# Service difficulty reports: Pratt & Whitney Canada PW127

A list on [Pratt & Whitney Canada PW127](https://openairdocs.org/engine/pratt-whitney-canada-pw127.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 20 · 996 reports

- [SDR 29GA2024120700001](https://openairdocs.org/sdr/29GA2024120700001.md): Engine · flamed out · Dec 7, 2024 · N705SV · Aerosp ATR72212A · Engine (Turbine/Turboprop)
  > ENGINE #1 FLAMEOUT ON APPROACH DUE TO FUEL STARVATION ACCOMPLISHED WITH A BRIEF LOSS OF POWER IN ENGINE #2. CORRECTIVE ACTION- PERFORMED VISUAL EXAMINATION OF FUEL LEVEL WITH MANUAL MAGNETIC INDICATOR. FOUND 880 LBS. OF FUEL ON RH AND NO INDICATION ON LH TANK
- [SDR 29GA2024090500001](https://openairdocs.org/sdr/29GA2024090500001.md): Oil System · low pressure · Sep 5, 2024 · N402SV · Aerosp ATR42500 · Engine Oil Pressure
  > LOSS OF OIL PRESSURE ON #2 ENGINE SHORTLY AFTER TAKEOFF VIEWED AT 30 PSI CLIMBING THROUGH 1000 FEET SETTLED AT 0PSI, ENGINE SHUT DOWN. CORRECTIVE ACTION-INSPECTED #2 ENGINE OIL FOR LEAKS ALSO CHECKED MCDU, FOUND MULTIPLE FAULTS FROM PREVIOUS DAYS. CLEARED ALL
- [SDR 29GA2024031200001](https://openairdocs.org/sdr/29GA2024031200001.md): Connector · loose · Mar 12, 2024 · N708SV · Aerosp ATR72212A · Turbine Engine System Wiring
  > #2 ENGINE OVER TORQUE ON TAKEOFF (111.1%) AFTER ABORTED TAKEOFF TQ REMAINED AT 70% WITH PL AT GROUND IDLE. TAKEOFF ABORTED BELOW 70 KNOTS. FOUND PEC SYSTEM FAULTY ON MCDU INSPECTED PVM AND FOUND LOOSE CANNON PLUG, RESECURED CONNECTOR, PERFORMED ERASING OF PEC
- [SDR 29GA2023110200001](https://openairdocs.org/sdr/29GA2023110200001.md): Engine · unknown · Nov 2, 2023 · N703SV · Aerosp ATR72212A · Engine (Turbine/Turboprop)
  > AT 1000 FEET FOUND EVIDENCE OF SPARKS COMING OUT OF #1 ENGINE EXHAUST. FOUND DAMAGED BLADES ON #1 ENGINE ASSY, REMOVED AND REPLACED ENGINE ASSY OPS AND LEAK CHECKS GOOD.
- [SDR 29GA2023082100001](https://openairdocs.org/sdr/29GA2023082100001.md): Oil Cap · loose · Aug 21, 2023 · N702SV · Aerosp ATR72212A · Turbine Engine Oil System
  > LEFT MASTER WARNING OIL PRESSURE LOSS. FOUND OIL CAP LOOSE, SERVICED ENGINE RESECURED CAP, REPLACED ENGINE IBV FILTER OPS CHECK GOOD.
