# Service difficulty reports: Bombardier DHC-8-314

A list on [Bombardier DHC-8-314](https://openairdocs.org/model/bombardier-dhc-8-314.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 65 reports

- [SDR CA190819005](https://openairdocs.org/sdr/CA190819005.md): Pin · melted · Aug 7, 2019 · Dhav DHC8314 · Light System Wiring
  > (CAN) CABIN CREW REPORTED ON LANDING THAT THE RH OVERHEAD LIGHTING HAD GONE OUT DURING FLIGHT.MAINTENANCE FOUND THAT THE CONNECTOR FOR THE RH SIDE CABIN LIGHTNING CONNECTOR BS2-P2 AND J2 HAD A MELTED TERMINAL AT PIN 7 ON THE PIN 2 CONNECTOR. (TC# 20190819005)
- [SDR CA190327004](https://openairdocs.org/sdr/CA190327004.md): Starter Gen · failed · Mar 26, 2019 · Dhav DHC8314 · Starter-Generator
  > (CAN) PILOTS STARTED THE RH ENGINE AND THE DC GENERATOR WOULD NOT COME ONLINE, SO THEY SHUT DOWN THE ENGINE AND WHEN THEY ATTEMPTED TO START THE ENGINE FOR THE SECOND TIME, THE ENGINE WOULD NOT ROTATE AND COULD ONLY GET 21 TO 22 VOLTS ON THE DC PANEL FROM EXTE
- [SDR CA190219003](https://openairdocs.org/sdr/CA190219003.md): Oil System · low pressure · Jan 16, 2019 · Dhav DHC8314 · Engine Oil Pressure
  > (CAN) `WHILE THE AIRCRAFT WAS CLIMBING ABOUT 10 MILES NORTH OF CYUL, THE FLIGHT CREW NOTED A LOW OIL PRESSURE INDICATION ON THE RIGHT HAND ENGINE. THE ENGINE PROPELLER WAS FEATHERED AS REQUIRED BY THE APPLICABLE CHECKLIST. THE FLIGHT CREW DECLARED AN EMERGENC
- [SDR CA160310011](https://openairdocs.org/sdr/CA160310011.md): Pump · failed · Mar 9, 2016 · Dhav DHC8314 · Hydraulic Pump (Electric/Engine), Main
  > (CAN) IN CRUISE, CREW NOTICE THAT THE HYDRAULIC LEVEL OF SYSTEM NR 2 WAS 0, THEY DECLARE AN EMERGENCY AND LANDED SAFELY. FURTHER INVESTIGATION, NO SIGN OF HYDRAULIC LEAK HAVE BEEN FOUND. THE AIRCRAFT NR 2 HYDRAULIC SYSTEM WAS SERVICED, SYSTEM WAS TESTED ON THE
- [SDR CA160106010](https://openairdocs.org/sdr/CA160106010.md): Precooler · cracked · Dec 24, 2015 · Dhav DHC8314 · Pneumatic Distribution System
  > (CAN) DURING TROUBLESHOOTING OF DE-ICE SNAG, FOUND NR 1 BLEED AIR PRE-COOLER TO HAVE A CRACK AT THE TUBE WELD. ALSO NOTED THAT THE DRIP PLATE HAD BECOME DETACHED AND CAUSED MINOR CHAFE DAMAGE TO THE INTERIOR COOLER FINS. MAINTENANCE ACTION WAS TO REPLACE THE D
- [SDR CA151221014](https://openairdocs.org/sdr/CA151221014.md): Check Valve · corroded · Dec 17, 2015 · Dhav DHC8314 · Emergency Exits
  > (CAN) WE HAD EXPERIENCED COUPLE OF IN FLIGHT DEPRESSURIZATION ALL CAUSED BY THE FWR R1 EMERGENCY DOOR SEAL WHICH DEFLATED IN CRUISE. INVESTIGATION REVEALED THAT SEAL CHECK VALVE WAS INTERNALLY LEAKING WHICH DIDN`T KEEP THE R1 DOOR INFLATED WHEN THE AIRCRAFT WA
- [SDR CA151202010](https://openairdocs.org/sdr/CA151202010.md): Rod End · loose · Dec 1, 2015 · Dhav DHC8314 · Elevator Control System
  > (CAN) DURING ELEVATOR REMOVAL, THE RIGHT ELEVATOR TRIM SCREW JACK ASSY ROD END CLEVIS WAS FOUND TO BE LOOSE, AND THE ROD END JAM NUT (ITEM 230) BACKED OFF. THERE ARE NO PROVISIONS FOR LOCKWIRE ON THE JAM NUT. NO DEFECTS WERE IDENTIFIED WITH THE OPERATION OF T
