# Service difficulty reports: N448SW

A list on [N448SW](https://openairdocs.org/aircraft/N448SW.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 · 138 reports

- [SDR SWIA2026081777217](https://openairdocs.org/sdr/SWIA2026081777217.md): Step · broken · Aug 17, 2026 · N448SW · Cndair CL6002B19 · Passenger/Crew Doors
  > DURING THE CLEANING OF THE STEPS A RIVET ATTACHMENT POINT WAS FOUND BROKEN ON THE FWD PANEL, STEP MID. COMPLIED WITH REO 601R-52-11-3130 DATE 2026-09-09 REPAIR TO PAX DOOR STAIR FWD SIDE PANEL
- [SDR SWIA2026081077220](https://openairdocs.org/sdr/SWIA2026081077220.md): Skin · damaged · Aug 10, 2026 · N448SW · Cndair CL6002B19 · Elevator, Plate/Skin
  > LEFT INBD ELEVATOR WAS FOUND DAMAGE. COMPLIED WITH REO 601R-55-21-634 DISPOSITION FOR MISSING MATERIAL AND DENT DAMAGE ON LT ELEVATOR LOWER SKIN INBOARD EDGE,NEAR FRONT SPAR DATUM
- [SDR SWIA2026073077222](https://openairdocs.org/sdr/SWIA2026073077222.md): Window Post · cracked · Jul 30, 2026 · N448SW · Cndair CL6002B19 · Fuselage Main, Structure
  > WINDSHIELD LT SIDE POST, AFTER NDT INSPECTION CRACK NOTED AND MARKED ON LH LOWER OB FITTING REMOVED AND REPLACED FITTING ON WINDSHIELD LH SIDE POST PN 601R33235-5S PO 2319 IAW CRJ200 SRM 53-11-35 SRM 51-42-21
- [SDR SWIA2026072377221](https://openairdocs.org/sdr/SWIA2026072377221.md): Post · cracked · Jul 23, 2026 · N448SW · Cndair CL6002B19 · Fuselage Main, Structure
  > ACCORDING WITH NDT INSPECTION WO 14350-3816, THE WINDSHIELD CENTER POST AND BULKHEAD AFT POST AT FS 20275 - 2 CRACKS NOTED. REMOVED AND REPLACED WINDSHIELD CENTER POST AND BULKHEAD AFT POST AT FS 20275 FITTING PN 601R33237-2S PO2319 AND STRAP PN 601R34012
- [SDR SWIA2026071577219](https://openairdocs.org/sdr/SWIA2026071577219.md): Bracket · cracked · Jul 15, 2026 · N448SW · Cndair CL6002B19 · Nacelle/Pylon, Main Frame
  > LEFT PYLON BRACKET CRACKED AT PYLON FS 605 ON BOTTOM SIDE. COMPLIED WITH REO 601R-54-61-150. REPAIR TO LT PYLON LEADING EDGE RIB AT 605.
- [SDR SWIA2021012376013](https://openairdocs.org/sdr/SWIA2021012376013.md): Link · damaged · Jan 23, 2026 · N448SW · Cndair CL6002B19 · Engine Mount Section
  > MX REQUESTS REMOVAL AND REPLACEMENT OF LH ENGINE FWD YOKE LINK. REMOVED AND REPLACED LT ENGINE FWD YOKE LINK IN REFERENCE TO AMM 71-21-01. REF CP CP 22184438-1 FOR TASK CARD.
