N820BX, cancelled May 1, 2014

Service difficulty reports · 271

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 = 'N820BX' AND deregistration_id = 'N820BX-2014-05-01'
  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 IXXAIXXA110031OEngine · power lossDURING CRUISE AT FL 380 IN CALM AIR, NR 2 ENG N1 RPM AND NR 2 RPM ROLLED BACKED TO 50 PERCENT N1 AND 85 PERCENT N2. EGT WAS 530°C FUEL FLOW DECREASED TO APPROX 700 LBS. OIL TEMP DECREASED TO ZERO AND OIL PRESS WAS AT 35 PSI FUEL PRESS FLUCTUATING BETWEEN 30 Mar 30, 2011 · N820BX · Doug DC871F · Engine (Turbine/Turboprop)SDR IXXA10SMN037SFitting · crackedDURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STA 902.000 LONGERON 5 LT. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA.INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-1-8B, AND SRM 51-3-1.Apr 9, 2010 · N820BX · Doug DC871F · Fuselage Main, Attach FittingsSDR 2010FA0000311Structure · cracked(SPUY) DURING ROUTINE C-CHECK INSPECTION, LT OTBD WING L/E INNER SECTION. LOWER PLATING CRACKED AT STA XFS 597.500.Mar 26, 2010 · N820BX · Doug DC871F · Wing Main, Frame StructureSDR 2010FA0000310Finger Doubler · corroded(SPUY) DURING ROUTINE C-CHECK INSP, FLIGHT COMPARTMENT - HORIZ PRESS PANEL (SUB FLOOR) FINGER DOUBLER CORRODED AT STA 58.000 AND LBL 19.Mar 26, 2010 · N820BX · Doug DC871F · Fuselage Floor PanelSDR 2010FA0000309Angle · cracked(SPUY) DURING ROUTINE C-CHECK INSPECTION, AFT FUSELAGE INTERNAL SECTION- RING ANGLE CRACKED AT STA FS 1690.000 BETWEEN 30L AND L36.Mar 26, 2010 · N820BX · Doug DC871F · Fuselage Miscellaneous StructureSDR 2010FA0000305Skin · damaged( SPUY) DURING ROUTINE C-CHECK INSPECTION, LT WING INBD FLAP - AFT UPPER SURFACE SKIN PANEL SHOWS SCRATCHES AND (05EA) DENTS (STA XW 1.000 - 91.000).Mar 26, 2010 · N820BX · Doug DC871F · Trailing Edge FlapsSDR 2010FA0000304Skin · dented( SPUY) DURING ROUTINE C-CHECK INSPECTION, RT WING INBD FLAP - FWD UPPER SURFACE SKIN PANEL SHOWS DENTS ( STA XW 104.000-122.000)Mar 26, 2010 · N820BX · Doug DC871F · Trailing Edge FlapsSDR 2010FA0000303Skin · dented( SPUY) DURING ROUTINE C-CHECK INSPECTION, RT WING OTBD FLAP - AFT LOWER SURFACE SKIN PANEL SHOWS INTERM REPAIR AND DENT ( STA XF375.00-415.00).Mar 26, 2010 · N820BX · Doug DC871F · Trailing Edge FlapsSDR 2010FA0000301Hook · cracked( SPUY) DURING ROUTINE C-CHECK INSPECTION, FUSELAGE NOSE SECTION SKIN - FWD PASSENGER DOOR HOLD OPEN HOOK CRACKED .5" AT STA FS 15,000, L-16.Mar 26, 2010 · N820BX · Doug DC871F · Passenger/Crew DoorsSDR 2010FA0000300Doubler · worn(SPUY) DURING ROUTINE C-CHECK INSP, FUSELAGE NOSE SECTION, INTERNAL DOUBLER WORN AND BROKEN AT STA FS-156.00 (THRU NR 2 ACCESS DOOR. GROUND PNEU CONNECTION).Mar 26, 2010 · N820BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA10SMN044SSkin · crackedDURING ROUTINE C-CHECK INSP FOUND FWD CARGO COMPARTMENT INTERNAL SKIN CORRODED AT STA FS 285.000 LONGERON 35 RT- LONGERON 36. