# Service difficulty reports: U/A Canada PT6A-6

A list on [U/A Canada PT6A-6](https://openairdocs.org/engine/u-a-canada-pt6a-6.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 92 reports

- [SDR G1IA20260810115](https://openairdocs.org/sdr/G1IA20260810115.md): Warning Message · multiple ind · Aug 10, 2026 · N557PC · Pilats PC1245 · Engine (Turbine/Turboprop)
  > HIGH ITT INDICATIONS WITH SUBSEQUENT EIS IND, INCLUDING CAUTION, WARNING & FLASHING ITT TEMP. ITT TEMP INDNS FLUCTUATE BTWN 920 & 960, REGARDLESS OF TORQUE SETTING. NO SECONDARY INDNS IN COCKPIT TO INCLUDE OIL TEMP NORMAL AS WELL AS ALL OTHER ENG INSTS. NO NOT
- [SDR ENHA20240403001](https://openairdocs.org/sdr/ENHA20240403001.md): Engine · fod · Mar 29, 2024 · N28AN · Cessna 208B · Engine (Turbine/Turboprop)
  > DURING FLIGHT, SMOKE AND BURNING SMELL NOTED IN CABIN. MX INSPECTED ENGINE AND FOUND A PIECE OF SPIRAL WRAP MELTED. REMOVED SPIRAL WRAP AND OPS CHECKED ENGINE. NO FURTHER DEFECTS NOTED.
- [SDR RU3A201910032048](https://openairdocs.org/sdr/RU3A201910032048.md): Clamp · leaking · Oct 1, 2019 · N69 · Beech 300BEECH · Engine Anti-Icing System
  > RIGHT BLEED AIR FAIL LIGHT ILLUMINATED. MAINTENANCE DISCOVERED SEVERAL HOLES RH INBD NAC EVA TUBING. R2 EVA TUBE, FOUND BAD CLAMPS AND SLEEVES (BLEED AIR LEAK) INSTALLED 3 NEW SLEEVES AND ALL NEW CLAMPS
- [SDR QMLA2016030616021](https://openairdocs.org/sdr/QMLA2016030616021.md): Motor · failed · Mar 9, 2016 · N724HF · Pilats PC1245 · Landing Gear Actuator
  > AFTER TAKEOFF, WENT TO BRING THE GEAR UP & NOTICED THE INTRANSIT LIGHTS STAYED LIT. THE HYD CAWS LIGHT CAME ON INDICATING THERE WAS A FAILURE OF THE SYS. CLIMBED UP TO 6000 FT, BEGAN TROUBLESHOOTING. ATTEMPTED RECYCLING THE GEAR, BUT WAS ONLY ABLE TO GET 2
- [SDR GLBA2013052800253](https://openairdocs.org/sdr/GLBA2013052800253.md): Frame · cracked · May 28, 2013 · N210GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE FUSELAGE FRAME AT FS 177.35 IN THE BEND RADIUS, 1" LENGTH. REPAIRED IAW EO 13-1900-53-043. MAJOR REPAIR.
- [SDR RL8R2014030700151](https://openairdocs.org/sdr/RL8R2014030700151.md): Carriage · damaged · Mar 13, 2013 · N702AV · Socata TBM700 · Trailing Edge Flaps
  > INBD FLAP CARRIAGE INSERTS HAVE LOOSENED UP UNDER NORMAL USE. COULD POSSIBLY LEAD TO FLAP CARRIAGE ATTACHMENT FAILURE DURING FLAP DEPLOYMENT WITH SUBSEQUENT LOSS OF FLAP OR WORSE. REQUIRES REPAIR TO FLAP END AND INSTALLATION OF NEW FLAP CARRIAGE INSERTS. TH
- [SDR 2012FA0000837](https://openairdocs.org/sdr/2012FA0000837.md): Support · damaged · Dec 28, 2012 · N842E · Beech 1900D · Fuselage Miscellaneous Structure
  > LEFT SUPPORT, AFT FLANGE RIVETS WERE MISSING. SUPPORT IS LOCATED BELOW THE CABIN FLOOR UNDER THE CENTER PEDESTAL.
