# Service difficulty reports: N541EA

A list on [N541EA](https://openairdocs.org/aircraft/N541EA.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 · 145 reports

- [SDR VNAA20260512038](https://openairdocs.org/sdr/VNAA20260512038.md): Skin · cracked · May 12, 2026 · N541EA · Cndair CL6002C10 · Nacelle/Pylon, Plate/Skin
  > CRACK WAS FOUND ON EXTERNAL SKIN LH UPPER ENGINE TRANSCOWL. CRACK WAS FOUND ON EXTERNAL SKIN LH UPPER ENGINE TRANSCOWL WAS REPAIRED PER REO 670-54-21-1818 REV. -A.
- [SDR VNAA20260512037](https://openairdocs.org/sdr/VNAA20260512037.md): Acoustic Panel · cracked · May 12, 2026 · N541EA · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > IN REF TO NRC 0254 AFTER REMOVAL OF COAMING LATCH CRACK ON ACUSTIC PANEL WAS FOUND UPPER LH TRANSCOWL. ACOUSTIC PANEL WAS FOUND UPPER LH TRANSCOWL WAS REPAIRED PER REO PER REO 670-54-21-1818 REV. -A.
- [SDR VNAA20260512036](https://openairdocs.org/sdr/VNAA20260512036.md): Intercostal · corroded · May 12, 2026 · N541EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AFTER CORROSION REMOVAL REWORKED AREA ON INTERCOSTAL STGR 21LH BTW FS=310 TO FS= 333 WAS FOUND OUT OF LIMITS E/E BAY. CORROSION ON INTERCOSTAL STGR 20LH BTW FS=319 TO FS= 333 (FWD E/E BAY) WAS REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01, WAS EVALUATED, THERE
- [SDR VNAA20260512035](https://openairdocs.org/sdr/VNAA20260512035.md): Fitting · corroded · May 12, 2026 · N541EA · Cndair CL6002C10 · Wing, Control Surface Attach Fittings
  > CORROSION ON BORE LUG L2, L5 AND L6 AT LH AILERON CENTRAL FITTINGS. HINGE FITTING AILERON LH BORE LUGS L2, L5 AND L6 WERE REPAIRED PER REO 670-57-61-237 REV -.
- [SDR VNAA20260512034](https://openairdocs.org/sdr/VNAA20260512034.md): Fitting · corroded · May 12, 2026 · N541EA · Cndair CL6002C10 · Wing, Control Surface Attach Fittings
  > CORROSION ON LUG BORES ON R3 AND R5 AT RH AILERON CENTRAL FITTING. CORROSION ON LUG BORE R5 AT RT AILERON CENTRAL FITTING WAS REPAIRED PER REO 670-57-61-237 REV:-- AND LUG R3 WAS CLEANING PER SRM 51-26-00-001-001-A01 CLEANING.-.
- [SDR VNAA20260512033](https://openairdocs.org/sdr/VNAA20260512033.md): Fitting · gouged · May 12, 2026 · N541EA · Cndair CL6002C10 · Wing, Control Surface Attach Fittings
  > GOUGE ON LATERAL FACE OF LUG R1 AND R2 AT RH AILERON CENTRAL FITTINGS. LATERAL FACE OF LUG R1 AND R2 AT RH AILERON CENTRAL FITTINGS WERE REPAIRED PER REO 670-57-61-237 REV -
- [SDR VNAA20260512032](https://openairdocs.org/sdr/VNAA20260512032.md): Angle · cracked · May 12, 2026 · N541EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CRACK ON OUTBD ANGLE ON CROSSBEAM FS 280 LBL-12 AT PAX CABIN FLOOR STRUCTURE. ANGLE WAS REPLACED ON CROSSBEAM FS 280 LBL-12 AT PAX CABIN FLOOR STRUCTURE PER CRJ700 SRM 51-42-21-001-001-A01.
- [SDR VNAA20260512031](https://openairdocs.org/sdr/VNAA20260512031.md): Support · cracked · May 12, 2026 · N541EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CRACKS ON DIAPHRAGM SUPPORT (ABOVE DOOR NET STRUCTURE) OF AFT BAGGAGE BAY STRUCTURE. DIAPHRAGM SUPPORT (ABOVE DOOR NET STRUCTURE) OF AFT BAGGAGE BAY STRUCTURE WAS REPLACED PER CRJ700 SRM 51-42-06-001-001-A01 PAR. AND SRM 51-41-02- 001-001-A01.
