N539EA

Service difficulty reports · 103

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 = 'N539EA' 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 VNAA20250329022Stringer · corrodedCORROSION ON STRINGER AND SPLICE 24RH BTW FS319.70 TO FS349 AT MAIN AVIONICS COMPARTMENT. STRINGER SPLICE 24RH ON FS 333.00 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-21-001-001-A01.Mar 3, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Main, Longeron/StringerSDR VNAA20250329021Stringer · corrodedCORROSION ON STRINGERS 26RH AND 27 BTW FS295 TO FS319.70 AT MAIN AVIONICS COMPARTMENT. CORROSION ON STRINGER 26RH, BTW FS295 TO FS319.70 AT MAIN AVIONICS COMPARTMENT WAS REMOVED PER CRJ 700 SRM 51-21-06-001-001-A01 AND WAS EVALUATED WITHIN LIMITS PER CRJ700 Mar 3, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Main, Longeron/StringerSDR VNAA20250330013Skin · damagedELONGATED DRILL HOLES ON DOOR LOWER SKIN WAS FOUND. AFTER REMOVE LOWER SEAL RETAINER DOOR SKIN AT FWD CARGO COMPARTMENT DOOR. ELONGATED DRILL HOLES ON DOOR LOWER SKIN WAS FOUND. AFTER REMOVE LOWER SEAL RETAINER DOOR SKIN AT FWD CARGO COMPARTMENT DOOR WERE RFeb 16, 2025 · N539EA · Bombdr CL6002D15 · Cargo/Baggage DoorsSDR VNAA20250330012Angle · corrodedCORROSION ON ANGLE (FS549.00, STRINGER 15L TO 18L)(SH670-33119-1) AT FRAME 549.00 LH SIDE WAS FOUND. CORROSION ON ANGLE (FS549.00, STRINGER 15L TO 18L)(SH670-33119-1) AT FRAME 549.00 LH SIDE WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-31-06-101-002-A01 AND Feb 9, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA20250330011Canister · crackedIN REF. TO TASK CARD TRFKE0013UTU:600-09E1-JIC, IT WAS DETECTED CRACK 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 - -.Feb 7, 2025 · N539EA · Bombdr CL6002D15 · Fuel StorageSDR VNAA20250330010Fitting · corrodedCORROSION ON BORE LUGS L5, L2, L1. AND SCRATCH ON LUG L3. AT LH AILERON CENTER FITTING. BORE LUGS L5, L2, L1. AT LH AILERON CENTER FITTING WERE REPAIRED PER REO 670-57-61-237 REV -- & L3 WAS CLEANED PER CRJ 700 SRM TASK 51-26-00-001-001-A01 PAR 5 B CLEANINGFeb 4, 2025 · N539EA · Bombdr CL6002D15 · AileronsSDR VNAA20250330009Fitting · corrodedCORROSION ON BORE LUGS NO.2R AND NO.5R AT RH AILERON CENTER FITTING. BORE LUGS NO.2R AND NO.5R AT RH AILERON CENTER FITTING WERE REPAIRED PER REO REO 670-57-61-237 REV --Feb 4, 2025 · N539EA · Bombdr CL6002D15 · AileronsSDR VNAA20250330008Skin · wornWEAR ON AFT EDGE OUBD SIDE OF UPPER/LOWER FWD CORE COWL AT RH ENGINE. AFT EDGE OUBD SIDE OF UPPER FWD CORE COWL AT RH ENGINE WAS REPAIRED PER REO 670-54-23-1288 REV. - -. LOWER FWD CORE COWL AT RH ENGINE MUST BE REPLACED UNDER NRC 00122.Feb 4, 2025 · N539EA · Bombdr CL6002D15 · Nacelle/Pylon, Plate/SkinSDR VNAA20250330007Crossbeam · wornLH CROSSBEAM AT FS 280.00 WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-00-01-101-001-A01 AND WAS REPLACED