# Service difficulty reports: N560NN

A list on [N560NN](https://openairdocs.org/aircraft/N560NN.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 · 52 reports

- [SDR VNAA2026062619801](https://openairdocs.org/sdr/VNAA2026062619801.md): Fan · failed · Jun 23, 2026 · N560NN · Cndair CL6002D24 · Air Distribution Fan
  > RECIRCULATION FAN FAULT MESSAGE. DEFERRED RECIRCULATION FAN NR 2 IAW MEL 21-22-01-2 CAT C. FC FUNCTION C/W BY PULLING AND COLLARING CBP-2 A5, B11. REMOVED AND REPLACED #2 RECIRCULATION FAN IAW CRJ900 AMM TASK21€“22€“10€“000/400€“801. OPS CHECK GOOD, THIS
- [SDR VNAA2026032414601](https://openairdocs.org/sdr/VNAA2026032414601.md): O-Ring · leaking · Mar 22, 2026 · N560NN · Cndair CL6002D24 · Turbine Engine Oil System
  > R ENG OIL PRESSURE WARNING ON CLIMB OUT FOLLOWED QRH / REMOVED RH ATS IAW CRJ 900 AMM 80-11-01-000-801-A01 AND FOUND O-RING ON SPLINED SHAFT TO BE INSTALLED INCORRECTLY, FOUND OIL ON UNDERSWIDE OF THE HOUSING SEEPING OUT FROM THE GEAR BOX. REMOVED AND REINSTA
- [SDR VNAA2025010311101](https://openairdocs.org/sdr/VNAA2025010311101.md): Acm · smoke · Dec 31, 2024 · N560NN · Cndair CL6002D24 · Cabin Cooling System
  > AFTER THE LH ENGINE WAS STARTED, THERE WAS FUMES AND A LIGHT HAZE THROUGHOUT THE CABIN AND COCKPIT. THE PLANE WAS DEBOARDED AND NO MEDICAL ATTENTION WAS REQUIRED. THE FUMES AND SMOKE WENT AWAY AFTER THE ENGINES WERE SHUT DOWN. / REMOVED AND REPLACED ACM IAW CR
- [SDR VNAA202401030101](https://openairdocs.org/sdr/VNAA202401030101.md): Unknown · fumes · Dec 31, 2024 · N560NN · Cndair CL6002D24 · Air Distribution System
  > AFTER THE LH ENGINE WAS STARTED, THERE WAS FUMES AND A LIGHT HAZE THROUGHOUT THE CABIN AND COCKPIT. THE PLANE WAS DEBOARDED AND NO MEDICAL ATTENTION WAS REQUIRED. THE FUMES AND SMOKE WENT AWAY AFTER THE ENGINES WERE SHUT DOWN. / SYSTEM IS DEFERRED AND WILL REQ
- [SDR VNAA2024101511101](https://openairdocs.org/sdr/VNAA2024101511101.md): Sensor · false indication · Oct 13, 2024 · N560NN · Cndair CL6002D24 · Landing Gear Brake System
  > BRAKE OVERHEAT WARNING MESSAGE, LEFT OUTBOARD BRAKE TEMP 20 AFTER TAKEOFF. REMOVED AND REPLACED THE LH OB THERMOCOUPLE IAW CRJ900 AMM 32-46-01-000/400-801-A01-PSA. SELF TEST GOOD.
- [SDR VNAA2023122811101](https://openairdocs.org/sdr/VNAA2023122811101.md): Probe · malfunctioned · Dec 25, 2023 · N560NN · Cndair CL6002D24 · Landing Gear Brake System
  > LH OB BTMS INDICATIONS ERRONEOUS AFTER TAKEOFF/ QRC/ QRH CW. / REMOVED AND REPLACED LHOB MLG BRAKE TEMPERATURE SENSOR IAW CRJ900 AMM 32-46-01-000/400-801-A01-PSA. OPERATIONAL CHECK GOOD.
