# Service difficulty reports: N561NN

A list on [N561NN](https://openairdocs.org/aircraft/N561NN.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 · 66 reports

- [SDR VNAA2026032514901](https://openairdocs.org/sdr/VNAA2026032514901.md): Window · burned · Mar 23, 2026 · N561NN · Cndair CL6002D24 · Flight Compartment Windows
  > FO SIDE WINDOW HEATING ELEMENT INTERMITTENT GLOWING/ARCHING AT BASE / REMOVED AND REPLACED THE RH COCKPIT WINDOW IAW CRJ 900 AMM 56-12-01-000/400-801-A01-PSA. OPS AND LEAK CHECK PASSED.
- [SDR VNAA2024060411101](https://openairdocs.org/sdr/VNAA2024060411101.md): Acm · failed · Jun 2, 2024 · N561NN · Cndair CL6002D24 · Cabin Cooling System
  > UPON DEPARTURE FROM CAK PASSING THROUGH 4,000' WE GOT AN ODOR OF AN ELECTRICAL BURNING SMELL IN THE COCKPIT. UPON CLIMBING THROUGH 10,000' OUTSIDE OF STERILE / REMOVED AND REPLACED THE L/H AND R/H AIR CYCLE MACHINE (ACM) AS REQUIRED IN ACCORDANCE WITH 900 CRJ
- [SDR VNAA202401040031](https://openairdocs.org/sdr/VNAA202401040031.md): Bracket · corroded · Jan 4, 2024 · N561NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON BRACKETS, MACHINED (5EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT. CORROSION ON BRACKETS, MACHINED (5EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-32-58-101-001-A01 AND WERE REPLACED PER
- [SDR VNAA202401040030](https://openairdocs.org/sdr/VNAA202401040030.md): Intercostal · corroded · Jan 4, 2024 · N561NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL BTW STGR 27 /STGR 26LH AND FS 661.00+8.40 / FS661.00 +16.00 AT FWD CARGO COMPARTMENT. CORROSION ON INTERCOSTAL BTW STGR 27 /STGR 26LH AND FS 661.00+8.40 / FS661.00 +16.00 AT FWD CARGO COMPARTMENT WAS REMOVED PER CRJ900 SRM 51-21-06-00
- [SDR VNAA202401040028](https://openairdocs.org/sdr/VNAA202401040028.md): Rib · cracked · Jan 4, 2024 · N561NN · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > CRACK WAS FOUND ON RIB LEADING EDGE SS57.16 AT RH WING. STEP 1 TO STEP 4 WAS PERFORMED PER REO 690-57-41-240 REV. -- AND DUE ADYACENT CRACK WAS FOUND RIB LEADING EDGE SS57.16 AT RH WING WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-00
- [SDR VNAA202401040027](https://openairdocs.org/sdr/VNAA202401040027.md): Rib · cracked · Jan 4, 2024 · N561NN · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > CRACK WAS FOUND ON RIB LEADING EDGE SS57.16 AT LH WING. STEP 1 TO STEP 4 WAS PERFORMED PER REO 690-57-41-240 REV. -- AND DUE ADYACENT CRACK WAS FOUND RIB LEADING EDGE SS57.16 AT LH WING WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-00
- [SDR VNAA202401040025](https://openairdocs.org/sdr/VNAA202401040025.md): Floor Support · corroded · Jan 4, 2024 · N561NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION AT LBL27 FLOOR BEAM BETWEEN FS=985.00 TO FS=1069.75. CORROSION ON FLOOR BEAM LBL27 BETWEEN FS=985.00 TO FS=1069.75 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-61-43-101-001-A02 AND WAS REPAIRED PER REO 690-53-61-1308 REV-- AND CRJ900 SRM 53-00-41-
- [SDR VNAA202401040024](https://openairdocs.org/sdr/VNAA202401040024.md): Floor Support · corroded · Jan 4, 2024 · N561NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION AT LBL9 FLOOR BEAM BETWEEN FS=1000.00 TO FS=1069.75. LBL9 FLOOR BEAM BETWEEN FS=1000.00 TO FS=1069.75 WAS REPAIRED PER REO 690-53-61-1305 REV. --
- [SDR VNAA202401040023](https://openairdocs.org/sdr/VNAA202401040023.md): Floor Support · corroded · Jan 4, 2024 · N561NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION AT RBL9 FLOOR BEAM BETWEEN FS= 1000.00 TO FS=1069.75. (SM). CORROSION AT RBL9 FLOOR BEAM BETWEEN FS= 1000.00 TO FS=1069.75 WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND WAS REPAIRED PER REO REO 690-53-61-1307 REV. --
