# Service difficulty reports: N200WN

A list on [N200WN](https://openairdocs.org/aircraft/N200WN.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 7 · 337 reports

- [SDR SWAA2026100237102](https://openairdocs.org/sdr/SWAA2026100237102.md): Fire Warning · illuminated · Sep 28, 2026 · N200WN · Boeing 7377H4 · Central Warning
  > CARGO FIRE DISCH IN FLIGHT. VERIFIED NO LEAKS IN BOTTLE COMPARTMEN. DISCHARGE SWITCH VERIFIED OPEN. IAW WDG 26-23-11. REPLACED CARGO FIRE PANEL IAW AMM 26-00-02. OPS CHECK GOOD.
- [SDR SWAA2026042791649](https://openairdocs.org/sdr/SWAA2026042791649.md): Battery Pack · no test · Apr 22, 2026 · N200WN · Boeing 7377H4 · Emergency Lighting
  > FWD ENTRY LEFT EMERGENCY BATTERY PACK M1675 FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06.
- [SDR SWAA2026042791650](https://openairdocs.org/sdr/SWAA2026042791650.md): Battery Pack · no test · Apr 22, 2026 · N200WN · Boeing 7377H4 · Emergency Lighting
  > AFT LEFT EMERGENCY BATTERY PACK M1673 FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06.
- [SDR SWAA2026042791648](https://openairdocs.org/sdr/SWAA2026042791648.md): Battery Pack · no test · Apr 22, 2026 · N200WN · Boeing 7377H4 · Emergency Lighting
  > AFT RT EMERGENCY BATTERY PACK M1672 FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06.
- [SDR SWAA2026041387852](https://openairdocs.org/sdr/SWAA2026041387852.md): Heads-Up Display · loose · Apr 8, 2026 · N200WN · Boeing 7377H4 · Landing and Taxi Aids
  > HGS COMBINER FELL DOWN ON CAPTS HEAD<[01] FOUND COMBINER TO HAVE A SOFT LATCH.SECURED COMBINER UP WITH ZIP TIE.OK TO CONT ON MEL 34-44-02.SP1 & 1 A C/W.?A/C DOWNGRADED TO CAT I STATUS.?;[02] 01 - REMOVED AND REPLACED PER [AMM 34-36-04-401-NG (HUD COMBINER - RE
- [SDR SWAA2025112638664](https://openairdocs.org/sdr/SWAA2025112638664.md): Bushing · worn · Nov 22, 2025 · N200WN · Boeing 7377H4 · Fuel Controlling System
  > NUMBER 2 ENGINE VERY SLOW TO SPOOL UP BOTH ON TAKEOFF AND ON LANDING WHEN THRUST REV ENGAGE. PERFORMED TEST 8 ACCELERATION CHECK ON NR 2 ENGINE ACCELERATION TIME IS 8.5 SECONDS. OUT OF LIMITS IAW AMM 71-00-00. PERFORMED TASK 71-00-00; TEST ACCELERATION CHEC
- [SDR SWAA2025111234401](https://openairdocs.org/sdr/SWAA2025111234401.md): Engine · abnormal · Nov 8, 2025 · N200WN · Boeing 7377H4 · Engine (Turbine/Turboprop)
  > NR 2 ENGINE GREATELY LAGS #1 ENGINE IN SPOOL UP CAUSING YAW WHEN USING REVERSE IN LANDING. PERFORMED ACCEL CHECK TEST 8 IAW AMM 73-21-00 OPS CHECK GOOD.PERFORMED THRUST LEVER ADJUSTMENT THRUST REVERSER POSITION ADJUSTMENT TEST IAW AMM 73-21-00-700-806-F00.
- [SDR SWAA2025061681776](https://openairdocs.org/sdr/SWAA2025061681776.md): Sign · detached · Jun 14, 2025 · N200WN · Boeing 7377H4 · Emergency Lighting
  > EXIT SIGN MID CABIN FELL OFF. INSTALLED COVER PER AMM CH 33-51-00.
