# Service difficulty reports: Pratt & Whitney Canada PW206C

A list on [Pratt & Whitney Canada PW206C](https://openairdocs.org/engine/pratt-whitney-canada-pw206c.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 63 reports

- [SDR 2026FA0000821](https://openairdocs.org/sdr/2026FA0000821.md): Regulator Valve · faulted · Oct 6, 2026 · N57HR · Agusta AW109SP · Turbine Engine Oil System
  > HELICOPTER N57HR EXPERIENCED NR 1 OIL HOT LIGHT IN FLIGHT. PER RFM IT SAYS TO ACHIEVE SAFE OEI FLIGHT AND SHUT DOWN ENGINE USING EMERGENCY SHUTDOWN IN AN EMERGENCY. 3-73 AND 3-20 IN RFM. WHICH IS WHAT THE CREW DID.
- [SDR QMLA2024030620028](https://openairdocs.org/sdr/QMLA2024030620028.md): Unknown · odor · Mar 6, 2024 · N129AR · Agusta A109E · Air Distribution System
  > DURING SHIFT CHANGE CREW REPORTED HAVING SLIGHT FUEL SMELL IN AFT CABIN, PILOT DID NOT REPORT ANY FUEL ODOR IN COCKPIT.
- [SDR QMLA2024021920021](https://openairdocs.org/sdr/QMLA2024021920021.md): Bladder · deteriorated · Feb 19, 2024 · N7UC · Agusta A109E · Fuel Storage
  > SLIGHT ODOR OF FUEL SMELL REPORTED IN FLIGHT
- [SDR QMLA2023083120068](https://openairdocs.org/sdr/QMLA2023083120068.md): Door · unknown · Aug 31, 2023 · N365AA · Agusta A109 · Doors
  > LEFT REAR PASSENGER DOOR OPENED DURING CRUISE FLIGHT. AIRCRAFT WAS SLOWED DOWN TO 25 KTS IN ORDER FOR CREW MEMBER TO ATTEMPT TO CLOSE IT. HE WAS UNABLE TO SLIDE IT CLOSED, AND CONTINUED TO HOLD THE DOOR UNTIL A PRECAUTIONARY LANDING COULD BE MADE. ONCE LANDED
- [SDR U0GA202307072410](https://openairdocs.org/sdr/U0GA202307072410.md): Lock Nut · cracked · Jul 6, 2023 · N820FT · Agusta A109E · Main Rotor Control
  > WHILE PERFORMING THE POST FLIGHT CHECK IT WAS FOUND THAT THE SWASHPLATE SUPPORT WAS LOOSE AT ITS MOUNTING POINT. UPON FURTHER INSPECTION IT WAS FOUND THAT ALL 6 NUTS WERE WORN AT THE BASE AND 5 OF THE 6 WERE CRACKED. ALL NUTS WERE BACKED OFF APPROX.1.5 TURNS A
- [SDR U0GA ASR8638](https://openairdocs.org/sdr/U0GA%20ASR8638.md): None · none · Sep 9, 2022 · N334J · Agusta A109E · Engine Oil Indicating System
  > #1 OIL CHIP CAUTION LIGHT ILLUMINATED. ENGINE SHUT DOWN PER EMERGENCY CHECKLIST. CORRECTIVE ACTION: REPLACED AND FLUSHED #1 ENGINE OIL. INSPECTED #1 ENGINE CHIP DETECTOR, PREFORMED GROUND RUN AND LEAK CHECK OF #1 ENGINE. NO DISCREPANCIES NOTED.
- [SDR FDEA202206251561](https://openairdocs.org/sdr/FDEA202206251561.md): Engine · failed · Jun 25, 2022 · N997FD · Boeing 757230 · Engine Oil Indicating System
  > DURING CLIMBOUT L ENGINE OIL TEMPERATURE CLIMBED INTO THE AMBER BAND (167 DEGREES). ACCOMPLISHED QRH AND OIL TEMP REMAINED HIGH. SHUTDOWN ENGINE IAW WITH QRH INSTRUCTIONS AND LANDED SINGLE ENGINE WITHOUT ISSUE. EMERGENCY DECLARED. AFTER SHUTDOWN L ENG SEC
- [SDR QMLA2021040920018](https://openairdocs.org/sdr/QMLA2021040920018.md): Frame · cracked · Apr 6, 2021 · N129AR · Agusta A109E · Fuselage Main, Frame
  > DURING AIRFRAME A5450 INSPECTION, FOUND CRACKS IN STATION 4960 FRAME IN AFT BAGGAGE COMPARTMENT.
