# Service difficulty reports: N468CA

A list on [N468CA](https://openairdocs.org/aircraft/N468CA.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 · 131 reports

- [SDR SWIA202155256](https://openairdocs.org/sdr/SWIA202155256.md): Skin · cracked · Jan 5, 2021 · N468CA · Cndair CL6002B19 · Wing, Plate/Skin
  > TRANSFER FROM EAML 554862. DAMAGE TO RIGHT WING TRAILING EDGE ROUGHLY 4 & 7/16" LONG CRACK & SPLIT IN THE TRAILING EDGE OF RT WINGLET & EXTENDS TO 1/2" MAX AROUND TO OUTBOARD SIDE OF WINGLET. DAMAGE IS OUT OF SRM LIMITS. REMOVED AND REPLACED THE RT LOWER OU
- [SDR SWIA202052789](https://openairdocs.org/sdr/SWIA202052789.md): Warning Message · illuminated · Sep 28, 2020 · N468CA · Cndair CL6002B19 · Cabin Cooling System
  > LEFT PACK HI PRESS AFTER TAKEOFF WHEN SWAPPING BLEEDS. FILED CLOSED RO 9/26/2020. DEFERRED LT PACK, PER MEL, DUE TO RT PACK BEING ALREADY DEFERRED. MAINT ACTION COMPLIED WITH. PLACARD INSTALLED.
- [SDR SWIA2020033049549](https://openairdocs.org/sdr/SWIA2020033049549.md): Angle · cracked · Mar 13, 2020 · N468CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > UPON REMOVAL FOR FOM FOUND CRACK IN ANGLE - FS280.00 STGR3L. (C-CHECK) RO 3/26/2020 REMOVED AND INSTALLED NEW ANGLE AT FS 280.00 STGR 3L REF. BOMBARDIER DWG. CRJ 200 SRM & COMPLIED WITH TASK CARD.
- [SDR SWIA2020033049537](https://openairdocs.org/sdr/SWIA2020033049537.md): Stringer Splice · cracked · Mar 13, 2020 · N468CA · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > FS280.00 AT STGR 3L, OUTBOARD STRINGER SPLICE ANGLE IS CRACKED (C-CHECK) RO 3/26/2020 REMOVED AND REPLACED THE FS280 STR3L OTBD SPLICE ANGLE REF CRJ200 SRM, BOMBARDIER DRAWING. COMPLIED WITH ST, LEAK CHECKS GOOD.
- [SDR SWIA2020033049535](https://openairdocs.org/sdr/SWIA2020033049535.md): Stringer Splice · cracked · Mar 12, 2020 · N468CA · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > FS280.00 AT STGR 3L, INBOARD STRINGER SPLICE ANGLE IS CRACKED (C-CHECK) RO 3/26/2020 REMOVED AND REPLACED THE FS280 STR3L INBD SPLICE ANGLE REF CRJ200 SRM, BOMBARDIER DRAWING. COMPLIED WITH ST, LEAK CHECKS GOOD.
- [SDR SWIA2020033049534](https://openairdocs.org/sdr/SWIA2020033049534.md): Fitting · cracked · Mar 12, 2020 · N468CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS280 BEAM/FLOOR SUPPORT BEAM CLIP CRACKED, O/B LBL9. (C-CHECK) RO 3/26/2020 REMOVED AND REPLACED FS 280 FLOOR BEAM CLIP AT OTBD AT LBL9 WITH NEW CLIP REF REO 601R-53-11-926 REV -B DATED 2006-05-10. SEE CONTINUE CARD FOR FUTHER DTAILS. COMPLIED WITH 51-900
- [SDR SWIA2020033049533](https://openairdocs.org/sdr/SWIA2020033049533.md): Fitting · cracked · Mar 12, 2020 · N468CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS280 BEAM/FLOOR SUPPORT BEAM CLIP CRACKED, I/B LBL9.REMOVED AND REPLACED FS 280 FLOOR BEAM CLIP AT INBD AT LBL9 WITH NEW CLIP REF REO 601R-53-11-926 REV -B DATED 2006-05-10. SEE CONTINUE CARD FOR FUTHER DTAILS COMPLIED WITH 51-900-1003-SKY.
- [SDR SWIA2020033049532](https://openairdocs.org/sdr/SWIA2020033049532.md): Fitting · cracked · Mar 12, 2020 · N468CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS280 BEAM/FLOOR SUPPORT BEAM CLIP CRACKED, O/B RBL9. (C-CHECK) RO 3/26/2020 REMOVED AND REPLACED FS 280 FLOOR BEAM CLIP AT OTBD AT RBL9 WITH NEW CLIP REF REO. SEE CONTINUE CARD FOR FUTHER DTAILS COMPLIED WITH.