- [SDR SWIA2025121700014](https://openairdocs.org/sdr/SWIA2025121700014.md): Bracket · faulted · Dec 14, 2025 · N448SW · Cndair CL6002B19 · Main Landing Gear
  > GEAR DISAGREE, NOSE GEAR DOOR OPEN WARMING MESSAGE ON ROTATION. EXECUTED THE QRH & RETURNED TO THE FIELD, ALL GEAR CAME DOWN WITHOUT A PROBLEM. NO ISSUE ON LANDING. FO NOTICED THE NOSE GEAR FEELING A LITTLE WOBBLY? ON TAKE OFF. (FLIGHT 5129) AFTER PERFORM
- [SDR SWIA2025121500004](https://openairdocs.org/sdr/SWIA2025121500004.md): Warning Message · illuminated · Dec 14, 2025 · N448SW · Cndair CL6002B19 · Landing Gear Door Retract Section
  > GEAR DISAGREE/ NOSE GEAR DOOR OPEN WARMING MESSAGE ON ROTATION. EXECUTED THE QRH AND RETURNED TO THE FIELD, ALL GEAR CAME DOWN WITHOUT A PROBLEM. NO ISSUE ON LANDING. FO NOTICED THE NOSE GEAR FEELING A LITTLE €ŒWOBBLY€? ON TAKE OFF. (FLIGHT 5129 - FILED
- [SDR SWI2025F00324](https://openairdocs.org/sdr/SWI2025F00324.md): Angle · corroded · Jan 15, 2025 · N448SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR STATION FS 349.00 HAS CORROSION (FILED CLOSED) REMOVED, RESTORED, LOCATED AND INSTALLED NEW PAX DOOR ANGLE IAW CRJ-200 SRM 51-21-06 AND 51-42-11. TASK CARD 51-900-1003-SKY COMPLETED. M-337 ATTACHED
- [SDR SWIA202503030115](https://openairdocs.org/sdr/SWIA202503030115.md): Angle · corroded · Jan 15, 2025 · N448SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR STATION FS 349.00 HAS CORROSION (FILED OPEN) REMOVED, RESTORED, LOCATED AND INSTALLED NEW PAX DOOR ANGLE IAW CRJ-200 SRM 51-21-06 AND 51-42-11. TASK CARD 51-900-1003-SKY COMPLETED. M-337 ATTACHED
- [SDR SWI2025F00323](https://openairdocs.org/sdr/SWI2025F00323.md): Yoke · worn · Jan 10, 2025 · N448SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR YOKE ASSY HAS WEAR MARK. COMPLETED TEMPORARY REPAIR TO PASSENGER DOOR CABLE YOKE ASSY IAW REO 601R-52-11-3038.
- [SDR SWI2025F00322](https://openairdocs.org/sdr/SWI2025F00322.md): Riser · corroded · Jan 10, 2025 · N448SW · Cndair CL6002B19 · Passenger/Crew Doors
  > FOUND CORROSION AFT DRAG RAISER UPPER CORNER. (FILED CLOSED) INSTALLED AFT NEW DRAG RAISER ( PAX DOOR) IAW CRJ 200 SRM 51-42-06 AND SRM 51-42-13. NO FOUND CORROSION ( NEW RAISER) TASK CARD 51-900-1003-SKY COMPLETED M-337 ATTACHED
- [SDR SWI2025F00321](https://openairdocs.org/sdr/SWI2025F00321.md): Angle · cracked · Jan 10, 2025 · N448SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR DRAG RAISER ANGLE IS CRACKED. (FILED CLOSED) REPAIRED PAX DOOR DRAG ANGLE IAW REO 601R-52-11-513. TASK CARD 51-900-1003-SKY COMPLETED M-337 ATTACHED
- [SDR SWI2025F00275](https://openairdocs.org/sdr/SWI2025F00275.md): Yoke · worn · Jan 10, 2025 · N448SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR YOKE ASSY HAS WEAR MARK. (FILED OPEN) COMPLETED TEMPORARY REPAIR TO PASSENGER DOOR CABLE YOKE ASSY IAW REO 601R-52-11-3038. TASK CARD 51-900-1003-SKY COMPLETED, M-337 ATTACHED
- [SDR SWI2025F00274](https://openairdocs.org/sdr/SWI2025F00274.md): Riser · corroded · Jan 10, 2025 · N448SW · Cndair CL6002B19 · Passenger/Crew Doors
