# Service difficulty reports: N246PS

A list on [N246PS](https://openairdocs.org/aircraft/N246PS.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 4 · 172 reports

- [SDR SWIA2026040975682](https://openairdocs.org/sdr/SWIA2026040975682.md): Landing Gear · warning message · Apr 9, 2026 · N246PS · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGE AFTER TAKEOFF WHEN RAISING GEAR. RAN QRH AND MESSAGE WAS CLEARED. (FLIGHT 5029) TROUBLESHOT GEAR DISAGREE & NOSE DOOR OPEN WARNING MESSAGE AFTER TAKEOFF WHEN RAISING GEAR. RAN QRH AND MESSAGE WAS CLEARED. IAW F
- [SDR SWIA2026012475579](https://openairdocs.org/sdr/SWIA2026012475579.md): Floor Support · corroded · Jan 24, 2026 · N246PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT PRESSURE FLOOR SUPPORT IS CORRODED AT BS 511. REPAIRED THE LT PRESSURE FLOOR SUPPORT IAW REO 601R-53-41-666, REV C,
- [SDR SWIA202603275594](https://openairdocs.org/sdr/SWIA202603275594.md): Stiffener · cracked · Jan 23, 2026 · N246PS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT WEB POWER ASSIST MOTOR STIFFENER FOUND TO BE CRACK. REMOVED, DRILLED UP AND INSTALLED NEW PAX DOOR STIFFENER ON THE AFT WEB IAW SRM 51-40-11 AND 51-42-06.
- [SDR SWIA2026012375590](https://openairdocs.org/sdr/SWIA2026012375590.md): Bracket · elongated · Jan 23, 2026 · N246PS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD4 AFT BRACKET FOUND TO HAVE ELONGATED HOLE FROM PREVIOUS REPAIR. REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD4 AFT BRACKET IAW SRM 51-40-11, & 51-42-06.
- [SDR SWIA2026032775586](https://openairdocs.org/sdr/SWIA2026032775586.md): Tee Fitting · corroded · Jan 21, 2026 · N246PS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FITTING ASSEMBLY COMMON TO BS 621 BULKHEAD, LBL 27, FLOORBEAM CAP HAS CORROSION ON TOP OTBD FLANGE. REMOVED AND REPLACED THE TEE FITTING IAW 51-42-06, 51-42-21, 51-42-22, 51-41-02, 51-40-11, 51-42-36, 51-45-00, 51-42-15, & 51-25-16.
- [SDR SWIA2026032775588](https://openairdocs.org/sdr/SWIA2026032775588.md): Floor Support · corroded · Jan 19, 2026 · N246PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO FLOOR SUPPORT CAP AT LBL 27, BETWEEN BS 574 - 621 HAS MULTIPLE AREAS OF CORROSION. REMOVED AND FABRICATED A FLOOR SUPPORT IAW SRM 51-24-36, AND 51-40-11. AND INSTALLED CARGO IAW REO 601R-53-61-3778, REV B.
- [SDR SWIA2026011875591](https://openairdocs.org/sdr/SWIA2026011875591.md): Fitting · cracked · Jan 18, 2026 · N246PS · Cndair CL6002B19 · Fuselage Main, Structure
  > WINDSHIELD CENTER POST LOWER LT FITTING IS CRACKED. REPLACED WINDSHIELD CENTER POST LOWER LH FITTING IAW SRM 51-42-21
- [SDR SWIA2026032775583](https://openairdocs.org/sdr/SWIA2026032775583.md): Fitting · cracked · Jan 18, 2026 · N246PS · Cndair CL6002B19 · Fuselage Main, Structure
  > WINDSHIELD CENTER POST LOWER RT FITTING IS CRACKED. REPLACED THE WINDSHIELD CENTER POST LOWER FITTING IAW SRM 51-42-21. MAJOR REPAIR.
- [SDR SWIA2026011875578](https://openairdocs.org/sdr/SWIA2026011875578.md): Intercostal · corroded · Jan 18, 2026 · N246PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > MAIN AVIONICS BAY, INTERCOSTAL AT BS 394 - 409 BETWEEN STRINGERS 26R & 27R HAS TWO AREAS OF MINOR CORROSION AND INTERCOSTAL AREA MINOR CORROSION. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06 & 51-42-21.
