# Service difficulty reports: N544EA

A list on [N544EA](https://openairdocs.org/aircraft/N544EA.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 2 · 90 reports

- [SDR VNAA202608210033](https://openairdocs.org/sdr/VNAA202608210033.md): Angle · corroded · Jul 12, 2026 · N544EA · Cndair CL6002C10 · Passenger/Crew Doors
  > AFT INNER SKIN WAS REMOVED, CORROSION ON INTERNAL ANGLE WAS FOUND AT PASSENGER DOOR. INTERNAL ANGLE OF PASSENGER DOOR WAS REPLACED IAW SRM 51-42-06-001-001-A01.
- [SDR VNAA202608210032](https://openairdocs.org/sdr/VNAA202608210032.md): Fitting · corroded · Jul 8, 2026 · N544EA · Cndair CL6002C10 · Fuselage, Equipment Attach Fittings
  > CORROSION FLOOR FITTING IN AFT ACCESS 108 OUT SIDE (1EA) ON GALLEY 1. FLOOR FITTING IN AFT ACCESS 108 OUT SIDE (1EA) ON GALLEY 1 WAS REPLACED IAW CMM 25-33-44, REV. 3.
- [SDR VNAA202608210031](https://openairdocs.org/sdr/VNAA202608210031.md): Lug · corroded · Jul 8, 2026 · N544EA · Cndair CL6002C10 · Ailerons
  > SECONDARY NRC AFTER LH AILERON BUSHINGS REMOVAL CORROSION FOUND ON FITTING #1, CENTER FITTING L2, L3, L5 AND FITTING #4 UPPER AND LOWER AT LH AILERON. FITTING #4 UPPER AND LOWER LUGS AT LH AILERON WERE CLEANED PER CRJ 700 SRM 51-26-00-001-001-A01 THEN INSPE
- [SDR VNAA202608210030](https://openairdocs.org/sdr/VNAA202608210030.md): Lug · corroded · Jul 8, 2026 · N544EA · Cndair CL6002C10 · Ailerons
  > AFTER RT AILERON BUSHINGS REMOVAL, CORROSION FOUND ON RT AILERON FITTING 1, LUG R2 & R5 ALSO ON FITTING 4 UPPER AND LOWER LUGS. UPPER & LOWER LUGS ON FITTNG 4 & HINGE FITTING 1 AT RT AILERON WERE CLEANED IAW SRM 51-26-00-001-001-A01, THEN INSPECTED IAW NDT MA
- [SDR VNAA202608210029](https://openairdocs.org/sdr/VNAA202608210029.md): Canister · cracked · Jul 5, 2026 · N544EA · Cndair CL6002C10 · Wing Main, Frame Structure
  > CRACK ON CANISTER WELDED NO. 3 ON STA WS 148.00 OF INTERNAL RH MAIN FUEL TANK. CANISTER, WELDED NO.3 IN STA. WS148 AT RH MAIN FUEL TANK. WAS REPAIR PER REO 670-57-42-577 REV. --.
- [SDR VNAA202608210028](https://openairdocs.org/sdr/VNAA202608210028.md): Canister · cracked · Jul 5, 2026 · N544EA · Cndair CL6002C10 · Wing Main, Frame Structure
  > CRACK ON CANISTER WELDED NO. 3 ON STA WS 148.00 OF INTERNAL LH MAIN FUEL TANK. CANISTER, WELDED NR 3 IN STA. WS148 AT RH MAIN FUEL TANK. WAS REPAIR PER REO 670-57-42-577 REV. --.
