N426FB, cancelled Apr 7, 2017
Service difficulty reports · 39
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 = 'N426FB' AND deregistration_id = 'N426FB-2017-04-07' 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 = 'N426FB' AND deregistration_id = 'N426FB-2017-04-07' 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 ARWA20020810TransducerLOG PAGE # 110608. DISCREPANCY: NEAR END OF TAKEOFF ROLL PTY MAIN GEAR SPOILER INOPERATIVE LIGHT CAME ON. CORRECTIVE ACTION:REMOVED AND REPLACED #5 ANTISKID TRANSDUCER OPERATIONAL CHECK NORMAL IAW 27-35-0.SDR ARWA20020802Control Panel · malfunctionedAFTER STARTING ENGINE NR 2 AND ENGINE NR 3 HAD SMOKE IN COCKPIT. CREW EVACUATED AIRCRAFT. FOUND NR 2 AC CONTROL PANEL BURNT OUT. REMOVED AND REPLACED NR 2 AC CONTROL PANEL IAW MM 24-5-7, ALSO REMOVED AND REPLACED GENERATOR RELAY IAW MM 24-5-3. OPERATIONS CSDR ARWA20020315Clutch · failedNR 2 ENGINE SHUTDOWN DUE FLUCTUATING OIL PRESSURE GAUGE AND LIGHT AND OIL QTY READING ZERO, NOTE OIL TEMP READING NORMAL 75 DEG. REMOVED AND REPLACED ENGINE. FUNCTIONAL TEST COMPLETED AND FOUND SATISFACTORY. ACFT RETURNED TO SERVICE. ENGINE SENT TO REPAIR SDR ARWA20020313Oil System · fluctuatesAT 1140Z NR 2 ENGINE SHUTDOWN DUE FLUCTUATING OIL PRESSURE GAUGE AND LIGHT AND OIL QTY READING ZERO, NOTE OIL TEMP READING NORMAL 75 DEG. REMOVED AND REPLACED ENGINE. FUNCTIONAL TEST COMPLETED AND FOUND SATISFACTORY. ACFT RETURNED TO SERVICE. ENGINE (S/N 6SDR ARWA20020314Fluid · lowUPON LANDING, HYDRAULIC PRESSURED DROPPED TO ZERO AFTER GEAR EXTENSION. ALL CHECKLIST ACCOMPLISHED. SERVICED HYDRAULIC IAW MM 12-4-0, NO LEAKS NOTED.SDR ARWA20020309Cylinder · leakingUPON CLEARING THE RUNWAY EXPERIENCED A TOTAL LOSS OF HYDRAULIC FLUID AND PRESSURE ALL CHECKLIST COMPLIED WITH. AIRBRAKE USED TO STOP AIRCRAFT WITHOUT INCIDENT. FOUND FWD LEFT BOGIE TRIM CYLINDER WITH HYDRAULIC LEAK. REMOVED AND REPLACED MLG FWD LEFT BOGIE TSDR ARWA20020308Indicator · sticksABORTED TAKEOFF DUE TO ENGINE NR 4 MOMENTARY POWER LOSS, ALL ENGINE PARAMETERS NORMAL. RETURN TO RAMP. PERFORMED ENGINE RUN-UP AND NOTICED EPR INDICATOR STICKING. REMOVED AND REPLACED EPR INDICATOR IAW MM 77-1-2 AND SYSTEMS OPS CHECKED NORMAL IAW MM 71-0.SDR ARWA20020307Volt Regulator · malfunctionedON FINAL APPROACH SMOKE CAME FROM RT SIDE OF COCKPIT. REMOVED AND REPLACED NR 4 VOLTAGE REGULATOR (BURNT) IAW MM 29-5-11, OPS CHECKED NORMAL IAW MM 24-5-1.SDR ARWA20020304Housing · damagedDURING CLIMBOUT THROUGH 16,000 FEET; NR 2 ENGINE OIL PRESSURE GAUGE BEGAN FLUCTUATING AT 180, AND NR 2 OIL PRESSURE LIGHT BEGAN FLICKERING, THEN WENT STEADY. ACCOMPLISHED APPROPRIATE ABNORMAL