- [SDR VNAA202401040021](https://openairdocs.org/sdr/VNAA202401040021.md): Floor Support · corroded · Jan 4, 2024 · N561NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION AT RBL27 FLOOR BEAM BETWEEN FS=1015.00 TO FS=1031.00. RBL27 FLOOR BEAM BETWEEN FS=1015.00 TO FS=1031.00 WAS REPAIRED PER REO 690-53-61-1306 REV. --
- [SDR VNAA202401040019](https://openairdocs.org/sdr/VNAA202401040019.md): Support · corroded · Jan 4, 2024 · N561NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON GALLEY SUPPORT BTW FS=310.00 LBL=20”, FWD FUSELAGE FLOOR STRUCTURE. CORROSION ON GALLEY SUPPORT BTW FS=310.00 LBL=20”, FWD FUSELAGE FLOOR STRUCTURE WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-43-101-001-A03 AND WAS REPLACED PER CRJ900 SRM 51
- [SDR VNAA202401040017](https://openairdocs.org/sdr/VNAA202401040017.md): Canister · cracked · Jan 4, 2024 · N561NN · Cndair CL6002D24 · Aircraft Fuel System
  > CRACK IN CANISTER WELDED NO.3 IN, STA. WS148 OF INTERNAL LH MAIN FUEL TANK. CANISTER WELDED NO.3 IN, STA. WS148 OF INTERNAL LH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV. --
- [SDR VNAA202401040016](https://openairdocs.org/sdr/VNAA202401040016.md): Seat Track · corroded · Jan 4, 2024 · N561NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL BTW FS 669.40 TO FS 977.00 AND STGR 15RH AT CABIN PAX. CORROSION ON SEAT RAIL BTW FS 669.40 TO FS 977.00 AND STGR 15RH AT CABIN PAX WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND CRJ900 SRM 53-51-49-101-001-A02 AND
- [SDR VNAA202401040014](https://openairdocs.org/sdr/VNAA202401040014.md): Seat Track · corroded · Jan 4, 2024 · N561NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL BTW FS 669.40 TO FS 977.00 AND STGR 15LH AT CABIN PAX. CORROSION ON SEAT RAIL BTW FS 669.40 TO FS 977.00 AND STGR 15LH AT CABIN PAX WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02, CRJ900 SRM 53-51-49-101-001-A02 AND WAS
- [SDR VNAA202401040013](https://openairdocs.org/sdr/VNAA202401040013.md): Seat Track · corroded · Jan 4, 2024 · N561NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL BTW FS 379.00 TO FS 669.40 AND STGR 15LH AT CABIN PAX. CORROSION ON SEAT RAIL BTW FS 379.00 TO FS 669.40 AND STGR 15LH AT CABIN PAX WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01, CRJ900 SRM 53-31-49-101-001-A02 AND WAS
- [SDR VNAA202401040012](https://openairdocs.org/sdr/VNAA202401040012.md): Seat Track · corroded · Jan 4, 2024 · N561NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL BTW FS 379.00 TO FS 669.40 AND STGR 15RH AT CABIN PAX. CORROSION ON SEAT RAIL BTW FS 379.00 TO FS 669.40 AND STGR 15RH AT CABIN PAX WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND WAS REPLACED PER AMM 53-00-49 (CONFI
- [SDR VNAA202401040007](https://openairdocs.org/sdr/VNAA202401040007.md): Door Sill · corroded · Jan 4, 2024 · N561NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON LOWER SIL BTW FS=1000.00 TO FS=1047.00 AT AFT BAGGAGE BAY DOOR SURROUND STRUCTURE. CORROSION ON LOWER SIL BTW FS=1000.00 TO FS=1047.00 AT AFT BAGGAGE BAY DOOR SURROUND STRUCTURE WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-61-23-101-001-A01 AND
- [SDR VNAA202401040006](https://openairdocs.org/sdr/VNAA202401040006.md): Seat Track · corroded · Jan 4, 2024 · N561NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL BTW FS 477.40 TO FS 693.00 LBL 9.00 AT CABIN PAX. CORROSION ON SEAT RAIL BTW FS 477.40 TO FS 693.00 LBL 9.00 AT CABIN PAX WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-31-49-101-001-A02 AND WAS REPLACED PER AMM 53-00-49 (CONFIG A12)
- [SDR VNAA202401040005](https://openairdocs.org/sdr/VNAA202401040005.md): Seat Track · corroded · Jan 4, 2024 · N561NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL BTW FS 477.40 TO FS 693.00 RBL 9.00 AT CABIN PAX. CORROSION ON SEAT RAIL BTW FS 477.40 TO FS 693.00 RBL 9.00 AT CABIN PAX WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-31-49-101-001-A02 AND WAS REPLACED PER AMM 53-00-49 (CONFIG A12).
