# Service difficulty reports: N145SK, cancelled May 13, 2004

A list on [N145SK, cancelled May 13, 2004](https://openairdocs.org/deregistered/N145SK-2004-05-13.md).

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

- [SDR S2YA03021](https://openairdocs.org/sdr/S2YA03021.md): Switch · out of adjust · Jun 6, 2003 · N145SK · Beech 1900D · Door Warning System
  > DURING FLIGHT 1070, THE CABIN DOOR ANNUNCIATOR ILLUMINATED AT 2 POUNDS OF DIFFERENTIAL PRESSURE. THE CREW DID AN AIR TURNBACK. THE SYSTEM WAS PUT ON MEL AND THE AIRCRAFT RETURNED TO SERVICE. ON 06/09 MECHANIC CLEARED THE MEL BY ADJUSTING THE LOWER SILL SWIT
- [SDR S2YA02041](https://openairdocs.org/sdr/S2YA02041.md): Switch · out of adjust · Oct 20, 2002 · N145SK · Beech 1900D · Door Warning System
  > FLT 1371 - MKE-LSE - SHORTLY AFTER TAKEOFF, THE CARGO DOOR ANNUNCIATOR ILLUMINATED. THE CREW MADE AN AIR TURN BACK TO MKE. MAINTENANCE INSPECTED THE DOOR, CLEANED AND ADJUST THE MICRO-SWITCHES. THE A/C WAS RETURN TO SERVICE WITH NO FURTHER DEFECTS. (M)
- [SDR S2YA02035](https://openairdocs.org/sdr/S2YA02035.md): Fuel Control · inoperative · Sep 3, 2002 · N145SK · Beech 1900D · Fuel Control/Turbine Engines
  > DURING FLIGHT, DURING INITIAL DECENT INTO THE RIGHT ENGINE STARTED LOSING POWER. THE CREW DIVERTED AND MADE AN UNEVENTFUL LANDING. MECHANIC INSPECTED THE AIRCRAFT AND REPLACE THE RIGHT ENGINES HIGH PRESSURE FUEL PUMP FOR TROUBLE SHOOTING BUT IT DID NOT FIX T
- [SDR S2YA00038](https://openairdocs.org/sdr/S2YA00038.md): Warning System · activated · Dec 11, 2000 · N145SK · Beech 1900D · Central Warning
  > FLT 1044 - MKE-GRB - DURING CLIMB-OUT, THE FO EFIS DISPLAY FAILED. THE CREW MADE AN AIR-TURN BACK AND AN UNEVENTFUL LANDING IN MKE. MAINTENANCE REPLACED THE NR 2 DPU, OPS CHECKED IT AND RETURNED THE AIRCRAFT TO SERVICE. (M)
- [SDR S2YA00037](https://openairdocs.org/sdr/S2YA00037.md): Switch · out of adj · Dec 11, 2000 · N145SK · Beech 1900D · Door Warning System
  > FLT 1221 - CVG-MKE - DURING CLIMB-OUT, THE CARGO DOOR ANNUNCIATOR ILLUMINATED. THE CREW MADE AN AIR-TURN-BACK AND AN UNEVENTFUL LANDING IN CVG. THE CREW CONTACTED MX AND PUT THE ANNUNCIATOR ON MEL. MAINTENANCE READJUSTED THE BOTTOM ROLLER SWITCH ON THE CARG
- [SDR S2YA00021](https://openairdocs.org/sdr/S2YA00021.md): Windshield · cracked · Jun 30, 2000 · N145SK · Beech 1900D · Flight Compartment Windows
  > FLT 1198 - MKE-IND - AT FL210, THE CO-PILOTS WINDSHIELD CRACKED. THE CREW MADE AN AIR-TURN-BACK AND AN UNEVENTFUL LANDING AT MKE. MAINTENANCE REMOVED AND REPLACED THE WINDSHIELD AND RETURNED THE AIRCRAFT TO SERVICE. (M)
- [SDR S2YA00019](https://openairdocs.org/sdr/S2YA00019.md): Circuit Breaker · inoperative · Jun 29, 2000 · N145SK · Beech 1900D · Main Landing Gear
