N649NN
Service difficulty reports · 42
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 = 'N649NN' 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 = 'N649NN' 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 VNAA2026092325301Door · gougedGOUGE DAMAGE AFT OF LOW PRESSURE DOOR. PERFORMED ALL WORK USING STEPS AND DRAWINGS LISTED IN REO 690-53-61-1813SDR VNAA202606120062Door · crackedCRACK IN DOOR LANDING WAS FOUND. DOOR LANDING WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01 AND SRM 51-42-10-001-001-A01.SDR VNAA202606120061Stiffener · corrodedCORROSION ON ANGLE BTW STGR 25LH/25RH AT BTW 55.265% AND 67.50 % SPAR DATUM. ANGLE (STIFFENER) BTW STGR 25LH/25RH AT BTW 55.265% AND 67.50 % SPAR DATUM WAS REPLACED PER SRM 51-42-06-001-001-A01.SDR VNAA202606120060Axle · corrodedLEFT RUSTED AND MISSING TOPCOAT ON ROOT RADIUS INBD AND OTBD SECTIONS PISTON, PISTON AXLE LT MLG. ROOT RADIUS INBD AND OTBD SECTIONS PISTON, PISTON AXLE LT MLG. WERE REPAIRED AND ATTENDED PER REO 670-32-11-361 REV. A.SDR VNAA202606120059Axle · corrodedEXPOSED MATERIAL ON ROOT SETTLEMENT AREA AT RH MLG PISTON AXLE. EXPOSED MATERIAL ON ROOT SETTLEMENT AREA AT RH MLG PISTON AXLE WAS ATTENDED PER REO 670-32-11-361 REV A.SDR VNAA202606120058Lug · corrodedSCRATCH FOUND ON LT AILERON HINGE LUG BORE L5 INNER AREA 6. SCRATCH ON LUG BORE L5 AT CENTER FITTING ON LT AILERON WAS REPAIRED PERREO 670-57-61-237 REV-.SDR VNAA202606120057Lug · corrodedDAMAGE FOUND LH AILERON CENTRAL HINGES LUG BORES L1, L2 AND L6. LUGS BORE L1, L2 & L6 AT CENTER FITTING AT LH AILERON WERE REPAIRED PERREO 670-57-61-237 REV--.SDR VNAA202606120056Skin Panel · damagedBURN SPOT AT FASTENER LOCATION AFTFUSELAGE SKIN FSFS210.92 - STR23L. BURN SPOT AT FASTENER LOCATION AFTFUSELAGE SKIN FSFS210.92 - STR23L WAS REPAIRED PER CRJ900 SRM 53-00-00-201-003-A03.SDR VNAA202606120055Skin · burnedBURN SPOT AT FASTENER LOCATION AFTFUSELAGE SKIN FS202.75-FS210.92 - STR25L. BURN SPOT AT FASTENER LOCATION AFTFUSELAGE SKIN FS202.75-FS210.92 - STR25L WAS REPAIRED PER CRJ900 SRM 53-00-00-201-003-A03.SDR VNAA202606120054Intercostal · crackedCRACK ON UPPER INTERCOSTAL RH SIDE BTW FS173 TO FS193 AND WL79.50 ON INTERNAL STRUCTURE AT NOSE ADG COMPARTMENT. INTERCOSTAL RT SIDE BTW FS173 TO FS193 AND WL79.50 ON INTERNAL STRUCTURE AT NOSE ADG COMPARTMENT WAS REPLACED PER SRM 51-42-10-001-001-A01 SRM 51-SDR VNAA202606120053Seat Track · corrodedCORROSION ON FLOOR SEAT RAILS BTW FS 485 TO FS 677 RH AND LH SIDE (6 E/AS) AT C PAX. CORROSION ON FLOOR SEAT RAILS BTW FS 485 TO FS 677 RH AND LH SIDE (6 E/AS) AT C PAX WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02 AND REPLACED PER CRJ-900 SDR VNAA202606120052Hinge · wornFREEPLAY ON BEARINGS OF RUDDER HINGE ASSY NBR 2 AND 3 IN TRAILING EDGE AREA AT VERTICAL STABILIZER. RUDDER