- [SDR VNAA202401040004](https://openairdocs.org/sdr/VNAA202401040004.md): Angle · corroded · Jan 4, 2024 · N561NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON ANGLE KICKPLATE (STGR 17L) AT PASSENGER DOOR SURROUND STRUCTURE FS 310.00- 333.00. CORROSION ON ANGLE KICKPLATE (STGR 17L) AT PASSENGER DOOR SURROUND STRUCTURE FS 310.00- 333.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-001-A02 AN
- [SDR VNAA202401040002](https://openairdocs.org/sdr/VNAA202401040002.md): Seat Track · corroded · Jan 4, 2024 · N561NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL BTW FS 374.00 TO FS 477.40 LBL 9.00 AT CABIN PAX. CORROSION ON SEAT RAIL BTW FS 374.00 TO FS 477.40 LBL 9.00 AT CABIN PAX WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01 AND WAS REPLACED PER AMM 53-00-49 (CONFIG A12)
- [SDR VNAA202401040001](https://openairdocs.org/sdr/VNAA202401040001.md): Seat Track · corroded · Jan 4, 2024 · N561NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL BTW FS 349.00 TO FS 477.40 RBL 9.00 AT CABIN PAX. SEAT RAIL (2 EAS) WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01 AND REPLACED PER CRJ900 AMM 53-00-49
- [SDR VNAA202401040015](https://openairdocs.org/sdr/VNAA202401040015.md): Intercostal · corroded · Nov 25, 2023 · N561NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTALS (2 EAS) IN STA. FS= 349 TO FS= 364 NEAR TO STGR 27 AT MAIN AVIONICS COMPARTMENT. (E/E). INTERCOSTALS (2 EAS) IN STA. FS= 349 TO FS= 364 NEAR TO STGR 27 AT MAIN AVIONICS COMPARTMENT. (E/E) WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM
- [SDR VNAA202401040034](https://openairdocs.org/sdr/VNAA202401040034.md): Canister · cracked · Nov 24, 2023 · N561NN · Bombdr CL6002D15 · Wing Miscellaneous Structure
  > CRACK IN CANISTER WELDED NO.3 IN, STA. WS148 OF INTERNAL RH MAIN FUEL TANK. CANISTER WELDED NO.3 IN, STA. WS148 OF INTERNAL RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV. --
- [SDR VNAA202401040033](https://openairdocs.org/sdr/VNAA202401040033.md): Floor Support · nicked · Nov 24, 2023 · N561NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > NICKS ON LONGITUDINAL BEAM LBL 27 BTW FS= 409.00 AND FS=421.00, FUSELAGE FLOOR STRUCTURE. LONGITUDINAL BEAM LBL 27 BTW FS= 409.00 AND FS=421.00, FUSELAGE FLOOR STRUCTURE WAS REPAIRED PER REO 690-53-21-1684 REV --
- [SDR VNAA202401040032](https://openairdocs.org/sdr/VNAA202401040032.md): Frame · corroded · Nov 24, 2023 · N561NN · Bombdr CL6002D15 · Fuselage Main, Frame
  > CORROSION ON FR 847+16.00 BTW STGR 26 LH/RH WAS FOUND. CORROSION ON FR 847+16.00 BTW STGR 26 LH/RH WAS EVALUATED OUT OF LIIMTS PER CRJ900 SRM 53-51-06-101-003-A05 AND WAS REPAIRED PER CRJ900 SRM 53-00-06-201-001-A03.
