# Service difficulty reports: N506CA

A list on [N506CA](https://openairdocs.org/aircraft/N506CA.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 5 · 216 reports

- [SDR SWIA2026020675220](https://openairdocs.org/sdr/SWIA2026020675220.md): Oxygen Mask · unwanted deploy · Feb 6, 2026 · N506CA · Cndair CL6002B19 · Passenger Oxygen System
  > DUE TO PASSENGER 02 SYSTEM DEPLOYMENT, PRIOR TO RETURN TO REVENUE SERVICE C/W AMM 05-51-35 MCI TYPE: SERVICEABLE / NEEDS ATTENTION (FLIGHT 5390) TROUBLESHOT LH PACK FAIL CAUSING CABIN ALT WARNING IN REF TO CRJ 200 FIM 21-50-00 FOR MOMENTARY PACK HIGH PRESSUR
- [SDR SWI2025F00736](https://openairdocs.org/sdr/SWI2025F00736.md): Switch · faulted · Jun 18, 2025 · N506CA · Cndair CL6002B19 · Cabin Cooling System
  > UPON TURNING OFF ANY ICE AT FL200, L PACK HIGH PRESS CAUTION MESSAGE. L PACK SUBSEQUENTLY TURNED OFF. (FLIGHT 5224 - FILED CLOSED)SPOKE WITH CREW AND CREW STATED THAT THEY WERE UNSURE IF L PACK HIGH PRESS MESSAGE OR L PACK HIGH TEMP MESSAGE DISPLAYED. PERFORM
- [SDR SWIA202506200016](https://openairdocs.org/sdr/SWIA202506200016.md): Regulator Valve · warning message · Jun 16, 2025 · N506CA · Cndair CL6002B19 · Air Distribution System
  > R PACK STATUS MESSAGE DURING TAXI. RESET PACK AND EXTINGUISHED. ON DEPARTURE WHEN SWAPPED BLEEDS AND DROPPED APU L PACK HI PRESSURE CAUTION. CABIN ALTITUDE HI CAUTION MESSAGE. REMAINED BELOW 10K FEET. CABIN ALTITUDE CLIMBED TO 9999 FEET. WORKED THROUGH QRH. LA
- [SDR SWIA20250311220](https://openairdocs.org/sdr/SWIA20250311220.md): Skin · damaged · Dec 20, 2024 · N506CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > OVERSIZED COUNTER-SINK LOCATED ON SKIN PANEL OF FS 202.75 BETWEEN STGR 15L AND STGR 16L REQUIRES REPAIR (FILED CLOSED) COMPLIED WITH ALL STEPS IN REO 601R-53-11-3966 REV-- DATED 2025-01-14. PERFORMED PERMANENT REPAIR TO THE FUSELAGE SKIN AND DOUBLER AT F
- [SDR SWIA20250110220](https://openairdocs.org/sdr/SWIA20250110220.md): Skin · damaged · Dec 20, 2024 · N506CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > OVERSIZED COUNTER-SINK LOCATED ON SKIN PANEL OF FS 202.75 BETWEEN STGR 15L AND STGR 16L REQUIRES REPAIR (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA202503111209](https://openairdocs.org/sdr/SWIA202503111209.md): Intercostal · damaged · Dec 9, 2024 · N506CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > REMOVE AND REPLACE INTERCOSTAL (600-33011) BETWEEN FS 193 TO FS 202.75 ABOVESTRG 12L JUST FORWARD OF PILOT WINDSHIELD WITH A SERVICEABLE UNIT DUE TO MISSING DRILLING. (FILED CLOSED) REMOVED AND REPLACED INTERCOSTAL (600-33011) BETWEEN FS 193 TO FS 202
- [SDR SWIA2025012709](https://openairdocs.org/sdr/SWIA2025012709.md): Intercostal · damaged · Dec 9, 2024 · N506CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > REMOVE AND REPLACE INTERCOSTAL (600-33011) BETWEEN FS 193 TO FS 202.75 ABOVESTRG 12L JUST FORWARD OF PILOT WINDSHIELD WITH A SERVICEABLE UNIT DUE TO MISSING DRILLING. (FILED OPEN) REMOVED AND REPLACED INTERCOSTAL (600-33011) BETWEEN FS 193 TO FS 202.7
- [SDR SWIA202503111201](https://openairdocs.org/sdr/SWIA202503111201.md): Intercostal · no discrepancy · Dec 1, 2024 · N506CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT TOP INTERCOSTAL (600-33011) REMOVED AT FS193 TO FOM. (FILED CLOSED) INSTALLED LEFT TOP INTERCOSTAL (600-33011) AT FS193 IN REFERENCE TO SRM 51-42-06 SEE TASK CARD 51-900-1003-SKY AND M-337. SEE CP29276351 FOR PRESURIZATION CHECK.