CHECKLISTS AND SHUTDOWN ENGINE AT 22:15 ENGINE OIL PRESSURE WINDMILSDR ARWA20020302Relief Valve · faultyDURING CLIMBOUT THROUGH 15,000 FT, NR 2 ENGINE OIL PRESSURE BEGAN FLUCTUATING, NR 2 OIL PRESSURE LIGHT ILLUMINATED. ACCOMPLISHED APPROPRIATE CHECK LISTS AND SHUT DOWN ENGINE AT 00:15Z, OIL WINDMILLED AT 12 PSI. AIRCRAFT RETURNED TO PTY AND LANDED UNEVENTFUL.SDR ARWA20011215Line · leakingNR 3 ENGINE LOSS OF OIL QUANTITY OSCILLATING OIL PRESS AND OIL PRESS WARNING ON AND OFF. SHUT DOWN NR 3 ENGINE AS PER ABNORMAL CHECKLIST OIL PRESS 15 PSI, 1 HOUR WINDMILLING. AIRCRAFT RETURNED TO KMIA UNEVENTFUL. INSPECTED ENGINE AND FOUND ENGINE OIL COOLERSDR ARWA20011210Brace · brokenAT FLIGHT LEVEL 31.0 HEARD LOUD BANG NOISE UNDER COCKPIT AREA, ALSO ON APPROACH LOWERING GEAR LARGE BANG AND AIRCRAFT SHOOK. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND LT NOSE LANDING GEAR SIDE BRACE RETRACT ACT LUG BROKEN. REMOVED AND REPLACED LT NOSE LANDINGSDR ARWA20011201Csd · failedON TAKEOFF AT KMIA, NR 4 GENERATOR ZNS FAULT; ABORTED TAKEOFF AT 90 KTS AND F/O LOST LIGHTS, INSTRUMENTS AND RADIO COMMUNICATION. F/O'S INSTRUMENTS AND LIGHT OPS CK NORMAL AFTER BUS RESET IAW MM 23-2-0 & 24-1-0. REMOVED AND REPLACED NR 4 ENGINE CSD ASSY IAW MSDR ARWA20011124Blade · failedON TAKE OFF MIAMI A LOUD BANG FOLLOWED BY HIGH VIBRATION ON NR 2 ENGINE REJECTED THE TAKE OFF ROLL. FOUND C2 BLADE FAILURE. REMOVED AND REPLACED NR 2 ENGINE. OPS AND LEAK CHECK NORMAL.SDR ARWA20011120Skin · corrodedAT STATIONS 960 TO 980 PITTING CORROSION AT INNER SIDE OF FUSELAGE SKIN BETWEEN STRINGERS 28R & 25R. REPAIRED FUSELAGE SKIN BETWEEN STATION 980 TO 1020 STR 28 & 25L IAW DRAWING AS 11354.SDR ARWA20011119Support · corrodedUPON INSPECTION THE FOLLOWING WAS FOUND: VERTICAL SUPPORT AT STATION 980 RT SIDE LOWER END CORRODED, WHERE SUPPORT ATTACHES TO CIRCUMFERENTIAL FRAME. REPAIRED VERTICAL SUPPORT AT STA 980 LT LOWER END IAW DRAWING NR AS 11355.SDR ARWA2001118Frame · corrodedUPON INSPECTION THE FOLLOWING WAS FOUND: AT STATION 980 AFT BELLY COMPARTMENT, APPROX S-31 CORROSION AT CIRCUMFERENTIAL. REPAIR STA 980 CIRCUMFERENTIAL APPROX S-31L IAW DRAWING AS 11356.SDR ARAWA000901Fuel Control · malfunctionedON APPROACH TO SKCL, NR 4 ENGINE FAILED. PERFORMED EMERGENCY PROCEDURES AS PER FINE AIR PROCEDURES. LANDING WITHOUT INCIDENT. REMOVED AND REPLACED NR 4 ENGINE FUEL CONTROL IAW MM 73-22-00. REMOVED AND REPLACED NR 4 ENGINE DRIVEN FUEL PUMP IAW MM 73-01-01. SDR 20001208AP006Fitting · crackedDURING AN INSPECTION FOUND THE FOLLOWING, CRACKED LEFT MLG AUXILIARY SPAR FITTING. REPLACED AUXILIARY SPAR FITTING IAW DOUGLAS DRAWING NR 