- [SDR VNAA202401040029](https://openairdocs.org/sdr/VNAA202401040029.md): Unknown · unknown · Nov 24, 2023 · N561NN · Bombdr CL6002D15 · Passenger/Crew Doors
  > FWD PAX ACCESS PANEL MOUNT HOLE ELONGATED. FWD PAX DOOR ACCESS PANEL MOUNT HOLE ELONGATED WAS REPAIRED PER ENGINEERING ORDER (REO) NUMBER 690-52-11-878 REV - - AND EA 21-C9-52-044 REV IR SECTION II - PERMANENT REPAIR
- [SDR VNAA202401040026](https://openairdocs.org/sdr/VNAA202401040026.md): Skin · dented · Nov 24, 2023 · N561NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > DENT ON EXTERNAL LOWER FUSELAGE SKIN BTW STGR 23R/24R AND FS 280-25" AT FWD FUSELAGE. DENT ON EXTERNAL LOWER FUSELAGE SKIN BTW STGR 23R/24R AND FS 280-25" AT FWD FUSELAGE WAS REPAIRED PER PER REO 670-51-00-085 REV. -A AND REO 690-53-11-1644 REV. --
- [SDR VNAA202401040022](https://openairdocs.org/sdr/VNAA202401040022.md): Retainer · nicked · Nov 24, 2023 · N561NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > NICKS ON CUTOUT STRCTURE OF CENTER BAGGAGE BAY DOORS, FS=519.64 BTW STRG 20L-21L AND FS=661.00 BTW STGR23L-STGR24L CUTOUT STRCTURE OF CENTER BAGGAGE BAY DOORS, FS=519.64 BTW STRG 20L-21L AND FS=661.00 BTW STGR23L-STGR24L WAS REPAIRED PER REO 690-53-31-797 RE
- [SDR VNAA202401040018](https://openairdocs.org/sdr/VNAA202401040018.md): Intercostal · corroded · Nov 24, 2023 · N561NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL ATTACHED TO STRINGER 20RH IN STA. FS= 319.70 TO FS= 349.00 AT MAIN AVIONICS COMPARTMENT. CORROSION ON INTERCOSTAL ATTACHED TO STRINGER 20RH IN STA. FS= 319.70 TO FS= 349.00 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS PER
- [SDR VNAA202001040011](https://openairdocs.org/sdr/VNAA202001040011.md): Floorbeam · cracked · Nov 24, 2023 · N561NN · Bombdr CL6002D15 · Fuselage Main, Floor Beam
  > CRACK ON COCKPIT FLOOR LONGITUDINAL BEAM (RBL12) TO CROSSBEAM FS 280.00, FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT. COCKPIT FLOOR LONGITUDINAL BEAM (RBL12) TO CROSSBEAM FS 280.00, FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1640 RE
- [SDR VNAA202401040010](https://openairdocs.org/sdr/VNAA202401040010.md): Web · cracked · Nov 24, 2023 · N561NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CRACK AT UPPER WEB OF ADG COMPARTMENT, BELOW OF SETTLEMENT AREA OF ADG HYD PUMB. UPPER WEB OF ADG COMPARTMENT, BELOW OF SETTLEMENT AREA OF ADG HYD PUMB WAS REPAIRED PER CRJ900 SRM 53-11-43-201-001-A01
- [SDR VNAA202401040009](https://openairdocs.org/sdr/VNAA202401040009.md): Hinge · damaged · Nov 24, 2023 · N561NN · Bombdr CL6002D15 · Fuselage, Door Hinge
  > DURING MEASURE WITH GO-NO-GO GAUGE IN JOB CARD TRFKE006TPGE STEP 13.2 AT FUSELAGE PIANO HINGE AT PASSENGER DOOR WAS FOUND OUT OF LIMITS. REPLACEMENT IT´S NECESSARY. PIANO HINGE AT PASSENGER DOOR WAS REPLACED PER CRJ900 SRM 53-21-23-201-007-A01
- [SDR VNAA20240104000](https://openairdocs.org/sdr/VNAA20240104000.md): Skin · corroded · Nov 24, 2023 · N561NN · Bombdr CL6002D15 · 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. CORROSION ON CUT OUT AT MAIN AVIONICS COMPARTMENT DOOR BTW FS 364.00 TO FS394.00 AND STGR 25LH TO 25RH WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND
- [SDR VNAA202401040003](https://openairdocs.org/sdr/VNAA202401040003.md): Arm · worn · Nov 22, 2023 · N561NN · Bombdr CL6002D15 · Cargo/Baggage Doors
  > WEAR ON ROTATING ARM AT FWD CARGO BAGGAGE BAY DOOR. ROTATING ARM AT FWD CARGO BAGGAGE BAY DOOR WAS REPAIRED PER REO 690-52-35-362 REV. --
- [SDR VNAA202202071112](https://openairdocs.org/sdr/VNAA202202071112.md): Epsu · faulty · Feb 3, 2022 · N561NN · Cndair CL6002D24 · Emergency Lighting
  > EMERGENCY LIGHTS INOP / REMOVED & REPLACED EPSU BATTERY PACK IAW CRJ900 AMM 33-51-17-000/400-801. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.
