N547NN
Service difficulty reports · 61
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 = 'N547NN' 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 = 'N547NN' 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 VNAA2026102126801Actuator · trippedFLAPS FAIL MSG DURING CRUISE, RAN QRH AND FLAPS DID NOT EXTEND PAST FLAPS 1 POSITION C/A REPLACED #4 FLAP ACTUATOR.SDR VNAA2026101926602Pdu · unserviceableFLAPS FAIL CAUTION MSG DURING CRUISE C/A T/S B1 006551 IAW CRJ 900 FIM 27ˆ’52ˆ’09ˆ’810ˆ’802. REMOVED AND REPLACED FLAP PDU IAW CRJ 900 AMM 27€“52€“37€“000/400€“801. OPS TEST GOOD NO DEFECTS NOTED. NO FLAP HALF SPEED OR FLAP FAIL MSG.SDR VNAA2026010611101Controller · faultedRIGHT PITOT HEAT CAUTION MSG. REMOVED AND REPLACED RT ADSHC IAW AMM 30-31-15-000/400-801. OPS CHECK GOOD. CYCLED AC AND RT PITOT HEAT NO FAULT.SDR VNAA2025051611101Windshield · arcedRIGHT WINDSHIELD HEAT ARCING IN FLIGHT BOTTOM SIDE. / REMOVED AND REPLACED RH WINDSHIELD IAW CRJ 900 AMM 56-11-01-000/400-801-A01-PSA. OPS CHECK AND LEAKS CHECKS GOOD. PRESSURE CHECK GOOD IAW CRJ 900 AMM 21-31-00-910-801-A02-PSA/ 21-31-00-910-802. NO FURTHER DSDR VNAA2024102211102Outflow Valve · malfunctionedCABIN ALT CAUTION THROUGH 10000FT. CABIN ALT WARNING ABOVE 11000 / FOUND GROUND VALVE TO BE DEFERRED IN THE WRONG POSITION. PERFORMED PRESSURIZATION OF THE A/C IAW CRJ-900 AMM 21-31-00-910-801-A02-PSA. PRESSURIZATION WAS GOOD. NO DEFECTS NOTEDSDR VNAA2024101111101Smoke Detector · false activationSMOKE AFT LAV WARNING MESSAGE IN FLIGHT AND ON GROUND MULTIPLE TIMES / CYCLED CBP-1 D9, AND PERFORMED OPS CHECK IAW CRJ 900 AMM 26-16-00-710-801-A01. OPS CHECK GOOD. FAULT COULD NOT DUPLICATE.SDR VNAA202409020010Skin · dentedDURING DETAILED VISUAL INSPECTION OF THE FUSELAGE SKIN IN REFERENCE TO JOB CARD TRFKE0080LHU/// DENT ON FUSELAGE SKIN FS 394.00 BLWN STGR 19 LH AND 20LH. DENT ON FUSELAGE SKIN FS 394.00 BLWN STGR 19 LH AND 20LH WAS REPAIRED PER REO 690-53-21-1823 REV--SDR VNAA202409010016Plate · corrodedCORROSION ON PLATE (2EAS) LBL3.5, FS540 AND FS650 OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT. CORROSION ON PLATE (2EAS) LBL3.5, FS540 AND FS650 OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT WAS EVALUATED OUT LIMITS PER CRJ900 SRM 53-32-58-101-001-A01 THERSDR VNAA202409020008Fitting · corrodedAFTER REMOVAL OF LH AILERON BUSHINGS AN BEARINGS, CORROSION AND WEAR WERE FOUND ON LUG BORE OF L 1, L2, L4, LS AND L6 OF CENTER HINGE FITTINGS OF LEFT AILERON. LUG BORE OF L1, L2, LS AND L6 OF CENTER HINGE FITTINGS OF LEFT AILERON WERE REPAIRED PER PER REO 67SDR VNAA202409020007Fitting · corrodedAFTER REMOTION OF BUSHINGS AND BEARINGS ON RH AILERON///CORROSION ON LUGS R1, R2, R5 AND R6. RH AILERON LUGS R1, R2, R5 AND R6 WERE REPAIRED PER REO 670-57-61-237 REV - - NOTES FSDR VNAA202409020006Seat Track · corrodedCORROSION ON SEAT RAILS RBL9 BTW FS 477.40 - FS 677.00 (3EA) AT PASSENGER CABIN. SEAT RAILS RBL9 BTW FS 477.40 - FS 677.00 (3EA) AT PASSENGER CABIN WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-31-49-101-001-A02 AND CRJ900 SRM 53-41-49-101-001-A02 AND WERESDR VNAA202409020005Seat Track · corrodedCORROSION ON SEAT RAILS LBL27 BTW FS 477.40 - FS 581.00 (2EA) AT PASSENGER CABIN. CORROSION ON SEAT RAILS LBL27 BTW FS 477.40 - FS 581.00 (2EA) AT PASSENGER CABIN. WAS EVALUATE PER CRJ-900 SRM 53-31-49-101-001-A02 AND SRM 53-41-49-101-001-A02 AND REPLACED SDR