- [SDR GLBA2012080700028](https://openairdocs.org/sdr/GLBA2012080700028.md): Spar Cap · cracked · Aug 7, 2012 · N100UX · Beech 1900D · Horizontal Stabilizer, Spar/Rib
  > DURING A SCHEDULED INSPECTION, FOUND TWO CRACKS IN THE RT SIDE OF THE VERTICAL STAB, RT FWD SPAR CAP ANGLE AT APPROX AREA VSS 84.10, 20 PERCENT. REPAIRED AFFECTED AREA IAW EO 12-1900-55-022. MAJOR REPAIR.
- [SDR EHAA20120729005](https://openairdocs.org/sdr/EHAA20120729005.md): Brake Assy · failed · Jul 29, 2012 · N171CJ · Beech 1900D · Landing Gear Brake System
  > RIGHT BRAKE FAILED ON LANDING. NO PEDAL PRESSURE ON EITHER PILOT'S OR CO-PILOT'S BRAKE PEDAL.
- [SDR 2011F00206](https://openairdocs.org/sdr/2011F00206.md): Engine · malfunctioned · Oct 2, 2011 · N136SL · Piagio P180 · Engine (Turbine/Turboprop)
  > RIGHT ENGINE SURGED AND OVER TORQUED, RT ENGINE SHUTDOWN IN THE AIR.
- [SDR GLBA20110801H](https://openairdocs.org/sdr/GLBA20110801H.md): Actuator · inoperative · Jul 29, 2011 · N210GL · Beech 1900D · Landing Gear Actuator
  > PILOT REPORTED THAT THE LT MLG BOTH GREEN "L" AND "H" ANNUNCIATORS FLICKERED THEN EXTINGUISHED THEN REILLUMINATED, NO UNSAFE INDICATIONS ON APPROACH & LANDING. MX REPLACED THE LT MLG ACTUATOR, OPS AND RIG CKS IAW TC. 1900-3230.10.
- [SDR 5APR577Y73](https://openairdocs.org/sdr/5APR577Y73.md): Motor · faulty · Jul 5, 2011 · N558AF · Pilats PC1245 · Landing Gear Retraction/Extension System
  > HYD CAWS ILLUMINATED ON GEAR RETRACTION, LANDING GEAR DID NOT RETRACT. THE HYD POWER PACK MOTOR WAS FOUND TO BE FAULTY. THE MOTOR WAS R & R WITH A SERVICEABLE UNIT PN 960.30.02.104 IAW AMM 12-A-29-10-06-00A-920A-A. PERFORMED RETRACTIONS AND EXTENSIONS OF LAN
- [SDR DYV2011F00000](https://openairdocs.org/sdr/DYV2011F00000.md): Tach Generator · malfunctioned · Jun 22, 2011 · N1083S · Beech C90A · Engine RPM Indicating System
  > THIS REPORT IS A SUPPLEMENT FROM 10 JUNE, 2011: THE PROP RPM INDICATION HAS FUNCTIONED NORMALLY SINCE THE INITIAL REPAIR OF THE ERRONIOUS INDICATION. THE PROP TACH GENERATOR WAS REPLACED WITH AN O/H PART. THE TIME SINCE NEW AND O/H ON THE FAILED PART IS UNK
- [SDR GUUA95553050311B](https://openairdocs.org/sdr/GUUA95553050311B.md): Angle · cracked · May 3, 2011 · N87555 · Beech 1900D · Fuselage Miscellaneous Structure
  > DURING SCHEDULED ROUTINE STRUCTURAL INSP DISCOVERED RT CLOSING ANGLE CRACKED 2.1 INCHES AT FS 288.0. STOP DRILLED CRACK AND INSTALLED 13.5 INCH REPAIR ANGLE.
- [SDR 2011FA0000212](https://openairdocs.org/sdr/2011FA0000212.md): Dipstick · broken · Mar 30, 2011 · N980BC · Beech B300 · Turbine Engine Oil System
  > OIL DIPSTICK SEPARATED AT OIL CAP, STEM AND FELL INTO OIL TANK. THE STICK AND STEM WERE NOT ASSEMBLED CORRECTLY. THE STICK WAS NOT PUSHED FAR ENOUGH IN THE STEM SO THE RETENTION PIN DID NOT ENGAGE.
