALLEY) IAW AMM 33-51-06-960-805. OPS CHECK GOOD.
- [SDR SWAA2026051394287](https://openairdocs.org/sdr/SWAA2026051394287.md): Fitting · cracked · Apr 30, 2026 · N475WN · Boeing 7377H4 · Wing Main, Frame Structure
  > LEFT WING INBD FIXED TE SEAL BULKHEAD FITTING CRACKED. REMOVED AND REPLACED THE LT WING INBD FIXED TE SEAL BULKHEAD FITTING IAW SRM 51-40-02, AND DWG 115A2930, REV E.
- [SDR SWAA2026051391619](https://openairdocs.org/sdr/SWAA2026051391619.md): Lens · missing · Apr 21, 2026 · N475WN · Boeing 7377H4 · Emergency Lighting
  > FOUND MISSING LENSE ON OVERHEAD STOWAGE BIN EMERGENCY LIGHT AT LT ROW 4. INSTALLED NEW LENS ON OVERHEAD STOWAGE BIN EMERGENCY LIGHT AT SEAT ROW 4ABC IAW AMM 33-51-03-960-801, STEP D.(3)(C).
- [SDR SWAA2026051391299](https://openairdocs.org/sdr/SWAA2026051391299.md): Angle · cracked · Apr 21, 2026 · N475WN · Boeing 7377H4 · Passenger/Crew Doors
  > FWD ENTRY DOOR; DOOR TARGET ANGLE CRACK. REMOVED AND REPLACED FWD ENTRY DOOR; DOOR TARGET ANGLE IAW SRM 51-40-02 AND IPC 52-11-00-02B. REMOVED AND REPLACED FWD ENTRY DOOR TARGET ANGLE IAW SRM 51-40-02 AND IPC 52-11-00-02B.
- [SDR SWAA2026051389820](https://openairdocs.org/sdr/SWAA2026051389820.md): Strap · out of tolerance · Apr 15, 2026 · N475WN · Boeing 7377H4 · Fuselage Main, Structure
  > FRAME STRAP AT BS 328 STR 20R-22R DOES NOT MATCH CONFIGURATION OF FIG 5 CUSTOMER CARD 5311-I-17336NG STEP 13, FOUND REPAIR AT BS 328 FRAME BETWEEN STRINGERS S-19 R AND S-24R CARD REQUIRES CONTACT ENGINEERING USING ESR OR TSR. VERIFIED PERFORM OP TEST OF IND
- [SDR SWAA2026051389817](https://openairdocs.org/sdr/SWAA2026051389817.md): Attach Angle · cracked · Apr 14, 2026 · N475WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > POSSIBLE CRACK IN LT AC PACK BAY AFT UPPER CORNER. REPLACEMENT ATTACH ANGLE FABRICATED AND INSTALLED PER EA 26-157-01152.
- [SDR SWAA2025072192500](https://openairdocs.org/sdr/SWAA2025072192500.md): Seat · out of alignment · Jul 18, 2025 · N475WN · Boeing 7377H4 · Passenger Compartment Equipment
  > CABIN SEAT RECLINE NEEDS TO BE INOP AT 11F (EXIT ROW). ADJUSTED SEAT 11F IAW AMM 25-22-00.
- [SDR SWAA2025032608684](https://openairdocs.org/sdr/SWAA2025032608684.md): Sign · detached · Mar 24, 2025 · N475WN · Boeing 7377H4 · Emergency Lighting
  > OVERHEAD EXIT SIGN ABOVE EXIT ROW FELL OFF<[01] REINSTALLED OVERHEAD EXIT SIGN ABOVE EXIT ROW IAW AMM 33-51-01
- [SDR SWAA2025022498480](https://openairdocs.org/sdr/SWAA2025022498480.md): Battery Pack · no test · Feb 21, 2025 · N475WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHTING BATTERY PACK AT R/H OVERWING EXIT FAILED THE CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.;[02] 02 - INSPECTED PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]
- [SDR SWAA2024101447685](https://openairdocs.org/sdr/SWAA2024101447685.md): Lens · missing · Oct 11, 2024 · N475WN · Boeing 7377H4 · Emergency Lighting
  > RH EMERGENCY EXIT DOOR LIGHT COVER MISSING (MID-CABIN) (OVERWING EXIT)<[01] INSTALLED RH OVERWING EMERGENCY EXIT DOOR RH SIDE OF DOOR EXIT INDICATOR LENS IAW AMM 33-51-01. NO DEFECTS NOTED AT THIS TIME.
