# Service difficulty reports: N563NN

A list on [N563NN](https://openairdocs.org/aircraft/N563NN.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 · 70 reports

- [SDR VNAA202606120003](https://openairdocs.org/sdr/VNAA202606120003.md): Skin · damaged · May 9, 2026 · N563NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE ON SEVERAL FASTENERS BTW STR 23L AND BS 210 - 265. LIGHTNING STRIKE ON SEVERAL FASTENERS BTW STGR 23L AND BS 210 - 265 WERE REPAIRED IAW SRM 53-00-00-201-003-A01.
- [SDR VNAA202606120022](https://openairdocs.org/sdr/VNAA202606120022.md): Fitting · corroded · May 7, 2026 · N563NN · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings
  > CORROSION FLOOR FITTING IN AFT ACCESS 109 (1EA) ON GALLEY 1. FLOOR FITTING P/N CDSP2019-7C-620 IN AFT ACCESS 109 (1EA) ON GALLEY 1 WAS REPLACED PER SAFRAN CMM 25-33-96
- [SDR VNAA202606120020](https://openairdocs.org/sdr/VNAA202606120020.md): Floor Support · cracked · May 6, 2026 · N563NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON FLOOR SUPPORT RBL 12.0 BTW FS 221.73 TO FS 229 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE) BELOW WL 79.50. CRACKED ON FLOOR SUPPORT RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT
- [SDR VNAA202606120019](https://openairdocs.org/sdr/VNAA202606120019.md): Seat Track · corroded · May 5, 2026 · N563NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SIDE SEAT RAIL 15RH (5EAS) BTW FS669.40 TO FS977. SIDE SEAT RAIL 15RH (5EAS) BTW FS669.40 TO FS977.00 AREA IS OUT LIMITS PER CRJ-900 SRM 53-31-43-101-001-A01 AND SEAT RAIL 15RH (5EAS) BTW FS669.40 TO FS977.00 WERE REPLACED PER CRJ-900 AMM 53-00-4
- [SDR VNAA202606120018](https://openairdocs.org/sdr/VNAA202606120018.md): Seat Track · corroded · May 5, 2026 · N563NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SIDE SEAT RAIL 15LH (7EAS) BTW FS669.40 TO FS977. SIDE SEAT RAIL 15LH (4EAS) BTW FS847+8 TO FS977.00 WERE EVALUATED EXCESSIVE DAMAGE PER CRJ-900 SRM 53-41-49-101-001-A02 AND CRJ-900 SRM 53-51-49-101-001-A02 AND REPLACED PER CRJ-900 AMM 53-00-49-400-
- [SDR VNAA202606120017](https://openairdocs.org/sdr/VNAA202606120017.md): Seat Track · corroded · May 5, 2026 · N563NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > SEVERAL DAMAGES FOUND ON ALL THREE VISIBLE SEAT RAILS ABOVE FLOOR FS477.40 TO FS693.00 AT 9LBL/9RBL (WEAR, NICKS, SCRATCHES, CORROSION, SECTIONS AT FS 477 TO 661+32 ON 9RBL WERE CLEANED PER CRJ900 SRM 51-26-00-001-001-A01 AND NO DAMAGE FOUND, CORROSION ON SE
- [SDR VNAA202606120016](https://openairdocs.org/sdr/VNAA202606120016.md): Seat Track · corroded · May 5, 2026 · N563NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > SEVERAL DAMAGES FOUND (WEAR,SCRATCHES, NICKS, CORROSION, GOUGES) ON ALL LH/RH THREE SEAT RAILS ABOVE FLOOR FS280.00 TO FS477.4. DUE EXCESIVE DAMAGE ON ALL LH/RH THREE SEAT RAILS ABOVE FLOOR FS280.00 TO FS477.40 WERE REPLACED PER CRJ-900 SRM 53-21-49-101-001-
- [SDR VNAA202606120015](https://openairdocs.org/sdr/VNAA202606120015.md): Seat Track · corroded · May 5, 2026 · N563NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > SEVERAL DAMAGES ( NICKS, GOUGES, WEAR, CORROSION, SCRATCHES) ON SIDE SEAT RAILS BOTH L/H AND R/H FS379.00 TO FS669.40 STRG15. SEVERAL DAMAGES (NICKS, GOUGES, WEAR, CORROSION, SCRATCHES) ON SIDE SEAT RAILS BOTH L/H AND R/H FS379.00 TO FS669.40 STRG15 WERE EVA
- [SDR VNAA202606120014](https://openairdocs.org/sdr/VNAA202606120014.md): Floor Support · corroded · May 5, 2026 · N563NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT BETWEEN FS=1015 TO FS=1031 LBL27 AT AFT BAGAGGE BAY. FLOOR SUPPORT BETWEEN FS=1015 TO FS=1031 LBL27 AT AFT BAGAGGE BAY. WAS REPAIRED PER SRM 53-00-41-201-001-A03.