- [SDR HDNA2019111800381](https://openairdocs.org/sdr/HDNA2019111800381.md): Engine · cracked · Nov 18, 2019 · N914ET · Urocop EC135P1 · Engine (Turbine/Turboprop)
  > WHILE ON FINAL APPROX 200-250 FEET WHEN THE NUMBER 1 ENGINE CHIP AND OIL PRESSURE LIGHT CAME ON CONFORMATION OF THESE INDICATIONS CONFIRMED WITH OIL PRESSURE INDICATION AT 0 PSI. THE #1 ENGINE WAS SECURED, AN EMERGENCY WAS DECLARED WITH A RUN ON LANDING PERFOR
- [SDR QMLA2018101618113](https://openairdocs.org/sdr/QMLA2018101618113.md): Chip Detector · activated · Oct 16, 2018 · N951AL · Agusta A109E · Main Rotor Gearbox
  > XMSN OIL CHIP (YELLOW CAUTION LIGHT) ILLUMINATED IN FLIGHT. IN ACCORDANCE WITH THE RFM SUPPLEMENT PAGES, ATTEMPTED TO EXTINGUISH THE CAUTION LIGHT WITH MOMENTARY ACTIVATION OF THE "CHIP BURNER" SWITCH. CAUTION LIGHT REMAINED ILLUMINATED. IN ACCORDANCE WITH
- [SDR QMLA201808218098](https://openairdocs.org/sdr/QMLA201808218098.md): Vertical Gyro · inoperative · Aug 20, 2018 · N951AL · Agusta A109E · Attitude Gyro and Indicating System
  > AIRCRAFT BEGAN TO MAKE LEFT AND RIGHT UN-COMMANDED ROLL INPUTS. THE INPUTS INCREASED IN AMPLITUDE AND RATE OVER THE COURSE OF THE NEXT TWO MINUTES. NO AIRCRAFT CAUTION INDICATIONS CAME ON, ISOLATED THE INPUTS USING SAS SWITCHES, ONCE SAS 2 WAS SWITCHED OFF, T
- [SDR QMLA2017072317070](https://openairdocs.org/sdr/QMLA2017072317070.md): Blower · failed · Jul 23, 2017 · N127AM · Agusta A109E · Engine Oil Temperature Regulator
  > AFTER TAKE OFF DURING CLIMB OUT, THE NR 2 ENGINE OIL TEMP. ROSE TO 120 DEGREES. AND A HIGH OIL TEMP CAUTION LIGHT ILLUMINATED. PILOT STARTED DESCENT AND AFTER LANDING SHUT ENGINE DOWN AND TAXIED TO PARKING LOCATION WITH NO FURTHER DIFFICULTY.
- [SDR QMLA2017050817048](https://openairdocs.org/sdr/QMLA2017050817048.md): Support Frame · cracked · May 8, 2017 · N7UC · Agusta A109E · Fuselage Main, Structure
  > THE PILOTS AFT DOOR POST IS CRACKED AT JUNCTION WHERE THE POST ATTACHES TO THE FLOOR. THE CRACK STARTS ON THE INSIDE AND REACHES AROUND TO THE FRONT SIDE OF THE POST.
