# Service difficulty reports: Pratt & Whitney Canada PW206B2

A list on [Pratt & Whitney Canada PW206B2](https://openairdocs.org/engine/pratt-whitney-canada-pw206b2.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 110 reports

- [SDR QMLA2026102220081](https://openairdocs.org/sdr/QMLA2026102220081.md): Blower Motor · failed · Oct 22, 2026 · N865NC · Urocop EC135P2 · Air Distribution Fan
  > WHILE ON THE GROUND GETTING READY TO LIFT OFF REX HELIPAD, THE CREW STATED THERE WAS A SMELL IN THE BACK. SHORTLY AFTER, THE SMELL INTENSIFIED ENOUGH FOR THE PILOT TO SMELL IT IN THE COCKPIT FOLLOWED BY THE CABIN BEING FILLED WITH SMOKE COMING OUT OF THE AIR V
- [SDR QMLA2026102120080](https://openairdocs.org/sdr/QMLA2026102120080.md): Unknown · odor · Oct 21, 2026 · N865NC · Urocop EC135P2 · Air Distribution System
  > 5 MINUTES PRIOR TO LANDING AT BASE, SMELLED BURNING ELECTRICAL ODOR IN COCKPIT. TURNED OFF AIRCRAFT FAN (AIR BLOWER) AND THE ODOR SUBSIDED. LANDED WITHOUT INCIDENT. MADE AIRCRAFT FAULT WRITE UP AND CALLED MECHANIC FOR TROUBLESHOOTING.
- [SDR 2026FA0000621](https://openairdocs.org/sdr/2026FA0000621.md): Fadec · failed · Aug 4, 2026 · N641EC · Urocop EC135P2 · Engine Controls
  > 3 MINUTES INTO THE FLIGHT, BOTH ENG MANUAL 2 AND FADEC FAIL 2 CAUTION ILLUMINATED. WHEN THE CAUTIONS ILLUMINATED THERE WAS NO INDICATION OF A FAIL ON THE FLI, TEMPERATURES, OR PRESSURES. FOLLOWING ACTIONS WERE TO REFER TO SECTION 3-27 OF THE FLIGHT MANUAL FOR
- [SDR QMLA2026071020044](https://openairdocs.org/sdr/QMLA2026071020044.md): Fadec · failed · Jul 10, 2026 · N253AM · Urocop EC135P2 · Engine Fuel and Control
  > NR 1 FADEC FAILURE IN FLIGHT
- [SDR QMLA2026040620025](https://openairdocs.org/sdr/QMLA2026040620025.md): Engine · contaminated · Apr 6, 2026 · N817LV · Urocop EC135P2 · Cabin Equipment/Furnishings
  > LAUNCHED FOR HOSPITAL TRANSFER. MEDIC SAID HE HAD SMOKE IN CABIN. ABORTED FLIGHT AND LANDED BACK AT BASE. AIRCRAFT INSPECTED AND RTS. SMELL DETERMINED TO BE FROM THE COMP WASH PREVIOUS TO THE FLIGHT.
- [SDR QMLA012920007](https://openairdocs.org/sdr/QMLA012920007.md): Unknown · vibration · Jan 29, 2026 · N917AC · Urocop EC135P2 · Main Rotor System
  > ACFT LAUNCHED FROM BASE, 13 MIN FLT WAS UNEVENTFUL, GW WAS 2754 & POWER WAS NORMAL. WHEN LIFTING FROM LOW ROOFTOP PAD, ACFT REQUIRED MORE TORQUE THAN EXPECTED TO HOGE, ASSUMPTION WAS HIGHER THAN EXPECTED WEIGHT BUT POST FLT DETAILED ANALYSIS: GW WAS 2778, OAT
- [SDR JBZA20251124001](https://openairdocs.org/sdr/JBZA20251124001.md): Fadec · inoperative · Nov 19, 2025 · N838CS · Urocop EC135P2 · Engine Fuel and Control
  > PILOT EXPERIENCED A NUMBER TWO FADEC FAILURE AND THE RESPECTIVE CAUTION LIGHTS ILLUMINATED, PILOT DETECTED A BURNING SMELL IN THE COCKPIT DIVERTED TO NUT TREE AIRPORT. TROUBLE SHOOTING REVEALED NR 2 FADEC TO BE THE SOURCE OF THE ODOR.
