# Service difficulty reports: N208WN

A list on [N208WN](https://openairdocs.org/aircraft/N208WN.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 9 · 417 reports

- [SDR SWAA2026100994144](https://openairdocs.org/sdr/SWAA2026100994144.md): Hydrolock · out of adjust · Oct 5, 2026 · N208WN · Boeing 7377H4 · Passenger Compartment Equipment
  > SEAT 5E WILL NOT STAY UPRIGHT. ADJUSTED SEAT HYDROLOCK IAW AMM 25-22-00 OPS CK GOOD
- [SDR SWAA2026100781291](https://openairdocs.org/sdr/SWAA2026100781291.md): Skin · cracked · Sep 25, 2026 · N208WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CRACK ON THE EXTERNAL GROUND ELECTRICAL POWER CUTOUT, LOWER AREA. REPAIRED THE EXTERNAL GROUND ELECTRICAL POWER CUTOUT IAW SRM 53-10-15-2R-4, REPAIR 4.
- [SDR SWAA2026100781953](https://openairdocs.org/sdr/SWAA2026100781953.md): Support Angle · cracked · Sep 17, 2026 · N208WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT ANGLE, BS 867, STR 3R. REPLACED THE SUPPORT ANGLE IAW SRM: 51-10-02-0G-0 146A7901, SHEET 19, REV-.
- [SDR SWAA2026100759352](https://openairdocs.org/sdr/SWAA2026100759352.md): Support Bracket · cracked · Sep 16, 2026 · N208WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACKED SUPPORT BRACKET FOR ACCESS PANEL 551FB ON THE LT WING. REPLACED THE SUPPORT BRACKET IAW SRM 51-10-02, ITEM 9, & SRM 51-40-02.
- [SDR SWAA2026100765174](https://openairdocs.org/sdr/SWAA2026100765174.md): Support Angle · cracked · Sep 16, 2026 · N208WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACKED SUPPORT ANGLE FOR ACCESS PANEL 551FB, LT WING. REPLACED SUPPORT ANGLE IAW SRM 51-40-02-0G-0, AND DWG 115A2710, SHEET 6, REV B.
- [SDR SWAA2026100702313](https://openairdocs.org/sdr/SWAA2026100702313.md): Angle · cracked · Sep 15, 2026 · N208WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACKED ANGLE, TRAILING EDGE ORSS 261 + 10 INCHES ON THE LT WING. REPLACED THE ANGLE IAW SRM 51-10-02-0G-0, ITEM 9, AND SRM 51-40-02-0G-0.
- [SDR SWAA2026100705700](https://openairdocs.org/sdr/SWAA2026100705700.md): Crossbeam · cracked · Sep 14, 2026 · N208WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACKED CROSSBEAM, BS 540, LBL45.5 - LBL 24.75. REPLACED THE CROSSBEAM IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, AND DWG 143A5240, SHEET 1, REV-.
- [SDR SWAA2026100742039](https://openairdocs.org/sdr/SWAA2026100742039.md): Plate · damaged · Sep 14, 2026 · N208WN · Boeing 7377H4 · Wing Main, Frame Structure
  > ELONGATED HOLES ON CORRUGATED PLATE TRAILING EDGE AT ORSS261 AT RT WING. REPLACED CORRUGATED PLATE TRAILING EDGE AT ORSS 261 AT RT WING IAW SRM 51-40-02, AND DRAWING 115A2001, REV-.
- [SDR SWAA2026100762383](https://openairdocs.org/sdr/SWAA2026100762383.md): Access Panel · damaged · Sep 14, 2026 · N208WN · Boeing 7377H4 · Wing, Plate/Skin
  > ELONGATED HOLES ON ACCESS PANEL 661BB ON RT WING. REPAIRED THE ACCESS PANEL 661BB IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2026100740145](https://openairdocs.org/sdr/SWAA2026100740145.md): Light · deteriorated · Sep 14, 2026 · N208WN · Boeing 7377H4 · Emergency Lighting
  > DETERIORATED PHOTOLUMINESCENT STRIP ALONG PASSENGER CABIN (1 KT) REPLACED THE PHOTOLUMINESCENT STRIP ALONG PASSENGER CABIN IAW AMM 33-51-15-400-802, AND DWG 33500007, SHEET 2, REV 3.
- [SDR SWAA2026100727826](https://openairdocs.org/sdr/SWAA2026100727826.md): Crossbeam · cracked · Sep 14, 2026 · N208WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACKED BREAK PANEL, BS 540 BTWN RBL 24.75 - BL 0. REPLACED THE BREAK PANEL IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, ITEM 9, DWG 143A5240, SHEET 13, REV A.