- [SDR JBZA201605310001](https://openairdocs.org/sdr/JBZA201605310001.md): Fire Warning · false activation · May 31, 2016 · N272SM · Agusta A109E · Fire Detection
  > WITHIN 5 MINUTES OF DEPARTURE, RECEIVED NR 1 ENGINE FIRE WARNING. DECLARED EMERGENCY AND BEGAN APPROPRIATE CHECKLIST. DUE TO CLOSE PROXIMITY TO AIRPORT COMPLETED CHECKLIST THROUGH ENGINE SHUTDOWN. REQUESTED AND RECEIVED NEGATIVE INDICATION OF ANY SIGNS OF F
- [SDR QMLA2015073115064](https://openairdocs.org/sdr/QMLA2015073115064.md): Shaft · sheared · Jul 31, 2015 · N127AM · Agusta A109E · Engine Oil Cooler
  > DISCOVERED DURING A SCHEDULED MAINTENANCE EVENT THE FOLLOWING DISCREPANCY. WHILE PERFORMING BULLETIN 109EP-1222 & AMC EO-06-6322-EO-452, 200 HOUR INSPECTION OF RIGHT SIDE OIL COOLER BLOWER FAN IMPELLER PLAY MEASUREMENT, HE FOUND THE PULLEY TO BE SLIPPING ON I
- [SDR JBZA20150710001](https://openairdocs.org/sdr/JBZA20150710001.md): Blade · broken · Jun 27, 2015 · N37RX · Urocop EC135P2 · Engine (Turbine/Turboprop)
  > AFTER PREFLIGHT PLANNING, ACFT DOCUMENT & AIRWORTHINESS INSPECTION & NORMAL STARTS, ACFT DEPARTED. AFTER UNEVENTFUL 1.6 HR FLIGHT, ACFT LANDED, TOOK ON 117 GALS JET A FROM FUEL TRUCK. AFTER APPROX 40 MINUTES, ANOTHER PREFLIGHT & UNEVENTFUL STARTS, DEPARTED P
- [SDR QMLA2015041415028](https://openairdocs.org/sdr/QMLA2015041415028.md): Grip · damaged · Apr 14, 2015 · N115GH · Agusta A109E · Main Rotor Head
  > AIRCRAFT LAST FLOWN, 35 MINUTE FERRY FLIGHT, MONDAY AFTERNOON, 4-13-15. ON TUESDAY APRIL 14TH 2015, AT APPROX 1000 HOURS, THE MECHANICS WERE PERFORMING AN AIRWORTHINESS CHECK ON THE AIRCRAFT, SN 11115. WHILE INSPECTING THE MAIN ROTOR AREA ON THE RT SIDE OF T
- [SDR CA150325003](https://openairdocs.org/sdr/CA150325003.md): Engine · overtorqued · Mar 4, 2015 · Engine (Turbine/Turboprop)
  > (CAN) ENGINE SUFFERED OVERTORQUE.
- [SDR CA150116002](https://openairdocs.org/sdr/CA150116002.md): Thrust Reverser · abnormal · Jan 12, 2015 · Cessna 680CE · Engine Thrust Reverser
  > (CAN) RT THRUST REVERSER LEVER WAS ACCELERATING THE ENGINE BEFORE THE THRUST REVERSER BUCKETS WERE DEPLOYED. DURING TROUBLE SHOOTING THE RH THRUST LEVER INTERLOCK SOLENOID IT WAS DISCOVERED THE ISSUE WAS THE MECHANICAL LOCK FOR THE LEVER. THE LOWER PIVOT POI
- [SDR IFJA2014110400001](https://openairdocs.org/sdr/IFJA2014110400001.md): Chip Detector · contaminated · Nov 2, 2014 · N508CF · Agusta A109E · Main Rotor Gearbox
  > DURING NORMAL CRUISE FLIGHT, THE PILOT RECEIVED A MAIN GEAR BOX CHIP LIGHT, PROCEEDED TO THE NEAREST AIRPORT WITH OUT INCIDENT. AFTER LANDING, THE MECH FOUND A FOUND A SMALL PIECE OF METAL ON THE CHIP DETECTOR, REMOVED THE PIECE OF METAL AND REINSTALLED THE
- [SDR CA141103011](https://openairdocs.org/sdr/CA141103011.md): Unknown · power loss · Oct 25, 2014 · Agusta A109E · Engine (Turbine/Turboprop)
  > (CAN) LOSS OF POWER, BOTH ENGINES, WHILE DESCENDING TO LAND AT HOSPITAL. AUTOROTATION INITIATED. POWER RESUMED AT 50` ABOVE HELIPAD, UNEVENTFUL LANDING. THIS IS THE SECOND OCCURRENCE ON THIS ACFT.