- [SDR VNAA202608210027](https://openairdocs.org/sdr/VNAA202608210027.md): Hinge Fitting · excess play · Jul 5, 2026 · N544EA · Cndair CL6002C10 · Rudder Structure
  > FREEPLAY ON BEARING OF RUDDER HINGE FITTING #3 AT REAR SPAR OF VERTICAL STABILIZER. BEARING OF RUDDER HINGE FITTING #3 AT REAR SPAR OF VERTICAL STABILIZER WAS REPLACED PER RIL #2103. REV. B. AND RIL #1213. 03)
- [SDR VNAA202608210026](https://openairdocs.org/sdr/VNAA202608210026.md): Seat Track · corroded · Jul 5, 2026 · N544EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL RBL9 (02 SEGMENTS), (SEG 1) BTW FS 677.00 TO FS 863.00, (SEG 2) BTW FS 863.00 TO FS 977.00 AT PASSENGER CABIN. CORROSION ON SEAT RAIL RBL9 (02 SEGMENTS), (SEG 1) BTW FS 677.00 TO FS 863.00, (SEG 2) BTW FS 863.00 TO FS 977.00 AT PASSENG
- [SDR VNAA202608210025](https://openairdocs.org/sdr/VNAA202608210025.md): Seat Track · corroded · Jul 5, 2026 · N544EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL LBL9 (02 SEGMENTS), (SEG 1) BTW FS 677.00 TO FS 863.00, (SEG 2) BTW FS 863.00 TO FS 989.00 AT PASSENGER CABIN. CORROSION ON SEAT RAIL LBL9 (02 SEGMENTS), (SEG 1) BTW FS 677.00 TO FS 863.00, (SEG 2) BTW FS 863.00 TO FS 989.00 AT PASSENGE
- [SDR VNAA202608210016](https://openairdocs.org/sdr/VNAA202608210016.md): Seat Track · corroded · Jul 5, 2026 · N544EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAILS LBL9 BTW FS 477.40 - FS 677.00 (3EA) AT PASSENGER CABIN. CORROSION ON SEAT RAILS LBL9 BTW FS 477.40 - FS 677.00 (3EA) AT PASSENGER CABIN WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01, EVALUATED OUT LIMITS PER CRJ 900 53-31-49-101-00
- [SDR VNAA202608210015](https://openairdocs.org/sdr/VNAA202608210015.md): Seat Track · corroded · Jul 5, 2026 · N544EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAILS RBL9 BTW FS 477.40.00 TO FS 693.00 (SEVERAL LOCATIONS). CORROSION ON SEAT RAILS RBL9 BTW FS 477.40.00 TO FS 693.00 WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01, EVALUATED OUT LIMITS PER CRJ 900 53-31-49-101-001-A02 AND REPLACED PE
- [SDR VNAA202608210014](https://openairdocs.org/sdr/VNAA202608210014.md): Seat Track · corroded · Jul 5, 2026 · N544EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAILS RBL9 BTW FS 349.00 - FS 477.40 AT PASSENGER CABIN. SEAT RAILS RBL9 BTW FS 349.00 - FS 477.40 AT PASSENGER CABIN WERE REPLACED PER CRJ-900 AMM 53-00-49
- [SDR VNAA202608210024](https://openairdocs.org/sdr/VNAA202608210024.md): Angle · corroded · Jul 4, 2026 · N544EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON MID CAP ANGLE AND KICK PLATE BTW FS 310.00 TO FS 349.00 AT PASSENGER DOOR FUSELAGE FRAME. CORROSION ON KICK PLATE BTW FS 310.00 TO FS 349.00 AT PASSENGER DOOR FUSELAGE FRAME WAS REMOVED AND EVALUATED WITHIN OF LIMITS PER CRJ-700 SRM 51-21-06-001