- [SDR SWAA2026100718728](https://openairdocs.org/sdr/SWAA2026100718728.md): Access Panel · elongated · Sep 14, 2026 · N208WN · Boeing 7377H4 · Wing, Plate/Skin
  > ELONGATED HOLES ON LT WING ACCESS PANEL 561BB. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.
- [SDR SWAA2026100779718](https://openairdocs.org/sdr/SWAA2026100779718.md): Tray Table · broken · Sep 13, 2026 · N208WN · Boeing 7377H4 · Passenger Compartment Equipment
  > BROKEN FOOD TRAY, PASSENGER SEAT ROW 1C, 14B, 14C, 26C, 20A, 26A, AND 26B. REPLACED THE FOODTRAYS IAW CMM 25-21-45, REV 07, DISASSEMBLY ITEM 3, STEP B (6), PAGE 3005, IPL FIGURE 4, PAGE 10102, AND ASSEMBLY ITEM 3, STEP AB (1), PAGE 7018, IPL FIGURE 4, PAGE 1
- [SDR SWAA2026100701870](https://openairdocs.org/sdr/SWAA2026100701870.md): Scuff Plate · cracked · Sep 13, 2026 · N208WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED SERVICE DOOR SCUFF PLATE. REPAIRED THE SCUFF PLATE IAW SRM 53-10-15-2R-2, REPAIR 2, & BAC 5975.
- [SDR SWAA2026100767136](https://openairdocs.org/sdr/SWAA2026100767136.md): Rib · cracked · Sep 13, 2026 · N208WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > CRACKED LEADING EDGE RIB, HSS 114.55 OF RT HORIZONTAL STAB. REPLACED THE RIB IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 186A1001, SHEET 10, REV A.
- [SDR SWAA2026100762037](https://openairdocs.org/sdr/SWAA2026100762037.md): Access Panel · cracked · Sep 12, 2026 · N208WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACKED BLADE ASSY ON THE LT HORIZONTAL STAB ACCESS PANEL 333AT. REPLACED THE BLADE ASSY FOR ACCESS PANEL 333AT IAW SRM 51-10-02, ITEM 9, AND SRM 51-40-02.
- [SDR SWAA2026100706824](https://openairdocs.org/sdr/SWAA2026100706824.md): Scuff Plate · cracked · Sep 12, 2026 · N208WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT. REPAIRED AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW SRM 53-30-15-2R-1 REPAIR 1. AND BAC 5975.
- [SDR SWAA2026100721741](https://openairdocs.org/sdr/SWAA2026100721741.md): Support Angle · cracked · Sep 12, 2026 · N208WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT ANGLE LOC BS 694 AND WL 204 RBL 24.75. REPLACED SUPPORT ANGLE IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, ITEM 9, & DWG 273A9110, SHEET 6, REV A.
- [SDR SWAA2026100721589](https://openairdocs.org/sdr/SWAA2026100721589.md): Support Angle · cracked · Sep 12, 2026 · N208WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT ANGLE, BS 694, WL 204, BL 0. REPLACED THE SUPPORT ANGLE & FASTENERS IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, & DWG 273A9110, SHEET 6, REV A.
- [SDR SWAA2026100721166](https://openairdocs.org/sdr/SWAA2026100721166.md): Scuff Plate · cracked · Sep 12, 2026 · N208WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED AFT CORNER OF SCUFF PLATE IN THE AFT CARGO BAY. REPAIRED AFT CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1.
- [SDR SWAA2026100722184](https://openairdocs.org/sdr/SWAA2026100722184.md): Access Panel · damaged · Sep 11, 2026 · N208WN · Boeing 7377H4 · Wing, Plate/Skin
  > ELONGATED HOLES ON ACCESS PANEL 561CB TRAILING EDGE AT LT WING. REPAIRED ACCESS PANEL 561CB TRAILING EDGE AT LT WING IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2026100782130](https://openairdocs.org/sdr/SWAA2026100782130.md): Access Panel · damaged · Sep 11, 2026 · N208WN · Boeing 7377H4 · Wing, Plate/Skin
  > ELONGATED HOLES OF ACCESS PANEL 661BB, ON RT WING. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2026100702179](https://openairdocs.org/sdr/SWAA2026100702179.md): Access Panel · damaged · Sep 11, 2026 · N208WN · Boeing 7377H4 · Wing, Plate/Skin
  > ELONGATED HOLES ON ACCESS PANEL 661CB, AT THE TRAILING EDGE OF RT WING. REPAIRED THE ACCESS PANEL 661CB IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2026100722013](https://openairdocs.org/sdr/SWAA2026100722013.md): Access Panel · damaged · Sep 11, 2026 · N208WN · Boeing 7377H4 · Wing, Plate/Skin
  > ELONGATED HOLES ON ACCESS PANEL 661AB AT RT WING. REPAIRED THE ACCESS PANEL 661AB AT RT WING IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2026100721953](https://openairdocs.org/sdr/SWAA2026100721953.md): Access Panel · damaged · Sep 11, 2026 · N208WN · Boeing 7377H4 · Wing, Plate/Skin
  > ELONGATED HOLES ON ACCESS PANEL 561AB AT LT WING. REPAIRED ACCESS PANEL 561AB AT LT WING IAW SRM-51-70-04-2R-10 REPAIR 10.