- [SDR SWIA2020033049530](https://openairdocs.org/sdr/SWIA2020033049530.md): Fitting · cracked · Mar 12, 2020 · N468CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS280 BEAM/FLOOR SUPPORT BEAM CLIP CRACKED, I/B RBL9. (C-CHECK) RO 3/26/2020 REMOVED AND REPLACED FS 280 FLOOR BEAM CLIP AT INBD AT RBL9 WITH NEW CLIP REF REO. SEE CONTINUE CARD FOR FUTHER DTAILS COMPLIED WITH.
- [SDR SWIA2020033049529](https://openairdocs.org/sdr/SWIA2020033049529.md): Post · cracked · Mar 12, 2020 · N468CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS409+128 LBL27 VERTICAL POST CRACKED AT THE INBOARD AFT LOWER RIVET. (C-CHECK) RO 3/26/2020 REMOVED AND REPLACED THE FS409+128 LBL27 VERTICAL POST REF BOMBARDIER REO. COMPLIED WITH ST, LEAK CHECKS GOOD.
- [SDR SWIA2020033049528](https://openairdocs.org/sdr/SWIA2020033049528.md): Post · cracked · Mar 12, 2020 · N468CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS409+128 LBL18 VERTICAL POST CRACKED AT THE OUTBOARD AFT LOWER RIVET (C-CHECK) RO 3/26/2020 REMOVED AND REPLACED THE FS409+128 LBL18 VERITCAL POST REF BOMBARDIER REO. COMPLIED WITH ST, LEAK CHECKS GOOD.
- [SDR SWIA2020033049526](https://openairdocs.org/sdr/SWIA2020033049526.md): Post · cracked · Mar 12, 2020 · N468CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS409+128 RBL27 VERTICAL POST CRACKED AT THE INBOARD AFT LOWER RIVET. (C-CHECK) RO 3/26/2020 REMOVED AND REPLACED THE FS409+128 RBL27 VERTICAL POST REF BOMBARDIER REO. COMPLIED WITH ST, LEAK CHECKS AND OP CHECKS GOOD.
- [SDR SWIA2020033049525](https://openairdocs.org/sdr/SWIA2020033049525.md): Stiffener · cracked · Mar 7, 2020 · N468CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > PRESSURE BILKHEAD AFT OF F/S 621.0 STIFFENER P/N 601R36008-51 IS CRACK (C-CHECK) RO 3/26/2020 REMOVED AND REPLACED THE FS621 STIFFENER REF BOMBARDIER DRAWING. COMPLIED WITH ST. LEAK CHECKS GOOD.
- [SDR SWIA2020033049571](https://openairdocs.org/sdr/SWIA2020033049571.md): Seat Track · corroded · Mar 4, 2020 · N468CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT RAIL RBL9 FS399-FS409+128 HAS CORROSION AROUND FASTENER HOLES. (C-CHECK) RO 3/26/2020 REMOVED AND REPLACED FLOOR SEAT RAIL FS399 - FS409+128 RBL9 REF CRJ200 AMM
- [SDR SWIA2020033049524](https://openairdocs.org/sdr/SWIA2020033049524.md): Floorbeam · out of limits · Mar 3, 2020 · N468CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > INBOARD FLANGE OF RBL9 FLOOR BEAM CAP AT FS409+98-FS409+104 FOUND TO BE OUT OF LIMITS ON JOB 2764961 OP 298 CAMP# 20550130, AND REQUIRES REPAIR. (C-CHECK) RO 3/26/2020 REPAIRED INBOARD FLANGE OF RBL9 FLOOR BEAM CAP AT FS409+98-FS409+104 REF. CRJ 200 SRM. T
- [SDR SWIA2020033049523](https://openairdocs.org/sdr/SWIA2020033049523.md): Floorbeam · out of limits · Mar 3, 2020 · N468CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > INBOARD FLANGE OF RBL9 FLOOR BEAM CAP AT FS409+71 FOUND TO BE OUT OF LIMITS ON JOB 2764961 OP 298 CAMP# 20550130, AND REQUIRES REPAIR.REPAIRED INBOARD FLANGE OF RBL9 FLOOR BEAM CAP AT FS409+71 REF. CRJ 200 SRM. TASK CARD COMPLIED WITH.
