# Service difficulty reports: N565NN

A list on [N565NN](https://openairdocs.org/aircraft/N565NN.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR VNAA2026010611103](https://openairdocs.org/sdr/VNAA2026010611103.md): Skin · dented · Jan 2, 2026 · N565NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > DENT BELOW CAPTAINS WINDSHIELD FROM BIRDSTRIKE BETWEEN FS210 AND FS 220 NEAR STR 12, IN THE FORM OF A IRREGULAR PENTAGON SIDES MESSURING 10" X 4-5/8"X 5-1/2" X 8" X 2-15/16" AND 0.25" DEEP AT THE DEEPEST POINT. PERFORMED PERMANENT REPAIR IAW REO 690-53-11-21
- [SDR VNAA2025062011101](https://openairdocs.org/sdr/VNAA2025062011101.md): Cover · missing · Jun 19, 2025 · N565NN · Cndair CL6002D24 · Service Doors
  > LOW PRESS AIR COVER MISSING / INSTALLED MISSING LOW PRESSURE GROUND CONNECTION COVER AND QUICK RELEASE PIN IAW CRJ 900 AMM 21-20-02-400-801-A01-PSA.
- [SDR VNAA2024061311101](https://openairdocs.org/sdr/VNAA2024061311101.md): Pseu · unserviceable · Jun 6, 2024 · N565NN · Cndair CL6002D24 · Landing Gear Position and Warning
  > GEAR DISAGREE MESSAGE ON APPROACH NOSE GEAR DID NOT DROP MANUAL EXTENSION PERFORMED AS PER QRH / REMOVED AND REPLACED NLG DOWNLOCK-ACTUATOR IAW CRJ900 AMM 32-32-08-000/400-801-A01. LANDING GEAR EXTENSION/RETRACTION SYSTEM OPS TESTED GOOD. REMOVED AND REPLACED
- [SDR VNAA2024060411102](https://openairdocs.org/sdr/VNAA2024060411102.md): Actuator · failed · Jun 2, 2024 · N565NN · Cndair CL6002D24 · Landing Gear Actuator
  > GEAR DISAGREE ON APPROACH, NOSE GEAR DID NOT COME DOWN FOR A FEW SECONDS, LATER ON WE GOT ALL DOWN 3 GREEN INDICATIONS AFTER CYCLING GEAR UP AND DOWN / REMOVED AND REPLACED NLG RECTRACT ACTUATOR IAW CRJ900 AMM 32-32-09-000-801/TR 32-0652. OPS CHECK AND LEAK CH
- [SDR VNAA20240212009](https://openairdocs.org/sdr/VNAA20240212009.md): Rib · cracked · Feb 2, 2024 · N565NN · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > CRACK ON RIB LEADING EDGE SS57.16 AT LH WING. RIB LEADING EDGE SS57.16 AT LH WING WAS REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01 AND SRM 51-42-21-001-001-A01
- [SDR VNAA20240214002](https://openairdocs.org/sdr/VNAA20240214002.md): Hinge Fitting · excess play · Jan 28, 2024 · N565NN · Cndair CL6002D24 · Vertical Stabilizer
  > FREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. HINGE FITTING NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WERE REPLACED PER RIL #2103 REV. B
- [SDR VNAA20240212007](https://openairdocs.org/sdr/VNAA20240212007.md): Stringer Splice · corroded · Jan 28, 2024 · N565NN · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSIÓN ON STRINGER AND SPLICE 25RH IN STA. FS=319.70 TO FS=333.00 AT MAIN AVIONICS COMPARTMENT. SUMMARY; STRINGER AND SPLICE 25RH IN STA. FS=319.70 TO FS=333.00 AT MAIN AVIONICS COMPARTMENT WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01. SRM 51-42-21-
