N527EA

Service difficulty reports · 130

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 = 'N527EA' 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 VNAA202511270012Lug · damagedTO PERFORM OVERSIZE BEARINGS INSTALLATON REWORK RH AILERON LUG R3 AND R4 TO INSTALL BEARING P/N: KSC432409B. PERFORM OVERSIZE AT RH AILERON LUG R3 AND R4 PER REO 670-57-61-458 REV. -AOct 17, 2025 · N527EA · Cndair CL6002C10 · AileronsSDR VNAA202511270008Hinge · corrodedAFTER HINGE FITTINGS REMOVAL IN REF NRC 0034 CORROSION IN UPPER HINGE WAS FOUND. UPPER HINGE OF TOILET SERVICE DOOR 196ER WAS REPLACED PER CRJ-700 SRM 51-41-02-001-001-A01Oct 13, 2025 · N527EA · Cndair CL6002C10 · Fuselage, Door HingeSDR VNAA202511270009Hinge Fitting · corrodedCORROSION ON FITTING CLOSING FWD AT SURROUND PASSENGER DOOR WAS FOUND. CORROSION ON FITTING CLOSING FWD AT SURROUND PASSENGER DOOR WAS EVALUATED EXCESSIVE DAMAGE PER CRJ-700 SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ700 SRM 51-42-06-001-001-A01, SRM 51-42Oct 1, 2025 · N527EA · Cndair CL6002C10 · Fuselage, Door HingeSDR VNAA202511270011Lug · corrodedTO PERFORM OVERSIZE BEARING INSTALLATON REWORK LH AILERON LUG L4 TO INSTALL BEARING P/N: KSC432409B-03. NEW BEARING (1EA) (LUG 4) PN:KSC432409B-03 AT AILERON LH WAS INSTALLED PER REO 670-57-61-457 REV -ASep 25, 2025 · N527EA · Cndair CL6002C10 · AileronsSDR VNAA202511270007Lug · corrodedAFTER BEARINGS AND BUSHINGS REMOVAL IN REF. TASK CARD 271500-RH-PSA-AILERON, CORROSION AND SCRATCHES WAS FOUND ON CENTER FITING LUGS R1, R2, R5 AND R6. AT RH AILERON. CENTER FITING LUGS R1, R2, R5 AND R6. AT RT AILERON WERE REPAIRED IAW REO 670-57-61-237 REV Sep 25, 2025 · N527EA · Cndair CL6002C10 · AileronsSDR VNAA202511270006Lug · corrodedCORROSION AND SCRATCHES ON OUT FITTING AND CENTER FITING LUGS L1,L2, L5 AND L6. AT LH AILERON WAS FOUND. CENTER FITING LUGS L1,L2, L5 AND L6. WERE REPAIRED PER REO 670-57-61-237 REV. - - PAR F AND OUT FITTTING LUGS WERE CLEANED PER PER CRJ-700 SRM 51-26-00-00Sep 25, 2025 · N527EA · Cndair CL6002C10 · AileronsSDR VNAA202511270005Frame · corrodedCORROSION ON FRAME FS1015.00 BTW STGR 21LH TO STGR 24RH AT INTERNAL STRUCTURE AFT CARGO COMPARTMENT. CORROSION ON FRAME BS 1015.00 BTW STGR 21LH TO STGR 24RH AT INTERNAL STRUCTURE AFT CARGO COMPARTMENT WAS EVALUATED OUT LIMITS IAW SRM 53-61-06-101-001-A01 ANSep 25, 2025 · N527EA · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA202511270004Floorbeam · corrodedCORROSION ON FLOOR BEAM LBL 27 BTW FS 1000.00 TO FS 1069.00 AT FLOOR STRUCTURE AFT CARGO COMPARTMENT. CORROSION ON FLOOR BEAM LBL 27 BTW FS 1000.00 TO FS 1069.00 AT FLOOR STRUCTURE AFT CARGO COMPARTMENT WAS EVALUATED EXCESSIVE DAMAGE IAW SRM 53-61-43-101-001Sep 25, 2025 · N527EA · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA202511270003Canister · crackedCRACK IN CANISTER WELDED NO.3, ON WS148.019 OF INTERNAL RH MAIN FUEL TANK. CANISTER WELDED NO.3, ON WS148.019 OF INTERNAL RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV. --Sep 25, 2025 · N527EA · Cndair CL6002C10 · Wing Main, Frame StructureSDR VNAA202511270002Seat Track · corrodedCORROSION ON SEAT RAIL RBL27.00 BTW FS977.00 TO FS1005.00 AT PASSENGER CABIN. DUE TO EXCESSIVE DAMAGE ON SEAT RAIL RBL27.00 BTW FS977.00 TO FS1005.00 AT PASSENGER CABIN WERE EVALUATED OUT OF LIMITS PER SRM 53-51-49-101-001-A01 AND WERE REPLACED PER CRJ700 AMMSep 25, 2025 · N527EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202511270010Stringer Splice · corrodedCORROSION ON STRINGER SPLICE 24RH BTW STA. FS= 319.00 AND FS= 333.00 AT MAIN AVIONICS COMPARTMENT. CORROSION ON STRINGER SPLICE 24RH WAS EVALUATED EXCESSIVE DAMAGE PER CRJ700 SRM 53-00-00-101-001-A01 AND REPLACED IAW SRM 51-42-06-001-001-A01.Sep 22, 2025 · N527EA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202511260007Stringer · corrodedCORROSION ON STRINGER 24R BTW FS485 AND FS501 AT FWD BAGGAGE BAY COMPARTMENT. CORROSION ON STRINGER 24R BTW FS485 AND FS501 AT FWD BAGGAGE BAY COMPARTMENT WAS REPAIRED PER REO 670-53-31-1111 REV-.Sep 22, 2025 · N527EA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNA2025F00041Stringer Splice · corrodedCORROSION ON STRINGER SPLICE 21RH IN STA. FS= 333.00 TO FS= 337 AT MAIN AVIONICS COMPARTMENT. CORROSION ON STRINGER SPLICE 21RH IN STA. FS= 333.00 TO FS= 337 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED FOR EXCESSIVE DAMAGE PER CRJ-700 SRM 53-00-00-101-001-A01 Sep 22, 2025 · N527EA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202511260004Intercostal · corrodedCORROSION ON INTERCOSTAL ATTACHED TO STGR 20RH BTW FS 310.00 AND FS 319.00 AT MAIN AVIONICS COMPARTMENT. INTERCOSTAL ATTACHED TO STGR 20RH BTW FS 310.00 AND FS 319.00 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED DUE EXCESSIVE DAMAGE PER CRJ-700 SRM 53-21-23-10Sep 22, 2025 · N527EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202511260003Stringer Splice · corrodedCORROSION ON STRINGER AND SPLICE 23RH BTW STA. FS= 310.00 AND FS= 333.00 AT MAIN AVIONICS COMPARTMENT. CORROSION SPLICE 23RH BTW STA. FS= 310.00 AND FS= 333.00 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED EXCEDED ALLOWABLE PER CRJ-700 SRM 53-00-00-101-001-A01 Sep 22, 2025 · N527EA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202511260002Stringer Splice · corrodedCORROSION ON STRINGER SPLICE 24RH BTW STA. FS= 319.00 AND FS= 333.00 AT MAIN AVIONICS COMPARTMENT. CORROSION ON STRINGER SPLICE 24RH BTW STA. FS= 319.00 AND FS= 333.00 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED EXCESSIVE DAMAGE PER CRJ700 SRM 53-00-00-101-001Sep 22, 2025 · N527EA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202511260001Stringer · corrodedCORROSION ON STRINGER AND SPLICE 25R BTW BS 310 AND 333 AT MAIN AVIONICS COMPARTMENT. CORROSION ON STRINGER 25R BTW BS 310 & BS 333 WAS EVALUATED EXCESSIVE DAMEGE IAW SRM 53-00-00-101-001-A01 AND REPLACED IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-00Sep 22, 2025 · N527EA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202511250010Stringer · corrodedCORROSION ON STRINGER 26LH AND STANDOFFS (2EAS) BTW STA. FS= 295.00 AND FS= 310.00 AT MAIN AVIONICS COMPARTMENT. STRINGER 26LH AND STANDOFFS (2EAS) BTW STA. FS= 295.00 AND FS= 310.00 AT MAIN AVIONICS COMPARTMENT WERE EVALUATED EXCESSIVE DAMAGE PER SRM 53-21-0Sep 22, 2025 · N527EA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202511250009Stringer · corrodedCORROSION ON STRINGER 26RH BTW STA. FS= 295.00 AND FS= 310.00 AT MAIN AVIONICS COMPARTMENT. CORROSION ON STRINGER 26RH BTW STA FS= 295.00 AND FS= 310.00 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED DUE EXCESSIVE DAMAGE PER CRJ-700 SRM 51-21-06-001-001-A01 AND Sep 22, 2025 · N527EA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202511250003Doubler · corrodedCORROSION ON DOUBLER OF FUSELAGE SKIN BTW FS 969.00 TO FS 1000. DOUBLER OF FUSELAGE SKIN BTW FS 969.00 TO FS 1000.00 WAS REPLACED PER REO 670-53-00-290 REV -FSep 20, 2025 · N527EA · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA202511250002Access Panel · corrodedCORROSION ON SETTLEMENT AREA OF ACCESS PANEL: 642BZ. CORROSION ON SETTLEMENT AREA OF ACCESS PANEL: 642BZ WAS EVALUATED EXCESSIVE DAMAGE PER SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ-700 SRM 51-42-21-001-001-A01.Sep 19, 2025 · N527EA · Cndair CL6002C10 · Wing, Plate/SkinSDR VNAA202511250001Hinge · corrodedCORROSION ON HINGE FITTINGS OF TOILET SERVICE DOOR 196ER. HINGE FITTINGS OF TOILET SERVICE DOOR 196ER WAS REPLACED PER CRJ-700 AMM 52-45-01-400-80.Sep 18, 2025 · N527EA · Cndair CL6002C10 · Fuselage, Door HingeSDR VNAA202511270001Seat Track · corrodedCORROSION ON LH SIDE SEAT RAILS LBL 45 (STRG 15LH) BTW FS 785TO FS 847, BTW FS 744 TO FS 785, BTW FS 661+16 TO FS 720, BTW FS 661 TO 549 & BTW FS 379 TO 548 AT PASSENGER CABIN. SEAT TRACK BTW FS 881 TO FS 913, BTW FS 661+16 TO FS 720, BTW FS 661 TO 549 & BTW Sep 5, 2025 · N527EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202511260010Seat Track · corrodedWEAR AND CORROSION ON RH SIDE SEAT RAILS RBL 45 (STGR 15RH) BTW FS 379 TO FS 394, BTW FS 469 TO FS 581, BTW FS 629 TO FS 661, BTW FS 744 TO FS 761 & BTW FS 785 TO FS 797 AT PASSENGER CABIN. RT SIDE SEAT RAILS RBL 45 (STGR 15RH) BTW FS 379 TO FS 394, BTW FS 46Sep 5, 2025 · N527EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202511260009Seat Track · corrodedCORROSION ON FLOOR SEAT RAILS BTW