- [SDR VNAA202110101111](https://openairdocs.org/sdr/VNAA202110101111.md): Window · arced · Oct 6, 2021 · N561NN · Cndair CL6002D24 · Flight Compartment Windows
  > CA SIDE WINDOW ARCING NEAR BOTTOM SEAL, JUST ABOVE AND SLIGHTLY LEFT OF ASH TRAY / PERFORMED GVI OF CA SIDE WINDOW IAW CRJ900 AMM 56-11-01-210-801-A01-PSA REV C. FOUND BUBBLING AND DISCOLORATION ON BOTTOM SIDE OF WINDOW, FOUND DAMAGE TO BE OUT OF LIMITS. PERFO
- [SDR VNAA202102231112](https://openairdocs.org/sdr/VNAA202102231112.md): Sensor · warning light · Feb 22, 2021 · N561NN · Cndair CL6002D24 · Airfoil Anti/De-ice System
  > JUST AFTER TAKEOFF, THE CREW RECEIVED A WING ANTI-ICE CAUTION MESSAGE. TO AVOID FLYING INTO POTENTIAL ICING CONDITIONS, THE CREW LEVELED OFF AT FL030 TO RUN THEIR QRH. THEY DECIDED TO RETURN TO FIELD. NO EMERGENCY WAS DECLARED. REMOVED AND REPLACED LT WING
- [SDR VNAA202102161111](https://openairdocs.org/sdr/VNAA202102161111.md): Warning Light · illuminated · Feb 12, 2021 · N561NN · Cndair CL6002D24 · Airfoil Anti/De-ice System
  > AT 80 KNOTS THE CREW RECIEVED AN AMBER ANTI ICE MESSAGE AND REJECTED THE TAKE OFF. THEY PULLED OVER AND CALLED MAINTENACE AT WHICH POINT THE MESSAGE WAS CLEARED. THE AIRCRAFT IS ON ITS WAY TO ITS DESTINATION. NO EMERGENCY.
- [SDR VNAA202101251111](https://openairdocs.org/sdr/VNAA202101251111.md): Connector · unsecure · Jan 24, 2021 · N561NN · Cndair CL6002D24 · Ice/Rain Protection System Wiring
  > ON THE TAKEOFF ROLL, AS THE CREW APPROACHED V1 (AT ABOUT 130 KIAS) THEY RECEIVED A WING OVERHEAT CAUTION MESSAGE AND DECIDED TO REJECT THE TAKEOFF. ONCE THEY WERE OFF, THE CREW MADE AN ANNOUCEMENT TO THE PAX OF WHAT OCCURRED, AND ALSO CONTACTED MAINTENANCE.
- [SDR VNAA202101041111](https://openairdocs.org/sdr/VNAA202101041111.md): Isolation Valve · failed · Dec 31, 2020 · N561NN · Cndair CL6002D24 · Engine Thrust Reverser
  > THE CREW REJECTED THE TAKE OFF FROM RUNWAY 25L. SPEED BELOW 40 KNOTS. RT REV UNSAFE AMBER MESSAGE. REMOVED AND REPLACED RT TR ISOLATION CONTROL VALVE, IAW CRJ900 AMM 78-32-09-000/400-801-A01.
- [SDR VNAA2020090311102](https://openairdocs.org/sdr/VNAA2020090311102.md): Rod · disconnected · Aug 31, 2020 · N561NN · Cndair CL6002D24 · Emergency Exits
  > OVERHEAD BIN INSTALLED INCORRECTLY CAUSING INTERFERENCE WITH EMERGENCY EXIT. CONDUCTED OPERATIONS CHECK ON EMERGENCY EXIT DOORS, FOUND RIGHT AFT HITTING BIN. FOUND ROD DISCONNECTED ON AFT END OF BIN 15. CONNECTED ROD IAW CRJ 900 AMM 25-23-01-000/400-801-A50.
