Boeing DHC-8-102

Service difficulty reports · 9,272

Newest first. General aviation reporting is voluntary.

Query with SQL
duckdb -csv -c "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 = 'DHC8102'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR HNAA2014052700164Actuator · false indicationNOSE RED UNSAFE AND GEAR HANDLE LIGHTS ILLUMINATED ON NORMAL GEAR EXTENSION. GEAR WARNING HORN SOUNDED, CYCLE GEAR AND RED UNSAFE LIGHT ILLUMINATED. USED ALTERNATE EXTENSION AND OPS CHECKED GOOD. R & R NOSE GEAR DRAG STRUT ACTUATOR IAW MM 32-30-36, LUBED PMay 27, 2014 · N805EX · Dhav DHC8102 · Landing Gear ActuatorSDR CA140603001Connector · damaged(CAN) FLIGHT CREW SELECTED GEAR DOWN AND DID NOT HAVE A GEAR DOWN INDICATION FOR THE LT MAIN. OPEN DOOR TO ACCESS THE EMERGENCY EXTENSION PUMP AND HAD 3 GREEN INDICATED. MAINTENANCE FOUND THAT PIN 2 HAD MIGRATED FROM CONNECTOR 3261-J17. REPLACE CONNECTOR ANMay 24, 2014 · Dhav DHC8102 · Landing Gear System WiringSDR HNAA2014052300162Pcu · failedNR 2 PROPELLER OVERSPEED DURING TAKE OFF ROLL. ABORTED TAKEOFF. 1215 RPM FOR APPROXIMATELY 2 SECONDS. R & R NR 2 PCU IAW 61-10-01, 76-00-01Q AND 72-00-10Q.May 23, 2014 · N810EX · Dhav DHC8102 · Propeller Controlling SystemSDR HNAA2014052100161Indicator · false indicationCAPTAIN'S AIRSPEED INDICATOR SHOWED READING IN EXCESS OF ACTUAL AIRSPEED AND ON GROUND, INDICATOR SHOWS 240 KNOTS. R & R CAPTAIN'S AIRSPEED INDICATOR. TESTED GOOD IAW 34-11-00.May 21, 2014 · N810EX · Dhav DHC8102 · Airspeed/Mach IndicatorSDR HNAA2014052100160Bulb · weakLEFT AFT EXTERNAL FUSELAGE EMERGENCY LIGHT IS DIM. R & R BULB, OPS CHECKED GOOD.May 21, 2014 · N815EX · Dhav DHC8102 · Emergency LightingSDR CA140520002Actuator · failed(CAN) DURING FLAP SYS RIGGING 1 OF THE FLAP ACTUATOR, LT OTBD POSITION WAS DIFFICULT TO TURN, EXCESSIVE FORCE WAS REQUIRED TO ROTATED EITHER THE INPUT OR THE OUTPUT SPLINES, ALSO AT SOME POINT IT FEEL LIKE IT HAS INTERNAL LOOSE BETWEEN THE GEARS.May 20, 2014 · Dhav DHC8102 · Trailing Edge Flap ActuatorSDR HNAA2014051900158Bulb · inoperativeREAR EMERGENCY LIGHT ON LT FUSELAGE IS INOPERATIVE. R & R LIGHT BULB. OPS CHECKED GOOD.May 19, 2014 · N942HA · Dhav DHC8102 · Emergency LightingSDR HNAA2014051900157Skin · damagedONE BURNED RIVET ON LT FUSELAGE SKIN 6.0" AFT OF VERTICAL FRONT BETWEEN STR 25A-26A. REMOVED RIVET AND BLENDED AREA. REMAINING .35" DEEP. REPAIRED IAW EO8-53-14-0224, EA 25-2014-150, REV A.May 19, 2014 · N933HA · Dhav DHC8102 · Fuselage Main, Plate/SkinSDR HNAA2014051900156Static Wick · burnedLEFT ELEVATOR OTBD STATIC WICK BURNED OFF AND MOUNTING PLATE DAMAGED. REMOVED OTBD END CAP, INSTALLED NEW END CAP, STATIC WICK AND MOUNTING PLATE IAW DWG 85520002 AND PREVIOUS REPAIR EA01-09126.May 19, 2014 · N933HA · Dhav DHC8102 · Pitot/Static SystemSDR HNAA2014051600155Brake Assy · malfunctionedDURING TAXI, WHEN BRAKES WERE APPLIED, ACFT SHOOK AND SHUTTERED. SEEMED TO BE FROM LT BRAKE ASSY WITH AND WITHOUT ANTI-SKID ON. R & R BRAKE ASSY. OPS CHECKED GOOD IAW WC 32-10-03I AND 32-42-11X.May 16, 2014 · N937HA · Dhav DHC8102 · Landing Gear Brake SystemSDR HNAA2014051400154Light · inoperativeRED FLOOR EMERGENCY LIGHT IS INOPERATIVE. R & R EMERGENCY LIGHT. OPS CHECKED GOOD.May 14, 2014 · N809EX · Dhav DHC8102 · Emergency LightingSDR HNAA2014051400153Socket · damagedOVERHEAD LIGHT AT ROW 4DF IS SPARKED AND SMOKED. CREW POWERED DOWN ACFT. OVERHEAD LIGHTS AND CIRCUIT BREAKER DEACTIVATED. INSPECTED OVERHEAD LIGHTING FOUND ONE SOCKET AT 4DF DAMAGED. REMOVED BULB IAW SP 33.1 AND DEACTIVATED SYSTEM.May 12, 2014 · N810EX · Dhav DHC8102 · Passenger Compartment LightingSDR HNAA2014051200152Unknown · odorODOR IN CABIN, OPERATED ENGINE BLEEDS IN VARIOUS MODES. NO ODOR.May 12, 2014 · N809EX · Dhav DHC8102 · Air Distribution SystemSDR CA140506009Oil Cooler · leaking(CAN) CREW SNAGGED THE ACFT WITH "RIGHT OIL LEAK". MAINTENANCE CHECKS FOUND THE OIL COOLER LEAKING FROM THE INBD SIDE AT THE BOTTOM OF THE FINS WHERE THEY MEET THE BASE. REPLACED RT ENGINE OIL COOLER.May 5, 2014 · Dhav DHC8102 · Engine Oil CoolerSDR HNAA2014050500149Light · missingRED FLOOR EMERGENCY LIGHT MISSING. INSTALLED RED FLOOR LIGHT MODULE. OPS CHECKED GOOD. OK FOR SERVICE.May 5, 2014 · N815EX · Dhav DHC8102 · Emergency LightingSDR CA140507004Pulley · seized(CAN) DURING ROUTINE RAMP INSPECTION AND WHILE OPERATING THE MLG ALTERNATE RELEASE HANDLE IN THE COCKPIT, THE ENGINEER FELT THE HANDLE WAS NOT COMING OUT AS USUAL. TROUBLESHOOTING REVEALED THAT THE LT MLG FORWARD DOOR ACTUATOR END PULLEY WAS SEIZED, NOT ALLOWIMay 3, 2014 · Dhav DHC8102 · Landing Gear Retraction/Extension SystemSDR CA140505014Control Cable · misrouted(CAN) WHILE PERFORMING A VISUAL INSPECTION IN THE FLIGHT COMPARTMENT UNDER FLOOR, AME TECH NOTICED MISROUTED CABLES BETWEEN AILERON AUTO-PILOT SERVO AND AILERON CABLES, BOTH SYS CABLES WERE MAKING CONTACT BETWEEN EACH OTHER, CHAFING. WHEN PERFORMING SUCH MAINMay 2, 2014 · Dhav DHC8102 · Aileron Control SystemSDR HNAA2014050200147Bulb · inoperativeLEFT AFT FUSELAGE EXTERIOR EMERGENCY LIGHT IS DIM. R & R BULB, AT LOCATION, OPS CHECKED GOOD.May 2, 2014 · N942HA · Dhav DHC8102 · Emergency LightingSDR HNAA2014050200146Relay · malfunctionedAFTER TAKEOFF, NOSE GEAR RED UNSAFE LIGHT REMAINED ON AFTER SELECTED UP. R & R RELAY 3261-510.May 2, 2014 · N912HA · Dhav DHC8102 · Landing Gear Retraction/Extension SystemSDR HNAA2014050200144Transceiver · intermittentWEATHER RADAR INTERMITTENT WITH ANT-FLIGHT MESSAGE. R & R WEATHER RADAR R/T IAW