# Service difficulty reports: N564NN

A list on [N564NN](https://openairdocs.org/aircraft/N564NN.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 · 62 reports

- [SDR VNAA2024122011101](https://openairdocs.org/sdr/VNAA2024122011101.md): Windshield · smoke · Dec 18, 2024 · N564NN · Cndair CL6002D24 · Flight Compartment Windows
  > RH BOTTOM WINDSHIELD HEAT STARTED SMOKING ON TAKEOFF/CLIMB. THE CREW REPORTED THE ODOR WAS AN ELECTRICAL SMELL AND LASTED LESS THAN 5 MINUTES. THE FUMES WERE IN THE COCKPIT. NO MEDICAL ATTENTION REQUESTED. / REMOVED AND REPLACED THE RH WINDSHIELD IAW CRJ 900 A
- [SDR VNAA202401230002](https://openairdocs.org/sdr/VNAA202401230002.md): Spoiler · dented · Jan 15, 2024 · N564NN · Cndair CL6002D24 · Spoilers
  > DENT ON INBOARD GROUND SPOILER AT RH WING. INBOARD GROUND SPOILER OF RH WING WAS REPAIRED PER REO NUMBER 690-57-71-076 REV --.
- [SDR VNAA202401220011](https://openairdocs.org/sdr/VNAA202401220011.md): Rib · damaged · Jan 14, 2024 · N564NN · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > PERM REPAIR BEFORE 20,826.13 FH - TAPE APPLIED - LH FIXED LE SKIN PANEL 521BL AND RIB WITHIN 800 FH FROM IR (BEFORE 20,826.13 FH), REPLACE OR REPAIR THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES. RIB WAS REPAIRED PER REO 690-57-41-408 REV. -- AN
- [SDR VNAA202401220003](https://openairdocs.org/sdr/VNAA202401220003.md): Web · cracked · Jan 14, 2024 · N564NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00. ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00 WAS REPAIRED PER CRJ900 SRM 53-11-43-201-001-A01
- [SDR VNAA202401210022](https://openairdocs.org/sdr/VNAA202401210022.md): Skin · worn · Jan 10, 2024 · N564NN · Cndair CL6002D24 · Wing, Plate/Skin
  > WEAR ON AREA OF SETTLEMENT OF FAIRINGS (683AB,686AB, 692AB, 695AB, 697AB) AT RH WING LOWER SKIN. WEAR ON AREA OF SETTLEMENT OF FAIRINGS (683AB,686AB, 692AB, 695AB, 697AB) AT RH WING LOWER SKIN WAS REPAIRED PER REO 690-57-21-445 REV.--
- [SDR VNAA202401210021](https://openairdocs.org/sdr/VNAA202401210021.md): Skin · nicked · Jan 10, 2024 · N564NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > SEVERAL NICKS ON FUSELAGE SKIN BTW STA. 1000 TO STA 1051.30 AND STGR 23RH TO STGR 27RH. REPAIR WAS PERFORMED PER REO 690-53-61-1324 REV - -
- [SDR VNAA202401210017](https://openairdocs.org/sdr/VNAA202401210017.md): Hinge Fitting · corroded · Jan 10, 2024 · N564NN · Cndair CL6002D24 · Ailerons
  > CORROSION ON CENTER HINGE FITTING BUSHINGS, LUG L1, L2 AND L6. CENTER HINGE FITTING BUSHINGS, LUG L1, L2 AND L6 WERE REPLACED PER CRJ 900 AMM 20-31-00-400-801-A01 AND CRJ 900 AMM 20-31-00-000-801-A01
- [SDR VNAA202401210014](https://openairdocs.org/sdr/VNAA202401210014.md): Fitting · corroded · Jan 10, 2024 · N564NN · Cndair CL6002D24 · Wing, Control Surface Attach Fittings
