N908HA, cancelled Sep 20, 2016
Service difficulty reports · 87
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 = 'N908HA' AND deregistration_id = 'N908HA-2016-09-20' 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 n_number = 'N908HA' AND deregistration_id = 'N908HA-2016-09-20' 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 HNAA2013112200583Bulb · inoperativeMIDDLE O/H EMERGENCY LIGHT IS INOPERATIVE. R & R BULB, OPS CHECKED GOOD.SDR HNAA2013082800479Bulb · failedCEILING ESCAPE PATH EMERGENCY LIGHT IS INOPERATIVE AT ROW 5DF. R & R BULB IAW AMM 33-51-00. OPS CHECKED GOOD.SDR HNAA2013073000434Trim System · out of adjustREJECTED TAKEOFF AT 20 KNOTS FOR WARNING HORN. ADJUSTED ELEVATOR TRIM, OPS NORMAL. PERFORMED WC 31-50-00Q, TAKEOFF WARNING SYS OPS CHECKED GOOD.SDR HNAA2013071900412Proximity Sensor · malfunctionedAFTER MLG RETRACTION, LEFT AMBER DOOR LIGHT ILLUMINATED. CYCLED LANDING GEAR HANDLE AND AFTER GEAR RETRACTION, BOTH AMBER LIGHTS FLICKERED AND STAYED OUT. R & R AFT PROXIMITY SENSOR AND GAPED IAW MM 32-10-21. OPS CHECKED GOOD ON RT SIDE SURGE DAMPER WAS REPASDR HNAA2013062600369Actuator · failedIN FLIGHT, LEFT TURNS ARE EXTREMELY DIFFICULT, FOUR TIMES MORE FORCE TO TURN LT THAN TO TURN RIGHT. R & R LT INBD SPOILER ACTUATOR. OPS CHECKED GOOD.SDR HNAA2013062600366Switch · failedF/A EMERGENCY LIGHT SWITCH WILL NOT ILLUMINATE. R & R F/A EMERGENCY LIGHT SWITCH. OPS CHECKED GOOD.SDR HNAA2013030600113Bulb · inoperativeFLOOR EMERGENCY LIGHT AT ROW 4 INOPERATIVE. R & R BULB. OPS CHECKED GOOD.SDR HNAA2013030600112Bulb · burned outLEFT SIDE, AFT EMERGENCY LIGHT IS DIM. R & R BULB. OPS CHECKED GOOD.SDR HNAA2013020400033Bulb · failedEMERGENCY FLOOR PATH LIGHT, 4TH FROM FORWARD POSITION IS INOPERATIVE. R & R BULB FOR EMERGENCY PATH FLOOR LIGHT. OPS CHECKED GOOD.SDR HNAA2013010701148Pseu · warning lightAFTER TAKEOFF, WITH GEAR UP, ALL UNSAFE LIGHTS FOR GEAR ARE ON. ALTERNATE INDICATION SHOWS THAT ALL ARE UP AND LOCKED. EXTENDED GEAR WITH ALTERNATE EXTENSION. JACKED ACFT. SWUNG GEAR SEVERAL TIMES. NO DEFECTS NOTED. R & R PSEU IAW MM 32-61-50. OPS CHECKSDR HNAA2012120301083Oil System · lowAFTER DEICING, ON TAKEOFF, NR 1 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED. ABORTED TAKEOFF AND SHUTDOWN NR 1 ENGINE. WARNING LIGHT WAS ILLUMINATED FOR APPR0X 5 SECONDS. INSPECTED NR 1 ENGINE AND FOUND ENGINE 3 QUARTS LOW. SERVICED ENGINE WITH 3 QUARTS OSDR HNAA2012112701073Warning Light · false activationNR 1 ITT INCREASED AND DECREASED ON CLIMBOUT. BOTH ANAOLOG AND DIGITAL. ALL OTHER PARAMETERS NORMAL. INSPECTED ENGINE WIRING FOR CONDITION AND SECURITY. CHECKED TRIM RESISTOR, READ WIRING FROM ENGINE TO GAUGE. CHECKED READING AT BOTH TERMINAL BLOCKS