# Service difficulty reports: Pratt & Whitney Canada PW118

A list on [Pratt & Whitney Canada PW118](https://openairdocs.org/engine/pratt-whitney-canada-pw118.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 18 · 873 reports

- [SDR ESPA202510010675](https://openairdocs.org/sdr/ESPA202510010675.md): Engine · fire · Oct 1, 2025 · N405PA · Emb EMB120ER · Engine (Turbine/Turboprop)
  > TRANSPORTING PASSENGERS FROM KNTD TO KNSI. ONCE THE ACFT BEGAN CLIMBING TO CRUISE ALTITUDE, CAPT & 1ST OFFICER NOTICED SIGNS OF A LT ENGINE FAILURE & RESPONDED TO AN ENGINE FAILURE. FA1 NOTIFIED CAPT OF THE ENG FIRE, & CAPT ATTEMPTED TO PUT OUT THE FIRE WHILE
- [SDR 2025F00223](https://openairdocs.org/sdr/2025F00223.md): Engine · fire · Jun 12, 2025 · N405PA · Emb EMB120 · Engine (Turbine/Turboprop)
  > ON JUNE 12TH, 2025, PHOENIX AIR GROUP, INC. (PAG) WAS TRANSPORTING PASSENGERS FROM POINT MUGU NAVAL AIR STATION (KNTD) TO SAN NICOLAS ISLAND NAVAL OUTLYING FIELD (KNSI) USING AIRCRAFT N405PA. ONCE THE AIRCRAFT BEGAN CLIMBING TO ITS CRUISE ALTITUDE, CAPTAIN 1
- [SDR HKGA20230623001](https://openairdocs.org/sdr/HKGA20230623001.md): Engine · failed · Jun 23, 2023 · N235SW · Emb EMB120ER · Engine (Turbine/Turboprop)
  > DURING TAKEOFF, LH ENG T6 OVER HEAT, ENGINE WAS SHUT DOWN AS A PRECAUTION. SMOKE WAS PRESENT IN THE COCKPIT. UPON WALKAROUND OIL WAS PRESENT ON THE EXTERIOR OF ENGINE COWING. MAINTENANCE PERFORMED A BORESCOPE AND IDENTIFIED OIL IN THE COMBUSTION CHAMBER WITH P
- [SDR JIKA2022102601](https://openairdocs.org/sdr/JIKA2022102601.md): Oil System · low · Oct 26, 2022 · N567SW · Emb EMB120ER · Turbine Engine Oil System
  > DURING CRUISE FLIGHT, GOT A MASTER WARNING AND THE OIL PRESSURE FOR RT ENGINE BEGAN TO FLICKER AND EVENTUALLY DROPPED BELOW 40 PSI. FOLLOWED QRH PROCEDURE & PREFORMED ENGINE SHUT DOWN. PILOT DID DECLARE AN EMERGENCY. DIVERTED TO MMIO, LANDED WITHOUT INCIDENT.
- [SDR HALA2022062800121](https://openairdocs.org/sdr/HALA2022062800121.md): None · none · Jun 27, 2022 · N209HA · Airbus A300* · Engine Fuel and Control
  > ETOPS - ENG 2 EIU FAULT // REMOVED AND REPLACED ENGINE SEL SW (6KS) PER TSM 73-25-00-810-425A & PERFORMED OPS TEST OF EIU 1 AND 2 PER AMM 73-25-34. OPS GOOD. 6/27/22 19845. PENDING ENGINE RUN. PERFORMED ENG 1 & 2 IDLE RUN. CHECK GOOD. NO FAULTS. OK FOR SVC.
- [SDR HALA2022061500113](https://openairdocs.org/sdr/HALA2022061500113.md): None · none · Jun 14, 2022 · N213HA · Airbus A321271N · Engine (Turbine/Turboprop)
  > DESCENDING THOUGHT 5,000' - 3,000 ' ENGINE AT IDLE EXPERIENCE DIRTY SHOCK SMELL AGAIN // FOUND EVIDANCE OF OIL LEAK ON #1 ENG AT 9 O CHOCK POSITION IN THE FIC REPLACED SEAL FROM LP62 OIL PRESSURE TUBE REF AMM PW 10006-C-72-00-30-00A-702A-B LEAK CHECK GOOD 1843
- [SDR HALA2022061300112](https://openairdocs.org/sdr/HALA2022061300112.md): None · none · Jun 10, 2022 · N217HA · Airbus A321271N · Compressor Bleed Valve
  > ETOPS - ECAM ENG 2 AIR SYS FAULT DESCENDING THROUGH 12,000' // REMOVED AND REPLACED #2 ENGINE BUFFER AIR VALVE PER AMM 75-26-04, PERFORMED TEST 3 IDLE RUN PER AMM 71-00-00, NO DEFECTS NOTED, SYSTEM CHECKED NORMAL. OK FOR SERVICE.