- [SDR SWAA2024060697878](https://openairdocs.org/sdr/SWAA2024060697878.md): Plate · loose · Jun 4, 2024 · N475WN · Boeing 7377H4 · Service Doors
  > AFT SERVICE DOOR HANDLE CAM PLATE IS LOOSE<[01] ADJUSTED CAM PLATE PER AMM 52-41-00
- [SDR SWAA2024050883134](https://openairdocs.org/sdr/SWAA2024050883134.md): Lamp · inoperative · May 7, 2024 · N475WN · Boeing 7377H4 · Emergency Lighting
  > FWD ENTRY EMERGENCY EXIT SLIDE LIGHT INOP<[01] REPLACED LAMP AT FWD ENTRY EMERGENCY EXIT SLIDE LIGHT IAW AMM 33-51-04-960-801; LIGHT CONTINUE INOP.;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] RECONNECTED FWD ENTRY EMERGNCY EXIT SLIDE LIGHT CONNECTOR AND PERFO
- [SDR SWAA2024050883133](https://openairdocs.org/sdr/SWAA2024050883133.md): Connector · out of adjust · May 7, 2024 · N475WN · Boeing 7377H4 · Light System Wiring
  > L/R OWE SLIDE LIGHT INOP ***CORRECTION TO TITLE*** L/H OWE SLIDE LIGHT INOP<[01] RECONNECTED LEFT FWD ESCAPE SLIDE LIGHT CONNECTOR AND PERFORMED GOOD FUNCTIONAL TEST PER AMM 33-51-04-960-801 STEP D (4).;[02] RELAMP L/R OWE SLIDE LIGHT AND PERFORMED GOOD FUNCTI
- [SDR SWAA2024050880661](https://openairdocs.org/sdr/SWAA2024050880661.md): Bulb · burned out · Apr 30, 2024 · N475WN · Boeing 7377H4 · Emergency Lighting
  > R/H OVERWING EXIT WINDOW LIGHT ASSY. HAS BURNED OUT EMERGENCY LIGHT BULB<[01] EMERGENCY LIGHT BULB REPLACED AT R/H OVERWING EXIT WINDOW LIGHT ASSY AND PERFORMED GOOD OPERATIONAL TEST IAW 33-51-01-960-801.;[02] CERTIFIED ACTION 1.;[03] CORRECTION CORRECTIVE ACT
- [SDR SWAA2024050977763](https://openairdocs.org/sdr/SWAA2024050977763.md): Stiffener · corroded · Apr 21, 2024 · N475WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON PASSENGER CABIN STIFFENER AT BS 706+7 RBL 63 WL 202<[01] REFER TO FAULT TTG8Q00SN4XS WHERE EA 24-153-01070 WAS ADDED AS A SUBTASK.;[02] CORRECTED MEASUREMENT TABLE.;[03] UPDATED STEP 2.1 AND 2.3
- [SDR SWAA2024050972772](https://openairdocs.org/sdr/SWAA2024050972772.md): Strap · corroded · Apr 9, 2024 · N475WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON STRAP AT MID PAX CABIN BS 711; RBL 63; WL 202. CORROSION ON STRAP AT MID PAX CABIN BS 706+2 RBL 63 WL 202.<[01] UPDATED STEPS 2;3 AND 4.;[02] UPDATED MEASUREMENTS TABLE;[03] PICTURES OF DAMAGE IS MISSING IN ATTACHMENTS.;[04] UPDATED STEP 2 AND 4;[
- [SDR SWAA2024050972767](https://openairdocs.org/sdr/SWAA2024050972767.md): Floor Panel · cracked · Apr 9, 2024 · N475WN · Boeing 7377H4 · Fuselage Floor Panel
  > PAX CABIN FLOOR PANEL BRAKE CRACKED AT BS 540; LBL 1 WL208.<[01] REMOVED AND REPLACED BREAK PANEL BS540 LBL1-LBL25 WL208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 143A0060 <BR>TASK COMPLETED;[02] VERIFIED ALL STEPS AND CORRECTIVE ACTION ITEMS; CARD COMPLETE
- [SDR SWAA2024050972768](https://openairdocs.org/sdr/SWAA2024050972768.md): Floor Panel · cracked · Apr 9, 2024 · N475WN · Boeing 7377H4 · Fuselage Floor Panel
  > PAX CABIN FLOOR PANEL BRAKE CRACKED AT BS 540; RBL 1 WL208.<[01] REMOVED AND REPLACED BREAK PANEL BS540 RBL1-RBL25 WL208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 143A0060 <BR>TASK COMPLETED;[02] VERIFIED ALL STEPS AND CORRECTIVE ACTION ITEMS; CARD COMPLETE.