MM 34-41-04. OPS CHECKED GOOD, OK FOR SERVICE.May 2, 2014 · N912HA · Dhav DHC8102 · Weather Radar SystemSDR HNAA2014043000142Boot · damagedEVIDENCE OF BIRDSTRIKE UNDER RT HORIZONTAL STABILIZER. PERFORMED BIRDSTRIKE INSPECTION, FUSELAGE TO NACELLE DE-ICE BOOT HAS 2 SMALL HOLES AND SMALL CUT TO REMOVE REMAINS. NO OTHER DEFECTS FOUND.Apr 30, 2014 · N804EX · Dhav DHC8102 · Airfoil Anti/De-ice SystemSDR HNAA2014042800141Skin · debondedSKIN DISBONDING AROUND PREVIOUS REPAIR. FABRICATED REPLACEMENT SKIN IAW OEM DG 85220498, DRILLED, DEBURRED AND PRIMED IAW EO8-52-11-0439.Apr 28, 2014 · N804EX · Dhav DHC8102 · Emergency ExitsSDR HNAA2014042800140Beam · crackedAFTER CENTER FRAME BETWEEN 1ST AND 2ND BEAM MEMBER IS CRACKED AT FWD RT SIDE. R & R NEW AFT CENTER FRAME MEMBER IAW DWG 852200055.Apr 28, 2014 · N804EX · Dhav DHC8102 · Fuselage Main, StructureSDR HNAA2014042800139Beam · crackedSECOND BEAM MEMBER IS CRACKED BELOW WINDOW AT SEVERAL LOCATIONS AROUND RIVETS. R & R UPPER AND LOWER SECTION OF BEAM IAW 85220005.Apr 28, 2014 · N804EX · Dhav DHC8102 · Fuselage Main, StructureSDR HNAA2014042800138Beam · crackedUPPER BEAM MEMBER IS CRACKED ABOVE WINDOW IN SEVERAL LOCATION, AFT SECTION. R & R LOWER SECTION OF UPPER BEAM IAW DWG 8520005.Apr 28, 2014 · N804EX · Dhav DHC8102 · Fuselage Main, StructureSDR CA140506008Oil Cooler · leaking(CAN) THE OIL PRESSURE LIGHT FOR THE RT ENGINE FLASHED TWICE, FOLLOWED BY A RAPID DROP TO ZERO ON THE OIL PRESSURE GAUGE. IMMEDIATELY CARRIED OUT THE ENGINE SHUTDOWN DRILL FOR THE NR 2 ENGINE. ONCE IT WAS SECURED AND FEATHERED DECLARED AN EMERGENCY. LANDED Apr 25, 2014 · Dhav DHC8102 · Engine Oil CoolerSDR HNAA2014042400137Wire · brokenNR 2 ENGINE OIL PRESSURE FLUXUATED BETWEEN 50-60 PSI DURING CRUISE FLIGHT. REDUCE POWER, PRESSURE STABILIZES AT 50 PSI. SWAPPED GAUGES, NO FIX. FOUND BROKEN WIRE AT OIL PRESSURE TRANSMITTER, REPLACED PINS IN OIL PSI TRANSMITTER C/P. RAN ACFT, OPS CHECKED Apr 24, 2014 · N935HA · Dhav DHC8102 · Engine Oil System WiringSDR CA140423008Actuator · cracked(CAN) DURING GROUND RUNS FOR UNRELATED MAINTENANCE WORK, IT WAS NOTED THAT THE LT OTBD SPOILER WAS NOT MOVING. MAINTENANCE DISCOVERED THAT THE LT OTBD ACTUATOR HOUSING HAD FRACTURED AT THE END CAP RESULTING IN A LEAK. THE ACTUATOR WAS REPLACED IAW THE AMM, PNApr 23, 2014 · Dhav DHC8102 · Drag Control ActuatorSDR CA140429005Housing · cracked(CAN) TAXIING FOR TAKEOFF, GOING THROUGH THE TAKEOFF CHECKLIST AND SELECTING THE FLIGHT TAXI SWITCH TO FLIGHT, THE RT OTBD SPOILER WOULD NOT DEPLOY UPWARDS. CREW RETURNED TO TERMINAL AND CONTACTED MAINTENANCE. MAINTENANCE INSPECTED THE PLANE AND CONFIRMED THApr 22, 2014 · Dhav DHC8102 · Drag Control ActuatorSDR HNAA2014042100136Smoke Detector · malfunctionedSMOKE