- [SDR Q0MF202009020372](https://openairdocs.org/sdr/Q0MF202009020372.md): Pump · abnormal · Aug 30, 2020 · N16856 · Aerosp ATR72212A · Engine Fuel Pump
  > ON AUG 30, MANDARIN AIRLINES B-16856 AE366 FROM MZG TO TSA, ENG 1 FLAME OUT DURING T/O PHASE AFTER POWER LEVER TO NOTCH, RTO. ACTION TAKEN: THE MECHANIC CHECK FOUND PEC FAULT CODE 31/32/71, REPLACED PEC FOR PREVENTIVE MAINTENANCE. CHECK QAR DATA FOUND ENG NR
- [SDR CA190730015](https://openairdocs.org/sdr/CA190730015.md): Bearing · making metal · Jul 29, 2019 · Turbine Engine Compressor Section
  > (CAN) ENGINE SERIAL WAS RECEIVED FOR INVESTIGATION AND REPAIR DUE TO OPERATOR REPORTED METAL CONTAMINATION. (TC# 20190730015)
- [SDR CA190624003](https://openairdocs.org/sdr/CA190624003.md): Blade · fractured · Jun 8, 2019 · Aerosp ATR72212A · Engine (Turbine/Turboprop)
  > (CAN) DURING GROUND RUN AFTER THE T6 CABLE REPLACEMENT, ENGINE SURGING OCCURRED AND UNUSUAL NOISE WAS HEARD. THE ENGINE WAS SHUT-DOWN AND DURING INSPECTION, WHILE MANUALLY TURNING THE PROPELLER, A NOTICEABLE RUBBING SOUND COULD BE HEARD. VISUAL INSPECTION VIA
- [SDR CA190826007](https://openairdocs.org/sdr/CA190826007.md): Line · cracked · Jun 8, 2019 · Turbine Engine Oil System
  > (CAN) ON AUG 7 IT WAS REPORTED THAT THERE WAS AN UNSCHEDULED REMOVAL DUE TO AN OIL SMELL IN THE CABIN. THE ENGINE SENT TO SHOP FOR INVESTIGATION AND REPAIR. DURING A LEAK CHECK, IT WAS FOUND A CRACK IN THE NO 5 BRG OIL PRESSURE LINE. (TC# 20190826007)
- [SDR CA190826006](https://openairdocs.org/sdr/CA190826006.md): Packing · leaking · Jun 1, 2019 · Turbine Engine Oil System
  > (CAN) IT WAS REPORTED THAT THERE WAS AN UNSCHEDULED ENGINE REMOVAL DUE TO AN OIL SMELL IN THE CABIN. THE ENGINE WAS SENT TO SHOP FOR INVESTIGATION AND REPAIR. THEIR INVESTIGATION REVEALED TWO DAMAGED O-RINGS ON THE SCAVENGE TRANSFER TUBE BETWEEN THE ICC AND GG
- [SDR CA190724003](https://openairdocs.org/sdr/CA190724003.md): Case · stained · May 30, 2019 · Turbine Section
  > (CAN) CUSTOMER REPORTED OIL SMELL IN THE CABIN. ON TROUBLESHOOTING OIL STAIN FOUND IN THE GG CASE AREA. (TC# 20190724003)
- [SDR CA190607003](https://openairdocs.org/sdr/CA190607003.md): Bearing · failed · May 25, 2019 · Aerosp ATR72212A · Turbine Engine Compressor Section
  > (CAN) CUSTOMER REPORTED THAT THE LEFT HAND ENGINE WAS SHUT DOWN IN FLIGHT AFTER THE CREW HEARD A LOUD NOISE WITHOUT ENGINE ALARM. SMOKE WAS OBSERVED AT THE STATION AND IN THE CABIN. (TC# 20190607003)
- [SDR CA190503003](https://openairdocs.org/sdr/CA190503003.md): Packing · leaking · Apr 26, 2019 · Aerosp ATR42* · Turbine Engine Compressor Section
  > (CAN) CUSTOMER REPORTED THAT DURING FLIGHT PILOT HAD A HEADACHE DUE TO OIL SMELL IN THE CABIN. ON TROUBLESHOOTING NOTICED OIL WETNESS WAS FOUND AROUND THE #5 BEARING HOUSING AREA ON #1 ENGINE. FURTHER TROUBLESHOOTING IS GOING ON. (TC# 20190503003)
- [SDR CA190425007](https://openairdocs.org/sdr/CA190425007.md): Fire Warning · illuminated · Apr 13, 2019 · Aerosp ATR72212A · Fire Detection
  > (CAN) DURING A LANDING APPROACH, WHILE AT APPROXIMATELY 2000 FT, THE RIGHT-HAND ENGINE FIRE WARNING ILLUMINATED. THE CREW ELECTED TO SHUT DOWN THE ENGINE, AND DECLARED AN EMERGENCY LANDING. THE AIRCRAFT LANDED UNEVENTFULLY, INVESTIGATION CARRIED OUT AND IS NOW