- [SDR CA151130006](https://openairdocs.org/sdr/CA151130006.md): Engine · smoke · Nov 15, 2015 · Dhav DHC8314 · Engine (Turbine/Turboprop)
  > (CAN) IT WAS REPORTED THAT, DURING THE ENGINE START, COCKPIT SMOKE WAS NOTICED AND THE LAVATORY SMOKE DETECTORS WERE ACTIVATED. NR 2 ENGINE WAS STARTED WITH ITS BLEED SWITCH SELECTED AT PROP FEATHER POSITION. NO 1 ENGINE WAS STARTED THEREAFTER, ITS BLEED SWITC
- [SDR CA150923002](https://openairdocs.org/sdr/CA150923002.md): Indicator · leaking · Sep 19, 2015 · Dhav DHC8314 · Airspeed/Mach Indicator
  > (CAN) AT FLIGHT LEVEL 240, IN IFR CONDITION, CAPTAIN SIDE INSTRUMENTS (ASI, ALTIMETER AND VSI)START TO SHOW ABNORMAL READING. THE AUTO PILOT AND YAW DAMPER KICK OFF AND AFTER A BRIEF ANALYSE CREW DETERMINED THAT THE COPILOT INSTRUMENTATION WAS RELIABLE. THE CR
- [SDR CA150923001](https://openairdocs.org/sdr/CA150923001.md): Altimeter · faulty · Sep 19, 2015 · Dhav DHC8314 · Altimeter, Barometric/Encoder
  > (CAN) BETWEEN START UP OF 2-1 ENGINES CREW HAD A STRONG ODOR OF BURNING ELECTRICAL COMING FROM RADIO CRATE BEHING CAPTAIN, SHORTLY AFTER, NR 2 ADC BREAKER TRIPPED AND PILOTS PROCEED TO SHUT DOWN. AFTER INVESTIGATION, MAINTENANCE FOUND THAT NR 2 SERVO ALTIMETER
- [SDR CA150910009](https://openairdocs.org/sdr/CA150910009.md): Wheel · detached · Sep 8, 2015 · Dhav DHC8314 · Wheel/Ski/Float
  > (CAN) HAD AN EVENT OF MAIN WHEEL ASSY (MWA) DETACHING FROM LH MLG POSITION AFTER TAKE-OFF. THE AIRCRAFT RETURNED BACK AND LANDED WITHOUT THE LT MWA. ALL PRECAUTIONS WERE TAKEN BY THE PILOT AT THE TIME OF LANDING (FUEL TRANSFER). POST LANDING INSPECTIONS PERFOR
- [SDR CA150909001](https://openairdocs.org/sdr/CA150909001.md): Venturi · cracked · Sep 7, 2015 · Dhav DHC8314 · Engine Bleed Air System
  > (CAN) DURING ENGINE OIL SERVICING, MAINTENANCE NOTICE THAT THE VENTURI ADAPTER FOR THE P3 BLEED AIR ON THE RT ENGINE WAS SPLIT OPEN. THE AFT INSULATION BLANKET WAS ALSO DAMAGED BY HEAT.
- [SDR CA150824014](https://openairdocs.org/sdr/CA150824014.md): Valve · leaking · Aug 2, 2015 · Dhav DHC8314 · Escape Slide
  > (CAN) THE DITCHING DAM DEPLOYED IN FLIGHT WE FEEL THIS WAS CAUSED BY CABIN PRESSURE LEAKING INTO THE DITCHING DAM. WHEN WE FIRST INSPECTED THE BURST DISK IT APPEARED TO BE FRACTURED (NOTE THE NITROGEN BOTTLE WAS STILL FULL) WHEN WE HOOKED UP REGULATED AIR AND
- [SDR CA150723003](https://openairdocs.org/sdr/CA150723003.md): Seal · deflated · Jul 22, 2015 · Dhav DHC8314 · Emergency Exits
  > (CAN) PILOT REPORTED: CABIN LOST PRESSURIZATION AT 25 000 FEETS. EMERGENCY DESCENT PERFORMED AND FLIGHT DIVERTED TO THE NEAREST AIRPORT. AIRCRAFT LANDED SUCCESSFULLY WITH NO PASSENGER INJURIES. MAINTENANCE PERSONNEL PERFORMED AN INSPECTION ON THE RH FWD TYPE 1
- [SDR CA150714012](https://openairdocs.org/sdr/CA150714012.md): Fuel/Oil Cooler · faulty · Jul 13, 2015 · Dhav DHC8314 · Engine Fuel/Oil Cooler
  > (CAN) FUEL TEMP CLIMBING TO MAX TEMP ON FUEL TEMP INDICATOR. RT FUEL TEMP AT 57 DEGREES.
