# Service difficulty reports: N820BX, cancelled May 1, 2014 A list on [N820BX, cancelled May 1, 2014](https://openairdocs.org/deregistered/N820BX-2014-05-01.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 6 · 271 reports - [SDR IXXAIXXA110031O](https://openairdocs.org/sdr/IXXAIXXA110031O.md): Engine · power loss · Mar 30, 2011 · N820BX · Doug DC871F · Engine (Turbine/Turboprop) > DURING 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 - [SDR IXXA10SMN037S](https://openairdocs.org/sdr/IXXA10SMN037S.md): Fitting · cracked · Apr 9, 2010 · N820BX · Doug DC871F · Fuselage Main, Attach Fittings > DURING 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. - [SDR 2010FA0000311](https://openairdocs.org/sdr/2010FA0000311.md): Structure · cracked · Mar 26, 2010 · N820BX · Doug DC871F · Wing Main, Frame Structure > (SPUY) DURING ROUTINE C-CHECK INSPECTION, LT OTBD WING L/E INNER SECTION. LOWER PLATING CRACKED AT STA XFS 597.500. - [SDR 2010FA0000310](https://openairdocs.org/sdr/2010FA0000310.md): Finger Doubler · corroded · Mar 26, 2010 · N820BX · Doug DC871F · Fuselage Floor Panel > (SPUY) DURING ROUTINE C-CHECK INSP, FLIGHT COMPARTMENT - HORIZ PRESS PANEL (SUB FLOOR) FINGER DOUBLER CORRODED AT STA 58.000 AND LBL 19. - [SDR 2010FA0000309](https://openairdocs.org/sdr/2010FA0000309.md): Angle · cracked · Mar 26, 2010 · N820BX · Doug DC871F · Fuselage Miscellaneous Structure > (SPUY) DURING ROUTINE C-CHECK INSPECTION, AFT FUSELAGE INTERNAL SECTION- RING ANGLE CRACKED AT STA FS 1690.000 BETWEEN 30L AND L36. - [SDR 2010FA0000305](https://openairdocs.org/sdr/2010FA0000305.md): Skin · damaged · Mar 26, 2010 · N820BX · Doug DC871F · Trailing Edge Flaps > ( 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). - [SDR 2010FA0000304](https://openairdocs.org/sdr/2010FA0000304.md): Skin · dented · Mar 26, 2010 · N820BX · Doug DC871F · Trailing Edge Flaps > ( SPUY) DURING ROUTINE C-CHECK INSPECTION, RT WING INBD FLAP - FWD UPPER SURFACE SKIN PANEL SHOWS DENTS ( STA XW 104.000-122.000) - [SDR 2010FA0000303](https://openairdocs.org/sdr/2010FA0000303.md): Skin · dented · Mar 26, 2010 · N820BX · Doug DC871F · Trailing Edge Flaps > ( 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). - [SDR 2010FA0000301](https://openairdocs.org/sdr/2010FA0000301.md): Hook · cracked · Mar 26, 2010 · N820BX · Doug DC871F · Passenger/Crew Doors > ( 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. - [SDR 2010FA0000300](https://openairdocs.org/sdr/2010FA0000300.md): Doubler · worn · Mar 26, 2010 · N820BX · Doug DC871F · Fuselage Main, Plate/Skin > (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). - [SDR IXXA10SMN044S](https://openairdocs.org/sdr/IXXA10SMN044S.md): Skin · cracked · Mar 10, 2010 · N820BX · Doug DC871F · Wing, Plate/Skin > DURING 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 - [SDR IXXA10SMN043S](https://openairdocs.org/sdr/IXXA10SMN043S.md): Finger Doubler · corroded · Mar 10, 2010 · N820BX · Doug DC871F · Fuselage Main, Structure > DURING 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 PRIMED - [SDR IXXA10SMN42S](https://openairdocs.org/sdr/IXXA10SMN42S.md): Seat Track · cracked · Mar 9, 2010 · N820BX · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings > DURING 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 PRIMED - [SDR IXXA10SMN041S](https://openairdocs.org/sdr/IXXA10SMN041S.md): Seat Track · cracked · Mar 9, 2010 · N820BX · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings > DURING 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 AN - [SDR IXXA10SMN040S](https://openairdocs.org/sdr/IXXA10SMN040S.md): Angle · cracked · Mar 9, 2010 · N820BX · Doug DC871F · Fuselage Miscellaneous Structure > DURING 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. INSTALL - [SDR IXXA10SMN038S](https://openairdocs.org/sdr/IXXA10SMN038S.md): Fitting · cracked · Mar 9, 