# Service difficulty reports: Pratt & Whitney Canada PW207D

A list on [Pratt & Whitney Canada PW207D](https://openairdocs.org/engine/pratt-whitney-canada-pw207d.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 133 reports

- [SDR 8LFA202609260005](https://openairdocs.org/sdr/8LFA202609260005.md): Heater · dirty · Sep 24, 2026 · N432LF · Bell 429 · Heating System
  > AIRCRAFT HEATER EMITTED A WHITE HAZE INTO THE CABIN WHEN TURNED ON. FURTHER INVESTIGATION DISCOVERED THAT THE HEATER HAD NOT BEEN USED DURING RECENT SUMMER MONTHS. THIS HAD BEEN THE FIRST ACTIVATION OF THE AIRCRAFT HEATER OF THE FALL SEASON. HEATING SYSTEM
- [SDR 8LFA202506170002](https://openairdocs.org/sdr/8LFA202506170002.md): Cap · broken · Jun 16, 2025 · N429LF · Bell 429 · Vertical Stabilizer
  > DURING POST FLIGHT PILOT WALK AROUND, NOTED UPPER CAP OF VERTICAL STABILIZER DEPARTED IN FLIGHT. EXPOSED WIRING WAS VISIBLE.
- [SDR QMLA2024080520096](https://openairdocs.org/sdr/QMLA2024080520096.md): Display · damaged · Aug 5, 2024 · N911NM · Bell 429 · Central Display
  > PILOT WRITE UP, DURING CRUISE FLIGHT L MFD (DU) DIMMED AND COULD NOT BE ADJUSTED BRIGHTER. ALSO AN ACRID SMELL WAS NOTABLE IN A/C. NO WARNING LIGHTS ILLUMINATED. AT BASE REMOVED DISPLAY UNIT FROM INSTRUMENT PANEL AND INSPECTED WIRES FOR ANY TYPE OF DAMAGE OR
- [SDR QMLA2022120520083](https://openairdocs.org/sdr/QMLA2022120520083.md): Actuator · damaged · Dec 1, 2022 · N911KX · Bell 429 · Hydraulic System, Main
  > ACTUATOR CONTROL TUBE END FITTING WORKING & RIVETS ATTACHING END FITTING WORKING, FOUND DURING 12 MO INSPECTION.
- [SDR CA190429022](https://openairdocs.org/sdr/CA190429022.md): Engine · making metal · Apr 25, 2019 · Bell 429 · Engine (Turbine/Turboprop)
  > (CAN) ENGINE CHIP LIGHT ILLUMINATED, FOLLOWING FLIGHT AME EXAMINED CHIP PLUG AND FOUND METAL BEYOND LIMITS ON MAGNETIC PLUG. (TC# 20190429022)
- [SDR CA190425011](https://openairdocs.org/sdr/CA190425011.md): Engine · making metal · Apr 4, 2019 · Bell 429 · Engine (Turbine/Turboprop)
  > (CAN) ON ENGINE START CHIP LIGHT ILLUMINATED, CHIP PLUG AND OIL FILTER FOUND TO CONTAIN UNACCEPTABLE AMOUNT OF METAL CONTAMINATION. (TC# 20190425011)
- [SDR CA190222008](https://openairdocs.org/sdr/CA190222008.md): Hub · damaged · Feb 18, 2019 · Bell 429 · Tail Rotor Head
  > (CAN) IT WAS REPORTED BY BELL: (FLIGHT SAFETY REPORT). AIRCRAFT COMES IN FOR RECONFIGURATION. AT DAILY INSPECTION, EXCESSIVE GAP WAS FOUND BETWEEN HUB AND BLADE ASSEMBLY. (NO TORQUE, HAND-TIGHT). NUT WAS DUE FOR RE-TORQUING AT 200HRS INSPECTION AND SHIP WAS 18
- [SDR 2018FA0000465](https://openairdocs.org/sdr/2018FA0000465.md): Compressor · coked · Aug 9, 2018 · N713NG · Bell 429 · Turbine Engine Compressor Section