- [SDR CA150709003](https://openairdocs.org/sdr/CA150709003.md): Actuator · inoperative · Jul 7, 2015 · Dhav DHC8314 · Landing Gear Door Actuator
  > (CAN) NOSE GEAR FAILED TO EXTEND ON THE FIRST ATTEMP, DURING INSPECTION IT WAS FOUND THAT THE NOSE GEAR DOOR ACTUATOR HAD AN INTERNAL LEAL ALLOWING FLUID TO PASS ON BOTH SIDES OF THE ACTUATOR.
- [SDR CA150703003](https://openairdocs.org/sdr/CA150703003.md): Manifold · broken · Jun 30, 2015 · Dhav DHC8314 · Steering Unit
  > (CAN) ON APPROACH, GEAR WAS SELECTED DOWN, HYDRAULIC POWER WAS LOST ON NR 2 SYSTEM. ALSO NR 2 HYDRAULIC FLUID WAS LOST. FOLLOWING SUCCESSFUL LANDING, THE AIRCRAFT WAS INSPECTED. THREE BOLTS WERE FOUND SHEARED ON TOP OF THE STEERING MANIFOLD, CAUSING THE HYDRA
- [SDR CA150618001](https://openairdocs.org/sdr/CA150618001.md): Regulator · damaged · Jun 15, 2015 · Dhav DHC8314 · Turbine Engine Oil System
  > (CAN) AFTER LANDING CREW NOTICE OIL DRIPPING OUT OF NR 1 ENG COWLING DRAIN. ON INVESTIGATION, THE LEAK WAS FOUND COMING FROM DAMAGED FITTING THREADS IN THE OIL PRESS REGULATOR HOUSING PN 3105735-01. HOUSING WAS REPLACED & THE ACFT WAS RETURN TO SERVICE.
- [SDR CA150518009](https://openairdocs.org/sdr/CA150518009.md): Engine · malfunctioned · Apr 24, 2015 · Dhav DHC8314 · Engine (Turbine/Turboprop)
  > (CAN) ON GND BEFORE ACFT TAKEOFF, WHEN THE PILOT PUSHED THE LEVER TO TAKEOFF POWER, THE LT ENG TORQUE DROPPED TO 0% & ENTERED INTO FEATHER POSITION. ENG WAS SHUTDOWN & RETURNED BACK TO AIRPORT UNEVENTFULLY. THE GND CREW CONFIRMED THAT THE PROPELLER COULD NOT
- [SDR CA150418001](https://openairdocs.org/sdr/CA150418001.md): Controller · odor · Apr 16, 2015 · Dhav DHC8314 · Cabin Pressure Controller
  > (CAN) ON LANDING, CAPTAIN SMELLED A BURN ODOR IN COCKPIT, FAINT. ON INSPECTION FOUND THE ODOR COMING FROM THE CABIN PRESSURE CONTROLLER. AFTER INVESTIGATION IN THE RECORD, IT`S NOT THE FIRST TIME THAT THIS PARTICULAR UNIT IS REMOVED FOR BURN ODOR. UNIT WILL
- [SDR CA150126005](https://openairdocs.org/sdr/CA150126005.md): Shroud · damaged · Jan 22, 2015 · Dhav DHC8314 · Turbine Section
  > (CAN) ENGINE WAS RETURNED TO THE SHOP DUE TO DETERIORATED CONDITION OF THE LP SHROUD SEGMENTS DISCOVERED DURING A SCHEDULED BORESCOPE INPSECTION IN THE FIELD. THE LP SHROUD SEGMENTS WERE SUBSEQUENTLY REMOVED FROM THE ENGINE AND INSPECTED AT PIECE-PART LEVEL.