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO Mar 10, 2010 · N820BX · Doug DC871F · Wing, Plate/SkinSDR IXXA10SMN043SFinger Doubler · corrodedDURING ROUTINE C-CHECK INSP FOUND FLIGHT COMPARTMENT HORIZONTAL PRESS PANEL (SUB FLOOR) FINGER DOUBLER CORRODED AT STA 58.000 LT BOTTOM LINE 19. REMOVED CORRODED DOUBLER. REMOVED DAMAGED AREA. FABRICATED DOUBLERS, SEGMENT PANEL, SPLICE. CLEANED, TREATED PRIMEDMar 10, 2010 · N820BX · Doug DC871F · Fuselage Main, StructureSDR IXXA10SMN42SSeat Track · crackedDURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT NR 5 SEAT TRACK LUG BROKEN AT STA 148.00-1570.000. REMOVED DAMAGED SEGMENT OF TRACK. REMOVED EXISTING FWD SPLICE HAT AND SPLICE PLATE. FABRICATED SPLICE HAT, AND SPLICE PLATE. CLEANED, TREATED AND PRIMEDMar 9, 2010 · N820BX · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA10SMN041SSeat Track · crackedDURING ROUTINE C CHECK INSP FOUND MAIN CARGO COMPARTMENT NR 4 SEAT TRACK LUG BROKEN AT STA 590.000. REMOVED DAMAGED SEGMENT OF TRACK. REMOVED EXISTING FWD SPLICE HAT AND SPLICE PLATE. FABRICATED SPLICE HAT, AND SPLICE PLATE. CLEANED, TREATED AND PRIMED AREA ANMar 9, 2010 · N820BX · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA10SMN040SAngle · crackedDURING ROUTINE C-CHECK INSP FOUND AFT FUSELAGE INTERNAL SECTION RING ANGLE CRACKED AT STA FS 1690.000 LONGERON 30, LT LONGERON 36. REMOVED CRACKED RING ANGLE. FABRICATED SPLICES. PERFORMED HEAT TREATMENT. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLMar 9, 2010 · N820BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA10SMN038SFitting · crackedDURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STA 680.000 LONGERON 11 RT. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-1-8B, AND SRM 51-3-1.Mar 9, 2010 · N820BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA10SMN039SFitting · crackedDURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT CTR WING FITTING CRACKED AT STA FS 702.000 LONGERON 21 RT AND LONGERON 20 RT. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1, AND SRM 51-1-Mar 6, 2010 · N820BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA10SMN035SSkin · misrepairedDURING ROUTINE C CHECK INSP FOUND LT WING OTBD FLAP AFT LOWER SKIN PANEL HAS IMPROPER REPAIR AT STA XF 304.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTAMar 6, 2010 · N820BX · Doug DC871F · Trailing Edge FlapsSDR IXXA10SMN030SSkin · misrepairedDURING ROUTINE C-CHECK INSP FOUND RT WING OTBD FLAP FWD LOWER SKIN IMPROPER REPAIR AT STA XF 227.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO DISCREPANCY FOUND. FABRICATED NEWMar 6, 2010 · N820BX · Doug DC871F · Trailing Edge FlapsSDR IXXA10SMN036SSkin · misrepairedDURING ROUTINE C-CHECK INSP FOUND LT WING OTBD FLAP FWD UPPER SKIN HAS IMPROPER REPAIR AT STA XF 432.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. BONDED PARTS AS NEEDED WITH Mar 6, 2010 · N820BX · Doug DC871F · Trailing Edge FlapsSDR IXXA10SMN034SSkin · misrepairedDURING ROUTINE C CHECK INSP, FOUND LT WING OTBD FLAP FWD LOWER SKIN HAS IMPROPER REPAIR AT STA XF 193.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. BONDED PARTS AS NEEDED WITHMar 6, 2010 · N820BX · Doug DC871F · Trailing Edge FlapsSDR IXXA10SMN033SSkin · dentedDURING ROUTINE C-CHECK INSP FOUND LT WING INBD FLAP AFT UPPER SURFACE SKIN HAS SCRATCHES AND DENTS AT STA XW 2.000 - 91.