- [SDR VNAA20260512030](https://openairdocs.org/sdr/VNAA20260512030.md): Skin · corroded · May 12, 2026 · N541EA · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > DURING EXTERNAL ZONAL INSPECTION OF THE REAR FUSELAGE: FS977.00 TO FS1098.00, ABOVE WL72.50, SEVERAL DENTS WERE FOUND ON EXTERNAL FUSELAGE SKIN BTW FS1015.00 TO FS1069.00 BTW STGR27 TO STGR 22 RH. AFTER REMOVAL OF PAINT, DVI WAS PERFORMED PER CRJ-700 NDT PART
- [SDR VNAA20260512029](https://openairdocs.org/sdr/VNAA20260512029.md): Structure · corroded · May 12, 2026 · N541EA · Cndair CL6002C10 · Aerodynamic Fairings
  > CORROSION ON SETTLEMENT SUPPORT STRUCTURE AT AFT C-CHANNEL ALONG AFT WING-TO-FUSELAGE FAIRING (196DR). SETTLEMENT SUPPORT STRUCTURE (STRAP) WAS REPLACED PER CRJ-700 SRM 51-42-10-001-001-A01.
- [SDR VNAA20260512028](https://openairdocs.org/sdr/VNAA20260512028.md): Seat Track · corroded · May 12, 2026 · N541EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK OF FS 582.00 TO FS 669.00 AND RBL 9 OF THE FUSELAGE FLOOR STRUCTURE. CORROSION ON SEAT TRACK OF FS 582.00 TO FS 669.00 AND RBL 9 OF THE FUSELAGE FLOOR STRUCTURE WAS REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01 AND THEREFORE OUT OF LIM
- [SDR VNAA20260512027](https://openairdocs.org/sdr/VNAA20260512027.md): Seat Track · corroded · May 12, 2026 · N541EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK OF FS 486.00 TO FS 581.00 AND LBL 9 OF THE FUSELAGE FLOOR STRUCTURE. CORROSION ON SEAT TRACK OF FS 486.00 TO FS 581.00 AND LBL 9 OF THE FUSELAGE FLOOR STRUCTURE. AT PASSENGER CABIN WAS REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01, WAS
- [SDR VNAA20260512026](https://openairdocs.org/sdr/VNAA20260512026.md): Intercostal · cracked · May 12, 2026 · N541EA · Cndair CL6002C10 · Wing Miscellaneous Structure
  > CRACK ON INTERCOSTAL, TIRE BURST COVER BEHIND PANEL 542AZ OF LH WING. INTERCOSTAL, TIRE BURST COVER BEHIND PANEL 542AZ OF LH WING WAS REPLACED PER CRJ-700 SRM 51-42-21-001-001-A01 PAR.6.C AND SRM 51-42-13-001-001-A01 PAR.6.C AND SRM 51-42-06-001-001-A01 PAR.
- [SDR VNAA20260512025](https://openairdocs.org/sdr/VNAA20260512025.md): Seat Track · corroded · May 12, 2026 · N541EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION WAS FOUND AT SEAT TRACK ON FS 364.00 TO 469.00 LBL 25 OF THE FUSELAGE FLOOR STRUCTURE. SEAT TRACK ON FS 364.00 TO 469.00 LBL 25 OF THE FUSELAGE FLOOR STRUCTURE WERE REPLACED PER CRJ700 AMM 53-00-49-400-801 (CONFIG A03)
- [SDR VNAA20260512024](https://openairdocs.org/sdr/VNAA20260512024.md): Floorbeam · corroded · May 12, 2026 · N541EA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > CORROSION ON BRACKETS FLOOR BEAM AT FS 284.00 RBL16 AND RBL36, ON BRACKET FLOOR BEAM FS 295.00 AND RBL 5 OF THE FUSELAGE FLOOR STRUCTURE. FLOORBEAM TEE REMOVED PER SRM 51-21-06-001-001-A01 AND AREAS IS OUT LIMITS PER CRJ700 SRM 53-21-43-101-001-A01 AND SRM 53