- [SDR VNAA202606120013](https://openairdocs.org/sdr/VNAA202606120013.md): Floor Support · corroded · May 5, 2026 · N563NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT FS=280.00 BTW RBL 9 AND LBL 9 AT FWD PASSENGER CABIN STRUCTURE. CORROSION ON FLOOR SUPPORT FS=280.00 BTW RBL 9 AND LBL 9 AT FWD PASSENGER CABIN STRUCTURE WAS EVALUATED OUT LIMITS PER SRM 53-00-00-101-001-A01 AND REPLACED PER SRM 51
- [SDR VNAA202606120012](https://openairdocs.org/sdr/VNAA202606120012.md): Fitting · corroded · May 5, 2026 · N563NN · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings
  > CORROSION ON FITTINGS SUPPORT (2 EAS) OF GALLEY ATTACHMENT FITTING FS=285.00 RBL 17 AND FS=288.00 LBL 20 AT FWD CPAX CABIN STRUCTURE. CORROSION ON FITTINGS SUPPORT (2 EAS) OF GALLEY ATTACHMENT FITTING FS=285.00 RBL 17 AND FS=288.00 LBL 20 AT FWD CPAX CABIN ST
- [SDR VNAA202606120011](https://openairdocs.org/sdr/VNAA202606120011.md): Bracket · corroded · May 5, 2026 · N563NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON MACHINED BRACKETS (5 EAS) STA FS=661, FS=565 AND FS=517 AT INTERNAL STRUCTURE FWD/CTR BAGGAGE BAY. PAINT ON MACHINED BRACKETS STA FS=661 (2EAS), AND FS=517 (1EAS) AT INTERNAL STRUCTURE FWD/CTR BAGGAGE BAY WERE REMOVED PER CRJ-900 SRM 51-26-01-00
- [SDR VNAA202606120010](https://openairdocs.org/sdr/VNAA202606120010.md): Cap · corroded · May 4, 2026 · N563NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON KICKPLATE AND MID CAP BTW FS 310.00 TO FS 349.00 AT SURROUND STRUCTURE PASSENGER DOOR. CORROSION ON KICKPLATE BTW BS 310 TO 349 AT SURROUND STRUCTURE PASSENGER DOOR WAS REMOVED PER SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN LIMITS PER SRM 53-0
- [SDR VNAA202606120009](https://openairdocs.org/sdr/VNAA202606120009.md): Floorbeam · cracked · May 4, 2026 · N563NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > DURING D.I OF THE TASK CARD: 53-10-219B CRACK WAS DETECTED ON UNDER FLOORBEAM AT F.S 280.00 RBL 12. FLOORBEAM AT F.S 280.00 RBL 12. WAS REPAIRED PER REO 690-53-11-2187 REV.- -
- [SDR VNAA202606120008](https://openairdocs.org/sdr/VNAA202606120008.md): Rib · cracked · May 3, 2026 · N563NN · Cndair CL6002D24 · Leading Edge Devices
  > CRACK ON RIB OF LEADING EDGE SS 58.00 AT RT WING. CRACK ON RIB OF LEADING EDGE SS 58.00 AT RT WING WAS REPLACED IAW SRM 51-42-06-001-001-A01, AND SRM 51-42-10-001-001-A01, AND SRM 51-42-21-001-001-A01.
- [SDR VNAA202606120007](https://openairdocs.org/sdr/VNAA202606120007.md): Rib · cracked · May 3, 2026 · N563NN · Cndair CL6002D24 · Leading Edge Devices
  > CRACK ON RIB OF LEADING EDGE STA SS 58.00 AT LH WING. CRACK ON RIB OF LEADING EDGE SS 58.00 AT LT WING WAS REPLACED IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-10-001-001-A01 AND SRM 51-42-21-001-001-A01.
