# Service difficulty reports: Pratt & Whitney Canada PT6A-67A

A list on [Pratt & Whitney Canada PT6A-67A](https://openairdocs.org/engine/pratt-whitney-canada-pt6a-67a.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 75 reports

- [SDR 2023FA0000806](https://openairdocs.org/sdr/2023FA0000806.md): Gcu · defective · Dec 2, 2023 · N4LG · Raythn B300RAYTHEON · AC Generator-Alternator
  > DC GENERATOR KICKED OFFLINE CAUSING BUS TIE TO TRIP AND LOSE OF PRESSURIZATION. REPLACED GENERATOR CONTROL UNIT, ADJUSTED PER MM. AIRCRAFT RETURNED TO SERVICE.
- [SDR 2020FA0000012](https://openairdocs.org/sdr/2020FA0000012.md): Turbine Blades · failed · May 24, 2019 · N8522Y · Airtrc AT802A · Turbine Section
  > ON MAY 24TH 2019 A SECOND STAGE POWER TURBINE BLADE FAILED PN 3044183-01. WHEN THE BLADE PORTION LEFT THE 2ND STAGE POWER TURBINE DISK PN 3037313 IT DESTROYED THE NEXT 5 BLADES IN ROTATION OF THE BLADED DISK. THE SUBSEQUENT OUT OF BALANCE CONDITION DESTROYED
- [SDR 2018FA0000113](https://openairdocs.org/sdr/2018FA0000113.md): Autopilot Sys · malfunctioned · Mar 22, 2018 · N700MM · Epic EPICLT · Autopilot System
  > AIRCRAFT EXPERIENCED A FAILURE OF THE PITCH TRIM ACTUATION IN FLIGHT AFTER THE AUTOPILOT AUTO TRIMMED THE PITCH TO A FULL NOSE DOWN POSITION.
- [SDR ESMR2016031131116](https://openairdocs.org/sdr/ESMR2016031131116.md): Transducer · erratic · Mar 10, 2016 · N401SM · Pilats PC1245 · Central Display
  > ACFT LINED UP FOR TAKEOFF. AFTER SETTING POWER AT 43 PSI TORQUE, A STANDARD TAKEOFF OCCURRED. AT APPROXIMATELY 300 FT AGL, THE MASTER CAUTION ILLUMINATED AND SAW THE TORQUE GAUGE SURGING BACK AND FORTH FROM 35-51 PSI, ABOVE MAX LIMITATIONS, WITHOUT ANYONE TO
- [SDR CA150716003](https://openairdocs.org/sdr/CA150716003.md): Support · damaged · Jul 12, 2015 · Airtrc AT802A · Wheel/Ski/Float
  > (CAN) BATHTUB FITTING FOUND IN FLOAT DURING PRECAUTIONARY INSPECTION, AFT FLOAT SUPPORT. HOLE ELONGATION NOTED IN RT FLOAT.
- [SDR CA150519021](https://openairdocs.org/sdr/CA150519021.md): Probe · loose · May 13, 2015 · Airtrc AT802A · Nacelle/Pylon, Bulkhead/Firewall
  > (CAN) ASYMMETRIC SCOOP INDICATION, LT DOWN STOP FOUND LOOSE. CHECKED, RETIGHTENED, SYS FUNCTIONS NORMALLY.
- [SDR CA150518004](https://openairdocs.org/sdr/CA150518004.md): Engine · malfunctioned · Apr 24, 2015 · Airtrc AT802A · Engine (Turbine/Turboprop)
  > (CAN) WHILE PERFORMING FIREFIGHTING OPERATIONS, THE PILOT REDUCED POWER TO 3000 FT/LB AND ENGINE ROLLED BACK DOWN TO 1000-1200 FT/LB INSTEAD. ENGINE LEVER PUSHED FORWARD TO 90 PERCENT AND THE ENGINE RESPONDED WELL. DID NOT REOCCUR AFTER, COULD NOT BE REPRODU
- [SDR CA141218005](https://openairdocs.org/sdr/CA141218005.md): Engine · power loss · Dec 5, 2014 · Enstrm F28A · Engine (Turbine/Turboprop)
  > (CAN) AFTER NORMAL APPROACH TO LAND, THE TORQUE DROPPED UN-COMMANDED FROM 3400LBS TO 2600LBS, THEN BACK UP AGAIN UN-COMMANDED. OTHER ENGINE PARAMETERS FOLLOWED.