- [SDR SWAA2026100750732](https://openairdocs.org/sdr/SWAA2026100750732.md): Access Panel · elongated · Sep 11, 2026 · N208WN · Boeing 7377H4 · Wing, Plate/Skin
  > ELONGATED HOLES ON THE LEFT WING ACCESS PANEL 561BB. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2026100702039](https://openairdocs.org/sdr/SWAA2026100702039.md): Skin · corroded · Sep 10, 2026 · N208WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CORROSION ON EXTERNAL SKIN AROUND DRAIN, BS 967 4 INCHES ON LOWER FUSELAGE. EVALUATED CORRODED AREA AND FOUND WITHIN LIMITS IAW SRM 53-00-01-1A-1, ALLOWABLE DAMAGE 1, PARAGRAPH 4.B(2)(D), FIGURE 103 SHEET 1, DETAIL C.
- [SDR SWAA2026100741321](https://openairdocs.org/sdr/SWAA2026100741321.md): Skin · cracked · Sep 9, 2026 · N208WN · Boeing 7377H4 · Leading Edge Devices
  > CRACKED LOWER SURFACE OF LEADING EDGE SLAT NR 3, NOSE SKIN AT THE ACTUATOR AROUND FASTENERS LT WING. REPAIRED LOWER SURFACE OF LEADING-EDGE SLAT 3 NOSE SKIN IAW SRM 57-42-01-2R-8.
- [SDR SWAA2026090822250](https://openairdocs.org/sdr/SWAA2026090822250.md): Carpet · out of position · Sep 3, 2026 · N208WN · Boeing 7377H4 · Passenger Compartment Equipment
  > CARPET STRIP INSTALLED STARTING FROM 4C AND ENDING UNDER 9C IS LAYING OVER THE PHOTO ILLUMINESCENT AISLE STRIP. ADJUSTED CARPET IAW AMM 25-27-15 02
- [SDR SWAA2026042088953](https://openairdocs.org/sdr/SWAA2026042088953.md): Light · contaminated · Apr 14, 2026 · N208WN · Boeing 7377H4 · Emergency Lighting
  > PASSENGER CABIN SEAT ROW 1DEF AND 1ABC PHOTOLUMINESCENT STRIPS HAVE MOISTURE UNDER LENS. R & R THE PHOTOLUMINESCENT STRIPS IAW AMM 33-51-15.
- [SDR SWAA2026041789656](https://openairdocs.org/sdr/SWAA2026041789656.md): Door · cracked · Apr 14, 2026 · N208WN · Boeing 7377H4 · Landing Gear Doors
  > LEFT MLG STRUT DOOR IS CRACKED AT THE LOWER FWD ATTACH POINT CASTING. REMOVED CENTER AND INNER DOORS ON L/H SIDE REF MM 32-13-11 OK TO CONT REF CDL 32-10-3. INSTALLED LT CENTER AND INNER DOODS IAW AMM 32-13-11ADJUSTMENT CK GOOD. REMOVED & INSTALLED LT CEN
- [SDR SWAA2026032482717](https://openairdocs.org/sdr/SWAA2026032482717.md): Slide · out of position · Mar 23, 2026 · N208WN · Boeing 7377H4 · Escape Slide
  > FWD SERVICE DOOR SLIDE DISPLACED IN CONTAINER. REPOSITIONED SLIDE IN CONTAINER PER MT 725-61-06
- [SDR SWAA2026021670581](https://openairdocs.org/sdr/SWAA2026021670581.md): Slide · low pressure · Feb 13, 2026 · N208WN · Boeing 7377H4 · Escape Slide
  > L1 SLIDE PRESSURE OUT OF GREEN. REMOVED AND REPLACED L1 DOOR ESCAPE SLIDE IAW AMM 25-66-01.