ON ENGISDR HNAA2012112601068Lens · dirtyEMERGENCY EXIT BETA LIGHT IS DIM. R & R BETA LIGHTS ON AFT EMERGENCY DOORS. CLEANED LENS COVER AND REINSTALLED. OPS CHECKED GOOD.SDR HNAA2012103101024Bulb · failedEMERGENCY FLOOR PATH LIGHT IS INOPERATIVE AT ROW 2DF. R & R BULB AT ROW 2DF EMERGENCY FLOOR PATH LIGHTING.SDR HNAA2012062200834Aileron · out of adjustCONTROL COLUMN IS 10-15 DEGREES RT OF CENTER ON TAKEOFF. LARGE CONTROL INPUTS REQUIRED AT 150 TO MAINTAIN LEVEL FLIGHT. ADJUSTED LT AILERON IAW MM 27-13-00. ACFT RELEASED FOR EVALUATION FLIGHT.SDR HNAA2012020800567Recorder · failedFDR CAUTION LIGHT ILLUMINATED. R & R FDR IAW 31-33-02. OPS CHECKED GOOD.SDR HNAA2012011600481Stringer · corrodedSTRINGER 31 RT AT STA X336 IS CORRODED. BLENDED MINOR SURFACE CORROSION IAW SRM 51-20-11. ALODINED AND PRIMED AREA IAW AMM 51-25-03.SDR HNAA2012011600480Structure · corrodedCORROSION FOUND AT S31, STA 207. BLENDED MINOR SURFACE CORROSION IAW SRM 51-20-11. ALODINED AND PRIMED AREA IAW AMM 51-25-03.SDR HNAA2012011600479Channel · corrodedPAX DOOR THRESHOLD CHANNEL IS CORRODED. CLEANED MINOR CORROSION OFF CHANNEL, ALODINED AND PRIMED.SDR HNAA2012011600478Threshold · corrodedPAX DOOR THRESHOLD IS CORRODED. R & R PAX DOOR THRESHOLD IAW ENG DWG 8531241.SDR HNAA2012011300475Battery Pack · inoperativeEMERGENCY LIGHTS ABOVE RT FWD EMERGENCY EXIT, GALLEY AND RT FWD FUSELAGE IS NOT WORKING. R & R LOWER EMERGENCY LIGHT BATTERY PACK.SDR HNAA2012011100471Bolt · corrodedLT TRIM TAB CONTROL ROD ATTACH HARDWARE HAS SURFACE CORROSION. R & R TRIM TAB CONTROL ATTACH HARDWARE IAW AMM 27-36-21.SDR HNAA2012010600456Light · brokenCENTER FLOOR PANEL NR 6 EMERGENCY LIGHT STRIP BROKEN. R & R EMERGENCY LIGHT STRIP ON PANEL.SDR HNAA2011111700386Lens · misinstalledEXIT LIGHT LENS COVER ABOVE RT FORWARD EMERGENCY EXIT NOT PROPERLY INSTALLED, CANNOT REMOVE EXIT FROM OPENING. REMOVED EXIT LENS COVER AND REINSTALLED DOOR CORRECTLY. OPERATES NORMALLY.SDR HNAA2011071400204Pressure Switch · malfunctionedUPON ADVANCING POWER LEVERS FOR TAKEOFF, THE ROLL SPOILERS OTBD HYD CAUTION LIGHT ILLUMINATED AND THE ROLL OTBD ADVISORY LIGHT STAYED ON. R & R ROLL SPOILER PSI SWITCH, GROUND RAN NR 2 ENGINE, OPS AND LEAKED CHECKED GOOD.SDR HNAA2011061300167Electronic Unit · failedCAN NOT TRANSMITT EITHER RADIO FROM NR1 ACP. R & R REU. OPS CHECKED GOOD. OK FOR SERVICE IAW -8 MM 23-50-00.SDR HNAA2011042400079Spoiler Sys · malfunctionedABORTED TAKEOFF DUE TO RT INBD AND OTBD SPOILERS NOT RETRACTING AFTER POWER LEVERS ADVANCED. AFTER CYCLING FLIGHT TAXI SWITCH AND ALL SPOILERS RETRACTED AFTER ADVANCING POWER LEVERS. INSPECTED RT SPOILERS, NO DEFECTS NOTED, GROUND RAN ACFT, CYCLED SPOILERS SSDR HNAA2011032000053Bulb · burned outROW 