  > FOUND CORROSION AFT DRAG RAISER UPPER CORNER. (FILED OPEN) INSTALLED AFT NEW DRAG RAISER ( PAX DOOR) IAW CRJ 200 SRM 51-42-06 AND SRM 51-42-13. NO FOUND CORROSION ( NEW RAISER) TASK CARD 51-900-1003-SKY COMPLETED M-337 ATTACHED
- [SDR SWIA202503030110](https://openairdocs.org/sdr/SWIA202503030110.md): Riser · cracked · Jan 10, 2025 · N448SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR DRAG RAISER ANGLE IS CRACKED. (FILED OPEN) REPAIRED PAX DOOR DRAG ANGLE IAW REO 601R-52-11-513. TASK CARD 51-900-1003-SKY COMPLETED M-337 ATTACHED
- [SDR SWIA20250311109](https://openairdocs.org/sdr/SWIA20250311109.md): Structure · cracked · Jan 9, 2025 · N448SW · Cndair CL6002B19 · Fuselage Main, Structure
  > THERE IS A CRACK ON WINGBOX (MARKED IN) INTERIOR @ FS 461 (FILED CLOSED) COMPLIED WITH REO 601R-53-41-3284 FOR REPAIR OF AREA DOUBLERS FABRICATED FROM 2024 T-3.050 AND 2024 T-3.040. TASK CARD 51-900-1003-SKY COMPLETED, M-337 ATTACHED
- [SDR SWIA20250303109](https://openairdocs.org/sdr/SWIA20250303109.md): Structure · cracked · Jan 9, 2025 · N448SW · Cndair CL6002B19 · Fuselage Main, Structure
  > THERE IS A CRACK ON WINGBOX (MARKED IN) INTERIOR @ FS 461 (FILED OPEN) COMPLIED WITH REO 601R-53-41-3284 FOR REPAIR OF AREA DOUBLERS FABRICATED FROM 2024 T-3.050 AND 2024 T-3.040. TASK CARD 51-900-1003-SKY COMPLETED, M-337 ATTACHED
- [SDR SWIA202263876](https://openairdocs.org/sdr/SWIA202263876.md): None · failed · Jan 14, 2022 · N448SW · Cndair CL6002B19 · Aileron Tab Control System
  > DUE TO FAILED BACKLASH OF RH AILERON SYTEM 2 PCU AND SYSTEM 3 PCU AFTER HARDWEAR AND PCU OUTPUT LINK CHANGE, RH AILERON REQUIRES ASSEMBLY REPLACEMENT. (FILED - CLOSED)REMOVED AND REPLACED RH AILERON PER AMM 27-15-01. SEE ATTACHED TASK CARD 27-900-1001-SKY FO
- [SDR SWIA202157572](https://openairdocs.org/sdr/SWIA202157572.md): Channel · corroded · Apr 7, 2021 · N448SW · Cndair CL6002B19 · Electrical/Electronic Compartment Doors
  > MAIN AVIONICS DOOR FWD PROXY SENSOR CHANNEL HAS SURFACE CORROSION. (FILED CLOSED) FABRICATED NEW MAIN AVIONICS DOOR FWD PROXY SENSOR CHANNEL (P/N 601R31049-43) IN REF TO BOMBARDIER DWG 601R31049. / REFERENCE CP 22580704 FOR REMOVAL AND INSTALLATION ALONG
- [SDR SWIA202157569](https://openairdocs.org/sdr/SWIA202157569.md): Frame · corroded · Apr 5, 2021 · N448SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME FS364.00 BETWEEN STR 26L, STR27 AND STR26R HAS CORROSION ON TOP SURFACE OF BOTTOM ANGLE. (FILED CLOSED) REMOVED AND REPLACED LOWER FRAME SECTOR FS 364.00 IN REF TO SRM 51-42-06 AND 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLETED M-337.
- [SDR SWIA202157570](https://openairdocs.org/sdr/SWIA202157570.md): Seat Track · corroded · Apr 2, 2021 · N448SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON LEFT SIDE SEAT RAIL NEAR SEAT 13AB (ROUGHLY FS 559.00+ 48 (FILED CLOSED) REMOVED LH SIDE SEAT RAIL BETWEEN FS535.02 - FS559.00+79. FABRICATED AND INSTALLED NEW SEAT RAIL IN REF TO REO 601R-53-00-055, REV C, DATED 2017-03-21.
