N853AX, cancelled Apr 25, 2007

Service difficulty reports · 52

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 = 'N853AX' AND deregistration_id = 'N853AX-2007-04-25'
  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 ABXA050068Panel · crackedDURING ROUTINE LINE MAINTENANCE AT ILN, FOUND A 2.250 INCH CRACK IN NR 2 PYLON OUTBOARD PLANK AT STA YN300. REPAIRED PYLON PLANK IAW ABX AIR REA D853-51551-MR USING 17-7 PH .080 INCH, PO 408448907.Mar 5, 2005 · N853AX · Doug DC861 · Nacelle/Pylon, Plate/SkinSDR ABXA040117Downlock Switch · corrodedAFTER GEAR EXTENSION, NOSE GEAR GREEN LIGHT DID NOT COME ON. NO RED UNSAFE LIGHT ON. REPLACED BULBS, NO HELP. CREW PERFORMED A GO-AROUND, CYCLED GEAR. VISUALLY CHECKED NOSE GEAR DOWN AND LOCKED, MADE NORMAL LANDING. GEAR PINNED AFTER LANDING AND AIRCRAFT Mar 26, 2004 · N853AX · Doug DC861 · Landing Gear Position and WarningSDR ABXA040087Fitting · crackedNR 3 PIT, AFT LOWER CARGO COMPARTMENT AFT DOOR JAMB FITTING WAS FOUND CRACKED DURING A LINE INSPECTION. REPLACED FITTING IAW DC-8 SRM 51-1-20D.Feb 23, 2004 · N853AX · Doug DC861 · Fuselage Main, Attach FittingsSDR ABXA030379Longeron · crackedRT MAIN LANDING GEAR WHEEL WELL LONGERON 24 AT STA. 875 TO 900 TRIPLER SHOWED EVIDENCE OF CRACK. REPAIRED AREA IAW DC-8 SRM 51-1-20D, 53-2-2, AND REA D853-48-35MR.Oct 2, 2003 · N853AX · Doug DC861 · Fuselage Main, Longeron/StringerSDR ABXA030380Skin · crackedAFT SERVICE DOOR JAMB UPPER AFT CORNER 3 INCHES X 8 INCHES AREA OF LIGHT SURFACE CORROSION AND A .1875 INCH CRACK AT FASTENER HOLE ON EXTERIOR FUSELAGE SKIN. REPAIRED AREA (REMOVED LIGHT SURFACE CORROSION, TRIMMED OUT CRACK, FABRICATED DOUBLERS -19, -21 AND FIOct 2, 2003 · N853AX · Doug DC861 · Fuselage Main, Plate/SkinSDR ABXA030384Bushing · corrodedRIGHT MAIN LANDING GEAR ATTACH FITTING (TRUNION) HAD BROWN GREASE EMITTING FROM LUGS AT FORWARD AND AFT ATTACH POINTS. REMOVED RIGHT MAIN LANDING GEAR IAW DC-8 MM 32-11-01. REMOVED AND REPLACED TRUNION BUSHINGS IAW DC-8 OHM 13-1-6 AND DAC SB 57-45, DC-8 SRM 51Oct 1, 2003 · N853AX · Doug DC861 · Wing, Landing Gear Attach FittingsSDR ABXA030383Strut · corrodedRT MAIN LANDING GEAR CYLINDER FORWARD LUG AFT SIDE HAD EVIDENCE OF CORROSION. CORROSION ON RIGHT MAIN LANDING GEAR CYLINDER WAS OUT OF LIMITS. REPLACED RIGHT GEAR WITH A SERVICEABLE ASSEMBLY. TRANSFERRED BRAKE ASSEMBLY 4 EA. IAW DC-8 MM 32-42-01. TRANSFERRED WOct 1, 2003 · N853AX · Doug DC861 · Main Landing Gear Strut/Axle/TruckSDR ABXA030382Bushing · corrodedLEFT MAIN LANDING GEAR ATTACH FITTING HAD BROWN GREASE EMITTING FROM LUGS AT BOTH ATTACH POINTS. REMOVED LEFT MAIN LANDING GEAR IAW DC-8 MM 32-11-01. REMOVED AND REPLACED TRUNION BUSHINGS IAW DC-8 OHM 13-1-6 AND DAC SB 57-45 AND DC-8 SRM 51-1-8. REINSTALLED LEOct 1, 2003 · N853AX · Doug DC861 · Wing, Landing Gear Attach FittingsSDR ABXA030381Skin · cracked11 EACH HOLES HAD CRACK INDICATION