PER CRJ700 SRM 51-42-21-001-001-A01 AND PER CRJ700 SRM 51-42-06-001-001-A01. AFT EDGE, OUBD SIDE OF UPPER/LOWER FWD CORE COWL AT LH ENGINE WERE REPAIREFeb 4, 2025 · N539EA · Bombdr CL6002D15 · Nacelle/Pylon, Main FrameSDR VNAA20250330006Floorbeam · corrodedAFTER REMOVAL OF FLOOR PANEL SUPPORT ANGLE, CORROSION WAS FOUND ON LH CROSSBEAM AT FS 280.00. LH CROSSBEAM AT FS 280.00 WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-00-01-101-001-A01 AND WAS REPLACED PER CRJ700 SRM 51-42-21-001-001-A01 AND PER CRJ700 SRM Feb 2, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Main, Floor BeamSDR VNAA20250330005Support Angle · crackedCRACK ON ANGLE SUPPORT FOR ACCESS PANELS 542AZ, 642AZ AT REAR AUXILIARY SPAR LH/RH WING. ANGLE SUPPORT FOR ACCESS PANELS 642AZ AT REAR AUXILIARY SPAR RH WING WAS REPLACED PER CRJ700 SRM 51-42-21-001-001-A01 AND ANGLE SUPPORT FOR ACCESS PANELS 542AZ AT REAR AFeb 2, 2025 · N539EA · Bombdr CL6002D15 · Wing Miscellaneous StructureSDR VNAA20250330004Stiffener · corrodedCORROSION ON STIFFENERS (2 EAS) AND DRAINS, FS985 TO FS1000 AND BTW STGR 26LH TO 25LH. STIFFENERS (2 EAS) AND DRAINS, FS985 TO FS1000 AND BTW STGR 26LH TO 25LH WERE EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-00-00-101-001-A01, MANUFACTURATED PER DWG MM670-6Feb 1, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA20250330003Shim · corrodedCORROSION ON SHIMS (4 EAS) BTW FS1031 TO FS1047 ALSO FS1000 TO FS1015 BTW STGR 27 TO 26LH AT AFT BAGGAGE BAY. CORROSION ON SHIMS (4 EAS) BTW FS1031 TO FS1047 ALSO FS1000 TO FS1015 BTW STGR 27 TO 26LH AT AFT BAGGAGE BAY WAS EVALUATED OUT OF LIMITS PER CRJ70Feb 1, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA20250329028Seat Track · corrodedCORROSION ON SEAT RAIL 3 EAS AT RBL 9 BTW STA 349 TO STA 677. SEAT RAIL 2 EAS AT RBL 9 BTW STA 349 TO STA 581 WERE CLEANED PER CRJ/700 SRM 51-26-00-001-001-A01 AND INSPECTED PER CRJ-700 SRM 51-26-00-001-001-A01 AND NO DAMAGE CORROSION WAS FOUND AND SEAT RAIL Feb 1, 2025 · N539EA · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20250329027Seat Track · corrodedCORROSION ON SIDE SEAT RAIL 3 EAS AT STGR 15RH BTW STA 379 TO STA 677. SIDE SEAT RAIL 3 EAS AT STGR 15RH BTW STA 379 TO STA 677 WERE FOUND OUT OF LIMITS PER CRJ 700 SRM 53-21-49-101-001-A01,SRM 53-31-49-101-001-A01 AND SRM 53-41-49- 101-001-A01 THEREFORE WERFeb 1, 2025 · N539EA · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20250329026Seat Track · corrodedCORROSION ON SIDE SEAT RAIL 5 EAS AT STGR 15LH BTW STA 379 TO STA 761. SIDE SEAT RAIL 5 EAS AT STGR 15LH BTW STA 379 TO STA 761 WERE FOUND OUT OF LIMITS PER CRJ 700 SRM 53-21-49-101-001-A01 ,SRM 53-31-49-101-001-A01 , AND SRM 53-41-49- 101-001-A01 THEREFORE WFeb 1, 2025 · N539EA · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20250329024Seat Track · corrodedCORROSION ON SIDE SEAT RAIL 2 EAS AT STGR 15LH