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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR HNAA2015073100248Light · brokenRIGHT FWD EMERGENCY LIGHT BASE IS BROKEN. REMOVED SCREWS, R & R LIGHT ASSY, AT SAID LOCATION, REINSTALLED SCREWS. OPS CHECKED GOOD.SDR HNAA2015073100247Longeron · damagedOTBD AND MID HOLE IN NR 2 NACELLE LONGERON, AT POSITION 300 IS SHOWING MECHANICAL DAMAGE. PERFORM RD8-54-3294 ON BOTH HOLES. MOST OTBD HOLE FINAL DIAMETER IS .280. MID HOLE FINAL DIAMETER IS .250, EO8-54-15-0151 AND EO8-54-15-0152.SDR HNAA2015073100246Structure · damagedMOST OTBD HOLE SHOWING MECHANICAL DAMAGE LESS THEN 80 PERCENT. PERFORMED RD8-54-3292.SDR HNAA2015072900245Light · inoperativeEMERGENCY FLOOR PATH LIGHT IS INOPERATIVE. R & R EMERGENCY FLOOR PATH LIGHT.SDR HNAA2015072900244Bulb · inoperativeFORWARD LT EMERGENCY LIGHT IS OUT. R & R BULB. OPS CHECKED GOOD.SDR HNAA2015072900243Bulb · inoperativeFLOOR EMERGENCY LIGHTS ARE INOPERATIVE AT ROW 1, FURTHER MOST FROM THE FRONT AND ROW 9. R & R THE EMERGENCY LIGHT BULBS. OPS CHECKED GOOD.SDR HNAA2015072900242Probe · malfunctionedDURING ENGINE RUNS FOR TROUBLESHOOTING, NR 2 ENGINE POWER LAGGED. SELECTED NR 2 ECU MODE ON MANUAL. NR 2 POWER IS NOW SATISFACTORY WITH A KNOB SPLIT BETWEEN 1.5 AND 3.0 THROUGHOUT RUN. FOUND NR 2, T1.8 PROBE SHORTED TO GROUND. R & R T1.8 PROBE IAW MM 72-01-SDR HNAA2015072900241Bulb · burned outEMERGENCY EXIT SIGN LIGHT IS BURNED OUT AT ROW 1DF. R & R BULB. OPS CHECKED GOOD.SDR HNAA2015072900240Engine · power lossAFTER CLEARED FOR TAKE OFF, IMMEDIATELY AFTER ADVANCING POWER LEVERS, ACFT VEERED TO THE RT. USED LT RUDDER AND BRAKE TO BRING ACFT BACK. ON STRAIGHTENING NOSE WHEEL, ADDED MORE POWER, ACFT VEERED RT AGAIN. NOSE WHEEL STEERING WAS OPERATIVE AND NO CAUTION LISDR HNAA2015072900239Bulb · inoperativeTWO RED FLOOR EMERGENCY LIGHTS ARE INOPERATIVE. R & R BULBS. OPS CHECKED GOOD.SDR HNAA2015072900238Power Supply · malfunctionedCABIN EMERGENCY LIGHT SYS FLASHES ON/OFF INTERMITTENTLY DURING FLIGHT. INSPECTED EMERGENCY LIGHT SYS, SWITCHES AND CIRCUIT BREAKERS. NO DEFECTS NOTED. INSPECTED BOTH BUSH BLOCKS, NO DEFECTS NOTED. R & R 3352.PS2 POWER SUPPLY AND BATTERY IAW MM 33-52-00 ANDSDR HNAA2015072200237Rod End · out of adjustLEFT MAIN GEAR DOOR ADVISORY LIGHT REMAINED ON FOR ABOUT 5 MINUTES, AFTER GEAR RETRACTED AND SELF EXTINGUISHED. ADJUST ROD END FOR FORWARD LT GEAR DOOR IAW MM 32-30-00. RETRACTED AND EXTENDED GEAR SEVERAL TIMES. OPS CHECKED GOOD.SDR HNAA2015072200236Bulb · inoperative4TH RED FLOOR EMERGENCY LIGHT IS INOPERATIVE. R & R 4TH RED FLOOR EMERGENCY LIGHT BULB. OPS CHECKED GOOD.SDR HNAA2015072000235Battery Pack · dischargedFORWARD