- [SDR SWAA2024121774916](https://openairdocs.org/sdr/SWAA2024121774916.md): Sign · broken · Dec 7, 2024 · N200WN · Boeing 7377H4 · Emergency Lighting
  > AFT LOWERED CEILING EXIT SIGN ASSY BROKEN.<[01] REMOVED AND REPLACED AFT LOWERED CEILING EMERGENCY EXIT SIGN ASSY AS PER B737 AMM 33-51-01-960-802. PERFORMED INSTALLATION TEST OF AFT LOWERED CEILING EMERGENCY EXIT SIGN ASSY AS PER B737 AMM 33-51-01-960-802.;[0
- [SDR SWAA2024121774308](https://openairdocs.org/sdr/SWAA2024121774308.md): Sign · damaged · Dec 5, 2024 · N200WN · Boeing 7377H4 · Emergency Lighting
  > G-1 GALLEY EXIT SIGN DAMAGED.<[01] REMOVED AND REPLACED G-1 GALLEY EXIT SIGN AS PER AMM 33-51-01-960-802.;[02] VERIFIED REMOVED AND REPLACED
- [SDR SWAA2024121773972](https://openairdocs.org/sdr/SWAA2024121773972.md): Scuff Plate · cracked · Dec 4, 2024 · N200WN · Boeing 7377H4 · Cargo Compartments
  > ACCOMPLISH WELD REPAIR OF AFT CARGO DOOR AREA AFT SCUFF PLATE<[01] RECEIVED WELDED AFT SCUFF PLATE OF AFT CARGO REF INSTALLATION TO TASK CARD TTG8Q003DUDR;[02] VERIFIED CONCERN
- [SDR SWAA2024121772279](https://openairdocs.org/sdr/SWAA2024121772279.md): Scuff Plate · cracked · Nov 27, 2024 · N200WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CORNER SCUFF PLATE AT AFT CARGO CRACKED<[01] RECEIVED FWD CORNER SCUFF PLATE AT AFT CARGO REF INSTALLATION TO TASK CARD TTG8Q003DUDR;[02] VERIFIED RECEIVED FWD CORNER SCUFF PLATE AT AFT CARGO REF INSTALLATION TO TASK CARD TTG8Q003DUDR
- [SDR SWAA2024121772280](https://openairdocs.org/sdr/SWAA2024121772280.md): Scuff Plate · cracked · Nov 27, 2024 · N200WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CORNER SCUFF PLATE AT AFT CARGO CRACKED<[01] RECEIVED AFT CORNER SCUFF PLATE AT AFT CARGO REF INSTALLATION TO TASK CARD TTG8Q003DUDR;[02] VERIFIED STEP 1
- [SDR SWAA2024121772281](https://openairdocs.org/sdr/SWAA2024121772281.md): Scuff Plate · cracked · Nov 27, 2024 · N200WN · Boeing 7377H4 · Cargo Compartments
  > AFT CORNER SCUFF PLATE AT FWD CARGO CRACKED<[01] RECEIVED AFT CORNER SCUFF PLATE AT FWD CARGO REF INSTALLATION TO TASK CARD TTG8Q003DUEY;[02] VERIFIED STEP 1
- [SDR SWAA2024121769906](https://openairdocs.org/sdr/SWAA2024121769906.md): Galley · corroded · Nov 20, 2024 · N200WN · Boeing 7377H4 · Buffet/Galleys
  > G-4 GALLEY COUNTERTOP HAS CORROSION.<[01] PART TRANSACTION ONLY; G-4 GALLEY INSTALLATION REF TASK CARD FOR JOB ACCOMPLISHMENT TTG8Q003E0PW;[02] VERIFIED PART TRANSACTION
- [SDR SWAA2024121760342](https://openairdocs.org/sdr/SWAA2024121760342.md): Fairing · elongated · Nov 15, 2024 · N200WN · Boeing 7377H4 · Aerodynamic Fairings
  > FUSELAGE CENTER LOWER AFT FAIRING 194E HAS SEVERAL OVERSIZED AND ELONGATED HOLES.<[01] INSTALLED A PERMANENT REPAIR TO DAMAGE FASTENERS HOLES AS MARKED ON LOWER AFT FAIRING #194E AS PER B737 SRM 51-70-04-2R-9 PARAG. 4 D-N AND SRM 51-70-04-2R-0 4 L-N MATERIALS