- [SDR QMLA2025110820112](https://openairdocs.org/sdr/QMLA2025110820112.md): Bypass Valve · faulted · Nov 8, 2025 · N533LC · Urocop EC135P2 · Turbine Engine Oil System
  > #2 ENG OIL TEMPERATURE WAS EXCEEDING LIMITATIONS IN FLIGHT AT 120KTS. IT WAS IN THE RED ZONE AND WAS INDICATING AT 142DEG C. OIL PRESSURE WAS IN NORMAL RANGE. NO CHANGE AFTER SLOWING DOWN OR BRINGING THE ENGINE TO IDLE. AN EMERGENCY ENGINE SHUTDOWN WAS PERFORM
- [SDR 454A250627095116](https://openairdocs.org/sdr/454A250627095116.md): Fadec · faulted · Jun 28, 2025 · N922NH · Urocop EC135P2 · Engine Fuel and Control
  > AIRCRAFT WAS ENROUTE TO SENDING FACILITY AND EXPERIENCED A FADEC MANUAL CAUTION LIGHT WITH A FEW OTHER INDICATOR LIGHTS ON THE #2 SIDE GOING OFF. HE IMMEDIATELY DECIDED TO DIVERT AND MAKE A PRECAUTIONARY LANDING AT KINT. UPON TRYING TO LAND THE FADEC DID FAIL
- [SDR QMLA2025020720014](https://openairdocs.org/sdr/QMLA2025020720014.md): Line · leaking · Feb 5, 2025 · N102HN · Urocop EC135P1 · Engine (Turbine/Turboprop)
  > LEAK FROM #1 ENGINE DISCOVERED ON POST FLIGHT INSPECTION UPON LANDING AT HOSPITAL. TIGHTENED LOOSE LINE,
- [SDR QMLA2025012020005](https://openairdocs.org/sdr/QMLA2025012020005.md): Windscreen · cracked · Jan 20, 2025 · N134AM · Urocop EC135P2 · Flight Compartment Windows
  > PILOTS' WINDSCREEN CRACKED WHILE RETURNING TO BASE.
- [SDR QMLA2024101520132](https://openairdocs.org/sdr/QMLA2024101520132.md): Transmission · making metal · Oct 12, 2024 · N535LN · Urocop EC135P2 · Main Rotor Gearbox
  > MAIN XMSN CHIP ILLUMINATED ON START. CLEANED MAG CHIP DETECTOR ENGINE RUNS COMPLETE. IAW AMM 63-40-00
- [SDR QMLA2024100420129](https://openairdocs.org/sdr/QMLA2024100420129.md): Starter Gen · faulted · Oct 3, 2024 · N136KY · Urocop EC135P2 · Starter-Generator
  > UPON CLIMB OUT, BATTERY DISCHARGE LIGHT ILLUMINATED AND SUBSEQUENT AUDIBLE ALARM, IT WENT OFF AND ON TWICE, OBSERVED VOLTAGE DROP AND SURGE, AS WELL AS CABIN LIGHT DIM AND BRIGHTEN AS WELL AS A HIGH PITCHED ELECTRICAL NOISE HEARD BY ALL 3 CREW MEMBERS. RETURNE
- [SDR QMLA202409182011](https://openairdocs.org/sdr/QMLA202409182011.md): Fadec · failed · Sep 18, 2024 · N135WJ · Urocop EC135P2 · Engine Fuel and Control
  > THE CREW AND I DEPARTED SHORTLY AFTER FOR AN APPROXIMATELY 22 MINUTE FLIGHT TO THE PICKUP LOCATION. WHILE THE AIRCRAFT WAS IN-GROUND EFFECT TO LAND AT THE SCENE; THE MASTER CAUTION, FADEC FAIL, FADEC MINR, AND FLI DEGR LIGHTS ON THE CAD APPEARED AND THE LOSS
- [SDR QMLA2024091420114](https://openairdocs.org/sdr/QMLA2024091420114.md): Heater · smoke · Sep 14, 2024 · N132HN · Urocop EC135P2 · Engine Bleed Air System
  > CREW ANNOUNCED SMOKE IN THE CABIN UPON TURNING HEATER ON
- [SDR QMLA2024091220113](https://openairdocs.org/sdr/QMLA2024091220113.md): Connector · dirty · Sep 12, 2024 · N533LF · Urocop EC135P2 · Fire Protection System Wiring
  > ERRONEOUS CARGO SMOKE WARNING LIGHT ILLUMINATED ON SHORT FINAL TO OCALA HOSPITAL. CLEANED CONNECTOR AND CONTACT ENHANCER.