- [SDR CA140910008](https://openairdocs.org/sdr/CA140910008.md): Control System · frozen · Aug 27, 2014 · Pilats PC1247 · Aileron Control System
  > (CAN) FLIGHT LEVEL 27,000 FT,OAT -45.THE AUTO PILOT DIS- ENGAGED AT THIS TIME THE PILOT TOOK CONTROL OF THE AIRCRAFT AND FOUND THE AILERON CONTROLS WERE FROZEN. THE PILOT DESENDED TO 15,000 FEET AT THIS POINT THE CONTROLS STARTED TO FREE UP AND AS THE AIRCRA
- [SDR UTUR2014FA0000399](https://openairdocs.org/sdr/UTUR2014FA0000399.md): Washer · misinstalled · Jun 11, 2014 · Turbine Engine Compressor Section
  > KEY WASHERS, THAT RETAINED COMPRESSOR BALANCE WEIGHTS WERE NOT BENT TO SECURE WEIGHTS. RETAINING RING THAT SECURE NR 1 BEARING OUTER HOUSINGTO NR 1 BEARING INNER HOUSING WAS MISSING, UNINSTALLED.
- [SDR UTUR2014FA0000400](https://openairdocs.org/sdr/UTUR2014FA0000400.md): Retaining Ring · missing · Jun 11, 2014 · Turbine Engine Compressor Section
  > KEY WASHERS THAT RETAIN COMPRESSOR BALANCE WEIGHTS WERE NOT BENT TO SECURE WEIGHTS. RETAINING RING THAT SECURE NR 1 BEARING OUTER HOUSING TO NR 1 BEARING INNER HOUSING WAS MISSING, UNINSTALLED.
- [SDR CA120620003](https://openairdocs.org/sdr/CA120620003.md): Indicator · fluctuates · May 5, 2012 · Airtrc AT802A · Engine BMEP/Torque Indicating
  > (CAN) TORQUE GAUGE FLUCTUATED. GAUGE REPLACED & CHECKED SERVICEABLE.
- [SDR CA120104004](https://openairdocs.org/sdr/CA120104004.md): Rib · cracked · Jan 4, 2012 · Airtrc AT802 · Trailing Edge Flaps
  > (CAN) CRACK IN RT FLAP L/E AND RIB AT FLAP BS 132.
- [SDR CA110613008](https://openairdocs.org/sdr/CA110613008.md): Motor · intermittent · Jun 8, 2011 · Airtrc AT802A · Trailing Edge Flap Control System
  > (CAN) FLAPS WOULD NOT RETRACT. DEAD SPOT IN FLAP MOTOR CAUSES INTERMITTENT OPERATION. THIS IS A RECURRING DEFECT IN THESE MOTORS. EXPERIENCED THE SAME SNAG LAST YEAR (2010).
- [SDR CA110607010](https://openairdocs.org/sdr/CA110607010.md): Frame · cracked · Jun 6, 2011 · Airtrc AT802A · Fuselage Main, Frame
  > CRACK FOUND UPPER DIAGONAL TUBE IN AFT FUSELAGE WHILE DOING SL 266 ON THIS TUBE NOTE: THIS ACFT IN MOUNTED ON WIPAIR FLOATS.
- [SDR CA110607011](https://openairdocs.org/sdr/CA110607011.md): Tube · cracked · Jun 6, 2011 · Airtrc AT802A · Fuselage Main, Frame
  > CRACK FOUND UPPER DIAGONAL TUBE IN AFT FUSELAGE WHILE DOING SL266 ON THIS TUBE. NOTE: THIS ACFT IN MOUNTED ON FLOATS.
- [SDR CA110321008](https://openairdocs.org/sdr/CA110321008.md): Rivet · damaged · Mar 21, 2011 · Airtrc AT802A · Wheel/Ski/Float
  > (CAN) RIGHT FLOAT FOAM TANK COMPARTMENT WAS FOUND TO HAVE NUMEROUS SHEARED OR WORKING RIVETS IN THE INBD LIP SEAL.