- [SDR CA190627003](https://openairdocs.org/sdr/CA190627003.md): Case · cracked · Mar 23, 2019 · Aerosp ATR72212A · Turbine Engine Combustion Section
  > (CAN) CREW REPORTED TO HAVE SMOG IN CABIN AND COCKPIT DURING CRUISE. AS PER MM, VISUAL INSPECTION OF BOTH ENGINE EXTERNAL OIL LEAKS CHECK C/O. NL SENSOR PACKING CONDITION CHECKED FOR OCM INSPECTION BUT NO ABNORMALITY FOUND. ALSO, AS PER MM CHECKED ENGINE SWITC
- [SDR MTNA20160909001](https://openairdocs.org/sdr/MTNA20160909001.md): Oil Cap · loose · Sep 7, 2016 · N804FX · Aerosp ATR72212 · Turbine Engine Oil System
  > ENROUTE, AT FL150, THE CREW NOTICED AN OIL LOW PRESSURE ALERT FOR ENGINE NR 1. AN EMERGENCY WAS DECLARED AND THE FLIGHT RETURNED TO DEPARTURE. FOUND OIL COM ON NR 1 ENGINE LOOSE. FOLLOWED STEPS IN EMM 72-00-02, FAULT ISOLATION 2, FIG 107. ENSURED SECURITY
- [SDR CA160216011](https://openairdocs.org/sdr/CA160216011.md): Blades · damaged · Feb 11, 2016 · Aerosp ATR72212A · Turbine Section
  > (CAN) DURING TAXI OUT THE MOMENT THE PILOT ADVANCED POWER LEVER, THERE WAS SMOKE IN CABIN. THE PILOT SHUTDOWN NR 2 ENGINE AND TAXIED BACK TO THE BAY. GROUND ENGINEER FOUND 3 TO 4 PT2 BLADES MISSING TIP HALVES. TURBO MACHINERY CHIP DETECTOR WAS FOUND WITH SIGNI
- [SDR CA160211001](https://openairdocs.org/sdr/CA160211001.md): Windshield · cracked · Feb 9, 2016 · Aerosp ATR42500 · Flight Compartment Windows
  > (CAN) AT TOP OF CLIMB FLIGHT CREW NOTED CO-PILOT MAIN WINDSHIELD HAD CRACKED. THE CREW RETURNED AND LANDED AT THE DEPARTURE AIRPORT. MAINTENANCE PERSONNEL REPLACED THE CO-PILOT WINDSHIELD IAW JIC 56-11-00. NO FURTHER FAULTS WERE NOTED.
- [SDR CA160216006](https://openairdocs.org/sdr/CA160216006.md): Thermocouple · malfunctioned · Feb 7, 2016 · Engine EGT/TIT Indicating System
  > (CAN) ABORTED TAKEOFF DUE TO ENGINE NR 1 HIGH ITT, 765C. DURING TROUBLESHOOTING, THERMOCOUPLE FAILED THE RESISTANCE CHECK. THERMOCOUPLES WERE CHANGED AND THE ACFT RETURN TO SERVICE.
- [SDR CA160121005](https://openairdocs.org/sdr/CA160121005.md): Seal · leaking · Jan 3, 2016 · Aerosp ATR72 · Turbine Engine Oil System
  > (CAN) CUSTOMER REPORTED THAT 20 MINUTES AFTER TAKEOFF, PILOT NOTICED A LOW OIL PRESSURE ON RT ENGINE. THE PILOT ELECTED TO SHUTDOWN THE RT ENGINE AND RETURN TO ORIGIN. ACFT LANDED UNEVENTFULLY. GROUND INSPECTION FOUND THE RT ENGINE BREATHER SEAL WAS LEAKING
- [SDR COEA2015123104801](https://openairdocs.org/sdr/COEA2015123104801.md): Landing · corroded · Dec 31, 2015 · N801FX · Aerosp ATR72212 · Nacelle/Pylon Miscellaneous Structure
  > HEAVY CHECK COE & MAJOR REPAIR. LT ENG NACELLE INBD AFT LANDING FOR PANEL 474AR, HAS CHAFING DAMAGE, LEVEL 2 CORROSION. REPAIR IAW SRAS CE 219 16 9937 DATED 2 2 2016.
- [SDR COEA2015123105801](https://openairdocs.org/sdr/COEA2015123105801.md): Landing · corroded · Dec 31, 2015 · N801FX · Aerosp ATR72212 · Nacelle/Pylon Miscellaneous Structure
  > HEAVY CHECK COE & MAJOR REPAIR. LT ENG NACELLE OTBD AFT LANDING FOR PANEL 473AL, HAS CHAFING DAMAGE, LEVEL 2 CORROSION. REPAIRED IAW SRAS CE 219 16 9938 DATED 2 2 2016.