- [SDR SWAA2024050972786](https://openairdocs.org/sdr/SWAA2024050972786.md): Support Bracket · cracked · Apr 9, 2024 · N475WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > PAX CABIN FLOOR PANEL SUPPORT BRACKET CRACKED AT BS 705; LBL 23 WL208.<[01] UPDATED STEP 1 AND COMPLETED STEP 3;[02] UPDATED STEP 4;[03] COMPLETED STEP 5.;[04] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL
- [SDR SWAA2024050972782](https://openairdocs.org/sdr/SWAA2024050972782.md): Attach Angle · cracked · Apr 9, 2024 · N475WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > PAX CABIN FLOOR ATTACH ANGLE CRACKED AT BS 693; LBL 22 WL203.<[01] COMPLETED STEP 1 AND VERIFIED ALL STEPS COMPLETE REMOVED AND REPLACED CRACKED CABIN FLOOR ATTACH ANGLE AT BS 693 LBL 22 WL 203 IAW SRM 51-40-02-0G-0 AND BOEING DWG 273A9110;[02] VERIFIED ITEM 1
- [SDR SWAA2024050972783](https://openairdocs.org/sdr/SWAA2024050972783.md): Attach Angle · cracked · Apr 9, 2024 · N475WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > PAX CABIN FLOOR ATTACH ANGLE CRACKED AT BS 693; RBL 22 WL203.<[01] COMPLETED STEPS 1 AND 2 REMOVED AND REPLACED CRACKED CABIN FLOOR ATTACH ANGLES AT BS 693 RBL 22 AND BL 0 ALL AT WL 203 VERIFIED ALL STEPS COMPLETE ALL IAW SRM 51-40-02-0G-0 AND BOEING DWG 273A9
- [SDR SWAA2024050971770](https://openairdocs.org/sdr/SWAA2024050971770.md): Bracket · corroded · Apr 7, 2024 · N475WN · Boeing 7377H4 · Emergency Equipment
  > CORROSION ON BOTH FED GRIT BAR FITTING BRACKETS COMMON TO FED MOPSILL. (MARKED)<[01] UPDATED STEP 1;[02] UPDATED STEPS 2 AND 3;[03] REMOVED BOTH FED GRIT BAR FITTING BRACKETS COMMON TO FED MOPSILL PER SRM 51-40-02-0G-0. NSTALLED BOTH FED GRIT BAR FITTING BRACK
- [SDR SWAA2024050971771](https://openairdocs.org/sdr/SWAA2024050971771.md): Floor Panel · corroded · Apr 7, 2024 · N475WN · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 221GF CORNER IS DAMAGED AND INSERTS ARE CORRODED. (MARKED)<[01] PARTIAL STEP 1;[02] COMPLETED STEP 1;[03] REMOVED PASSENGER CABIN FLOOR PANEL 221GF PER AMM 53-21-00-000-801. CABIN FLOOR PANEL 221GF WITH CORNER DAMAGED AND INSERTS CORRODED WAS
- [SDR SWAA2024050871767](https://openairdocs.org/sdr/SWAA2024050871767.md): Floor Support · cracked · Apr 7, 2024 · N475WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL COMMON TO FLOOR BOARD HOLE AT BS 322 LBL 45 WL 208 (MARKED)<[01] REMOVED AND REPLACED INTERCOSTAL BS312-BS328 LBL45 WL208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 141A5400.;[02] VERIFIED ALL STEPS AND CORRECTIVE ACTION ITEMS; CARD COMPLETE.
