N604NN
Service difficulty reports · 35
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 = 'N604NN' 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 = 'N604NN' 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 VNAA20260304003Web · crackedCRACK ON WEB BTW FS195 AND WL79.50 (RH SIDE) ON INTERNAL STRUCTURE AT FWD EQUIPEMENT COMPARTMENT. THE WEB WAS REPAIRED IAW SRM 53-11-43-201-001-A01SDR VNAA20260304025Seat Track · corrodedFOUR CORRODED SEAT TRACKS, BS 364 - 581, LBL 9 AND TWO FROM BS 376 - 677, LBL 26 IN THE PASSENGER CABIN. THE SEAT TRACKS WERE EVALUATED OUT OF LIMITS IAW SRM 53-21-49-101-001-A01, SRM 53-31-49-101-001-A02, AND SRM 53-41-49-101-001-A02 AND WERE REPLACED IAW ASDR VNAA20260304023Fitting · corrodedCORROSION FLOOR FITTING ACCESS 107. REPLACED IAW CMM 25-33-21.SDR VNAA20260304022Lug · corrodedCORROSION ON BORE LUG # R1, R5 & R6 OF CENTER HINGE FITTING AT RH AILERON. BORE LUG NR R1, & R6 OF CENTER HINGE FITTING AT RT AILERON WERE CLEANEDIAW SRM 51-26-00-001-001-A01, AND BORE LUG NR R5 WAS REPAIRED IAW REO 670-57-61-237, REV--.SDR VNAA20260304021Pressure Deck · corrodedAFTER REMOVAL OF BLIND BOLT ON THE PRESSURE SILL DECK STEP 8, CORROSION FOUND AT SEVERAL BOLT HOLES. REPAIRED IAW REO 690-53-41-578. REV A.SDR VNAA20260304027Hinge Fitting · excess playFREE PLAY ON SELF-ALIGN SELF-LUBE BEARING PLAIN ON HINGE FITTING NR 3 ON THE VERTICAL STAB REAR SPAR MIDDLE SECTION. HINGE FITTING NR 3 AT VERTICAL STAB WAS REPLACED IAW SRM 51-42-21-001-001-A01, AND RIL 2103, REV B.SDR VNAA20260304020Door · missingFORWARD LAVATORY SERVICE DOOR MISSING. FORWARD LAV SERVICE DOOR INSTALLED IAW SRM 51-42-06-001-001-A01, AND AMM 52-45-17-400-801,CONFIG A02.SDR VNAA20260304011Hinge Fitting · corrodedCORROSION ON HINGE FITTING AND HINGE ARM ACCESS 196ER. CORROSION ON HINGE ARM WAS REMOVED IAW SRM 51-21-06-001-A01 HINGE FITTING WAS REPLACEDSDR VNAA20260304010Floor Support · crackedCRACK ON FLOOR BEAM RBL 12 FS BTW FS 221.73 TO FS 229.0 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL 79.50. CRACK ON FLOOR BEAM RBL 12 FS BTW FS 221.73 TO FS 229.0 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOORSDR VNAA20260304026Skin · dentedSEVERAL DENTS ON THE SKIN OF ALONG THE SETTLEMENT AREA VENTRAL FIN LT & RT. THE SKIN WAS REPAIRED IAW REO 670-51-00-085, REV A, REO 690-53-71-104, REV-, REO 690-53-61-1737, REV -, AND REO 690-53-61-1738 REV -.SDR VNAA20260304024Seat Track · corrodedSEAT TRACK CORRODED BS 597 TO 677. REPLACED IAW AMM 53-00-49.SDR VNAA20260304018Seat Track · corrodedCORROSION FOUND ON THE SEAT TRACK, BS 349 - 477, RBL9. THE SEAT TRACK EVALUATED OUT OF LIMITS IAW SRM 53-21-49-101-A01, AND REPLACED IAW