- [SDR VNAA202608210022](https://openairdocs.org/sdr/VNAA202608210022.md): Seat Track · corroded · Jul 4, 2026 · N544EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL LBL9 (02 SEGMENTS), (SEG 1) BTW FS 485.00 TO FS 581.00, (SEG 2) BTW FS 581.00 TO FS 677.00 AT PASSENGER CABIN. CORROSION ON SEAT RAIL LBL9 (02 SEGMENTS), (SEG 1) BTW FS 485.00 TO FS 581.00, (SEG 2) BTW FS 581.00 TO FS 677.00 AT PASSENG
- [SDR VNAA202608210012](https://openairdocs.org/sdr/VNAA202608210012.md): Web · cracked · Jul 4, 2026 · N544EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CRACK ON PREVIOUS REPAIR OF ADG COMPARTMENT UPPER WEB, BELOW SETTLEMENT ADG RETRACTION PUMP AREA. ADG COMPARTMENT UPPER WEB, BELOW SETTLEMENT ADG RETRACTION PUMP AREA WAS REPAIRED PER CRJ-700 SRM 53-11-43-201-001-A01
- [SDR VNAA202608210023](https://openairdocs.org/sdr/VNAA202608210023.md): Seat Track · corroded · Jul 3, 2026 · N544EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL RBL9 (03 SEGMENTS), (SEG 1) BTW FS 349.00 TO FS 485.00, (SEG 2) BTW FS 485.00 TO FS 581.00, (SEG 3) BTW FS 581.00 TO FS 677.00 AT PASSENGER CABIN. CORROSION ON SEAT RAIL RBL9 (03 SEGMENTS), (SEG 1) BTW FS 349.00 TO FS 485.00, (SEG 2) B
- [SDR VNAA202608210021](https://openairdocs.org/sdr/VNAA202608210021.md): Seat Track · corroded · Jul 3, 2026 · N544EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAILS (L/H AND R/H) (4 EAS) LOCATED APPROXIMATELY AT FS 785.15 TO 938.00 ON PAX CABIN. CORROSION ON SIDE SEAT RAILS (L/H AND R/H) (4 EAS) LOCATED APPROXIMATELY AT FS 785.15 TO 938.00 ON PAX CABIN WERE EVALUATED DUE TO EXCESSIVE DAMAGE P
- [SDR VNAA202608210020](https://openairdocs.org/sdr/VNAA202608210020.md): Seat Track · corroded · Jul 3, 2026 · N544EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAILS L/H (5 EAS) LOCATED APPROXIMATELY AT FS 379.00 TO 761.85 ON PAX CABIN. CORROSION ON SIDE SEAT RAILS L/H (5 EAS) LOCATED APPROXIMATELY AT FS 379.00 TO 761.85 ON PAX CABIN WAS REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01, WERE EVA
- [SDR VNAA202608210019](https://openairdocs.org/sdr/VNAA202608210019.md): Seat Track · corroded · Jul 3, 2026 · N544EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAILS R/H (5 EAS) LOCATED APPROXIMATELY AT FS 485.00 TO 761.85 ON PAX CABIN. CORROSION ON SIDE SEAT RAILS R/H (5 EAS) LOCATED APPROXIMATELY AT FS 485.00 TO 761.85 ON PAX CABIN WAS REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01, WERE EVAL
- [SDR VNAA202608210018](https://openairdocs.org/sdr/VNAA202608210018.md): Fitting · corroded · Jul 3, 2026 · N544EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION OF FITTING SUPPORT (2 EA) AT FWD GALLEY. CORROSION OF FITTING SUPPORT (2 EA) AT FWD GALEY WAS EVALUATED OUT LIMITS PER CRJ 700 SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ700 SRM 51-42-21-001-001-A01.
