N101UE
Service difficulty reports · 28
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 = 'N101UE' 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 = 'N101UE' 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 TIMA201911220001Pitot Tube · defectiveON 11/20/2019 101-UE LOST AIRSPEED INDICATION ON THE LEFT SIDE WHILE IN ROUTE TO CEDAR CITY. THE PILOT WAS ABLE TO LAND WITHOUT INCIDENT. IT IS DETERMINED THAT THE PITOT TUBE WAS ONLY HEATING ON THE AFT PORTION.SDR TIMA20170811011Line · chafedAFTER A NORMAL TAKEOFF, THE PILOT WAS UNABLE TO MAINTAIN CLIMB POWER AND TORQUE ON THE LT ENGINE. AS POWER CONTINUED TO DECREASE, THE PILOT SHUT DOWN THE LT ENGINE AND RETURNED TO DEPARTURE FOR AN UNEVENTFUL LANDING. INSPECTION REVEALED THAT THE PRIMARY FUSDR HSYA2011062411Wire · loosePILOT REPORTED - OVERHEAD PANEL OVERHEATING WITH A STRONG ELECTRICAL BURNING ODOR IN-FLIGHT. WINDSHIELD WIPERS CYCLED ONCE UNCOMMANDED. MAINTENANCE TROUBLESHOOTING - MAINTENANCE LOWERED OVERHEAD CONTROL PANEL TO TROUBLESHOOT, FOUND BALLAST RESISTOR HAD A LOSDR HSYA2011042211Skin · corrodedFUSELAGE STATION 438 HAS AREA OF EXFLOLIATION CORROSION ON LOWER FUSELAGE SKIN. CUT OUT EXFLOLIATED AREA AND FABRICATED FILLER (1.8750" X 2.6250") USING MATERIAL SPEC. 2024T3 .025. FABRICATED DOUBLER (5.1875" X 6.0625") USING MATERIAL SPEC. 2024T3 .032. CLEANSDR HSYA2010082910Skin · corrodedSTATION 453 HAS EXFOLIATION CORROSION FUSELAGE BELLY SKIN. CUT OUT SKIN CORROSION (2.5" X 3.25") AND FABRICATED FILLER FROM .040 2024T3-FABRICATED DOUBLER (5.75" X 6.75") FROM .050 2024T3. CLEANED, TREATED, PRIMED AND SEALED- INSTALLED IAW SRM 51-70-00, 53-30-SDR HSYA2010012410Resistor · hotENROUTE, PILOT OF FLIGHT 145 REPORTED THAT HE OBSERVED AN ACRID/BURNING ODOR IN THE COCKPIT. ATTEMPTED TO ISOLATE THE SOURCE VIA TURNING OFF ALL NON ESSENTIAL SYS THEN REACTIVATING THEM ONE BY ONE. HE WAS UNABLE TO ISOLATE THE SOURCE. ACFT LANDED WITHOUT INCIDSDR HSYA2009061809Attach Fitting · crackedFOUND BOTH THE LT AND RT AILERON BALANCE WEIGHT CLIPS CRACKED IN HALF. REMOVED AND REPLACED BALANCE WEIGHT CLIPS IAW KIT NR 129-4036-001.SDR HSYA20080102Rib · crackedDURING SCHEDULED MX - SIM TASK 55-30-00 (1200 FLT HR/ 24 MO) REF. B1900 STRUCTURAL INSPECTION MANUAL, MX PERFORMED A VISUAL INSPECTION OF THE VERTICAL STABILIZER STRUCTURAL COMPONENTS AND FOUND RIB, AT CANTED STAB. STA. 69.184, CRACKED ON THE RT SIDE FLANGE ATSDR HSYA20071201Engine · reads highDURING CRUISE, THE CREW REPORTED THAT THE LT ENGINE INDICATED ABNORMALLY HIGH ITT. THE CREW ELECTED TO RETURN DEPARTURE AND LANDED WITH OUT INCIDENT. MX PERFORMED A LT ENGINE ITT THERMOCOUPLE LOOP RESISTANCE CHECK AND ADJUSTED. MX ALSO PERFORMED AND ITT CALISDR HSYA200700001Rotor Shaft · shearedUPON REACHING ALTITUDE THE RT ENGINE LOST OIL AND FUEL PRESSURE AND THE ENGINE SHUTDOWN. THE AIRCRAFT RETURNED TO DEPARTURE AND LANDED WITHOUT FURTHER INCIDENT. THE NR 2 ENGINE WAS REMOVED AND SENT FOR TEARDOWN TO DETERMINE CAUSE OF THE FAILURE. ON TEARDOWN TSDR GLBA2003018TransmitterHIGH OIL PRESS RT ENG, R&R LH OIL PRESS TRANSMITTER OPS CKE LEAK CKE GOODSDR 20001229AP009Gyro · precessesNR 2 DIRECTIONAL GYRO PRECESSING CONSTANTLY. REMOVED AND REPLACED NR 2 DIRECTINAL GYRO. (M)SDR GLBA97079Connector · dirtyORD - AIR TURN BACK, AFTER CAPTAINS ALTIMETER, ALTITUDE PRESELECT, TCAS