N912HA, cancelled Sep 21, 2016

Service difficulty reports · 90

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 = 'N912HA' AND deregistration_id = 'N912HA-2016-09-21'
  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 HNAA0700278Switch · looseWHEN THE GEAR WAS SELECTED DOWN, THE CREW GOT THREE RED LIGHTS. PERFORMED EMERGENCY EXTENSION AND GOT THREE GREEN LIGHTS. THE LANDING GEAR SELECTOR VALVE WAS REPLACED. ON 1 DECEMBER WHEN THE GEAR WAS SELECTED DOWN, THE CREW GOT THREE RED LIGHTS, AFTER LEVELNov 29, 2007 · N912HA · Dhav DHC8102 · Landing Gear Position and WarningSDR HNAA0700127Clamp · damagedRIGHT WING AUX FUEL BOOST PUMP CLAMP RING FOUND DAMAGED AND CORRODED. RIGHT WING AUX FUEL BOOST PUMP CLAMP RING REPLACED AS PER S/B 8-57-28, LEAK CHECK REF SEQ 23.Jun 28, 2007 · N912HA · Dhav DHC8102 · Fuel Boost PumpSDR HNAA0700128Doubler · corrodedLEFT AUX BOOST PUMP (FUEL) WING DOUBLER FOUND CORRODED INSIDE AND OUTSIDE FUEL TANK. LEFT AUX BOOST PUMP (FUEL) WING DOUBLER INSIDE AND OUTSIDE OF FUEL TANK CORROSION REMOVED IAW RD8-57-3679 (MATERIAL REMAINING .415") S/B 8-57-28 PREVIOUSLY COMPLIED WITH. HFJun 28, 2007 · N912HA · Dhav DHC8102 · Wing Miscellaneous StructureSDR HNAA070128Doubler · corrodedLEFT AUX BOOST PUMP (FUEL) WING DOUBLER FOUND CORRODED INSIDE AND OUTSIDE FUEL TANK. LEFT AUX BOOST PUMP (FUEL) WING DOUBLER INSIDE AND OUTSIDE OF FUEL TANK CORROSION REMOVED IAW RD8-57-3679 (MATERIAL REMAINING .415") S/B 8-57-28 PREVIOUSLY COMPLIED WITH. HFJun 28, 2007 · N912HA · Dhav DHC8102 · Wing, Plate/SkinSDR HNAA0700123Skin · corrodedSIX BLIND FASTENERS FOUND CORRODED ON RIGHT SIDE OF SKIN OF FORE RUDDER NEXT TO LOWER ACTUATOR FITTING. RIGHT SIDE OF SKIN OF FORE RUDDER NEXT TO ACTUATOR FITTING 6 BLIND FASTENERS REPLACED IAW RD8-55-024.Jun 27, 2007 · N912HA · Dhav DHC8102 · Rudder, Plate/SkinSDR HNAA0700125Doubler · damagedCORROSION FOUND IN VARIOUS PLACES IN LAV SERVICE PANEL. LAVATORY MACHINED SERVICE DOOR DOUBLER REPAIRED AS PER 8-53-07-3235 AND INSTALLED WITH SOLID RIVETS AS PER SRM 51-40-00, HFEC CUT OUT NO CRACKS.Jun 26, 2007 · N912HA · Dhav DHC8102 · Service DoorsSDR HNAA0700124Panel · corrodedELEVEN CORRODED HOLES ON STRESS PANEL 521AT. ELEVEN BUSHINGS FABRICATED LOCALLY IAW WITH RD 8-53-2674 ACCESS PANEL 521AT REPLACED ON SEQ 5042.Jun 26, 2007 · N912HA · Dhav DHC8102 · Wing, Plate/SkinSDR HNAA0700126Skin · corrodedRIGHT WING AUX FUEL BOOST PUMP SKIN DOUBLER CORROSION SUSPECTED ON PREVIOUS BLENDED AREA (INSIDE TANK). RIGHT WING AUX FUEL PUMP WING BLENDED AS PER RD 8-57-1907 (.45 MIN REMAINING) SB 8-57-28 FOUND PREVIOUSLY COMPLIED WITH. HFEC & DISBOND C/O IAW RD 8-57-19Jun 26, 2007 · N912HA · Dhav DHC8102 · Wing, Plate/SkinSDR HNAA00125Panel · corrodedCORROSION FOUND IN