# Service difficulty reports: N215WN

A list on [N215WN](https://openairdocs.org/aircraft/N215WN.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 · 291 reports

- [SDR SWAA2026080446798](https://openairdocs.org/sdr/SWAA2026080446798.md): Starter · failed · Jul 31, 2026 · N215WN · Boeing 7377H4 · Engine Starter
  > DURING PUSH BACK NR 2 ENG FAILED TO START. NO ROTATION. REMOVED AND REPLACED NR 2 ENGINE STARTER IAW AMM 80-11-01 OPS AND LEAK CHECKED GOOD.
- [SDR SWAA2026021269236](https://openairdocs.org/sdr/SWAA2026021269236.md): Isolator · cracked · Feb 10, 2026 · N215WN · Boeing 7377H4 · Emergency Equipment
  > PASSENGER CABIN FORWARD GALLEY SERVICE DOOR FORWARD UPPER SLIDE ISOLATOR CRACKED. R & R UPPER SLIDE ISOLATOR IAW SRM 51-40-02.
- [SDR SWAA2025122254056](https://openairdocs.org/sdr/SWAA2025122254056.md): Slide · low pressure · Dec 19, 2025 · N215WN · Boeing 7377H4 · Escape Slide
  > AFT SERVICE DOOR SLIDE LOW PRESSURE<[01] R&R AFT SERVICE ESCAPE SLIDE PER AMM 25-66-01; MT 725-61-06 REM/INSTL
- [SDR SWAA2025100620121](https://openairdocs.org/sdr/SWAA2025100620121.md): Lens · damaged · Oct 1, 2025 · N215WN · Boeing 7377H4 · Emergency Lighting
  > AFT LAVATORY EMERGENCY EXIT SIGN HAS DAMAGED LENS. REMOVED AND REPLACED DAMAGED LENS FROM AFT LAV EMERGENCY EXIT SIGN AND PERFORMED GOOD INSTALLATION TEST IAW AMM 33-51-01-960-802.
- [SDR SWAA2025090309867](https://openairdocs.org/sdr/SWAA2025090309867.md): Handle · loose · Aug 30, 2025 · N215WN · Boeing 7377H4 · Passenger/Crew Doors
  > ASSIST HANDLE ON FWD ENTRY DOOR LOOSE RE-SECURED FWD ENTRY DOOR ASSIST HANDLE PER AMM 52-11-31. RESECURED ASSIST HANDLE PER AMM 52-11-31.<BR><BR>3194309
- [SDR SWAA2025072894222](https://openairdocs.org/sdr/SWAA2025072894222.md): Fairing · damaged · Jul 22, 2025 · N215WN · Boeing 7377H4 · Nacelle/Pylon, Main Frame
  > STRUT FAIRING ON NR 2 ENGINE AT 3 O`CLOCK POSITION HAS ELONGATED HOLE. PARTIALLY INSTALLED STRUT FAIRING PANEL IAW AMM 73-21-06, FINISHED INSTALLING REMAINING 2 SCREWS COMMON TO STRUT FAIRING REF AMM 73-21-06.
- [SDR SWAA2025062584647](https://openairdocs.org/sdr/SWAA2025062584647.md): Girt Bar · out of position · Jun 23, 2025 · N215WN · Boeing 7377H4 · Emergency Equipment
  > FWD SERVICE DOOR GIRT BAR TO SLIDE IS OUT OF POSITION<[01] RESET GIRT BAR AS NEEDED PER SIP
- [SDR SWAA2025060377055](https://openairdocs.org/sdr/SWAA2025060377055.md): Holder · broken · Jun 1, 2025 · N215WN · Boeing 7377H4 · Emergency Equipment
  > FWD GALLEY EMERGENCY FLASHLIGHT HOLDER BROKEN <[01]. REPLACED BROKEN FLASHLIGHT HOLDER PER SRM 51-40-01 AND AMM 25-64-00.
- [SDR SWAA2025022498262](https://openairdocs.org/sdr/SWAA2025022498262.md): Lamp · inoperative · Feb 23, 2025 · N215WN · Boeing 7377H4 · Emergency Lighting
  > RH EMERGENCY EXIT WINDOW EXIT LIGHT BULB OUT <[01]. CORRECTLY INSTALLED RH EMERGENCY WINDOW EXIT LIGHT LAMP PER AMM 33-25-00-960-804;[02] VERIFIED CORRECTIVE ACTION #1.
