N633NN
Service difficulty reports · 31
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 = 'N633NN' 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 = 'N633NN' 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 VNAA2026090424301Acm · leakingR BLEED DUCT WARNING MSG IN FLIGHT C/A C/W REMOVAL AND REINSTALLATION OF RH ACM IAW CRJ 900 AMM 21-51-08-000/400-801SDR VNAA2026090123901Duct · leakingL BLEED DUCT WARNING MSG IN FLIGHT RUN QRH, REMOVED AND REPLACED THE BLEED-AIR CROSSOVER DUCT IAW CRJ 900 AMM 36-19-09-000/400-801-A04. PERFORMED LEAK TEST OF THE BLEED-AIR DISTRIBUTION SYSTEM IAW CRJ 900 AMM 36-10-00-790-801. OPS CHECK GOOD AT THIS TIME.SDR VNAA2026061618901Selector Valve · unserviceablePROX SYSTEM CAUTION. QRH PROCEDURE COMPLETED. REMOVED AND REPLACED VALVE ASSY MLG SELECTOR IAW AMM 32-32-10-000-400-801-A01. OPS CHECK OF THE LANDING GEAR EXTENSION/RETRACTION SYSTEM GOOD AT THIS TIME. THIS CLEARS PROX SYSTEM CAUTION MESSAGE.SDR VNAA2026042016501Wire Harness · damagedSTEERING INOP CAUTION MSG AFTER TAKEOFF. AFTER GEAR SELECTED UP. REMOVED AND REPLACED STEERING WHEEL WIRING HARNESS IAW AMM 32-21-01-000/400-803-A01. PERFORMED BITE TEST OF THE STEERING MANIFOLD IAW AMM 32-50-00-740-801-A01 AND OPS TEST IAW AMM 32-51-00-710-SDR VNAA202508200026Door · abnormalPREVIOUS REPAIR WHITOUT TRACKING FOR PSA ON LOWER FAN COWL DOOR AT LH ENGINE BTWN 5 AND 6 O´CLOCK POSITION. PREVIOUS REPAIR WHITOUT TRACKING FOR PSA ON LOWER FAN COWL DOOR AT LH ENGINE BTWN 5 AND 6 O´CLOCK POSITION WAS REMOVED AND WAS REPAIRED PER REO 690-54SDR VNAA20250820005Door · dentedDENTS ON LOWER FAN COWL DOOR BTWN 4 TO 6´OCLOCK POSITION (5 EAS) AT LH ENGINE. DENTS ON LOWER FAN COWL DOOR BTWN 4 TO 6´OCLOCK POSITION (5 EAS) AT LH ENGINE WERE REPAIRED PER REO 690-54-14-774. REV-.SDR VNAA202508200024Fitting · crackedDISCREPANCY: CORROSION ON FLOOR FITTING PN: A414251-1 1EA AND PN: A414252-3 1EA AT FWD LAV. FLOOR FITTING PN: A414252-3 (1 EA ) AND FLOOR FITTING PN: A414251-1 (1 EA ) AT FWD LAV WERE REPLACED PER SAFRAN CMM 25-40-40SDR VNAA202508200023Seat Track · crackedBROKEN RH SIDE SEAT RAIL MOUNTING BTW FS847.00 TO FS881.00 AND STGR 15R. SEAT RAIL MOUNTING BTW FS847.00 TO FS881.00 AND STGR 15R WAS FABRICATED PER DWG SH690-37558 SNIEO S03 AND THEREFORE WAS REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01SDR VNAA202508200022Bulkhead Web · corrodedAFTER REMOVAL OF CAP ANGLE, CORROSION ON WEB OF BULKHEAD FS 280.00 LH SIDE . EVALUATED, DUE TO EXCESSIVE CORROSION ON WEB OF BULKHEAD FS 280.00 LH SIDE, IT IS OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND REPAIRED PER CRJ-900 SRM 53-11-10-201-004-A01.SDR VNAA202508200021Bulkhead Web · corrodedAFTER REMOVAL OF CAP ANGLE. CORROSION ON WEB OF BULKHEAD FS 280.00 RH SIDE . EVALUATED, DUE TO EXCESSIVE CORROSION ON