# Service difficulty reports: N101UE

A list on [N101UE](https://openairdocs.org/aircraft/N101UE.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR TIMA201911220001](https://openairdocs.org/sdr/TIMA201911220001.md): Pitot Tube · defective · Nov 20, 2019 · N101UE · Beech 1900C · Pitot/Static Anti-Ice System
  > ON 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 TIMA20170811011](https://openairdocs.org/sdr/TIMA20170811011.md): Line · chafed · Aug 11, 2017 · N101UE · Beech 1900C · Engine Fuel Distribution
  > AFTER 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 FU
- [SDR HSYA2011062411](https://openairdocs.org/sdr/HSYA2011062411.md): Wire · loose · Jun 24, 2011 · N101UE · Beech 1900C · Ice/Rain Protection System Wiring
  > PILOT 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 LO
- [SDR HSYA2011042211](https://openairdocs.org/sdr/HSYA2011042211.md): Skin · corroded · Apr 22, 2011 · N101UE · Beech 1900C · Fuselage Miscellaneous Structure
  > FUSELAGE 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. CLEAN
- [SDR HSYA2010082910](https://openairdocs.org/sdr/HSYA2010082910.md): Skin · corroded · Aug 26, 2010 · N101UE · Beech 1900C · Fuselage Main, Plate/Skin
  > STATION 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 HSYA2010012410](https://openairdocs.org/sdr/HSYA2010012410.md): Resistor · hot · Jan 24, 2010 · N101UE · Beech 1900C · Ice/Rain Protection System Wiring
  > ENROUTE, 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 INCID
- [SDR HSYA2009061809](https://openairdocs.org/sdr/HSYA2009061809.md): Attach Fitting · cracked · Jul 2, 2009 · N101UE · Beech 1900C · Ailerons
  > FOUND 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 HSYA20080102](https://openairdocs.org/sdr/HSYA20080102.md): Rib · cracked · Jan 6, 2008 · N101UE · Beech 1900C · Vertical Stabilizer, Spar/Rib
  > DURING 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 AT
- [SDR HSYA20071201](https://openairdocs.org/sdr/HSYA20071201.md): Engine · reads high · Dec 3, 2007 · N101UE · Beech 1900C · Engine (Turbine/Turboprop)
  > DURING 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 CALI
- [SDR HSYA200700001](https://openairdocs.org/sdr/HSYA200700001.md): Rotor Shaft · sheared · Feb 27, 2007 · N101UE · Beech 1900C · Turbine Engine Accessory Drive
  > UPON 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 T
- [SDR GLBA2003018](https://openairdocs.org/sdr/GLBA2003018.md): Transmitter · Feb 19, 2003 · N101UE · Beech 1900C · Engine Oil System (Airframe Furnished)
  > HIGH OIL PRESS RT ENG, R&R LH OIL PRESS TRANSMITTER OPS CKE LEAK CKE GOOD
- [SDR 20001229AP009](https://openairdocs.org/sdr/20001229AP009.md): Gyro · precesses · Sep 7, 2000 · N101UE · Beech 1900C · Directional Gyro and Indicating System
  > NR 2 DIRECTIONAL GYRO PRECESSING CONSTANTLY. REMOVED AND REPLACED NR 2 DIRECTINAL GYRO. (M)
- [SDR GLBA97079](https://openairdocs.org/sdr/GLBA97079.md): Connector · dirty · Apr 22, 1997 · N101UE · Beech 1900C · Navigation System
  > ORD - AIR TURN BACK, AFTER CAPTAINS ALTIMETER, ALTITUDE PRESELECT, TCAS AND TRANSPONDER FAILED. MAINTENANCE CLEANED SEVERAL CANNON PLUGS. (M)
- [SDR GLBA97029](https://openairdocs.org/sdr/GLBA97029.md): Bulb · failed · Feb 17, 1997 · N101UE · Beech 1900C · Emergency Lighting
  > SPW - EMERGENCY LIGHTS MISSING ONE BULB ON RIGHT SIDE, BURNED OUT. MAINTENANCE REPLACED BULB. (M)
