N159A, cancelled Oct 24, 2007
Service difficulty reports · 54
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 = 'N159A' AND deregistration_id = 'N159A-2007-10-24' 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 = 'N159A' AND deregistration_id = 'N159A-2007-10-24' 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 COMA0010042Actuator · failedFLAP ANNUNCIATOR CONTROL FAULT APPEARED ON TAKEOFF ROLL. REMOVED LEFT INBOARD FLAP ACTUATOR AND INSTALLED A SERVICEABLE ONE.SDR COMA0010041Actuator · leakingFOUND RIGHT INBOARD FLAP ACTUATOR LEAKING. REMOVED AND REPLACED RIGHT INBOARD FLAP ACTUATOR. AIRCRAFT RETURNED TO SERVICE.SDR COMA0010046Actuator · malfunctionedFLAP CONTROL FAULT DURING T/O. REPLACED THE LEFT HAND INBOARD FLAP ACTUATOR.SDR COMA0010038Annunciator · malfunctionedFLAP CONTROL FAULT WARNING DURING TAKEOFF. REPLACED THE FLAP ANNUNCIATOR PANEL.SDR COMA0010029Control Unit · malfunctionedFLAP CONTROL FAULT. REPLACED THE FLAP CONTROL UNIT.SDR COMA0010012Switch · failedMASTER WARNING LIGHT ON. WILL NOT CANCEL. ADJUSTED THE FUEL SERVICE DOOR SWITCHES.SDR COMA0010002Flap · malfunctionedFLAP CONTROL FAULT DURING TAKEOFF. COULD NOT DUPLICATE, NO FAULTS FOUND IN FLAP SYSTEM.SDR COMA9910146Annunciator · failedTAKEOFF WAS ABORTED DUE TO MULTIPLE ERRATIC WARNINGS ON ANNUNCIATOR. REPLACED THE ANNUNCIATOR PANEL ASSEMBLY.SDR COMA9910145Warning · activatedFLAP CONTROL FAULT WARNING. COULD NOT DUPLICATE. SYSTEM TEST WAS NORMAL.SDR COMA9910096Battery · dischargedEMERGENCY LIGHTS ARE INOPERABLE. REPLACED EMERGENCY BATTERIES.SDR COMA9910083Indicator · malfunctionCOPILOTS AIR SPEED INDICATOR STUCK AT 100 KTS. REPLACED AIRSPEED INDICATOR.SDR COMA9910029Warning · malfunctionedFLAP CONTROL FAULT WARNING DURING TAKEOFF. COULD NOT DUPLICATE, OPERATIONAL CHECK OF FLAP SYSTEM WAS NORMAL.SDR COMA9910018Guide · corrodedDURING ROUTINE MAINTENANCE, THE UPPER CABLE GUIDE FITTING ON THE CARGO DOOR WAS FOUND TO HAVE SEVERE EXFOLIATION CORROSION. CORROSION WAS APPROX .1875 IN DEPTH OVER AN AREA OF 1X .50. THE FITTING WAS REPLACED WITH A SERVICEABLE FITTING AS PER EMB MAINTENANCESDR COMA9810286Relay · malfunctionEMERGENCY LIGHTS WILL NOT TURN OFF. REPLACED RELAY KO201.SDR COMA9810275Control · malfunctionedFLAP CONTROL FAULT DURING TAKEOFF. CANNOT DUPLICATE DISCREPANCY. C/W SERVICE BULLETIN 120-027-0067 FOR TROUBLESHOOTING.SDR COMA9810263Lamp · failedONE EMERGENCY LIGHT IS INOPERABLE. REPLACED LIGHT BULB.SDR COMA9810036Fan · failedAT CRUISE FLIGHT THE COCKPIT AND CABIN STARTED FILLING UP WITH SMOKE. CREW DESCENDED FROM 17,000 FT AND MADE UNSCHEDULED LANDING. FOUND RIGHT RECIRCULATION FAN TO BE FAULTY. REMOVED AND REPLACED FAN.SDR COMA9710413Stator · crackedDURING TEARDOWN OF BRAKE ASSY P/N 2-1585, THE ACCESSORY SHOP FOUND THE NUMBER ONE STATOR CRACKED. OVERHAULED BRAKE.SDR COMA9710412Stator · crackedDURING TEAR DOWN OF BRAKE ASSY P/N 2-1585, THE ACCESSORY SHOP FOUND THE NUMBER ONE STATOR CRACKED. OVERHAULED