VNAA202409020004Seat Track · corrodedCORROSION ON SEAT RAILS LBL9 BTW FS 581.00 - FS 677.40 (3 EAS) AT PASSENGER CABIN. CORROSION ON SEAT RAILS LBL9 BTW FS 581.00 - FS 677.40 (3 EAS) AT PASSENGER CABIN. WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02 AND CRJ-900 SRM 53-41-49-101-0SDR VNAA202409020003Seat Track · corrodedCORROSION ON LH SIDE SEAT TRACK BTW FS 379.00 - FS 677.00 (4 EAS) AT PASSENGER CABIN. CORROSION ON LH SIDE SEAT TRACK BTW FS 379.00 - FS 677.00 (4 EAS) AT PASSENGER CABIN. WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01 AND CRJ-900 SRM 53-31-49SDR VNAA202409020001Seat Track · corrodedCORROSION ON SEAT RAIL BTW FS 669.40 TO FS 977.00 AND STGR 15LH AT CABIN PAX. CORROSION ON SEAT RAIL BTW FS 669.40 TO FS 977.00 AND STGR 15LH AT CABIN PAX.SDR VNAA202409010029Skin · dentedSEVERAL DENTS ON EXTERNAL FUSELAGE SKIN IN AREA COVERED BY RH VENTRAL FIN FAIRING. CORRECTIVE ACTION: SEVERAL DENTS ON EXTERNAL FUSELAGE SKIN IN AREA COVERED BY RH VENTRAL FIN FAIRING. WERE REPAIRED PER REO 670-51-00-085 REV -A AND PER REO 690-53-00-569 REV -SDR VNAA202409010028Skin · dentedSEVERAL DENTS ON EXTERNAL FUSELAGE SKIN IN AREA COVERED BY LH VENTRAL FIN FAIRING. SEVERAL DENTS ON EXTERNAL FUSELAGE SKIN IN AREA COVERED BY LH VENTRAL FIN FAIRING WERE REPAIRED PER REO 670-51-00-085 REV -A AND PER REO 690-53-71-079 REV -SDR VNAA202409010026Seat Track · corrodedCORROSION AT SEAT RAIL OF LBL9 BTW FS349.00 TO FS 477.40. SEAT RAIL OF LBL9 BTW FS349.00 TO FS 477.40 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 CONF(A12).SDR VNAA202409010027Floor Support · corrodedCORROSION ON GALLEY FLOOR SUPPORTS (4EAS) LOCATED BTW FS 280.00 - FS 295.00 AND AT FUSELAGE FLOOR STRUCTURE. GALLEY FLOOR SUPPORTS (4EAS) LOCATED BTW FS 280.00 - FS 295.00 AND AT FUSELAGE FLOOR STRUCTURE WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01SDR VNAA202409010025Floor Support · corrodedCORROSION ON UPPER FACE OF FLOOR SUPORT RBL 9.00 BTW FS 1000.00 TO FS 1069.75 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE. UPPER FACE OF FLOOR SUPPORT RBL 9.00 BTW FS 1000.00 TO FS 1069.75 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE WAS REPAIRED PER REO 690-53-61-1SDR VNAA202409010022Frame · corrodedCORROSION ON FRAME FS1088.20 BTWN STGR 27 AND STGR 25LH AT AFT BAGGAGE BAY COMPARTMENT. CORROSION ON FRAME FS1088.20 BTWN STGR 27 AND STGR 25LH AT AFT BAGGAGE BAY COMPARTMENT WAS REMOVED PER CRJ 900 SRM 51-21-06-001-001-A01 AND WAS EVALUATED WITHIN LIMITS PESDR VNAA202409010020Floorbeam · corrodedCORROSION ON FLOOR SUPPORT FS=281 BETWEEN STGR 25LH TO 25RH AT MAIN AVIONICS COMPARTMENT. FLOOR SUPPORT FS=281 BETWEEN STGR 25LH TO 25RH AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01SDR VNAA202409010019Beam · corrodedCORROSION ON BEAM SIDE AT AFT BAGGAGE BAY COMPARTMENT FLOOR STRUCTURE. BEAM SIDE AT AFT BAGGAGE BAY COMPARTMENT FLOOR STRUCTURE WAS REPAIRED PER REO 690-53-61-1431 REV - -SDR VNAA202409010017Skin · corrodedCORROSION ON INTERNAL SKIN CUT OUT, (SEAL SEATLEMENT AREA), DOOR SURROUND STRUCTURE, MAIN AVIONICS COMPARTMENT. CORROSION ON INTERNAL SKIN CUT OUT, (SEAL SEATLEMENT AREA), DOOR SURROUND STRUCTURE, MAIN AVIONICS COMPARTMENT WAS REMOVED AND FOUND WHITHIN LIMITSSDR VNAA202409010011Floorbeam · corrodedCORROSION ON FLOORBEAM FS280 (RBL9 TO LBL9) AT CABIN FLOOR STRUCTURE. FLOORBEAM FS280 (RBL9 TO LBL9) AT CABIN FLOOR STRUCTURE IT IS OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 THEREFORE WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-10-SDR VNAA202409010007Duct · crackedCRACK ON AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH. AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH. (SM) WAS REPAIRED PER PER. REO. 690-28-25-023 REV.