N585NN

Service difficulty reports · 58

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 = 'N585NN' 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 VNAA2026090824501Heater · inoperativeLEFT PITOT HEAT CAUTION MSG / REMOVED AND REPLACED ADSHC (A78) IAW CRJ 900 AMM 30-31-15-000/400-801-A01. OPS CHECK GOOD.Sep 4, 2026 · N585NN · Cndair CL6002D24 · Pitot/Static Anti-Ice SystemSDR VNAA2026073021601Warning Message · false activationINTERMITTENT RUDDER LIMIT AND XPDR FAIL CAUTION MSG IN FLIGHT WITH INTERMITTENT LOSS OF OIL TEMP, OIL PRESS, CABIN PRESS, AND APU DOOR IN POSITION INDICATION. CREW INFORMED ISSUE HAPPENED UPON TAKEOFF. RERACKED PSEU IAW AMM 32-61-01-000/400-801. OPS CHECK OFJul 27, 2026 · N585NN · Cndair CL6002D24 · Central WarningSDR VNAA2026071221001Steering Sys · faultedSTEERING INOP ON TAKEOFF. PERFORMED MIPM RESET. PROBLEM DID NOT REOCCURJul 8, 2026 · N585NN · Cndair CL6002D24 · Landing Gear Steering SystemSDR VNAA2024120811101Windshield · crackedRH WINSHIELD STARTED ARCING CAUSING CRACK. REMOVED AND REPLACED THE RH WINDSHIELD IAW CRJ 900 AMM 56-10-05-000/400-801-A01.Dec 4, 2024 · N585NN · Cndair CL6002D24 · Flight Compartment WindowsSDR VNAA2024120411102Life Vest · unserviceablePFD 1 FAILS WITH ELECTRICAL BURNING SMELL AND PFD 1 CB PANEL 2 V10 POPPED. PILOTS DESCRIBED HOW THEY SMELLED AN €ŒELECTRICAL BURNING SMELL€?. THE LOCATION OF THE SMELL WAS REPORTED IN THE COCKPIT. THE SOURCE OF THE SMELL WAS THE #1 PFD, WHILE THE DURATION OFDec 2, 2024 · N585NN · Cndair CL6002D24 · Central DisplaySDR VNAA20240726009Seat Track · corrodedCORROSION ON RH SIDE SEAT RAIL BTW FS744.15 TO FS 969.00 (6EA) CORROSION ON RH SIDE SEAT RAIL BTW FS744.15 TO FS 969.00 (6EA) WERE EVALUATED OUT LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 THEREFORE SEAT RAIL BTW FS744.15 TO FS 969.00 (6EA) WERE REPLACED PER CJun 21, 2024 · N585NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20240726004Seat Track · corrodedCORROSION ON SEAT RAILS OF RBL9 BTW FS349.00 TO FS677.00 (6EA). CORROSION ON SEAT RAILS OF RBL9 BTW FS349.00 TO FS677.00 (6EA) WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01 THEREFORE SEAT RAILS OF RBL9 BTW FS349.00 TO FS677.00 (6EA) WERE REJun 21, 2024 · N585NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20240726003Seat Track · corrodedCORROSION ON LH SIDE SEAT RAIL BTW FS744.15 TO FS 969.00 (5EA). CORROSION ON LH SIDE SEAT RAIL BTW FS744.15 TO FS 969.00 (5EA) WERE EVALUATED OUT LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 THEREFORE LH SIDE SEAT RAIL BTW FS744.15 TO FS 969.00 (5EA) WERE REJun 21, 2024 · N585NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20240726002Seat Track · corrodedCORROSION ON LH SIDE SEAT RAIL BTW FS379.00 TO FS677.00 (5EA). LH SIDE SEAT RAIL BTW FS379.00 TO FS677.00 (5EA) WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01 AND CRJ900 SRM 53-31-49-101-001-A02 AND WERE REPLACED PER CRJ-900 AMM 53-00-49-A1Jun 21, 2024 · N585NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20240726001Seat Track · corrodedCORROSION ON RH SIDE SEAT RAIL BTW FS379.00 TO FS 720.85 (5EA) RH SIDE SEAT RAIL BTW FS379.00 TO FS 720.85 (5EA) WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01 AND CRJ900SRM 53-31-49-101-001-A02 AND WERE REPLACED PER CRJ-900 AMM 53-00-49-A12Jun 21, 2024 · N585NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20240723018Hinge