HINGE ASSY NBR 2 AND 3 IN TRAILING EDGE AREA AT VERTICAL STABILIZER WERE REPLACED PER RIL #2103 REV.B AND RIL #1213 REV.ASDR VNAA202606120051Support Fitting · corrodedCORROSION ON GALEY FITTING SUPPORT IN FS 295 RBL 6 AT CPAX. CORROSION ON GALEY FITTING SUPPORT IN FS 295 RBL 6 AT CPAX WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01.SDR VNAA202606120050Floorbeam · crackedCRACKED CENTER FLOOR BEAM FS 280.00 LBL 12.0 BELOW WL72.50 AT COCKPIT. CENTER FLOOR BEAM FS 280, LBL 12.0 BELOW WL72.50 AT COCKPIT WAS REPAIRED PER REO 690-53-11-2172 REV--.SDR VNAA202606120049Bracket · corrodedCORROSION ON BRACKET MACHINED (2EA) BTW STGR 27 AND FS 629 TO FS 661+16 AT FWD BAGGABE BAY. BRACKET MACHINED (2EA) BTW STGR 27 AND FS 629 TO FS 661+16 AT FWD BAGGABE BAY WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 AND SRM 51-42-22-001-001-A01.SDR VNAA202606120048Seat Track · corrodedCORROSION ON SIDE SEAT RAILS BTW FS 379 TO FS 669.4 LH SIDE (5 E/AS) AT C PAX. CORROSION ON SIDE SEAT RAILS BTW FS 379 TO FS 669.4 LH SIDE (5 E/AS) AT C PAX WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01, SRM 53-31-49-101-001-A02 AND REPLACESDR VNAA202606120047Seat Track · corrodedCORROSION ON SIDE SEAT RAILS BTW FS 379 TO FS 669.4 RH SIDE (5 E/AS) AT C PAX. CORROSION ON SIDE SEAT RAILS BTW FS 379 TO FS 669.4 RH SIDE (5 E/AS) AT C PAX WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01, SRM 53-31-49-101-001-A02 AND REPLACSDR VNAA202606120046Seat Track · corrodedCORROSION ON SIDE SEAT RAILS BTW FS 669 TO FS 847 LH SIDE (3 E/AS) ALSO BTW FS 847.20 TO FS 985 LH SIDE (3 E/AS) AT C PAX. CORROSION ON SIDE SEAT RAILS BTW FS 669 TO FS 847 LH SIDE (3 E/AS) ALSO BTW FS 847.20 TO FS 985 LH SIDE (3 E/AS) AT C PAX WAS EVALUATEDSDR VNAA202606120045Seat Track · corrodedCORROSION ON SIDE SEAT RAILS BTW FS 669 TO FS 847 RH SIDE (3 E/AS) ALSO BTW FS 847.20 TO FS 997 RH SIDE (2 E/AS) AT C PAX. SIDE SEAT RAILS BTW FS 669 TO FS 847 RH SIDE (3 E/AS) ALSO BTW FS 847.20 TO FS 997 RH SIDE (2 E/AS) AT C PAX WAS EVALUATED PER SRM 53-4SDR VNAA202606120044Access Panel · corrodedCORROSION ON SEVERAL LOCATIONS OF THE ACCESS PANEL SEATING SURFACE (621AT, 621AB & 621BR) (521AT, 521AB & 521BR) BOTH WINGS. CORROSION ON SEVERAL LOCATIONS OF THE ACCESS PANEL SEATING SURFACE (621AT, 621AB & 621BR) (521AT, 521AB & 521BR) BOTH WINGS. WERE REPASDR VNAA202606120043Rib · crackedCRACK ON RIB LEADING EDGE SS 57.16 AT RT WING. CRACK ON RIB LEADING EDGE SS 57.16 AT RT WING WAS REPAIRED PER REO 690-57-41-240 REV-.SDR VNAA202606120042Splice · corrodedCORROSION ON DOUBLER SPLICE ON FS349 STGR 17L AT PASSENGERS CABIN FLOOR. DOUBLER SPLICE (FITTING) ON FS349 STGR 17L AT PASSENGERS CABIN FLOOR WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01.SDR VNAA202606120041Web · crackedCRACK ON FLOOR