N565NN
Service difficulty reports · 47
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "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"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR VNAA2026010611103Skin · dentedDENT 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 690-53-11-21SDR VNAA2025062011101Cover · missingLOW 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 VNAA2024061311101Pseu · unserviceableGEAR 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 VNAA2024060411102Actuator · failedGEAR 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 CHSDR VNAA20240212009Rib · crackedCRACK 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-A01SDR VNAA20240214002Hinge Fitting · excess playFREE 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. BSDR VNAA20240212007Stringer Splice · corrodedCORROSIÓN 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 VNAA20240212001Drag Angle · crackedCRACK 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-900SDR VNAA20240212010Seat Track · corrodedCORROSION 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 VNAA20240214011Skin · damagedFUSE 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 VNAA20240214010Seat Track · corrodedCORROSION 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 FSSDR VNAA20240214009Frame · corrodedCORROSION 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 53-00-06-201-0SDR VNAA20240214008Canister · crackedCRACK 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 VNAA20240214007Canister · crackedCRACK 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 VNAA20240214006Seat Track · corrodedCORROSION 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) WSDR VNAA20240214005Seat Track · gougedGOUGES 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 ASDR VNAA20240214003Skin · dentedINITIAL 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 RSDR VNAA20240213006Support · crackedAFTER 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 690-28-25SDR VNAA20240212006Intercostal · corrodedCORROSION 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-A01SDR VNAA20240213005Seat Track · corrodedCORROSION 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 EVSDR VNAA20240213004Seat Track · corrodedCORROSION 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 VNAA20240214004Door Sill · corrodedCORROSION 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 VNAA20240212008Stringer · corrodedCORROSION 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 VNAA20240212005Floorbeam · crackedIN 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 690-5SDR VNAA20240212004Bracket · corrodedCORROSION 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 FS501SDR VNAA20240212003Skin · damagedPERM 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 LOCSDR VNAA20240212002Skin · damagedPERM 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 VNAA202303231111Pseu · unserviceableGEAR 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 VNAA202303021111Outflow Valve · unserviceableAUTO 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 VNAA202302171112None · noneSIGNIFICANT 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 VNAA20240214001Rib · crackedCRACK 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-A01SDR VNAA202209081111Fadec · unserviceableDUAL 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 71-00-00-710-801SDR VNAA202203231111None · unserviceableAIRCRAFT 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 VNAA2020092711101Unknown · odorSMELL 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 CHESDR VNAA2020052711101Warning System · false activationON 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 DECSDR VNAA202005129995Angle · corrodedFS 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 VNAA2019122861102Bearing Race · damagedGEAR 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. GEARSDR VNAA2019120961101Control Lever · failedGEAR 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 VNAA2019060111101Windshield · failedCAPTAINS WINDSHIELD SHATTERED ON APPROACH INTO CLT. MX REPLACED LH WINDSHIELD.SDR VNAA2018111511102Unknown · odorDURING 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 THESDR VNAA2018092971101A/C Pack · seizedUPON 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 PACKSDR VNAA2018091911101Warning System · false activationAFTER 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 VNAA2017071911101A/C Pack · failedTHE 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 ISSSDR VNAA2016050700004Handle · unsecureAFT 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 VNAA2016041400015Brake · overheatedBRAKE OVERHEAT MESSAGE DURING APPROACH. THE CREW DECLARED AN EMERGENCY, CONTINUED THE APPROACH, AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED CHECKS IAW THE AMM.SDR VNAA2015091700019Warning Message · illuminatedCREW 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 VNAA2015040600013Connector · disconnected2 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.
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