N506CA

Service difficulty reports · 216

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR SWIA2026020675220Oxygen Mask · unwanted deployDUE 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 PRESSURFeb 6, 2026 · N506CA · Cndair CL6002B19 · Passenger Oxygen SystemSDR SWI2025F00736Switch · faultedUPON 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. PERFORMJun 18, 2025 · N506CA · Cndair CL6002B19 · Cabin Cooling SystemSDR SWIA202506200016Regulator Valve · warning messageR 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. LAJun 16, 2025 · N506CA · Cndair CL6002B19 · Air Distribution SystemSDR SWIA20250311220Skin · damagedOVERSIZED 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 FDec 20, 2024 · N506CA · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA20250110220Skin · damagedOVERSIZED 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 PROGRESSDec 20, 2024 · N506CA · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202503111209Intercostal · damagedREMOVE 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 202Dec 9, 2024 · N506CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2025012709Intercostal · damagedREMOVE 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 202.7Dec 9, 2024 · N506CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202503111201Intercostal · no discrepancyLEFT 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.Dec 1, 2024 · N506CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2025012701None · noneLEFT 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.Dec 1, 2024 · N506CA · Cndair CL6002B19 · Standard Practices/StructuresSDR SWI2025F00317Frame · damagedTRANSFER 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 SNov 23, 2024 · N506CA · Cndair CL6002B19 · Fuselage Main, FrameSDR SWI2025F00316Intercostal · damagedTRANSFER 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 STRNov 23, 2024 · N506CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2025F00315Skin · damagedTRANSFER 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 FASTENov 23, 2024 · N506CA · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA20250311023Stringer · damagedTRANSFER 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 STRINNov 23, 2024 · N506CA · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA202501270096Frame · damagedTRANSFER 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 STENov 23, 2024 · N506CA · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202501270095Intercostal · damagedTRANSFER 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 STRINNov 23, 2024 · N506CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202501270094Skin · damagedTRANSFER 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 FASTENov 23, 2024 · N506CA · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2025012700123Stringer · damagedTRANSFER 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 STRINGENov 23, 2024 · N506CA · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA20240713Engine · shutdownAT 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 TRANSJul 13, 2024 · N506CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWI20240515000413Bracket · crackedAFT 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 REFERENCApr 30, 2024 · N506CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI20240515000412Bracket · crackedAFT 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) WApr 30, 2024 · N506CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI20240515000411Vane · damagedLH 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 2012-12-1Apr 30, 2024 · N506CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWI20240515000410Vane · chafedRH 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 2012-12-1Apr 30, 2024 · N506CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWI20240515000408Pressure Blkhd · gougedFWD 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 CHILDApr 24, 2024 · N506CA · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA202265543None · crackedFO 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 WINDOApr 29, 2022 · N506CA · Cndair CL6002B19 · Window/Windshield SystemSDR SWIA202265442None · damagedTRANSFER 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 HORIZONTApr 11, 2022 · N506CA · Cndair CL6002B19 · Horizontal Stabilizer, Plate/SkinSDR SWIA202156358Anchor Fitting · corrodedWHILE 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 Jan 30, 2021 · N506CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202156357Control Rod · corrodedLEFT 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 CHECJan 24, 2021 · N506CA · Cndair CL6002B19 · Elevator Control SystemSDR SWIA202156311Structure · chafedCHAFFING 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 51-9Jan 19, 2021 · N506CA · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA202156305Stringer · damagedFOUND 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 SJan 19, 2021 · N506CA · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA202156323Floor Support · corrodedFLOOR 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 51-900-1Jan 17, 2021 · N506CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202156322Skin · dentedDENT 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.Jan 16, 2021 · N506CA · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202156321Floorbeam · damagedFOUND 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.Jan 11, 2021 · N506CA · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202156363Skin · damagedCAMP 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 FJan 3, 2021 · N506CA · Cndair CL6002B19 · Elevator, Plate/SkinSDR SWIA202156314Skin · damagedRIGHT 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 MAJORJan 3, 2021 · N506CA · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA202156366Cap · brokenRIGHT 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 Jan 2, 2021 · N506CA · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA202056320Pan · corrodedSERVICE 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, CDec 24, 2020 · N506CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202056355Bolt · corrodedWHILE 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.Dec 23, 2020 · N506CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202056354Bolt · corrodedWHILE 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.Dec 23, 2020 · N506CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202056353Rod End · corrodedLEFT 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).Dec 23, 2020 · N506CA · Cndair CL6002B19 · AileronsSDR SWIA202056326Angle · crackedOBLIQUE 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.Dec 23, 2020 · N506CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202056315Skin · damagedRIGHT 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 SKDec 22, 2020 · N506CA · Cndair CL6002B19 · Elevator, Plate/SkinSDR SWIA202056306Hinge Fitting · gougedRIGHT 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.Dec 22, 2020 · N506CA · Cndair CL6002B19 · AileronsSDR SWIA202056304Skin · damagedRIGHT 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. WEIDec 22, 2020 · N506CA · Cndair CL6002B19 · Elevator, Plate/SkinSDR SWIA202056352Skin · corrodedVERTICAL 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.Dec 20, 2020 · N506CA · Cndair CL6002B19 · Vertical Stabilizer, Plate/SkinSDR SWIA202056351Stop Fitting · corrodedFORWARD 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.Dec 19, 2020 · N506CA · Cndair CL6002B19 · Service DoorsSDR SWIA202056350Seat Track · corrodedRIGHT 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.Dec 19, 2020 · N506CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202056349Seat Track · corrodedLEFT 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.Dec 19, 2020 · N506CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202056348Seat Track · corrodedLEFT 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.Dec 19, 2020 · N506CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202056347Seat Track · corrodedLEFT 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. Dec 19, 2020 · N506CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202056346Seat Track · corrodedRIGHT 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 53-01-11-40Dec 19, 2020 · N506CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
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