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 HNAA2014032800111Bulb · inoperativePAX DOOR FLOOR EMERGENCY LIGHT BULB IS INOPERATIVE. R & R BULB, OPS CHECKED GOOD.Mar 28, 2014 · N943HA · Dhav DHC8102 · Emergency LightingSDR HNAA2014032800110Control Box · malfunctionedDURING CLIMB OUT, ALL EMERGENCY LIGHTS CAME ON AND FLICKERED. R & R LIGHT CONTROL BOX. GROUND RAN ACFT. OPS CHECKED GOOD. OK FOR SERVICE IAW -8 MM 33-51-00.Mar 28, 2014 · N804EX · Dhav DHC8102 · Emergency LightingSDR HNAA2014032800109Connector · dirtyEMERGENCY LIGHTS FLICKERED IN FLIGHT. CLEANED AND RESEATED CONNECTOR FOR EMERGENCY LIGHT CONTROL BOX. GROUND CHECKED ACFT. OPS CHECKED NORMAL AT THIS TIME.Mar 28, 2014 · N804EX · Dhav DHC8102 · Light System WiringSDR HNAA2014032400106Bulb · inoperativeEMERGENCY LIGHT INOPERATIVE BETWEEN ROWS 3 AND 4. R & R BULB. OPS CHECKED GOOD.Mar 24, 2014 · N912HA · Dhav DHC8102 · Emergency LightingSDR HNAA2014032400105Inverter · failedELECTRICAL ODOR IN COCKPIT. SECONDARY INVERTER FOUND TO BE AT FAULT.Mar 24, 2014 · N936HA · Dhav DHC8102 · Electrical Power SystemSDR HNAA2014032400104Transmitter · failedNR 2 ENGINE OIL PRESSURE AT 48 PSI. R & R OIL PRESSURE TRANSMITTER IAW MM 79-36-03. OPS AND LEAKED CHECKED GOOD.Mar 24, 2014 · N935HA · Dhav DHC8102 · Engine Oil PressureSDR HNAA2014032400103Wire · brokenDURING FLIGHT, ACFT WAS AT 5000 FT, CABIN ALTITUDE WAS ABOUT 2000 FT. CAPTAIN TURNED OFF BLEEDS, ACFT CONTINUED TO PRESSURIZE DOWN TO APPROXIMATELY 500 FT. CABIN ALTITUDE WITH BOTH BLEEDS REMAINING IN THE OFF POSITION. AFTER RETURN, FOUND BROKEN WIRE 2121-2Mar 24, 2014 · N941HA · Dhav DHC8102 · Pneumatic System WiringSDR CA140328001Sequence Valve · failed(CAN) CREW REPORTED THAT AFTER TAKEOFF, THE NOSE GEAR DOORS DID NOT CLOSE POST GEAR RETRACTION. THE GEAR WAS CYCLED IAW CREW QRH AND EXPERIENCED THE SAME RESULT. CREW OPTED TO SELECT GEAR DOWN, DUE TO ICING CONDITIONS, THE FLIGHT DIVERTED. MAINTENANCE ACTIMar 21, 2014 · Dhav DHC8102 · Landing Gear Retraction/Extension SystemSDR HNAA2014032100100Battery Pack · inoperativeEMERGENCY LIGHTS DS3, DS4 AND FORWARD EXIT AFT 2 IS INOPERATIVE. R & R EMERGENCY LIGHT BATTERY IAW AMM 33-52-00 AT PS1. OPS CHECKED GOOD.Mar 21, 2014 · N814EX · Dhav DHC8102 · Emergency LightingSDR HNAA2014032100099Power Supply · inoperativeRT AFT EMERGENCY EXIT EGRESS LIGHT, CENTER CEILING AISLE LIGHT IS INOPERATIVE. R & R POWER SUPPLY. OPS CHECKED GOOD.Mar 21, 2014 · N814EX · Dhav DHC8102 · Emergency LightingSDR HNAA2014031900094Lead · damagedEMERGENCY LIGHTS FLICKERED DURING CLIMBOUT, CYCLED EMERGENCY LIGHT CONTROL SWITCH AND OPS