  > DURING ENGINE POWER ASSURANCE CHECK A 15 DEGREE DROP IN MGT MARGIN TREND WAS NOTED. REPEATED PERFORMANCE RECOVERY WASHES PROVIDED ONLY A VERY SLIGHT INCREASE IN MARGIN. BORESCOPE INSPECTION OF COMPRESSOR SECTION REVEALED A BUILDUP OF COOKED ON OIL ON IMPELLE
- [SDR 2018FA0000467](https://openairdocs.org/sdr/2018FA0000467.md): Compressor · coked · Aug 9, 2018 · N713NG · Bell 429 · Turbine Engine Compressor Section
  > DURING ENGINE POWER ASSURANCE CHECK A 15 DEGREE DROP IN MGT MARGIN TREND WAS NOTED. REPEATED PERFORMANCE RECOVERY WASHES PROVIDED ONLY A VERY SLIGHT INCREASE IN MARGIN. BORESCOPE INSPECTION OF COMPRESSOR SECTION REVEALED A BUILDUP OF COOKED ON OIL ON IMPELLE
- [SDR 2018FA0000468](https://openairdocs.org/sdr/2018FA0000468.md): Compressor · coked · Aug 9, 2018 · N713NG · Bell 429 · Turbine Engine Compressor Section
  > DURING ENGINE POWER ASSURANCE CHECK A 15 DEGREE DROP IN MGT MARGIN TREND WAS NOTED. REPEATED PERFORMANCE RECOVERY WASHES PROVIDED ONLY A VERY SLIGHT INCREASE IN MARGIN. BORESCOPE INSPECTION OF COMPRESSOR SECTION REVEALED A BUILDUP OF COOKED ON OIL ON IMPELLE
- [SDR CA180706011](https://openairdocs.org/sdr/CA180706011.md): Gearbox · loose · Jul 3, 2018 · Bell 429 · Tail Rotor Gearbox
  > (CAN) THE FOLLOWING WAS REPORTED TO BELL: UPON UNSCHEDULED INSPECTION OF THE TAILROTOR GEARBOX BY RECOMMENDATION OF BELL CSR, THE OPERATOR DISCOVERED PLAY BETWEEN THE TAILROTOR GEARBOX AND THE TAIL BOOM. THE AIRCRAFT HAS APPROXIMATELY 1400 FLIGHT HOURS LOGGED
- [SDR CA180510009](https://openairdocs.org/sdr/CA180510009.md): Bracket · cracked · May 10, 2018 · Bell 429 · Tail Rotor Drive System
  > (CAN) DURING VISUAL INSPECTION, THE BRACKET P/N: 429-035-704-125, WHICH IS THE NUT PLATE HOLDER OF THE ATTACHMENT OF THE LOWER PART OF THE TAIL ROTOR GEARBOX COVER FAIRING, WAS FOUND CRACKED ON THE ENTIRE PORTION OF THE TOP LEG OF THE BRACKET. (TC# 2018051000
- [SDR CA180510012](https://openairdocs.org/sdr/CA180510012.md): Wire Harness · failed · May 10, 2018 · Bell 429 · Engine Indicating System Wiring
  > (CAN) FAILED INSULATION CHECK 77-21-00 PARA C. (TC# 20180510012)
- [SDR B1HR2018021500001](https://openairdocs.org/sdr/B1HR2018021500001.md): Insert · backed out · Feb 16, 2018 · N9CR · Bell 429 · Humidity Control System
  > INSERTS SECURING THE CONDENSER BLOWER MOTOR TO THE FAN HOUSING ARE BACKING OUT. THERE ARE 3 FASTENERS SECURING THE MOTOR TO THE FAN HOUSING, WE HAD ONE INSERT BACK OUT WHILE PERFORMING AIR COMM'S SERVICE BULLETIN 429-201-1. AD2017-05-51 HAS BEEN ISSUE DEALING
- [SDR QMLA2016082516097](https://openairdocs.org/sdr/QMLA2016082516097.md): Firewall · cracked · Aug 25, 2016 · N862NC · Bell 429 · Fuselage Main, Bulkhead
  > DURING AIRWORTHINESS CHECK, FOUND THE FORWARD CENTER ENGINE FIREWALL PANEL CRACKED IN 2 PLACES, FROM THE BOTTOM AND FROM A LOWER STIFFENER SOLID RIVET. THIS ACFT REMAINS OUT OF SERVICE AT THE TIME OF THIS SUBMISSION AWAITING A REPLACEMENT FIREWALL OR REPAIR.