- [SDR CA101007006](https://openairdocs.org/sdr/CA101007006.md): Seal · leaking · Oct 4, 2010 · Airtrc AT802A · Wheel/Ski/Float
  > INBD MAIN WHEEL SEALS ON FLOATS LEAK EXCESSIVE AMOUNTS OF GREASE. IF GREASE IS NOT REMOVED FREQUENTLY IT CAN LEAK ON TO BRAKES CAUSING A FIRE. GREASE IS LEAKING FROM BETWEEN M/W HUB AND SEAL DUE TO A LOOSE FIT. UPON FURTHER INVESTIGATION, ALL AMPHIB FLOATS F
- [SDR CA100930002](https://openairdocs.org/sdr/CA100930002.md): Control Cable · damaged · Sep 27, 2010 · Airtrc AT802A · Wheel/Ski/Float
  > WATER RUDDER RETRACT CABLES BECOME SPIKED WITHIN 100 HRS OF NEW INSTALL, WHERE CABLE RESTS ON NYLON PULLEY AT FLOAT AFT BULKHEAD. CABLE PIN, CABLE-RUDDER RETRACT (2) 10A08000-166.
- [SDR CA100930003](https://openairdocs.org/sdr/CA100930003.md): Roll Pin · misinstalled · Sep 27, 2010 · Airtrc AT802A · Ailerons
  > SERVERAL OF THE LARGE DIAMETER HOLLOW FLIGHT CONTROL PUSH TUBES HAVE THEIR ROD ENDS HELD ON WITH ROLL PINS. THESE ROLL PINS SHOULD BE LOCKWIRED AROUND THE TUBE TO PREVENT THE ROLL PIN FROM FALLING OUT IF IT GETS LOOSE.
- [SDR CA100923009](https://openairdocs.org/sdr/CA100923009.md): Screw · wrong part · Sep 9, 2010 · Airtrc AT802A · Emergency Equipment
  > WHILE CARRYING OUT THE INSTALLATION OF THE AIR BAG SYS INTO ACFT, THE 2 LAP BELT INFLATOR TUBES BECAME DAMAGED DUE TO CHAFING/CATCHING ON SCREWS USED IN THE INSTALLATION. THE DAMAGE WAS NOT BEYOND LIMITS AS LISTED IN THE AIR BAG SICA. THE PROBLEM STEMS FROM
- [SDR CA101006003](https://openairdocs.org/sdr/CA101006003.md): Turbine Blades · failed · Aug 8, 2010 · Turbine Section
  > (CAN) IFSD (SINGLE ENGINE) DURING T/O ROLL, A LOUD NOISE WAS HEARD, THE PROPELLER SEIZED AND FLAMES CAME OUT OF THE EXHAUST. THE T/O WAS ABORTED AND THE ACFT STOPPED SAFELY ON THE STRIP. THE ENGINE WAS REMOVED AND FORWARDED FOR REPAIRS WHERE FRACTURED 2ND ST
- [SDR CA100729005](https://openairdocs.org/sdr/CA100729005.md): Proximity Switch · loose · Jul 25, 2010 · Airtrc AT802A · Landing Gear Position and Warning
  > DURING LANDING, PILOT OBSERVED NO RT NLG DOWN LIGHT INDICATION. FOUND RT NLG DOWN SWITCH HAD COME LOOSE AND SWITCH ROTATED AWAY FROM MAGNETIC PICKUP BUILT INTO RAM ASSY.
- [SDR CA100702004](https://openairdocs.org/sdr/CA100702004.md): Seal · leaking · Jun 22, 2010 · Propeller Assembly
  > IFSD (SINGLE ENGINE) DURING A TEST FLIGHT FOLLOWING ENGINE MAINTENANCE, A LOSS OF OIL PRESSURE OCCURRED AND OIL APPEARED ON THE WINDSHIELD. THE ENGINE WAS SHUT DOWN AND A SAFE DEAD STICK LANDING WAS ACCOMPLISHED. THE ENGINE WAS REMOVED AND SENT TO THE SHOP W
- [SDR CA100615002](https://openairdocs.org/sdr/CA100615002.md): Bolt · failed · Jun 10, 2010 · Turbine Engine Reduction Gear
  > ENGINE WAS REMOVED, SUBSEQUENT TO POWER SECTION CHIP DETECTOR FLAG ILLUMINATION DURING FLIGHT. AFTER FLIGHT CHECK, PILOT FOUND THAT PROPELLER WAS DIFFICULT TO TURN MANUALLY. THE CHIP DETECTOR AND MAIN OIL FILTER WAS NOTED FULL OF METAL DEBRIS. DURING DISMAN
- [SDR CA100604005](https://openairdocs.org/sdr/CA100604005.md): Wire · shorted · Jun 3, 2010 · Airtrc AT802A · Electrical Power System Wiring
  > PILOT REPORTED THAT THE FOAM SYS C/B KEPT POPPING FROM TIME TO TIME. INVESTIGATE FOUND THAT THE WIRING TO THE FOAM C/B WAS COMING FROM THE PROTECTED SIDE OF THE AUTO PILOT C/B. THE WIRING WAS CORRECTED TO STOP EITHER C/B FROM POPPING.
