# Service difficulty reports: U/A Canada PT6A-45

A list on [U/A Canada PT6A-45](https://openairdocs.org/engine/u-a-canada-pt6a-45.md).

Newest first. General aviation reporting is voluntary.

- [SDR 2011F00057](https://openairdocs.org/sdr/2011F00057.md): Display · failed · Mar 3, 2011 · N17WC · Beech B300 · Central Display
  > THE COPILOTS EHSI WOULD NOT POWER UP, SCREEN REMAINED BLANK.
- [SDR 9CC2011F00000](https://openairdocs.org/sdr/9CC2011F00000.md): Blower · failed · Feb 9, 2011 · N60VP · Beech C90A · Air Distribution Fan
  > ENVIROMENTAL BLOWER FAILED, SMOKE IN CABIN.
- [SDR 2011FA0000072](https://openairdocs.org/sdr/2011FA0000072.md): Brake Assy · leaking · Jan 22, 2011 · N911RX · Beech B200 · Landing Gear Brake System
  > DURING LANDING ROLL-OUT AND AFTER UTILIZING BETA OR DISCING TO SLOW THE ACFT DOWN TO TAXI SPEEDS, I SWITCHED TO WHEEL BRAKING AND THERE WAS NO PRESSURE ON THE LT SIDE. GROUND CONTROL WAS ABLE TO CLEAR ME TO THE SIGNATURE RAMP AREA WITHOUT REQUIRING A FULL-STO
- [SDR GUUA95452122910A](https://openairdocs.org/sdr/GUUA95452122910A.md): Cable · broken · Dec 29, 2010 · N87554 · Beech 1900D · Passenger/Crew Doors
  > DURING SCHEDULED ROUTINE MX, DISCOVERED AIRSTAIR DOOR FWD CABLES BROKEN, FWD CAMS WILL NOT ROTATE. REPLACED AIRSTAIR DOOR CABLE ASSY.
- [SDR GUUA95457112510A](https://openairdocs.org/sdr/GUUA95457112510A.md): Stringer · corroded · Nov 25, 2010 · N87554 · Beech 1900D · Wing, Longeron/Stringer
  > DURING SCHEDULED ROUTINE INSP, DISCOVERED CORROSION ON THE RT WING LOWER SKIN BONDED STRINGER AT WS 114.25 TO WS 124.25 CUT OUT 4.5 INCH SECTION ON CORRODED STRINGER. FABRICATED AND INSTALLED FROWARD REPAIR ANGLE AND AFT REPAIR ANGLE ON RIGHT WING LOWER BONDE
- [SDR GUUA95453102810A](https://openairdocs.org/sdr/GUUA95453102810A.md): Skin · chafed · Oct 28, 2010 · N87554 · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING SCHEDULED ROUTINE INSP DISCOVERED SKIN CHAFE LT PRESSURE PLATE AREA APPROX FS 258 AT WS 305. REPAIRED SKIN CHAFE INSTALLED DOUBLER 2.5 X 10.5 INCHES ON LT PRESSURE PLATE AREA AT FS 258, WS 305.
- [SDR GUUA95453102510C](https://openairdocs.org/sdr/GUUA95453102510C.md): Angle · cracked · Oct 25, 2010 · N87554 · Beech 1900D · Fuselage Miscellaneous Structure
  > DURING SCHEDULED ROUTINE INSP DISCOVERED AIRSTAIR DOOR FWD ANGLE CRACKED AT LOWER SNUBBER ATTACH POINTS APPROX FS 150 AT STR 9L. REMOVED 28 INCH SECTION OF -3 ANGLE AND INSTALLED -3 FILLER ANGLE AND 8.5 INCH UPPER SPLICE AND 6.5 INCH LOWER -11 SPLICE ANGLE.
- [SDR GUUA95457032010A](https://openairdocs.org/sdr/GUUA95457032010A.md): Spar · damaged · Mar 20, 2010 · N87554 · Beech 1900D · Wing Spar
  > COMPLIED WITH COLD EXPANSION OF FASTENER HOLES IN THE WING REAR SPAR LOWER CAP IAW FAA APPROVED DATA CONTAINED IN THE ACFT COMPANY KIT 118-4014-0003. NOTE: ACFT DOWN FOR KIT WING REAR SPAR INSTALLATION.
- [SDR COEA0701756](https://openairdocs.org/sdr/COEA0701756.md): Tire · failed · Dec 27, 2007 · N756FX · Cessna 208B · Tire
  > AFTER LANDING, DURING ROLLOUT PILOT OBSERVED A STRONG VIBRATION THAT SUBSIDED AS THE AC SLOWED. GROUND PERSONAL CONFIRMED THE RT MAIN TIRE WAS FLAT. REPLACED RT MAIN TIRE AND WHEEL ASSY. (K)
- [SDR MT92007F00000](https://openairdocs.org/sdr/MT92007F00000.md): Tube · split · Jul 16, 2007 · N162SA · Cessna 208B · Tire Tube
  > AIRCRAFT LANDED ON ITS SCHEDULED ROUTE, WHEN IT EXPERIENCED A FLAT TIRE ON ROLL OUT. THIS CAUSED THE CLOSURE OF THE ACTIVE RUNWAY. MAINTENANCE PERSONNEL REPLACED THE TIRE AND TOWED THE PLANE BACK TO THE RAMP. THE TIRE WAS DISASSEMBLED AND IT WAS FOUND THAT
- [SDR 2005FA0001059](https://openairdocs.org/sdr/2005FA0001059.md): Antenna · inoperative · Apr 29, 2005 · N302EH · Dhav DHC6300 · Central Display