- [SDR QMLA2016071816075](https://openairdocs.org/sdr/QMLA2016071816075.md): Access Panel · cracked · Jul 18, 2016 · N862NC · Bell 429 · Fuselage Main, Bulkhead
  > DURING AIRWORTHINESS CHECK, FOUND THE AFT ENGINE FIREWALL ACCESS PANEL CRACKED AROUND THE BOTTOM 2 FASTENERS. THIS ACFT REMAINS OUT OF SERVICE AT THE TIME OF THIS SUBMISSION AWAITING A REPLACEMENT FIREWALL FROM MFG.
- [SDR QMLA2016041916041](https://openairdocs.org/sdr/QMLA2016041916041.md): Unknown · odor · Apr 19, 2016 · N861NC · Bell 429 · Air Distribution System
  > DURING TRAINING FLIGHT CREW NOTICED EXHAUST SMELL IN CABIN. THE SMELL CLEARED ITSELF ON THE LEG BACK TO BASE. MX ARRIVED TO INSPECT THE ACFT & COULD NOT IDENTIFY THE SOURCE OF THE SMELL. THE ACFT WAS THEN RELEASED BACK TO SERVICE.
- [SDR CA160217001](https://openairdocs.org/sdr/CA160217001.md): Spring · debonded · Feb 15, 2016 · Bell 429 · Main Rotor Transmission Mount
  > (CAN) DEBONDING BETWEEN INNER MEMBER AND OUTER MEMBER OF ASSY. THE PITCH RESTRAINT SPRING ASSY DID HAVE AN ASB 429-13-10 ON 29 APRIL 2013 ON A LIMITED QUANTITY OF UNITS THAT WERE MANUFACTURED WITH INADEQUATE ADHESIVE MIX RATIO BETWEEN THE TUBE AND THE HOUSING
- [SDR CA160217004](https://openairdocs.org/sdr/CA160217004.md): Spring · debonded · Feb 15, 2016 · Bell 429 · Main Rotor Transmission Mount
  > (CAN) DEBONDING BETWEEN INNER MEMBER AND OUTER MEMBER OF ASSY. THE PITCH RESTRAINT SPRING ASSY DID HAVE AN ASB 429-13-10 ON 29 APRIL 2013 ON A LIMITED QUANTITY OF UNITS THAT WERE MFG WITH INADEQUATE ADHESIVE MIX RATIO BETWEEN THE TUBE AND THE HOUSING. THIS CO
- [SDR CA160215011](https://openairdocs.org/sdr/CA160215011.md): Spring · debonded · Feb 13, 2016 · Bell 429 · Main Rotor Transmission Mount
  > (CAN) DEBONDING BETWEEN INNER MEMBER AND OUTER MEMBER OF ASSY. THE PITCH RESTRAINT SPRING ASSY DID HAVE AN ASB 429-13-10 ON 29 APRIL 2013 ON A LIMITED QTY OF UNITS THAT WERE MANUFACTURED WITH INADEQUATE ADHESIVE MIX RATIO BETWEEN THE TUBE AND THE HOUSING. THI
- [SDR CA160215012](https://openairdocs.org/sdr/CA160215012.md): Spring · debonded · Feb 13, 2016 · Bell 429 · Main Rotor Transmission Mount
  > (CAN) DEBONDING BETWEEN INNER MEMBER AND OUTER MEMBER OF ASSY. THE PITCH RESTRAINT SPRING ASSY DID HAVE AN ASB 429-13-10 ON 29 APRIL 2013 ON A LIMITED QTY OF UNITS THAT WERE MFG WITH INADEQUATE ADHESIVE MIX RATIO BETWEEN THE TUBE AND THE HOUSING. THIS CONDITI
- [SDR CA160212001](https://openairdocs.org/sdr/CA160212001.md): Restraint · unknown · Feb 8, 2016 · Bell 429 · Main Rotor Transmission Mount
