N594NN

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 = 'N594NN' 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 VNAA2025082211101Windshield · arcedLEFT FRONT WINSHIELD ARCING IN FLIGHT. / REMOVED AND REPLACED LH WINDSHIELD IAW CRJ-900 AMM 56-11-01-000/400-801-A01-PSA. OPS TEST AND LEAK TEST GOODAug 19, 2025 · N594NN · Cndair CL6002D24 · Window System WiringSDR VNAA2025061311101Gasket · failedANTI-ICE DUCT WARNING MSG IN FLIGHT. / REMOVED AND REPLACED THE LH TELESCOPIC DUCT GASKETS IAW CRJ 900 AMM 30-11-10-000/400-801. LEAK TEST GOOD.Jun 12, 2025 · N594NN · Cndair CL6002D24 · Airfoil Anti/De-ice SystemSDR VNAA202503070041Skin · corrodedCORROSION ON SKIN PANEL IN STA. FS= 295 TO FS= 310 BETWEEN STGR 24RH TO 25RH AT MAIN AVIONICS COMPARTMENT. CORROSION ON SKIN PANEL IN STA. FS= 295 TO FS= 310 BETWEEN STGR 24RH TO 25RH AT MAIN AVIONICS COMPARTMENT WAS REPAIRED PER REO 690-53-21-1884 REV - .Mar 7, 2025 · N594NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202503070040Stringer Splice · corroded"IN REF TO NRC 00139. AFTER REMOVAL OF STRINGER 25RH IN STA. FS= 319.70TO FS= 333.00, SPLICE FOUND CORRODED AT MAIN AVIONICS COMPARTMENT. CORRECTIVE ACTION:EVALUATED,DUE TO EXCESSIVE DAMAGE ON SPLICE STRINGER 25RH IN STA. FS= 319.70 TO FS= 333.00 PER CRJ/900 Mar 7, 2025 · N594NN · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR VNAA202503070039Skin · dentedDENT ON EXTERNAL SKIN BTW FS 437.00 TO FS 453.00 AND STGR 16RH TO 17RH AT FWD FUSELAGE. DENT ON EXTERNAL SKIN BTW FS 437.00 TO FS 453.00 AND STGR 16RH TO 17RH AT FWD FUSELAGE WAS EVALUATED WITHIN LIMITS PER CRJ-900 SRM 53-00-01-101-001-A01.Mar 7, 2025 · N594NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202503070038Floor Support · crackedCRACK ON FLOOR BEAM RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL79.50). CRACK ON FLOOR BEAM RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOORMar 7, 2025 · N594NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202503070037Canister · crackedCRACK IN CANISTER WELDED NO.3, ON WS148.01 OF INTERNAL RH MAIN FUEL TANK. CANISTER WELDED NO.3, ON WS148.01 OF INTERNAL RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577. REV.--.."Mar 7, 2025 · N594NN · Cndair CL6002D24 · Wing Main, Frame StructureSDR VNAA202503070036Stringer · crackedCRACK ON STGR 3LH (LINTEL AREA) FS280.00 AT CIRCUNFERENTIAL SKIN JOINT. CRACK ON STGR 3LH (LINTEL AREA) FS280.00 AT CIRCUNFERENTIAL SKIN JOINT WAS REPAIRED PER REO 690-53-21-1892 REV - -. THE AIRCRAFT MUST NOT BE OPERATED BEYOND 12 MONTHS FROM THE ISSUE DATE Mar 7, 2025 · N594NN · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR VNAA202503070035Canister · crackedCRACK 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 REO 670-57-42-577. REV-.Mar 7, 2025 · N594NN · Cndair CL6002D24 · Wing Main, Frame StructureSDR VNAA202503070034Bearing · excess playFREE 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 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WERE REPLACED PER RIL#2103 REV. B.Mar 7, 2025 · N594NN · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous StructureSDR VNAA202503070033Fitting · corrodedCORROSION ON SETTLEMENT FITTING OF ENTRANCE COMPARTMENT (3EA) (FLOOR STRUCTURE AREA). FITTING OF ENTRANCE COMPARTMENT (3EAS) (FLOOR STRUCTURE AREA) WERE EVALUATED EXCESIVE DAMAGE PER CRJ-900 SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ-900 SRM 51-42-21-001-0Mar 7, 2025 · N594NN · Cndair CL6002D24 · Fuselage Main, Attach FittingsSDR VNAA202503070032Seat Track · corrodedCORROSION ON SEAT RAILS OF RBL9 BTW FS349.00 TO FS 693.00 (5EA). SEAT RAILS OF RBL9 BTW FS349.00 TO FS 693.00 (5EA) WERE FOUND OUT OF LIMITS PER CRJ-900 SRM 53-2149-101-001-A01,SRM 53-31-49-101-001-A02 AND SRM 53-41-49-101-001-A02. REPLACED PER CRJ-900 AMM 5Mar 7, 2025 · N594NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202503070031Seat Track · corrodedCORROSION ON SEAT RAILS OF LBL9 BTW FS349.00 TO FS 693.00 (4EA). SEAT RAILS OF LBL9 BTW FS349.00 TO FS 693.00 (4EA) WERE FOUND OUT OF LIMITS PER CRJ-900 SRM 53-2149-101-001-A02 AND CRJ-900 SRM 53-3149-101-001-A02. REPLACED PER CRJ-900 AMM 53-00-49 (CONFIG AMar 7, 2025 · N594NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202503070030Seat Track · corrodedCORROSION ON SEAT RAILS OF RBL9 BTW F5693.00 TO FS977.00. (3EA). SEAT RAILS OF RBL9 BTW FS693.00 TO FS977.00. (3EA) WERE FOUND OUT OF LIMITS PER CRJ/900 SRM 53-41-49-101-001-A02 AND PER CRJ/900 SRM 53-51-49-101-001-A02. REPLACED PER CRJ-900 AMM 53-00-49 (CONFMar 7, 2025 · N594NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202503070029Seat Track · corrodedCORROSION ON SEAT RAILS OF LBL9 BTW FS 693.00 TO FS 977.00. (3EA). SEAT RAILS OF LBL9 BTW FS 693.00 TO FS 977.00 WERE FOUND OUT OF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 AND SRM 53-51-49-101-001-A02 THEREFORE WERE REPLACED PER CRJ-900 AMM 53-00-49 (CONFIMar 7, 2025 · N594NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202503070028Frame · corrodedCORROSION BTW FRAME FS1000.00 AND 1015.00 STGR 24RH AT AFT BAGGAGE BAY COMPARTMENT. CORROSION BTW FRAME FS1000.00 AND 1015.00 STGR 24RH AT AFT BAGGAGE BAY COMPARTMENT WAS REPAIRED PER REO 690-53-61-1508 REV. - .Mar 7, 2025 · N594NN · Cndair CL6002D24 · Fuselage Main, FrameSDR VNAA202503070027Frame · corrodedCORROSION ON FRAME FS1051.30 BTWN STGR 26LH AND STGR 26RH AT AFT BAGGAGE BAY COMPARTMENT. REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01.Mar 7, 2025 · N594NN · Cndair CL6002D24 · Fuselage Main, FrameSDR VNAA202503070026Door Sill · corrodedCORROSION ON AFT CARGO COMPARTMENT DOOR SILL BTW FS 1000.00 TO FS 1047.00, BTW STGR 17LH AND STGR 18LH. DOOR SILL BTW FS 1000.00 TO FS 1047.00, BTW STGR 17LH AND STGR 18LH WAS EVALUATED DAMAGE EXCESIVE PER CRJ-900 SRM 53-00-00-101-001-A01 AND REPLACED PER CRMar 7, 2025 · N594NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202503070025Floorbeam · corrodedAFTER REMOVAL OF FLOOR PANEL SUPPORT ANGLE, CORROSION ON LH CROSSBEAM AT FS 280.00 AT LBL 9. LH CROSSBEAM AT FS 280.00 AT LBL 9.00 WAS FOUND OUT OF LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01 THEREFORE WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01,CRJ-900Mar 7, 2025 · N594NN · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR VNAA202503070024Seat Track · corrodedCORROSION SIDE SEAT RAIL 15RH (4 EAS) BTW F5379.00 TO FS669A0. SIDE SEAT RAIL 15RH (4EAS) BTW FS379.00 TO FS669.40 DUE TO EXCESIVE DAMAGE THEY ARE OUT OF LIMITS PER CRJ/900 SRM 53-21-49-101-001-A01 AND PER CRJ/900 SRM 53-31-49-101-001-A02 THEREFORE WERE REPLAMar 7, 2025 · N594NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202503070023Seat Track · corrodedCORROSION SIDE SEAT RAIL 15LH (4 EAS) BTW FS379.00 TO FS669.4. SIDE SEAT RAIL 15LH (4 EAS) BTW FS379.00 TO FS669.40 WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01 AND SRM 53-31-49-101-001-A02 AND REPLACED PER CRJ-900 AMM 53-00-49 (CONF A12Mar 7, 2025 · N594NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202503070022Seat Track · corrodedCORROSION ON SIDE SEAT RAIL 15RH (5EAS) BTW FS 669.40 TO FS 977. CORROSION ON SIDE SEAT RAIL 15RH (5EAS) BTW FS 669.40 TO FS 977.00 WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 AND REPLACED PER CRJ-900 AMM 53-00-49 (CONFIG A12).Mar 7, 2025 · N594NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202503070020Angle · corrodedCORROSION ON ANGLE MOUNTING AND ANGLES (3EAS) BTW FS310 TO FS319 AT GALLEY SERVICE DOOR SURROUND STRUCTURE. ANGLE MOUNTING AND ANGLES (3EAS) BTW FS310 TO FS319 AT GALLEY SERVICE DOOR SURROUND STRUCTURE WERE FOUND OUT OF LIMITS PER CRJ-900 SRM 53-00-00-101-0Mar 7, 2025 · N594NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202503070021Seat Track · corrodedCORROSION ON SIDE SEAT RAIL 15LH (4EAS) BTW FS 669.40 TO FS 977. SIDE SEAT RAIL 15LH (4EAS) BTW FS 669.40 TO FS 977.00 WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 AND WERE REPLACED PER CRJ-900 AMM 53-00-49 (CONFIG A12).Mar 7, 2025 · N594NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202503070019Stringer · corrodedCORROSION ON STRINGER 25RH IN STA. FS= 319.70TO FS= 333.00AT MAIN AVIONICS COMPARTMENT. STRINGER 25RH IN STA. FS= 319.70TO FS= 333.00AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ 900 SRM 53-00-00-101-001-A01. AND REPLACED PER CRJ-900 SRMMar 7, 2025 · N594NN · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR VNAA202503070017Stringer · corrodedCORROSION ON STRINGER 25RH IN STA. FS= 319.70TO FS= 333.00AT MAIN AVIONICS COMPARTMENT. STRINGER 25RH IN STA. FS= 319.70TO FS= 333.00AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ 900 SRM 53-00-00-101-001-A01. AND REPLACED PER CRJ-900 SRMMar 7, 2025 · N594NN · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR VNA2025F00008Stringer · corrodedCORROSION ON STRINGER 26RH IN STA. FS= 333.00 TO FS= 349.00 AT MAIN AVIONICS COMPARTMENT. STRINGER 26RH IN STA. FS= 333.00 TO FS= 349.00 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ 900 SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ-900 SRMar 7, 2025 · N594NN · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR VNA2025F00007Retainer · damagedELONGATED HOLE ON AFT RETAINER SEAL BTW STGR 23LH AND STGR 22LH OF THE FWD BAGGAGE BAY DOOR AT C1. ELONGATED HOLE ON AFT RETAINER SEAL BTW STGR 23LH AND STGR 22LH OF THE FWD BAGGAGE BAY DOOR AT C1 WAS REPAIRED PER REO 690-53-31-918 REV --.Mar 7, 2025 · N594NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202503070016Intercostal · corrodedCORROSION ON INTERCOSTAL LH BTW FS349.00 TO FS364.00 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT. INTERCOSTAL LH BTW FS349.00 TO FS364.00 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED AND NOT ALLOW DAMAGE PER CRJ-900 SRM 53-21-23-101-003-A02, REPLACEMar 7, 2025 · N594NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202503070015Bracket · corrodedCORROSION ON MACHINED BRACKETS (9 EAS) BTW FS 517.00 TO FS 661.00, BTW STGR 22LH TO STGR 24RH AT FWD BAGGAGE BAY (C1). BRACKETS (6 EAS) BTW FS 517.00 TO FS 661.00, BTW STGR 22LH TO STGR 24RH AT FWD BAGGAGE BAY (C1) WERE EVALUATED EXCESSIVE DAMAGE PER CRJ-900Mar 7, 2025 · N594NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202503070014Web · crackedCRACK AT UPPER WEB OF ADG COMPARTMENT, BELOW OF SETTLEMENT AREA OF ADG PUMB. UPPER WEB OF ADG COMPARTMENT, BELOW OF SETTLEMENT AREA OF ADG PUMB WAS REPAIRED PER REO 670-53-11-509 REV -E AND REO 670-53-11-1943 REV - -.Mar 7, 2025 · N594NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202503070013Skin · corrodedCORROSION ON SKIN PANEL BTW FS 280.00 TO FS 295.00 STGR 25RH TO STGR 24 RH. CORROSION ON SKIN PANEL BTW FS 280.00 TO FS 295.00 STGR 25RH TO STGR 24 RH WAS REPAIRED PER REO 690-53-21-1884 REV - -.Mar 7, 2025 · N594NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202503070012Joint · corrodedCORROSION ON CIRCUMFERENTIAL JOINT FS 280.00 TO FS 282.86 BTW STGR 25LH TO STGR 25 RH. CIRCUMFERENTIAL JOINT FS 280.00 TO FS 282.86 BTW STGR 25LH TO STGR 25 RH WAS REPAIRED PER REO 690-53-21-1885 REV.--. THE AIRCRAFT MUST NOT BE OPERATED BEYOND 12 MONTHS FROMar 7, 2025 · N594NN · Cndair CL6002D24 · Fuselage Main, StructureSDR VNAA202503070011Floorbeam · corroded"CORROSION ON FLOOR PANEL SUPPORT ANGLE UPPER FACE AT FS280.00 BTW RBL 9.00 AND LBL 9.00. FLOOR PANEL SUPPORT ANGLE UPPER FACE AT FS280.00 BTW RBL 9.00 AND LBL 9.00 WAS EVALUATED OUT OF LIMITS PER CRJ/900 SRM 53-00-01-001-001-A01 AND REPLACED PER CRJ-900 SRM Mar 7, 2025 · N594NN · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR VNAA202503070010Support · 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. CRACK ON AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH WAS REPAIRED PER REO 690-28-25Mar 7, 2025 · N594NN · Cndair CL6002D24 · Aerodynamic FairingsSDR VNAA202503070009Plate · corrodedCORROSION ON KICKPLATE AND MID CAP BTW FS 310.00 TO FS 349.00 AT SURROUND STRUCTURE PASSENGER DOOR. KICKPLATE AND MID CAP BTW FS 310.00 TO FS 349.00 AT SURROUND STRUCTURE PASSENGER DOOR WERE EVALUATED EXCESSIVE CORROSION PER CRJ-900 SRM 53-00-00-101-001-A01 Mar 7, 2025 · N594NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202503070008Floor Support · crackedCRACK ON COCKPIT FLOOR LONGITUDINAL BEAM (LBL12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT. FLOOR LONGITUDINAL BEAM ON COCKPIT (LBL12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1935 REV.-Mar 7, 2025 · N594NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202503070007Beam · crackedCRACK ON COCKPIT FLOOR LONGITUDINAL BEAM (LBL12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT. FLOOR LONGITUDINAL BEAM ON COCKPIT (LBL12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1935 REV.--Mar 7, 2025 · N594NN · Cndair CL6002D24 · Fuselage Main, StructureSDR VNAA202503070006Skin · wornWEAR ON AREA OF SETTLEMENT OF FAIRINGS 686AB AND 692AB AT RH WING LOWER SKIN. REPAIRED PER REO 690-57-21-508 REV. -.Mar 7, 2025 · N594NN · Cndair CL6002D24 · Wing, Plate/SkinSDR VNAA202503070005Skin · damagedLIGHTNING STRIKE DAMAGE TO LOWER BELLY PANEL SKIN BTWN FS250.00-FS265.00 & STR25R-STR26R). REPAIRED PER REO 690-53-11-1937 REV --PERMANENT REPAIR.Mar 7, 2025 · N594NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202503070004Skin · gougedFUSELAGE SKIN MULTIPLE BLENDED GOUGE BTWN FS1015.00 - FS1051.30. FUSELAGE SKIN MULTIPLE BLENDED GOUGE BTWN FS1015.00 - FS1051.30 WERE REPAIRED PER REO 690-53-61-1505 REV --PERMANENT DISPOSITION.Mar 7, 2025 · N594NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202503070003Skin · wornCHAFE DAMAGE TO INNER SIDE OF LH PYLON UPPER SKIN BTW FS1098.20 - FS1108.00 AND PBL59.90 - PBL69.30. CHAFE DAMAGE TO INNER SIDE OF LH PYLON UPPER SKIN BTW FS1098.20 - FS1108.00 AND PBL59.90 - PBL69.30 WAS REPAIRED PER REO 690-54-51-061 REV.