  > CORROSION ON CENTER HINGE FITTING INNER LUG BORE, LUG L1, L2 AND L6 WAS FOUND. CORROSION ON CENTER HINGE FITTING INNER LUG BORE, LUG L1, L2 AND L6 WERE REPAIRED PER REO 670-57-61-237 REV. --
- [SDR VNAA202401210013](https://openairdocs.org/sdr/VNAA202401210013.md): Skin · worn · Jan 10, 2024 · N564NN · Cndair CL6002D24 · Wing, Plate/Skin
  > WEAR ON SETTLEMENT AREA OF FAIRING 597AB AT LH WING LOWER SKIN. WEAR ON SETTLEMENT AREA OF FAIRING 597AB AT LH WING LOWER SKIN WAS REPAIRED PER. REO 690-57-21-444 REV.--
- [SDR VNAA202401210012](https://openairdocs.org/sdr/VNAA202401210012.md): Skin · worn · Jan 10, 2024 · N564NN · Cndair CL6002D24 · Wing, Plate/Skin
  > WEAR ON SETTLEMENT AREA OF FAIRING 595AB AT LH WING LOWER SKIN. WEAR ON SETTLEMENT AREA OF FAIRING 595AB AT LH WING LOWER SKIN WAS REPAIRED PER. REO 690-57-21-444 REV.--
- [SDR VNAA202401210011](https://openairdocs.org/sdr/VNAA202401210011.md): Skin · worn · Jan 10, 2024 · N564NN · Cndair CL6002D24 · Wing, Plate/Skin
  > WEAR ON SETTLEMENT AREA OF FAIRING 586AB AT LH WING LOWER SKIN. WEAR ON SETTLEMENT AREA OF FAIRING 586AB AT LH WING LOWER SKIN
- [SDR VNAA202401210010](https://openairdocs.org/sdr/VNAA202401210010.md): Skin · worn · Jan 10, 2024 · N564NN · Cndair CL6002D24 · Wing, Plate/Skin
  > WEAR ON SETTLEMENT AREA OF FAIRING 592AB AT LH WING LOWER SKIN. WEAR ON SETTLEMENT AREA OF FAIRING 592AB AT LH WING LOWER SKIN WAS REPAIRED PER. REO 690-57-21-444 REV.--
- [SDR VNAA202401210005](https://openairdocs.org/sdr/VNAA202401210005.md): Seat Track · corroded · Jan 8, 2024 · N564NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAIL STGR 15 LH/RH BTW FS 669.40 TO FS 720.85. SIDE SEAT RAIL STGR 15 LH/RH BTW FS 669.40 TO FS 720.85 WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 AND WERE REPLACED PER CRJ-900 AMM 53-00-49.
- [SDR VNAA202401220009](https://openairdocs.org/sdr/VNAA202401220009.md): Skin · dented · Jan 7, 2024 · N564NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > DENT ON EXTERNAL FUSELAGE SKIN BTW FS 169.00 TO FS 173.00 BTW STGR 19 LH TO STGR 23 LH, WL 87.90. DENT ON EXTERNAL FUSELAGE SKIN BTW FS 169.00 TO FS 173.00 BTW STGR 19 LH TO STGR 23 LH, WL 87.90. WAS REPAIRED PER. REO 690-53-11-1660 REV -- AND REO 670-51-00-
- [SDR VNAA202401220006](https://openairdocs.org/sdr/VNAA202401220006.md): Skin · nicked · Jan 7, 2024 · N564NN · Cndair CL6002D24 · Trailing Edge Flaps
  > SEVERAL NICKS AND DENTS ON LOWER SKIN OF RH INBOARD FLAP FLS 15.00 TO FLS 65.5. SEVERAL NICKS ON LOWER SKIN OF RH INBOARD FLAP FLS 15.00 TO FLS 65.5, WERE BLENDED OUT PER CRJ-900 SRM 51-12-00-001-001-A01 AND WERE EVALUATE AREA BTW FLS 30.00 TO FLS 65.5 IS WI
- [SDR VNAA202401210001](https://openairdocs.org/sdr/VNAA202401210001.md): Bracket · corroded · Jan 7, 2024 · N564NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON BRACKETS, MACHINED (5EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT. DUE TO STRUCTURE NO DAMAGE ALLOWED PER CRJ900 SRM 51-42-22-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01 AND DETAILED VISUAL INSPECTION OF THE BRACKET MACHINE (1EA) AT