WEB LH SIDE FS193 (BELOW BRAKE ACCUMULATOR INDICATION SUPPORT DOUBLER) AT ELECTRICAL BAY. FLOOR WEB LH SIDE FS193 (BELOW BRAKE ACCUMULATOR INDICATION SUPPORT DOUBLER) AT ELECTRICAL BAY WAS REPAIRED PER REO 690-53-11-2173 REV. --.SDR VNAA202606120040Frame · corrodedCORROSION ON FRAME FS 295.00 BTW STGR 26L AND 26R AT AVIONICS COMPARTMENT. CORROSION ON FRAME FS 295.00 BTW STGR 26L AND 26R AT AVIONICS COMPARTMENT WAS REMOVED IAW SRM 51-21-06-001-001-A01. AREA ON FRAME FS 295 BTW STGR 27 AND 26R IT IS WITHIN LIMITS IAW SRMSDR VNAA202606120039Floorbeam · crackedCRACKED CENTER FLOOR BEAM FS 280.0 RBL 12.0 BELOW WL72.50 AT COCKPIT. CENTER FLOOR BEAM FS 280.0 RBL 12.0 BELOW WL72.50 AT COCKPIT WAS REPAIRED PER REO 690-53-11-2174 REV. - -.SDR VNAA202606120038Angle · corrodedCORROSION ON ANGLE AND KICK PLATE OF PASSENGER DOOR FLOOR STRUCTURE. ANGLE & KICK PLATE OF PASSENGER DOOR FLOOR STRUCTURE WERE EVALUATED OUT OF LIMITS IAW SRM 53-21-23-101-001-A02 & REPLACED IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 & SRM 51-41-0SDR VNAA202606120037Web · crackedCRACK ON FLOOR WEB RH SIDE FS193 (BELOW ADG PUMP) AT FWD ELECTRICAL BAY INTTERNAL STRUCTURE. FLOOR WEB RH SIDE BS 193 (BELOW ADG PUMP) AT FWD ELECTRICAL BAY INTTERNAL STRUCTURE WAS REPAIRED IAW SRM 53-11-43-201-001-A01.SDR VNAA202606120063Bracket · crackedCRACK ON CORNERS SUPPORT PLATE OF MAIN BATTERY DIRECT BUSS (JB6) AT FWD EQUIPMENT COMPARTMENT. SUPPORT PLATE OF MAIN BATTERY DIRECT BUSS (JB6) AT FWD EQUIPMENT COMPARTMENT WAS REPLACED PER SRM 51-42-21-001-001-A01.SDR VNAA202606120036Intercostal · corrodedCRACK ON UPPER INTERCOSTAL LT SIDE BTW BS 173 TO BS 193 AND WL 79.50 ON INTERNAL STRUCTURE AT NOSE HYDRAULICS COMPARTMENT. UPPER INTERCOSTAL LH SIDE BTW BS 173 TO BS 193 AND WL79.50 ON INTERNAL STRUCTURE AT NOSE HYDRAULICS COMPARTMENT WAS REPAIRED PER EA 5311SDR VNAA202606120035Intercostal · corrodedCRACK ON UPPER INTERCOSTAL LH SIDE BTW FS173 TO FS193 AND WL79.50 ON INTERNAL STRUCTURE AT NOSE HYDRAULICS BAY. UPPER INTERCOSTAL LH SIDE BTW FS173 TO FS193 AND WL79.50 ON INTERNAL STRUCTURE AT NOSE HYDRAULICS COMPARTMENT WAS REPAIRED PER EA 5311-2026-0474 SESDR VNAA202606120034Door · corrodedCORROSION & RUSTED NUTS FOUND AT SEVERAL POINTS ON FRAMES & RIBS PLATES STRIP MLG DOOR (MATING SURFACE WITH BELLY PANELS) (LT & RT EXTERNAL AND INERNAL ZONE) AT BS 881 - 847. CORROSION AT SEVERAL POINTS ON FRAMES & RIBS PLATES STRIP MLG DOOR (MATING SURFACE WSDR VNAA202606120033Support Plate · corrodedCORROSION ON HYD PLATES ON LH/RH MAIN WHEEL WELL AND RH MLG HYDRAULIC LINES SUPPORT PLATE (IN BK, LG EXT, LG RET) AT MLG WHEEL WELL AREAS, RBL40, RBL 45 AND LBL45, LBL40. CORROSION ON HYD PLATES ON LH/RH MAIN WHEEL WELL & RT MLG HYDRAULIC LINES SUPPORT PLATESDR VNAA202606120032Support Plate · corrodedCORROSION