N619NN
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 = 'N619NN' 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 = 'N619NN' 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 VNAA202304270005Stringer · corrodedCORROSION ON STGR 26R BTW FS=364.00/349.0 AT MAIN AVIONICS COMPARTMENT. (E/E)SDR VNAA202304270004Frame · corrodedCORROSION ON FRAME FS= 364.00 BETWEEN STRG 26RH TO 26RH AT MAIN AVIONICS COMPARTMENTSDR VNAA202304270023Skin · dentedSEVERAL NICKS AND DENTS ON LOWER SKIN OF RH INBOARD FLAP FROM FLS 15.00 TO FLS 65.50SDR VNAA202304270003Support · corrodedCORROSION ON LH/RH MLG SIDE STAY SUPPORT.SDR VNAA202304270033Support · corrodedCORROSION ON SUPPORTS (2EA) AT LH WHEEL WELL AREA BTW FS=797 TO FS=830 AND LBL / RBL 45".SDR VNAA202304270008Channel · corrodedCORROSION ON INTERNAL PRODUCTION DOUBLER AND ANCHORE NUT IN STA. FS=310 BETWEEN STRG 26LH TO 26RH AT MAIN AVIONICS COMPARTMENTSDR VNAA202304270020Skin · corrodedCORROSION ON LEADING EDGE (LIP SKIN) OF RH ENGINE INLET COWL.SDR VNAA202304270010Acoustic Liner · dentedDENT AT 7:00 O'CLOCK POSITION CLOSE TO THE LEADING EDGE ON METAL PERFORATE ACOUSTIC LINER OF RIGHT FORWARD CORE COWLSDR VNAA202304270019Lug · corrodedCORROSION ON BORE LUGS AT HINGE FITTING #2 (I/B AND O/B) & HINGE FITTING#3 (O/B), RH AILERONSDR VNAA202304270018Hinge Fitting · wornAFTER RUDDER REMOVAL, FREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NO.2 AND NO. 3 AT VERYTICAL STABILIZER REAR SPAR MIDDLE SECTION.SDR VNAA202304270017Coupling · corrodedCORROSION ON COUPLINGS OF FUEL OVERWING VENT TUBING, LOCATED IN WHEEL WELL AREA BTW FS=797.00 TO FS= 813 AND RBL 39".SDR VNAA202304270015Hinge Fitting · corrodedCORROSION ON LOWER RUDDER HINGE AT REAR SPAR OF VERTICAL STABILIZERSDR VNAA202304270014Angle · corrodedCORROSION ON KICK PLATE ANGLE AT LOWER SILL, FUSELAGE PASSENGER DOOR FRAMESDR VNAA202304270013Cap · corrodedCORROSION ON MID CAP AT LOWER SILL, FUSELAGE PASSENGER DOOR FRAMESDR VNAA202304270012Skin · dentedDENTS ON EXTERNAL FUSELAGE SKIN, REAR FUSELAGE SKIN COVERED BY RH VENTRAL FIN FAIRINGSDR VNAA202304270011Skin · dentedDENTS ON EXTERNAL FUSELAGE SKIN, REAR FUSELAGE SKIN COVERED BY LH VENTRAL FIN FAIRING.SDR VNAA202304270009Seat Track · corrodedCORROSION AT SEAT RAIL LBL 9.0 BETWEEN FS364.00-FS485.00SDR VNAA202304270035Support · corrodedCORROSION ON HYD LINE SUPPORTS (4 EAS) AT LH / RH WHEEL WELL AREA BTW FS=797 TO FS= 830 AND LBL 40" AND 35" / RBL 40" AND 35"SDR VNAA202304270034Support · corrodedCORROSION ON LH/RH CONNECTORS SUPPORT PX10J1, PX01J1 AND PX09J1.SDR VNAA202304270032Retainer · corrodedCORROSION ON SEAL RETAINER OF LH/RH WING TO FUSELAGE FAIRING AT WHEEL WELL AREA.SDR VNAA202304270031Rib · corrodedCORROSION ON RIB #1 AT RH WING.SDR VNAA202304270030Access Panel · corrodedCORROSION ON SETTLEMENT AREA OF ACCESS PANELS 542AZ, 542BZ, 642BZ AND 642AZSDR VNAA202304270029Door · corrodedCORROSION ON RH MLG DOOR ON INTERNAL AND EXTERNAL SKINSDR VNAA202304270028Skin · corrodedCORROSION ON LH MLG DOOR ON INTERNAL AND EXTERNAL SKINSDR VNAA202304270007Frame · corrodedCORROSION ON FRAME FS= 310 BETWEEN STRG 24LH TO 25RH AT MAIN AVIONICS COMPARTMENT. (E/E)SDR VNAA202304270006Frame · corrodedCORROSION ON FRAME FS=333 BETWEEN STRG 25LH TO 26RH AT MAIN AVIONICS COMPARTMENT. (E/E)SDR VNAA202304270002Pressure Deck · corrodedCORROSION ON DOUBLER OF WING STUD LOWER SKIN AT LH WHEELWELL AREA BTW FS 797 TO FS=830 AND LBL 38".SDR VNAA202304270001Block · corrodedCORROSION ON LH/RH MLG HYDRAULICS LINES BLOCKS AND THEIR SUPPORTSSDR VNAA202304270027Valve · corrodedCORROSION ON FLOATATION VALVE OF AFT ACCESSORIES COMPARTMENT BULKHEAD FS 1098SDR VNAA202304270026Cylinder · corrodedCORROSION IN LOWER SURFACE OF NLG OUTER CYLINDERSDR VNAA202304270025Retainer · corrodedCORROSION ON RETAINER SEALS AT ACCESS PANEL 583AB, 583BB, 683AB, 683BBSDR VNAA202304270024Frame · corrodedCORROSION ON FWD HANDLE FRAME AT FWD / CENTER BAGGAGE BAY DOOR INTERNAL STRUCTURE.SDR VNAA202304270022Skin · corrodedCORROSION WAS FOUND IN DRAIN OF THE LOWER TAILCONE FS1181.00.SDR VNAA202304270021Channel · corrodedIN TAILCONE AND THE DRAG ANGLE ADJACENT TO BELOW RUDDER WAS FOUND CORROSIONSDR VNAA202304270016Doubler · corrodedCORROSION ON LIGHTNING PROTECTION STRIP ON RH/LH HORIZONTAL STABILIZER TIP EXTERNAL STRUCTURE (ACCESS PANEL 343BR AND 333BL)
Back to N619NN