# Service difficulty reports: N559NN

A list on [N559NN](https://openairdocs.org/aircraft/N559NN.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 · 75 reports

- [SDR VNAA2026062920404](https://openairdocs.org/sdr/VNAA2026062920404.md): Fan · unserviceable · Jun 26, 2026 · N559NN · Cndair CL6002D24 · Air Distribution Fan
  > APU DOOR CAUTION MSG AFTER TAKE OFF. FA AND AFT FA REPORT A STRONG BURNING ODOR AT THE SAME TIME DURING TAKE OFF. RAN APU DOOR CAUTION QRH FAULT PERSISTED / REMOVED AND REPLACED RH RECIRCULATION FAN IAW AMM 21-22-10-000/400 801-A01. LEAK TEST PASS OP TEST G
- [SDR VNAA2025022111103](https://openairdocs.org/sdr/VNAA2025022111103.md): Door · open · Feb 18, 2025 · N559NN · Cndair CL6002D24 · Accessory Compartment Doors
  > LOW PRESSURE AIR DOOR LEFT OPEN, COVER MISSING / REMOVED AND REPLACED LOW PRESSURE AIR DOOR IAW CRJ 900 AMM 52-45-53-400-801.
- [SDR VNAA2024111911101](https://openairdocs.org/sdr/VNAA2024111911101.md): Drain · overflow · Nov 16, 2024 · N559NN · Cndair CL6002D24 · Fuselage Structure (General)
  > ELECTRICAL FIRE SMELL OBSERVED IN GALLEY IN FLIGHT. CREW COMMUNICATION WAS ESTABLISHED, AND NO SMELL WAS OBSERVED IN THE FLIGHT DECK OR BY PASSENGERS IN THE CABIN. NOTE: NO FIRE OR SMOKE PRESENT. / TROUBLESHOT SMELL OBSERVED IN GALLEY IN FLIGHT. TAXIED AIRCRAF
- [SDR VNAA2024092711102](https://openairdocs.org/sdr/VNAA2024092711102.md): Warning Message · false activation · Sep 26, 2024 · N559NN · Cndair CL6002D24 · Door Warning System
  > AVIONICS BAY DOOR AMBER CAS MESSAGE IN FLIGHT / PERFORMED OPS CHECK OF MAIN AVIONICS DOOR IAW CRJ 900 AMM 52-42-00-710-801-A01. NO FOD FOUND AND DOOR IS CLOSED.
- [SDR VNAA202311230004](https://openairdocs.org/sdr/VNAA202311230004.md): Floorbeam · cracked · Nov 2, 2023 · N559NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CRACKED CENTER COCKPIT FLOOR BEAM LBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. FLOOR BEAM LBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1614. REV.--
- [SDR VNAA202311260012](https://openairdocs.org/sdr/VNAA202311260012.md): Hinge · corroded · Oct 31, 2023 · N559NN · Cndair CL6002D24 · Ailerons
  > AFTER REMOVAL OF BUSHINGS, BEARINGS, AND HARDWARE, CORROSION ON HINGE FITTING LUG BORES AT LH AILERON, HINGE NO. 2 BOTH LUG BORES, HINGE NO. 3 BOTH LUG BORES, HINGE NO. 4 BORE LUG (SINGLE BORE LUG) AND BOTH PCU OUTPUT LINKS LUG BORES. HINGE FITTING LUG BORES
- [SDR VNAA202311230010](https://openairdocs.org/sdr/VNAA202311230010.md): Stringer · corroded · Oct 31, 2023 · N559NN · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION AROUND FASTENERS ABOVE STGR 26RH AND BTW FS364.00 - FS349.00 AT AVIONIC COMPARTMENT DOOR SURROUND STRUCTURE. STRINGER 26R BTW FS364.00 - FS349.00 AT AVIONIC COMPARTMENT DOOR SURROUND STRUCTURE WAS REPLACED PER CRJ900 SRM 51-42-06-001-A01 AND CRJ90
- [SDR VNAA202311230007](https://openairdocs.org/sdr/VNAA202311230007.md): Web · cracked · Oct 31, 2023 · N559NN · Cndair CL6002D24 · Fuselage Internal Mounting Structure
  > CRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00. CRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00 WAS REPAIRED PER CRJ900 SRM SRM 53-11-43-201-001-A01
- [SDR VNAA20231120004](https://openairdocs.org/sdr/VNAA20231120004.md): Access Panel · worn · Oct 31, 2023 · N559NN · Cndair CL6002D24 · Wing, Plate/Skin
  > WEAR ON LEADING EDGE ACCESS PANELS 622 AR AND 622BR ALSO NICK ON ACCESS PANEL 622BR. REPAIRED PER EA 23-C9-57-1502 REV IR. SECTION III - PERMANENT REPAIR AND EA 23-C9-57-1503 REV IR. SECTION III - PERMANENT REPAIR
- [SDR VNAA202311250001](https://openairdocs.org/sdr/VNAA202311250001.md): Skin · corroded · Oct 29, 2023 · N559NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > CORROSION AROUND SETTLEMENT AREA WAS FOUND AT THE MAIN AVIONICS COMPARTMENT DOOR BETWEEN FS364 TO FS 394 AND STGR 25R - STGR 25L. CORROSION AROUND SETTLEMENT AREA WAS FOUND AT THE MAIN AVIONICS COMPARTMENT DOOR BETWEEN FS364 TO FS394 AND STGR25R/STGR25L WAS R
- [SDR VNAA202311230003](https://openairdocs.org/sdr/VNAA202311230003.md): Skin · worn · Oct 29, 2023 · N559NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > WEAR ON EXTERNAL FUSELAGE SKIN BTW FS 897.00 TO FS 913.00, BTW STGR 27 TO STGR 26LH. EXTERNAL FUSELAGE SKIN BTW FS 897.00 TO FS 913.00, BTW STGR 27 TO STGR 26LH WAS REPAIRED PER REO 670-53-00-290 REV. -F AND EA 23-C9-53-1442 REV.IR
- [SDR VNAA20231121002](https://openairdocs.org/sdr/VNAA20231121002.md): Plate · corroded · Oct 29, 2023 · N559NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON CONNECTORS SUPPORT PLATES LH/RH (PX33, PX17, PX34, PX19) ON LH/RH MAIN WHEEL WELL. DUE TO EXCESIVE CORROSION ON CONNECTORS SUPPORT PLATES LH/RH (PX33, PX17, PX34, PX19) ON LH/RH MAIN WHEEL WELL WERE REPLACED PER CRJ900 SRM 53-00-00-101-001-A01 A
- [SDR VNAA202311230005](https://openairdocs.org/sdr/VNAA202311230005.md): Floorbeam · cracked · Oct 28, 2023 · N559NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CRACKED CENTER COCKPIT FLOOR BEAM RBL12 @ FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT
- [SDR VNAA202311260006](https://openairdocs.org/sdr/VNAA202311260006.md): Floor Support · corroded · Oct 26, 2023 · N559NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON UPPER FACE OF FLOOR BEAM LBL 27 BTW FS 1006.00 TO FS 1047.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE. FLOOR BEAM LBL 27 BTW FS 1006.00 TO FS 1047.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE WAS REPAIRED PER EA 23-C9-53-1465 REV. IR
- [SDR VNAA202311260002](https://openairdocs.org/sdr/VNAA202311260002.md): Angle · cracked · Oct 26, 2023 · N559NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON CLIP, STGR 7LH TO FS 1051.30 ON AFT BAGGAGE BAY DOOR SURROUND STRUCTURE. CLIP, STGR 7LH TO FS 1051.30 ON AFT BAGGAGE BAY DOOR SURROUND STRUCTURE WAS REPLACED PER EA 23-C9-53-1463 REV. IR