- [SDR SWIA2026032775577](https://openairdocs.org/sdr/SWIA2026032775577.md): Stringer · cracked · Jan 18, 2026 · N246PS · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STRINGER 3L IS CRACKED AT AFT SIDE OF BS 280. PERFORMED A MAJOR REPAIR BY REMOVING AND REPLACING 2 EA 3L SPLICE ANGLES AT AFT SIDE OF FS 280 IAW SRM 51-42-06 AND 51-40-11 REV.399. MAJOR REPAIR.
- [SDR SWIA202603275599](https://openairdocs.org/sdr/SWIA202603275599.md): Former · corroded · Jan 15, 2026 · N246PS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FWD FORMER FOUND TO BE CORRODED. REMOVED AND REPLACED PAX DOOR FWD UPPER FORMER IAW SRM 51-42-06, 51-42-21, AND 51-40-11.
- [SDR SWIA2026011575598](https://openairdocs.org/sdr/SWIA2026011575598.md): Skin · chafed · Jan 15, 2026 · N246PS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > RIGHT WING HAS CHAFING ON LOWER WING PLANK AT RBL 45 FROM CONTACT WITH BELLY FAIRING 193AB. REPAIRED THE RT WING LOWER WING PLANK AT RBL 45 IAW REO 601R-57-21-880, REV D.
- [SDR SWIA2026011575597](https://openairdocs.org/sdr/SWIA2026011575597.md): Intercostal · corroded · Jan 15, 2026 · N246PS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR MID DD4 INTERCOSTAL FOUND TO BE CORRODED REQUIRES REPLACEMENT. REMOVED AND REPLACED PAX DOOR MID DD4 INTERCOSTAL IAW SRM 51-42-06. & 51-40-11.
- [SDR SWIA202603275596](https://openairdocs.org/sdr/SWIA202603275596.md): Former · corroded · Jan 15, 2026 · N246PS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT FORMER FOUND TO BE CORRODED REQUIRES REPLACEMENT. REMOVED AND REPLACED AFT FORMER IAW SRM 51-42-06, 51-40-11, 51-42-13 AND 51-42-21.
- [SDR SWIA2026011575592](https://openairdocs.org/sdr/SWIA2026011575592.md): Hinge · damaged · Jan 15, 2026 · N246PS · Cndair CL6002B19 · Fuselage, Door Hinge
  > PAX DOOR HINGE HAS ELONGATED HOLE AFT SIDE FIRST LUG REQUIRES EVALUATION REPAIRED ELONGATED HOLE IAW REO 601R-52-11-3078 REV -.
- [SDR SWIA2026011575589](https://openairdocs.org/sdr/SWIA2026011575589.md): Intercostal · corroded · Jan 15, 2026 · N246PS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR MID DD6 INTERCOSTAL FOUND TO BE CORRODED. REMOVED AND REPLACED PAX DOOR MID INTERCOSTAL IAW SRM 51-42-06, 51-42-21, & 51-40-11.
- [SDR SWIA2026032775585](https://openairdocs.org/sdr/SWIA2026032775585.md): Intercostal · corroded · Jan 15, 2026 · N246PS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT DD4 INTERCOSTAL FOUND TO BE CORRODED. REMOVED AND REPLACED PAX DOOR INTERCOSTAL IAW SRM 51-40-11,& 51-42-06.
- [SDR SWIA2026011575584](https://openairdocs.org/sdr/SWIA2026011575584.md): Intercostal · cracked · Jan 15, 2026 · N246PS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT DD1 INTERCOSTAL FOUND TO BE CRACKED. REMOVED AND REPLACED PAX DOOR AFT INTERCOSTAL IAW SRM 51-42-06, & 51-40-11.
- [SDR SWIA2026011575581](https://openairdocs.org/sdr/SWIA2026011575581.md): Intercostal · corroded · Jan 15, 2026 · N246PS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR MID DD2 INTERCOSTAL FOUND TO BE CORRODED. REMOVED AND REPLACED THE PAX DOOR THE INTERCOSTAL IAW CRJ 200 SRM 51-42-06, & 51-42-21, 51-40-11.
- [SDR SWIA2026032775580](https://openairdocs.org/sdr/SWIA2026032775580.md): Intercostal · corroded · Jan 15, 2026 · N246PS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT DD5 INTERCOSTAL FOUND TO BE CORRODED. REMOVED AND INSTALLED A NEW PAX DOOR AFT DD5 INTERCOSTAL IAW SRM 51-40-11, AND 51-42-06.
