N574NN

Service difficulty reports · 54

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 = 'N574NN' 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 VNAA2026102026701Fan · failedEVACUATION FOR FUMES IN AIRCRAFT. C/W FIM 21-22-00-810-806-A01 AND 21-21-00-810-806-A01. CABIN FUMES APPEAR TO BE FROM ACTIVATION OF O2 GENERATORS. FLIGHT DECK FUMES APPEAR RELATED TO NR 2 DISPLAY FAN FAIL. REMOVED AND REPLACED DISPLAY COOLING FAN NR 2 IAW AOct 17, 2026 · N574NN · Cndair CL6002D24 · Air Distribution FanSDR VNAA2026062920101Actuator · unserviceablePITCH FEEL CAUTION IN FLIGHT / REMOVED LINEAR ACTUATOR #1 A141 AND INSTALLED LINEAR ACTUATOR #2 A140 IN ITS POSITION. OPS CHECK GOOD. INSTALLED NEW LINEAR ACTUATOR IAW AMM 27-31-23-400-801-A01-PSA. OPS CHECK GOOD AT THIS TIME.Jun 25, 2026 · N574NN · Cndair CL6002D24 · Elevator Tab Control SystemSDR VNAA2026062319201Door · faultedOVERHEAD BIN AT 15AC NOT ALLOWING FWD AND AFT EMERGENCY EXITS TO OPEN FOR EGRESS / PERFORMED ADJUSTMENT OF THE RODS OF THE OVERHEAD STORAGE COMPARTMENT INSTALLED ABOVE THE OVERWING EMERGENCY EXIT ON OVERHEAD BIN AT SEATS 15,16AC IAW AMM 25-23-00-820-803. INSTAApr 22, 2026 · N574NN · Cndair CL6002D24 · DoorsSDR VNAA2024110811101Brake · fadedI BELIEVE WE HAD A FLAT TIRE ON T/O. SLOWER ACCELLERATION. / PERFORMED GVI OF #1 BRAKE AS REQUIRED. BLED #1 BRAKE IAW CRJ900 AMM 32-43-00-870-801-A01-PSA. BRAKE #1 OPS CHECK SAT. A/C OK TO CONTINUE SERVICE. TAXI CHECK PERFORMED WITH CREW. NO DEFECTS NOTED.Nov 7, 2024 · N574NN · Cndair CL6002D24 · Landing Gear Brake SystemSDR VNAA202405130029Fitting · corrodedIN REFERENCE NRC 00204: FABRICATE FITTING PN: A414252-3 (1EA) FWD LAV IN REFERENCE EA NO: A1-690-25-00182. FITTING PN: A414252-3 (1EA) FWD LAV WAS FABRICATED PER EA NO: A1-690-25-00182 SECTION III-PERMANENT REPAIR REV-- DATE 2024-04-26Apr 26, 2024 · N574NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA202405130028Fitting · corrodedWORK SHOP INTERIOR SHEET METAL: CORROSION ON FITING (1EA) BELOW THE SERVICE TABLE AT FWD LAV. FITTING P/N: A414252-3 (1EA) BELOW THE SERVICE TABLE AT FWD LAV. WAS REPLACED PER SAFRAN CMM 25-40-40Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA202405130027Skin · damagedLIGHTNING STRIKE ON EXTERNAL FUSELAGE ON FS 661 + 8 AND FS 661 + 16 BTW STGR 26/27 LH LIGTHING STRIKE ON EXTERNAL FUSELAGE ON FS 661 + 8 AND FS 661 + 16 BTW STGR 26/27 LH WAS REPAIRED PER REO 690-53-31-833 REV.- -Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Fuselage Main, Plate/SkinSDR VNAA202405130026Skin · corrodedCORROSION ON STGR 22RH BTW FS 1015.00 AND FS 1031.00 AT AFT CARGO COMPARTMENT, SKING WAS DRILLING IN REF NRC 00116. STRINGER 22RH BTW FS1015 TO FS1031 AT AFT CARGO COMPARTMENT AND FUSELAGE SKIN WERE REPAIRED PER REO 690-53-61-1377 REV --Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Fuselage Main, Plate/SkinSDR VNAA202405130025Hinge Fitting · corrodedCORROSION ON BORE LUGS L4, L5 & L6 AT HINGE FITTINGS OF THE LH AILERON ASSY. BORE LUGS L4, L5 & L6 AT HINGE FITTINGS OF THE LH AILERON ASSY WERE REPAIRED PER REO 670-57-61-237 REV. --Apr 18, 2024 · N574NN · Bombdr CL6002D15 · AileronsSDR VNAA202405130024Floorbeam · crackedCRACK ON FLOOR BEAM RBL12, FS 