BTW STA 785 TO STA 977. SEAT RAIL (1EA) AT STGR 15LH BTW STA 785 TO STA 863 WAS FOUND OUT OF LIMITS PER CRJ/700 SRM 53-41-49-101-001-A01 THEREFORE WAS REPLACED PER CRJ700 AMM 53-00-49 (CONFING A03) AND SEAT RAFeb 1, 2025 · N539EA · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20250330001Rib · corrodedGOUGES ON RH WING TE ASSY, RIB FLS13.65. RIB WAS REPLACED PER REO 670-57-51-590 REV - -.Jan 31, 2025 · N539EA · Bombdr CL6002D15 · Wing, Rib/BulkheadSDR VNAA20250329023Skin · corrodedCORROSION ON CUT OUT INNER FACE AT E/E DOOR SETTLEMENT AREA. CORROSION ON CUT OUT INNER FACE AT E/E DOOR SETTLEMENT AREA WAS REPAIRED PER REO 690-53-21-032 REV - -Jan 31, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Main, Plate/SkinSDR VNAA20250329034Intercostal · corrodedCORROSION ON INTERCOSTAL STGR 21LH FS310 TO FS333 AT MAIN AVIONICS COMPARTMENT. INTERCOSTAL STGR 21LH FS310 TO FS333 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-21-23-101-001-A01 AND REPLACED PER CRJ700 SRM 51-42-21-001-001-AJan 30, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA20250329033Intercostal · corrodedCORROSION ON INTERCOSTAL STGR 20RH FS310 TO FS319.70 AT MAIN AVIONICS COMPARTMENT. INTERCOSTAL STGR 20RH FS310 TO FS319.70 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-21-23-101-002-A01 AND REPLACED PER CRJ700 SRM 51-42-21-001-Jan 30, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA20250329032Stringer Splice · corrodedCORROSION ON STRINGER AND SPLICE 26RH BTW FS319.70 TO FS349 AT MAIN AVIONICS COMPARTMENT. VALUATED, AFTER PAINT REMOVAL ON STRINGER 26RH BTW FS319.70 TO FS349 AT MAIN AVIONICS COMPARTMENT VISUAL INSPECTION WAS PERFORMED PER CRJ/700 NDTM PART 01 TASK 51-20-Jan 30, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Main, Longeron/StringerSDR VNAA20250329031Stringer Splice · corrodedCORROSION ON STRINGER AND SPLICE 25RH BTW FS310 TO FS333 AT MAIN AVIONICS COMPARTMENT. CORROSION ON STRINGER AND SPLICE 25RH BTW FS310 TO FS333 AT MAIN AVIONICS COMPARTMENT WAS REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01, EVALUATED OUT OF LIMITS PER CRJ70Jan 30, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Main, Longeron/StringerSDR VNAA20250329018Frame · corrodedCORROSION ON FRAME FS295 BTW STGR 25RH TO 25LH, AT MAIN AVIONICS COMPARTMENT. CORROSION ON FRAME FS295 BTW STGR 25RH TO 25LH, AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-21-06-101-001-A01 AND WAS REPAIRED PER CRJ-700 SRM 53-00-Jan 30, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Main, FrameSDR VNA2025F00009Support Fitting · corrodedCORROSION ON JACK FITTING SUPPORT RH/LH SIDE FS 265 TO FS 280 BL 0 AT INTERNAL FUSELAGE. CORROSION ON JACK FITTING SUPPORT RH/LH SIDE FS 265 TO FS 280 BL 0 AT INTERNAL FUSELAGE WAS REMOVED PER CRJ700 SRM 51-21-06-001-001-A01, JACK FITTING SUPPORT RH WAS EVALJan 29, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA20250329030Floorbeam · corrodedCORROSION ON LH FLOOR POST AT FS 280 AND LBL 11.16 WAS FOUND. CORROSION ON LH FLOOR POST AT FS 280 AND LBL 11.16 WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-00-00-101-001-A01 AND REPLACED PER PER CRJ700 SRM 51-42-21-001-001-A01.Jan 29, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Main, Floor BeamSDR VNAA20250329029Seat Track · corrodedCORROSION ON SEAT RAIL 3 EAS AT LBL 9 BTW STA 379 TO STA 677. SEAT RAILS 2 EAS AT LBL 9 BTW STA 379 TO STA 581 WERE CLEANED PER CRJ700 SRM 51-26-00-001-001-A01 AND WERE REINSPECTED PER CRJ/700 NDTM PART 01 TASK 51-20-009-210 (CONFIG A01) AND NOT CORROSION FOJan 29, 2025 · N539EA · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20250329025Seat Track · corrodedCORROSION ON SIDE SEAT RAIL 2 EAS AT STGR 15RH BTW STA 785 TO STA 977. EVALUATED, DUE TO ONLY ONE TYPE OF DAMAGE IS ALLOWED AT ANY TYPICAL CROSS-SECTION ALONG THE LENGTH OF A SIDE SEAT RAIL 2 EAS AT STGR 15RH BTW STA 785 TO STA 977 AT PASSENGER CABIN PER CRJJan 29, 2025 · N539EA · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20250329010Housing · wornWEAR ON EXTERNAL HANDLE HOUSING AT AFT BAGGAGE BAY DOOR. WEAR ON EXTERNAL HANDLE HOUSING AT AFT BAGGAGE BAY DOOR WAS REPAIRED PER REO 670-52-31-031 REV -BJan 29, 2025 · N539EA · Bombdr CL6002D15 · Cargo/Baggage DoorsSDR VNAA20250329009Skin · corrodedCORROSION ON DRAIN HOLES ON FS946 BTW STGR 26L-26R AT AFT FUSELAGE. CORROSION ON DRAIN HOLES ON FS946 BTW STGR 26L-26R AT AFT FUSELAGE WAS REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01 AND REPAIRED PER REO 670-53-51-340 REV- -.Jan 29, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Main, Plate/SkinSDR VNAA20250329008Frame · wornWEAR ON FRAME AT FS1162 AND BTW STGR 7L-8L AT AFT ACCESSORIES COMPARTMENT. FRAME AT FS1162 AND BTW STGR 7L-8L AT AFT ACCESSORIES COMPARTMENT WAS REPAIRED PER REO 670-53-71-096REV. - - AND REO 670-53-71-047 REV. -A.Jan 29, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Main, FrameSDR VNAA20250329007Hinge · corrodedCORROSION ON AFT, MIDDLE AND FWD HINGE AT STEP PLATE C2, AND ILLEGIBLE BLACK/YELLOW MARKING AND DECAL OF FLAP STEP PLATE. AFT, MIDDLE AND FWD HINGE AT STEP PLATE C2 WERE EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-61-58-101-001-A01 AND WERE REPLACED PER CRJ700Jan 29, 2025 · N539EA · Bombdr CL6002D15 · Fuselage, Door HingeSDR VNAA20250330002Floor Support · corrodedCORROSION ON FLOOR SUPPORTS (7EAS) LOCATED BTW FS280 TO FS310 AND LBL20'' AND LBL38'', RBL4'', RBL 18'' RBL38" AT FUSELAGE FLOOR STRUCTURE. FLOOR SUPPORTS (7EAS) LOCATED BTW FS280 TO FS310 AND LBL20'' AND LBL38'', RBL4'', RBL 18'' RBL38" AT FUSELAGE FLOOR SJan 28, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA20250329020Frame · corrodedCORROSION ON FRAME FS319.70 BTW STGR 19LH TO 21LH AND 24LH TO 25RH AT MAIN AVIONICS