Fitting · excess playINITIAL INSPECTION: FREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. HINGE FITTING NO, 2 AND NO, 3 WERE REPLACED PER RIL #2103 REV. B.Jun 21, 2024 · N585NN · Bombdr CL6002D15 · Vertical StabilizerSDR VNAA20240723017Seat Track · corrodedDISCREPANCY: CORROSION ON SEAT RAILS OF LBL9 BTW FS708.00 TO FS1000.00. CORROSION ON SEAT RAILS OF LBL9 BTW FS708.00 TO FS1000.00. EVALUATED OUT LIMITS PER CRJ900 SRM 53-41-49-101-001-A02, SEAT RAILS OF LBL9 BTW FS708.00 TO FS1000.00. REPLACED PER AMM 53-Jun 21, 2024 · N585NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20240723016Seat Track · corrodedCORROSION ON SEAT RAILS OF RBL9 BTW FS693.00 TO FS847+16. CORROSION ON SEAT RAILS OF RBL9 BTW FS693.00 TO FS847+16. EVALUATED OUT LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 THEREFORE SEAT RAILS OF RBL9 BTW FS693.00 TO FS847+16 WAS REPLACED PER PER CRJ900 AMJun 21, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA20240726015Frame · corrodedCORROSION ON FRAME FS= 310.00 BETWEEN STRG 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT. (E/E) CORROSION ON FRAME FS= 310.00 BETWEEN STRG 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT WAS REMOVED AND EVALUTED WITHIN LIMITS PER CRJ900 SRM 53-00-06-201-005-A01Jun 20, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Main, FrameSDR VNAA20240726006Mount · corrodedCORROSION ON ANGLE, MOUNTING BTW FS 319.70 AND FS 349.00 AT SERVICE DOOR SURROUND STRUCTURE. CORROSION ON ANGLE, MOUNTING BTW FS 319.70 AND FS 349.00 AT SERVICE DOOR SURROUND STRUCTURE WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-002-A02 AND REPLAJun 20, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Structure (General)SDR VNAA20240723008Bracket · corrodedCORROSION ON BRACKETS, MACHINED (6EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT. BRACKETS, MACHINED (6EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-32-58-101-001-A01 AND WERE REPLACED PER CRJ900 SRM Jun 20, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA20240726013Floorbeam · corrodedCORROSION INSIDE OF FLOOR PANEL SUPPORT ANGLE WITH THE CROSSBEAM UNION AT FS280.00 BTW RBL 12.00 AND LBL 12.00. FLOOR PANEL SUPPORT ANGLE WITH THE CROSSBEAM UNION AT FS280.00 BTW RBL 12.00 AND LBL 12.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101Jun 19, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Main, Floor BeamSDR VNAA20240726011Frame · corrodedCORROSION ON CIRCUMFERENTIAL JOINT FS 280.00 TO FS 282.86 BTW STGR 23LH TO STGR 22RH. CORROSION ON CIRCUMFERENTIAL JOINT FS 280.00 TO FS 282.86 BTW STGR 23LH TO STGR 22RH WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01, EVALUATED WITHIN LIMITS PER CRJ900 SRM Jun 19, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Main, FrameSDR VNAA20240726010Strap · corrodedCORROSION ON JOINT STRAP FS= 333.00 BETWEEN STRG 27 TO 26RH AT MAIN AVIONICS COMPARTMENT. (E/E). JOINT STRAP FS= 333.00 BETWEEN STRG 27 TO 26RH AT MAIN AVIONICS COMPARTMENT. (E/E). WAS REPAIRED PER REO 690-53-21-1789 REV - -Jun 19, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA20240724004Lug · corrodedCORROSION ON HOUSING OF LUG 5 AT RH AILERON WAS FOUND. LUG 5 WAS REPAIRED PER REO 670-57-61-237 REV ORIGINALJun 19, 2024 · N585NN · Bombdr CL6002D15 · Wing, Control Surface Attach FittingsSDR VNAA20240726017Floorbeam · corrodedSECONDARY NRC FROM NRC 00122': AFTER REMOVAL, CORROSION ON RH FLOOR SUPPORT BEAM AT BULKHEAD FS 280.00. RH FLOOR SUPPORT BEAM AT BULKHEAD FS 280.