TWO RED EMERGENCY LIGHTS ARE INOPERATIVE. FOUND BATTERY DISCHARGED AT CEILING ROW 3. R & R THE BATTERY. OPS CHECKED GOOD.SDR HNAA2015072000233Switch · contaminatedBETA WARNING HORN SOUNDED DURING TAKEOFF. INSPECTED BETA WARNING HORN SWITCH. FOUND SWITCH COATED IN A STICKY SUBSTANCE. CLEANED SWITCH. INSPECTED ASSOCIATED WIRING WITH NO DEFECTS. SYSTEM OPS CHECKED GOOD IAW WC 34-10-20Q.SDR HNAA2015071700232Bulb · inoperativeF/A'S EMERGENCY NORMAL GREEN LIGHT IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.SDR HNAA2015071700231Seat Track · corrodedSEAT TRACK IS CORRODED AT CENTER FLOORBOARD SIDE IN FRONT OF PAX DOOR. AREA IS OUT OF LIMITS IAW RD8-53-4698. R & R DAMAGED SEAT ON OF FORWARD CENTER LT SEAT TRACK IAW RD8-53-3074 AND REF EO8-53-15-0144.SDR HNAA2015071700230Seat Track · corrodedFORWARD LT SEAT TRACK IS CORRODED IN FRONT OF CLOSET FLOOR PAN. R & R DAMAGED SECTION OF FORWARD CENTER SEAT TRACK IAW RD8-53-3074 AND EO8 53-15- 0144.SDR HNAA2015071500228Blade · damagedAFTER TAKEOFF, HIT MULTIPLE BIRDS. COMPLIED WITH ACFT AND ENGINE INSPECTION IAW -8MM 05-50-26. AIRCRAFT INSPECTION AFTER BIRDSTRIKE FOUND LIGHT ENGINE PROP BLADE HAD EXCESSIVE PLAY AT HUB ATTACH POINT.SDR HNAA2015071500227Bulb · inoperativeEMERGENCY SIDEWALL LIGHTS ARE INOPERATIVE AT ROW 4AC AND ROW 4DF. R & R BULBS, OPS CHECKED GOOD.SDR CA150714013Switch · shorted(CAN) FLIGHT CREW REPORTED THAT DURING TAKEOFF THE NR 1 ENG HAD TORQUE & PROP FLUCTUATIONS & AS A RESULT THEY DID A PRECAUTIONARY SHUTDOWN OF THE NR 1 ENG. THE ACFT RETURNED TO THE DEPARTURE AIRPORT. TROUBLESHOOTING DETERMINED THAT THE ENG PARAMETER FLUCTUATSDR HNAA2015071000223Proximity Sensor · false indicationRIGHT MLG AMBER DOOR LIGHT REMAINED ON AFTER RETRACTION. CREW CYCLED GEAR IAW CHECKLIST. LIGHT WENT OUT, THEN CAME BACK ON. R & R MLG FORWARD DOOR PROXIMITY SENSOR IAW MM 20-45-09 AND MM 32-10-36. ADJUSTED FORWARD RT DOOR ACTUATOR IAW MM 32-10-21. OPERATESDR CA150710008Actuator · failed(CAN) ACFT RETURNED TO THE GATE DUE TO LOSS OF THE NR 1 HYD SYSTEM WITH AN ASSOCIATED ISO CAUTION LIGHT. MAINTENANCE REPLACED THE LT INBD SPOILER ACTUATOR DUE TO END CAP SEPARATION FROM ACTUATOR HOUSING.SDR HNAA2015070800222Threshold · corrodedPAX DOOR THRESHOLD IS CORRODED. REMOVED CORRODED THRESHOLD, DRILLED NEW THRESHOLD. INSTALLED NEW THRESHOLD IAW DWG 85321241.SDR HNAA2015070800221Skin · damagedSKIN CORRODED AND CRACKED AT BS 201.15 BETWEEN STRINGERS 32P AND 32S. REPAIRED AREA IAW EA26-2015-087 AND EO8-53-15-0135.SDR HNAA2015070800220O-Ring · damagedNR 1 HYDRAULIC ISOLATION VALVE CAUTION LIGHT ILLUMINATED, ROLL SPOILER INBD HYD CAUTION LIGHT CAME ON AND OFF SEVERAL TIMES, BUT EXTINGUISHED. HYDRAULIC