# Service difficulty reports: N982HA, cancelled Oct 28, 2009 A list on [N982HA, cancelled Oct 28, 2009](https://openairdocs.org/deregistered/N982HA-2009-10-28.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR HNAA2009031400091](https://openairdocs.org/sdr/HNAA2009031400091.md): Light · inoperative · Mar 4, 2009 · N982HA · Dhav DHC8102 · Emergency Lighting > ONE EMERGENCY ESCAPE PATH FLOOR LIGHT AT ROW 7 INOP. REMOVED AND REPLACED LIGHT BULB. - [SDR HNAA200911200393](https://openairdocs.org/sdr/HNAA200911200393.md): Bypass Switch · failed · Jan 7, 2009 · N982HA · Dhav DHC8102 · Fuel Controlling System > NR 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 PRE - [SDR HNAA2008113000333](https://openairdocs.org/sdr/HNAA2008113000333.md): Apu · odor · Nov 30, 2008 · N982HA · Dhav DHC8102 · APU Bleed Air System > UPON 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 SERVICE - [SDR HNAA2009021200050](https://openairdocs.org/sdr/HNAA2009021200050.md): Panel · corroded · Sep 13, 2008 · N982HA · Dhav DHC8102 · Wing Miscellaneous Structure > DURING '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, REGISTRATIO - [SDR HNAA2009020100041](https://openairdocs.org/sdr/HNAA2009020100041.md): Access Panel · corroded · Sep 13, 2008 · N982HA · Dhav DHC8102 · Wing, Plate/Skin > RT 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. - [SDR HNAA2009010900382](https://openairdocs.org/sdr/HNAA2009010900382.md): Door Frame · corroded · Sep 11, 2008 · N982HA · Dhav DHC8102 · Fuselage Main, Structure > DURING 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. - [SDR HNAA0800014](https://openairdocs.org/sdr/HNAA0800014.md): Door Seal · dirty · Dec 18, 2007 · N982HA · Dhav DHC8102 · Passenger/Crew Doors > WITH 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 CHECKED - [SDR HNAA0700295](https://openairdocs.org/sdr/HNAA0700295.md): Galley · odor · Dec 17, 2007 · N982HA · Dhav DHC8102 · Buffet/Galleys > ELECTRICAL 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. - [SDR HNAA0700286](https://openairdocs.org/sdr/HNAA0700286.md): Smoke Detector · defective · Dec 5, 2007 · N982HA · Dhav DHC8102 · Smoke Detection > BAG 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. - [SDR HNAA0700156](https://openairdocs.org/sdr/HNAA0700156.md): Mixer Box · worn · Jul 26, 2007 · N982HA · Dhav DHC8102 · Air Distribution System > CABIN 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. - [SDR HNAA070156](https://openairdocs.org/sdr/HNAA070156.md): Mixer Box · worn · Jul 26, 2007 · N982HA · Dhav DHC8102 · Air Distribution System > CABIN 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. - [SDR HNAA0700079](https://openairdocs.org/sdr/HNAA0700079.md): Hydraulic Line · leaking · Apr 16, 2007 · N982HA · Dhav DHC8102 · Hydraulic System, Main > WHILE 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 AC - [SDR HNAA0700224](https://openairdocs.org/sdr/HNAA0700224.md): Threshold · corroded · Jan 18, 2007 · N982HA · Dhav DHC8102 · Fuselage Miscellaneous Structure > AIR STAIR DOOR MAIN ENTRANCE THRESHOLD MEMBER CORRODED. REPLACED THRESHOLD. - [SDR HNAA0700229](https://openairdocs.org/sdr/HNAA0700229.md): Bracket · corroded · Jan 5, 2007 · N982HA · Dhav DHC8102 · Fuselage Main, Attach Fittings > CORROSION FOUND ON BRACKET AND CARGO FLOOR AT X598 ZONE 144 NEAR ENTRANCE AFT. CORROSION ON CARGO FLOOR REMOVED AND BRACKET REPLACED. - [SDR HNAA0700228](https://openairdocs.org/sdr/HNAA0700228.md): Seat Track · corroded · Jan 5, 2007 · N982HA · Dhav DHC8102 · Fuselage, Seat/Cargo Attach Fittings > SURFACE CORROSION ON LEFT INBOARD SEAT TRACK IN CARGO AREA. REPLACED LEFT INBOARD SEAT TRACK AFT CARGO BAY. - [SDR HNAA0700227](https://openairdocs.org/sdr/HNAA0700227.md): Seat Track · corroded · Jan 5, 2007 · N982HA · Dhav DHC8102 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON RIGHT INBOARD SEAT TRACK AT X201.00. REPLACED