280.00 AT FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. FLOOR BEAM RBL12, FS 280.00 AT FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1725 REV. - -Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Fuselage Main, Floor BeamSDR VNAA202405130023Floorbeam · crackedCRACK ON FLOOR BEAM LBL12, FS 280.00 AT FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. FLOOR BEAM LBL12, FS 280.00 AT FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1724 REV. - -Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Fuselage Main, Floor BeamSDR VNAA202405130022Canister · crackedDURING INSPECTION OF THE TASK CARD TRFKE000WLRC: 600-08E2-JIC IT WAS DETECTED CRACK 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 REPAIRED PER REO PER REO 670-57-42-Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Fuel StorageSDR VNAA202405130021Floor Support · corrodedCORROSION ON LBL27 FLOOR BEAM UPPER FACE BETWEEN FS1000.00- FS1047.00 AT AFT CARGO COMPRTMENT. LBL27 FLOOR BEAM UPPER FACE BETWEEN FS1000.00- FS1047.00 AT AFT CARGO COMPRTMENT WAS REPAIRED PER REO 690-53-61-1379. REV. --Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA202405130020Floorbeam · corrodedCORROSION ON LBL9 FLOOR BEAM UPPER FACE BETWEEN FS1000.00- FS1047.00 AT AFT CARGO COMPRTMENT. LBL9 FLOOR BEAM UPPER FACE BETWEEN FS1000.00- FS1047.00 AT AFT CARGO COMPRTMENT WAS REPAIRED PER REO 690-53-61-1374. REV. --Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Fuselage Main, Floor BeamSDR VNAA202405130019Doubler · corrodedCORROSION WAS FOUND ON AFTER ATG ANTENNA DOUBLERS INTERNAL STRUCTURE AND STIFFENERS BTW STA: 1007. STG 25R TO 26R. TG ANTENNA DOUBLERS INTERNAL STRUCTURE AND STIFFENERS WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND WERE REPLACED PEApr 18, 2024 · N574NN · Bombdr CL6002D15 · Fuselage Main, Plate/SkinSDR VNAA202405130018Seat Track · corrodedCORROSION ON SEAT RAIL RBL 9, LBL9 AND LBL27 BTW FS485.00 TO FS693.00 ON PASSENGER COMPARTMENT FLOOR STRUCTURE. SEAT RAIL RBL 9, LBL9 AND LBL27 BTW FS485.00 TO FS693.00 ON PASSENGER COMPARTMENT FLOOR STRUCTURE WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 5Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202405130017Seat Track · corrodedSENGER COMPARTMENT FLOOR STRUCTURE. DUE TO CORROSION ON SEAT RAILS RBL 9, LBL9 AND LBL27 BTW FS 349.00 TO FS 485.00 WAS NOT ALLOWED, WERE FOUND OUT OF LIMITS AND MUST BE REPLACED PER CRJ900 SRM 53-21-49-101-001-A01 AND CRJ-900 AMM 53-00-49 (CONFIG A12)Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202405130016Seat Track · corrodedCORROSION ON RH SIDE SEAT RAIL AT STGR 15RH, BTW FS 744.15 TO FS 761.85. E TO NOT PERMISIBLE DAMAGE ON RH SIDE SEAT RAIL AT STGR 15RH, BTW FS 744.15 TO FS 761.85 WAS REPLACED PER CRJ/900 SRM 53-41-49-101-001-A02 AND CRJ900 AMM 53-00-49 (CONFIG A12)Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202405130015Seat Track · corrodedCORROSION ON RH SIDE SEAT RAIL AT STGR 15RH, BTW FS 708.00 TO FS 720.85. DUE TO NOT ALLOWED DAMAGED ON SIDE SEAT RAIL OF STRG 15RH, BTW FS 677.00 TO FS 720.85 WAS REPLACED PER CRJ900 SRM 53-41-49-101-001-A02 AND CRJ900 AMM 53-00-49 (CONFIG A12)Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202405130014Rib · crackedAFTER INTERNAL ZONAL INSPECTION, CRACK ON WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF RH WING. WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF RH WING WAS REPAIRED PER REO 690-57-51-346 REV.--Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Wing, Rib/BulkheadSDR VNAA202405130013Rib · crackedAFTER INTERNAL ZONAL INSPECTION, CRACK ON WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF LH WING. WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF LH WING WAS REPAIRED PER REO 690-57-51-347 REV.--Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Wing, Rib/BulkheadSDR VNAA202405130012Bracket · corrodedCORROSION ON BRACKETS, MACHINED (7EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT. BRACKETS, MACHINED (7EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT WERE EVALUATED OUT OF LIMITS PER SRM CRJ900 SRM 53-32-58-101-001-A01 AND REPLACE PER CRJ900 SRM 51-Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA202405130011Web · crackedCRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00. ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00 WAS REPAIRED PER CRJ900 SRM 53-11-43-201-001-A01Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA202405130010Support Fitting · corrodedCORROSION ON RH JACK FITTING SUPPORT RH, BTW FS265.00 TO FS278.00, BL0.00. IN REF TO: CARD TRFKE000YVWZ, CORROSION ON FRAME FS265.00 BTW SRGR 27 TO STGR 26RH. CORROSION ON RH JACK FITTING SUPPORT RH, BTW FS265.00 TO FS278.00, BL0.00 AND ON FRAME FS265.00 BTW Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Fuselage Main, StructureSDR VNAA20240513008Flap · nickedSEVERAL NICKS ON LOWER SKIN OF LH INBOARD FLAP BTW FLS 15.00 TO FLS 65.50. SEVERAL NICKS ON LOWER SKIN OF LH INBOARD FLAP BTW FLS 15.00 TO FLS 65.50 WERE BLENDED OUT PER CRJ900 SRM 51-12-00-001-001-A01 AND WERE EVALUATED BTW FLS15 TO FLS42 OUT OF LIMITS Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Trailing Edge FlapsSDR VNAA20240513007Skin · dentedDENTS (3 LOCATIONS) ON LOWER SKIN OF RH INBOARD FLAP BTW FLS 75.60 TO FLS 92.80. DENTS ON LOWER SKIN OF RH INBOARD FLAP BTW FLS 75.60 TO FLS 92.80 WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 57-52-01-101-001-A01 AND WERE REPAIRED PER CRJ900 SRM 57-52-01-201-Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Trailing Edge FlapsSDR VNAA20240513006Skin · nickedSEVERAL NICKS ON LOWER SKIN OF RH INBOARD FLAP BTW FLS 15.00 TO FLS 65.50. SEVERAL NICKS ON LOWER SKIN OF RH INBOARD FLAP BTW FLS 15.00 TO FLS 65.50 WERE BLENDED OUT PER CRJ900 SRM 51-12-00-001-001-A01 AND WERE EVALUATED BTW FLS15 TO FLS42 OUT OF LIMITS AND BApr 18, 2024 · N574NN · Bombdr CL6002D15 · Trailing Edge FlapsSDR VNAA20240513005Hinge Fitting · excess playFREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. HINGE NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WERE REPLACED PER RIL #2103 REV. B.Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Rudder StructureSDR VNAA20240513004Rib · crackedAFTER INTERNAL ZONAL INSPECTION, CRACK ON WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF LH WING. WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF LH WING WAS REPAIRED PER REO 690-57-51-347 REV.--Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Wing, Rib/BulkheadSDR VNAA20240513003Bracket · corrodedCORROSION ON BRACKETS, MACHINED (7EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT. : BRACKETS, MACHINED (7EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT WERE EVALUATED OUT OF LIMITS PER SRM CRJ900 SRM 53-32-58-101-001-A01 AND REPLACE PER CRJ900 SRM Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA20240513002Skin · 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 WERE REPAIRED PER REO 690-57-21-460 REV. - -Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Wing, Plate/SkinSDR VNAA20240513009Tie Bar · wornINITIAL INSPECTION: WEAR ON THRUST REVERSER FLOATING TIE BAR (2EA) UPPER AND LOWER AT RH ENGINE. R ON THRUST REVERSER FLOATING TIE BAR (2EA) UPPER AND LOWER AT RH ENGINE WERE REPAIRED PER REO 690-54-22-066 REV. --, REO 690-54-22-067 REV. --, REO 690-54-24-015Apr 8, 2024 · N574NN · Bombdr CL6002D15 · Engine Thrust ReverserSDR VNAA20240513001Skin · wornWEAR ON AREA OF SETTLEMENT OF FAIRINGS (583AB, 586AB, 592AB, 595AB, 597AB) AT LH WING LOWER SKIN. AREA OF SETTLEMENT OF FAIRINGS (583AB, 586AB, 592AB, 595AB, 597AB) AT LH WING LOWER SKIN WERE REPAIRED PER REO 690-57-21-459 REV. - -Mar 20, 2024 · N574NN · Bombdr CL6002D15 · Wing, Plate/SkinSDR VNAA202304061112Unknown · unknown12€? SCRATCH WITH A MAX DEPTH OF .002€? IN THE LEADING EDGE OF THE #2 RH SLAT LEADING EDGE SKIN. PERMANENT REPAIR WAS C/W PER REO 690-57-42-972 INSTRUCTIONS.Apr 5, 2023 · N574NN · Cndair CL6002D24 · Wing, Control SurfacesSDR VNAA202210061113None · noneELECTRICAL SMELL IN A/C CABIN AND CARGO COMP ON GROUND / CW CRJ 900 FIM 21-21-00-810-806(A01). NO DEFECTS NOTED.Oct 5, 2022 · N574NN · Cndair CL6002D24 · Air Distribution SystemSDR VNAA202103291111Acm · failedON TAXI OUT THE CAPTAIN/FO BEGAN TO SMELL A BURNING SMELL THEN GOT A CALL FROM THE FA IN THE BACK SAYING THERE IS SMOKE. THE PAX THEN EVACUATED THROUGH THE MAIN CABIN DOOR ON THE TAXIWAY. THE SMOKE WAS COMING FROM THE CENTER OF THE AIRCRAFT ACCORDING TO THE FAMar 29, 2021 · N574NN · Cndair CL6002D24 · Cabin Cooling SystemSDR VNAA202102091112Skin · dentedDURING OVERNIGHT MAINTENANCE AT DAYTON, OH (DAY), TECHNICIANS FOUND A DENT IN THE TOP FUSELAGE NOSE SKIN PANEL CENTERED ON THE PANEL AND LOCATED SLIGHTLY AFT OF THE FS 169 SPLICE. THE DENT MEASURES APPROXIMATELY 4.6Ï¿½ X 4.5Ï¿½ X .15Ï¿½ DEEP AND IS NOT WITHIN Feb 5, 2021 · N574NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202102051111Stringer · damagedREMOVED AND REPLACED ZONE 210 CENTER-LINE STRINGER ZONE 210 BELOW UPPER NOSE SKIN FORWARD EQUIPMENT COMPARTMENT, FROM FS169.00 TO FS202.75 PN CC670-33116-1 IAW CRJ900 SRM 51-42-06 AND SRM 51-40-11. THIS IS A MAJOR REPAIR. FORM 337 COMPLETED.Feb 3, 2021 · N574NN · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR VNAA2020080499911Frame · corrodedFWD AVI BAY FS 295 FRAME CORRODED BETWEEN STRG 26L TO 26R. INSTALLED NEW FRAME SEGMENT, 2 SPLICES, AND ATTACHING ANGLES AND PERFORMED FS295.00 FRAME REPAIR IAW CRJ900 SRM 53-00-06-201-006-A01.Aug 4, 2020 · N574NN · Bombdr CL6002D15 · Fuselage Main, FrameSDR VNAA2020080499910Floorbeam · corrodedFS 280 FLOOR SUPPORT CROSSBEAM FLOOR SUPPORT J-ANGLE CORRODED BETWEEN LBL 9 AND RBL 9. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE FS 280 J ANGLE BETWEEN LBL 9 & RBL 9 IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.Aug 4, 2020 · N574NN · Bombdr CL6002D15 · Fuselage Main, Floor BeamSDR VNAA202008049999Web · crackedUPON REMOVAL OF PAX DOOR FWD HANDRAIL RETAINING BRACKET, FOUND FWD PAX DOOR STAIR WEB CRACKED. REPAIR DAMAGE IAW SRM 52-11-04-201-004-A01Aug 4, 2020 · N574NN · Bombdr CL6002D15 · Passenger/Crew DoorsSDR VNAA202008049998Intercostal · corrodedUPON INSPECTION OF FS 349-364, INTERCOSTAL AT LBL 3 CORRODED AROUND LIGHTNING HOLES. FOUND INTERCOSTAL AND RBL3 FS 349-364 TO BE CORRODED AROUND LIGHTNING HOLES AS WELL. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE INTERCOSTAL (P/N SH670-32075-4) IAW CRJ900 Aug 4, 2020 · N574NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA202008049997Floor Support · corrodedPAX DOOR SILL LOWER FLOOR SUPPORT ANGLE IS CORRODED. LOCATED, DRILLED AND INSTALLED PAX DOOR LOWER SILL FLOOR ANGLE SUPPORT IAW CRJ 900 SRM 51-40-11-001-001-A01.Aug 4, 2020 · N574NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA202008049996Bracket · corrodedFWD BAGGAGE BAY FLOOR STRUCTURE AT FS 581, LBL 2.6 MACHINED BRACKET CORRODED. LOCATED, DRILLED AND INSTALLED NEW MACHINED BRACKET IAW CRJ 900 SRM 51-40-11-001-001-A01.Aug 4, 2020 · N574NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA202008049995Bracket · corrodedFWD BAGGAGE BAY FLOOR STRUCTURE AT FS 533, LBL 2.6 MACHINED BRACKET CORRODED. COMPLETED REPAIR IAW STS EA 80-2020-001-001 REV IRAug 4, 2020 · N574NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA202008049994Intercostal · corrodedAVI BY, FS 349-364 INTERCOSTAL AT LBL 3 CORRODED AROUND LIGHTING HOLES STRG 27L. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE INTERCOSTAL SH670-32075-3 IAW CRJ 900 SRMS 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-40-11-001-001-A01.Aug 4, 2020 · N574NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA202008049993Seat Track · corrodedSEAT TRACKS LH AND RH SIDES FROM STA 379 TO 969 ARE CORRODED. FABRICATED AND REPLACED SEAT TRACKS IAW CRJ 900 SRM 53-00-49-201-002-A01 AND 51-40-11-001-001-A01. 22 TOTAL REPLACED.Aug 4, 2020 · N574NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202008049992Drag Angle · crackedPASSENGER DOOR AFT DRAG ANGLE APPEARS TO BE CRACKED AT ASSIST PULLEY BRACKET. FABRICATED NEW ANGLE AND INSTALLED IAW SRM 52-11-04-201-002-A01.Aug 4, 2020 · N574NN · Bombdr CL6002D15 · Passenger/Crew DoorsSDR VNAA202008049991Drag Angle · crackedLEFT VERTICAL STAB AFT DRAG ANGLE CRACKED .2" LONG AT FWD END. LOCATED, DRILLED AND INSTALLED NEW LEFT VERTICAL STAB AFT DRY ANGLE IAW SRM 51-40-11-001-001-A01.Aug 4, 2020 · N574NN · Bombdr CL6002D15 · Vertical StabilizerSDR VNAA2019103111101Probe · failedDURING CLIMB, RECEIVED BRAKE OVERHEAT MSG. CREW DECLARED AN EMERGENCY AND RETURNED TO CLT. TRUCKS DID ROLL. AIRCRAFT LANDED AND WAS INSPECTED BY FIRE DEPT. AIRCRAFT THEN TAXIED TO THE GATE. MX DEFERRED RH IB BRAKE TEMP INDICATION. REMOVED AND REPLACED RHOct 31, 2019 · N574NN · Cndair CL6002D24 · Landing Gear Brake System
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