- [SDR VNAA202606120006](https://openairdocs.org/sdr/VNAA202606120006.md): Web · cracked · May 1, 2026 · N563NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON ELECTRICAL BAY WEB FLOOR LH SIDE FS193. CRACK ON ELECTRICAL BAY WEB FLOOR LH SIDE FS193 WAS REPAIRED PER CRJ-900 SRM 53-11-43-201-001-A01.
- [SDR VNAA202606120005](https://openairdocs.org/sdr/VNAA202606120005.md): Web · cracked · May 1, 2026 · N563NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193. ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00. WAS REPAIRED PER CRJ-900 SRM 53-11-43-201-001-A01
- [SDR VNAA202606120004](https://openairdocs.org/sdr/VNAA202606120004.md): Bracket · corroded · Apr 30, 2026 · N563NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON BRACKET (FWD SURFACE) OF CONNECTOR HARNESSES AT LT (PX19P1 AND PX34P1) RT (PX17P1 AND PX33P1) MLG WHEEL WELL. CORROSION ON BRACKET (FWD SURFACE) OF CONNECTOR HARNESSES AT LH(PX19P1 AND PX34P1) / RH(PX17P1 AND PX33P1) MLG WHEEL WELL WAS REMOVED P
- [SDR VNAA202606120002](https://openairdocs.org/sdr/VNAA202606120002.md): Skin · nicked · Apr 28, 2026 · N563NN · Cndair CL6002D24 · Trailing Edge Flaps
  > SEVERAL NICKS ON INNER SURFACE OF INB FLAP AT LT & RT WING. INNER SURFACE OF INB FLAP AT LT WING WAS BLEND OUT PER SRM 51-12-00-001-001-A01, AND EVALUATED WITHIN LIMITS IAW SRM 57-52-01-101-001-A01. AND INNER SURFACE OF INB FLAP AT RT WING WAS REPAIRED PER SR
- [SDR VNAA202606120001](https://openairdocs.org/sdr/VNAA202606120001.md): Skin · corroded · Apr 28, 2026 · N563NN · Cndair CL6002D24 · Wing, Plate/Skin
  > CORROSION ON LOWER SKIN BTW WS405 TO WS413 APPROX AT LH WING. CORROSION ON LOWER SKIN BTW WS405 TO WS413 APPROX AT LH WING WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01, EVALUATED OUT LIMITS PER CRJ900 SRM 57-00-01-101-001-A03 AND REPLACED PER CRJ-900 SRM
- [SDR VNAA2024031111101](https://openairdocs.org/sdr/VNAA2024031111101.md): Servo · failed · Mar 7, 2024 · N563NN · Cndair CL6002D24 · Flight Control System
  > ON APPROACH WITH AUTOPILOT OFF COULD NOT PUSH CONTROL COLUMN FORWARD EASILY CAUSING GO AROUND / PERFORMED THE OPERATION TEST OF THE ELEVATOR CONTROL SYSTEM IAW CRJ900 AMM 27-31-00-710-801. PERFORMED THE FUNCTIONAL TEST OF THE PITCH FEEL SYSTEM IAW CRJ900 AMM 2
- [SDR VNAA2024021100025](https://openairdocs.org/sdr/VNAA2024021100025.md): Web · cracked · Feb 11, 2024 · N563NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PAX DOOR FORWARD WEB IS CRACKED. REMOVED AND REPLACED PAX DOOR FORWARD WEB I.A.W. BOMBARDIER CRJ900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-14-001-001-A01
- [SDR VNAA2024F00000](https://openairdocs.org/sdr/VNAA2024F00000.md): Web · cracked · Feb 11, 2024 · N563NN · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR FORWARD WEB IS CRACKED. REMOVED AND REPLACED PAX DOOR FORWARD WEB I.A.W. BOMBARDIER CRJ900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-14-001-001-A01
- [SDR VNAA2024021100024](https://openairdocs.org/sdr/VNAA2024021100024.md): Cowling · chafed · Feb 11, 2024 · N563NN · Cndair CL6002D24 · Nacelle/Pylon, Main Frame
  > CHAFE ON R/H ENGINE UPPER FAN COWL INNER SURFACE ON INTERNAL DOUBLER NEAR FWD LATCH, MARKED WITH TAPE INSTALLED NEW R/H UPPER FAN COWL INTERNAL DOUBLER P/N CN622-0430-205 IAW CRJ900 SRM 51-42-13-001-001-A01 HN00130177 DISCREPANCY: CHAFE ON R/H ENGINE UPPER
