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

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

Newest first. General aviation reporting is voluntary.

Page 1 of 37 · 1,812 reports

- [SDR TIMA20250603003](https://openairdocs.org/sdr/TIMA20250603003.md): Engine · power loss · Jun 3, 2025 · N247GL · Beech 1900D · Engine (Turbine/Turboprop)
  > AFTER LEVELING OFF AT 14000' LEFT FUEL PRESSURE ANNUNCIATION CAME ON, STNADBY PUMP TURNED ON, FUEL PRESSURE ANNUMC REMAINED ON, FLOW DROPPED, ENGINE ROLLED BACK. PUSHED PROPS/POWER UP, LEFT ENGINE REMINED ROLLED BACK (11%) N1. SHUTDOWN ENGINE CUTOFF, FEATHERED
- [SDR TIMA2024071105007](https://openairdocs.org/sdr/TIMA2024071105007.md): Engine · power loss · Jul 5, 2024 · N184UX · Beech 1900D · Engine (Turbine/Turboprop)
  > AFTER DESCENDING AND LEVELING OFF LEFT ENGINE TORQUE NOT RISISNG PROPERLY AND INCORRECT ENGINE CONTROL/FEEL, PILOT NOTICED IMPROPER PWOER OUT OF LEFT ENGINE AND DECLARED EMERGENCY DUE TO PARITAL POWER ON LEFT ENGINE. PILOT WAS CLEARED TO LAND. LANDED SAFELY AN
- [SDR TIMA20240705007](https://openairdocs.org/sdr/TIMA20240705007.md): Engine · low torque · Jul 5, 2024 · N169GL · Beech 1900D · Engine (Turbine/Turboprop)
  > AFTER DESCENDING AND LEVELING OFF LEFT ENGINE TORQUE NOT RISING PROPERLY AND INCORRECT ENGINE CONTROL / FEEL, PILOT NOTICED IMPROPER POWER OUT OF LEFT ENGINE AND DECLARED EMERGENCY DUE TO PARITIAL POWER ON LEFT ENGINE. PILOT WAS CLEARD TO LAND. LANDED SAFELY A
- [SDR CA190621007](https://openairdocs.org/sdr/CA190621007.md): Torque Tube · cracked · Jun 20, 2019 · Beech 1900D · Rudder Control System
  > (CAN) DURING HEAVY CHECK 3RD PARTY MRO IDENTIFED RUDDER TORQUE SHAFT LOOSE AND A CIRCUMFERENTIAL CRACK.
- [SDR CA190513002](https://openairdocs.org/sdr/CA190513002.md): Pressure Switch · leaking · May 11, 2019 · Beech 1900D · Engine Oil Pressure
  > (CAN) AFTER DEPARTING OUT OF XXX WE HAD THE #2 ENGINE BOUNCING BETWEEN 4000-2500 TORQUE, AT 400 FEET WE BROUGHT POWER BACK TO CLIMB POWER AND THE TORQUE WAS STEADY, SO WE THOUGHT IT WAS JUST THE GAUGE. WHEN WE WERE CRUISING TO XXX AT 4500 FEET WE HAD A LOW OIL
- [SDR CA190501023](https://openairdocs.org/sdr/CA190501023.md): Screw · damaged · May 1, 2019 · Beech 1900D · Main Landing Gear
  > (CAN) UPON APPROCH INTO XXXX, FLIGHT CREW OF C-XXXX ATTEMPTED TO SELECT GEAR DOWN. `LANDING GEAR CONTROL` CIRCUIT BREAKER FOUND TO BE `POPPED`. BREAKER RESET & DOWN SELECTION RE-SELECTED. POSITIVE DOWN LOCK INDICATION FOR BOTH MAINS ACHIEVED, NEGATIVE INDICATI
- [SDR CA190415001](https://openairdocs.org/sdr/CA190415001.md): Governor · weak · Apr 13, 2019 · Beech 1900D · Propeller Governor
  > (CAN) LEFT ENGINE AUTO FEATHER ENGAGED ON APPROACH PILOT REPORTED PROP FEATHERED FOR ABOUT 3 SEC WHEN POWER WAS REDUCED BEFORE SELECTING FLAP 35. IT CAUSED THE PLANE TO YAW QUITE A BIT CORRECTION P/N OS GOVERNOR 210961C (TC# 20190415001)
