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.

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.Aug 30, 2002 · N426FB · Doug DC85F54 · Flight Control SystemSDR 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 CAug 4, 2002 · N426FB · Doug DC85F54 · AC Power Distribution SystemSDR 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 Mar 27, 2002 · N426FB · Doug DC85F54 · Alternator-Generator DriveSDR 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 6Mar 27, 2002 · N426FB · Doug DC85F54 · Turbine Engine Oil SystemSDR ARWA20020314Fluid · lowUPON LANDING, HYDRAULIC PRESSURED DROPPED TO ZERO AFTER GEAR EXTENSION. ALL CHECKLIST ACCOMPLISHED. SERVICED HYDRAULIC IAW MM 12-4-0, NO LEAKS NOTED.Mar 22, 2002 · N426FB · Doug DC85F54 · Hydraulic System, MainSDR 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 TMar 21, 2002 · N426FB · Doug DC85F54 · Landing Gear Retraction/Extension SystemSDR 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.Mar 15, 2002 · N426FB · Doug DC85F54 · Engine Pressure Ratio (EPR)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.Mar 13, 2002 · N426FB · Doug DC85F54 · AC RegulatorSDR 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 WINDMILMar 6, 2002 · N426FB · Doug DC85F54 · Turbine Engine Oil SystemSDR 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.Mar 5, 2002 · N426FB · Doug DC85F54 · Turbine Engine Oil SystemSDR 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 COOLERDec 28, 2001 · N426FB · Doug DC85F54 · Engine Oil Distribution (Airframe Furnished)SDR 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 LANDINGDec 18, 2001 · N426FB · Doug DC85F54 · Nose/Tail Landing GearSDR 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 MDec 1, 2001 · N426FB · Doug DC85F54 · Alternator-Generator DriveSDR 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.Dec 1, 2001 · N426FB · Doug DC85F54 · Turbine Engine Compressor SectionSDR 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.Nov 20, 2001 · N426FB · Doug DC85F54 · Fuselage Main, Plate/SkinSDR 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.Nov 20, 2001 · N426FB · Doug DC85F54 · Fuselage Miscellaneous StructureSDR 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.Nov 20, 2001 · N426FB · Doug DC85F54 · Fuselage Main, FrameSDR 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. Sep 16, 2000 · N426FB · Doug DC8F54 · Fuel Control/Reciprocating EnginesSDR 20001208AP006Fitting · crackedDURING AN INSPECTION FOUND THE FOLLOWING, CRACKED LEFT MLG AUXILIARY SPAR FITTING. REPLACED AUXILIARY SPAR FITTING IAW DOUGLAS DRAWING NR 5802630. (M)Jul 6, 2000 · N426FB · Doug DC8F54 · Fuselage Miscellaneous StructureSDR 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)Jul 6, 2000 · N426FB · Doug DC8F54 · Wing SparSDR 20001208AP001Fitting · crackedDURING AN INSPECTION FOUND THE FOLLOWING, CRACKED FITTING LEFT SIDE LONGERON 24. REPLACED CRACK LONGERON FITTING IAW DOUGLAS DRAWING NR 5802709. (M)Jul 6, 2000 · N426FB · Doug DC8F54 · Fuselage Miscellaneous StructureSDR 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)Aug 31, 1999 · N426FB · Doug DC8F54 · Wing SparSDR 2000ZZZM248Skin · crackedDURING D-CHECK INSPECTION, FOUND LEADING UPPER CAP CRACKED. REPAIRED CRACK ON WING RIGHT IAW FINE AIRLINES EA NR G5711-02:00. (M)Apr 21, 1999 · N426FB · Doug DC8F54 · Leading Edge DevicesSDR 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)Jul 22, 1997 · N426FB · Doug DC8F54 · Fuel Control/Turbine EnginesSDR 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.Feb 28, 1997 · N426FB · Doug DC8F54 · Landing Gear DoorsSDR 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.Feb 28, 1997 · N426FB · Doug DC8F54 · Landing Gear DoorsSDR 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.Feb 28, 1997 · N426FB · Doug DC8F54 · Landing Gear DoorsSDR 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.Feb 28, 1997 · N426FB · Doug DC8F54 · Landing Gear DoorsSDR 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 PEROct 21, 1996 · N426FB · Doug DC8F54 · Landing Gear Position and WarningSDR 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.Aug 18, 1996 · N426FB · Doug DC8F54 · Flight Compartment LightingSDR 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 SAug 6, 1996 · N426FB · Doug DC8F54 · Landing Gear Door Retract SectionSDR 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.Jul 5, 1996 · N426FB · Doug DC8F54 · Trailing Edge FlapsSDR 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-Jul 5, 1996 · N426FB · Doug DC8F54 · Trailing Edge FlapsSDR 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 ISJul 5, 1996 · N426FB · Doug DC8F54 · Trailing Edge FlapsSDR 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 ISSUEJul 5, 1996 · N426FB · Doug DC8F54 · Trailing Edge FlapsSDR 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.Apr 19, 1996 · N426FB · Doug DC8F54 · Autopilot SystemSDR 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 ACMay 4, 1995 · N426FB · Doug DC8F54 · Landing Gear Door Retract SectionSDR 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.Apr 29, 1995 · N426FB · Doug DC8F54 · Fuel StorageSDR 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 AIRCMar 27, 1995 · N426FB · Doug DC8F54 · Pressure Regulator/Outflow Valve
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