# Service difficulty reports: N539EA A list on [N539EA](https://openairdocs.org/aircraft/N539EA.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 3 · 103 reports - [SDR VNAA20250329022](https://openairdocs.org/sdr/VNAA20250329022.md): Stringer · corroded · Mar 3, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Main, Longeron/Stringer > CORROSION 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. - [SDR VNAA20250329021](https://openairdocs.org/sdr/VNAA20250329021.md): Stringer · corroded · Mar 3, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Main, Longeron/Stringer > CORROSION 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 - [SDR VNAA20250330013](https://openairdocs.org/sdr/VNAA20250330013.md): Skin · damaged · Feb 16, 2025 · N539EA · Bombdr CL6002D15 · Cargo/Baggage Doors > ELONGATED 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 R - [SDR VNAA20250330012](https://openairdocs.org/sdr/VNAA20250330012.md): Angle · corroded · Feb 9, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Miscellaneous Structure > CORROSION 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 - [SDR VNAA20250330011](https://openairdocs.org/sdr/VNAA20250330011.md): Canister · cracked · Feb 7, 2025 · N539EA · Bombdr CL6002D15 · Fuel Storage > IN 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 - -. - [SDR VNAA20250330010](https://openairdocs.org/sdr/VNAA20250330010.md): Fitting · corroded · Feb 4, 2025 · N539EA · Bombdr CL6002D15 · Ailerons > CORROSION 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 CLEANING - [SDR VNAA20250330009](https://openairdocs.org/sdr/VNAA20250330009.md): Fitting · corroded · Feb 4, 2025 · N539EA · Bombdr CL6002D15 · Ailerons > CORROSION 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 -- - [SDR VNAA20250330008](https://openairdocs.org/sdr/VNAA20250330008.md): Skin · worn · Feb 4, 2025 · N539EA · Bombdr CL6002D15 · Nacelle/Pylon, Plate/Skin > WEAR 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. - [SDR VNAA20250330007](https://openairdocs.org/sdr/VNAA20250330007.md): Crossbeam · worn · Feb 4, 2025 · N539EA · Bombdr CL6002D15 · Nacelle/Pylon, Main Frame > 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 51-42-06-001-001-A01. AFT EDGE, OUBD SIDE OF UPPER/LOWER FWD CORE COWL AT LH ENGINE WERE REPAIRE - [SDR VNAA20250330006](https://openairdocs.org/sdr/VNAA20250330006.md): Floorbeam · corroded · Feb 2, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Main, Floor Beam > AFTER 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 - [SDR VNAA20250330005](https://openairdocs.org/sdr/VNAA20250330005.md): Support Angle · cracked · Feb 2, 2025 · N539EA · Bombdr CL6002D15 · Wing Miscellaneous Structure > CRACK 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 A - [SDR VNAA20250330004](https://openairdocs.org/sdr/VNAA20250330004.md): Stiffener · corroded · Feb 1, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Miscellaneous Structure > CORROSION 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 MM670-6 - [SDR VNAA20250330003](https://openairdocs.org/sdr/VNAA20250330003.md): Shim · corroded · Feb 1, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Miscellaneous Structure > CORROSION 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 CRJ70 - [SDR VNAA20250329028](https://openairdocs.org/sdr/VNAA20250329028.md): Seat Track · corroded · Feb 1, 2025 · N539EA · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings > CORROSION 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 - [SDR VNAA20250329027](https://openairdocs.org/sdr/VNAA20250329027.md): Seat Track · corroded · Feb 1, 2025 · N539EA · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings > CORROSION 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 WER - [SDR VNAA20250329026](https://openairdocs.org/sdr/VNAA20250329026.md): Seat Track · corroded · Feb 1, 2025 · N539EA · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings > CORROSION 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 W - [SDR VNAA20250329024](https://openairdocs.org/sdr/VNAA20250329024.md): Seat Track · corroded · Feb 1, 2025 · N539EA · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings > CORROSION 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 RA - [SDR VNAA20250330001](https://openairdocs.org/sdr/VNAA20250330001.md): Rib · corroded · Jan 31, 2025 · N539EA · Bombdr CL6002D15 · Wing, Rib/Bulkhead > GOUGES ON RH WING TE ASSY, RIB FLS13.65. RIB WAS REPLACED PER REO 670-57-51-590 REV - -. - [SDR VNAA20250329023](https://openairdocs.org/sdr/VNAA20250329023.md): Skin · corroded · Jan 31, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Main, Plate/Skin > CORROSION 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 - - - [SDR VNAA20250329034](https://openairdocs.org/sdr/VNAA20250329034.md): Intercostal · corroded · Jan 30, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Miscellaneous Structure > CORROSION 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-A - [SDR VNAA20250329033](https://openairdocs.org/sdr/VNAA20250329033.md): Intercostal · corroded · Jan 30, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Miscellaneous Structure > CORROSION 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- - [SDR VNAA20250329032](https://openairdocs.org/sdr/VNAA20250329032.md): Stringer Splice · corroded · Jan 30, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Main, Longeron/Stringer > CORROSION 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- - [SDR VNAA20250329031](https://openairdocs.org/sdr/VNAA20250329031.md): Stringer Splice · corroded · Jan 30, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Main, Longeron/Stringer > CORROSION 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 CRJ70 - [SDR VNAA20250329018](https://openairdocs.org/sdr/VNAA20250329018.md): Frame · corroded · Jan 30, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Main, Frame > CORROSION 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- - [SDR VNA2025F00009](https://openairdocs.org/sdr/VNA2025F00009.md): Support Fitting · corroded · Jan 29, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Miscellaneous Structure > CORROSION 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 EVAL - [SDR VNAA20250329030](https://openairdocs.org/sdr/VNAA20250329030.md): Floorbeam · corroded · Jan 29, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Main, Floor Beam > CORROSION 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. - [SDR VNAA20250329029](https://openairdocs.org/sdr/VNAA20250329029.md): Seat Track · corroded · Jan 29, 2025 · N539EA · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings > CORROSION 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 FO - [SDR VNAA20250329025](https://openairdocs.org/sdr/VNAA20250329025.md): Seat Track · corroded · Jan 29, 2025 · N539EA · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings > CORROSION 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 CRJ - [SDR VNAA20250329010](https://openairdocs.org/sdr/VNAA20250329010.md): Housing · worn · Jan 29, 2025 · N539EA · Bombdr CL6002D15 · Cargo/Baggage Doors > WEAR 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 -B - [SDR VNAA20250329009](https://openairdocs.org/sdr/VNAA20250329009.md): Skin · corroded · Jan 29, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Main, Plate/Skin > CORROSION 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- -. - [SDR VNAA20250329008](https://openairdocs.org/sdr/VNAA20250329008.md): Frame · worn · Jan 29, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Main, Frame > WEAR 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. - [SDR VNAA20250329007](https://openairdocs.org/sdr/VNAA20250329007.md): Hinge · corroded · Jan 29, 2025 · N539EA · Bombdr CL6002D15 · Fuselage, Door Hinge > CORROSION 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 CRJ700 - [SDR VNAA20250330002](https://openairdocs.org/sdr/VNAA20250330002.md): Floor Support · corroded · Jan 28, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Miscellaneous Structure > CORROSION 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 S - [SDR VNAA20250329020](https://openairdocs.org/sdr/VNAA20250329020.md): Frame · corroded · Jan 28, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Main, Frame > CORROSION 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-A - [SDR VNAA20250329019](https://openairdocs.org/sdr/VNAA20250329019.md): Frame · corroded · Jan 28, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Main, Frame > CORROSION 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-A0 - [SDR VNAA20250329017](https://openairdocs.org/sdr/VNAA20250329017.md): Angle · corroded · Jan 28, 2025 · N539EA · Bombdr CL6002D15 · Aerodynamic Fairings > CORROSION 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-7 - [SDR VNAA20250329016](https://openairdocs.org/sdr/VNAA20250329016.md): Support · cracked · Jan 28, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Miscellaneous Structure > IN 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 REP - [SDR VNAA20250329006](https://openairdocs.org/sdr/VNAA20250329006.md): Bracket · corroded · Jan 28, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Miscellaneous Structure > CORROSION 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 BRAC - [SDR VNAA20250329005](https://openairdocs.org/sdr/VNAA20250329005.md): Frame · corroded · Jan 28, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Main, Frame > CORROSION 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. - -. - [SDR VNAA20250329004](https://openairdocs.org/sdr/VNAA20250329004.md): Frame · corroded · Jan 28, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Main, Frame > CORROSION 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-A01 - [SDR VNAA20250329003](https://openairdocs.org/sdr/VNAA20250329003.md): Support Plate · corroded · Jan 28, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Main, Structure > CORROSION 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 - [SDR VNAA20250329002](https://openairdocs.org/sdr/VNAA20250329002.md): Access Panel · corroded · Jan 28, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Main, Structure > CORROSION 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 A - [SDR VNAA20250329001](https://openairdocs.org/sdr/VNAA20250329001.md): Repair · worn · Jan 28, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Main, Plate/Skin > WEAR 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.-F - [SDR VNAA20250329015](https://openairdocs.org/sdr/VNAA20250329015.md): Support Plate · corroded · Jan 27, 2025 · N539EA · Bombdr CL6002D15 · Fuselage Main, Structure > CORROSION 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 CR - [SDR VNAA20250329014](https://openairdocs.org/sdr/VNAA20250329014.md): Access Panel · corroded · Jan 27, 2025 · N539EA · Bombdr CL6002D15 · Passenger/Crew Doors > CORROSION 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 UN - [SDR VNAA20250329013](https://openairdocs.org/sdr/VNAA20250329013.md): Spar · cracked · Jan 27, 2025 · N539EA · Bombdr CL6002D15 · Landing Gear Doors > CRACK 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-A01 - [SDR VNAA20250329012](https://openairdocs.org/sdr/VNAA20250329012.md): Exhaust Cone · dented · Jan 26, 2025 · N539EA · Bombdr CL6002D15 · Engine Collector/Tailpipe/Nozzle > DENT 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 - - - [SDR VNAA20250329011](https://openairdocs.org/sdr/VNAA20250329011.md): Hinge · corroded · Jan 26, 2025 · N539EA · Bombdr CL6002D15 · Fuselage, Door Hinge > CORROSION 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 W - [SDR VNAA2024092011102](https://openairdocs.org/sdr/VNAA2024092011102.md): Selector Valve · faulted · Sep 19, 2024 · N539EA · Cndair CL6002C10 · Landing Gear Position and Warning > GEAR 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. - [SDR VNAA2024092011101](https://openairdocs.org/sdr/VNAA2024092011101.md): Warning Message · false activation · Sep 18, 2024 · N539EA · Cndair CL6002C10 · Landing Gear Position and Warning > PROX 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 GOOD Next page: https://openairdocs.org/aircraft/N539EA/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/aircraft/N539EA/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.