N560NN

Service difficulty reports · 52

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 = 'N560NN' AND registry_match = 'registration'
  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 VNAA2026062619801Fan · failedRECIRCULATION FAN FAULT MESSAGE. DEFERRED RECIRCULATION FAN NR 2 IAW MEL 21-22-01-2 CAT C. FC FUNCTION C/W BY PULLING AND COLLARING CBP-2 A5, B11. REMOVED AND REPLACED #2 RECIRCULATION FAN IAW CRJ900 AMM TASK21€“22€“10€“000/400€“801. OPS CHECK GOOD, THISJun 23, 2026 · N560NN · Cndair CL6002D24 · Air Distribution FanSDR VNAA2026032414601O-Ring · leakingR ENG OIL PRESSURE WARNING ON CLIMB OUT FOLLOWED QRH / REMOVED RH ATS IAW CRJ 900 AMM 80-11-01-000-801-A01 AND FOUND O-RING ON SPLINED SHAFT TO BE INSTALLED INCORRECTLY, FOUND OIL ON UNDERSWIDE OF THE HOUSING SEEPING OUT FROM THE GEAR BOX. REMOVED AND REINSTAMar 22, 2026 · N560NN · Cndair CL6002D24 · Turbine Engine Oil SystemSDR VNAA2025010311101Acm · smokeAFTER THE LH ENGINE WAS STARTED, THERE WAS FUMES AND A LIGHT HAZE THROUGHOUT THE CABIN AND COCKPIT. THE PLANE WAS DEBOARDED AND NO MEDICAL ATTENTION WAS REQUIRED. THE FUMES AND SMOKE WENT AWAY AFTER THE ENGINES WERE SHUT DOWN. / REMOVED AND REPLACED ACM IAW CRDec 31, 2024 · N560NN · Cndair CL6002D24 · Cabin Cooling SystemSDR VNAA202401030101Unknown · fumesAFTER THE LH ENGINE WAS STARTED, THERE WAS FUMES AND A LIGHT HAZE THROUGHOUT THE CABIN AND COCKPIT. THE PLANE WAS DEBOARDED AND NO MEDICAL ATTENTION WAS REQUIRED. THE FUMES AND SMOKE WENT AWAY AFTER THE ENGINES WERE SHUT DOWN. / SYSTEM IS DEFERRED AND WILL REQDec 31, 2024 · N560NN · Cndair CL6002D24 · Air Distribution SystemSDR VNAA2024101511101Sensor · false indicationBRAKE OVERHEAT WARNING MESSAGE, LEFT OUTBOARD BRAKE TEMP 20 AFTER TAKEOFF. REMOVED AND REPLACED THE LH OB THERMOCOUPLE IAW CRJ900 AMM 32-46-01-000/400-801-A01-PSA . SELF TEST GOOD.Oct 13, 2024 · N560NN · Cndair CL6002D24 · Landing Gear Brake SystemSDR VNAA2023122811101Probe · malfunctionedLH OB BTMS INDICATIONS ERRONEOUS AFTER TAKEOFF/ QRC/ QRH CW. / REMOVED AND REPLACED LHOB MLG BRAKE TEMPERATURE SENSOR IAW CRJ900 AMM 32-46-01-000/400-801-A01-PSA. OPERATIONAL CHECK GOOD.Dec 25, 2023 · N560NN · Cndair CL6002D24 · Landing Gear Brake SystemSDR VNAA202312140008Skin · dentedDESCRIPTION: SEVERAL DENTS ON FUSELAGE SKIN, SETTLEMNT AREA OF LEFT VENTRAL FIN FAIRING BTW FS 1069.75 TO REAR SPAR DATUM STABILIZER 67.5%, BTW STGR 22LH TO STGR 21LH. CORRECTIVE ACTION: SEVERAL DENTS ON FUSELAGE SKIN, SETTLEMNT AREA OF LEFT VENTRAL FIN FAIRINDec 3, 2023 · N560NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202312130015Support · crackedCRACK ON REFUEL MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH. REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH WAS REPEIRED PER REO 690-28-25-012 REV--Nov 30, 2023 · N560NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202312130016Bracket · corrodedCORROSION ON BRACKET MACHINED (8EA'S) ON FLOOR STRUCTURE AT FWD CARGO COMPARTMENT BTW FS 517 TO FS 661.00+16.00 AND BTW STGR 23 RH TO 22LH. DUE TO NOT DAMAGE ALLOWABLE ON BRACKETS MACHINED (8 EA´S) ON FLOOR STRUCTURE AT FWD CARGO COMPARTMENT BTW FS 517 TO FSNov 29, 2023 · N560NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202312130021Floor Support · corrodedUPPER FACE OF FLOOR BEAM RBL 9 BTW FS 1000.00 TO FS 1047.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE. UPPER FACE OF FLOOR BEAM RBL 9 BTW FS 1000.00 TO FS 1047.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE WAS REPAIRED PER REO 690-53-61-1299. REV --Nov 28, 2023 · N560NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202312130020Floor Support · corrodedDESCRIPTION: CORROSION ON UPPER FACE OF FLOOR BEAM LBL 9 BTW FS 1000.00 TO FS 1047.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE. CORRECTIVE ACTION: CORROSION ON UPPER FACE OF FLOOR BEAM LBL 9 BTW FS 1000.00 TO FS 1047.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURENov 28, 2023 · N560NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202312130019Floor Support · corrodedCORROSION ON UPPER FACE OF FLOOR BEAM LBL27 BTW FS 1000.00 TO FS 1047.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE. UPPER FACE OF FLOOR BEAM LBL 27 BTW FS 1000.00 TO FS 1047.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE WAS REPAIRED PER REO 690-53-61-1293. REV.-Nov 28, 2023 · N560NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202312130018Hinge Fitting · corrodedCORROSION ON AILERON HINGE FITTING LUG BORE NO. 4 OUTBOARD AT LH WING REAR SPAR. AILERON HINGE FITTING LUG BORE NO. 4 OUTBOARD AT LH WING REAR SPAR WAS REPAIRED PER ETI-900-23-006 REV. ORIGINAL & REO 690-57-51-315 REV. - -Nov 28, 2023 · N560NN · Cndair CL6002D24 · AileronsSDR VNAA202312130017Hinge Fitting · corrodedCORROSION ON AILERON HINGE FITTING LUG BORE NO. 4 INBOARD AT RH WING REAR SPAR. AILERON HINGE FITTING LUG BORE NO. 4 INBOARD AT RH WING REAR SPAR WAS REPAIRED PER ETI-900-23-005 REV. ORIGINAL & REO 690-57-51-314 REV. - -Nov 28, 2023 · N560NN · Cndair CL6002D24 · AileronsSDR VNAA202312130001Skin · wornDESCRIPTION: WEAR ON LOWER WING SKIN RH/LH, WS264.00, WS128.00, WS178.00 (SETTLEMENT AREA OF WING ACCESS PANEL 686AB, 692AB, 586AB, 592AB AND 597AB). CORRECTIVE ACTION: LOWER WING SKIN RH /LH, WS264.00, WS128.00, WS178.00 (SETTLEMENT AREA OF WING ACCESS PANENov 28, 2023 · N560NN · Cndair CL6002D24 · Wing, Plate/SkinSDR VNAA202312140007Seat Track · corrodedDESCRIPTION: CORROSION ON FLOOR SEAT RAIL AT LBL 9.00 FROM FS 371.00 TO FS 681.00 CPAX. CORRECTIVE ACTION: FLOOR SEAT RAIL AT LBL 9.00 FROM FS 371.00 TO FS 485.00 CPAX WAS CLEANED PER CRJ900 SRM 51-26-00-001-001-A01 AND DETAILED VISUAL INSPECTION WAS PERFORMEDNov 27, 2023 · N560NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202312140006Seat Track · corrodedDESCRIPTION: CORROSION ON FLOOR SEAT RAIL AT RBL 9.00 FROM FS 349.00 TO FS 681.00 CPAX CORRECTIVE ACTION: DUE TO EXCESSIVE DAMAGE ON FLOOR SEAT RAIL AT RBL 9.00 FROM FS 349.00 TO FS 681.00 CPAX WAS REPLACED PER CRJ-900 SRM 53-41-49-101-001-A02 AND CRJ900 AMM 5Nov 27, 2023 · N560NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202312140003Seat Track · corrodedCORROSION ON SIDE SEAT RAIL STGR 15 RH BTW FS 785.15 TO FS 847 + 48.00. DUE TO EXCESSIVE DAMAGE ON SIDE SEAT RAIL STGR 15 RH BTW FS 785.15 TO FS 847 + 48.00 WAS REPLACED PER CRJ-900 SRM 53-41-49-101-001-A02 AND CRJ-900 AMM 53-00-49 (A12)Nov 21, 2023 · N560NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202312140001Seat Track · corrodedCORROSION ON SIDE SEAT RAIL STGR 15 RH BTW FS 677 TO 720.85. DUE TO EXCESSIVE DAMAGE ON SIDE SEAT RAIL STGR 15 RH BETWEEN FS677 - FS720.85 WAS REPLACED PER CRJ-900 SRM 53-41-49-101-001-A02 AND CRJ-900 AMM 53-00-49 (A12)Nov 21, 2023 · N560NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202312140010Hinge · corrodedCORROSION ON HINGE AT PASSENGER DOOR UPPER STEP. DUE TO DAMAGE IS NOT ALLOWABLE ON HINGE AT PASSENGER DOOR UPPER STEP WAS REPLACED PER CRJ900 SRM 52-11-04-101-001-A01 AND CRJ900 AMM 52-11-04 (CONFIG A01)Nov 11, 2023 · N560NN · Cndair CL6002D24 · Fuselage, Door HingeSDR VNAA202312140009Skin · dentedDESCRIPTION: SEVERAL DENTS ON FUSELAGE SKIN, SETTLEMNT AREA OF RIGTH VENTRAL FIN FAIRING BTW FS 1069.75 TO REAR SPAR DATUM STABILIZER 67.5%, BTW STGR 22RH TO STGR 21RH.CORRECTIVE ACTION: SEVERAL DENTS ON FUSELAGE SKIN, SETTLEMNT AREA OF RIGTH VENTRAL FIN FAIRINov 11, 2023 · N560NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202312140005Seat Track · corrodedCORROSION ON SIDE SEAT RAIL STGR 15 LH BTW FS 785.15 TO FS 847 +48.00. SIDE SEAT RAIL STGR 15 LH BTW FS 785.15 TO FS 847 +48.00 AT PASSENGER CABIN FLOOR STRUCTURE WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 FIGURE 53-41-49-991-806 AND WAS Nov 9, 2023 · N560NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202312140004Seat Track · corrodedCORROSION ON SIDE SEAT RAIL STGR 15 LH BTW FS 744.15 TO FS 761.85. SIDE SEAT RAIL STGR 15 LH BTW FS 744.15 TO FS 761.85 AT PASSENGER CABIN FLOOR STRUCTURE WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND WAS REPLACED PER CRJ900 AMM 53-00-49Nov 9, 2023 · N560NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202312140002Seat Track · corrodedDESCRIPTION: CORROSION ON SIDE SEAT RAIL STGR 15 RH BTW FS 744.15 TO FS 761.85 CORRECTIVE ACTION: SIDE SEAT RAIL STGR 15 RH BTW FS 744.15 TO FS 761.85 AT PASSENGER CABIN FLOOR STRUCTURE WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND WAS RNov 9, 2023 · N560NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202312130022Seat Track · corrodedCORROSION ON