- [SDR VNAA20260512023](https://openairdocs.org/sdr/VNAA20260512023.md): Bracket · cracked · May 12, 2026 · N541EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CRACK ON OXYGEN SERVICE PANEL BRACKET (LOWER AFT CORNER) AT FWD FUSELAGE. PANEL BRACKET ON OXYGEN SERVICE (LOWER AFT CORNER) AT FWD FUSELAGE WAS REPLACED PER CRJ-700 SRM 51-42-06-001-001-A01 "
- [SDR VNAA20260512022](https://openairdocs.org/sdr/VNAA20260512022.md): Angle · corroded · May 12, 2026 · N541EA · Cndair CL6002C10 · Passenger/Crew Doors
  > AFTER REMOVAL OF MIDCAP ANGLE, CORROSION ON KICKPLATE ANGLE WAS FOUND AT SURROUND STRUCTURE OF PASSENGER DOOR. CORROSION ON KICKPLATE ANGLE WAS FOUND AT SURROUND STRUCTURE OF PASSENGER DOOR WAS REMOVED PER SRM 51-21-06-001-001-A01 AND AREA WAS FOUND OUT LIMI
- [SDR VNAA20260512021](https://openairdocs.org/sdr/VNAA20260512021.md): Angle · cracked · May 12, 2026 · N541EA · Cndair CL6002C10 · Wing Miscellaneous Structure
  > CRACK ON ANGLE OF SETTLEMENT AREA OF ACCESS PANEL 642AZ (ATTATCHED TO REAR SPAR) AT RH WING. ANGLE OF SETTLEMENT AREA OF ACCESS PANEL 642AZ (ATTATCHED TO REAR SPAR) AT LH WING. WAS REPLACED PER SRM 51-42-21-001-001-A01.
- [SDR VNAA20260512020](https://openairdocs.org/sdr/VNAA20260512020.md): Angle · cracked · May 12, 2026 · N541EA · Cndair CL6002C10 · Wing Miscellaneous Structure
  > CRACK ON ANGLE OF SETTLEMENT AREA OF ACCESS PANEL 542AZ (ATTATCHED TO REAR SPAR) AT LH WING. ANGLE OF SETTLEMENT AREA OF ACCESS PANEL 542AZ (ATTATCHED TO REAR SPAR) AT LH WING. WAS REPLACED IAW SRM 51-42-21-001-001-A01.
- [SDR VNAA20260512019](https://openairdocs.org/sdr/VNAA20260512019.md): Frame · cracked · May 12, 2026 · N541EA · Cndair CL6002C10 · Engine Thrust Reverser
  > CRACK ON LH UPPER/LOWER THRUST REVERSER TORQUE BOX FWD FRAME AT LH ENGINE. LT UPPER/LOWER THRUST REVERSER TORQUE BOX FWD FRAME AT LH ENGINE.WERE REPAIRED PER REO 670-54-22-154 REV-- AND REO 670-54-22-155 REV-.
- [SDR VNAA20260512018](https://openairdocs.org/sdr/VNAA20260512018.md): Support Beam · chafed · May 12, 2026 · N541EA · Cndair CL6002C10 · Engine Thrust Reverser
  > CHAFE DAMAGE UPPER/LOWER CASCADE SUPPORT BEAM AT LT/RT ENGINE. CHAFE DAMAGE UPPER/LOWER CASCADE SUPPORT BEAM AT LH/RH ENGINE WERE REPAIRED PER REO 670-54-22-160 REV- -, REO 670-54-22-161 REV- -. REO 670-54-22-159 REV- -. AND PER REO 670-54-22-162 REV- -.
- [SDR VNAA20260512017](https://openairdocs.org/sdr/VNAA20260512017.md): Angle · cracked · May 12, 2026 · N541EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CRACKED INTERNAL ANGLE OF EXTERNAL POWER RECEPTACLE SUPPORT STRUCTURE. ANGLE OF EXTERNAL POWER RECEPTACLE SUPPORT WAS REPLACED PER SRM 51-42-06-001-001-A01.
- [SDR VNAA20260512016](https://openairdocs.org/sdr/VNAA20260512016.md): Striker · corroded · May 12, 2026 · N541EA · Cndair CL6002C10 · Cargo/Baggage Doors
  > CORROSION ON LOWER STRIKER OF CARGO DOOR SURROUND STRUCTURE. REPLACED PER CRJ 700 SRM 51-42-21-001-001-A01.