AND TRANSPONDER FAILED. MAINTENANCE CLEANED SEVERAL CANNON PLUGS. (M)SDR GLBA97029Bulb · failedSPW - EMERGENCY LIGHTS MISSING ONE BULB ON RIGHT SIDE, BURNED OUT. MAINTENANCE REPLACED BULB. (M)SDR GLBA97013Downlock Switch · out of adjustSPI - GEAR WOULD NOT RETRACT. MAINTENANCE ADJUSTED LT MAIN LANDING GEAR DOWNLOCK SWITCH. (M)SDR GLBA97010Switches · dirtySPI - GEAR HANDLE REMAINS RED WITH GEAR UP. MAINTENANCE CLEANED UPLOCK AND DOWNLOCK SWITCHES. (M)SDR GLBA96227Gear Handle · intermittentDVL - RED LIGHTS REMAIN ILLUMINATED WHEN GEAR IS UP. MAINTENANCE REMOVED AND REPLACED LANDING GEAR HANDLE AND PC RELAY BOARD. TEST FLIGHT NORMAL. (X)SDR GLBA96225Uplock Switch · failedDVL - AFTER GEAR RETRACTION, GEAR UNSAFE LIGHTS REMAINED ILLUMINATED. MAINTENANCE ADJUSTED PEDESTAL SWITCH TO OBTAIN LOWER N1 SETTING FOR GEAR UNSAFE LIGHT. TEST FLIGHT NORMAL. LEFT UPLOCK SWITCH WAS LATER REPLACED. (X)SDR GLBA96210Wipers · malfunctionedORD - WINDSHIELD WIPERS DO NOT WORK WITH SWITCH IN SLOW MODE, NO OPERATION AND STRONG SMELL OF ELECTRICAL ODOR. OVERHEAD PANEL EXTREMELY HOT. MAINTENANCE INSPECTED ELECTRICAL SYSTEM AND OPERATIONS OF WIPERS OK IN ALL MODES. NO OVERHEAT OF PANELS. (M)SDR GLBA96175Truss · crackedSPW - MAINTENANCE FOUND LEFT TRUSS CRACKED AT AREA 'A' OF INBOARD SIDE. REMOVED AND REPLACED TRUSS. (M)SDR GLBA96178Actuator · bindingORD - ON TOUCHDOWN THE RUDDER PEDALS JAMMED. AIRCRAFT PULLED HARD RIGHT AND FELT A SNAP BEFORE NORMAL STEERING WAS AVAILABLE. MAINTENANCE REMOVED AND REPLACED NOSE STEERING ACTUATOR. (M)SDR GLBA96154Fire Loop · failedDEN - FALSE FIRE INDICATION FOR RIGHT ENGINE. MAINTENANCE REMOVED AND REPLACED FORWARD FIRE LOOP ON RIGHT ENGINE. SYSTEM OPERATES NORMALLY. (M)SDR GLBA96124Fire Light · illuminatedMUN - RIGHT ENGINE 'FIRE PULL' LIGHT ILLUMINATED DURING SINGLE ENGINE TURN. MAINTENANCE INSPECTED FIRE ZONE AND FOUND NO DAMAGE, COULD NOT DUPLICATE PROBLEM. (M)SDR GLBA96086Intransit Light · illuminatedMSP - CREW REPORTED, THE GEAR 'INTRANSIT' LIGHT ILLUMINATED WITH GEAR DOWN. MX INSPECTED SYSTEM AND PERFORMED NUMEROUS GEAR SWINGS BUT COULD NOT DUPLICATE DISCREPANCY ON THE GROUND OR ON TEST FLIGHT. (M)SDR GLBA96056Cowl Latch · wornLAN - DURING CLIMB-OUT, CREW OBSERVED LEFT TOP COWL WAS DETACHED FROM INBOARD LATCHES (OUTBOARD LATCHES REMAINED LATCHED). CREW ELECTED AN AIR TURN BACK AND MADE AN UNEVENTFUL LANDING. MAINTENANCE REPLACED INBOARD, AFT COWL LATCH AND RESECURED COWL. (M)SDR 95ZZZX6639Control Handle · openJMS - ON DEPARTURE FROM JMS, THE CREW DETERMINED THE LANDING GEAR WOULD NOT RETRACT. THEY ELECTED AN AIR TURN BACK AND ACCOMPLISHED AN UNEVENTFUL LANDING. MAINTENANCE REPLACED THE LANDING GEAR CONTROL HANDLE. THE GEAR SWING AND OPS CHECK WERE SATISFACTORY.SDR 95ZZZX6638Switches · frozenDVL - AFTER DEPARTURE, THE CREW ELECTED AN AIR TURN BACK DUE TO INABILITY TO RETRACT LANDING GEAR. MAINTENANCE PLACED THE AIRPLANE IN A HEATED HANGAR, THAWED OUT THE SWITCHES, AND ACCOMPLISHED SATISFACTORY GEAR SWINGS.SDR 95ZZZM487Truss · crackedSPW - DURING ROUTINE INSPECTION, MAINTENANCE FOUND THE OUTER LEFT ENGINE TRUSS CRACKED AT UPPER WELD ON COWL ATTACH BRACKET ON TUBE, APPROXIMATELY .5 INCH LONG ON OUTER AND .125 INCH LONG ON INNER. BOTH CRACKS WERE REPAIRED IAW BEECH KIT NR 129-9006.
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