- [SDR CA150113017](https://openairdocs.org/sdr/CA150113017.md): Engine · shutdown · Dec 17, 2014 · Dhav DHC8314 · Engine (Turbine/Turboprop)
  > (CAN) JUST AFTER TAKEOFF THE CREW HEARD A LOUD NOISE FROM ONE OF THE ENGINES. THE CREW CONFIRMED THAT THE ENGINE HAD AN ISSUE AND SHUT THE ENGINE DOWN. THE ACFT RETURNED TO DEPARTURE AIRPORT FOR A SAFE LANDING. THE ENGINE WAS REPLACED.
- [SDR CA141218016](https://openairdocs.org/sdr/CA141218016.md): Turbine · failed · Dec 17, 2014 · Dhav DHC8314 · Turbine Section
  > (CAN) DURING TAKE-OFF & FOLLOWING ROTATION, THE FLIGHT CREW HEARD AN UNUSUAL NOISE FROM THE NR 2 ENGINE AREA. THE FLIGHT CREW OBSERVED ENGINE INSTRUMENT INDICATIONS CONSISTENT WITH AN ENGINE FAILURE & CONDUCTED A SHUTDOWN OF THE NR 2 ENGINE IAW STANDARD OPERA
- [SDR CA141110013](https://openairdocs.org/sdr/CA141110013.md): Line · corroded · Nov 10, 2014 · Dhav DHC8314 · Airfoil Anti/De-ice System
  > (CAN) DURING A ROUTINE MAINTENANCE CHECK, TASK 7610/05 (UNRELATED TO THE ISSUE) A DE-ICE LINE WAS FOUND TO BE CORRODED UNDER THE CUSHIONED CLAMPS. THE CUSHION CLAMPS WERE WEATHERED AND HARDENED. THE DE-ICE LINE (PN 83010019-21) RUNS BETWEEN THE FUSELAGE AND TH
- [SDR CA140826022](https://openairdocs.org/sdr/CA140826022.md): Rotor · seized · Aug 16, 2014 · Dhav DHC8314 · Turbine Engine Compressor Section
  > (CAN) DURING REVENUE FLIGHT, AS A CARGO FLIGHT, DURING CLIMB CONDITION AT AROUND 16500 THE LEFT ENGINE PARAMETERS STARTED FLUCTUATING AND ENGINE SHUTDOWN BY ITSELF. NO AIR RESTART ATTEMPTED, SINCE PROP DID NOT FEATHER WHEN CLA FUEL CUT OFF POSITION SELECTED. A
- [SDR CA140818004](https://openairdocs.org/sdr/CA140818004.md): Engine · making metal · Aug 16, 2014 · Dhav DHC8314 · Engine (Turbine/Turboprop)
  > (CAN) CAPTAIN REPORTED DURING CLIMB THROUGH 16000 FEET, WAS ADJUSTING POWER LEVER AND NOTICE LEFT ITT ABOUT 40 DEGREE HIGHER THAN RIGHT ENGINE. ALSO NOTICE THAT NL START TO DROP AND THE ENGINE QUIT SUDDENTLY. AIRCRAFT LAND SAFELY. UPON PRELIMINARY INSPECTION
- [SDR CA140721010](https://openairdocs.org/sdr/CA140721010.md): Propeller · malfunctioned · Jul 9, 2014 · Dhav DHC8314 · Propeller System
  > (CAN) IT WAS REPORTED THAT THE ACFT EXPERIENCED AN UNCOMMANDED AUTOFEATHER DURING CLIMB. MORE DETAILS WERE REQUESTED TO THE CUSTOMER.
