N466AW
Service difficulty reports · 169
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 = 'N466AW' 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 = 'N466AW' 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 A6WA200740445O-Ring · failedDURING CLIMB AT 25,000 FT, LT ENGINE LOW OIL PRESSURE WARNING ILLUMINATED 23 PSI 2-3 SECONDS AS PER QRH REDUCED THRUST LEVER, OIL PRESSURE STAYED BETWEEN 30-40 PSI LOW OIL PRESSURE ILLUMINATED. REMOVED AND REPLACED ENGINE NR 1 HYD ENGINE DRIVEN PUMP O-RINGS ASDR A6WA200740468Skin · corrodedLEFT FUEL TANK ACCESS CUTOUT 540BB AT WS 54.897 HAS CORROSION IN NON-CRITICAL AREA MEASURING 3.5 INCH BY .35 NCH BY .004 INCH DEEP ALONG INBOARD LIP LANDING. MAINTENANCE BLENDED CORROSION ON LEFT FUEL TANK ACCESS CUTOUT 540BB AT WS 54.897 IAW BOMBARDIER REO 6SDR A6WA200740439Floorbeam · crackedFOUND RIGHT 621 FLOOR SUPPORT ANGLE IS CRACKED. (M)SDR A6WA200740438Floorbeam · crackedFOUND LEFT 621 FLOOR SUPPORT ANGLE IS CRACKED. (M)SDR A6WA200740437Drag Angle · crackedFOUND PASSENGER DOOR AFT DRAG ANGLE IS CRACKED. (M)SDR A6WA200740436Skin · corrodedFUSELAGE EXTERIOR LOWER SKIN HAS 2 AREAS OF CORROSION LOCATED AT FS 586 FUSELAGE DRAIN HOLES .1 AREA MEASURES APPROX 1 INCH BY .75 INCH OTHER AREA MEASURES APPROX .50 INCH BY .50 INCH. BOTH AREAS ARE APPROX .005 INCH DEEP. (M)SDR A6WA200740435Intercostal · crackedFOUND RT SIDE FS 621 TO FS 625.30 INTERCOSTAL AT STRINGER 14R IS CRACKED NEAR RADIUS APPROX 1 INCH LONG. (M)SDR A6WA200740434Intercostal · crackedLT SIDE FS 621 TO FS 625.30 INTERCOSTAL AT STRINGER 14L IS CRACKED NEAR RADIUS APPROX .8 INCH LONG. (M)SDR A6WA200740400Door · out of rig(DURING WALKAROUND) SERVICE DOOR OUTER HANDLE IS DIFFICULT TO OPEN. RIGGED SERVICE DOOR UPPER STABILIZER BAR AND CLEANED SERVICE DOOR SEAL AND OUTER HANDLE. OPS CHECK GOOD IAW AMM 52-41-00. (K)SDR A6WA200740031Unknown · unknownAT TAKEOFF UNDER 80 KNOTS, RED WARNING IDG MESSAGE FOLLOWED BY GEN 2 CAUTION MESSAGE BRAKE TEMPS NR 1 AND 2 AT 4, NR 3 AT 6, AND NR 4 AT 4. SERVICED OIL ON IDG NR 2 IAW AMM 12-13-24. OPS CHECK GOOD. ALL PARAMETER DO NOT REQUIRE REJECTED TAKEOFF INSPECTION ISDR A6WA200640340Flap · malfunctionedFLAPS FAIL ON APPROACH AT 20 DEGREES. (M)SDR A6WA200640292Fairing · looseUNUSUAL VIBRATION IN AIRFRAME AND YOKE WHEN FLAPS EXTENDED AND RETRACTED. FOUND FORWARD AND AFT MOUNTS OF RIGHT AND LEFT BELLY FAIRING TO HAVE EXCESS MOVEMENT. SEALANT BROKEN AND BELLY FAIRING LOOSE. (M)SDR A6WA200640146Skin · damagedFOUND FUSELAGE SKIN PANEL DAMAGED BETWEEN FS 605 AND 621 BETWEEN STRINGERS 20L AND 21L. REPAIRED BY REMOVING DAMAGE, FABRICATING FILLER AND DOUBLER, INSTALLING EXTERNAL NON-FLUSH DOUBLER IAW BSC EO 601R-53-8866. (M)SDR A6WA200640148Stringer · bentFS 605 STRINGER 20L IS BENT. (K) MAINTENANCE REPAIRED BY REMOVING DAMAGE SECTION OF STRINGER FS 600 TO 620, FABRICATED REPLACEMENT STRINGER AND SPLICES, INSTALLED REPAIR PARTS IAW CRJ 200 SRM 53-00-03 PAGE 204. (M)SDR A6WA200640147Skin · damagedFUSELAGE SKIN DAMAGED BETWEEN FS 605 AND 621 BETWEEN STRINGERS 18L AND 20L. (K) MAINTENANCE REPAIRED BY REMOVING DAMAGE, RE-CONTOURED SKIN, FABRICATING FILLER AND DOUBLER, INSTALLING FILLER AND EXTERNAL NON-FLUSH DOUBLER IAW BSC EO 601R-53-8866. (M)SDR A6WA200640094Solenoid Valve · leakingDURING APU START UP IN FLIGHT, SIGNIFICANT FUEL SMELL DETECTED BY FLIGHT CREW. REMOVED AND REPLACED APU FUEL SHUT-OFF SOLENOID VALVE IAW SRM. LEAK AND OPS CHECK GOOD. (K)SDR A6WA200540293Angle · crackedLT FS 625 OBLIQUE ANGLE CRACKED NEAR RADIUS APPROX 1.0 INCH LONG. REPLACED ANGLE IAW SRM. (K)SDR A6WA200540292Drag Angle · crackedPASSENGER DOOR AFT DRAG ANGLE CRAKED APPROX 1 INCH LONG ADJECENT TO DOOR ASSIST CABLE PULLEY BRACKET. CUT OUT DAMAGED AREA, PERFORMED EDDY CURRENT, FABED REPAIR ANGLE, SPLICES AND INSTALLED IAW EO. (K)SDR A6WA200440186Strut · dischargedGEAR DISAGREE AFTER TAKEOFF, COMPLIED WITH QRH LANDING WEIGHT 47,000 LBS. JACKED AIRCRAFT AND OBSERVED NLG NOT SELF-CENTERING SERVICED HYDRAULIC FLUID IN STRUT AND NITROGEN CHARGE IAW MM 12-1232. JACKED AIRCRAFT AGAIN, NLG CENTERS ON ITS OWN. SWUNG ALL 3 GE
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