# Service difficulty reports: N230PS, cancelled Dec 9, 2025 A list on [N230PS, cancelled Dec 9, 2025](https://openairdocs.org/deregistered/N230PS-2025-12-09.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 2 · 84 reports - [SDR VNAA201909289996](https://openairdocs.org/sdr/VNAA201909289996.md): Bulkhead · damaged · Sep 28, 2019 · N230PS · Bombdr CL6002D15 · Fuselage Main, Bulkhead > FS 621 RPB WEB HAS APPLIED CIC ON BULKHEAD REPAIR DOUBLER AND TRIPLER IAW CRJ 200 SRM 51-21-11.ONE AREA WITH INDICATIONS NOTED IN THE HEEL LINE AREA OF BL 0 VERT POST AT WL 109-WL114 60%. FAILED NDT INSP - [SDR VNAA201909289995](https://openairdocs.org/sdr/VNAA201909289995.md): Former · not reported · Sep 28, 2019 · N230PS · Bombdr CL6002D15 · Passenger/Crew Doors > DURING INSPECTION OF PAX DOOR FORMER FS 347.2REPAIRED PAX DOOR FORMER AND PULLEY BY INSTALLING OVERSIZED FASTENER'S IAW BOMBARDIER REO #601R-52-11-2756 REV-- DATE 2019-08-28.5 AT DATUM 4 IS SEPERATING PER TO 52-579-001-18-REQ - [SDR VNAA201909289994](https://openairdocs.org/sdr/VNAA201909289994.md): Gusset · corroded · Sep 28, 2019 · N230PS · Bombdr CL6002D15 · Fuselage Miscellaneous Structure > INTERCOSTALS AND GUSSET PLATES BETWEEN STGR 13L AND 17L AT FS 310 ARE CORRODED.. REMOVED GUSSET IAW CRJ200 SRM 51-42-06 FOUND TO BE CORRODED BEYOND LIMITS, REQUIRES REPLACEMENT - [SDR VNAA201909289993](https://openairdocs.org/sdr/VNAA201909289993.md): Frame · cracked · Sep 28, 2019 · N230PS · Bombdr CL6002D15 · Fuselage Main, Frame > FS 333 FRAME IS CRACKED BETWEEN STGR 0 AND STGR 1L. 8/24/19 (PCC) M/A: 1. REMOVED FRAME SECTOR FROM FS 333 STGR 0-3L IAW CRJ 200 SRM 51-42-06. 8/26/19 C/A: 1. RECEIVED NEW FRAME SECTOR PART 601R32004-41 LOCATED AND DRILLED NEW FRAME AND INSTALLED NEW FRAME SEC - [SDR VNAA201909289992](https://openairdocs.org/sdr/VNAA201909289992.md): Skin · cracked · Sep 28, 2019 · N230PS · Bombdr CL6002D15 · Passenger/Crew Doors > PAX DOOR INNER SKIN CORRODED AT HINGE SIDE IN 2 LOCATIONS. 08/27/19 M/A: 1. UPON FURTHER INVESTIGATION FOUND INNER SKIN CRACKED ON PAX DOOR REQUIRES REPLACEMENT REMOVED INNER SKIN IAW CRJ 200 SRM 51-42-06,51-42-10,51-42-22,51+42-21 REV 37 JUL10/18. 08/29/19 C/ - [SDR VNAA201909289991](https://openairdocs.org/sdr/VNAA201909289991.md): Intercostal · corroded · Sep 28, 2019 · N230PS · Bombdr CL6002D15 · Fuselage Miscellaneous Structure > PAX DOOR TOP INTERCOSTAL IS CORRODED. M/A: 1. REMOVED INTRCOSTAL PERPENDICULAR TO THE DISCREPANT INTERCOSTAL FOR ACCESS. 08/29/19 C/A: 1. OK TO INSTALL. WVAC 52 INSP REINSTALLED PERPENDICULAR INTERCOSTAL WITH SERVICEABLE INTERCOSTAL 601R318057-1 - [SDR VNAA2019092800000](https://openairdocs.org/sdr/VNAA2019092800000.md): Web · corroded · Sep 28, 2019 · N230PS · Bombdr CL6002D15 · Passenger/Crew Doors > PAX DOOR AFT WEB IS CORRODED ON BOTH SIDES AT THE TOP. M/A: 1. UPON FURTHER INVESTIGATION, FOUND PAX DOOR AFT WEB TO BE CORRODED BEYOND LIMITS, REQUIRES REPAIR OR REPLACEMENT. 