- [SDR QMLA2024090520106](https://openairdocs.org/sdr/QMLA2024090520106.md): Motor · malfunctioned · Sep 5, 2024 · N533LF · Urocop EC135P2 · Windshield/Door Rain/Ice Removal
  > SMELLED BURNING FUMES COMMENSURATE WITH WINDSHIELD WIPER MALFUNCTION ON SHORT FINAL TO BASE
- [SDR QMLA2024062520071](https://openairdocs.org/sdr/QMLA2024062520071.md): Bypass Valve · faulted · Jun 23, 2024 · N586AM · Urocop EC135P2 · Main Rotor Gearbox
  > THE PILOT PICKED UP PATIENT AS DESIGNATED LZ/SCENE AND DEPARTED THE SCENE FOR DESERT REGIONAL MEDICAL CENTER. WHILE ON CLIMB OUT (AROUND 1000') OVER MOUNTAINOUS TERRAIN, PILOT SCANNED ENGINE & TRANSMISSION TEMPS & PRESSURES. WHEN PILOT LOOKED AT NR 1 ENG COLU
- [SDR 2024F00052](https://openairdocs.org/sdr/2024F00052.md): Frame · cracked · Mar 7, 2024 · N135CM · Urocop EC135P2 · Fuselage Main, Frame
  > FRAME 5 FOUND CRACKED AT MOUNTING LOCATIONS FOR METRO AFT MED WALL
- [SDR JBZA20240131001](https://openairdocs.org/sdr/JBZA20240131001.md): Heater · odor · Jan 27, 2024 · N837CS · Urocop EC135P2 · Heating System
  > DURING FLIGHT THE CREW SMELLED AN ELECTRICAL BURNING ODOR AND DIVERTED TO SAN MARTIN AIRPORT. PRIOR TO THIS FLIGHT THE AIRCRAFT HAD BEEN PARKED OUTSIDE IN HEAVY RAIN. THE AIRCRAFT WAS VISUALLY INSPECTED BY A COMPANY AMT FOR THE SOURCE OF THE ODOR, WITHOUT IDEN
- [SDR QMLA2023100520083](https://openairdocs.org/sdr/QMLA2023100520083.md): Unknown · unknown · Oct 4, 2023 · N132HN · Urocop EC135P2 · Engine (Turbine/Turboprop)
  > SHORTLY AFTER TAKEOFF AROUND 60KIAS THE LOW ROTOR WARNING SOUNDED. THE #1 ENGINE SHOWED LOWER N2 AND TORQUE THAN THE #2. #1 ENG N2 WAS APPROXIMATELY 90% AND #1 NEEDLE ON FLI WAS BETWEEN 4 AND 5 MARKINGS. I MADE THE DECISION TO ABORT THE FLIGHT TO KCRW. AS I B
- [SDR U0GA TL 248039](https://openairdocs.org/sdr/U0GA%20TL%20248039.md): Control Rod · cracked · Sep 12, 2023 · N325DB · Urocop EC135P2 · Main Rotor Control
  > DURING AIRCRAFT INSPECTION PROMPTED BY SIMILAR DEFECT ON ANTHER FLEET AIRCRAFT. CRACK FOUND ON LH (LONGITUDNAL) MR SERVO INPUT FLIGHT CONTROL ROD. REF EC135P2+ IPC IPC 22-18-10-01, ITEM 10
- [SDR U0GA FCD 00487](https://openairdocs.org/sdr/U0GA%20FCD%2000487.md): Control Rod · cracked · Sep 12, 2023 · N228BJ · Urocop EC135P2 · Main Rotor Control