- [SDR VNAA2024021100023](https://openairdocs.org/sdr/VNAA2024021100023.md): Seat Track · corroded · Feb 11, 2024 · N563NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > SIDE SEAT RAIL AT STGR 15R IS CORRODED BETWEEN FS 847+16 AND FS 897. REMOVED AND FABRICATED NEW SIDE SEAT RAIL AT STRR 15 BETWEEN FS 847 +16 TO FS 897 IAW CRJ 900 REO 670-53-00-587 REV C DATED 2023-02-08. INSTALLED NEW SEAT RAIL IAW CRJ 900 AMM 53-00-49-400-
- [SDR VNAA2024021100022](https://openairdocs.org/sdr/VNAA2024021100022.md): Seat Track · corroded · Feb 11, 2024 · N563NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > SIDE SEAT RAIL AT STGR 15R IS CORRODED BETWEEN FS 785.15 AND FS 847+8. REMOVED AND FABRICATED NEW SIDE SEAT RAIL AT STRR 15 BETWEEN FS 785.15 TO FS 847+8 IAW CRJ 900 REO 670-53-00-587 REV C DATED 2023-02-08. INSTALLED NEW SEAT RAIL IAW CRJ 900 AMM 53-00-49-4
- [SDR VNAA2024021100021](https://openairdocs.org/sdr/VNAA2024021100021.md): Seat Track · corroded · Feb 11, 2024 · N563NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > SIDE SEAT RAIL AT STGR 15R IS CORRODED BETWEEN FS 670 AND FS 720.85. REMOVED AND FABRICATED NEW SIDE SEAT RAIL AT STR. R 15 BETWEEN FS 670 TO FS 720.85 IAW CRJ 900 REO 670-53-00-587 REV C DATED 2023-02-08. INSTALLED NEW SEAT RAIL IAW CRJ 900 AMM 53-00-49-400-
- [SDR VNAA2024021100020](https://openairdocs.org/sdr/VNAA2024021100020.md): Seat Track · corroded · Feb 11, 2024 · N563NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > SIDE SEAT RAIL AT STGR 15L IS CORRODED BETWEEN FS 785.15 AND FS 847+8. REMOVED AND FABRICATED NEW SIDE SEAT RAIL AT STR15L BETWEEN FS 785.15 TO FS 847+8 IAW CRJ 900 REO 670-53-00-587 REV C DATED 2023-02-08. INSTALLED NEW SEAT RAIL IAW CRJ 900 AMM 53-00-49-40
- [SDR VNAA2024021100019](https://openairdocs.org/sdr/VNAA2024021100019.md): Skin · dented · Feb 11, 2024 · N563NN · Cndair CL6002D24 · Trailing Edge Flaps
  > HN00129326: DISCREPANCY: R/H INBOARD FLAP HAS (1EA) DENT BETWEEN F.L.S. 15.00 AND F.L.S. 24.00 NEAR TRAILIND EDGE ON LOWER SKIN. CORRECTIVE ACTION: REPAIRED DENTED LOWER SKIN IAW CRJ 900 SRM 57-52-01-201-001-A01 TYPE IV REPAIR.
- [SDR VNAA2024021100018](https://openairdocs.org/sdr/VNAA2024021100018.md): Drag Angle · cracked · Feb 11, 2024 · N563NN · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT DRAG ANGLE IS CRACKED AT MOTOR ASSIST PULLEY LOCATION. REMOVED AFT DRAG ANGLE IAW CRJ900 SRM 51-42-06-001-001-A01. INSTALLED NEW SERVICEABLE DRAG ANGLE P/N 601R31772-5S IAW CRJ900 SRM 51-42-06-001-001-A01
- [SDR VNAA2024021100017](https://openairdocs.org/sdr/VNAA2024021100017.md): Drag Angle · cracked · Feb 11, 2024 · N563NN · Cndair CL6002D24 · Vertical Stabilizer
  > VERTICAL STABILIZER, L/H AFT DRAG ANGLE IS CRACKED. INSTALLED NEW SERVICEABLE L/H AFT DRAG ANGLE IAW CRJ 900 SRM 51-42-21-001-001-A01 AND 51-42-13-001-001-A01
- [SDR VNAA2024021100016](https://openairdocs.org/sdr/VNAA2024021100016.md): Plate · corroded · Feb 11, 2024 · N563NN · Cndair CL6002D24 · Fuselage, Door Hinge
  > CORROSION FOUND ON FORWARD LAV OUTBOARD FORWARD MOUNTING PLATE. REMOVED AND REPLACED PLATE I.A.W. CRJ900 SRM 51-41-02-001-001-A01.