- [SDR SWIA2026011575576](https://openairdocs.org/sdr/SWIA2026011575576.md): Intercostal · corroded · Jan 15, 2026 · N246PS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR MID DD3 INTERCOSTAL FOUND TO BE CORRODED REQUIRES REPLACEMENT REMOVED AND REPLACED PAX DOOR DD3 MID INTERCOSTAL IAW SRM 51-42-06. 51-42-21, & 51-40-11.
- [SDR SWIA2026010675593](https://openairdocs.org/sdr/SWIA2026010675593.md): Hinge · chafed · Jan 6, 2026 · N246PS · Cndair CL6002B19 · Fuselage, Door Hinge
  > PAX DOOR, FUSELAGE SIDE HINGE HALF HAS CHAFE DAMAGE AT 4TH, 6TH AND 8TH LUGS FROM THE FRONT AND GOUGE DAMAGE AT THE LAST LAND FROM CONTACT WITH ROLL PIN. REMOVED / REPLACED PAX DOOR HINGE HALF IAW SRM 53-21-23.
- [SDR SWIA202603275595](https://openairdocs.org/sdr/SWIA202603275595.md): Skin · dented · Jan 4, 2026 · N246PS · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP HAS 1 DENT, MID CHORD AT APPROX. F.L.S. 75.00. REPAIRED THE LT INBD FLAP MID CHORD AT APPROX FLS 75.00 IAW REO 601R-57-52-678, REV C.
- [SDR SWIA2026032775582](https://openairdocs.org/sdr/SWIA2026032775582.md): Skin · dented · Dec 24, 2025 · N246PS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > PROTUDING DENT IN FUSELAGE EXTERNAL SKIN BETWEEN BS 280 TO 295, STGR 24L TO 25L. REPAIRED THE SKIN IAW REO 601R-53-21-3783, REV-, SRM 51-42-06, 51-42-21, & 51-25-01.
- [SDR SWIA2025122275587](https://openairdocs.org/sdr/SWIA2025122275587.md): Skin · dented · Dec 22, 2025 · N246PS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > TWO DENTS LOCATED RIGHT SIDE OF NOSE SKIN JUST ABOVE RT NLG FWD DOOR AND TO THE RIGHT OF GPU ACCESS DOOR: DENT 1 MEASURES -.02 IN DEPTH,0.8 IN WIDTH, DENT 2 MEASURES - 1" L X 1" W X.03" D. REMOVED AND REPLACED RIGHT SIDE NOSE SKIN IAW SRM 51-42-06, 51-40-1
- [SDR SWIA2026032775575](https://openairdocs.org/sdr/SWIA2026032775575.md): Skin · dented · Sep 18, 2025 · N246PS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > COMPLY WITH PERMANENT REPAIR ON RA ID: 94891PER TEMP REPAIR REO 601R-53-61-8247 REV-, DENT WITH BLENDED SCRATCH DAMAGE ON FUSELAGE SKIN BETWEEN FS605.00 - FS 621.00 NEAR STGR 19L IS STRUCTURALLY ACCEPTABLE FOR 1200 FH FROM THE TIME OF INCORPORATION OF THIS REO
- [SDR SWIA202507030617](https://openairdocs.org/sdr/SWIA202507030617.md): Warning Message · illuminated · Jun 17, 2025 · N246PS · Cndair CL6002B19 · Engine Thrust Reverser
  > D:R REV UNLOCKED CAUTION MESSAGE APPEARED TWICE IN FLIGHT AFTER TAKEOFF AND WENT AWAY AFTER A COUPLE SECONDS BOTH TIMESC: MEL 78-30-1CAT C DUE ON 06/27/2025NOTE: DUE TO ODI RTF, SMOD APPROVAL IS REQUIRED BEFORE RTS.R REV UNLOCKED CAUTION MESSAGE APPEARED TWICE
- [SDR SWIA202506180017](https://openairdocs.org/sdr/SWIA202506180017.md): Warning Message · false activation · Jun 17, 2025 · N246PS · Cndair CL6002B19 · Engine Thrust Reverser
  > D:R REV UNLOCKED CAUTION MESSAGE APPEARED TWICE IN FLIGHT AFTER TAKEOFF AND WENT AWAY AFTER A COUPLE SECONDS BOTH TIMESC: MEL 78-30-1CAT C DUE ON 06/27/2025NOTE: DUE TO ODI RTF, SMOD APPROVAL IS REQUIRED BEFORE RTS.R REV UNLOCKED CAUTION MESSAGE APPEARED TWICE