FS 881 TO FS 913, BTW FS 661+16 TO FS 720, BTW FS 661 TO 549 & BTW FS 379 TO 548 AT LBL 9 PASSENGER CABIN. CORROSION ON FLOOR SEAT RAILS BTW FS 881 TO FS 913, BTW FS 661+16 TO FS 720, BTW FS 661 TO 549 & BTW FS 379 TO 548 ATSep 5, 2025 · N527EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202511260008Seat Track · corrodedWEAR AND CORROSION ON FLOOR SEAT RAILS BTW FS 349 TO FS 364, BTW FS 661+46 TO 661+74, BTW FS 720 TO FS 744 & BTW FS 847 TO FS 977 AT RBL 9 PASSENGER CABIN. FLOOR SEAT RAILS BTW FS 349 TO FS 364, BTW FS 661+46 TO 661+74, BTW FS 720 TO FS 744 & BTW FS 847 TO FSep 5, 2025 · N527EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202511260006Panel · corrodedCORROSION ON THE MATING SURFACE OF THE PANEL ASSEMBLY FROM SS15.50 TO SS39.00 (ACCESS 621AB), AS WELL AS CORROSION ON MATING SURFACE OF LOWER EDGE OF ACCESS 621AT, RIGHT WING. CORROSION ON THE MATING SURFACE OF THE PANEL ASSEMBLY FROM SS15.50 TO SS39.00 (ACCESSep 4, 2025 · N527EA · Cndair CL6002C10 · Wing, Plate/SkinSDR VNAA202511250008Landing · corrodedCORROSION ON SETTLEMENT AREA OF ACCESS PANEL 521AT AT LH WING. SETTLEMENT AREA OF ACCESS PANEL 521AT AT LT WING (LT SIDE FRAME HOUSING LANDING P/N: CC670-12111-5) WAS EVALUATED OUT OF LIMITS PER SRM 57-41-01-101-001-A01 REPLACED PER CRJ900 SRM 51-42-06-001-0Sep 4, 2025 · N527EA · Cndair CL6002C10 · Wing, Plate/SkinSDR VNAA202511250006Intercostal · corrodedCRACK ON INTERCOSTAL BTW FS173 TO FS179 AND WL79.50 INTERNAL STRUCTURE AT FWD EQUIPMENT COMPARTMENT. INTERCOSTAL BTW FS173 TO FS179 AND WL79.50 INTERNAL STRUCTURE AT FWD EQUIPMENT COMPARTMENT WAS REPLACED PER SRM 51-42-10-001-001-A01, SRM 51-42-06-001-001-A0Sep 4, 2025 · N527EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202511250005Web · crackedCRACK ON WEB BTW FS195 TO FS205 AND WL79.50 INTERNAL STRUCTURE AT FWD EQUIPMENT COMPARTMENT. WEB BTW FS195 TO FS205 AND WL79.50 INTERNAL STRUCTURE AT FWD EQUIPMENT COMPARTMENT WAS REPAIRED PER CRJ-900 SRM 53-11-43-201-001-A01.Sep 4, 2025 · N527EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202511250004Angle · corrodedCORROSION ON SETTLEMENT AREA (UPPER SURFACE) OF ACCESS PANEL 362AR AT AFT FUSELAGE. ANGLE P/N: WA670-30111-3 ON SETTLEMENT AREA (UPPER SURFACE) OF ACCESS PANEL 362AR AT AFT FUSELAGE WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND DWG 670-30111 REV. C.Sep 3, 2025 · N527EA · Cndair CL6002C10 · Horizontal Stabilizer Miscellaneous StructureSDR VNAA202511250007Intercostal · corrodedCORROSION ON LATCH PIN INTERCOSTAL LEFT TO STG•R 27 AND BTW FS394 TO FS400 INTERNAL STRUCTURE AT AVIONICS COMPAR•TMENT. LATCH PIN INTERCOSTAL LEFT TO STGR27 AND BTW FS394 TO FS400 INTERNAL STRUCTURE AT AVIONICS COMPARTMENT WAS REPLACED PER SRM 51-42-06-001-0Sep 2, 2025 · N527EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2025052311101Overheat