ON RIGHT WING 505F PANEL. REMOVED -19 CLIP, FABRICATED NEW CLIP, ALODINED, PRIMED, INSTALLED IAW DC-8 SRM 51-1-8 AND DWG NR 5613609. FABRICATED EXTERNAL DOUBLER AND INNER DOUBLER IAW REA D857-48044MR, ALODINED, PRIMED AND INSOct 1, 2003 · N853AX · Doug DC861 · Wing, Plate/SkinSDR ABXA030378Support Fitting · corrodedCORROSION ON UPPER CHORD OF CENTER WING REAR SPAR AT PRESSURE BULKHEAD F.S. 855, LEFT BUTT LINE 11 - 21. REMOVED AND INSTALLED BLOWOUT PANEL 3 EA. VERTICAL STIFFENERS, WEB ATTACH ANGLE, DOUBLER, FITTING AND SHEAR WEB ATTACH ANGLE IAW DC-8 SRM 51-30-0 AND 51-1-Oct 1, 2003 · N853AX · Doug DC861 · Wing, Center BoxSDR ABXA030114Skin · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON THE LEFT WING, UPPER PLATING. REPAIRED AREA IAW REA D857-46919.Mar 11, 2003 · N853AX · Doug DC861 · Wing, Plate/SkinSDR ABXA030036Power Supply · dischargedUPON MOVING AIRCRAFT, FOUND EMERGENCY POWER SUPPLY INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY. OPS CHECKED GOOD IAW DC-8 AMM 24-28-00-0.Jan 15, 2003 · N853AX · Doug DC861 · Battery/Charger SystemSDR ABXA020149Bearing · brokenAILERONS WERE VERY DIFFICULT TO TURN TO THE LEFT WITH HYDRAULIC POWER ON. REPLACED THE RIGHT AILERON REVERSION MECHANISM BEARING ASSEMBLY FOR TAB LOCKOUT IAW DC-8 OVERHAUL MANUAL 27-6-2. PERFORMED TEST OF REVERSION MECHANISM IAW DC-8 MM 27-11-08. NO DISCREPAug 28, 2002 · N853AX · Doug DC861 · Aileron Control SystemSDR ABXA020001Light · inoperativeEMERGENCY EXIT LIGHT DISARM LIGHT, AMBER LIGHT WAS INOP. RELAMPED, OPS CHECKED NORMAL, REF DC-8 MM 33L.Jun 24, 2002 · N853AX · Doug DC861 · Emergency LightingSDR ABXA010670Fitting · corrodedRIGHT MAIN LANDING GEAR WHEEL WELL, LONGERON 24 RIGHT, FITTING HAD EXFOLIATION CORROSION AT STATION 879. REMOVED CORRODED FITTING. FABRICATED REPAIR PARTS IAW DC-8 SRM 53-2-0. INSTALLED NEW FITTING AND REPAIR PARTS IAW DC-8 SRM 53-2-0.Jan 15, 2002 · N853AX · Doug DC861 · Fuselage Miscellaneous StructureSDR ABXA010668Fitting · corrodedFORWARD CARGO, STATION LONGERON 29 LEFT AND LONGERON 30 LEFT Z-ANGLE CORRODED. REMOVED CORRODED FITTING. RECEIVED NEW FITTING P/N 3755822-505N. FABRICATED REPAIR ANGLES IAW DC-8 SRM 53-2-0. INSTALLED Z-FITTING AND REPAIR ANGLES IAW DC-8 SRM 53-2-0.Jan 12, 2002 · N853AX · Doug DC861 · Fuselage Miscellaneous StructureSDR ABXA010667Fitting · corrodedFORWARD CARGO, STATION 320, BETWEEN LONGERON 28 LEFT - LONGERON 29 LEFT, Z-ANGLE CORRODED. REMOVED OLD FITTING. RECEIVED NEW FITTING P/N 3155822-505N. FABRICATED REPAIR ANGLES IAW DC-8 SRM 53-2-0.Jan 12, 2002 · N853AX · Doug DC861 · Fuselage Miscellaneous StructureSDR ABXA010666Spar · corrodedLEFT WING, FORWARD SPAR CAP AT XFS 520.76 HOLE HAD A CRACK INDICATION WITH HFEC DETERMINE CRACK LENGH AND LOCATION IAW ES00046. REPAIRED CRACKED HOLE IAW DAC DWG 4709980 AND DC-8 SRM 51-1-25. ALODINED AND PRIMED IAW DC-8 SRM 51-1-8.Jan 10, 2002 · N853AX · Doug DC861 · Wing StructureSDR ABXA010665Skin · corrodedRIGHT WING, TOP SURFACE BY STATION XRS 172, CORROSION ON SKIN. REPAIRED IAW ABX REA D857-40949-MR AND DC8 SRM 57-2-0, 51-1-26, 51-1-8 AND 51-1-20D.Jan 9, 2002 · N853AX · Doug DC861 · Wing, Plate/SkinSDR ABXA010793Stringer · crackedUPPER LEFT STRINGER 1 WAS CRACKED AT FS 1870, ABOVE BULKHEAD IN TAIL CONE FORWARD AREA. REPAIRED AREA IAW DC-8 SRM 51-1-21, 51-1-20, 51-1-8, 53-2-0 AND REA D853-40948MR.Jan 8, 2002 · N853AX · Doug DC861 · Fuselage Main, Longeron/StringerSDR ABXA010669Splice · crackedAFT CARGO, FS 1040 - 1060, LONGERON 31 RIGHT, SPLICE FITTING WAS CRACKED. RECEIVED NEW FITTING P/N 3750257-1. INSTALLED IAW DC-8 SRM 51-1-20D. REMOVED DAMAGED FITTING IAW DC-8 SRM 51-3-2.Dec 29, 2001 · N853AX · Doug DC861 · Fuselage Miscellaneous StructureSDR ABXA010529Hydraulic System · lowTHE GENERAL HYDRAULIC SYSTEM NEEDED SERVICED. THE SYSTEM INDICATED ZERO DURING APPROACH AND LANDING. MAINTENANCE SERVICED THE GENERAL HYDRAULIC SYSTEM IAW DC-8 MAINTENANCE MANUAL.Oct 6, 2001 · N853AX · Doug DC861 · Hydraulic System, MainSDR ABXA010217Control Valve · failedTHE NOSE LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF FROM ILN. THE CREW COMPLETED THE ABNORMAL CHECKLIST AND RE-CYCLED THE LANDING GEAR. THE AIRCRAFT WAS INSPECTED FOR AND COMPLETED A MAINTENANCE FERRY FLIGHT FROM EWR TO ILN. ILN MAINTENANCE INSPECTED AND May 2, 2001 · N853AX · Doug DC861 · Landing Gear Retraction/Extension SystemSDR ABXA9900678Handle · defectiveUNABLE TO OPEN COCKPIT DOOR FROM INSIDE COCKPIT. REPAIRED COCKPIT DOOR HANDLE, OPS CHECKED GOOD.Aug 27, 1999 · N853AX · Doug DC861 · Fixed Inner DoorsSDR ABXA9900567Lock · defectiveDURING PREFLIGHT INSPECTION, THE COCKPIT DOOR LOCK WAS INOPERATIVE. THE DOOR WOULD NOT UNLOCK WHEN CLOSED. INSTALLED NEW LATCH HANDLE AS REQUIRED, OPS CHECKED GOOD.Jul 8, 1999 · N853AX · Doug DC861 · Fixed Inner DoorsSDR ABXA9900381Window · lack of lubeUNABLE TO OPEN CAPTAIN'S CLEARVIEW WINDOW (EMERGENCY EXIT). LUBRICATED CAPTAIN'S CLEARVIEW WINDOW LINKAGE, OPS CHECKED GOOD.May 24, 1999 · N853AX · Doug DC861 · Flight Compartment WindowsSDR ABXA9900139Engine · failedDURING CLIMB, NR 1 ENGINE CREATED LOUD BANG. N1 AND N2 RPM DROPPED BY ONE HALF, EGT WENT TO 640 DEGREES. ENGINE ANTI-ICE WAS ON. SHUT ENGINE DOWN. FIRE BOTTLES WERE NOT USED. REPLACED NR 1 ENGINE.Feb 25, 1999 · N853AX · Doug DC861 · Engine (Turbine/Turboprop)SDR 98ZZZX4211Beam · crackedAT C-CHECK, CRACKS WERE FOUND IN THE J-BEAM WHICH IS ATTACHED TO THE AFT FACE OF THE AFT PRESSURE BULKHEAD. THE CRACKS ORIGINATE IN THE RADII ADJACENT TO ATTACH BOLTS APPROXIMATELY ONE INCH EACH SIDE OF THE AIRCRAFT CENTERLINE. SUBMITTER STATED THE CRACKS APOct 21, 1998 · N853AX · Doug DC861 · Fuselage Miscellaneous StructureSDR 98ZZZX4210Beam · crackedAT C-CHECK, CRACKS WERE FOUND IN THE J-BEAM WHICH IS ATTACHED TO THE AFT FACE