N600NN
Service difficulty reports · 68
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 = 'N600NN' 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 = 'N600NN' 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 VNAA2026090224201Access Panel · missingACCESS PANEL ON TOP OF LT WING MISSING (591AT). PREFORMED GVI IAW AMM 05-20-00-210-801-PSA STEP B, NO DEFECTS NOTED. INSTALLED TRAILING EDGE WEDGE IAW AMM 57-52-32-400-807-A01.SDR VNAA2026050817702Ecu · faultedSTEERING INOP CAUTION IN FLIGHT SYSTEM DID NOT COME BACK AFTER RESETING WITH QRH PROCEDURES. / INTERROGATED MDC FOUND MULTIPLE B1 CODES FOR NWS ECU REMOVED AND REPLACED NWS ECU IAW CRJ900 AMM 32€“51€“10€“000/400-801. OPS CHECK GOOD.SDR VNAA2026050417406Control Wheel · unserviceableSTEERING INOP CAUTION ON APPROACH PRIOR TO GEAR DOWN SELECTION. REMOVED AND REPLACED THE PILOT HAND WHEEL CONTROL IAW AMM 32-51-01-000/400-801-A01. PERFORMED OPERATIONAL TEST OF THE NOSE WHEEL STEERING IAW AMM 32-51-00-710-801-A01. THE OPERATIONAL CHECK GOODSDR VNAA2026050417204Warning Message · false activationSTEERING INOP CAUTION IN FLIGHT. PERFORMED SYSTEM RESET PER MIPM MSG EXTINGUISHED AND DID NOT REOCCUR.SDR VNAA2026042916801Control Handle · inoperativeSTEERING INOP IN FLIGHT. / REMOVED AND REPLACED PILOT HAND CONTROL IAW CRJ 900 AMM 32€“51€“01€“000/400€“801. OPS CHECK GOOD.SDR VNAA2026012011201Windshield · crackedENROUTE TO CVG THE CREW SAW A CRACK IN THE WINDSHIELD AND GOT A WINDSHIELD HEAT CAUTION MESSAGE. REMOVED AND REPLACED RH WINDSHIELD IAW CRJ-900 AMM 56-11-01-000/400-801-A01-PSA. COMPLETED FINIAL TORQUE CHECK, SEALED AND COMPLETED OPS CHECK (OPS CHECK GOOD)SDR VNAA20250715034Skin · gougedGOUGES AT HOLE COUNTERSINK TO LH WING FIXED L/E PANEL AT SLAT STA. 144.94. GOUGES AT HOLE COUNTERSINK TO LH WING FIXED L/E PANEL AT SLAT STA. 144.94 WAS REPAIRED PER REO 690-57-41-522 REV. - - .SDR VNAA20250715027Panel · gougedGOUGES AT HOLE COUNTERSINK TO LH WING FIXED L/E PANEL AT SLAT STA. 144.94. GOUGES AT HOLE COUNTERSINK TO LH WING FIXED L/E PANEL AT SLAT STA. 144.94 WAS REPAIRED PER REO 690-57-41-522 REV. - - .SDR VNAA20250715023Seat Track · corrodedCORROSION ON FITING (PN: A414251-1) 1EA FRONT CORNER AT FWD LAV. FITTING (PN: A414251-1) 1EA FRONT CORNER AT FWD LAV WAS REPLACE PER SAFRAN CMM 25-40-40.SDR VNAA20250715022Fitting · corrodedCORROSION ON FLOOR FITTING (PN: CDSP2019-7C-620) 1EA ACCESS 107 COUNTER AT GALLEY 1. BRACKET FLOOR FITTING ACCESS 107 COUNTER AT GALLEY 1 WAS REPLACED PER SAFRAN CMM 25-33-96SDR VNAA20250715026Seat Track · corrodedCORROSION ON SEAT RAILS OF RBL9 BTW FS581.00 TO FS693.00 (3EA). SEAT RAILS OF LBL9 BTW FS581.00 TO FS693.00 (3EA) WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02 AND SRM 53-41-49-101-001-A02 AND REPLACED PER CRJ-900 AMM 53-00-49 AND SRM 51-41SDR VNAA20250715025Seat Track · corrodedCORROSION ON SEAT RAILS OF RBL9 BTW FS581.00 TO FS693.00 (3EA). SEAT RAILS OF LBL9 BTW FS581.00 TO FS693.00 (3EA) WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02 AND SRM 53-41-49-101-001-A02 AND REPLACED PER CRJ-900 AMM 53-00-49 AND SRM 51-41SDR VNAA20250715024Seat Track · corrodedCORROSION ON SEAT RAILS OF RBL9 BTW FS581.00 TO FS693.00 (3EA). SEAT RAILS OF