N597NN

Service difficulty reports · 57

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 = 'N597NN' 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 VNAA2026072821401Windshield · crackedFO SIDE WINDSHIELD CRACKING, PERFORMED DAMAGE CHECK OF THE FO SIDE WINDSHIELD IAW AMM 56-11-01-210-801-PSA AND FOUND INTERLAYER BUBBLING IN THE TOP OUTBOARD CORNER. DAMAGE IS WITHIN LIMITS. PERFORMED OPS CHECK OF THE RH WINDSHIELD/SIDE WINDOW TEMP CONTROLLER Jul 24, 2026 · N597NN · Cndair CL6002D24 · Flight Compartment WindowsSDR VNAA2025081911102Warning Message · illuminatedL ENG ITT WENT TO 966°C ON T/O WHILE IN TOGA FULL THRUST TO CLIMB TO LOWER ITT. / PERFORMED ENGINE WASH WITH CLEANING SOLUTION FOR PERFORMANCE IAW AMM 72-00-00-100-803-A01-PSA. ITT WITHIN LIMITS.Aug 17, 2025 · N597NN · Cndair CL6002D24 · Central WarningSDR VNAA202504140020Skin · wornSKIN, FUSELAGE BETWEEN FS 1031.00-FS1051.30 & STR21R-STR26R PERFORM INSPECTION EVERY 15800 FC FROM INITIAL REPAIR PER STS EA 48-2019-090 REV A. SKIN, FUSELAGE BETWEEN FS 1031.00-FS1051.30 & STR21R-STR26R WAS REPAIRED PER REO 690-53-61-1531 REV.--Mar 12, 2025 · N597NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202504130008Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE AND FWD DRAG ANGLE (2 E/AS) BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE AND FWD DRAG ANGLEMar 11, 2025 · N597NN · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous StructureSDR VNAA202504140019Frame · damagedELONGATED HOLE ON FRAME BTW STA FS 661.00 + 62.00 STRG 23LH TO STRG 24LH AT FWD CARGO COMPARTMENT. ELONGATED HOLE ON FRAME BTW STA FS 661.00 + 62.00 STRG 23LH TO STRG 24LH AT FWD CARGO COMPARTMENT WAS REPAIRED PER EA NO: 53-2025-0353 REV.--Mar 10, 2025 · N597NN · Cndair CL6002D24 · Fuselage Main, FrameSDR VNAA202504140018Frame · wornWEAR ON FRAME BTW FS785.15 AT RH AFT EMERGENCY DOOR. WEAR ON FRAME BTW FS785.15 AT RH AFT EMERGENCY DOOR WAS BLENDED PER CRJ 900 SRM 51-12-00-001-001-A01 AND EVALUATED WITHIN LIMITS PER REO 690-53-41-524 REV. - -.Mar 10, 2025 · N597NN · Cndair CL6002D24 · Fuselage Main, FrameSDR VNAA202504140021Fitting · corrodedCORROSION ON FITTING (2EA) BELOW THE SERVICE TABLE AND AISLE SIDE AT FWD LAV. FITTING PN:A414252-3 (1EA) BELOW THE SERVICE TABLE WAS REPLACED PER SAFRAN CMM 25-40-40 AND FITTING PN: A414251-1 (1EA) AISLE SIDE AT FWD LAV WAS FABRICATED AND INSTALLED PER EAMar 9, 2025 · N597NN · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR VNAA202504140017Rib · crackedCRACK IN FIXED LEADING EDGE RIB SS57.16 AT RH WING. RIB CRACKED SS57.16 AT RH WING WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-10-001-001-A01.Mar 9, 2025 · N597NN · Cndair CL6002D24 · Wing, Rib/BulkheadSDR VNAA202504140015Canister · crackedCRACKS IN CANISTER, WELDED NO.3 IN STA. WS148 OF INTERNAL LH MAIN FUEL TANK. CANISTER, WELDED NO.3 IN STA. WS148 OF INTERNAL LH MAIN FUEL TANK WAS REPAIRED PER REO670-57-42-577. REV.--.Mar 9, 2025 · N597NN · Cndair CL6002D24 · Wing Miscellaneous StructureSDR VNAA202504140013Canister · crackedCRACKS IN CANISTER, WELDED NO.3 IN STA. WS148 OF INTERNAL RH MAIN FUEL TANK. CANISTER, WELDED NO.3 IN STA. WS148 OF INTERNAL RH MAIN FUEL TANK WAS REAPIARED PER REO670-57-42-577. REV.