- [SDR VNAA202608210017](https://openairdocs.org/sdr/VNAA202608210017.md): Access Panel · corroded · Jul 3, 2026 · N544EA · Cndair CL6002C10 · Wing, Plate/Skin
  > CORROSION ON CONTERSINKS OF ACCESS PANEL 542AT,642 AT ACCESS PANEL 642AT MUST BE REPLACED IAW TICKET #86402, AND ACCESS PANEL 542AT WAS REPAIRED PER REO 670-57-21-1146 REV. -A
- [SDR VNAA202608210010](https://openairdocs.org/sdr/VNAA202608210010.md): Bracket · cracked · Jul 3, 2026 · N544EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CRACKS ON SUPPORT BASE MAIN BATTERY DIRECT BUS (JB6) AT FWD EQUIPMENT COMPARTMENT. CRACKED SUPPORT BASE MAIN BATTERY DIRECT BUS (JB6) AT FWD EQUIPMENT COMPARTMENT WAS REPLACED PER CRJ-700 SRM 51-42-06-001-001-A01
- [SDR VNAA202608210013](https://openairdocs.org/sdr/VNAA202608210013.md): Bracket · corroded · Jul 2, 2026 · N544EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION BRACKETS MACHINE (5 EA) OF (LBL 2.6), (LBL 24), BTW FS 517-597, AT FWD SURROUND STRUCTURE CARGO COMPARMENT. PAINT ON BRACKETS MACHINE (2 EAS) WAS REMOVED AND NO DAMAGE WAS FOUND. FINISH PAINT WAS RESTORED PER CRJ700 SRM 51-26-01-001-001-A01 AND SRM
- [SDR VNAA202608210011](https://openairdocs.org/sdr/VNAA202608210011.md): Web · cracked · Jul 2, 2026 · N544EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CRACK ON WEB BTW FS195 TO FS205 AND WL79.50 (LH SIDE) ON INTERNAL STRUCTURE AT FWD EQUIPMENT COMPARTMENT. WEB BTW FS195 TO FS205 AND WL79.50 (LH SIDE) ON INTERNAL STRUCTURE AT FWD EQUIPMENT COMPARTMENT WAS REPAIRED PER CRJ 700 SRM 53-11-43-201-001-A01
- [SDR VNAA202608210009](https://openairdocs.org/sdr/VNAA202608210009.md): Floorbeam · cracked · Jul 2, 2026 · N544EA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > CRACK ON CROSSBEAM FITTING BTW FS W280 LBL 12 (BELOW FLOOR) AT PASSENGER CABIN. FLOORBEAM BTW FS W280 LBL 12 AT PASSENGER CABIN WAS REPAIRED PER CRJ-700 SRM 53-11-43-201-003-A01
- [SDR VNAA202608210008](https://openairdocs.org/sdr/VNAA202608210008.md): Drag Angle · cracked · Jul 2, 2026 · N544EA · Cndair CL6002C10 · Fuselage, Stabilizer Attach Fittings
  > CRACK ON FWD DRAG ANGLE APPROX 43.75% MID SPAR DATUM AT VERTICAL STABILIZER (RH SIDE). FWD DRAG ANGLE APPROX 43.75% MID SPAR DATUM AT VERTICAL STABILIZER (RH SIDE) WAS REPAIRED PER CRJ 700 SRM 55-31-00-201-001-A01
- [SDR VNAA202608210005](https://openairdocs.org/sdr/VNAA202608210005.md): Skin · cracked · Jul 2, 2026 · N544EA · Cndair CL6002C10 · Leading Edge Devices
  > IAW TRFKE00F6TG7: 2800FH PERM REPAIR - TEMPORARY DISPOSITION FOR REWORKED DENT TO LHS SLAT#1 OUTER SKIN AND LOWER ANGLE AT WS58.75. ENGINEERING COMMENTS: ANGLE PN CC670-12648-1 MUST BE REPLACED. TRFKE00F6TG7 DISPLAYED THAT THE ENTIRE SLAT PN CC670-12600-3 IS
- [SDR VNAA202608210007](https://openairdocs.org/sdr/VNAA202608210007.md): Stiffener · corroded · Jun 28, 2026 · N544EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON STIFFENER 1EA, CLIP 1EA ALSO INTERNAL SKIN LP GROUND CONNECTION ACCESS SERVICING DOOR 182BR. CORROSION CLIP 1EA ALSO INTERNAL SKIN LP GROUND CONNECTION ACCESS SERVICING DOOR 182BR. WAS REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01 AND WAS EVALUATE