--SDR VNAA202409010024Floor Support · corrodedCORROSION ON UPPER FACE OF FLOOR SUPPORTLBL 9.00 BTW FS 1000.00 TO FS 1069.75 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE. FLOOR SUPPORT LBL 9.00 BTW FS 1000.00 TO FS 1069.75 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE WAS REPAIRED PER REO 690-53-61-1435 REV: - -SDR VNAA202409010023Floor Support · corrodedCORROSION ON UPPER FACE OF FLOOR SUPPORT LBL 27 BTW FS 1000.00 TO FS 1069.75.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE. FLOOR SUPPORTLBL 27 BTW FS 1000.00 TO FS 1069.75.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE WAS REPAIRED PER REO 690-53-61-1434 REV - -SDR VNAA202409010018Fitting · corrodedCORROSION ON JACK FITTING SUPPORTS (2EAS) BTW FS=265.00 AND FS=280.00 AT AT MAIN AVIONICS COMPARTMENT. (E/E). JACK FITTING SUPPORTS (2EAS) BTW FS=265.00 AND FS=280.00 AT AT MAIN AVIONICS COMPARTMENT. (E/E) WERE REPAIRED PER REO 690-53-11-1831 REV. --SDR VNAA202409010013Floor Support · corrodedCORROSION ON FLOOR SUPPORT RBL12.0 AND LBL12.0 BTW FS260 TO FS280 AT FLIGHT COMPARTMENT. CORROSION ON FLOOR SUPPORT RBL12.0 AND LBL12.0 BTW FS260 TO FS280 AT FLIGHT COMPARTMENT WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01. ON FLOOR SUPPORT LBL12.0 BTW FS26SDR VNAA202409020009Retainer · corrodedAFTER SEAL AT AFT BAGGAGE BAY DOOR REMOVAL, CORROSION ON AFT RETAINER SEAL CORNER LWR AND RETAINER SEAL LWR. AFT RETAINER SEAL CORNER LWR AND RETAINER SEAL LWR WERE EVALUATED OUT LIMITS PER CRJ-900 SRM 51-42-21-001-001-A01 THEREFORE WERE REPLACED PER CRJ-900 SDR VNAA202409010015Bracket · corrodedCORROSION ON BRACKETS, MACHINED (10EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT. BRACKETS, MACHINED (2EAS) (P/N:SH670-33389-1) WERE CLEANED AND NO DAMAGES WERE FOUND PER CRJ-900 SRM 51-26-00-001-001-A01, AND BRACKETS MACHINED (8EAS) WERE EVALUATED OUT SDR VNAA202409010012Floorbeam · corrodedCORROSION ON RH CROSSBEAM FS 280 AT COCKPIT CABIN FLOOR. CORROSION ON RH CROSSBEAM FS 280 AT COCKPIT CABIN FLOOR WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01 THEREFORE RH CROSSBEAM FS 280 WAS REPLACED PER PER CRJ-900 SRM 51-42-06-001-001-A01,SDR VNAA202409010010Floor Support · crackedCRACK ON FLOOR SUPPORT RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL79.50). FLOOR SUPPORT RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STSDR VNAA202409010009Floorbeam · crackedCRACKED CENTER COCKPIT FLOOR BEAM RBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. CENTER COCKPIT FLOOR BEAM RBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1808. REV.