# Service difficulty reports: Bombardier DHC-8-315

A list on [Bombardier DHC-8-315](https://openairdocs.org/model/bombardier-dhc-8-315.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 124 reports

- [SDR 2023FA0000406](https://openairdocs.org/sdr/2023FA0000406.md): Valve · unreliable · Aug 9, 2023 · Dhav DHC8315 · Landing Gear Brake System
  > WITH #2 ENGINE RUNNING, PARKING BRAKE SET, WHILE STARING #1 ENGINE AIRCRAFT STARTED TO MOVE FORWARD MAKING CONTACT WITH GSE (TUG) ATTACHED TO STARTING POWER UNIT. AFTER COMPLETING FUNCTION CHECK WITH SYSTEM PRESSURE AT 3000PSI PRESSURE AT THE BRAKE UNIT WOULD
- [SDR 3SDR20210216006](https://openairdocs.org/sdr/3SDR20210216006.md): Stick Shaker · faulted · Jan 15, 2021 · N807MR · Dhav DHC8315 · Stall Warning System
  > DURING FLIGHT, STICK PUSHER DID NOT ACTIVATE AND DID NOT GIVE ANY INDICATION OF A SYSTEM FAILURE.
- [SDR K08R202010290001](https://openairdocs.org/sdr/K08R202010290001.md): Tscu · malfunctioned · Oct 29, 2020 · Dhav DHC8315 · Propeller System
  > A SCHEDULED FLIGHT, THE FLIGHT CREW HAD ENGINES OPERATING AND GOING THROUGH THEIR GROUND CHECKS WHEN THEY HAD THE NR 1 ENGINE FEATHERING DURING AUTO-FEATHER CHECK. INITIAL AUTO-FEATHER CHECK, THE FLIGHT CREW HAD BOTH SWITCHES, NR 1 AND NR 2 AUTO-FEATHER, IN TH
- [SDR CA190806001](https://openairdocs.org/sdr/CA190806001.md): Wire · shorted · Aug 5, 2019 · Dhav DHC8315 · Electrical Power System Wiring
  > (CAN) #1 AC GENERATOR FAILED IN FLIGHT. RESET CONDUCTED AND DID NOT WORK. GCU CHANGED. GENERATOR ALSO CHANGED.TEST OK THEN FAILED ON SUBSEQUENT START. FURTHER TROUBLESHOOTING REVEALED A SHORTED WIRE. CONNECTORS 2421-P2, P4, P5, P7 DISCONNECTED & BACKSHELLS REM
- [SDR CA191115005](https://openairdocs.org/sdr/CA191115005.md): Wire · damaged · Aug 4, 2019 · Dhav DHC8315 · Ice/Rain Protection System Wiring
  > (CAN) FROM PILOT REPORT - DURING FLARE ON LANDING, ELEVATORS JAMMED AND THE AIRCRAFT WAS NOT ABLE TO BE PITCHED UPWARDS OF 2-3 DEGREES. AIRCRAFT TOUCHED DOWN AT LOW PITCH ATTITUDE. NO CREW CO-ORDINATION PROCEDURE INITIATED BY CAPTAIN (OPERATING RIGHT HAND SEAT
- [SDR CA190725002](https://openairdocs.org/sdr/CA190725002.md): Blade · damaged · Jul 18, 2019 · Dhav DHC8315 · Engine (Turbine/Turboprop)
  > (CAN) AIRCRAFT CLIMBED TO INITIAL CRUISE AT FL190 BUT ENCOUNTERED ICING. ICING WAS BEING SHED NORMALLY BUT CREW ELECTED TO CLIMB TO AVOID IT. AS THEY CLIMBED THE AIRCRAFT SHUDDERED AND YAWED. THEY NOTED LH ENGINE ITT INCREASING AND TORQUE DECREASING, OIL PRESS
- [SDR V0XR20190723001](https://openairdocs.org/sdr/V0XR20190723001.md): Channel · corroded · May 22, 2019 · N568AW · Dhav DHC8315 · Fuselage Miscellaneous Structure
  > PAX DOOR SILL BELOW FLOOR HAVE SIGNS OF CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED THRESHOLD CHANNEL IAW SRM 51-42-05, 51-42-45, 51-40-07, AMM 20-30-06 AND RD8-53-8921 ISSUE 1 DATED 16 NOV 2006.