- [SDR VNAA202312140008](https://openairdocs.org/sdr/VNAA202312140008.md): Skin · dented · Dec 3, 2023 · N560NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > DESCRIPTION: 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. CORRECTIVE ACTION: SEVERAL DENTS ON FUSELAGE SKIN, SETTLEMNT AREA OF LEFT VENTRAL FIN FAIRIN
- [SDR VNAA202312130015](https://openairdocs.org/sdr/VNAA202312130015.md): Support · cracked · Nov 30, 2023 · N560NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON REFUEL MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH. REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH WAS REPEIRED PER REO 690-28-25-012 REV--
- [SDR VNAA202312130016](https://openairdocs.org/sdr/VNAA202312130016.md): Bracket · corroded · Nov 29, 2023 · N560NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON BRACKET MACHINED (8EA'S) ON FLOOR STRUCTURE AT FWD CARGO COMPARTMENT BTW FS 517 TO FS 661.00+16.00 AND BTW STGR 23 RH TO 22LH. DUE TO NOT DAMAGE ALLOWABLE ON BRACKETS MACHINED (8 EA´S) ON FLOOR STRUCTURE AT FWD CARGO COMPARTMENT BTW FS 517 TO FS
- [SDR VNAA202312130021](https://openairdocs.org/sdr/VNAA202312130021.md): Floor Support · corroded · Nov 28, 2023 · N560NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > UPPER FACE OF FLOOR BEAM RBL 9 BTW FS 1000.00 TO FS 1047.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE. UPPER FACE OF FLOOR BEAM RBL 9 BTW FS 1000.00 TO FS 1047.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE WAS REPAIRED PER REO 690-53-61-1299. REV --
- [SDR VNAA202312130020](https://openairdocs.org/sdr/VNAA202312130020.md): Floor Support · corroded · Nov 28, 2023 · N560NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > DESCRIPTION: CORROSION ON UPPER FACE OF FLOOR BEAM LBL 9 BTW FS 1000.00 TO FS 1047.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE. CORRECTIVE ACTION: CORROSION ON UPPER FACE OF FLOOR BEAM LBL 9 BTW FS 1000.00 TO FS 1047.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE
- [SDR VNAA202312130019](https://openairdocs.org/sdr/VNAA202312130019.md): Floor Support · corroded · Nov 28, 2023 · N560NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON UPPER FACE OF FLOOR BEAM LBL27 BTW FS 1000.00 TO FS 1047.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE. UPPER FACE OF FLOOR BEAM LBL 27 BTW FS 1000.00 TO FS 1047.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE WAS REPAIRED PER REO 690-53-61-1293. REV.-
- [SDR VNAA202312130018](https://openairdocs.org/sdr/VNAA202312130018.md): Hinge Fitting · corroded · Nov 28, 2023 · N560NN · Cndair CL6002D24 · Ailerons
  > CORROSION ON AILERON HINGE FITTING LUG BORE NO. 4 OUTBOARD AT LH WING REAR SPAR. AILERON HINGE FITTING LUG BORE NO. 4 OUTBOARD AT LH WING REAR SPAR WAS REPAIRED PER ETI-900-23-006 REV. ORIGINAL & REO 690-57-51-315 REV. - -
- [SDR VNAA202312130017](https://openairdocs.org/sdr/VNAA202312130017.md): Hinge Fitting · corroded · Nov 28, 2023 · N560NN · Cndair CL6002D24 · Ailerons
  > CORROSION ON AILERON HINGE FITTING LUG BORE NO. 4 INBOARD AT RH WING REAR SPAR. AILERON HINGE FITTING LUG BORE NO. 4 INBOARD AT RH WING REAR SPAR WAS REPAIRED PER ETI-900-23-005 REV. ORIGINAL & REO 690-57-51-314 REV. - -