  > DURING AIRCRAFT INSPECTION PROMPTED BY SIMILAR DEFECT ON ANOTHER FLEET AIRCRAFT. CRACK FOUND ON LH (LONGITUDNAL) MR SERVO INPUT FLIGHT CONTROL ROD. REF EC135P2+ IPC IPC 22-18-10-01, ITEM 10
- [SDR U0GA TL 247933](https://openairdocs.org/sdr/U0GA%20TL%20247933.md): Control Rod · cracked · Sep 11, 2023 · N127JL · Urocop EC135P2 · Main Rotor Control
  > DURING AIRCRAFT AAIP INSPECTION CRACK FOUND ON LH (LONGITUDNAL) MR SERVO INPUT FLIGHT CONTROL ROD. REF EC135P2+ IPC IPC 22-18-10-01, ITEM 10
- [SDR VE7A20231010303](https://openairdocs.org/sdr/VE7A20231010303.md): Bypass Valve · overtemp · Sep 11, 2023 · N376PH · Urocop EC135P2 · Engine (Turbine/Turboprop)
  > NUMBER 1 ENGINE OIL TEMPERATURE APPROACHED REDLINE. DID NOT EXCEED BUT DID APPROACH.
- [SDR QMLA2023081920063](https://openairdocs.org/sdr/QMLA2023081920063.md): Bypass Valve · unknown · Aug 18, 2023 · N911EF · Urocop EC135P2 · Turbine Engine Oil System
  > MY NORMAL CROSS CHECK IDENTIFIED A DISPARITY IN #1 AND #2 ENGINE OIL TEMPERATURE OF APPROXIMATELY 12 DEGREES C AFTER ABOUT 5 MINUTES OF FLIGHT AT CRUISE. ABOUT 12 MILES SOUTH OF THE CITY OF LAS CRUCES, NM I NOTICED THE #2 OIL TEMP CLIMB ACCELERATE SO I REDUCED
- [SDR QMLA2023081420061](https://openairdocs.org/sdr/QMLA2023081420061.md): Unknown · unknown · Aug 14, 2023 · N132HN · Urocop EC135P2 · Engine (Turbine/Turboprop)
  > #1 ENGINE FAILURE IN FLIGHT
- [SDR QMLA2023041820030](https://openairdocs.org/sdr/QMLA2023041820030.md): Sliding Window · unknown · Apr 16, 2023 · N139TJ · Urocop EC135P2 · Window/Windshield System
  > WE (PILOT, NURSE, MEDIC) WERE RETURNING FROM OUR FUELING POINT AFTER COMPLETING AN INTER-FACILITY TRANSFER. APPROXIMATELY FOUR MINUTES INTO A SIX-MINUTE FLIGHT, THE PARAMEDIC SITTING IN THE COPILOT SEAT (WITHOUT CONTROLS), ASKED IF HE COULD OPEN THE SLIDING
- [SDR 2A6D20220831001](https://openairdocs.org/sdr/2A6D20220831001.md): Frame Angle · elongated · Aug 31, 2022 · N241AM · Urocop EC135P2 · Fuselage Structure (General)
  > DAMAGE TO THE FRAME WAS DISCOVERED IN THE FORM OF AN ELONGATED HOLE TO FRAME AT STA X4709
- [SDR 2A6D202208311002](https://openairdocs.org/sdr/2A6D202208311002.md): Frame · cracked · Aug 31, 2022 · N241AM · Urocop EC135P2 · Fuselage Main, Frame
  > DURING THE INSPECTION REQUIRED BY ASB21-01 SECTION 4, DAMAGE WAS DISCOVERED AT FRAME 5 ADJACENT TO THE MEDICAL EQUIPMENT WALL.
