N607NN
Service difficulty reports · 38
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 = 'N607NN' 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 = 'N607NN' 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 VNAA2026071320009Retainer · corrodedSECONDARY NRC AFTER PRESSURE SEAL REMOVAL ON AFT CARGO DOOR, CORROSION FOUND SEVERAL PLACES ON BOTTOM FACE AFT CARGO COMPARTMENT. CORROSION ON RETAINERS SEAL (3 EAS) AT AFT DOOR C2. WERE REMOVED PER CRJ 900 SRM SRM 51-21-06-001-001-A01. AND FOUND OUT OF LIMITSDR VNAA2026071320008Hinge Fitting · corrodedCORROSION ON CENTER HINGUE FITTING L5 WAS FOUND. CENTER HINGE FITTING LUG BORE L5 AILERON LH WAS REPAIRED PER REO 670-57-61-237 REV --SDR VNAA2026071320007Hinge Fitting · corrodedCORROSION ON CENTER HINGUE FITTING R2 WAS FOUND. CENTER HINGE FITTING LUG BORE R2 AILERON RH WAS REPAIRED PER REO 670-57-61-237 REV --SDR VNAA2026071320006Fitting · corrodedCORROSION FLOOR FITTING IN FWD ON ENTRANCE (1EA). CORROSION FLOOR FITTING IN FWD ON ENTRANCE (1EA) WAS REPLACED PER CMM 25-33-06SDR VNAA2026071320004Fitting · corrodedCORROSION FLOOR FITTING IN AFT ACCESS 107 OUT SIDE (1EA) ON GALLEY 1. FLOOR FITTING IN AFT ACCESS 107 OUT SIDE (1EA) ON GALLEY 1 WAS REPLACED PER CMM 25-33-21.SDR VNAA2026071320003Fitting · corrodedCORROSION FLOOR FITTING IN AFT ACCESS 109 (1EA) ON GALLEY 1. FLOOR FITTING IN AFT ACCESS 109 (1EA) ON GALLEY 1 WAS REPLACED PER CMM 25-33-21.SDR VNAA2026071320002Fitting · corrodedCORROSION FLOOR FITTING IN FWD ACCESS 107 (1EA) ON GALLEY 1. FLOOR FITTING IN FWD ACCESS 107 (1EA) ON GALLEY 1 WAS REPLACED PER CMM 25-33-21SDR VNAA202607120020Hinge · wornEXCCESSIVE FREE PLAY (LATERAL AND LONGITUDINAL) OF BEARINGS FOUND ON BOTH 2 CENTRAL RUDDER HINGES OF VERTICAL STABILAZER REAR SPAR. HINGE 3 WAS REPAIRED PER RIL #1213 REV. A. AND HINGE 2 WAS REPLACED PER RIL #2103 REV. B.SDR VNAA202607120019Rib · crackedCRACK ON OUTB MACHINED RIB OF FLS 168.07 TRAILING EDGE AREA AT WING RH. RIB OF FLS 168.07 TRAILING EDGE AREA AT RH WING WAS REPAIRED PER REO 690-57-51-542 REV. - -SDR VNAA202607120018Floorbeam · crackedCRACK ON CENTER FLOOR BEAM RBL12.0 BTW 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL79.50). CENTER FLOOR BEAM RBL12.0 BTW 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR SSDR VNAA202607120017Frame · damagedFOLDED FRAME (FS1015.00) BTW STGR 17L TO 19L ON LOWER SURROUND STRUCTURE AT AFT BAGGAGE BAY DOOR. FOLDED FRAME (FS1015.00) BTW STGR 17L TO 19L ON LOWER SURROUND STRUCTURE AT AFT BAGGAGE BAY DOOR WAS REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01 AND SRM 51-42-SDR VNAA202607120016Seat Track · corrodedCORROSION ON FLOOR SEAT RAILS BTW FS=349 TO FS=477 AND RBL 9'' ALSO IN FS 379 AND LBL 9 AT CPAX. FLOOR SEAT RAILS BTW FS=349 TO FS=477 AND RBL 9'' ALSO IN FS 379 AND LBL 9 AT CPAX WERE REPLACED PER CRJ900 AMM 53-00-49-400-801 (CONFIG A12)SDR VNAA202607120015Seat Track · corrodedCORROSION ON SIDE SEAT RAIL STGR 16L, BS 501 TO BS 549 AND BS 645 TO BS 693 AT CPAX. SIDE SEAT TRACAK STR 16L, BS 501 TO BS 549 AND BS 645 TO BS 693 AT CPAX WERE REPLACE IAW AMM 53-00-49-400-801 (CONFIG A12).SDR VNAA202607120014Seat Track · corrodedCORROSION ON SIDE SEAT RAIL STGR 15 RH, FS 453 TO FS 501 AND FS 661+74 TO FS 693 AT CPAX. SIDE SEAT RAIL STGR 15 RH, BS 453 TO BS 501 AND BS 661+74 TO BS 693 AT CPAX WERE REPLACED IAW AMM 53-00-49-400-801 (CONFIG A12).SDR VNAA2026071320005Fitting · corrodedCORROSION FLOOR FITTING IN FRONT PAPER CONTAINER AND UNDER WASTE CONTAINER ON FWD LAV (1EA). FLOOR FITTING IN FRONT PAPER CONTAINER AND UNDER WASTE CONTAINER ON FWD LAV (1EA) WAS REPLACED PER SAFRAN CMM 25-40-19.SDR VNAA202607120013Seat Track · corrodedCORROSION ON SEAT TRACK BTW FS 693 TO FS 927 AND STGR 15LH AT CABIN PAX. SEAT TRACK REPLACED IAW AMM 53-00-49 (CONFIG A12)SDR VNAA202607120012Seat Track · corrodedCORROSION ON SEAT TRACK BTW FS 693 TO FS 927 AND STGR 15RH AT CABIN PAX. THE SEAT TRACK REPLACED IAW AMM 53-00-49-400-801(CONFIG A12).SDR VNAA202607120011Bulkhead · corrodedDURING INSPECTION OF THE JOB CARD TRFKE00CCHN1: CORROSION ON DOOR POST BULKHEAD AT RBL 12 & LBL 12 AT FS 280.00 AT RH/LH SIDE LOWER SECTION. CORROSION ON DOOR POST BULKHEAD AT RBL 12 & LBL 12 AT FS 280.00 AT RH/LH SIDE LOWER SECTION WAS REMOVED PER CRJ 900 SSDR VNAA202607120010Rib · crackedCRACKED MACHINED RIB SS 15.50 ON INBD FIXED LEADING EDGE AT RH WING. RIB SS 15.50 ON INBD FIXED LEADING EDGE AT RT WING REPAIR PER REO 690-57-41-613 REV - -SDR VNAA202607120009Web · crackedCRACK ON ELECTRICAL BAY FLOOR WEB LH SIDE FS193.00 ( BELOW ACCUMULATOR GAUGE INDICATOR) AT FWD EQUIPMENT COMPARTMENT. CRACK ON ELECTRICAL BAY FLOOR WEB LH SIDE FS193.00 ( BELOW ACCUMULATOR GAUGE INDICATOR) AT FWD EQUIPMENT COMPARTMENT WAS REPAIRED PER SRM 53-SDR VNAA202607120008Stand Off · crackedCRACK PAD SUPPORT (1EA) AT RH AFT CORE. PAD SUPPORT (1EA) AT RH AFT CORE WAS REPLACED PER SRM 51-42-06-001-001-A01.SDR VNAA202607120007Skin · damagedWEAR ON EXTERNAL SKIN AT FS 910 AND FS 919, STRINGER 27 ON CENTER FUSELAGE. WEAR ON EXTERNAL SKIN AT FS 919 STRINGER 27 ON CENTER FUSELAGE WAS BLEND OUT PER CRJ-900 SRM 51-12-00-001-001-A01 AND FOUND WITHIN LIMITS PER CRJ900 SRM 53-51-01-101-003-A05 AND WEAR SDR VNAA202607120006Box Beam · damaged800FH PERM REPAIR - TEMPORARY REPAIR FOR DAMAGED HOLE TO LH NLG BOX SIDE BEAM BETWEEN FS228.42-FS235.00 THIS TEMPORARY REPAIR IS ACCEPTABLE FOR 800 FLIGHT HOURS FROM THE TIME OF INCORPORATION OF THIS REO. // ENGINEERING COMMENTS: FWD FITTING STR 26A LH (PN CC6SDR VNAA202607120005Fairing · dented3801.90FH PERM REPAIR - LH FLAP STUB FAIRING (171DL) WITHIN 3801.90 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. LH FLAP STUB FAIRING (171DL) WAS REPAIRED PER EA NO: 53SDR VNAA202607120004Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FW/AFT DRAG ANGLE BTW 