- [SDR SWAA2025121544175](https://openairdocs.org/sdr/SWAA2025121544175.md): End Plug · missing · Dec 9, 2025 · N208WN · Boeing 7377H4 · Escape Slide
  > AFT GALLEY R2 SLIDE COVER CENTER BUMPER STRIP MISSING END CAP. REPLACED AFT GALLEY R2 SLIDE COVER CENTER BUMPER STRIP END CAP IAW AMM 25-66-01.
- [SDR SWAA2025121548850](https://openairdocs.org/sdr/SWAA2025121548850.md): Strip · missing · Dec 9, 2025 · N208WN · Boeing 7377H4 · Escape Slide
  > AFT GALLEY R2 SLIDE COVER CENTER BUMPER STRIP MISSING END CAP. REPLACED AFT GALLEY R2 SLIDE COVER CENTER BUMPER STRIP END CAP IAW AMM 25-66-01.
- [SDR SWAA2025121244180](https://openairdocs.org/sdr/SWAA2025121244180.md): Girt Bar · out of adjust · Dec 9, 2025 · N208WN · Boeing 7377H4 · Emergency Equipment
  > FWD ENTRY DOOR SLIDE GIRT BAR HANGING LOW. RESECURED CABIN FWD ENTRY DOOR SLIDE GIRT BAR IAW AMM 25-66-01.
- [SDR SWAA2025121244179](https://openairdocs.org/sdr/SWAA2025121244179.md): Girt Bar · out of adjust · Dec 9, 2025 · N208WN · Boeing 7377H4 · Emergency Equipment
  > FWD SERVICE DOOR SLIDE GIRT BAR HANGING LOW. SECURED CABIN FWD SERVICE DOOR SLIDE GIRT BAR IAW AMM 25-66-01.
- [SDR SWAA2025121248853](https://openairdocs.org/sdr/SWAA2025121248853.md): Girt Bar · out of adjust · Dec 9, 2025 · N208WN · Boeing 7377H4 · Emergency Equipment
  > FWD SERVICE DOOR SLIDE GIRT BAR HANGS LOW. SECURED CABIN FWD SERVICE DOOR SLIDE GIRT BAY IAW AMM 25-66-01.
- [SDR SWAA2025121248854](https://openairdocs.org/sdr/SWAA2025121248854.md): Girt Bar · out of adjust · Dec 9, 2025 · N208WN · Boeing 7377H4 · Emergency Equipment
  > FWD ENTRY DOOR SLIDE GIRT BAR HANGS LOW. SECURED CABIN FWD ENTRY DOOR SLIDE GIRT BAY IAW AMM 25-66-01.
- [SDR SWAA2025091112695](https://openairdocs.org/sdr/SWAA2025091112695.md): Retainer · loose · Sep 8, 2025 · N208WN · Boeing 7377H4 · Emergency Equipment
  > FWD BOARDING DOOR EVACUATION SLIDE RETAINING CLIP IS LOOSE. SECURED CLIP ON FWD ENTRY DOOR REF S.I.P.
- [SDR SWAA2025042226194](https://openairdocs.org/sdr/SWAA2025042226194.md): Screw · loose · Apr 18, 2025 · N208WN · Boeing 7377H4 · Passenger Compartment Equipment
  > LOSE SCREW ON 10C TRAY TABLE<[01] TIGHTEN SCREW ON ROW 10C TRAY TABLE PER SIP
- [SDR SWAA2024112160351](https://openairdocs.org/sdr/SWAA2024112160351.md): Shield · cracked · Nov 15, 2024 · N208WN · Boeing 7377H4 · Nacelle/Pylon Miscellaneous Structure
  > REJECT: #1 ENGINE I/B FAN COWL OIL ACCESS DOOR SHIELD; CRACK STILL EXISTS.<[01] REPLACED #1 ENGINE IB FAN COWL OIL ACCESS DOOR SHIELD AND OPENED/CLOSED IB FAN COWL PER AMM 71-11-02; SRM 51-40-02.;[02] VERIFIED MEASUREMENTS;[03] VERIFIED CORRECTIVE ACTION ITEM
- [SDR SWAA2024112059272](https://openairdocs.org/sdr/SWAA2024112059272.md): Light · inoperative · Nov 12, 2024 · N208WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHT L1191 (EXIT INDICATOR LIGHT); R/H G4 GALLEY INOP EMERGENCY LIGHT L1191 (EXIT INDICATOR LIGHT) R/H G4 GALLEY INOP<[01] RELAMPED EMERGENCY LIGHT L1191 (EXIT INDICATOR LIGHT); R/H G4 GALLEY; PERFORMED GOOD TEST PER AMM 33-51-01-960-801;[02] VERIFI
- [SDR SWAA2024112059045](https://openairdocs.org/sdr/SWAA2024112059045.md): Scuff Plate · cracked · Nov 12, 2024 · N208WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD SERVICE DOOR SCUFF PLATE IS CRACKED<[01] REMOVED AND REPAIRED FSD SCUFF PLATE AND THEN INSTALLED IAW AMM 51-21-72-370-804 AMM 53-11-01-000-801 AMM 53-11-01-420-801 SRM 53-10-15-2R-2 PARA 4.B.(3) AND SOPM 20-20-02;[02] JOB COMPLETE.