WEB OF BULKHEAD FS 280.00 RH SIDE, IT IS OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND REPAIRED PER CRJ-900 SRM 53-11-10-201-004-ASDR VNAA202508200020Floorbeam · corrodedAFTER REMOTION OF FLOOR PANEL SUPPORT ANGLE. CORROSION ON CROSSBEAM RH AT FS280.00. CROSSBEAM RH AT FS280.00 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-10-001-001-A01 AND SRM 51-42-21-001-001-A01.SDR VNAA202508200019Floorbeam · corrodedAFTER REMOTION OF FLOOR PANEL SUPPORT ANGLE. CORROSION ON CROSSBEAM LH AT FS280. CROSSBEAM LH AT FS280.00 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-10-001-001-A01 AND SRM 51-42-21-001-001-A01.SDR VNAA20250820007Drag Angle · crackedDISCREPANCY: CRACK ON LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM. CRACK ON LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5%SDR VNAA20250820006Drag Angle · crackedDISCREPANCY: CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM. CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5SDR VNAA202508200018Lug · corrodedAFTER REMOTION OF BEARINGS AND BUSHINGS: CORROSION ON LUG R1, R3, R4, R5 AND R6 AT RH AILERON SURFACE. LUGS R1, R3, R4 AND R6 WERE CLEANED PER CRJ 900 SRM TASK 51--26-00-001-001-A01 CLEANING THEREFORE IT DOES NOT PRESENT DAMAGE R5 WAS REPAIRED PER REO 670-57SDR VNAA202508200017Seat Track · corrodedCORROSION IN SEAT RAIL LBL9 BTW FS364.00 TO FS682.00 (4 EAS). SEAT RAIL LBL9 BTW FS364.00 TO FS682.00 (4 EAS) ARE OUT OF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01 AND SRM 53-31-49-101-001-A02 THEREFORE WERE REPLACED PER CRJ-900 AMM 53-00-49 (CONFIG A12).SDR VNAA202508200016Seat Track · corrodedCORROSION IN SEAT RAIL LBL27 BTW FS364.00 TO FS581.00 (3 EAS). SEAT RAIL LBL27 BTW FS364.00 TO FS581.00 (3 EAS) ARE OUT OF LIMITS PER SRM 53-21-49-101-001-A01 AND SRM 53-31-49-101-001-A02 THEREFORE WERE REPLACED PER CRJ-900 AMM 53-00-49-000-801-A12.SDR VNAA20250820014Seat Track · corrodedCORROSION ON LH SIDE SEAT RAIL BTW FS379.00 TO FS969.00 (11 EAS). LH SIDE SEAT RAIL BTW FS379.00 TO FS969.00 (11 EAS) ARE OUT OF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01, SRM 53-31-49-101-001-A02,SRM 53-41-49-101-001-A02 AND SRM 53-51-49-101-001-A02 THERSDR VNAA20250820003Rib · crackedCRACK ON RIB LEADING EDGE SS57.16 AT LH WING FRONT SPAR. THE LH WING FRONT SPAR, RIB LEADING EDGE SS57.16 WAS REPAIRED PER REO 690-57-41-240 REV -.SDR VNAA20250820002Drip Tray · corrodedCORROSION ON LH DRIP TRAY AT FS280.00 AT PASSENGER CABIN DUE TO EXCESIVE CORROSIÓN ON LH DRIP TRAY AT FS280.00 AT PASSENGER CABIN WAS FOUND OUT OF LIMITS PER CRJ-900 SRM 53-21-43-101-001-A03 THEREFORE WAS REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01 AND CRJ SDR VNAA20250820001Drip Tray · corrodedCORROSION ON LH DRIP TRAY AT FS280.00 AT PASSENGER CABIN. DUE TO EXCESIVE