- [SDR VNAA20240212001](https://openairdocs.org/sdr/VNAA20240212001.md): Drag Angle · cracked · Jan 28, 2024 · N565NN · Cndair CL6002D24 · Vertical Stabilizer
  > CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM. CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ-900
- [SDR VNAA20240212010](https://openairdocs.org/sdr/VNAA20240212010.md): Seat Track · corroded · Jan 27, 2024 · N565NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH SIDE SEAT RAILS BTW FS669.40 TO FS913.00. LH SIDE SEAT RAILS BTW FS669.40 TO FS913.00 (6EA) ARE OUT OF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 NOTE 1. AND WERE REPLACED PER CRJ-900 AMM 53-00-49 (CONFIG A12)
- [SDR VNAA20240214011](https://openairdocs.org/sdr/VNAA20240214011.md): Skin · damaged · Jan 14, 2024 · N565NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > FUSE SKIN LIGHTING STRIKE DAMAGE REPAIR. FUSE SKIN LIGHTING STRIKE DAMAGED WERE REPAIRED PER CRJ-900 SRM 53-00-00-201-003-A03 AND REO 690-53-11-1676 REV. --
- [SDR VNAA20240214010](https://openairdocs.org/sdr/VNAA20240214010.md): Seat Track · corroded · Jan 11, 2024 · N565NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AND SCRATCHES ON FLOOR LH SEAT RAIL BTW FS 847.00 +16.00 TO FS 977.00 (SEVERAL LOCATIONS) AND CORROSION ON FLOOR RH SEAT RAIL BTW FS 897.00 TO FS 913.00. FLOOR LH SEAT RAIL BTW FS 847.00 +16.00 TO FS 977.00 AND FLOOR RH SEAT RAIL BTW FS 897.00 TO FS
- [SDR VNAA20240214009](https://openairdocs.org/sdr/VNAA20240214009.md): Frame · corroded · Jan 10, 2024 · N565NN · Cndair CL6002D24 · Fuselage Main, Frame
  > CORROSION ON FRAME, LOCATED BTW FS=1015.00 AND STGR 25LH TO 25RH AT REAR FUSELAGE INTERNAL STRUCTURE, BELOW FLOOR. FRAME, LOCATED BTW FS=1015.00 AND STGR 25LH TO 25RH AT REAR FUSELAGE INTERNAL STRUCTURE, BELOW FLOOR WAS REPAIRED PER CRJ-900 SRM 53-00-06-201-0
- [SDR VNAA20240214008](https://openairdocs.org/sdr/VNAA20240214008.md): Canister · cracked · Jan 10, 2024 · N565NN · Cndair CL6002D24 · Wing Miscellaneous Structure
  > 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 VNAA20240214007](https://openairdocs.org/sdr/VNAA20240214007.md): Canister · cracked · Jan 10, 2024 · N565NN · Cndair CL6002D24 · 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 VNAA20240214006](https://openairdocs.org/sdr/VNAA20240214006.md): Seat Track · corroded · Jan 10, 2024 · N565NN · Cndair CL6002D24 · Fuselage Internal Mounting Structure
  > CORROSION ON SIDE SEAT RAIL BWT FS 565 TO FS: 669.40 OF STGR15R SIDE SEAT RAILS BWT FS 565 TO FS: 669.40 OF STGR 15R (3EAS) ARE OUT OFF LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02 NOTE 1. THEREFORE SIDE SEAT RAILS BWT FS: 565 TO FS: 669.40 OF STGR 15R (3EAS) W
- [SDR VNAA20240214005](https://openairdocs.org/sdr/VNAA20240214005.md): Seat Track · gouged · Jan 10, 2024 · N565NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > GOUGES ON SIDE SEAT RAIL BWT FS 437 TO FS: 533 OF STGR15R SIDE SEAT RAILS FS 379 TO FS 565 STG 15 RH (2EAS) ARE OUT OFF LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02 NOTE 1,THEREFORE SIDE SEAT RAILS FS 379 TO FS 565 STG 15 RH ( 2 EA) WERE REPLACED PER CRJ-900 A