- [SDR SWIA202502140009](https://openairdocs.org/sdr/SWIA202502140009.md): Fuel Sys · leaking · Feb 9, 2025 · N246PS · Cndair CL6002B19 · Fuel Controlling System
  > R FUEL LO PRESS CAUTION MESSAGE ON APPROACH. DECIDED TO CONTINUE FOR LANDING. NOTICED A SMELL OF JET FUEL AND A FUEL IMBALANCE OF OVER 1000 POUNDS ABOUT A MINUTE PRIOR TO LANDING. (FLIGHT 5861 - FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA2024121701368](https://openairdocs.org/sdr/SWIA2024121701368.md): Warning Message · false activation · Dec 16, 2024 · N246PS · Cndair CL6002B19 · Landing Gear Door Actuator
  > AFTER TAKEOFF. GEAR DISAGREE. NOSE WHEEL DID NOT SHOW UP. FOLLLOWED QRH. OPS NORMAL (FLIGHT 5736 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 29325778 WITH THE FOLLOWING CORRECTIVE ACTION: "SEE CAMP CP 29325888 FOR FDR DOWNLOAD. SEE CAMP
- [SDR SWIA20241203001](https://openairdocs.org/sdr/SWIA20241203001.md): Window · cracked · Dec 3, 2024 · N246PS · Cndair CL6002B19 · Flight Compartment Windows
  > LEFT WINDSCREEN CRACKED ENTIRELY IN THE CRUISE. FOLLOWED QRH. (FLIGHT 5197 - FILED CLOSED) REMOVED AND REPLACED CA SIDE WINDOW PER CRJ 200 AMM 56-12-01-000-801 AND 56-12-01-400-801. REF TASK CARD 56-220-1000-SKY FOR WORK ACCOMPLISHED. LEAK CHECK GOOD AT
- [SDR SWI2024F01279](https://openairdocs.org/sdr/SWI2024F01279.md): Flap System · failed · Nov 19, 2024 · N246PS · Cndair CL6002B19 · Trailing Edge Flap Control System
  > D: DUE TO FLAP FAIL EVENT, COMPLY WITH AD 2009-06-12 WITHIN 10 FLIGHT CYCLES. REFERENCE FORM M-267A.C: MCI*** REVIEW PREVIOUS HISTORY ***FLAPS FAILS CAUTION MESSAGE DURING APPROACH. FLAPS DID NOT EXTEND PAST 0. (FLIGHT 5367 - FILED CLOSED) NOV 19, 2024
- [SDR SWIA20241116](https://openairdocs.org/sdr/SWIA20241116.md): Flap System · failed · Nov 16, 2024 · N246PS · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > EXTERNAL DAMAGE TO FUSELAGE SKIN AT FR. FS379.00 STGR 20L MARKED (C-CHECK RO 04/30/2025) PERFORMED EXTERNAL DOUBLER REPAIR ON FUSELAGE SKIN AT FS379.00 BETWEEN STGR-19L THRU STGR-21L PER CRJ200 SRM 53-00-31. PERFORMED LEAK CHECK OF DOUBLER REPAIR PER CRJ200 A
- [SDR SWIA20241115024](https://openairdocs.org/sdr/SWIA20241115024.md): Access Panel · corroded · Oct 24, 2024 · N246PS · Cndair CL6002B19 · Wing, Plate/Skin
  > FOUND POSSIBLE CORROSION ON THE LEFT WING FUEL ACCESS HOLE 510AB ON THE FWD AND INBOARD LIP. (MARKED WITH TAPE) (FILED CLOSED) REPAIRED CORROSION DAMAGE ON FUEL ACCESS PANEL OPENING 510AB ON THE FWD AND INBOARD LIP WITH REFERENCE TO REO 601R-57-21-030 R
- [SDR SWIA20241108024](https://openairdocs.org/sdr/SWIA20241108024.md): Skin · corroded · Oct 24, 2024 · N246PS · Cndair CL6002B19 · Wing, Plate/Skin
  > FOUND POSSIBLE CORROSION ON THE LEFT WING FUEL ACCESS HOLE 510AB ON THE FWD AND INBOARD LIP. (MARKED WITH TAPE) (FILED OPEN) REPAIRED CORROSION DAMAGE ON FUEL ACCESS PANEL OPENING 510AB ON THE FWD AND INBOARD LIP WITH REFERENCE TO REO 601R-57-21-030 REV
- [SDR SWI2024F01253](https://openairdocs.org/sdr/SWI2024F01253.md): Access Panel · corroded · Oct 23, 2024 · N246PS · Cndair CL6002B19 · Wing, Plate/Skin