- [SDR SWIA2025012701](https://openairdocs.org/sdr/SWIA2025012701.md): None · none · Dec 1, 2024 · N506CA · Cndair CL6002B19 · Standard Practices/Structures
  > LEFT TOP INTERCOSTAL (600-33011) REMOVED AT FS193 TO FOM. (FILED OPEN) INSTALLED LEFT TOP INTERCOSTAL (600-33011) AT FS193 IN REFERENCE TO SRM 51-42-06 SEE TASK CARD 51-900-1003-SKY AND M-337. SEE CP29276351 FOR PRESURIZATION CHECK.
- [SDR SWI2025F00317](https://openairdocs.org/sdr/SWI2025F00317.md): Frame · damaged · Nov 23, 2024 · N506CA · Cndair CL6002B19 · Fuselage Main, Frame
  > TRANSFER FROM EAML 1476474: REF AML 1472665: BIRDSTRIKE DAMAGE NOTED ON FRAME FS193.00 (DWG: 600-34011, AL ALY ALCD 7075-T62, 0.063€? NOM. THK., REF). DENT: 0.250€? DEPTH CRACK ON RADIUS: 4.20€? L (FLIGHT 5952 - FILED CLOSED) COMPLIED WITH ALL S
- [SDR SWI2025F00316](https://openairdocs.org/sdr/SWI2025F00316.md): Intercostal · damaged · Nov 23, 2024 · N506CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > TRANSFER FROM EAML 1476476: REF AML 1472665: BIRDSTRIKE DAMAGE NOTED ON INTERCOSTAL (DWG: 600-33011, AL ALY ALCD 2024-T42, 0.032€? NOM. THK., REF) DENT: 1.90€? L X 0.050€? D (FLIGHT 5952 - FILED CLOSED) REMOVED DAMAGED INTERCOSTAL JUST ABOVE STR
- [SDR SWI2025F00315](https://openairdocs.org/sdr/SWI2025F00315.md): Skin · damaged · Nov 23, 2024 · N506CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > TRANSFER FROM EAML 1476473: REF AML 1472665: BIRDSTRIKE DAMAGE NOTED ON FUSELAGE SKIN (DWG: 601R33010, AL ALY ALCD 2024-T42, 0.063€? PAD UP THK., 0.038€? CHEM. MILL. THK., REF. DENT: 11.50€? L X 2.50€? W X 0.100€? D €¢ 7-OFF PULLED MS20426AD4 FASTE
- [SDR SWIA20250311023](https://openairdocs.org/sdr/SWIA20250311023.md): Stringer · damaged · Nov 23, 2024 · N506CA · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > TRANSFER FROM EAML 1476475: REF AML 1472665: BIRDSTRIKE DAMAGE NOTED ON STRINGER 14L (DWG: 600-33011, AL ALY ALCD 2024-T42, 0.032€? NOM. THK., REFDENT: 2.50€? L X 0.100€? D CRACK: 0.050€? L (FLIGHT 5952 - FILED CLOSED) REMOVED AND REPLACED STRIN
- [SDR SWIA202501270096](https://openairdocs.org/sdr/SWIA202501270096.md): Frame · damaged · Nov 23, 2024 · N506CA · Cndair CL6002B19 · Fuselage Main, Frame
  > TRANSFER FROM EAML 1476474: REF AML 1472665: BIRDSTRIKE DAMAGE NOTED ON FRAME FS193.00 (DWG: 600-34011, AL ALY ALCD 7075-T62, 0.063€? NOM. THK., REF). DENT: 0.250€? DEPTH CRACK ON RADIUS: 4.20€? L (FLIGHT 5952 - FILED OPEN) COMPLIED WITH ALL STE
- [SDR SWIA202501270095](https://openairdocs.org/sdr/SWIA202501270095.md): Intercostal · damaged · Nov 23, 2024 · N506CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > TRANSFER FROM EAML 1476476: REF AML 1472665: BIRDSTRIKE DAMAGE NOTED ON INTERCOSTAL (DWG: 600-33011, AL ALY ALCD 2024-T42, 0.032€? NOM. THK., REF) DENT: 1.90€? L X 0.050€? D (FLIGHT 5952 - FILED OPEN) REMOVED DAMAGED INTERCOSTAL JUST ABOVE STRIN
