# Service difficulty reports: N256PS, cancelled Feb 26, 2025 A list on [N256PS, cancelled Feb 26, 2025](https://openairdocs.org/deregistered/N256PS-2025-02-26.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 · 73 reports - [SDR VNAA2019122421105](https://openairdocs.org/sdr/VNAA2019122421105.md): Adg · unwanted deploy · Dec 22, 2019 · N256PS · Cndair CL6002B19 · Electrical Power System > ADG SELF DEPLOYED IN FLIGHT - ADG SELF DEPLOYED IN FLIGHT - PERFORMED VISUAL INSPECTION OF ADG. NO DEFECTS NOTED. RE-STOWED ADG. - [SDR VNAA2019120911102](https://openairdocs.org/sdr/VNAA2019120911102.md): Unknown · odor · Dec 9, 2019 · N256PS · Cndair CL6002B19 · Air Distribution System > ON APPROACH INTO DCA THE FA REPORTED A STRONG FUEL SMELL. AS THEY PASSED THRU 2500 ON FINAL THE SMELL HAD INCREASED AND THE CREW DONNED 02 MASKS. THE CREW DID DECLARE AN EMERGENCY WITH ATC. UPON LANDING THE CREW AND PAX THEN EVACUATED AT THE INTERSECTION OF TW - [SDR VNAA2019071011102](https://openairdocs.org/sdr/VNAA2019071011102.md): Oil System · low · Jul 10, 2019 · N256PS · Cndair CL6002B19 · Turbine Engine Oil System > EMERGENCY LANDING INTO DCA. CREW REPORTED A LT OIL PRESSURE MESSAGE 4 MILES OUT FROM DCA. LT ENG STARTED LOSING THRUST. CREW REDUCED LT ENG TO IDLE AND LANDED SAFELY. CREW KEPT IT IN IDLE ALL THE WAY TO THE GATE. MX SERVICED LT ENG 5.5 QT FOUND OUT OF LIMITS - [SDR VNAA2019061541101](https://openairdocs.org/sdr/VNAA2019061541101.md): Drag Angle · cracked · Jun 4, 2019 · N256PS · Cndair CL6002B19 · Passenger/Crew Doors > (CAK), MAINTENANCE NOTED THAT THE AFT DRAG ANGLE HAS A CRACK MEASURING 0.85Ï¿½ LONG WHICH IS LOCATED IN THE RADIUS OF THE DRAG ANGLE. THE CRACK IS LOCATED BETWEEN A PREVIOUS REPAIR AND THE PULLEY SUPPORT BRACKET. THE AFT DRAG ANGLE (P/N 600-31907) IS FABRICATE - [SDR VNAA2019052711101](https://openairdocs.org/sdr/VNAA2019052711101.md): Light · inoperative · May 27, 2019 · N256PS · Cndair CL6002B19 · Emergency Lighting > MIDDLE CEILING EMERGENCY LIGHT AFTER EMERGENCY SIGN WILL NOT ILLUMINATE. REMOVED AND REPLACED MIDDLE AFT CEILING EMERGENCY FLOODLIGHT IAW CRJ200 AMM 33-51-16-000/400-801. OPS TESTS GOOD AT THIS TIME. - [SDR VNAA2019012599910](https://openairdocs.org/sdr/VNAA2019012599910.md): Rib · cracked · Jan 25, 2019 · N256PS · Cndair CL6002B19 · Wing, Rib/Bulkhead > DURING ACCESS FOR TRUNNION REPLACEMENT, FOUND BATT RIB AT WS 56.30 TO BE CRACKED AT TOP AFT CORNER. - [SDR VNAA2019012599909](https://openairdocs.org/sdr/VNAA2019012599909.md): Angle · cracked · Jan 25, 2019 · N256PS · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings > DURING REMOVAL FOR ACCESS FOR RT TRUNNION REPLACEMENT. FOUND IB CAP ANGLE TO BE CRACKED, REQUIRING REPLACEMENT. - [SDR VNAA2019012599908](https://openairdocs.org/sdr/VNAA2019012599908.md): Bulkhead · damaged · Jan 25, 2019 · N256PS · Cndair CL6002B19 · Fuselage Main, Bulkhead > FS 621 RPB WEB HAS AN AREA OF MULTIPLE INDICATIONS NOTED AT BL0 WL109 TO WL111.5 BY 60% FSH. FAILED NDT INSP. - [SDR