- [SDR CA100604004](https://openairdocs.org/sdr/CA100604004.md): Relay · miswired · May 28, 2010 · Airtrc AT802A · Flight Control System Wiring
  > FLAPS BECAME INTERMITTENT AT ANY POSITION AND SELECTING UP OR DOWN. FLAP MOTOR FOUND TO HAVE DEAD SPOTS ON ARMATURE. WHILE INVESTIGATING FLAP SNAG, IT WAS FOUND THAT THE FLAP UP AND DOWN RELAYS NORMALLY CLOSED AND OPEN CONTACTS WERE OPPOSITE AS SHOWN IN WIRI
- [SDR CA091207003](https://openairdocs.org/sdr/CA091207003.md): Switch · shorted · Dec 4, 2009 · Airtrc AT802A · Control Column Section
  > (CAN) THERE IS A POSSIBILITY OF A SHORT CIRCUIT OF WIRING IN THE STICK GRIP ASSY. IF THE AIP DISC SWITCH IS INSTALLED AT A CERTAIN ANGLE AND THE TERMINALS ARE LEFT TOO LONG, IT CAN CONTACT THE PTT SWITCH AND CAUSE THE GRIP TO GET QUITE HOT. THIS HAPPENED AND
- [SDR CA090902002](https://openairdocs.org/sdr/CA090902002.md): Mount Bracket · cracked · Aug 30, 2009 · Airtrc AT802A · Horizontal Stabilizer Structure
  > FWD INBD MOUNTING BRACKET CRACKED AND SEPARATED FROM AUX FINLET ASSY.
- [SDR CA090820009](https://openairdocs.org/sdr/CA090820009.md): Pump · leaking · Aug 19, 2009 · Airtrc AT802A · Engine Fuel Pump
  > (CAN) ENGINE DRIVEN PUMP LEAKING BY DRIVE SEAL, THIS FILLED ENVIRO CAN TO OVERFLOWING CAUSING FUEL ODOR IN COCKPIT. (TC 20090820009)
- [SDR CA090806004](https://openairdocs.org/sdr/CA090806004.md): Bearing · destroyed · Aug 3, 2009 · Airtrc AT802 · Wheel/Ski/Float
  > UPON LANDING THE PILOT HEARD A BANG AND NOTICED THE TAIL WHEEL TO BE VERY ROUGH AND LOOSE. LT WHEEL BRG AND RACES FOUND DESTROYED, ALL ROLLERS WERE MISSING. WHEEL ASSY AND AXLE WERE REPLACED.
- [SDR CA090723009](https://openairdocs.org/sdr/CA090723009.md): Stud · broken · Jul 22, 2009 · Airtrc AT802A · Trailing Edge Flaps
  > (CAN) FLAP MOTOR MOUNTING STUD SHEARED.
- [SDR CA090604002](https://openairdocs.org/sdr/CA090604002.md): Indicator · inoperative · May 30, 2009 · Airtrc AT802A · Fuel Quantity Indicator
  > (CAN) ACFT WAS LOW ON FUEL AND GIVING INCORRECT FUEL INDICATION. PILOT ATTEMPTED TO BALANCE THE FUEL LOAD ON THE GAUGES CAUSING THE RT WING TO EMPTY AND CAUSE A FLAME-OUT. THUS FORCING A LANDING ON THE HIGHWAY.
- [SDR CA090501006](https://openairdocs.org/sdr/CA090501006.md): Wire · burned · Apr 28, 2009 · Airtrc AT802 · Flight Control System Wiring
  > (CAN) THE AILERON TRIM TAB POWER WIRE THAT RUNS BEHIND THE CIRCUIT BREAKER PANEL BURNED AND WENT UP IN SMOKE WHILE PERFORMING UNRELATED MX IN THE HANGAR. WIRE WAS REPLACED AND TRIM TAB SYS CHECKS SERVICEABLE.
