N982HA, cancelled Oct 28, 2009

Service difficulty reports · 32

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N982HA' AND deregistration_id = 'N982HA-2009-10-28'
  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 HNAA2009031400091Light · inoperativeONE EMERGENCY ESCAPE PATH FLOOR LIGHT AT ROW 7 INOP. REMOVED AND REPLACED LIGHT BULB.Mar 4, 2009 · N982HA · Dhav DHC8102 · Emergency LightingSDR HNAA200911200393Bypass Switch · failedNR 1 FUEL FILTER BYPASS CAUTION LIGHT ILLUMINATED WHEN SETTING TAKE OFF POWER THEN EXTINGUISHED WHEN POWER REDUCED TO FLIGHT IDLE. R&R NR 1 HIGH PRESSURE FILTER AND BYPASS SWITCH. INSPECTED OLD FILTER NO DEBRIS FOUND. GROUND RUN ACFT OPS CHECK GOOD. LOW PREJan 7, 2009 · N982HA · Dhav DHC8102 · Fuel Controlling SystemSDR HNAA2008113000333Apu · odorUPON APU FAILURE, SMOKE ODOR FILLED THE CABIN AND COCKPIT. MAINTENANCE INSPECTED THE APU BAY AND FOUND NO LEAKS. APU WAS RUN FOR 10 MINUTES WITH AND WITHOUT BLEEDS ON. NO DEFECTS WERE NOTED AND NO ODORS WERE DETECTED. AIRCRAFT WAS THEN RELEASED FOR SERVICENov 30, 2008 · N982HA · Dhav DHC8102 · APU Bleed Air SystemSDR HNAA2009021200050Panel · corrodedDURING 'C' CHECK INSPECTIONS, THE LT WING STRESS PANEL, 522AT, WAS FOUND TO HAVE CORROSION IN SOME OF THE SCREW COUNTER SINKS THAT WAS BEYOND ACCEPTABLE LIMITS. THE PANEL WAS REPLACED. THIS IS AN AMENDMENT TO HNAA2009010900383 TO CORRECT ITEM 1C, REGISTRATIOSep 13, 2008 · N982HA · Dhav DHC8102 · Wing Miscellaneous StructureSDR HNAA2009020100041Access Panel · corrodedRT WING ACCESS PANEL 622 AT (STRESS PANEL) HAS 2 HOLES CORRODED. CORROSION FOUND TO BE IN LIMIT PER RD8-57-1715. REPAIR HOLES IAW RD8-57-1715.Sep 13, 2008 · N982HA · Dhav DHC8102 · Wing, Plate/SkinSDR HNAA2009010900382Door Frame · corrodedDURING C-CHECK INSP, THE LAVATORY SERVICE DOOR FRAME WAS FOUND TO HAVE CORROSION ON IT. THE DOOR FRAME WAS REPLACED IAW SRM PROCEDURES. ADDITIONALLY, THE PAX DOOR THRESHOLD WAS FOUND TO BE CORRODED. THAT ITEM, P/N 85320686-101, WAS ALSO REPLACED.Sep 11, 2008 · N982HA · Dhav DHC8102 · Fuselage Main, StructureSDR HNAA0800014Door Seal · dirtyWITH ALL DOOR INDICATIONS NORMAL, DOOR SEAL WOULD NOT INFLATE. MAINTENANCE INSPECTED DOOR SEAL SUPPLY LINES AND PRESSURIZING VALVE, NOTING NO DEFECTS. DOOR SEAL WAS CLEANED OF DIRT AND GRIME. DOOR SEAL AT THIS TIME INFLATED PROPERLY AND AIRCRAFT WAS CHECKEDDec 18, 2007 · N982HA · Dhav DHC8102 · Passenger/Crew DoorsSDR HNAA0700295Galley · odorELECTRICAL ODOR IN CABIN. FLIGHT 4165, LGA TO ROA. LGA MNT PERFORMED HIDDEN DAMAGE INSPECTION AND FOUND HOT JUG IN NR 1 POSITION OVERHEATED AND CAUSING ODOR. REMOVED HOT JUG AS PRECAUTION, ITEM PLACED ON MEL. ROA MTN REMOVED AND REPLACED HOT JUG.Dec 17, 2007 · N982HA · Dhav DHC8102 · Buffet/GalleysSDR HNAA0700286Smoke Detector · defectiveBAG BAY SMOKE WARNING AND MASTER WARNING LIGHT ILLUMINATED SEVERAL TIMES ON DESCENT TO HTS STARTING AT 6000 FEET THROUGH TOUCHDOWN. REMOVED AND REPLACED BOTH SMOKE DETECTORS IN THE BAG BAY, OPERATIONAL CHECK GOOD.Dec 5, 2007 · N982HA · Dhav DHC8102 · Smoke DetectionSDR HNAA0700156Mixer Box · wornCABIN GOT VERY HOT AFTER TAKEOFF FLIGHT DECK COLD. AFTER SEVERAL PAX GOT SICK, F/A INFORMED CREW THAT