  > FOUND UPPER UAT ANTENNA UNSERVICEABLE DURING UAT UPGRADE. (K)
- [SDR RU32005F00001](https://openairdocs.org/sdr/RU32005F00001.md): Warning Light · false indication · Mar 24, 2005 · N76 · Beech 300BEECH · Landing Gear Position and Warning
  > ON FINAL APPROACH, LOWERED GEAR AT FAF - NO LEFT MAIN GEAR LIGHT. CYCLED GEAR ONCE INSIDE FAF - STILL NO LIGHTS, EXECUTED FLY BY RWY 4R. 2 AIRLINE CREWS ADVISED ALL 3 GEARS APPEAR DOWN. FLEW LT TRAFFIC, CYCLED GEAR 3RD TIME, OBSERVED GEAR RETRACT AND EXTEND
- [SDR 2003FA0000915](https://openairdocs.org/sdr/2003FA0000915.md): Indicator · failed · Aug 25, 2003 · N64BP · Cessna 208B · Propeller Indication System
  > PROPELLER RPM INDICATED 300 RPM HIGH DURING FLIGHT. PILOT PERFORMED PRECAUTIONARY LANDING. NO OTHER PERIMETER FLUCTUATIONS. REPLACED INDICATOR WITH NEW PART. OPERATIONAL CHECK GOOD.
- [SDR 2003FA0000893](https://openairdocs.org/sdr/2003FA0000893.md): Indicator · malfunctioned · Aug 11, 2003 · N64BP · Cessna 208B · Propeller Indication System
  > PROPELLER RPM GAUGE INDICATED 300 RPM OVER REDLINE DURING FLIGHT. PILOT PERFORMED PRECAUTIONARY LANDING AT FIELD OTHER THAN PLANNED. FURTHER INVESTIGATION OF ENGINE AND SYSTEM: NOR TORQUE FLUCTUATUON, NO ITT FLUCTUATION, NO N FLUCTUATION, INDICATOR FAILURE O
- [SDR J7B2003F00000](https://openairdocs.org/sdr/J7B2003F00000.md): Rivet · loose · Dec 16, 2002 · N64BP · Cessna 208B · Wing, Plate/Skin
  > LOOSE AND WORKING RIVETS IN INBOARD LEADING EDGE ATTACHMENT TO FORWARD SPAR RT AND LT WING.
- [SDR D5H2002F00000](https://openairdocs.org/sdr/D5H2002F00000.md): Pin · loose · Sep 10, 2002 · N64BP · Cessna 208B · Propeller/Propulsor System Wiring
  > PILOT REPORTED SMOKE IN COCKPIT 30 MINUTES INTO FLIGHT. CONNECTOR FROM PROPELLER HEAT CIRCUIT BREAKER (P-186/J-186). CONNECTOR, 12 GAUGE WIRE(HA-36). MAINTENANCE CREW FOUND CONNECTOR FULLY ENGAGED AND STILL ATTACHED TO WIRE BUNDLE. MAINTENANCE FOUND TERMIN
- [SDR DAT2002F00001](https://openairdocs.org/sdr/DAT2002F00001.md): Blade · broken · Jun 26, 2002 · N167RC · Stbros SD330 · Turbine Section
  > LT ENGINE STARTED TO SHAKE AFTER START UP. THE CREW SHUTDOWN THE ENGINE AND EXITED THE AIRCRAFT. MAINTENANCE INSPECTED THE LT ENGINE AND FOUND 2 BROKEN PT BLADES WHICH CAUSED BINDING OF THE POWER SECTION. THE POWER SECTION IS BEING REMOVED AND REPLACED.
- [SDR 98ZZZX4303](https://openairdocs.org/sdr/98ZZZX4303.md): Gas Generator · failed · Oct 23, 1998 · N55AN · Stbros SD330 · Turbine Engine Compressor Section
  > AIRCRAFT DEPARTED, ABOUT 5 MINUTES AFTER LEVELING OFF, RT ENGINE SPUN DOWN. LANDED BACK AT BASE WITH SINGLE ENGINE, WITHOUT TRYING TO RESTART IT. NOTICED THE RIGHT TORQUE GAUGE DROPPED, BUT DISREGARDED IT BECAUSE ALL OTHER GAUGES WERE NORMAL. MECHANIC DISPA
- [SDR 99ZZZX606](https://openairdocs.org/sdr/99ZZZX606.md): Turbine Section · leaking · Mar 13, 1998 · N938MA · Stbros SD330 · Turbine Section
  > A RECURRENCE OF THE LEAKING OIL ON THE LEFT POWER SECTION, PAGE 84101. THE REPAIR DID NOT HOLD. THE POWER SECTION WAS REMOVED AND REPLACED. RUN AND LEAK CHECKED GOOD.
- [SDR 97ZZZX2005](https://openairdocs.org/sdr/97ZZZX2005.md): Gas Generator · seal failed · Apr 25, 1997 · N936MA · Stbros SD330 · Turbine Section
  > PILOTS REPORTED SMOKE IN COCKPIT AND CLOSED PRSOV VALVE STOPPING THE SMOKE. SEVERAL MINUTES LATER, THE PILOTS NOTICED TORQUE AND OIL PRESSURE FLUCTUATING. FEATHERED AND SHUT DOWN ENGINE AND LANDED WITHOUT INCIDENCE. ENGINE WAS LEAKING OIL FROM THE COMPRESSO

## 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 engine_model_key = 'PT6A45'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/u-a-canada-pt6a-45/reports

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