CHECKED NOMAL. INSPECTED AND FOUND BAD PROPELLER LEAD ON NR 2 PROP, NR 3 BLADE. R & R LEAD. OPS CHECKED GOOD. OK FOR SERVICE.Mar 19, 2014 · N935HA · Dhav DHC8102 · Propeller/Propulsor System WiringSDR HNAA2014031900093Line · disconnectedBOTH NR 1 AND 2 ENGINES BLEED AIR CAUTION HOT LIGHT CYCLING ON & OFF DURING FLIGHT. ACFT WAS DEICED HEAVILY BEFORE FLIGHT. FOUND P3 LINE TO BLEED SWITCH DISCONNECTED. REINSTALLED AND R & R LT AND RT BLEED HIGH PRESSURE SWITCHES. OPS CHECKED GOOD ON RUN.Mar 19, 2014 · N805EX · Dhav DHC8102 · Pneumatic Distribution SystemSDR HNAA2014031700091Unknown · smokeCABIN AND FLIGHT DECK HAD SMOKE WITH BLEEDS ON, DISIPATED WITH BLEEDS OFF. ACFT WAS DIVERTED.Mar 17, 2014 · N930HA · Dhav DHC8102 · Air Distribution SystemSDR HNAA2014031400088Autofeather Sys · malfunctionedAUTOFEATHER DID NOT ARM DURING TAKEOFF ROLL, CYCLED CIRCUIT BREAKER Q4 NO FIX. GROUND RAN ACFT AND PERFORMED OPS CHECK OF AUTO FEATHER SYS IAW MANUAL. SYS OPERATES NORMAL AT THIS TIME.Mar 14, 2014 · N914HA · Dhav DHC8102 · Propeller Feathering/ReversingSDR HNAA2014031400087Bulb · dimLEFT OF EXTERIOR EMERGENCY LIGHT IS DIM. R & R BULB IAW AMM 33-51-00.Mar 14, 2014 · N936HA · Dhav DHC8102 · Emergency LightingSDR HNAA2014031400086Light · inoperativeNR 2 EMERGENCY LIGHT IS OUT. R & R NR 2 EMERGENCY LIGHT IAW AMM 33-51-11.Mar 14, 2014 · N936HA · Dhav DHC8102 · Emergency LightingSDR HNAA2014031400085Bulb · inoperativeROW 2 EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT BULB AT ROW 2.Mar 14, 2014 · N930HA · Dhav DHC8102 · Emergency LightingSDR HNAA2014031000083Unknown · odorVERY STRONG ODOR OF EXHAUST FUMES IN COCKPIT, ESPECIALLY AT LOWER POWER SETTINGS WITH POWER LEVERS AT FLIGHT IDLE, ODOR GETS WORSE. GROUND RAN ACFT. ODOR IS ONLY PRESENT WITH ENGINE BLEEDS ON. OK WITH BLEEDS OFF.Mar 10, 2014 · N937HA · Dhav DHC8102 · Air Distribution SystemSDR HNAA2014031000081Pump · malfunctionedWHEN STANDBY HYD PUMPS WERE SELECTED ON, NR 1 AC GENERATOR DROPS OFF LINE, BUT WILL RESET. R & R NR 2 STANDBY AD NR 2 CASE DRAIN FILLER ELEMENT IAW AMM 29-11-17. OPS AND LEAKED CHECKED GOOD IAW SRT MM. OK FOR SERVICE.Mar 10, 2014 · N938HA · Dhav DHC8102 · Hydraulic Pump (Electric/Engine), MainSDR HNAA2014031000080Brush Block · malfunctionedEMERGENCY LIGHTS FLICKERS ON & OFF INFLIGHT. R & R NR 1 ENGINE BRUSH BLOCK IAW MM 61-10-11. OPS CHECKED GOOD. THE AC CONTACTOR BOXES WERE INSPECTED AND NO DEFECTS WERE NOTED.Mar 10, 2014 · N935HA · Dhav DHC8102 · Electrical Power SystemSDR HNAA2014031000079Control Box · malfunctionedEMERGENCY LIGHTS FLICKER ON & OFF INFLIGHT. R & R EMERGENCY LIGHT CONTROL