AMM 53-00-49-400-801, CONFIG A12.SDR VNAA20260304017Floorbeam · corrodedAFTER REMOVING FLOOR PANEL, CORROSION WAS FOUND ON THE FLOORBEAM BS 280. THE RT FLOORBEAM WAS REPAIRED IAW REO 690-53-11-2134, REV-.SDR VNAA20260304016Floorbeam · corrodedAFTER TO REMOVED FLOOR PANEL THE FLOORBEAM, BS280 CORRODED. THE FLOORBEAM WAS REPAIRED IAW REO 690-53-11-2133, REV -.SDR VNAA20260304009Drag 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) REPAIRED PER CRJ900 SRM 55-31-00-201-001-A01SDR VNAA20260304008Seat Track · corrodedCORROSION ON SEAT RAIL FROM FS349.00 TO FS477.00 AT RBL9 (2EAS). SEAT RAILS FROM FS349.00 TO FS477.00 AT RBL9 (2EAS) WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-A01 AND REPLACED PER CRJ 900 AMM 53-00-49-400-801 (CONFIG A12)SDR VNAA20260304007Floorbeam · corrodedAFTER TO REMOVED FLOOR PANEL SUPPORT ANGLE CORROSION WAS FOUND ON THE RH CROSSBEAM FS280.00 AT COCKPIT CABIN FLOOR. RH CROSSBEAM FS280.00 AT COCKPIT CABIN FLOOR WAS REPAIRED PER REO 690-53-11-2134 REV--.SDR VNAA20260304006Floorbeam · corrodedAFTER TO REMOVED FLOOR PANEL SUPPORT ANGLE CORROSION WAS FOUND ON THE LH CROSSBEAM FS280.00 AT COCKPIT CABIN FLOOR. LH CROSSBEAM FS280.00 AT COCKPIT CABIN FLOOR WAS REPAIRED PER REO 690-53-11-2133 REV - -SDR VNAA20260304015Seat Track · corrodedCORROSION ON SIDE SEAT TRACK LT FOUR AREAS, RT 4 AREAS. BTW BS 379 AND 669, S15L ANDS15R. REPLACED IAW AMM 53-00-49-400-801-A12.SDR VNAA20260304014Seat Track · corrodedCORROSION ON SIDE SEAT TRACK LT, 6 AREAS, RT 6 AREAS, BTW BS 669.40 AND 977 S15L & S15R. THE SEAT TRACKS WERE CLEANED IAW SRM 51-26-00-001-001-A01, AND DUE TO EXCESSIVE DAMAGE, REPLACED IAW SRM 53-41-49-101-001-A02, SRM 53-51-49-101-001-A02, & AMM 53-00-49-SDR VNAA20260304005Seat Track · corrodedCORROSION ON SIDE SEAT RAIL LH (4EAS) RH (4EAS) BTW FS379.00 AND FS669 AT STGR15L AND AT STGR15R ON CABIN PAX. SIDE SEAT RAIL LH (4EAS) RH (4EAS) BTW FS379.00 AND FS669 AT STGR15L AND AT STGR15R ON CABIN PAX WERE REPLACED PER AMM 53-00-49-400-801-A12SDR VNAA20260304004Seat Track · corrodedCORROSION ON SIDE SEAT RAIL LH( 6EAS) RH (6EAS) BTW FS669.40 AND FS977 AT STGR15L AND AT STGR15R ON CABIN PAX. SIDE SEAT RAIL LH (1 EA) AND RH (1 EA) BTW FS847+6 TO FS847+20 AT STGR15L AND AT STGR15R ON CABIN PAX WERE CLEANED PER CRJ900 SRM 51-26-00-001-001-ASDR VNAA20260304013Web · crackedCRACKED WEB BTW BS 195, WL 79.50, RT SIDE, ON INTERNAL STRUCTURE AT FWD EQUIPEMENT COMPARTMENT. THE WEB WAS REPAIRED IAW SRM 53-11-43-201-001-A01.SDR VNAA20260304012Floorbeam · crackedCRACKED COCKPIT FLOORBEAM, RBL 12. REPAIRED IAW REO 690-53-11-2131, REV-.SDR VNAA20260304002Hinge Fitting · corrodedCORROSION ON HINGE FITTING AND