- [SDR VNAA202312130001](https://openairdocs.org/sdr/VNAA202312130001.md): Skin · worn · Nov 28, 2023 · N560NN · Cndair CL6002D24 · Wing, Plate/Skin
  > DESCRIPTION: WEAR ON LOWER WING SKIN RH/LH, WS264.00, WS128.00, WS178.00 (SETTLEMENT AREA OF WING ACCESS PANEL 686AB, 692AB, 586AB, 592AB AND 597AB). CORRECTIVE ACTION: LOWER WING SKIN RH /LH, WS264.00, WS128.00, WS178.00 (SETTLEMENT AREA OF WING ACCESS PANE
- [SDR VNAA202312140007](https://openairdocs.org/sdr/VNAA202312140007.md): Seat Track · corroded · Nov 27, 2023 · N560NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > DESCRIPTION: CORROSION ON FLOOR SEAT RAIL AT LBL 9.00 FROM FS 371.00 TO FS 681.00 CPAX. CORRECTIVE ACTION: FLOOR SEAT RAIL AT LBL 9.00 FROM FS 371.00 TO FS 485.00 CPAX WAS CLEANED PER CRJ900 SRM 51-26-00-001-001-A01 AND DETAILED VISUAL INSPECTION WAS PERFORMED
- [SDR VNAA202312140006](https://openairdocs.org/sdr/VNAA202312140006.md): Seat Track · corroded · Nov 27, 2023 · N560NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > DESCRIPTION: CORROSION ON FLOOR SEAT RAIL AT RBL 9.00 FROM FS 349.00 TO FS 681.00 CPAX CORRECTIVE ACTION: DUE TO EXCESSIVE DAMAGE ON FLOOR SEAT RAIL AT RBL 9.00 FROM FS 349.00 TO FS 681.00 CPAX WAS REPLACED PER CRJ-900 SRM 53-41-49-101-001-A02 AND CRJ900 AMM 5
- [SDR VNAA202312140003](https://openairdocs.org/sdr/VNAA202312140003.md): Seat Track · corroded · Nov 21, 2023 · N560NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAIL STGR 15 RH BTW FS 785.15 TO FS 847 + 48.00. DUE TO EXCESSIVE DAMAGE ON SIDE SEAT RAIL STGR 15 RH BTW FS 785.15 TO FS 847 + 48.00 WAS REPLACED PER CRJ-900 SRM 53-41-49-101-001-A02 AND CRJ-900 AMM 53-00-49 (A12)
- [SDR VNAA202312140001](https://openairdocs.org/sdr/VNAA202312140001.md): Seat Track · corroded · Nov 21, 2023 · N560NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAIL STGR 15 RH BTW FS 677 TO 720.85. DUE TO EXCESSIVE DAMAGE ON SIDE SEAT RAIL STGR 15 RH BETWEEN FS677 - FS720.85 WAS REPLACED PER CRJ-900 SRM 53-41-49-101-001-A02 AND CRJ-900 AMM 53-00-49 (A12)
- [SDR VNAA202312140010](https://openairdocs.org/sdr/VNAA202312140010.md): Hinge · corroded · Nov 11, 2023 · N560NN · Cndair CL6002D24 · Fuselage, Door Hinge
  > CORROSION ON HINGE AT PASSENGER DOOR UPPER STEP. DUE TO DAMAGE IS NOT ALLOWABLE ON HINGE AT PASSENGER DOOR UPPER STEP WAS REPLACED PER CRJ900 SRM 52-11-04-101-001-A01 AND CRJ900 AMM 52-11-04 (CONFIG A01)
- [SDR VNAA202312140009](https://openairdocs.org/sdr/VNAA202312140009.md): Skin · dented · Nov 11, 2023 · N560NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > DESCRIPTION: SEVERAL DENTS ON FUSELAGE SKIN, SETTLEMNT AREA OF RIGTH VENTRAL FIN FAIRING BTW FS 1069.75 TO REAR SPAR DATUM STABILIZER 67.5%, BTW STGR 22RH TO STGR 21RH.CORRECTIVE ACTION: SEVERAL DENTS ON FUSELAGE SKIN, SETTLEMNT AREA OF RIGTH VENTRAL FIN FAIRI
- [SDR VNAA202312140005](https://openairdocs.org/sdr/VNAA202312140005.md): Seat Track · corroded · Nov 9, 2023 · N560NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAIL STGR 15 LH BTW FS 785.15 TO FS 847 +48.00. SIDE SEAT RAIL STGR 15 LH BTW FS 785.15 TO FS 847 +48.00 AT PASSENGER CABIN FLOOR STRUCTURE WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 FIGURE 53-41-49-991-806 AND WAS
