# Service difficulty reports: N438SW

A list on [N438SW](https://openairdocs.org/aircraft/N438SW.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 3 · 145 reports

- [SDR SWIA202264770](https://openairdocs.org/sdr/SWIA202264770.md): None · cracked · Mar 1, 2022 · N438SW · Cndair CL6002B19 · Fuselage, Equipment Attach Fittings
  > PAX DOOR ANGLE, NEAR DOOR HINGE HAS A CRACK. MARKED. (FILED CLOSED) REPLACED PAX DOOR UPPER ANGLE NEAR DOOR HINGE IN REFERENCE TO CRJ 200 SRM 51-42-06
- [SDR SWIA202157732](https://openairdocs.org/sdr/SWIA202157732.md): Skin · dented · Apr 18, 2021 · N438SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RH INBOARD FLAP LOWER SKIN HAS DENT APPROX. 6" INBOARD OF INBOARD EDGE AND 2" FWD OF TRAILING EDGE. (FILED CLOSED)COMPLIED WITH PERMANENT REPAIR OF THE RH INBOARD FLAP LOWER SKIN 6" INBOARD OF THE INBOARD EDGE AND 2" FWD OF THE TRAILING EDGE IN REFERENCE T
- [SDR SWIA202157729](https://openairdocs.org/sdr/SWIA202157729.md): Intercostal · cracked · Apr 18, 2021 · N438SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FRAME 621.00 INTERCOSTAL CONNECTING TO Z-MEMBER AT STR 14R CRACKED. (CRJ-200 SRM 53-61-17 ITEM #50) (FILED CLOSED) REMOVED AND REPLACED FRAME 621.00 INTERCOSTAL CONNECTING TO Z-MEMBER AT STR 14R IN REF TO SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1
- [SDR SWIA202157728](https://openairdocs.org/sdr/SWIA202157728.md): Skin · dented · Apr 18, 2021 · N438SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RH INBOARD FLAP HAS DENT ON LOWER SKIN APPROX. 12" FROM TRAILING EDGE AND 27" FROM INBOARD EDGE. (FILED CLOSED) COMPLIED WITH THE PERMANENT REPAIR OF THE RH INBOARD FLAP LOWER SKIN APPROX 12" FROM THE TRAILING EDGE AND 27" FROM THE INBOARD EDGE IN RE
- [SDR SWIA202157733](https://openairdocs.org/sdr/SWIA202157733.md): Bracket · cracked · Apr 16, 2021 · N438SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CARGO COMPARTMENT NET PAN FITTING BRACKET AT FS605.00 AND LBL 38.40 IS CRACKED. (FILED CLOSED) REMOVED AND REPLACED CARGO COMPARTMENT NET PAN FITTING BRACKET AT FS605.00 AND LBL 38.40 IN REF TO SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY. COM
- [SDR SWIA202157731](https://openairdocs.org/sdr/SWIA202157731.md): Floor Support · corroded · Apr 16, 2021 · N438SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO COMPARTMENT FLOOR LANDING PLATE HAS SEVERAL AREAS OF CORROSION ALONG TOP SURFACE. (FILED CLOSED) REMOVED AND REPLACED CARGO COMPARTMENT FLOOR LANDING PLATE IN REF TO SRM 51-42-06 AND 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLETED M-
- [SDR SWIA202157730](https://openairdocs.org/sdr/SWIA202157730.md): Fairing · chafed · Apr 16, 2021 · N438SW · Cndair CL6002B19 · Nacelle/Pylon, Main Frame
  > CHAFE DAMAGE BETWEEN L/H PYLON TRAILING EDGE FAIRING AND FUSELAGE AT FS 736.00. (FILED CLOSED) REPAIRED CHAFE DAMAGE TO LH FUSELAGE SKIN BETWEEN FS700.00 - FS755.00 AND STR9R - STR12R PER REO 601R-53-61-268, REV A, DATED 2000-07-11. COMPLIED WITH TASK
- [SDR SWIA202005150728](https://openairdocs.org/sdr/SWIA202005150728.md): Door · open · May 14, 2020 · N438SW · Cndair CL6002B19 · Service Doors
  > EXTREMELY LOUD NOISE AFTER TAKEOFF WITH STALL FAIL CAUTION MESSAGE FLIGHT 4291 - FILED OPEN PLEASE REFERENCE AML 430131. FOUND THE OXY DOOR OPEN WHEN THE AIRCRAFT TAXIED BACK TO THE GATE. DUE TO THE DISRUPTION OF THE AIR FLOW FROM THE OXY DOOR. PERFORMED S
- [SDR SWIA2019092746360](https://openairdocs.org/sdr/SWIA2019092746360.md): Angle · damaged · Sep 10, 2019 · N438SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > REPAIR LH BULKHEAD ANGLE @ F 202 BETWEEN LBL 13.73 -LBL 22.00 9C-CHECK) RO: 06/26/2019 PERFORMED REPAIR TO LH BULKHEAD ANGLE @ F 202 BETWEEN LBL 13.73 -LBL 22.00 IAW REO. LEAK CHECK GOOD,
- [SDR SWIA2019092746359](https://openairdocs.org/sdr/SWIA2019092746359.md): Structure · damaged · Aug 10, 2019 · N438SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PILOTS FLOOR AND NOSE COMPARTMENT FLOOR DAMAGED BETWEEN FS.169.00 - FS.220.00 LHS (C-CHECK) RO: 09/26/2019 PERFORMED REPAIR OF PILOTS FLOOR AND NOSE COMPARTMENT FLOOR BETWEEN FS.169.00 - FS.220.00 LHS IAW SRM.