- [SDR VNAA202608210006](https://openairdocs.org/sdr/VNAA202608210006.md): Drag Angle · cracked · Jun 28, 2026 · N544EA · Cndair CL6002C10 · Fuselage, Stabilizer Attach Fittings
  > CRACK ON AFT DRAG ANGLE APPROX 43.75% MID SPAR DATUM AT VERTICAL STABILIZER (RH SIDE). AFT DRAG ANGLE APPROX 43.75% MID SPAR DATUM AT VERTICAL STABILIZER (RH SIDE).WAS REPAIRED PER CRJ700 SRM 55-31-00-201-001-A01
- [SDR VNAA202608210004](https://openairdocs.org/sdr/VNAA202608210004.md): Drag Angle · cracked · Jun 28, 2026 · N544EA · Cndair CL6002C10 · Fuselage, Stabilizer Attach Fittings
  > CRACK ON AFT DRAG ANGLE APPROX 43.75% MID SPAR DATUM AT VERTICAL STABILIZER (LH SIDE). CRACK ON AFT DRAG ANGLE APPROX 43.75% MID SPAR DATUM AT VERTICAL STABILIZER (LH SIDE) WAS REPAIRED PER CRJ-700 SRM 55-31-00-201-001-A01. PAX DOOR HINGE PN 601R318073-5 WAS
- [SDR VNAA202608210003](https://openairdocs.org/sdr/VNAA202608210003.md): Hinge · worn · Jun 28, 2026 · N544EA · Cndair CL6002C10 · Fuselage, Door Hinge
  > IN REF TO TRFKE00EQGY2: PERM REPAIR - PASSENGER DOOR HINGE REPLACEMENT REPLACE THE PASSENGER DOOR HINGE IN ACCORDANCE WITH CRJ700 SRM TASK 52-11-01-201-002-A01. AFTER HINGE REPLACEMENT. SEND E-MAIL REQUEST TO DL_PSA_MAINTENANCE_PROGRAMS@PSAAIRLINES.COM TO COMP
- [SDR VNAA202608210002](https://openairdocs.org/sdr/VNAA202608210002.md): Skin · gouged · Jun 28, 2026 · N544EA · Cndair CL6002C10 · Passenger/Crew Doors
  > GOUGE - LH PAX DOOR CUTOUT AT FS 349 WITHIN 5371.31 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. DISPOSITION FOR REWORKED GOUGE DAMAGE TO FUSELAGE SKIN AT FS349.00 BTW S
- [SDR VNAA202608210001](https://openairdocs.org/sdr/VNAA202608210001.md): Hinge Fitting · corroded · Jun 28, 2026 · N544EA · Cndair CL6002C10 · Spoilers
  > IN REF TO TRFKE00A2A3A: PERM REPAIR - BLENDED GOUGE DAMAGE TO R/H OUTB'D HINGE FITTING GROUND SPOILER STA 21.8 REPAIR OR REPLACE PART IN ACCORDANCE WITH APPROVED PROCEDURES WITHIN 8000 FH. ENGINEERING COMMENTS: HINGE FITTING MUST BE REPLACED PN CC670-16052-4.
- [SDR VNAA202509060001](https://openairdocs.org/sdr/VNAA202509060001.md): Attach Fitting · worn · Aug 28, 2025 · N544EA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FOLDING STEP (CONTROL ROD ATTACH L-BRACKET IS LOOSE AND SLOT FOR CONTROL ROD IS BINDING FROM ELONGATED JAGGED HOLE). REMOVED AND REPLACED BRACKET IAW SRM 51-40-11-001-001-A01 AND MHIRJ CMM 52-11-00.
- [SDR VNAA2024062011101](https://openairdocs.org/sdr/VNAA2024062011101.md): Control Handle · failed · Jun 19, 2024 · N544EA · Cndair CL6002C10 · Landing Gear Selector
  > RED GEAR DISAGREE MSG AFTER TAKE OFF / FOUND LG SELECTOR PANEL DIRTY WITH TYPICAL FUZZY CONTAMINATION, REMOVED AS REQUIRED, NO OTHER DISCREPANCIES NOTED. REPLACED LG LEVER IAW CRJ 700 AMM 32-31-01-000/400-802. ALL OPS CHECKS GOOD AT THIS TIME, NO FAULTS NOTED,
- [SDR VNAA202302180003](https://openairdocs.org/sdr/VNAA202302180003.md): None · dented · Feb 18, 2023 · N544EA · Cndair CL6002C10 · Wing, Control Surfaces
  > EA22-C7-57-1405 (PERM REPAIR BEFORE 27,133.27 FH - LH IB FLAP) WITHIN 800FLIGHT HOURS (27,133.27FH), REPAIR OR REPLACE OF THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES.