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-06-001-Jun 16, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Main, Floor BeamSDR VNAA20240726016Floorbeam · corrodedSECONDARY NRC FROM NRC 00122': AFTER REMOVAL, CORROSION ON LH FLOOR SUPPORT BEAM AT BULKHEAD FS 280.00. LH FLOOR SUPPORT BEAM AT BULKHEAD FS 280.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-06-001-0Jun 16, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Main, Floor BeamSDR VNAA20240726014Post · corrodedIN REF TO: DURING INSPECTION OF THE TASK CARD 53-10-219B, IT WAS DETECTED CORROSION ON BULKHEAD DOOR POST RBL 12 & LBL 12 AT FS280.00. BULKHEAD DOOR POST RBL 12 AND LBL 12 WERE REPAIRED PER CRJ900 SRM 53-11-10-201-006-A01Jun 16, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Main, StructureSDR VNAA20240726012Intercostal · corrodedINITIAL INSPECTION: CORROSION ON INTERCOSTAL ATTACHED TO STRINGER 20RH IN FS= 333.0 TO FS= 349.00 AT MAIN AVIONICS COMPARTMENT. (E/E). INTERCOSTAL ATTACHED TO STRINGER 20RH IN FS= 333.0 TO FS= 349.00 WAS EVALUATED PER CRJ900 SRM 53-21-23-101-002-A02 AND WASJun 16, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA20240726005Bulkhead Web · corrodedCORROSION ON LH LOWER WEB AT BULKHEAD FS 280.00 LBL 12 ABOVE FLOOR. CORROSION ON LH LOWER WEB AT BULKHEAD FS 280.00 LBL 12 ABOVE FLOOR WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-11-10-201-003-A01 AND WAS REPAIRED PER CRJ-900 SRM 53-11-10-201-003-A01.Jun 16, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Main, BulkheadSDR VNAA20240724005Floor Support · crackedSECONDARY NRC: IN REFERENCE TO JOB TRFKE000YVW3:53-10-303-JIC/001. AFTER REMOVAL FLOOR SUPPORT, CRACK ON FLOOR SUPPORT OF LBL12 BTW FS280 TO FS265 WAS FOUND. FLOOR SUPPORT OF LBL12 BTW FS280 TO FS265 WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01, CRJ900 Jun 16, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA20240723015Seat Track · corrodedDISCREPANCY: CORROSION ON SEAT RAILS OF LBL9 BTW FS364.00 TO FS708.00. FLOOR SEAT RAILS OF LBL9 BTW FS364.00 TO FS708.00 (5EA) ARE OUT OFF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01,SRM 53-31-49-101-001-A02 AND SRM 53-41-49-101-001-A02 AND REPLACED PER CRJ-Jun 16, 2024 · N585NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20240723014Skin · gouged1211.83FH PERM REPAIR - TEMPORARY FOR LH SLAT NO.3 TE SKIN GOUGE WITHIN 1211.83 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. LH SLAT TE SKIN WAS REPAIRED PER REO 690-57Jun 16, 2024 · N585NN · Bombdr CL6002D15 · Wing Miscellaneous StructureSDR VNAA20240723013Skin · wornWEAR ON AREA OF SETTLEMENT OF FAIRINGS (586AB, 592AB, 595AB, 597AB) AT LH WING LOWER SKIN. AREA OF SETTLEMENT OF FAIRINGS (586AB, 592AB, 595AB, 597AB) AT LH WING LOWER SKIN WAS REPAIRED PER REO 690-57-21-477 REV - -Jun 16, 2024 · N585NN · Bombdr CL6002D15 · Wing, Plate/SkinSDR VNAA20240723012Fitting · damagedPERM REPAIR BEFORE 19,411.07 FH - TEMPORARY REPAIR FOR BURR DAMAGE TO NLG LOCK LINK FITTING BOLT HOLE THE SUBJECT CONDITION IS STRUCTURALLY ACCEPTABLE FOR 3650 FLIGHT HOURS FROM TIME OF INCORPORATION OF THIS REO AT REV - -. NLG LOCK LINK FITTING WAS REPAIREJun 16, 2024 · N585NN · Bombdr CL6002D15 · Fuselage, Landing Gear Attach FittingsSDR VNAA20240723011Skin · wornWEAR ON AREA