- [SDR CA160203002](https://openairdocs.org/sdr/CA160203002.md): Eec · faulted · Dec 14, 2015 · Aerosp ATR72 · Fuel Controlling System
  > (CAN) ELECTRONIC ENGINE CONTROL NR 1 FAULT LIGHT ILLUMINATED DURING TAKEOFF ROLL. THE TAKEOFF WAS ABORTED. THE ELECTRONIC ENGINE CONTROL DATA WAS EXTRACTED AND ELECTRONIC ENGINE CONTROL FC 39/87 WERE FOUND. ALL FAULT CODES WERE ERASED, ENGINE GROUND RUN WAS
- [SDR CA151216015](https://openairdocs.org/sdr/CA151216015.md): Engine · smoke · Dec 10, 2015 · Aerosp ATR72212A · Engine (Turbine/Turboprop)
  > (CAN) DURING TAXI TO THE GATE, THE CONTROL TOWER INFORMED THE CREW THAT SMOKE WAS COMING OUT OF THE NR 1 ENGINE. THE ENGINE HAD BEEN FEATHERED WHEN THE SMOKE CAME OUT. THE CREW RECEIVED A FIRE WARNING AND PULLED THE TEE HANDLE AS A PRECAUTIONARY MEASURE, RES
- [SDR CA151216012](https://openairdocs.org/sdr/CA151216012.md): Unknown · odor · Dec 3, 2015 · Aerosp ATR72212A · Air Distribution System
  > (CAN) THIS ENGINE HAS BEEN EXPERIENCING BLEED AIR CONTAMINATION SINCE NOV. 6TH. DECONTAMINATION OF THE ACFT AIR SYS WAS PERFORMED, REPLACEMENT OF THE AIR CYCLE MACHINE, ENGINE BLEED VALVE ETC. TO NO AVAIL, OIL ODOR RETURNED AFTER A WEEK OF OPERATION AT WHICH
- [SDR CA151130004](https://openairdocs.org/sdr/CA151130004.md): Engine · unknown · Nov 13, 2015 · Engine (Turbine/Turboprop)
  > (CAN) ( XIAN- MA 60) WHILE PERFORMING AN EMERGENCY LANDING, THE ACFT EXITED THE END OF THE RUNWAY. THE ACFT SUFFERED DAMAGE TO THE LANDING GEAR AND TAIL SECTION, OTHER DAMAGES LIKELY TO BE PRESENT BUT NOT VISIBLE. WITNESSES REPORTED POSSIBLE ENGINE ISSUES.
- [SDR CA151130005](https://openairdocs.org/sdr/CA151130005.md): Blades · damaged · Nov 13, 2015 · Aerosp ATR72212A · Turbine Section
  > (CAN) DURING A WALK-AROUND, PRIOR TO FLIGHT, THE PILOT DISCOVERED MULTIPLE BLADE DAMAGE TO THE SECOND POWER TURBINE STAGE. ACFT GROUNDED AND WAITING FINAL INSPECTION FOR DISPOSITION.