- [SDR SWIA2019092746358](https://openairdocs.org/sdr/SWIA2019092746358.md): Skin Panel · damaged · Aug 10, 2019 · N438SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DAMAGED SKIN PANEL P/N 601R-33010-107 BETWEEN FS.193.00 - FS.210.00 LHS (C-CHECK) RO: 09/26/2019 REPLACED SKIN PN 601R-33010-107 BETWEEN FS193.00-FS210 LHS IAW SRM. LEAK CHECK GOOD.
- [SDR SWIA2019092746370](https://openairdocs.org/sdr/SWIA2019092746370.md): Frame · corroded · May 30, 2019 · N438SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 605.0 FRAME FWD SIDE FROM 22L TO 25R HAS CORROSION (C-CHECK) RO: 09/26/2019 REMOVED CORROSION ON FS 605.0 FRAME FWD SIDE FROM 22L TO 25R, INSTALLED NEW FRAME AT FS605 FROM STGR20L-STGR20R IAW SRM. LEAK CHECK GOOD.
- [SDR SWIA2019092746357](https://openairdocs.org/sdr/SWIA2019092746357.md): Panel · corroded · May 30, 2019 · N438SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT HAND PRESSURE FLOOR SILL PANEL FROM APPROXIMATELY FS429.0 TO FS559.0 HAS SEVERAL SPOTS OF CORROSION. (C-CHECK) RO: 09/26/2019 REMOVED CORROSION FROM THE RIGHT HAND FLOOR SILL PANEL FROM APROX FS429.0 TO FS559.0 IAW REO. LEAK CHECK GOOD.
- [SDR SWIA201946356](https://openairdocs.org/sdr/SWIA201946356.md): Panel · corroded · May 30, 2019 · N438SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT HAND PRESSURE FLOOR SILL PANEL FROM APPROXIMATELY FS 409.0+133 TO FS559.0 HAS SEVERAL SPOTS OF CORROSION. (C-CHECK) RO: 09/26/2019 BLENDED OUT CORROSION ON LEFT HAND PRESSURE FLOOR SILL PANEL FROM APPROXIMATELY FS 409.0+133 TO FS559.0 IAW REO. LEAK CHECK
- [SDR SWIA2019092746369](https://openairdocs.org/sdr/SWIA2019092746369.md): Vane · gouged · May 29, 2019 · N438SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBOARD FLAP. CENTER OUTBOARD VANE CAP GOUGED. (C-CHECK) RO: 09/26/2019 REMOVED AND REPLACED THE LH INBD FLAP CENTER OTBD VANE CAP WITH NEW PART IAW SRM.
- [SDR SWIA2019092746368](https://openairdocs.org/sdr/SWIA2019092746368.md): Channel · corroded · May 28, 2019 · N438SW · Cndair CL6002B19 · Wing Miscellaneous Structure
  > R/H MLG WHEEL WELL WS 53.60 BATT CHANNEL HAS CORROSION AROUND CANNON PLUGS (C-CHECK) RO: 09/26/2019 REMOVED AND REPLACED R/H BATT RIB ANGLE WS 53.60 WITH NEW PART IAW SRM.
- [SDR SWIA2019092746355](https://openairdocs.org/sdr/SWIA2019092746355.md): Channel · corroded · May 28, 2019 · N438SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > L/H MLG WHEEL WELL WS 53.60 BATT CHANNEL HAS CORROSION AROUND CANNON PLUGS (C-CHECK) RO: 09/26/2019 REPLACED CORRODED ANGLE WITH NEW ANGLE P/N 601R10203 -33 IAW SRM.
