# Service difficulty reports: Embraer EMB-110P2

A list on [Embraer EMB-110P2](https://openairdocs.org/model/embraer-emb-110p2.md).

Newest first. General aviation reporting is voluntary.

- [SDR AU510001837](https://openairdocs.org/sdr/AU510001837.md): Steering Sys · unserviceable · Nov 9, 2005 · Emb EMB110P2 · Landing Gear Steering System
  > NOSE WHEEL STEERING SYSTEM FAULTY. STEERING SYSTEM TRAVEL WAS RESTRICTED. LT MAIN LANDING GEAR AND NOSE GEAR RAN OFF RUNWAY AND BECAME BOGGED IN THE SOFT SURFACE AT THE SIDE OF THE RUNWAY.
- [SDR 2005FA0000570](https://openairdocs.org/sdr/2005FA0000570.md): Line · cracked · Mar 7, 2005 · N24AN · Emb EMB110P2 · Aircraft Fuel Distribution System
  > FOUND FUEL BYPASS TUBE ASSY CRACKED WHERE TUBE WELDED TO FLARE END OF B-NUT FITTING. TUBE APPEARS TO BE MFG WITH SMALLER RADIUS TO FIT INSIDE FLARE, CAUSING WEAK POINT. SUGGEST CLOSER INSPECTION AT THIS AREA DURING ROUTINE INSPECTION AND PRESSURE CHECK WITH
- [SDR AUS20011268](https://openairdocs.org/sdr/AUS20011268.md): Pipe · cracked · Nov 22, 2001 · Emb EMB110P2 · Engine Fuel Distribution
  > (AUS) PIPE LOCATED BETWEEN FCU AND START CONTROL VALVE CRACKED AT FITTING.
- [SDR AUS20010952](https://openairdocs.org/sdr/AUS20010952.md): Pipe · cracked · Aug 29, 2001 · Emb EMB110P2 · Engine Fuel Distribution
  > (AUS) PIPE LOCATED BETWEEN FCU AND START CONTROL VALVE CRACKED AT FITTING.
- [SDR AU010324](https://openairdocs.org/sdr/AU010324.md): Door · disconnected · Mar 17, 2001 · Emb EMB110P2 · Landing Gear Doors
  > (AUS) NOSE LANDING GEAR DOORS DISCONNECTED ON TAKEOFF PREVENTING NOSE LANDING GEAR FROM RETRACTING. SUSPECT DOORS INCORRECTLY ATTACHED. PERSONNEL/MAINTENANCE ERROR.
- [SDR AU981659](https://openairdocs.org/sdr/AU981659.md): Switch · malfunctioned · Dec 28, 1998 · Emb EMB110P2 · Landing Gear Position and Warning
  > (AUS) WITH LANDING GEAR SELECTED DOWN, THE RT SIDE HAD NO DOWNLOCK INDICATION. FAULT TRACED TO FAULTY UPLOCK MICROSWITCH - DOWNLOCK MICROSWITCH WAS ALSO REPLACED. SUSPECT WATER INGRESS INTO THE MICROSWITCH.
- [SDR AU981658](https://openairdocs.org/sdr/AU981658.md): Switch · malfuncitioned · Dec 28, 1998 · Emb EMB110P2 · Landing Gear Position and Warning
  > (AUS) WITH LANDING GEAR SELECTED DOWN, THE RIGHT SIDE HAD NO DOWNLOCK INDICATION. FAULT TRACED TO FAULTY UPLOCK MICROSWITCH. SUSPECT WATER INGRESS INTO THE MICROSWITCH.
- [SDR AU980407](https://openairdocs.org/sdr/AU980407.md): Blade · separated · Mar 25, 1998 · Emb EMB110P2 · Turbine Section
  > (AUS) ENGINE POWER TURBINE BLADE SEPARATED APPROXIMATELY 12.7MM (0.5 INCH) FROM THE BLADE ROOT. ECONDARY DAMAGE TO OTHER BLADES AND EXHAUST DUCT ASSEMBLY.