VARIOUS PLACES IN LAV SERVICE PANEL. LAVATORY MACHINED SERVICE DOOR DOUBLER REPAIRED AS PER 8-53-07-3235 AND INSTALLED WITH SOLID RIVETS AS PER SRM 51-40-00 HFEC CUTOUT NO CRACKS.Jun 26, 2007 · N912HA · Dhav DHC8102 · Service DoorsSDR HNAA0700134Failsafe · corrodedRIGHT ELEV O/B HINGE FAIL SAFE CORRODED.Jun 6, 2007 · N912HA · Dhav DHC8102 · Elevator, Spar/RibSDR HNAA0700133Drain Line · corrodedCORROSION FOUND ON LAV DRAIN TUBE FLANGE.Jun 1, 2007 · N912HA · Dhav DHC8102 · Waste Disposal SystemSDR HNAA0700132Skin Panel · debondedDISBOND DETECTED ON LEFT FUSELAGE SKIN PANEL BETWEEN FUSELAGE STA 488.50 AND STA 510.00 AND BETWEEN STR 23 AND STR 24.May 29, 2007 · N912HA · Dhav DHC8102 · Fuselage Main, Plate/SkinSDR HNAA0700053Light · inoperativeEMERGENCY LIGHT SWITCH ON FLIGHT ATTENDANTS PANEL IS NOT ILLUMINATED. RELAMPED SWITCH.Mar 25, 2007 · N912HA · Dhav DHC8102 · Emergency LightingSDR HNAA0600219Unknown · odorELECTRICAL BURNING ODOR LT CABIN BETWEEN ROWS 1 AND 2. AFTER SELECTING OVERHEAD LIGHTS OFF ODOR DISSIPATED, ISSUED MEL. MORE TO FOLLOW.Jan 12, 2007 · N912HA · Dhav DHC8102 · Air Distribution SystemSDR HNAA0600114Coffeemaker · overheatedBURNING ODOR IN CABIN AND COCKPIT. FOUND SEAL ON HOT JUG BURNING DUE TO NO LIQUID INSIDE REMOVED AND REPLACED HOT JUG.Sep 16, 2006 · N912HA · Dhav DHC8102 · Buffet/GalleysSDR HNAA0600044Door · out of rigNOSE GEAR DOOR AMBER LIGHT REMAINED ON AFTER TAKEOFF. RIGGED NOSE GEAR DOOR SYSTEM.Jun 1, 2006 · N912HA · Dhav DHC8102 · Landing Gear Door Retract SectionSDR HNAA0600049Selector Valve · faultyLANDING GEAR WOULD NOT EXTEND WHEN SELECTED. CREW PERFORMED ALTERNATE EXTENSION AND ALL GEAR EXTENDED NORMALLY. AN EMERGENCY WAS DECLARED. THE LANDING GEAR SELECTOR VALVE WAS REPLACED.May 30, 2006 · N912HA · Dhav DHC8102 · Landing Gear SelectorSDR HNAA0600023Connector · dirtyDURING CLIMBOUT RIGHT A/C BUSS FELL OFF LINE WITH ASSOCIATED TRU CAUTION LIGHT. CLEANED NR 2 AC GEN CONNECTOR.Apr 8, 2006 · N912HA · Dhav DHC8102 · AC Generation SystemSDR HNAA0500102Shim · out of adjustAIRCRAFT RETURNED TO FIELD DUE TO OIL PRESSURE RISING TO 70 PSI ON CLIMBOUT. REMOVED TWO SHIMS AT OIL PRESSURE REGULATOR.Dec 7, 2005 · N912HA · Dhav DHC8102 · Engine Oil PressureSDR HNAA0500100Switch · lack of lubeDURING CLIMBOUT AT ABOUT 200 TO 300 FEET NR 2 PROP CYCLED ABOUT 150 TO 200 RPM AND TQ CYCLED 85 TO 115 PERCENT FOR ABOUT 90 SECONDS. LUBED BETA BACK UP POWER LEVER SWITCHES, REINSTATED BETA LOCKOUT SWITCHES AND C/W BETA GROUND LOGIC WORK CARD.Nov 27, 2005 · N912HA · Dhav DHC8102 · Propeller Controlling SystemSDR HNAA0500079Check Valve · crackedAT GEAR RETRACTION NR 2 ISOV CAUTION LIGHT ILLUMINATED FOLLOWED BY ROLL SPOILER HYD. CAUTION LIGHT NR 2 QUANTITY DROPPED TO 1/2 QT. SYSTEM