- [SDR K97A2014F00157](https://openairdocs.org/sdr/K97A2014F00157.md): Skin · cracked · Sep 23, 2014 · N102H · Agusta A109E · Rotorcraft Tail Boom
  > WHEN THE LEFT HORIZONTAL STABILIZER WAS REMOVED FOR ELECTRICAL TROUBLESHOOTING, 7 CRACKS IN THE SHEET METAL WERE FOUND ON THE INBD RIB AND FORE AND AFT SPARS WHERE THEY ATTACH TO THE INBD RIB. CRACKS CANNOT BE SEEN WITH THE STABILIZER INSTALLED. A TORQUE TUB
- [SDR 2A6R20140711001](https://openairdocs.org/sdr/2A6R20140711001.md): Combustion Liner · cracked · Jul 9, 2014 · N817LV · Urocop EC135P2 · Turbine Engine Combustion Section
  > DURING 800 HOUR BORESCOPE INSPECTION OF ENG CRACKS WERE FOUND IN THE COMBUSTION CHAMBER LINER ASSEMBLY. REPLACED LINER ASSEMBLY WITH A NEW ONE.
- [SDR 2A6R201407110002](https://openairdocs.org/sdr/2A6R201407110002.md): Combustion Liner · cracked · Jul 9, 2014 · N817LV · Urocop EC135P2 · Turbine Engine Combustion Section
  > DURING 800 HOUR BORESCOPE INSPECTION OF ENG CRACKS WERE FOUND IN THE COMBUSTION CHAMBER LINER ASSEMBLY. REPLACED LINER ASSEMBLY WITH A NEW ONE.
- [SDR QMLA2014060514064](https://openairdocs.org/sdr/QMLA2014060514064.md): Unknown · odor · Jun 5, 2014 · N539LN · Urocop EC135P2 · Air Distribution System
  > IN ROUTE, PILOT SMELLED WHAT HE THOUGHT WAS A STRONG URINE SMELL. HE ASKED THE CREW IF THE PATIENT HAD URINATED & THEY SAID HE HAD NOT. THE PILOT THEN DROPPED THE CREW & DEPARTED SOLO SHOOTING A PRACTICE ILS APPROACH & RETURNED TO PICK UP CREW. UPON RETURN
- [SDR CA140416001](https://openairdocs.org/sdr/CA140416001.md): Latch · worn · Apr 14, 2014 · Agusta A109S · Passenger/Crew Doors
  > (CAN) DURING APPROACH THE CABIN LT DOOR OPENED IN FLIGHT. THE CREW SLOWED THE ACFT DOWN AND CONTINUED WITH THE APPROACH AND LANDED SAFELY. MAINTENANCE REMOVED AND INSPECTED THE DOOR, THE DOOR SAFETY LATCHING MECHANISM WAS REPLACED, THE DOOR WAS ALSO RE-ADJUS
- [SDR CA140401014](https://openairdocs.org/sdr/CA140401014.md): Manifold · leaking · Mar 28, 2014 · Cessna C37 · Fuel Controlling System
  > (CAN) DURING CRUISE, THE ACFT EXPERIENCE A HARD ABRUPT YAW AND COCKPIT AVIONIC DISPLAY (CAD) DISPLAYED NR 2 ENGINE FAIL. THE PILOT SHUTDOWN AND SECURED THE ENGINE. DIVERTED AND LANDED WITH NO FURTHER INCIDENT. THE NR 2 FUEL MANIFOLD WAS FOUND TO BE LEAKING AT
- [SDR CA140314001](https://openairdocs.org/sdr/CA140314001.md): Engine · flamed out · Mar 3, 2014 · Engine (Turbine/Turboprop)
  > THE PILOT REPORTED THE NR 2 ENGINE FLAMED OUT WHEN TRANSITIONING FROM IDLE TO FLIGHT. A TECH OUTSIDE OF HELICOPTER ADVISED OF WHITE SMOKE FROM ENGINE EXHAUST AT THE MOMENT OF ENGINE FLAMEOUT. SUBSEQUENT TROUBLESHOOTING COULD NOT REPRODUCE THE PROBLEM.