--.Mar 7, 2025 · N594NN · Cndair CL6002D24 · Nacelle/Pylon, Plate/SkinSDR VNAA202503070002Skin · crackedPERM REPAIR BEFORE 19,970.55 FH - SKIN LWR BELLY PANEL WITHIN 4,663.83 FH (BEFORE 23,204.37 FH) REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES. SKIN LWR BELLY PANEL WAS REPAIRED PER REO 670-53-11-2098 REV. - -Mar 7, 2025 · N594NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNA2025F00006Skin · crackedPERM REPAIR BEFORE 19,970.55 FH - SKIN LWR BELLY PANEL WITHIN 4,663.83 FH (BEFORE 23,204.37 FH) REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES. SKIN LWR BELLY PANEL WAS REPAIRED PER REO 670-53-11-2098 REV. -.Mar 7, 2025 · N594NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202503070001Panel · damagedELONGATED HOLE TO RH WING FIXED L/E PANEL THE SUBJECT CONDITION IS STRUCTURALLY ACCEPTABLE FOR 4900 FLIGHT HOURS FROM TIME OF INCORPORATION OF THIS REO AT REV "- -". REF REO 690-57-41-386-D ** REF REO 690-57-41-387 FOR PERM REPAIR INSTRUCTIONS. ELONGATED HOLMar 7, 2025 · N594NN · Cndair CL6002D24 · Wing, Plate/SkinSDR VNAA2024050811101Control Unit · faultedSTALL FAIL, FLAPS FAIL, SLATS FAIL, PITCH FEEL, AND RUD LIMITER CAUTION MSGS IN FLIGHT / REMOVED AND REPLACED SFECU 1 IAW CRJ 900 AMM 27-51-05-000/400-801-A01. OPS CHECK GOOD AT THIS TIME.May 6, 2024 · N594NN · Cndair CL6002D24 · Leading Edge Slat Control SystemSDR VNAA2023102711101Windshield · faultedTHE CREW GOT A MESSAGE FOR WINDSHIELD HEAT CAUTION MESSAGE / REMOVED AND INSTALLED RH WINDSHIELD IAW CRJ 900 AMM 56-11-01-000/400-801-A01-PSA. OPS CHECK OF THE WINDSHIELD SENSOR AND WIPER BLADE GOOD. PRESSURIZATION LEAK CHECK GOOD AT THIS TIME.Oct 25, 2023 · N594NN · Cndair CL6002D24 · Flight Compartment WindowsSDR VNAA202309121111Selector Valve · unserviceableGEAR DISAGREE WARNING MSG. PERFORMED QRH WITH MANUAL EXTENSION. / REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE IAW CRJ900 AMM 32-32-10-000 / 400-801-A01. OPS CHECKS GOOD AND LEAK CHECK GOOD. FAULT NO LONGER REMAINS.Sep 11, 2023 · N594NN · Cndair CL6002D24 · Landing Gear SystemSDR VNAA202205041111None · noneDURING CLIMB CREW NOTICED HIGH VIBS BUT NEEDLE STILL IN GREEN. AT FL290 NEEDLE MOVED TO YELLOW CREW RAN THROUGH CHECK LIST AND PULL THE POWER BACK AND CONTINUE TO CLIMB TO FL310 THE NEEDLE CAME BACK TO GREEN FOR FEW MIN. THEN NEEDLE WENT INTO YELLOW AGAIN. CREMay 1, 2022 · N594NN · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR VNAA202201111111Selector Valve · false indicationAFTER TAKEOFF THE CREW GOT A GEAR DISAGREE MESSAGE AND RAN THE QRH & QRC. THE DECISION WAS MADE TO DIVERT TO BHM. ATC DECLARED A EMERGENCY FOR THE CREW. AS A PRECAUTION THE CREW DID HAVE EMERGENCY TRUCKS IN BHM ON STANDBY DURING LANDING BUT THEY WERE NOT NEEDEJan 7, 2022 · N594NN · Cndair CL6002D24 · Landing Gear Retraction/Extension System
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