OF THE AFT PRESSURE BULKHEAD. THE CRACKS ORIGINATE IN THE RADII ADJACENT TO ATTACH BOLT APPROXIMATELY ONE INCH EACH SIDE OF THE AIRCRAFT CENTERLINE. SUBMITTER STATED THE CRACKS APPOct 21, 1998 · N853AX · Doug DC861 · Fuselage Miscellaneous StructureSDR ABXA9800637Turbo Comp · defectiveNR 2 CTC BEGAN TO HOWL ON DESCENT, ACCOMPANIED BY SMELL LIKE BURNING RUBBER. *S/D* REPLACED NR 2 CTC IAW DC8 MM 21-10-01.Jul 22, 1998 · N853AX · Doug DC861 · Cabin Compressor SystemSDR ABXA9800606Bulkhead Tee Cap · crackedAFT PRESS BULKHEAD TEE CAP CRACKED AT LONGERON 10R. REPAIRED IAW DC8 SRM 53-2-5, 51-1-20D AND 51-3-0.Jul 1, 1998 · N853AX · Doug DC861 · Fuselage Main, BulkheadSDR ABXA9800605Fitting · crackedMAIN CABIN LONGERON END FITTING AT STATION 860, LONGERON 10R CRACKED. REPAIRED IAW DC8 SRM'S 51-1-24 AND 51-1-20D.Jul 1, 1998 · N853AX · Doug DC861 · Fuselage Miscellaneous StructureSDR ABXA9800604Bulkhead Web · crackedRADOME BULKHEAD, RIGHT WEB HAS TWO 15 INCH CRACKS, 6 ABOVE AND BELOW FRP. REPAIRED IAW ABX REA D853-23417 MR.Jul 1, 1998 · N853AX · Doug DC861 · Fuselage Main, BulkheadSDR ABXA9800600Fitting · crackedCRACK IN LOWER NR 2 MAIN TANK JUST INBOARD OF XRS 74 STRINGER NR 51 ON FWD AND AFT SIDE OF SPLICE. REPAIRED TWO CRACKED FITTINGS IAW DC8 SRM'S 51-1-24, 51-1-8, AND 51-1-20D.Jun 30, 1998 · N853AX · Doug DC861 · Wing Miscellaneous StructureSDR ABXA9800599Fitting · crackedSTRINGER END FITTING CRACKED AFT SIDE OF STRINGER NR 51 OUTBOARD IN NR 2 MAIN TANK AT STATION 74.000. REPAIRED IAW DC8 SRM 51-1-24 AND 51-1-20D.Jun 30, 1998 · N853AX · Doug DC861 · Fuselage, Wing Attach FittingsSDR ABXA9800598Fitting · crackedMAIN CABIN, LONGERON END FITTING AT STATION 900 LONGERON 8R CRACKED. REPAIRED IAW DC8 SRM 51-3-2 AND 51-1-20D.Jun 30, 1998 · N853AX · Doug DC861 · Fuselage Miscellaneous StructureSDR ABXA9800597Longeron · corrodedAFT LOWER CARGO COMPARTMENT STATION 1230, LONGERON 29L INSIDE TORQUE BOX, WEB CORRODED. REPAIRED IAW ABX REA D853-23409MR REV-A,Jun 30, 1998 · N853AX · Doug DC861 · Fuselage Main, Longeron/StringerSDR ABXA9800553Beam · crackedAFT PRESSURE BULKHEAD AFT SIDE, HORIZONTAL BEAM HAS 3.5 CRACK ON LOWER FLANGE AND 1 CRACK ON UPPER FLANGE AT AIRCRAFT CENTERLINE, 24 ABOVE FRP. REPAIRED PER ABX REA D853-23406MR.Jun 22, 1998 · N853AX · Doug DC861 · Fuselage Main, BulkheadSDR ABXA9800552Flange · crackedAFT PRESSURE BULKHEAD AFT SIDE HORIZONTAL BEAM HAS 3 CRACK ON LOWER FLANGE AT AIRCRAFT CENTERLINE. REPAIRED IAW ABX REA D853-23407MR.Jun 22, 1998 · N853AX · Doug DC861F · Fuselage Main, BulkheadSDR ABXA9800551Trunnion · corrodedRIGHT HAND MAIN LANDING GEAR TRUNNION CORRODED. FABRICATED BUSHINGS PER AD 71-25-09 AND ABX REA D832-23410MR.Jun 22, 1998 · N853AX · Doug DC861 · Main Landing Gear Attach SectionSDR ABXA9800550Longeron · crackedLONGERON 2R CRACKED AT STATION 1790 CANTED BULKHEAD. REPAIRED IAW ABX REA D853-23411MR.Jun 22, 