- [SDR CA190403020](https://openairdocs.org/sdr/CA190403020.md): Pushrod · worn · Apr 3, 2019 · Beech 1900D · Power Lever
  > (CAN) DURING INSPECTION IT WAS DISCOVERED THAT THERE WAS WEAR ON THE RH POWER LEVER PEDESTAL PUSH ROD. IT WAS DETERMINED TO ORIGINATE FROM INTERFERENCE WITH THE LH PROPELLER CONTROL. AFTER CONSULTATION WITH BEECHCRAFT IT WAS FOUND THAT THE DIAGRAM SHOWING INST
- [SDR CA181015014](https://openairdocs.org/sdr/CA181015014.md): Buss Bar · corroded · Oct 12, 2018 · Beech 1900D · Electrical Power System Wiring
  > (CAN) DURING TROUBLE SHOOTING FOUND OUT THAT BUS BAR WAS CORRODED AND NOT MAKING PROPER CONTACTS WHEN GPU IS ATTACHED. BUS BAR WAS REPLACED ALONG WITH RECEPTACLE FOR FIX. SYSTEM CHECKED SERVICEABLE AND AIRCRAFT WAS RELEASED FOR SERVICE. (TC# 20181015014)
- [SDR CA180707001](https://openairdocs.org/sdr/CA180707001.md): Transducer · disconnected · Jul 4, 2018 · Beech 1900D · Brake Anti-Skid Section
  > (CAN) ATTACH SCREWS P/N MS24693-S24 BECAME FREE OF WHEEL SPEED TRANSDUCER P/N 140-04715. TRANSDUCER WAS ABLE TO SHIFT INSIDE THE AXLE ALLOWING FOR THE TRANSDUCER TO LOOSE WHEEL SPEED INPUT, DUE TO SEPARATION FROM DRIVE HUBCAP P/N 114-810055-3. ONLY INDICATIO
- [SDR CA180222015](https://openairdocs.org/sdr/CA180222015.md): Landing Gear · damaged · Feb 16, 2018 · Beech 1900D · Nose/Tail Landing Gear
  > (CAN) DURING PUSH BACK IN YUL, DUE TO ICY CONDITION NOSE STEERING EXCEEDED NOSE GEAR STEERING LIMIT AND DAMAGE TO STEERING BUNGEE, SHIMMY DAMPER, GUIDE AND ALIGNMENT BRACKET. ALL THE DAMAGED PARTS HAVE BEEN REPLACED INCLUDING NOSE GEAR ASSEMBLY FOR FIX. (TC
- [SDR GLBA2016042500583](https://openairdocs.org/sdr/GLBA2016042500583.md): Pcb · faulty · Apr 24, 2016 · N231YV · Beech 1900D · Propeller Feathering/Reversing
  > PILOT REPORTED THAT THE AUTOFEATHER ARMED WITH N1 ABOUT 95%, AFX DISABLE ILLUMINATED & RT AUTOFEATHER FAILED TO ARM. REPLACED PCB A123, PN ON & OFF 129-364091-9, SN OFF 446C95, SN ON 925I94, IAW AIM 10-24-01. VERIFIED RIGGING OF ARMING SWITCHES IAW MM 61-21-
- [SDR GLBA2016041400580](https://openairdocs.org/sdr/GLBA2016041400580.md): Unknown · malfunctioned · Apr 14, 2016 · N153GL · Beech 1900D · Propeller Feathering/Reversing
  > PILOT REPORTED THAT THEY HAD UNSCHEDULED AUTOFEATHER CYCLING ON FINAL. PERFORMED AUTOFEATHER OPERATIONAL CHECKS & COULD NOT DUPLICATE DISCREPANCY SIGNED OFF USING REF 1900DMM 61-21-00. OPERATIONS CHECKED GOOD.
- [SDR GLBA2016040800579](https://openairdocs.org/sdr/GLBA2016040800579.md): Autofeather Sys · unknown · Apr 5, 2016 · N254GL · Beech 1900D · Propeller Feathering/Reversing
  > PILOT REPORTED THAT THE LT ENG AUTO FEATHER CYCLED SEVERAL TIMES ON APPROACH. COMPLIED WITH FCD 1900-08-61-01, NO DEFECTS NOTED.