- [SDR VNAA2024021100015](https://openairdocs.org/sdr/VNAA2024021100015.md): Hinge · corroded · Feb 11, 2024 · N563NN · Cndair CL6002D24 · Fuselage, Door Hinge
  > PAX DOOR PIANO HINGE IS WORN/CHAFED. REMOVED AND REPLACED PAX DOOR PIANO HINGE IAW CRJ-900 SRM 53-21-23-201-007-A01
- [SDR VNAA2024021100014](https://openairdocs.org/sdr/VNAA2024021100014.md): Plate · corroded · Feb 11, 2024 · N563NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FORWARD LAV, OUTBOARD FORWARD MOUNTING PLATE CORRODED. REMOVED AND REPLACED PLATE I.A.W. CRJ900 SRM 51-24-36-001-001-A01, 51-40-11-001-001-A01 AND 51-21-16-001-001-A01.
- [SDR VNAA2024021100013](https://openairdocs.org/sdr/VNAA2024021100013.md): Cargo Track · corroded · Feb 11, 2024 · N563NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > FWD CARGO TIE DOWN PLATES AT FS 629.00 AND FS 661+16 JUST INBOARD OF STRINGER 27 ARE CORRODED ON UPPER SURFACE. REMOVED AND REPLACED FWD AND AFT TIE DOWN PLATES IAW CRJ900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01,51-45-00-001-001-
- [SDR VNAA2024021100012](https://openairdocs.org/sdr/VNAA2024021100012.md): Cargo Track · corroded · Feb 11, 2024 · N563NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > HN00131132: DISCREPANCY: FWD CARGO TIE DOWN PLATES AT FS 517.00 AND FS 565.00 JUST INBOARD OF STRINGER 27 ARE CORRODED ON UPPER SURFACE. CORRECTIVE ACTION: REMOVED AND REPLACED FWD AND AFT TIE DOWN PLATES IAW CRJ900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A
- [SDR VNAA2024021100011](https://openairdocs.org/sdr/VNAA2024021100011.md): Intercostal · corroded · Feb 11, 2024 · N563NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PAX DOOR INTERCOSTAL BETWEEN FS347 AND FS 335 AT DATUM 4 IS CORRODED. REMOVED AND REPLACED INTERCOSTAL AT DATUM 4 FS 347 AND FS 335 IAW CRJ900 SRM 51-42-06-001-001-A01.
- [SDR VNAA2024021100010](https://openairdocs.org/sdr/VNAA2024021100010.md): Skin · corroded · Feb 11, 2024 · N563NN · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR INNER SKIN CORRODED AROUND MULTIPLE FASTENERS. REMOVED AND REPLACED PAX DOOR INNER SKIN I.A.W. BOMBARDIER CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-14-001-001-A01 601R318024-15S
- [SDR VNAA202402110009](https://openairdocs.org/sdr/VNAA202402110009.md): Former · corroded · Feb 11, 2024 · N563NN · Cndair CL6002D24 · Passenger/Crew Doors
  > FOUND AFT FORMER ON PAX DOOR TO BE CORRODED AROUND SEVERAL FASTENER HOLES. REMOVED AFT PAX DOOR FORMER IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 AND 51-42-14-001-001-A01. INSTALLED NEW P/N 601R318034-5 AFT PAX DOOR FORMER IAW CRJ900 SRM 51
- [SDR VNAA202402110008](https://openairdocs.org/sdr/VNAA202402110008.md): Angle · distorted · Feb 11, 2024 · N563NN · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > LH UPPER ANGLE ON THE AFT FACE OF THE FS 280 BULKHEAD IS BENT AND DISTORTED. LOCATED AND DRILLED NEW SERVICEABLE STIFFENING ANGLE PN: CC670-34249-1 IAW CRJ-900 SRM 51-40-11-001-001-A01.
- [SDR VNAA202402110007](https://openairdocs.org/sdr/VNAA202402110007.md): Seat Track · corroded · Feb 11, 2024 · N563NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SIDE SEAT RAIL CORRODED STR 15R FS 744.15 TO FS 761.85. REMOVED AND REPLACED WITH NEW PN: SH690-36285-1 CABIN SIDE SEAT TRACK AT STR 15R FS 744.15 TO FS 761.85 IAW CRJ 900 AMM 53-00-49-000-801. (CONFIG. A12).