- [SDR SWIA202501270094](https://openairdocs.org/sdr/SWIA202501270094.md): Skin · damaged · Nov 23, 2024 · N506CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > TRANSFER FROM EAML 1476473: REF AML 1472665: BIRDSTRIKE DAMAGE NOTED ON FUSELAGE SKIN (DWG: 601R33010, AL ALY ALCD 2024-T42, 0.063€? PAD UP THK., 0.038€? CHEM. MILL. THK., REF. DENT: 11.50€? L X 2.50€? W X 0.100€? D €¢ 7-OFF PULLED MS20426AD4 FASTE
- [SDR SWIA2025012700123](https://openairdocs.org/sdr/SWIA2025012700123.md): Stringer · damaged · Nov 23, 2024 · N506CA · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > TRANSFER FROM EAML 1476475: REF AML 1472665: BIRDSTRIKE DAMAGE NOTED ON STRINGER 14L (DWG: 600-33011, AL ALY ALCD 2024-T42, 0.032€? NOM. THK., REFDENT: 2.50€? L X 0.100€? D CRACK: 0.050€? L (FLIGHT 5952 - FILED OPEN) REMOVED AND REPLACED STRINGE
- [SDR SWIA20240713](https://openairdocs.org/sdr/SWIA20240713.md): Engine · shutdown · Jul 13, 2024 · N506CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > AT 11000 FT AND DESCENDING WE HEARD A METALLIC TWANGING SOUND LIKE A ROPE BRAKING. ENGINE TWO THRUST REDUCED TO AT NEAR IDLE AT ABOUT 30% N1. EMERGENCY DECLARED RAN QRH ABNORMAL 1-4 AND SECURED ENGINE. (FLIGHT 4318 - FILED CLOSED)THIS DISCREPANCY WAS TRANS
- [SDR SWI20240515000413](https://openairdocs.org/sdr/SWI20240515000413.md): Bracket · cracked · Apr 30, 2024 · N506CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT SIDE OF FS621.00 JUST OUTBOARD OF RBL 36.20 AND INLINE WITH STRINGER 15R, INTERCOSTAL CRACKED. (C-CHECK RO 5/14/2024) REMOVED AND REPLACED INTERCOSTAL/BRACKET ON AFT SIDE OF FS621.00 JUST OUTBOARD OF RBL 36.20 AND INLINE WITH STRINGER 15R WITH REFERENC
- [SDR SWI20240515000412](https://openairdocs.org/sdr/SWI20240515000412.md): Bracket · cracked · Apr 30, 2024 · N506CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT SIDE OF FS621.00 JUST OUTBOARD OF LBL 36.20 AND INLINE WITH STRINGER 15R, INTERCOSTAL CRACKED. (C-CHECK RO 5/14/2024) REMOVED AND REPLACED INTERCOSTAL/BRACKET ON AFT SIDE OF FS621.00 JUST OUTBOARD OF LBL 36.20 AND INLINE WITH (CORRECTED STRINGER 15L) W
- [SDR SWI20240515000411](https://openairdocs.org/sdr/SWI20240515000411.md): Vane · damaged · Apr 30, 2024 · N506CA · Cndair CL6002B19 · Trailing Edge Flaps
  > LH WING IB FLAP MOVEABLE VANE HAS CHAFFING DAMAGE WHERE THE VANE MEETS THE STOPS IN THREE SPOTS. (C-CHECK RO 5/14/2024) PERFORMED TEMPORARY REPAIR OF THREE AREAS OF CHAFING DAMAGE TO THE LH IB FLAP VANE IN REF TO REO 601R-57-52-004, REV D, DATED 2012-12-1
- [SDR SWI20240515000410](https://openairdocs.org/sdr/SWI20240515000410.md): Vane · chafed · Apr 30, 2024 · N506CA · Cndair CL6002B19 · Trailing Edge Flaps
  > RH WING IB FLAP MOVEABLE VANE HAS CHAFFING DAMAGE WHERE THE VANE MEETS THE STOPS IN THREE SPOTS. (C-CHECK RO 5/14/2024) PERFORMED TEMPORARY REPAIR OF THREE AREAS OF CHAFING DAMAGE TO THE RH IB FLAP VANE IN REF TO REO 601R-57-52-004, REV D, DATED 2012-12-1