- [SDR VNAA202302180002](https://openairdocs.org/sdr/VNAA202302180002.md): None · corroded · Feb 18, 2023 · N544EA · Cndair CL6002C10 · Fuselage Main, Structure
  > TWO HUCK-BOLTS ARE CORRODED AT FS 797 ON THE RH PRESSURE FLOOR TAB IN THE WHEEL WELL (RBL 36.)
- [SDR VNAA202202180001](https://openairdocs.org/sdr/VNAA202202180001.md): None · none · Feb 18, 2023 · N544EA · Cndair CL6002C10 · Fuselage Main, Structure
  > TWO HUCK-BOLTS ARE CORRODED AT FS 797 ON THE RH PRESSURE FLOOR TAB IN THE WHEEL WELL (RBL 36.)
- [SDR VNAA202302100004](https://openairdocs.org/sdr/VNAA202302100004.md): Doubler · corroded · Feb 10, 2023 · N544EA · Cndair CL2151A10 · Fuselage Main, Structure
  > ANTENNA DOUBLER IS CORRODED BETWEEN F.S. 280 TO F.S. 295 AND AT STGR 27 CORRECTIVE ACTION REMOVED ANTENNA DOUBLER BETWEEN F.S.295-F.S.310 IAW CRJ 700 SRM 51-42-06-001-001-A01. INSTALLED NEW ANTENNA DOUBLER BETWEEN F.S.295-F.S.310 IAW CRJ 700 SRM 51-42-06-
- [SDR VNAA202302090003](https://openairdocs.org/sdr/VNAA202302090003.md): Frame · corroded · Feb 9, 2023 · N544EA · Bombdr BD1001A10 · Fuselage Main, Structure
  > DISCREPANCY: F.S. 1088.20 FRAME IS CORRODED BETWEEN STGR 26R TO STGR 26L. CORRECTIVE ACTION: COMPLIED WITH REPAIR TO F.S. 1088.20 FRAME BETWEEN STGR 26R TO STGR 26L IAW OLIVER WYMAN CAVOK EA 23-C7-53-0116, DATED 2/26/23, REV IR.
- [SDR VNAA202302090002](https://openairdocs.org/sdr/VNAA202302090002.md): Frame · corroded · Feb 9, 2023 · N544EA · Bombdr BD1001A10 · Fuselage Main, Structure
  > F.S. 333 FRAME IS CORRODED BETWEEN STGR 27 TO STGR 26L. CORRECTIVE ACTION: REPAIRED FS 333 LOWER FRAME SEGMENT IAW CRJ-700 SRM 53-00-06-201-006-A01.
- [SDR VNAA202302090001](https://openairdocs.org/sdr/VNAA202302090001.md): None · corroded · Feb 9, 2023 · N544EA · Bombdr BD1001A10 · Fuselage Main, Structure
  > NUT PLATE CHANNEL BETWEEN F.S. 1000 TO F.S. 1015 AND BETWEEN STGR 27 TO STGR 26L IS CORRODED. CORRECTIVE ACTION: INSTALLED NEW NUT PLATE CHANNEL P/N MM670-70327-001 BETWEEN F.S. 1000 TO F.S. 1015 AND BETWEEN STGR 27 TO STGR 26L IAW CRJ700 SRM 51-42-06-0
- [SDR VNAA2023013198008](https://openairdocs.org/sdr/VNAA2023013198008.md): Stringer · corroded · Jan 31, 2023 · N544EA · Cndair CL6002C10 · Fuselage Structure (General)
  > STGR 26R IS CORRODED BETWEEN F.S. 295 TO F.S. 310.
- [SDR VNAA202301298007](https://openairdocs.org/sdr/VNAA202301298007.md): Intercostal · corroded · Jan 30, 2023 · N544EA · Cndair CL6002C10 · Service Doors
  > SERVICE DOOR INTERCOSTAL IS CORRODED BETWEEN F.S. 310 TO F.S. 319.70 AND AT STGR19R.