  > MKE-IND - FLT 1052 - SHORTLY AFTER TAKEOFF, THE CREW WAS GOING TO SELECT GEAR UP BUT NOTED THE J HOOK WAS ENGAGED. THE CREW MOVED THE J HOOK AND ATTEMPTED TO RETRACT THE GEAR BUT IT STILL INDICATING DOWN AND LOCKED. THE CREW MADE AN AIR-TURN-ACK AND AN UNEVE
- [SDR S2YA00001](https://openairdocs.org/sdr/S2YA00001.md): Motor · failed · Jan 6, 2000 · N145SK · Beech 1900D · Landing Gear Retraction/Extension System
  > FLT 1120 - MKE-GRR - SHORTLY AFTER TAKEOFF, THE CREW SELECTED GEAR UP. THE RED GEAR HANDLE (INTRANSIT) LIGHT ILLUMINATED AND THE LANDING GEAR RELAY CIRCUIT BREAKER (CB) POPPED. THE CREW RESET THE CB AND IT POPPED AGAIN. THE CREW THEN SELECTED GEAR DOWN AND
- [SDR S2YA99031](https://openairdocs.org/sdr/S2YA99031.md): Harness · shorted · Dec 27, 1999 · N145SK · Beech 1900D · Landing Gear Position and Warning
  > FLT 1826 - MKE-CMH - THE STALL WARNING (HEAT) LIGHT ILLUMINATED. THE CREW CYCLED THE SWITCH SEVERAL TIMES AND THEN MADE AN AIRTURN BACK TO MKE. MAINTENANCE INSPECTED THE SYSTEM AND FOUND HIGH RESISTANCE FOR THE GROUND WIRE ON THE LEFT SQUAT SWITCH. MAINTENA
- [SDR S2YA98024](https://openairdocs.org/sdr/S2YA98024.md): Control Cable · loose · Aug 17, 1998 · N145SK · Beech 1900D · Propeller Controlling System
  > LSE/MKE - FLT 1090 - WHILE CLIMBING THROUGH 6,700 FEET, THE RT ENGINE TORQUE INCREASED MOMENTARILY AND THEN SLOWLY STARTED TO DECREASE. THE CREW SECURED THE ENGINE AS THE TORQUE DROPPED PAST 1,000 FEET/POUNDS. DECLARED AN EMERGENCY AND DIVERTED TO MSN WHERE
- [SDR S2YA970027](https://openairdocs.org/sdr/S2YA970027.md): Air Cycle Mach · seized rotor · Aug 4, 1997 · N145SK · Beech 1900D · Cabin Cooling System
  > MKE/BNA - FLT 1267 - DURING TAXI OUT TO TAKEOFF, FLIGHT CREW FOUND THEY COULD ONLY GET HOT AIR OUT OF THE ENVIRONMENTAL SYSTEM. THE CREW RETURNED TO THE GATE, DEPLANED THE PASSENGERS, AND NOTIFIED MAINTENANCE. MAINTENANCE DECIDED TO PLACE THE ACM ON MEL. TH
- [SDR S2YA970003](https://openairdocs.org/sdr/S2YA970003.md): Press/Temp Ind · failed · Jan 30, 1997 · N145SK · Beech 1900D · Engine Oil Temperature
  > OMA/MCI - FLT 1059 - FLIGHT CREW NOTICED THE LT ENGINE OIL PRESSURE WAS AT 60 PSI DURING CLIMB OUT FROM OMA. THEY DECIDED TO RETURN TO OMA. MAINTENANCE CHECKED THE ENGINE OIL, INSPECTED THE OIL FILTER, AND THE CHIP DETECTOR WITH NO PROBLEMS FOUND. THEY REPL
- [SDR S2YA970002](https://openairdocs.org/sdr/S2YA970002.md): Transducer · malfunctioned · Jan 29, 1997 · N145SK · Beech 1900D · Engine Oil Pressure
  > CGV/MKE - FLT 1027 - AFTER FLIGHT CREW REACHED CRUISING ALTITUDE, ENGINES WERE SET TO CRUISE POWER. THE CREW NOTICED THE LT ENGINE OIL PRESSURE AT 65 PSI. THEY DECLARED AN EMERGENCY AND DIVERTED TO IND. MAINTENANCE INSPECTED THE LT ENGINE OIL FILTER, CHECKE
- [SDR S2YA97006](https://openairdocs.org/sdr/S2YA97006.md): Vertical Gyro · failed · Jan 1, 1997 · N145SK · Beech 1900D · Attitude Gyro and Indicating System