BRAKE.SDR COMA9710319Propeller · damagedRT PROPELLER STRUCK GROUND EQUIPMENT DURING TAXI OPERATION. REPLACED THE RT PROPELLER AND ENGINE.SDR COMA9710307Control Module · failedLANDING GEAR DID NOT RETRACT WHEN SELECTED UP. REPLACED THE LANDING GEAR CONTROL MODULE.SDR COMA9710165Skin · dentedDURING INSPECTION, FOUND A DENT IN THE RIGHT WING LOWER SKIN BETWEEN RIBS 24 AND 25 AFT OF THE AUXILIARY SPAR. CUT OUT DENT AND INSTALLED A FILLER OF THE SAME THICKNESS, INSTALLED AN INTERNAL DOUBLER MADE OF 0.040 INCH 2024-T3 AND AN EXTERNAL DOUBLER MADE OF SDR COMA9710151Relay · inoperativeRIGHT HAND PROPELLER AUTO FEATHER SYSTEM DOES NOT TEST. REPLACED RELAY K0039, SYSTEM TEST NORMAL.SDR COMA9710149Skin · corrodedON 2C INSPECTION, THE LOWER FUSELAGE SKIN WAS FOUND CORRODED UNDER THE TITANIUM STRAP AT FRAME 21, BETWEEN STRINGERS 19L AND 20L. THE SKIN WAS REPAIRED PER SRM 53-00-01, FIGURE 202.SDR COMA9710148Skin · corrodedON 2C INSPECTION, THE LOWER FUSELAGE SKIN WAS FOUND CORRODED UNDER TITANIUM STRAP AT FRAME 23, BETWEEN STRINGERS 20R AND 21R. THE SKIN WAS REPAIRED PER AERODESIGN REPORT NR 1896-1, REV A, DATED 2-7-97.SDR COMA9710147Sill · corrodedON 2C INSPECTION, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT SILL WAS FOUND CORRODED. REPLACED WITH A NEW PART PER SRM 51 STANDARD PRACTICES.SDR COMA9710146Crossbeam · corrodedON 2C INSPECTION, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT CROSSBEAM WAS FOUND CORRODED. REPLACED WITH A NEW PART PER SRM 51 STANDARD PRACTICES.SDR COMA9710145Butt Strap · corrodedON 2C INSPECTION, THE FUSELAGE FLOOR SUPPORT STRUCTURE LT BUTT-STRAP WAS FOUND CORRODED. REPLACED WITH A NEW PART PER SRM 51 STANDARD PRACTICES.SDR COMA9710144Butt Strap · corrodedON 2C INSPECTION, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT BUTT-STRAP WAS FOUND CORRODED. REPLACED WITH A NEW PART PER SRM 51 STANDARD PRACTICES.SDR COMA9710143Butt Strap · corrodedON 2C INSPECTION, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT BUTT STRAP WAS FOUND CORRODED. REPLACED WITH A NEW PART PER SRM 51 STANDARD PRACTICES.SDR COMA9710142Omega Beam · corrodedON 2C INSPECTION, THE FUSELAGE FLOOR SUPPORT STRUCTURE LT OMEGA BEAM WAS FOUND CORRODED. REPLACED WITH A NEW PART PER SRM 51 STANDARD PRACTICES.SDR COMA9710141Supporting Sect · corrodedON 2C INSPECTION, THE FWD SECTION RT SIDEWALL SEAT TRACK SUPPORTING SECTION WAS FOUND CORRODED. REPLACED WITH A NEW PART PER SRM CHAPT 51 STANDARD PRACTICES.SDR COMA9710140Supporting Sect · corrodedON 2C INSPECTION, THE AFT SECTION RT SIDEWALL SEAT TRACK SUPPORTING SECTION WAS FOUND CORRODED. REPLACED WITH A NEW PART PER SRM CHAPT 51 STANDARD PRACTICES.SDR COMA9710139Butt Strap · corrodedON 2C INSPECTION, THE FUSLEAGE FLOOR SUPPORT STRUCTURE CENTER BUTT STRAP WAS FOUND CORRODED. REPLACED WITH A NEW PART PER SRM 51 STANDARD PRACTICES AND AERODESIGN REPORT NR 1671-1, REV IR, DATED 10-22-95.SDR COMA9710138Angle · corrodedON 2C INSPECTION, THE