# Service difficulty reports: N911EB, cancelled Apr 11, 2018

A list on [N911EB, cancelled Apr 11, 2018](https://openairdocs.org/deregistered/N911EB-2018-04-11.md).

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

- [SDR HDNA201006212010](https://openairdocs.org/sdr/HDNA201006212010.md): Clamp · loose · Jun 21, 2010 · N911EB · Bolkms BO105S · Engine Collector/Tailpipe/Nozzle
  > AT TAKEOFF, THE NR1 ENGINE FIRE LIGHT ILLUMINATED. THE ACFT RETURNED TO LANDING ZONE WITHOUT INCIDENT. UPON INSP, IT WAS FOUND THAT THE NR 1 ENGINE INBD EXHAUST STACK HAD COME LOOSE FROM THE TURBINE EXHAUST COLLECTOR AND HAD WEDGED ITSELF INTO THE ENGINE COWLI
- [SDR HDN2008F00000](https://openairdocs.org/sdr/HDN2008F00000.md): Fire Detector · corroded · Jul 17, 2008 · N911EB · Bolkms BO105S · Fire Detection
  > NR 1 ENG FIRE DETECTOR WARNING LIGHT ILLUMINATED DURING CRUISE FLIGHT. AC DIVERTED FROM FLIGHT PATH AND LANDED ON THE SHOULDER OF THE ROAD. IT WAS DETERMINED THAT THERE WAS NOT A FIRE. MAINT WAS DISPATCHED TO THE LZ. IT WAS DETERMINED THAT CORROSION WAS EV
- [SDR HDNR200400001](https://openairdocs.org/sdr/HDNR200400001.md): Shield · separated · Jul 4, 2004 · N911EB · Bolkms BO105S · Turbine Section
  > THE NR 1 NOZZLE SHIELD DOME SEPARATED CAUSING THE TURBINE NR 8 BEARING SCAVENGE STRUT TO CLOG WITH CARBON INDUCED BY THE EXCESS HEAT ALLOWED IN THE AREA BY THE MISSING DOME. WHEN THE SCAVENGE FLOW WAS COMPLETELY LOST, THE OIL WAS FORCED THROUGH THE NR 8 LABYR
- [SDR HEEA063428](https://openairdocs.org/sdr/HEEA063428.md): Warning Box · malfunctioned · Aug 6, 1999 · N911EB · Bolkms BO105S · Main Rotor Indicating System
  > RPM WARNING BOX MALFUNCTION CAUSES RPM LIGHT TO CONTINUOUSLY BLINK.
- [SDR HEEA062408](https://openairdocs.org/sdr/HEEA062408.md): Nozzle Shield · cracked · Jun 1, 1999 · N911EB · Bolkms BO105S · Turbine Section
  > ENGINE REMOVED DUE TO SMOKE ON SHUTDOWN. UPON INSPECTION OF TURBINE PARTS NOTED: CRACKED BEYOND SERVICEABLE LIMITS ON NR 1 NOZZLE SHIELD DOME AS MARKED.
- [SDR HEEA060457](https://openairdocs.org/sdr/HEEA060457.md): Control Unit · malfunctioned · Jan 25, 1999 · N911EB · Bolkms BO105S · VHF Communications System
  > CONTROL UNIT TRANSMITS CONSTANTLY. PERFORMED PRELIMINARY INSPECTION AND FOUND THUMBWHEEL INTERMITTENT.
- [SDR HEEA0016760](https://openairdocs.org/sdr/HEEA0016760.md): Indicator · erratic · Nov 6, 1998 · N911EB · Bolkms BO105S · Fuel Quantity Indicator
  > FUEL LEVEL GAUGE, ERRATIC INDICATION READINGS.
- [SDR HEEA0016652](https://openairdocs.org/sdr/HEEA0016652.md): Drive Shaft · worn · Nov 5, 1998 · N911EB · Bolkms BO105S · Tail Rotor Drive Shaft
  > TAIL ROTOR WORN BEYOND LIMITS.
- [SDR HEEA0016645](https://openairdocs.org/sdr/HEEA0016645.md): Transponder · malfunctioned · Nov 5, 1998 · N911EB · Bolkms BO105S · ATC Transponder System
  > REPLY LIGHT BLINKS CONTINUOUSLY.
- [SDR HEEA0015151](https://openairdocs.org/sdr/HEEA0015151.md): Indicator · malfunctioned · Jul 1, 1998 · N911EB · Bolkms BO105S · Directional Gyro and Indicating System
  > COURSE POINTER ON INDICATOR IS INOPERATIVE.
- [SDR HEEA0015106](https://openairdocs.org/sdr/HEEA0015106.md): Indicator · reads high · Jul 1, 1998 · N911EB · Bolkms BO105S · Engine EGT/TIT Indicating System