08/31/19 C/A: 1. REMOVED AND REPLACED PAX DOOR AFT WEB WITH NEW SERVICEABLE WEB PN#6 - [SDR VNAA2019072811102](https://openairdocs.org/sdr/VNAA2019072811102.md): Inverter · failed · Jul 28, 2019 · N230PS · Cndair CL6002B19 · Emergency Lighting > RH OVERWING EMERGENCY EXIT LOWER LIGHT INOP. R&R INVERTER IAW CRJ 200 AMM 33-51-02-000/400-801. OPS CHECK GOOD. - [SDR VNAA2019062311102](https://openairdocs.org/sdr/VNAA2019062311102.md): Control Unit · failed · Jun 21, 2019 · N230PS · Cndair CL6002B19 · Trailing Edge Flap Control System > DURING APPROACH THE CREW RECEIVED A FLAP FAIL CAUTION MESSAGE. FLAPS WERE INDICATING 30 DEGREES WHEN THE MESSAGE CAME ON. CREW DID A GO AROUND AND DECLARED AND EMERGENCY TO GET THE LONG RUNWAY AND RECEIVE PRIORITY HANDLING. MAINTENANCE COMPLIED WITH TO 27-05 - [SDR VNAA2019032211102](https://openairdocs.org/sdr/VNAA2019032211102.md): Pdu · failed · Mar 22, 2019 · N230PS · Cndair CL6002B19 · Trailing Edge Flap Actuator > DURING LANDING FLAPS FAILED AT 8. CREW RAN QRH AND DECLARED EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT AND TAXIED TO GATE 1. 24-MAR-2019 15:27 EST / C/E TO 27-050-004-09 DOF. R/R FLAP PDU IAW AMM 27-52-01-000/400-801. RE RIGGED LT AND RT BPSU'S IAW AMM 27-51- - [SDR VNAA2018111311101](https://openairdocs.org/sdr/VNAA2018111311101.md): Switch · malfunctioned · Nov 13, 2018 · N230PS · Cndair CL6002B19 · Airfoil Anti/De-ice System > DURING CLIMB CREW BECAME AWARE THE WING ANTI-ICE WAS NOT WORKING. FOLLOWED QRH. CONTACTED ATC AND DECLARED AN EMERGENCY AS THEY WERE IN ICING CONDITIONS AND REQUESTED AN EXPEDITED DECENT TO FL100. UPON REACHING FL100, EMERGENCY CANCELLED. LANDED WITHOUT INCIDE - [SDR VNAA2018073111102](https://openairdocs.org/sdr/VNAA2018073111102.md): Selector Panel · malfunctioned · Jul 31, 2018 · N230PS · Cndair CL6002B19 · Cabin Pressure Control System > AS THE AIRCRAFT CLIMBED THROUGH FLIGHT LEVEL 230, THE CREW RECEIVED A CABIN ALTITUDE PRESSURIZATION MESSAGE. THE CREW RAN THE IMMEDIATE ACTION LIST AND BEGAN IMMEDIATE DECENT. THE CREW DEPLOYED OXYGEN MASKS AND DECLARED AN EMERGENCY. THE FLIGHT LANDED WITHOUT - [SDR VNAA2017102399903](https://openairdocs.org/sdr/VNAA2017102399903.md): Rib · cracked · Oct 23, 2017 · N230PS · Cndair CL6002B19 · Horizontal Stabilizer, Spar/Rib > FOUND RIB AT ES 14.47 CRACKED. REMOVED THE DAMAGED RIB. AND INSTALLED A REPLACEMENT IAW SRM 51-42-06, 51-42-13, AND EO SNIEO S06. - [SDR VNAA2017102399902](https://openairdocs.org/sdr/VNAA2017102399902.md): Bulkhead Web · cracked · Oct 23, 2017 · N230PS · Cndair CL6002B19 · Fuselage Main, Bulkhead > FOUND THE REAR PRESSURE BULKHEAD WEB BS 621, HAD MULTIPLE CRACK INDICATIONS NOTED AT RBL 27.5, WL 103, TWO INCHES LONG AND 100% FSH. PERFORMED AN