# Bombardier DHC-8-314 - Type: Aircraft model (FAA registry) - Registry code: 1390013 - Manufacturer (registry): BOMBARDIER INC - Model: DHC-8-314 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 ยท Turbo-prop - Seats: 61 - Weight class: 20,000 lb and over - Certification: Type certificated - Registered aircraft: 0 - Page: https://openairdocs.org/model/bombardier-dhc-8-314 Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. None matched. ## Registered aircraft None registered with this model now. ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (65, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR CA190819005](https://openairdocs.org/sdr/CA190819005), Aug 7, 2019: PIN. MELTED. (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 LIGHTNI - [SDR CA190327004](https://openairdocs.org/sdr/CA190327004), Mar 26, 2019: STARTER GEN. FAILED. (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 - [SDR CA190219003](https://openairdocs.org/sdr/CA190219003), Jan 16, 2019: OIL SYSTEM. LOW 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 PR - [SDR CA160310011](https://openairdocs.org/sdr/CA160310011), Mar 9, 2016: PUMP. FAILED. (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 HYDRA - [SDR CA160106010](https://openairdocs.org/sdr/CA160106010), Dec 24, 2015: PRECOOLER. CRACKED. (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 DETACHE - [SDR CA151221014](https://openairdocs.org/sdr/CA151221014), Dec 17, 2015: CHECK VALVE. CORRODED. (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 - [SDR CA151202010](https://openairdocs.org/sdr/CA151202010), Dec 1, 2015: ROD END. LOOSE. (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. THER - [SDR CA151130006](https://openairdocs.org/sdr/CA151130006), Nov 15, 2015: ENGINE. SMOKE. (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 - [SDR CA150923002](https://openairdocs.org/sdr/CA150923002), Sep 19, 2015: INDICATOR. LEAKING. (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 - [SDR CA150923001](https://openairdocs.org/sdr/CA150923001), Sep 19, 2015: ALTIMETER. FAULTY. (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 TRIPP - [SDR CA150910009](https://openairdocs.org/sdr/CA150910009), Sep 8, 2015: WHEEL. DETACHED. (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 PRECAUT - [SDR CA150909001](https://openairdocs.org/sdr/CA150909001), Sep 7, 2015: VENTURI. CRACKED. (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 - [SDR CA150824014](https://openairdocs.org/sdr/CA150824014), Aug 2, 2015: VALVE. LEAKING. (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 APP - [SDR CA150723003](https://openairdocs.org/sdr/CA150723003), Jul 22, 2015: SEAL. DEFLATED. (CAN) PILOT REPORTED: CABIN LOST PRESSURIZATION AT 25 000 FEETS. EMERGENCY DESCENT PERFORMED AND FLIGHT DIVERTED TO THE NEAREST AIRPORT. AIRCRAFT LANDED SUCCESS - [SDR CA150714012](https://openairdocs.org/sdr/CA150714012), Jul 13, 2015: FUEL/OIL COOLER. FAULTY. (CAN) FUEL TEMP CLIMBING TO MAX TEMP ON FUEL TEMP INDICATOR. RT FUEL TEMP AT 57 DEGREES. - [SDR CA150709003](https://openairdocs.org/sdr/CA150709003), Jul 7, 2015: ACTUATOR. INOPERATIVE. (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 PAS - [SDR CA150703003](https://openairdocs.org/sdr/CA150703003), Jun 30, 2015: MANIFOLD. BROKEN. (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 AIRCRA - [SDR CA150618001](https://openairdocs.org/sdr/CA150618001), Jun 15, 2015: REGULATOR. DAMAGED. (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 - [SDR CA150518009](https://openairdocs.org/sdr/CA150518009), Apr 24, 2015: ENGINE. MALFUNCTIONED. (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 SHU - [SDR CA150418001](https://openairdocs.org/sdr/CA150418001), Apr 16, 2015: CONTROLLER. ODOR. (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 - [SDR CA150126005](https://openairdocs.org/sdr/CA150126005), Jan 22, 2015: SHROUD. DAMAGED. (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. T - [SDR CA150113017](https://openairdocs.org/sdr/CA150113017), Dec 17, 2014: ENGINE. SHUTDOWN. (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 - [SDR CA141218016](https://openairdocs.org/sdr/CA141218016), Dec 17, 2014: TURBINE. FAILED. (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 INDICAT - [SDR CA141110013](https://openairdocs.org/sdr/CA141110013), Nov 10, 2014: LINE. CORRODED. (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 C - [SDR CA140826022](https://openairdocs.org/sdr/CA140826022), Aug 16, 2014: ROTOR. SEIZED. (CAN) DURING REVENUE FLIGHT, AS A CARGO