- [SDR SWAA2025022498258](https://openairdocs.org/sdr/SWAA2025022498258.md): Battery Pack · inoperative · Feb 23, 2025 · N215WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHT INSIDE CABIN ROW 12 ABC; 9 ABC ARE INOP <[01]. DURING TROUBLESHOOTING; DETERMINED THAT THIS DEFECT AND DEFECT TTG8Q00YW88E ARE BOTH CONTROLLED BY BATTERY CHARGER/POWER SUPPLY ASSEMBLY M1670 PER WDM 33-51-13. REPLACED BATTERY PACK/CHARGER ASSEMB
- [SDR SWAA2025022499085](https://openairdocs.org/sdr/SWAA2025022499085.md): Charger · inoperative · Feb 23, 2025 · N215WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHT INSIDE CABIN ROW 12 ABC; 9 ABC ARE INOP <[01]. DURING TROUBLESHOOTING; DETERMINED THAT THIS DEFECT AND DEFECT TTG8Q00YW88E ARE BOTH CONTROLLED BY BATTERY CHARGER/POWER SUPPLY ASSEMBLY M1670 PER WDM 33-51-13. REPLACED BATTERY PACK/CHARGER ASSEMB
- [SDR SWAA2025022498257](https://openairdocs.org/sdr/SWAA2025022498257.md): Battery Pack · inoperative · Feb 23, 2025 · N215WN · Boeing 7377H4 · Emergency Lighting
  > AFT OF WING EMERGENCY SLIDE LIGHT BOTH LH AND RH SIDE ARE OUT <[01]. DURING TROUBLESHOOTING; DETERMINED THAT THIS DEFECT AND DEFECT TTG8Q00YW88S ARE BOTH CONTROLLED BY BATTERY CHARGER/POWER SUPPLY ASSEMBLY M1670 PER WDM 33-51-13. REPLACED BATTERY PACK/CHARGER
- [SDR SWAA2025022499086](https://openairdocs.org/sdr/SWAA2025022499086.md): Charger · inoperative · Feb 23, 2025 · N215WN · Boeing 7377H4 · Emergency Lighting
  > AFT OF WING EMERGENCY SLIDE LIGHT BOTH LH AND RH SIDE ARE OUT <[01]. DURING TROUBLESHOOTING; DETERMINED THAT THIS DEFECT AND DEFECT TTG8Q00YW88S ARE BOTH CONTROLLED BY BATTERY CHARGER/POWER SUPPLY ASSEMBLY M1670 PER WDM 33-51-13. REPLACED BATTERY PACK/CHARGER
- [SDR SWAA2025022498256](https://openairdocs.org/sdr/SWAA2025022498256.md): Light · disconnected · Feb 22, 2025 · N215WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHT INOP AFT OF FED <[01]. CHECKED FOR GROUND AND POWER AT L731 (FORWARD ESCAPE SLIDE LIGHT); FOUND NEITHER GROUND OR VOLTAGE AY L731 LIGHT SOCKET PER WDM 33-51-12. FOUND INCOMPLETE CONNECTION AT D11074. RECONNECTED AND TESTED PER WDM 33-51-12
- [SDR SWAA2025022497379](https://openairdocs.org/sdr/SWAA2025022497379.md): Light · burned out · Feb 19, 2025 · N215WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHT SIDEWALL SIGN AT L/H OVERWING EXIT HAS BURNED OUT BULBS <[01]. RELAMPED EMERGENCY EXIT LIGHT AT L/H SIDEWALL OVERWING EXIT AND PERFORMED A SATISFACTORY TEST OF NEW LAMPS IAW AMM 33-51-01-960--801 STEPS 2.C.(1); (A); 1); 4); B); (C); (2)-(
- [SDR SWAA2025022496769](https://openairdocs.org/sdr/SWAA2025022496769.md): Battery Pack · inoperative · Feb 16, 2025 · N215WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHTS FWD RIGHT OVERDOOR EXIT INOP L1067 <[01]. PER TROUBLESHOOTING PERFORMED GOOD CONTINUITY CHECK FROM CONNECTOR D10750 TO CONNECTOR D2968 IAW WDM 33-51-12; SWAP OF BATTERY PACKS BETWEEN M1675 AND M1674 PERFORMED; FAILURE CHANGED; BATTERY PACK M16
- [SDR SWAA2025022494152](https://openairdocs.org/sdr/SWAA2025022494152.md): Lens · damaged · Feb 8, 2025 · N215WN · Boeing 7377H4 · Emergency Lighting