- [SDR SWIA2019092746354](https://openairdocs.org/sdr/SWIA2019092746354.md): Channel · cracked · May 28, 2019 · N438SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > L/H MLG WHEEL WELL WS 53.60 BATT CHANNEL CRACKED (C-CHECK) RO: 09/26/2019 REMOVED AND REPLACED L/H MLG WHEEL WELL WS 53.60 BATT CHANNEL IAW SRM. LEAK CHECK GOOD.
- [SDR SWIA2019092746367](https://openairdocs.org/sdr/SWIA2019092746367.md): Access Panel · chafed · May 24, 2019 · N438SW · Cndair CL6002B19 · Wing, Plate/Skin
  > THE LH WING UPPER SKIN ACCESS PANEL 540AT'S NUTPLATE RING/CHANNEL IS CHAFED AT MULTIPLE AREAS OF ITS UPPER SURFACE. (C-CHECK) RO: 09/26/2019 BLENDED OUT CHAFEF MARKS ON LH WING UPPER SKIN ACCESS PANEL 540AT RING/CHANNEL IAW REO.
- [SDR SWIA2019092746366](https://openairdocs.org/sdr/SWIA2019092746366.md): Skin · chafed · May 24, 2019 · N438SW · Cndair CL6002B19 · Trailing Edge Flaps
  > THE RH INBOARD FLAP VANE'S SKIN HAS 3 CHAFES ALONG THE LEADING EDGE, AND 3 CHAFES ALONG THE TRAILING EDGE UPPER SURFACE. (C-CHECK) RO: 09/26/2019 BLENDED THE RH INBD FLAP VANE LEADING EDGE SKIN AT 3 LOCATIONS IAW REO, AND THE TRAILING EDGE AT 2 LOCATIONS IAW S
- [SDR SWIA2019092746365](https://openairdocs.org/sdr/SWIA2019092746365.md): Skin · chafed · May 24, 2019 · N438SW · Cndair CL6002B19 · Trailing Edge Flaps
  > THE LH INBOARD FLAP VANE'S SKIN HAS 3 CHAFES ALONG THE LEADING EDGE, AND 2 CHAFES ALONG THE TRAILING EDGE UPPER SURFACE. (C-CHECK) RO: 09/26/2019 BLENDED THE LH INBD FLAP VANE LEADING EDGE SKIN AT 3 LOCATIONS IAW REO, AND THE TRAILING EDGE AT 2 LOCATIONS IAW S
- [SDR SWIA2019092746353](https://openairdocs.org/sdr/SWIA2019092746353.md): Angle · cracked · May 24, 2019 · N438SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT HAND BATT RIB ANGLE CRACKED. (C-CHECK) RO: 09/26/2019 REMOVED AND REPLACED LH BATT RIB ANGLE IAW SRM.
- [SDR SWIA2019092746364](https://openairdocs.org/sdr/SWIA2019092746364.md): Skin · chafed · May 23, 2019 · N438SW · Cndair CL6002B19 · Ailerons
  > L/H AILERON UPPER LEADING EDGE SKIN IS CHAFFED ALL THE WAY ACROSS (C-CHECK) RO: 09/26/2019 BLENDED L/H AILERON UPPER LEADING EDGE SKIN. REPLACED WITH NEW PART, PART NUMBER 601R13031-165 IAW REO AND SRM.
- [SDR SWIA2019092746363](https://openairdocs.org/sdr/SWIA2019092746363.md): Plate · corroded · May 23, 2019 · N438SW · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR PROTECTOR PLATE IS CORRODED AROUND THE FASTENER HOLES (C-CHECK) RO: 09/26/2019 REPLACED SERVICE DOOR PROTECTOR PLATE WITH NEW PART FROM STORES P/N: 601R38957-31 P/O: T-48438 IAW SRM.
- [SDR SWIA2017120543932](https://openairdocs.org/sdr/SWIA2017120543932.md): Duct · failed · Oct 29, 2017 · N438SW · Cndair CL6002B19 · Air Distribution System
  > CABIN ALTITUDE CAUTION. RIGHT PACK OVER PRESSURE. EMERGENCY DECLARED. EMERGENCY DESCENT. O2 MASKS DEPLOYED. (FLT 4883) REMOVED AND REPLACED RT AC UPPER SUPPLY DUCT ASSY IAW AMM. OPS CHECK GOOD.
- [SDR SWIA201743319](https://openairdocs.org/sdr/SWIA201743319.md): Fitting · corroded · Apr 29, 2017 · N438SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > BS 349 FLOORBEAM FITTING HAS CORROSION AT RBL 42. INSTALLED A NEW FITTING IAW REO.