COMPARTMENT. SECTION OF FRAME FS319.70 BTW STGR 19LH TO 21LH WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-00-06-201-005-A01 AND WAS REPLACED PER CRJ700 SRM 51-42-06-01-001-AJan 28, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Main, FrameSDR VNAA20250329019Frame · corrodedCORROSION ON FRAME FS310 BTW STGR 26RH TO 26LH, AT MAIN AVIONICS COMPARTMENT. FRAME FS310 BTW STGR 26RH TO 26LH, AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-21-06-101-002-A01 AND WAS REPAIRED PER CRJ700 SRM 53-00-06-201-006-A0Jan 28, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Main, FrameSDR VNAA20250329017Angle · corrodedCORROSION ON JOINT ANGLE AT WING TO FUSELAGE FAIRINGSUPPORTFS939BTWSTGR26L-26R. EVALUATED, DUE TO EXCESSIVE ALLOWABLE DAMAGE ON JOINT ANGLE AT WING TO FUSELAGE FAIRING SUPPORT FS939 BTW STGR 26L-26R PER CRJ-700 SRM 53-00-01-101-001-A01 AND REPLACED PER CRJ-7Jan 28, 2025 · N539EA · Bombdr CL6002D15 · Aerodynamic FairingsSDR VNAA20250329016Support · crackedIN REF TO: DURING INSPECTION OF THE TASK CARD 100-08E2-JIC CRACK ON AFT REFUEL DUCT MOUNTING SUPPORT BTW FS677.00 TO FS669.4 AND STGR 21RH TO STGR 22RH WAS DETECTED.. AFT REFUEL DUCT MOUNTING SUPPORT BTW FS677.00 TO FS669.4 AND STGR 21RH TO STGR 22RH WAS REPJan 28, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA20250329006Bracket · corrodedCORROSION ON PLATES (5EAS) UPPER FACE ON FWD CARGO COMPARTMENT. PLATE (1EA) WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-32-58-101-001-A01 AND REPLACED PER CRJ700 SRM 51-42-21-001-001-A01 AND CRJ700 SRM 51-42-22-001-001-A01. PAINT ON AREAS ON MACHINED BRACJan 28, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA20250329005Frame · corrodedCORROSION ON FRAME AT FS 565.00 BTW STGR 16 TO STGR 17 LH SIDE AT CPAX. CORROSION ON FRAME AT FS 565.00 BTW STGR 16 TO STGR 17 LH SIDE AT CPAX WAS REMOVED PER CRJ700 SRM 51-21-06-001-001-A01 AND WAS REPAIRED PER REO 670-53-31-1007 REV. - -.Jan 28, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Main, FrameSDR VNAA20250329004Frame · corrodedCORROSION ON FRAME AT FS 549.00 BTW STGR 16 TO STGR 17 LH SIDE AT CPAX. CORROSION ON FRAME AT FS 549.00 BTW STGR 16 TO STGR 17 LH SIDE AT CPAX WAS REMOVED PER CRJ700 SRM 51-21-06-001-001-A01 AND WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-31-06-101-002-A01Jan 28, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Main, FrameSDR VNAA20250329003Support Plate · corrodedCORROSION ON HYD LINES SUPPORT PLATES (IN BK, LG EXT, LG RET) LH/RH (4 E/A'S) AT RH/LH MAIN WHEEL WELL. CORROSION ON HYD LINES SUPPORT PLATES (IN BK, LG EXT, LG RET) LH/RH (4 E/A'S) AT RH/LH MAIN WHEEL WELLWAS REMOVED PER CRJ700 SRM 51-21-06-001-001-A01 AND Jan 28, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Main, StructureSDR VNAA20250329002Access Panel · corrodedCORROSION ON SETTLEMENT AREA OF ACCESS PANEL 195AB. CORROSION ON