6 EMERGENCY FLOOR PATH LIGHT IS INOP. R & R LIGHT BULB AT ROW 6, OPS CHECKED GOOD.SDR HNAA2011030900040Inverter · failed26AC AND SECONDARY INVERTER CAUTION LIGHTS ILLUMINATED IN FLIGHT. SECONDARY INVERTER AND 115AC CIRCUIT BREAKER POPPED. LOST INSTRUMENT POWER RT SIDE INVERTERS WITH SECONDARY CIRCUIT BREAKER OUT 115 AC BUSS CIRCUIT BREAKER RESETS. R & R SECONDARY INVERTER IASDR HNAA2011021500021Switch · failedLT ELEVATOR HORN HEAT CAUTION LIGHT ILLUMINATED IN FLIGHT. REMOVED SWITCH 3015-S4 AND RETERMINATED WIRING 33A16-1 AND 9C16A-1 REF, WIRING DIAGRAM 30-25-02. OPS CHECKED GOOD IAW WORKCARD 30-10-10F.SDR HNAA2011021500008Lamp · burned outROW 2 CEILING EMERGENCY LIGHT INOP. RELAMP ROW 2 CEILING EMERGENCY LIGHT, OPS CHECKED GOOD.SDR HNAA2010091600216Oil Cooler · malfunctionedON CLIMBOUT, NR1 ENGINE OIL TEMP CLIMBED TO 125 DEGREES C. CYCLED ENGINE INTAKE DOOR TO SEE IF TEMP WOULD DECREASE. TEMP STAYED THE SAME. THEN REDUCED TORQUE TO 50 PERCENT. TEMP WENT TO 120 DEGREES C AFTER 18 MINUTES. REDUCED TORQUE TO 37.5 PERCENT. THEN SDR HNAA2010071300176Control Handle · malfunctionedAT ROTATION, AN ABNORNAL THUMP SOUND WAS HEARD FROM NOSE GEAR. RED NOSE GEAR UNSAFE LIGHT STAYED ON AND LT AND RT MAIN DOOR AMBER LIGHTS STAYED ON. AFTER APPR0X 4 MINUTES, GEAR RETRACTED AND LIGHTS EXTINGUISHED. PERFORMED ALTERNATE EXTENSION AT DESTINATION.SDR HNAA2009090300273Frame Splice · crackedSPLICE IS CRACKED ON LT SIDE OF FLIGHT COMPARTMENT FRAME JOINT AT STA X136.8 AND STR. 15P. ON LT SIDE OF FLIGHT COMPARTMENT FRAME JOINT AT STA. 136.8 AND STR 15P SPLICE REMOVED AND REPLACED IAW SRM 51-40-00 PD 1777.SDR HNAA2009090300278Housing · corrodedLEFT AUX BOOST PUMP RECEIVER FOUND CORRODED ON THREAD. LT AUX BOOST PUMP ASSY REMOVED AND REINSTALLED. TRANSFERED ON TASK CARD 005-55-13I. REMOVED AND REINSTALLED PLUG-IN ELEMENT IAW 28-21-16. NEW AUX PUMP RECEIVER INSTALLED IAW 28-21-16. OPS AND LEAK CHECKESDR HNAA2009090300276Angle · corrodedCORROSION FOUND ON PAX DOOR SHELL ANGLE AT BOTTOM AFT CORNER. PAX DOOR SHELL ANGLE REPLACED IAW MM 52-10-00 WITH SERVICABLE PART ON CARD SEC 2518.SDR HNAA2009090300275Fitting · corrodedCABIN INTERNAL LAVATORY FITTING CORRODED. CABIN INTERNAL LAVATORY FITTING REPLACED AND NEW PART INSTALLED IAW SRM 51-40-00, DWA 85320983 AND RD8-511-102SDR HNAA2009090300274Bracket · corrodedCORROSION FOUND ON PAX DOOR STEP BRACKETS (UNDERNEATH STAIRS, BOTH CTR BRACKETS AND FWD BOTTOM BRACKETS). PAX DOOR STEP BRACKET (BOTH CTR AND FWD BOTTOM) REPLACED IAW MM 20-14-01.SDR HNAA2009090300272Intercostal · corrodedCABIN UNDER FLOOR STA X396 RUDDER BELLCRANK INTERCOSTAL CORRODED. RUDDER CABLE TENSION RELEASED 07-06-09. UPPER CHANNEL OF CONTROL RUDDER SYS CTR BELLCRACK REPLACED