- [SDR JIKA2021062901](https://openairdocs.org/sdr/JIKA2021062901.md): Hmu · failed · Jun 29, 2021 · N179CA · Emb EMB120 · Engine (Turbine/Turboprop)
  > WHILE CRUISING AT 10,000 FEET, WITHOUT WARNING THE NUMBER 2 ENGINE FAILED. FIRST OFFICER CALLED OUT "POWER LOSS" ON NUMBER 2, MEMORY ITEMS AND QRH WERE COMPLETED. ATC AND DISPATCH WAS ADVISED. KRIV WAS CHOSEN AS NEAREST SUITABLE AIRPORT, SINGLE ENGINE APPROACH
- [SDR FXGAEMBN568SW](https://openairdocs.org/sdr/FXGAEMBN568SW.md): Cabin Pressure · erratic · Nov 26, 2020 · N568SW · Emb EMB120ER · Cabin Pressure Control System
  > CABIN ALTITUDE WARNING CAME ON DURING DEPARTURE OUT OF KOGD TO KLRP. RETURNED TO DEPARTURE AIRPORT (KOGD). PERFORMED PRESSURIZATION SYSTEM OPERATIONS CHECK NORMAL, REFERENCE EMB 120 MM CH 21-30-01.
- [SDR JIKA202006231801](https://openairdocs.org/sdr/JIKA202006231801.md): Transmitter · defective · Jun 18, 2020 · N266AS · Emb EMB120ER · Engine Oil Pressure
  > AFTER DEPARTING KPDX THE CREW HAD JUST COMPLETED THEIR CRUISE CHECKLIST AND WHILE FLYING AT THE NORMAL CRUISE ALTITUDE OF 15,000 FEET WHEN THE RIGHT ENGINE OIL PRESSURE BEGAN TRENDING TOWARD LOW PRESSURE. WITHIN 30 SECONDS, THE RIGHT ENGINE OIL PRESSURE SETTLE
- [SDR KCQA201911010001](https://openairdocs.org/sdr/KCQA201911010001.md): Eec · malfunctioned · Oct 7, 2019 · N121CZ · Emb EMB120ER · Fuel Controlling System
  > DURING FLIGHT RH ENGINE EEC FAILURE ANNUNCIATED WITH POWER REDUCTION TO ZERO PERCENT TORQUE. CREW PERFORMED QRH PROCEDURE, UNABLE TO RESTORE POWER ABOVE FLT IDLE. AIRCRAFT DIVERTED TO SUITABLE AIRPORT WITH PROPELLER IN FEATHER. AFTER LANDING ENGINE POWER AND E
- [SDR JIKA2019091001](https://openairdocs.org/sdr/JIKA2019091001.md): Hmu · erratic · Sep 3, 2019 · N567SW · Emb EMB120ER · Fuel Control/Turbine Engines
  > THE FLIGHT CREW REPORTED THAT AT APPROXIMATELY 800-1000' AGL, THE LT PROPELLER INADVERTENTLY FEATHERED. THE FLIGHT CREW RAN THE "INADVERTENT PROPELLER FEATHER" QRH AND WAS ABLE TO UNFEATHER THE PROPELLER, PERFORMED A PRECAUTIONARY AIR RETURN WITH BOTH ENGINES
- [SDR 2018F00120](https://openairdocs.org/sdr/2018F00120.md): Hub · fractured · Jun 26, 2018 · Engine (Turbine/Turboprop)
  > ENGINE REMOVED FOR HIGH N2 VIBRATION & HPC STAGE 8 DAMAGED. AFT HUB, KNIFE-EDGEED FRACTURE CONFIRMED.