  > AFT LAVE 'B' EMERGENCY EXIT LIGHT LENS DAMAGED<[01] REMOVED AND REPLACED AFT LAVE 'B' EMERGENCY EXIT LIGHT LENS PER AMM 33-51-01-960-801;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
- [SDR SWAA2025022493806](https://openairdocs.org/sdr/SWAA2025022493806.md): Wire · broken · Feb 7, 2025 · N215WN · Boeing 7377H4 · Light System Wiring
  > G-1 GALLEY MOUNTED EMERGENCY EXIT LIGHT WIRE BROKEN AT CONNECTOR<[01] DISCONNECTABLE SPLICE AT EMERGENCY EXIT LIGHT-FWD-FLOOR PROXIMITY G-1 GALLEY WAS REPLACED AND A SATISFACTORY OPERATIONAL TEST OF THE EMERGENCY LIGHTS WAS PERFORMED WITH NO DEFECTS FOUND IAW
- [SDR SWAA2025022489513](https://openairdocs.org/sdr/SWAA2025022489513.md): Baffle · cracked · Jan 25, 2025 · N215WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO BAY L/H BAFFLE CRACKED BS440 TO BS460 LBL22 WL156<[01] CORRECTION: FORWARD CARGO BAY L/H BAFFLE CRACKED BS440 TO BS460 LBL22 WL156 [TTG8Q00YBXHD].;[02] REMOVED DAMAGED BAFFLE AND INSTALLED NEW BAFFLE AS PER SRM 51-40-02-0G-0 AND DRAWING 143A7505 REV.
- [SDR SWAA2025022588983](https://openairdocs.org/sdr/SWAA2025022588983.md): Vapor Barrier · cracked · Jan 24, 2025 · N215WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > STIFFENER CRACKED COMMON TO VAPOR BARRIER BS663 LBL26 WL151 <[01]. REMOVED AND REPLACED NEW STIFFENER COMMON TO VAPOR BARRIER BS663 LBL26 WL151 IAW SRM 51-40-02-0G-0 AND DWG 111A1000 REV:-.
- [SDR SWAA2025022488980](https://openairdocs.org/sdr/SWAA2025022488980.md): Baffle · cracked · Jan 23, 2025 · N215WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FORWARD CARGO BAY BAFFLE IS CRACKED BS460 TO BS480 LBL25 WL156<[01] REMOVED DAMAGED BAFFLE AND INSTALLED NEW BAFFLE AS PER SRM 51-40-02-0G-0 AND DRAWING 143A7505 REV.-.;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2025022588169](https://openairdocs.org/sdr/SWAA2025022588169.md): Seat Track · corroded · Jan 22, 2025 · N215WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LBL 45 SEAT TRACK WELL AT STA 500A+8; WL 208.1. <[01] DISCREPANCY RECORD ON CCN TTG8Q00Y9RNQ REQUIRED REMOVED AND REPLACED THEREFORE CARD TO BE CLOSED AND ALL WORK DONE WAS RECORDED ON TTG8Q00Y9RNQ; [02] DISCREPANCY RECORD ON CCN TTG8Q00Y9RNQ REQU
- [SDR SWAA2025022588170](https://openairdocs.org/sdr/SWAA2025022588170.md): Seat Track · corroded · Jan 22, 2025 · N215WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LBL 24 SEAT TRACK WELL AT STA 500B+18; WL 208.1. <[01] DISCREPANCY RECORD ON CCN TTG8Q00Y9RP3 REQUIRED REMOVED AND REPLACED THEREFORE CARD TO BE CLOSED AND ALL WORK DONE WAS RECORDED ON TTG8Q00Y9RP3; [02] DISCREPANCY RECORD ON CCN TTG8Q00Y9RP3 REQ
- [SDR SWAA2025022488151](https://openairdocs.org/sdr/SWAA2025022488151.md): Strap · corroded · Jan 22, 2025 · N215WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO BAY FLOOR T STRAP BS 727D+5 RBL 9 TO RBL 18 WL 156<[01] CORRECTION TO DISCREPANCY; SHOULD READ; CORROSION ON AFT CARGO BAY FLOOR T STRAP BS 727D+5 RBL 9 TO RBL 18 WL 156;[02] EVALUATED CORROSION FOUND TO BE OUT OF LIMITS; RECEIVED NEW ST