HINGE ARM AT ACCESS PANEL 196ER WAS REMOVED PER SRM 51-21-06-001-A01 EVAL WITHIN LIMITS BUT REPLACEDSDR VNAA20260304001Drag Angle · crackedCRACK ON VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT LH DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) DRAG ANGLE WAS REPAIRED PER SRM 55-31-00-201-001-A01SDR VNAA2025120311101Window · arcedRH SIDE WINDOW ARC AROUND FL 210 ON DECENT. / REMOVED AND REPLACED THE RH SIDE WINDOW IAW CRJ AMM 56-12-01-400-801-A01-PSA. OPS CHECKS GOOD. LEAK CHECK GOOD. NO DEFECTS NOTED.SDR VNAA2024082711104Pump · unserviceableHYDRAULIC EDP1A CAUTION MSG. / R/R LEFT ENGINE EDP IAW CRJ 900 AMM 29-11-01-000/400-801-A01. R/R LH EDP CASE DRAIN FILTER AND EDP PRESSURE FILTER IAW CRJ 900 AMM 29-11-40-000/400-801 AND AMM 29-11-09-000/400-801. OPS CHECK AND LEAK CHECK GOOD, NO EDP1A CAUTIOSDR VNAA2023092711101Motor · faultedAFTER HOLDING FOR 20 MINUTES TO GET INTO DCA THE CREW RECEIVED 2 HYD CAUTION MESSAGES IN FLIGHT. REMOVED AND REPLACED HYD SYS #2 ACMP IAW CRJ 900 29-11-03-000/400-801-A01. LEAK CHECK & OPS CHECK GOOD AT THIS TIMESDR VNAA202308211112Unknown · unknownFO WINDSHIELD CRACKED DUE TO ARCING/ REMOVED AND REPLACED FO WINDSHIELD IAW CRJ 900 AMM 56-11-01-000/400-801-A01-PSA.SDR VNAA202308211111Windshield · unserviceableFO'S WINDSHIELD WAS ARCING ON DECENT WITH SWITCH SET LOW / DEFERRED R WINDSHIELD HEAT PER MEL 30-41-1 CAT C M/FC C/W BY COLLARING CBP2- G13, A10, A11 AND TESTING LH WINDOW HEAT SYSTEM. REMOVED AND REPLACED FO WINDSHIELD IAW CRJ 900 AMM 56-11-01-000/400-801-A01SDR VNAA202301298003Panel · crackedCRACK ON FWD SIDE PANEL BTW MIDDLE STEP AND TOP STEP OF PASSENGER DOOR STRUCTURE. FWD SIDE PANEL BTW MIDDLE STEP AND TOP STEP OF PASSENGER DOOR STRUCTURE WAS REPAIRED PER CRJ-900 SRM-52-11-04-201-004- A01.SDR VNAA202301298002Panel · crackedCRACK ON AFT SIDE PANEL BTW LOWER-MIDDLE STEP AND MIDDLE STEP OF PASSENGER DOOR STRUCTURE. INSPECTION WAS ACCOMPLISHED ON AFT SIDE PANEL BTW LOWER-MIDDLE STEP AND MIDDLE STEP OF PASSENGER DOOR STRUCTURE, NO CRACKS WERE FOUND PER CRJ700/900/1000 NDT MANUAL PARSDR VNAA202301298001Panel · crackedCRACK ON AFT SIDE PANEL BTW MIDDLE STEP AND TOP STEP OF PASSENGER DOOR STRUCTUR. SIDE PANEL BTW MIDDLE STEP AND TOP STEP OF PASSENGER DOOR STRUCTURE. WAS REPAIRED PER CRJ-900 SRM-52-11-04-201-004- A01SDR VNAA202102131111Relay · malfunctionedAT APPROXIMATELY 50 KNOTS ON RUNWAY 36, CREW RECEIVED A R REV UNSAFE CAUTION MESSAGE. CREW EXITED THE RUNWAY WITHOUT ISSUE AND RETURNED TO THE GATE. THE AIRCRAFT IS CURRENTLY IN WORK TO DEFER THE RH THRUST REVERSER.R/R K30 RELAY IN JB-5 IAW CRJ 900 AMM 24-03-
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