- [SDR SWAA2024121759717](https://openairdocs.org/sdr/SWAA2024121759717.md): Structure · elongated · Nov 13, 2024 · N200WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CABIN WET AREA R-2 DOOR LOWER SILL INNER SUPPORT O/B HAS 3EA ELONGATED HOLES MKD DOTS<[01] SUMMARY=INSTALLED EWIS PROTECTION DURING MAINTENANCE AS PER REF B/737 AMM 20-60-07-913-801.<BR>REMOVED AFT CABIN WET AREA R-2 DOOR LOWER SILL INNER CHORD AS PER B-73
- [SDR SWAA2024121759705](https://openairdocs.org/sdr/SWAA2024121759705.md): Support · cracked · Nov 13, 2024 · N200WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > MAIN CABIN CENTER SECTION FLOOR SUPPORT BREAK CRACKED @ FWD FACE STA 540 LBL-1<[01] REMOVED AND REPLACED FLOOR SUPPORT BREAK AT MAIN CABIN CENTER SECTION STA 540 LBL-1REF B737 SRM 51-40-02-0G-0; AIPC 53-42-11-66;[02] RII- VERIFIED REPLACED
- [SDR SWAA2024121759706](https://openairdocs.org/sdr/SWAA2024121759706.md): Support · cracked · Nov 13, 2024 · N200WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > MAIN CABIN CENTER SECTION FLOOR SUPPORT BREAK CRACKED @ FWD FACE STA 540 RBL-1 MKD DOT<[01] REMOVED AND REPLACED FLOOR SUPPORT BREAK AT MAIN CABIN CENTER SECTION STA 540 RBL-1 IAW B/737 SRM 51-40-02-0G-0.<BR><BR>MIXED SEALANT 0870B002 AT 12:00 PM ON 11/20/2024
- [SDR SWAA2024121759025](https://openairdocs.org/sdr/SWAA2024121759025.md): Scuff Plate · cracked · Nov 12, 2024 · N200WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CABIN GALLEY R-1 DOOR FUS CUTOUT LOWER SILL SCUFF PLATE EDGE CRACKED 2EA PLACES<[01] SUMMARY=LOCATED DRILLED AND COUNTERSANK NEW SCUFF PLATE AS PER B 737 SRM 51-40-05-0G-0 & SRM 51-40-08-0G-0. (SCUFF PLATE TO BE INSTALLED ON ITEMTTG8Q003E01N);[02] CORRECTI
- [SDR SWAA2024121759026](https://openairdocs.org/sdr/SWAA2024121759026.md): Support Angle · corroded · Nov 12, 2024 · N200WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CABIN R-1 DOOR CUTOUT LOWER SILL SCUFF PLATE SUPPORT ANGLE FWD SPOTS SURFACE CORR MKD DOTS<[01] REMOVED CORROSION AT FWD CABIN R-1 DOOR CUTOUT LOWER SILL SCUFF PLATE SUPPORT ANGLE AS PER SRM 51-10-02-0G-0. ORIGINAL METERIAL 0.090' MATERIAL LOST 0.027' MATE
- [SDR SWAA2024121758500](https://openairdocs.org/sdr/SWAA2024121758500.md): Stringer · cracked · Nov 11, 2024 · N200WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > FWD MAIN CABIN WET AREA SIDEWALL S-16L CRACKED BETWEEN STA 294 & 303.9<[01] ACCOMPLISHED REPAIR PER EA 24-153-03228 REF: TTG8Q00X5QPQ<BR>& TTG8Q00XDWZU;[02] VERIFIED REPAIR
- [SDR SWAA2024121758752](https://openairdocs.org/sdr/SWAA2024121758752.md): Stiffener · cracked · Nov 11, 2024 · N200WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > STIFFENER CRACKED AT STA 663; RBL 25; WL 148<[01] SUMMARY:REMOVED AND REPLACED NEW STIFFENER ON STA 663;RBL 25 WL 148 AS PER B/737 SRM 51-40-02-0G-0 AND DW 111A1000;;[02] VERIFIED STEP#1.