--SDR VNAA202409010008Intercostal · wornWORN INTERCOSTAL LOCATED AT STRINGER 3 RH BTW FS 364.00 TO FS 379.00 AT PASSENGER COMPARTMENT INTERNAL STRUCTURE. INTERCOSTAL LOCATED AT STRINGER 3 RH BTW FS 364.00 TO FS 379.00 AT PASSENGER COMPARTMENT INTERNAL STRUCTURE WAS REPLACED PER CRJ900 SRM 51-42-06-SDR VNAA202409010002Skin · nickedSEVERAL NICKS ON LOWER SKIN OF RH INBOARD FLAP FLS 15.00 TO FLS 65.5 AT RH WING. LOWER SKIN OF RH INBOARD FLAP FLS 15.00 TO FLS 65.5 AT RH WING WAS BLENDED OUT PER CRJ900 SRM 51-12-00-001-001-A01, BTW FLS 45.00 TO FLS 65.5 WAS EVALUATED WITHIN LMIMITS PER CSDR VNAA202409010004Shield · chafedMULTIPLE CHAFFING ON RH ENGINE LWR FWD CORE COWL FIRE SHIELD. RH ENGINE LWR FWD CORE COWL FIRE SHIELD WAS REPAIRED PER EA 23-C9-54-0901 REV IR AND REO 690-54-23-387 REV --SDR VNAA202409010003Skin · dentedDENT ON SKIN LWR BELLY PANEL. SKIN LWR BELLY PANEL WAS REPAIRED PER REO 690-53-11-1823 REV --SDR VNAA202409010001Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT/FDW DRAG ANGLES BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM. CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT/FDW DRAG ANGLES BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM WERE RSDR VNAA202409020002Seat Track · corrodedCORROSION ON RH SIDE SEAT TRACK BTW FS 379.00 - FS 677.00 (6 EAS) AT PASSENGER CABIN. RIGHT SIDE SEAT TRACK BTW FS 379.00 - FS 677.00 AT PASSENGER CABIN WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01 AND WERE REPLACED PER CRJ900 AMM 53-00-49SDR VNAA202409010030Seat Track · corrodedCORROSION ON SEAT RAIL BTW FS 669.40 TO FS 977.00 AND STGR 15RH AT CABIN PAX. SEAT RAIL BTW FS 669.40 TO FS 977.00 AND STGR 15RH AT CABIN PAX WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND WERE REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A1SDR VNAA202409010021Plate · corrodedCORROSION ON PLATE (3EAS) AT AF BAGGAGE BAY COMPARMENT FLOOR STRUCTURE. PLATE (3EAS) AT AF BAGGAGE BAY COMPARMENT WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-32-58-101-001-A01 AND WERE REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-0SDR VNAA202409010006Rib · crackedCRACK ON OUTB MACHINED RIB OF WS 163.00 TRAILING EDGE AT RH WING. OUTB MACHINED RIB OF WS 163.00 TRAILING EDGE AT RH WING WAS REPAIRED PER REO 690-57-51-363 REV. - -SDR VNAA202409010005Rib · crackedCRACK ON OUTB MACHINED RIB OF WS 163.00 TRAILING EDGE AT LH WING. OUTB MACHINED RIB OF WS 163.00 TRAILING EDGE AT LH WING WAS REPAIRED PER REO 690-57-51-362 REV. - -SDR VNAA202307311112Dcu · faultedELEVATOR SPLIT CAUTION IN FLIGHT WITH A CAS MISCOMPARE STATUS / R & R BOTH DCU'S IAW CRJ 900 AMM 31-41-04-000/400-801-A01. PERFORMED OPS TEST IAW AMM 31-41-04-710-801-A02. OPS TEST GOOD AT THIS TIMESDR VNAA202302171111Sensor · unserviceableDURING CLIMB OUT THEY RECEIVED A CAUTION ELEVATOR SPLIT MESSAGE AND A CAS MISCOMP STATUS MSG. REMOVED AND REPLACED LH AND RH ELEVATOR POSITION TRANSMITTERS IAW CRJ900 AMM 27-34-10-000/400-801SDR VNAA202302091111None · noneCLIMBING OUT FROM CLT RCVD ELEVATOR SPLIT CAUTION MSG NORMAL ELEVATOR INPUT BEING APPLIED. CLIMBING LEFT TURN BETWEEN 6K AND 8K FT AT 250 KTS. COMPLETED DOUBLE TENSIONING OF ELEVATOR CONTROL CABLES IAW CRJ900 AMM 21-31-00-750-801SDR VNAA202110051112Transmitter · faultedSHORTLY AFTER TAKEOFF CREW RECEIVED AN "ELEVATOR SPLIT CAUTION MESSAGE". THEY DECLARED EMERGENCY AND RETURNED TO SAV. THEY DID NOT LAND OVERWEIGHT AND RETURNED TO THE GATE WITHOUT FURTHER ISSUE. NO FURTHER INFORMATION AT THIS TIME. ELEVATOR SPLIT CAUTION MSG SDR VNAA2020102011118Warning Message · false activationPRECAUTIONARY ENGINE SHUTDOWN DUE TO HIGH OIL TEMPERATURE. AIR RETURN TO CLT FOR RT ENGINE OIL HIGH TEMPERATURE. REMOVED AND REPLACED DCU 1, IAW CRJ 900 AMM 31-41-04-000/400-801. OPERATIONS CHECKED GOOD. PERFORMED OPERATIONS CHECK OF DCU 1, IAW CRJ 900 AMM
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