VNAA2019012599907](https://openairdocs.org/sdr/VNAA2019012599907.md): Bulkhead · cracked · Jan 25, 2019 · N256PS · Cndair CL6002B19 · Fuselage Main, Bulkhead > FS 621 RPB WEB HAS AN AREA OF MULTIPLE INDICATIONS NOTED AT RBL 27 WL 83 TO WL 90 BY 60% FSH. FAILED NDT INSP. - [SDR VNAA2019012599906](https://openairdocs.org/sdr/VNAA2019012599906.md): Trunnion · cracked · Jan 25, 2019 · N256PS · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings > FOUND INDICATION ON RT TRUNNION 2ND HOLE FROM AFT OF TRUNNION OTBD HOLE 65% FSH AT TOP AFT SIDE OF HOLE FAILS NDT. - [SDR VNAA2019012599905](https://openairdocs.org/sdr/VNAA2019012599905.md): Trunnion · cracked · Jan 25, 2019 · N256PS · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings > FOUND INDICATION ON RT TRUNNION 2ND HOLE FROM AFT OF TRUNNION INBD HOLE 95% FSH AT TOP OF HOLE AFT SIDE OF HOLE FAILS NDT. - [SDR VNAA2019012599904](https://openairdocs.org/sdr/VNAA2019012599904.md): Seat Track · corroded · Jan 25, 2019 · N256PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK CLBL9 CORRODED AND DAMAGED BETWEEN FS559.00+112.00+643. FABRICATED NEW SEAT TRACK LBL9 FS559.00+112 TO 559.00+643 AND INSTALLED. - [SDR VNAA2019012599903](https://openairdocs.org/sdr/VNAA2019012599903.md): Floorbeam · cracked · Jan 25, 2019 · N256PS · Cndair CL6002B19 · Fuselage Main, Floor Beam > LBL27 CARGO FLOOR HAS CORROSION AROUND NUT PLATES ON O/B FLANGE BETWEEN FS574 AND FS621. UPON FURTHER INVESTIGATION, FOUND CARGO FLOOR BEAM CAP CRACKED, REQUIRES REPLACEMENT. REMOVED AND REPLACED FLOOR BEAM CAP. - [SDR VNAA2019012599902](https://openairdocs.org/sdr/VNAA2019012599902.md): Frame · cracked · Jan 25, 2019 · N256PS · Cndair CL6002B19 · Fuselage Main, Frame > FS605 FRAME IS CORRODED BETWEEN STR 26L & 26R. FRAME WAS REPLACED. - [SDR VNAA2019012599901](https://openairdocs.org/sdr/VNAA2019012599901.md): Support Angle · cracked · Jan 25, 2019 · N256PS · Cndair CL6002B19 · Fuselage Main, Floor Beam > LBL9 FLOORBEAM IB SUPPORT ANGLE AT FS280 LBL 9 IS CRACKED. - [SDR VNAA2018092211101](https://openairdocs.org/sdr/VNAA2018092211101.md): Bpsu · malfunctioned · Sep 22, 2018 · N256PS · Cndair CL6002B19 · Trailing Edge Flap Control System > FLIGHT CREW HAD A "FLAPS FAIL" CAUTION MESSAGE OCCUR EN ROUTE. DECLARED AND EMERGENCY AND DIVERTED TO THE NEAREST SUITABLE AIRPORT. MAINTENANCE DEFERRED FLAP SYSTEM. COMPLIED WITH T/O AND AD, R&R L BPSU. CHECKS GOOD. CLEARED FLAP MEL. - [SDR VNAA2017101311101](https://openairdocs.org/sdr/VNAA2017101311101.md): Seal · leaking · Oct 13, 2017 · N256PS · Cndair CL6002B19 · Turbine Engine Oil System > RIGHT ENGINE SHUTDOWN IN FLIGHT BY CREW DUE TO OIL FLUCTUATIONS. AICRAFT LANDED WITHOUT ISSUE. MX ADDED 6 QRTS OF OIL AND THE RT ENGINE FAILED THE CONSUMPTION CHECK. MX REPLACED THE ATS, IDG, AND EDP CARBON SEALS, RUN AND LEAK CHECKED GOOD. - [SDR VNAA2017050200003](https://openairdocs.org/sdr/VNAA2017050200003.md): Plate · corroded · May 2, 2017 · N256PS · Cndair CL6002B19 · Passenger/Crew Doors > PASSENGER DOOR AFT ANCHOR FITTING SERATATED PLATE IS CORRODED. REMOVED AND REPLACED NEW SERVICEABLE AFT ANCHOR FITTING SEPARATED PLATE. - [SDR VNAA2017050200002](https://openairdocs.org/sdr/VNAA2017050200002.md): Seat Track · corroded · May 2, 2017 · N256PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > RH PAX SEAT TRACKS CORRODED AT BS 409.00+32 TO 409.00+64 AND AT BS 461.00. FABRICATED A NEW SEAT TRACK IAW REO 601R-53-00-485. INSTALLED THE SEAT TRACK IAW AMM 53-01-11-400-802. - [SDR VNAA20170502HMV01](https://openairdocs.org/sdr/VNAA20170502HMV01.md): Seat Track · corroded · May 2, 2017 · N256PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > LEFT SIDE PAX SEAT TRACKS CORRODED AT THE FOLLOWING BS 364 - 409+96. REMOVED DAMAGED SEAT TRACKS AND REPLACED WITH NEW IAW AMM 53-01-11-000-802. - [SDR VNAA20170429HMV01](https://openairdocs.org/sdr/VNAA20170429HMV01.md): Bulkhead Web · cracked · Apr 29, 2017 · N256PS · Cndair CL6002B19 · Fuselage Main, Bulkhead > REAR PRESSURE BULKHEAD HAS MULTIPLE CRACK INDICATIONS. PERFORMED A MAJOR REPAIR TO THE BS 621 PRESSURE BULKHEAD AT RBL 9.5, WL76, LBL 9.5, WL 76, LBL 18, WL 76. - [SDR VNAA2017042500030](https://openairdocs.org/sdr/VNAA2017042500030.md): Stringer · cracked · Apr 25, 2017 · N256PS · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer > STRINGER 3L CRACKED AT BS 378.5 AFT END OF PASSENGER DOOR’S UPPER SILL. PERFORMED A MAJOR REPAIR TO STRINGER 3L BETWEEN BS 379 AND 394. - [SDR VNAA2017042500029](https://openairdocs.org/sdr/VNAA2017042500029.md): Skin · corroded · Apr 25, 2017 · N256PS · Cndair CL6002B19 · Fuselage Main, Plate/Skin > FUSELAGE SKIN BETWEEN BS 559.16 AND 559.112, STRINGERS 26L AND 26R, CORRODED. PERFORMED A MAJOR REPAIR TO FUSELAGE SKIN. - [SDR VNAA2016122100039](https://openairdocs.org/sdr/VNAA2016122100039.md): Transducer · faulty · Dec 21, 2016 · N256PS · Cndair CL6002B19 · Landing Gear Position and Warning > LANDING GEAR FAILED TO RETRACT. REMOVED AND REPLACED THE WHEEL SPEED TRANSDUCER. - [SDR VNAA2016122100038](https://openairdocs.org/sdr/VNAA2016122100038.md): Handle · inoperative · Dec 21, 2016 · N256PS · Cndair CL6002B19 · Landing Gear Selector > LANDING GEAR FAILED TO RETRACT. REMOVED AND REPLACED THE LANDING GEAR HANDLE ASSEMBLY. - [SDR VNAA2016073100033](https://openairdocs.org/sdr/VNAA2016073100033.md): Battery Pack · discharged · Jul 31, 2016 · N256PS · Cndair CL6002B19 · Emergency Lighting > EMERGENCY LIGHTS NOT WORKING. MAINTENANCE INSPECTED, REMOVED AND REPLACED NR 4 BATTERY PACK AND PERFORMED CHECK IAW AMM. AIRCRAFT RELEASED FOR SERVICE. - [SDR VNAA2016073100032](https://openairdocs.org/sdr/VNAA2016073100032.md): Battery Pack · discharged · Jul 31, 2016 · N256PS · Cndair CL6002B19 · Emergency Lighting > EMERGENCY LIGHTS NOT WORKING. REMOVED AND REPLACED THE NR 3 BATTERY PACK AND CHECKED IAW AMM. AIRCRAFT RELEASED FOR SERVICE. - [SDR VNAA2016073100031](https://openairdocs.org/sdr/VNAA2016073100031.md): Battery Pack · discharged · Jul 31, 2016 · N256PS · Cndair CL6002B19 · Emergency Lighting > EMERGENCY LIGHTS NOT WORKING. MAINTENANCE INSPECTED, R & R NR 2 BATTERY PACK AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE. - [SDR VNAA2016032800035](https://openairdocs.org/sdr/VNAA2016032800035.md): Carbon Seal · damaged · Mar 28, 2016 · N256PS · Cndair CL6002B19 · AC Generator-Alternator > CREW REPORTED A LOUD NOISE FROM LT ENGINE FOLLOWED BY PFC, MFD, ACARS, AND LT/RT WINDSHIELD HEAT TEMPORARY FAILURE. THEY DECLARED AN EMERGENCY, DIVERTED TO NEAREST FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE IDG ACCESSORY GEAR BOX C - [SDR VNAA2016032800034](https://openairdocs.org/sdr/VNAA2016032800034.md): Generator · failed · Mar 28, 2016 · N256PS · Cndair CL6002B19 · AC Generator-Alternator > CREW REPORTED A LOUD NOISE FROM LT ENGINE FOLLOWED BY PFC, MFD, ACARS, AND LT, RT WINDSHIELD HEAT TEMPORARY FAILURE. THEY DECLARED AN EMERGENCY, DIVERTED TO NEAREST FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE LT ENGINE IDG, AND PERF - [SDR VNAA2015111400006](https://openairdocs.org/sdr/VNAA2015111400006.md): Seal · obstructed · Nov 14, 2015 · N256PS · Cndair CL6002B19 · Passenger/Crew Doors > CREW REPORTED LOUD SQUEAL FROM MAIN CABIN DOOR IN FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, REMOVED DEBRIS FROM PASSENGER DOOR SEAL AREA AND PRESSURIZED ACFT IAW AMM. NO DEFECTS NOTED. ACFT RELEASED FOR SERVICE. - [SDR VNAA2015082700032](https://openairdocs.org/sdr/VNAA2015082700032.md): Post · cracked · Aug 27, 2015 · N256PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > CRACK NOTED AT BS 409 AND VERTICAL POST AT LBL 18, INBD CHANNEL WL 60 APPROXIMATELY.100 INCHES IN LENGTH VERTICALLY AND 53 PERCENT FULL SCREEN HEIGHT. - [SDR VNAA2015072800041](https://openairdocs.org/sdr/VNAA2015072800041.md): Battery Pack · crew error · Jul 28, 2015 · N256PS · Cndair CL6002B19 · Emergency Lighting > CREW REPORTED EMERGENCY LIGHTS WOULD NOT ILLUMINATE. SWITCH WAS LEFT IN THE ARM POSITION. MAINTENANCE INSPECTED, R & R EMERGENCY LIGHT BATTERY PACK NR 4 AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE. - [SDR VNAA2015072800040](https://openairdocs.org/sdr/VNAA2015072800040.md): Battery Pack · crew error · Jul 28, 2015 · N256PS · Cndair CL6002B19 · Emergency Lighting > CREW REPORTED EMERGENCY LIGHTS WOULD NOT ILLUMINATE. SWITCH WAS LEFT IN THE ARM POSITION. MAINTENANCE INSPECTED, R & R EMERGENCY LIGHT BATTERY PACK NR 3 AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE. - [SDR VNAA2015072800039](https://openairdocs.org/sdr/VNAA2015072800039.md): Battery Pack · crew error · Jul 28, 2015 · N256PS · Cndair CL6002B19 · Emergency Lighting > CREW REPORTED EMERGENCY LIGHTS WOULD NOT ILLUMINATE. SWITCH WAS LEFT IN THE ARM POSITION. MAINTENANCE INSPECTED, R & R EMERGENCY LIGHT BATTERY PACK NR 2 AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE. - [SDR VNAA2015072800038](https://openairdocs.org/sdr/VNAA2015072800038.md): Battery Pack · crew error · Jul 28, 2015 · N256PS · Cndair CL6002B19 · Emergency Lighting > CREW REPORTED EMERGENCY LIGHTS WOULD NOT ILLUMINATE. SWITCH WAS LEFT IN THE ARM POSITION. MAINTENANCE INSPECTED, R & R EMERGENCY LIGHT BATTERY PACK NR 1 AND PERFORMED CHECKS IAW AMM ACFT RELEASED FOR SERVICE. - [SDR VNAA2015051500018](https://openairdocs.org/sdr/VNAA2015051500018.md): Light · inoperative · May 15, 2015 · N256PS · Cndair CL6002B19 · Emergency Lighting > CREW REPORTED FORWARD EMERGENCY LIGHT, NR 1 IN FORWARD CABIN ABOVE ROW 2, INOPERATIVE. MAINTENANCE INSPECTED, R & R FORWARD OVERHEAD CEILING EMERGENCY FLOODLIGHT AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE. - [SDR VNAA2015042200039](https://openairdocs.org/sdr/VNAA2015042200039.md): Bulb · inoperative · Apr 22, 2015 · N256PS · Cndair CL6002B19 · Emergency Lighting > CREW REPORTED FORWARD EMERGENCY FLOOD LIGHT IN CEILING INOPERATIVE. MAINTENANCE INSPECTED, R & R FORWARD CEILING EMERGENCY FLOOD LIGHT BULB AND PERFORMED CHECKS IAW AMM. AIRCRAFT RELEASED FOR SERVICE. - [SDR VNAA2014050100003](https://openairdocs.org/sdr/VNAA2014050100003.md): Light · inoperative · May 1, 2014 · N256PS · Cndair CL6002B19 · Emergency Lighting > CREW REPORTED FORWARD ORANGE SECTION OF FLOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE INSPECTED, R & R NR 1 FLOOR LIGHT ASSY AND ORANGE OVERLAY AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE. - [SDR VNAA2014032500020](https://openairdocs.org/sdr/VNAA2014032500020.md): Light · inoperative · Mar 25, 2014 · N256PS · Cndair CL6002B19 · Emergency Lighting > CREW REPORTED EMERGENCY FLOOR LIGHTS AT ROW 1 AND ROW 2 WOULD NOT LIGHT UP AND WERE TORN OUT OF TRACK. MAINTENANCE INSPECTED, R & R EMERGENCY FLOOR LIGHTS AT ROW 1 AND ROW 2 AND PERFORMED CHECKS IAW AMM. AIRCRAFT RELEASED FOR SERVICE. - [SDR VNAA2014022000016](https://openairdocs.org/sdr/VNAA2014022000016.md): Static Wick · damaged · Feb 20, 2014 · N256PS · Cndair CL6002B19 · Pitot/Static System > CREW SUSPECTED A LIGHTNING STRIKE AND REPORTED 2 STATIC WICKS MISSING, 1 ON TAIL AND 1 ON RT WING. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION AND R & R RT HORIZONTAL STABILIZER TIP, REPAIRED RT HORIZONTAL STABILIZER TIP RIB SCREW HOLES AND R & R STATIC - [SDR VNAA2013121400008](https://openairdocs.org/sdr/VNAA2013121400008.md): Window · cracked · Dec 14, 2013 · N256PS · Cndair CL6002B19 · Flight Compartment Windows > CREW REPORTED CAPTAIN SIDE WINDOW, BOTTOM RT CORNER LOOKED CRACKED. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED CAPTAIN SIDE WINDOW IAW COMPONENT MM, FOUND NO DAMAGE OR CRACKS, BUT FOUND SPEED TAPE PEELING ON WINDOW SIDE STRAP. - [SDR VNAA2013110300002](https://openairdocs.org/sdr/VNAA2013110300002.md): Bulkhead · cracked · Nov 3, 2013 · N256PS · Cndair CL6002B19 · Fuselage Main, Bulkhead > DURING SCHEDULED MX FOUND FS 202 PRESSURE BULKHEAD CRACKED AROUND THE PARKING BRAKE CUTOUT. FS 202 PRESSURE BULKHEAD AT THE PARKING BRAKE CUTOUT WAS INSPECTED AND REPAIRED USING AMM. ACFT WAS RELEASED FOR SERVICE. DUP OF 20131103, ADDED END