- [SDR GLBA20110303H](https://openairdocs.org/sdr/GLBA20110303H.md): Frame · cracked · Mar 3, 2011 · N100UX · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED ROUNTINE INSP MX FOUND THE RT SIDE WALL HEAVY ANGLE AT FS 303, CRACKED IN THE BEND RADIUS, APPROX 1" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-010. MATERIALS UTILIZED ARE INCLUDED IN
- [SDR GLBA20110214G](https://openairdocs.org/sdr/GLBA20110214G.md): Structure · damaged · Feb 12, 2011 · N218YV · Beech 1900D · Vertical Stabilizer Miscellaneous Structure
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX THE RT STABILON WAS DAMAGED. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSP IAW EO 11-1900-55-003. MATERIALS UTILIZED ARE INCLUDED IN THE EO.
- [SDR GLBA20110202F](https://openairdocs.org/sdr/GLBA20110202F.md): Structure · cracked · Feb 2, 2011 · N218YV · Beech 1900D · Horizontal Stabilizer Structure
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND 4 CRACKS AROUND THE VENT HOLE IN THE VERT STAB BEHIND THE BULLET CTR WEB, ALL 4 CRACKS ARE.5" IN LENGTH. SUPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR AND RETENTION OF THE PAP
- [SDR GUUA52121310A](https://openairdocs.org/sdr/GUUA52121310A.md): Handle · stiff · Dec 13, 2010 · N87555 · Beech 1900D · Emergency Exits
  > DURING SCHEDULED ROUTINE INSP DISCOVERED LT EMERGENCY EXIT HANDLE STIFF TO OPERATE. LUBRICATED LT EMERGENCY EXIT HANDLE.
- [SDR GUUA95552121310A](https://openairdocs.org/sdr/GUUA95552121310A.md): Handle · stiff · Dec 13, 2010 · N87555 · Beech 1900D · Emergency Exits
  > DURING SCHEDULED ROUTINE INSP DISCOVERED LT EMERGENCY EXIT HANDLE STIFF TO OPERATE. LUBRICATED LT EMERGENCY EXIT HANDLE.
- [SDR GLBA20101206A](https://openairdocs.org/sdr/GLBA20101206A.md): Bleed Air Sys · inoperative · Dec 6, 2010 · N210GL · Beech 1900D · Engine Bleed Air System
  > CLIMBING THROUGH 20,000 FT COULDN'T GET CABIN TO QUIT CLIMBING, HAD TO DEPLOY MASKS & RETURN TO DEPARTURE, DIR STUCK AT 3.4 PSI WOULD NOT GO HIGHER. STOWED & RELOCKED MASKS IAW MM 35-20-01. RAN ENG & PRESSURIZED - NO AIR FROM LT BLEED, REMOVED ORIFICE PLATE F
- [SDR E81RTT40346](https://openairdocs.org/sdr/E81RTT40346.md): Bearing · disintegrated · Nov 15, 2010 · N363CA · Raythn B300RAYTHEON · Starter-Generator
  > (E81RINVESTIGATED REPORTED IN-FLIGHT LOSS OF LT ENG DC GENERATOR FUNCTION. INITIAL VISUAL INSP OF LT ENGINE STARTER GENERATOR SHOWED INTERNAL FAILURE, METALLIC DEBRIS IN ADJACENT ENGINE COMPARTMENT AREA. UPON DISASSEMBLY, FOUND ANTI-DRIVE END BRG HAD FAILED, C
- [SDR 2010FA0001127](https://openairdocs.org/sdr/2010FA0001127.md): Light · false indication · Oct 19, 2010 · N107SL · Piagio P180 · Door Warning System
  > BAGGAGE DOOR ANNUNCIATOR LIGHT ON IN FLIGHT.
- [SDR GLBA201009061](https://openairdocs.org/sdr/GLBA201009061.md): Autofeather Sys · malfunctioned · Sep 6, 2010 · N100UX · Beech 1900D · Propeller Feathering/Reversing
  > CYCLED IN DURING APPROACH LT ENGINE ENTERED FEATHER & OUT OF FEATHER. MX TROUBLESHOT AUTOFEATHER SYS, SYS FOUND TO OPERATE NORMALLY IAW BMM 61-21-00.
- [SDR 2010F00204](https://openairdocs.org/sdr/2010F00204.md): Fire Warning · false activation · Sep 4, 2010 · N131SL · Piagio P180 · Fire Detection
  > LT ENGINE FIRE WARNING LIGHT CAME ON IN FLIGHT, INDICATION ONLY, ENGINE WAS SHUTDOWN IN FLIGHT.