- [SDR VNAA20240214003](https://openairdocs.org/sdr/VNAA20240214003.md): Skin · dented · Jan 9, 2024 · N565NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > INITIAL INSPECTION: SEVERAL DENTS ON FUSELAGE SKIN, SETTLEMNT AREA OF LEFT AND RIGTH VENTRAL FIN FAIRING BTW FS 1126.00 TO REAR SPAR DATUM STABILIZER 67.5% SEVERAL DENTS ON FUSELAGE SKIN, SETTLEMNT AREA OF LEFT AND RIGTH VENTRAL FIN FAIRING BTW FS 1126.00 TO R
- [SDR VNAA20240213006](https://openairdocs.org/sdr/VNAA20240213006.md): Support · cracked · Jan 9, 2024 · N565NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFTER REMOVAL OF LOWER FUSELAGE FAIRINGS, CRACK ON AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH. CRACK ON 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
- [SDR VNAA20240212006](https://openairdocs.org/sdr/VNAA20240212006.md): Intercostal · corroded · Jan 9, 2024 · N565NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON LH INTERCOSTAL IN STA. FS= 349 TO FS= 364 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT INTERCOSTAL NO DAMAGE ALLOWED, PER CRJ-900 SRM 53-21-23-101-003-A02 THEREFORE WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01
- [SDR VNAA20240213005](https://openairdocs.org/sdr/VNAA20240213005.md): Seat Track · corroded · Jan 8, 2024 · N565NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACKS LBL 27 STA 485 TO STA 501 (1E/A), LBL 9 STA 581 TO STA 661+90 (2E/A) AND RBL 9 STA 349 TO STA 661+90(5E/A). SEAT TRACKS LBL 27 STA 485 TO STA 501 (1E/A), LBL 9 STA 581 TO STA 661+90 (2E/A) AND RBL 9 STA 349 TO STA 661+90(5E/A) WERE EV
- [SDR VNAA20240213004](https://openairdocs.org/sdr/VNAA20240213004.md): Seat Track · corroded · Jan 8, 2024 · N565NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SIDE SEAT RAILS BTW FS669.40 TO FS985.00 (6EA). RH SIDE SEAT RAILS BTW FS669.40 TO FS985.00 (6EA) WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 AND REPLACED PER CRJ-900 AMM 53-00-49 (CONFIG A12)
- [SDR VNAA20240214004](https://openairdocs.org/sdr/VNAA20240214004.md): Door Sill · corroded · Jan 7, 2024 · N565NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO COMPARTMENT DOOR SILL BTW FS 1000.00 TO FS 1047.00, BTW STGR 17LH AND STGR 18LH. (SM) DOOR SILL BTW FS 1000.00 TO FS 1047.00, BTW STGR 17LH AND STGR 18LH WAS REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01 PAR. 6.C. CRJ 900 SRM 51-42-10-
- [SDR VNAA20240212008](https://openairdocs.org/sdr/VNAA20240212008.md): Stringer · corroded · Jan 7, 2024 · N565NN · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 24R IN STA. FS= 333.00 TO FS= 349 AT MAIN AVIONICS COMPARTMENT. STRINGER 24R IN STA. FS= 333.00 TO FS= 349 AT MAIN AVIONICS COMPARTMENT WAS REPAIRED PER CRJ-900 SRM 53-00-03-201-001-A02.