BOX. OPS CHECKED GOOD AT THIS TIME. OK FOR SERVICE.Mar 10, 2014 · N935HA · Dhav DHC8102 · Emergency LightingSDR HNAA2014030700074Unknown · odorCREW REPORTED PETROLEUM ODOR, STARTED WHEN ACFT WAS IN STEEP DESCENT AND CLEARED BEFORE LANDING. R & R CONDENSER MIXER, HEAT EXCHANGER, IAW ACM. GROUND RAN, OPS CHECKED GOOD.Mar 5, 2014 · N930HA · Dhav DHC8102 · Air Distribution SystemSDR HNAA2014030700075Battery Pack · inoperativeEMERGENCY LIGHTS WILL NOT TEST. R & R EMERGENCY LIGHT BATTERY IAW WC'S 33-50-03 AND 33-50-05. OPS CHECKED GOOD, OK FOR SERVICE.Mar 5, 2014 · N940HA · Dhav DHC8102 · Emergency LightingSDR HNAA2014030500069Light · dimRIGHT AFT, RIGHT FORWARD, LEFT AFT BETA LIGHTS DIMMER THAN REFERENCE LIGHT. REMOVED & REPLACED 3 BETA LIGHTS.Mar 4, 2014 · N930HA · Dhav DHC8102 · Emergency LightingSDR CA140307001Socket · burned(CAN) UPON ARRIVAL AT THE ACFT FLIGHT CREW REPORTED AN ELECTRICAL ODOR IN THE CABIN. MAINTENANCE FOUND A BURNED FIX LAMP HOLDER ON ONE OF THE CABIN SIDEWALL FLUORESCENT LAMP FIXTURE. THE LAMP ASSY WAS DISABLED AND THE ACFT RELEASE UNDER MEL. LAMP HOLDER WAS Mar 3, 2014 · Dhav DHC8102 · Passenger Compartment LightingSDR CA140305002Windshield · failed(CAN) DURING CRUISE, F/O WINDSHIELD SHATTERED. FLIGHT CREW ELECTED TO DIVERT TO THE NEAREST SUITABLE AIRPORT AND LANDED WITHOUT FURTHER INCIDENT. VISUAL INSPECTION OF THE WINDSHIELD BY MAINTENANCE CONFIRMED THAT ONLY THE OUTER FACE WAS SHATTERED. DECISION WAMar 3, 2014 · Dhav DHC8102 · Flight Compartment WindowsSDR HNAA2014030300065Boot · failedNR 2 BOOT ON RT WING WOULD NOT INFLATE OR INDICATE. R & R L/E 613BR IAW AMM 57-00-00. OPS CHECKED GOOD.Mar 2, 2014 · N816EX · Dhav DHC8102 · Airfoil Anti/De-ice SystemSDR HNAA2014030300064Bulb · inoperativeEMERGENCY LIGHT INOPERATIVE. R & R BULB.Mar 2, 2014 · N933HA · Dhav DHC8102 · Emergency LightingSDR HNAA2014030300066Smoke Detector · false activationDURING APPROACH, SMOKE WARNING LIGHT ILLUMINATED BRIEFLY, APPROXIMATELY FIVE SECONDS. ALONG WITH THE MASTER WARNING. EXTINGUISHED BY THEMSELVES. NO SMOKE DETECTED. R & R NR 2 CARGO BAY SMOKE DETECTOR IAW MM 26-12-06. OPS CHECKED GOOD. INSPECTED FOR SIGNSFeb 28, 2014 · N807EX · Dhav DHC8102 · Smoke DetectionSDR HNAA2014030300063Bulb · burned outTWO FLOOR EMERGENCY LIGHTS INOPERATIVE, 6TH FROM FRONT AND 13TH FROM FRONT. R & R EMERGENCY FLOOR LIGHT BULBS. OPS CK'D GOOD. RESECURED LIGHT COVERFeb 28, 2014 · N911HA · Dhav DHC8102 · Emergency LightingSDR HNAA2014022800061Stiffener · crackedVERTICAL STIFFNER ON LT SIDE OF RADAR BULKHEAD IS CRACKED MAT TOP END. CRACK EXTENDS FROM TOP RIVET TO EDGE OF