- [SDR VNAA202311250008](https://openairdocs.org/sdr/VNAA202311250008.md): Intercostal · corroded · Oct 23, 2023 · N559NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL AT STGR 20RH BTW FS310.00 TO FS 319.70 AT MAIN AVIONICS COMPARTMENT INTERNAL STRUCTURE. CORROSION ON INTERCOSTAL AT STGR 20RH BTW FS310.00 TO FS 319.70 AT MAIN AVIONICS COMPARTMENT INTERNAL STRUCTURE WAS REMOVED PER CRJ900 SRM 51-21-0
- [SDR VNAA202311250002](https://openairdocs.org/sdr/VNAA202311250002.md): Intercostal · corroded · Oct 23, 2023 · N559NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL AT STGR 20R BTW FS333.00 TO FS 364.00. CORROSION ON INTERCOSTAL BTW FS 333.00 TO FS 364.00 STRG 20RH WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND WAS EVALUATED AREA BTW FS349.00 TO FS364.00 IS WITHIN LIMITS AND AREA BTW FS333.0
- [SDR VNAA202311230008](https://openairdocs.org/sdr/VNAA202311230008.md): Stringer · worn · Oct 20, 2023 · N559NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > WEAR ON STRINGER 3 RH BTW FS 364.00 TO FS 379.00 AT PASSENGER COMPARTMENT INTERNAL STRUCTURE. STRINGER 3 RH BTW FS 364.00 TO FS 379.00 AT PASSENGER COMPARTMENT INTERNAL STRUCTURE WAS FABRICATED AND REPLACE PER PER EA 23-C9-53-1448. REV. IR. SECTION III-PERMAN
- [SDR VNAA20231120001](https://openairdocs.org/sdr/VNAA20231120001.md): Skin · damaged · Oct 19, 2023 · N559NN · Cndair CL6002D24 · Trailing Edge Flaps
  > NICKS AND DENTS ON LOWER SKIN OF RH INBOARD FLAP BTW FLS 15.00 TO FLS 65.5. NICKS AND DENTS ON LOWER SKIN OF RH INBOARD FLAP BTW FLS 15.00 TO FLS 65.5 WERE BLENDED OUT PER CRJ-900 SRM 51-12-00-001-001-A01 AND REWORKED AREA ON FLS45.00 TO 65.5 WAS EVALUATED IS
- [SDR VNAA202311250011](https://openairdocs.org/sdr/VNAA202311250011.md): Seat Track · corroded · Oct 17, 2023 · N559NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH SIDE SEAT RAIL AT STGR 15LH, BTW FS669.40 TO FS720.85. DUE TO EXCESSIVE CORROSION ON LH SIDE SEAT RAIL AT STGR 15LH, BTW FS669.40 TO FS720.85. WAS REPLACED PER CRJ-900 SRM 53-41-49-101-001-A02 AND CRJ-900 AMM 53-00-49 (CONFIG A12)
- [SDR VNAA202311250010](https://openairdocs.org/sdr/VNAA202311250010.md): Seat Track · corroded · Oct 17, 2023 · N559NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH SIDE SEAT RAIL AT STGR 15LH, BTW FS 847.00 + 18.00 TO FS899.70. DUE TO EXCESSIVE CORROSION ON LH SIDE SEAT RAIL AT STGR 15LH, BTW FS 847.00 + 18.00 TO FS899.70. WAS REPLACED PER CRJ-900 SRM 53-41-49-101-001-A02 AND CRJ-900 AMM 53-00 (CONFIG A1
- [SDR VNAA202311250004](https://openairdocs.org/sdr/VNAA202311250004.md): Seat Track · corroded · Oct 17, 2023 · N559NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SIDE SEAT RAIL AT STGR 15 RH, BTW FS 669.40 TO FS 720.85. DUE TO NOT PERMISIBLE DAMAGE ON SIDE SEAT RAIL 15 RH, BTW FS 669.40 TO FS 720.85. AT PASSENGER CABIN WAS REPLACED PER CRJ-900 SRM 53-41-49-101-001-A02 AND CRJ-900 AMM 53-00-49 (CONFIG.