- [SDR VNAA20260512015](https://openairdocs.org/sdr/VNAA20260512015.md): Fitting · corroded · May 12, 2026 · N541EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON MID CAP ANGLE OF PASSENGER DOOR SURROUND STRUCTURE. CORROSION ON MID CAP ANGLE WAS REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01 AND IS OUT OFF LIMITS PER CRJ-700 SRM 53-21-23-101-001-A01 AND MID CAP ANGLE WAS REPLACED PER CRJ-700 SRM 51-41-02-00
- [SDR VNAA20260512014](https://openairdocs.org/sdr/VNAA20260512014.md): Fitting · corroded · May 12, 2026 · N541EA · Cndair CL6002C10 · Fuselage Main, Frame
  > INITIAL INSPECTION: CORROSION ON FRAME FITTING FS 319 STGR 17RH AT CPAX. FRAME FITTING WAS REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01, WAS EVALUATED, THEREFORE IT IS OUT LIMITS PER CRJ700 SRM 53-21-23-101-001-A01 AND REPLACED PER CRJ-700 SRM 51-42-21-001-
- [SDR VNAA20260512013](https://openairdocs.org/sdr/VNAA20260512013.md): Bracket · corroded · May 12, 2026 · N541EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON BRACKET MACHINED FS=515 STGR 22LH TO STGR 23LH AND BTW FS=661 TO 645 STGR 24 LH TO STGR 25LH AT FORDWARD BAGGAGE BAY. WERE EVALUATED,DUE NOT ALLOWABLE DAMAGE BRACKET MACHINED FS=515 STGR 22LH TO STGR 23LH AND BTW FS=661 TO 645 STGR 24 LH TO STGR
- [SDR VNAA20260512012](https://openairdocs.org/sdr/VNAA20260512012.md): Panel · cracked · May 12, 2026 · N541EA · Cndair CL6002C10 · Fuselage Structure (General)
  > CORROSION AND CRACK ON DIVERTER PANELS (3EAS). REPAIRED PER EA 5321-2026-0502 REV - -, EA 5321-2026-0501 REV - - AND EA 5321-2026-0488 REV -.
- [SDR VNAA20260512011](https://openairdocs.org/sdr/VNAA20260512011.md): Seat Track · corroded · May 12, 2026 · N541EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AND GOUGES ON SEAT RAIL (3EAS) FS349 TO FS485, FS485 TO FS 581 RBL 9 AND FS 379 TO 485 LBL 9 AT PASSENGER CABIN. SEAT RAIL (3EAS) FS349 TO FS485, FS485 TO FS 581 RBL 9 AND FS 379 TO 485 LBL 9 AT PASSENGER WERE REPLACED PER CRJ 700 SRM 53-00-49-400-
- [SDR VNAA20260512010](https://openairdocs.org/sdr/VNAA20260512010.md): Seat Track · corroded · May 12, 2026 · N541EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AND GOUGES ON SIDE SEAT RAIL (5EAS) FS711 TO FS761 (LH), FS677 TO FS711 (LH), FS573 TO FS677 (LH), FS379 TO 477 RH/LH AT PASSENGER CABIN. SEAT RAIL (5EAS) FS711 TO FS761 (LH), FS677 TO FS711 (LH), FS573 TO FS677 (LH), FS379 TO 477 RH/LH AT PASSENGE
- [SDR VNAA20260512009](https://openairdocs.org/sdr/VNAA20260512009.md): Skin · damaged · May 12, 2026 · N541EA · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > PERM REPAIR - PANEL 196DR NUT PLATE ASSEMBLY OVERSIZED HOLE 1. WITHIN 1556 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. // ENGINEERING COMMENTS: REPLACE NUT PLATE ASSY. M
- [SDR VNAA20260512008](https://openairdocs.org/sdr/VNAA20260512008.md): Hinge · worn · May 12, 2026 · N541EA · Cndair CL6002C10 · Fuselage, Door Hinge
  > IN REF TO TRFKE00EQGM3: PERM REPAIR - PASSENGER DOOR SURROUND STRUCTURE - HINGE REPLACEMENT REPLACE THE PASSENGER DOOR HINGE IN ACCORDANCE WITH CRJ700 SRM TASK 53-21-23-201-007-A01. SEND E-MAIL REQUEST TO DL_PSA_MAINTENANCE_PROGRAMS@PSAAIRLINES.COM TO COMPLETE
- [SDR VNAA20260512006](https://openairdocs.org/sdr/VNAA20260512006.md): Web · cracked · May 12, 2026 · N541EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CRACK ON FLOOR WEB LEFT SIDE (BELOW BRAKE ACCUMULATOR INDICATION SUPPORT DOUBLER) FS193.00 AT FWD EQUIPMENT COMPARTMENT. FLOOR WEB LEFT SIDE (BELOW BRAKE ACCUMULATOR INDICATION SUPPORT DOUBLER) FS193.00 AT FWD EQUIPMENT COMPARTMENT. WAS REPAIRED PER CRJ 700 S
- [SDR VNAA20260512007](https://openairdocs.org/sdr/VNAA20260512007.md): Drip Tray · cracked · May 12, 2026 · N541EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > IN REF TO TRFKE00CFJVX: 4790FH PERM REPAIR - DAMAGE DRIP TRAY DRAIN TUBE FITTING WITHIN 4790 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. // ENGINEERING COMMENTS: REPLACE
- [SDR VNAA20260512005](https://openairdocs.org/sdr/VNAA20260512005.md): Plate · cracked · May 12, 2026 · N541EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CRACKS ON MOUNTING PLATE FWD/AFT CORNERS OF JB6 AT FWD EQUIPMENT COMPARTMENT. MOUNTING PLATE WAS REPLACED PER SRM 51-42-06-001-001-A01.
