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 CA140728004Skin · damaged(CAN) DURING HEAVY MAINTENANCE INSPECTION, THE RT ELEVATOR, INBD T/E WAS FOUND TO BE LOOSE, DAMAGED WITH SEVERAL RIVET HEADS PULLED THROUGH THE ELEVATOR SKIN. ASSESSMENT AND APPROVED REPAIR TO BE CARRIED OUT.SDR HNAA2014072500215Connector · damagedEMERGENCY LIGHT IS INOPERATIVE AT ROW 6. R & R 1 PIN IN CONNECTOR IAW MM 20-45-09. OPS CHECKED GOOD.SDR HNAA2014072300214Selector Valve · unknownON GEAR DOWN SELECTION, ALL THREE GEAR RED LIGHTS ILLUMINATED. SELECTED GEAR INHIBIT SWITCH, LANDING GEAR EXTENDED NORMALLY , THREE GREEN ILLUMINATED. JACKED ACFT AND SWUNG GEAR SEVERAL TIMES. NO DEFECTS NOTED. R & R GEAR SELECTOR VALVE IAW WC 32-30-41R FOSDR HNAA2014072300213Control Handle · malfunctionedDURING GEAR DOWN SELECTION, THREE RED GEAR UNSAFE LIGHTS ILLUMINATED WITH NO INTRANSIT LIGHT. PERFORMED ALL GEAR SELECTION WITH THREE GREEN ALTERNATE INDICATION. VERIFIED ALL RELEASE AND EXTEND DOORS WERE CLOSED PRIOR TO ALT EXTENSION. R & R LANDING GEAR HASDR HNAA2014072300212Brake Assy · unknownACFT WOULD NOT MOVE WITH PARKING BRAKE DISENGAGED. R & R NR 1 AND NR 2 BRAKE AND WHEEL ASSY IAW WC 32-10-03L AND 32-42-11X. OPS CHECKED GOOD.SDR HNAA2014072100211Actuator · malfunctionedAFTER TAKE OFF, SELECTED GEAR UP, RT MLG RED UNSAFE LIGHT ILLUMINATED, AMBER LIGHT ILLUMINATED ON LT MLG AND NLG. R & R NR 2 RETRACT ACTUATOR AND FITTING IAW MM32-30-11. OPS AND LEAKED CHECKED GOOD.SDR HNAA2014072100210Light · unsecureEMERGENCY FLOOR LIGHT EXTRUDED AT ROW 7. FITTED EMERGENCY LIGHTS BACK ON TRACK. OK FOR SERVICE.SDR CA140722002Indicator · failed(CAN) AFTER TAKEOFF THE OIL PRESSURE DROPPED TO 45 PSI ON THE LT ENGINE. CREW FOLLOWED QRH AND FEATHERED ENGINE FOR LOW OIL PRESSURE AND FLEW BACK TO THE AIRPORT. AFTER LANDING, VERIFIED OIL LEVEL AND CHECKED ENGINE CONDITION PANEL WITH NO FAULTS FOUND. DISSDR CA140721019Bushing · corroded(CAN) DURING SCHEDULED ENGINE CHANGE, PLAY WAS NOTICED AT THE RT NACELLE STRUCTURE OTBD LOWER STRUT ASSY LOWER ATTACHMENT POINT. BOLT, WAS REMOVED AND FRETTING CORROSION WAS NOTICED ON IT AND ON SHEAR BUSHING, 240. BUSHING, 240, WAS ALSO WORN OUT AND THE FLANSDR HNAA2014071800209Terminal · burnedBRIEF HOT ODOR NOTICED DURING FINAL. SELECTED COFFEEMAKER OFF AND ODOR WENT AWAY. FOUND ONE PIN SOCKET BURN. COMPLIED WITH WC 25-00-004N. R & R RECEPTACLE TO NR 1 HOT JUG AND INSTALLED 2 NEW RING TERMINALS. R & R NR 1 HOT JUG. OPS CHECKED GOOD.SDR HNAA2014071800208Acm · failedSMOKE AND BURNING ODOR INDICATED ON FLIGHT DECK DURING APPROACH. INSPECTED ACM AND FOUND BURNED OIL AND METAL SHAVINGS FROM OIL SAMPLE. R & R ACM IAW 21-50-03. OPS CHECKED GOOD. OK FOR SERVICE.SDR HNAA2014071600207Battery Pack · malfunctionedALL CABIN EMERGENCY LIGHTS ON POWER SUPPLY, 3351PS2, COME ON FOR ONE OR TWO SECONDS AND THEN SHUTOFF. ALL OTHER EMERGENCY LIGHTS