# Service difficulty reports: N530EA

A list on [N530EA](https://openairdocs.org/aircraft/N530EA.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 · 107 reports

- [SDR VNAA2026090724401](https://openairdocs.org/sdr/VNAA2026090724401.md): Window · arced · Sep 3, 2026 · N530EA · Cndair CL6002C10 · Flight Compartment Windows
  > R WINDOW ARCING IN FLIGHT FOLLOWED BY R WINDOW CAUTION C/A REMOVED RH SIDE WINDOW IAW AMM 56-12-01-000-801-A01-PSA. COMPLETED INSTALLATION OF WINDOW IAW AMM 56-12-01-400-801-A01-PSA UP TO
- [SDR VNAA2026081923103](https://openairdocs.org/sdr/VNAA2026081923103.md): Clamp · loose · Aug 17, 2026 · N530EA · Cndair CL6002C10 · Pneumatic System
  > LEFT BLEED DUCT WARNING MSG IN FLIGHT FOLLOWED BY L BLEED CAUTION MSG AND A CABIN ALT MSG AT 10K FT. HAZE IN CABIN. PERFORMED LEAK CHECK OF LT ECS IAW AMM 21-51-00-790-801. FOUND V-BAND CLAMP AT AFT OF LT DUAL HEAT EXCHANGER LOOSE. REINSTALLED CLAMP (FIGURE 40
- [SDR VNAA2026072821502](https://openairdocs.org/sdr/VNAA2026072821502.md): Aoa · faulted · Jul 27, 2026 · N530EA · Cndair CL6002C10 · Stall Warning System
  > FLAP FAIL IN FLIGHT QRH C/W SPEED TAPE STAYED AT 230 KTS WITH FLAPS INDICATING AT 0. REMOVED AND REPLACED RH AOA VANE IAW AMM 27-35-05-000/400-801-A01. OPS CHECKED GOOD IAW AMM 27-35-05-710-801-A01. PERFORMED MDC TEST OF SFECUS, BOTH PASSED.
- [SDR VNAA202607010016](https://openairdocs.org/sdr/VNAA202607010016.md): Hinge · excess play · May 22, 2026 · N530EA · Cndair CL6002C10 · Wing, Control Surface Attach Fittings
  > AFTER REMOVAL, FREE PLAY WAS FOUND ON HINGES OF STUB FAIRINGS 171DL AND 172DR. HINGES OF STUB FAIRINGS 171DL AND 172DR WERE REPLACED PER CRJ 700 SRM 51-42-21-001-001-A01.
- [SDR VNAA202607010015](https://openairdocs.org/sdr/VNAA202607010015.md): Lug · corroded · May 22, 2026 · N530EA · Cndair CL6002C10 · Wing, Control Surface Attach Fittings
  > CORROSION AND WEAR ON RH AILERON BORE LUGS OF HINGES: HINGE 1=[AIL STA=311.539] R1=[AIL STA=336.4015], R2=[AIL STA=337.657], R3=[AIL STA=338.424], R4=[AIL STA=342.123], R5=[AIL STA=342.911], R6=[AIL STA=344.1665], HINGE 4 UPPER AND LOWER=[AIL STA=364.016]. LU
- [SDR VNAA202607010013](https://openairdocs.org/sdr/VNAA202607010013.md): Fitting · corroded · May 20, 2026 · N530EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR FITTING IN FWD ACCESS 107 (1EA) ON GALLEY 1. NEW FLOOR FITTING P/N: CDSP2019-7C-620 IN FWD ACCESS 107 (1EA) ON GALLEY 1. WAS REPLACED IAW CMM 25-33-44
- [SDR VNAA202607010012](https://openairdocs.org/sdr/VNAA202607010012.md): Stand Off · corroded · May 16, 2026 · N530EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON THE ELECTRICAL WIRING HARNESS SUPPORT BTW S26L TO S25L AND BTW BS 265.00 TO 250. ELECTRICAL WIRING HARNESS SUPPORT BTW S26L TO S25L AND BTW BS 265 TO 250 WAS REPLACED IAW SRM 51-42-06-001-001-A01 AND SRM 51-41-02-001-001-A01.