- [SDR SWAA2024121758750](https://openairdocs.org/sdr/SWAA2024121758750.md): Guide Arm · corroded · Nov 11, 2024 · N200WN · Boeing 7377H4 · Galley Doors
  > R1 DOOR GUIDE ARM CORRODED<[01] REMOVED AND REPLACED R1 DOOR GUIDE ARM PER B737 AMM 52-41-21-400-801-NG FINAL INSTALLATION AND ADJUSTMENT REF TTG8Q00X0R56<BR>TORQUE WRENCH B/C 175286 CAL DUE DATE 07-02-2025;[02] VERIFIED STEP 1
- [SDR SWAA2024101447698](https://openairdocs.org/sdr/SWAA2024101447698.md): Transmitter · faulty · Oct 12, 2024 · N200WN · Boeing 7377H4 · Trailing Flap Position Indicating System
  > FLAPS WOULD NOT EXTEND PAST 5 WITH 15 SELECTED. FLAPS MOVED TO 15 MANUALLY NO NEEDLE SPLIT NOTED<[01] TROUBLESHOT PER FIM 27-51 TASK 801 & 820; FSEU BITE SHOWS MSG # 27-52260; TE FLAP SNSR R. R & R?D RT FLAP POSITION TRANSMITTER & FLAP POSITION INDICATOR PER
- [SDR SWAA2024080221719](https://openairdocs.org/sdr/SWAA2024080221719.md): Slide · out of adjust · Aug 1, 2024 · N200WN · Boeing 7377H4 · Escape Slide
  > AFT SLIDE CAPT SIDE NOT PACKED CORRECTLY REF: BAR CODE ID TTG8Q00UYJU5<[01] RE-PACKED CAPTAINS SIDE AFT ESCAPE SLIDE IAW MT 725-61-06.
- [SDR SWAA2024080221387](https://openairdocs.org/sdr/SWAA2024080221387.md): Slide · out of adjust · Aug 1, 2024 · N200WN · Boeing 7377H4 · Escape Slide
  > AFT SLIDE CAPT SIDE NOT PACKED CORRECTLY<[01] RE-PACKED CAPTAINS SIDE AFT ESCAPE SLIDE IAW AMM 25-66-01. OK FOR SERVICE.
- [SDR SWAA2024072516672](https://openairdocs.org/sdr/SWAA2024072516672.md): Seat · out of adjust · Jul 24, 2024 · N200WN · Boeing 7377H4 · Passenger Compartment Equipment
  > CAPTAINS SIDE EXIT ROW 12A SEAT STAYS RECLINED.<[01] ADJUSTED PAX SEAT IN 12A PER MM 25-22-00 OPS CHECK GOOD;[02] FAULT RAISED IN ERROR.
- [SDR SWAA2024072214652](https://openairdocs.org/sdr/SWAA2024072214652.md): Bottle · out of limits · Jul 19, 2024 · N200WN · Boeing 7377H4 · Escape Slide
  > LEFT FWD DOOR ESCAPE SLIDE PRESSURE OUT OF LIMITS<[01] 01 - REMOVED AND REPLACED FORWARD ENTRY ESCAPE SLIDE PER [AMM 25-66-01-401-NG (DOOR-MOUNTED ESCAPE SYSTEM - REMOVAL/INSTALLATION - PERMANENT)] REF MT 725-61-06.