--Mar 9, 2025 · N597NN · Cndair CL6002D24 · Wing Miscellaneous StructureSDR VNAA202504140012Intercostal · corrodedCORROSION ON INTERCOSTALS (2 EAS) IN STA. FS= 349 TO FS= 364 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT. INTERCOSTALS (2EAS) BTW FS349.00 TO FS364.00 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-003-A02 ANDMar 9, 2025 · N597NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202504140010Doubler · corrodedCORROSION ON INTERNAL PRODUCTION DOUBLER IN STA. FS= 295 TO FS= 310 BTWN STGR 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT. (E/E) INTERNAL PRODUCTION DOUBLER IN STA. FS= 295 TO FS= 310 BTWN STGR 26LH TO 26RH AT MAIN AVIONICS COMPARTMEN WAS EVALUATED OUT OF LIMIMar 9, 2025 · N597NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202504140014Frame · corrodedCORROSION ON FRAME 1088.20 BTW STGR 25LH/STGR 27 AT AFT BAGGAGE BAY COMPARTMENT. CORROSION ON FRAME 1088.20 BTW STGR 25LH/STGR 27 AT AFT BAGGAGE BAY COMPARTMENT WAS REMOVED PER CRJ 900 SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN LIMITS PER CRJ-900 SRM 52-3Mar 8, 2025 · N597NN · Cndair CL6002D24 · Fuselage Main, FrameSDR VNAA202504140011Stringer · corrodedCORROSION ON STRINGER 22RH BTWN FS. 333.00 TO FS 349.00 AT MAIN AVIONICS COMPARTMENT. (E/E). CORROSION ON STRINGER 22RH BTWN FS. 333.00 TO FS 349.00 AT MAIN AVIONICS COMPARTMENT. (E/E) WAS EVALUATED OUT LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND REPLACED Mar 8, 2025 · N597NN · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR VNAA202504140009Stringer · corrodedCORROSION ON STGR 27 BTWN FS 280.00 AND FS 310. CORROSION ON STGR 27 BTWN FS 280.00 AND FS 310.00 WERE EVALUATED OUT LIMITS PER CRJ900 SRM 53-21-03-101-002-A04 AND REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.Mar 8, 2025 · N597NN · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR VNAA202504140008Stringer · crackedCRACK ON STGR 3LH (LINTEL AREA) STA. FS280.00 AT CIRCUNFERENTIAL SKIN JOINT. CRACK ON STGR 3LH (LINTEL AREA) STA. FS280.00 AT CIRCUNFERENTIAL SKIN JOINT WAS REPAIRED PER 690-53-21-1908 REV. --.THE AIRCRAFT MUST NOT BE OPERATED BEYOND 12 MONTHS FROM THE ISSUEMar 8, 2025 · N597NN · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR VNAA202504140007Seat Track · corrodedCORROSION ON SIDE SEAT RAIL 15RH (5EAS) BTW FS 379.00 TO FS 669.40. SIDE SEAT RAIL 15RH (5EAS) BTW FS 379.00 TO FS 669.40 WERE EVALUATED DUE TO EXCESSIVE DAMAGE PER CRJ-900 SRM 53-41-49-101-001-A02 AND SRM 53-51-49-101-001-A02 AND REPLACED PER CRJ-900 AMM 53Mar 7, 2025 · N597NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202504140006Seat Track · corrodedCORROSION ON SIDE SEAT RAIL 15LH (5 EAS) BTW FS 379.00 TO FS 669.40. SIDE SEAT RAIL 15LH (5 EAS) BTW FS 379.00 TO FS 669.40 WERE EVALUATED PER CRJ-900 SRM 53-21-49-101-001-A01 AND REPLACED PER CRJ-900 AMM 53-00-49-400-801-A12Mar 7, 2025 · N597NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202504140005Seat Track · corrodedCORROSION ON SIDE SEAT RAIL 15LH (6EAS) BTW FS 669.40 TO FS 977. SIDE SEAT RAIL 15LH (6EAS) BTW FS 669.40 TO FS 977.00 WERE EVALUATED DUE TO EXCESSIVE DAMAGE PER CRJ/900 SRM 53-41-49-101-001-A02 AND REPLACED PER CRJ/900 SRM 53-00-49-400-801 (CONFIG A12)Mar 7, 2025 · N597NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202504140004Seat Track · corrodedCORROSION ON SIDE SEAT RAIL 15RH (6EAS) BTW FS 669.40 TO FS 977. SIDE SEAT RAIL 15RH (6EAS) BTW FS 669.40 TO FS 977.00 WERE EVALUATED DUE TO EXCESSIVE DAMAGE PER CRJ900 SRM 53-41-49-101-001-A02 AND SRM 53-51-49-101-001-A02 AND REPLACED PER CRJ-900 AMM 53-00-Mar 7, 2025 · N597NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202504140003Angle · corrodedCORROSION ON MID CAP BTW FS 310.00 TO FS 349.00 AT SURROUND STRUCTURE PASSENGER DOOR. CORROSION ON MID CAP BTW FS 310.00 TO FS 349.00 AT SURROUND STRUCTURE PASSENGER DOOR WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-001-A02 AND WAS REPLACED PER CRMar 7, 2025 · N597NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202504140002Seat Track · corrodedCORROSION ON SEAT RAILS OF LBL27 BTW FS477.40 TO FS581.00 (2EA). DUE TO EXCESIVE DAMAGE SEAT RAILS OF LBL27 BTW FS477.40 TO FS581.00 (2EA) WERE REPLACED PER CRJ-900 SRM 53-31-49-101-001-A02 , CRJ-900 SRM 53-31-49-991-806 AND PER CRJ-900 AMM 53-00-49.Mar 7, 2025 · N597NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202504140001Seat Track · corrodedCORROSION ON SEAT RAILS OF LBL9 BTW FS364.00 TO FS693.00 (5EA). DUE TO EXCESSIVE DAMAGE ON SEAT RAILS OF LBL9 BTW FS364.00 TO FS693.00 (5EA) WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01, CRJ-900 SRM 53-31-49-101-001-A02 AND CRJ-900 SRM 5Mar 7, 2025 · N597NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202504130015Seat Track · corrodedCORROSION ON SEAT RAILS OF RBL9 BTW FS349.00 TO FS693.00 (6EA) SUMMARY: SEAT RAILS OF RBL9 BTW FS349.00 TO FS693.00 (6EA) WERE EVALUATED OUT LIMITS PER CRJ 900 SRM 53-21-49-101-001-A01 AND SRM 53-31-49-101-001-A02 AND SRM 53-41-49-101-001-A02 AND WERE REPLACEDMar 7, 2025 · N597NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202504130010Hinge · wornWEAR ON PASSENGER DOOR HINGE (FUSELAGE SIDE) LUG LAND. PASSENGER DOOR HINGE (FUSELAGE SIDE) LUG LAND WAS REPAIRED PER REO 670-52-11-511 REV. -EMar 7, 2025 · N597NN · Cndair CL6002D24 · Fuselage, Door HingeSDR VNAA202504130014Bracket · corrodedCORROSION ON MACHINED BRACKET (7EA) OF FLOOR STRUCTURE AT FWD CARGO COMPARTMENT. MACHINED BRACKET (3EA) OF FLOOR STRUCTURE AT FWD CARGO COMPARTMENT (FS533/FS549, BTW STGR 25/24, FS 565 BTW STGR 21/22, FS 645/ 661 BTW STGR 25/24 WERE CLEANED PER CRJ900 SRM 51-Mar 6, 2025 · N597NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202504130013Web · crackedCRACK ON ELECTRICAL BAY FLOOR WEB RH SIDE (BELOW ADG SUPPORT DOUBLER) FS193. CRACK ON ELECTRICAL BAY FLOOR WEB RH SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00 WAS REPAIRED PER REO 690-53-11-1965 REV. -- AND PER REO 670-53-11-509 REV. -EMar 6, 2025 · N597NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202504130011Skin Panel · dentedDENT ON FWD FUSELAGE SKIN ON STGR 22 LH BTW FS 349.00 TO FS 364.00. DENT ON FWD FUSELAGE SKIN ON STGR 22 LH BTW FS 349.00 TO FS 364.00. WAS REPAIRED PER 690-53-21-1907 REV. --. UNTIL A TRANSPORT CANADA ACCEPTED NDTM TECHNIQUE HAS BEEN MADE AVALIABLE, THE AIRMar 6, 2025 · N597NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202504130009Plate · corrodedCORROSION WAS FOUND ON KICKPLATE OF SURROUND STRUCTURE