- [SDR CA190628009](https://openairdocs.org/sdr/CA190628009.md): Engine · deteriorated · Apr 30, 2019 · Dhav DHC8315 · Engine (Turbine/Turboprop)
  > (CAN) AIRCRAFT REPORTED STALL/SURGE AROUND 60-70% DURING ACCELERATION AND DECELERATION. PILOTS REPORTED THE DEFECT ON THE#1 ENGINE, HOWEVER UPON INVESTIGATION THE ENGINEERS REPORTED IT ON BOTH ENGINES. CUSTOMER CHECKED THE BLEED SYSTEM AND CONDUCTED A CAPPED R
- [SDR CA190409001](https://openairdocs.org/sdr/CA190409001.md): Tire · failed · Mar 10, 2019 · Dhav DHC8315 · Tire
  > (CAN) REPETITIVE DOUBLE TIRE FAILURES WITH DR26222T TIRE INSTALLED. WHILE TAXING TO THE RUNWAY FOR TAKEOFF, BOTH LEFT MAIN WHEELS FAILED(NO 1 TIRE DEFLATED AND NO 2 TIRE BURST. A PREVIOUS CASE WAS IN NOV 2015 ON ANOTHER A/C.
- [SDR CA190226003](https://openairdocs.org/sdr/CA190226003.md): Line · leaking · Feb 26, 2019 · Dhav DHC8315 · Hydraulic System, Main
  > (CAN) TOTAL LOSS OF FLUID FROM #1 HYDRAULIC SYSTEM DURING CRUISE. AIRCRAFT LANDED SAFELY AND TAXIED TO THE GATE. (SEE ALSO CASA SDR #2019611953376/611953376) (TC# 20190226003)
- [SDR CA190226011](https://openairdocs.org/sdr/CA190226011.md): Inverter · failed · Feb 22, 2019 · Dhav DHC8315 · AC Inverter
  > (CAN) PILOT REPORTED: SMOKE SMELL IN THE COCKPIT, AND WE FOUND THAT THE SOURCE OF THE SMELL WAS THE PRIMARY INVERTER. WE CURRENTLY DO NOT HAVE ACCESS TO A SERVICEABLE INVERTER, PLEASE CONFIRM THAT WE CAN FLY THE AIRCRAFT AS PER THE MEL ITEM 24-2 WITH THIS INV
- [SDR CA181119017](https://openairdocs.org/sdr/CA181119017.md): Strut · discharged · Nov 15, 2018 · Dhav DHC8315 · Nose/Tail Landing Gear Strut/Axle
  > (CAN) ON APPROACH, THE AIRCRAFT NOSE LANDING GEAR FAILED TO EXTEND UNDER NORMAL OR ALTERNATE EXTENSION. DUE TO WEATHER AND RUNWAY CONDITIONS THE AIRCRAFT THEN PROCEEDED TO ANOTHER AIRPORT NEARBY (STEPHENVILLE/YJT) WERE THEY DID AN EMERGENCY LANDING WITH THE N
- [SDR CA180208004](https://openairdocs.org/sdr/CA180208004.md): Transducer · faulty · Feb 1, 2018 · Dhav DHC8315 · Turbine Engine Oil System
  > (CAN) PILOT CARRIED OUT NR 2 ENG SHUTDOWN DUE TO LOW OIL PRESSURE INDICATION DEFECT, WAS FIXED BY REPLACING THE TRANSDUCER. THE PINS APPEARED TO BE STAINED/CONTAMINATED, SO CONTACTS WERE CLEANED. (TC NR 20180208004).
- [SDR CA160203011](https://openairdocs.org/sdr/CA160203011.md): Engine · malfunctioned · Jan 25, 2016 · Dhav DHC8315 · Engine (Turbine/Turboprop)
  > (CAN) WHILE STARTING THE ENGINES WITH INTENT TO PERFORM A TEST FLIGHT, FOLLOWING THE 500 HRS INSPECTION REQUIREMENTS, ON SELECTION OF BLEEDS TO MAX., A STRONG OIL ODOR WAS PRESENT. THE ACFT TAXIED WITH THE ODOR CONTINUING FOR A FURTHER 5 MINUTES. THE CREW TRI
- [SDR CA151216002](https://openairdocs.org/sdr/CA151216002.md): Warning Light · illuminated · Dec 2, 2015 · Dhav DHC8315 · Central Warning
  > (CAN) CUSTOMER REPORTED A FUEL BY-PASS INDICATION IN COCKPIT AND POWER FLUCTUATIONS. THE CREW ELECTED TO PERFORM A COMMANDED IFSD.