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. BONDED PARMar 6, 2010 · N820BX · Doug DC871F · Wing, Plate/SkinSDR IXXA10SMN032SSkin · dentedDURING ROUTINE C-CHECK INSP FOUND RT WING INBD FLAP FWD UPPER SURFACE SKIN HAS DENTS AT STA XW 104.000 - 122.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLEMar 6, 2010 · N820BX · Doug DC871F · Wing, Plate/SkinSDR IXXA10SMN031SSkin · misrepairedDURING C-CHECK INSP, FOUND RT WING OTBD FLAP AFT LOWER HAS IMPROPER REPAIR AT STA XF 375.000 - 415.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. BONDED PARTS AS NEEDED WITH Mar 6, 2010 · N820BX · Doug DC871F · Wing, Plate/SkinSDR IXXA10SMN046SSkin · brokenDURING ROUTINE C-CHECK INSP FOUND FUSELAGE NOSE SECTION INTERNAL DOUBLER WORN AND BROKEN AT STA FS -156.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO CRACKS OR CORROSION NOTED. FAMar 5, 2010 · N820BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA10SMN029SHook · crackedDURING ROUTINE C-CHECK INSP FOUND FWD PASSENGER DOOR HOLD OPEN HOOK CRACKED AT STA FS 15.000 LONGERON 16 LT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO CRACKS OR CORROSION NOTED. FABRICATED REPAIR DOUBLERS, FILMar 5, 2010 · N820BX · Doug DC871F · Passenger/Crew DoorsSDR IXXA090052OEngine · power lossDURING CRUISE, SHUT DOWN NR 2 ENGINE DUE TO POWER LOSS AND VIBRATION. CREW LANDED WITHOUT FUTHER INCIDENT. MAINTENANCE REPLACED NR 2 ENGINE. OPERATIONAL CHECK GOOD IAW ATI ERH 70.01. AIRCRAFT WAS RETURNED TO SERVICE.Sep 18, 2009 · N820BX · Doug DC871F · Engine (Turbine/Turboprop)SDR IXXA090026SSkin · misrepairedDURING ROUTINE CPCP INSPECTION, FOUND IMPROPER REPAIR AT STATION FS 143 LONGERON 28.5 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. NO CRACK’S OR CORROSION NOTED. FABRICATED NEW SKIN. CLEANED, TREATED, AND PRIMED AREA AND Apr 10, 2009 · N820BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA090025SSkin · misrepairedDURING ROUTINE CPCP INSPECTION, FOUND IMPROPER REPAIR AT STATION FS 31 LONGERON 30.5 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. NO CRACK’S OR CORROSION NOTED. FABRICATED NEW SKIN. CLEANED, TREATED, AND PRIMED AREA AND RApr 10, 2009 · N820BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA090024SSkin · misrepairedDURING ROUTINE CPCP INSPECTION, FOUND IMPROPER REPAIR AT STATION FS287 LONGERON 35.5 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. NO CRACK’S OR CORROSION NOTED. FABRICATED NEW SKIN. CLEANED, TREATED, AND PRIMED AREA AND REApr 10, 2009 · N820BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA090023SSkin · misrepairedDURING ROUTINE CPCP INSPECTION, FOUND IMPROPER REPAIR AT STATION FS160 LONGERON 22 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. NO CRACK’S OR CORROSION NOTED. FABRICATED NEW SKIN. CLEANED, TREATED, AND PRIMED AREA AND REPAApr 10, 2009 · N820BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA090022SSkin · misrepairedDURING ROUTINE CPCP INSPECTION, FOUND IMPROPER REPAIR AT STATION FS 1718 LONGERON 17.5. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. NO CRACK’S OR CORROSION NOTED. FABRICATED NEW SKIN. CLEANED, TREATED, AND PRIMED AREA AND REPAIRApr 10, 2009 · N820BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA090021SSkin · misrepairedDURING ROUTINE CPCP INSPECTION, FOUND IMPROPER REPAIR AT STATION FS1204 LONGERON 16.25. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. NO CRACK’S OR CORROSION NOTED. FABRICATED NEW SKIN. CLEANED, TREATED, AND PRIMED AREA AND REPAIApr 10, 2009 · N820BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA090020SSkin · misrepairedDURING ROUTINE CPCP INSPECTION, FOUND IMPROPER REPAIR AT STATION FS363 LONGERON 36. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. NO CRACK’S OR CORROSION NOTED. FABRICATED NEW SKIN. CLEANED, TREATED, AND PRIMED AREA AND REPAIR PARApr 10, 2009 · N820BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA090019SSkin · misrepairedDURING ROUTINE CPCP INSPECTION, FOUND IMPROPER REPAIR AT STATION FS 349. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. NO CRACK’S OR CORROSION NOTED. FABRICATED NEW SKIN. CLEANED, TREATED, AND PRIMED AREA AND REPAIR PARTS. INSTAApr 10, 2009 · N820BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA090018SSkin · misrepairedDURING ROUTINE CPCP INSPECTION, FOUND IMPROPER REPAIR AT STATION FS 1348 LONGERON 35.5 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. NO CRACK’S OR CORROSION NOTED. MANUFACTURED REPAIR PARTS. CLEANED, TREATED, AND PRIMED ARApr 4, 2009 · N820BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA090001OIndication Sys · malfunctionedDURING CRUISE NR 2 ENG OIL QUANTITY INDICATED 0, OIL PRESSURE 25 PSI, OIL TEMP FLUCTUATING 70C. THE CREW SHUTDOWN NR 2 ENG. OIL QUANTITY RETURNED NORMAL, OIL PRESSURE INDICATED 0-3 PSI. ON APPROACH N2 INDICATED 0 RPM, N1 INDICATED 10 RPM, AIRSPEED 170 KNOTS ORJan 9, 2009 · N820BX · Doug DC871F · Engine Oil Indicating SystemSDR IXXA080038OPressure Switch · defectiveDURING TAKEOFF FROM KTOL AT APPROXIMATELY NINTY KNOTS THE CREW HAD A NUMBER TWO LOW OIL PRESSURE LIGHT FLICKER FOR ABOUT 1/2 SECOND WHILE SETTING MAX POWER OF EIGHTY-SEVEN PERCENT N1. POWER WAS AT ABOUT EIGHTY-SIX PERCENT AT THE TIME THEN LIGHT CAME ON STEADYDec 15, 2008 · N820BX · Doug DC871F · Engine Oil Indicating SystemSDR IXX2008F00019Fire Detector · malfunctionedFLT NR: ATN 820/KDFW TO KIAH. DURING CRUISE FROM KDFW TO KIAH THE NR 3 FIRE WARNING CAME ON. THE CREW ACCOMPLISHED THE APPROPRIATE CHECK LIST AND DISCHARGED BOTH FIRE BOTTLES, AND CONTINUED TO KIAH AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LT FAN, RJul 18, 2008 · N820BX · Doug DC871F · Fire DetectionSDR IXX2008F00015Fire Warning · illuminatedDURING CRUISE, THE NR (3) FIRE WARNING CAME ON. THE CREW ACCOMPLISHED THE APPROPRIATE CHECK LIST AND DISCHARGED BOTH FIRE BOTTLES, AND CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. CORRECTIVE ACTION IN PROGRESS (K)Jul 18, 2008 · N820BX · Doug DC871F · Fire DetectionSDR IXX2008F00008Fire Warning · illuminatedDURING CRUISE, NR 2 FIRE WARNING CAME ON, THE CREW DISCHARGED BOTH FIRE BOTTLES AND SHUTDOWN NR (2) ENGINE. CREW LANDED WITHOUT INCIDENT. IN WORK. (K)Jul 8, 2008 · N820BX · Doug DC871F · Fire DetectionSDR IXX2008F00002Indicator · inoperativeON TAKEOFF ROLL, CAPTAIN AIRSPEED DID NOT REGISTER 80 