- [SDR GLBA97013](https://openairdocs.org/sdr/GLBA97013.md): Downlock Switch · out of adjust · Jan 21, 1997 · N101UE · Beech 1900C · Landing Gear Retraction/Extension System
  > SPI - GEAR WOULD NOT RETRACT. MAINTENANCE ADJUSTED LT MAIN LANDING GEAR DOWNLOCK SWITCH. (M)
- [SDR GLBA97010](https://openairdocs.org/sdr/GLBA97010.md): Switches · dirty · Jan 11, 1997 · N101UE · Beech 1900C · Landing Gear Position and Warning
  > SPI - GEAR HANDLE REMAINS RED WITH GEAR UP. MAINTENANCE CLEANED UPLOCK AND DOWNLOCK SWITCHES. (M)
- [SDR GLBA96227](https://openairdocs.org/sdr/GLBA96227.md): Gear Handle · intermittent · Nov 22, 1996 · N101UE · Beech 1900C · Landing Gear Selector
  > DVL - RED LIGHTS REMAIN ILLUMINATED WHEN GEAR IS UP. MAINTENANCE REMOVED AND REPLACED LANDING GEAR HANDLE AND PC RELAY BOARD. TEST FLIGHT NORMAL. (X)
- [SDR GLBA96225](https://openairdocs.org/sdr/GLBA96225.md): Uplock Switch · failed · Nov 19, 1996 · N101UE · Beech 1900C · Landing Gear Position and Warning
  > DVL - 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 GLBA96210](https://openairdocs.org/sdr/GLBA96210.md): Wipers · malfunctioned · Oct 29, 1996 · N101UE · Beech 1900C · Windshield/Door Rain/Ice Removal
  > ORD - 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 GLBA96175](https://openairdocs.org/sdr/GLBA96175.md): Truss · cracked · Aug 12, 1996 · N101UE · Beech 1900C · Engine Mount Section
  > SPW - MAINTENANCE FOUND LEFT TRUSS CRACKED AT AREA 'A' OF INBOARD SIDE. REMOVED AND REPLACED TRUSS. (M)
- [SDR GLBA96178](https://openairdocs.org/sdr/GLBA96178.md): Actuator · binding · Aug 9, 1996 · N101UE · Beech 1900C · Steering Unit
  > ORD - 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 GLBA96154](https://openairdocs.org/sdr/GLBA96154.md): Fire Loop · failed · Jul 16, 1996 · N101UE · Beech 1900C · Fire Detection
  > DEN - FALSE FIRE INDICATION FOR RIGHT ENGINE. MAINTENANCE REMOVED AND REPLACED FORWARD FIRE LOOP ON RIGHT ENGINE. SYSTEM OPERATES NORMALLY. (M)
- [SDR GLBA96124](https://openairdocs.org/sdr/GLBA96124.md): Fire Light · illuminated · Jun 24, 1996 · N101UE · Beech 1900C · Fire Detection
  > MUN - RIGHT ENGINE 'FIRE PULL' LIGHT ILLUMINATED DURING SINGLE ENGINE TURN. MAINTENANCE INSPECTED FIRE ZONE AND FOUND NO DAMAGE, COULD NOT DUPLICATE PROBLEM. (M)
- [SDR GLBA96086](https://openairdocs.org/sdr/GLBA96086.md): Intransit Light · illuminated · May 9, 1996 · N101UE · Beech 1900C · Landing Gear Position and Warning
  > MSP - 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 GLBA96056](https://openairdocs.org/sdr/GLBA96056.md): Cowl Latch · worn · Mar 19, 1996 · N101UE · Beech 1900C · Engine Cowling System
  > LAN - 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 95ZZZX6639](https://openairdocs.org/sdr/95ZZZX6639.md): Control Handle · open · Nov 2, 1995 · N101UE · Beech 1900C · Landing Gear Selector
  > JMS - 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 95ZZZX6638](https://openairdocs.org/sdr/95ZZZX6638.md): Switches · frozen · Nov 2, 1995 · N101UE · Beech 1900C · Landing Gear Retraction/Extension System
  > DVL - 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 95ZZZM487](https://openairdocs.org/sdr/95ZZZM487.md): Truss · cracked · Aug 8, 1995 · N101UE · Beech 1900C · Engine Mount Section
  > SPW - 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.

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N101UE/reports

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