- [SDR S6GA2014F00005](https://openairdocs.org/sdr/S6GA2014F00005.md): Turbine Wheel · damaged · Sep 21, 2013 · N41NM · Agusta A109E · Turbine Section
  > PILOT REPORTED NR 1 ENGINE CHIP LIGHT ILLUMINATED AND HEARD NOISE, BROUGHT ENGINE TO IDLE, AS NOISE INCREASED, SHUTDOWN ENGINE. MADE UNEVENTFUL SINGLE ENGINE LANDING AT NEAREST AIRPORT. MX FOUND OIL FILTER BY-PASS BUTTON POPPED, CHIP DETECTOR COVERED WITH P
- [SDR S6GA2013F00000](https://openairdocs.org/sdr/S6GA2013F00000.md): Engine · failed · Sep 21, 2013 · N41NM · Agusta A109E · Engine (Turbine/Turboprop)
  > DURING CRUISE FLIGHT, NR 1 ENGINE CHIP LIGHT ILLUMINATED AND HEARD STRANGE NOISE. BROUGHT NR 1 ENGINE TO IDLE. AS NOISE INCREASED, SHUT ENGINE OFF. MADE UNEVENTFUL SINGLE ENGINE LANDING. MX FOUND THAT NR 1 ENGINE OIL FILTER BYPASS BUTTON HAD POPPED. CHI
- [SDR CA131007002](https://openairdocs.org/sdr/CA131007002.md): Engine · making metal · Sep 21, 2013 · Agusta A109E · Engine (Turbine/Turboprop)
  > (CAN) DURING CRUISE WITH NO PATIENTS ON BOARD, THE ENGINE NR 1 CHIP LIGHT ILLUMINATED AND AN UNUSUAL NOISE WAS HEARD. THE PILOT REDUCED POWER, THE NOISE GOT WORSE, THE PILOT ELECTED TO SHUTDOWN & SECURE THE ENGINE. THE FLIGHT WAS DIVERTED AND AN UNEVENTFUL S
- [SDR K97A2013F00102](https://openairdocs.org/sdr/K97A2013F00102.md): Lever · grooved · Apr 25, 2013 · N103H · Agusta A109E · Tail Rotor Head
  > TORQUE SHAFT LEVER ASSY IS WORN WHERE RIGID CONNECTING LINK ATTACHES. GROOVE WORN IN TS LEVER ASSY.
- [SDR DT1R20130425003](https://openairdocs.org/sdr/DT1R20130425003.md): Gear · cracked · Apr 23, 2013 · N143CF · Agusta A109E · Main Rotor Gearbox
  > DURING THE ACCOMPLISHMENT OF AN TECHNICAL BULLETIN BT109EP-128 ON A MAIN GEARBOX; A CROWN GEAR, WAS FOUND TO HAVE A CRACK. THE CROWN GEAR WILL BE REPLACED BY A NEW SUPPORT ASSY.
- [SDR 2013FA0000267](https://openairdocs.org/sdr/2013FA0000267.md): Control System · restricted · Apr 20, 2013 · N606SP · Agusta A109E · Tail Rotor Control System
  > PILOT COMPLAINED ABOUT LOSS OF TAIL ROTOR CONTROL ON LANDING. CHECKED PITCH CONTROL MECHANISM, RIGGING OF CONTROL RODS AND FOUND NORMAL. USING T/R PITCH RIGGING TOOLS FOUND FULL LT PEDAL DEFLECTION LACKING 4-5 DEGREES FULL TRAVEL. SIDE PANEL CARPET SEEMED T
- [SDR K97A2012F00175](https://openairdocs.org/sdr/K97A2012F00175.md): Bushing · debonded · Oct 5, 2012 · N102H · Agusta A109E · Tail Rotor Head
  > DURING PRE-FLIGHT CHECK, PILOT COMPLAINED THAT THE TAIL ROTOR PEDALS WERE STIFF. MECHANIC CONFIRMED THIS AND DETERMINED THAT THE TAIL ROTOR HUB ASSEMBLY NEEDED TO BE DISSASEMBLED FOR FURTHER INVESTIGATION. UPON DISSASEMBLY MECHANIC FOUND TEFLON FRICTION WASHE
- [SDR CA120924011](https://openairdocs.org/sdr/CA120924011.md): Blade · damaged · Sep 22, 2012 · Agusta A109E · Main Rotor Blades
  > (CAN) UPON APPROACH HEARD "SWISHING" SOUND, POWER REDUCED, SOUND WENT AWAY. POST FLIGHT INSPECTION:.3333 OF THE LOWER SURFACE OF THE TRIM TAB IS MISSING.
