# Service difficulty reports: N5742H, cancelled Jul 15, 2003

A list on [N5742H, cancelled Jul 15, 2003](https://openairdocs.org/deregistered/N5742H-2003-07-15.md).

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

- [SDR HEEA0015719](https://openairdocs.org/sdr/HEEA0015719.md): Nozzle · damaged · Aug 20, 1998 · N5742H · Bell 206L1 · Fuel Injector Nozzle
  > ENGINE REMOVED DUE TO LOW POWER. UPON INSPECTION OF TURBINE PARTS NOTED: CRACKED BEYOND SERVICEABLE LIMITS ON NR 1 NOZZLE VANES AND OUTER SHROUD.
- [SDR HEEA0015718](https://openairdocs.org/sdr/HEEA0015718.md): Nozzle · damaged · Aug 20, 1998 · N5742H · Bell 206L1 · Fuel Injector Nozzle
  > ENGINE REMOVED DUE TO LOW POWER. UPON INSPECTION OF TURBINE PARTS NOTED: COATING LIFTING FROM NR 2 NOZZLE 1ST AND 2ND STAGE TIP PATH.
- [SDR HEEA0015298](https://openairdocs.org/sdr/HEEA0015298.md): Starter · failed · Jul 27, 1998 · N5742H · Bell 206L1 · Starter-Generator
  > STARTER/GENERATOR ARCHING AND GENERATOR WILL NOT COME ON LINE. INSPECTED BY ACCESSORY OVERHAUL SHOP AND FOUND BRUSHES EXCESSIVELY WORN AND COMMUTATOR BURNED AND PITTED.
- [SDR 98ZZZX2082](https://openairdocs.org/sdr/98ZZZX2082.md): Engine · failed · Nov 16, 1997 · N5742H · Bell 206L1 · Engine (Turbine/Turboprop)
  > IN-FLIGHT, ENGINE OIL PRESSURE AND TORQUE PRESSURE BEGAN TO FLUCTUATE. LANDED ON OFFSHORE PLATFORM WITHOUT INCIDENT. MAINTENANCE FOUND OIL TANK LEVEL SEVERAL QUARTS LOW. REPLACED ENGINE ASSY.
- [SDR HEEA0011324](https://openairdocs.org/sdr/HEEA0011324.md): Indicator · inoperative · Oct 8, 1997 · N5742H · Bell 206L1 · Engine EGT/TIT Indicating System
  > TOT INDICATOR FAILED. NEEDLE STICKS
- [SDR HEEA0011313](https://openairdocs.org/sdr/HEEA0011313.md): Fin Assy · separated · Oct 8, 1997 · N5742H · Bell 206L1 · Vertical Stabilizer
  > FIN ASSY CORRODED AND SEPARATED BEYOND REPAIR.
- [SDR HEEA0011267](https://openairdocs.org/sdr/HEEA0011267.md): Transponder · inoperative · Oct 8, 1997 · N5742H · Bell 206L1 · ATC Transponder System
  > TRANSPONDER UNIT INOPERATIVE. TEST LIGHT WILL NOT COME ON.
- [SDR HAIHEEA9743](https://openairdocs.org/sdr/HAIHEEA9743.md): Nozzle · defective · Apr 30, 1997 · N5742H · Bell 206L1 · Turbine Section
  > RECEIVED PART FROM MACHINE SHOP. INSPECTION REVEALED; TIP PATH LIFTING ON #2 NOZZLE #2 TIP AS MARKED. INSTALLED A STANDARD AERO OVERHAULED #2 NOZZLE.
- [SDR HAIHEEA9737](https://openairdocs.org/sdr/HAIHEEA9737.md): Oil Cooler · defective · Apr 30, 1997 · N5742H · Bell 206L1 · Engine Oil Cooler
  > HIGH ENGINE OIL TEMPERATURE. ENG OIL COOLER MALFUNCTION.
- [SDR HAIHEEA9708](https://openairdocs.org/sdr/HAIHEEA9708.md): Tach Gen · malfunction · Apr 30, 1997 · N5742H · Bell 206L1 · Main Rotor Indicating System
  > TACH GEN SUSPECT BEARING OIL SOAKED.
- [SDR HAIHEEA9633](https://openairdocs.org/sdr/HAIHEEA9633.md): Indicator · error · Apr 29, 1997 · N5742H · Bell 206L1 · Engine RPM Indicating System
  > GAS PRODUCER INDICATOR EXCESSIVE FRICTION ERROR.
- [SDR HAIHEEA9524](https://openairdocs.org/sdr/HAIHEEA9524.md): Actuator · bearing frozen · Apr 23, 1997 · N5742H · Bell 206L1 · Main Rotor Control
  > ACTUATOR BEARING FROZEN.
- [SDR HEEA968495](https://openairdocs.org/sdr/HEEA968495.md): Sensor · defective · Nov 20, 1996 · N5742H · Bell 206L1 · Main Rotor Indicating System
  > SENSOR DEFECTIVE. LOW ROTOR LIGHT WILL NOT COME ON. REPLACED WITH SERVICEABLE SENSOR.
- [SDR HEEA967422](https://openairdocs.org/sdr/HEEA967422.md): Nozzle · cracked · Jun 17, 1996 · N5742H · Bell 206L1 · Turbine Section
  > ENGINE REMOVED DUE TO HIGH OIL CONSUMPTION. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: CRACKED AND BOWED BEYOND SERVICEABLE LIMITS ON #1 NOZZLE VANES. REPLACED DISCREPANT PART.
- [SDR HEEA966662](https://openairdocs.org/sdr/HEEA966662.md): Restraint · worn excess · Feb 6, 1996 · N5742H · Bell 206L1 · Main Rotor Transmission Mount
  > RESTRAINT IS WORN EXCESSIVELY. (BEARING WORN)
- [SDR HEEA955616](https://openairdocs.org/sdr/HEEA955616.md): Battery · weak · Aug 25, 1995 · N5742H · Bell 206L1 · Battery/Charger System
  > BATTERY WEAK. INSPECTED BY ACCESSORY SHOP. THIS BATTERY HAS BEEN LEAD TESTED AND FOUND TO BE WEAK AS RECEIVED. FURTHER INSPECTION FOUND ELECTROLYTE DISCOLORED AND BATTERY FAILED TO COME UP TO REQUIRED 1.55 VOLTS AT END OF CHARGE.
- [SDR HEEA955066](https://openairdocs.org/sdr/HEEA955066.md): Support · req replacement · May 23, 1995 · N5742H · Bell 206L1 · Main Rotor Mast/Swashplate
  > AS PER ASB 206L-93-89 REV. B (REPLACEMENT OF -109 SUPPORT WITH -113 SUPPORT)

## 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 = 'N5742H' AND deregistration_id = 'N5742H-2003-07-15'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N5742H-2003-07-15/reports

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