INTERIM REPAIR THE BULKHEAD IAW REO 601R-53-61-1285, REV E., - [SDR VNAA2017102399901](https://openairdocs.org/sdr/VNAA2017102399901.md): Bulkhead Web · cracked · Oct 23, 2017 · N230PS · Cndair CL6002B19 · Fuselage Main, Bulkhead > FOUND THE REAR PRESSURE BULKHEAD WEB WITH MULTIPLE CRACK INDICATIONS AT RBL 18, WL 103, TWO INCHES LONG 50% FSH. FAILED NDT INSPECTION. PERFORM INTERIM REPAIR IAW REO 601R-53-61-1285, REV E. - [SDR VNAA2017102299921](https://openairdocs.org/sdr/VNAA2017102299921.md): Seat Track · corroded · Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > RIGHT HAND SIDE SEAT TRACK FS 544-559+80 SEGMENT IS CORRODED. REMOVED AND REPLACED SEAT TRACK AT FS 544-559+80 WITH A NEW SERVICEABLE SEAT TRACK SEGMENT P/N 601R38312-25 IAW AMM TASK 53-01-11-000/400-802 AND REO 601R-53-00-055 REV C DATED 2017-03-21. - [SDR VNAA2017102299920](https://openairdocs.org/sdr/VNAA2017102299920.md): Seat Track · corroded · Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > RIGHT HAND SIDE SEAT TRACK FS 499-544 SEGMENT IS CORRODED. REMOVED AND REPLACED SEAT TRACK AT FS 499-544 WITH A NEW SERVICEABLE SEAT TRACK SEGMENT P/N 601R38312-131 IAW AMM TASK 53-01-11-000/400-802 AND REO 601R-53-00-055 REV C DATED 2017-03-21. - [SDR VNAA2017102299919](https://openairdocs.org/sdr/VNAA2017102299919.md): Seat Track · corroded · Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > RIGHT HAND SIDE SEAT TRACK FS 559-499 SEGMENT IS CORRODED. REMOVED AND REPLACED SEAT TRACK AT FS 559-499 WITH A NEW SERVICEABLE SEAT TRACK SEGMENT P/N 601R38312-115 IAW AMM TASK 53-01-11-000/400-802 AND REO 601R-53-00-055 REV C DATED 2017-03-21. - [SDR VNAA2017102299918](https://openairdocs.org/sdr/VNAA2017102299918.md): Seat Track · corroded · Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > RIGHT HAND SIDE SEAT TRACK FS 409+112 - 449 SEGMENT IS CORRODED. REMOVED AND REPLACED SEAT TRACK AT FS FS 409+112 - 449 WITH A NEW SERVICEABLE SEAT TRACK SEGMENT P/N 601R38312-119 IAW AMM TASK 53-01-11-000/400-802 AND REO 601R-53-00-055 REV C DATED 2017-03-21. - [SDR VNAA2017102299917](https://openairdocs.org/sdr/VNAA2017102299917.md): Seat Track · corroded · Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > RIGHT HAND SIDE SEAT TRACK FS 409+16 - 409+112 SEGMENT IS CORRODED. REMOVED AND REPLACED SEAT TRACK AT FS 409+16 – 409+112 WITH A NEW SERVICEABLE SEAT TRACK SEGMENT P/N 601R38312-29 IAW AMM TASK 53-01-11-000/400-802 AND REO 601R-53-00-055 REV C DATED 2017-03-2 - [SDR VNAA2017102299916](https://openairdocs.org/sdr/VNAA2017102299916.md): Seat Track · corroded · Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > RIGHT HAND SIDE SEAT TRACK FS 364 - 409+16 SEGMENT IS CORRODED. REMOVED AND REPLACED SEAT TRACK AT FS 364 - 409+16 WITH A NEW SERVICEABLE SEAT TRACK SEGMENT P/N 601R38312-31 IAW AMM TASK 53-01-11-000/400-802 AND REO 