- [SDR CA160229004](https://openairdocs.org/sdr/CA160229004.md): Hose · leaking · Feb 26, 2016 · Beech 1900D · Hydraulic System, Main
  > (CAN) ON APPROACH WITH GEAR SELECTED TO THE DOWN POSITION THE CREW NOTICED THERE WERE NO THREE GREEN OR RED GEAR HANDLE LIGHTS ILLUMINATED. THE GEAR WAS CYCLED A SECOND TIME WITH THE SAME RESULT. THE GEAR RELAY POPPED. THE CREW USED THE MANUAL GEAR EXTENSION P
- [SDR CA160209004](https://openairdocs.org/sdr/CA160209004.md): Angle · cracked · Feb 4, 2016 · Beech 1900D · Fuselage Miscellaneous Structure
  > (CAN) DURING A STRUCTURAL INSPECTION MAINTENANCE FOUND THE RH CLOSING ANGLE CRACKED 1.5 INCHES RFS 303. CLOSING ANGLE CRACK WAS REPAIRED IAW CAS ENGINEERING EA B1900-53-011, RDA-A-RA16-009/D. ORIGINAL SRM CLOSING ANGLE REPAIR REMOVED AND AN EXTENDED REPAIR A
- [SDR CA160202006](https://openairdocs.org/sdr/CA160202006.md): Line · melted · Feb 2, 2016 · Beech 1900D · Ice Detection
  > (CAN) DURING INSPECTION FOUND RT TAILET DE-ICE BOOT NOT INFLATING. HAD POSITIVE INDICATION, DE-ICE BOOT SHOULD BE INFLATED. FOUND DE-ICE LINE TO TAILET MELTED BY TAIL LOG LIGHT. WHEN DE-ICE LINE MELTED IT SEALED LINE COMPLETELY NOT ALLOWING PRESSURE SENSOR
- [SDR CA160203021](https://openairdocs.org/sdr/CA160203021.md): Connector · broken · Feb 1, 2016 · Beech 1900D · Landing Gear System Wiring
  > (CAN) ON DEPARTURE, THE CREW REPORTED THAT THE GEAR WOULD NOT RETRACT AFTER DEPARTURE WHEN THE HANDLE WAS SELECTED TO THE UP POSITION. 3 GREEN LIGHT EXTINGUISHED BUT THE RED LIGHT REMAINED ILLUMINATED IN THE HANDLE. THE GEAR HANDLE WAS SELECTED TO THE DOWN PO
- [SDR CA160202001](https://openairdocs.org/sdr/CA160202001.md): Actuator · cracked · Jan 25, 2016 · Beech 1900D · Landing Gear Actuator
  > (CAN) LEFT MLG END CAP INSPECTION CARRIED OUT INDICATION OF CRACK FOUND BY NDI. LEFT MLG ACTUATOR REPLACED.