- [SDR VNAA202607010011](https://openairdocs.org/sdr/VNAA202607010011.md): Hinge · excess play · May 16, 2026 · N530EA · Cndair CL6002C10 · Vertical Stabilizer
  > FREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NO. 2 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. FREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NO. 2 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WAS REPLACED PER RIL #
- [SDR VNAA202607010010](https://openairdocs.org/sdr/VNAA202607010010.md): Seat Track · corroded · May 16, 2026 · N530EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL RBL 9 (3EAS), LBL 9 (2EAS), RBL 26 (1EA) BTW FS 693 TO 1015. EVALUATED, SEAT RAIL RBL 9 (3EAS), LBL 9 (2EAS), RBL 26 (1EA) BTW FS 693 TO 1015 WERE OUT OF LIMITS DUE TO EXCESSIVE DAMAGE PER SRM 53-51-49-101-001-A01 AND REPLACED PER CRJ-7
- [SDR VNAA202607010009](https://openairdocs.org/sdr/VNAA202607010009.md): Frame · corroded · May 16, 2026 · N530EA · Cndair CL6002C10 · Fuselage Main, Frame
  > CORROSION ON FRAME AT FS 863 BTW STRG 26R TO 26L (BELOW FLOOR STRUCTURE). FRAME AT FS 863 BTW STRG 20R TO STRG 20L (BELOW FLOOR STRUCTURE) WAS REPLACED PER CRJ-700 SRM 51-42-06-001-001-A01
- [SDR VNAA202607010008](https://openairdocs.org/sdr/VNAA202607010008.md): Angle · cracked · May 16, 2026 · N530EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE AT LH COCKPIT BULKHEAD AFT FACE BTW FS 280.00. CRACK ON ANGLE AT LH COCKPIT BULKHEAD AFT FACE BTW FS 280.00 WAS REPLACED PER CRJ 700 SRM 51-42-06-001-001-A01
- [SDR VNAA202607010007](https://openairdocs.org/sdr/VNAA202607010007.md): Fitting · corroded · May 15, 2026 · N530EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORTS (4 EAS) LOCATED BTW FS280 TO FS295, LBL20, LBL38, RBL19, RBL37 AND (1 EA) BTW FS310 TO FS319 LBL 20 AT FUSELAGE FLOOR STRUCTURE. WERE EVALUATED, DUE TO EXCESSIVE DAMAGE ON FLOOR SUPPORTS (4 EAS) LOCATED BTW FS280 TO FS295, LBL20, L
- [SDR VNAA202607010006](https://openairdocs.org/sdr/VNAA202607010006.md): Strap · chafed · May 15, 2026 · N530EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CHAFING ON UPPER FRAME INNER STRAP AT STGR 3LH & FS349.00, FUSELAGE PASSENGER DOOR SURROUND STRUCTURE. UPPER FRAME INNER STRAP AT STGR 3LH & FS349.00, FUSELAGE PASSENGER DOOR SURROUND STRUCTURE WAS REPLACED PER SRM 51-42-21-001-001-A01.