601R-53-00-055 REV C DATED 2017-03-21. - [SDR VNAA2017102299915](https://openairdocs.org/sdr/VNAA2017102299915.md): Seat Track · corroded · Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > LEFT HAND SIDE SEAT TRACK FS 544 - 559+80 SEGMENT IS CORRODED. REMOVED & REPLACED SIDE SEAT TRACK FS 544 - 559+80 PN: 601R38312-25 IAW AMM TASK 53-01-11-400-802 AND REO 601R-53-00-055 REV C DATED 2017-03-21. - [SDR VNAA2017102299914](https://openairdocs.org/sdr/VNAA2017102299914.md): Seat Track · corroded · Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > LEFT HAND SIDE SEAT TRACK FS 499 - 544 SEGMENT IS CORRODED. REMOVED AND REPLACED SEAT TRACK AT FS 499 - 544 WITH A NEW SERVICEABLE SEAT TRACK SEGMENT P/N 601R38312-131 IAW AMM TASK 53-01-11-000/400-802 AND REO 601R-53-00-055 REV C DATED 2017-03-21. - [SDR VNAA2017102299913](https://openairdocs.org/sdr/VNAA2017102299913.md): Seat Track · corroded · Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > LEFT HAND SIDE SEAT TRACK FS 449 - 499 SEGMENT IS CORRODED. REMOVED AND REPLACED SEAT TRACK AT FS 449 - 499 WITH A NEW SERVICEABLE SEAT TRACK SEGMENT P/N 601R38312-115 IAW AMM TASK 53-01-11-000/400-802 AND REO 601R-53-00-055 REV C DATED 2017-03-21. - [SDR VNAA2017102299912](https://openairdocs.org/sdr/VNAA2017102299912.md): Seat Track · corroded · Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > LEFT HAND SIDE SEAT TRACK FS 409+112 - 449 SEGMENT IS CORRODED. REMOVED AND REPLACED SEAT TRACK AT FS 409+112 - 449 WITH A NEW SERVICEABLE SEAT TRACK SEGMENT P/N 601R38312-119 IAW AMM TASK 53-01-11-000/400-802 AND REO 601R-53-00-055 REV C DATED 2017-03-21. - [SDR VNAA2017102299911](https://openairdocs.org/sdr/VNAA2017102299911.md): Seat Track · corroded · Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > LEFT HAND SIDE TRACK FS 409+16 - 409+112 SEGMENT CORRODED. REMOVED AND REPLACED SEAT TRACK AT FS 409+16 - 409+112 WITH A NEW SERVICEABLE SEAT TRACK SEGMENT P/N 601R38312-29 IAW AMM TASK 53-01-11-400-802 AND REO 601R-53-00-055 REV C DATED 2017-03-21. - [SDR VNAA2017102299910](https://openairdocs.org/sdr/VNAA2017102299910.md): Seat Track · corroded · Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > LEFT HAND SIDE SET TRACK FS 364 - 409+16 SEGMENT IS CORRODED. REMOVED LT SIDE SEAT TRACK FROM FS 364-406+16 IAW AMM 53-01-11-000-802. INSTALLED NEW SERVICEABLE LT SIDE SEAT TRACK FROM FS 364-409+16 P/N 601R38312-31 IAW AMM 53-01-11-400-802. FABRICATED NEW SERV - [SDR VNAA2017102299909](https://openairdocs.org/sdr/VNAA2017102299909.md): Seat Track · corroded · Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > ALL CARGO BAY FLOOR SEAT TRACKS ARE CORRODED FROM FS 559+80 TO FS 621. REMOVED ALL CARGO BAY FLOOR SEAT TRACKS FROM FS 559+79 TO FS 621 IAW AMM 53-01-11-000-802. INSTALLED 7 EA NEW SERVICEABLE CARGO FLOOR SEAT TRACKS IAW AMM 53-01-11-400-802 