1998 · N853AX · Doug DC861 · Fuselage Main, Longeron/StringerSDR ABXA9800571Frame · corrodedFORWARD LOWER CARGO CIRCUMFERENTIAL FRAME CORRODED AT STATION 80, LONGERON 29R. REPAIRED IAW DC8 SRM 55-2-2 AND 51-1-9A.Jun 6, 1998 · N853AX · Doug DC861 · Fuselage Main, FrameSDR ABXA9800443Switch · defectiveNR 1 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED ON CLIMBOUT. OIL QUANTITY, TEMPERATURE AND PRESSURE WERE NORMAL. PERFORMED ABNORMAL PROCEDURE. LIGHT REMAINED ON. PRECAUTIONARY ENGINE SHUTDOWN. REPLACED NR 1 ENGINE LOW OIL PRESSURE SWITCH. OPS CHECKED NORMMay 3, 1998 · N853AX · Doug DC861 · Engine Oil PressureSDR ABXA9800136Retract Mech · out of adjustAFTER TAKEOFF AND GEAR RETRACTION, VIBRATION COULD BE FELT AND HEARD FROM NOSE GEAR AREA. ALL INDICATIONS WERE GOOD. RECYCLED GEAR THREE TIMES, ON THIRD TIME, VIBRATION CEASED. REPLACED DOOR BUMPERS, AND PERFORMED ADJUST/TEST IAW DC8 MM 32-20-00, NO DEFECTSMar 2, 1998 · N853AX · Doug DC861 · Landing Gear Retraction/Extension SystemSDR ABXA9701338Control Cable · defectiveON CLIMBOUT WITH GEAR HANDLE UP GEAR UNSAFE AND LEFT DOOR NOT LATCHED LIGHTS ILLUMINATED. RECYCLED GEAR TWICE, LIGHTS REMAINED ON. IN CRUISE LEFT DOOR AND LEFT AND RIGHT GEAR NOT LATCHED LIGHTS CAME ON. REPLACED CABLE RUN 112C, RIGHT MLG DOOR LATCH AND ROLLJul 31, 1997 · N853AX · Doug DC861 · Landing Gear Door Retract SectionSDR ABXA9700898Spring · out of adjustFIRST OFFICER'S WINDOW WOULD NOT OPEN. REPOSITIONED WINDOW LATCH SPRING. FIRST OFFICER'S WINDOW OPS CHECKED GOOD IAW DC-8 M.M. 56-40.Apr 18, 1997 · N853AX · Doug DC861 · Flight Compartment WindowsSDR ABXA9700289Window · out of adjustDURING PREFLIGHT, WAS UNABLE TO OPEN FIRST OFFICER'S CLEARVIEW WINDOW. CLEANED AND LUBRICATED WINDOW AND SEAL. ADJUSTED LOWER AFT HOOK FITTING PER DC-8 MM 56-10-3. OPS CHECKED GOOD.Mar 26, 1997 · N853AX · Doug DC861 · Flight Compartment WindowsSDR ABXA9700021Fitting · looseWHEN GEAR HANDLE WAS PLACED UP AFTER TAKEOFF, THE AILERON CONTROL MANUAL LIGHT ILLUMINATED ACCOMPANIED BY PRESSURE LOSS. QUANTITY REMAINED AT FULL. PERFORMED GEAR SWING WITH EXTERNAL HYDRAULIC SOURCE AND AILERON POWER ON. FOUND HYDRAULIC LEAK AT NR 3 PYLON Jan 29, 1997 · N853AX · Doug DC861 · Hydraulic System, MainSDR ABXA9700013Lock Bar · out of adjustFIRST OFFICER'S SLIDING WINDOW/EMERGENCY EXIT WOULD NOT OPEN. ADJUSTED UPPER LOCK BAR IAW DC-8 MM, OPS CHECKED GOOD.Jan 20, 1997 · N853AX · Doug DC861 · Flight Compartment WindowsSDR ABXA9600678Gear Indication · malfunctionedON FINAL WHEN GEAR HANDLE PUT IN DOWN POSITION, NO NOSE GEAR GREEN LIGHT, HAD GEAR UNSAFE LIGHT. RECYCLED GEAR, GOT NORMAL INDICATION. PERFORMED ADJUSTMENT TEST OF NOSE LANDING GEAR SYSTEM IAW DC-8 MM 32-31-0. OPERATIONAL CHECK OF INDICATION AND MECHANICAL Dec 5, 1996 · N853AX · Doug DC861 · Landing Gear Position and Warning
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