N290UE, cancelled Feb 14, 2007
Service difficulty reports · 33
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 = 'N290UE' AND deregistration_id = 'N290UE-2007-02-14' 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 = 'N290UE' AND deregistration_id = 'N290UE-2007-02-14' 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 A6WA200560020Seal · leakingRT ZONE HI TEMP CAPTAIN ILLUMINATED ENROUTE IN ICING CONDITIONS. REPLACED SEALS AT NR 4 PYLON LEADING EDGE AND LEAK CHECKED WING ANTI-ICE. OPS CHECKED GOOD. (K)SDR A6WA200460034Bottle · dischargedNR 1 INTAKE ASSEMBLY INBOARD FIRE BOTTLE EXCEEDS LOW WEIGHT LIMIT. REMOVED AND REPLACED FIRE BOTTLE. (M)SDR A6WA200360032Smoke · detectedON TAXI, CABIN AND COCKPIT FILLED WITH SMOKE. MAINTENANCE PERFORMED DUCT CONTAMINATION CLEARING PROCEDURES PER SUP 96-31. CABIN TEMP CONTROL OPS NORMAL, OK FOR SERVICE. (M)SDR A6WA200360023Skin · dentedDENTS OUT OF LIMITS ON THE RT AIR BRAKE. REPAIR REQUESTED FOR BAE SYSTEM REF AVMAX FAX 1584-6900003.SDR AW6A200360021Panel · dentedDENTS OUT OF LIMITS ON THE LT WING PANEL BETWEEN RIB 14A AND 15. REPAIR REQUESTED FOR BAE SYSTEM REF.SDR A6WA200360022Structure · dentedDENTS OUT OF LIMITS ON THE RT ELEVATOR AND TABS. REPAIR REQUESTED FOR BAE SYSTEM REF AVMAX FAX 1584.SDR A6WA200360012Longeron · corrodedFORWARD CARGO DOOR CUTOUT LOWER LONGEORN CORROSION DAMAGE COMPLETELY THROUGH THE FACE LONGERON. REPAIR REQUESTED FOR BEE SYSTEM REF AVMAX-FAX 1584-60000. (M)SDR A6WA200360010Frame · crackedFRAME 32 MLG WHEEL WELL RIGHT AFT BULKHEAD CRACKED IN TWO PLACES IN LOWER FALSE DIAPHRAGM FOR FAIRING ATTACHMENT. PATCH TWO ABOVE AREAS PER SRM 51-71-11. DOUBLE ROW RIVETS 2024 T3 .050 ALUM. (M)SDR A6WA200100058Fcu · malfunctionedDURING CLIMB NR 3 ENGINE DID NOT RESPOND TO THRUST LEVER POWER CHANGES THEN NR 3 ENGINE TGT STARTED CLIMBING TO 870 DEGRESS PERFORMED SHUTDOWN. MAINTENANCE REMOVED AND REPLACED FUEL CONTROL UNIT.SDR A6WA200100024Cable · detachedFWD PAX SLIDE DEPLOY CABLE NOT ATTACHED TO GIRT BAR. MAINTENANCE REMOVED AND REPLACED EVACUATION SLIDE ASSEMBLY.SDR A6WA200100015Unknown · odorFLIGHT ATTENDANT REPORTED LIGHT SMOKE ODOR COMING FROM SEAT 18 D&F AREA INFLIGHT. MAINTENANCE INSPECTED SEAT AREA, NO ODOR NOTED. NO ODOR NOTED FROM AIR CONDITIONING PACKS AS WELL.SDR A6WA0000020Battery · dischargedNR 2 EVAC SLIDE LIGHTING BATTERY FAILS VOLTAGE CHECK. REMOVED AND REPLACED NR 2 SLIDE ASSY. (M)SDR A6WA0000019Valve · out of adjNR 2 ENGINE PRODUCED 89.0 PERCENT N1 ON FULL POWER APPLICATION AT ASE N1 REF CALLED FOR 93.4 PERCENT ENGINE ANTI-ICE ON 904 TGT. REMOVED AND REPLACED NR 2 ENGINE FCU POPPET VALVE C/W BLEED BAND ADJUSTMENT AND TAKEOFF POWER CHECK. (M)SDR A6WA9900032Rib · crackedAFT CARGO DOOR UPPER MOST RIB IS CRACKING LOCATED UNDER UPPER AFT HINGE 'L' BRACKET ON UPPER MOST RIB IAW BAE REPAIR DRAWING REF HC523H9001 AND FOUND SERVICEABLE. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)SDR A6WA9900031Bracket · crackedLEFT WING TE SHROUD LOWER SKIN STIFFENER AFT (TAG) ANGLE BRACKET CRACKED BETWEEN RIB 8 AND RIB 9. REPLACED BRACKET. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)SDR A6WA9900030Stiffener · brokenLEFT WING TE TOP SHROUD SKIN STIFFENER TO FALSE SPAR (AFT END) BROKEN BETWEEN RIBS 7 AND 8. REPLACED STIFFENER. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)SDR A6WA9900029Bracket · crackedLEFT WING TE SHROUD UPPER SKIN STIFFENER TO FALSE SPARE ANGLE BRACKET CRACKED BETWEEN RIBS 7 AND 8. REPLACED BRACKET. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)SDR A6WA9900028Angle · corrodedRIGHT WEB CLOSING ANGLE AFT OF FRAME 50 HAS ONE INCH CRACK. REPAIRED IAW BAE SRM 51-71-11 FIG 2. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)SDR A6WA9900033Stiffener · crackedRIGHT WING STIFFENER BETWEEN RIBS 7 AND 8 CRACKED AT FORWARD END. REPLACED STIFFENER. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)SDR A6WA9900027Stiffener · crackedLEFT WING STIFFENER BETWEEN RIBS 7 AND 8 CRACKED AT FORWARD ENGINE. REPLACED STIFFENER. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)SDR A6WA9900038Structure · crackedFUSELAGE STRUCTURE AFT OF FRAME 50 ABOVE LT UPPER AIRBRAKE HINGE CORNER IS CRACKED. REPAIRED PER BAE FAX JM/RJ0491-96. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)SDR A6WA9900037Structure · crackedFUSELAGE STRUCTURE AFT OF FRAME 50 ABOVE RIGHT UPPER AIRBRAKE HINGE CORNER IS CRACKED. REPAIRED PER FAX JM/RJ049-96. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)SDR A6WA9900036Rivet · shearedFUSELAGE STRUCTURE AFT OF FRAME 50 ABOVE RT UPPER AIRBRAKE HINGE HAS RIVETS SHEARED OFF FOR CORNER ANGLE BRACKET. REPLACED RIVETS. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)SDR A6WA9900035Rivet · shearedFUSELAGE STRUCTURE AFT OF FRAME 50 ABOVE LT AIRBRAKE HINGE HAS RIVETS SHEARED OFF FOR CORNER ANGLE BRACKET. REPLACED RIVETS. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)SDR A6WA9900034Gusset · crackedFUSELAGE STRUCTURE AFT OF FRAME 50 ABOVE LT UPPER AIRBRAKE HINGE HAS A FILLER PANEL CRACKED AT THE LIGHTNING HOLE. REPLACED GUSSET PLATE. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)SDR A6WA9900022Angle · crackedFORWARD PASSENGER DOOR HAS 2 EACH CRACKED ANGLES IN THE HANDLE BOX AREA. MFG AND REPLACED PER BAE DRAWINGS HC521H0507 AND HC521H0508. INSTALLED ANGLES PER SRM AND BAE FAX DJR/RJ0049-97. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)SDR A6WA9900026Gusset · corrodedSEVERAL GUSSET PLATES ON FLOOR ARE CORRODED (SURFACE CORROSION) AFT VESTIBULE. REPLACED CORRODED GUSSET PLATES, 2 EACH. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)SDR A6WA9900025Seat · crackedFORWARD F/A SEAT PAN CRACKED. REPLACED PAN. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)SDR A6WA9900024Longeron · crackedFRAME 29 MLG BAY ROOF LONGERONS CRACKED, NR 3 AND NR 15, NEAR FORWARD ENG. REPAIRED PER BAE REPAIR DRAWING HC536H9211. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)SDR A6WA9900023Bolt · brokenFRAME 29 LEFT AND RIGHT BOTTOM BOLT OF WING ATTACHMENT BRACKET HEAD APPEARS TO BE BROKEN. REMOVED BOLT, CLEANED AND INSPECTED HOLE, PREP, ALODINE, PRIMED AND INSTALLED NEW BOLT AND NUT IAW FAX DJR/RJ0022/96 AND DJR/RJ0721-96. WITCO BOND WILL BE APPLIED ON WOSDR 99ZZZM601Structure · crackedDURING SCHEDULED NDT INSPECTION OF NGL RETRACTION JACK MOUNT STRUCTURE, FOUND CRAKS IN JACK PIN STRUCTURE BORE. (M)SDR 98ZZZX3983Switch · contaminatedMYR - FLT 690 - UPON GEAR RETRACTION, LANDING GEAR DID NOT RETRACT. CLEANED SQUAT SWITCHES.SDR 98ZZZX3984Rod · brokenATW - FORWARD PASSENGER DOOR DROPS BELOW DOOR FRAME WHEN OPENED AND DOES NOT DROP AND LATCH PROPERLY WHEN CLOSED. REPLACED BROKEN LOWER ROD END ON THE CONTROL SHAFT ASSY TO TORQUE SHAFT CONTROL ROD. REPLACED LOWER HINGE COVER. NOTE: REMOVED AND REPLACED EV
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