- [SDR VNAA202311250009](https://openairdocs.org/sdr/VNAA202311250009.md): Seat Track · corroded · Oct 16, 2023 · N559NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH SEAT RAIL AT LBL 9, BTW FS 847.00 + 16.00 TO FS954.00 AT PASSENGER COMPARTMENT FLOOR STRUCTURE. DUE TO EXCESSIVE CORROSION ON LH SEAT RAIL AT LBL 9, BTW FS 847.00 + 16.00 TO FS 954.00 WAS REPLACED PER CRJ-900 SRM 53-31-49-101-001-A02 AND CRJ-9
- [SDR VNAA202311230009](https://openairdocs.org/sdr/VNAA202311230009.md): Seat Track · corroded · Oct 16, 2023 · N559NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON FLOOR SEAT RAIL LBL 9 BTW FS379.00 TO FS485.00. DUE TO EXCESSIVE CORROSION ON FLOOR SEAT RAIL LBL 9 BTW FS379.00 TO FS485.00. WAS REPLACED PER CRJ-900 SRM 53-21-49-101-001-A01 AND CRJ-900 AMM 53-00-49-000-801 (CONFIG. A12) AND AMM 53-00-49-400-8
- [SDR VNAA202311230002](https://openairdocs.org/sdr/VNAA202311230002.md): Drag Angle · cracked · Oct 11, 2023 · N559NN · Cndair CL6002D24 · Vertical Stabilizer
  > CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATU
- [SDR VNAA202311230001](https://openairdocs.org/sdr/VNAA202311230001.md): Drag Angle · cracked · Oct 11, 2023 · N559NN · Cndair CL6002D24 · Vertical Stabilizer
  > CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM
- [SDR VNAA202311260013](https://openairdocs.org/sdr/VNAA202311260013.md): Skin · dented · Oct 8, 2023 · N559NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > FUSELAGE DENT, AFT OF AFT CARGO DOOR WITHIN 800 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR/REPLACEMENT OF THE DAMAGE IN ACCORDANCE WITH APPROVED PROCEDURES. FUSELAGE DENT AFT OF AFT CARGO DOOR WAS REPAIRED PER EA 21-C9-53-866 REV. D SECTION I
- [SDR VNAA202311260011](https://openairdocs.org/sdr/VNAA202311260011.md): Aileron · corroded · Oct 8, 2023 · N559NN · Cndair CL6002D24 · Ailerons
  > CORROSION BORES ON AILERON HINGE FITTING LUG BORE AT RH HINGE NO 1, NO 2, NO 3 & NO 4 AND BOTH PCU OUTPUT LINK LUG BORES WAS FOUND. CORROSION BORES ON AILERON HINGE FITTING LUG BORE AT RH HINGE NO 1, NO 2, NO 3 & NO 4 AND BOTH PCU OUTPUT LINK LUG BORES WERE R
- [SDR VNAA202311260010](https://openairdocs.org/sdr/VNAA202311260010.md): Aileron · corroded · Oct 8, 2023 · N559NN · Cndair CL6002D24 · Ailerons
  > CORROSION BORES ON AILERON HINGE FITTING LUG BORE AT RH WING REAR SPAR HINGE NO 1, NO 2, NO 3 & NO 4 WAS FOUND. CORROSION BORES ON AILERON HINGE FITTING LUG BORE AT RH WING REAR SPAR HINGE NO 1, NO 2, NO 3 & NO 4 WERE REPAIRED PER REO 690-57-51-306 REV. -A
- [SDR VNAA202311260009](https://openairdocs.org/sdr/VNAA202311260009.md): Aileron · worn · Oct 8, 2023 · N559NN · Cndair CL6002D24 · Ailerons
  > AFTER REMOVAL OF RH AILERON BUSHINGS, BEARINGS AND HARDWARE, WEAR AT SEVERAL LOCATIONS (OUTER FACES OF LUGS) OF RH AILERON CENTER HINGE FITTING. (OUTER FACES OF LUGS) OF RH AILERON CENTER HINGE FITTING. WERE REPAIRED PER REO. 690-57-61-305. REV. --
- [SDR VNAA202311260008](https://openairdocs.org/sdr/VNAA202311260008.md): Floorbeam · corroded · Oct 8, 2023 · N559NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > AFTER FLOOR SUPPORT LBL 11 TO RBL 11 FS280 REMOVAL, CORROSION ON FLOOR STRUCTURE CROSSBEAM AT FS280.00. FLOOR STRUCTURE CROSSBEAM AT FS280.00 WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01
- [SDR VNAA202311250003](https://openairdocs.org/sdr/VNAA202311250003.md): Post · corroded · Oct 8, 2023 · N559NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR POST BL 11.16 RH LOWER SIDE AT BULKHEAD FS 280.00. FLOOR POST BL 11.16 RH LOWER SIDE AT BULKHEAD FS 280.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42
- [SDR VNAA20231120002](https://openairdocs.org/sdr/VNAA20231120002.md): Skin · worn · Oct 8, 2023 · N559NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > WEAR ON SETTLEMENT AREA OF ACCESS PANEL 686AB. WEAR ON SETTLEMENT AREA OF ACCESS PANEL 686AB WAS REPAIRED PER EA 23-C9-57-1447 REV IR SECTION III PERMANENT REPAIR.