OF SETTLEMENT OF FAIRINGS (683AB,686AB, 692AB, 695AB, 697AB) AT RH WING LOWER SKIN. AREA OF SETTLEMENT OF FAIRINGS (683AB,686AB, 692AB, 695AB, 697AB) AT RH WING LOWER SKIN WAS REPAIRED PER REO 690-57-21-478 REV - -.Jun 16, 2024 · N585NN · Bombdr CL6002D15 · Wing, Plate/SkinSDR VNAA20240723010Seat Track · damagedTEMP/PERM REPAIR FOR MISSING, LOOSE, OR DAMAGED ALIGNMENT RIVETS AT CAPT/FO'S SEAT TRACKS PERMANENT REPAIR PILOT/CO-PILOT SEAT TRACK WEAR STRIP DUE TO MISSING OR LOOSE FASTENERS SEE INDIVIDUAL WO OR LB AND REO 670-53-11-210-C FOR DETAILS. PILOT/CO-PILOTJun 16, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA20240723004Floorbeam · crackedCRACKED CENTER COCKPIT FLOOR BEAM LBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. FLOOR BEAM LBL12 AT FS280.00 FLOOR INTERNAL SUPPORT STRUCTURE WAS REPAIRED PER REO 690-53-11-1790 REV. --Jun 16, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Main, Floor BeamSDR VNAA2024072300Drag Angle · crackedINITIAL INSPECTION: CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 20.0% FRNT SPAR DATUM TO STGR DATUM TO 25.93% STGR DATUM. FWD DRAG ANGLE BTW 20.0% FRONT SPAR DATUM RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT WAS REPAIRED PER Jun 16, 2024 · N585NN · Bombdr CL6002D15 · Vertical StabilizerSDR VNAA20240723001Intercostal · corrodedCORROSION ON INTERCOSTAL (2 EAS) BTW FS 349.00 TO FS 364.00, BTW STGR 26LH AND STGR 26RH OF MAIN AVIONICS COMPARTMENT INTERNAL STRUCTURE. (SM). INTERCOSTALS (2EAS) BTW FS349 TO FS364 WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-003-A02 AND WERE Jun 16, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA20240726008Angle · corrodedCORROSION ON ANGLE, LOWER SILL (4EAS) BTW FS 319.70 TO FS 349.00 AT SERVICE DOOR SURROUND STRUCTURE. ANGLE, LOWER SILL (4EAS) BTW FS 319.70 TO FS 349.00 WERE EVALUATED OUT OF LIMITS PER CRJ 900 SRM 53-00-00-101-001 -A01 AND WERE REPLACED PER CRJ900 SRM 51-42May 14, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA20240726007Strap · corrodedINITIAL INSPECTION: CORROSION ON STRAP, INNER (2EAS) FS 319.70 AND FS 349.00 OF STGR 17RH AT SERVICE DOOR SURROUND STRUCTURE. STRAP, INNER (2EAS) FS 319.70 AND FS 349.00 OF STGR 17RH AT SERVICE DOOR SURROUND STRUCTURE WERE EVALUATED OUT OF LIMITS PER CRJ900 SMay 14, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA20240724003Floor Support · crackedCRACK ON FLOOR SUPPORT RBL 12.0 BTW FS 220.00 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE. FLOOR SUPPORT RBL 12.00 BTW FS 220.00 TO FS 229.00 WAS REPAIRED PER REO 690-53-11-1797 REV. - -May 14, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA20240724002Canister · crackedSETTLEMENT FITTING AT FS310 LBL37 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-43-101-001-A03 AND WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01. CANISTER OF SLAT TRACK 1-3 AT RH FUEL TANK WAS REPAIRED PER REO 670-57-42-577. REV. - -May 14, 2024 · N585NN · Bombdr CL6002D15 · Wing Main, Frame StructureSDR VNAA20240724001Fitting · corrodedCORROSION ON SETTLEMENT FITTING (1EA) FS 310 ( LBL37) OF ENTRANCE COMPARTMENT AT FUSELAGE FLOOR STRUCTURE. SETTLEMENT FITTING AT FS310 LBL37 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-43-101-001-A03 AND WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01May 14, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA20240723009Plate · corrodedINITIAL