- [SDR CA151130020](https://openairdocs.org/sdr/CA151130020.md): Unknown · odor · Nov 19, 2015 · Dhav DHC8315 · Air Distribution System
  > (CAN) DURING CLIMB PASSING 2,800, AS THE BLEEDS WERE TURNED ON, AN OIL ODOR IN THE COCKPIT. THE CREW CONTINUED THE CLIMB TO 8,000, BLEEDS WERE TURNED OFF AND THE CABIN WAS VENTILATED THROUGH RAM AIR. THE CREW ELECTED TO RETURN TO THE DEPARTURE AIRPORT WHERE
- [SDR CA151030004](https://openairdocs.org/sdr/CA151030004.md): Compressor · contaminated · Oct 19, 2015 · Dhav DHC8315 · Turbine Engine Compressor Section
  > (CAN) THIS ENGINE HAS HAD REPEAT EVENTS OF OIL ODOR IN CABIN, THE 1ST EVENT TROUBLESHOOTING IDENTIFIED OIL AROUND THE HIGH PRESSURE COMPRESSOR. MAINTENANCE ACTIONS WERE TAKEN AND THE ACFT FLEW A 2HRS TEST FLIGHT WITHOUT ANY ISSUES AND WAS RELEASED FOR SERVICE.
- [SDR CA151006003](https://openairdocs.org/sdr/CA151006003.md): Unknown · odor · Sep 21, 2015 · Dhav DHC8315 · Air Distribution System
  > (CAN) OIL ODOR IN THE CABIN OCCURRED ON CLIMBOUT FROM TRANSIENT ALTITUDE. ALL CREW MEMBERS WENT ON OXYGEN TO THE DESTINATION. ACFT LANDED UNEVENTFULLY. TROUBLESHOOTING ONGOING.
- [SDR CA150828004](https://openairdocs.org/sdr/CA150828004.md): Blades · missing · Jul 7, 2015 · Dhav DHC8315 · Turbine Section
  > (CAN) CUSTOMER JUST REPORTED THAT THEY HAD IFSD EVENT ON NR 2 ENGINE DURING CRUISE. ENGINE WAS SENT FOR HSI & INVESTIGATION. HEAVY DAMAGES WERE FOUND IN HOT SECTION GAS PATH. ALL HPT BLADES WERE MISSING WITH ONLY BLADE PLATFORM REMAINING. THIS CAUSED SUBSTAN
- [SDR CA150629006](https://openairdocs.org/sdr/CA150629006.md): Engine · odor · Jun 19, 2015 · Dhav DHC8315 · Engine (Turbine/Turboprop)
  > (CAN) WHILE ON A SURVEILLANCE MISSION, SURVEILLANCE CREW REPORTED INTERMITTENT OIL SMELL IN THE CABIN WITH CRUISE POWER AT 60% TORQUE. PILOTS WERE NOTIFIED & POWER ADJUSTED TO 65%, AIR QUALITY IMPROVED. NO SMELL WAS EVIDENT IN THE COCKPIT. MISSION WAS COMPL
- [SDR CA150519008](https://openairdocs.org/sdr/CA150519008.md): Oil System · odor · Apr 30, 2015 · Dhav DHC8315 · Turbine Engine Oil System
  > (CAN) THE CREW EXPERIENCED AN OIL SMELL IN CABIN EVENT. THE EVENT OCCURRED PRIOR TO TAKEOFF, WHEN THE ENG POWER LEVER WAS MOVED FROM BELOW FLIGHT IDLE INTO DISK. THE CREW REGARDED THIS EVENT AS SEVERAL. CREW WERE SENT TO HOSPITAL FOR CHECKS. MFG WILL INVES
- [SDR 2015FA0000147](https://openairdocs.org/sdr/2015FA0000147.md): Collar · cracked · Apr 17, 2015 · N806MR · Dhav DHC8315 · Nacelle/Pylon, Main Frame
  > DURING VISUAL INSPECTION OF LT NACELLE HORSE COLLAR ASSY FOUND A 1.1250 CRACK DAMAGE ON FORWARD OUTER ANGLE, DAMAGE CRACK WAS REPORTED TO MFG HELP DESK. MFG PROVIDED A PERMANENT REPAIR FOR THIS CRACK DAMAGE ON THE LT NACELLE HORSE COLLAR.