- [SDR SWAA2024050971400](https://openairdocs.org/sdr/SWAA2024050971400.md): Skin · cracked · Apr 6, 2024 · N475WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > RIGHT HORIZONTAL STABILIZER LOWER SKIN IS CRACKED AT I/B SIDE OF RIB STAB STA 193.90; 17 INCHED FWD OF R/S<[01] UPDATED MEASUREMENT TABLE.;[02] REMOVED DAMAGE AND INSTALLED REPAIR @ RH HORIZONTAL STABILIZER LOWER SKIN @ STA 193.90 IAW SRM 55-10-01-2R-11.;[03]
- [SDR SWAA2024050970964](https://openairdocs.org/sdr/SWAA2024050970964.md): Lens · broken · Apr 5, 2024 · N475WN · Boeing 7377H4 · Emergency Lighting
  > G-4 GALLEY EXIT LIGHT LENS BROKEN.<[01] REMOVED AND REPLACED G-4 GALLEY EXIT LIGHT LENS PER AMM 33-51-01-960-801 STEPS 2.C.(1)(A); (4);[02] VERIFIED CORRECTIVE ACTION. CARD COMPLETE.
- [SDR SWAA2024050971132](https://openairdocs.org/sdr/SWAA2024050971132.md): Vapor Barrier · debonded · Apr 5, 2024 · N475WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > EXISTING REPAIR COMMON TO BS663 WL150 LBL16 VAPOR BARRIER WAS FOUND TO BE DISBONDED<[01] RECEIVED NEW VAPOR BARRIER. LOCATED AND DRILLED REPLACEMENT VAPOR BARRIER AS PER BOEING DRAWINGS 111A1151; 111A1001; 144A7100; 111A1000; 111A7000 AND 737-700 SRM 51-40-05-
- [SDR SWAA2024050970744](https://openairdocs.org/sdr/SWAA2024050970744.md): Shield · corroded · Apr 5, 2024 · N475WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS767+3 TO BS794 RBL22 WL156<[01] SHIELD FOUND TO BE OUT OF LIMITS; REMOVED AND REPLACED; NEW PART LOCATED; DRILLED AND INSTALLED IAW SRM 51-40-02-0G-0 AND DWG 146A0081.;[02] VERI
- [SDR SWAA2024050970743](https://openairdocs.org/sdr/SWAA2024050970743.md): Shield · corroded · Apr 5, 2024 · N475WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY ATTACH ANGLE UNDER SHIELD HAS MULTIPLE AREAS UNDER NUT PLATES BS767 TO BS787 RBL21 WL156<[01] ANGLE UNDER SHIELD FOUND TO BE OUT OF LIMITS; REMOVED AND REPLACED; NEW PART LOCATED; DRILLED AND INSTALLED IAW SRM 51-40-02-0G-0 AND DWG 146A
- [SDR SWAA2024050970745](https://openairdocs.org/sdr/SWAA2024050970745.md): Support · corroded · Apr 5, 2024 · N475WN · 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] AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE FOUND TO BE OUT OF LIMITS; REMOVED AND REPLACED; NEW PART LOCATED; DRILLED
- [SDR SWAA2024050970961](https://openairdocs.org/sdr/SWAA2024050970961.md): Support · corroded · Apr 5, 2024 · N475WN · 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] AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE FOUND TO BE OUT OF LIMITS; REMOVED AND REPLACED; NEW PART LOCATED; DRILLED AND
- [SDR SWAA2024050970957](https://openairdocs.org/sdr/SWAA2024050970957.md): Intercostal · corroded · Apr 5, 2024 · N475WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY INTERCOSTAL BS807+2 S-27R WL150<[01] CORROSION ON INTERCOSTAL WAS FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED INTERCOSTAL AS PER SRM 51-40-02 AND DWG 146A8132.;[02] STEP # 2 COMPLETE; TASK CARD COMPLETE.
- [SDR SWAA2024050970958](https://openairdocs.org/sdr/SWAA2024050970958.md): Intercostal · corroded · Apr 5, 2024 · N475WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY INTERCOSTAL BS787+6 S-27R WL150<[01] CORROSION ON INTERCOSTAL WAS FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED INTERCOSTAL AS PER SRM 51-40-02 AND DWG 146A8132.;[02] STEP # 2 COMPLETED TASK CARD COMPLETE.