- [SDR 2016FA0000463](https://openairdocs.org/sdr/2016FA0000463.md): Duct · torn · Sep 28, 2016 · N410PA · Emb EMB120 · Air Distribution System
  > APPROX 1245 LOCAL TIME, WHEN RT "DUCT LEAK" LIGHT ILLUMINATED. CREW SECURED THE RT ENGINE BLEED VALVE AND RT AC PACK, WAITED THREE MINUTES FOR COOL DOWN AND ANNUNCIATOR TO EXTINGUISH. "DUCT LEAK" LIGHT DID NOT EXTINGUISH. CREW SECURED RT ENGINE IN FLIGHT AN
- [SDR 2015FA0000467](https://openairdocs.org/sdr/2015FA0000467.md): Sending Unit · malfunctioned · Sep 28, 2015 · Emb EMB120ER · Fuel Quantity Sensor
  > AFTER 35 MINUTES AT FL150, PILOT OBSERVED LOW FUEL PRESSURE AND LOSS OF TORQUE. AFTER PARKING, TECH TRIED TO START ENGINE BUT THE RESULT WAS NEGATIVE. CONFIRMED THE MAIN FUEL QUANTITY INDICATOR AND THE RT FUEL INDICATOR MEASURES WERE ERRONEOUS REGARDING TO T
- [SDR JIKA2015091401](https://openairdocs.org/sdr/JIKA2015091401.md): Engine · power loss · Sep 14, 2015 · N201YW · Emb EMB120ER · Engine (Turbine/Turboprop)
  > SHORTLY AFTER TAKEOFF, THE PILOT HEARD A LOUD BANG FROM THE RT ENG & LOST POWER. THE PILOT PERFORMED AN INFLIGHT SHUTDOWN OF THE RT ENG, RETURNED & LANDED WITHOUT INCIDENT. THE RT ENG IS BEING REPLACED. A FOLLOW UP TO THIS SDR WILL BE SUBMITTED WHEN A TEAR
- [SDR JIKA2015091301](https://openairdocs.org/sdr/JIKA2015091301.md): Wire · broken · Sep 13, 2015 · N257AS · Emb EMB120ER · Engine Indicating System Wiring
  > SHORTLY AFTER TAKEOFF, THE PILOT OBSERVED THE LT ENG, DUCT LEAK ANNUNCIATOR LIGHT ILLUMINATED & AURAL WARNING SOUNDED. THE PILOT FOLLOWED PROCEDURES IN QRH & PERFORMED PRECAUTIONARY IN FLIGHT SHUT DOWN OF THE LT ENG. PILOT DECIDED TO RETURN & LANDED WITHOUT
- [SDR 2015FA0000468](https://openairdocs.org/sdr/2015FA0000468.md): Sensor · failed · Aug 31, 2015 · Emb EMB120ER · Fuel Quantity Sensor
  > AFTER 35 MINUTES AT FL150, PILOT OBSERVED LOW FUEL PRESSURE AND LOSS OF TORQUE. AFTER PARKING, TECHS TRY TO START ENGINE BUT THE RESULT WAS NEGATIVE. CONFIRMED THAT THE MAIN FUEL QUANTITY INDICATOR AND THE RT FUEL INDICATOR MEASURES WERE ERRONEOUS REGARDING
- [SDR GN0A20150624001](https://openairdocs.org/sdr/GN0A20150624001.md): Access Panel · unsecure · Jun 23, 2015 · N654CT · Emb EMB120ER · Wing, Plate/Skin
  > ON TAKEOFF, CREW RECEIVED SERVICE DOOR LIGHT & AURAL WARNING. TAKEOFF WAS ABORTED & ACFT RETURNED TO GATE. CREW FOUND FASTENER ON PRESS REFUELING ACCESS PANEL NOT SECURED. PANEL WAS SECURED & WARNING LIGHT EXTINGUISHED. ACFT RETURNED TO SERVICE.