- [SDR VNAA202312140004](https://openairdocs.org/sdr/VNAA202312140004.md): Seat Track · corroded · Nov 9, 2023 · N560NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAIL STGR 15 LH BTW FS 744.15 TO FS 761.85. SIDE SEAT RAIL STGR 15 LH BTW FS 744.15 TO FS 761.85 AT PASSENGER CABIN FLOOR STRUCTURE WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND WAS REPLACED PER CRJ900 AMM 53-00-49
- [SDR VNAA202312140002](https://openairdocs.org/sdr/VNAA202312140002.md): Seat Track · corroded · Nov 9, 2023 · N560NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > DESCRIPTION: CORROSION ON SIDE SEAT RAIL STGR 15 RH BTW FS 744.15 TO FS 761.85 CORRECTIVE ACTION: SIDE SEAT RAIL STGR 15 RH BTW FS 744.15 TO FS 761.85 AT PASSENGER CABIN FLOOR STRUCTURE WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND WAS R
- [SDR VNAA202312130022](https://openairdocs.org/sdr/VNAA202312130022.md): Seat Track · corroded · Nov 9, 2023 · N560NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL RBL 9 BTW FS 847.00 + 16.00 TO FS 977.00 AT PASSENGER CABIN FLOOR STRUCTURE. SEAT RAIL RBL 9 BTW FS 847.00 + 16.00 TO FS 977.00 AT PASSENGER CABIN FLOOR STRUCTURE WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-51-49-101-001-A02 AND WAS RE
- [SDR VNAA202312130014](https://openairdocs.org/sdr/VNAA202312130014.md): Intercostal · corroded · Nov 7, 2023 · N560NN · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSION ON INTERCOSTALS (2 EAS)AT RH/LH SIDE IN STA. FS= 349 TO FS= 364 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT. (E/E) INTERCOSTALS (2 EAS)AT RH/LH SIDE IN STA. FS= 349 TO FS= 364 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT. (E/E) WERE REPLACED PER CRJ900
- [SDR VNAA202312130013](https://openairdocs.org/sdr/VNAA202312130013.md): Drag Angle · cracked · Nov 6, 2023 · N560NN · 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). RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE
- [SDR VNAA202312130012](https://openairdocs.org/sdr/VNAA202312130012.md): Drag Angle · cracked · Nov 6, 2023 · N560NN · Cndair CL6002D24 · Vertical Stabilizer
  > DESCRIPTION: 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). CORRECTIVE ACTION: DRAG ANGLE WAS REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01
- [SDR VNAA202312130003](https://openairdocs.org/sdr/VNAA202312130003.md): Web · cracked · Nov 6, 2023 · N560NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > DESCRIPTION: CRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00. (SM) CORRECTIVE ACTION: ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00. (SM) WAS REPAIRED PER REO 690-53-11-1637. REV -- AND CRJ-900 SRM 5
- [SDR VNAA202312130011](https://openairdocs.org/sdr/VNAA202312130011.md): Skin · damaged · Nov 5, 2023 · N560NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > DESCRIPTION: LIGHTNING STRIKE ON FWD FUSELAGE, ABOVE FLOOR BTW STGR 7-8 LH AND FS 501.00 CORRECTIVE ACTION: LIGHTNING STRIKE ON FWD FUSELAGE, ABOVE FLOOR BTW STGR 7-8 LH AND FS 501.00 WAS REPAIRED PER CRJ900 SRM 53-00-00-201-003-A03.