- [SDR 2012FA0000158](https://openairdocs.org/sdr/2012FA0000158.md): Support · worn · Mar 13, 2012 · N298R · Agusta A109E · Engine Mount Section
  > DURING ACCOMPLISHMENT OF 109EP-112, ENGINE MOUNT INSTALLATION INSPECTION AND RT AND LT V-SHAPED SUPPORTS AND REAR SUPPORT LEGS REPLACEMENT. NR 2 ENGINE INBD MOUNT V-SHAPED SUPPORT, FORWARD LEG HAD LATERAL PLAY. UPON REMOVAL OF MOUNT, MOUNT BOLT WAS FOUND WOR
- [SDR QMLA2012030812047](https://openairdocs.org/sdr/QMLA2012030812047.md): Mount · damaged · Mar 3, 2012 · N5UV · Agusta A109E · Engine Mount Section
  > AFTER INSTALLING NR 2 ENGINE, DISCOVERED INBD BI-POD MOUNT LOOSE AT LOWER ENGINE DECK FLOOR. CHECKED NR 1 ENGINE AND DICOVERED IT ALSO WAS LOOSE. SUSPECT DAMAGE TO U-CHANNEL AT STRUCTURE WHERE INBD MOUNTS CONNECT. IN THE PROCESS OF REMOVING ENGINE TO FURTHER
- [SDR CA111215008](https://openairdocs.org/sdr/CA111215008.md): Bushing · cracked · Dec 15, 2011 · Cessna 680CE · Engine Thrust Reverser
  > (CAN) WHEN DISASSEMBLED FOR 1200-HR LUBRICATION OF THE THRUST REVERSER LATCHBOX SHOULDER BOLT, PN: 07ND78423-1, QTY 7 OF 8 BUSHINGS, PN: NAS77A4-009, WERE FOUND CRACKED AND/OR SEPARATED.
- [SDR QMLA2011102311103](https://openairdocs.org/sdr/QMLA2011102311103.md): Unknown · odor · Oct 23, 2011 · N62UP · Urocop EC135P2 · Air Distribution System
  > CREW REPORTED SMELLING FUEL THROUGHOUT THE CABIN APPROX 15 MINUTES INTO FLIGHT. THE ODOR LASTED FOR ABOUT A MINUTE, AND THEN DISAPPEARED. LANDED AT DESTINATION WITHOUT INCIDENT. OPEN BOTH ENGINE COWLINGS AFTER SHUTDOWN TO INSPECT FOR ANY SIGN OF A FUEL LEAK
- [SDR QMLA2011090211090](https://openairdocs.org/sdr/QMLA2011090211090.md): Housing · broken · Sep 2, 2011 · N911UF · Agusta A109E · Aircraft Fuel Filter/Strainer
  > ACFT DEPARTED FOR REVENUE FLIGHT. MX WAS NOTIFIED BY GROUND CREW OF POSSIBLE FUEL ON THE HELIPAD. NOTIFIED PILOT OF PRESSENCE OF FUEL AND ADVISED HIM TO LAND AS SOON AS POSSIBLE. UPON MX ARRIVAL AT ACFT, APPLIED POWER TO NR1 FUEL BOOST PUMP AND NOTICED FUEL L
- [SDR CA110803009](https://openairdocs.org/sdr/CA110803009.md): Oil System · leaking · Jul 22, 2011 · Piper J3C65 · Turbine Engine Oil System
  > (CAN) DURING CRUISE, THE PILOT NOTICED THE LOW OIL PRESSURE WARNING LIGHT AND SAW PRESSURE WAS FLUCTUATING. WHEN THE PRESSURE FLUCTUATED DOWN TO 10 PSI THE ENGINE WAS SHUTDOWN. AN UNEVENTFUL SINGLE ENGINE LANDING FOLLOWED. INITIAL REPORTS OBSERVED LARGE QUANTI
- [SDR CA110711010](https://openairdocs.org/sdr/CA110711010.md): Fuel Control · failed · Jun 30, 2011 · Agusta A109E · Fuel Control/Turbine Engines
  > FLAMEOUT ON GROUND PRIOR TO FLIGHT, THE NR 1 ENG HAD AN UNCOMMANDED SHUTDOWN AS THE OIL PRESSURE INDICATION WAS READING ZERO. THE PROBLEM WAS TRACED BACK TO A CONTAMINATED P3 AIR PASSAGE AT THE MAIN OIL PRESSURE SHUT OFF VALVE. ALL LINES AND PASSAGES WERE CL
- [SDR 1EXA01282011001](https://openairdocs.org/sdr/1EXA01282011001.md): Blade · debonded · Jan 28, 2011 · N272SM · Agusta A109E · Main Rotor Blades