RBL9 BTW FS581.00 TO FS693.00 (3EA) WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02 AND SRM 53-41-49-101-001-A02 AND REPLACED PER CRJ-900 AMM 53-00-49 AND CRJ-900 SDR VNAA20250715014Mount · corrodedCORROSION ON ANGLE MOUNTING OF SERVICE DOOR SURROUND. ANGLE MOUNTING OF SERVICE DOOR SURROUND WAS EVALUATED WITH EXCESSIVE DAMAGE PER CRJ-900 SRM 53-21-23-101-002-A02 AND REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.SDR VNAA20250714007Canister · crackedCRACK IN CANISTER, WELDED NO.3 IN STA. WS148 AT LH MAIN FUEL TANK. CRACK IN CANISTER, WELDED NO.3 IN STA. WS148 AT LH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV -SDR VNAA20250714009Seat Track · corrodedCORROSION ON LH SIDE SEAT RAIL BTW FS379.00 TO FS677.00 (3EA). LH SIDE SEAT RAIL BTW FS379.00 TO FS677.00 (3EA) WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01, SRM 53-31-49-101-001-A02 AND REPLACED PER CRJ-900 AMM 53-00-49.SDR VNAA20250714008Seat Track · corrodedCORROSION ON RH SIDE SEAT RAIL BTW FS379.00 TO FS677.00 (4EA). RH SIDE SEAT RAIL BTW FS379.00 TO FS677.00 (4EA) WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01, SRM SRM 53-31-49-101-001-A02 AND REPLACED PER CRJ-900 AMM 53-00-49.SDR VNAA20250715008Drag Angle · crackedCRACK ON VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT/FDW LH DRAG ANGLES BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT/FDW LH DRAG ANGLES BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TSDR VNAA20250715007Drag Angle · crackedCRACK ON VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT RH DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT RH DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BLSDR VNAA20250714006Rib · crackedCRACK ON MACHINED RIB LEADING EDGE SS58.41 AT LEFT WING. CRACK ON MACHINED RIB LEADING EDGE SS58.41 AT LEFT WING WAS REPAIRED REO 690-57-41-240 REV --SDR VNAA20250714010Bracket · corrodedCORROSION ON BRACKETS, MACHINED (6EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT. BRACKET MACHINED FS 517.00, FS565.00 BTW STRG 26/27, FS 533.00 BTW FS549.00 STRG24/25RH AND FS629 BTW STGR 26 TO 27 LH (4 EAS) ON FWD / CTR BAGGAGE-BAY WERE EVALUATED OUT OSDR VNAA20250714005Seat Track · corrodedCORROSION ON SEAT RAILS AT RBL9/LBL9 FROM FS693 TO FS 1000.00 AND RBL27/LBL27 BTW FS927 TO FS1000 AT PASSENGER COMPARTMENT INTERNAL STRUCTURE. CORROSION ON SEAT RAILS AT RBL9/LBL9 FROM FS693 TO FS 1000.00 AND RBL27/LBL27 BTW FS927 TO FS1000 WAS EVALUATED OUTSDR VNAA20250714004Seat Track · corrodedCORROSION ON SEAT RAIL BTW FS 744.15 TO FS 977.00 AND STGR 15LH AT CABIN PAX. SEAT RAIL BTW FS 744.15 TO FS 977.00 AND STGR 15LH AT CABIN PAX WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 AND CRJ-900 SRM 53-51-49-101-001-A02 AND WERE REPLACSDR VNAA20250714003Seat Track · corrodedCORROSION ON SEAT RAIL BTW FS 744.15 TO FS 977.00 AND STGR 15RH AT CABIN PAX. SEAT RAIL BTW FS 744.15 TO FS 977.00 AND STGR 15RH AT CABIN PAX. WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 AND SRM 53-51-49-101-001-A02 AND REPLACED PER CRJSDR VNAA20250714002Skin · corrodedCORROSION WAS FOUND AFTER ATG ANTENNA ON CONNECTORS SKIN SETTLEMENT AREA BTW STA: 1007. 