SEAT RAIL RBL 9 BTW FS 847.00 + 16.00 TO FS 977.00 AT PASSENGER CABIN FLOOR STRUCTURE. SEAT RAIL RBL 9 BTW FS 847.00 + 16.00 TO FS 977.00 AT PASSENGER CABIN FLOOR STRUCTURE WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-51-49-101-001-A02 AND WAS RENov 9, 2023 · N560NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202312130014Intercostal · corrodedCORROSION ON INTERCOSTALS (2 EAS)AT RH/LH SIDE IN STA. FS= 349 TO FS= 364 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT. (E/E) INTERCOSTALS (2 EAS)AT RH/LH SIDE IN STA. FS= 349 TO FS= 364 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT. (E/E) WERE REPLACED PER CRJ900 Nov 7, 2023 · N560NN · Cndair CL6002D24 · Fuselage Main, StructureSDR VNAA202312130013Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACENov 6, 2023 · N560NN · Cndair CL6002D24 · Vertical StabilizerSDR VNAA202312130012Drag Angle · crackedDESCRIPTION: CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CORRECTIVE ACTION: DRAG ANGLE WAS REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01Nov 6, 2023 · N560NN · Cndair CL6002D24 · Vertical StabilizerSDR VNAA202312130003Web · crackedDESCRIPTION: CRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00. (SM) CORRECTIVE ACTION: ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00. (SM) WAS REPAIRED PER REO 690-53-11-1637. REV -- AND CRJ-900 SRM 5Nov 6, 2023 · N560NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202312130011Skin · damagedDESCRIPTION: LIGHTNING STRIKE ON FWD FUSELAGE, ABOVE FLOOR BTW STGR 7-8 LH AND FS 501.00 CORRECTIVE ACTION: LIGHTNING STRIKE ON FWD FUSELAGE, ABOVE FLOOR BTW STGR 7-8 LH AND FS 501.00 WAS REPAIRED PER CRJ900 SRM 53-00-00-201-003-A03.Nov 5, 2023 · N560NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202312130010Skin · damagedDESCRIPTION: LIGHTNING STRIKE ON FWD FUSELAGE, ABOVE FLOOR BTW STGR 15 LH AND FS661.00+32.00. CORRECTIVE ACTION: LIGHTNING STRIKE ON FWD FUSELAGE, ABOVE FLOOR BTW STGR 15 LH AND FS661.00+32.00 WAS REPAIRED PER CRJ900 SRM 53-00-00-201-003-A03.Nov 5, 2023 · N560NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202312130009Skin · damagedDESCRIPTION: LIGHTNING STRIKE ON FWD FUSELAGE, ABOVE FLOOR BTW STGR 16-17 LH AND FS501.00-FS517.00 CORRECTIVE ACTION: LIGHTNING STRIKE ON FWD FUSELAGE, ABOVE FLOOR BTW STGR 16-17 LH AND FS501.00-FS517.00 WAS REPAIRED PER CRJ900 SRM 53-00-00-201-003-A03.Nov 5, 2023 · N560NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202312130008Skin · damagedDESCRIPTION: LIGHTNING STRIKE ON CENTER FUSELAGE, ABOVE FLOOR BTW STGR 14 LH AND FS830.40-FS830.40+16. CORRECTIVE ACTION: LIGHTNING STRIKE ON CENTER FUSELAGE, ABOVE FLOOR BTW STGR 14 LH AND FS830.40-FS830.40+16 WAS REPAIRED PER CRJ900 SRM 53-00-00-201-003-A03.Nov 5, 2023 · N560NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202312130007Skin · burnedDESCRIPTION: LIGHTNING STRIKE ON CENTER FUSELAGE, ABOVE FLOOR BTW STGR 11 LH AND FS693.00-FS708.00. CORRECTIVE ACTION: LIGHTNING STRIKE ON CENTER FUSELAGE, ABOVE FLOOR BTW STGR 11 LH AND FS693.00-FS708.00 WAS REPAIRED PER CRJ900 SRM 53-00-00-201-003-A03.Nov 5, 2023 · N560NN · Cndair CL6002D24 · Fuselage Main, StructureSDR VNAA202312130006Skin · damagedDESCRIPTION: LIGHTNING STRIKE ON REAR FUSELAGE BTW FS 1088.20 AND STGR O- STGR 1 RH. CORRECTIVE ACTION: LIGHTNING STRIKE ON REAR FUSELAGE BTW FS 1088.20 AND STGR O- STGR 1 RH WAS REPAIRED PER CRJ900 SRM 53-00-00-201-003-A03.Nov 5, 2023 · N560NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202312130005Skin · nickedNICK (1EA) ON REAR FUSELAGE BTW FS1015.00-FS1031.00 AND STGR 18-19 RH. NICK (1EA) ON REAR FUSELAGE BTW FS1015.00-FS1031.00 AND STGR 18-19 RH WAS BLEND OUT PER CRJ-900 SRM 51-12-00-001-001-A01 AND EVALUATED WITHIN LIMITS PER CRJ900 SRM 53-61-01-101-004-A02, FNov 5, 2023 · N560NN · Cndair CL6002D24 · Fuselage Main, StructureSDR VNAA202312130004Skin · corrodedCORROSION ON CUT OUT AT MAIN AVIONICS COMPARTMENT DOOR BTW FS 364.00 TO FS394.00 AND STGR 25LH TO 25RH. CUT OUT AT MAIN AVIONICS COMPARTMENT DOOR BTW FS 364.00 TO FS394.00 AND STGR 25LH TO 25RH WAS REPAIRED PER REO 690-53-21-032. REV --Nov 5, 2023 · N560NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202312130002Skin · nickedDESCRIPTION: SEVERAL NICKS ON REAR FUSELAGE BTW FS1015.00-FS1051.30 AND STGR 24RH-27RH CORRECTIVE ACTION: SEVERAL NICKS ON REAR FUSELAGE BTW FS1015.00-FS1051.30 AND STGR 24RH-27RH WERE REPAIRED PER REO 690-53-61-1290 REV - -, AND EVALUATED WITHIN LIMITS PER CRNov 3, 2023 · N560NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA2023092611102Fadec · warning messageL FADEC FAULT 1 STATUS MSG. REMOVED AND REPLACED L FADEC IAW CRJ 900 AMM 73-21-01-000/400-801. PERFORMED READ BACK OF THE ENGINE CONFIGURATION DATA WITH THE MDC. DATA READ BACK GOOD. POBIT CHECK GOOD AT THIS TIME.Sep 21, 2023 · N560NN · Cndair CL6002D24 · Fuel Controlling SystemSDR VNAA202309221111Control Valve · intermittentL PACK INTERMITTENT IN FLIGHT / REMOVED AND REPLACED LH FLOW CONTROL VALVE IAW CRJ900 AMM 21-53-14-000/400-801-A01. OPS AND LEAK CHECK GOOD.Sep 20, 2023 · N560NN · Cndair CL6002D24 · Cabin Cooling SystemSDR VNAA202305011111Shock Absorber · unserviceableGEAR DISAGREE MSG WHEN GEAR SELECTED UP ON CLIMBOUT / REMOVED NLG SHOCK STRUT IAW CRJ900 AMM 32-21-01-000-801. COMPLETED THE INSTALLATION OF THE NLG SHOCK STRUT IAW CRJ900 AMM 32-21-01-400-801. FINISHED INSTALL OF NLG SHOCK STRUST ASSY FROM STEP B(8) AND ON IAApr 28, 2023 · N560NN · Cndair CL6002D24 · Main Landing Gear Strut/Axle/TruckSDR VNAA202303301112Pin · unserviceableN1 FAN VIB R ENG CW QRH 2-32 AND QRH 2.10 ( INTENSIONAL SHUTDOWN) VIB INTERMITTENT BUT BECAME PRESSISTANT 1.7 - 1.9 N1. REMOVED AND REPLACED RH ENGINE FAN