SEAT RAIL. - [SDR HNAA0700226](https://openairdocs.org/sdr/HNAA0700226.md): Frame · corroded · Jan 5, 2007 · N982HA · Dhav DHC8102 · Fuselage Main, Frame > CORROSION FOUND ON FRAME UNDERFLOOR AT X201.1560 BETWEEN STR 32S AND 30S. REPAIRED FRAME IAW ENGINEERING ORDER. - [SDR HNAA0700225](https://openairdocs.org/sdr/HNAA0700225.md): Seat Track · corroded · Jan 5, 2007 · N982HA · Dhav DHC8102 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON FORWARD LEFT SEAT RAIL. REMOVED CORROSION AND RETREATED RAIL. - [SDR HNAA0600116](https://openairdocs.org/sdr/HNAA0600116.md): Unknown · odor · Sep 25, 2006 · N982HA · Dhav DHC8102 · Air Distribution System > HOT 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. - [SDR HNAA0500096](https://openairdocs.org/sdr/HNAA0500096.md): Engine · smoke · Oct 26, 2005 · N982HA · Dhav DHC8102 · Engine (Turbine/Turboprop) > IN 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. - [SDR HNAA0500088](https://openairdocs.org/sdr/HNAA0500088.md): Actuator · bypassing · Oct 6, 2005 · N982HA · Dhav DHC8102 · Landing Gear Actuator > NOSE GEAR DID NOT EXTEND WHEN GEAR HANDLE SELECTED DOWN, GEAR DID EXTEND WHEN ALT. EXTENSION PROCEDURE WAS FOLLOWED. REMOVED AND REPLACED NOSE DOOR ACTUATOR. - [SDR HNAA0500072](https://openairdocs.org/sdr/HNAA0500072.md): Actuator · leaking · Jul 28, 2005 · N982HA · Dhav DHC8102 · Spoilers > NR 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 - [SDR HNAA0500026](https://openairdocs.org/sdr/HNAA0500026.md): Selector Valve · malfunctioned · Mar 18, 2005 · N982HA · Dhav DHC8102 · Landing Gear Retraction/Extension System > GEAR 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 REQ - [SDR HNAA0400072](https://openairdocs.org/sdr/HNAA0400072.md): Threshold · corroded · Jul 29, 2004 · N982HA · Dhav DHC8102 · Fuselage Miscellaneous Structure > PAX DOOR THRESHOLD CORRODED ON SILL PLATE. REMOVED AND REPLACED THRESHOLD. - [SDR HNAA0400071](https://openairdocs.org/sdr/HNAA0400071.md): Panel · corroded · Jul 29, 2004 · N982HA · Dhav DHC8102 · Wing, Plate/Skin > DURING C-CHECK INSPECTION FOUND STRESS PANELS 523 AND 623 AT WITH CORROSION IN COUNTERSINKS. REMOVED AND REPLACED PANELS. - [SDR PCAA0303050](https://openairdocs.org/sdr/PCAA0303050.md): Hydraulic Line · leaking · Mar 3, 2003 · N982HA · Dhav DHC8102 · Hydraulic System, Main > SYR-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 MAINT - [SDR HNAA0100079](https://openairdocs.org/sdr/HNAA0100079.md): Hydraulic System · malfunctioned · Dec 7, 2001 · N982HA · Dhav DHC8102 · Hydraulic System, Main > LOST 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 DUPLI - [SDR HNAA0100043](https://openairdocs.org/sdr/HNAA0100043.md): Engine · smoke · Aug 1, 2001 · N982HA · Dhav DHC8102 · Engine (Turbine/Turboprop) > CREW REPORTED SMOKE/MIST FORMED IN THE CABIN AND COCKPIT. WHEN ENGINE BLEEDS WERE TURNED OFF SMOKE DISSIPATED. REPLACED #1 ENGINE. - [SDR HNAA0000041](https://openairdocs.org/sdr/HNAA0000041.md): Cable · jammed · May 16, 2000 · N982HA · Dhav DHC8102 · Passenger/Crew Doors > PAX 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. - [SDR HNAA0000004](https://openairdocs.org/sdr/HNAA0000004.md): Window · cracked · Jan 11, 2000 · N982HA · Dhav DHC8102 · Flight Compartment Windows > THE 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. - [SDR HNAA9698232](https://openairdocs.org/sdr/HNAA9698232.md): Prpm Indicator · failed · May 21, 1996 · N982HA · Dhav DHC8102 · Propeller Indication System > FLT 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 DECLARE - [SDR 96ZZZM1043](https://openairdocs.org/sdr/96ZZZM1043.md): Eec · failed · May 21, 1996 · N982HA · Dhav DHC8102 · Fuel Control/Turbine Engines > FLT 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 DECLARE ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N982HA-2009-10-28/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.