- [SDR VNAA202311260007](https://openairdocs.org/sdr/VNAA202311260007.md): Bracket · corroded · Oct 5, 2023 · N559NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON BRACKETS, MACHINED (4EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT. DUE TO BRACKETS MACHINED (4EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT NOT ALLOWABLE DAMAGE PER CRJ900 SRM 53-32-58-101-001-A01 WERE REPLACED PER CRJ900 SRM 51-42-2
- [SDR VNAA202311260004](https://openairdocs.org/sdr/VNAA202311260004.md): Floor Support · corroded · Oct 5, 2023 · N559NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON UPPER FACE OF FLOOR BEAM RBL 27 BTW FS 1000.00 TO FS 1069.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE. FLOOR BEAM RBL 27 BTW FS 1000.00 TO FS 1069.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE WAS REPAIRED PER EA 23-C9-53-1504 REV. IR
- [SDR VNAA202311260001](https://openairdocs.org/sdr/VNAA202311260001.md): Skin · dented · Oct 4, 2023 · N559NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > SEVERAL DENTS ON FUSELAGE SKIN, SETTLEMNT AREA OF RIGHT VENTRAL FIN FAIRING BTW FS 1069.75 TO REAR SPAR DATUM STABILIZER 67.5%, BTW STGR 22RH TO STGR 21RH. DENTS ON FUSELAGE SKIN, SETTLEMNT AREA OF RIGHT VENTRAL FIN FAIRING BTW FS 1069.75 TO REAR SPAR DATUM ST
- [SDR VNAA202311250020](https://openairdocs.org/sdr/VNAA202311250020.md): Skin · dented · Oct 4, 2023 · N559NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > SEVERAL DENTS ON FUSELAGE SKIN, SETTLEMNT AREA OF LEFT VENTRAL FIN FAIRING BTW FS 1069.75 TO REAR SPAR DATUM STABILIZER 67.5%, BTW STGR 22LH TO STGR 21LH. DENTS ON FUSELAGE SKIN, SETTLEMNT AREA OF LEFT VENTRAL FIN FAIRING BTW FS 1069.75 TO REAR SPAR DATUM STA
- [SDR VNAA202311250019](https://openairdocs.org/sdr/VNAA202311250019.md): Hinge · excess play · Oct 4, 2023 · N559NN · Cndair CL6002D24 · Rudder Structure
  > AFTER RUDDER REMOVAL, FREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. RUDDER HINGE FITTINGS NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WAS REPLACED PER CRJ-9
- [SDR VNAA202311260005](https://openairdocs.org/sdr/VNAA202311260005.md): Floor Support · corroded · Oct 3, 2023 · N559NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON UPPER FACE OF FLOOR BEAM LBL 9 BTW FS 1006.00 TO FS 1057.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE. FLOOR BEAM LBL 9 BTW FS 1006.00 TO FS 1057.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE WAS REPAIRED PER EA 23-C9-53-1479 REV. IR
- [SDR VNAA202311260003](https://openairdocs.org/sdr/VNAA202311260003.md): Floor Support · corroded · Oct 3, 2023 · N559NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON UPPER FACE OF FLOOR BEAM RBL 9 BTW FS 1000.00 TO FS 1069.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE. FLOOR BEAM RBL 9 BTW FS 1000.00 TO FS 1069.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE WAS REPAIRED PER EA 23-C9-53-1491 REV. IR SECTION III - P
- [SDR VNAA202311250018](https://openairdocs.org/sdr/VNAA202311250018.md): Seat Track · corroded · Oct 3, 2023 · N559NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON SEAT RAIL LBL9 BTW FS 581 TO FS 669.40 (2EA´S). SEAT RAIL LBL9 BTW FS 581 TO FS 669.40 WAS REPLACED PER CRJ900 AMM 53-00-49
- [SDR VNAA202311250017](https://openairdocs.org/sdr/VNAA202311250017.md): Seat Track · corroded · Oct 3, 2023 · N559NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON SEAT RAIL RBL9 BTW FS585 TO FS 669.40 (3EA´S). SEAT RAIL RBL9 BTW FS585 TO FS 669.40 (3EA´S) WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-31-49-101-001-A02 AND WAS REPLACED PER CRJ900 AMM 53-00-49