- [SDR VNAA202401210006](https://openairdocs.org/sdr/VNAA202401210006.md): Seat Track · corroded · Jan 5, 2024 · N564NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAIL STGR 15 LH/RH BTW FS 744.15 TO FS 761.85. SIDE SEAT RAILS STGR 15 LH/RH BTW FS 744.15 TO FS 761.85. WERE EVALUATED OUT LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND WERE REPLACED PER CRJ900 AMM 53-00-49
- [SDR VNAA202401210019](https://openairdocs.org/sdr/VNAA202401210019.md): Skin · dented · Jan 4, 2024 · N564NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > SEVERAL DENTS ON FUSELAGE SKIN, SETTLEMENT AREA OF RIGHT VENTRAL FIN FAIRING BTW FS 1069.75 TO REAR SPAR DATUM STABILIZER 67.5%, BTW STGR 22RH TO STGR 21RH. SEVERAL DENTS ON FUSELAGE SKIN, SETTLEMENT AREA OF RIGHT VENTRAL FIN FAIRING BTW FS 1069.75 TO REA
- [SDR VNAA202401210018](https://openairdocs.org/sdr/VNAA202401210018.md): Skin · dented · Jan 4, 2024 · N564NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > SEVERAL DENTS ON FUSELAGE SKIN, SETTLEMENT AREA OF LEFT VENTRAL FIN FAIRING BTW FS 1069.75 TO REAR SPAR DATUM STABILIZER 67.5%, BTW STGR 22LH TO STGR 21LH. SEVERAL DENTS ON FUSELAGE SKIN, SETTLEMENT AREA OF LEFT VENTRAL FIN FAIRING BTW FS 1069.75 TO REAR SP
- [SDR VNAA202401210016](https://openairdocs.org/sdr/VNAA202401210016.md): Floor Support · corroded · Jan 4, 2024 · N564NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON UPPER FACE OF FLOOR SUPPORT LBL 9.00 AT AFT CARGO COMPARTMEN INTERNAL STRUCTURE FROM FS 1000.00 TO FS 1088.20. UPPER FACE OF FLOOR BEAM LBL 9.00 AT AFT CARGO COMPARTMEN INTERNAL STRUCTURE FROM FS 1000.00 TO FS 1088.20 WAS REPAIRED PER REO 690-53
- [SDR VNAA202401210003](https://openairdocs.org/sdr/VNAA202401210003.md): Floorbeam · cracked · Jan 4, 2024 · N564NN · Bombdr CL6002D15 · Fuselage Main, Floor Beam
  > CRACKED CENTER COCKPIT FLOOR BEAM RBL12 AT FS280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. CENTER COCKPIT FLOOR BEAM RBL12 AT FS280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1651. REV.-
- [SDR VNAA202401210007](https://openairdocs.org/sdr/VNAA202401210007.md): Seat Track · corroded · Dec 29, 2023 · N564NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAIL STGR 15 LH/RH BTW FS 785.15 TO FS 847.00 +8.40. DUE TO EXCESSIVE DAMAGE ON LH AND RH SIDE SEAT TRACK BTW FS=785.15 AND FS=847.00+8.40 WAS REPLACED PER CRJ-900 SRM 53-41-49-101-001-A02 AND CRJ-900 AMM 53-00-49 (CONF A12)
- [SDR VNAA202401210002](https://openairdocs.org/sdr/VNAA202401210002.md): Floorbeam · cracked · Dec 29, 2023 · N564NN · Bombdr CL6002D15 · Fuselage Main, Floor Beam
  > CRACKED ANGLES OF PREVIOUS REPAIR AT CENTER COCKPIT FLOOR BEAM LBL12 AT FS280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. PREVIOUS REPAIR AT CENTER COCKPIT FLOOR BEAM LBL12 AT FS280.00 FLOOR INTERNAL SUPPORT STRUCTURE WAS REPLACED PER REO