- [SDR CA140711004](https://openairdocs.org/sdr/CA140711004.md): Engine · power loss · Jul 9, 2014 · Dhav DHC8314 · Engine (Turbine/Turboprop)
  > (CAN) AFTER TAKE OFF, TORQUE INCREASED ON ENGINE NR 2 SLIGHTLY. AFTER ADJUSTING POWER LEVER, TORQUE ON NR 2 DECREASED TO ABOUT 30% AND AUTOFEATHER KICKED IN. CREW SHUT DOWN THE FEATHER ENGINE AND LAND SAFELY. FDR WAS PULL FOR DOWNLOAD AND FOUND OUT THAT THERE
- [SDR CA140526009](https://openairdocs.org/sdr/CA140526009.md): Blade · unsecure · May 24, 2014 · Dhav DHC8314 · Propeller Blade Section
  > (CAN) ACFT EXPERIENCED HEAVY VIBRATION, AND MANAGED TO LAND SAFELY AT DEPARTURE AIRPORT. ON THE GROUND, MAINTENANCE FOUND THAT LT PROPELLER BLADE WAS IN A ZERO PITCH ANGLE WHEN ALL THE OTHER WERE IN FEATHER. AFTER DISSASSEMBLY, THE PROPELLER BLADE PIN WAS FO
- [SDR CA140319007](https://openairdocs.org/sdr/CA140319007.md): Bearing · split · Mar 17, 2014 · Dhav DHC8314 · Propeller Blade Section
  > (CAN) NR 1 PROPELLER ASSY REMOVED FOR UNSCHEDULED MAINTENANCE. IT WAS DISCOVERED THAT ONE BALL BEARING WAS SPLIT IN HALF IN THE BALL RETAINER ASSY. DAMAGED BALL WAS LOCATED IN THE MIDDLE OF THE RETAINER. THE SPLIT BALL BEARING DAMAGED ADJACENT BEARING RACE,
- [SDR CA140114001](https://openairdocs.org/sdr/CA140114001.md): Fitting · cracked · Jan 12, 2014 · Dhav DHC8314 · Engine Fuel Distribution
  > (CAN) DURING REPLACEMENT OF NR 2 ENGINE ON, AN FITTING FOUND CRACKED AT TWO PLACES ON MAIN FUEL HOSE ASSY, BETWEEN ENGINE AND FIREWALL. THE COMPANY HAS INITIATED A FLEET INSPECTION AS A RESULT OF THIS FINDING.
- [SDR CA140113001](https://openairdocs.org/sdr/CA140113001.md): Actuator · failed · Dec 29, 2013 · Dhav DHC8314 · Landing Gear Retraction/Extension System
  > (CAN) DURING A ZONAL INSPECTION OF THE NR 2 NACELLE IT WAS FOUND THAT 1 OF THE 2 ASSIST SPRINGS LOCATED IN THE MLG UPLOCK ACTUATOR WAS BROKEN. THE LT MLG UPLOCK ACTUATOR WAS THEN INSPECTED AND THE SAME CONDITION, 1 OF THE 2 SPRINGS BROKEN WAS ALSO FOUND. THE
- [SDR CA131202008](https://openairdocs.org/sdr/CA131202008.md): Autofeather Sys · failed · Nov 27, 2013 · Dhav DHC8314 · Propeller Feathering/Reversing
  > (CAN) THE PILOTS REPORTED THE AUTOFEATHER FAILED TO ARM AND ELECTED TO ABORT THE TAKEOFF AND TO RETURN TO THE GATE. TROUBLESHOOTING IS ONGOING. FDR DATA WAS REQUESTED.
- [SDR CA131126007](https://openairdocs.org/sdr/CA131126007.md): Control Unit · misinstalled · Nov 25, 2013 · Dhav DHC8314 · Compressor Bleed Control
  > (CAN) DURING ROUTINE MAINTENANCE THE RIGHT HAND ENGINE P2.5/P3 SWITCHING VALVE WAS INSPECTED IAW TASK 7230/30. THIS TASK REQUIRES THE DISASSEMBLY OF THE SWITCHING VALVE IAW THE PRATT & WHITNEY MAINTENANCE MANUAL, WHICH REQUIRES A FULL DISASSEMBLY OF THE VALVE.