- [SDR SWIA2020033049522](https://openairdocs.org/sdr/SWIA2020033049522.md): Floorbeam · out of limits · Mar 3, 2020 · N468CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > INBOARD FLANGE OF RBL9 FLOOR BEAM CAP AT FS409+5-FS409+26 FOUND TO BE OUT OF LIMITS ON JOB 2764961 OP 298 CAMP# 20550130, AND REQUIRES REPAIR. (C-CHECK) RO 3/26/2020 REPAIRED RBL9 FLOOR BEAM CAP AT FS409+5-FS409+26 REF. CRJ 200 SRM REPAIR. TASK CARD COMPLI
- [SDR SWIA2020033049573](https://openairdocs.org/sdr/SWIA2020033049573.md): Support Angle · corroded · Feb 27, 2020 · N468CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *CORROSION SUPPORT ANGLES CORRODED AT FASTENER LOCATIONS ON INBD SIDE OF FLOORBEAM FROM FS 409.00 - 406.00+96 AT RBL 9 (MARKED) (C-CHECK) RO 3/26/2020 CORROSION ON RBL9 FLOOR BEAM INBOARD FLANGE FOUND TO BE OUT OF LIMITS REF. CRJ 200 SRM. REFERENCE THE FO
- [SDR SWIA2020033049521](https://openairdocs.org/sdr/SWIA2020033049521.md): Floorbeam · corroded · Feb 27, 2020 · N468CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > *CORROSION SUPPORT ANGLES CORRODED AT FASTENER LOCATIONS ON INBD SIDE OF FLOORBEAM FROM FS 409.00 - 406.00+96 ST LBL 9 (MARKED)REMOVED AND INSTALLED NEW FLOOR BEAM FROM 409.00 - 409 +96 AT LBL 9 REF, BOMBARDIER DWG. CRJ 200 SRM. COMPLIED WITH TASK CARD
- [SDR SWIA2020033049520](https://openairdocs.org/sdr/SWIA2020033049520.md): Frame · cracked · Feb 26, 2020 · N468CA · Cndair CL6002B19 · Fuselage Main, Frame
  > *FS 333 AT STR 1R FRAME CRACKED (C-CHECK) RO 3/26/2020 REMOVED AND REPLACED THE FS333 FRAME STR1R REF CRJ200 SRM, SRM, BOMBARDIER DRAWING. COMPLIED WITH ST, LEAK CHECKS GOOD.
- [SDR SWIA2020033049516](https://openairdocs.org/sdr/SWIA2020033049516.md): Floor Support · corroded · Feb 25, 2020 · N468CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *CORROSION AROUND HOLE ON LH FLOOR SUPPORT BEAM AT FS 349.00, BL 20 (MARKED) (C-CHECK) RO 3/26/2020 COMPLIED WITH PERMANENT REPAIR CORROSION AROUND HOLE ON LH FLOOR SUPPORT BEAM AT FS 349.00, BL 20 REF REO, VERIFIED ALL STEPS COMPLIED WITH, COMPLETED TASK
- [SDR SWIA2020033049515](https://openairdocs.org/sdr/SWIA2020033049515.md): Former · corroded · Feb 24, 2020 · N468CA · Cndair CL6002B19 · Passenger/Crew Doors
  > FOUND CORROSION ON PAX DOOR AFT FORMER. (C-CHECK) RO 3/26/2020 --BLENDED CORROSION ON THE PAX DOOR AFT FORMER "OUT OF LIMITS" REF CRJ200 SRM (ORIGINAL:.063) - (REMAINING:.058) - (LOSS:.005). --REMOVED AND REPLACED PAX DOOR AFT FORMER REF CRJ200 SRM, BOM
- [SDR SWIA2020033049514](https://openairdocs.org/sdr/SWIA2020033049514.md): Skin · cracked · Feb 21, 2020 · N468CA · Cndair CL6002B19 · Wing, Plate/Skin
  > RH WING PLANK ACCESS HOLE FOR PANEL 650BB IS CRACKED ON INNER EDGE. (C-CHECK) RO 3/26/2020 BLENDED CORROSION AT RH WING PLANK ACCESS HOLE 650BB REF BOMBARDIER REO, REO. ROTO PEENED AND RESTORED FINISH. ALL CHECKS GOOD. COMPLETED TASK CARD, WEIGHT CHANGE
- [SDR SWIA2020033049557](https://openairdocs.org/sdr/SWIA2020033049557.md): Hinge Arm · cracked · Feb 20, 2020 · N468CA · Cndair CL6002B19 · Emergency Exits
  > * CREW ESCAPE HATCH HAS SUSPECT CRACK AT HINGE ARM.(MARKED) (C-CHECK) RO 3/26/2020 REMOVED AND REPLACED HINGE ARM REF SRM
- [SDR SWIA2020033049555](https://openairdocs.org/sdr/SWIA2020033049555.md): Support Fitting · cracked · Feb 20, 2020 · N468CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *RH WINDSHIELD SIDE POST BOTTOM SUPPORT AFT SIDE, POSSIBLE CRACK (MARKED) (C-CHECK) RO 3/26/2020 REMOVED DAMAGE SUPPORT FITTING, RECEIVED LOCATED DRILLED AND INSTALLED NEW RH WINDSHIELD SIDE POST BOTTOM SUPPORT AFT SIDE, FITTING.REF CRJ200 SRM.