Loop · faultedL BLEED DUCT WARNING MSG ON CLIMB, FL260. / REMOVED AND REPLACED LOOP MT141 IAW CRJ 700 AMM 36-21-01-000/400-806-A04. OPS CHECK GOOD AT THIS TIME. PERFORMED UNATE SCAN OF AILC. AILC OPS CHECKS GOOD AT THIS TIME.May 19, 2025 · N527EA · Cndair CL6002C10 · Overheat DetectionSDR VNAA2025051311101Clamp · looseL BLEED DUCT WARNING MSG. / INSPECTED LOOP IN AEB AND FOUND BLUE ADEL CLAMP THAT HOLD BOTH LOOPS IN PLACED EXTREMELY LOOSE (HOLDING BY ONE THREAD) CAUSING BOTH LOOPS TO TOUCH. RETORQUED CLAMP PER AMM 20-21-00-910-801-A01 AND 36-21-00-910-801-A01. NO OTHER DEFEMay 12, 2025 · N527EA · Cndair CL6002C10 · Pneumatic SystemSDR VNAA2025050111102Shutoff Valve · unserviceableL BLEED DUCT WARNING IN FLIGHT. / REMOVED AND REPLACED #1 PRSOV IAW CRJ 700 AMM 36-12-01-000/400-801. OPS CHECK GOOD AND LEAK CHECK GOOD.Apr 30, 2025 · N527EA · Cndair CL6002C10 · Pneumatic Distribution SystemSDR VNAA2025042911101Overheat Loop · faultedL BLEED DUCT WARNING MSG / REMOVED AND REPLACED LH BLEED LOOP A WIRE AND CONNECTORS FROM MT139P1 TO MT141P1 WITH NEW INSULATORS AS AN ASSY ROBBED FROM N534AE IAW FIM 36-21-01-810-801-A01. OPS CHECKS GOOD. LH BLEED LOOP A CHECKS AT 66 OHMS.Apr 27, 2025 · N527EA · Cndair CL6002C10 · Overheat DetectionSDR VNAA2025041511103Bleed Valve · tornL BLEED DUCT WARNING MSG WHILE CLIMBING THROUGH FL 210 / FOUND INSULATION MUFF FOR THE CROSS BLEED VALVE TORN. REMOVED AND REPLACED INSULATION MUFF IAW CRJ-700 AMM 36-13-15-400-801 AND 36-21-00-910-801. OPS TEST AND LEAK TEST GOOD. L BLEED DUCT WARNING MSG DIDApr 14, 2025 · N527EA · Cndair CL6002C10 · Compressor Bleed ValveSDR VNAA202502120006Angle · crackedWHILE PREFORMING WEB REPAIR FOUND ANGLE, BL26.00 FS280.00 TO BE CRACKED. CORRECTIVE ACTION: REMOVED CRACKED ANGLE. INSTALLED NEW WEB ANGLE PN: CC670-34117-6 AT BL26.00 FS280.00 IAW CRJ700 SRM 51-42-06-001-001-A01. HN00217765Feb 12, 2025 · N527EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202502120005Web · corroded"LH FS280 LOWER WEB FOUND TO BE CORRODED. PERFORMED REPAIR OF LH BULKHEAD LOWER WEB FS280 IAW CRJ700 SRM 53-11-10-201-004-A01. HN00217439"Feb 12, 2025 · N527EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202502120004Web · corroded"RH FS280 LOWER WEB FOUND TO BE CORRODED. PERFORMED REPAIR OF RH BULKHEAD LOWER WEB FS280 IAW CRJ700 SRM 53-11-10-201-004-A01.HN00217405"Feb 12, 2025 · N527EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202502120003Angle · corrodedJ ANGLE FOUND TO BE CORRODED AT FS280 BETWEEN LBL9 AND RBL9.CORRECTIVE ACTION: REMOVED J ANGLE AT FS280 IAW CRJ700 SRM 51-42-06-001-001-A01. LOCATED, DRILLED, AND DEBURRED J ANGLE AT FS280 PN: CC670-34095-1SB AND SPLICE ANGLE PN: CC670-34098-1 IAW CRJ700 SRM Feb 12, 2025 · N527EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202502120002Floorbeam · corrodedLH FS280 FLOOR BEAM FOUND TO BE CORRODED AND CRACKED. REQUIRES REPLACEMENT. : REMOVED RH FS280 FLOOR BEAM IAW CRJ700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-42-13-001-001-A01. LOCATED, DRILLED, AND DEBURRED RH FS280 FLOOR BEAM PN: CC670-34094-1Feb 12, 2025 · N527EA · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA202502120001Floorbeam · corroded"RH FS280 FLOOR BEAM FOUND TO BE CORRODED AND CRACKED. REQUIRES REPLACEMENT, REMOVED RH FS280 FLOOR BEAM IAW CRJ700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-42-13-001-001-A01. LOCATED, DRILLED, AND DEBURRED RH FS280 FLOOR BEAM PN: CC670-34094-2SFeb 12, 2025 · N527EA · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA202305091111Unknown · unknownMAIN PASSENGER DOOR WARNING MSG CAME ON IN CRUISE FLIGHT, RAMP PERSONNEL NOTED OUTER HANDLE OPEN. INNER HANDLE HANDLE IN PROPER POSITION AND LOCKED / INSPECTED MAIN DOOR LINKAGE WITH NO FAULTS NOTED. PERFORMED OPS CHECK OF DOOR IAW CRJ 700 AMM 52-11-00-710-801May 6, 2023 · N527EA · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA202303301111Unknown · unknownRH LOWER WING SKIN BETWEEN WS314.5 €“ 330.45 & STGR10 €“ STGR11. C/W PERMANENT REPAIR OF E.A. 22-C7-57-1591 REV A IAW E.A. INSTRUCTIONS.Mar 29, 2023 · N527EA · Cndair CL6002C10 · Wing StructureSDR VNAA202208119991Panel · corrodedNDT FAILED HOLE ON R/H LOWER WING PLANK, I/B ROW, AFT FASTENERAug 8, 2022 · N527EA · Bombdr BD1001A10 · Fuselage Main, StructureSDR VNAA202204069991Skin · dentedREPAIRED MULTIPLE DENTS ON THE OUTSIDE LOWER SKIN JUST AFT OF THE AFT EQUIPMENT BAY DOOR BETWEEN FS1162 TO SPAR DATUM 55.63 AND STRS 23R-23-L PER REO 670-53-71-088 CONSIDERED A MAJOR REPAIR.Apr 6, 2022 · N527EA · Bombdr CL6002D15 · Fuselage Structure (General)SDR V0XD20211228001Skin · dentedDENT ON FUSELAGE SKIN AT FS 1031 ON STGR 25R MEASURING 1.00"L X .5"W .031"D. CORRECTIVE ACCTION: REPAIRED AREA BY DRESSING BACK DENT AT FS 1031 ON STGR 25R TO .950"L X .475"W X .011"D AND FABRICATED DOUBLER REPAIR PARTS AND INSTALLED THEM AT FS 1031 AT STGR 2Dec 23, 2021 · N527EA · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA202201029992Angle · corrodedAFT WING TO BODY SUPPORT ATTACHMENT ANGLE IS CORRODED AT F.S. 953 FROM B.L. 24L-24R. CORRECTIVE ACTION: REMOVED AND REPLACED ANGLE (P/N: SH670-39189-1) I/A/W CRJ 700 SRM 51-40-00.Dec 21, 2021 · N527EA · Cndair CL6002C10 · Fuselage, Wing Attach FittingsSDR V0XD20211213003Angle · corrodedAFT WING TO BODY SUPPORT ATTACHMENT ANGLE IS CORRODED AT F/S. 953 FROM B/L 24L-24R. CORRECTIVE ACTION: REMOVED AND REPLACED ANGLE (P/N: SH670-39189-1) IAW CRJ 700 SRM 51-40-00.Dec 21, 2021 · N527EA · Cndair CL6002C10 · Wing, Fuselage Attach Fittings
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