- [SDR SWIA202157568](https://openairdocs.org/sdr/SWIA202157568.md): Support Angle · cracked · Apr 1, 2021 · N448SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > CARGO DOOR OPENING UPPER BEAM AFT SUPPORT ANGLE IS CRACKED. FS621.00 AT WL 115.08. (FILED CLOSED) REMOVED AND REPLACED CARGO DOOR OPENING UPPER BEAM AFT SUPPORT ANGLE IN REF TO SRM 51-42-21. COMPLIED WITH 51-900-1003-SKY. COMPLETED M-337.
- [SDR SWIA2019060745965](https://openairdocs.org/sdr/SWIA2019060745965.md): Intercostal · corroded · Apr 22, 2019 · N448SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR CENTER INTERCOSTAL DD6 HAS CORROSION. (C-CHECK) REMOVED AND REPLACED PAX DOOR CENTER INTERCOSTAL DD6 IAW REO.
- [SDR SWIA2019060745964](https://openairdocs.org/sdr/SWIA2019060745964.md): Intercostal · corroded · Apr 22, 2019 · N448SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR CENTER INTERCOSTAL DD4 HAS CORROSION. (C-CHECK) REMOVED AND REPLACED PAX DOOR CENTER INTERCOSTAL DD4 IAW REO.
- [SDR SWIA2019060745963](https://openairdocs.org/sdr/SWIA2019060745963.md): Intercostal · corroded · Apr 22, 2019 · N448SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT INTERCOSTAL DD3 HAS CORROSION. (C-CHECK) REPLACED INTERCOSTAL WITH NEW IAW SRM. ALL CHECKS GOOD.
- [SDR SWIA2019060745960](https://openairdocs.org/sdr/SWIA2019060745960.md): Splice Angle · corroded · Apr 13, 2019 · N448SW · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION ON FS409 FRAME SPLICE ANGLE BETWEEN STR 26L & 26R. (C-CHECK) INSTALLED NEW SPLICE ANGLE P/N 601R32200-17 IAW SRM AND REO. NO DEFECTS NOTED.
- [SDR SWIA2019060745959](https://openairdocs.org/sdr/SWIA2019060745959.md): Frame · corroded · Apr 13, 2019 · N448SW · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION ON AFT SIDE OF FS310 FRAME BETWEEN STR 26L & 26R. (C-CHECK) RO: 06/05/2019 REMOVED AND INSTALLED NEW FRAME IAW SRM. ALL CHECKS GOOD.
- [SDR SWIA2019060745958](https://openairdocs.org/sdr/SWIA2019060745958.md): Hinge · gouged · Apr 10, 2019 · N448SW · Cndair CL6002B19 · Rudder Structure
  > BOTH MIDDLE HINGES FOR RUDDER ATTACH ON VERTICAL STAB GOUGED. (C-CHECK) RO: 06/05/2019 BLENDED AND REPAIRED BOTH MIDDLE HINGES FOR RUDDER ATTACH ON VERTICAL STAB IAW SRM AND REO.
- [SDR SWIA2019060745961](https://openairdocs.org/sdr/SWIA2019060745961.md): Bulkhead Web · corroded · Apr 9, 2019 · N448SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621.0 BETWEEN LBL 9 AND LBL 27 HAS CORROSION. (C-CHECK) REPAIRED FS621 BETWEEN LBL9 AND LBL27 FLOOR SUPPORT IAW REO.
- [SDR SWIA2019060745962](https://openairdocs.org/sdr/SWIA2019060745962.md): Intercostal · corroded · Apr 7, 2019 · N448SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD3 MIDDLE HAS CORROSION. (C-CHECK) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD3 IAW REO.