  > (CAN) DURING FLIGHT, A "BANG" HAS BEEN HEARD BY BOTH CREW. NO LOST OF FLIGHT OR ENGINE CONTROLS HAS BEEN NOTICED, NO ABNORMAL VIBRATIONS OBSERVED AND NO INDICATION OF ANY PROBLEMS FROM SYS ON DISPLAY UNITS. NO OTHERS OBSERVATIONS FOR THE REST OF FLIGHT AND LA
- [SDR CA160215018](https://openairdocs.org/sdr/CA160215018.md): Slide · failed · Feb 2, 2016 · Bell 429 · Flight Compartment Equipment
  > (CAN) GLARE SHIELD EXTENSION SLIDE CAME APART IN FLIGHT DROPPING THE BEARINGS IN THE COCKPIT.
- [SDR CA160125017](https://openairdocs.org/sdr/CA160125017.md): Spring · debonded · Jan 21, 2016 · Bell 429 · Main Rotor Transmission Mount
  > (CAN) PILOTS NOTED AN INCREASE IN VIBRATION AND A DEGRADE OF RIDE. ALSO TRANSMISSION STOP CONTACT WAS HEARD. THE HELICOPTER LANDED AND REMAINED AT LOCATION. THE CUSTOMER`S MAINTENANCE REPORT FINDING BOTH FORWARD AND AFT PITCH RESTRAINT SPRINGS DEBONDED.
- [SDR CA160128004](https://openairdocs.org/sdr/CA160128004.md): Spring · debonded · Jan 21, 2016 · Bell 429 · Main Rotor Transmission Mount
  > (CAN) PILOT REPORTED A VIBRATION, ABNORMAL AND "SHIFTING" FELT IN HOVER AND DURING FLIGHT. A PRECAUTIONARY LANDING WAS CARRIED OUT. PILOTS OBSERVED THAT THE TRANSMISSION WAS RESTING ON "PIN BACK-UP MOUNTS". AN AME WAS DISPATCHED TO INSPECT THE ACFT, A FLIGH
- [SDR CA160128005](https://openairdocs.org/sdr/CA160128005.md): Spring · failed · Jan 21, 2016 · Bell 429 · Main Rotor Transmission Mount
  > (CAN) PILOT REPORTED A VIBRATION (ABNORMAL) AND "SHIFTING" FELT IN HOVER AND DURING FLIGHT. A PRECAUTIONARY LANDING WAS CARRIED OUT. PILOTS OBSERVED THAT THE TRANSMISSION WAS RESTING ON "PIN BACK-UP MOUNTS". AN AME WAS DISPATCHED TO INSPECT THE ACFT, A FLIGHT
- [SDR CA160125015](https://openairdocs.org/sdr/CA160125015.md): Display · failed · Jan 13, 2016 · Bell 429 · Central Display
  > (CAN) THE FOLLOWING HAS BEEN REPORTED TO MFG: THE LT DU WENT BLANK DURING FLIGHT WITH ASSOCIATED CAS MESSAGE AND A BURNING ODOR, BUT NO SMOKE. THE ACFT LANDED SAFELY AT THE BASE, AND FAULT WAS CONFIRMED TO BE THE DU.
- [SDR CA160108001](https://openairdocs.org/sdr/CA160108001.md): Bracket · cracked · Jan 6, 2016 · Bell 429 · Fuselage Miscellaneous Structure
  > (CAN) ALUMINUM PANEL REFERRED TO AS A BRACKET HAS CRACKS STARTING AT THE ANTENNA MOUNTING HOLE WHICH IS ALSO USED AS THE GROUNDING POINT FOR THE ANTENNA. IF LT UNDETECTED THE ELT ANTENNA MOUNTED TO THIS PANEL COULD DEPART THE ACFT.