AT PASSENGER DOOR (L1). CORROSION ON KICKPLATE OF SURROUND STRUCTURE AT PASSENGER DOOR (L1) WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND WAS EVALUATED WITHIN LIMITS PER CRJ900 SRM 53-21-23-101-001-Mar 5, 2025 · N597NN · Cndair CL6002D24 · Fuselage Main, StructureSDR VNAA202504130007Drag Angle · crackedCRACK 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). CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM Mar 5, 2025 · N597NN · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous StructureSDR VNAA202504130004Skin · wornWEAR ON SETTLEMENT AREA OF ACCESS PANELS 683AB, 686AB, 692AB 695AB AND 697AB. WEAR ON SETTLEMENT AREA OF ACCESS PANELS 683AB, 695AB AND 697AB WERE BLEND OUT PER CRJ-900 SRM 51-12-00-001-001-A01 EVALUATED WITHIN LIMITS PER CRJ-900 SRM 57-00-01-101-001-A03. WEMar 5, 2025 · N597NN · Cndair CL6002D24 · Wing, Plate/SkinSDR VNAA202504130002Skin · scratchedSCRATCHES ON WINGS LOWER SURFACE RH WING REAR SIDE BTW WS294.50-WS343.50 AND LH WING REAR SIDE AT WS294.50. SCRATCHES ON WINGS LOWER SURFACE RH WING REAR SIDE BTW WS294.50-WS343.50 AND LH WING REAR SIDE AT WS294.50 WERE BLENDED PER CRJ-900 SRM 51-12-00-001-Mar 4, 2025 · N597NN · Cndair CL6002D24 · Wing, Plate/SkinSDR VNAA202504130001Fireshield · wornRH LWR FWD CORE COWL WITHIN 6803.22 FH'S (BEFORE19,898.24 FH'S) REPAIR OR REPLACE THE DISCREPANT ITEM. RH LWR FWD CORE COWL, FIRE SHIELD WERE REPLACED PER. CRJ-900 S.R.M 54-23-00-201-005-A01 AND PER CRJ900 SRM 51-42-06-001-001-A01.Mar 4, 2025 · N597NN · Cndair CL6002D24 · Nacelle/Pylon, Main FrameSDR VNAA202504140016Seat Track · corrodedCORROSION ON FLOOR SEAT RAIL BTW FS 847.00 TO FS977.00 LH/RH (4EAS) AT CABIN PAX. FLOOR SEAT RAIL BTW FS 847.00 TO FS977.00 LH/RH (4EAS) AT CABIN PAX WERE EVALUATED DUE TO EXCESSIVE DAMAGE PER CRJ-900 SRM 53-41-49-101-001-A02 AND SRM 53-51-49-101-001-A02 ANFeb 17, 2025 · N597NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202504130005Hinge · corrodedCORROSION ON HINGE AT ACCESS PANEL 832ET. DUE TO EXCESSIVE DAMAGE ON HINGE AT ACCESS PANEL 832ET WAS EVALUATED PER CRJ-900 SRM 52-11-04-101-001-A01 AND REPLACE PER CRJ-900 SRM 51-41-02-001-001-A01Feb 17, 2025 · N597NN · Cndair CL6002D24 · Passenger/Crew DoorsSDR VNAA2024070811101Windshield · unserviceableRH WINDSHIELD HEAT TERMINAL CONNECTION BLOCK STARTED TO SPARK AND CREATE ELECTRICAL ODOR ON SHORT FINAL, SWITCHED RH WINDSHIELD HEAT TO THE OFF POSITION ORDOR AND SPARKS STOPPED / REMOVED AND REPLACED RH WINDSHIELD IAW CRJ 900 AMM 56-11-01-000/400-801-A01-PSA.Jul 5, 2024 · N597NN · Cndair CL6002D24 · Flight Compartment WindowsSDR VNAA2024042611101None · noneRESET THE AIRCRAFT THEN PERFORMED THE OPERATION TEST OF THE ANTI-SKID CONTROL SYSTEM IAW CRJ 900 AMM 32-44-00-710-801-A01. OPS TEST GOOD AT THIS TIME AND NO FAULT FOUND.Apr 25, 2024 · N597NN · Cndair CL6002D24 · Standard Practices/StructuresSDR VNAA202302271114None · noneDURING OPERATIONS AT HEBRON KY (CVG), THE MAINTENANCE REPORTS A DENT WITH A MINOR GOUGE ON THE L/H FORWARD EMERGENCY EXIT DOOR FORWARD EDGE. DAMAGE 1: 0.5€? L X .25 W X .021€? D. / PERM REPAIR COMPLETED IAW EA-22-C9-52-1317-A.Feb 26, 2023 · N597NN · Cndair CL6002D24 · Emergency ExitsSDR VNAA202110219999Web · crackedFOUND PASSENGER