- [SDR SWIA2019012945478](https://openairdocs.org/sdr/SWIA2019012945478.md): Apu · smoke · Jan 28, 2019 · N448SW · Cndair CL6002B19 · Airborne Auxiliary Power Unit (APU) System
  > SMOKE TOILET CAUTION. WHEN ON APPROACH. APU WAS RUNNING. RAN QRH PROCEDURE AND MESSAGE CLEARED. COULD SMELL BURNING SMELL IN THE COCKPIT. THE SMELL DISSIPATED AFTER THE QRH PROCEDURE. (FLT#4990) FO: 01/29/2019 CLOSED REMOVED AND REPLACED APU ASSY. LEAK AND OPS
- [SDR SWIA2019011545444](https://openairdocs.org/sdr/SWIA2019011545444.md): Control Lever · failed · Jan 11, 2019 · N448SW · Cndair CL6002B19 · Landing Gear Selector
  > UPON BRINGING GEAR HANDLE UP GEAR DID NOT RETRACT. PARKING BRAKE SOV AND INBOARD ANTISKID CAUTION ILLUMINATED. COMPLIED WITH QRH. RETURNED TO FIELD. (FLT 4042) CLOSED REMOVED AND REPLACED THE LANDING GEAR LEVER ASSY IAW AMM. ALL OPS CHECKS GOOD. JACKED THE AIR
- [SDR SWIA201743294](https://openairdocs.org/sdr/SWIA201743294.md): Line · failed · May 10, 2017 · N448SW · Cndair CL6002B19 · Hydraulic System, Main
  > LOST NR 3 HYD SYSTEM DURING CLIMB OUT. HAD TO PERFORM MANUAL EXTENSION OF GEAR. NR 3 HYD SYSTEM SHOWS 5 PERCENT QUANTITY. REPLACED THE 3A AND 3B PUMP FLEX LINES IAW AMM. LEAK CHECKED GOOD.
- [SDR SWIA201743158](https://openairdocs.org/sdr/SWIA201743158.md): Skin · chafed · Mar 12, 2017 · N448SW · Cndair CL6002B19 · Ailerons
  > LEFT AILERON, LOWER SKIN LEADING EDGE FOUND CHAFED FROM WS 303 - 309, AND 347 - 352.29. REMOVED AND REPLACED THE LT AILERON LOWER SKIN LE IAW SRM.
- [SDR SWIA201743157](https://openairdocs.org/sdr/SWIA201743157.md): Vane · chafed · Mar 10, 2017 · N448SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP VANE, OTBD VANE CAP FOUND CHAFED. REPLACED THE VANE CAP IAW SRM.
- [SDR SWIA201743156](https://openairdocs.org/sdr/SWIA201743156.md): Vane · chafed · Mar 10, 2017 · N448SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP VANE MIDDLE VANE CAP FOUND CHAFED. REPLACED THE VANE CAP IAW SRM.
- [SDR SWIA201743155](https://openairdocs.org/sdr/SWIA201743155.md): Vane · chafed · Mar 10, 2017 · N448SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP VANE, INBD VANE CAP FOUND CHAFED. REMOVED AND REPLACED THE INBD VANE CAP IAW SRM.
- [SDR SWIA201743154](https://openairdocs.org/sdr/SWIA201743154.md): Vane · chafed · Mar 10, 2017 · N448SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBD FLAP VANE, OTBD VANE CAP FOUND CHAFED. INSTALLED A NEW OTBD VANE CAP IAW SRM.
- [SDR SWIA201743153](https://openairdocs.org/sdr/SWIA201743153.md): Vane · chafed · Mar 10, 2017 · N448SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBD FLAP VANE, MIDDLE VANE CAP CHAFED. INSTALLED A NEW VANE CAP IAW SRM.
- [SDR SWIA201743152](https://openairdocs.org/sdr/SWIA201743152.md): Vane · chafed · Mar 10, 2017 · N448SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBD FLAP VANE, INBD VANE CAP CHAFED. REPLACED THE FLAP INBD VANE CAP IAW SRM.
- [SDR SWIA201743151](https://openairdocs.org/sdr/SWIA201743151.md): Web · cracked · Mar 9, 2017 · N448SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT SIDE TRU BAY WEB, BS 195.0 CRACKED. REPAIRED THE WEB IAW REO.
- [SDR SWIA201642934](https://openairdocs.org/sdr/SWIA201642934.md): Bracket · damaged · Dec 20, 2016 · N448SW · Cndair CL6002B19 · Main Landing Gear
  > AFTER TAKE OFF NOSE GEAR WOULD NOT RETRACT. REMOVED AND REPLACED THE OLEO SENSOR BRACKET AND PERFORMED EXTENSION AND RETRACTION AND OPS CHECK, NO DEFECTS NOTED.