  > EGT/TIT INDICATOR READS HIGH AND FLUCTUATES AT 900 DEGREES WHEN VIBRATING.
- [SDR HEEA0014539](https://openairdocs.org/sdr/HEEA0014539.md): Indicator · faulty · Jun 4, 1998 · N911EB · Bolkms BO105S · Engine Oil Pressure
  > OIL PRESSURE NR 2 NEEDLE PEGS OUT WHEN POWER APPLIED.
- [SDR HEEA0014001](https://openairdocs.org/sdr/HEEA0014001.md): Turbine Wheel · pitted · Apr 21, 1998 · N911EB · Bolkms BO105S · Turbine Section
  > RECEIVING INSPECTION REVEALED: PITS BEYOND SERVICEABLE LIMITS ON NR2 WHEEL BLENDED AREA E (AFT) AS MARKED. NOTE: BLENDING OF THESE PITS WOULD EXCEED OVERHAUL LIMITS OF.050 DEEP. INSTALLED A NEW NR2 WHEEL.
- [SDR HEEA0013702](https://openairdocs.org/sdr/HEEA0013702.md): Transducer · failed · Apr 2, 1998 · N911EB · Bolkms BO105S · Fuel Pressure Indicator
  > TRANSDUCER HIGH OUT OF TOLERANCE THROUGHOUT.
- [SDR HEEA0013384](https://openairdocs.org/sdr/HEEA0013384.md): Indicator · failed · Mar 18, 1998 · N911EB · Bolkms BO105S · Engine Oil Pressure
  > NR2 ENGINE OIL PRESSURE HIGH AT 100%.
- [SDR HEEA0012951](https://openairdocs.org/sdr/HEEA0012951.md): Indicator · sticking · Feb 10, 1998 · N911EB · Bolkms BO105S · Engine RPM Indicating System
  > SINGLE RPM INDICATOR STICKING.
- [SDR HEEA0012512](https://openairdocs.org/sdr/HEEA0012512.md): Transducer · failed · Jan 6, 1998 · N911EB · Bolkms BO105S · Fuel Pressure Sensor
  > TRANSDUCER READS HIGH OUT OF TOLERANCE AT 95 PSI.
- [SDR HEEA0012215](https://openairdocs.org/sdr/HEEA0012215.md): Center Case · worn · Dec 3, 1997 · N911EB · Bolkms BO105S · Main Rotor Gearbox
  > CENTER CASE LINER LOOSE AND T/R BORE WORN.
- [SDR HEEA0012214](https://openairdocs.org/sdr/HEEA0012214.md): Upper Housing · worn · Dec 3, 1997 · N911EB · Bolkms BO105S · Main Rotor Gearbox
  > UPPER HOUSING BUSHING BORE WORN IN AREA 3.
- [SDR HEEA0012118](https://openairdocs.org/sdr/HEEA0012118.md): Bushing · separated · Nov 19, 1997 · N911EB · Bolkms BO105S · Engine Mount Section
  > INNER BUSHING SEPARATED FROM RUBBER. REPLACED WITH SERVICEABLE PART.
- [SDR HEEA0010404](https://openairdocs.org/sdr/HEEA0010404.md): Indicator · error · Jul 9, 1997 · N911EB · Bolkms BO105S · Engine EGT/TIT Indicating System
  > EXH TEMP INDICATOR EXCESSIVE FRICTION ERROR.
- [SDR HEEA0010302](https://openairdocs.org/sdr/HEEA0010302.md): Flux Valve · malfunction · Jun 26, 1997 · N911EB · Bolkms BO105S · Directional Gyro and Indicating System
  > FLUX VALVE CAUSES HSI TO SEARCH. FLUX VALVE IS 15 FEET OFF.
- [SDR HEEA0010184](https://openairdocs.org/sdr/HEEA0010184.md): Indicator · sticks · Jun 19, 1997 · N911EB · Bolkms BO105S · Engine RPM Indicating System
  > RPM INDICATOR STICKS UP TO 30%.
- [SDR HAIHEEA9945](https://openairdocs.org/sdr/HAIHEEA9945.md): Blade · cracked · May 28, 1997 · N911EB · Bolkms BO105S · Main Rotor Blades
  > BLADE IS CRACKED. NOSE AND NECK SHELL CRACKED. ALL LEADING EDGE ABRASION STRIPS SEPARATED EXCEPT #1 CENTER.
- [SDR HAIHEEA9864](https://openairdocs.org/sdr/HAIHEEA9864.md): Transducer · failed · May 13, 1997 · N911EB · Bolkms BO105S · Fuel Pressure Sensor
  > TRANSDUCER READS HIGH OUT OF TOLERANCE.
