N230PS, cancelled Dec 9, 2025

Service difficulty reports · 84

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 = 'N230PS' AND deregistration_id = 'N230PS-2025-12-09'
  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 VNAA201909289996Bulkhead · damagedFS 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 INSPSep 28, 2019 · N230PS · Bombdr CL6002D15 · Fuselage Main, BulkheadSDR VNAA201909289995Former · not reportedDURING 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-REQSep 28, 2019 · N230PS · Bombdr CL6002D15 · Passenger/Crew DoorsSDR VNAA201909289994Gusset · corrodedINTERCOSTALS 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 REPLACEMENTSep 28, 2019 · N230PS · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA201909289993Frame · crackedFS 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 SECSep 28, 2019 · N230PS · Bombdr CL6002D15 · Fuselage Main, FrameSDR VNAA201909289992Skin · crackedPAX 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/Sep 28, 2019 · N230PS · Bombdr CL6002D15 · Passenger/Crew DoorsSDR VNAA201909289991Intercostal · corrodedPAX 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 601R318057-1Sep 28, 2019 · N230PS · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA2019092800000Web · corrodedPAX 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#6Sep 28, 2019 · N230PS · Bombdr CL6002D15 · Passenger/Crew DoorsSDR VNAA2019072811102Inverter · failedRH OVERWING EMERGENCY EXIT LOWER LIGHT INOP. R&R INVERTER IAW CRJ 200 AMM 33-51-02-000/400-801. OPS CHECK GOOD.Jul 28, 2019 · N230PS · Cndair CL6002B19 · Emergency LightingSDR VNAA2019062311102Control Unit · failedDURING 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 27-05Jun 21, 2019 · N230PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA2019032211102Pdu · failedDURING 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-Mar 22, 2019 · N230PS · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR VNAA2018111311101Switch · malfunctionedDURING 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 INCIDENov 13, 2018 · N230PS · Cndair CL6002B19 · Airfoil Anti/De-ice SystemSDR VNAA2018073111102Selector Panel · malfunctionedAS 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 Jul 31, 2018 · N230PS · Cndair CL6002B19 · Cabin Pressure Control SystemSDR VNAA2017102399903Rib · crackedFOUND 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.Oct 23, 2017 · N230PS · Cndair CL6002B19 · Horizontal Stabilizer, Spar/RibSDR VNAA2017102399902Bulkhead Web · crackedFOUND 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.,Oct 23, 2017 · N230PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2017102399901Bulkhead Web · crackedFOUND 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.Oct 23, 2017 · N230PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2017102299921Seat Track · corrodedRIGHT 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.Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2017102299920Seat Track · corrodedRIGHT 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.Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2017102299919Seat Track · corrodedRIGHT 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.Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2017102299918Seat Track · corrodedRIGHT 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.Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2017102299917Seat Track · corrodedRIGHT 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 2017-03-2Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2017102299916Seat Track · corrodedRIGHT 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.Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2017102299915Seat Track · corrodedLEFT 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.Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2017102299914Seat Track · corrodedLEFT 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.Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2017102299913Seat Track · corrodedLEFT 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.Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2017102299912Seat Track · corrodedLEFT 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.Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2017102299911Seat Track · corrodedLEFT 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.Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2017102299910Seat Track · corrodedLEFT 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 SERVOct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2017102299909Seat Track · corrodedALL 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, Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2017102299908Doubler · corrodedDRAIN 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.Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2017102299907Frame · corrodedFUSELAGE 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.Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage Main, FrameSDR VNAA2017102299906Frame · corrodedFUSELAGE 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.Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage Main, FrameSDR VNAA2017102299905Angle · crackedFS 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.Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2017102299904Door Sill · corrodedRIGHT 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.Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2017102299903Door Sill · corrodedLEFT 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.Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2017102299902Seat Track · corrodedLBL 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 60Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2017102299901Seat Track · corrodedLBL 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.Oct 22, 2017 · N230PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2016020400007Thrust Reverser · warning lightCREW 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.Feb 4, 2016 · N230PS · Cndair CL6002B19 · Engine Thrust ReverserSDR VNAA2016012200017Floor Support · corrodedRT 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.Jan 22, 2016 · N230PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2016012200016Floor Support · corrodedLT PRESSURE FLOOR SILL ANGLE HAS SEVERAL AREAS OF MINOR CORROSION BETWEEN FS 461 - 473. REMOVED APPROXIMATELY .004" OF DAMAGE FROM SILL ANGLE.Jan 22, 2016 · N230PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2016010300004Warning Message · illuminatedCREW 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.Jan 3, 2016 · N230PS · Cndair CL6002B19 · Engine Thrust ReverserSDR VNAA2015121300009Wire · looseCREW 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 Dec 13, 2015 · N230PS · Cndair CL6002B19 · Light System WiringSDR VNAA2015092800028Actuator · bindingCREW 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 RELEASEDSep 28, 2015 · N230PS · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR VNAA2015092300021Connector · damagedCREW 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 SENSOSep 23, 2015 · N230PS · Cndair CL6002B19 · Flight Control System WiringSDR VNAA2015092300020Sensor · damagedCREW 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 ELECTRSep 23, 2015 · N230PS · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR VNAA2015061500010Control Unit · failedCREW 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 IJun 15, 2015 · N230PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA2015052500021Electronic Unit · malfunctionedCREW 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. ACMay 25, 2015 · N230PS · Cndair CL6002B19 · Landing Gear Position and WarningSDR VNAA2015051000014Wire · brokenCREW 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.May 10, 2015 · N230PS · Cndair CL6002B19 · Light System WiringSDR VNAA2015010400003Connector · damagedCREW 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.Jan 4, 2015 · N230PS · Cndair CL6002B19 · Light System WiringSDR VNAA2015010400004Light · damagedAFT EMERGENCY LIGHT PIN BROKEN. MAINTENANCE INSPECTED, R & R LAST LIGHT STRIP OF EMERGENCY FLOOR LIGHTS AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Jan 4, 2015 · N230PS · Cndair CL6002B19 · Emergency LightingSDR VNAA2014041100010Selector Valve · failedCREW 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.Apr 11, 2014 · N230PS · Cndair CL6002B19 · Landing Gear Retraction/Extension System
Back to N230PS, cancelled Dec 9, 2025