- [SDR GN0A20150320001](https://openairdocs.org/sdr/GN0A20150320001.md): Warning System · false activation · Mar 20, 2015 · N654CT · Emb EMB120ER · Trailing Flap Position Indicating System
  > DURING TAKEOFF ROLL ABOVE V1, CREW RECEIVED A FLAP ASYMMETRY WARNING ON THE OTBD FLAP PANELS. THE CREW FOLLOWED PROCEDURES & CONTINUED THE TAKEOFF THEN RETURNED TO THE AIRPORT & LANDED WITHOUT FURTHER INCIDENT. PERFORMED FLAP OPERATIONAL TEST & CYCLED THE FL
- [SDR GN0A20150222001](https://openairdocs.org/sdr/GN0A20150222001.md): Unknown · malfunctioned · Feb 22, 2015 · N653CT · Emb EMB120ER · Cabin Pressure Control System
  > WHILE ON DESCENT, PASSING THROUGH FLIGHT LEVEL 180, THE CABIN PRESS STARTED TO CLIMB TO 10000’. THE CREW USED THE PRESSURIZATION CONTROL SWITCH TO CHANGE CABIN PRESS CONTROL FROM AUTO TO MANUAL. THE CONTROL IS A THREE POSITION GUARDED SWITCH WITH SETTINGS AU
- [SDR FAA2015120900010](https://openairdocs.org/sdr/FAA2015120900010.md): Blade · cracked · Dec 9, 2014 · N652CT · Emb EMB120RT · Propeller Blade Section
  > CRACK INDICATION OF FILLET RADIUS OF BLADE SHANK, FOUND DURING MAJOR INSPECTION.
- [SDR SWIA201439483](https://openairdocs.org/sdr/SWIA201439483.md): Indicator · faulty · Oct 12, 2014 · N234SW · Emb EMB120ER · Engine Oil Indicating System
  > LOST LT ENGINE OIL PRESSURE INDICATION DURING CRUISE. INDICATION RETURNED WHEN AT IDLE BUT WENT AWAY AT POWER. REPLACED LT OIL PRESSURE TRANSDUCER AND GAUGE.
- [SDR GN0A20141003001](https://openairdocs.org/sdr/GN0A20141003001.md): Processing Unit · failed · Oct 2, 2014 · N652CT · Emb EMB120ER · Integrated Flight System
  > WHILE ON TAKEOFF ROLL THE CAPTAIN REPORTED HIS EADI DISPLAY WENT BLANK. THE TAKEOFF WAS ABORTED & THE ACFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. THE LT DPU HAD FAILED. A SERVICEABLE UNIT WAS INSTALLED WITH THE SYS CHECKING NORMAL IAW THE ACFT MM.
- [SDR GN0A20140824001](https://openairdocs.org/sdr/GN0A20140824001.md): Access Panel · unsecure · Aug 24, 2014 · N654CT · Emb EMB120ER · Wing, Plate/Skin
  > SHORTLY AFTER DEPARTURE THE DOOR WARNING LIGHT ON OVERHEAD PANEL ILLUMINATED ALONG WITH AN AURAL WARNING ACTUATION. THE ACFT RETURNED & LANDED WITHOUT INCIDENT. THE PRESS REFUELING ACCESS PANEL WAS FOUND IN AN UNSECURE POSITION. THE PANEL WAS SECURED & THE
- [SDR SWIA201439199](https://openairdocs.org/sdr/SWIA201439199.md): Control Unit · malfunctioned · Aug 21, 2014 · N581SW · Emb EMB120ER · Propeller Controlling System
  > RT PROPELLER OVERSPEED AFTER TAKEOFF. CREW SAW 103.5 PERCENT WHEN THEY SHUT THE ENGINE DOWN. RETURNED TO DEPARTURE. R & R RT ENGINE PROPELLER CONTROL UNIT IAW AMM. OPS CHECKED GOOD.
- [SDR FXGA201408221431](https://openairdocs.org/sdr/FXGA201408221431.md): Skin · cracked · Aug 20, 2014 · N1105G · Emb EMB120FC · Fuselage Main, Plate/Skin
  > TO REPAIR A CRACK ON THE FUSELAGE SKIN AT FS 2389 AT CENTERLINE. CUT OUT DAMAGE & INSTALL REPAIR DOUBLER ISE RDT2014-120-06-15-20 & EMAIL TITLED EDT2014-120-061520. PERMANENT REPAIR INSPECTION REQUIRED. INTERNAL & EXTERNAL DETAILED INSPECTION REQUIRED AT EV
- [SDR SWIA201439154](https://openairdocs.org/sdr/SWIA201439154.md): Governor · malfunctioned · Aug 18, 2014 · N581SW · Emb EMB120ER · Propeller Governor
  > DURING CLIMBOUT, THE CREW NOTICED THE PROPELLERS SUDDENLY FELT OUT OF SYNC. CAPTAIN NOTICED THE RT PROPELLER AT 103 PERCENT. ACFT RETURNED TO THE FIELD. REPLACED RT PROPELLER OVERSPEED GOVERNOR. SYS OPS NORMAL.