- [SDR SWAA2025022488150](https://openairdocs.org/sdr/SWAA2025022488150.md): Strap · corroded · Jan 22, 2025 · N215WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO BAY FLOOR T STRAP BS 767+5 RBL 12 - TO RBL 19 WL 156<[01] EVALUATED CORROSION FOUND TO BE OUT OF LIMITS; RECEIVED NEW STRAP AND PAINTED WHITE ALL PER SRM 51-10-02; MM 51-21-73-370-804 AND ACO 5360-E-16462;[02] VERIFIED CORRECTIVE ACTION
- [SDR SWAA2025022488537](https://openairdocs.org/sdr/SWAA2025022488537.md): Attach Angle · corroded · Jan 22, 2025 · N215WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CORROSION AFT CARGO BAY ATTACH ANGLE UNDER SHIELD HAS MULTIPLE AREAS UNDER NUT PLATES BS767 TO BS787 RBL21 WL156<[01] CORROSION ON AFT CARGO BAY ATTACH ANGLE UNDER SHIELD BS 767 TO 787 RBL 21 WL 156; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE
- [SDR SWAA2025022488538](https://openairdocs.org/sdr/SWAA2025022488538.md): Shield · corroded · Jan 22, 2025 · N215WN · 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] CORROSION ON AFT CARGO BAY FWD SHIELD; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. REMOVED; REPLACED AND INSTALLED AFT CARGO
- [SDR SWAA2025022488148](https://openairdocs.org/sdr/SWAA2025022488148.md): Support Plate · corroded · Jan 21, 2025 · N215WN · 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] CORROSION ON AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE; FOUND TO BE OUT LIMITS. REMOVE AND REPLACE L/H FLOOR TO SIDEWALL
- [SDR SWAA2025022488149](https://openairdocs.org/sdr/SWAA2025022488149.md): Support · corroded · Jan 21, 2025 · N215WN · 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] DAMAGED ON R/H FLOOR TO SIDEWALL SUPPORT PLATE; FOUND TO BE OUT OF LIMITS. REMOVED; REPLACED AND INSTALLED NEW FLOOR TO SIDEW
- [SDR SWAA2025022487908](https://openairdocs.org/sdr/SWAA2025022487908.md): Threshold · cracked · Jan 21, 2025 · N215WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY AFT CORNER THRESHOLD IS CRACKED <[01]. REPAIRED AFT CARGO BAY AFT CORNER THRESHOLD PER SRM 53-60-15-2R-1.
- [SDR SWAA2025022487909](https://openairdocs.org/sdr/SWAA2025022487909.md): Threshold · cracked · Jan 21, 2025 · N215WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY FORWARD CORNER THRESHOLD IS CRACKED <[01]. REPAIRED AFT CARGO BAY FORWARD CORNER THRESHOLD PER SRM 53-60-15-2R-1.
- [SDR SWAA2025022487794](https://openairdocs.org/sdr/SWAA2025022487794.md): Floor Panel · delaminated · Jan 20, 2025 · N215WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 242NF DELAMINATED. (CUSTOMER REQUEST)<[01] PASSENGER CABIN FLOOR PANEL 242NF WITH UPPER SKIN DELAMINATIONS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.
- [SDR SWAA2025022487795](https://openairdocs.org/sdr/SWAA2025022487795.md): Floor Panel · delaminated · Jan 20, 2025 · N215WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 242MF DELAMINATED. (CUSTOMER REQUEST)<[01] PASSENGER CABIN FLOOR PANEL 242MF WITH UPPER SKIN DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.
- [SDR SWAA2025022487797](https://openairdocs.org/sdr/SWAA2025022487797.md): Floor Panel · delaminated · Jan 20, 2025 · N215WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 241SF DELAMINATED. (CUSTOMER REQUEST)<[01] PASSENGER CABIN FLOOR PANEL 241SF WITH UPPER SKIN DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.