FUNCTION NORMAL. SLAVED IN POWER SUPPLY BASE AND EMERGENCY LIGHTS CONTROL BOX. NO FIX. R & R BATTERY IAW MM 33-51-00. OPS CHECSDR HNAA2014071600206Skin · damagedMULTIPLE RIVETS ARE PULLING THROUGH THE SKIN AT RT FWD SIDE OF BS 182 STRINGER 31P. REPAIRED IAW EA15-2014-151B AND EO8-53-14-0282.SDR HNAA2014071600205Smoke Detector · false activationSMOKE WARNING AFTER NR 1 ENGINE STA LIGHT EXTINGUISHED AFTER NR 1 ENGINE SHUTDOWN. INSPECTED BAG BAY. NO DEFECTS NOTED. R & R NR 1 AND NR 2 BAG BAY SMOKE DETECTORS. RAN ACFT. SMOKE DETECTORS OPS CHECKED NORMAL. NO DEFECTS NOTED, OK FOR SERVICE.SDR HNAA2014071400204Lamp · inoperativeEMERGENCY PATH LIGHT 4TH FROM FRONT INOPERATIVE. REPLACED THE LAMP, OPS CHECKED GOOD, OK FOR SERVICE.SDR HNAA2014071400202Module · failedCABIN EMERGENCY LIGHTS 11TH FROM FRONT OF AIRCRAFT INOPERATIVE. R & R EMERGENCY LIGHT MODULE IAW PPS 9.09 AND AMM 33-51-11.SDR CA140714015Cable Assy · frayed(CAN) CAPTAIN REPORTED THAT THE BRAKE PEDALS WERE SPLIT WITH THE RH PEDAL GRABBING AND FELT IT WAS GOING LOWER WHEN PEDAL DEPRESSED. FOLLOWING A CLOSE INSPECTION OF THE BRAKE CONTROL CABLES, THE AME FOUND FRAYING OF THE RH BRAKE CABLE BENEATH THE FLIGHT DECK ASDR HNAA2014071100201Arm · out of adjustAFTER TAKEOFF, LEFT INBD ROLL SPOILER WOULD NOT RETRACT. ACFT RETURNED TO DEPARTURE. FOUND POTENTIOMETER ARM OVER-CENTER. ADJUSTED ARM IAW MM 27-05-11. REINSTALLED PANEL 532BB, OPS CHECKED GOOD AT THIS TIME. REVERIFIED LT INBD SPOILER FDAU READOUT IAW MSDR HNAA2014071100200Bulb · inoperativeF/S EMERGENCY LIGHT SWITCH DOES NOT ILLUMINATED. R & R BULB. OPS CHECKED GOOD.SDR CA140710002Actuator · cracked(CAN) MAINTENANCE RECEIVED A REPORT OF HYDRAULIC FLUID LEAK AT THE GATE AREA AND THE FLIGHT DECK INDICATOR SHOWED 1 QUART. MAINTENANCE ACTION FOUND THAT THE RIGHT HAND, FORWARD, MLG DOOR ACTUATOR WAS CRACKED ON THE UPPER END. THE ACTUATOR WAS REPLACED IAW AMMSDR HNAA2014070700197Battery Pack · inoperativeOVERHEAD EMERGENCY EXIT SIGN IS INOPERATIVE AT ROW 4. R & R EMERGENCY LIGHT BATTERY PACK ABOVE ROW 7DF IAW MM 33-51-00.SDR CA140721008Engine · malfunctioned(CAN) DURING FLIGHT AT 16000 FEET, THE CREW FELT A NOTICEABLE YAW THEY NOTICED THE ENGINE NR 2 DISTINCT TORQUE FLUCTUATIONS FOLLOWED BY TORQUE AND ITT PARAMETERS DROPPING RAPIDLY. THE CREW THEN ELECTED TO PERFORM THE CHECKLIST AND SHUTDOWN PROCEDURE, BY THE TSDR CA140707003Control Unit · malfunctioned(CAN) IN CRUISE, FLIGHT CREW OBSERVED TORQUE FLUCTUATION ON THE NR 2 ENGINE ASSOCIATED WITH NOTICEABLE YAW MOVEMENT. DECISION WAS TAKEN TO SHUTDOWN THE ENGINE, THE CHECKLIST WAS INITIATED BUT BY THE TIME IT WAS COMPLETED THE ENGINE HAD STOPPED ON ITS OWN. ANSDR HNAA2014070200196Controller · failedDUAL RESPONDER FAILUE ASSOCIATED WITH FAIL LIGHT AS REPORTED BY ATC. R & R MODES TCAS CONTROLLER. OPS CHECKED GOOD IAW MM 34-47-03.SDR HNAA2014063000195Power Supply · failedEMERGENCY