- [SDR SWIA201437647](https://openairdocs.org/sdr/SWIA201437647.md): Pcu · out of adjust · May 14, 2014 · N234SW · Emb EMB120ER · Propeller Controlling System
  > WITH CL AT MAX LEFT NP CONSISTENT AT 101.5 PERCENT. ADJUSTED LT PCU SPEED CONTROL SCREW.2500" COUNTER CLOCKWISE IAW CMM.
- [SDR SWIA201437103](https://openairdocs.org/sdr/SWIA201437103.md): Skin · cracked · Apr 11, 2014 · N224SW · Emb EMB120ER · Nacelle/Pylon, Plate/Skin
  > RIGHT ENGINE TOP COWL, WHERE THE FORWARD INBD DOOR HOLD OPEN ROD ATTACHES HAS A CRACK APPROXIMATELY 1.5" LONG. REPAIRED 1.5" LONG CRACK ON HALF FRAME. LOCATED ON RT ENGINE TOP COWL BY FWD INBD DOOR HOLD OPEN ROD ATTACHES IAW ETD.
- [SDR SWIA201437102](https://openairdocs.org/sdr/SWIA201437102.md): Mount · chafed · Apr 10, 2014 · N224SW · Emb EMB120ER · Engine Mount Section
  > LEFT ENGINE INBD FRONT MOUNT CHAFED AFT OF MOUNTING BOLT. REPLACED LT ENG FWD INBD UPPER MOUNT IAW SRM AND AMM.
- [SDR GN0A20140327001](https://openairdocs.org/sdr/GN0A20140327001.md): Flap · malfunctioned · Mar 26, 2014 · N654CT · Emb EMB120ER · Trailing Edge Flap Control System
  > AFTER TAKEOFF THE CREW SELECTED THE FLAPS UP, THE INBD & NACELLE PANELS RETRACTED TO 0° WHILE THE OTBD PANELS REMAINED AT 15° TAKEOFF POSITION. THIS CONDITION CAUSED THE FLAP DISAGREEMENT WARNING TO ACTIVATE. THE ACFT RETURNED TO FRG & LANDED WITHOUT INCIDEN
- [SDR GLBA2014011000365](https://openairdocs.org/sdr/GLBA2014011000365.md): Oil System · low pressure · Jan 9, 2014 · N293UX · Emb EMB120ER · Engine Oil Indicating System
  > PILOT REPORTED THAT DURING FLIGHT, NR 2 ENGINE OIL PRESSURE LOW LIGHT ILLUMINATED & THEN WENT OUT. THE ENGINE OIL PRESSURE WAS BETWEEN 40-55 & FLUCTUATING, POWER WAS REDUCED TO IDLE & PROP FEATHERED. THE ENGINE OIL PRESSURE NEVER WENT BELOW 40. EMERGENCY DE
- [SDR CA140107001](https://openairdocs.org/sdr/CA140107001.md): Blade · cracked · Jan 7, 2014 · Turbine Section
  > (CAN) DURING ROUTINE HOT SECTION INSPECTION OF THE ENGINE A SINGLE BLADE WAS FOUND WITH A CRACK IN THE RIVET SLOT AREA OF THE FIR TREE. THE BLADES HAD ACCUMULATED 9268.5 HRS. TSN. THE BLADES WERE INSTALLED IN THIS ENGINE AT 3038.5 HOURS TSN IN 2004 AND HAVE A
- [SDR GN0A11182013](https://openairdocs.org/sdr/GN0A11182013.md): Relay · faulty · Nov 17, 2013 · N652CT · Emb EMB120ER · DC Generating System