  > POSSIBLE CORROSION ON RIGHT WING FUEL ACCESS HOLE 640BB, INBOARD/OUTBOARD/AFT LIP. (MARKED WITH TAPE) (FILED CLOSED) REPAIRED CORROSION DAMAGE ON RH FUEL ACCESS PANEL OPENING 640BB ON THE FWD AND INBOARD LIP WITH REFERENCE TO REO 601R-57-21-030 REV "-L" D
- [SDR SWIA20241115023](https://openairdocs.org/sdr/SWIA20241115023.md): Skin · gouged · Oct 23, 2024 · N246PS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > MULTIPLE GOUGES/SCRATCHES FOUND ON THE EXTERIOR, AFT OF FS559.00 +112 BETWEEN STRG 22R AND STRG 23R, JUST AFT OF THE LOW AIR GROUND CONNECTION ACCESS DOOR. (MARKED WITH TAPE) (FILED CLOSED) COMPLIED WITH REO 601R-53-61-8244 DATED: 2024-10-26 REV - TEMPO
- [SDR SWI2024F01201](https://openairdocs.org/sdr/SWI2024F01201.md): Skin · corroded · Oct 23, 2024 · N246PS · Cndair CL6002B19 · Wing, Plate/Skin
  > POSSIBLE CORROSION ON RIGHT WING FUEL ACCESS HOLE 640BB, INBOARD/OUTBOARD/AFT LIP. (MARKED WITH TAPE) (FILED OPEN) REPAIRED CORROSION DAMAGE ON RH FUEL ACCESS PANEL OPENING 640BB ON THE FWD AND INBOARD LIP WITH REFERENCE TO REO 601R-57-21-030 REV "-L" DAT
- [SDR SWIA2024110823](https://openairdocs.org/sdr/SWIA2024110823.md): Skin · gouged · Oct 23, 2024 · N246PS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > MULTIPLE GOUGES/SCRATCHES FOUND ON THE EXTERIOR, AFT OF FS559.00 +112 BETWEEN STRG 22R AND STRG 23R, JUST AFT OF THE LOW AIR GROUND CONNECTION ACCESS DOOR. (MARKED WITH TAPE) (FILED OPEN) COMPLIED WITH REO 601R-53-61-8244 DATED: 2024-10-26 REV - TEMPORA
- [SDR SWIA202411150927](https://openairdocs.org/sdr/SWIA202411150927.md): Door Sill · corroded · Sep 27, 2024 · N246PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA54264-601R-53-41-666 N246PS MXCODEID49635-DTI - L/H FLOOR SILL FROM FS409+128 TO FS559 HAS CORROSION IN SEVERAL NUT PLATE HOLES. REPAIRED IAW REO 601R-53-41-66, REV C, DATED 11/06/2012. DVI BLENDED AREA OF FLOOR SIL
- [SDR SWIA20241108927](https://openairdocs.org/sdr/SWIA20241108927.md): Nut Plate · corroded · Sep 27, 2024 · N246PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA54263-601R-53-41-666 N246PS MXCODEID49634-DTI - R/H FLOOR SILL FROM FS409+128 TO FS559 HAS CORROSION IN SEVERAL NUT PLATE HOLES. REPAIRED IAW REO 601R-53-41-66, REV C, DATED 11/06/2012. DVI BLENDED AREA OF FLOOR SIL
- [SDR SWIA202402260001](https://openairdocs.org/sdr/SWIA202402260001.md): Warning Message · illuminated · Feb 20, 2024 · N246PS · Cndair CL6002B19 · Overheat Detection
  > AT ABOUT 800 FEET SHORT FINAL RECEIVED A MLG OVHT FAIL CAUTION. AS WE CONTINUED IT BECAME INTERMITTENT THEN TURNED INTO A MLG OVHT WARNING. AS WE ROLLED OUT THE WARNING WENT AWAY BUT WE NOTICED A BURNT RUBBER SMELL TAXING OFF THE RUNWAY. WE CALLED TOWER TO SEN
- [SDR SWIA202402210001](https://openairdocs.org/sdr/SWIA202402210001.md): Warning Message · illuminated · Feb 20, 2024 · N246PS · Cndair CL6002B19 · Overheat Detection
  > AT ABOUT 800 FEET SHORT FINAL RECEIVED A MLG OVHT FAIL CAUTION. AS WE CONTINUED IT BECAME INTERMITTENT THEN TURNED INTO A MLG OVHT WARNING. AS WE ROLLED OUT THE WARNING WENT AWAY BUT WE NOTICED A BURNT RUBBER SMELL TAXING OFF THE RUNWAY. WE CALLED TOWER TO SEN