- [SDR VNAA202312130010](https://openairdocs.org/sdr/VNAA202312130010.md): Skin · damaged · Nov 5, 2023 · N560NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > DESCRIPTION: LIGHTNING STRIKE ON FWD FUSELAGE, ABOVE FLOOR BTW STGR 15 LH AND FS661.00+32.00. CORRECTIVE ACTION: LIGHTNING STRIKE ON FWD FUSELAGE, ABOVE FLOOR BTW STGR 15 LH AND FS661.00+32.00 WAS REPAIRED PER CRJ900 SRM 53-00-00-201-003-A03.
- [SDR VNAA202312130009](https://openairdocs.org/sdr/VNAA202312130009.md): Skin · damaged · Nov 5, 2023 · N560NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > DESCRIPTION: LIGHTNING STRIKE ON FWD FUSELAGE, ABOVE FLOOR BTW STGR 16-17 LH AND FS501.00-FS517.00 CORRECTIVE ACTION: LIGHTNING STRIKE ON FWD FUSELAGE, ABOVE FLOOR BTW STGR 16-17 LH AND FS501.00-FS517.00 WAS REPAIRED PER CRJ900 SRM 53-00-00-201-003-A03.
- [SDR VNAA202312130008](https://openairdocs.org/sdr/VNAA202312130008.md): Skin · damaged · Nov 5, 2023 · N560NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > DESCRIPTION: LIGHTNING STRIKE ON CENTER FUSELAGE, ABOVE FLOOR BTW STGR 14 LH AND FS830.40-FS830.40+16. CORRECTIVE ACTION: LIGHTNING STRIKE ON CENTER FUSELAGE, ABOVE FLOOR BTW STGR 14 LH AND FS830.40-FS830.40+16 WAS REPAIRED PER CRJ900 SRM 53-00-00-201-003-A03.
- [SDR VNAA202312130007](https://openairdocs.org/sdr/VNAA202312130007.md): Skin · burned · Nov 5, 2023 · N560NN · Cndair CL6002D24 · Fuselage Main, Structure
  > DESCRIPTION: LIGHTNING STRIKE ON CENTER FUSELAGE, ABOVE FLOOR BTW STGR 11 LH AND FS693.00-FS708.00. CORRECTIVE ACTION: LIGHTNING STRIKE ON CENTER FUSELAGE, ABOVE FLOOR BTW STGR 11 LH AND FS693.00-FS708.00 WAS REPAIRED PER CRJ900 SRM 53-00-00-201-003-A03.
- [SDR VNAA202312130006](https://openairdocs.org/sdr/VNAA202312130006.md): Skin · damaged · Nov 5, 2023 · N560NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > DESCRIPTION: LIGHTNING STRIKE ON REAR FUSELAGE BTW FS 1088.20 AND STGR O- STGR 1 RH. CORRECTIVE ACTION: LIGHTNING STRIKE ON REAR FUSELAGE BTW FS 1088.20 AND STGR O- STGR 1 RH WAS REPAIRED PER CRJ900 SRM 53-00-00-201-003-A03.