- [SDR VNAA20260512004](https://openairdocs.org/sdr/VNAA20260512004.md): Angle · cracked · May 12, 2026 · N541EA · Cndair CL6002C10 · Cargo/Baggage Doors
  > CRACKED AFT UPPER ANGLE OF FIRE PROTECTION KIT AT FWD BAGGAGE BAY DOOR. CRACKED AFT UPPER ANGLE OF FIRE PROTECTION KIT AT FWD BAGGAGE BAY DOOR WAS REPLACED PER CRJ-700 SRM 51-42-10-001-001-A01 AND SRM 51-41-02-001-001-A01
- [SDR VNAA20260512003](https://openairdocs.org/sdr/VNAA20260512003.md): Retainer Seal · cracked · May 12, 2026 · N541EA · Cndair CL6002C10 · Passenger/Crew Doors
  > CRACKED UPPER SEAL RETAINER AT PASSENGER DOOR. UPPER SEAL RETAINER AT PASSENGER DOOR WAS REMPLACED PER CRJ-700 SRM 51-42-10-001-001-A01
- [SDR VNAA20260512002](https://openairdocs.org/sdr/VNAA20260512002.md): Handle · cracked · May 12, 2026 · N541EA · Cndair CL6002C10 · Passenger/Crew Doors
  > CRACKS (4 EAS) ON EXTERNAL HANDLE FLAPER CORNERS AT PASSENGER DOOR. EXTERNAL FLAP HANDLE AT PASSENGER DOOR WAS REPLACED PER CRJ-700 SRM 51-42-06-001-001-A01 AND PLACARD WAS INSTALLED PER CRJ-700 AMM 20-60-04-400-801.
- [SDR VNAA20260512001](https://openairdocs.org/sdr/VNAA20260512001.md): Hinge Fitting · corroded · May 12, 2026 · N541EA · Cndair CL6002C10 · Fuselage, Door Hinge
  > CORROSION ON HINGE FITTINGS (2 EAS) AND HARDWARE OF AFT LAVATORY SERVICE DOOR. CORROSION ON HINGE FITTINGS (2 EAS) OF AFT LAVATORY SERVICE DOOR WERE REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01 AND THEREFORE IT IS OUT OF LIMITS PER CRJ-700 SRM 53-00-00-101-00
- [SDR VNAA202209029949](https://openairdocs.org/sdr/VNAA202209029949.md): Stringer · corroded · Sep 2, 2022 · N541EA · Cndair CL6002C10 · Fuselage Structure (General)
  > CORROSION ON STRG 26LH BTW FS. 280/265 AT FWD AVIONICS COMPARTMENT.
- [SDR VNAA202209029948](https://openairdocs.org/sdr/VNAA202209029948.md): Splice · corroded · Sep 2, 2022 · N541EA · Cndair CL6002C10 · Fuselage Structure (General)
  > CORROSION ON SPLICE AT FS333 & STGR 25RH, FWD EQUIPMENT BAY.
- [SDR VNAA202209029947](https://openairdocs.org/sdr/VNAA202209029947.md): Stringer Splice · corroded · Sep 2, 2022 · N541EA · Cndair CL6002C10 · Fuselage Structure (General)
  > CORROSION ON SPLICE AT FS333 & STGR 26RH, FWD E/E EQUIPMENT BAY.