- [SDR CA160108002](https://openairdocs.org/sdr/CA160108002.md): Bracket · cracked · Jan 6, 2016 · Bell 429 · Fuselage Miscellaneous Structure
  > (CAN) ALUMINUM PANEL REFERRED TO AS A BRACKET HAS CRACKS STARTING AT THE ANTENNA MOUNTING HOLE WHICH IS ALSO USED AS THE GROUNDING POINT FOR THE ANTENNA. IF LEFT UNDETECTED THE ELT ANTENNA MOUNTED TO THIS PANEL COULD DEPART THE ACFT.
- [SDR CA160108003](https://openairdocs.org/sdr/CA160108003.md): Bracket · cracked · Jan 6, 2016 · Bell 429 · Fuselage Miscellaneous Structure
  > (CAN) ALUMINUM PANEL REFERRED TO AS A BRACKET HAS CRACKS STARTING AT THE ANTENNA MOUNTING HOLE WHICH IS ALSO USED AS THE GROUNDING POINT FOR THE ANTENNA. IF LEFT UNDETECTED THE ELT ANTENNA MOUNTED TO THIS PANEL COULD DEPART THE ACFT.
- [SDR CA160125013](https://openairdocs.org/sdr/CA160125013.md): Brake · malfunctioned · Dec 20, 2015 · Bell 429 · Landing Gear Brake System
  > (CAN) THE FOLLOWING HAS BEEN REPORTED TO MFG: FOLLOWING A NORMAL START AND RUN UP TO 100 PERCENT NR, THE PARKING BRAKE HANDLE WAS THEN RELEASED BY PLACING PRESSURE ON THE TOE BRAKES AND PUSHING THE BRAKE HANDLE DOWN. NO CAS MESSAGES ILLUMINATED PRIOR TO OR D
- [SDR CA151031008](https://openairdocs.org/sdr/CA151031008.md): Shroud · cracked · Oct 30, 2015 · Engine Fuel Distribution
  > (CAN) THE ACFT MADE A SAFE LANDING ON THE RUNWAY AT THE LOCAL AIRPORT AFTER AN ENGINE IN-FLIGHT SHUTDOWN. THE LOWER SHROUD ON THE FMM CRACKED AROUND ONE OF THE HIGH PRESSURE FUEL FITTINGS WHICH GOES INTO THE BOTTOM OF THE FMM. THE WEIGHT OF THE FUEL HOSE AND
- [SDR CA160111006](https://openairdocs.org/sdr/CA160111006.md): Fuel Sys · malfunctioned · Oct 30, 2015 · Bell 427 · Fuel Controlling System
  > (CAN) AT ALTITUDE OF 500FT, SPEED 120KTS AND TORQUE 85 PERCENT THE PILOT EXPERIENCED A YAW TO THE RT. SAW AN INDICATION OF NR 1 ENGINE FAILED. FOLLOWED THE EMERGENCY PROCEDURE, FLEW ABOUT 13 MINUTES WITH 1 OPERATING ENGINE, ENG 2, AND LANDED SAFELY AT THE NE
- [SDR CA160119005](https://openairdocs.org/sdr/CA160119005.md): Shroud · cracked · Oct 30, 2015 · Bell 427 · Aircraft Fuel Distribution System
  > (CAN) THE FOLLOWING HAS BEEN REPORTED TO MFG: IN-FLIGHT SHUTDOWN OF A ENGINE. THE ACFT MADE A SAFE LANDING ON THE RUNWAY AT THE LOCAL AIRPORT AND NO ADDITIONAL DAMAGE WAS DONE TO THE ACFT OR PERSONNEL. FROM WHAT THEY HAVE SO FAR DETERMINED, THE LOWER SHROUD
- [SDR CA150925002](https://openairdocs.org/sdr/CA150925002.md): Engine · malfunctioned · Sep 9, 2015 · Bell 429 · Engine (Turbine/Turboprop)
  > (CAN) THE OPERATOR REPORTED AN AIR TURN BACK DUE TO HIGH ITT, LT ENGINE ON TAKEOFF, ITT ROSE TO JUST SHORT OF RED LINE, LATER DECREASED WITH REDUCED POWER.