- [SDR SWIA202266909](https://openairdocs.org/sdr/SWIA202266909.md): Sensor · failed · Nov 20, 2022 · N246PS · Cndair CL6002B19 · Landing Gear Position and Warning
  > ON DEPARTURE WHEN RETRACTING GEAR, RECEIVED A GEAR DISAGREE WARNING MESSAGE, STEERING INOP CAUTION, AND WOW INPUT CAUTION. NOSE GEAR DID NOT RETRACT. RAN QRH, GEAR EXTENDED, MESSAGE CLEARED. RAN QRH FOR STEERING INOP AND MESSAGE CLEARED. NORMAL LANDING. NOSE G
- [SDR SWIA202265572](https://openairdocs.org/sdr/SWIA202265572.md): None · odor · May 7, 2022 · N246PS · Cndair CL6002B19 · Air Conditioning System
  > FLIGHT ATTENDANT, PASSENGER, AND FIRST OFFICER SMELLED A FAINT BURNING SMELL SIMILAR TO A MATCH OR A CANDLE FOR 10-15 MINUTES DURING FLIGHT. (FLIGHT 4722 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 24788702 WITH THE FOLLOWING CORRECTIVE
- [SDR SWIA202158727](https://openairdocs.org/sdr/SWIA202158727.md): Angle · cracked · Jun 8, 2021 · N246PS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR HAS A APPROXIMATE 2 INCH CRACK ON AFT ANGLE PIECE NEXT TO DOOR MOTOR CABLE PULLEY (FILED CLOSED) REMOVED PREVIOUS REPAIR TO PAX DOOR AFT DRAG ANGLE AND INSTALLED NEW REPAIR REFERENCING SRM 52-12-55, 51-42-13, 51-42-22 AND GENERIC REO 601R-52-11
- [SDR SWIA202156388](https://openairdocs.org/sdr/SWIA202156388.md): Bracket · cracked · Feb 10, 2021 · N246PS · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT FLAP STUB FAIRING HAS A CRACKED/DAMAGED FWD HINGE. (C-CHECK) RO 2/21/2021. REMOVED AND REPLACED BROKEN BRACKET ON LT STUB FAIRING IAW CRJ200 SRM 51-42-06.
- [SDR SWIA202156382](https://openairdocs.org/sdr/SWIA202156382.md): Floorbeam · corroded · Jan 29, 2021 · N246PS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOOR BEAM AFT OF F.S 559+80 AT LBL 9.0 HAS CORROSION AT NUTPLATE MARKED WITH RED TAPE (C-CHECK) RO 2/21/2021 PERFORMED REPAIR TO F.S 559. +87€? AT LBL 9.0€? FLOOR BEAM SUPPORT FLANGE IAW REO 601R-53-00-827 REV: -- DATE 2021-01-30 AND REF: CRJ 200 SRM 5
- [SDR SWIA202156381](https://openairdocs.org/sdr/SWIA202156381.md): Floorbeam · corroded · Jan 29, 2021 · N246PS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOOR BEAMS AFT OF FS 559+80 ON LBL 9 AND RBL 9 HAVE CORROSION AT NUTPLATE LOCATIONS MARKED WITH RED TAPE. (C-CHECK) RO 2/21/2021. PERFORMED REPAIR TO FS 559. + 87€? AT RBL 9 FLOOR BEAM SUPPORT FLANGE IAW REO 601R-53-00-827 REV: -- DATE 2021-01-30 AND REF:
- [SDR SWIA202156380](https://openairdocs.org/sdr/SWIA202156380.md): Floor Support · damaged · Jan 15, 2021 · N246PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND 1 EA ELONGATED NUTPLATE HOLE ON LT FLOOR SILL AT APPROX FS 529.00. (C-CHECK) RO 2/21/2021. REPAIRED ELONGATED NUTPLATE HOLE ON LT FLOOR SILL AT APPROX FS 529.00 IAW CRJ 200 REO 601R-53-41-2855 REV -- DATE 2021-02-09. COMPLETED TASK CARD 51-900-1003-S

Next page: https://openairdocs.org/aircraft/N246PS/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 = 'N246PS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N246PS/reports

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