- [SDR 2A6D20220726001](https://openairdocs.org/sdr/2A6D20220726001.md): Floor Support · corroded · Jul 26, 2022 · N241AM · Urocop EC135P2 · Fuselage Structure (General)
  > THE UPPER T-CAP ON FRAME 3 AT (X FS 3150) (Z WL 1365) (Y BL 0) WAS FOUND TO HAVE CORROSION UNDER A NUTPLATE ON THE BOTTOM OF THE MAIN CABIN FLOOR. ALSO, THE FRAME 3 WEB AT (X FS 3150) (Z WL 1150) (Y BL 0) WAS FOUND TO HAVE DENT DAMAGE NEAR A STIFFENER
- [SDR QMLA2022072220045](https://openairdocs.org/sdr/QMLA2022072220045.md): Unknown · odor · Jul 20, 2022 · N533LF · Urocop EC135P2 · Air Distribution System
  > WHILE FLYING, MYSELF AND THE CREW NOTICED A ELECTRICAL BURNING ODOR. AT THIS POINT I WAS ON APPROACH TO KSRQ SO I CONTINUED TO LAND ON FBO RAMP WITHOUT INCIDENT. AFTER THOROUGH INSPECTION OF AIRCRAFT WE FOUND NOTHING UNUSUAL AND SMELL OR ODOR WAS NO LONGER E
- [SDR 2A6D20220712](https://openairdocs.org/sdr/2A6D20220712.md): Keelbeam · damaged · Jul 12, 2022 · N241AM · Urocop EC135P2 · Fuselage Main, Structure
  > DAMAGE WAS NOTED TO THE LH KEEL BEAM CAP (PN: L533M1009203) IN THE HORIZONTAL FLANGE IN THE FORM OF AN AREA OF CORROSION MEASURED TO BE APPROXIMATELY 0.30” X 0.30” AND 0.009” DEEP, AS WELL AS 4EA ADDITIONAL HOLES DRILLED THROUGH THE FLANGE, AND A SECTION OF MA
- [SDR 2A6D2022070711001](https://openairdocs.org/sdr/2A6D2022070711001.md): Mount · gouged · Jul 7, 2022 · N241AM · Urocop EC135P2 · Fuselage Main, Structure
  > DAMAGE TO THE TRANSMISSION DECK (PN: L533M1017293) IN THE FORM OF DENTS LOCATED FWD OF BOTH THE LH AND RH ARIS MOUNT. THERE ARE 2EA DENTED AREAS FWD OF THE LH ARIS MOUNT LOCATED BENEATH THE GUSSETS (PN: L533M1017256) AFFECTING BOTH THE XMSN DECK AND THE BELO
- [SDR 2A6D20220707002](https://openairdocs.org/sdr/2A6D20220707002.md): Tail Boom · damaged · Jul 7, 2022 · N241AM · Urocop EC135P2 · Rotorcraft Tail Boom
  > DAMAGE TO THE INNER SKIN PLIES OF THE LH TAIL BOOM SKIN (PN: L535A1601107). THE INNER SKIN HAS BEEN DRILLED THROUGH AT 6EA POINTS OF A MOUNTING PLATE FOR THE VOR ANTENNA
- [SDR M3XA20210506004](https://openairdocs.org/sdr/M3XA20210506004.md): Bypass Valve · malfunctioned · May 5, 2021 · N135WL · Urocop EC135P2 · Turbine Engine Oil System
  > PILOT REPORTED IN CRUISE FLIGHT THAT THE #1 ENGINE OIL TEMPERATURE WAS HIGH. MECHANIC REPLACED #1 ENGINE OIL BYPASS VALVE.