- [SDR VNAA202607010005](https://openairdocs.org/sdr/VNAA202607010005.md): Seat Track · corroded · May 15, 2026 · N530EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > INITIAL INSPECTION: CORROSION ON LH SEAT RAIL LBL26 01 SEGMENT BTW FS364 TO FS485 AT PAX CABIN. EVALUATED, LH SEAT RAIL LBL26 01 SEGMENT BTW FS364 TO FS485 AT PAX CABIN. AT PASSENGER COMPARTMENT WAS OUT OF LIMITS TO EXCESSIVE DAMAGE PER CRJ-700 SRM 53-21-49-1
- [SDR VNAA202607010004](https://openairdocs.org/sdr/VNAA202607010004.md): Seat Track · corroded · May 15, 2026 · N530EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AND GOUGES ON LH/RH SIDE SEAT RAIL AT STGR 15 BTW FS 669 AND FS 977 AT PAX CABIN. LT & RT SIDE SEAT RAIL AT STGR 15 BTW FS 669 AND FS 977 AT PAX CABIN WERE EVALUATED OUT OF LIMITS TO EXCESSIVE DAMAGE PER SRM 53-41-49-101-001-A01, SRM 53-51-49-101-00
- [SDR VNAA202607010003](https://openairdocs.org/sdr/VNAA202607010003.md): Seat Track · corroded · May 15, 2026 · N530EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AND GOUGES ON LH SIDE SEAT RAIL AT STGR 15L 03 SEGMENTS: (01) BTW STA FS379 TO FS483, INITIAL INSPECTION: CORROSION AND GOUGES ON RH SIDE SEAT RAIL AT STGR 15R 03 SEGMENTS: BTW STA FS379 TO FS483, FS483 TO FS573, FS573 TO FS669 AT PASSENGER COMPART
- [SDR VNAA202607010002](https://openairdocs.org/sdr/VNAA202607010002.md): Seat Track · corroded · May 15, 2026 · N530EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AND GOUGES ON LH SIDE SEAT RAIL AT STGR 15L 03 SEGMENTS: (01) BTW STA FS379 TO FS483, (02) FS483 TO FS573, (03) FS573 TO FS669 AT PASSENGER COMPARTMENT. WERE EVALUATED, LH SIDE SEAT RAIL AT STGR 15L 03 SEGMENTS: (01) BTW STA FS379 TO FS483, (02) FS4
- [SDR VNAA202607010001](https://openairdocs.org/sdr/VNAA202607010001.md): Seat Track · corroded · May 15, 2026 · N530EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RT SEAT RAIL RBL9 03 SEGMENTS: (01) BTW FS350.00 TO FS485.00. (02) BTW FS485 TO FS581, (03) BTW FS581 TO FS677 AT PAX CABIN. WERE EVALUATED, RH SEAT RAIL RBL9 03 SEGMENTS: (01) BTW FS350.00 TO FS485.00. (02) BTW FS485 TO FS581, (03) BTW FS581 TO
- [SDR VNAA202606300015](https://openairdocs.org/sdr/VNAA202606300015.md): Seat Track · corroded · May 15, 2026 · N530EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH SEAT RAIL LBL 9, 03 SEGMENTS: (01) BTW FS375 TO FS485. (02) BTW FS485 TO FS581. (03) BTW FS581 TO FS677. AT PAX CABIN. EVALUATED, LH SEAT RAIL LBL 9, 03 SEGMENTS: (01) BTW FS375 TO FS485. (02) BTW FS485 TO FS581. (03) BTW FS581 TO FS677. AT PA
- [SDR VNAA202606300014](https://openairdocs.org/sdr/VNAA202606300014.md): Hinge Fitting · corroded · May 14, 2026 · N530EA · Cndair CL6002C10 · Aileron Control System
  > CORROSION AROUND OF THE BOLTS AND RUSTED BOLTS ON BONDING JUMPERS 1,2,3,4, LT AILERON HINGE FITTING. HINGE FITTING NBR 3 ON LH AILERON WAS CLEANED AROUND OF THE BOLTS OF BONDING JUMPER AND AFTER CLEAN DVI WAS PERFORMED AND NOT CORROSION WAS FOUND IAW SRM 51-2
- [SDR VNAA202607010014](https://openairdocs.org/sdr/VNAA202607010014.md): Lug · corroded · May 12, 2026 · N530EA · Cndair CL6002C10 · Wing, Control Surface Attach Fittings
  > CORROSION AND WEAR ON LH AILERON BORE LUGS OF HINGES 2 AND 3 (6EA) L1=[AIL STA=336.4015], L2=[AIL STA=337.657], L3=[AIL STA=338.424], L4=[AIL STA=342.123], L5=[AIL STA=342.911], L6=[AIL STA=344.1665]. L4=[AIL STA=342.123] WAS CLEANED PER SRM 51-26-00-001-001-A