BLADE PINS IAW CRJ 900 AMM 12ˆ’20ˆ’72ˆ’640ˆ’803 (CONFIG A01). TORQUE CHECK GOOD.Mar 27, 2023 · N560NN · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR VNAA202303201111Fadec · unserviceableDURING TAKEOFF/CLIMB AT 14000 R FADEC CAUTION MESSAGE. R/R RH FADEC IAW CRJ 900 AMM 73-21-01-000/400-801. OPS CHECK GOOD.Mar 18, 2023 · N560NN · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR VNAA202103041112Windshield · failedBURNING ODOR FROM FLIGHT DECK SMOKE FROM LOWER LEFT SIDE OF WINDSHIELD ON THE CA SIDE. INSPECTED CA WINDSHIELD IAW CRJ 900 AMM 56-11-01-210-80-A01-PSA. FOUND ARCING ON THE TERMINAL BLOCK. REMOVED THE SIDE STRAP IAW CRJ 900 AMM 56-10-05-000-801-A01 AND REMOVED Mar 2, 2021 · N560NN · Cndair CL6002D24 · Flight Compartment WindowsSDR VNAA202101261114Proximity Sensor · abnormalDURING CLIMB OUT FROM PNS, THE CREW RECEIVED A NOSE GEAR DOOR OPEN WARNING. THEY RAN THE QRH, WHICH INSTRUCTED THEM TO LAND AT THE NEAREST SUITABLE AIRPORT. THEY CHOSE TO RETURN TO PNS. NO EMERGENCY WAS DECLARED. REMOVED AND REPLACED PROXIMITY SENSOR PX31, Jan 25, 2021 · N560NN · Cndair CL6002D24 · Landing Gear Position and WarningSDR VNAA2020062511103Battery Pack · dischargedOVERHEAD CABIN EMERGENCY LIGHTS FACING AIRCRAFT FRONT AND OVERWING EXIT EMERGENCY LIGHTS NEAR FLOOR BY FORWARD EXIT FLICKERING AND GOING OUT. MX REPLACED ALL 4 EMERGENCY BATTERY PACKS. OPS CHECK GOOD. BATTERY PACK 1 P/N OFF 2013-1A S/N OFF 73997 TSN 35158 HJun 24, 2020 · N560NN · Cndair CL6002D24 · Emergency LightingSDR VNAA2019100191102Acm · failedSMOKE STARTED FILLING THE CABIN WHILE TAXIING TO THE GATE IN CLT. THE CREW CALLED FOR FIRE TRUCKS HAD THE PASSENGERS DEPLANE THROUGH THE MAIN CABIN IN THE WEST HARDSTAND. NO INJURIES WERE REPORTED. REMOVED AND REPLACED L/H PACK AIR CYCLE MACHINE OPS CHECK GOSep 30, 2019 · N560NN · Cndair CL6002D24 · Cabin Cooling SystemSDR VNAA2018112611102Pin · disconnectedTHE AIRCRAFT DIVERTED DUE TO LEFT AND RIGHT WING ANTI-ICE CAUTION MESSAGE AND FLAPS FAIL. MAINTENANCE WAS DISPATCHED AND FOUND PIN 4 ON CONNECTOR A105P1. RECONNECT PIN AND ALL PROBLEMS OPERATIONAL CHECK GOODNov 26, 2018 · N560NN · Cndair CL6002D24 · Flight Control System WiringSDR VNAA2018031611101Warning Message · illuminatedDURING APPROACH, THE CREW RECEIVED AN OUTBOARD SPOILERONS, OUTBAORD SPOILERS CAUTION MESSAGE. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. SYSTEM RESET, MESSAGE CLEARED DID NOT REOCCUR.Mar 16, 2018 · N560NN · Cndair CL6002D24 · Drag Control SystemSDR VNAA2016120400008Acm · seizedRIGHT AIR CONDITIONING PACK PRODUCED SMOKE IN THE CABIN. THE CREW RETURNED TO GATE. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE AIR CYCLE MACHINE, AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.Dec 4, 2016 · N560NN · Cndair CL6002D24 · Cabin Cooling System
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