  > FLIGHT 652 ACY TO ORF WHILE TAXING FOR TAKEOFF THE APU GEN DROPPED OFF LINE. THE FLIGHT CREW FOLLOWED QRH PROCEDURES & RESET THE GEN WHICH CAME BACK ON LINE. ON CLIMB OUT THE APU GEN AGAIN DROPPED OFF LINE. THE CREW SHUTDOWN THE APU AS THE RT EADI & EHSI DI
- [SDR GN0A020130701001](https://openairdocs.org/sdr/GN0A020130701001.md): Unknown · malfunctioned · Jun 28, 2013 · N652CT · Emb EMB120ER · Landing Gear Retraction/Extension System
  > WHEN LANDING GEAR SELECTED UP AFTER TAKEOFF, ALL GEAR REMAINED DOWN AND LOCKED WITH CORRESPONDING DISAGREEMENT LIGHTS (BOTH GREEN & RED) ILLUMINATED ON THE LANDING GEAR SELECTOR INDICATOR. CYCLED THE GEAR SELECTOR HANDLE THREE TIMES WITH THE SAME RESULTS. FOL
- [SDR GLBA2013042900244](https://openairdocs.org/sdr/GLBA2013042900244.md): Wire · loose · Apr 27, 2013 · N96ZK · Emb EMB120ER · Light System Wiring
  > PILOT REPORTED THAT THE WHITE EMERGENCY LIGHT AT ROW 6, LT SIDE IS INOPERATIVE. MX REPAIRED A LOOSE WIRE AT THE CONNECTION, OPS CHECKED GOOD.
- [SDR SWIA201435820](https://openairdocs.org/sdr/SWIA201435820.md): Line · chafed · Jan 28, 2013 · N581SW · Emb EMB120ER · Engine Oil Distribution (Airframe Furnished)
  > LT ENG OIL PRESSURE WARNING LIGHT, AURAL WARNING & FLUCTUATING INDICATION, SHUT DOWN ENG. FLT 7400 CHAFED LINE BETWEEN OIL COOLER & ENG.
- [SDR FXGA201212260001](https://openairdocs.org/sdr/FXGA201212260001.md): Control Unit · leaking · Dec 18, 2012 · N1110J · Emb EMB120FC · Turbine Engine Oil System
  > NR 2 OIL PRESSURE WAS FLUCTUATING BETWEEN 55-40 PSI. NR 2 OIL PRESSURE AURAL WARNING ENGINE "OIL" SHUTDOWN. REPLACED NR 2 PCU IAW MM 61-21-00. GROUND OPS AND LEAK CHECK GOOD. PCU WAS FOUND TO BE LEAKING EXTERNALLY AT REAR OF UNIT.
- [SDR GN0A20121110001](https://openairdocs.org/sdr/GN0A20121110001.md): Line · loose · Nov 10, 2012 · N650CT · Emb EMB120ER · Engine Oil Distribution (Airframe Furnished)
  > KCMH TO CMI: ON TAKEOFF ROLL THE MASTER WARNING ILLUMINATED "LEFT ENGINE OIL" ALONG WITH THE AURAL WARNING "ENGINE OIL" ACTIVATED. THE TAKEOFF WAS ABORTED AND AFTER THE LEFT ENGINE WAS SHUT DOWN, OIL WAS SEEN LEAKING FROM THE LEFT ENGINE. MAINTENANCE FOUND
- [SDR FXGA20121030001](https://openairdocs.org/sdr/FXGA20121030001.md): Attach Angle · cracked · Oct 26, 2012 · N1110J · Emb EMB120FC · Vertical Stabilizer, Attach Fittings
  > DURING INSPECTION, FOUND RT VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE CRACKED AT THE AFT PRESSURE BULKHEAD.