- [SDR VNAA2020072511101](https://openairdocs.org/sdr/VNAA2020072511101.md): Controller · failed · Jul 24, 2020 · N561NN · Cndair CL6002D24 · Windshield/Door Rain/Ice Removal
  > CREW INITIALLY REPORTED TO THE DISPATCHER PACK SMELL IN THE COCKPIT. INFORMATION WAS LATER REVEALED THAT THE CREW DECLARED AN EMERGENCY DUE TO THE WINDSHIELD HEATING ELEMENT CRACKLING AND SPARKING. THE CREW REPORTED THE PROBLEM TO MAINTENANCE IN CLT HOWEVER DI
- [SDR VNAA2020072311102](https://openairdocs.org/sdr/VNAA2020072311102.md): Unknown · odor · Jul 19, 2020 · N561NN · Cndair CL6002D24 · Air Distribution System
  > CREW REPORTED BAD ODOR FROM LT A/C PACK DURING FLIGHT. COMPLIED WITH HIGH POWER ENGINE RUNS WITH PACKS ON IAW AMM 21-51-00-710-801. NO ODOR PRESENT, OPS CHECKED GOOD.
- [SDR VNAA2020071501102](https://openairdocs.org/sdr/VNAA2020071501102.md): Unknown · odor · Jul 12, 2020 · N561NN · Cndair CL6002D24 · Air Distribution System
  > STRONG ODOR IN COCKPIT PRIOR TO ACTIVATING PACKS. PERFORMED OPS TEST OF THE RECIRCULATION FAN. PERFORMED OPS TEST OF THE DISPLAY COOLING SYSTEM. PERFORMED OPS TEST OF THE AIR CONDITIONING DISTRIBUTION SYSTEM, OPS CHECK GOOD NO UNUSUAL ODOR DETECTED.
- [SDR VNAA202003249995](https://openairdocs.org/sdr/VNAA202003249995.md): Joint · corroded · Mar 24, 2020 · N561NN · Bombdr CL6002D15 · Fuselage Main, Structure
  > CIRCUMFERENTIAL JOINT FROM F.S. 280.00 TO F.S. 282.86 BETWEEN STGR 27 AND STGR 25R CORRODED AROUND SEVERAL FASTENERS. COMPLETED EA 48-2020-055 REV IR.
- [SDR VNAA202003249994](https://openairdocs.org/sdr/VNAA202003249994.md): Angle · corroded · Mar 24, 2020 · N561NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > FS 280.00 FWD J ANGLE IS CORRODED. REMOVED DAMAGED FWD "J" ANGLE AT FS280 IAW CRJ 900 SRM 51-42-06-001-001-A01. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE J-ANGLE IAW CRJ 900 SRM 51-40-11-001-001-A01.
- [SDR VNAA202003249992](https://openairdocs.org/sdr/VNAA202003249992.md): Drag Angle · cracked · Mar 24, 2020 · N561NN · Bombdr CL6002D15 · Aerodynamic Fairings
  > SUSPECT CRACK AT LH AFT TAIL CONE DRAG ANGLE. REMOVED LH AFT TAIL CONE DRAG ANGLE (PART #AV670-21186-003) IAW CRJ 900 SRM 51-40-00-001-001-A01. INSTALLED NEW LH AFT DRAG ANGLE IAW CRJ 900 SRM 51-42-13-001-001-A01,51-42-21-001-001-A01, AND 51-42-22-001-001-A01.
- [SDR VNAA202003249991](https://openairdocs.org/sdr/VNAA202003249991.md): Drag Angle · cracked · Mar 24, 2020 · N561NN · Bombdr CL6002D15 · Aerodynamic Fairings
  > SUSPECT CRACK AT RH AFT TAIL CONE DRAG ANGLE. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE RH AFT DRY ANGLE PN:AV670-21186-004 IAW CRJ 900 SRM 51-40-11-001-001-A01.
- [SDR VNAA202003249993](https://openairdocs.org/sdr/VNAA202003249993.md): Frame · corroded · Mar 24, 2020 · N561NN · Bombdr CL6002D15 · Fuselage Main, Frame
  > FRAME AT FS 310.00 IS CORRODED BETWEEN STGR 26L AND 26R. REMOVED DAMAGED SECTION AND INSTALLED FRAME AND SPLICE AT FS 310, 26L TO 26R PER CRJ900 SRM 53-00-06-995-815.

Next page: https://openairdocs.org/aircraft/N561NN/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 = 'N561NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N561NN/reports

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