KNOTS (ANALOG NEEDLE AT ZERO, DIGITAL READOUT ERROR). CREW REJECTED TAKEOFF AT 80 KNOTS, THE CREW RETURNED TO BLOCKS WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED CAPTAIN MACH AIRSPEED INDICATOR OPERAJul 2, 2008 · N820BX · Doug DC871F · Airspeed/Mach IndicatorSDR MAS2008F00009Control Valve · leakingON CLIMBOUT FROM KPHL HYDRAULIC PRESSURE WENT TO ZERO, HYDRAULIC FLUID LEVEL TO STANDPIPE, THE CREW DECLARED EMERGENCY AND LANDED INTO KTOL WITHOUT INCIDENT. MAINTENANCE INSPECTED HYDRAULIC SYSTEM AND FOUND SLOT CONTROL VALVE LEAKING, MAINTENANCE REPLACED SLOTJun 17, 2008 · N820BX · Doug DC871F · Hydraulic System, MainSDR IXXA080024OFire Loop · intermittentDURING CRUISE FROM KSJC TO KRFD NUMBER ONE ENGINE FIRE INDICATION AT FL 350 WITH FIRE WARNING LIGHT ON. AFTER SILENCING THE BELL THE CREW DISCHARGED THE FIRE AGENT, AFTER THIRTY SECONDS THE FIRE LIGHT REMAINED ON AND THE CREW DISCHARGED THE SECOND BOTTLE AND May 28, 2008 · N820BX · Doug DC871F · Fire DetectionSDR IXXA080023OTerminal · defectiveDURING CLIMB FROM KSJC TO KRFD NUMBER ONE ENGINE FIRE WARNING LIGHT AND BELL CAME ON INTERMITTENTLY. ALL ENGINE INSTRUMENT INDICATIONS WERE NORMAL. WHEN THROTTLE WAS REDUCED TO IDLE FIRE INDICATION CAME BACK AND SILENCED ON IT'S OWN. THE CREW RAN THE QRH CHMay 28, 2008 · N820BX · Doug DC871F · Fire Protection System WiringSDR IXXA080015OController · malfunctionedDURING CLIMB-OUT FROM KTOL, FIRST OFFICERS WINDSHIELD SHATTERED IN FLIGHT CLIMBING THROUGH 25000 FT. THE CREW RETURNED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED FIRST OFFICERS WINDOW AND WINDOW TEMP CONTROLLER. OPERATIONAL CHECK Apr 30, 2008 · N820BX · Doug DC871F · Windshield/Door Rain/Ice RemovalSDR IXXA080013OConnector · damagedDURING CRUISE FROM KLAX TO KTOL THE CREW HAD A FIRE WARNING INDICATION ON NUMBER ONE ENGINE, ALL PARAMETERS WERE WITHIN NORMAL LIMITS. NUMBER ONE ENGINE WAS SHUTDOWN IAW THE QRH AND THE INBOARD FIRE BOTTLE WAS DISCHARGED. THE FIRE WARNING INDICATION EXTINGUIApr 16, 2008 · N820BX · Doug DC871F · Fire Protection System WiringSDR IXXA080012OIndicator · failedDURING CLIMB-OUT FROM KTOL, THE CREW NOTICE V1=134 NOTICE HESITATION IN AIR SPEED INCREASE AT VR AT 151 AIRSPEED FAILED TO INCREASE IN EXTERNAL MODE. WHEN SWITCH TO STANDBY AIRSPEED INDICATE 220KTS WHICH MATCHED TO FMS SPEEDS. THE CREW RETURNED TO KTOL AND LApr 11, 2008 · N820BX · Doug DC871F · Airspeed/Mach IndicatorSDR IXXA080011OFire Loop · shortedDURING CRUISE FROM KBFI TO KPDX AT FL160 NUMBER ONE ENGINE FIRE WARNING BELL AND LIGHT CAME ON. THE MASTER FIRE WARNING WOULD NOT SILENCE BELL. THE FIRE LIGHT AND BELL BECAME INTERMITTENT WHILE THE CREW RAN THE APPROPRIATE CHECKLIST. THE CREW SHUTDOWN NUMBERApr 2, 2008 · N820BX · Doug DC871F · Fire DetectionSDR IXXA080007OTransfer Valve · defectiveAFTER ROTATION FROM KLRD AIRCRAFT DID A UNCOMMANDED YAW TO THE LEFT AND RIGHT, THE CREW TURNED YAW DAMPER OFF AND OSCILLATION DAMPENED OUT. THE CREW RETURNED TO KLRD AND LANDED WITH OUT INCIDENT. MAINTENANCE DEFERRED THE AUTO PILOT SYSTEM IAW ATI MEL 22-01-0Feb 21, 2008 · N820BX · Doug DC871F · Auto Flight System
Back to N820BX, cancelled May 1, 2014