- [SDR 2015FA0000153](https://openairdocs.org/sdr/2015FA0000153.md): Angle · cracked · Mar 12, 2015 · N807MR · Dhav DHC8315 · Nacelle/Pylon Miscellaneous Structure
  > DURING ENGINE REMOVAL FOR HSI AN INSPECTION OF THE NACELLE AREA WAS CONDUCTED PER THE OEM, WE NOTICED BOTH LEFT AND RIGHT ENGINE FRONT NACELLE HORSE COLLAR LOWER LEFT AND RIGHT ANGEL 20MM AND 22MM CRACKED AT THE BEND RADIUS HORIZONTALITY, THE REPAIR WAS MADE
- [SDR 2015FA0000152](https://openairdocs.org/sdr/2015FA0000152.md): Angle · cracked · Feb 28, 2015 · N808MR · Dhav DHC8315 · Nacelle/Pylon Miscellaneous Structure
  > DURING ENGINE CHANGE AND INSPECTION OF THE NACELLE AREA NOTICED A ONE INCH CRACK ON THE HORSE COLLAR BOTTOM LEFT SIDE AT THE OUTER ANGEL OF THE ENGINE NACELLE HORSE COLLAR ASSY THE CRACK RAN AT THE ANGLE BEND HORIZONTALITY, THE REPAIR WAS MADE IAW DRAWING RIGH
- [SDR CA150217008](https://openairdocs.org/sdr/CA150217008.md): Warning Light · illuminated · Feb 14, 2015 · Dhav DHC8315 · Hydraulic Pump (Electric/Engine), Main
  > (CAN) DIVERSION DUE TO NR 2 HYD PUMP CAUTION LIGHT ILLUMINATED.
- [SDR CA150109005](https://openairdocs.org/sdr/CA150109005.md): Outflow Valve · failed · Jan 8, 2015 · Dhav DHC8315 · Pressure Regulator/Outflow Valve
  > (CAN) INITIAL REPORT INDICATED PRESSURIZATION SYSTEM WAS NOT WORKING AND CABIN WAS TOO COLD. NO CONTROL WITH AUTO OR MAN. NO FAULT INDICATION. TEMPORARY CONTROL GAINED AFTER SWITCHING BLEEDS OFF THEN ON BUT PROBLEM CONTINUED. CABIN TEMPERATURE WAS LOW AND VENT
- [SDR CA141229011](https://openairdocs.org/sdr/CA141229011.md): Pitot Tube · cracked · Dec 28, 2014 · Dhav DHC8315 · Pitot/Static System
  > (CAN) FLIGHT DIVERTED DUE TO ROLL OB SPOILER CAUTION LIGHT. MAINTENANCE FOUND THAT BOTH PITOT ACCUMULATORS WERE FULL TO THE TOP WITH WATER. CARRIED OUT A LEAK CHECK AND FOUND EXCESSIVE LEAKING ON PITOT NR 1. INSPECTED EACH PITOT CONNECTIONS TO FIND THE SOURCE
- [SDR CA141229009](https://openairdocs.org/sdr/CA141229009.md): Engine · making metal · Dec 28, 2014 · Dhav DHC8315 · Engine (Turbine/Turboprop)
  > (CAN) CAPTAIN REPORTED SMOKE IN THE FLIGHT DECK AND DIVERTED, NO INCIDENTS UPON LANDING. MAINTENANCE PERSONNEL AFTER INVESTIGATION FOUND CODE 939 RGB CHIP DETECT FAIL ON NR 2 ENGINE. CHIP DETECTOR INSPECTED AND METAL FOUND. AIRCRAFT REMOVED FROM SERVICE UNTI
- [SDR CA141229007](https://openairdocs.org/sdr/CA141229007.md): Pushrod · disconnected · Dec 24, 2014 · Dhav DHC8315 · Landing Gear Door Retract Section
  > (CAN) FOLLOWING TAKEOFF, THE LH FWD MLG DOOR DID NOT CLOSE. THERE WAS NO FLIGHT DECK INDICATION BUT THE DOOR WAS VISUALLY CONFIRMED TO BE OPEN. THE AIRCRAFT RETURNED TO THE POINT OF DEPARTURE AND LANDED NORMALLY. UPON INSPECTION, IT WAS DISCOVERED THAT THE PUS
- [SDR CA141223003](https://openairdocs.org/sdr/CA141223003.md): Pump · leaking · Dec 22, 2014 · Dhav DHC8315 · Hydraulic Pump (Electric/Engine), Main
