N930FT, cancelled Aug 8, 2006

Service difficulty reports · 21

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 = 'N930FT' AND deregistration_id = 'N930FT-2006-08-08'
  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 NACA20030103Pressure Switch · false indicationNR 1 ENGINE OIL PRESSURE WARNING LIGHT(BYPASS), FLICKERING DURING CLIMB. INSPECTED NR 1 ENGINE MAIN OIL FILTER. NO METAL FOUND, INSTALLED NEW FILTER. DEFERRED OIL FILTER BYPASS INDICATION. OIL FILTER ON 12 HOUR INPECTION INTERVAL I.A.W. 727 MEL 79-2.Aug 6, 2003 · N930FT · Boeing 727100 · Engine Oil Indicating SystemSDR NACA20030101Warning Light · malfunctionedAFTER TAKE-OFF THE WHEEL WELL FIRE WARNING ILLUMINATED AND BELL SOUNDED. BOTH EXTINGUISHED UPON GEAR EXTENSION. CREW REPORTED HEAVY BRAKING AT PAEN. INSPECTED WHEEL WELL AND LOOPS. NO EVIDENCE OF FIRE NOTED. OPERATED WHEEL WELL FIRE WARNING TEST MULTIPLE TIMESAug 1, 2003 · N930FT · Boeing 727100 · Smoke DetectionSDR NACA20030096Switch · false indicationNR 2 SLAT INDICATES FORWARD AMBER LIGHT AND F.E. TRANSITE LIGHT WITH FLAPS UP. REPLACED NR 2 SLAT EXTEND SWITCH.Jul 22, 2003 · N930FT · Boeing 727100 · Leading Edge Slat ActuatorSDR NACA20030095Actuator · false indicationNR 2 SLAT LIGHT ON IN FLT WITH FLAPS IN UP POSITION. REPLACED SLAT ACTUATOR.Jul 21, 2003 · N930FT · Boeing 727100 · Leading Edge Slat ActuatorSDR NACA20030085Hinge · corrodedLT WING KRUEGER FLAP MOUNT BRACKET HINGE ASSEMBLY CORRODED. REMOVED AND REPLACED HINGE ASSEMBLY.May 8, 2003 · N930FT · Boeing 72723 · Leading Edge DevicesSDR NACA20030082Coupler · oscillatesRIGHT ON TAKE-OFF, UPPER YAW DAMPER OSCILATE AUTO PILOT DISENGAGE, LIGHT STAYED ON, WIND SHEAR CAUTION LIGHT STAYS ON. REPLACED UPPER YAW DAMPER COUPLER AND TESTED GOOD.Apr 3, 2003 · N930FT · Boeing 727100 · Autopilot SystemSDR NACA20030076Engine · shortedDISCREPANCY: ABORTED TAKE OFF DUE TO #1 ENGINE OIL PRESSURE LIGHT ILLUMINATED.CORRECTIVE ACTION: REMOVED MOISTURE FROM OIL DIFFERENTIAL PRESSURE SWITCH CANNON PLUG.Feb 11, 2003 · N930FT · Boeing 727100 · Engine Oil System WiringSDR NACA20030073Volt Regulator · trippedDISCREPANCY: ON TAKE OFF ROLL LOST #1 ENG GEN ESSENTIAL POWER WITH #3 ENGINE GENERATOR SELECTED.CORRECTIVE ACTION: REPLACED #1 VOLTAGE REGULATOR.Feb 6, 2003 · N930FT · Boeing 727100 · AC Power Distribution SystemSDR NACA20020021Spar Cap · corrodedDISCREPANCY: During "C" inspection, I.G. corrosion was discovered on the L/H wing aft spar lower chord, from w.s. 224.5 TO w.s. 241.0.CORRECTIVE ACTION: Lower spar cap being replaced from LBL 70.5 to W.S. 259.May 21, 2002 · N930FT · Boeing 72723 · Wing Main, Frame StructureSDR NACA20020036Attach FittingDURING "C" CHECK INSPECTION FOUND 2 EA STARTED DRILL HOLES IN THE ATTACH FITTING AT B.S. 1183, WL 278, AND RBL 27. CORRECTED BY INSTALLING 2 PIECE FREEZE PLUG, AND DOUBLER PER BOEING PROVIDED REPAIR PLAN NAC-ANC-02-00003H AND REIVISION NAC-ANC-02-00004H.Mar 14, 2002 · N930FT · Boeing 72723 · Fuselage Main, StructureSDR NACA20010038Smoke Detector · malfunctionedMECHANICAL INTERRUPTION IN ANCHORAGE AT 1522Z DUE TO LOWER CARGO FIRE WARNING HORN WENT OFF 3 TIMES. OPENED BOTH BELLY DOORS