- [SDR VNAA202401220012](https://openairdocs.org/sdr/VNAA202401220012.md): Support · cracked · Dec 27, 2023 · N564NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK AT FWD RH/LH CORNER SUPPORT OF THE JB 6 MODULE AT FWD EQUIPMENT COMPARTMENT. SUPPORT OF THE JB 6 MODULE AT FWD EQUIPMENT COMPARTMENT WAS REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01
- [SDR VNAA202401210015](https://openairdocs.org/sdr/VNAA202401210015.md): Seat Track · corroded · Dec 16, 2023 · N564NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACKS LBL 27 STA 485 TO STA 501 (1E/A), LBL 9 STA 565 TO STA 661+90 (3E/A) AND RBL 9 STA 349 TO STA 469 (1E/A), STA 581 TO STA 661+90(2E/A). SEAT TRACKS LBL 27 STA 485 TO STA 501 (1E/A), LBL 9 STA 565 TO STA 661+90 (3E/A) AND RBL 9 STA 349
- [SDR VNAA202401210004](https://openairdocs.org/sdr/VNAA202401210004.md): Stringer · corroded · Dec 16, 2023 · N564NN · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION AT STRINGER AND STRINGER SPLICE STGR 21 RH, BTW FS 330.00 TO FS 349.00. CORROSION AT STRINGER 21 RH, BTW FS 330.00 TO FS 349.00 WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND WAS EVALUATED WITHIN LIMITS PER CRJ900 SRM 53-21-03-101-006-A04 AND S
- [SDR VNAA202401210009](https://openairdocs.org/sdr/VNAA202401210009.md): Intercostal · corroded · Dec 15, 2023 · N564NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTALS(3EAS) BTW FS=349 TO FS=364 NEAR STGR 27 AND STGR 26RH AT MAIN AVIONICS COMPARTMENT. INTERCOSTALS(2EAS) BTW FS=349 TO FS=364 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-003-A02 AN
- [SDR VNAA202401220010](https://openairdocs.org/sdr/VNAA202401220010.md): Skin · damaged · Dec 14, 2023 · N564NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE DAMAGE ON FUSELAGE SKINS AT STR 16R THE SUBJECT CONDITION IS STRUCTURALLY ACCEPTABLE FOR 400 FLIGHT HOURS FROM TIME OF INCORPORATION OF THIS REO AT REV -- LIGHTNING STRIKE DAMAGE ON FUSELAGE SKINS AT STR 16R WAS REPAIRED PER REO 690-53-11-165
- [SDR VNAA202401230001](https://openairdocs.org/sdr/VNAA202401230001.md): Floorbeam · cracked · Dec 13, 2023 · N564NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CRACKED ANGLES OF PREVIOUS REPAIR AT CENTER COCKPIT FLOOR BEAM LBL12 AT FS280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT. PREVIOUS REPAIR AT CENTER COCKPIT FLOOR BEAM LBL12 AT FS280.00 FLOOR INTERNAL SUPPORT STRUCTURE WAS REPLACED PER REO 690-53-11-16
- [SDR VNAA202401220016](https://openairdocs.org/sdr/VNAA202401220016.md): Skin · damaged · Dec 13, 2023 · N564NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > BURN MARK ON FUSELAGE SKIN BTW FS.469.00 TO FS 477.40 AND BTW STGR13RH TO STGR14RH. BURN MARK ON FUSELAGE SKIN BTW FS.469.00 TO FS 477.40 AND BTW STGR13RH TO STGR14RH WAS REPAIRED PER REO 670-53-00-045 REV. -K DISPOSITION: 1. B-PERMANENT DISPOSITION/. B3/.