- [SDR VNAA202301298006](https://openairdocs.org/sdr/VNAA202301298006.md): Skin · gouged · Jan 29, 2023 · N544EA · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE SKIN HAS 2EA.SCRATCHES APPROX. 1 INCH LONG AT F,S.265, 3 INCHES BELOW PILOT WINDSHIELD. CORRECTIVE ACTION: REPAIRED FUSELAGE SKIN AT F.S. 265 STGR 12 IAW OLIVER WYMAN EA 23-C7-53-0096 REV IR, DATED 01/23/2023.
- [SDR VNAA202301298005](https://openairdocs.org/sdr/VNAA202301298005.md): Attach Fitting · gouged · Jan 29, 2023 · N544EA · Cndair CL6002C10 · Fuselage, Wing Attach Fittings
  > L/H AFT WING TO FUSELAGE ATTACHMENT FITTING IS GOUGED ON THE AFT I/B EDGE APPROXIMATELY.009" DEEP AND 3" IN LENGTH. CORRECTIVE ACTION: REPAIRED L/H AFT WING FUSELAGE ATTACHMENT FITTING IAW OLIVER WYMAN EA 23-C7-57-0110 REV IR, DATED 01/23/2023.
- [SDR VNAA202301298004](https://openairdocs.org/sdr/VNAA202301298004.md): Fitting · gouged · Jan 29, 2023 · N544EA · Cndair CL6002C10 · Fuselage, Wing Attach Fittings
  > R/H AFT WING TO FUSELAGE ATTACHMENT FITTING IS GOUGED ON THE AFT I/B EDGE APPROXIMATELY.008" DEEP AND 2" IN LENGTH. CORRECTIVE ACTION: REPAIRED R/H AFT WING FUSELAGE ATTACHMENT FITTING IAW OLIVER WYMAN EA 23-C7-57-0111 REV IR, DATED 01/23/2023.
- [SDR VNAA202209281111](https://openairdocs.org/sdr/VNAA202209281111.md): None · arced · Sep 26, 2022 · N544EA · Cndair CL6002C10 · Flight Compartment Windows
  > CA WINDSHIELD DELAMINATING AND ARCING. REMOVED AND REPLACED CA'S WINDSHIELD IAW CRJ 700 AMM 56-11-01-000/400-801-PSA. C/W (L/H) WINDSHIELD INSTALLATION IAW CRJ700 AMM 56-11-01-400-801-PSA. OPS CHECKS AND LEAK CHECKS GOOD AT THIS TIME, NO DEFCECTS NOTED."
- [SDR VNAA2022092499981](https://openairdocs.org/sdr/VNAA2022092499981.md): Stringer · cracked · Sep 24, 2022 · N544EA · Bombdr CL6002D15 · Fuselage Structure (General)
  > STRINGER 3L LINTEL IS CRACKED FROM THE FWD EDGE OF THE STRINGER THRU.2" AFT OF THE 3RD AFT FASTENER HOLE. FAILED NDT INSPECTION. PERFORMED REPAIR OF STRINGER 3L LINTEL IAW REO 670-53-21-493 REV D.
- [SDR V0XD20220714001](https://openairdocs.org/sdr/V0XD20220714001.md): Skin · damaged · Jun 27, 2022 · N544EA · Cndair CL6002C10 · Fuselage Main, Structure
  > LH FUSELAGE SKIN AT FS565 AND STRINGER 17L HAS A PREVIOUS BLEND. CORRECTIVE ACTION: ACCOMPLISHED PERMANENT REPAIR TO THE LH FUSELAGE SKIN BY STRIPPING PAINT, PERFORMING UT AND UT INSPECTIONS AND RESTORING FINISH IAW OLIVER WYMAN CAVOK EA 22-C7-53-0443 REV A. N

Next page: https://openairdocs.org/aircraft/N544EA/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 = 'N544EA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N544EA/reports

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