- [SDR SWAA2024061902297](https://openairdocs.org/sdr/SWAA2024061902297.md): Fire Loop · inoperative · Jun 16, 2024 · N200WN · Boeing 7377H4 · Fire Detection
  > #1 ENG B FIRE LOOP INOP #1 ENG B FIRE LOOP INOP 16-JUN-2024 06:50 UTC R&R ENGINE AND APU FIRE DETECTION MODULE IAW AMM 25-10-01 OPS CHECK GOOD.<[01] COULD NOT DUPLICATE FAULT ON GROUND; FOUND ENGINE AND APU FIRE CONTROL MODULE WITH MULTIPLE TEST LIGHTS INOP. R
- [SDR SWAA2024022957306](https://openairdocs.org/sdr/SWAA2024022957306.md): Charger · inoperative · Feb 29, 2024 · N200WN · Boeing 7377H4 · Emergency Lighting
  > R/H EMERGENCY EXIT HATCH ( EXIT) LIGHT INOP<[01] REPLACED BATTERY CHARGER AND EXIT SIGN ASSY PER AMM 33-51-01
- [SDR SWAA2023080885865](https://openairdocs.org/sdr/SWAA2023080885865.md): Girt Bar · out of adjust · Aug 4, 2023 · N200WN · Boeing 7377H4 · Emergency Equipment
  > R-1 SLIDE PACK GRIT BAR RIGHT. CLIP LOOSE<[01] ADJUSTED R1 SLIDE GRIT BAR RH CLIP PER AMM SIP. NO FURTHER DEFECTS NOTED AT THIS TIME
- [SDR SWAA2023071778010](https://openairdocs.org/sdr/SWAA2023071778010.md): Light · inoperative · Jul 13, 2023 · N200WN · Boeing 7377H4 · Emergency Lighting
  > PASSENGER CABIN: RIGHT OVER WING EXIT; LIGHT IS INOPERABLE. PASSENGER CABIN: RIGHT OVER WING EXIT LIGHT IS INOPERABLE.<[01] RELAMPED EXIT LIGHT PER AMM 33-51-01;[02] C/W INSPECTION PER AMM 33-51-01.
- [SDR SWAA2023071778019](https://openairdocs.org/sdr/SWAA2023071778019.md): Light · delaminated · Jul 13, 2023 · N200WN · Boeing 7377H4 · Emergency Lighting
  > PASSENGER CABIN: SECTION OF PHOTO ILLUMINATED STRIP IS DELAMINATED NEXT TO THE AFT RIGHT WINDSCREEN.<[01] REMOVED AND REPLACED PHOTO STRIP PER AMM 33-51-15;[02] C/W INSPECTION PER AMM 33-51-15.
- [SDR SWAA2023041124818](https://openairdocs.org/sdr/SWAA2023041124818.md): Slide · out of adjust · Apr 7, 2023 · N200WN · Boeing 7377H4 · Escape Slide
  > L2 SLIDE OUTSIDE OF CONTAINER<[01] RESECURED SLIDE CONTAINER COVER IAW AMM 25-66-01
- [SDR SWAA2022113076721](https://openairdocs.org/sdr/SWAA2022113076721.md): Power Supply · inoperative · Nov 30, 2022 · N200WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHT AFT OF LEFT WING INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY IAW AMM 33-51-06. OPS CHECKED GOOD.
- [SDR SWAA2022112173210](https://openairdocs.org/sdr/SWAA2022112173210.md): Lamp · inoperative · Nov 19, 2022 · N200WN · Boeing 7377H4 · Emergency Lighting
  > BURNED EMERGENCY LIGHT EXTERNAL AFT LT 2022-585774 / [01] REPLACED LAMP ON EMERGENCY LIGHT EXTERNAL AFT LT IAW B737-700 AMM 33-51-04-960-801 TEST OK.;[02] REPLACED LAMP ON EMERGENCY LIGHT EXTERNAL AFT LT IAW B737-700 AMM 33-51-04-960-801 TEST OK.
- [SDR SWAA2022112273209](https://openairdocs.org/sdr/SWAA2022112273209.md): Lamp · burned out · Nov 18, 2022 · N200WN · Boeing 7377H4 · Emergency Lighting
  > BURNED OUT LIGHT EMERGENCY AFT RT OVER GALLEY. REPLACED THE LAMPS IAW AMM 33-51-01-960-801.