NR TO CONTROL N - [SDR VNAA201311070001](https://openairdocs.org/sdr/VNAA201311070001.md): Bulkhead · cracked · Nov 3, 2013 · N256PS · Cndair CL6002B19 · Fuselage Main, Bulkhead > DURING SCHEDULED MX FOUND FS 202 PRESSURE BULKHEAD CRACKED AROUND THE PARKING BRAKE CUTOUT. FS 202 PRESSURE BULKHEAD AT THE PARKING BRAKE CUTOUT WAS INSPECTED AND REPAIRED USING AMM. ACFT WAS RELEASED FOR SERVICE. - [SDR VNAA2013080600001](https://openairdocs.org/sdr/VNAA2013080600001.md): Cabin Pressure · malfunctioned · Aug 6, 2013 · N256PS · Cndair CL6002B19 · Cabin Pressure Control System > CREW REPORTED ALL PRESSURIZATION SHUT OFF AT FL 240. FOLLOWED EMERGENCY DESCENT PROCEDURE AND QRH. LT PACK HIGH TEMP MESSAGE ALSO RECEIVED IN THE DESCENT. DIVERTED, DROPPED MASKS AND LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED MAINFEED MANIFOLD FOR CRACKS - [SDR VNAA2013072500019](https://openairdocs.org/sdr/VNAA2013072500019.md): A/C Pack · malfunctioned · Jul 25, 2013 · N256PS · Cndair CL6002B19 · Cabin Cooling System > CREW REPORTED RT PACK HIGH PRESSURE MESSAGE ON TAKEOFF. ABORTED TAKEOFF AND RETURNED TO GATE. MX COMPLIED WITH OPS CHECK OF RT PACK IAW ACFT MM. ACFT RELEASED FOR SERVICE. - [SDR VNAA2012112600019](https://openairdocs.org/sdr/VNAA2012112600019.md): Inverter · inoperative · Nov 26, 2012 · N256PS · Cndair CL6002B19 · Emergency Lighting > CREW REPORTED FLOOR EMERGENCY LIGHTS FROM ROW NINE (9) AFT INOPERATIVE. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED NUMBER FOUR (4) INVERTER AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE. - [SDR VNAA2012062900013](https://openairdocs.org/sdr/VNAA2012062900013.md): Bpsu · failed · Jun 29, 2012 · N256PS · Cndair CL6002B19 · Trailing Flap Position Indicating System > CREW REPORTED FLAPS FAIL CAUTION MESSAGE WHILE CLIMBING THROUGH 11,000 FEET. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED LEFT BPSU (BRAKE AND POSITION SENSOR UNIT) AND PERFORMED CHECKS USING FIM. AIRC - [SDR VNAA2012062800012](https://openairdocs.org/sdr/VNAA2012062800012.md): Bpsu · failed · Jun 28, 2012 · N256PS · Cndair CL6002B19 · Trailing Flap Position Indicating System > CREW RECEIVED FLAPS FAIL AMBER MESSAGE IN FLIGHT. CREW LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED LEFT BPSU (BRAKE AND POSITION SENSOR UNIT) AND PERFORMED CHECKS USING FIM. AIRCRAFT RELEASED FOR SERVICE. - [SDR VNAA2012062800011](https://openairdocs.org/sdr/VNAA2012062800011.md): Warning System · false activation · Jun 28, 2012 · N256PS · Cndair CL6002B19 · Trailing Flap Position Indicating System > CREW RECEIVED FLAPS FAIL AMBER MESSAGE IN FLIGHT. CREW LANDED WITHOUT INCIDENT. SYSTEM RESET AND AIRCRAFT RELEASED FOR SERVICE USING AD PROCEDURE. Next page: https://openairdocs.org/deregistered/N256PS-2025-02-26/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 = 'N256PS' AND deregistration_id = 'N256PS-2025-02-26' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N256PS-2025-02-26/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.