- [SDR CA150914008](https://openairdocs.org/sdr/CA150914008.md): Bearing · separated · Aug 31, 2015 · Bell 429 · Main Rotor Head
  > (CAN) ELASTOMERIC MATERIAL SEPARATED FROM PARENT METAL.
- [SDR CA150914009](https://openairdocs.org/sdr/CA150914009.md): Bypass Valve · cracked · Aug 31, 2015 · Bell 429 · Engine Oil Temperature Regulator
  > (CAN) PILOT REPORTED HIGHER THAN NORMAL ENGINE OIL TEMPERATURE. BYPASS VALVE REMOVED FOR INSPECTION AND FOUND TO BE CRACKED.
- [SDR CA150828001](https://openairdocs.org/sdr/CA150828001.md): Engine · power loss · Aug 14, 2015 · Bell 429 · Engine (Turbine/Turboprop)
  > (CAN) ON APPROACH TO LANDING THE PILOT DETECTED A FAULT IN THE ROTOR AND BEGAN AN EMERGENCY LANDING. THERE WAS A REPORTED POWER LOSS AND THE AIRCRAFT FELL FROM A HEIGHT OF 5 METERS.
- [SDR CA150623007](https://openairdocs.org/sdr/CA150623007.md): Clamp · loose · Jun 23, 2015 · Bell 429 · Landing Gear Position and Warning
  > (CAN) CLAMP DOES NOT PROVIDE SUFFICIENT CLAMPING FORCE TO PREVENT WOG SWITCH BRACKET FROM MOVING, CREATING A CONDITION OF OUT OF CALIBRATION. REPRESENTATIVES HAVE BEEN INFORMED.
- [SDR CA150616002](https://openairdocs.org/sdr/CA150616002.md): Bearing · rotated · Jun 16, 2015 · Bell 429 · Rotorcraft Flight Control
  > (CAN) BEARING WAS NOTICED TO BE ROTATING INSIDE HOUSING. PART WAS REMOVED & FOUND THAT BEARING WAS IMPROPERLY STAKED. PART WAS REPLACED WITH NEW PART.
- [SDR CA150615009](https://openairdocs.org/sdr/CA150615009.md): Mast · corroded · Jun 12, 2015 · Bell 429 · Main Rotor Mast/Swashplate
  > (CAN) THE FOLLOWING HAS BEEN REPORTED. MAST CORROSION FOUND DURING A SCHEDULED MAST INSPECTION. AFTER REMOVING THE MAST NUT, WATER WAS NOTED AROUND THE MAST NUT AREA. WHEN THE HUB WAS LIFTED WATER WAS NOTED RUNNING OUT.
- [SDR CA150615012](https://openairdocs.org/sdr/CA150615012.md): Mast · corroded · Jun 1, 2015 · Bell 429 · Main Rotor Mast/Swashplate
  > (CAN) THE FOLLOWING HAS BEEN REPORTED. MAIN ROTOR HUB WAS REMOVED DURING ROUTINE MX & WATER WAS FOUND IN THE MAIN ROTOR HUB TO MAST JOINT AREA. FURTHER INSPECTION REVEALED PITTING IN THE AREA ON THE MAST LOWER CONE SEAT AREA. MAST & MAST ADAPTER ASSEMBLY PN
- [SDR CA150501002](https://openairdocs.org/sdr/CA150501002.md): Bearing · worn · Apr 28, 2015 · Bell 429 · Tail Rotor Head
  > (CAN) DURING ROUTINE INSPECTION, EXCESS PLAY OBSERVED IN TAIL ROTOR PITCH LINK. ATTACHED VIDEO SHOWS THE PRESENT CONDITION.