- [SDR 2010FA0000884](https://openairdocs.org/sdr/2010FA0000884.md): Fitting · cracked · Aug 23, 2010 · N107SL · Piagio P180 · Horizontal Stabilizer, Attach Fittings
  > RUDDER TRIM TAB ACTUATOR FITTING IS CRACKED ON LOWER LUG. CRACK EXTENDS FROM BEARING BORE THROUGH THE ENTIRE LUG THICKNESS. CRACK ORIGINATED AT SPOTS WHERE BEARING WAS STAKED INTO LUG.
- [SDR GUUA95532052710A](https://openairdocs.org/sdr/GUUA95532052710A.md): Motor · inoperative · May 27, 2010 · N87555 · Beech 1900D · Landing Gear Retraction/Extension System
  > DURING DESCENT WHEN EXTENDING LANDING GEAR THE MOTOR STOPPED RUNNING, AND THE IN TRANSIT LIGHT REMAINED ILLUMINATED, THE LANDING GEAR HORN BEGAN TO SOUND WITH NO MOVEMENT OF POWER LEVERS, NO ILLUMINATION OF 3 GREEN LIGHTS AFTER A FEW SECONDS THE 3 GREEN LANDIN
- [SDR 19MA201002086413](https://openairdocs.org/sdr/19MA201002086413.md): Drain · clogged · Feb 8, 2010 · N886MA · Beech 1900D · Fuel Storage
  > WHILE PERFORMING 36 MONTH FUEL COLLECTOR TANK INSP, INSPECTOR WAS UNABLE TO LOCATE THE COLLECTOR TANK AFT DRAIN OPENING IN LT COLLECTOR TANK. REMOVED DRAIL LINES FROM LOWER NACELLE AREA TO INSERT PIN UP THROUGH DRAIN FITTING TO TANK AREA TO LOCATE HOLES BUT FO
- [SDR CA090608001](https://openairdocs.org/sdr/CA090608001.md): Turbine · stalled · May 8, 2009 · Turbine Section
  > (CAN) EIR ENGINE STALLING.
- [SDR DYV2009F00000](https://openairdocs.org/sdr/DYV2009F00000.md): Downlock Switch · intermittent · Jan 29, 2009 · N1083S · Beech C90A · Landing Gear Position and Warning
  > BEFORE LANDING, WHEN GEAR WAS SELECTED DOWN, THE RT GREEN DOWN LIGHT FAILED TO ILLUMINATE. THE GEAR UNSAFE LIGHT AND HORN DID NOT INDICATE AN UNLOCKED GEAR. AFTER A FLYBY AND A VISUAL LOOK BY GROUND PERSONNEL, THE FAILED GEAR LIGHT CAME ON AND A LANDING WAS
- [SDR CA081125018](https://openairdocs.org/sdr/CA081125018.md): Blades · failed · Nov 16, 2008 · Turbine Section
  > (CAN) ACFT TYPE ID PC-9. WHILE APPLYING POWER DURING A TOUCH AND GO, THE ENGINE STARTED VIBRATING. THE PILOT REDUCED THE POWER TO IDLE AND ABORTED T/O. AS THE A/C SLOWED DOWN ON THE RUNWAY, OIL BEGAN TO SPRAY OVER THE CANOPY. ONCE CLEARED OF THE RUNWAY, THE
- [SDR GLB2008F00003](https://openairdocs.org/sdr/GLB2008F00003.md): Skin · cracked · Jul 14, 2008 · N100UX · Beech 1900D · Fuselage Main, Plate/Skin
  > POPPED RIVET HEADS AND CRACK FOUND AT STATION 163.975 ABOVE AIRSTAIR DOOR. MAINTENANCE STOP DRILLED AROUND RIVETS AND REPAIRED THE AFFECTED AREA IAW B1900D SRM 53-90. RII INSPECTION COMPLIED IAW TASKCARD 8.2.1. (K)
- [SDR GLB2008F00004](https://openairdocs.org/sdr/GLB2008F00004.md): Skin · cracked · Jul 14, 2008 · N192GL · Beech 1900D · Fuselage Main, Plate/Skin
  > BELLY SKIN CRACKED APPROXIMATELY 2 INCHES IN LENGTH AT FS 298.25 TO FS 300.25 APPROXIMATELY 5 INCHES OB OF STRINGER 12R AND APPROX 2 INCHES FROM OB EDGE OF BELLY SKIN. MAINTENANCE REMOVED DAMAGED SKIN AND PATCHED IAW SRM 53-90. PATCH 18 INCHES BY 4.5 INCHES.