- [SDR SWI20240515000408](https://openairdocs.org/sdr/SWI20240515000408.md): Pressure Blkhd · gouged · Apr 24, 2024 · N506CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FWD FACE OF THE REAR PRESSURE BULKHEAD AT FS 621.00 HAS 7 GOUGE MARKS AND 7 DAMAGED RIVET HEADS. (C-CHECK RO 5/14/2024) REPAIRED FWD FACE OF THE REAR PRESSURE BULKHEAD AT FS 621.00 WITH REFERENCE TO REO 601R-53-61-8186 REV "--" DATED 2024-05-01. SEE CHILD
- [SDR SWIA202265543](https://openairdocs.org/sdr/SWIA202265543.md): None · cracked · Apr 29, 2022 · N506CA · Cndair CL6002B19 · Window/Windshield System
  > FO NOTICED 2 SMALL WINDOW CRACKS AFTER TAKEOFF. SHORTLY AFTER, WE GOT R WINDOW HEAT CAUTION. RAN THAT QRH & DID NOT CLEAR. THE CRACK WAS GROWING. RAN ABNORM 11-19 AND CRACK DID NOT GROW ANY MORE. (FLIGHT 4613 - FILED CLOSED) REMOVED AND REPACED FO'S WINDO
- [SDR SWIA202265442](https://openairdocs.org/sdr/SWIA202265442.md): None · damaged · Apr 11, 2022 · N506CA · Cndair CL6002B19 · Horizontal Stabilizer, Plate/Skin
  > TRANSFER FROM EAML 881085: TRANSFERRED FROM CAMP 24616514. HORIZONTAL STAB RH, OUTER PIVOT PIN BUSHING ON THE OUTB SIDE IS DAMAGED AND OUT OF LIMITS. (FILED CLOSED) SERVICE BULLETIN 601R-55-009, STABILIZER- REPLACEMENT OF THE PIVOT PIN BUSHING IN HORIZONT
- [SDR SWIA202156358](https://openairdocs.org/sdr/SWIA202156358.md): Anchor Fitting · corroded · Jan 30, 2021 · N506CA · Cndair CL6002B19 · Passenger/Crew Doors
  > WHILE REMOVING PAX DOOR AFT COUNTERBALANCE ANCHOR-FITTING (PN 601R38074-3) TO FOM, FOUND SERRATED SIDE TO BE CORRODED. NO ALLOWABLE LIMITS PER SRM 52-00-27 (C-CHECK) RO 2/17/2021 RECEIVED REPLACEMENT PAX DOOR AFT ANCHOR FITTING, REFERENCE CAMP 22008656 FOR
- [SDR SWIA202156357](https://openairdocs.org/sdr/SWIA202156357.md): Control Rod · corroded · Jan 24, 2021 · N506CA · Cndair CL6002B19 · Elevator Control System
  > LEFT ELEVATOR CONTROL ROD 600-92602-81 AFT ROD END BEARING IS CORRODED AND HAS ROUGH MOVEMENT. (C-CHECK) RO 2/17/2021. REMOVED AND REPLACED LT ELEVATOR CONTROL ROD IAW CRJ200 AMM 27-31-35-400-801, RIG CHECK GOOD IAW CRJ 200 AMM 27-31-00-830-805, AND OPS CHEC
- [SDR SWIA202156311](https://openairdocs.org/sdr/SWIA202156311.md): Structure · chafed · Jan 19, 2021 · N506CA · Cndair CL6002B19 · Fuselage Main, Structure
  > CHAFFING ON FUSELAGE BEHIND RT AFT PYLON SEALS (C-CHECK) RO 2/17/2021. REPAIRED CHAFFED AREA ON FUSELAGE BEHIND RT AFT PYLON SEALS IAW MHIRJ 601R-53-61-7554 REV -- (P2) DATED 2021-01-27 AND BOMBARDIER REO 601R-53-61-268 REV A DATED 2000-07-11. TASK CARD 51-9
- [SDR SWIA202156305](https://openairdocs.org/sdr/SWIA202156305.md): Stringer · damaged · Jan 19, 2021 · N506CA · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > FOUND MULTIPLE OVERSIZED HOLES FROM FS 310 TO FS 333 AT STRINGER 20L. (C-CHECK) RO 2/17/2021. REPLACED STRINGER 20L FROM FS 310 TO FS 333 IAW CRJ 200 SRM 51-42-06 AND 51-42-21. REMOVED FOR ACCESS AND REINSTALLED FS 319 AND FS 333 FRAME SECTORS IAW CRJ 200 S
- [SDR SWIA202156323](https://openairdocs.org/sdr/SWIA202156323.md): Floor Support · corroded · Jan 17, 2021 · N506CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR BEAM AT LBL 9 HAS MINOR CORROSION FROM FS 409.00+128 TO FS 559.00. (C-CHECK) RO 2/17/2021. COMPLIED WITH REO 601R-53-41-2841 REV -- DATED 2021-01-13 FOR REPAIR OF THE FLOOR BEAM AT LBL 9 BETWEEN FS 409.00+128 TO FS 559.00. COMPLETED TASK CARD 51-900-1