- [SDR VNAA202209029946](https://openairdocs.org/sdr/VNAA202209029946.md): Stringer · corroded · Sep 2, 2022 · N541EA · Cndair CL6002C10 · Fuselage Structure (General)
  > CORROSION ON STGR 24RH BTW FS477.4-FS501, FWD CARGO COMPARTMENT
- [SDR VNAA202209029945](https://openairdocs.org/sdr/VNAA202209029945.md): Splice · corroded · Sep 2, 2022 · N541EA · Cndair CL6002C10 · Fuselage Structure (General)
  > CORROSION ON SPLICE AT FS477.4 & STGR 24RH, FWD CARGO COMPARTMENT
- [SDR VNAA202209029944](https://openairdocs.org/sdr/VNAA202209029944.md): None · none · Sep 2, 2022 · N541EA · Cndair CL6002C10 · Fuselage Structure (General)
  > SCRATCHES ON LH SIDE SEAT RAIL STRUCTURE BETWEEN FS669 TO FS785, SCRATCHES AND CORROSION BETWEEN FS785 TO FS861 AND SCRATCHES BETWEEN FS861
- [SDR VNAA202209029943](https://openairdocs.org/sdr/VNAA202209029943.md): None · none · Sep 2, 2022 · N541EA · Cndair CL6002C10 · Fuselage Structure (General)
  > SCRATCHES ON RH SIDE SEAT RAIL STRUCTURE BETWEEN FS669 TO FS785, SCRATCHES AND CORROSION BETWEEN FS785 TO FS861 AND SCRATCHES BETWEEN FS861
- [SDR VNAA202209029942](https://openairdocs.org/sdr/VNAA202209029942.md): Plate · corroded · Sep 2, 2022 · N541EA · Cndair CL6002C10 · Fuselage Structure (General)
  > CORROSION ON NET ATTACHMENT PLATES (3 EAS) ON AFT BAGGAGE BAY DOOR CUTOUT STRUCTURE BETWEEN FS=1000.00 AND FS=1047.00.
- [SDR VNAA202209029941](https://openairdocs.org/sdr/VNAA202209029941.md): None · none · Sep 2, 2022 · N541EA · Cndair CL6002C10 · Fuselage Structure (General)
  > CRACK ON CLIP AT AFT BAGGAGE BAY DOOR CUTOUT STRUCTURE BETWEEN FS=1047.00/FS=1051.30 AND STGR 7LH.
- [SDR VNAA202209029940](https://openairdocs.org/sdr/VNAA202209029940.md): None · corroded · Sep 2, 2022 · N541EA · Cndair CL6002C10 · Wing, Nacelle/Pylon Attach Fittings
  > PITTING CORROSION ON SLAT TRACKS 3-2 (SEVERAL LOCATION AT UPPER SURFACE), SLAT #3 LH WING.
- [SDR VNAA202209029950](https://openairdocs.org/sdr/VNAA202209029950.md): Web · none · Sep 2, 2022 · N541EA · Cndair CL6002C10 · Fuselage Structure (General)
  > CORROSION ON FLOOR PROTECTOR WEBS AT FUSELAGE LOWER FRAME SERVICE DOOR CORROSION ON FLOOR PROTECTOR WEBS WAS REMOVED PER CRJ/700 SRM 51-21-06-001-001-A01 AND MEASUREMENT WAS PERFORMED ON FLOOR PROTECTOR WEBS (4EA'S) WITH ORIGINAL THICKNESS IS 0.063 AND MINIM
- [SDR VNAA202209029951](https://openairdocs.org/sdr/VNAA202209029951.md): None · none · Sep 2, 2022 · N541EA · Cndair CL6002C10 · Fuselage Structure (General)
  > AFTER REMOVAL OF RH/LH MLG´S PISTON AXLE, CORROSION ON THREADS OF CYLINDER ASSY RH/ LH MLG´S}. (AYP) THREADS OF CYLINDER ASSY AT LH MLG WAS CLEANED PER CRJ700 SRM 51-26-00-001-001-A01 AND AFTER CLEANLINESS, AREA WAS INSPECTED PER CRJ-700 SRM 51-11-00-001-001

Next page: https://openairdocs.org/aircraft/N541EA/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 = 'N541EA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N541EA/reports

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