- [SDR VNAA202312130005](https://openairdocs.org/sdr/VNAA202312130005.md): Skin · nicked · Nov 5, 2023 · N560NN · Cndair CL6002D24 · Fuselage Main, Structure
  > NICK (1EA) ON REAR FUSELAGE BTW FS1015.00-FS1031.00 AND STGR 18-19 RH. NICK (1EA) ON REAR FUSELAGE BTW FS1015.00-FS1031.00 AND STGR 18-19 RH WAS BLEND OUT PER CRJ-900 SRM 51-12-00-001-001-A01 AND EVALUATED WITHIN LIMITS PER CRJ900 SRM 53-61-01-101-004-A02, F
- [SDR VNAA202312130004](https://openairdocs.org/sdr/VNAA202312130004.md): Skin · corroded · Nov 5, 2023 · N560NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > CORROSION ON CUT OUT AT MAIN AVIONICS COMPARTMENT DOOR BTW FS 364.00 TO FS394.00 AND STGR 25LH TO 25RH. CUT OUT AT MAIN AVIONICS COMPARTMENT DOOR BTW FS 364.00 TO FS394.00 AND STGR 25LH TO 25RH WAS REPAIRED PER REO 690-53-21-032. REV --
- [SDR VNAA202312130002](https://openairdocs.org/sdr/VNAA202312130002.md): Skin · nicked · Nov 3, 2023 · N560NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > DESCRIPTION: SEVERAL NICKS ON REAR FUSELAGE BTW FS1015.00-FS1051.30 AND STGR 24RH-27RH CORRECTIVE ACTION: SEVERAL NICKS ON REAR FUSELAGE BTW FS1015.00-FS1051.30 AND STGR 24RH-27RH WERE REPAIRED PER REO 690-53-61-1290 REV - -, AND EVALUATED WITHIN LIMITS PER CR
- [SDR VNAA2023092611102](https://openairdocs.org/sdr/VNAA2023092611102.md): Fadec · warning message · Sep 21, 2023 · N560NN · Cndair CL6002D24 · Fuel Controlling System
  > L FADEC FAULT 1 STATUS MSG. REMOVED AND REPLACED L FADEC IAW CRJ 900 AMM 73-21-01-000/400-801. PERFORMED READ BACK OF THE ENGINE CONFIGURATION DATA WITH THE MDC. DATA READ BACK GOOD. POBIT CHECK GOOD AT THIS TIME.
- [SDR VNAA202309221111](https://openairdocs.org/sdr/VNAA202309221111.md): Control Valve · intermittent · Sep 20, 2023 · N560NN · Cndair CL6002D24 · Cabin Cooling System
  > L PACK INTERMITTENT IN FLIGHT / REMOVED AND REPLACED LH FLOW CONTROL VALVE IAW CRJ900 AMM 21-53-14-000/400-801-A01. OPS AND LEAK CHECK GOOD.
- [SDR VNAA202305011111](https://openairdocs.org/sdr/VNAA202305011111.md): Shock Absorber · unserviceable · Apr 28, 2023 · N560NN · Cndair CL6002D24 · Main Landing Gear Strut/Axle/Truck
  > GEAR DISAGREE MSG WHEN GEAR SELECTED UP ON CLIMBOUT / REMOVED NLG SHOCK STRUT IAW CRJ900 AMM 32-21-01-000-801. COMPLETED THE INSTALLATION OF THE NLG SHOCK STRUT IAW CRJ900 AMM 32-21-01-400-801. FINISHED INSTALL OF NLG SHOCK STRUST ASSY FROM STEP B(8) AND ON IA
- [SDR VNAA202303301112](https://openairdocs.org/sdr/VNAA202303301112.md): Pin · unserviceable · Mar 27, 2023 · N560NN · Cndair CL6002D24 · Engine (Turbine/Turboprop)
  > N1 FAN VIB R ENG CW QRH 2-32 AND QRH 2.10 ( INTENSIONAL SHUTDOWN) VIB INTERMITTENT BUT BECAME PRESSISTANT 1.7 - 1.9 N1. REMOVED AND REPLACED RH ENGINE FAN BLADE PINS IAW CRJ 900 AMM 12ˆ’20ˆ’72ˆ’640ˆ’803 (CONFIG A01). TORQUE CHECK GOOD.
- [SDR VNAA202303201111](https://openairdocs.org/sdr/VNAA202303201111.md): Fadec · unserviceable · Mar 18, 2023 · N560NN · Cndair CL6002D24 · Engine (Turbine/Turboprop)
  > DURING TAKEOFF/CLIMB AT 14000 R FADEC CAUTION MESSAGE. R/R RH FADEC IAW CRJ 900 AMM 73-21-01-000/400-801. OPS CHECK GOOD.