- [SDR HAIHEEA9831](https://openairdocs.org/sdr/HAIHEEA9831.md): Wheel · blade defects · May 8, 1997 · N911EB · Bolkms BO105S · Turbine Section
  > TURBINE REMOVED DUE TO CYCLED OUT #1 AND #2 WHEELS. UPON INSPECTION OF TURBINE PARTS NOTED: MINOR SULFIDATION ON ALL BLADES ON #1 WHEEL. SCRAPPED PART.
- [SDR HAIHEEA9830](https://openairdocs.org/sdr/HAIHEEA9830.md): Shield · cracked · May 8, 1997 · N911EB · Bolkms BO105S · Turbine Section
  > ENGINE REMOVED DUE TO TURBINE #1 AND #2 WHEEL CYCLES. UPON INSPECTION OF TURBINE PARTS NOTED: CRACKED BEYOND SERVICEABLE LIMITS ON #1 NOZZLE SHIELD ABOUT 75 PERCENT AROUND DOME AND EXTENDING INTO THE CENTER OF DOME UNDER DEFLECTOR. CEB-A-1341 WASCOMPLIED WI
- [SDR HAIHEEA9530](https://openairdocs.org/sdr/HAIHEEA9530.md): Gyro · defective · Apr 23, 1997 · N911EB · Bolkms BO105S · Directional Gyro and Indicating System
  > DIR GYRO VERY SLOW TO SPOOL UP HSI. CAUSES HSI TO GO OFF LINE.
- [SDR HEEA979029](https://openairdocs.org/sdr/HEEA979029.md): Transponder · defective · Feb 10, 1997 · N911EB · Bolkms BO105S · ATC Transponder System
  > INTERMITTENT OPERATION IN FLIGHT. PERFORMED PRELIMINARY INSPECTION. TROUBLESHOT AND REPLACED SWITCH BOARD ASSY P/N 200-0381-01. REPAIRED. BENCH CHECK GOOD.
- [SDR HEEA967114](https://openairdocs.org/sdr/HEEA967114.md): Control Unit · defective · May 6, 1996 · N911EB · Bolkms BO105S · HF Communications System
  > TRANSCEIVER RECEIVES SCRATCHY ON CHANNEL 5.
- [SDR HEEA966916](https://openairdocs.org/sdr/HEEA966916.md): Control Unit · defective · Apr 2, 1996 · N911EB · Bolkms BO105S · VHF Communications System
  > TRANSMITS BUT WILL NOT RECEIVE. VERIFIED UNIT DOES NOT RECEIVE. REPLACED ON/OFF SWITCH. REPAIRED. BENCH CHECK GOOD.
- [SDR HEEA966839](https://openairdocs.org/sdr/HEEA966839.md): Indicator · sticks · Mar 8, 1996 · N911EB · Bolkms BO105S · Main Rotor Indicating System
  > ROTOR NEEDLE INTERMITTENTLY STICKS.
- [SDR HEEA966800](https://openairdocs.org/sdr/HEEA966800.md): Antenna · wont test · Feb 28, 1996 · N911EB · Bolkms BO105S · Ground Proximity System
  > ANTENNA WILL NOT TEST.
- [SDR HEEA966730](https://openairdocs.org/sdr/HEEA966730.md): Control Unit · failed · Feb 26, 1996 · N911EB · Bolkms BO105S · VHF Communications System
  > DISPLAY WILL NOT COME ON. REPLACED FUSE F1 AND DIODE CR5. REPAIRED. DISPLAY DOES NOT DIM. REPLACED PHOTOCELL RT1. REPAIRED. REPLACED INTERMITTENT THUMBWHEEL ASSY. BENCH CHECK GOOD.
- [SDR HEEA966704](https://openairdocs.org/sdr/HEEA966704.md): Indicator · defective · Feb 20, 1996 · N911EB · Bolkms BO105S · Ground Proximity System
  > WILL NOT TEST. REPLACED CRACKED LENS AND RUBBER GASKET. ALIGNED AND CALIBRATED TO SPECS. BENCH CHECK GOOD.
- [SDR HEEA966664](https://openairdocs.org/sdr/HEEA966664.md): Indicator · defective · Feb 6, 1996 · N911EB · Bolkms BO105S · Engine RPM Indicating System
  > #1 AND #2 NEEDLES HAVE A 10% TORQUE SPLIT.

## 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 = 'N911EB' AND deregistration_id = 'N911EB-2018-04-11'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N911EB-2018-04-11/reports

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