IMMEDIATELY UPON AIRCRAFT RETURN. FOUND NO SMOKE OR FIRE. UNLOADED BELLY'S AND PERFORMED LOWER CARGO SMOKE/FIRE PROTECTOR TEST, IAW Nov 10, 2001 · N930FT · Boeing 72723 · Smoke DetectionSDR NACA2001018Disk · vibrationMI AT ANC AT 2102Z, ENGINE SHUTDOWN DUE TO SEVERE VIBRATION. REMOVED AND REPLACED NR 1 ENGINE.Apr 30, 2001 · N930FT · Boeing 72723 · Turbine SectionSDR NACA20010005Control Unit · malfunctionedWITH ANTI SKID ON BRAKES RELEASED ON ROLLOUT. REPLACED ANTI SKID CONTROL MODULE.Jan 23, 2001 · N930FT · Boeing 72723 · Brake Anti-Skid SectionSDR NACA20010004Switch · dirtyON LANDING AT ANCHORAGE LOSS OF BRAKE, LOSS OF LEFT PACK, LOSS OF APU, GPWS, AND STICK SHAKER CAME ON. CLEANED NOSE GEAR SAFETY WARNING SWITCH.Jan 20, 2001 · N930FT · Boeing 72723 · Landing Gear Position and WarningSDR NACA200000018Brake · overheatedON DOWN WIND AT AKN, WHEEL WELL WARNING LIGHT AND BELL SOUNDED. AS SOON AS THE GEAR WENT OUT AS PER PROCEDURES THE BELL AND LIGHT WENT OUT, VISUAL VERIFICATION WITH CONTROL TOWER EVERYTHING LOOKED NORMAL WITH THEM. INSPECTED MAIN GEAR BRAKES FOR LEAKAGE AND Aug 16, 2000 · N930FT · Boeing 72723 · Overheat DetectionSDR 98ZZZM502Longeron · wornDURING C-CHECK INSPECTION DISCOVERED WEAR MARKS ON THE LEFT AND RIGHT KEEL BEAM LONGERONS AT THE MAIN LANDING GEAR DOOR HINGES, STATION 947 LEFT AND STATION 910 RIGHT. REPAIRED BY BLENDING AWAY THE DAMAGED AREAS, FLAP PEENED, ALODINED, PRIMED AND CORROSION PRJun 1, 1998 · N930FT · Boeing 72723 · Fuselage Main, Longeron/StringerSDR 98ZZZM501Skin · crackedDURING C-CHECK INSPECTION DISCOVERED A CRACK IN THE FIXED LEADING EDGE SKIN AT RIGHT WING LEADING EDGE STATION 155. REPAIRED BY TRIMMING OUT THE CRACK, HFEC NDT INSPECTING, FABRICATING AND INSTALLING A REPAIR DOUBLER AND FILLER WITH BLUEPRINT TYPE FASTENERS. Jun 1, 1998 · N930FT · Boeing 72723 · Wing, Plate/SkinSDR 98ZZZM500Bulkhead Fitting · corrodedDURING C-CHECK INSPECTION, DISCOVERED CORROSION ON THE RIGHT BULKHEAD TERMINAL FITTING AT STATION 870. REPAIRED BY BLENDING AWAY THE CORROSION, HFEC NDT INSPECTING, FLAP PEENING BLENDED AREA, ALODINING AND DOUBLE PRIMING BARE ALUMINUM AREAS. REPAIRED IAW EVIJun 1, 1998 · N930FT · Boeing 72723 · Fuselage Main, BulkheadSDR 97ZZZX3523Actuator · inaccurateANC - FLT 74 - RETURNED TO ANC AT 0235Z DUE TO NR 7 LEADING EDGE SLAT INDICATING IN-TRANSIT. MAINTENANCE REPLACED NR 7 LEADING EDGE SLAT ACTUATOR DUE TO FAULTY INDICATION AND RETURNED AIRCRAFT TO SERVICE. (X)Jul 12, 1997 · N930FT · Boeing 72723 · Leading Edge Slat ActuatorSDR 97ZZZX3517Slat Actuator · leakingON TAKEOFF ROLL, A-SYSTEM LOW LEVEL LIGHT CAME ON, TAXIED OFF AT BRAVO TO COMPANY RAMP. MAINTENANCE REPLACED NR 5 LEADING EDGE SLAT ACTUATOR AND RETURNED AIRCRAFT TO SERVICE. (X)Jun 8, 1997 · N930FT · Boeing 72723 · Leading Edge Slat ActuatorSDR 96ZZZX1465Windshield · crackedANC - FLT 105 - RETURNED TO ANC DUE TO FAILURE OF CAPTAIN'S WINDSHIELD OUTER PANEL. MAINTENANCE REPLACED L1 WINDOW. REPLACED WINDSHIELD HEAT CONTROLLER AS A PRECAUTIONARY MEASURE. ACFT RETURNED TO SERVICE.Jan 10, 1996 · N930FT · Boeing 72723 · Flight Compartment Windows
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