- [SDR CA090828004](https://openairdocs.org/sdr/CA090828004.md): Spacer · mismanufactured · Apr 24, 2009 · Fuel Controlling System
  > APPROX 5 MINUTES AFTER TAKEOFF ENGINE FLAMED OUT AND THE ACFT WAS FORCED TO DITCH. SUBSEQUENT INVESTIGATION REVEALED FCU DISTRESS ASSOCIATED WITH A BRG SPACER MFG ERROR.
- [SDR CA081031004](https://openairdocs.org/sdr/CA081031004.md): Roll Pin · missing · Oct 31, 2008 · Airtrc AT802A · Aileron Control System
  > (CAN) LT WING AILERON PUSHROD ASSY FOUND TO BE MISSING ONE ROLL PIN THAT RETAINS THE INBD END ROD END BEARING. THIS IS A DEFECT FROM THE FACTORY (INSIDE OF HOLE IS PAINTED). ALL OTHER ROD ENDS INSPECTED NO OTHER DEFECTS FOUND, ARROW SHOWS MISSING PIN HOLE.
- [SDR CA080723003](https://openairdocs.org/sdr/CA080723003.md): Sealant · failed · Jul 18, 2008 · Airtrc AT802 · Propeller Blade Section
  > (CAN) DURING CLIMB OUT PILOT EXPERIENCED A BUILD UP OF GREASE ON WINDSHIELD. PILOT ABORTED LOAD IN DESIGNATED AREA AND RETURNED TO BASE. UPON INSP GREASE APPEARED TO BE COMING FROM 1 OR 2 BLADE CLAMPS. BLADE CLAMP SEALS WERE REPLACED IN BOTH UNITS. NO OBVIOUS
- [SDR CA080414006](https://openairdocs.org/sdr/CA080414006.md): Static Line · deteriorated · Apr 7, 2008 · Airtrc AT802A · Autopilot System
  > DURING RE-ACTIVATION OF THE AIRCRAFT, THE MAINTENANCE CREW NOTICED THAT THE STATIC LINE FOR THE AUTO PILOT ALTITUDE HOLD P/N 0807-1 WAS DETERIORATED AND CRACKED. THE LINE WAS REPLACED WITH A SERVICEABLE PART. ALL OTHER AIRCRAFT IN THE FLEET WILL BE INSPECTED
- [SDR CA080128004](https://openairdocs.org/sdr/CA080128004.md): Control Cable · stuck · Jan 28, 2008 · Airtrc AT802A · Rudder Control System
  > (CAN) DURING INSP, THE LT RUDDER CABLE WAS FOUND SNAGGED ON THE WATER RUDDER CABLE PULLEY GUARD. (TC NR 20080128004)
- [SDR DATA200700010](https://openairdocs.org/sdr/DATA200700010.md): Line · broken · Nov 27, 2007 · N136LR · Stbros SD360300 · Fuel Controlling System
  > ENGINE FAILED APPROX 15 MILES SSW OF NEW HOPE VA. LEFT ENGINE INSTRUMENTS DECREASING. INFORMED FO TO CONFIRM LEFT ENGINE FAILURE. COMPLETED PROCEDURE ACCORDING TO ACC SOP. DECLARED EMERGENCY AND ADVISED ATC. CLEARED TO LAND ON ILS 35L. LANDED SAFELY NO F
- [SDR CA071203004](https://openairdocs.org/sdr/CA071203004.md): Spring · cracked · Nov 1, 2007 · Airtrc AT802A · Horizontal Stabilizer Miscellaneous Structure
  > (CAN) CRACK FOUND ON TAIL SPRING BEGINNING FROM FWD ATTACH HOLE EXTENDING ALONG SIDE OF SPRING. CRACK THEN EXTENDS TO TOP OF SPRING. LENGTH OF CRACK TOTALS APPROX 6 INCHES. (TC NR 20071203004)
- [SDR CA071204002](https://openairdocs.org/sdr/CA071204002.md): Circuit Breaker · cracked · Nov 1, 2007 · Airtrc AT802A · AC Power Distribution System
  > (CAN) CB CRACKED. (TC NR 20071204002)
- [SDR CA071204003](https://openairdocs.org/sdr/CA071204003.md): Nut · broken · Nov 1, 2007 · Airtrc AT802A · Fuselage Miscellaneous Structure
  > (CAN) THE VACUUM SWITCH WAS SUPPLIED BY MFG. PLASTIC ADJUSTING NUT SPLIT, PREVENTING THE VACUUM SWITCH FROM INDICATING A LOW FUEL PRESSURE WARNING. (TC NR 20071204003)