- [SDR SWIA2020033049510](https://openairdocs.org/sdr/SWIA2020033049510.md): Hinge · chafed · Feb 20, 2020 · N468CA · Cndair CL6002B19 · Rudder Structure
  > *RUDDER UPPER CENTER HINGE CHAFFED ON RUDDER SIDE (C-CHECK) RO 3/26/2020 BLENDED THE CHAFFED AREA OF THE RUDDER UPPER CENTER HINGE, NDT'ED REPAIR, ROTO PEENED THE HINGE AND RESTORE THE FINISH. COMPLIED WITH ALL STEPS OF REO.REF REO.
- [SDR SWIA2020033049509](https://openairdocs.org/sdr/SWIA2020033049509.md): Hinge Fitting · chafed · Feb 20, 2020 · N468CA · Cndair CL6002B19 · Rudder Structure
  > *RUDDER UPPER CENTER HINGE ON ACFT SIDE CHAFFED (C-CHECK) RO 3/26/2020 BLENDED CHAFE ON UPPER CENTER RUDDER HINGE FITTING, AIRCRAFT SIDE. STRUCTURALLY ACCEPTABLE. REF. BOMBARDIER REO. RESTORED FINISH, NO DEFECTS NOTED, BLENDED AREA L=.700" X W=.275" X D=.0
- [SDR SWIA2020033049508](https://openairdocs.org/sdr/SWIA2020033049508.md): Intercostal · corroded · Feb 20, 2020 · N468CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *INTERCOSTAL AT FS 310 LH SIDE FWD OF PAX DOOR CORRODED (C-CHECK) RO 3/26/2020 REMOVED AND REPLACED THE LH FS310 INTERCOSTAL FWD OF PAX DOOR REF CRJ200 SRM, BOMBARDIER DRAWING. LEAK CHECKS GOOD. COMPLIED WITH ST.
- [SDR SWIA2020033049569](https://openairdocs.org/sdr/SWIA2020033049569.md): Fastener · corroded · Feb 19, 2020 · N468CA · Cndair CL6002B19 · Spoilers
  > *LH WING INBD FLIGHT SPOILER OUTBD HINGE HARDWARE CORRODED (C-CHECK) RO 3/26/2020 INSTALLED 1 EACH NEW SERVICEABLE SHIM ( TEFLON PAD) AT L/H WING FLIGHT SPOILER, OTBD SIDE. REF. CRJ 200 AMM
- [SDR SWIA2020033049567](https://openairdocs.org/sdr/SWIA2020033049567.md): Fastener · corroded · Feb 19, 2020 · N468CA · Cndair CL6002B19 · Spoilers
  > *LH WING OUTBD GROUND SPOILER INBD AND OUTBD HINGE HARDWARE CORRODED (C-CHECK) RO 3/26/2020 REMOVED AND REPLACED R/H WING OTBD GROUND SPOILER OTBD AND INBD HINGE HARDWARE. REF. CRJ 200 AMM. OPERATIONAL TEST GOOD AT THIS TIME, NO DEFECTS NOTED.
- [SDR SWIA2020033049565](https://openairdocs.org/sdr/SWIA2020033049565.md): Fastener · corroded · Feb 19, 2020 · N468CA · Cndair CL6002B19 · Spoilers
  > *LH WING INBD GROUND SPOILER PCU UPPER LINK HARDWARE CORRODED (C-CHECK) RO 3/26/2020 CLEANED AND INSPECTED LEFT WING INBOARD GROUND SPOILER PCU LINK HARDWARE. NO CORROSION NOTED. CHECKED GOOD. REF CRJ 200 SRM.