- [SDR SWAA2022112264981](https://openairdocs.org/sdr/SWAA2022112264981.md): Beam · cracked · Oct 27, 2022 · N200WN · Boeing 7377H4 · Wing Main, Frame Structure
  > FOUND 2 E/A CRACK O N INTERNAL BEAM 2022-585731 / [01] REMOVED AND REPLACED SLAT 7 DUE TO 2 E/A CRACK FOUND ON INTERNAL BEAM IAW B737-700 AMM 27-81-21-000-801 AND 27-81-21-40-801; AND PERFORMED LEADING EDGE SLAT ADJUSTMENT IAW B737-700 AMM 27-81-00-820-803.
- [SDR SWAA2022112264432](https://openairdocs.org/sdr/SWAA2022112264432.md): Floor Support · cracked · Oct 25, 2022 · N200WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS344 TO BS360 LBL12 WL 208.1 FWD GALLEY AND LAV. REPLACED FLOOR SUPPORT IAW SRM 51-40-02 AND DWG 141A5400 REV A.
- [SDR SWAA2022112163655](https://openairdocs.org/sdr/SWAA2022112163655.md): Plate · corroded · Oct 24, 2022 · N200WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON PLATE LOCATED BETWEEN BS 787 AND BS 807 S- 25R AND WL 156 AFT CARGO COMPARTMENT 2022-585714 / [01] REPLACED PLATE LOCATED BETWEEN BS 787 AND BS 807 S- 25R AND WL 156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 STEP 9;[02] JOB COMPLETED.
- [SDR SWAA2022112263650](https://openairdocs.org/sdr/SWAA2022112263650.md): Support Angle · corroded · Oct 23, 2022 · N200WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ANGLE, BS 847, LBL 19, AFT CARGO COMPARTMENT. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02 ITEM 9, AND 51-40-02.
- [SDR SWAA2022112263651](https://openairdocs.org/sdr/SWAA2022112263651.md): Support Angle · corroded · Oct 23, 2022 · N200WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORRODED SUPPORT ANGLE, BS 867, LBL 10, AFT CARGO COMPARTMENT. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, AND 51-40-02.
- [SDR SWAA2022112263322](https://openairdocs.org/sdr/SWAA2022112263322.md): Floorbeam · corroded · Oct 22, 2022 · N200WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION FLOORBEAM, BS 986.5, RBL 39.5, WL 208.1.
- [SDR SWAA2022112263323](https://openairdocs.org/sdr/SWAA2022112263323.md): Floorbeam · corroded · Oct 22, 2022 · N200WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION FLOORBEAM, BS 986.5, RBL 35.5, WL 208.1.
- [SDR SWAA2022112263326](https://openairdocs.org/sdr/SWAA2022112263326.md): Floorbeam · corroded · Oct 22, 2022 · N200WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION FLOORBEAM, BS 986.5, LBL38, WL 208.1.
- [SDR SWAA2022112263324](https://openairdocs.org/sdr/SWAA2022112263324.md): Floorbeam · corroded · Oct 22, 2022 · N200WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION FLOORBEAM, BS 986.5, LBL 41, WL 208.1. REPAIRED IAW EA 22-153-03296-WIP1 AND EA 22-153-03296.
- [SDR SWAA2022112263321](https://openairdocs.org/sdr/SWAA2022112263321.md): Floorbeam · corroded · Oct 22, 2022 · N200WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION FLOORBEAM, BS 986.5, RBL 43, WL 208.1. REPAIRED IAW EA 22-153-03281 WIP1 AND EA 22-153-03281.
- [SDR SWAA2022112263325](https://openairdocs.org/sdr/SWAA2022112263325.md): Floorbeam · corroded · Oct 22, 2022 · N200WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORRODED FLOORBEAM BS 312 RBL20 WL208.1.
- [SDR SWAA2022112262957](https://openairdocs.org/sdr/SWAA2022112262957.md): Stub Frame · cracked · Oct 21, 2022 · N200WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACKED STUB FRAME LOCATED BS294.5 RBL55 WL209. REPLACED THE STUB FRAME IAW SRM 51-10-02 ITEM 9 AND DWG-141A8370 REV D.

Next page: https://openairdocs.org/aircraft/N200WN/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 = 'N200WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N200WN/reports

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