- [SDR SWIA202156322](https://openairdocs.org/sdr/SWIA202156322.md): Skin · dented · Jan 16, 2021 · N506CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT LOCATED 4 INCHES FORWARD OF FS 394 STGR 16R. (C-CHECK) RO 2/17/2021. REPAIRED DAMAGE IAW REO 601R-53-21-3378 REV-- DATED 2021-01-21, COMPLETED MAJOR REPAIR TASK CARD 51-900-1003-SKY, AND FORM M-337. NO WEIGHT CHANGE.
- [SDR SWIA202156321](https://openairdocs.org/sdr/SWIA202156321.md): Floorbeam · damaged · Jan 11, 2021 · N506CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FOUND THERE TO BE 1 EA ELONGATED HOLE ON THE RT PRESSURE FLOOR SILL AT FS 559 BETWEEN RBL 36 AND RBL 45. (C-CHECK) RO 2/17/2021. REPAIRED DAMAGE IAW REO 601R-53-41-2847 REV A DATED 2021-01-26. COMPLETED MAJOR REPAIR TASK CARD 51-900-1003-SKY AND FORM M-337.
- [SDR SWIA202156363](https://openairdocs.org/sdr/SWIA202156363.md): Skin · damaged · Jan 3, 2021 · N506CA · Cndair CL6002B19 · Elevator, Plate/Skin
  > CAMP NR 22026917 RT ELEVATOR LOWER SKIN FLUSH REPAIR REQUIRES FABRICATION OF DOUBLER AND REPAIR PARTS. (C-CHECK) RO 2/17/2021. FABRICATED AND DRILLED ELEVATOR SKIN NON-FLUSH REPAIR FIGURE 204 REPAIR PARTS: DOUBLER ITEM NR 3 FIGURE 201, AND FILLER ITEM NR 1 F
- [SDR SWIA202156314](https://openairdocs.org/sdr/SWIA202156314.md): Skin · damaged · Jan 3, 2021 · N506CA · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT FUEL BOOST PUMP CUTOUT LANDINGS HAVE MULTIPLE INDICATIONS 50% FSH AROUND ENTIRE CIRCUMFERENCE. FAILED NDT INSPECTION, (C-CHECK) RO 2/17/2021. REPAIRED RT FUEL BOOST PUMP CUTOUT LANDING IAW REO 601R-57-21-3405 REV --, DATED 2021-01-22. COMPLETED MAJOR
- [SDR SWIA202156366](https://openairdocs.org/sdr/SWIA202156366.md): Cap · broken · Jan 2, 2021 · N506CA · Cndair CL6002B19 · Fuselage Main, Structure
  > RIGHT FLOOR FLOOR BEAM CAP FOR THE SEAT TRACK BETWEEN FS 409+128 TO FS 559+4 RBL 9 HAS 8 BROKEN SCREWS STUCK AND 1 MISSING RIVNUT. (C-CHECK) RO 2/17/2021. TECHNICIAN TAPPED OUT 8 BROKEN SCREWS FROM RT FLOOR BEAM CAP AND INSTALLED 1 RIVNUT BETWEEN FS 409+128
- [SDR SWIA202056320](https://openairdocs.org/sdr/SWIA202056320.md): Pan · corroded · Dec 24, 2020 · N506CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR LOWER PAN HAS CORROSION. (C-CHECK) RO 2/17/2021. REPAIRED SERVICE DOOR FWD LOWER PAN IAW REO 601R-52-41-444 REV --, DATED 2021-01-21, REPLACED SERVICE DOOR AFT LOWER PAN IAW CRJ 200 SRM 51-42-06 REV 38 B DATED 25-NOV-2020 AND DWG NR 601R38304, C
- [SDR SWIA202056355](https://openairdocs.org/sdr/SWIA202056355.md): Bolt · corroded · Dec 23, 2020 · N506CA · Cndair CL6002B19 · Trailing Edge Flaps
  > WHILE REMOVING RT O/B FLAP HINGE ARM ASSEMBLIES AT WS 178.00 AND WS 264.00 FOUND HARDWARE TO BE CORRODED. (C-CHECK) RO 2/17/2021. RECEIVED SERVICEABLE HARDWARE. REFERENCE CAMP 21819157-1 FOR INSTALL.