ON CONNECTORS SUPPORT PLATES LH/RH (PX33, PX17, PX34, PX19) AT LT/RT MAIN WHEEL WELL AREA. CORROSION ON CONNECTORS SUPPORT PLATES LT/RT (PX33, PX17, PX34, PX19) AT LH/RH MAIN WHEEL WELL AREA WAS REMOVED PER SRM 51-21-06-001-001-A01, EVALUATED OUT OFSDR VNAA202606120031Channel · corrodedCORROSION ON GANG CHANNEL AT LT/RT WINGS. CORROSION ON GANG CHANNEL AT LT/RT WINGS WAS EVALUATED OUT OF LIMITS IAW SRM 51-10-06-001-001-A01 & REPLACED IAW SRM 51-41-02-001-001-A01 AND SRM 51-42-06-001-001-A01.SDR VNAA202606120030Angle · corrodedCORROSION ON ANGLE, MLG ELECTRICAL/HYDRAULIC PROTECTIVE COVER AT BEHIND PANEL 642AZ OF RT WING. ANGLE, MLG ELECTRICAL/HYDRAULIC PROTECTIVE COVER AT BEHIND PANEL 642AZ OF RH WING WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 54-00-00-101-001-A01 AND REPLACED PER SDR VNAA202606120084Intercostal · crackedCRACK ON INSTERCOSTAL, TIRE BURST COVER AT BEHIND PANEL 542AZ OF LH WING. INTERCOSTAL, TIRE BURST COVER AT BEHIND PANEL 542AZ OF LH WING WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01 AND SRM 51-42-21-001-001-A01SDR VNAA202606120029Intercostal · crackedCRACK ON INSTERCOSTAL, TIRE BURST COVER AT BEHIND PANEL 642AZ OF RH WING. INSTERCOSTAL, TIRE BURST COVER AT BEHIND PANEL 642AZ, OF RH WING WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01 AND SRM 51-42-21-001-001-A01SDR VNAA202606120028Hinge Arm · nickedINTERNAL ZONAL INSPECTION OF THE FWD BAGGAGE BAY DOOR, NICKS AND EXPOSED MATERIAL WERE FOUND AT HINGE ARMS. FWD BAGGAGE BAY DOOR, NICKS AND EXPOSED MATERIAL WERE FOUND AT HINGE ARMS WERE REPAIRED PER CRJ-900 SRM 52-35-09-201-001-A01SDR VNAA202606120027Retainer · corrodedCORROSION ON PRESSURE SEAL RETAINER AROUND MAIN AVIONICS COMPARTMENT DOOR. ORROSION ON PRESSURE SEAL RETAINER AROUND MAIN AVIONICS COMPARTMENT DOOR (3EAS) WERE EVALUATED OUT OF LIMITS PER CRJ 900 SRM 51-10-06-001-001-A01 AND REPLACED PER CRJ-900 SRM 51-42-06-SDR VNAA202606120026Support Angle · corrodedCORROSION ON ANGLE SUPPORT UPPER AND LOWER FACE LBL 50 TO LBL 70 REAR SPAR AREA LH MLG. ANGLE SUPPORT UPPER AND LOWER FACE LBL 50 TO LBL 70 REAR SPAR AREA LH MLG WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 54-00-00-101-001-A01 AND REPLACED PER CRJ900 SRM 51-42SDR VNAA202606120025Support · crackedCRACKED INTERNAL SUPPORT OF EXTERNAL POWER RECEPTACLE. INTERNAL SUPPORT OF EXTERNAL POWER RECEPTACLE WAS REPLACED PER SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.SDR VNAA202606120024Shim · corrodedCORROSION ON SHIMS AND NUTS OF HINGE SUPPORT OF ACCESS PANEL 182BR. SHIMS AND NUTS OF HINGE SUPPORT OF ACCESS PANEL 182BR WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 51-10-06-001-001-A01 AND REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-41-02-001-
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