2010 · N820BX · Doug DC871F · Fuselage Main, Attach Fittings > DURING 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. - [SDR IXXA10SMN039S](https://openairdocs.org/sdr/IXXA10SMN039S.md): Fitting · cracked · Mar 6, 2010 · N820BX · Doug DC871F · Fuselage Main, Attach Fittings > DURING 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- - [SDR IXXA10SMN035S](https://openairdocs.org/sdr/IXXA10SMN035S.md): Skin · misrepaired · Mar 6, 2010 · N820BX · Doug DC871F · Trailing Edge Flaps > DURING 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. INSTA - [SDR IXXA10SMN030S](https://openairdocs.org/sdr/IXXA10SMN030S.md): Skin · misrepaired · Mar 6, 2010 · N820BX · Doug DC871F · Trailing Edge Flaps > DURING 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 NEW - [SDR IXXA10SMN036S](https://openairdocs.org/sdr/IXXA10SMN036S.md): Skin · misrepaired · Mar 6, 2010 · N820BX · Doug DC871F · Trailing Edge Flaps > DURING 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 - [SDR IXXA10SMN034S](https://openairdocs.org/sdr/IXXA10SMN034S.md): Skin · misrepaired · Mar 6, 2010 · N820BX · Doug DC871F · Trailing Edge Flaps > DURING 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 WITH - [SDR IXXA10SMN033S](https://openairdocs.org/sdr/IXXA10SMN033S.md): Skin · dented · Mar 6, 2010 · N820BX · Doug DC871F · Wing, Plate/Skin > DURING 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 PAR - [SDR IXXA10SMN032S](https://openairdocs.org/sdr/IXXA10SMN032S.md): Skin · dented · Mar 6, 2010 · N820BX · Doug DC871F · Wing, Plate/Skin > DURING 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. INSTALLE - [SDR IXXA10SMN031S](https://openairdocs.org/sdr/IXXA10SMN031S.md): Skin · misrepaired · Mar 6, 2010 · N820BX · Doug DC871F · Wing, Plate/Skin > DURING 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 - [SDR IXXA10SMN046S](https://openairdocs.org/sdr/IXXA10SMN046S.md): Skin · broken · Mar 5, 2010 · N820BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING 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. FA - [SDR IXXA10SMN029S](https://openairdocs.org/sdr/IXXA10SMN029S.md): Hook · cracked · Mar 5, 2010 · N820BX · Doug DC871F · Passenger/Crew Doors > DURING 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, FIL - [SDR IXXA090052O](https://openairdocs.org/sdr/IXXA090052O.md): Engine · power loss · Sep 18, 2009 · N820BX · Doug DC871F · Engine (Turbine/Turboprop) > DURING 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. - [SDR IXXA090026S](https://openairdocs.org/sdr/IXXA090026S.md): Skin · misrepaired · Apr 10, 2009 · N820BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING 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 - [SDR IXXA090025S](https://openairdocs.org/sdr/IXXA090025S.md): Skin · misrepaired · Apr 10, 2009 · N820BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING 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 R - [SDR IXXA090024S](https://openairdocs.org/sdr/IXXA090024S.md): Skin · misrepaired · Apr 10, 2009 · N820BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING 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 RE - [SDR IXXA090023S](https://openairdocs.org/sdr/IXXA090023S.md): Skin · misrepaired · Apr 10, 2009 · N820BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING 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 REPA - [SDR IXXA090022S](https://openairdocs.org/sdr/IXXA090022S.md): Skin · misrepaired · Apr 10, 2009 · N820BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING 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 REPAIR - [SDR IXXA090021S](https://openairdocs.org/sdr/IXXA090021S.md): Skin · misrepaired · Apr 10, 2009 · N820BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING 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 REPAI - [SDR IXXA090020S](https://openairdocs.org/sdr/IXXA090020S.md): Skin · misrepaired · Apr 10, 2009 · N820BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING 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 PAR - [SDR IXXA090019S](https://openairdocs.org/sdr/IXXA090019S.md): Skin · misrepaired · Apr 10, 2009 · N820BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING 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. INSTA - [SDR IXXA090018S](https://openairdocs.org/sdr/IXXA090018S.md): Skin · misrepaired · Apr 4, 2009 · N820BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING 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 AR - [SDR IXXA090001O](https://openairdocs.org/sdr/IXXA090001O.md): Indication Sys · malfunctioned · Jan 9, 2009 · N820BX · Doug DC871F · Engine Oil Indicating System > DURING 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 OR - [SDR IXXA080038O](https://openairdocs.org/sdr/IXXA080038O.md): Pressure Switch · defective · Dec 15, 2008 · N820BX · Doug DC871F · Engine Oil Indicating System > DURING 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 STEADY - [SDR IXX2008F00019](https://openairdocs.org/sdr/IXX2008F00019.md): Fire Detector · malfunctioned · Jul 18, 2008 · N820BX · Doug DC871F · Fire Detection > FLT 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, R - [SDR IXX2008F00015](https://openairdocs.org/sdr/IXX2008F00015.md): Fire Warning · illuminated · Jul 18, 2008 · N820BX · Doug DC871F · Fire Detection > DURING 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) - [SDR IXX2008F00008](https://openairdocs.org/sdr/IXX2008F00008.md): Fire Warning · illuminated · Jul 8, 2008 · N820BX · Doug DC871F · Fire Detection > DURING 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) - [SDR IXX2008F00002](https://openairdocs.org/sdr/IXX2008F00002.md): Indicator · inoperative · Jul 2, 2008 · N820BX · Doug DC871F · Airspeed/Mach Indicator > ON 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 OPERA - [SDR MAS2008F00009](https://openairdocs.org/sdr/MAS2008F00009.md): Control Valve · leaking · Jun 17, 2008 · N820BX · Doug DC871F · Hydraulic System, Main > ON 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 SLOT - [SDR IXXA080024O](https://openairdocs.org/sdr/IXXA080024O.md): Fire Loop · intermittent · May 28, 2008 · N820BX · Doug DC871F · Fire Detection > DURING 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 - [SDR IXXA080023O](https://openairdocs.org/sdr/IXXA080023O.md): Terminal · defective · May 28, 2008 · N820BX · Doug DC871F · Fire Protection System Wiring > DURING 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 CH - [SDR IXXA080015O](https://openairdocs.org/sdr/IXXA080015O.md): Controller · malfunctioned · Apr 30, 2008 · N820BX · Doug DC871F · Windshield/Door Rain/Ice Removal > DURING 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 - [SDR IXXA080013O](https://openairdocs.org/sdr/IXXA080013O.md): Connector · damaged · Apr 16, 2008 · N820BX · Doug DC871F · Fire Protection System Wiring > DURING 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 EXTINGUI - [SDR IXXA080012O](https://openairdocs.org/sdr/IXXA080012O.md): Indicator · failed · Apr 11, 2008 · N820BX · Doug DC871F · Airspeed/Mach Indicator > DURING 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 L - [SDR IXXA080011O](https://openairdocs.org/sdr/IXXA080011O.md): Fire Loop · shorted · Apr 2, 2008 · N820BX · Doug DC871F · Fire Detection > DURING 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 NUMBER - [SDR IXXA080007O](https://openairdocs.org/sdr/IXXA080007O.md): Transfer Valve · defective · Feb 21, 2008 · N820BX · Doug DC871F · Auto Flight System > AFTER 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 22-01-0 Next page: https://openairdocs.org/deregistered/N820BX-2014-05-01/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N820BX-2014-05-01/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.