- [SDR CA151117017](https://openairdocs.org/sdr/CA151117017.md): Autofeather Sys · malfunctioned · Nov 9, 2015 · Aerosp ATR72 · Propeller Feathering/Reversing
  > (CAN) WHILE CRUISING AT FL160, THE LT ENGINE POWER ROLLED BACK AND SELF-RECOVERED 10 SECONDS LATER. THE FLIGHT CONTINUED TO DESTINATION WHERE IT LANDED UNEVENTFULLY. TROUBLESHOOTING LED TO THE REPLACEMENT OF THE AUTO FEATHER UNIT, AFU, BEFORE THE ACFT WAS RET
- [SDR CA151201004](https://openairdocs.org/sdr/CA151201004.md): Engine · flamed out · Nov 9, 2015 · Aerosp ATR42500 · Engine (Turbine/Turboprop)
  > (CAN) FLIGHT CREW REPORTED UN-COMMANDED ENGINE FLAMEOUT AND AUTO RELIGHT ON THE LT ENGINE AFTER 08 SEC DURING CLIMB AT FL215. THE PROBLEM WAS NOT REPRODUCED DURING THE TROUBLESHOOTING. THE AFU WAS REPLACED AS A PRECAUTIONARY MEASURE AND THE ACFT IS BACK IN OP
- [SDR CA151117009](https://openairdocs.org/sdr/CA151117009.md): Eec · faulted · Nov 2, 2015 · Aerosp ATR72 · Fuel Control/Turbine Engines
  > (CAN) WHILE SETTING TAKEOFF POWER AS THE PILOT GRADUALLY ADVANCED THE THROTTLE, AN ELECTRONIC ENGINE CONTROL 1 FAULT WAS TRIGGERED. THE TAKEOFF WAS ABORTED AND THE ACFT SAFELY VACATED THE RUNWAY. THE ACFT SYS WENT BACK TO NORMAL AFTER RESETTING THE ELECTRONIC
- [SDR CA151030005](https://openairdocs.org/sdr/CA151030005.md): Engine · overtorqued · Oct 21, 2015 · Aerosp ATR72 · Engine (Turbine/Turboprop)
  > (CAN) DURING LANDING PHASE, WITH POWER LEVERS SET AT 45, THE RT ENGINE FUEL FLOW AND HIGH PRESSURE COMPRESSOR SPEED, NH, STARTED TO INCREASE WITHOUT ANY PILOT INPUTS, THE ENGINE WENT IN OVERTORQUE CONDITION REACHING 129 PERCENT. THE PILOT INITIATED A GO AROUN
- [SDR CA151029016](https://openairdocs.org/sdr/CA151029016.md): Engine · contaminated · Oct 18, 2015 · Aerosp ATR72212A · Engine (Turbine/Turboprop)
  > (CAN) DURING DESCENT, WHEN BOTH POWER LEVERS WERE MOVED TO IDLE, A SIGNIFICANT AMOUNT OF SMOKE APPEARED IN COCKPIT WITH SMOKE FUME ODOR. AN UNEVENTFUL LANDING FOLLOWED AT DESTINATION. POST FLIGHT INSPECTION FOUND OIL INSIDE THE GAS GENERATOR AND INTERCOMPRESSO
- [SDR CA151029006](https://openairdocs.org/sdr/CA151029006.md): Engine · malfunctioned · Oct 12, 2015 · Engine (Turbine/Turboprop)
  > (CAN) DURING TAKE-OFF, THE CREW FELT A BUMP FROM RIGHT SIDE OF THE AIRCRAFT. THE MASTER WARNING SYSTEM ANNOUNCED HIGH PRESSURE COMPRESSOR SPEED (NH) DROP WITH ENGINE ELECTRONIC CONTROL AND ENGINE PROPELLER CONTROL FAULTS. TAKE-OFF WAS ABORTED, POWER LEVER MOVE
- [SDR CA151015007](https://openairdocs.org/sdr/CA151015007.md): Blade · fractured · Oct 4, 2015 · Aerosp ATR72212A · Turbine Section
  > (CAN) IN CRUISE FLIGHT, THE PILOT SHUTDOWN THE LT ENGINE AFTER LOW OIL PRESSURE WARNING. THE ACFT RETURNED TO ORIGIN AND MADE AN UNEVENTFUL LANDING. TROUBLESHOOTING REVEALED PT2 BLADE WERE FRACTURED. THE ENGINE WILL BE REMOVED FOR INVESTIGATION.
- [SDR CA151015010](https://openairdocs.org/sdr/CA151015010.md): Oil System · leaking · Oct 2, 2015 · Aerosp ATR72212A · Turbine Engine Oil System
  > (CAN) DURING FLIGHT, REPORTS OF FLUID LEAKING FROM THE NACELLE FUEL/OIL DRAIN OF NR 1 ENGINE PROMPTED THE CREW TO SHUT THE ENGINE DOWN. NO COCKPIT INDICATIONS REPORTED. THE ACFT LANDED SINGLE ENGINE WITHOUT ANY FURTHER PROBLEMS. POST FLIGHT INSPECTION FOUND
- [SDR CA151015001](https://openairdocs.org/sdr/CA151015001.md): Engine · making metal · Sep 30, 2015 · Aerosp ATR72212A · Engine (Turbine/Turboprop)
  > (CAN) DURING FLIGHT, THE PILOT RECEIVED A LOW OIL PRESSURE WARNING AND FOLLOWED PROCEDURES AND SHUT THE ENGINE DOWN. AN UNEVENTFUL SINGLE ENGINE LANDING FOLLOWED. POST FLIGHT INSPECTION REVEALED A SIGNIFICANT AMOUNT OF DEBRIS ON THE 1 OF THE CHIP DETECTORS.