  > (CAN) FLIGHT CREW CARRIED OUT AN INFLIGHT TURN AROUND DUE TO NR 1 HYDRAULIC ISOLATION CAUTION LIGHT ILLUMINATED AFTER DEPARTURE, NR 1 HYDRAULIC QUANTITY INDICATED 5%. AFTER INTENSIVE TROUBLE SHOOTING PERFORMED BY MAINTENANCE PERSONNEL IT WAS DETERMINED THAT T
- [SDR CA141211001](https://openairdocs.org/sdr/CA141211001.md): Coffeemaker · overheated · Dec 10, 2014 · Dhav DHC8315 · Buffet/Galleys
  > (CAN) IN CRUISE FLIGHT THE FA REPORTED A SMOKE SMELL FROM THE GALLEY AREA. THE GALLEY CB WERE PULLED & THE SMELL DISSIPATED. THE AIRCRAFT CONTINUED TO DESTINATION. IT WAS DETERMINED THAT THE RIGHT COFFEE BREWER WAS OVERHEATING, THE RIGHT COFFEE BREWER WAS RE
- [SDR CA141211003](https://openairdocs.org/sdr/CA141211003.md): Union · leaking · Dec 9, 2014 · Dhav DHC8315 · Hydraulic System, Main
  > (CAN) HYDRAULIC FLUID WAS NOTED ON THE AIRCRAFT IN THE VICINITY OF THE NOSE LANDING GEAR. MAINTENANCE INSPECTION CONFIRMED THAT THE LEAK WAS COMING FROM THE NLG LOCK ACTUATOR ASSEMBLY. BOTH UNIONS ON THE ACTUATOR WERE FOUND LOOSE & WERE TIGHTENED. ONE FLEX
- [SDR CA150113011](https://openairdocs.org/sdr/CA150113011.md): Engine · power loss · Dec 5, 2014 · Dhav DHC8315 · Engine (Turbine/Turboprop)
  > (CAN) THE NR 2 ENGINE WAS NOT ABLE TO DEVELOP POWER ON TAKEOFF ROLL. MAXIMUM OF 45 PERCENT TORQUE ACHIEVEABLE. TAKEOFF ABORTED AND ACFT RETURNED TO RAMP. MFC AND FUEL PUMP REPLACED AND ACFT RETURNED TO SERVICE.
- [SDR CA141210003](https://openairdocs.org/sdr/CA141210003.md): Pin · grounded · Dec 4, 2014 · Dhav DHC8315 · Electrical Power System Wiring
  > (CAN) WHILE CLIMBING FLIGHT CREW RECEIVED A NR 2 AC BUSS CAUTION LIGHT THROUGH ABOUT FL 240, AND THEN THE RH AC BUS CAUTION LIGHT ALSO CAME ON. FLIGHT CREW COMPLETED THE AC GEN CAUTION LIGHT CHECKLIST AND THE BOTH LIGHTS WENT OUT AND CAME BACK ON. FLIGHT CREW
- [SDR CA141125002](https://openairdocs.org/sdr/CA141125002.md): Shutoff Valve · unknown · Nov 24, 2014 · Dhav DHC8315 · Cabin Pressure Control System
  > (CAN) DURING CLIMB THROUGH FL 130 CREW ENCOUNTERED PRESSURIZATION PROBLEM. AT ONE POINT PRESSURIZATION SEEMED STABILIZED BUT CABIN STARTED TO RISE AGAIN. AIRCRAFT RETURNED TO FIELD. MAINTENANCE REPLACED THE LH NAPRSOV DUE TO FAULT CODES 1006 & 1007. PRESSU
- [SDR CA141008015](https://openairdocs.org/sdr/CA141008015.md): Engine · odor · Sep 30, 2014 · Dhav DHC8315 · Engine (Turbine/Turboprop)
  > (CAN) WHILE ON A NON-REVENUE FLIGHT (NO PASSENGERS)Ï¿½THE LAV SMOKE DETECTOR SOUNDED WITH NO SMOKE OR ODOR APPARENT TO THE FLIGHT CREW. MAINTENANCE INVESTIGATED AND DISCOVERED THERE WAS AN OILY ODOR COMING FROM THE #1 ENGINE BLEED AIR SYSTEM AND WERE ABLE TO D
- [SDR CA141010002](https://openairdocs.org/sdr/CA141010002.md): Engine · leaking · Sep 20, 2014 · Dhav DHC8315 · Turbine Engine Oil System
  > THE ACFT DEPARTED, JUST AFTER ROTATION THE COCKPIT AND CABIN WERE FILLED WITH SMOKE, AN EMERGENCY WAS DECLARED AND THE ACFT EVACUATED ON THE RAMP. THE ACFT WAS TOWED BACK TO THE GATE. THE ON GROUND TROUBLESHOOTING REVEALED AN AIRFRAME PART WAS LEAKING OIL SO I