PRESSURE WAS GOOD FOR THE FLIGHT, BUT QUANTITY WAS LOW. ALL OTHER INDICATIONS NORMAL. R & R O-RING ON PRSDR HNAA201070800218Indicator · failedTERRAIN INOPERATIVE CAUTION LIGHT ILLUMINATED FOLLOWED BY ELECTRICAL ODOR AND FAILURE OF RADAR INDICATOR. R & R RADAR INDICATOR IAW 34-41-04. OPS CHECKED GOOD.SDR HNAA2015070600217Control Box · malfunctionedEMERGENCY LIGHTS FLICKERED ON CLIMBOUT. R & R EMERGENCY LIGHTS CONTROL BOX IAW 33-51-00.SDR HNAA2015070600216Light · abnormalEMERGENCY LIGHTS FLICKERED ON CLIMBOUT, GOES OUT WHEN SELECTING PROP HEAT ON. INSPECTED AND CLEANED BOTH BRUSH BLOCKS. NO DEFECTS NOTED. GROUND RAN ACFT. OPS CHECKED NORMAL AT THIS TIME.SDR HNAA2015070600215Wire · chafedADVANCED POWER LEVERS FOR TAKEOFF, DURING FERRY FLIGHT AND LT MLG UNSAFE RED LIGHT AND GEAR HANDLE LIGHT ILLUMINATED. FOUND MULTIPLE CHAFED WIRES. HA300, SEQ 20, 18 AND 17. OPS CHECKED GOOD.SDR HNAA2015070600214Wire · chafedLEFT MAIN GEAR UNSAFE LIGHT AND GEAR HANDLE LIGHT AND WARNING HORN ILLUMINATED, SOUNDED. TAKEOFF REJECTED. FOUND MULTIPLE CHAFED WIRES. HA 300, SEQ 20,18 AND 17 FOR C/A. OPS CHECKED GOOD.SDR HNAA2015070600213Warning Light · illuminatedRIGHT AC BUSS AND RT TRU ILLUMINATED DURING FLIGHT. R & R NR 2 AC GENERATOR IAW WORK CARD 24-20-11R. OPS CHECKED GOOD.SDR CA150629015Feeder Cable · chafed(CAN) DURING INSPECTION, DISCOVERED CHAFING DAMAGE TO THE LT SIDE MAIN DC GEN FEEDER WIRES. SUSPECT THE DAMAGE MAY BE CAUSED BY THE DEICE BOOT AIR SUPPLY FLEX HOSE. SIMILAR FINDINGS WERE NOTED ON THE RT SIDE OF THIS ACFT & ON THE RT & LT OF A SECOND ACFT.SDR HNAA2015062900212Bulb · inoperativeEMERGENCY LIGHT IS INOPERATIVE AT ROW 8DF. R & R BULB IN ROW 8 EMERGENCY LIGHT. OPS CHECKED GOOD.SDR HNAA2015062900210Generator · not reportedR & R NR 1 AC GENERATOR IAW WORK CARD 24-20-11R. R & R NR 1 AC GCU AND SECURED WITH RETAINED HARDWARE. OPS AND LEAKED CHECKED GOOD. OK FOR SERVICE.SDR HNAA2015062900209Inverter · malfunctionedPRIMARY INVERTER CAUTION LIGHT ILLUMINATED. R & R PRIMARY INVERTER IAW MM24-22-00. OPS CHECKED GOOD. OK FOR SERVICE.SDR HNAA2015062900208Apu · odorWITH APU BLEED SELECTED ON, GET A FUEL ODOR IN CABIN. R & R APU IAW WORK CARD 49-20-02X. OPS AND LEAKED CHECKED GOOD. NO ODOR OF FUEL WHEN APU BLEEDS SELECTED ON.SDR CA150624002Valve · cracked(CAN) LOSS OF HYD FLUID ON NR 1 SYS. ENG WAS SHUTDOWN. MX ACTION FOUND THAT THE NR 2 SIDE, RT AFT QLV AT FAULT, CRACKED & LEAKING. THE VLV WAS REMOVED & SERV UNIT INSTALLED. FUNCTION & LEAK CHECKED SERV.SDR HNAA2015062400206Relay · no testBETA LOCKOUT WILL NOT TEST. R & R RELAY 3313-K1 IAW WIRING MANUAL 32-42-00. OPS CHECKED GOOD IAW MM 61-42-00. PERFORMED WC 61-20-10Q. OK FOR SERVICE.SDR