- [SDR VNAA202401220013](https://openairdocs.org/sdr/VNAA202401220013.md): Skin · corroded · Dec 13, 2023 · N564NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > CORROSION ON INNER SKIN SURFACE AT THE MAIN AVIONICS BAY DOOR CUTOUT BTW FS 364.00 TO FS394.00, BTW STGR 25LH TO 25RH. THE MAIN AVIONICS BAY DOOR CUTOUT BTW FS 364.00 TO FS394.00, BTW STGR 25LH TO 25RH WAS REPAIRED PER REO 690-53-21-032 REV - -
- [SDR VNAA202401220008](https://openairdocs.org/sdr/VNAA202401220008.md): Skin · damaged · Dec 13, 2023 · N564NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > BURN MARK ON FUSELAGE SKIN BTW FS 533.00 TO FS 549.00 AND BTW STGR13RH TO STGR14RH. BURN MARK ON FUSELAGE SKIN BTW FS 533.00 TO FS 549.00 AND BTW STGR13RH TO STGR14RH WAS REPAIRED PER REO 690-53-31-801 REV. --
- [SDR VNAA202401220007](https://openairdocs.org/sdr/VNAA202401220007.md): Skin · damaged · Dec 13, 2023 · N564NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > BURN MARK ON FUSELAGE SKIN BTW FS 477.40 TO FS 485.00 AND BTW STGR13RH TO STGR14RH. BURN MARK ON FUSELAGE SKIN BTW FS 477.40 TO FS 485.00 AND BTW STGR13RH TO STGR14RH WAS REPAIRED PER REO 690-53-31-801 REV. --
- [SDR VNAA202401210008](https://openairdocs.org/sdr/VNAA202401210008.md): Rib · cracked · Dec 13, 2023 · N564NN · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > AFTER INTERNAL ZONAL INSPECTION, CRACKED WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF RH WING. RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF RH WING WAS REPAIRED PER REO 690-57-51-319 REV. --
- [SDR VNAA202401220015](https://openairdocs.org/sdr/VNAA202401220015.md): Skin · damaged · Dec 12, 2023 · N564NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE ON FUSELAGE SKIN BTW FS517.00 TO FS 533.00 AND BTW STGR13RH TO STGR14RH. LIGHTNING STRIKE ON FUSELAGE SKIN BTW FS517.00 TO FS 533.00 AND BTW STGR13RH TO STGR14RH WAS REPAIRED PER CRJ-900 SRM 53-00-00-201-003-A03
- [SDR VNAA202401220014](https://openairdocs.org/sdr/VNAA202401220014.md): Skin · damaged · Dec 12, 2023 · N564NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE ON FUSELAGE SKIN BTW FS549.00 TO FS 565.00 AND BTW STGR13RH TO STGR14RH. LIGHTNING STRIKE ON FUSELAGE SKIN BTW FS549.00 TO FS 565.00 AND BTW STGR13RH TO STGR 14RH WAS REPAIRED PER CRJ-900 SRM 53-00-00-201-003-A03
- [SDR VNAA202401220002](https://openairdocs.org/sdr/VNAA202401220002.md): Skin · worn · Dec 12, 2023 · N564NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > WEAR ON EXTERNAL FUSELAGE SKIN (2EAS) BTW FS 897.70 TO FS 927.00, BTW STGR 27 TO STGR 26LH. WEAR ON EXTERNAL FUSELAGE SKIN (2EAS) BTW FS 897.70 TO FS 927.00, BTW STGR 27 TO STGR 26LH WAS REPAIRED PER REO 690-53-51-393 REV --