- [SDR CA160118009](https://openairdocs.org/sdr/CA160118009.md): Switch · faulty · Jan 18, 2016 · Beech 1900D · Landing Gear Position and Warning
  > (CAN) MAINTENANCE WERE UNABLE TO SILENCE LANDING GEAR WARNING HORN ONCE ACTIVATED. TROUBLESHOOTING REVEALED THAT THE RT MLG SWITCH ASSY, A108 WAS AT FAULT. THE SWITCH ASSLY WAS REPLACED. SUCCESSFUL GEAR SWINGS WERE CARRIED OUT AND SYS FUNCTION TESTED SERVICEA
- [SDR CA160118013](https://openairdocs.org/sdr/CA160118013.md): Spar Cap · corroded · Jan 15, 2016 · Beech 1900D · Horizontal Stabilizer, Spar/Rib
  > (CAN) DURING PLATE NUT INSPECTION AT OTBD LT HORIZONTAL STABILIZER, CORROSION WAS FOUND ON LOWER SPAR CAP AT PLATE NUTS AND 2 FASTENERS JUST INBD OF CENTER ELEVATOR HINGE ARM. AFTER INSPECTION CORROSION WAS FOUND ON LOWER OTBD AND UPPER CENTER SPAR CAPS. REP
- [SDR CA160120010](https://openairdocs.org/sdr/CA160120010.md): Truss · cracked · Jan 14, 2016 · Beech 1900D · Engine Mount Section
  > (CAN) DURING A H-CHECK NDT INSPECTION OF AN ENGINE MOUNT IAW MFG RECOMMENDATIONS A SUSPECT CRACK WAS INDICATED IN 1 OF THE WELDED AREAS. THE SUBJECT ENGINE TRUSS WAS REMOVED AND SENT TO AN APPROVED VENDOR FOR REPAIR. DURING THE INSPECTION/REPAIR PHASE THE V
- [SDR CA160118004](https://openairdocs.org/sdr/CA160118004.md): Actuator · worn · Jan 7, 2016 · Beech 1900D · Trailing Edge Flap Actuator
  > (CAN) DURING A DAILY INSPECTION, THE RT FLAP WAS FOUND TO HAVE EXCESSIVE PLAY. UPON INSPECTION FOUND INBD FLAP ACTUATOR HAD EXCESSIVE END PLAY AND WAS REMOVED FOR REPAIR. DURING TEARDOWN IT WAS FOUND THAT THERE WERE INTERNAL INCORRECT PARTS. ACTUATOR REPAIRE
- [SDR CA160106007](https://openairdocs.org/sdr/CA160106007.md): Support Bracket · damaged · Jan 5, 2016 · Beech 1900D · Nacelle/Pylon Miscellaneous Structure
  > (CAN) GPU POWER PLUG AND STRUCTURAL SUPPORT BRACKET FOUND DAMAGED DURING LINE INSPECTION. GROUND POWER STRUCTURAL BASE BRACKET REPAIRED. REPAIR PORTION OF BRACKET MADE FROM NEW PART.
- [SDR CA160108008](https://openairdocs.org/sdr/CA160108008.md): Skin · damaged · Jan 4, 2016 · Beech 1900D · Wing, Plate/Skin
  > (CAN) LT AND RT L/E SKINS FOUND DAMAGED AT HSS 5.00. LY L/E SKIN AND DOUBLER AT HSS 5.00 REPAIRED. DAMAGE SKIN AND DOUBLER TRIMMED AWAY. SKIN INSERTION MADE FROM 2024-T3-.032. DOUBLER INSERTION FROM 2024-T3-.040. REPAIR REINFORCEMENT INNER DOUBLERS MADE F
- [SDR CA151229020](https://openairdocs.org/sdr/CA151229020.md): Spar Cap · cracked · Dec 27, 2015 · Beech 1900D · Wing Spar
  > (CAN) DURING COMPLETION OF AN I-CHECK AND AD2013-24-03, CRACKING IN VERTICAL STABILIZER. MAINTENANCE DISCOVERED THAT BOTH LT AND RT VERTICAL STABILIZER. SPAR CAPS WERE FOUND CRACKED AT UPPER HOLES. ALSO, BOTH HAT SECTIONS WERE ALSO CRACKED WHICH WILL BE MI
- [SDR CA151223007](https://openairdocs.org/sdr/CA151223007.md): Proximity Switch · out of adjust · Dec 20, 2015 · Beech 1900D · Landing Gear Position and Warning
  > (CAN) ON APPROACH CREW REPORTED RT MAIN GEAR WAS NOT INDICATING DOWN AND LOCKED WHEN IN THE AIR AND GEAR HANDLE IS IN THE DOWN POSITION. CHECKLIST PROCEDURES CARRIED OUT AND ACFT LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO INVESTIGATE THE ISSUE. T
- [SDR CA151221008](https://openairdocs.org/sdr/CA151221008.md): Uplock Switch · corroded · Dec 19, 2015 · Beech 1900D · Landing Gear Position and Warning
  > (CAN) CREW REPORTED LANDING GEAR INDICATION CIRCUIT BREAKER POPPED. LOST THREE (3) GREEN INDICATION. CREW FOLLOWED CHECKLIST, RESET CB, 3 GREEN INDICATION WAS EVIDENT AND ACFT LANDED WITHOUT INCIDENT. ACFT WAS INSPECTED BY MAINTENANCE AND IT WAS DISCOVERED T
- [SDR CA151218003](https://openairdocs.org/sdr/CA151218003.md): Display · malfunctioned · Dec 17, 2015 · Beech 1900D · Central Display
  > (CAN) ELECTRICAL BURNING ODOR WAS DETECTED DURING FLIGHT, ISAT SYS CONTROL PANEL WAS SUSPECTED THE SOURCE. ISAT CIRCUIT BREAKER PULLED. ISAT CONTROL HEAD INSPECTED AND FOUND BURNED INTERNALLY. CONTROL HEAD REPLACED, TEST FOUND SERVICEABLE.