- [SDR VNAA202402110006](https://openairdocs.org/sdr/VNAA202402110006.md): Mount · corroded · Feb 11, 2024 · N563NN · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings
  > SUSPECTED CORROSION FOUND ON FWD LAV OUTBOARD FWD MOUNTING PLATE. REMOVED FWD LAV OUTBOARD FWD MOUNTING PLATE IAW CRJ900 SRM 51-41-02-001-001-A01. INSTALLED NEW FWD MOUNT PLATE PN: CDSP2023-0990 TO FWD LAV IAW SRM 51-41-02-001-001-A01.
- [SDR VNAA202402110005](https://openairdocs.org/sdr/VNAA202402110005.md): Seat Track · corroded · Feb 11, 2024 · N563NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT RAIL AT RBL9 HAS CORROSION FS581-661+32. REMOVED AND REPLACED RBL9 SEAT RAIL BETWEEN FS 581 AND FS 661+32 IAW CRJ-900 AMM 53-00-49-400-801-A12.
- [SDR VNAA202402110004](https://openairdocs.org/sdr/VNAA202402110004.md): Seat Track · corroded · Feb 11, 2024 · N563NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > RBL9 SEAT RAIL AT FS501 HAS CORROSION. REMOVED AND REPLACED WITH NEW PN: SH690-33407-1 SEAT RAIL AT FS 501 RBL 9 IAW CRJ 900 AMM 53-00-49-000-801. (CONFIG. A12).
- [SDR VNAA202402110003](https://openairdocs.org/sdr/VNAA202402110003.md): Seat Track · corroded · Feb 11, 2024 · N563NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > N00130578: DISCREPANCY: RBL9 SEAT RAIL HAS CORROSION BETWEEN FS477 AND FS485 CORRECTIVE ACTION: REMOVED RBL9 SEAT RAIL BETWEEN FS477 AND FS485 IAW CRJ900 AMM 53-00-49-000-801(CONFIG A12). INSTALLED NEW SERVICEABLE SEAT RAIL WITH P/N SH690-33407-1 AT RBL9 IAW C
- [SDR VNAA202402110002](https://openairdocs.org/sdr/VNAA202402110002.md): Seat Track · corroded · Feb 11, 2024 · N563NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 SEAT RAIL BETWEEN FS409 AND FS469 HAS GOUGES AND CORROSION. REMOVED SEAT RAIL AT RBL9 BETWEEN FS208 TO FS477.40 IAW CRJ900 AMM 53-00-49-000-801( CONFIG A12). INSTALLED NEW SERVICEABLE SEAT RAIL WITH P/N SH670-32159-1 AT RBL9 BETWEEN FS208 TO FS477.40 I
- [SDR VNAA202402110001](https://openairdocs.org/sdr/VNAA202402110001.md): Web · cracked · Feb 11, 2024 · N563NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > HN00130391: DISCREPANCY: PAX DOOR AFT WEB IS CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED PAX DOOR AFT WEB I.A.W. BOMBARDIER CRJ900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-14-001-001-A01.
- [SDR VNAA202307051112](https://openairdocs.org/sdr/VNAA202307051112.md): Adc · unserviceable · Jul 2, 2023 · N563NN · Cndair CL6002D24 · Air Data Computer
  > MOMENTARY LOSS OF ADC 1 AFTER ROTATION / REMOVED AND REPLACED ADC #1 IAW CRJ 900 AMM 34-13-01-000/400-801-A01-PSA. PERFORMED FUNCTIONAL TEST OF THE #1 ATC ALTTITUDE REPORTING (MODE C) IAW CRJ 900 AMM 34-54-00-720-802. FUCNTIONAL TEST GOOD. IFR 6000 USED FOR TE
- [SDR VNAA202307051111](https://openairdocs.org/sdr/VNAA202307051111.md): Adc · unserviceable · Jul 2, 2023 · N563NN · Cndair CL6002D24 · Air Data Computer
  > MOMENTARY LOSS OF ADC 2 AT V1 / REMOVED AND REPLACED ADC #2 IAW CRJ 900 AMM 34-13-01-000/400-801-A01-PSA. PERFORMED FUNCTIONAL TEST OF THE #2 ATC ALTTITUDE REPORTING (MODE C) IAW CRJ 900 AMM 34-54-00-720-802. FUCNTIONAL TEST GOOD. IFR 6000 USED FOR TEST. / "

Next page: https://openairdocs.org/aircraft/N563NN/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 = 'N563NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N563NN/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.