- [SDR SWIA201743318](https://openairdocs.org/sdr/SWIA201743318.md): Floorbeam · corroded · Apr 26, 2017 · N438SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > BS 589 FLOORBEAM HAS CORROSION BETWEEN LBL 27 - RBL 36. REPLACED THE THREE CAP STRAPS IAW SRM.
- [SDR SWIA201743317](https://openairdocs.org/sdr/SWIA201743317.md): Fairing · chafed · Apr 25, 2017 · N438SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT FLAP STUB FAIRING CHAFED. REMOVED THE STUB FAIRING AND REPLACED WITH NEW, IAW AMM.
- [SDR SWIA201743316](https://openairdocs.org/sdr/SWIA201743316.md): Seal · torn · Apr 24, 2017 · N438SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP INBD SEAL TORN. REPLACED IAW SRM.
- [SDR SWIA201743315](https://openairdocs.org/sdr/SWIA201743315.md): Panel · chafed · Apr 24, 2017 · N438SW · Cndair CL6002B19 · Ailerons
  > LEFT AILERON LOWER SKIN LEADING EDGE SHROUDS HAVE CHAFE DAMAGE. REMOVED AND REPLACEED THE FIXED PANELS IAW SRM.
- [SDR SWIA201743314](https://openairdocs.org/sdr/SWIA201743314.md): Panel · chafed · Apr 24, 2017 · N438SW · Cndair CL6002B19 · Wing Main, Frame Structure
  > PANEL 699CB CHAFED. INSTALLED A REPLACEMENT PANEL IAW REO AND SRM.
- [SDR SWIA201743313](https://openairdocs.org/sdr/SWIA201743313.md): Intercostal · corroded · Apr 24, 2017 · N438SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL AT DD4 BETWEEN BS 320 AND 338 CORRODED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM.
- [SDR SWIA201743312](https://openairdocs.org/sdr/SWIA201743312.md): Plate · corroded · Apr 23, 2017 · N438SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR FLOOR PLATE IS CORRODED. REPLACED THE PLATE IAW SRM.
- [SDR SWIA201541204](https://openairdocs.org/sdr/SWIA201541204.md): Floor Skin · cracked · May 5, 2015 · N438SW · Cndair CL6002B19 · Fuselage Floor Panel
  > PRESSURE FLOOR SKIN AT FS 456 BETWEEN BL0 AND LBL9 CRACKED. INSTALLED REPAIR PARTS 601R-53-41-1898-5, 601R-53-41-1898-6, 601R-53-41-1898-7, 601R-53-41-1898-8 JUST FWD OF FS460 AT FS456 IAW REO.
- [SDR SWIA201541191](https://openairdocs.org/sdr/SWIA201541191.md): Floor Panel · damaged · May 5, 2015 · N438SW · Cndair CL6002B19 · Fuselage Floor Panel
  > DOUBLER COMMON TO PRESSURE FLOOR WEB BETWEEN RBL 27.5 AND RBL 36 AT BS 47. INSTALLED 601R-53-41-1905-1, 601R-53-41-1905-2, 601R-53-41-1905-3, 601R-53-41-19054-4 DOUBLERS AND SHIM COMMON TO PRESSURE FLOOR WEB BETWEEN RBL27.5 AND RBL36.0 AT FS 478.00, IAW REO.
- [SDR SWIA201541198](https://openairdocs.org/sdr/SWIA201541198.md): Frame · damaged · May 3, 2015 · N438SW · Cndair CL6002B19 · Fuselage Main, Frame
  > LOWER FRAME SECTOR AT BS 333 BETWEEN S23L - 23R DAMAGED. INSTALLED NEW LOWER FRAME SECTOR ASSY IAW SRM.
- [SDR SWIA201541193](https://openairdocs.org/sdr/SWIA201541193.md): Floorbeam · corroded · May 1, 2015 · N438SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION ON TOP SURFACE OF FS 280 BEAM FROM RBL 9 TO LBL 9. R & R SPLICED SECTION, PN 600-34017-595 OF FS280 BEAM FROM RBL 9 TO LBL 9 IAW SRM.
- [SDR SWIA201541207](https://openairdocs.org/sdr/SWIA201541207.md): Stiffener · cracked · Apr 30, 2015 · N438SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > VERTICAL POST AT FS 409+128, RBL 27 INBD SIDE IS CRACKED IN LOWER RADUIS. REMOVED AND INSTALLED NEW INBD VERT POST AT FS 409.+128 RBL 27 IAW SRM AND STS EA.