- [SDR CA151221001](https://openairdocs.org/sdr/CA151221001.md): Keelbeam · cracked · Dec 17, 2015 · Beech 1900D · Fuselage Main, Keel
  > (CAN) INBD KEEL WEB FLANGE, PN: 114-980024 OF RT NACELLE FOUND CRACKED APPROXIMATELY 1.0 IN LENGTH. REPAIR CARRIED OUT. DAMAGED PORTION OF KEEL WEB FLANGE REMOVED 1.25. INSERTION PACKER AND REPAIR ANGLE MADE FROM 2024-T3, 0.063" ALUMINUM. ALL REPAIR MADE
- [SDR CA151207007](https://openairdocs.org/sdr/CA151207007.md): Packing · leaking · Dec 4, 2015 · Beech 1900D · Turbine Engine Oil System
  > (CAN) DURING REPLACEMENT OF AN ENGINE OIL FILTER MAINTENANCE FOUND A BATCH OF AS3209-224 RINGS, ENGINE OIL FILTER, THE ONE THAT GOES AROUND THE OUTSIDE OF THE FILTER, THAT ARE THE INCORRECT SIZE. THE CORRECT SIZE FOR AN AS3209-224 IS 1.75 ID AND 2 OD. LOT 150
- [SDR CA160208002](https://openairdocs.org/sdr/CA160208002.md): Gas Generator · damaged · Dec 4, 2015 · Turbine Section
  > (CAN) ENGINE WAS SENT TO O/H SHOP WITH THE OPERATOR REPORTING METAL IN OIL. DUE TO THE TSO OF THE POWER SECTION BEING 7597HRS, THE OPERATOR ELECTED TO REPAIR THE GAS GENERATOR MODULE AND O/H THE POWER SECTION. THIS REPORT IS ISSUED TO DISCUSS THE FINDINGS ASS
- [SDR CA151201011](https://openairdocs.org/sdr/CA151201011.md): Switch · out of adjust · Nov 30, 2015 · Beech 1900D · Door Warning System
  > (CAN) WHILE ENROUTE THE CREW NOTICED THE, CARGO DOOR, ANNUNCIATOR HAD ILLUMINATED. THE CREW ELECTED TO DIVERT TO AIRPORT AS MAINTENANCE PERSONNEL WERE AVAILABLE TO ASSESS THE SITUATION. THE ACFT LANDED WITHOUT INCIDENT. UPON INSPECTION MAINTENANCE FOUND THE A
- [SDR CA151130011](https://openairdocs.org/sdr/CA151130011.md): Switch · out of adjust · Nov 28, 2015 · Beech 1900D · Door Warning System
  > (CAN) ON A FLIGHT THE CREW NOTICED THE, CABIN DOOR, WARNING LIGHT WAS ILLUMINATED. THE CREW ELECTED TO RETURN TO THE AIRPORT AS MAINTENANCE WAS AVAILABLE AT THIS STATION. THE ACFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ACFT AND FOUND SWITCH, PN: M
- [SDR CA151202004](https://openairdocs.org/sdr/CA151202004.md): Engine · overtemp · Nov 27, 2015 · Beech 1900D · Engine (Turbine/Turboprop)
  > (CAN) ENGINE WAS SENT FOR REPAIR WITH THE OPERATOR REPORTING AN IN FLIGHT-SHUTDOWN IFSD, THE ENGINE TEMPERATURE CLIMBED BEYOND NORMAL OPERATING LEVELS. NO OVERTEMP EVENT WAS RECORDED. THE OPERATOR ALSO REPORTED FOD AND A GRINDING NOISE WHEN ROTATING THE COMP
- [SDR CA151210006](https://openairdocs.org/sdr/CA151210006.md): Stringer · corroded · Nov 24, 2015 · Beech 1900D · Wing, Longeron/Stringer
  > (CAN) DURING A SCHEDULED FUEL TANK INSPECTION UTILIZING X-RAY THE FOLLOWING DEFECTS WERE NOTED. LEFT LOWER STR CORRODED BETWEEN LT WING STA 114-124 AT 39.5 PERCENT CHORD. RT AFT FLANGE OF FWD WING SPAR CORRODED BETWEEN RT WING STA 114-124 -LT FUEL STRAINER B
- [SDR CA151125009](https://openairdocs.org/sdr/CA151125009.md): Duct · cracked · Nov 23, 2015 · Beech 1900D · Ice/Rain Protection System
  > (CAN) BRAKE DEICE WARNING ILLUMINATED IN FLIGHT. FOUND CRACK ON BLEED AIR DUCT 129-550067-1 CAUSING EVA TUBE TO MELT AND TRIGGER LIGHT.