- [SDR SWAA2024112058524](https://openairdocs.org/sdr/SWAA2024112058524.md): Lens · out of adjust · Nov 10, 2024 · N208WN · Boeing 7377H4 · Emergency Lighting
  > RH EMERGENCY EXIT HATCH OVERHEAD LIGHT LENS INSTALLED INCORRECTLY. (MARKED)<[01] REMOVED AND INSTALLED R/H EMERGENCY EXIT HATCH OVERHEAD LIGHT LENS IAW SOPM 20-50-01;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
- [SDR SWAA2024112057854](https://openairdocs.org/sdr/SWAA2024112057854.md): Panel · delaminated · Nov 7, 2024 · N208WN · Boeing 7377H4 · Aerodynamic Fairings
  > PANEL 193AL; DELAMINATED.<[01] PANEL 193AL HAS MULTIPLE AREAS OF DAMAGE AND IS BEYOND ECONOMICAL REPAIR. PANEL WAS REPLACED IAW SRM 51-10-02-0G-0 PARAGRAPH 9; AND IPC 53-14-00-03A ITEM 230.;[02] VERIFIED JOB COMPLETE
- [SDR SWAA2024112055350](https://openairdocs.org/sdr/SWAA2024112055350.md): Skin Panel · cracked · Oct 31, 2024 · N208WN · Boeing 7377H4 · Trailing Edge Flaps
  > PERFORM PERMANENT REPAIR ON LH WING TRAILING EDGE UPPER SKIN PANEL 551DT WITH UPPER SKIN CRACK AND EDGE DAMAGE<[01] PERFORMED PERMANENT REPAIR ON LH WING TRAILING EDGE UPPER SKIN PANEL 551DT WITH UPPER SKIN CRACK AND EDGE DAMAGE IAW SRM 51-70-05-2R-6.;[02] VER
- [SDR SWAA2024112053731](https://openairdocs.org/sdr/SWAA2024112053731.md): Seat Track · corroded · Oct 25, 2024 · N208WN · Boeing 7377H4 · Fuselage Internal Mounting Structure
  > PASS. CABIN SEAT TRACK LBL 45 HAS CORROSION ON WELL; STA480+2.5; STA500+9.5 TO 500A; 500A+17 AND 500B+2; WL 208<[01] THIS FAULT WILL BE RESOLVED ON FAULT # TTG8Q00WNP86;[02] VERIFIED CORRECTION ACTION ITEM 1 MEASUREMENT FIELD; CARD ACCOMPLISHED ON FAULT # TTG8
- [SDR SWAA2024112052267](https://openairdocs.org/sdr/SWAA2024112052267.md): Scuff Plate · cracked · Oct 23, 2024 · N208WN · Boeing 7377H4 · Cargo Compartments
  > FWD CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED<[01] REPAIRED FWD CARGO BAY FWD CORNER SCUFF PLATE<BR>IAW 53-30-15-2R-1<BR>FWD CARGO BAY FWD CORNER SCUFF PLATE WILL BE INSTALLED ON CARD# TTG8Q006MGJX;[02] VERIFIED ITEM 1 AND TASK CARD COMPLETED.
- [SDR SWAA2024112152064](https://openairdocs.org/sdr/SWAA2024112152064.md): Frame · cracked · Oct 22, 2024 · N208WN · Boeing 7377H4 · Fuselage Main, Frame
  > FRAME ASSEMBLY CRACKED IN PAX CABIN AT BS312; 11INCHES BELOW S-4L.<[01] ACCOMPLISHED REPAIR PER EA#M-22-153-01244 REV B;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.

Next page: https://openairdocs.org/aircraft/N208WN/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 = 'N208WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N208WN/reports

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