- [SDR VNAA202401220001](https://openairdocs.org/sdr/VNAA202401220001.md): Bracket · cracked · Dec 12, 2023 · N564NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH. AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH WAS REPAIRED PER REO 690-28-25-014 REV.--
- [SDR VNAA202401220005](https://openairdocs.org/sdr/VNAA202401220005.md): Skin · worn · Dec 11, 2023 · N564NN · Cndair CL6002D24 · Wing, Plate/Skin
  > DURING INSPECTION OF THE TASK CARD TRFKE001TJNJ:500-07-JIC IT WAS DETECTED WEAR ON SETTLEMENT AREA OF FAIRING 583AB AT LH WING LOWER SKIN. WEAR ON SETTLEMENT AREA OF FAIRING 583AB AT LH WING LOWER SKIN WAS REPAIRED PER REO 690-57-21-444 REV.--
- [SDR VNAA202401220004](https://openairdocs.org/sdr/VNAA202401220004.md): Skin · damaged · Dec 11, 2023 · N564NN · Cndair CL6002D24 · Trailing Edge Flaps
  > NICKS AND DENTS ON LOWER SKIN OF LH INBOARD FLAP FLS 15.00 TO FLS 65.5. AREA ON LOWER SKIN OF LH INBOARD FLAP FLS 15.00 TO FLS 42.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 57-52-01-101-001-A01 AND REPAIRED PER CRJ900 SRM 57-52-01-201-005-A01 AND AREA ON
- [SDR VNAA202202181111](https://openairdocs.org/sdr/VNAA202202181111.md): Controller · unserviceable · Feb 15, 2022 · N564NN · Cndair CL6002D24 · Cabin Pressure Controller
  > DURING CLIMB AT FL 200 THE CREW RECEIVED A CABIN ALT WARNING MESSAGE. THE OXYGEN MASKS FELL AND THE CREW DECLARED AN EMERGENCY AND RETURNED TO DFW. THEY HELD FOR QUITE SOME TIME TO BURN OFF GAS SO THEY DID NOT LAND OVERWEIGHT. TRUCKS ROLLED. THE FLIGHT LANDED
- [SDR VNAA202112071111](https://openairdocs.org/sdr/VNAA202112071111.md): Windshield · cracked · Dec 3, 2021 · N564NN · Cndair CL6002D24 · Flight Compartment Windows
  > APPROX 150 NM FROM CLT, THE WINDSCREEN BEGAN TO CRACK. THE CREW REQUESTED PRIORITY INTO CLT, HOWEVER DID NOT DECLARE AN EMERGENCY. DURING FLIGHT THE CRACK DID DEVELOP SOME, BUT IT STOPPED AS THEY DESCENDED. THEY LANDED SAFELY AND TAXIED TO THE GATE ON THEIR OW
- [SDR VNAA202105071111](https://openairdocs.org/sdr/VNAA202105071111.md): Hinge Fitting · gouged · May 5, 2021 · N564NN · Cndair CL6002D24 · Rudder Structure
  > DURING ROUTINE MAINTENANCE, THE RUDDER HINGE FITTING (P/N CC670-22162-5) WAS FOUND TO HAVE SEVERAL LOCATIONS OF GOUGES ON THE CORNERS OF THE CENTER LUGS. THE MEASUREMENTS OF THE DAMAGE ARE AS FOLLOWS:.377Ï¿½ LONG X.033Ï¿½ DEEP,.334Ï¿½ LONG X.025Ï¿½ DEEP,.
- [SDR VNAA2020080111101](https://openairdocs.org/sdr/VNAA2020080111101.md): Control Lever · failed · Jul 31, 2020 · N564NN · Cndair CL6002D24 · Landing Gear Selector
  > GEAR DISAGREE MESSAGE IMMEDIATELY UPON SELECTING HANDLE. CYCLE HANDLE, NO CHANGE. PULLED MANUAL RELEASE HANDLE. NO EVIDENCE OF GEAR MOVEMENT UNTIL MANUAL RELEASE. REMOVED AND REPLACED LANDING GEAR LEVER IAW AMM OPS CHECK GOOD AT THIS TIME.