- [SDR CA160106002](https://openairdocs.org/sdr/CA160106002.md): Switch · out of adjust · Nov 22, 2015 · Beech 1900D · Door Warning System
  > (CAN) CREW REPORTED A DOOR UNSAFE LIGHT ON DEPARTURE. THE CREW CANCELLED IFR AND RETURNED TO THE AIRPORT. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO INSPECT THE ACFT. AFTER INSPECTING THE ACFT THE CARGO DOOR SILL SWITCH WAS FOUND OUT O
- [SDR CA151116009](https://openairdocs.org/sdr/CA151116009.md): Frame · cracked · Nov 13, 2015 · Beech 1900D · Fuselage Main, Frame
  > (CAN) DURING STRUCTURAL INSPECTION A-CHECK ITEM 37, WHICH STATES AT FS 288 CHECK FOR STRESSED AND MISSING FASTENERS ON THE LOWER FUSELAGE BULKHEAD, PN 114-430094-13 OR -15. PERFORM AN NDI EDDY CURRENT CHECK ON SPECIFIC FASTENERS ON THE LT AND RT SIDE OF THE B
- [SDR CA151201010](https://openairdocs.org/sdr/CA151201010.md): Oil System · pressure loss · Nov 13, 2015 · Beech 1900D · Engine Oil Indicating System
  > (CAN) THE AIRCRAFT WAS ON A FLIGHT AND WAS DIVERTED DUE TO LOSS OF OIL PRESSURE. THE PILOT NOTICED THE OIL PRESSURE DROPPING OFF LINE AND THE TQ WAS FLUCTUATING. THE ENGINE AUTO FEATHERED ON ITS OWN AND THE PILOT SHUTDOWN THE ENGINE. THE ACFT DID AN UNEVENTFUL
- [SDR CA151120002](https://openairdocs.org/sdr/CA151120002.md): Oil System · low pressure · Nov 10, 2015 · Turbine Engine Oil System
  > (CAN) AIRCRAFT LOST OIL PRESSURE ON RT ENGINE IN CRUISE FLIGHT. AS A RESULT, AUTOFEATHER ENGAGED AND RT PROPELLER FEATHERED. CREW DECLARED EMERGENCY AND LANDED SAFELY.