- [SDR SWIA202056354](https://openairdocs.org/sdr/SWIA202056354.md): Bolt · corroded · Dec 23, 2020 · N506CA · Cndair CL6002B19 · Trailing Edge Flaps
  > WHILE REMOVING LT O/B FLAP HINGE ARM ASSEMBLIES AT WS 178.00 AND 264.00, FOUND HARDWARE TO BE CORRODED. (C-CHECK) RO 2/17/2021. RECEIVED SERVICEABLE PARTS. REFERENCE CAMP 21819156-1 FOR INSTALL.
- [SDR SWIA202056353](https://openairdocs.org/sdr/SWIA202056353.md): Rod End · corroded · Dec 23, 2020 · N506CA · Cndair CL6002B19 · Ailerons
  > LEFT AILERON PCU ROD ENDS HAVE CORROSION. (C-CHECK) RO 2/17/2021. REMOVED AND INSTALLED INBOARD AND OUTBOARD PCU FROM LT AILERON IAW AMM 27-14-01-00-801/27-14-01-4000-801 AND SKYWEST SUPPLEMENT TASK 27-900-1002-SKY (CL600-2B19).
- [SDR SWIA202056326](https://openairdocs.org/sdr/SWIA202056326.md): Angle · cracked · Dec 23, 2020 · N506CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > OBLIQUE ANGLE CRACKED AT FS 621.00 TO FS 625.00 RBL 45 STRGR 14 WL 97.5 (C-CHECK) RO 2/17/2021. TECH REPLACED OBLIQUE ANGLE AT RBL 45 BETWEEN FS 621.00-FS 625.00 IAW CRJ 200 SRM 51-40-11, 51-25-00 AND 51-42-21.
- [SDR SWIA202056315](https://openairdocs.org/sdr/SWIA202056315.md): Skin · damaged · Dec 22, 2020 · N506CA · Cndair CL6002B19 · Elevator, Plate/Skin
  > RIGHT ELEVATOR CENTER LOWER T/E SKIN HAS DAMAGE ON CORNER APPROX 1/2 INCH. (C-CHECK) RO 2/17/2021. REPAIRED RT ELEVATOR SKIN DAMAGE WITH SINGLE SIDED ELEVATOR SKIN NON-FLUSH REPAIR IAW CRJ 200 SRM 55-20-00 REV 38B DATED 11/25/2020. COMPLETED FORM 337 AND SK
- [SDR SWIA202056306](https://openairdocs.org/sdr/SWIA202056306.md): Hinge Fitting · gouged · Dec 22, 2020 · N506CA · Cndair CL6002B19 · Ailerons
  > RIGHT AILERON NR 4 HINGE LUG HAS A GOUGE. (C-CHECK) RO 2/17/2021. COMPLIED WITH MHIRJ REO 601R-57-61-764 REV-- DATE 2021-01-01, TASK CARD 51-900-1003-SKY COMPLETED AND FORM M-337 ATTACHED. NO WEIGHT CHANGE.