- [SDR VNAA202003099995](https://openairdocs.org/sdr/VNAA202003099995.md): Angle · corroded · Mar 9, 2020 · N564NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > WHILE PERFORMING REPLACEMENT OF FUSELAGE PAX DOOR HINGE, FOUND KICK PLATE ANGLE TO BE CORRODED IN CENTER OF DOOR WAY. 02/25/20 (ROSEM) M/A: 1. NA C/A: 1. UPON REMOVAL OF MID CAP ANGLE FOUND IT TO BE CORRADED BEYOND REPAIRABLE LIMITS IAW CRJ900 SRM 53-00-00-101
- [SDR VNAA202003099994](https://openairdocs.org/sdr/VNAA202003099994.md): Angle · corroded · Mar 9, 2020 · N564NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > F.S 280 FWD J-ANGLE CORRODED 2/19/20. (TK) M/A: 1. N/A C/A: 1. FOUDN THE FWD J-ANGLE (FS280) TO BE OUT OF ALLOWABLE LIMITS IAW CRJ 900 AMM 53-00-00-001-A01. MTC 02/25/20 M/A: 2. REMOVED THE FS280 J-ANGLE IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-00
- [SDR VNAA202003099993](https://openairdocs.org/sdr/VNAA202003099993.md): Floorbeam · cracked · Mar 9, 2020 · N564NN · Bombdr CL6002D15 · Fuselage Main, Floor Beam
  > L/H COCKPIT FLOOR BEAM, FWD SIDE F.S280, LBL12.00 IS CRACKED WHERE BEAM ATTACHES TO F.S.280. 2/18/20. (TK) M/A: 1. BOMBARDIER REO 690-53-11-1227 REQUIRES COMPLETION. MTC 2/19/20 C/A: 1. C/W STEPS 1-3 OF BOMBARDIER REO 690-53-11-1227, REV.P1 DATED 2020-2-19. MT
- [SDR VNAA202003099992](https://openairdocs.org/sdr/VNAA202003099992.md): Drag Angle · cracked · Mar 9, 2020 · N564NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > AFT FUSELAGE R/H FWD DRAG ANGLE CRACKED. 2/18/20. (TK) M/A: 1. R/H FWD DRAG ANGLE REQUIRES REPAIR IAW CRJ900 SRM 55-31-00-201-001-A01. 2/19/20 C/A: 1. C/W STEPS 1&2 OF CRJ900 SRM 55-51-00-201-001-A01. 2/19/20 M/A: 2. NDT REQUIRED IAW STEP 3 OF SRM 55-31-00-201
- [SDR VNAA202003099991](https://openairdocs.org/sdr/VNAA202003099991.md): Drag Angle · cracked · Mar 9, 2020 · N564NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > AFT FUSELAGE L/H AFT DRAG ANGLE CRACKED. 2/17/20 (PCC) M/A: 1. REMOVED CRACKED DRAG ANGLE IAW CRJ 900 SRM 51-42-13-001-001-A01,51-42-20-001-001-A01,AND 51-42-22-001-001-A01. 02/18/20 C/A: 1. INSTALLED NEW SERVICEABLE DRAG ANGLE IAW CRJ 900 SRM 51-42-13-001-001
- [SDR VNAA2019051211101](https://openairdocs.org/sdr/VNAA2019051211101.md): Manifold · failed · May 12, 2019 · N564NN · Cndair CL6002D24 · Landing Gear Steering System
  > THE CREW RECEIVED A NOSE WHEEL STEERING INOP CAUTION MESSAGE IN FLIGHT. THEY DECLARED EMERGENCY LANDING INTO CLT. R&R NWS MANIFOLD, OPS CHECK GOOD.

Next page: https://openairdocs.org/aircraft/N564NN/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 = 'N564NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N564NN/reports

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