5802630. (M)SDR 20001208AP002Spar Cap · crackedDURING AN INSPECTION OF THE PYLON FOUND FORWARD SPAR CRACK AT STATION XFS 550. REPAIRED FORWARD PYLON IAW DOUGLAS DRAWING NR 5802712. (M)SDR 20001208AP001Fitting · crackedDURING AN INSPECTION FOUND THE FOLLOWING, CRACKED FITTING LEFT SIDE LONGERON 24. REPLACED CRACK LONGERON FITTING IAW DOUGLAS DRAWING NR 5802709. (M)SDR 2000ZZZM231Spar · crackedDURING D-CHECK INSPECTION, FOUND 4 INCH CRACK IN RIGHT LOWER SPAR CAP AT XCW 69.5. REPAIRED ACCOMPLISH IAW BOEING SERVICE ENGINEERING FAX FAS-MIA-99-0010RR AND SRO8570012 PER FINE AIR EA G5710-02, 00. (M)SDR 2000ZZZM248Skin · crackedDURING D-CHECK INSPECTION, FOUND LEADING UPPER CAP CRACKED. REPAIRED CRACK ON WING RIGHT IAW FINE AIRLINES EA NR G5711-02:00. (M)SDR 97ZZZX3558Fuel Contl Unit · defectiveDURING FLARE AT LANDING MIAMI, NR 3 ENGINE FLAMED OUT. TROUBLESHOOTING ON GROUND REVEALED DEFECTIVE ENGINE FUEL CONTROL UNIT. REPLACED FCU, TRIMMED ENGINE, AND RETURNED ACFT TO SERVICE. (X)SDR 97ZZZM435Brackets · brokenON ROUTINE INSPECTION, FOUND RIGHT MAIN LANDING GEAR CENTER DOOR MISSING AND RETAINING BRACKETS BROKEN. INSPECTED AIRCRAFT, FOUND SLIGHT DAMAGE AFT OF DOOR ON WING FAIRING. REPAIRED DAMAGED AREA. REPLACED DOOR AND BRACKETS AND RETURNED AIRCRAFT TO SERVICE.SDR 97ZZZM434Brackets · brokenON ROUTINE INSPECTION, FOUND RIGHT MAIN LANDING GEAR CENTER DOOR MISSING AND RETAINING BRACKETS BROKEN. INSPECTED AIRCRAFT, FOUND SLIGHT DAMAGE AFT OF DOOR ON WING FAIRING. REPAIRED DAMAGED AREA. REPLACED DOOR AND BRACKETS AND RETURNED AIRCRAFT TO SERVICE.SDR 97ZZZM433Brackets · brokenON ROUTINE INSPECTION, FOUND RIGHT MAIN LANDING GEAR CENTER DOOR MISSING AND RETAINING BRACKETS BROKEN. INSPECTED AIRCRAFT, FOUND SLIGHT DAMAGE AFT OF DOOR ON WING FAIRING. REPAIRED DAMAGED AREA. REPLACED DOOR AND BRACKETS AND RETURNED AIRCRAFT TO SERVICE.SDR 97ZZZM432Brackets · brokenON ROUTINE INSPECTION, FOUND RIGHT MAIN LANDING GEAR CENTER DOOR MISSING AND RETAINING BRACKETS BROKEN. INSPECTED AIRCRAFT, FOUND SLIGHT DAMAGE AFT OF DOOR ON WING FAIRING. REPAIRED DAMAGED AREA. REPLACED DOOR AND BRACKETS AND RETURNED AIRCRAFT TO SERVICE.SDR 96ZZZM1441Switch · roller missingAFTER TAKEOFF MIA, RIGHT MAIN GEAR LIGHT UNSAFE LIGHT ON AFTER GEAR RETRACTION. FOLLOWED ABNORMAL PROCEDURES AND LIGHT STAYED ON. RETURNED TO MIA AND MADE LANDING WITHOUT INCIDENT. FOUND RIGHT DOOR LATCH SWITCH ROLLER MISSING. REPLACED SWITCH CHECKS OK PERSDR 96ZZZM1289Ballast · defectiveAFTER LANDING MIAMI, INSTRUMENT WHITE LIGHT BALLAST STARTED TO SMOKE. PULLED CIRCUIT BREAKER. INSPECTION REVEALED DEFECTIVE BALLAST. REPLACED BALLAST AND RETURNED AIRCRAFT TO