- [SDR CA140922010](https://openairdocs.org/sdr/CA140922010.md): Acm · failed · Sep 20, 2014 · Dhav DHC8315 · Cabin Cooling System
  > (CAN) AIRCRAFT EXPERIENCED SMOKE IN THE CABIN AND COCKPIT IMMEDIATELY UPON TAKEOFF FROM THE AIRPORT. AN INSPECTION OF THE AIRCRAFT AND SYSTEMS DETERMINED THAT THE SMOKE WAS CAUSED BY A FAULT WITH THE AFT AIR CYCLE MACHINE (ACM). THE OIL LEVEL WAS FOUND TO BE
- [SDR CA141212008](https://openairdocs.org/sdr/CA141212008.md): Bracket · cracked · Jun 25, 2014 · Dhav DHC8315 · Drag Control System
  > (CAN) BRACKET FOUND CRACKED.
- [SDR CA140630004](https://openairdocs.org/sdr/CA140630004.md): Autofeather Sys · malfunctioned · Jun 15, 2014 · Dhav DHC8315 · Propeller Feathering/Reversing
  > (CAN) DURING TAKEOFF ROLL, THE AUTOFEATHER SYS DID NOT ARM UPON SETTING TAKEOFF POWER. THE TAKEOFF WAS ABORTED AND THE ACFT RETURNED TO THE GATE. TROUBLESHOOTING LED TO THE REPLACEMENT OF THE AUTOFEATHER UNIT BEFORE THE ACFT WAS RETURNED TO SERVICE.
- [SDR 2014FA0000318](https://openairdocs.org/sdr/2014FA0000318.md): Stringer · cracked · May 14, 2014 · N807MR · Dhav DHC8315 · Fuselage Main, Longeron/Stringer
  > INSPECTED ACFT AND FOUND NO CRACKS IN THE FS 222.0 AND 252.30 OUTSIDE SKIN, FOUND THE FORWARD AND AFT STRINGERS IN THE INTERNAL STRUCTURE THAT SUPPORTS THE ANTENNA WERE CRACKED. THIS ACFT IS MODIFIED FOR SPECIAL MISSION MARITIME PATROL WITH A CAMERA MOUNTED
- [SDR 2014FA0000317](https://openairdocs.org/sdr/2014FA0000317.md): Stringer · cracked · May 14, 2014 · N808MR · Dhav DHC8315 · Fuselage Main, Longeron/Stringer
  > A POSSIBLE PRESSURIZATION ISSUE, INSPECTED THE VHF ANTENNA FOR POSSIBLE EXTERNAL SKIN CRACKS IN THE PRESSURE VESSEL AND FOUND NO CRACKS IN THE BS 222 - 252.3 OUTSIDE SKIN, FOUND THE FORWARD AND AFT STRINGERS IN THE INTERNAL STRUCTURE THAT SUPPORTS THE ANTENN
- [SDR 2014FA0000316](https://openairdocs.org/sdr/2014FA0000316.md): Skin · cracked · May 14, 2014 · N806MR · Dhav DHC8315 · Fuselage Main, Plate/Skin
  > ACFT EXPERIENCED PRESSURIZATION PROBLEM, MECHANIC CHECKED FUSELAGE DRAIN SEAL UNDER THE BELLY, DISCOVERED A LARGE CRACK IN THE SKIN BETWEEN BS 222 - 252.3. ALSO FOUND CRACK DAMAGE IN THE SKIN AROUND NR 2 VHF ANTENNA BASE FRAME, LOCATED AT THE CENTER LOWER FU
- [SDR 2014FA0000315](https://openairdocs.org/sdr/2014FA0000315.md): Stringer · cracked · May 14, 2014 · N807MR · Dhav DHC8315 · Fuselage Main, Longeron/Stringer
  > POSSIBLE PRESSURIZATION ISSUE ON ACFT, INSPECTED THE VHF ANTENNA FOR POSSIBLE EXTERNAL SKIN CRACKS IN THE PRESSURE VESSEL, FOUND NO CRACKS IN THE OUTSIDE SKIN BS 222-252.3, FOUND THE FORWARD AND AFT STRINGERS IN THE INTERNAL STRUCTURE THAT SUPPORTS THE ANTEN
- [SDR CA140211007](https://openairdocs.org/sdr/CA140211007.md): Starter Gen · shorted · Feb 1, 2014 · Dhav DHC8315 · Starter-Generator
  > (CAN) DURING MAINTENANCE TROUBLESHOOTING OF APU GENERATOR DEFECT THE STARTER/GENERATOR DEVELOPED AN INTERNAL SHORT OVERHEATED AND CAUGHT FIRE. THE FIRE WAS EXTINGUISHED WITH NO COLLATERAL DAMAGE TO THE APU OR SURROUNDING STRUCTURE.