- [SDR SWIA2020033049564](https://openairdocs.org/sdr/SWIA2020033049564.md): Fastener · corroded · Feb 19, 2020 · N468CA · Cndair CL6002B19 · Spoilers
  > *RH WING OUTBD GROUND SPOILER INBD END HINGE HARDWARE CORRODED (C-CHECK) RO 3/26/2020 REMOVED AND REPLACED THE NUT WASHER AND COTTER PIN WITH NEW REF AMM, SYSTEM OPS CHECK GOOD.
- [SDR SWIA2020033049562](https://openairdocs.org/sdr/SWIA2020033049562.md): Fastener · corroded · Feb 19, 2020 · N468CA · Cndair CL6002B19 · Spoilers
  > RH WING FLT SPOILER INBD HINGE HARDWARE CORRODED (C-CHECK) RO 3/26/2020 REMOVED AND REPLACED R/H WING FLIGHT SPOILER INBOARD HINGE HARDWARE. REF. CRJ 200 AMM. OPERATIONAL TEST GOOD AT THIS TIME, NO DEFECTS NOTED.
- [SDR SWIA2020033049558](https://openairdocs.org/sdr/SWIA2020033049558.md): Support Channel · cracked · Feb 19, 2020 · N468CA · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > *CARGO DOOR FWD BOTTOM TRACK SUPPORT IS CRACKED (MARKED) (C-CHECK) RO 3/26/2020 REPLACED CARGO DOOR FWD BOTTOM TRACK SUPPORT CHANNEL WITH NEW PN 601R35050-25 PO# T-52593 REF CRJ 200 SRM 51-42-06.
- [SDR SWIA2020033049505](https://openairdocs.org/sdr/SWIA2020033049505.md): Skin · damaged · Feb 19, 2020 · N468CA · Cndair CL6002B19 · Rudder, Plate/Skin
  > *RUDDER LOWER LEADING EDGE ON RH SIDE DAMAGED (C-CHECK) RO 3/26/2020 REMOVED AND REPLACED THE DAMAGED RH LOWER LE RUDDER SKIN REF CRJ200 SRM, BOMBARDIER DRAWING. RESTORED FINISH. COMPLIED WITH ST
- [SDR SWIA2020033049561](https://openairdocs.org/sdr/SWIA2020033049561.md): Skin · corroded · Feb 18, 2020 · N468CA · Cndair CL6002B19 · Passenger/Crew Doors
  > *CORROSION ON SKIN AT ALL SMALL ACCESS PANELS SCREW HOLES ON PAX DOOR (C-CHECK) RO 3/26/2020 --BLENDED CORROSION AROUND ACCESS PANEL SCREW HOLES 832AL & 832GL "OUT OF LIMITS" DUE TO COMPLETE MATERIAL LOSS (ORIGINAL:.040) - (REMAINING:.000) - (LOSS:.040
- [SDR SWIA2020033049504](https://openairdocs.org/sdr/SWIA2020033049504.md): Skin · dented · Feb 15, 2020 · N468CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > ADM #1293. FS 625.25 AND STR 15.75R RIGHT SIDE OF AIRCRAFT BELLOW ENGINE. FOUND TO BE A DENTED SCRATCH MEASURES 2.55 INCHES LONG AND.011 INCHES DEEP. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD AC
- [SDR SWIA202033049503](https://openairdocs.org/sdr/SWIA202033049503.md): Bulkhead · cracked · Jan 22, 2020 · N468CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: AD - COMPLY WITH PARAGRAPH (J) OF AD BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL (J)(2) MODIFYING THE RPB AND
- [SDR SWIA2019110846735](https://openairdocs.org/sdr/SWIA2019110846735.md): Vertical Support · cracked · Nov 8, 2019 · N468CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING NDT INSPECTION AT FS 409.0+128 VERTICAL POST AT BL 0.0 FOUND CRACKS AROUND RIVET ON RH STIFFENER AT FIRST RIVET ON STIFFENING STRAP. FIRST CRACK EXTENDING OUTWARD FROM RIVET VERTICALLY ALONG STIFFENER MEASURING L=0.117IN. SECOND CRACK EXTENDING FROM RIV
- [SDR SWIA2019071246054](https://openairdocs.org/sdr/SWIA2019071246054.md): Bypass Valve · failed · Jul 11, 2019 · N468CA · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > AFTER TAKE OFF, RECEIVED GEAR DISAGREE WARNING WITH NOSE GEAR NOT UP AND LOCKED. PERFORMED QRH PROCEDURE AND NOSE GEAR CAME DOWN & LOCKED WITH 3 GREEN. LANDED WITHOUT INCIDENT. (FLT#4249) FO: 07/12/2019 CLOSED REMOVED AND REPLACED MANUAL BYPASS NOSE DOOR VALVE
- [SDR SWIA2019032645661](https://openairdocs.org/sdr/SWIA2019032645661.md): Uplock · defective · Mar 26, 2019 · N468CA · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > RECEIVED GEAR DISAGREE WARNING MESSAGE AND NOSE GEAR WARNING MESSAGE. PERFORMED QRH PROCEDURE AND MESSAGES CLEARED. RETURNED TO FIELD. (FLT#3736) CLOSED REMOVED AND REPLACED UPLOCK PIN AND BRACKET IAW CMM. RIGGED UPLOCK PIN REF IAW AMM, OPS CHECK GOOD. PERFORM
- [SDR SWIA2018040544462](https://openairdocs.org/sdr/SWIA2018040544462.md): Warning Message · illuminated · Apr 4, 2018 · N468CA · Cndair CL6002B19 · Cabin Pressure Control System
  > CLIMBING THROUGH 25,000 FT, CABIN ALTITUDE CAUTION, THEN WARNING. RAN QRH. ALL MASKED DROPPED AND DONNED, EMERGENCY DESCENT.