50 STG 25R TO 26R. CORROSION WAS FOUND AFTER ATG ANTENNA ON CONNECTORS SKIN SETTLEMENT AREA BTW STA: 1007. 50 STG 25R TO 26R WAS REPAIRED PER EA 53-20-25-0854 REV. A.SDR VNAA20250714001Doubler · corrodedCORROSION ON PRODUCTION DOUBLER OF ANTENNA AND ATTACH ANLGES BTW FS1000-FS1015 AND STRINGERS 25RH-26RH AT AFT CARGO COMPARTMENT. PRODUCTION DOUBLER OF ANTENNA AND ATTACH ANLGES BTW FS1000-FS1015 AND STRINGERS 25RH-26RH AT AFT CARGO COMPARTMENT WERE REPLACED PSDR VNAA20250714014Web · crackedCRACK AT UPPER WEB OF ADG COMPARTMENT, BELOW OF SETTLEMENT AREA OF ADG PUMP. AREA AROUND ADG PUMP WAS REPAIRED PER CRJ-900 SRM 53-11-43-201-001-A01SDR VNAA20250714015Retainer · wornWEAR IN SEAL RETAINER NEAR 7-8 HRS AT LH AFT CORE COWL. SEAL RETAINER NEAR 7-8 HRS AT LH AFT CORE COWL WAS REPAIRED PER REO 690-54-13-239 REV. - ASDR VNAA20250714013Drip Tray · corrodedCORROSION ON FLOOR PANEL SUPPORT ANGLE BTW LBL 9.00 / RBL 9.00 AT FS 280. CORROSION ON FLOOR PANEL SUPPORT ANGLE BTW LBL 9.00 / RBL 9.00 AT FS 280.00 WAS REMOVED PER CRJ/900 SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN LIMITS PER CRJ-900 SRM 53-21-43-101-001SDR VNAA20250714011Plate · corrodedCORROSION ON UPPER/LOWER FACE OF PLATE LBL 3.4 BTW FS 645.00 AND FS 661.00 AT FWD CARGO COMPARTMENT. CORROSION ON UPPER/LOWER FACE OF PLATE LBL 3.4 BTW FS 645.00 AND FS 661.00 AT FWD CARGO COMPARTMENT WAS EVALUATED OUT LIMITS PER CRJ 900 SRM 53-32-58-101-001-SDR VNAA20250714020Plate · crackedCORROSION ON PROTECTOR PLATE ON LOWER SILL AT GALLEY SERVICE DOOR SURROUND STRUCTURE. PROTECTOR PLATE ON LOWER SILL AT GALLET SERVICE DOOR SURROUND STRUCTURE WAS EVALUATED OUT OF LIMITS PER CRJ-900 - SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ900 SRM 51-42SDR VNAA20250715003Skin · dentedDENT ON EXTERNAL SKIN RH SIDE BTW FS409.00 TO FS421.00 AND STGR 8RH TO 9RH AT FORWARD FUSELAGE. DENT ON EXTERNAL SKIN RH SIDE BTW FS409.00 TO FS421.00 AND STGR 8RH TO 9RH AT FORWARD FUSELAGE WAS REPAIRED PER REO 690-53-21-1980 REV.- -.SDR VNAA20250715002Skin · wornWEAR ON AREA OF SETTLEMENT OF FAIRINGS (583AB, 586AB, 592AB, 595AB, 597AB) AT LH WING LOWER SKIN. WEAR ON AREA OF SETTLEMENT OF FAIRINGS (583AB, 586AB, 592AB, 595AB, 597AB) AT LH WING LOWER SKIN. WAS BLENDED OUT PER CRJ-900 SRM 51-12-00-001-001-A01 AND SETTLESDR VNAA20250715001Skin · wornWEAR 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 BLENDED OUT PER CRJ-900 SRM 51-12-00-001-001-A01 AND AREA OFSDR VNAA20250714018Skin · damagedFUSELAGE SKIN LIGHTNING STRIKE DAMAGE AT FASTENER LOCATION. REPAIRED PER REO 670-53-00-045 REV-K , SECTION 2SDR VNAA20250714019Skin · damagedFUSELAGE SKIN LIGHTNING STRIKE DAMAGE REPAIR AROUND FASTENER COUNTERSINK. FUSELAGE SKIN LIGHTNING STRIKE DAMAGE REPAIR AROUND FASTENER COUNTERSINK WERE REPAIRED PER REO 670-53-00-045 REV-K , SECTION 3SDR VNAA20250715012Hinge 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 VNAA20250715011Seat Track · damagedMISSING, LOOSE, OR DAMAGED ALIGNMENT RIVETS AT CAPT/FO'S SEAT TRACKS PILOT/CO-PILOT SEAT TRACK WEAR STRIP. PILOT SEAT TRACK OB WAS REPAIRED PER REO 670-53-11-210 REV.- D AND SEAT TRACKS CO-PILOT IB AND OB AND PILOT SEAT TRACK IB MUST BE ATTENDED UNDER NRCS 00SDR VNAA20250715010Skin · damaged3895FH PERM REPAIR - REQUEST FOR EXTENSION TO NEXT C CHECK OF EA 23-C9-53-1114 REV A WITHIN 3895 FLIGHT HOURS AFTER SECTION I OF REV.A, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART.// ENGINEERING COMMESDR VNAA20250715009Seat Track · damagedMISSING, LOOSE, OR DAMAGED ALIGNMENT RIVETS AT CAPT/FO'S SEAT TRACKS PILOT/CO-PILOT SEAT TRACK WEAR STRIP. CO-PILOT SEAT TRACK IB WAS REPAIRED PER REO 670-53-11-210 REV.- D AND SEAT TRACKS CO-PILOT OB, CAPTAIN IB AND OB MUST BE ATTENDED UNDER NRCS 00013/NRC 0SDR VNAA20250714012Floorbeam · corrodedCORROSION ON FLOOR PANEL SUPPORT ANGLE BTW LBL 9.00 / RBL 9.00 AT FS 280. CORROSION ON FLOOR PANEL SUPPORT ANGLE BTW LBL 9.00 / RBL 9.00 AT FS 280.00 WAS REMOVED PER CRJ/900 SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN LIMITS PER CRJ-900 SRM 53-21-43-101-001SDR VNAA20250714017Skin · damagedTEMPORARY REPAIR FOR LIGHTNING STRIKE DAMAGE TO FUSELAGE SKINS WITHIN 1942 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. PERM REPAIR - FUSELAGE SKIN LIGHTNING STRIKE DAMSDR VNAA20250714016Seat Track · damagedMISSING, LOOSE, OR DAMAGED ALIGNMENT RIVETS AT CAPT/FO'S SEAT TRACKS PILOT/CO-PILOT SEAT TRACK WEAR STRIP. SAME PILOT SEAT TRACK IB WAS REPAIRED PER REO 670-53-11-210 REV.- D AND SEAT TRACKS CO-PILOT IB AND OB AND PILOT SEAT TRACK OB MUST BE ATTENDED UNDER NRSDR VNAA20250715033Skin · nickedNICK ON FUSELAGE SKIN BTW FS645.00-FS661.00 AND STGR 17LH-STGR 18LH AT FWD FUSELAGE. NICK ON FUSELAGE SKIN BTW FS645.00-FS661.00 AND STGR 17LH-STGR 18LH AT FWD FUSELAGE WAS REPAIRED PER REO 690-53-31-1024 REV.--.SDR VNAA20250715032Skin · dentedPROTUBERANCE DENT ON FUSELAGE SKIN BTW FS295.00 / FS310.00 AND STGR 26RH / STGR 27 AT FWD FUSELAGE. E ACTION: PROTUBERANCE DENT ON FUSELAGE SKIN BTW FS295.00 / FS310.00 AND STGR 26RH / STGR 27 AT FWD FUSELAGE WAS REPAIRED PER REO 690-53-21-1976 REV.- -SDR VNAA20250715031Skin · wornDURING INSPECTION OF THE RC TRFKE001VY3R WEAR ON SETTLEMENT AREA WAS DETECTED OF FAIRINGS (583AB,586AB,592AB,595AB,597AB) AT LH WING LOWER SKIN. RRECTIVE ACTION: WEAR ON SETTLEMENT AREA OF FAIRINGS (583AB,586AB,592AB,595AB,597AB) AT LH WING LOWER SKIN WERE BLESDR VNAA20250715030Skin · nickedSEVERAL NICKS ON EXTERNAL SKIN BTW FS 1015.00/FS 1051.30 AND STGR 27/STGR 24R AT REAR FUSELAGE. NICKS ON EXTERNAL SKIN BTW FS 1015.00/FS 1051.30 AND STGR 27/STGR 24R AT REAR FUSELAGE WAS BLEND OUT CRJ900 SRM 51-12-00-001-001-A01 AND FOUND SKIN BTW FS 1015/FS SDR VNAA20250715029Skin · wornDURING INSPECTION OF THE RC TRFKE001P4A1 WEAR ON SETTLEMENT AREA WAS DETECTED OF FAIRINGS (683AB,686AB,692AB,695AB,697AB) AT RH WING LOWER SKIN RECTIVE ACTION: WEAR ON SETTLEMENT AREA WAS DETECTED OF FAIRINGS (683AB,686AB,692AB,695AB,697AB) AT RH WING LOWER SKSDR VNAA20250715028Stiffener · damaged3200FH PERM REPAIR - TEMPORARY DISPOSITION FOR MULTIPLE DAMAGE IN RH NLG WHEEL WELL & AVIONICS BAY HARNESS WITHIN 3200FH, PERFORM A PERMANENT REPAIR OR REPLACE PART(S) IAW APPROVED PROCEDURES.// ENGINEERING COMMENTS: SUBMIT A NEW RFTS & DAMAGE REPORT. ECTIVE SDR VNAA20250715021Fitting · corrodedCORROSION ON HOUSING LUGS R5, R6 AT AILERON RH. HOUSING LUGS R5, R6 AT AILERON RH WERE REPAIRED PER REO 670-57-61-237 REV - -
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