STIFFENER. REPAIRED LT STIFFENER IAW EO8-53-14-0084.Feb 28, 2014 · N808EX · Dhav DHC8102 · Fuselage Main, BulkheadSDR HNAA2014022800060Bulb · inoperativeMOST AFT RT EMERGENCY LIGHT IS INOPERATIVE. REMOVED LENS, REPLACED BULB, RE-SECURED LENS WITH RETAINED HARDWARE. OPS CHECKED GOOD.Feb 28, 2014 · N814EX · Dhav DHC8102 · Emergency LightingSDR HNAA2014022600059Doubler · corrodedLAVATORY SERVICE DOOR LOWER CUT OUT IS CORRODED. REMOVED MACHINED DOUBLER. INSTALLED NEW DOUBLER IAW DWG 85320983.Feb 26, 2014 · N808EX · Dhav DHC8102 · Fluid Service DoorsSDR HNAA2014022600058Service Door · corrodedLAVATORY EXTERNAL SERVICE DOOR ASSY IS CORRODED. REMOVED CORRODED LAV. SERVICE DOOR ASSY, INSTALLED NEW LAVATORY SERVICE DOOR ASSY IAW DWG 85320983.Feb 26, 2014 · N808EX · Dhav DHC8102 · Fluid Service DoorsSDR HNAA2014022400056Lamp · inoperativeEMERGENCY LIGHT INOPERATIVE AT ROW 1. R & R EMERGENCY LIGHT LAMP AT ROW 1. OPS CHECKED GOOD.Feb 24, 2014 · N943HA · Dhav DHC8102 · Emergency LightingSDR HNAA2014022400055Unknown · odorCREW REPORTED FUEL ODOR WITH APU BLEEDS ON. INSPECTED APU BAY, NO FUEL LEAKS NOTED.Feb 24, 2014 · N805EX · Dhav DHC8102 · Air Distribution SystemSDR HNAA2014022400054Brush Block · failedRT AC BUSS FAILURE IN FLIGHT WITH ASSOCIATED CAUTION LIGHTS. GROUND RAN ACFT. COULD NOT DUPLICATE. INSPECTED NR 2 AC CONTACTOR BOX WIRING. NO DISCREPANCES NOTED. NR 2 PROP BLADES AND LEADS. INSPECTED NR 2 ENGINE LIP HEATER. R & R 2 BRUSH BLOCK AS PRECAUTIFeb 24, 2014 · N935HA · Dhav DHC8102 · Propeller/Rotor Anti-Ice/De-Ice SystemSDR HNAA2014022400053Spinner · crackedIN CRUISE FLIGHT, ACFT EXPERIENCED MODERATE TURBULENCE WITH A 45 DEGREE LT BANK AND A 20 DEGREE PITCH UP ACCOMPANIED BY NUMEROUS ITEMS BEING DISLODGED FROM POSITION. YD AND AP BOTH DISENGAGED AND ACFT EXPERIENCED A 300 TO 400 FOOT LOSS IN ALTITUDE. COMPLIED Feb 24, 2014 · N942HA · Dhav DHC8102 · Propeller Spinner SectionSDR HNAA2014021900052Line · leakingINFLIGHT, NR 2 HYD ISOLATION VALVE CAUTION LIGHT ILLUMINATED AND ASSOCIATED LOSS OF NR 2 HYD QTY, NR 2 SYSTEM .7 REMAINS. FOUND NR 2 SYSTEM PRESSURE LINE LEAKING IN FLAP WELL BETWEEN FUSELAGE AND NR 1 NACELLE. REMOVED RIDGED LINE AND INSTALLED TEMP FLEX LINFeb 19, 2014 · N941HA · Dhav DHC8102 · Hydraulic System, MainSDR HNAA2014021900051Warning Horn · false activationBETA WARNING HORN SOUNDED DURING CLIMB OUT AT ABOUT 50 FT ALTITUDE. VERIFIED BETA LOCK OUT OPS NORMAL AND CIRCUIT BREAKER PULLED AND COLLARED. CLEANED POWER LEVER SWITCH. OPS CHECKED GOOD.Feb 19, 2014 · N812EX · Dhav DHC8102 · Central WarningSDR HNAA2014021700049Support · corrodedCOAT CLOSET OTBD