- [SDR SWIA201844429](https://openairdocs.org/sdr/SWIA201844429.md): Control Handle · failed · Mar 27, 2018 · N468CA · Cndair CL6002B19 · Landing Gear Selector
  > RETURNED TO FIELD FOR GEAR NOT RETRACTING AFTER TAKEOFF. ALL GEAR WOULD NOT RETRACT BUT WAS INDICATING GREEN. REMOVED AND REPLACED THE LANDING GEAR CONTROL HANDLE IAW AMM. PERFORMED NUMEROUS GEAR SWINGS. OPS CHECKED GOOD.
- [SDR SWIA2017111543865](https://openairdocs.org/sdr/SWIA2017111543865.md): Tire · failed · Oct 10, 2017 · N468CA · Cndair CL6002B19 · Tire
  > NR 1 MAIN TIRE FAILED DURING TAKEOFF. EMERGENCY DECLARED. REMOVED AND REPLACED THE NR 1 AND 2 MLG WHEEL ASSEMBLIES.
- [SDR SWIA201439469](https://openairdocs.org/sdr/SWIA201439469.md): Door Sill · cracked · Sep 24, 2014 · N468CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CRACK FOUND ON CARGO DOOR SILL AT BS 605 AT AFT CARGO DOOR STOP. R & R CARGO DOOR SILL IAW REO.
- [SDR SWIA201439468](https://openairdocs.org/sdr/SWIA201439468.md): Floorbeam · cracked · Sep 24, 2014 · N468CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FOUR INCH CRACK ON BS 280 FLOORBEAM LOWER RADIUS FROM RBL 9 - 13. REPAIRED IAW REO.
- [SDR SWIA201439467](https://openairdocs.org/sdr/SWIA201439467.md): Floor Support · corroded · Sep 24, 2014 · N468CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT SIDE FUSELAGE, BS 559+96 - 574, FOUND CORROSION ON FLOOR SUPPORT AROUND NUTPLATE HOLES. BLENDED CORROSION IAW REO.
- [SDR SWIA201439466](https://openairdocs.org/sdr/SWIA201439466.md): Floor Support · corroded · Sep 23, 2014 · N468CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT SIDE FUSELAGE BS 589 - 605, FOUND CORROSION ON FLOOR SUPPORT AROUND NUTPLATE HOLES. BLENDED CORROSION IAW REO.
- [SDR SWIA201439465](https://openairdocs.org/sdr/SWIA201439465.md): Floor Support · corroded · Sep 23, 2014 · N468CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT SIDE FUSELAGE BS 559+80 - 574, FOUND CORROSION ON FLOOR SUPPORT AROUND NUTPLATE HOLES. BLENDED CORROSION IAW REO.
- [SDR SWIA201439464](https://openairdocs.org/sdr/SWIA201439464.md): Floor Support · corroded · Sep 23, 2014 · N468CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT SIDE FUSELAGE, BS 574 - 589, FOUND CORROSION ON FLOOR SUPPORT AROUND NUTPLATE HOLES. BLENDED CORROSION IAW REO.

Next page: https://openairdocs.org/aircraft/N468CA/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 = 'N468CA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N468CA/reports

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