- [SDR VNAA20240212005](https://openairdocs.org/sdr/VNAA20240212005.md): Floorbeam · cracked · Jan 7, 2024 · N565NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > IN REF TO: DURING INSPECTION OF THE TASK CARD 53-10-219B, IT WAS DETECTED CRACK ON RIVETS AREA BELOW FLOOR AT BULKHEAD DOOR POST, BTW RBL9 AND FS 280.00. CRACK ON RIVETS AREA BELOW FLOOR AT BULKHEAD DOOR POST, BTW RBL9 AND FS 280.00 WAS REPAIRED PER REO 690-5
- [SDR VNAA20240212004](https://openairdocs.org/sdr/VNAA20240212004.md): Bracket · corroded · Jan 7, 2024 · N565NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON BRACKET MACHINED (4EA) AT INTERNAL STRUCTURE FWD BAGGAGE BAY CARGO BELOW FLOOR BETWEEN STGR 23RH/23LH AND FS501.00 TO FS661.00+32.00. BRACKET MACHINED (4EA) AT INTERNAL STRUCTURE FWD BAGGAGE BAY CARGO BELOW FLOOR BETWEEN STGR 23RH/23LH AND FS501
- [SDR VNAA20240212003](https://openairdocs.org/sdr/VNAA20240212003.md): Skin · damaged · Jan 5, 2024 · N565NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > PERM REPAIR - LOWER FUSELAGE SKIN MULTIPLE LIGHTNING STRIKES WITHIN 746.25 FHS FROM REV.-- (STARTING AT 19,934.42 FH), REPAIR, OR REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES IN REF TRFKE00BDQWC:EA A1-690-53-00002. LIGHTNINGS STRIKES LOC
- [SDR VNAA20240212002](https://openairdocs.org/sdr/VNAA20240212002.md): Skin · damaged · Jan 5, 2024 · N565NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > PERM REPAIR BEFORE 20,720.22 FH - LIGHTNING STRIKE STR24R-STR25R AT FS 235.00 THE SUBJECT CONDITION IS STRUCTURALLY ACCEPTABLE FOR 900 FLIGHT HOURS FROM THE TIME OF INCORPORATION OF THIS REO AT REV IN REF TRFKE00BD723:690-53-11-1621. PERM REPAIR BEFORE 20,720.
- [SDR VNAA202303231111](https://openairdocs.org/sdr/VNAA202303231111.md): Pseu · unserviceable · Mar 21, 2023 · N565NN · Cndair CL6002D24 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE IN FLIGHT. NOSE GEAR DID NOT EXTEND. CYCLED HANDLE ALL GEAR EXTENDED. R/R PSEU IAW CRJ 900 AMM 32-61-01-000/400-801. EXTENDED AND RETRACTED LANDING GEAR SEVERAL TIMES. NO DEFECTS NOTED. OPS CHK GOOD AT THIS TIME.
- [SDR VNAA202303021111](https://openairdocs.org/sdr/VNAA202303021111.md): Outflow Valve · unserviceable · Feb 27, 2023 · N565NN · Cndair CL6002D24 · Cabin Pressure Control System
  > AUTO PRESS AMBER MSG ON CLIMBOUT. PERFORMED TROUBLESHOOTING IAW CRJ 900 FIM 21-31-00-810-803. REMOVED AND REPLACED OUTFLOW VALVE CRJ 900 AMM 21-32-01-000/400/801/A01. OPS CHECK GOOD.
- [SDR VNAA202302171112](https://openairdocs.org/sdr/VNAA202302171112.md): None · none · Feb 16, 2023 · N565NN · Cndair CL6002D24 · Passenger/Crew Doors
  > SIGNIFICANT CORROSION FOUND ON FOLDING STEP HINGE, IDENTIFIED AS LEVEL 2 CORROSION ACCORDING TO GMM 14.12.1. REMOVED AND REPLACED PASSENGER DOOR FOLDING STEP HINGE IAW 52-11-04-400-801-A01. OPS CHECK GOOD, NO OTHER DEFECTS NOTED AT THIS TIME.