- [SDR GUU2008F00003](https://openairdocs.org/sdr/GUU2008F00003.md): Wire · broken · Jul 1, 2008 · N87555 · Beech 1900D · Landing Gear System Wiring
  > AFTER TAKEOFF LANDING GEAR DID NOT RETRACT, LANDING GEAR CIRCUIT BREAKER POPPED WHEN HANDLE PUT DOWN WITH ONLY (2) GREEN LIGHTS. CIRCUIT BREAKER PUSHED IN AND GEAR WENT DOWN BREAKER POPPED AGAIN. RETURNED TO PBI LANDED WITHOUT INCIDENT. REPAIRED BROKEN WIRE S
- [SDR GUUA04210803](https://openairdocs.org/sdr/GUUA04210803.md): Cap · missing · Apr 21, 2008 · N87555 · Beech 1900D · Landing Gear Retraction/Extension System
  > FLIGHT 9197, AFTER TAKEOFF, NOSE LANDING GEAR TAKES EXCESS TIME TO RETRACT. INSTALLED AIR REGULATOR PORT CAP. OPERATIONAL CHECK NORMAL.
- [SDR GUUA04050801](https://openairdocs.org/sdr/GUUA04050801.md): Torque Tube · corroded · Apr 5, 2008 · N87555 · Beech 1900D · Elevator Structure
  > DURING SCHEDULED ROUTINE MAINTENANCE, DISCOVERED LT ELEVATOR TORQUE TUBE EXFOLIATED. REPLACED LT ELEVATOR TORQUE TUBE.
- [SDR GUUA04040801](https://openairdocs.org/sdr/GUUA04040801.md): Cable · broken · Apr 4, 2008 · N87555 · Beech 1900D · Entrance Stairs
  > FLIGHT: 9205, PILOT REPORTED (4) REAR CAMS ON FWD CABIN DOOR WILL NOT ROTATE WHEN DOOR IS SECURED. REPLACED AIRSTAIR DOOR DOWN AFT CABLE.
- [SDR AMWA89766BC](https://openairdocs.org/sdr/AMWA89766BC.md): Battery · discharged · Jan 24, 2008 · N135YV · Beech 1900D · Battery/Charger System
  > AFTER TAKEOFF, BATTERY CHARGE ANNUNCIATOR ILLUMINATED. MAINT REPLACED BATTERY AND CLEARED DISCREPANCY.
- [SDR AMWA89551BC](https://openairdocs.org/sdr/AMWA89551BC.md): Gcu · malfunctioned · Jan 10, 2008 · N135YV · Beech 1900D · DC Generating System
  > DURING FLIGHT THE BATTERY CHARGE ANNUNCIATOR ILLUMINATED. MAINT PARALLELED BOTH GCU'S AND CLEARED DISCREPANCY.
- [SDR AMWA89557BC](https://openairdocs.org/sdr/AMWA89557BC.md): Battery · discharged · Jan 10, 2008 · N135YV · Beech 1900D · Battery/Charger System
  > BATTERY CHARGE ANNUNCIATOR LIGHT ILLUMINATED IN FLIGHT. MAINT REPLACED BATTERY AND CLEARED DISCREPANCY.
- [SDR GLBA20061041](https://openairdocs.org/sdr/GLBA20061041.md): Bulb · burned out · Jan 1, 2008 · N210GL · Beech 1900D · Emergency Lighting
  > SMOKE/ODOR - PILOTS REPORTED THE GLARESHIELD INSTRUMENT EMERGENCY LIGHTS WERE SMOKING ON THE GROUND AFTER STARTING ENGINES. REMOVED EMERGENCY FUSE F127. MAINTENANCE REMOVED EMERGENCY FUSE F127 AND REMOVED AND REPLACED BULB IAW MM 33-10. OPERATIONAL CHECK GO
- [SDR GUUA12040702](https://openairdocs.org/sdr/GUUA12040702.md): Hinge Bracket · corroded · Dec 4, 2007 · N218YV · Beech 1900D · Elevator Miscellaneous Structure
  > DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RT OB ELEVATOR HINGE BRACKET EXFOLIATED. REPLACED RT OB ELEVATOR HINGE BRACKET.