SETTLEMENT AREA OF ACCESS PANEL 195AB WAS REMOVED PER CRJ700 SRM 51-21-06-001-001-A01. LANDING DOOR SECTION AND STRAP AFT SIDE WERE EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-00-00-101-001-A01 AJan 28, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Main, StructureSDR VNAA20250329001Repair · wornWEAR ON PREVIOUS REPAIR DOUBLER, LOCATED BTW FS985 TO FS969 AND STGR 26L TO 26R. PREVIOUS REPAIR DOUBLER, LOCATED BTW FS985 TO FS969 AND STGR 26L TO 26R WAS REPAIRED PER REO 670-53-00-290 REV.-FJan 28, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Main, Plate/SkinSDR VNAA20250329015Support Plate · corrodedCORROSION ON METAL SUPPORT OF CONNECTORS PX34-PX33/ PX17-PX33 RH/LH SIDE AT WHEEL WELL AREA. CORROSION ON METAL SUPPORT RH OF CONNECTORS PX34-PX33/ PX17-PX33 AT WHEEL WELL AREA WAS REMOVED PER CRJ700 SRM 51-21-06-001-001-A01 AND EVALUATE WITHIN LIMITS PER CRJan 27, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Main, StructureSDR VNAA20250329014Access Panel · corrodedCORROSION ON ACCESS PANEL 832DT AND 832AT. CORROSION ON ACCESS PANEL 832DT AND 832AT WAS REMOVED PER CRJ700 SRM 51-21-06-001-001-A01. ACCESS PANEL 832DT WAS EVALUATED WITHIN LIMITS PER CRJ700 SRM 52-11-04-101-001-A01. ACCESS PANEL 832AT MUST BE REPLACED UNJan 27, 2025 · N539EA · Bombdr CL6002D15 · Passenger/Crew DoorsSDR VNAA20250329013Spar · crackedCRACK ON FRONT SPAR OF LH MAIN LANDING GEAR DOOR. FRONT SPAR OF LH MAIN LANDING GEAR DOOR WAS REPLACED PER CRJ700 SRM 51-42-06-001-001-A01, PER CRJ700 SRM 51-42-21-001-001-A01 AND PER CRJ700 SRM 51-42-10-001-001-A01Jan 27, 2025 · N539EA · Bombdr CL6002D15 · Landing Gear DoorsSDR VNAA20250329012Exhaust Cone · dentedDENT ON EXHAUST NOZZLE BTW 9-10 O'CLOCK POSITION AT RH ENGINE. DENT ON EXHAUST NOZZLE BTW 9-10 O'CLOCK POSITION AT RH ENGINE WAS REPAIRED PER REO 670-51-00-085 REV.-A AND PER REO 670-54-15-933 REV - -Jan 26, 2025 · N539EA · Bombdr CL6002D15 · Engine Collector/Tailpipe/NozzleSDR VNAA20250329011Hinge · corrodedCORROSION ON HINGES AND HINGE FITTINGS AT AFT LAVATORY SERVICE DOOR 196ER AND WEAR ON HINGES (2 E/AS) OF ACCESS PANEL 195CB (ATACHMENT HARDWARE INCLUED). HINGES (2 E/AS) OF ACCESS PANEL 195CB WERE CLEANED PER CRJ700 SRM 51-26-00-001-001-A01 AND NO DAMAGES WJan 26, 2025 · N539EA · Bombdr CL6002D15 · Fuselage, Door HingeSDR VNAA2024092011102Selector Valve · faultedGEAR DISAGREE WARNING MSG. / REMOVED AND REPLACED SELECTOR VALVE IAW CRJ700 AMM 32-32-10-000/400-801-A01. ALL OPS CHECKS GOOD AT THIS TIME NO LEAKS NOTED. THIS CLEARS MEL.Sep 19, 2024 · N539EA · Cndair CL6002C10 · Landing Gear Position and WarningSDR VNAA2024092011101Warning Message · false activationPROX SYSTEM CAUTION MSG IN FLIGHT / C/W POWER-UP TEST OF LANDING GEAR PSS IAW CRJ 700 AMM 32-61-00-740-801. OPS CHECK GOODSep 18, 2024 · N539EA · Cndair CL6002C10 · Landing Gear Position and Warning
Back to N539EA