- [SDR SWAA2024050970962](https://openairdocs.org/sdr/SWAA2024050970962.md): Intercostal · corroded · Apr 5, 2024 · N475WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY INTERCOSTAL BS767+3 S-27R WL150<[01] CORROSION ON INTERCOSTAL WAS FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED INTERCOSTAL AS PER SRM 51-40-02 AND DWG 146A8132.;[02] STEP # 2 COMPLETE TASK CARD COMPLETE.
- [SDR SWAA2024050970963](https://openairdocs.org/sdr/SWAA2024050970963.md): Intercostal · corroded · Apr 5, 2024 · N475WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY INTERCOSTAL BS767+5 S-25R WL150<[01] INTERCOSTAL FOUND TO BE OUT OF LIMITS; REMOVED AND REPLACED; NEW PART LOCATED; DRILLED AND INSTALLED IAW SRM 51-40-02-0G-0 AND DWG 146A0081.;[02] VERIFIED ALL STEPS AND CORRECTIVE ACTION ITEMS; CARD
- [SDR SWAA2024050970349](https://openairdocs.org/sdr/SWAA2024050970349.md): Threshold · cracked · Apr 4, 2024 · N475WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY FORWARD CORNER THRESHOLD IS CRACKED<[01] COMPLETED STEP 5;6.;[02] REPAIRED AFT CARGO BAY FORWARD CORNER THRESHOLD BY WELDING; APPLIED CHEMICAL CONVERSION AND PRIMED; ALL PER SRM 53-60-15-2R-1;[03] VERIFIED CORRECTIVE ACTION 2
- [SDR SWAA2024050970152](https://openairdocs.org/sdr/SWAA2024050970152.md): Stringer · cracked · Apr 3, 2024 · N475WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER MAIN DISTRIBUTION BAY BS535 S-23R WL150<[01] CRACK FOUND TO BE OUT OUR LIMITS AS PER SRM 53-00-03-1A-1; REMOVED DAMAGED SECTION OF STRINGER 23 R/H BETWEEN BS 500D+12' TO BS 536 PER SRM 53-00-03-2R-1 AND REPAIRED PER SRM 53-00-03-2R-1 AND EA 24
- [SDR SWAA2024050970153](https://openairdocs.org/sdr/SWAA2024050970153.md): Stringer · cracked · Apr 3, 2024 · N475WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER MAIN DISTRIBUTION BAY BS535 S-25L WL150<[01] CRACK FOUND TO BE OUT OUR LIMITS AS PER SRM 53-00-03-1A-1;REMOVED DAMAGED SECTION OF STRINGER 25 L/H BETWEEN BS 500D+11.5' TO BS 536 PER SRM 53-00-03-2R-1 PAR 4;STEP B;FIG 205 AND REPAIRED IAW SRM
- [SDR SWAA2024050969922](https://openairdocs.org/sdr/SWAA2024050969922.md): Stiffener · cracked · Apr 3, 2024 · N475WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > LH HORIZONTAL STABILIZER RIB AT STAB STA 129.50 IS CRACKED AT 2ND STIFFENER<[01] CUT AND REMOVED CRACK DAMAGE ON LEFT HAND HORIZONTAL STABILIZER INSPAR RIB AT STAB STA 129.50 AT 2ND STIFFENER FROM FRONT SPAR AND INSTALLED REPAIR IAW SRM 55-10-09-2R-4 REPAIR 4.
- [SDR SWAA2024050970154](https://openairdocs.org/sdr/SWAA2024050970154.md): Rib · cracked · Apr 3, 2024 · N475WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > R/H HORIZONTAL STAB REMOVABLE L/E 4TH RIB FROM I/B END IS CRACKED<[01] REMOVED RH HORIZONTAL STABILIZER LEADING EDGE RIB #4 IAW SRM 51-40-02-0G-0.;[02] RELACED R/H HORIZONTAL STAB. REMOVEABLE L/E RIB; 4TH FROM I/B END IAW SRM 51-40-02 0G-0 PARA. 4 AND BOEING D
- [SDR SWAA2024050969571](https://openairdocs.org/sdr/SWAA2024050969571.md): Skin · debonded · Apr 2, 2024 · N475WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > PANEL 192JR OUTER SKIN IS DISBONDED NEAR CENTER OF PANEL. (MARKED)<[01] PANEL 192JR OUTER SKIN WAS DISBONDED NEAR CENTER OF PANEL AND REPAIRED IAW SRM 51-70-05-2R-2;[02] JOB COMPLETE.