- [SDR VNA2026F00008](https://openairdocs.org/sdr/VNA2026F00008.md): Striker · worn · May 12, 2026 · N530EA · Cndair CL6002C10 · Cargo/Baggage Doors
  > WEAR ON FORWARD BAGGAGE BAY DOOR SURROUND AT FS=533.00 AND SGTR=23L TO SGTR=22LER, SRM 53-11-43-201-001-A01. FORWARD BAGGAGE BAY DOOR SURROUND (STRIKER SEAL) AT FS=533.00 AND SGTR=23L TO SGTR=22L WAS BLENDED OUT AND WAS EVALUATED, DAMAGE IS 80% OF ORIGINAL TH
- [SDR VNAA202606300012](https://openairdocs.org/sdr/VNAA202606300012.md): Web · cracked · May 12, 2026 · N530EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CRACK ON LH ELECTRICAL BAY WEB FLOOR FS 193.00 (BELOW ACCUMULATOR GAUGE INDICATOR) AT FWD EQUIPMENT COMPARTMENT. CRACK ON LH ELECTRICAL BAY WEB FLOOR FS 193.00 (BELOW ACCUMULATOR GAUGE INDICATOR) AT FWD EQUIPMENT COMPARTMENT WAS REPAIRED PER CRJ 700 SRM 53-1
- [SDR VNAA202606300011](https://openairdocs.org/sdr/VNAA202606300011.md): Access Panel · corroded · May 12, 2026 · N530EA · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > CORROSION AT SETTLEMENT AREA OF ACCESS PANEL 542BZ,542AZ AND 642AZ. CORROSION AT SETTLEMENT AREA OF ACCESS PANEL 542AZ WAS REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01 AND WAS FOUND WITHIN OF LIMITS PER SRM 53-00-00-101-001-A01. ACCESS PANELS 542BZ AND 642AZ
- [SDR VNAA202606300010](https://openairdocs.org/sdr/VNAA202606300010.md): Skin · corroded · May 12, 2026 · N530EA · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > CORROSION ON SETTLEMENT AREA OF E/E COMPARTMENT DOOR AT EXTERNAL SURROUND. SETTLEMENT AREA OF E/E COMPARTMENT DOOR AT EXTERNAL SURROUND WAS REPAIRED PER REO 670-53-21-242 REV. -C
- [SDR VNAA202606300009](https://openairdocs.org/sdr/VNAA202606300009.md): Diaphragm · cracked · May 12, 2026 · N530EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CRACK ON RH DIAPHRAGM OF MAIN WHEEL WELL BIN SUPPORT FS 797.00 AND RBL34 AT RH MAIN WHEEL WELL AREA. CRACK ON RH DIAPHRAGM OF MAIN WHEEL WELL BIN SUPPORT FS 797.00 AND RBL34 AT RH MAIN WHEEL WELL AREA WAS REPLACED PER SRM 51-41-02-001-001-A01.
- [SDR VNAA202606300008](https://openairdocs.org/sdr/VNAA202606300008.md): Support · cracked · May 12, 2026 · N530EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CRACK ON ATTACHMENT ANGLE OF DIAPHRAGM AT SUPPORT OF AFT WING TO FUSELAGE FAIRING LT SIDE, FS909. THE ATTACH ANGLE OF DIAPHRAGM AT SUPPORT OF AFT WING TO FUSELAGE FAIRING LT SIDE, WAS REPAIRED IAW REO 670-53-82-478, REV -A.
- [SDR VNAA202606300007](https://openairdocs.org/sdr/VNAA202606300007.md): Attach Angle · cracked · May 12, 2026 · N530EA · Cndair CL6002C10 · Passenger/Crew Doors
  > CRACK ON ATTACHMENT ANGLE INNER SKIN-TO-AFT SIDE PANEL NEAR TO PULLEY SUPPORT AT PASSENGER DOOR EXTERNAL STRUCTURE. ATTACHMENT ANGLE INNER SKIN-TO-AFT SIDE PANEL NEAR TO PULLEY SUPPORT AT PASSENGER DOOR EXTERNAL STRUCTURE WAS REPAIRED PER CRJ-700 SRM 52-11-04
- [SDR VNAA202606300006](https://openairdocs.org/sdr/VNAA202606300006.md): Latch · worn · May 11, 2026 · N530EA · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > WEAR ON LATCH REIFORCING OF ACCESS DOOR 444BB AT RT ENGINE. LATCH REIFORCING OF ACCESS DOOR 444BB AT RH ENGINE WAS REPLACED PER CRJ-700 SRM 51-42-06-001-001-A01.