- [SDR GN0A10042012001](https://openairdocs.org/sdr/GN0A10042012001.md): Engine · oscillates · Oct 4, 2012 · N650CT · Emb EMB120ER · Engine (Turbine/Turboprop)
  > FLIGHT 17155 KFRG-KACY: AFTER TAKEOFF AND WHILE CLIMBING THROUGH 5000FT THE RIGHT ENGINE STARTED OSCILLATING WITH AN AIRCRAFT YAWING MOTION. THE RIGHT NP WAS FLUCTUATING BETWEEN 97% AND 104% WITH THE ASSOCIATED ENGINE TORQUE FLUCTUATING 72% TO 84%. THE CREW
- [SDR GN0A20120930001](https://openairdocs.org/sdr/GN0A20120930001.md): Control Panel · failed · Sep 30, 2012 · N652CT · Emb EMB120ER · Flight Controller
  > AUO TO (UOX): AFTER TAKEOFF WHILE CLIMBING THROUGH 3500FT THE AUTO-PILOT WAS ENGAGED. WHEN PASSING 5000FT THE LEFT FLIGHT DIRECTOR BARS PITCHED DOWN 2.5° WHICH CAUSED THE AUTO-PILOT TO COMMAND THE AIRCRAFT FOLLOW. THE LEFT AUTO-PILOT WAS DISENGAGED AND AIRC
- [SDR SWIA201231748](https://openairdocs.org/sdr/SWIA201231748.md): Bearing · failed · Sep 8, 2012 · N236SW · Emb EMB120ER · Propeller Hub Section
  > RIGHT PROPELLER HUB LEAKING OIL. INSPECTED AND FOUND RIGHT PROPELLER NR 4 BEARING RACE FAILURE CAUSING DAMAGE TO RIGHT PROPELLER HUB. REPLACED RIGHT PROPELLER HUB AND ACTUATOR. P/N OFF: 782501-8 S/N OFF: 1785.
- [SDR GN0A07032012](https://openairdocs.org/sdr/GN0A07032012.md): Unknown · malfunctioned · Jul 3, 2012 · N651CT · Emb EMB120ER · Landing Gear Retraction/Extension System
  > THE LEFT MAIN GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM TNN. CREW SELECTED THE LANDING GEAR DOWN AND ALL THREE GEAR INDICATED DOWN AND LOCKED. THE AIRCRAFT RETURNED TO TNN AND LANDED WITHOUT INCIDENT. MAINTENANCE COULD NOT DUPLICATE THE PROBLEM WITH THE AIR
- [SDR GN0A05282012](https://openairdocs.org/sdr/GN0A05282012.md): Control Panel · contaminated · May 28, 2012 · N650CT · Emb EMB120ER · Autopilot System
  > FLIGHT 15976 (MER) TO (GCN): WHILE CLIMBING THROUGH 11,000FT THE AUTO-PILOT ENGAGED WITHOUT THE CREW SELECTING THE SYSTEM ON. NEITHER CONTROL WHEEL A/P DISCONNECT SWITCH WOULD DISENGAGE THE AUTO-PILOT. THE FIRST OFFICER HAD TO HOLD DOWN THE DISCONNECT BUTTO
- [SDR GLBA201203281](https://openairdocs.org/sdr/GLBA201203281.md): Fan · smoke · Mar 28, 2012 · N297UX · Emb EMB120ER · Air Distribution Fan
  > A/C PACKS SMOKE ON GROUND. MX REPLACED THE LT GROUND COOLING FAN, OPS CHECKED GOOD REF MM 21-51-03.
- [SDR GN0A201204010324](https://openairdocs.org/sdr/GN0A201204010324.md): Fuel Filter · dirty · Mar 24, 2012 · N651CT · Emb EMB120ER · Engine Fuel Distribution
  > ON TAKEOFF FROM ATLANTIC CITY (ACY), CREW RECEIVED AN AURAL WARNING CHIME ALONG WITH WARNING LIGHT ON THE MULTIPLE ALARM PANEL FUEL AND THE RIGHT ENGINE FUEL FILTER LIGHT ILLUMINATION. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURT
- [SDR FXGA20120323001](https://openairdocs.org/sdr/FXGA20120323001.md): Skin · corroded · Mar 23, 2012 · N1105G · Emb EMB120FC · Fuselage Main, Plate/Skin
  > DURING HEAVY MX, FOUND LOWER BELLY SKIN, CORRODED IN SEVERAL SPOTS. SKIN WAS REPLACED.
- [SDR FXGA20120323002](https://openairdocs.org/sdr/FXGA20120323002.md): Stringer · corroded · Mar 23, 2012 · N1105G · Emb EMB120FC · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MX, FOUND LT PROFILE STRINGER CORRODED. STRINGER WAS REPLACED.

Next page: https://openairdocs.org/engine/pratt-whitney-canada-pw118/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 = 'PW118'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/pratt-whitney-canada-pw118/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.