- [SDR VNAA202311250016](https://openairdocs.org/sdr/VNAA202311250016.md): Hinge · worn · Oct 3, 2023 · N559NN · Cndair CL6002D24 · Fuselage, Door Hinge
  > WEAR ON SEVERAL LUG OF PASSENGER DOOR HINGE (PASSENGER DOOR SIDE) WERE BLENDED OUT AND REWORKED AREA WAS MEASURED AND FOUND WITH THE FOLLOWING DIMENTION: MINIMUM REMAINING LUG WALL THICKNESS IS 0.104IN, THEREFORE REWORKED AREAS ARE WITHIN LIMITS PER CRJ-900 SR
- [SDR VNAA202311250015](https://openairdocs.org/sdr/VNAA202311250015.md): Hinge · worn · Oct 3, 2023 · N559NN · Cndair CL6002D24 · Fuselage, Door Hinge
  > WEAR ON SEVERAL LUG LANDS OF PASSENGER DOOR HINGE (FUSELAGE SIDE). LUG LANDS OF PASSENGER DOOR HINGE (FUSELAGE SIDE) WAS REPAIRED PER REO 690-53-21-1668 REV.--
- [SDR VNAA202311250014](https://openairdocs.org/sdr/VNAA202311250014.md): Angle · corroded · Oct 3, 2023 · N559NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON MID CAP ANGLE ON STGR 18LH BTW FS 310.00 TO FS 349.00 AT PASSENGER DOOR FUSELAGE FRAME. MID CAP ANGLE ON STGR 18LH BTW FS 310.00 TO FS 349.00 AT PASSENGER DOOR FUSELAGE FRAME WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-23-101-001-A02 AND RE
- [SDR VNAA202311250013](https://openairdocs.org/sdr/VNAA202311250013.md): Angle · corroded · Oct 3, 2023 · N559NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON LOWER ANGLE KICK PLATE ON STGR 18LH BTW FS 310.00 TO FS 349.00 AT PASSENGER DOOR FUSELAGE FRAME. LOWER ANGLE KICK PLATE ON STGR 18LH BTW FS=310.00 TO FS= 349.00 WAS REPLACED PER SRM 51-42-06-001-001-A01
- [SDR VNAA202311250012](https://openairdocs.org/sdr/VNAA202311250012.md): Striker · corroded · Oct 3, 2023 · N559NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION AT SEAL STRIKER BTW FS 320.00 TO FS 349.00 OF SERVICE DOOR SURROUND STRUCTURE SEAL STRIKER BTW FS 320.00 TO FS 349.00 OF SERVICE DOOR SURROUND STRUCTURE WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01
- [SDR VNAA202311250007](https://openairdocs.org/sdr/VNAA202311250007.md): Skin · corroded · Oct 3, 2023 · N559NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > CORROSION ON FUSELAGE SKIN FS= 319.00 TO FS= 333.00 BTWN STGR 25RH TO STGR 24RH AT MAIN AVIONICS COMPARTMENT. FUSELAGE SKIN FS= 319.00 TO FS= 333.00 BTWN STGR 25RH TO STGR 24RH AT MAIN AVIONICS COMPARTMENT WAS REPAIRED PER EA 23-C9-53-1547 REV. IR SECTION III
- [SDR VNAA202311250006](https://openairdocs.org/sdr/VNAA202311250006.md): Seat Track · corroded · Oct 3, 2023 · N559NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SIDE SEAT RAIL AT STGR 15 RH, BTW FS 847.00 + 19.00 TO FS900.00. RH SIDE SEAT RAIL AT STGR 15 RH, BTW FS 847.00 + 19.00 TO FS900.00 WAS REPLACED PER CRJ900 AMM 53-00-49
- [SDR VNAA202311250005](https://openairdocs.org/sdr/VNAA202311250005.md): Seat Track · corroded · Oct 3, 2023 · N559NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SIDE SEAT RAIL AT STGR 15 RH, BTW FS785.15 TO FS847.00 + 8.00. CORROSION ON RH SIDE SEAT RAIL AT STGR 15 RH, BTW FS785.15 TO FS847.00 + 8.00 WAS REPLACED PER CRJ900 AMM 53-00-49

Next page: https://openairdocs.org/aircraft/N559NN/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 = 'N559NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N559NN/reports

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