# Service difficulty reports: N527EA

A list on [N527EA](https://openairdocs.org/aircraft/N527EA.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 · 130 reports

- [SDR VNAA202511270012](https://openairdocs.org/sdr/VNAA202511270012.md): Lug · damaged · Oct 17, 2025 · N527EA · Cndair CL6002C10 · Ailerons
  > TO 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. -A
- [SDR VNAA202511270008](https://openairdocs.org/sdr/VNAA202511270008.md): Hinge · corroded · Oct 13, 2025 · N527EA · Cndair CL6002C10 · Fuselage, Door Hinge
  > AFTER 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-A01
- [SDR VNAA202511270009](https://openairdocs.org/sdr/VNAA202511270009.md): Hinge Fitting · corroded · Oct 1, 2025 · N527EA · Cndair CL6002C10 · Fuselage, Door Hinge
  > CORROSION 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 51-42
- [SDR VNAA202511270011](https://openairdocs.org/sdr/VNAA202511270011.md): Lug · corroded · Sep 25, 2025 · N527EA · Cndair CL6002C10 · Ailerons
  > TO 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 -A
- [SDR VNAA202511270007](https://openairdocs.org/sdr/VNAA202511270007.md): Lug · corroded · Sep 25, 2025 · N527EA · Cndair CL6002C10 · Ailerons
  > AFTER 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
- [SDR VNAA202511270006](https://openairdocs.org/sdr/VNAA202511270006.md): Lug · corroded · Sep 25, 2025 · N527EA · Cndair CL6002C10 · Ailerons
  > CORROSION 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 51-26-00-00
- [SDR VNAA202511270005](https://openairdocs.org/sdr/VNAA202511270005.md): Frame · corroded · Sep 25, 2025 · N527EA · Cndair CL6002C10 · Fuselage Main, Frame
  > CORROSION 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 AN
- [SDR VNAA202511270004](https://openairdocs.org/sdr/VNAA202511270004.md): Floorbeam · corroded · Sep 25, 2025 · N527EA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > CORROSION 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 53-61-43-101-001
- [SDR VNAA202511270003](https://openairdocs.org/sdr/VNAA202511270003.md): Canister · cracked · Sep 25, 2025 · N527EA · Cndair CL6002C10 · Wing Main, Frame Structure
  > CRACK 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. --
- [SDR VNAA202511270002](https://openairdocs.org/sdr/VNAA202511270002.md): Seat Track · corroded · Sep 25, 2025 · N527EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION 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 AMM
- [SDR VNAA202511270010](https://openairdocs.org/sdr/VNAA202511270010.md): Stringer Splice · corroded · Sep 22, 2025 · N527EA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION 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.
- [SDR VNAA202511260007](https://openairdocs.org/sdr/VNAA202511260007.md): Stringer · corroded · Sep 22, 2025 · N527EA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION 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-.
- [SDR VNA2025F00041](https://openairdocs.org/sdr/VNA2025F00041.md): Stringer Splice · corroded · Sep 22, 2025 · N527EA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION 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
- [SDR VNAA202511260004](https://openairdocs.org/sdr/VNAA202511260004.md): Intercostal · corroded · Sep 22, 2025 · N527EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION 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 53-21-23-10
- [SDR VNAA202511260003](https://openairdocs.org/sdr/VNAA202511260003.md): Stringer Splice · corroded · Sep 22, 2025 · N527EA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION 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
- [SDR VNAA202511260002](https://openairdocs.org/sdr/VNAA202511260002.md): Stringer Splice · corroded · Sep 22, 2025 · N527EA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION 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 53-00-00-101-001
- [SDR VNAA202511260001](https://openairdocs.org/sdr/VNAA202511260001.md): Stringer · corroded · Sep 22, 2025 · N527EA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION 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 51-42-21-001-00
- [SDR VNAA202511250010](https://openairdocs.org/sdr/VNAA202511250010.md): Stringer · corroded · Sep 22, 2025 · N527EA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION 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 53-21-0
- [SDR VNAA202511250009](https://openairdocs.org/sdr/VNAA202511250009.md): Stringer · corroded · Sep 22, 2025 · N527EA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION 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
- [SDR VNAA202511250003](https://openairdocs.org/sdr/VNAA202511250003.md): Doubler · corroded · Sep 20, 2025 · N527EA · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > CORROSION 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 -F
- [SDR VNAA202511250002](https://openairdocs.org/sdr/VNAA202511250002.md): Access Panel · corroded · Sep 19, 2025 · N527EA · Cndair CL6002C10 · Wing, Plate/Skin
  > CORROSION 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.
- [SDR VNAA202511250001](https://openairdocs.org/sdr/VNAA202511250001.md): Hinge · corroded · Sep 18, 2025 · N527EA · Cndair CL6002C10 · Fuselage, Door Hinge
  > CORROSION 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.
- [SDR VNAA202511270001](https://openairdocs.org/sdr/VNAA202511270001.md): Seat Track · corroded · Sep 5, 2025 · N527EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION 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
- [SDR VNAA202511260010](https://openairdocs.org/sdr/VNAA202511260010.md): Seat Track · corroded · Sep 5, 2025 · N527EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > WEAR 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 46
- [SDR VNAA202511260009](https://openairdocs.org/sdr/VNAA202511260009.md): Seat Track · corroded · Sep 5, 2025 · N527EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > 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 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 AT