- [SDR CA151007009](https://openairdocs.org/sdr/CA151007009.md): Autofeather Sys · malfunctioned · Sep 29, 2015 · Aerosp ATR72 · Propeller Feathering/Reversing
  > (CAN) AN UNCOMMANDED AUTOFEATHER EVENT TOOK PLACE ON THE RT ENGINE DURING APPROACH. DURING DESCENT PRIOR TO THE UNCOMMANDED AUTOFEATHER, HEAVY VIBRATIONS WERE OBSERVED. AFTER TROUBLESHOOTING THE AUTOFEATHER UNIT WAS REPLACED.
- [SDR CA151007012](https://openairdocs.org/sdr/CA151007012.md): Engine · power loss · Sep 29, 2015 · Aerosp ATR72 · Engine (Turbine/Turboprop)
  > (CAN) WHILE STABILIZED AT FL180, NR 2 ENGINE HAD ALL PARAMETERS DECREASED. AS NT DROPPED TO APPROXIMATELY 60 PERCENT THE AUTOMATIC RELIGHT TURNED IT ON AGAIN. CREW NOTED MASTER WARNING AND ENGINE FLAMEOUT MESSAGES. FLIGHT RESUMED WITH NO FURTHER INCIDENT.
- [SDR CA151007001](https://openairdocs.org/sdr/CA151007001.md): Engine · power loss · Sep 26, 2015 · Aerosp ATR72212A · Engine (Turbine/Turboprop)
  > (CAN) THE PILOT REPORTED THAT DURING THE LAST STAGE OF CRUISE AND DURING DESCENT, THEY HAVE EXPERIENCED A REPETITIVE RAPID FLUCTUATION AND TORQUE DROP OF THE ENGINE INSTALLED ON THE LT POSITION WITH YAW MOVEMENT OF THE ACFT. UNEVENTFUL LANDING WAS MADE. TORQ
- [SDR CA151007008](https://openairdocs.org/sdr/CA151007008.md): Bearing · leaking · Sep 26, 2015 · Aerosp ATR72212A · Turbine Engine Oil System
  > (CAN) SMOKE FOUND IN COCKPIT AND CABIN DURING DECREASING POWER LEVER. AFTER TROUBLESHOOTING, AN OIL LEAK FROM BEARING NR 5 IS SUSPECTED.
- [SDR CA151006014](https://openairdocs.org/sdr/CA151006014.md): Engine · leaking · Sep 24, 2015 · Aerosp ATR72212A · Engine (Turbine/Turboprop)
  > (CAN) OIL ODOR IN CABIN REPORTED DURING DESCENT PHASE OF THE FLIGHT. UNEVENTFUL LANDING COMPLETED. BOROSCOPE INSPECTIONS AFTER 3 ENGINE RUNS REVEALED FRESH AND COOKED OIL IN THE INTERMEDIATE COMPRESSOR CASE. THE OPERATOR WAITING RECOMMENDATION.
- [SDR CA151007005](https://openairdocs.org/sdr/CA151007005.md): Engine · power loss · Sep 22, 2015 · Aerosp ATR72212A · Engine (Turbine/Turboprop)
  > (CAN) CUSTOMER REPORTED THAT WHEN POWER LEVER IS AT TAKEOFF, RT ENGINE WAS UNABLE TO ACHIEVE TAKEOFF POWER WITH NO INCREASE IN TORQUE. FSR PROVIDED TROUBLESHOOTING RECOMMENDATIONS TO CUSTOMER.