- [SDR CA131122002](https://openairdocs.org/sdr/CA131122002.md): Check Valve · failed · Nov 21, 2013 · Dhav DHC8314 · Passenger/Crew Doors
  > (CAN) AIR UNIT RECENTLY HAD ISSUE WITH RT TYPE 1 EMERGENCY EXIT ON ACFT, WHERE DOOR DIDN`T PROPERLY SEAL. AFTER INVESTIGATION, FOUND THAT THE PROBLEM WAS CAUSE BY THE CHECK VALVE, THAT KEEPS THE DOOR SEAL PRESSURIZED WHILE THE ACFT IS ON THE GROUND AND THE H
- [SDR CA131118024](https://openairdocs.org/sdr/CA131118024.md): Piston · broken · Nov 18, 2013 · Dhav DHC8314 · Nose/Tail Landing Gear
  > (CAN) DURING PRE-FLIGHT WALKAROUND, THE NOSE GEAR SHOCK-STRUT WAS NOTED TO BE FLAT. UPON CLOSER INSPECTION THE BOTTOM FLANGE, WHICH HAS SPANNER WRENCHING FLATS, ON THE PISTON CAP WAS FOUND CRACKED AND BROKEN OFF. THE PISTON CAP WAS REPLACED. TOTAL CYCLES ON T
- [SDR CA130911004](https://openairdocs.org/sdr/CA130911004.md): Strut · worn · Sep 9, 2013 · Dhav DHC8314 · Engine Mount Section
  > (CAN) DURING SCHEDULED ENGINE CHANGE, 1 OF THE REAR ENGINE VERTICAL STRUT WAS FOUND WITH THE BEARING WORN OUT, WAY BEYOND LIMITS. AS PRECAUTIONNARY THE COMPANY HAS INITIATE A FLEET INSPECTION AS A RESULT OF THIS FINDING.
- [SDR CA130614010](https://openairdocs.org/sdr/CA130614010.md): Connector · dirty · Jun 12, 2013 · Dhav DHC8314 · Turbine Engine System Wiring
  > (CAN) EXPERIENCED A PROBLEM WHERE NR 1 ENGINE AUTOFEATHER IN FLIGHT FOR NO REASON. CAUSE OF THE PROBLEM FOUND TO BE OIL CONTAMINATION IN ELECTRICAL CONNECTOR FOR NR 1 ENGINE TORQUE PROBE. CONNECTOR WAS REMOVED, CLEANED AND REINSTALLED. GROUND TEST CARRY OUT
- [SDR CA130606006](https://openairdocs.org/sdr/CA130606006.md): Wire · loose · May 31, 2013 · Dhav DHC8314 · Landing Gear System Wiring
  > (CAN) WHEN SELECTING GEAR DOWN ONLY 3 RED LIGHTS COME ON, NO AMBER, NO GREEN, AND THE ALL 3 GEARS PHYSICALLY DIDN`T MOVE. CREW USE THE ALTERNATE GEAR EXTENSION TO LAND SAFELY. THE PLANE WAS FERRY TO A MAIN BASE, WHERE WIRING TO THE INHIBIT SWITCH WERE FOUND LO
- [SDR CA130516006](https://openairdocs.org/sdr/CA130516006.md): Indicator · smoke · May 14, 2013 · Dhav DHC8314 · Weather Radar System
  > (CAN) CREW REPORTED ODOR OF BURNED AND SMOKE FROM THE CENTER CONSOL, WHILE IN CRUISE. CREW DECLARED EMERGENCY, AND SAFELY LAND. AFTER INSPECTION, ENGINEER FOUND WEATHER RADAR INDICATOR CAUSED THE SMOKE AND THE ODOR. A DETAIL VISUAL OF THE WIRING HAVE BEEN C/O
- [SDR CA130430018](https://openairdocs.org/sdr/CA130430018.md): Stop Fitting · cracked · Apr 28, 2013 · Dhav DHC8314 · Passenger/Crew Doors
  > (CAN) DURING MRB TASK 5310-09J AFT NR 5 DOOR STOP HAVE BEEN FOUND CRACKED.
- [SDR CA130402002](https://openairdocs.org/sdr/CA130402002.md): Switch · malfunctioned · Mar 26, 2013 · Dhav DHC8314 · Engine Oil Pressure
  > (CAN) 5 MINUTES AFTER DEPARTURE, CREW RECIEVED A 2 ENGINE OIL PRESSURE WARNING LIGHT, GAGE STILL SHOWED PRESSURE, CREW SHUTDOWN ENGINE IAW QRH, ACFT DIVERTED TO SEPT ILES DUE TO WEATHER. MAINTENANCE INSPECTED WIRING AND FOUND NO FAULT, OIL PRESSURE WARNING L
- [SDR CA121211008](https://openairdocs.org/sdr/CA121211008.md): Engine · fluctuates · Nov 24, 2012 · Dhav DHC8314 · Engine (Turbine/Turboprop)
  > (CAN) DURING FINAL APPROACH, THE PILOT OBSERVED TORQUE FLUCTUATIONS. POWER WAS ADDED BUT THERE WAS NO ENGINE RESPONSE. THE ENGINE WAS SHUTDOWN AND SECURED BEFORE AN AN UNEVENTFUL SINGLE ENGINE LANDING WAS PERFORMED. TROUBLESHOOTING IS ONGOING.