- [SDR SWAA2025022487796](https://openairdocs.org/sdr/SWAA2025022487796.md): Floor Panel · delaminated · Jan 20, 2025 · N215WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 241RF DELAMINATED. (CUSTOMER REQUEST)<[01] PASSENGER CABIN FLOOR PANEL 241RF; WITH DELAMINATION; WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] JOB COMPLETE.
- [SDR SWAA2025022487793](https://openairdocs.org/sdr/SWAA2025022487793.md): Floor Panel · delaminated · Jan 20, 2025 · N215WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 241TF DELAMINATED. (CUSTOMER REQUEST)<[01] PASSENGER CABIN FLOOR PANEL 241TF WITH UPPER SKIN DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.
- [SDR SWAA2025022487628](https://openairdocs.org/sdr/SWAA2025022487628.md): Floor Panel · delaminated · Jan 20, 2025 · N215WN · Boeing 7377H4 · Fuselage Floor Panel
  > MAIN CABIN; FLOOR PANEL 241AAF TOP LAYER FIBER GLASS EXPOSED.<[01] 241AAF; WITH UPPER SURFACE DAMAGE; WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHE
- [SDR SWAA2025022586847](https://openairdocs.org/sdr/SWAA2025022586847.md): Former · cracked · Jan 17, 2025 · N215WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > WING TO BODY FAIRING FORMER IS CRACKED BS 500D BETWEEN STRINGER 19 AND 20 L/H <[01]. REMOVED DAMAGED FAIRING FORMER AND INSTALLED NEW FAIRING FORMER BS 500D BETWEEN STRINGER 19 AND 20 L/H IAW SRM 51-40-02-0G-0 AND DWG 116A3110 REV:- AND 116A3010 REV:-.; [02] V
- [SDR SWAA2025022487207](https://openairdocs.org/sdr/SWAA2025022487207.md): Stiffener · cracked · Jan 17, 2025 · N215WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > STIFFENER CRACKED AT BS 250 LBL 4 WL 208 <[01]. REMOVE AND REPLACED STIFFENER AT BS 250 LBL 4 WL 208 I.A.W SRM 51-10-02-0G-0; SRM 51-40-02-0G-0 AND BOEING DWG 141A5100 REV:
- [SDR SWAA2025022586760](https://openairdocs.org/sdr/SWAA2025022586760.md): Panel · cracked · Jan 16, 2025 · N215WN · Boeing 7377H4 · Fuselage Floor Panel
  > CRACKED PANEL BREAK BS 540 BL 0 - RBL 25 WL 207 (MARKED) <[01]. REPLACED CRACKED PANEL BREAK WITH NEW AT BS 540 BL 0 - RBL 25 WL 207. REMOVED PART AND FOUND NO ALLOWABLE LIMITS IAW SRM 51-10-02 STEP 9 AND SRM 51-40-02. LOCATED AND DRILLED NEW SERVICEABLE PART
- [SDR SWAA2025022487904](https://openairdocs.org/sdr/SWAA2025022487904.md): Floor Panel · delaminated · Jan 16, 2025 · N215WN · Boeing 7377H4 · Fuselage Floor Panel
  > PANEL 241BF HAS BUBBLES; DENTS AND FRAYED ON TOP PLY FIBERGLASS (MARKED)<[01] PANEL 241BF WITH BUBBLES (DELAMINATION); DENTS AND FIBERGLASS STRAND FRAYING ON TOP PLY AS MARKED WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO
- [SDR SWAA2025022586303](https://openairdocs.org/sdr/SWAA2025022586303.md): Vapor Barrier · cracked · Jan 15, 2025 · N215WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > L/H B.S. 663 VAPOR BARRIER IS CRACKED AT MID SPAN <[01]. L/H B.S. 663 VAPOR BARRIER DAMAGE AT MID SPAN HAS BEEN REPAIRED PER [SRM 51-70-04-2R-10-A00755 (REPAIR 10 - REPAIR OF DAMAGE THAT IS MORE THAN 0.50 INCH IN SOLID LAMINATES - AIRFRAME - PERMANENT)] ATTAC
- [SDR SWAA2025022486038](https://openairdocs.org/sdr/SWAA2025022486038.md): Door · corroded · Jan 15, 2025 · N215WN · Boeing 7377H4 · Service Doors
  > LAV SERVICE DOOR IS CORRODED AT BONDING JUMPER ATTACH POINT <[01]. EVALUATED CORROSION ON LAV SERVICE DOOR; FOUND 0.040 REMOVED FROM ORIGINAL.100 IN A 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 52-40-01-1A-4;[02] REMOVED AND REPLACED DAMAGED LAV SERVICE D
- [SDR SWAA2025022586024](https://openairdocs.org/sdr/SWAA2025022586024.md): Skin · cracked · Jan 14, 2025 · N215WN · Boeing 7377H4 · Leading Edge Devices
  > RH WING #5 SLAT FOUND CRACK AT LEADING EDGE NOSE SKIN LOWER SURFACE FASTENER; MARKED <[01]. REPAIRED RH WING #5 SLAT AT LEADING EDGE NOSE SKIN LOWER SURFACE IAW SRM 51-40-02-0G-0 AND SRM 57-42-01-2R-8; REPAIR 8; FIG. 202.; [02] VERIFIED CORRECTIVE ACTION.