  > DURING THE MONTH OF JANUARY, SEVEN 332D-11T VERTICAL GYROS (P/N 622-4565-001) FAILED. THE TIMES FOR THE VG'S WERE: 1,639.3 HRS ON N NR 145SK; 5,375.1 HRS ON N NR 79SK; 6,125.4 ON N NR 801SK; 2,328.9 HRS ON N NR 831SK; 3,063.1 HRS ON N NR 881SK; 6,820.9 HRS
- [SDR S2YA960021](https://openairdocs.org/sdr/S2YA960021.md): Terminal · loose · Jul 30, 1996 · N145SK · Beech 1900D · Door Warning System
  > AFTER THE FLIGHT CREW DEPARTED MKE ON FLT NR 1157 FOR MSN, FOUND THAT THE CARGO DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT AND DECIDED TO RETURN TO MKE, MEL'D THE CARGO DOOR ANNUNCIATOR SYSTEM 52-2 CAT C. MAINTENANCE LATER FOUND A LOOSE TERMINAL SCREW ON A MICROS
- [SDR S2YA960012](https://openairdocs.org/sdr/S2YA960012.md): Fire Loop · malfunctioned · Jun 25, 1996 · N145SK · Beech 1900D · Fire Detection
  > FLT 1050 - MKE - ON APPROACH, CREW NOTICED THE LT FIRE PULL 'T' HANDLE ILLUMINATED IN FLIGHT, THEY PROCEEDED TO SHUT DOWN THE ENGINE AND DISCHARGED THE FIRE EXTINGUISHER BOTTLE. AN EMERGENCY WAS DECLARED, THEY LANDED AND DISEMBARKED PAX OFF WING. MAINTENANCE
- [SDR S2YA960003](https://openairdocs.org/sdr/S2YA960003.md): Bulbs · failed · Feb 28, 1996 · N145SK · Beech 1900D · Landing Gear Position and Warning
  > CMH - FLT 1829 - THE FLIGHT CREW NOTICED THE LT MAIN GEAR ANNUNCIATOR FAILED TO ILLUMINATE WITH GEAR HANDLE IN THE DOWN POSITION. AN EMERGENCY WAS DECLARED AND FLIGHT LANDED UNEVENTFULLY. MAINTENANCE REPLACED BOTH LAMPS IN THAT POSITION AND ONE MORE IN ANOTH
- [SDR S2YA960001](https://openairdocs.org/sdr/S2YA960001.md): Gcu · failed · Feb 21, 1996 · N145SK · Beech 1900D · DC Regulator
  > MKE - FLT 1099 - THE LT DC GENERATOR WOULD NOT RESET AFTER TAKEOFF, RETURNED TO MKE. MAINTENANCE REPLACED THE LT DC GENERATOR CONTROL UNIT, PARALLELED THE CIRCUIT, CHECKED FOR PROPER OPERATION, AND RETURNED TO SERVICE. (X)
- [SDR S2YA950024](https://openairdocs.org/sdr/S2YA950024.md): Air Distr · odor · Oct 18, 1995 · N145SK · Beech 1900D · Air Distribution System
  > AS FLT 1093 - MKE-LSE - PROGRESSING IN THE AREA NORTH OF MSN, THE CREW NOTICED THE SMELL OF SMOKE IN THE CABIN, THOUGHT TO BE ENVIRONMENTAL. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO MSN. A MECHANIC WAS FLOWN THERE, HE GROUND RAN THE AIRCRAFT WITH ALL E
- [SDR S2YA950007](https://openairdocs.org/sdr/S2YA950007.md): Connector · loose · May 18, 1995 · N145SK · Beech 1900D · Weather Radar System
  > THE CREW REPORTED THEIR RADAR FAULTED SEVERAL TIMES DURING AN ATTEMPTED FERRY FLIGHT AND THEN FAILED. THEY THEN TURNED BACK TO THEIR ORIGINATION BECAUSE OF WEATHER CONDITIONS. MAINTENANCE RESEATED THE CANNON PLUGS AT THE COLLINS WX RADAR CONTROL PANEL, PN 62

## 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 = 'N145SK' AND deregistration_id = 'N145SK-2004-05-13'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N145SK-2004-05-13/reports

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