INSPECTION: CORROSION ON UPPER/LOWER FACE OF PLATE LBL 3.4 BTW FS533.00 AND FS 549.00 AT FWD CARGO COMPARTMENT. CORROSION ON UPPER/LOWER FACE OF PLATE LBL 3.4 BTW FS533.00 AND FS 549.00 AT FWD CARGO COMPARTMENT.May 14, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA20240723007Skin · corrodedCORROSION ON JOINT PLATE UPPER LONGERON AND AFT HINGE BTW FS549.00 AND FS565.00 AT FWD BAGGAGE BAY DOOR SURROND STRUCTURE. JOINT PLATE UPPER LONGERON WAS REPAIRED PER REO 690-53-31-847 REV. -- AND AFT HINGE BTW FS549.00 AND FS565.00 AT FWD BAGGAGE BAY DOOR SUMay 14, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Main, Plate/SkinSDR VNAA20240723006Web · crackedCRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00. ELECTRICAL BAY FLOOR WEB RH FS193 WAS REPAIRED PER CRJ-900 SRM 53-11-43-201-001-A01.May 14, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA20240723005Support · crackedAFTER REMOVAL OF LOWER FUSELAGE FAIRINGS, CRACK ON AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH. (SM). REFUEL DUCT MOUNTING SUPPORT WAS REPAIRED PER REO 690-28-25-022 REV.--May 14, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA20240723002Fireshield · damagedRH ENGINE LWR FWD CORE COWL FIRE SHIELD WITHIN 2,566.78 FLIGHT HOURS FROM IR (BEFORE 19,384.43FH) REPAIR OR REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES. FIRESHIELD LWR FWD CORE COWL RH ENGINE WAS REPAIRED PER REO 690-54-23-384 REV - -May 14, 2024 · N585NN · Bombdr CL6002D15 · Nacelle/Pylon, Bulkhead/FirewallSDR VNAA2024021211101Pin · unserviceableINSPECTED LH FAN BLADES FOR STIFFNESS, NO DEFECTS FOUND, VIBE CHECK GOOD IAW CRJ 900 AMM 72-21-02-200-803-A01. HIGH TORQUE PIN T/S DUE WITHIN 15 CYCLES. / REMOVED AND REPLACED LH ENGINE FAN BLADE PINS IAW CRJ 900 AMM 72-21-02-000/400-801-A01-PSA. PERFORMED VIBFeb 8, 2024 · N585NN · Cndair CL6002D24 · Turbine Engine Air Inlet SectionSDR VNAA2024010311102Unknown · unknownPAX DOOR WARNING MSG IN FLIGHT, PEFORMED QRH FOLLOWED BY CABIN ALT, ALSO FOLLOWED BY PROX SYSTEM FAULT ONE STATUS MSG+MANAULLY DEPLOYED MASKS FA NOTED WHISTLINGS SOUND COMING FROM PAX / C/W FULL RIG CHECK OF PAX DOOR IAW CRJ900 AMM 52-11-00-720-802-A01. NO OUTDec 31, 2023 · N585NN · Cndair CL6002D24 · Door Warning SystemSDR VNAA202304121111Fmu · unserviceableL ENGINE FLAMEOUT CAUTION MESSAGE IN FLIGHT, N1 AND N2 BOTH DECREASED MOMENTARILY THEN CAME BACK TO NORMAL INDICATIONS L ITT EXCEED C MESSAGE FOLLOWED / COMPLIED LH ENGINE BORESCOPE INSP. OF THE STAGE 1 AND 2 HPT, COMBUSTION LINER AND TURBINE NOZZLE IAW CRJ 90Apr 8, 2023 · N585NN · Cndair CL6002D24 · Engine Fuel and ControlSDR VNAA202207181113Sensor · unserviceableRTF-LH OB BTMS WENT TO 2O IN FLIGHT / FOUND #1 MLG BTMS CONNECTER SLIGHTLY LOOSE. DEFERRED #1 MLG BTMS PER CRJ900 MEL 32-46-01 OPTION 4 CAT C. C/W M FUNCTION BY CAPPING CONNECTER WITH METAL DUST CAP AND SECURING TO HARNESS. REMOVED AND REPLACED #1 BRANK TEMP SJul 16, 2022 · N585NN · Cndair CL6002D24 · Wheel/Ski/FloatSDR VNAA202206131111None · nonePERMANENT REPAIR DUE TO FUSELAGE SKIN BETWEEN FS 364.00 AND FS 379.00 AND STR 22R- STR 23R / COMPLIED WITH EDDY CURRENT OF CUT OUT SECTIONS OF REPAIR AREA SURROUNDING FS 364.00, FS 379.00, AND STR 22R-23R USING REO 690-53-21-1520 REV. P2 AND CRJ900 NDTM 51-20Jun 10, 2022 · N585NN · Cndair CL6002D24 · Fuselage Main, Structure
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