CORROSIÓN ON LH DRIP TRAY AT FS280.00 AT PASSENGER CABIN WAS FOUND OUT OF LIMITS PER CRJ-900 SRM 53-21-43-101-001-A03 THEREFORE WAS REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01 AND CRSDR VNAA20250820015Seat Track · corrodedCORROSION ON RBL9 SEAT RAIL BTW FS349.00 TO FS682.00 (6 EAS). DUE TO EXCESSIVE DAMAGE ON SEAT RAIL ON RBL9 SEAT RAIL BTW FS349.00 TO FS682.00 (6 EAS) WERE FOUND OUT OF LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02 THEREFORE WERE REPLACED PER CRJ-900 AMM 53-0SDR VNAA20250820013Rib · crackedCRACK ON INBD MACHINED RIB OF WS 163.00 TRAILING EDGE AT LH WING. CRACK ON INBD MACHINED RIB OF WS 163.00 TRAILING EDGE AT LH WING WAS REPAIRED PER REO 690-57-51-452 REV -.SDR VNAA20250820012Door Seal · corrodedCORROSION ON ANGLE LOWER SEAL AT GALLEY SERVICE DOOR SURROUND STRUCTURE. DUE TO EXCESIVE CORROSIÓN ON ANGLE LOWER SEAL AT GALLEY SERVICE DOOR SURROUND STRUCTURE IS OUT OFF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 THEREFORE WAS REPLACED PER CRJ900 SRM 51-42-SDR VNAA20250820010Rib · crackedCRACK ON OUTB MACHINED RIB OF WS 163.00 TRAILING EDGE AT RH WING. CRACK ON OUTB MACHINED RIB OF WS 163.00 TRAILING EDGE AT RH WING WAS REPAIRED PER REO 690-57-51-450 REV - -SDR VNAA20250820009Rib · crackedCRACK ON OUTB MACHINED RIB OF WS 163.00 TRAILING EDGE AT LH WING. CRACK ON OUTB MACHINED RIB OF WS 163.00 TRAILING EDGE AT LH WING WAS REPAIRED PER REO 690-57-51-451 REV. -.SDR VNAA202508200025Skin · dentedDISCREPANCY: DENT ON INLET COWL AT 6 O´CLOCK POSITION AT LH ENGINE PREVIOUSLY MARKED AND WHITOUT TRACKING FOR PSA. DENT ON INLET COWL AT 6 O´CLOCK POSITION AT LH ENGINE PREVIOUSLY MARKED AND WHITOUT TRACKING FOR PSA WAS REPAIRED PER REO 690-54-11-560 REV- ANSDR VNAA20250820004Skin · dentedDENT ON INLET COWL SKIN AT 6 O'CLOCK POSITION LH ENGINE. DENT ON INLET COWL SKIN AT 6 O'CLOCK POSITION LH ENGINE WAS REPAIRED PER REO 690-54-11-560 REV- - AND PER 670-54-11-1108 REV. NC.SDR VNAA20250820008Shield · chafedLH ENG FIRE SHIELD WITHIN 2140.41 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. ENGINEERING COMMENTS: LH ENG FIRE SHIELD REPAIR AS PER SRM TASK 54-23-00-201-005-A01. IF NSDR VNAA2024042511103Pcu · faultedOB SPOILERONS / OB FLIGHT SPOILERS CAUTION MESSAGE ON DECENT AFTER SELECTION TO DEPLOY SPOILERS / INTERROGATED MDC AND FOUND B1 CODE 007920, TROUBLESHOT IAW CRJ900 FIM 27-64-01-810-817-A01-PSA AND DETERMINED PCU MPE34 TO BE AT FAULT. REMOVED AND REPLACED THE RSDR VNAA2024022511101Acm · seizedSHORTLY AFTER TO. FA REPORTED SMOKE IN CABIN. AFTER LANDING R PACK AUTO FAIL CAUTION MSG. EVACUATED ON TAXIWAY / TROUBLESHOT IAW CRJ900 FIM 21-21-00-810-806 AND FIM 21-22-00-810-806. FOUND RH AIR CONDITIONING PACK TO BE SEIZED, NO SIGNS OF SMOKE WHEN INOP REMO
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