- [SDR CA151106006](https://openairdocs.org/sdr/CA151106006.md): Actuator · binding · Nov 2, 2015 · Beech 1900D · Trailing Edge Flap Actuator
  > (CAN) AFTER LANDING THE FLIGHT CREW PERFORMED THE AFTER LANDING CHECKLIST AND SELECTED THE FLAPS TO FULL UP POSITION THEY NOTICED THAT THE INDICATOR STOP AT THE 15 DEGREE SETTING. AFTER PARKING THE ACFT THE FLIGHT CREW CHECKED THE FLAPS AND FOUND THEM AT OR L
- [SDR CA151121002](https://openairdocs.org/sdr/CA151121002.md): Wire Harness · burned · Nov 2, 2015 · Beech 1900D · Ice/Rain Protection System Wiring
  > (CAN) PILOT REPORTED LT PROPELLER HEAT AMPERAGE INDICATING "LOW". UPON FURTHER EXAMINATION/TROUBLESHOOTING, MAINTENANCE DISCOVERED THE PROP HEAT WIRING HARNESS HAD NO PROTECTIVE SHEATHING INSTALLED. WITH NO PROTECTIVE SHEATHING, THE WIRE RUBBED AGAINST THE S
- [SDR CA151103008](https://openairdocs.org/sdr/CA151103008.md): Angle · out of position · Nov 1, 2015 · Beech 1900D · Propeller Controlling System
  > (CAN) THE PILOT REPORTED THAT THE LT ENGINE WOULD ONLY STAY IN FEATHER IF THE PROP CONTROL LEVER IS HELD DOWN. IT WAS NOTED THAT THE AUTO FEATHER SYS TESTED SERVICEABLE. THE CLIP ITEM, NR 18 AS DEPICTED WAS INCORRECTLY POSITIONED ON THE FWD SIDE OF THE BRACK
- [SDR CA151102008](https://openairdocs.org/sdr/CA151102008.md): Shaft · sheared · Oct 31, 2015 · Beech 1900D · Elevator Tab Control System
  > (CAN) ELEVATOR TRIM ISSUE IN FLIGHT. TRIM ACTUATOR SHAFT FOUND SHEARED.
- [SDR CA151027001](https://openairdocs.org/sdr/CA151027001.md): Engine · power loss · Oct 25, 2015 · Beech 1900D · Engine (Turbine/Turboprop)
  > (CAN) FLIGHT CREW NOTICED LT BLEED FAIL DURING TAKEOFF, JUST AFTER, THE LT TORQUE DECREASED ALONG WITH THE LT PROP RPM. THE ITT STARTED TO INCREASE BEFORE THE CREW SHUTDOWN THE ENGINE. ACFT RETURNED BACK TO THE AIRPORT WITHOUT ANY FURTHER INCIDENT, THE ENGIN
- [SDR CA151031004](https://openairdocs.org/sdr/CA151031004.md): Gearbox · damaged · Oct 25, 2015 · Beech 1900D · Accessory Gearboxes
  > (CAN) ON THE CLIMBOUT THE CREW OBSERVED ABNORMAL TORQUE AND ITT INDICATIONS. AS A PRECAUTION, THE CREW ELECTED TO SHUTDOWN THE LT ENGINE. THE ACFT RETURNED WHERE AN UNEVENTFUL LANDING WAS CARRIED OUT. FLIGHT CREW REPORTED NOISE CAN BE HEARD COMING FROM THE A
- [SDR CA151019007](https://openairdocs.org/sdr/CA151019007.md): Line · cracked · Oct 19, 2015 · Beech 1900D · Pneumatic Distribution System
  > (CAN) LINE CRACKED AT FLARED AREA.
- [SDR CA151022010](https://openairdocs.org/sdr/CA151022010.md): Sensor · dirty · Oct 19, 2015 · Beech 1900D · Door Warning System
  > (CAN) AFTER TAKEOFF WHILE ENROUTE AND CLIMBING THROUGH 3500 ASL, THE CARGO DOOR LIGHT AND MASTER WARNING ILLUMINATED. A DECISION WAS MADE TO RETURN PROMPTLY SUSPECTING POSSIBILITY OF BEING MORE THAN JUST A FAULTY SENSOR. AFTER CONFERRING WITH ATC THE CREW REQ
- [SDR CA151016009](https://openairdocs.org/sdr/CA151016009.md): Line · cracked · Oct 15, 2015 · Beech 1900D · Pneumatic Distribution System
  > (CAN) BLEED AIR LINE CRACKED AND SEPARATED AROUND FLANGE AREA THAT MOUNTS TO LT ENGINE FIRE WALL CAUSING BLEED AIR FAIL INDICATION.

Next page: https://openairdocs.org/engine/pratt-whitney-canada-pt6a-67d/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 = 'PT6A67D'
ORDER BY difficulty_date DESC
```

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

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