55.625% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM. (ET) HFEC INSPECTION WAS PERFORMED 01 CRACK WAS FOUND ON AFT DRAG ANGLE AND FWD DRAG ANGLE NO CRACKS WERE FOUND. IAW NDT SDR VNAA202607120003Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM. REPAIRED PER SRM 55-31-00-201-001-A01SDR VNAA202607120002Angle · crackedRACK AFT ANGLE ON PASSENGER DOOR. CRACK AFT ANGLE ON PASSENGER DOOR WAS REPAIR PER SRM 52-11-04-201-002-A01.SDR VNAA202607120001Handle · wornWEAR ON HANDLE FRAME AT AFT BAGGAGE BAY DOOR. DOOR WAS REPAIRED PER REO 670-52-31-031 REV. - BV. - BSDR VNAA2026071320001Access Panel · crackedCRACK ON ACCESS PANEL 172CR AT OVER WING FAIRING. ACCESS PANEL 172CR AT OVER WING FAIRING WAS REPAIRED PER REO 679-53-82-430 REV - -, AND STIFFENER WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01.SDR VNAA2024120311102Steering Sys · abnormalSTEERING INOP CAUTION ON TAKEOFF CLIMB / PERFORMED MIPM RESET. MSG EXTINGUISHED. PROBLEM DID NOT REOCCUR.SDR VNAA2024120311101Steering Sys · abnormalSTEERING INOP CAUTION MSG AFTER TAKEOFF / C/W MIPM RESET FOR STEERING INOP, FAULT DID NOT REOCCUR.SDR VNAA202308221112Manifold · unserviceableSTEERING INOP MESSAGE AFTER TAKEOFF. QRH PROCEDURE DID NOT CLEAR MESSAGE. / TROUBLESHOT STEERING INOP THROUGH B1-007464 FOUND IN MDC IAW CRJ 900 FIM 32-51-50-810-801. REMOVED AND REPLACED STEERING MANIFOLD IAW CRJ 900 AMM 32-51-50-000/400-801. BITE TEST AND OPSDR VNAA202308221111Selector Valve · unserviceableSTEERING INOP IN FLIGHT, AFTER GEAR UP / R/R LANDING GEAR SELECTOR VALVE IAW CRJ 900 AMM 32-32-15-000/400-801. T/S IAW CRJ 900 FIM 32-51-50-810-801. B1-007464. OPS/LEAK CHECK GOOD.SDR VNAA202303110003Plate · crackedPERM REPAIR NEEDS PERFORMED FOR CRACKS IN ZONE 5 ON AFT SIDE OF PAX DOOR : PERFORMED PERMANENT REPAIR
TO PAX DOOR ZONE 5 IAW CRJ-900 SRM 52-11-04-201-006-A01SDR VNAA202303110002Drag Angle · crackedPERM REPAIR NEEDS PERFORMED FOR CRACKS IN ZONE 3 ON AFTSIDE OF PAX DOOR : REPAIRED DAMAGED PAX DOOR AFT DRAG ANGLE IAW CRJ 900 SRM 52-11-04-201-002-A01 REPAIR TYPE 1 STEPS 5.B THROUGH CLOSE-OUT. REFERENCE THE TASK SECTION OF THIS CARD FOR WORK PERFORMEDSDR VNAA202303110001Web · crackedPERM REPAIR OF CRACK DAMAGE TO PAX DOOR NEEDS PERFORMED: REPAIRED PAX DOOR FWD WEB IAW CRJ-900 SRM 52-11-04-201-004-A01.SDR VNAA202012181111Trim System · abnormalRTO-THE CREW REJECTED THE TAKE OFF FROM RUNWAY 36R AT IDLE PWER AND SPEED NOT ABOVE TAXI SPEED FOR AN AILERON TRIM UNCOMMANDED FULL LEFT WING DOWN AND RUDDER TRIM UNCOMMANDED FULL LEFT RUDDER. CBP 2 F3 POPPED. THE CREW IS CURRENTLY RETURNING TO THE GATE FOR SDR VNAA2019090911102Transmitter · out of rigIN LEVEL FLIGHT CREW RECEIVED ELEVATOR SPLIT CAUTION MESSAGE. CREW RAN THRU THE QRH, DECLARED AN EMERGENCY AND LANDED GSP WITHOUT INCIDENT. RE-RIGGED/INDEXED LEFT ELEVATOR POSITION TRANSMITTER. SYSTEM OPS CHECKED GOOD.
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