- [SDR VNAA202103041112](https://openairdocs.org/sdr/VNAA202103041112.md): Windshield · failed · Mar 2, 2021 · N560NN · Cndair CL6002D24 · Flight Compartment Windows
  > BURNING ODOR FROM FLIGHT DECK SMOKE FROM LOWER LEFT SIDE OF WINDSHIELD ON THE CA SIDE. INSPECTED CA WINDSHIELD IAW CRJ 900 AMM 56-11-01-210-80-A01-PSA. FOUND ARCING ON THE TERMINAL BLOCK. REMOVED THE SIDE STRAP IAW CRJ 900 AMM 56-10-05-000-801-A01 AND REMOVED
- [SDR VNAA202101261114](https://openairdocs.org/sdr/VNAA202101261114.md): Proximity Sensor · abnormal · Jan 25, 2021 · N560NN · Cndair CL6002D24 · Landing Gear Position and Warning
  > DURING CLIMB OUT FROM PNS, THE CREW RECEIVED A NOSE GEAR DOOR OPEN WARNING. THEY RAN THE QRH, WHICH INSTRUCTED THEM TO LAND AT THE NEAREST SUITABLE AIRPORT. THEY CHOSE TO RETURN TO PNS. NO EMERGENCY WAS DECLARED. REMOVED AND REPLACED PROXIMITY SENSOR PX31,
- [SDR VNAA2020062511103](https://openairdocs.org/sdr/VNAA2020062511103.md): Battery Pack · discharged · Jun 24, 2020 · N560NN · Cndair CL6002D24 · Emergency Lighting
  > OVERHEAD CABIN EMERGENCY LIGHTS FACING AIRCRAFT FRONT AND OVERWING EXIT EMERGENCY LIGHTS NEAR FLOOR BY FORWARD EXIT FLICKERING AND GOING OUT. MX REPLACED ALL 4 EMERGENCY BATTERY PACKS. OPS CHECK GOOD. BATTERY PACK 1 P/N OFF 2013-1A S/N OFF 73997 TSN 35158 H
- [SDR VNAA2019100191102](https://openairdocs.org/sdr/VNAA2019100191102.md): Acm · failed · Sep 30, 2019 · N560NN · Cndair CL6002D24 · Cabin Cooling System
  > SMOKE STARTED FILLING THE CABIN WHILE TAXIING TO THE GATE IN CLT. THE CREW CALLED FOR FIRE TRUCKS HAD THE PASSENGERS DEPLANE THROUGH THE MAIN CABIN IN THE WEST HARDSTAND. NO INJURIES WERE REPORTED. REMOVED AND REPLACED L/H PACK AIR CYCLE MACHINE OPS CHECK GO
- [SDR VNAA2018112611102](https://openairdocs.org/sdr/VNAA2018112611102.md): Pin · disconnected · Nov 26, 2018 · N560NN · Cndair CL6002D24 · Flight Control System Wiring
  > THE AIRCRAFT DIVERTED DUE TO LEFT AND RIGHT WING ANTI-ICE CAUTION MESSAGE AND FLAPS FAIL. MAINTENANCE WAS DISPATCHED AND FOUND PIN 4 ON CONNECTOR A105P1. RECONNECT PIN AND ALL PROBLEMS OPERATIONAL CHECK GOOD
- [SDR VNAA2018031611101](https://openairdocs.org/sdr/VNAA2018031611101.md): Warning Message · illuminated · Mar 16, 2018 · N560NN · Cndair CL6002D24 · Drag Control System
  > DURING APPROACH, THE CREW RECEIVED AN OUTBOARD SPOILERONS, OUTBAORD SPOILERS CAUTION MESSAGE. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. SYSTEM RESET, MESSAGE CLEARED DID NOT REOCCUR.
- [SDR VNAA2016120400008](https://openairdocs.org/sdr/VNAA2016120400008.md): Acm · seized · Dec 4, 2016 · N560NN · Cndair CL6002D24 · Cabin Cooling System
  > RIGHT AIR CONDITIONING PACK PRODUCED SMOKE IN THE CABIN. THE CREW RETURNED TO GATE. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE AIR CYCLE MACHINE, AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Next page: https://openairdocs.org/aircraft/N560NN/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 = 'N560NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N560NN/reports

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