- [SDR VNAA20240214001](https://openairdocs.org/sdr/VNAA20240214001.md): Rib · cracked · Feb 2, 2023 · N565NN · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > CRACK ON MACHINED RIB LEADING EDGE SS58.41 AT RIGHT WING. (SM) RIB LEADING EDGE SS58.41 AT RIGHT WING WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01
- [SDR VNAA202209081111](https://openairdocs.org/sdr/VNAA202209081111.md): Fadec · unserviceable · Sep 5, 2022 · N565NN · Cndair CL2151A10 · Engine (Turbine/Turboprop)
  > DUAL R ENG FADEC FAULT RESULTING IN R ENG FLAMEOUT DURING CLIMB. HAD SUCCESSFUL AUTO RE-LIGHT. PREFORMED A VISUALLY CHECK OF RH FADEC AND MADE SURE ALL CONNECTORS ARE SECURED, NO DEFECTS NOTED. PERFORMED A POWER ON BUILT IN TEST IAW CRJ900 AMM 71-00-00-710-801
- [SDR VNAA202203231111](https://openairdocs.org/sdr/VNAA202203231111.md): None · unserviceable · Mar 20, 2022 · N565NN · Cndair CL6002D24 · Landing Gear Steering System
  > AIRCRAFT RETURNED TO CLT AFTER RECEIVING NWS STEERING INOP MSG. ARFF RESPONDING. RTF-NOSEWHEEL STEERING INOP IN FLIGHT / T/S B1 CODE 007464 PER CRJ 900 FIM 32-51-50-810-801, REMOVED AND REPLACED NWS STEERING MANIFOLD IAW CRJ 900 AMM 32-51-50-000/400-801, OPS
- [SDR VNAA2020092711101](https://openairdocs.org/sdr/VNAA2020092711101.md): Unknown · odor · Sep 27, 2020 · N565NN · Cndair CL6002D24 · Air Distribution System
  > SMELL OF SMOKE IN COCKPIT AND CABIN DESCENDING THROUGH FL 250 TO 120 FT, NOTED IN CLOUD LAYER. CLEARED ONCE OUT OF CLOUD LAYER. SMELLED LIKE BURNING WOOD. C/W GVI OF AIR CONDITIONING SYSTEM AND PERFORMED OPS CHECK, IAW CRJ 900 AMM 21-51-00-710-801. OPS CHE
- [SDR VNAA2020052711101](https://openairdocs.org/sdr/VNAA2020052711101.md): Warning System · false activation · May 26, 2020 · N565NN · Cndair CL6002D24 · Landing Gear Brake System
  > ON APPROACH INTO CLT, THE CREW RECEIVED A BRAKE OVERHEAT CAUTION MESSAGE FOR THE LT MAIN GEAR WHEEL WELL. THE CREW RAN THE QRH, WHICH INCLUDED LOWERING THE GEAR. UPON DOING THIS, THE CAUTION MESSAGE WENT AWAY. AS A PRECAUTIONARY MEASURE THOUGH, THE CREW DEC
- [SDR VNAA202005129995](https://openairdocs.org/sdr/VNAA202005129995.md): Angle · corroded · May 12, 2020 · N565NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > FS 280.00 CROSSBEAM, FWD J ANGLE CORRODED. LOCATED, DRILLED AND INSTALLED NEW ANGLE ASSY AT FS280 LBL 12-RBL 12 IAW CRJ900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01.
- [SDR VNAA2019122861102](https://openairdocs.org/sdr/VNAA2019122861102.md): Bearing Race · damaged · Dec 26, 2019 · N565NN · Cndair CL6002D24 · Nose/Tail Landing Gear Strut/Axle
  > GEAR DISAGREE WARNING AFTER RAISING GEAR LEVER AFTER TAKE OFF. R&R LANDING GEAR CONTROL PANEL. OPS CHECK BAD. REMOVED NLG PISTON AXLE ASSY AND FOUND UPPER BEARING TO BE DAMAGED ON INNER RACE. REPLACED INNER STRUT BEARING AND REPACKED THE STRUT IAW AMM. GEAR
- [SDR VNAA2019120961101](https://openairdocs.org/sdr/VNAA2019120961101.md): Control Lever · failed · Dec 6, 2019 · N565NN · Cndair CL6002D24 · Landing Gear Selector
  > GEAR DISAGREE WARNING MSG AFTER TAKEOFF RETURN TO FIELD. ALL THREE INDICATED DOWN AND GREEN, DID NOT GET ANY GEAR RETRACTION OR MOVEMENT. REMOVED AND REPLACED LANDING GEAR LEVER. OPS CHECK GOOD AT THIS TIME.
- [SDR VNAA2019060111101](https://openairdocs.org/sdr/VNAA2019060111101.md): Windshield · failed · Jun 1, 2019 · N565NN · Cndair CL6002D24 · Flight Compartment Windows
  > CAPTAINS WINDSHIELD SHATTERED ON APPROACH INTO CLT. MX REPLACED LH WINDSHIELD.