CA150625001Actuator · fractured(CAN) ON TAKEOFF, FLIGHT CREW HEARD A BANG, BUT CONTINUED ON. DURING CLIMB UPON FLAP RETRACTION, FLAPS REMAINED AT 5 & HYD SYS NR 1 FLUID LEVEL WAS OBSERVED DOWN TO 1 QUART. FLIGHT CREW DECLARED AN EMER & LANDED TO A NEARBY AIRPORT WITHOUT FURTHER INCIDENT. SDR HNAA2015062200201Pseu · malfunctionedRIGHT MAIN GEAR DOOR ADVISORY LIGHT ILLUMINATED AFTER RETRACTION. CYCLES GEAR IAW CHECKLIST AND NO FIX. R & R PSUE. CHECKED MEMORY CODE RECALL. NO CODES DISPLAYED. COMPLIED WITH NEAR/FAR TEST AND OPS CHECKED GOOD IAW 32-61-50.SDR HNAA2015061900198Battery Pack · inoperativeAFT EMERGENCY EGRESS LIGHT IS INOPERATIVE. R & R EMERGENCY LIGHT BATTERY AT ROW 3AC IAW MM 33-51-05. OPS CHECKED GOOD.SDR HNAA2015061700196Warning Horn · false activationTAKEOFF WARNING HORN SOUNDED AT APPROXIMATELY 75 KNOTS ON TAKEOFF ROLL. OPS CHECKED TAKEOFF WARNING HORN SYS IAW MM 31-51-00.SDR HNAA2015061700195Actuator · out of rigRIGHT MAIN AMBER GEAR DOOR LIGHT REMAINED ON AFTER GEAR RETRACTION, CYCLED GEAR, NO FIX. INSPECTED AND FOUND RT FORWARD GEAR DOOR ACTUATOR OUT OF RIG. RIGGED ACTUATOR IAW MM 32-10-36. OPS CHECKED GOOD.SDR HNAA2015061700194Light · inoperativeAFT EMERGENCY LIGHT IS INOPERATIVE AT ROW 9. R & R EMERGENCY LIGHT IAW 33-51-11. OPS CHECKED GOOD.SDR CA150701004Engine · overtorqued(CAN) THE ENG HAD AN UN-COMMANDED AUTO FEATHER EARLIER TODAY ON THE NR 1 ENG. TROUBLESHOOTING HAS DETERMINED THE CAUSE TO BE A LOSS OF TORQUE SIGNAL ON THE NR 1 ENG. THE FDR DATA ANALYSIS REVEALED AN OVER TORQUE. THE ENG WAS REMOVED & WILL BE SENT FOR REPAISDR CA150619013Engine · malfunctioned(CAN) UN-COMMANDED AUTO FEATHER OF NR 1 ENG ON CLIMB OUT AT 500 FEET. SHUT THE ENG, TURNED AROUND & HAD AN UNEVENTFUL LANDING. DETERMINED THE CAUSE TO BE A LOSS OF TORQUE SIGNAL ON THE NR 1 ENG. IAW FDR READ OUT & CONFIRMATION FROM MFG, THE ENG SUSTAINED A SDR CA150615013Plate · detached(CAN) ENGINE WAS SENT TO OVERHAUL FOR A SCHEDULED HOT SECTION INSPECTION. FOLLOWING REMOVAL OF THE HOT SECTION, THE LP STATOR BAFFLE RETAINING PLATE WAS FOUND TO BE LIBERATED & TWO GAS GEN CASE DIFFUSER TUBES WERE FRACTURED. SEE ETR REPORT PW100 2015-0615.SDR CA150616003Axle · bent(CAN) BEFORE MORNING DEPARTURE, RAMP CREW REPORTED THAT LT NOSE WHEEL APPEARED TO BE CROOKED. TROUBLESHOOTING BY LOCAL MX REVEALED THAT THE AXLE WAS BENT. THE FLIGHT DATA RECORDER WAS DOWNLOADED, DATA ANALYSIS DID NOT SHOW ANY HARD LANDING EVENT. INSPECTION SDR HNAA2015061200193Bulb · inoperative5TH FROM FRONT, FORWARD EMERGENCY PATH LIGHT IS INOPERATIVE, BETWEEN ROWS 1 AND 2. R & R BULBS A FORWARD EMERGENCY PATH LIGHTS. OPS CHECKED GOOD.
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