- [SDR CA150408012](https://openairdocs.org/sdr/CA150408012.md): Engine · flamed out · Mar 30, 2015 · Engine (Turbine/Turboprop)
  > (CAN) DURING FLIGHT THE ENGINE HAD A FLAMEOUT JUST BEFORE TOUCHDOWN, AT ABOUT 10 FEET FROM THE GROUND. MFG WILL INVESTIGATE TO ESTABLISH ROOT CAUSE & PROVIDE INFORMATION THROUGH SUBSEQUENT SERVICE DIFFICULTY REVIEW MEETING & SUPPORTING DOCUMENTS OR OTHER AGRE
- [SDR CA150310004](https://openairdocs.org/sdr/CA150310004.md): Warning Light · illuminated · Feb 23, 2015 · Bell 429 · Landing Gear Retraction/Extension System
  > (CAN) DURING FLIGHT, PILOT ONBOARD HAS ADVISED THEY HAVE THE LANDING GEAR MAINTENANCE & WOG MAINTENANCE CAS LIGHTS ILLUMINATED AND THAT THE LANDING GEAR DOES NOT COME ALL THE WAY UP.
- [SDR CA150429012](https://openairdocs.org/sdr/CA150429012.md): Bearing · damaged · Feb 4, 2015 · Bell 429 · Main Rotor Control
  > (CAN) PILOT REPORTED INTERMITTENT COLLECTIVE CONTROL RESTRICTIONS AT VARIOUS POWER SETTINGS THROUGHOUT THE COLLECTIVE CONTROL RANGE. ENGINEER REPORTED THE PROBLEM WAS BEING CAUSED BY MOISTURE INGRESS AND THEREBY LOSS OF LUBRICATION TO THE BEARINGS, PN MS2764
- [SDR CA150204007](https://openairdocs.org/sdr/CA150204007.md): Landing Gear · damaged · Jan 27, 2015 · Bell 429 · Nose/Tail Landing Gear
  > (CAN) DURING TROUBLESHOOTING TO DETERMINE CAUSE OF PREVIOUSLY REPORTED NOSE WHEEL UNSAFE CAUTION WITH GEAR IN THE DOWN POSITION, THE 2 BOLTS SECURING THE OVER-CENTERING DRIVE LINK WERE FOUND TO BE BENT, THE LINK ITSELF, AND THE LARGE AREA WASHER, PN NAS1149C04
- [SDR CA150204012](https://openairdocs.org/sdr/CA150204012.md): Bearing · dislodged · Jan 27, 2015 · Bell 429 · Tail Rotor Head
  > (CAN) DURING PREFLIGHT, PILOT NOTICED BEARING DISLODGED FROM LINK. PILOT STATES THE LINK WAS NOT LIKE THAT THE PREVIOUS DAY DURING PREFLIGHT.
- [SDR CA150113029](https://openairdocs.org/sdr/CA150113029.md): Landing Gear · collapsed · Jan 11, 2015 · Bell 429 · Nose/Tail Landing Gear
  > (CAN) ON APPROACH TO LAND, THE NOSE GEAR INDICATED UNSAFE AFTER GEAR LOWERING. A/C WAS BROUGHT TO A HOVER AND THE MECHANIC CONFIRMED GEAR APPEARED SAFE. A/C WAS LANDED AND TAXIED TO PARKING. FURTHER INSPECTION WAS CONDUCTED BY THE MECH AND ALL SEEMED NORMAL.
- [SDR CA141201004](https://openairdocs.org/sdr/CA141201004.md): Control Cable · cracked · Nov 19, 2014 · Bell 429 · Turbine Engine System Wiring
  > (CAN) NR 2 ENGINE IS BEING REPLACED DUE TO OIL PRESSURE ISSUES IN FIGHT. ENGINEER FOUND CRACKED CABLE N1 ON THE CONNECTION TO PLA.

Next page: https://openairdocs.org/engine/pratt-whitney-canada-pw207d/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 = 'PW207D'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/pratt-whitney-canada-pw207d/reports

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