- [SDR SWIA201642932](https://openairdocs.org/sdr/SWIA201642932.md): Sensor · failed · Dec 16, 2016 · N448SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > AIRCRAFT RETURNED TO THE FIELD WITH A GEAR DISAGREE. NOSE GEAR DID NOT RETRACT. RIGGED PS23 IAW AMM. PERFORMED GEAR SWINGS OF NLG IAW AMM. NO DEFECTS NOTED AT THIS TIME.
- [SDR SWIA201641764](https://openairdocs.org/sdr/SWIA201641764.md): Landing Gear · malfunctioned · Jan 14, 2016 · N448SW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > DURING TAKEOFF, RECEIVED GEAR DISAGREE, NOSE DID NOT COME UP. THEN ON APPROACH FOLLOWED QRH AND USED THE MANUAL EXTENSION AND ALL 3 CAME DOWN. ALSO RECEIVED NWS INOPERATIVE BUT CLEARED IN FLT. ALSO HAD WOW OUTPUT CAUTION MSG AND EXTINGUISHED ON GROUND. WORK
- [SDR SWIA201540975](https://openairdocs.org/sdr/SWIA201540975.md): Frame · corroded · Mar 23, 2015 · N448SW · Cndair CL6002B19 · Fuselage Main, Frame
  > RT FRAME SECTOR AT FS513, RBL 36, WL 75 CORRODED ON FWD AND AFT EDGES. C-CHECK RO 4/2/15, REMOVED CORROSION FROM RT FRAME SECTOR AT FS513, RBL 36, WL 75 ON FWD AND AFT EDGES. BLENDED, NDT AND VISUALLY INSPECTED NO DEFECTS NOTED, ROTO PEENED REWORKED AREA RES
- [SDR SWIA201540971](https://openairdocs.org/sdr/SWIA201540971.md): Frame · unknown · Mar 18, 2015 · N448SW · Cndair CL6002B19 · Fuselage Main, Frame
  > REPLACE FUSELAGE FRAME AT FS 349.00, STR L24 TO R24. C-CHECK, RO 4/2/15, R & R OLD FRAME WITH NEW FRAME AT FS 349.00, STR L24 TO R24, WEIGHT REMOVED 1.3LB, WEIGHT ADDED 1.3LB.
- [SDR SWIA201540982](https://openairdocs.org/sdr/SWIA201540982.md): Structure · chafed · Mar 15, 2015 · N448SW · Cndair CL6002B19 · Landing Gear Doors
  > LEFT MLG DOOR HAS CHAFE DAMAGE ON INTERIOR SIDE AT DOUBLER, LOWER FWD CORNER AREA, C-CHECK, RO 4/2/15, CHAFING DAMAGE IS CONTAINED TO INNER SKIN FILLER FROM PREVIOUS REPAIR AND IS NOT WITHIN LIMITS IAW SRM. R & R REPAIR FILLER, PN 601R-52-82-016-3 IAW SRM.
- [SDR SWIA201540981](https://openairdocs.org/sdr/SWIA201540981.md): Lug · gouged · Mar 15, 2015 · N448SW · Cndair CL6002B19 · Main Landing Gear
  > LEFT MLG DOOR CENTER LUG HAS CHAFE DAMAGE. EVALUATED LT MLG DOOR CENTER BELLCRANK LUG GOUGE DAMAGE MEASURES AT.074 DEEP ON SIDE SURFACE LUG IS OUT OF REPAIR LIMITS MAX DEPTH ALLOWED ON SIDE FACE IS.060 CUMULATIVE BOTH SIDE REF REO. INSTALLED NEW LT M/L/G
- [SDR SWIA201540980](https://openairdocs.org/sdr/SWIA201540980.md): Skin · corroded · Mar 15, 2015 · N448SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE INTERIOR SKIN AT AVIONICS DOOR CUT-OUT, HAS CORROSION AROUND PERIMETER OF CUTOUT, C-CHECK RO 4/2/15. BLENDED OUT CORROSION FROM FUSELAGE AREA AROUND AVIONICS DOOR CUTOUT INNER SKIN DOUBLER REF 200. REO ORIGINAL THICKNESS OF FUSELAGE INTERIOR SKIN AVI

Next page: https://openairdocs.org/aircraft/N448SW/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 = 'N448SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N448SW/reports

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