- [SDR SWIA201541206](https://openairdocs.org/sdr/SWIA201541206.md): Stiffener · cracked · Apr 30, 2015 · N438SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > VERTICAL POST AT FS 409+128, LBL 27 OTBD SIDE IS CRACKED IN LOWER RADIUS. REMOVED AND INSTALLED NEW VERTICAL POST AT FS 409+128, LBL 27 OTBD IAW STS EA.
- [SDR SWIA201541205](https://openairdocs.org/sdr/SWIA201541205.md): Stiffener · cracked · Apr 30, 2015 · N438SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > VERTICAL POST AT 409+128, LBL 27 INBD SIDE IS CRACKED IN LOWER RADIUS. REMOVED AND INSTALLED NEW INBD VERTICAL POST AT FS 409 +128 LBL 27 IAW SRM.
- [SDR SWIA201541190](https://openairdocs.org/sdr/SWIA201541190.md): Skin · gouged · Apr 29, 2015 · N438SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN GOUGED AND DENTED AT BS 684 BETWEEN STR 8 - 9R. REPAIRED DAMAGED SKIN, CUT-OUT AND COLD WORKED DAMAGED FUSELAGE, NDT REPAIR AREA NO DEFECTS NOTED, INSTALLED REPAIR DOUBLER, RESTORED FINISH IAW STS EA.
- [SDR SWIA201541192](https://openairdocs.org/sdr/SWIA201541192.md): Angle · corroded · Apr 28, 2015 · N438SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT SPLICE ANGLE AT BS 364 BETWEEN S25L - 25R IS CORRODED. C-CHECK, REPLACED AFT SPLICE ANGLE AT FS 364, STR 25L TO STR 25R IAW REO.
- [SDR SWIA201541203](https://openairdocs.org/sdr/SWIA201541203.md): Floor Support · cracked · Apr 27, 2015 · N438SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CRACK IN AFT CARGO DOOR FLOOR SILL PLATE. R & R CARGO FLOOR SILL IAW SRM.
- [SDR SWIA201541200](https://openairdocs.org/sdr/SWIA201541200.md): Floor Skin · cracked · Apr 27, 2015 · N438SW · Cndair CL6002B19 · Fuselage Floor Panel
  > PRESSURE FLOOR SKIN CRACKED AT BS 456 BETWEEN BL 0 AND RBL 9. INSTALLED REPAIR IAW REO.
- [SDR SWIA201541201](https://openairdocs.org/sdr/SWIA201541201.md): Door Frame · cracked · Apr 26, 2015 · N438SW · Cndair CL6002B19 · Fuselage Main, Structure
  > RIGHT FORWARD AVIONICS BAY LANDING CRACKED AT FS 193 FRAME. REPAIRED RT FORWARD AVIONICS BAY LANDING CRACK AT FS 193, FRAME IAW REO.
- [SDR SWIA201541208](https://openairdocs.org/sdr/SWIA201541208.md): Vane · chafed · Apr 25, 2015 · N438SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RT INBD FLAP VANE CHAFED L/E MIDDLE. INSTALLED NEW RT INBD FLAP VANE MIDDLE L/E IAW SRM.
- [SDR SWIA201541202](https://openairdocs.org/sdr/SWIA201541202.md): Vane · chafed · Apr 25, 2015 · N438SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBD FLAP VANE CHAFED L/E OTBD. R & R RT INBD FLAP VANE OTBD L/E PANEL 601R14303-44 IAW SRM.
- [SDR SWIA201541199](https://openairdocs.org/sdr/SWIA201541199.md): Support Bracket · cracked · Apr 25, 2015 · N438SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR HAS HANDLE MOUNTING ASSEMBLY SUPPORT BRACKET CRACK. REMOVED AND INSTALLED NEW SUPPORT BRACKET FOR PASSENGER DOOR MOUNTING HANDLE IAW SRM AND REO.
- [SDR SWIA201541197](https://openairdocs.org/sdr/SWIA201541197.md): Vane · chafed · Apr 25, 2015 · N438SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP VANE CHAFED L/E OTBD. INSTALLED NEW LT INBD FLAP VANE OTBD L/E PANEL IAW SRM.
- [SDR SWIA201541196](https://openairdocs.org/sdr/SWIA201541196.md): Vane · chafed · Apr 25, 2015 · N438SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP VANE CHAFED L/E MIDDLE. REPLACED LT INBD FLAP VANE L/E MIDDLE SECTION IAW REO.

Next page: https://openairdocs.org/aircraft/N438SW/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 = 'N438SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N438SW/reports

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