- [SDR VNAA2018111511102](https://openairdocs.org/sdr/VNAA2018111511102.md): Unknown · odor · Nov 15, 2018 · N565NN · Cndair CL6002D24 · Air Distribution System
  > DURING TAKEOFF THE CREW SMELLED SMOKE IN BOTH THE COCKPIT AND THE CABIN. DECLARED AN EMERGENCY AND RETURNED TO THE FIELD IN CLT. PULLED OFF TO THE HARDSTAND WHERE THE TRUCKS MET THEM. NO VISIBLE SMOKE WAS DETECTED. DID NOT NEED TO EVACUATE. ABLE TO TAXI TO THE
- [SDR VNAA2018092971101](https://openairdocs.org/sdr/VNAA2018092971101.md): A/C Pack · seized · Sep 27, 2018 · N565NN · Cndair CL6002D24 · Cabin Cooling System
  > UPON LANDING CREW REPORTED SMOKE IN THE CABIN. THEY EVACUATED THE A/C AND THE FIRE DEPARTMENT RESPONDED. THE FIRE DEPARTMENT CHECKED THE A/C FOR EVIDENCE OF FIRE AND THEY WERE UNABLE TO FIND ANY HOT SPOTS OR EVIDENCE OF FIRE. MX INSPECTED AND FOUND THE RH PACK
- [SDR VNAA2018091911101](https://openairdocs.org/sdr/VNAA2018091911101.md): Warning System · false activation · Sep 18, 2018 · N565NN · Cndair CL6002D24 · Door Warning System
  > AFTER TAKEOFF OUT OF DCA THE CREW RECEIVED A SERVICE DOOR CAUTION MSG IN FLIGHT AND COULD NOT GET THE AIRCRAFT TO PRESSURIZE. AIRCRAFT WAS FERRIED TO GSP AND THEY COULD NOT DUPLICATE THE ISSUE. ALL OPS CHECKED GOOD.
- [SDR VNAA2017071911101](https://openairdocs.org/sdr/VNAA2017071911101.md): A/C Pack · failed · Jul 19, 2017 · N565NN · Cndair CL6002D24 · Cabin Cooling System
  > THE AIRCRAFTS CABIN AND COCKPIT FILLED UP WITH SMOKE DURING TAXI ON THE RAMP. THEY STOPPED AND EVACUATED THE PASSENGERS THROUGH THE MAIN CABIN DOOR ONTO THE RAMP. MAINTENANCE INSPECTED THE AIRCRAFT AND DISCOVERED THAT THE LH AIRCONDITIONING PACK CAUSED THE ISS
- [SDR VNAA2016050700004](https://openairdocs.org/sdr/VNAA2016050700004.md): Handle · unsecure · May 7, 2016 · N565NN · Cndair CL6002D24 · Cargo/Baggage Doors
  > AFT CARGO DOOR OPEN MESSAGE AFTER TAKEOFF. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, CLOSED POPPED DOOR LATCH HANDLE, AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2016041400015](https://openairdocs.org/sdr/VNAA2016041400015.md): Brake · overheated · Apr 14, 2016 · N565NN · Cndair CL6002D24 · Landing Gear Brake System
  > BRAKE OVERHEAT MESSAGE DURING APPROACH. THE CREW DECLARED AN EMERGENCY, CONTINUED THE APPROACH, AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED CHECKS IAW THE AMM.
- [SDR VNAA2015091700019](https://openairdocs.org/sdr/VNAA2015091700019.md): Warning Message · illuminated · Sep 17, 2015 · N565NN · Cndair CL6002D24 · Door Warning System
  > CREW REPORTED AFT CARGO DOOR AMBER MESSAGE. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. AFT CARGO DOOR INDICATION DEFERRED IAW MEL. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2015040600013](https://openairdocs.org/sdr/VNAA2015040600013.md): Connector · disconnected · Apr 6, 2015 · N565NN · Cndair CL6002D24 · Light System Wiring
  > 2 LEFT FORWARD OVERWING EMERGENCY LIGHTS REPORTED INOPERATIVE. MAINTENANCE TROUBLESHOT SYS AND FOUND CONNECTOR AT 12 A/C SIDEWALL DISCONNECTED. MAINTENANCE RESECURED CONNECTOR AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

## 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 = 'N565NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N565NN/reports

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