- [SDR VNAA202606300005](https://openairdocs.org/sdr/VNAA202606300005.md): Angle · cracked · May 10, 2026 · N530EA · Cndair CL6002C10 · Wing Miscellaneous Structure
  > IN REF TO JOB CARD 600-13E1-JIC DURING INSPECTION: CRACK ON ANGLE OF MID INTERCOSTAL OF SETTLEMENT AREA OF ACCESS PANEL 642AZ AT RH MLG WHEEL WELL. ANGLE OF MID INTERCOSTAL OF SETTLEMENT AREA OF ACCESS PANEL 642AZ AT RH MLG WHEEL WELL. WAS REPLACED PER CRJ700
- [SDR VNAA202606300004](https://openairdocs.org/sdr/VNAA202606300004.md): Angle · cracked · May 10, 2026 · N530EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > IN REF TO JOB CARD 500-13E1-JIC DURING INSPECTION: CRACK ON ANGLE OF MID INTERCOSTAL OF SETTLEMENT AREA OF ACCESS PANEL 542AZ AT LH MLG WHEEL WELL. ANGLE OF MID INTERCOSTAL OF SETTLEMENT AREA OF ACCESS PANEL 542AZ AT LT MLG WHEEL WELL. WAS REPLACED IAW SRM 51
- [SDR VNAA202606300003](https://openairdocs.org/sdr/VNAA202606300003.md): Shield · chafed · May 10, 2026 · N530EA · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > RIGHT CORE COWL FIRE SHIELD CHAFE WITHIN 5335.13 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IAW APPROVED PROCEDURES OR REPLACE PART. ENGINEERING COMMENTS: EVALUATE SRM 54-23-00-201-005-A01 FOR A PERMANENT REPAIR IF OUT OF LI
- [SDR VNAA202606300002](https://openairdocs.org/sdr/VNAA202606300002.md): Skin · damaged · May 10, 2026 · N530EA · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > FUSELAGE LIGHTNING STRIKE DAMAGE. DAMAGE AROUND FASTENER CSK BY NEXT HEAVY MAINTENANCE VISIT (HMV), PERFORM PERMANENT REPAIR PER SRM 53-00-00-201-003-A03 SECTION 5.C.(4) - PERMANENT DISPOSITION TO FUSELAGE SKIN AROUND THE FASTENER COUNTERSINK FOR DAMAGE DEPTH
- [SDR VNAA202606300001](https://openairdocs.org/sdr/VNAA202606300001.md): Skin · dented · May 9, 2026 · N530EA · Cndair CL6002C10 · Leading Edge Devices
  > THREE DENTS ON UPPER SKIN OF SLAT NR 3 AT LT WING BTW SS 407-425. THE DENTS ON UPPER SKIN OF SLAT NR 3 AT LT WING BTW SS 407- 425 WERE REPAIRED IAW REO 670-57-42-2510.