- [SDR VNAA202511260008](https://openairdocs.org/sdr/VNAA202511260008.md): Seat Track · corroded · Sep 5, 2025 · N527EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > WEAR 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 F
- [SDR VNAA202511260006](https://openairdocs.org/sdr/VNAA202511260006.md): Panel · corroded · Sep 4, 2025 · N527EA · Cndair CL6002C10 · Wing, Plate/Skin
  > CORROSION 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 (ACCES
- [SDR VNAA202511250008](https://openairdocs.org/sdr/VNAA202511250008.md): Landing · corroded · Sep 4, 2025 · N527EA · Cndair CL6002C10 · Wing, Plate/Skin
  > CORROSION 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 51-42-06-001-0
- [SDR VNAA202511250006](https://openairdocs.org/sdr/VNAA202511250006.md): Intercostal · corroded · Sep 4, 2025 · N527EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CRACK 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-A0
- [SDR VNAA202511250005](https://openairdocs.org/sdr/VNAA202511250005.md): Web · cracked · Sep 4, 2025 · N527EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CRACK 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.
- [SDR VNAA202511250004](https://openairdocs.org/sdr/VNAA202511250004.md): Angle · corroded · Sep 3, 2025 · N527EA · Cndair CL6002C10 · Horizontal Stabilizer Miscellaneous Structure
  > CORROSION 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.
- [SDR VNAA202511250007](https://openairdocs.org/sdr/VNAA202511250007.md): Intercostal · corroded · Sep 2, 2025 · N527EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION 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 51-42-06-001-0
- [SDR VNAA2025052311101](https://openairdocs.org/sdr/VNAA2025052311101.md): Overheat Loop · faulted · May 19, 2025 · N527EA · Cndair CL6002C10 · Overheat Detection
  > L 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.
- [SDR VNAA2025051311101](https://openairdocs.org/sdr/VNAA2025051311101.md): Clamp · loose · May 12, 2025 · N527EA · Cndair CL6002C10 · Pneumatic System
  > L 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 DEFE
- [SDR VNAA2025050111102](https://openairdocs.org/sdr/VNAA2025050111102.md): Shutoff Valve · unserviceable · Apr 30, 2025 · N527EA · Cndair CL6002C10 · Pneumatic Distribution System
  > L 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.
- [SDR VNAA2025042911101](https://openairdocs.org/sdr/VNAA2025042911101.md): Overheat Loop · faulted · Apr 27, 2025 · N527EA · Cndair CL6002C10 · Overheat Detection
  > L 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.
- [SDR VNAA2025041511103](https://openairdocs.org/sdr/VNAA2025041511103.md): Bleed Valve · torn · Apr 14, 2025 · N527EA · Cndair CL6002C10 · Compressor Bleed Valve
  > L 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 DID
- [SDR VNAA202502120006](https://openairdocs.org/sdr/VNAA202502120006.md): Angle · cracked · Feb 12, 2025 · N527EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > WHILE 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. HN00217765
- [SDR VNAA202502120005](https://openairdocs.org/sdr/VNAA202502120005.md): Web · corroded · Feb 12, 2025 · N527EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > "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"
- [SDR VNAA202502120004](https://openairdocs.org/sdr/VNAA202502120004.md): Web · corroded · Feb 12, 2025 · N527EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > "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"
- [SDR VNAA202502120003](https://openairdocs.org/sdr/VNAA202502120003.md): Angle · corroded · Feb 12, 2025 · N527EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > J 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
- [SDR VNAA202502120002](https://openairdocs.org/sdr/VNAA202502120002.md): Floorbeam · corroded · Feb 12, 2025 · N527EA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > LH 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: CC670-34094-1
- [SDR VNAA202502120001](https://openairdocs.org/sdr/VNAA202502120001.md): Floorbeam · corroded · Feb 12, 2025 · N527EA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > "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: CC670-34094-2S
- [SDR VNAA202305091111](https://openairdocs.org/sdr/VNAA202305091111.md): Unknown · unknown · May 6, 2023 · N527EA · Cndair CL6002C10 · Passenger/Crew Doors
  > MAIN 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 52-11-00-710-801
- [SDR VNAA202303301111](https://openairdocs.org/sdr/VNAA202303301111.md): Unknown · unknown · Mar 29, 2023 · N527EA · Cndair CL6002C10 · Wing Structure
  > RH 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.
- [SDR VNAA202208119991](https://openairdocs.org/sdr/VNAA202208119991.md): Panel · corroded · Aug 8, 2022 · N527EA · Bombdr BD1001A10 · Fuselage Main, Structure
  > NDT FAILED HOLE ON R/H LOWER WING PLANK, I/B ROW, AFT FASTENER
- [SDR VNAA202204069991](https://openairdocs.org/sdr/VNAA202204069991.md): Skin · dented · Apr 6, 2022 · N527EA · Bombdr CL6002D15 · Fuselage Structure (General)
  > REPAIRED 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.
- [SDR V0XD20211228001](https://openairdocs.org/sdr/V0XD20211228001.md): Skin · dented · Dec 23, 2021 · N527EA · Cndair CL6002C10 · Fuselage Main, Structure
  > DENT 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 2
- [SDR VNAA202201029992](https://openairdocs.org/sdr/VNAA202201029992.md): Angle · corroded · Dec 21, 2021 · N527EA · Cndair CL6002C10 · Fuselage, Wing Attach Fittings
  > AFT 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.
- [SDR V0XD20211213003](https://openairdocs.org/sdr/V0XD20211213003.md): Angle · corroded · Dec 21, 2021 · N527EA · Cndair CL6002C10 · Wing, Fuselage Attach Fittings
  > AFT 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.

Next page: https://openairdocs.org/aircraft/N527EA/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 = 'N527EA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N527EA/reports

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