- [SDR QMLA2020090820044](https://openairdocs.org/sdr/QMLA2020090820044.md): Unknown · odor · Sep 7, 2020 · N814LN · Urocop EC135P2 · Air Distribution System
  > PILOT / CREW REPORTED SMOKE AND SMELL IN CABIN AFTER TURNING ON AIRCRAFT HEAT TO DEFOG WINDSCREEN. CORRECTIVE ACTION, INSPECTED BOTH ENGINES AND HEATER MIXING VALVE FOR OBVIOUS DEFECTS, NONE NOTED. HAD PILOT RUN BOTH ENGINES AND TURN ON BLEED AIR FOR HEAT.
- [SDR HDNA2020090300393](https://openairdocs.org/sdr/HDNA2020090300393.md): Bypass Valve · defective · Sep 3, 2020 · N135LL · Urocop EC135P2 · Engine Oil Temperature Regulator
  > THE NR 2 ENGINE OIL TEMPERATURE EXCEEDED THE MAX CONTINUOUS OPERATING RANGE THRESHOLD, WHICH RESULTED IN THE ENGINE BEING PLACED IN THE IDLE DETENT AND THE PILOT PERFORMING A RUN ON LANDING AT HIS INTENDED AIRPORT. THIS DISCREPANCY WAS TROUBLESHOT TO A DEFECT
- [SDR M3XA2020070130005](https://openairdocs.org/sdr/M3XA2020070130005.md): Unknown · malfunctioned · Jun 28, 2020 · N830MT · Urocop EC135P2 · Engine (Turbine/Turboprop)
  > PILOT REPORTED ON GLIMB OUT AT 80 KNOTS HEARD A SERIES OF LOUD REPORT ON NR 1 ENGINE SIDE. MECHANIC INVESTIGATED BY INSPECTING XMSN AND DRIVETRAIN COMPONENTS AND NR 1 AND NR 2 ENGINES AND FOUND NO DEFECTS OR ABNORMALITIES. DOWNLOADED ENGINE DCU'S AND FORWARD
- [SDR JBZA20200603001](https://openairdocs.org/sdr/JBZA20200603001.md): Fuel Nozzle · leaking · May 30, 2020 · N834CS · Urocop EC135P2 · Fuel Injector Nozzle
  > EXPERIENCED A NR 2 ENGINE IN-FLIGHT FLAMEOUT DURING A TRAINING FLIGHT, SUCCESSFULLY PERFORMED AN AIR RESTART OF ENGINE NR 2. A NORMAL APPROACH TO A LANDING WAS MADE. TROUBLESHOOTING INSPECTION REVEALED LOOSE FUEL NOZZLE.
- [SDR QMLA20191126001](https://openairdocs.org/sdr/QMLA20191126001.md): Pump · fire · Nov 26, 2019 · N438CM · Urocop EC135P2 · Cabin Equipment/Furnishings
  > WHILE EN-ROUTE TO PICK-UP A BABY WITH THE NICU TEAM AND THE SPARE ISOLETTE, A PUMP ON THE ISOLETTE CAUGHT ON FIRE IN CRUISE FLIGHT. THE FLIGHT MEDIC WAS ABLE TO EXTINGUISH THE FIRE WITH A BOTTLE OF WATER BEFORE THE FLIGHT NURSE WAS ABLE TO PASS THE FLIGHT MEDI
- [SDR CA190704004](https://openairdocs.org/sdr/CA190704004.md): Nipple · defective · Jun 21, 2019 · Urocop EC135P2 · Engine (Turbine/Turboprop)
  > (CAN) DURING FINAL APPROACH TO LAND AT 400 FT ABOVE GROUND, OIL PRESSURE LOSS AND COMPRESSOR SURGE OCCURRED. THEREAFTER, A NORMAL BUT RAPID LANDING IN A FIELD WITH AN EMERGENCY SHUTDOWN OF BOTH ENGINES WAS EXECUTED. THE ENGINE WAS RUN FOR AN ESTIMATED 15 SECON
- [SDR CA190604004](https://openairdocs.org/sdr/CA190604004.md): Engine · surges · May 22, 2019 · Engine (Turbine/Turboprop)