WITH NEW PART LOCALLY FABRICATED, (FABRICATION COVERED ON WC SEQ 20-70) INSTALLED WITH SOLSDR HNAA2009082900266Skin · corrodedCATEGORY 1 CORROSION FOUND UNDER THE LT WING AUX BOOST PUMP EXTERNAL ANTI FRET RING ON THE LWR WING SKIN. LT AUX BOOST PUMP EXTERNAL AND INTERNAL SURFACE OF DOUBLER REPAIRED IAW RD8-57-4320 AND RD8-57-1907.SDR HNAA2009082700263Skin · dentedDURING HEAVY CHECK THE FOLLOWING DENTS FOUND ON RT FUSELAGE SKIN BETWEEN STA X136.8 AND 151.6 BETWEEN STR 23S-24S. BOTH DENTS FOUND TO BE IN LIMITS IAW EA 01-09233 AND EO 8-53-09-304.SDR HNAA2009082700259Structure · dentedDURING HEAVY CHECK A DENT WAS REPORTED AT 2 INCHES AFT OF THE PRESSURE BULKHEAD, HAS AN INSPECTION INTERVAL ESTABLISHED BY AN EO SIGNED BY A PERSON NOT AUTHORIZED AS A DT ENGINEER TO DETERMINE AN INSPECTION INTERVAL. THE DENT MAY NOT BE LOCATED IN THIS AREA SSDR HNAA2009090300277Panel · corrodedRIGHT WING STRESS PANEL 623AT CORRODED. RT WING STRESS PANEL 623AT REPLACED IAW AMM 57-20-05 PG 2425. RT WING STRESS PANEL 623AT INSTALLATION COVERED BY CARD 57-25-02R.SDR HNAA2009090300270Angle · corrodedBAGGAGE COMPARTMENT FLOOR LEVEL AT STA 597, STEP ANGLE FOUND CORRODED. REMOVED AND REPLACED IAW SRM 51-40-00 AT FLOOR LEVEL STA X 597 STEP ANGLE.SDR HNAA2009012000005Apu · smokeWITH AUXILIARY POWER UNIT RUNNING AND BLEEDS ON, SMOKE IN CABIN AND LAVATORY SMOKE DETECTOR SOUNDS. RAN AUXILIARY POWER UNIT WITH BLEED ON, VISIBLE HAZE APPEARS. INSP AUXILIARY POWER UNIT AREA NO DEFECTS NOTED. RAN ENGINES WITH BLEEDS NO HAZE NOTED. R&R AUXISDR HNAA2009011200395Ahrs · failedNR 2 ATTITUDE HEADING AND REFERENCE SYSTEM. R&R NR 2 ATTITUDE HEADING AND REFERENCE SYSTEM COMPUTER. OPS CHECK GOOD IAW MM 34-20-01.SDR HNAA2008121000347Light · inoperativeTHE 2ND CEILING EMERGENCY LIGHT INOP. RELAMP 2ND CEILING EMERGENCY LIGHT BULB.SDR HNAA2008120800341Hydraulic System · contaminatedJUST AFTER TAKEOFF, THE 'RUDDER PRESSURE' AND 'RUDDER FULL PRESSURE' CAUTION LIGHTS ILLUMINATED. THE CREW ELECTED TO RETURN TO THE ORIGINATING AIRFIELD. AFTER THE LANDING GEAR AND FLAPS WERE EXTENDED, THE CAUTION LIGHTS EXTINGUISHED. BOTH HYDRAULIC SYSTEMS SDR HNAA2008120600339Smoke Detector · malfunctionedDURING OPERATIONS, THE LAVATORY SMOKE DETECTOR BEGAN SOUNDING CONTINUOUSLY. THE TEST SWITCH WAS CYCLED AND THE UNIT OPERATED NORMALLY. THE AIRCRAFT WAS NOT TAKEN OUT OF SERVICE.SDR HNAA2008112100337Smoke Detector · defectiveTHE LAVATORY SMOKE DETECTOR SOUNDED OFF ABOUT 10 TIMES WITHOUT EVIDENCE OF SMOKE OR FUMES. THE SMOKE DETECTOR WAS DE-ACTIVATED IAW SPECIAL PROCEDURES. MAINTENANCE REPLACED THE DEFECTIVE UNIT, RE-ACTIVATED THE SYSTEM AND OPS CHECKED THE UNIT. OPS CHECKS WERE
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