- [SDR CA150925001](https://openairdocs.org/sdr/CA150925001.md): Oil System · pressure loss · Sep 9, 2015 · Aerosp ATR72212 · Engine Oil Pressure
  > (CAN) ACFT EXPERIENCED AN INFLIGHT ENGINE SHUTDOWN SHORTLY AFTER TAKEOFF. THE FLIGHT CREW REPORTED THE NR 2 ENGINE WITH A LOW OIL PRESSURE WARNING ON THE CREW ALERT PANEL, CAP, FOLLOWED BY THE LOCAL RED LED ALERT ON THE ENGINE OIL PRESSURE GAUGE. JUST AS THE
- [SDR CA150901002](https://openairdocs.org/sdr/CA150901002.md): Eec · faulted · Aug 21, 2015 · Aerosp ATR72212A · Fuel Controlling System
  > (CAN) TAKEOFF WAS ABORTED DUE TO ELECTRONIC ENGINE CONTROL FAULT OCCURRENCE WHEN POWER LEVER WAS ADVANCED TO TAKEOFF NOTCH. CUSTOMER MONITORED THE SITUATION AND AS THERE WAS NO CHANGE IN ENGINE PERFORMANCE ASSOCIATED WITH THESE F/A, THE ACFT RETURNED TO SERVI
- [SDR CA150907001](https://openairdocs.org/sdr/CA150907001.md): Engine · power loss · Aug 19, 2015 · Engine (Turbine/Turboprop)
  > (CAN) DURING CLIMB AT 1,500 FT, PILOT NOTICED RT ENGINE TQ AND NP DROP. ALTITUDE WAS MAINTAINED. PILOT SELECTED POWER MANAGEMENT SWITCH TO MAX CONTINUOUS AND ENGINE RECOVERED. ACFT TURNED BACK TO DEPARTURE AIRPORT AND LANDED UNEVENTFULLY.
- [SDR CA150818001](https://openairdocs.org/sdr/CA150818001.md): Brake · burned · Aug 7, 2015 · Aerosp ATR42500 · Propeller System
  > (CAN) DURING FLIGHT, THE ALARM, PROPELLER BRAKE UNLOCK, FLASHED ONE TIME, AFTER LANDING DURING TAXIING A THICK WHITE SMOKE FROM THE FRONT OF RT ENGINE WAS OBSERVED, PROPELLER BREAKS WERE NOT ENGAGED. AFTER ENGINE SHUTDOWN CUSTOMER WITNESSED A LOT OF HYD FLUID
- [SDR CA150817007](https://openairdocs.org/sdr/CA150817007.md): Engine · power loss · Aug 6, 2015 · Engine (Turbine/Turboprop)
  > (CAN) DURING TAKEOFF, AT ALTITUDE OF APPROXIMATELY 100 FT LT ENGINE PROPELLER SPEED NP, DROPPED DOWN FROM 99 PERCENT TO 7PERCENT, TORQUE, TQ, DROPPED FROM 90 TO 0. THE RT ENGINE TORQUE, TQ, UPTRIMMED TO 102. PILOT SELECTED POWER MANAGEMENT TO MAX CONTINUOUS.
- [SDR CA150731002](https://openairdocs.org/sdr/CA150731002.md): Blade · distressed · Jul 29, 2015 · Aerosp ATR72212A · Turbine Section
  > (CAN) DURING PUSHBACK, AFTER RELEASE PROPELLER BRAKE, PILOT NOTICED ABNORMAL SOUND FROM RT ENGINE. ACFT RETURNED TO BAY AND ENGINE WAS SHUTDOWN. GROUND INSPECTION FOUND PT2 BLADE DISTRESS. THE CUSTOMER PLANS TO PERFORM A BORESCOPE INSPECTION TO DETERMINE THE
- [SDR CA150802001](https://openairdocs.org/sdr/CA150802001.md): Engine · failed · Jul 28, 2015 · Aerosp ATR72212A · Engine (Turbine/Turboprop)
  > (CAN) ACFT WAS PERFORMING TAXIING WHEN PILOTS WERE NOTIFIED THAT FIRE WAS COMING OUT OF NR 2 ENGINE EXHAUST. THE CREW SHUTDOWN THE ENGINE AND ACTIVATED 1ST STAGE FIRE EXTINGUISHER SYS. GROUND CREW CONFIRMED THE PROPELLER DOES NOT ROTATE FREELY AND ENGINE AN
- [SDR CA150728001](https://openairdocs.org/sdr/CA150728001.md): Engine · flamed out · Jul 19, 2015 · Aerosp ATR72 · Engine (Turbine/Turboprop)
  > (CAN) CUSTOMER REPORTED LT ENGINE FLAME OUT IN FLIGHT AND AFTER APPROXIMATELY 20 SECONDS, ENGINE RECOVERED ITSELF, ACFT LANDED UNEVENTFULLY.

Next page: https://openairdocs.org/engine/pratt-whitney-canada-pw127/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 = 'PW127'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/pratt-whitney-canada-pw127/reports

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