- [SDR CA121204002](https://openairdocs.org/sdr/CA121204002.md): Engine · power loss · Nov 23, 2012 · Dhav DHC8314 · Engine (Turbine/Turboprop)
  > (CAN) THE CREW REPORTED TORQUE FLUCTUATIONS. ABOUT 4 MILES OUT, THE CREW NOTED A CHANGE IN ENGINE NOISE FOLLOWED BY A SLIGHT YAW. CREW SELECTED MAX POWER BUT THE LT ENGINE DID NOT RESPOND. THE LT TORQUE GAGE SHOWED 3 DOTTED LINES ACROSS THE DIGITAL READING.
- [SDR CA120723013](https://openairdocs.org/sdr/CA120723013.md): Starter Gen · failed · Jul 23, 2012 · Dhav DHC8314 · Starter-Generator
  > (CAN) APPROX 1 HR AFTER DEPARTURE, THE PILOTS NOTICED NR 2 DC GEN WARN LIGHT CAME ON AND AFTER A MINUTE OR 2, THE NR 2 DC GEN HOT LIGHT ILLUMINATED. THE PILOTS SELECTED THE 2 DC GEN OFF IAW QRH. THE NR 2 DC GEN HOT LIGHT EXTINGUISHED APPROXIMATELY 20-25 MINUT
- [SDR CA120807003](https://openairdocs.org/sdr/CA120807003.md): Tube · disconnected · Jul 4, 2012 · Dhav DHC8314 · Aircraft Fuel Distribution System
  > (CAN) THE ACFT ORIGINAL SNAG WAS A FUEL PRESSURE CAUTION LIGHT WOULD ILLUMINATE IN FLIGHT. THE FOLLOWING ACTIONS WERE TAKEN, FUEL FILTER REPLACED, GROUND CHECKED SERVICEABLE, ON THE SUBSEQUENT FLIGHT, 15 MINUTES AFTER TAKEOFF THE CAUTION LIGHT ILLUMINATED AG
- [SDR JJBA20111008001](https://openairdocs.org/sdr/JJBA20111008001.md): Sensor · dirty · Oct 8, 2011 · N839CA · Dhav DHC8314 · Smoke Detection
  > FLIGHT CREW REPORTED BAGGAGE SMOKE DETECTOR LIGHT ILLUMINATED ON LANDING ROLL. MX CREW CLEANED SENSING COMPONENTS, PERFORMED OPS CHECK SATISFACTORY.
- [SDR JJBA20110927001A](https://openairdocs.org/sdr/JJBA20110927001A.md): Brake · broken · Sep 27, 2011 · N839CA · Dhav DHC8314 · Brake
  > DURING LINE CHECK, MX FOUND MAIN WHEEL BRAKE ROTOR IN PIECES. R & R BRAKE, PERFORMED OPS AND LEAK CHECK SATISFACTORY.
- [SDR CA110725014](https://openairdocs.org/sdr/CA110725014.md): Actuator · leaking · Jul 24, 2011 · Dhav DHC8314 · Landing Gear Actuator
  > AFTER TAKEOFF, THE LANDING GEAR WAS SELECTED UP AND THE NOSE GEAR WAS VERY SLOW TO RETRACT. THE ACFT LANDED SAFELY WITHOUT FURTHER INCIDENT. MX INVESTIGATED AND DISCOVERED THAT THE NOSE GEAR DOOR ACTUATOR PN 82910016-009 WAS THE CAUSE OF THE SLOW RETRACTION
- [SDR CA110725011](https://openairdocs.org/sdr/CA110725011.md): Light · melted · Jul 21, 2011 · Dhav DHC8314 · Flight Compartment Lighting
  > DURING FLIGHT, THE CREW NOTICED THE ODOR OF SMOKE ON THE FLIGHT DECK, A SMALL AMOUNT OF SMOKE WAS NOTICED AROUND THE OVERHEAD PANEL ON CAPTAIN SIDE. AN EMERGENCY WAS DECLARED AND THE ACFT LANDED SAFELY. MX INVESTIGATED AND FOUND THE OVERHEAD READING LIGHT ON

Next page: https://openairdocs.org/model/bombardier-dhc-8-314/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 aircraft_model_key = 'DHC8314'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/bombardier-dhc-8-314/reports

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