FLIGHT, DURING CLIMB CONDITION AT AROUND 16500 THE LEFT ENGINE PARAMETERS STARTED FLUCTUATING AND ENGINE SHUTDOWN BY ITS - [SDR CA140818004](https://openairdocs.org/sdr/CA140818004), Aug 16, 2014: ENGINE. MAKING METAL. (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 - [SDR CA140721010](https://openairdocs.org/sdr/CA140721010), Jul 9, 2014: PROPELLER. MALFUNCTIONED. (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), Jul 9, 2014: ENGINE. POWER LOSS. (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. CR - [SDR CA140526009](https://openairdocs.org/sdr/CA140526009), May 24, 2014: BLADE. UNSECURE. (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 - [SDR CA140319007](https://openairdocs.org/sdr/CA140319007), Mar 17, 2014: BEARING. SPLIT. (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 - [SDR CA140114001](https://openairdocs.org/sdr/CA140114001), Jan 12, 2014: FITTING. CRACKED. (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 INITIAT - [SDR CA140113001](https://openairdocs.org/sdr/CA140113001), Dec 29, 2013: ACTUATOR. FAILED. (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 - [SDR CA131202008](https://openairdocs.org/sdr/CA131202008), Nov 27, 2013: AUTOFEATHER SYS. FAILED. (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 REQ - [SDR CA131126007](https://openairdocs.org/sdr/CA131126007), Nov 25, 2013: CONTROL UNIT. MISINSTALLED. (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 SWITCHI - [SDR CA131122002](https://openairdocs.org/sdr/CA131122002), Nov 21, 2013: CHECK VALVE. FAILED. (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 - [SDR CA131118024](https://openairdocs.org/sdr/CA131118024), Nov 18, 2013: PISTON. BROKEN. (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, - [SDR CA130911004](https://openairdocs.org/sdr/CA130911004), Sep 9, 2013: STRUT. WORN. (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 - [SDR CA130614010](https://openairdocs.org/sdr/CA130614010), Jun 12, 2013: CONNECTOR. DIRTY. (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 FO - [SDR CA130606006](https://openairdocs.org/sdr/CA130606006), May 31, 2013: WIRE. LOOSE. (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 - [SDR CA130516006](https://openairdocs.org/sdr/CA130516006), May 14, 2013: INDICATOR. SMOKE. (CAN) CREW REPORTED ODOR OF BURNED AND SMOKE FROM THE CENTER CONSOL, WHILE IN CRUISE. CREW DECLARED EMERGENCY, AND SAFELY LAND . AFTER INSPECTION, ENGINEER FOUN - [SDR CA130430018](https://openairdocs.org/sdr/CA130430018), Apr 28, 2013: STOP FITTING. CRACKED. (CAN) DURING MRB TASK 5310-09J AFT NR 5 DOOR STOP HAVE BEEN FOUND CRACKED. - [SDR CA130402002](https://openairdocs.org/sdr/CA130402002), Mar 26, 2013: SWITCH. MALFUNCTIONED. (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 - [SDR CA121211008](https://openairdocs.org/sdr/CA121211008), Nov 24, 2012: ENGINE. FLUCTUATES. (CAN) DURING FINAL APPROACH, THE PILOT OBSERVED TORQUE FLUCTUATIONS. POWER WAS ADDED BUT THERE WAS NO ENGINE RESPONSE. THE ENGINE WAS SHUTDOWN AND SECURED BEFOR - [SDR CA121204002](https://openairdocs.org/sdr/CA121204002), Nov 23, 2012: ENGINE. POWER LOSS. (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 TH - [SDR CA120723013](https://openairdocs.org/sdr/CA120723013), Jul 23, 2012: STARTER GEN. FAILED. (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 - [SDR CA120807003](https://openairdocs.org/sdr/CA120807003), Jul 4, 2012: TUBE. DISCONNECTED. (CAN) THE ACFT ORIGINAL SNAG WAS A FUEL PRESSURE CAUTION LIGHT WOULD ILLUMINATE IN FLIGHT. THE FOLLOWING ACTIONS WERE TAKEN, FUEL FILTER REPLACED, GROUND CHECKE - [SDR JJBA20111008001](https://openairdocs.org/sdr/JJBA20111008001), Oct 8, 2011: SENSOR. DIRTY. 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), Sep 27, 2011: BRAKE. BROKEN. 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), Jul 24, 2011: ACTUATOR. LEAKING. 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 - [SDR CA110725011](https://openairdocs.org/sdr/CA110725011), Jul 21, 2011: LIGHT. MELTED. 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 EMERGENC All 65: https://openairdocs.org/model/bombardier-dhc-8-314/reports.md ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Boeing Of Canada Ltd/Dehav Div DHC-8-314](https://openairdocs.org/model/boeing-of-canada-ltd-dehav-div-dhc-8-314): 0 registered aircraft, registry code 1386090 - [Dehavilland DHC-8-314](https://openairdocs.org/model/dehavilland-dhc-8-314): 0 registered aircraft, registry code 2809009 --- 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.