  > (CAN) CUSTOMER REPORTED THAT DURING LANDING ON A HIGH ALTITUDE MISSION (10`440 FT) #2 ENGINE SURGED. THE PILOT TRIED SEVERAL HOVERING MANEUVERS AND FINALLY DECIDED TO LAND AND SHUT DOWN THE ENGINE. SUBSEQUENT POWER CHECKS REVEALED THAT THE ENGINE SURGED 3 TIME
- [SDR QMLA2019032819032](https://openairdocs.org/sdr/QMLA2019032819032.md): Compressor · damaged · Mar 28, 2019 · N241AM · Urocop EC135P2 · Engine (Turbine/Turboprop)
  > ON THE FIRST FLIGHT OF THE DAY, FOR A ROUTINE VFR INTER FACILITY TRANSFER FROM EL CENTRO TO UCSD LA JOLLA IN SAN DIEGO, WE DEPARTED BASE AND FLEW TO EL CENTRO REGIONAL MEDICAL CENTER. WE HAD A STANDARD VFR FUEL LOAD OF 96 GALLONS WITH AN EXPECTED PATIENT WEIGH
- [SDR QMLA2019030619025](https://openairdocs.org/sdr/QMLA2019030619025.md): Impeller · damaged · Mar 6, 2019 · N615LF · Urocop EC135P2 · Turbine Engine Compressor Section
  > ON AIRWORTHINESS CHECK DAMAGE WAS OBSERVED ON THE NR 2 ENGINE IMPELLER BLADES.
- [SDR 2A6R2019022251401](https://openairdocs.org/sdr/2A6R2019022251401.md): Bulkhead Web · corroded · Feb 6, 2019 · N137AM · Urocop EC135P2 · Fuselage Main, Bulkhead
  > SN 0326 WAS FOUND TO HAVE CORROSION DAMAGE TO THE RH FS 3150 ANGLE, T—CAP AND BULKHEAD WEB. REPAIR REQUIRED WAS REPLACEMENT OF THE T-CAP AND ANGLES AND DOUBLER INSTALLATION ON THE WEB.
- [SDR QMLA2018100411810](https://openairdocs.org/sdr/QMLA2018100411810.md): Engine · making metal · Oct 1, 2018 · N533LF · Urocop EC135P2 · Engine (Turbine/Turboprop)
  > WHILE IN CRUISE FLIGHT ON AN INTER-FACILITY TRANSFER THE MASTER CAUTION AND NR 2 ENGINE CHIP LIGHT ILLUMINATED. THE PILOT ENGAGED THE "BURN CHIP" SWITCH AND THE LIGHT WENT OUT. AT THAT TIME, THE PILOT TURNED THE HELICOPTER TOWARD THE NEAREST AIRPORT WHICH WAS
- [SDR M3XA2018091800000](https://openairdocs.org/sdr/M3XA2018091800000.md): Bypass Valve · sticking · Sep 17, 2018 · N135VV · Urocop EC135P2 · Engine Oil Distribution (Airframe Furnished)
  > NR 2 ENG OIL TEMP INDICATION OUT OF LIMITS. PRECAUTIONARY LANDING WAS MADE AT AIRPORT.
- [SDR CA180822008](https://openairdocs.org/sdr/CA180822008.md): Transmitter · faulted · Aug 13, 2018 · Urocop EC135P2 · Main Rotor Gearbox
  > (CAN) TRANSMISSION OIL PRESSURE SENDER FAILURE ON START UP. PRESSURE WARNING SWITCH FUNCTIONING. THIS IS THE SECOND FAILURE OF THIS PRESSURE SYSTEM IN 2133 HRS. (TC# 20180822008)
- [SDR M3XA2017071804](https://openairdocs.org/sdr/M3XA2017071804.md): Bypass Valve · stuck · Jul 17, 2017 · N135VV · Urocop EC135P2 · Turbine Engine Oil System
  > IN CRUSE FLIGHT OIL TEMP LIGHT CAME ON. ACFT LANDED SAFELY. OIL COOLER BYPASS VALVE ISSUE.

Next page: https://openairdocs.org/engine/pratt-whitney-canada-pw206b2/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 = 'PW206B2'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/pratt-whitney-canada-pw206b2/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.