- [SDR SWAA2024012242952](https://openairdocs.org/sdr/SWAA2024012242952.md): Light · inoperative · Jan 20, 2024 · N475WN · Boeing 7377H4 · Emergency Lighting
  > FWD GALLEY EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED BATTERY PACK FOR THE FWD GALLEY EMERGENCY LIGHTS. OPS CHECK GOOD PER AMM 3351-06
- [SDR SWAA2023100908168](https://openairdocs.org/sdr/SWAA2023100908168.md): Isolator · cracked · Oct 6, 2023 · N475WN · Boeing 7377H4 · Escape Slide
  > FORWARD GALLEY SERVICE DOOR (R1). AFT SLIDE RETAINER ISOLATOR CRACKED.<[01] REMOVED AND REPLACED PER SRM 51-40-02;[02] C/W INSPECTION PER SRM 51-40-02.
- [SDR SWAA2023100908160](https://openairdocs.org/sdr/SWAA2023100908160.md): Light · missing · Oct 6, 2023 · N475WN · Boeing 7377H4 · Emergency Lighting
  > PASSENGER CABIN: LEFT EVACUATION STRIP AT SEAT 1C IS SHORT.<[01] INSTALLED MISSING PHOTOLUMINESCENT STRIP PER AMM 33-51-15;[02] C/W INSPECTION PER AMM 33-51-15.
- [SDR SWAA2023071176892](https://openairdocs.org/sdr/SWAA2023071176892.md): Sign · missing · Jul 10, 2023 · N475WN · Boeing 7377H4 · Emergency Lighting
  > AFT CAPTAINS SIDE WHITE EXIT SIGN COVER BY ENTRY DOOR MISSING.<[01] INSTALLED NEW EMERGENCY EXIT SIGN IAW SIP.
- [SDR SWAA2023060856454](https://openairdocs.org/sdr/SWAA2023060856454.md): Girt Bar · out of adjust · Jun 6, 2023 · N475WN · Boeing 7377H4 · Emergency Equipment
  > LEFT FORWARD ENTRY DOOR PARTIALLY OPENED WITH SLIDE GIRT BARS STILL ARMED. RAFT FELL OUT OF BOX BUT DID NOT INFLATE.<[01] UPDATED PART REQ FOR SLIDE R&R;[02] R/R FWD ENTRY ESCAPE SLIDE IAW AMM 25-66-01.
- [SDR SWAA2023030611016](https://openairdocs.org/sdr/SWAA2023030611016.md): Bracket · cracked · Mar 1, 2023 · N475WN · Boeing 7377H4 · Galley Doors
  > AFT SERVICE R2 DOOR LOWER PANEL 844DZ AFT BRACKET CRACKED<[01] REMOVED AND REPLACED AFT SERVICE R2 DOOR LOWER PANEL 844DZ AFT BRACKET PER AMM 52-41-00
- [SDR SWAA2022122284549](https://openairdocs.org/sdr/SWAA2022122284549.md): Battery Pack · no test · Dec 21, 2022 · N475WN · Boeing 7377H4 · Emergency Equipment
  > ONE FWD EMERGENCY FLASHLIGHT WILL NOT TEST. R & R THE FWD EMERGENCY FLASHLIGHT BATTERY PACK IAW MM 25-64-00. OPS NORMAL
- [SDR SWAA2022071126184](https://openairdocs.org/sdr/SWAA2022071126184.md): Light · inoperative · Jul 6, 2022 · N475WN · Boeing 7377H4 · Emergency Lighting
  > COCKPIT EMERGENCY LIGHT DOES NOT COME ON / [01] REPLACED M1219 OPS CHECK GOOD PER AMM 33-51-00

Next page: https://openairdocs.org/aircraft/N475WN/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 = 'N475WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N475WN/reports

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