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.
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
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 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.SDR 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 SDR 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.SDR 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.SDR 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 FISDR 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 51SDR 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 WSDR 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 LESDR 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 INSSDR 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-SDR ABXA030114Skin · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON THE LEFT WING, UPPER PLATING. REPAIRED AREA IAW REA D857-46919.SDR 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.SDR 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 DISCREPSDR ABXA020001Light · inoperativeEMERGENCY EXIT LIGHT DISARM LIGHT, AMBER LIGHT WAS INOP. RELAMPED, OPS CHECKED NORMAL, REF DC-8 MM 33L.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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 SDR ABXA9900678Handle · defectiveUNABLE TO OPEN COCKPIT DOOR FROM INSIDE COCKPIT. REPAIRED COCKPIT DOOR HANDLE, OPS CHECKED GOOD.SDR 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.SDR ABXA9900381Window · lack of lubeUNABLE TO OPEN CAPTAIN'S CLEARVIEW WINDOW (EMERGENCY EXIT). LUBRICATED CAPTAIN'S CLEARVIEW WINDOW LINKAGE, OPS CHECKED GOOD.SDR 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.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 APSDR 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 APPSDR 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.SDR 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.SDR ABXA9800605Fitting · crackedMAIN CABIN LONGERON END FITTING AT STATION 860, LONGERON 10R CRACKED. REPAIRED IAW DC8 SRM'S 51-1-24 AND 51-1-20D.SDR ABXA9800604Bulkhead Web · crackedRADOME BULKHEAD, RIGHT WEB HAS TWO 15 INCH CRACKS, 6 ABOVE AND BELOW FRP. REPAIRED IAW ABX REA D853-23417 MR.SDR 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.SDR 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.SDR ABXA9800598Fitting · crackedMAIN CABIN, LONGERON END FITTING AT STATION 900 LONGERON 8R CRACKED. REPAIRED IAW DC8 SRM 51-3-2 AND 51-1-20D.SDR ABXA9800597Longeron · corrodedAFT LOWER CARGO COMPARTMENT STATION 1230, LONGERON 29L INSIDE TORQUE BOX, WEB CORRODED. REPAIRED IAW ABX REA D853-23409MR REV-A,SDR 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.SDR ABXA9800552Flange · crackedAFT PRESSURE BULKHEAD AFT SIDE HORIZONTAL BEAM HAS 3 CRACK ON LOWER FLANGE AT AIRCRAFT CENTERLINE. REPAIRED IAW ABX REA D853-23407MR.SDR ABXA9800551Trunnion · corrodedRIGHT HAND MAIN LANDING GEAR TRUNNION CORRODED. FABRICATED BUSHINGS PER AD 71-25-09 AND ABX REA D832-23410MR.SDR ABXA9800550Longeron · crackedLONGERON 2R CRACKED AT STATION 1790 CANTED BULKHEAD. REPAIRED IAW ABX REA D853-23411MR.SDR ABXA9800571Frame · corrodedFORWARD LOWER CARGO CIRCUMFERENTIAL FRAME CORRODED AT STATION 80, LONGERON 29R. REPAIRED IAW DC8 SRM 55-2-2 AND 51-1-9A.SDR 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 NORMSDR 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 DEFECTSSDR 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 ROLLSDR 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.SDR 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.SDR 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 SDR 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.SDR 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
Back to N853AX, cancelled Apr 25, 2007