PRESSURE REMAINED NORMAL. REPLACED CHECK VALVE.Aug 26, 2005 · N912HA · Dhav DHC8102 · Hydraulic System, MainSDR HNAA0500045Proximity Sensor · brokenLEFT AMBER GEAR DOOR LIGHT ON DURING GEAR RETRACTION. REPLACED PROXIMITY SENSOR. (M)May 16, 2005 · N912HA · Dhav DHC8102 · Landing Gear Position and WarningSDR HNAA0500001Wire Harness · misroutedAFTER TAKEOFF NOSE GEAR WOULD NOT RETRACT AND LT & RT GEAR DOORS REMAINED OPEN, NOSE GEAR RED TRANSIT LIGHT STAYED ILLUMINATED. LT AND RT MAINS RETRACTED NORMALLY. REROUTED ELECTRICAL HARNESS AND SEATED CONNECTORS, OPS CHECK GOOD.Jan 5, 2005 · N912HA · Dhav DHC8102 · Landing Gear System WiringSDR HNAA0400176Connector · not seatedAFTER TAKEOFF NOSE GEAR WOULD NOT RETRACT AND LT/RT GEAR DOORS REMAINED OPEN, NOSE GEAR RED TRANSIT LIGHT STAYED ILLUMINATED. LT AND RT MAINS RETRACTED NORMALLY. REROUTED ELECTRICAL HARNESS AND SEATED CONNECTOR OPS CHECK GOOD.Jan 5, 2005 · N912HA · Dhav DHC8102 · Landing Gear Retraction/Extension SystemSDR HNAA0400156Door · out of adjustAFTER GEAR RETRACTION LEFT MAIN GEAR DOOR LT CAME ON AND VISUALLY CONFIRMED DOOR OPEN. DUE TO THE AIRSPEED RESTRICTION, A/C RETURNED TO PHL. A/C WILL FERRY TO SBY FOR REPAIRS. ADJUSTED LEFT FWD GEAR DOOR. GEAR SWINGS, OP'S CHECK GOOD.Oct 25, 2004 · N912HA · Dhav DHC8102 · Landing Gear Door Retract SectionSDR HNAA0400035Acm · seizedACM SEIZES UP AND SMOKED UP CABINApr 7, 2004 · N912HA · Dhav DHC8102 · Cabin Cooling SystemSDR HNAA0200075Boot · contaminatedON CLIMBOUT DEICE PRESSURE DROPPED TO 10 PSI FOLLOWED BY ILLUMINATION OF THE DEICE PRESSURE CAUTION LIGHT. RT WING SECOND BOOT FROM TIP AND ALL TAIL BOOTS WOULD NOT SHOW INFLATION. AIRCRAFT RETURNED TO FIELD. MAINTENANCE PURGED WATER FROM SYSTEM. GROUND CHNov 5, 2002 · N912HA · Dhav DHC8102 · Airfoil Anti/De-ice SystemSDR HNAA0200050Potentiometer · inoperativeUNCOMMANDED LEFT WING DOWN TRIM IN FLIGHT, RECENTERED TRIM WITH AILERON TRIM SWITCH. REPLACED AILERON TRIM TAB POTENTIOMETER.Jul 12, 2002 · N912HA · Dhav DHC8102 · Aileron Tab Control SystemSDR HNAA0100077Hydraulic Line · leaking#2 HYDRAILIC SYSTEM FLUID LOSS DOWN TO ISOLATION VALVE ACTUATION. PRESSURE REMAINED NORMAL WITH APPROX. 1/2 QT. INDICATED RESERVOIR QUANTITY. AIRCRAFT DIVERTED TO SAV. FOUND FLEX LINE TO NLG DRAG STRUT ACTUATOR LEAKING. REPLACED FLEX LINE.Nov 21, 2001 · N912HA · Dhav DHC8102 · Hydraulic Power SystemSDR HNAA0100017Indicator · defectiveWHILE PARKING THE AIRCRAFT CREW NOTICED RADAR INDICATOR CRT WAS COVERED WITH GREEN LINES AND A BURNING SMELL COMING FROM THE INDICATOR. REPLACED RADAR INDICATOR.Mar 8, 2001 · N912HA · Dhav DHC8102 · Weather Radar SystemSDR HNAA0000054Frame · corrodedFRAME LEG AT STA 240.5 OUTBOARD OF STRINGER 31 CORRODED AT WATERWAY PASSAGE. REPAIRED