- [SDR CA140109005](https://openairdocs.org/sdr/CA140109005.md): Check Valve · leaking · Jan 3, 2014 · Dhav DHC8315 · Hydraulic System, Main
  > (CAN) WHILE ON THE GROUND AT THE AIRPORT TERMINAL THE FLIGHT CREW STARTED THE ENGINES AND NOTICED THAT THE NR 2 HYDRAULIC SYS FLUID HAD DEPLETED. THE RELATED HYDRAULIC PRESSURE INDICATIONS ALSO ILLUMINATED. THE FLIGHT CREW SHUTDOWN THE ENGINES, ONCE THE FLIGH
- [SDR CA130909010](https://openairdocs.org/sdr/CA130909010.md): Propeller · leaking · Sep 5, 2013 · Dhav DHC8315 · Propeller Assembly
  > (CAN) DURING ACFT TURN-AROUND FLIGHT CREW NOTICED LARGE AMOUNT OF ENGINE OIL AROUND THE LT PROPELLER & FWD ENGINE COWLS. SUBSEQUENT INVESTIGATION BY MAINTENANCE FOUND THE OIL EMANATING FROM THE NR 3 BLADE SEAL AREA. UPON REMOVAL OF THE BLADE ASSY IT THE BLAD
- [SDR CA130705002](https://openairdocs.org/sdr/CA130705002.md): Rotor · broken · Jul 4, 2013 · Dhav DHC8315 · Landing Gear Brake System
  > (CAN) DURING A WHEEL ASSEMBLY REPLACEMENT THE AME FOUND NR 3 & NR 4 BRAKE ASSY ROTATIONAL DISKS, ROTOR, BROKEN, NR 3 HAD 2 AND NR 4 HAD 1 BROKEN DISK. BRAKE ASSY WEAR PIN INDICATED BOTH BRAKES TO BE SERVICEABLE.
- [SDR CA130416010](https://openairdocs.org/sdr/CA130416010.md): Oil System · low pressure · Apr 3, 2013 · Dhav DHC8315 · Engine Oil Indicating System
  > (CAN) DURING REVENUE FLIGHT, THE ACFT WAS IN CLIMB WHEN PILOTS GOT A LOW OIL PRESSURE WARNING FOLLOWED BY A DROP IN OIL PRESSURE ON THE INDICATOR. WHEN THE PRESSURE DROPPED BELOW 50 PSI, THE PILOTS PERFORMED A COMMANDED IFSD AND CONTINUED TO THE PLANNED DESTI
- [SDR CA130404006](https://openairdocs.org/sdr/CA130404006.md): Oil System · leaking · Apr 2, 2013 · Dhav DHC8315 · Turbine Engine Oil System
  > (CAN) IN CLIMB, THROUGH 15,000 FT CREW GOT NR 2 ENG OIL PRESSURE MASTER CAUTION ANNUNCIATOR. THEY OPERATED AT FLIGHT IDLE IAW QRH UNTIL OIL PRESSURE STARTED TO DECREASE BELOW 50 PSI. ENGINE RT WAS THEN SHUTDOWN IN FLIGHT. ENGINE LOST 9 QUARTS OF OIL. FOUND

Next page: https://openairdocs.org/model/bombardier-dhc-8-315/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 = 'DHC8315'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/bombardier-dhc-8-315/reports

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