SUPPORT RAIL HAS CORROSION 3 INCHES AFT OF FRAME BS 215. BLENDED MINOR SURFACE CORROSION ON SUPPORT RAIL. ALODINED AND PRIMED IAW SRM 51-20-11, 51-20-16 AND 51-20-36.Feb 17, 2014 · N808EX · Dhav DHC8102 · Fuselage Miscellaneous StructureSDR HNAA2014021700048Seat Track · corrodedLEFT SEAT TRACK FLANGE HAS CORROSION BETWEEN BS 201.15 TO BS 222. BLENDED MINOR SURFACE CORROSION. ALODINED AND PRIMED AREA IAW SRM 51-20-11, 51-20-16 AND 51-20-36.Feb 17, 2014 · N808EX · Dhav DHC8102 · Fuselage, Seat/Cargo Attach FittingsSDR HNAA2017021700048Seat Track · corrodedLEFT HAND IBD SEAT TRACK COAT CLOSET FLANGE HAS SUFACE CORROSION BETWEEN BS 201.15 TO 222. BLENDED MINOR SURFACE CORROSION FROM SEAT TRACK. ALODINE AND PRIMED AREA IAW SRM 51-20-11, 51-20-16 AND 51-20-36.Feb 17, 2014 · N808EX · Dhav DHC8102 · Fuselage, Seat/Cargo Attach FittingsSDR HNAA2014021300042Shear Tie · corrodedCORROSION ON FRAME LEG. BLENDED LIGHT CORROSION ON FRAME LEG IAW SRM 51-20-11, 51-20-16 AND 51-20-36.Feb 13, 2014 · N808EX · Dhav DHC8102 · Fuselage Internal Mounting StructureSDR HNAA2014021300043Shear Tie · corrodedMINOR SURFACE CORROSION ON FRAME LEG. BLENDED MINOR SURFACE CORROSION FROM FRAME LEG, ALODINED AND PRIMED AREA IAW SRM 51-20-11, 51-20-16 AND 51-20-36.Feb 13, 2014 · N808EX · Dhav DHC8102 · Fuselage Internal Mounting StructureSDR HNAA2014021300047Frame · corrodedLIGHT CORROSION ON FRAME LEG BS 240.5. BLENDED LIGHT CORROSION IAW SRM 51-20-11, 51-20-16 AND 51-20-36.Feb 13, 2014 · N808EX · Dhav DHC8102 · Fuselage Main, FrameSDR HNAA2014021300046Frame · corrodedCORROSION ON FRAME LEG. BLENDED LIGHT CORROSION BS 222. ALODINED AND PRIMED IAW SRM 51-20-11, 51-20-16 AND 51-20-36.Feb 13, 2014 · N808EX · Dhav DHC8102 · Fuselage Main, FrameSDR HNAA2014021300045Shear Tie · corrodedCORROSION ON FRAME LEG. BLENDED CORROSION BS 291.4. ALODINED AND PRIMED IAW SRM 51-20-11, 51-20-16 AND 51-20-36.Feb 13, 2014 · N808EX · Dhav DHC8102 · Fuselage Internal Mounting StructureSDR HNAA2014021300044Shear Tie · corrodedCORROSION ON FRAME LEG. BLENDED LIGHT CORROSION BS 201, ALODINED AND PRIMED IAW SRM 51-20-11, 51-20-16 AND 51-20-36.Feb 13, 2014 · N808EX · Dhav DHC8102 · Fuselage Internal Mounting StructureSDR HNAA2014021200038Inverter · inoperativeDURING BOARDING, SMOKE ODOR INDICATED ON FLIGHT DECK WITH POSSIBLE CIRCUIT BREAKER TRIPPED, IMEDIATELY FOLLOWED BY SMOKE BEHIND CAPTAIN`S SEAT AND FLASH OF POSSIBLE SECONDARY INVERTER CAUTION LIGHT. FOUND AUXILARY INVERTER INOPERATIVE. R & R INVERTER. OPS CFeb 12, 2014 · N810EX · Dhav DHC8102 · AC Inverter
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