- [SDR VNAA20250625007](https://openairdocs.org/sdr/VNAA20250625007.md): Transcowl · temp repair · Jun 24, 2025 · N530EA · Cndair CL6002C10 · Engine Thrust Reverser
  > EA 54-2025-0682 (140FH PERM REPAIR - SPEED TAPE APPLIED - RH ENGINE TRANS COWL ACCES PANEL FWD LATCH OPENS IN FLIGHT) WITHIN 140 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PA
- [SDR VNAA20250625006](https://openairdocs.org/sdr/VNAA20250625006.md): Pulley Bracket · chafed · Jun 24, 2025 · N530EA · Cndair CL6002C10 · Fuselage Main, Structure
  > HN00246730 DISCREPANCY: FOUND RH SIDE FS280 AILERON PULLEY BRACKET TO BE CHAFED AND REQUIRE REPLACEMENT. CORRECTIVE ACTION: LOCATED AND DRILLED NEW BRACKET P/N CC670-94802-7-01, AND TRANSFERRED BRACKET FROM OLD PULLEY IAW CRJ-700-SRM-51-40-11-001-001-A01 AND 5
- [SDR VNAA2050625005](https://openairdocs.org/sdr/VNAA2050625005.md): Bulkhead Web · corroded · Jun 24, 2025 · N530EA · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > FOUND CORROSION ON FS 280 R/H LOWER WEB. UPON FURTHER INVESTIGATION FOUND CORROSION ON FS 280 R/H LOWER WEB FOUND TO BE OUT OF LIMITS IAW CRJ 700 SRM 53-11-10-201-003-A01. FABRICATED, LOCATED AND DRILLED FS 280 RH LOWER WEB AND BUTTSTRAP FROM MATERIAL 7075-T6
- [SDR VNAA20250625004](https://openairdocs.org/sdr/VNAA20250625004.md): Bulkhead Web · corroded · Jun 24, 2025 · N530EA · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > FOUND CORROSION ON FS 280 L/H LOWER WEB. UPON FURTHER INVESTIGATION FOUND CORROSION ON FS 280 L/H LOWER WEB FOUND TO BE OUT OF LIMITS IAW CRJ 700 SRM 53-11-10-201-003-A01. FABRICATED, LOCATED AND DRILLED FS 280 LH LOWER WEB AND BUTTSTRAP FROM MATERIAL 7075-T
- [SDR VNAA20250625003](https://openairdocs.org/sdr/VNAA20250625003.md): Floorbeam · corroded · Jun 24, 2025 · N530EA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FOUND CORROSION ON FS 280 "J" ANGLE. UPON FURTHER INVESTIGATION ON FS 280 "J" ANGLE FOUND TO BE OUT OF LIMITS IAW CRJ 700 SRM 53-00-00-101-001-A01. LOCATED AND DRILLED NEW J ANGLE P/N CC670-34095-1SB IAW CRJ-700-SRM-51-40-11-001-001-A01. INSTALLED FS 280 NEW
- [SDR VNAA20250625002](https://openairdocs.org/sdr/VNAA20250625002.md): Floorbeam · corroded · Jun 24, 2025 · N530EA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FOUND CORROSION ON FS 280 R/H CROSS BEAM. UPON REMOVAL OF R/H CROSS BEAM FOUND R/H CORROSION CAP ANGLE DAMAGE REQUIRES REPLACEMENT. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE RH CORROSION CAP ANGLE P/N CC670-34096-2 IAW CRJ 700 SRM 51-42-06-001-001- A01.
- [SDR VNAA20250625001](https://openairdocs.org/sdr/VNAA20250625001.md): Floorbeam · corroded · Jun 24, 2025 · N530EA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FOUND CORROSION @ L/H F.S.280 BEAM. INSTALLED NEW FS 280 LH CROSSBEAM P/N CC670-34094-2 AND INSTALLED NEW LH CORROSION CAP ANGLE PN CC670-34096-1 IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01 & 51-42-22-001-001-A01.
- [SDR VNAA2025041511104](https://openairdocs.org/sdr/VNAA2025041511104.md): Terminal Block · smoke · Apr 14, 2025 · N530EA · Cndair CL6002C10 · Window System Wiring
  > CA FRONT WINDSHIELD LOWER TERMINAL BLOCK SMOKING ON FINAL. TURNED OFF WINDSHIELD HEAT SMOKE WENT AWAY. NO MEDICAL ATTENTION WAS REPORTED. / REMOVED AND REPLACED WINDSHIELD IAW CRJ700 AMM 56-11-01-000/400-801-A01-PSA. OPS CHECK GOOD. LEAK CHECK GOOD.
- [SDR VNAA2024121011101](https://openairdocs.org/sdr/VNAA2024121011101.md): Selector Valve · unserviceable · Dec 9, 2024 · N530EA · Cndair CL6002C10 · Landing Gear Steering System
  > STEERING INOP CAUTION MSG ON T/O / REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE IAW CRJ700 AMM 32-32-10-000/400-801. OPS CHECK GOOD. NO STEERING CAUTION MSG AT ANY POINT.