- [SDR AMWA223904](https://openairdocs.org/sdr/AMWA223904.md): Skin · corroded · Oct 16, 2007 · N161YV · Beech 1900D · Fuselage Main, Plate/Skin
  > SURFACE TYPE CORROSION FOUND ON INTERIOR SURFACE OF FUSELAGE SKIN IN AIRCRAFT BELLY. FS213.25, 228.25, AND 243.25 ALONG STRINGER 16. INSPECTED, CLEANED AND REPAIRED IAW DER SUPPLIED REPAIR DATA.
- [SDR GLBA20061004](https://openairdocs.org/sdr/GLBA20061004.md): Angle · cracked · Sep 21, 2007 · N210GL · Beech 1900D · Fuselage Main, Structure
  > LT HEAVY ANGLE CRACKED AT FS STA 288.0 FORWARD END IN BEND RADIUS. 09-26-07 CRACK APPROXIMATELY 1.75" IN LENGTH. MAINTENANCE INSTALLED REPAIR ANGLE I.A.W. BEECH SRM 53-90-23. REPAIR LENGTH 13.8 INCHES..080 2024-0.
- [SDR GLBA20061005](https://openairdocs.org/sdr/GLBA20061005.md): Frame · cracked · Sep 21, 2007 · N210GL · Beech 1900D · Fuselage Main, Frame
  > FRAME CRACKED AT FS 164 AT STRINGER 9AL. CRACK LENGTH APPROXIMATELY 4 INCHES. 09-26-07 REPAIRED FRAME CRACK AT STRINGER RELIEF HOLE FS 164 AT STRINGER 9AR IAW BEECH 1900D SRM 51-70. REAPIR APPROXIMATELY 2.5" BY 4.1".080 2024 T-3.
- [SDR 2007FA0000735](https://openairdocs.org/sdr/2007FA0000735.md): Ground Wire · broken · Aug 9, 2007 · N1925P · Beech B200 · Electrical Power System Wiring
  > WIRE NR P73G16N AT RT ENGINE FIREWALL GROUND POINT GS15 SEPARATED FROM THE WIRE TERMINAL DURING CRUISE FLIGHT. THIS WIRE CONNECTS GROUND TO THE GCU PIN G. THE RT GENERATOR OUTPUT SPIKED AND OPENED THE 325 AMP RT BUSS CURRENT LIMITER, THE 50 AMP RT INVERTER CUR
- [SDR N843E12007](https://openairdocs.org/sdr/N843E12007.md): Hed · faulted · Aug 1, 2007 · N843E · Beech 1900D · Battery/Charger System
  > CREW LEFT STATION. TWENTY MINUTES IN FLIGHT "BATT TIE OPEN" ANNUNCIATOR ILLUMINATED. CREW RETURNED TO STATION WITHOUT ISSUE. REMOVED AND REPLACED BATTERY HED. OPS CHECK GOOD.
- [SDR 2007FA0000884](https://openairdocs.org/sdr/2007FA0000884.md): Plate · cracked · Jul 17, 2007 · N9602F · Cessna 208 · Landing Gear Brake System
  > FOUND TORQUE PLATE CRACKED DURING ROUTINE INSPECTION. (K)
- [SDR NSVA20070140](https://openairdocs.org/sdr/NSVA20070140.md): Fitting · loose · May 27, 2007 · N136MJ · Beech 1900D · Turbine Engine Oil System
  > RT ENG OIL PRESS FLUCTUATED BETWEEN 65-70 THEN DROPPED BELOW 60 PSI WITH LOW OIL PRESS LIGHT ILLUMINATED. INFLIGHT SHUTDOWN. TIGHTENED OIL COOLER RETURN LINE FITTING IAW BE1900 MM 71-00-00, GROUND RAN AIRCRAFT 20 MIN IAW CRUISE CONFIGURATION, ALL ENGINE PAR
- [SDR MDGA200700001](https://openairdocs.org/sdr/MDGA200700001.md): Engine · unknown · May 5, 2007 · N977AA · Beech C90 · Engine (Turbine/Turboprop)
  > INFLIGHT SHUT DOWN OF RIGHT ENGINE. TIME SINCE OH WAS 1210.00 HOURS.

Next page: https://openairdocs.org/engine/u-a-canada-pt6a-6/reports.md?page=2

## 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 = 'PT6A6'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/u-a-canada-pt6a-6/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.