- [SDR CA980415023](https://openairdocs.org/sdr/CA980415023.md): Py Line · cracked · Mar 10, 1998 · Emb EMB110P2 · Fuel Control/Reciprocating Engines
  > (CAN) DUE TO EXCESSIVE VIBRATION ON NR 2 ENGINE CAUSED BY FAULTY STARTER/GENERATOR, THE PY LINE CRACKED RESULTING IN A DROP IN NG.
- [SDR CA980415022](https://openairdocs.org/sdr/CA980415022.md): Start/Gen · failed · Mar 6, 1998 · Emb EMB110P2 · Starter-Generator
  > (CAN) NR 2 ENGINE STARTER GENERATOR WAS UNSERVICEABLE AND CAUSING VIBRATION ON THE ENGINE CAUSING THE SHUTDOWN OF THE ENGINE IN-FLIGHT, AS A PRECAUTIONARY MEASURE. POST-FLIGHT THE STARTER GENERATOR WAS REPLACED.
- [SDR AU970719](https://openairdocs.org/sdr/AU970719.md): Indicator System · out of adjust · Jun 26, 1997 · Emb EMB110P2 · Engine Indicating System
  > (AUS) RH AND LH TORQUE SYSTEMS, RH AND LH T5 INDICATORS, RH T5 CIRCUIT RESISTANCE, LH AND RH FUEL PRESSURE INDICATION SYSTEMS, RH LOWFUEL WARNING SYSTEM, LH AND RH FUEL QUANTITY SYSTEMS, LH OIL PRESSURE INDICATION, LH GYRO COMPASS, STANDBY COMPASS AND RH GYRO
- [SDR AU970649](https://openairdocs.org/sdr/AU970649.md): Switch · out of adjust · Jun 3, 1997 · Emb EMB110P2 · Door Warning System
  > (AUS) REAR ENTRY DOOR MICROSWITCH OUT OF ADJUSTMENT
- [SDR AU970652](https://openairdocs.org/sdr/AU970652.md): Door Post · damaged · May 14, 1997 · Emb EMB110P2 · Fuselage Miscellaneous Structure
  > (AUS) FUSELAGE DOOR PILLAR AND DOOR MAIN CABLE ATTACHMENT BRACKET CRACKED.
- [SDR AU970414](https://openairdocs.org/sdr/AU970414.md): Pump · failed · Apr 21, 1997 · Emb EMB110P2 · Fuel Boost Pump
  > (AUS) LH MAIN FUEL BOOST PUMP FAILED
- [SDR AU970069](https://openairdocs.org/sdr/AU970069.md): Blade · damaged · Jan 17, 1997 · Emb EMB110P2 · Turbine Section
  > (AUS) ALL COMPRESSOR TURBINE BLADES DAMAGED BY FOD - DAMAGE INCLUDED BENDING OF BLADE LEADING EDGES AND MISSING SECTIONS - INVESTIGATION FOUND FOD TO BE A POWER TURBINE CONTAINMENT RING RETAINING BOLT
- [SDR AU960324](https://openairdocs.org/sdr/AU960324.md): Case · cracked · Feb 9, 1996 · Emb EMB110P2 · Turbine Engine Combustion Section
  > (AUS) RH ENGINE GAS GENERATOR CASE CRACKED IN AREA AROUND THE UPPER ENGINE LORD MOUNT BRACKET ATTACHMENT RUNNING ALONG THE INNER EDGEOF THE WELD BEAD - CRACK LENGTH 25.4MM (1IN)
- [SDR AU960107](https://openairdocs.org/sdr/AU960107.md): Brake Disc · worn · Jan 30, 1996 · Emb EMB110P2 · Landing Gear Brake System
  > (AUS) LH MAIN WHEEL BRAKE DISC CRACKED IN TWO

## 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 aircraft_model_key = 'EMB110P2'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/embraer-emb-110p2/reports

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