WARNING LIGHT ILLUMINATED WITH NO EVIDENCE OF SMOKE. R & R NR 2 BAG BAY SMOKE DETECTOR. OPS CHECKED GOOD.Apr 21, 2014 · N931HA · Dhav DHC8102 · Smoke DetectionSDR HNAA2014042100135Bulb · dimEMERGENCY CEILING LIGHT DIM AT ROW 1AND 3. R & R EMERGENCY EMERGENCY CEILING LIGHT BULBS AT ROW 1 AND 3. OPS CHECKED GOOD.Apr 21, 2014 · N815EX · Dhav DHC8102 · Emergency LightingSDR ERAA201404210021Skin · crackedLEFT AILERON LOWER SKIN FOUND CRACKED AT AFT EDGE AROUND OTBD SPRING TAB HINGE AT SAT YW 47. REPAIR WITH PATCH AT AFT EDGE AROUND OTBD SPRING TAB HINGE AREA YW 471 IAW RD 8-27-017 REV 2.Apr 21, 2014 · N891EA · Dhav DHC8102 · AileronsSDR ERAA201404190020Skin Panel · dentedDENT DAMAGE TO AFT FUSELAGE LOWER SKIN PANEL 85530014 LOCATED AFT OF ACCESS DOOR AT MID SPAR BETWEEN STRINGER 29P - 29S. REPAIRED WITH PATCH IAW 8-55-2680.Apr 19, 2014 · N891EA · Dhav DHC8102 · Fuselage Main, Plate/SkinSDR CA140425002Diode · burned(CAN) DURING SCHEDULED REPLACEMENT OF A RT MLG COMPONENT, A BURNED DIODE WAS OBSERVED IN THE NACELLE. DIODE 2762-CR4, WDM 27-19-01 SHEET 4, WAS REPLACED, ROLL SPOILER SYS TESTED AND THE ACFT RELEASED FOR SERVICE.Apr 18, 2014 · Dhav DHC8102 · Drag Control SystemSDR CA140506007Oil Cooler · leaking(CAN) COMPLETE OIL LOSS OF NR 2 ENGINE AFTER SHUTDOWN AND INSPECTION, FOUND OIL LEAK TO BE COMING FROM OIL COOLER ON NR 2 ENGINE. OIL COOLER FITTINGS FOUND DRY. FOUND LOWER COOLER FINS TO BE WET. REPLACED R/E OIL COOLER AND ATTACHING FITTINGS O-RINGS. REPLEApr 17, 2014 · Dhav DHC8102 · Engine Oil CoolerSDR HNAA2014041600132Transceiver · malfunctionedWEATHER RADAR NOT PAINTING CORRECTLY. R & R RADAR TRANSCEIVER IAW MM 34-41-04 AND BULLETIN 34-18. OPS CHECKED GOOD. OK FOR SERVICE.Apr 16, 2014 · N839EX · Dhav DHC8102 · Weather Radar SystemSDR HNAA2014041100128Battery · overtempAUX BATTERY WARNING LIGHT ILLUMINATED DURING FLIGHT, SELECTED OFF IAW CHECKLIST. AUXILLARY BATTERY TEMP CONTINUED TO RISE INTO THE RED. R & R AUXILLARY BATTERY IAW MM 24-32-00. GROUND CHECKED GOOD.Apr 11, 2014 · N837EX · Dhav DHC8102 · Battery/Charger SystemSDR HNAA2014041000127Seat Track · corrodedCOROSION FOUND ON RT SEAT TRACK BETWEEN BS 217 AND 222. R & R SEAT TRACK IAW RD8-53-3071.Apr 10, 2014 · N812EX · Dhav DHC8102 · Fuselage, Seat/Cargo Attach FittingsSDR HNAA2014041000126Seat Track · corrodedCORROSION FOUND ON LT SEAT TRACK BETWEEN BS 202 AND 222. R & R SEAT TRACK IAW RD8-53-3074.Apr 10, 2014 · N812EX · Dhav DHC8102 · Fuselage, Seat/Cargo Attach FittingsSDR HNAA2014040900124Connector · disconnectedEMERGENCY EXIT LIGHT AT RT SIDE IS INOPERATIVE. FOUND WIRE CONNECTOR TO LIGHT ASSY NOT CONNECTED. CONNECTED WIRING HARNESS, OPS CHECKD GOOD.Apr 9, 2014 · N816EX · Dhav DHC8102 · Light System WiringSDR ERAA20140019Structure · dentedDENT AT X 291.4 - X 333.3, STRINGER 30P & 31P. REPAIRED TO RD 8-53-13611.Apr 7, 2014 · N891EA · Dhav DHC8102 · Fuselage Miscellaneous StructureSDR HNAA2014040400122Inverter · failedSTRONG FISH ODOR IN COCKPIT. INSPECTED PRIMARY, SECONDARY AND AUX INVERTER. NO DEFECTS NOTED. OPS CHCKED INVERTERS. NO ODOR, OPS CHECKED GOOD.Apr 4, 2014 · N933HA · Dhav DHC8102 · AC InverterSDR HNAA2014040400123Garlock Seal · leakingDURING FLIGHT, AT LOW POWER SETTINGS, HOT ODOR IS EMITTED IN COCKPIT AND CABIN AT HIGH POWER SETINGS AND ON GROUND. INSPECTED BOTH ENGINE AIR SWITCHING VALVES AND APU AREA. NO DISCREPANCIES NOTED. FOUND NR 2 ENGINE GARLOCK SEAL LEAKING. R & R GARLOCK SEAL. Apr 4, 2014 · N936HA · Dhav DHC8102 · Turbine Engine Oil SystemSDR HNAA2014040400120Inverter · odorSTRONG FISH ODOR IN COCKPIT, THROUGH ENTIRE FLIGHT. R & R SECONDARY INVERTER IAW MM 24-22-00. OPS CHECKED GOOD.Apr 4, 2014 · N805EX · Dhav DHC8102 · AC InverterSDR HNAA2014040400119Connector · contaminatedEMERGENCY LIGHTS ILLUMINATED INTERMITTENTLY DURING FLIGHT. INSPECTED NR 1 BRUSH BLOCK CONNECTOR AND FOUND TO BE CONTAMINATED WITH DEICE FLUID. CLEANED AS REQUIRED STANDARD PRACTICE. GROUND RAN ACFT. OPS CHECKED NORMAL.Apr 4, 2014 · N804EX · Dhav DHC8102 · Ice/Rain Protection System WiringSDR HNAA2014040400118Unknown · odorBURNING ODOR IN CABIN AT ROWS 4 AND 5. INSPECTED CABIN LIGHTING SYS AND BEHIND CABIN OVERHEAD PANELS. NO DEFECTS NOTED. GROUND RAN ACFT, NO ODOR NOTED AT THIS TIME. OK FOR SERVICE.Apr 4, 2014 · N936HA · Dhav DHC8102 · Air Distribution SystemSDR HNAA2014040200117Bulb · inoperativeFORWARD EMERGENCY FLOOR PATH LIGHT IS INOPERATIVE AT ROW 1DF. R & R BULBS AT EMERGENCY FLOOR PATH LIGHT IN ROW 1DF. OPS CHECKED GOOD.Apr 2, 2014 · N839EX · Dhav DHC8102 · Emergency LightingSDR HNAA2014040200116Seal · leakingELECTRICAL ODOR WHEN BLEEDS ARE SELECTED ON. INSPECTED AND FOUND SEAL BAD IN BYPASS BLEED LINE AND MAJOR LEAK AT HEAT EXCHANGER. R & R SEALS, SECURED HEAT EXCHANGER BLEED LINE. RAN APU, NO LEAKS NOTED.Apr 2, 2014 · N936HA · Dhav DHC8102 · Pneumatic Distribution SystemSDR HNAA2014033100114Connector · dirtyEMERGENCY LIGHT FLICKERING IN FLIGHT. CLEANED AND RESEATED CONNECTOR ON EMERGENCY LIGHT CONTROL BOX. OPS CHECKED NORMAL AT THIS TIME.Mar 31, 2014 · N804EX · Dhav DHC8102 · Light System WiringSDR HNAA2014033100113Connector · contaminatedLEFT AC BUSS CAUTION LIGHT WITH ASSOCIATED CAUTION LIGHTS ILLUMINATED DURING CLIMB OUT. INSPECTED LT AC CONTACTOR BOX. NO DISCREPANCIES. FOUND WATER IN NR 1 AC GENERATOR CONNECTOR. CLEANED AND RECONNECTED. GROUND RAN OPERATING AC BUSS SYSTEM. OPS CHECKED NMar 31, 2014 · N804EX · Dhav DHC8102 · Electrical Power System Wiring
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