FUSELAGE FLOOR SUPPORT STRUCTURE Z-ANGLE WAS FOUND CORRODED. REPLACED WITH A NEW PART PER SRM 51 STANDARD PRACTICES.SDR COMA9710137Angle · corrodedON 2C INSPECTION, THE AFT RIGHT EMERGENCY EXIT LOWER GUIDE PIN RECEPTACLES ON FUSELAGE AND THE LOWER ANGLE THEY'RE ATTACHED TO WERE FOUND CORRODED. THE LOWER ANGLE AND BOTH RECEPTACLES WERE REPLACED PER SRM CHAPT 51 STANDARD PRACTICES.SDR COMA9710136Skin · corrodedON 2C INSPECTION, THE FUSELAGE PASSENGER DOOR SURROUND STRUCTURE INNER SKIN WAS FOUND CORRODED BETWEEN FRAMES 15 AND 15A, JUST ABOVE STRINGER 17L. AN EXTERNAL DOUBLER REPAIR WAS INSTALLED PER AERODESIGN REPORT NR 2118-2, REV IR, DATED 2-8-97.SDR COMA9710135Skin · gougedON 2C CHECK, THE CARGO DOOR OUTER SKIN WAS FOUND GOUGED ALONG THE TOP EDGE BY CONTACTING THE FUSELAGE FIXED STOPS DURING DOOR OPENING AND CLOSING. THE SKIN WAS REPAIRED PER SRM 52-30-01, PG 201 TO 203.SDR COMA9610268Actuator · malfunctionFLAP ASYMMETRY WARNING WHEN FLAPS SELECTED TO 25 DEGREES. REPLACED THE RT INBD FLAP ACTUATOR.SDR COMA9610255Fuel Hose · leakingRT ENGINE IS LEAKING FUEL. REPLACED LEAKING PRIMARY FLOW HOSE ASSY.SDR COMA9610254Prop Blade · crackedRT PROPELLER, NR 1 BLADE IS CRACKED NEAR THE TIP AT TWO PLACES. REMOVED AND REPLACED THE NR 1 BLADE ASSY.SDR COMA9610185Hyd Pump · failedLEFT ENGINE DRIVEN HYDRAULIC PUMP FAILED. REPLACED HYDRAULIC PUMP.SDR COMA9610183Connector · defectiveLEFT ENGINE LOW HYDRAULIC PRESSURE WARNING DURING CLIMB. REPAIRED WIRING CONNECTOR JO807 IN LT ENGINE NACELLE.SDR COMA9610176Wow Sensor · failedLANDING GEAR HANDLE COULD NOT BE SELECTED TO UP POSITION. REPLACED THE RT MLG, WEIGHT ON WHEELS PROXIMITY SENSOR.SDR COMA9610153Skin · corrodedSEVERE CORROSION WAS FOUND DURING INSPECTION ON THE LOWER FUSELAGE SKIN AT FRAME 22 BETWEEN STRINGERS 21R AND 20R. THE CORROSION IS WHERE THE SKIN CONTACTS THE TITANIUM REINFORCING STRAP P/N 120-22409-001. THE DAMAGED AREA WAS REMOVED AND A REPAIR INSTALLED SDR COMA9610122Actuator · malfunctionFLAP DISAGREEMENT WARNING. INBD FLAPS INDICATE 5 DEGREES DOWN WHEN SELECTED UP. REPLACED THE LT INBD FLAP ACTUATOR. PART TOTAL CYCLES, 7,272.SDR COMA9610111Brake · wornLEFT ANTI-SKID INOP WARNING DURING LANDING. LT MLG OUTBD TIRE FOUND FLAT DURING POST FLIGHT. REPLACED THE LT MLG OUTBD BRAKE ASSY.SDR COMA9511985Battery · dischargedBACKUP BATTERY DOES NOT TEST. REPLACED THE EMERGENCY POWER SUPPLY BATTERY.SDR COMA9511962Bracket · crackedTHE CARGO DOOR LIFTING MECHANISM TORSION BAR FORWARD SUPPORT ATTACH BRACKET WAS FOUND CRACKED. THE BRACKET WAS REPLACED WITH SUBSTITUTE PART OF THICKER MATERIAL (P/N 120-20235-005), PER AERODESIGN REPORT NR 1397-1, DATED 2-15-95.SDR COMA1956Valve · stuckDURING FLIGHT, THE NR 1 ENGINE OIL PRESSURE DECREASED TO 52 PSI, ALONG WITH SOUND OF RELAYS CLICKING IN PILOTS SIDE PANEL. WHILE THE PROPELLER WAS IN FEATHER OIL PRESSURE RETURNED TO 60 PSI. REMOVED AND REPLACED THE P2.5 SWITCHING VALVE.
Back to N159A, cancelled Oct 24, 2007