IAW SRM 53-20-21.Jul 6, 2000 · N912HA · Dhav DHC8102 · Fuselage Main, FrameSDR HNAA9900068Actuator · leakingUPON GEAR RETRACTION THE RT MLG DOOR REMAINED OPEN. CYCLED GEAR, DOOR CLOSED NORMALLY. REMOVED AND REPLACED NR 2 MLG DOOR ACTUATOR.Jun 13, 1999 · N912HA · Dhav DHC8102 · Landing Gear Door ActuatorSDR HNAA9900067Retract Mech · malfunctionedRT MAIN LANDING GEAR DOOR DID NOT CLOSE AFTER RETRACTION. CYCLED GEAR AND OK.Jun 13, 1999 · N912HA · Dhav DHC8102 · Landing Gear Door Retract SectionSDR 98ZZZX2254Battery · dischargedPHL/SBY - FLT 3221 - AFT CEILING EMERGENCY DOWN LIGHT INOPERABLE. LEFT EMERGENCY EGRESS EXIT SIGN AND LOCATOR LIGHTS INOPERABLE. REPLACED EMERGENCY LIGHT BATTERY PACK 3351-PS3.Feb 12, 1998 · N912HA · Dhav DHC8102 · Emergency LightingSDR HNAA9591231Control Unit · failedCHO/CLT - FLT 3156 - DURING PRE-FLIGHT CHECKS, THE AUTOFEATHER TEST WAS FOUND INOPERATIVE. COULD NOT DUPLICATE. REMOVED AND REPLACED THE NR 1 AND NR 2 TORQUE SENSOR CONTROL UNITS. REFERENCE CONTROL NR 96ZZZX323. (X)Dec 30, 1995 · N912HA · Dhav DHC8102 · Propeller Controlling SystemSDR 96ZZZX323Control Unit · failedCHO/CLT - FLT 3156 - DURING PRE-FLIGHT CHECKS, THE AUTOFEATHER TEST WAS FOUND INOPERATIVE. COULD NOT DUPLICATE. REMOVED AND REPLACED THE NR 1 AND NR 2 TORQUE SENSOR CONTROL UNITS. REFERENCE CONTROL NR HNAA9591231.Dec 30, 1995 · N912HA · Dhav DHC8102 · Propeller Controlling SystemSDR 95ZZZM250Sensor · malfunctionFLT 3409 - FLL-TPA - WHILE ATTEMPTING TO SET TAKEOFF POWER, NR 1 ENGINE TORQUE DID NOT COME UP AND PROPELLER WENT INTO FEATHER. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. REMOVED AND REPLACED THE NR 1 TORQUE SENSOR ELECTRONIC CONJul 20, 1995 · N912HA · Dhav DHC8102 · Engine BMEP/Torque IndicatingSDR 95ZZZM249Tseu · malfunctionFLT 3409 - FLL-TPA - WHILE ATTEMPTING TO SET TAKEOFF POWER, NR 1 ENGINE TORQUE DID NOT COME UP AND PROPELLER WENT INTO FEATHER. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. REMOVED AND REPLACED THE NR 1 TORQUE SENSOR ELECTRONIC CONJul 20, 1995 · N912HA · Dhav DHC8102 · Engine BMEP/Torque IndicatingSDR 95ZZZX3548Ecu · failedCHO/BWI - FLT 3201 - ON CLIMB-OUT, NR 1 ENGINE TORQUE UPTRIMMED TO 125 PERCENT. AT FLIGHT IDLE, STILL AT 110 PERCENT. CAPTAIN SHUT ENGINE DOWN IN-FLIGHT. AIRCRAFT DIVERTED TO RIC AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 ENGINE ELECTRONIC CONTRJul 7, 1995 · N912HA · Dhav DHC8102 · Fuel Control/Turbine EnginesSDR 95ZZZM124Eel Connector · looseFLT NR 3427 - HPN-PHL - DURING PREFLIGHT WALKAROUND, TWO RED EMERGENCY FLOOR LIGHTS WERE FOUND INOP AT ROW 1. SECURED THE CONNECTOR UNDER THE FLOOR AT ROW 1.May 24, 1995 · N912HA · Dhav DHC8102 · Emergency Lighting
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