SERVICE.SDR 96ZZZM1247Rod Assy · brokenAFTER TAKEOFF, PARAMARIBO, EXPERIENCED LOUD NOISE AND SLIGHT VIBRATION IN NOSE AREA. DIVERTED TO POS AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED A BROKEN ROD ASSY AT THE STRUT END ON THE AFT RIGHT NOSE GEAR DOOR. REPLACED ROD ASSEMBLY, PERFORMED GEAR SSDR 96ZZZX3635Clevis · crackedDURING C-CHECK INSPECTION, A CRACK WAS FOUND EMANATING FROM A FASTENER HOLE IN THE INBOARD FLAP. REPAIRED CLEVIS BY INSTALLING A 2.0 INCH BY 2.0 INCH DOUBLER MADE OF .125 A1S1 301 1/2 H MATERIAL IAW EO 960511. 8110-3 ISSUED BY DER SW-713.SDR 96ZZZX3634Clevis · crackedDURING C-CHECK INSPECTION, A CRACK WAS FOUND EMANATING FROM A FASTENER HOLE IN THE LOWER TANG OF THE RIGHT WING INBOARD FLAP LOWER CLEVIS. REPAIRED CLEVIS BY INSTALLING A 2.0 INCH BY 2.0 INCH DOUBLER MADE OF .125 A1S1 301 1/2 H MATERIAL IAW EO 9606181. 8110-SDR 96ZZZM1229Clevis · crackedDURING C-CHECK INSPECTION, A CRACK WAS FOUND EMANATING FROM A FASTENER HOLE IN THE LOWER TANG OF THE RIGHT WING INBOARD FLAP LOWER CLEVIS. REPAIRED CLEVIS BY INSTALLING A 2 INCH BY 2 INCH DOUBLER MADE OF .125 A1S1 301 1/2 H MATERIAL IAW EO 9606181. 8110-3 ISSDR 96ZZZM1228Clevis · crackDURING C-CHECK INSPECTION, A CRACK WAS FOUND EMANATING FROM A FASTENER HOLE IN THE LOWER TANG OF THE CLEVIS ON THE LEFT WING INBOARD FLAP. REPAIRED CLEVIS BY INSTALLING A 2 INCH BY 2 INCH DOUBLER MADE OF .125 A1S1 301 1/2 H MATERIAL IAW EO 960511. 8110 ISSUESDR 96ZZZM873Controller · overheatedIN CRUISE EXPERIENCED O-ZONE ODOR AND INTERMITTENT SMOKE FROM BEHIND INSTRUMENT PANEL WHEN AUTO-PILOT WAS ENGAGED. GROUND INSPECTION REVEALED AUTOPILOT CONTROLLER WAS SHORTED/OVERHEATED. REPLACED CONTROLLER AND AIRCRAFT RETURNED TO SERVICE.SDR 95ZZZZ234Rod Assy · unlockedAFTER TAKEOFF MIAMI FELT SEVERE VIBRATION. RETURNED TO MIAMI AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED RT NOSE LANDING GEAR DOOR OPEN. CLEANED, LUBED AND RESET RT FWD DOOR ROD AND OPS CHECKED OK. PERFORMED OVERWEIGHT LANDING INSPECTION. RETURNED ACSDR 95ZZZX2311Cap Assy · leakingMIAMI - AFTER TAKEOFF, NOTED FUEL LOSS FROM NR 1 ALT FUEL TANK. RETURNED TO MIAMI. LANDED WITHOUT INCIDENT. INSPECTION REVEALED LEAKING FUEL TANK CAP AT NR 1 ALT TANK. REPLACED FUEL TANK CAP. AIRCRAFT RETURNED TO SERVICE. TOTAL CYCLES 20,256.SDR 95ZZZX1933Actuator · motor inopMIA - AFTER TAKEOFF, COULD NOT PRESSURIZE AIRCRAFT. RETURNED TO MIAMI AND MADE LANDING WITHOUT INCIDENT. PERFORMED OVERWEIGHT INSPECTION. GROUND INSPECTION REVEALED DEFECTIVE OUTFLOW VALVE ACTUATOR. REPLACED ACTUATOR AND GROUND CHECKED OKAY. RETURNED AIRC
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