  > ON PREFLIGHT INSP, FOUND THE INBD BLADE SPOILER SEPARATED ABOUT 6 INCHES FROM THE OTBD SECTION OF SPOILER, PILOT SAID ON HIS WAY, THAT HE FELT A THAT THE FLIGHT WAS NOT AS SMOOTH, AFTER REACHING DESTINATION, ON INSP OF THE BLADE FOUND THE SEPARATION ON THE BLA
- [SDR QMLA2011123111001](https://openairdocs.org/sdr/QMLA2011123111001.md): Unknown · odor · Dec 31, 2010 · N911UF · Agusta A109E · Air Distribution System
  > THE PILOT AND MEDICAL CREW ONBOARD THE ACFT ALL SMELLED A STRONG FUEL ODOR SHORTLY AFTER TAKEOFF. THE PILOT IMMEDIATELY RETURNED TO THE HANGAR THAT HE JUST DEPARTED TO HAVE MX LOOK INTO THE PROBLEM. THE MECHANIC TROUBLESHOT THE PROBLEM COULD NOT DUPLICATE ON
- [SDR 2010FA0000850](https://openairdocs.org/sdr/2010FA0000850.md): Efi · failed · Aug 6, 2010 · N530KS · Agusta A109E · Navigation System
  > UPON RECEIVING THE EFI, IT WAS TURNED ON AND IT OPERATED NORMALLY FOR ABOUT 2 MINUTES, EXCEPT THE CURRENT DRAW WAS HIGH. AT THE END OF THIS PERIOD, AN ACRID ODOR WAS DETECTED BY THE TECH AND THE TEST WAS STOPPED. THE DEFECT AND ITS ROOT CAUSE IS STILL BEING
- [SDR NXTA11220](https://openairdocs.org/sdr/NXTA11220.md): Terminal · broken · Feb 8, 2010 · N146CF · Agusta A109E · Electrical Power System Wiring
  > A BROKEN ELECTRICAL WIRE TERMINAL CARRYING 115 VAC CONTACTED THE GROUND SIDE OF THE GFCI ELECTRICAL OUTLET AND MELTED THE PLASTIC BACK OF THE OUTLET. PILOT NOTICED SMELL AND CREW REPORTED SEEING "VISIBLE VAPOR" IN THE AFT CABIN OF THE AIRCRAFT. PILOT MADE AN
- [SDR CA100203001](https://openairdocs.org/sdr/CA100203001.md): Engine · power loss · Jan 25, 2010 · Engine (Turbine/Turboprop)
  > (CAN) AFTER TAKEOFF THE ENGINE SUFFERED A DROP IN TORQUE FROM 75 PERCENT TO 68 PERCENT ACCOMPANIED WITH FLUCTUATIONS. THE PILOT SWITCHED TO MANUAL MODE AND THE PROBLEM PERSISTED, THEN HE SWITCHED AGAIN TO AUTOMATIC AND THE TORQUE DROPPED FROM 67 PERCENT TO 58
- [SDR CA090311006](https://openairdocs.org/sdr/CA090311006.md): Eec · failed · Mar 2, 2009 · Fuel Controlling System
  > (CAN) PILOT NOTICED NO TQ INDICATION ON RT ENG DURING RESTORATION OF ENG CONTROL TO ITS NORMAL POSITION, AFTER A EEC LIGHT ILLUMINATION. EEC LIGHT WENT OUT, ACFT FUNCTIONED NORMALLY, FLIGHT CONTINUED. ON SHORT FINAL TO HOME BASE, LIGHT CAME ON AGAIN, ACFT LAND
- [SDR CA081125020](https://openairdocs.org/sdr/CA081125020.md): Engine · making metal · Nov 21, 2008 · Agusta A109E · Engine (Turbine/Turboprop)
  > (CAN) PILOT REPORTED NR 2 ENG CHIP LIGHT ILLUMINATED AT TOP OF CLIMBOUT, IMMEDIATELY FOLLOWED BY A SURGE AND POWER LOSS. PILOT PREPARED FOR A RUN-ON LANDING. NR 2 ENG WAS SECURED, PASSENGERS WERE BRIEFED AND TRAFFIC AND DISPATCH WERE ALERTED. NR 1 ENG WENT TO

Next page: https://openairdocs.org/engine/pratt-whitney-canada-pw206c/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 = 'PW206C'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/pratt-whitney-canada-pw206c/reports

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