- [SDR SWAA2025022586029](https://openairdocs.org/sdr/SWAA2025022586029.md): Slat · cracked · Jan 14, 2025 · N215WN · Boeing 7377H4 · Leading Edge Devices
  > LH WING #2 SLAT FOUND CRACK AT LEADING EDGE NOSE SKIN LOWER SURFACE FASTENER; MARKED <[01]. REPAIRED LH WING #2 SLAT AT LEADING EDGE NOSE SKIN LOWER SURFACE IAW SRM 57-42-01-2R-8 REPAIR 8 ALTERNATIVE 1.; [02] VERIFIED CORRECTIVE ACTION 1.
- [SDR SWAA2025022586030](https://openairdocs.org/sdr/SWAA2025022586030.md): Slat · cracked · Jan 14, 2025 · N215WN · Boeing 7377H4 · Leading Edge Devices
  > LH WING #4 SLAT FOUND CRACK AT LEADING EDGE NOSE SKIN LOWER SURFACE FASTENER; MARKED <[01]. REPAIRED LH WING #4 SLAT AT LEADING EDGE NOSE SKIN LOWER SURFACE IAW SRM 57-42-01-2R-8.; [02] CORRECTED MEASUREMENT TABLE; [03] VERIFIED CORRECTIVE ACTION.
- [SDR SWAA2024110455247](https://openairdocs.org/sdr/SWAA2024110455247.md): Acm · seized · Oct 30, 2024 · N215WN · Boeing 7377H4 · Cabin Cooling System
  > ON CLIMB OUT F/A NOTICED SMOKE SMELL. NO SMOKE VISIBLE+ SMELL CLEARED AFTER A MINUTE. RAN PACKS FUL COLD BUT DUCT TEMP NEVER WENT BELOW 80 DEGREES. AFTER LANDING- DUCT TEMP RAN AWAY+RT PAC TRIP OFF LIGHT ILLUM TURNED RT PACK OFF FOR TAXI IN. PACK TRIP LT CLEAR
- [SDR SWAA2024091135478](https://openairdocs.org/sdr/SWAA2024091135478.md): Charger · inoperative · Sep 8, 2024 · N215WN · Boeing 7377H4 · Emergency Lighting
  > 3 INTERIOR AND 1 EXTERIOR EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED CHARGER ASSEMBLY AND BATTERY PACK FWD OF LH EMERGENCY EXIT DOOR IAW AMM 33-51-06. OPS CHECK GOOD
- [SDR SWAA2023110316359](https://openairdocs.org/sdr/SWAA2023110316359.md): Seal · cracked · Oct 31, 2023 · N215WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > -LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED.<[01] REMOVED AND REPLACED LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL PER AMM 53-31-31
- [SDR SWAA2023072882803](https://openairdocs.org/sdr/SWAA2023072882803.md): Panel · out of adjust · Jul 27, 2023 · N215WN · Boeing 7377H4 · Wing Structure
  > RH WING INBOARD FIXED TRAILING EDGE UPPER PANEL IS OUT OF ADJUSTMENT.<[01] ADJUSTED PANEL REF AMM 57-50-01.;[02] REMOVED INSPECTION REQUIREMENTS. ADJUSTED PANEL REF AMM 57-50-01.

Next page: https://openairdocs.org/aircraft/N215WN/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 = 'N215WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N215WN/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.