- [SDR SWIA202056304](https://openairdocs.org/sdr/SWIA202056304.md): Skin · damaged · Dec 22, 2020 · N506CA · Cndair CL6002B19 · Elevator, Plate/Skin
  > RIGHT ELEVATOR CENTER T/E UPPER SURFACE HAS DAMAGE IN CORNER OF METAL. (C-CHECK) RO 2/17/2021. REPAIRED RT ELEVATOR CENTER TRAILING EDGE UPPER SURFACE IAW CRJ 200 SRM 55-20-00 REV 38B DATED 25 NOV 2020 AND SKYCARD 51-900-1003-SKY AND COMPLETED FORM 337. WEI
- [SDR SWIA202056352](https://openairdocs.org/sdr/SWIA202056352.md): Skin · corroded · Dec 20, 2020 · N506CA · Cndair CL6002B19 · Vertical Stabilizer, Plate/Skin
  > VERTICAL STABILIZER UPPER SKIN PLATE HAS FIVE FASTENERS AFT THAT HAVE RUSTED HEADS AND CORRODED TAILS. (C-CHECK) RO 2/17/2021. REMOVED AND REPLACED 5 EA FASTENERS ON THE VERTICAL STAB UPPER SKIN IAW CRJ 200 SRM 51-42-22.
- [SDR SWIA202056351](https://openairdocs.org/sdr/SWIA202056351.md): Stop Fitting · corroded · Dec 19, 2020 · N506CA · Cndair CL6002B19 · Service Doors
  > FORWARD AND AFT SERVICE DOOR STOP FITTINGS HAVE CORRODED HARDWARE AND REQUIRES REPLACEMENT. (C-CHECK) RO 2/17/2021. REMOVED AND REPLACED CORRODED SERVICE DOOR STOP FITTING HARDWARE IAW SRM 51-41-02.
- [SDR SWIA202056350](https://openairdocs.org/sdr/SWIA202056350.md): Seat Track · corroded · Dec 19, 2020 · N506CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT FLOOR SEAT RAIL CORRODED BETWEEN FS 409 AND FS 409+126 AT RBL 9 (C-CHECK) RO 2/17/2021. REMOVED DAMAGED RT SEAT TRACK ON FS 409 TO FS 409+126 AT RBL 9, AND INSTALLED NEW SERVICEABLE SEAT TRACK THAT WAS FABRICATED FROM CAMP NR 22075041.
- [SDR SWIA202056349](https://openairdocs.org/sdr/SWIA202056349.md): Seat Track · corroded · Dec 19, 2020 · N506CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT FLOOR SEAT RAIL CORRODED BETWEEN FS 409 AND FS 409+126 AT LBL 9 (C-CHECK) RO 2/17/2021. REMOVED AND REPLACED LT FLOOR SEAT RAIL BETWEEN FS 409 AND FS 409+126 AT LBL9 WITH SERVICEABLE ONE IAW CRJ 200 AMM 53-01-11-400-802.
- [SDR SWIA202056348](https://openairdocs.org/sdr/SWIA202056348.md): Seat Track · corroded · Dec 19, 2020 · N506CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT FLOOR SEAT RAIL CORRODED BETWEEN FS 349 AND FS 399.50 AT LBL 9 (C-CHECK) RO 2/17/2021. REMOVED AND REPLACED FLOOR SEAT RAIL PN 601R31032-15 WITH SAME PN IAW CRJ 200 AMM 53-01-11-000-802 & 53-01-11-400-802.
- [SDR SWIA202056347](https://openairdocs.org/sdr/SWIA202056347.md): Seat Track · corroded · Dec 19, 2020 · N506CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT FLOOR SEAT RAIL CORRODED BETWEEN FS 409.+126 AND FS 559+4 AT LBL 9 (C-CHECK) RO 2/17/2021. REMOVED DAMAGED SEAT TRACK BETWEEN FS 409+126 TO FS 559+4 AT LBL 9 AND INSTALLED NEW SERVICEABLE SEAT TRACK IAW CRJ200-AMM-53-01-11-000-802, AND 53-01-11-400-802.
- [SDR SWIA202056346](https://openairdocs.org/sdr/SWIA202056346.md): Seat Track · corroded · Dec 19, 2020 · N506CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT FLOOR SEAT RAIL CORRODED BETWEEN FS 409.+126 AND FS 559+4 AT RBL 9 (C-CHECK) RO 2/17/2021. REMOVED DAMAGED SEAT TRACK AT RBL 9 BETWEEN FS 409+126 AND FS 559+4 AND INSTALLED WITH NEW SERVICEABLE SEAT TRACK IAW CRJ200-AMM-53-01-11-000-802 AND 53-01-11-40

Next page: https://openairdocs.org/aircraft/N506CA/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 = 'N506CA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N506CA/reports

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