DOOR AFT STAIR WEB TO HAVE A CRACK AT ZONE-3. REPAIRED CRACK ON AFT STAIR WEB IAW CRJ900 SRM 52-11-04-201-004-A01.Oct 21, 2021 · N597NN · Bombdr CL6002D15 · Passenger/Crew DoorsSDR VNAA202110219998Seat Track · corrodedRH SIDE SEAT TRACK FS785-FS847+8.4 SEGMENT IS CORRODED. INSTALLED RH SIDE SEAT TRACK FS 785-FS 847+8.4 IAW CRJ 900 AMM 53-00-49-400-801-A12Oct 21, 2021 · N597NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202110219997Seat Track · corrodedRH SIDE SEAT TRACK FS744.15-FS761.85 SEGMENT IS CORRODED. INSTALLED NEW RH SIDE SEAT TRACK FS744.15 TO FS761.85 IAW CRJ900 AMM 53-00-49-400-801-A12.Oct 21, 2021 · N597NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202110219996Seat Track · corrodedLH SIDE SEAT TRACK FS847+8.4-847+20 SEGMENT IS CORRODED. INSTALLED L/H SIDE SEAT RAIL TRACK FROM FS847+8.4-FS847+20 IAW CRJ900 AMM 53-00-49-400-801-A12.Oct 21, 2021 · N597NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202110219995Seat Track · corrodedLH SIDE SEAT TRACK FS785-FS847+8.4 SEGMENT IS CORRODED. INSTALLED NEW SERVICEABLE LH SIDE SEAT RAIL FS785-FS847+8.4 IAW CRJ900 AMM 53-00-49-400-801 CONFIG A12.Oct 21, 2021 · N597NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202110219994Seat Track · corrodedLH SIDE SEAT TRACK FS744.15-761.85 SEGMENT IS CORRODED. INSTALLED NEW SEAT TRACK AT LH FS744.15 TO FS761.85 PER CRJ900 AMM 53-00-49-400-801-A12.Oct 21, 2021 · N597NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202110219993Seat Track · corrodedCORROSION ON FLOOR SEAT TRACK AT RBL9 FROM FS 349.00 TO FS 485.00. INSTALLED FLOOR SEAT TRACK AT RBL 9 FROM FS 349.00 TO 485.00 IAW CRJ 900 AMM 53-00-44-400-801-A12.Oct 21, 2021 · N597NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202110219992Seat Track · corrodedCORROSION ON FLOOR SEAT TRACK AT LBL 9 FROM FS 364.00 TO FS 485.00. INSTALLED FLOOR SEAT TRACK AT LBL 9 FROM FS 364.00 TO FS 485.00 IAW CRJ 900 AMM 53-00-44-400-801-A12.Oct 21, 2021 · N597NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202110219991Web · crackedPAX DOOR AFT WEB CRACKED. PERFORM PERMANENT REPAIR OF PAX DOOR WEB AFT SIDE OF DOOR AT ZONE 2 E PER CRJ 900 SRM 52-11-04-201-004-A01 PAR 5-6Oct 21, 2021 · N597NN · Bombdr CL6002D15 · Passenger/Crew DoorsSDR VNAA202109021111Terminal Block · arcedON DECENT THE RH TERMINAL BLOCK SPARKED. THE CREW RAN THE QRC AND QRH AND DID A RESET WINDOW HEAT MESSAGE AND THE MESSAGE CAME BACK IMMEDIATELY. THE CREW THEN TURNED OFF THE WINDOW HEAT AND THE MESSAGE DID NOT RETURN AND THEY DID NOT HAVE ANY FURTHER ISSUES. NAug 30, 2021 · N597NN · Cndair CL6002D24 · Window System WiringSDR VNAA202011201111Windshield · debondedWHILE ON DESCENT INTO SBN, THE F/O WINDSHIELD CRACKED TOWARDS THE MIDDLE OF THE WINDOW. ATC DECLARED AN EMERGENCY, THE FLIGHT LANDED WITHOUT INCIDENT. A RESCUE FLIGHT IS BEING SENT UP TO RECOVER THE TURN FLIGHT SBN TO CLT.Nov 19, 2020 · N597NN · Cndair CL6002D24 · Flight Compartment WindowsSDR VNAA2020090511102Bracket · brokenSERVICE DOOR UPPER STABILIZER BAR DOOR BRACKET BROKEN. REMOVED AND REPLACED UPPER STABILIZER BAR DOOR BRACKET ON THE SERVICE DOOR. OPS CHECK GOOD.Sep 4, 2020 · N597NN · Cndair CL6002D24 · Service Doors
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