THE CABIN WAS TOO HOT TO CONTINUE. ACFT WAS APPROX 20 MILES OUT OF LGA, ACFT RETURNED TO FIELD. CONTACTED LGA MX. ACFT HAS BEEN WRITTEN UP TWICE BEFORE. Jul 26, 2007 · N982HA · Dhav DHC8102 · Air Distribution SystemSDR HNAA070156Mixer Box · wornCABIN GOT VERY HOT AFTER TAKEOFF, FLIGHT DECK COLD. AFTER SEVERAL PAX GOT SICK, F/A INFORMED CREW THAT THE CABIN WAS TOO HOT TO CONTINUE. ACFT WAS APPROX 20 MILES OUT OF LGA, ACFT RETURNED TO FIELD. CONTACTED LGA MX. ACFT HAS BEEN WRITTEN UP TWICE BEFORE. Jul 26, 2007 · N982HA · Dhav DHC8102 · Air Distribution SystemSDR HNAA0700079Hydraulic Line · leakingWHILE CLIMBING THROUGH 17,000 FEET ABOUT 40 MILES EAST OF PIT, THE NUMBER 2 HYDRAULIC SYSTEM DROPPED TO 1/2 QUART. RETURNED TO PIT, DECLARED AN EMERGENCY. FLIGHT LANDED AND TAXIED TO GATE WITHOUT FURTHER INCIDENT. INSPECTED AND FOUND LEAK AT THE STEERING ACApr 16, 2007 · N982HA · Dhav DHC8102 · Hydraulic System, MainSDR HNAA0700224Threshold · corrodedAIR STAIR DOOR MAIN ENTRANCE THRESHOLD MEMBER CORRODED. REPLACED THRESHOLD.Jan 18, 2007 · N982HA · Dhav DHC8102 · Fuselage Miscellaneous StructureSDR HNAA0700229Bracket · corrodedCORROSION FOUND ON BRACKET AND CARGO FLOOR AT X598 ZONE 144 NEAR ENTRANCE AFT. CORROSION ON CARGO FLOOR REMOVED AND BRACKET REPLACED.Jan 5, 2007 · N982HA · Dhav DHC8102 · Fuselage Main, Attach FittingsSDR HNAA0700228Seat Track · corrodedSURFACE CORROSION ON LEFT INBOARD SEAT TRACK IN CARGO AREA. REPLACED LEFT INBOARD SEAT TRACK AFT CARGO BAY.Jan 5, 2007 · N982HA · Dhav DHC8102 · Fuselage, Seat/Cargo Attach FittingsSDR HNAA0700227Seat Track · corrodedCORROSION ON RIGHT INBOARD SEAT TRACK AT X201.00. REPLACED SEAT RAIL.Jan 5, 2007 · N982HA · Dhav DHC8102 · Fuselage, Seat/Cargo Attach FittingsSDR HNAA0700226Frame · corrodedCORROSION FOUND ON FRAME UNDERFLOOR AT X201.1560 BETWEEN STR 32S AND 30S. REPAIRED FRAME IAW ENGINEERING ORDER.Jan 5, 2007 · N982HA · Dhav DHC8102 · Fuselage Main, FrameSDR HNAA0700225Seat Track · corrodedCORROSION ON FORWARD LEFT SEAT RAIL. REMOVED CORROSION AND RETREATED RAIL.Jan 5, 2007 · N982HA · Dhav DHC8102 · Fuselage, Seat/Cargo Attach FittingsSDR HNAA0600116Unknown · odorHOT ELECTRICAL ODOR CENTER OF CABIN. PERFORMED HIDDEN DAMAGE INSPECTION AND PULLED ANC COLLARED RT MAIN CIRCUIT BREAKER S1 IAW SPECIAL PROCEDURES 33.1. SYSTEM MELD, MORE TO FOLLOW.Sep 25, 2006 · N982HA · Dhav DHC8102 · Air Distribution SystemSDR HNAA0500096Engine · smokeIN FLIGHT SMOKE IN CABIN AND COCKPIT. USED COCKPIT 02 MASKS. TURNED 13 BLEED OFF AND OPENED OUTFLOW VALVE ON DESCENT TO CLEAR SMOKE AND FLY UNPRESSURIZED, THEN TURNED OFF NR 2 BLEED DIVERTED AND DECLARED EMERGENCY. REMOVED AND REPLACED NR 2 ENGINE.Oct 26, 2005 · N982HA · Dhav DHC8102 · Engine (Turbine/Turboprop)SDR HNAA0500088Actuator · bypassingNOSE GEAR DID NOT EXTEND WHEN GEAR HANDLE SELECTED DOWN, GEAR DID EXTEND WHEN ALT. EXTENSION PROCEDURE WAS FOLLOWED. REMOVED AND REPLACED NOSE DOOR ACTUATOR.Oct 6, 2005 · N982HA · Dhav DHC8102 · Landing Gear ActuatorSDR HNAA0500072Actuator · leakingNR 1 HYDRAULIC ISOLATION VALVE CAUTION LIGHT ILLUMINATED WHEN TAKING RUNWAY FOR TAKEOFF. NR 1 HYDRAULIC QUANTITY WENT TO 1.0 NORMAL BRAKING FAILED. CREW SHUT DOWN NR 1 ENGINE AND RETURNED TO GATE. REMOVED AND REPLACED THE LEFT WING INBOARD ROLL SPOILER PER Jul 28, 2005 · N982HA · Dhav DHC8102 · SpoilersSDR HNAA0500026Selector Valve · malfunctionedGEAR WOULD NOT EXTEND ON 2ND ATTEMPT. FOLLOWED EMERGENCY CHECK LIST. PERFORMED ALT EXTENSION, GEAR DOWN AND LOCKED. INSPECTED PSEU FOR FAULT CODES NONE FOUND CYCLED GEAR 10 TIMES WITH NO DEFECT NOTED. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE AS REQMar 18, 2005 · N982HA · Dhav DHC8102 · Landing Gear Retraction/Extension SystemSDR HNAA0400072Threshold · corrodedPAX DOOR THRESHOLD CORRODED ON SILL PLATE. REMOVED AND REPLACED THRESHOLD.Jul 29, 2004 · N982HA · Dhav DHC8102 · Fuselage Miscellaneous StructureSDR HNAA0400071Panel · corrodedDURING C-CHECK INSPECTION FOUND STRESS PANELS 523 AND 623 AT WITH CORROSION IN COUNTERSINKS. REMOVED AND REPLACED PANELS.Jul 29, 2004 · N982HA · Dhav DHC8102 · Wing, Plate/SkinSDR PCAA0303050Hydraulic Line · leakingSYR-FLIGHT#3963. CREW REPORTED THAT THE #2 HYDRAULIC ISOLATION VALVE CAUTION LIGHT ILLUMINATED AFTER GEAR EXTENSION. 1.4 QUARTS REMAINING IN #2 SYSTEM. MAINTENANCE REPLACED A HYDRAULIC LINE IN THE LEFT WHEEL WELL IN ACCORDANCE WITH THE DEHAVILLAND DASH 8 MAINTMar 3, 2003 · N982HA · Dhav DHC8102 · Hydraulic System, MainSDR HNAA0100079Hydraulic System · malfunctionedLOST NR 1 HYDRAULIC SYSTEM PRESSURE WITH NR 2 ENGINE RUNNING DURING SINGLE ENGINE TAXI. NO NORMAL BRAKING. I/B ROLL SPLR, RUD HYD AND RUD FULL PRESS CAUTION LIGHTS ILLUMINATED. NORMAL BRAKING RETURNED DURING RETURN TAXI TO GATE. MAINTENANCE COULD NOT DUPLIDec 7, 2001 · N982HA · Dhav DHC8102 · Hydraulic System, MainSDR HNAA0100043Engine · smokeCREW REPORTED SMOKE/MIST FORMED IN THE CABIN AND COCKPIT. WHEN ENGINE BLEEDS WERE TURNED OFF SMOKE DISSIPATED. REPLACED #1 ENGINE.Aug 1, 2001 · N982HA · Dhav DHC8102 · Engine (Turbine/Turboprop)SDR HNAA0000041Cable · jammedPAX DOOR WOULD NOT FULLY OPEN. FOUND THE DOOR COUNTERBALANCE CABLE OFF OF THE CABLE DRUM. REPLACED THE CABLE, COUNTERBALANCE GAS STRUTS AND INSTALLED MODIFIED CABLE DRUM GUARD.May 16, 2000 · N982HA · Dhav DHC8102 · Passenger/Crew DoorsSDR HNAA0000004Window · crackedTHE CAPTAINS SIDE WINDOW OUTER PLY CRACKED IN FLIGHT. PIECES OF THE OUTER PLY SEPARATED FROM THE AIRCRAFT AND DAMAGED THE NR 1 PROP NR 1 BLADE. REPLACED THE CAPTAINS SIDE WINDOW AND NR 1 BLADE ON NR 1 PROP.Jan 11, 2000 · N982HA · Dhav DHC8102 · Flight Compartment WindowsSDR HNAA9698232Prpm Indicator · failedFLT 3091 - PHL-DCA - WHILE IN CRUISE, AT 5000 FEET, THE NR 2 ENGINE ROLLED BACK LOSING TORQUE, ITT AND FUEL FLOW. NH STABILIZED AT 54 PERCENT. ENGINE WAS OPERATED IN FEATHER UNIT TOUCHDOWN IN ORDER TO RETAIN ELECTRIC AND HYDRAULIC POWER. THE CAPTAIN DECLAREMay 21, 1996 · N982HA · Dhav DHC8102 · Propeller Indication SystemSDR 96ZZZM1043Eec · failedFLT 3091 - PHL-DCA - WHILE IN CRUISE, AT 5000 FEET, THE NR 2 ENGINE ROLLED BACK LOSING TORQUE, ITT AND FUEL FLOW. NH STABILIZED AT 54 PERCENT. ENGINE WAS OPERATED IN FEATHER UNIT TOUCHDOWN IN ORDER TO RETAIN ELECTRIC AND HYDRAULIC POWER. THE CAPTAIN DECLAREMay 21, 1996 · N982HA · Dhav DHC8102 · Fuel Control/Turbine Engines
Back to N982HA, cancelled Oct 28, 2009