P/N 601R31032-51, - [SDR VNAA2017102299908](https://openairdocs.org/sdr/VNAA2017102299908.md): Doubler · corroded · Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > DRAIN MAST DOUBLER BETWEEN FS 605 AND FS 621 AND STR 25R - STR 26R IS CORRODED. REMOVED AND INSTALLED DRAIN MAST DOUBLER PN: 601R43216-9 IAW SRM 51-42-06. - [SDR VNAA2017102299907](https://openairdocs.org/sdr/VNAA2017102299907.md): Frame · corroded · Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage Main, Frame > FUSELAGE FRAME FS 605 IS CORRODED FROM STR 26L TO 24R. REMOVED AND INSTALLED FS 605 FRAME SECTOR PN 601R36026-27 IAW SRM 51-42-06. - [SDR VNAA2017102299906](https://openairdocs.org/sdr/VNAA2017102299906.md): Frame · corroded · Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage Main, Frame > FUSELAGE FRAME FS 589 IS CORRODED FROM STR 27L TO STR 26R. REMOVED AND INSTALLED NEW LOWER FRAME SECTOR PN 601R36025-61 AT FS 589 A IAW SRM 51-42-21. - [SDR VNAA2017102299905](https://openairdocs.org/sdr/VNAA2017102299905.md): Angle · cracked · Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > FS 621 BULKHEAD FLOOR SILL ANGLE IS CRACKED AT LBL 43. REMOVED AND INSTALLED SERVICEABLE FLOOR SILL ANGLE P/N 601R-53-61-004-1 FROM LBL 36-43 FS 621 IAW SRM 51-42-06 & SRM 51-42-21. - [SDR VNAA2017102299904](https://openairdocs.org/sdr/VNAA2017102299904.md): Door Sill · corroded · Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > RIGHT HAND FLOOR SILL IS CORRODED FROM FS 559+80 TO FS 559+112. REMOVED AND INSTALLED RT FLOOR NEW SILL PLATE PN 601R31133-102 FROM FS 559+80 TO FS 559+112 IAW SRM 51-42-06 & 51-42-21. - [SDR VNAA2017102299903](https://openairdocs.org/sdr/VNAA2017102299903.md): Door Sill · corroded · Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > LEFT HAND FLOOR SILL IS CORRODED FROM FS 559+80 TO FS 621. REMOVED CARGO FLOOR SILL IAW SRM 51-42-06 & 51-42-21. LOCATE, DRILL & INSTALL NEW CARGO DOOR SILL P/N 601R3501263 IAW SRM 51-40-11 & REO 601R-53-61-1574 REV B DATED 2012-04-15. - [SDR VNAA2017102299902](https://openairdocs.org/sdr/VNAA2017102299902.md): Seat Track · corroded · Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > LBL 9 AND RBL 9 FLOOR SEAT TRACK SEGMENTS ARE CORRODED FROM FS 399 TO FS 409+128. LOCATED, FABRICATED, DRILLED AND COUNTERSUNK SEAT TRACK RBL 9 FS 399 TO FS 409+128 PER REO 601R-53-00-485 REV B DATED 2016-04-01. REMOVED AND INSTALLED FABRICATE SEAT TRACK PN 60 - [SDR VNAA2017102299901](https://openairdocs.org/sdr/VNAA2017102299901.md): Seat Track · corroded · Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > LBL 9 AND RBL 9 FLOOR SEAT TRACK SEGMENTS ARE CORRODED FROM FS 364 TO FS 399. REMOVED AND INSTALLED NEW SERVICEABLE SEAT TRACK P/N 601R31032-15 & SCREW NAS517 IAW AMM 53-01-11-000/400-802. - [SDR VNAA2016020400007](https://openairdocs.org/sdr/VNAA2016020400007.md): Thrust Reverser · warning light · Feb 4, 2016 · N230PS · Cndair CL6002B19 · Engine Thrust Reverser > CREW REPORTED INTERMITTENT LT REVERSER UNLOCKED CAUTION MESSAGE IN FLIGHT. MESSAGE WENT FROM INTERMITTENT TO STEADY. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE DEFERRED LT THRUST REVERSER IAW MEL. ACFT RELEASED FOR SERVICE. - [SDR VNAA2016012200017](https://openairdocs.org/sdr/VNAA2016012200017.md): Floor Support · corroded · Jan 22, 2016 · N230PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > RT PRESSURE FLOOR SILL ANGLE IS CORRODED AT FS 513 AND BETWEEN FS 461 AND FS 473. REMOVED APPROXIMATELY.004" OF DAMAGE FROM SILL ANGLE, APPROXIMATELY.076" MATERIAL REMAINING. - [SDR VNAA2016012200016](https://openairdocs.org/sdr/VNAA2016012200016.md): Floor Support · corroded · Jan 22, 2016 · N230PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > LT PRESSURE FLOOR SILL ANGLE HAS SEVERAL AREAS OF MINOR CORROSION BETWEEN FS 461 - 473. REMOVED APPROXIMATELY.004" OF DAMAGE FROM SILL ANGLE. - [SDR VNAA2016010300004](https://openairdocs.org/sdr/VNAA2016010300004.md): Warning Message · illuminated · Jan 3, 2016 · N230PS · Cndair CL6002B19 · Engine Thrust Reverser > CREW REPORTED LT REVERSER UNLOCKED CAUTION MESSAGE APPEARED INTERMITTENTLY SEVERAL TIMES DURING FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE DEFERRED LT THRUST REVERSER IAW MEL. ACFT RELEASED FOR SERVICE. - [SDR VNAA2015121300009](https://openairdocs.org/sdr/VNAA2015121300009.md): Wire · loose · Dec 13, 2015 · N230PS · Cndair CL6002B19 · Light System Wiring > CREW REPORTED EMERGENCY EXIT FLOOR LIGHTING STRIP WIRES PULLED LOOSE AT LAVATORY. MAINTENANCE INSPECTED AND FOUND LIGHTING STRIP CONTACT ENDS PULLED OUT. MAINTENANCE CRIMPED NEW CONTACT ENDS ON, SECURED LIGHT STRIP TO FLOOR AND PERFORMED CHECKS IAW AMM. ACFT - [SDR VNAA2015092800028](https://openairdocs.org/sdr/VNAA2015092800028.md): Actuator · binding · Sep 28, 2015 · N230PS · Cndair CL6002B19 · Trailing Edge Flap Actuator > CREW REPORTED FLAPS FAIL MESSAGE AT 160 KNOTS AND 40/39 DEGREE ASYMMETRY ON EXTENSION. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT IAW ACFT FIM, R & R RT INBD FLAP OTBD ACTUATOR AND PERFORMED CHECKS IAW AMM. ACFT RELEASED - [SDR VNAA2015092300021](https://openairdocs.org/sdr/VNAA2015092300021.md): Connector · damaged · Sep 23, 2015 · N230PS · Cndair CL6002B19 · Flight Control System Wiring > CREW REPORTED FLAPS FAIL MESSAGE WHILE SELECTING FLAPS FROM 8 TO 20 DEGREES. FLAPS REMAINED AT 8 DEGREES. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT IAW ACFT FIM, R & R MATING CONNECTOR PLUG FOR LT BRAKE AND POSITION SENSO - [SDR VNAA2015092300020](https://openairdocs.org/sdr/VNAA2015092300020.md): Sensor · damaged · Sep 23, 2015 · N230PS · Cndair CL6002B19 · Trailing Flap Position Indicating System > CREW REPORTED FLAPS FAIL MESSAGE WHILE SELECTING FLAPS FROM 8 TO 20 DEGREES. FLAPS REMAINED AT 8 DEGREES. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT IAW ACFT FIM, R & R LT BRAKE AND POSITION SENSOR UNIT DUE TO BENT ELECTR - [SDR VNAA2015061500010](https://openairdocs.org/sdr/VNAA2015061500010.md): Control Unit · failed · Jun 15, 2015 · N230PS · Cndair CL6002B19 · Trailing Edge Flap Control System > CREW REPORTED FLAPS FAIL AMBER MESSAGE ON APPROACH. FLAPS FAILED AT ZERO DEGREES. CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM IAW ACFT FAULT ISOLATION MANUAL, FIM, R & R FLAP ELECTRONIC CONTROL UNIT, FECU, AND PERFORMED CHECKS I - [SDR VNAA2015052500021](https://openairdocs.org/sdr/VNAA2015052500021.md): Electronic Unit · malfunctioned · May 25, 2015 · N230PS · Cndair CL6002B19 · Landing Gear Position and Warning > CREW REPORTED WOW INPUT CAUTION, WOW OUTPUT CAUTION, WOW OUTPUT STATUS AND PROXIMITY SYS FAULT STATUS MESSAGES. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, RERACKED PROXIMITY SENSOR ELECTRONIC UNIT (PSEU) AND PERFORMED CHECKS IAW AMM. AC - [SDR VNAA2015051000014](https://openairdocs.org/sdr/VNAA2015051000014.md): Wire · broken · May 10, 2015 · N230PS · Cndair CL6002B19 · Light System Wiring > CREW REPORTED PASSENGER DOOR EMERGENCY EXIT SIGN ON FORWARD CLOSET OUT. MAINTENANCE INSPECTED, FOUND BROKEN WIRE AT CONNECTOR, R & R CONNECTOR AND MULE PIN AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE. - [SDR VNAA2015010400003](https://openairdocs.org/sdr/VNAA2015010400003.md): Connector · damaged · Jan 4, 2015 · N230PS · Cndair CL6002B19 · Light System Wiring > CREW REPORTED EMERGENCY LIGHTS AFT OF ROW 8 WOULD NOT ILLUMINATE WHEN TESTED. MAINTENANCE INSPECTED, R & R CONNECTOR PINS, SOCKETS, JUMPER AND 1 LIGHT STRIP AND PERFORMED CHECKS AMM. ACFT RELEASED FOR SERVICE. - [SDR VNAA2015010400004](https://openairdocs.org/sdr/VNAA2015010400004.md): Light · damaged · Jan 4, 2015 · N230PS · Cndair CL6002B19 · Emergency Lighting > AFT EMERGENCY LIGHT PIN BROKEN. MAINTENANCE INSPECTED, R & R LAST LIGHT STRIP OF EMERGENCY FLOOR LIGHTS AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE. - [SDR VNAA2014041100010](https://openairdocs.org/sdr/VNAA2014041100010.md): Selector Valve · failed · Apr 11, 2014 · N230PS · Cndair CL6002B19 · Landing Gear Retraction/Extension System > CREW REPORTED GEAR DISAGREE WARNING MESSAGE AFTER LANDING GEAR SELECTED UP. RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R MLG SELECTOR VALVE AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE. Next page: https://openairdocs.org/deregistered/N230PS-2025-12-09/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 = 'N230PS' AND deregistration_id = 'N230PS-2025-12-09' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N230PS-2025-12-09/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.