LIGHTS SELECTED, FUSELAGE LIGHTS MOMENTARILY CAME ON AND THEN WENT OFF. R & R EMERGENCY LIGHT POWER SUPPLIES IAW WC 33-50-05. OPS CHECKED GOOD.SDR HNAA2014063000194Lock · deployedAFTER GEAR RETRACTION, LT, RT, AND NOSE DOOR AMBER LIGHT AND NOSE GREEN AND RED LIGHTS REMAINED ILLUMINATED. AFTER ALTERNATE EXTENSION, RED UNSAFE LIGHT WENT OUT AND ALL 3 GREEN GEAR INDICATIONS ILLUMINATED. INSPECTED ACFT AND FOUND NOSE GEAR GROUND LOCK DESDR HNAA2014063000193Pressure Switch · malfunctionedWHEN SETTING POWER LEVERS TO TAKEOFF, NR 2 ENGINE HYDRAULIC CAUTION LIGHT ILLUMINATED. WHEN REDUCING POWER, CAUTION LIGHT WENT OUT. INSPECTED NR 2 HYDRAULIC PUMP PRESSURE SWITCH WIRING. NO DEFECTS NOTED. R & R PRESSURE SWITCH IAW MM 29-11-17. GROUND RAN NR 2 SDR HNAA2014063000192Wire · brokenCENTER AISLE OVERHEAD EMERGENCY EXIT SIGN IS INOPERATIVE. REPAIRED BROKEN WIRE AT LIGHT ASSY. OPS CHECKED GOOD.SDR HNAA2014063000191Inverter · failedWITH PRIMARY INVERTERS OFF, AUX INVERTER SELECTED TO LT SIDE. L26 AC CAUTION LIGHT IS ILLUMINATED. CREW NOTED FISH ODOR IN FLIGHT DECK. R & R AUX INVERTER IAW MM 24-22-00. PERFORMED OPS CHECK OF 400 HZ SYSTEM IAW MM 24-22-00. OPS CHECKED GOOD AT THIS TIME. SDR HNAA2014062400187Engine · out of rigDURING CLIMBOUT WITH NR 1 POWER LEVER FULL. COULD NOT MAINTAIN CLIMB TORQUE. RIGGED NR 1 ENGINE. GROUND RAN ACFT. OPS CHECKED GOOD.SDR HNAA2014062400186Display · malfunctionedRADAR DISPLAYED TX FLT, WOULD NOT PAINT WEATHER, CYCLED OFF AND ON THREE TIMES. RADAR OPS NORMAL. R & R RADAR INDICATOR AND RT IAW 34-41-04, OPS CHECKED GOOD, OK FOR SERVICE. INSPECTED CONNECTORS NO DEFECTS NOTED.SDR CA140630015Engine · malfunctioned(CAN) SUBSEQUENT TO TAKEOFF, THE FLIGHT CREW POSITIONED ENGINES FROM TAKEOFF MODE TO CLIMB SETTINGS. UPON THE INITIAL TRANSIENT POWER CHANGE, FLIGHT OBSERVED NR 1 ENGINE TORQUE INDICATION WENT TO "ZERO" WITH A SLIGHT POWER CHANGE. THE FLIGHT CREW ELECTED TO SSDR HNAA2014062400188Propeller · vibrationSEVERE PROPELLER VIBRATION. SHIMED NR 100 AND 200 PROPELLER BLADES IAW MM 61-10-00. . OPS CHECKED GOOD DURING ENGINE RUNS.SDR CA140701003Engine · failed(CAN) DURING DESCENT, HIGH VIBRATIONS WERE FELT AND A F/A SAW FLAMES OUT OF THE NR 2 ENGINE EXHAUST. THE ENGINE WAS SHUTDOWN AND AN UNEVENTFUL SINGLE ENGINE LANDING FOLLOWED AT DESTINATION. ENGINE STATUS AND CONDITION IS UNKNOWN.SDR CA140619008Skin · corroded6" OPENING CORRODED IN BELLY SKIN AT X480, STR 32. EXTENSIVE LEVEL 2/3 CORROSION AND DISBOND. COMPLETE SKIN REPLACEMENT IAW APPROVED REFERENCE.SDR HNAA2014061800185Monitor · inoperativeAC POWER MONITOR IS BLANK. R & R AC POWER MONITOR IAW 24-29-05. OPS CHECKED GOOD.SDR HNAA2014061800184Knob · unsecureFIRST OFFICER`S TRANSMIT SELECT KNOB ON ACP LOOSE. SECURED SELECT KNOB. OPS CHECKED GOOD. OK FOR SERVICE.SDR HNAA2014061600183Bulb · inoperativeFIFTH CABIN EMERGENCY LIGHT FROM REAR IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.SDR HNAA2014061300180Pcu · malfunctionedAFTER ROTATION, NR 2 PROPELLER INDICATED 1236 FOR 5 SECONDS, TORQUE INDICATED 87-88 PERCENT. R & R NR 2 PCU IAW 61-10-10R AND WC 76-00-01Q. OPS CHECK AND LEAK CHECKED GOOD. OK FOR SERVICE.SDR HNAA2014061300179Switch · out of adjustTAKEOFF WARNING HORN SOUNDED WHEN ADVANCING POWER LEVERS. RESET PARAMETERS, STILL SOUNDS. ADJUSTED NR 1 CONDITION LEVER SWITCH 3151-S3 IAW MM 76-10-13. OPS CHECKED GOOD.SDR HNAA2014061100177Gauge · erraticREJECTED TAKEOFF DUE TO NR 2 ITT GAUGE ERRATIC. CREW REPORTED GAUGE ANALOG/DIGITAL SWUNG FULL SCALE. R & R NR 2 ITT GAUGE. POWER RAN ACFT FOR 10 MINUTES. OPS CHECKED GOOD. OK FOR SERVICE IAW MM 77-20-00.SDR HNAA2014061100176Unknown · odorAUXLILLARY POWER UNIT. FUEL ODOR IN CABIN WITH APU RUNNING, CLEARED WHEN OFF. INSPECTED APU COMPARTMENT.SDR CA140610003Bracket · loose(CAN) DURING INVESTIGATION OF A HYD LEAK, MAINTENANCE PERSONNEL NOTICED THAT THE MOUNTING BRACKET FOR THE RT INBD ROLL SPOILER ACTUATOR WAS LOOSE. FURTHER INVESTIGATION FOUND NO DAMAGE TO THE BRACKET BUT THAT THE FASTENERS WERE COMING LOOSE. THE BRACKET WAS SDR HNAA2014060400170Bulb · inoperativeF/A'S EMERGENCY LIGHT SWITCH BACKLIGHTING IS INOPERATIVE IN NORM POSITION. R & R BULB. OPS CHECKED GOOD.SDR HNAA2014060200169Contactor · burnedAPU FAIL LIGHT ILLUMINATED DURING START. AUX AND MAIN CIRCUIT BREAKERS TRIPPED. SMOKE, FIRED BOTTLE. FOUND APU START CONTACTOR WELDED. COLLARED CIRCUIT BREAKER. R & R APU START CONTACTOR AND SMALL CABLE ASSY, EGT, SWAP HARNESS IAW BULLETIN 49-8. OPS CHECSDR HNAA2014060200168Transducer · out of adjustNOSE WHEEL STEERING HAS LT TURN TENDENCIES. DURING TAKEOFF ROLL, RT RUDDER PEDAL INPUT REQUIRED FOR CENTER LINE. KICKS OFF YAW DAMP. YAW DAMP RETURN AFTER TAKEOFF. ADJUSTED NOSE WHEEL STEERING LVDT IAW MM 32-50-00. TAXI ACFT. OPS CHECKED GOOD. OK FOR SESDR CA140602030Sequence Valve · failed(CAN) AFTER TAKEOFF THE RT MLG FAILED TO RETRACT. THE ACFT RETURNED TO THE DEPARTURE AIRPORT FOR AN UNEVENTFUL LANDING. MAINTENANCE REPLACED THE RT MLG SEQUENCE VALVE, CARRIED OUT GEAR SWINGS AND RETURNED THE ACFT TO SERVICE.SDR CA140602035Skin · cracked(CAN) WHILE PERFORMING AN INSPECTION AFTER AN ABNORMAL ACFT VIBRATION REPORT, SMALL CRACKS WERE FOUND ALONG YH13.80, LT ELEVATOR LOWER SKIN. DAMAGE WAS REPAIRED IAW RD 8-55-2693 AND THE ACFT RELEASED FOR SERVICE.SDR HNAA2014052900167Sign · unsecureROW 4 AC SIDEWALL EMERGENCY EXIT SIGN UNSECURE. SECURED EMERGENCY EXIT SIGN AT ROW 4AC.SDR HNAA2014052900165Wire Harness · damagedAFTER GEAR RETRACTION, WOW CAUTION LIGHT ILLUMINATED AND EXTINGUISHED TWO TIMES. NORMAL GEAR EXTENSION FOR LANDING. PSEU CODE 12, RT GEAR WOW CHECK. WIRING FROM 3261-P15 TO SENSOR FOUND INDUCTANCE AND RESISTANCE HIGH. R & R RT GEAR WOW 1 HARNESS. JACKED AND
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