- [SDR VNAA2024060511103](https://openairdocs.org/sdr/VNAA2024060511103.md): Unknown · odor · Jun 3, 2024 · N530EA · Cndair CL6002C10 · Air Distribution System
  > ELECTRICAL BURNING SMELL/ODOR REQUIRES FTS. / PERFORMED T/S IAW CRJ700 FIM 21-21-00-810-806-A01 / FIM 21-22-00-810-806-A01 TRIED TO DUPLICATE FAULT AND IDENTIFY THE SOURCE OF THE SMELL BY CHECKING THE CABIN THROUGHLY WITH APU RUNNING, LH/RH ENGINE RUNNING ON I
- [SDR VNAA2024060511102](https://openairdocs.org/sdr/VNAA2024060511102.md): Unknown · odor · Jun 3, 2024 · N530EA · Cndair CL6002C10 · Air Distribution System
  > FUME SMELL IN THE CABIN / INSPECTED CABIN FOR FUMES/SMELL WITH SAME CONFIG AS REPORTED, COULD NOT DUPLICATE FAULT IAW CRJ700 FIM 21-22-00-810-806-A01.
- [SDR VNAA2024041411102](https://openairdocs.org/sdr/VNAA2024041411102.md): Unknown · odor · Apr 11, 2024 · N530EA · Cndair CL6002C10 · Air Distribution System
  > FA REPORTS BURNING SMELL IN FIRST CLASS, BOTH PACKS ON, DURING PREFLIGHT / TROUBLESHOT ABNORMAL SMELL IAW CRJ700 FIM 21-22-00-810-806 CAUSE 12. FOUND CHECKS TO BE NORMAL AND NO ABNORMAL SMELLS OR FUMES. SUSPECT BURNING COFFEE IN COFFEE MAKER TO BE ROOT CAUSE.
- [SDR VNAA2024040911101](https://openairdocs.org/sdr/VNAA2024040911101.md): Warning Message · false indication · Apr 7, 2024 · N530EA · Cndair CL6002C10 · Landing Gear Steering System
  > STEERING INOP CAUTION MSG ON ROTATION. / PERFORMED OPS CHECK OF THE NOSE WHEEL STEERING IAW CRJ700 AMM 32-51-00-710-801-A01. OPS CHECK GOOD AT THIS TIME.
- [SDR VNAA202304211112](https://openairdocs.org/sdr/VNAA202304211112.md): Fuse · unserviceable · Apr 19, 2023 · N530EA · Cndair CL6002C10 · Landing Gear Brake System
  > IB GND SPLRS, HYD 3 LO PRESS, IB BRAKE PRESS. LOST HYD SYSTEM 3 UPON LANDING. REMOVED AND REPLACED RH SYSTEM 3 VOLUMETRIC FUSE IAW CRJ700 AMM 32-43-21-000/400-801-A01. LEAK CHECK GOOD. HYD 3 SYSTEM SERVICED IAW CRJ700 AMM 12-12-29-611-801-A01
- [SDR VNAA202301251111](https://openairdocs.org/sdr/VNAA202301251111.md): Skin · damaged · Jan 25, 2023 · N530EA · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > GOUGE & DENT DAMAGE TO FUSELAGE SKIN BTW FS1015.00 - FS1051.30 AND STR21R - STR26R. PERMANENT REPAIR WAS PERFORMED IAW EA 22-C7-53-0942.
- [SDR VNAA202204199994](https://openairdocs.org/sdr/VNAA202204199994.md): Stub Frame · corroded · Apr 19, 2022 · N530EA · Cndair CL6002C10 · Fuselage Main, Structure
  > DESCRIPTION OF DAMAGE: FWD BAGGAGE BAY DOOR FWD LOWER STUB FRAME AT F.S. 549 IS CORRODED.

Next page: https://openairdocs.org/aircraft/N530EA/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 = 'N530EA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N530EA/reports

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