- [SDR CA070830001](https://openairdocs.org/sdr/CA070830001.md): Bolt · broken · Aug 27, 2007 · Airtrc AT802A · Fuselage Miscellaneous Structure
  > (CAN) RETARDANT WAS DISCOVERED LEAKING FROM AROUND THE TANK DOORS. UPON INVESTIGATION, IT WAS NOTED THAT THE BOLT SECURING THE ANGLE INSIDE THE RT DISPERSAL GATE ASSY WAS BROKEN. THE BOLT WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (TC NR 2007083000
- [SDR CA070618003](https://openairdocs.org/sdr/CA070618003.md): Actuator · failed · Jun 16, 2007 · Airtrc AT802A · Trailing Edge Flap Actuator
  > (CAN) DURING APPROACH FOR A SCOOPING OPERATION, THE FLAPS WOULD NOT EXTEND WITH AN AIR LOAD. THE AIRCRAFT RETURNED TO BASE. UPON INVESTIGATION BY MAINTENANCE STAFF, FLAPS WOULD EXTEND THE FIRST 10 DEGREES WITH NO AIR LOAD AND THE ACTUATOR MADE A GRINDING NO
- [SDR CA070803005](https://openairdocs.org/sdr/CA070803005.md): Turbine Blades · fractured · May 30, 2007 · Airtrc AT802A · Turbine Section
  > (CAN) THE ENGINE LOST POWER ON TAKEOFF ROLL AND THE TAKEOFF WAS ABORTED. SUBSEQUENT INSPECTION REVEALED FRACTUED POWER TURBINE BLADES AND A DISCONNECTION BETWEEN THE POWER TURBINE AND PROP. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLI
- [SDR CA070514051](https://openairdocs.org/sdr/CA070514051.md): Engine · flamed out · Apr 18, 2007 · Airtrc AT802 · Engine (Turbine/Turboprop)
  > (CAN) THE ENGINE FLAMED OUT IN FLIGHT. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070514051)
- [SDR SWD2007F00002](https://openairdocs.org/sdr/SWD2007F00002.md): Gas Generator · eroded · Mar 19, 2007 · N805D · Airtrc AT802A · Engine (Turbine/Turboprop)
  > AS THE HEAD BOLTS WERE BEING REMOVED FOR HSI. ONE NUT DETACHED FROM THE BOLT SHANK WITH THE THREAD INSIDE THE NUT. CLOSE INSPECTION OF THE ADJACENT BOLT REVEALED SEVERE EROSION (NOT CORROSION OR STRETCH DAMAGE) TO THE BOLT SHANK. IT WAS FURTHER NOTED AND PH
- [SDR CA070316002](https://openairdocs.org/sdr/CA070316002.md): Line · broken · Mar 16, 2007 · Airtrc AT802 · Pneumatic Distribution System
  > (CAN) DURING ANNUAL INSPECTION, THE BLEED AIR LINE FOR THE CABIN HEATER WAS FOUND UNSECURED UNDER THE COCKPIT FLOOR. FURTHER INVESTIGATION FOUND THE MUFFLER FOR THE LINE BROKEN IN (2) PIECES AT THE FWD END. THE PARTS WERE REPLACED. THE REMAINING AIRCRAFT IN TH
- [SDR CA070313008](https://openairdocs.org/sdr/CA070313008.md): Fitting · chafed · Mar 13, 2007 · Airtrc AT802 · Compressor Bleed Control
  > (CAN) UPON INSPECTION OF THE P3 AIR LINES, IT WAS DISCOVERED THAT THERE WAS NO CLEARANCE BETWEEN THE P3 FILTER HOUSING NIPPLE FITTING (P/N 3024606) AND THE ENGINE REAR FIRE SEAL PLATES (P/N 3031003 AND 3031004). UPON REPOSITIONING OF THE FIRE SEAL PLATES, IT

Next page: https://openairdocs.org/engine/pratt-whitney-canada-pt6a-67a/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 = 'PT6A67A'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/pratt-whitney-canada-pt6a-67a/reports

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