N818AX, cancelled Apr 7, 2004

Service difficulty reports · 87

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 = 'N818AX' AND deregistration_id = 'N818AX-2004-04-07'
  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 ABXA030145Control Cable · brokenSPOILER CABLE S-23 BROKEN IN LT WHEEL WELL. REPLACED CABLES S-23 AND S-24. COMPLIED WITH SPOILER ADJ/TEST IAW WORK PACK 60172912. PERFORMED VISUAL INSPECTION OF SPOILER HYDRAULIC CONTROL LIMIT SWITCH CONNECTOR, P1-1036. FOUND CONNECTOR AND WIRING NEAR CONNECTOMay 14, 2003 · N818AX · Doug DC863 · Drag Control SystemSDR ABXA030143Switch · brokenIN FLIGHT, WITH LANDING GEAR UP, SPOILER PUMP RAN AND PRESSURE INDICATED 3000 PSI. PUMP TURN OFF WITH SWITCH OFF. FOUND CABLE FOR LANDING INPUT FLIGHT SPOILER HYDRAULIC PUMP LIMIT SWITCH BROKEN. REPLACED CABLE IAW REA D827-47-355. COMPLIED WITH SPOILER ADJ/TESMay 13, 2003 · N818AX · Doug DC863 · Drag Control SystemSDR ABXA030120Engine · defectiveON CLIMBOUT, THE NR 4 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED. NR 4 OIL PRESSURE NOTED TO BE 32 PSI. WHEN POWER REDUCED, OIL PRESSURE WAS 20 PSI. SHUT DOWN THE NR 4 ENGINE AT 1036Z. WINDMILLING OIL PRESSURE 8-10 PSI IN CLIMB AND CRUISE. AIRCRAFT FERMar 18, 2003 · N818AX · Doug DC863 · Engine (Turbine/Turboprop)SDR ABXA030045Battery Pack · dischargedEMERGENCY EXIT LIGHTS EXTREMELY DIM. NOTICED AFTER POWER LOAD. REPLACED EMERGENCY BATTERY PACK IAW DC-8 MM 33-50-01-2. OPS CHECKED GOOD.Jan 23, 2003 · N818AX · Doug DC863 · Emergency LightingSDR ABXA020346Warning Light · illuminatedNOSE GEAR FAILED UPLATCH GEAR UNSAFE LIGHT ON WITH GEAR RETRACTED. FOUND NOSE GEAR PIN INSTALLED WHEN AIRCRAFT TAXIED IN. INSPECTED NOSE GEAR AND CABLES FOR SAFETY OF FLIGHT INSPECTION. NO DEFECTS FOUND. AIRCRAFT OK FOR FLIGHT.Dec 4, 2002 · N818AX · Doug DC863 · Landing Gear Position and WarningSDR ABXA020227Drive Unit · brokenON LANDING ROLL, SPOILER HANDLE CAME BACK, SPOILERS DEPLOYED. BLUE SPOILER EXTEND LIGHT CAME ON, THEN WENT OUT. SPOILER EXTEND LIGHT TESTED, BUT LIGHT WOULD NOT COME ON WITH MANUAL SPOILER EXTENSION. FOUND GROUND SPOILER PULLEY BRACKET IN RIGHT WHEEL WELL AOct 4, 2002 · N818AX · Doug DC863 · Drag Control SystemSDR ABXA020083Landing Gear · corrodedRIGHT MAIN LANDING GEAR WAS CORRODED IN THE FORWARD ATTACH LUG. REPLACED THE RIGHT MAIN LANDING GEAR.Aug 20, 2002 · N818AX · Doug DC863 · Main Landing GearSDR ABXA010724Landing Gear · out of adjustNOSE LANDING GEAR FAILED UPLATCH CHECK AFTER TAKEOFF. RECYCLED THE LANDING GEAR AND TRIED AGAIN, IT ALSO FAILED ON THE SECOND ATTEMPT. BOTH TIMES IT SOUNDED LIKE THE NOSE GEAR CAME COMPLETELY OUT OF THE WHEEL WELL. PERFORMED ADJUSTMENT AND TEST OF THE NOSE Feb 19, 2002 · N818AX · Doug DC863 · Landing Gear Retraction/Extension SystemSDR ABXA010470Aspirator · leakingTHERE WAS A SLOW HYDRAULIC LEAK DURING CLIMB AND CRUISE. LOST APPROXIMATELY 2 GALLONS IN 15 MINUTES. FOUND THE HYDRAULIC RESERVOIR ASPIRATOR LEAKING WHEN ENGINE WAS RUNNING. REPLACED THE ASPIRATOR IAW DC-8 MM 29-10-05-02-0001. RAN ENGINE, OPS AND LEAK CHECSep 7, 2001 · N818AX · Doug DC863 · Hydraulic Reservoir, MainSDR ABXA010435O-Ring · leakingGENERAL HYDRAULIC SYSTEM QUANTITY DECREASED FROM FULL TO JUST ABOVE STAND PIPE DURING INITIAL CLIMB. REPACKED O-RING AT RESTRICTOR VALVE GOING TO THE ASPIRATOR ON THE MAIN HYDRAULIC RESERVOIR. LEAK CHECKED GOOD. SERVICED HYDRAULIC SYSTEM.Aug 13, 2001 · N818AX · Doug DC863 · Hydraulic Reservoir, MainSDR ABXA010391Splice · crackedLONGERON 31 LEFT SPLICE FITTING CRACKED AT STA 1270. REMOVED AND REPLACED SPLICE FITTING IAW DC-8 SRM.Jul 2, 2001 · N818AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA010390Intercostal · crackedAFT LOWER CARGO INTERCOSTAL CRACKED AT STA 1004, LONGERON 35 RIGHT. REMOVED AND REPLACED CRACKED INTERCOSTAL IAW DAC DWG 5779929, DC-8 SRM 51-1-8, AND 51-1-20D.Jul 2, 2001 · N818AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA010389Frame · crackedAFT LOWER CARGO FRAME AT STA 1420, LONGERON 35 RIGHT WAS CRACKED ABOVE LONGERON 35 RIGHT. REMOVED AND REPLACED DAMAGED FRAME SECTION IAW DC-8 SRM.Jul 2, 2001 · N818AX · Doug DC863 · Fuselage Main, FrameSDR ABXA010388Skin · corrodedFUSELAGE SKIN BULGING AT FASTENER, AT APPROXIMATELY FS 205, LONGERON 31 LEFT. REMOVED CORROSION. REPLACED FINGER DOUBLER AND REPAIRED AREA IAW DC-8 SRM 51-1-20D, 51-1-21, 53-2-0, 51-1-8, 51-1-11, AND REA D853-40861MR.Jun 28, 2001 · N818AX · Doug DC863 · Fuselage Main, Plate/SkinSDR ABXA010385Frame · crackedAFT LOWER CARGO FRAME AT STA 1440, LONGERON 35 RIGHT WAS CRACKED ABOVE LONGERON 35 RIGHT. REPLACED REPAIR ANGLE IAW DC-8 SRM 53-2-0, 51-1-21, 51-1-20D, AND 51-1-8.Jun 19, 2001 · N818AX · Doug DC863 · Fuselage Main, FrameSDR ABXA010558Bulkhead · crackedMAIN CABIN AFT PRESSURE BULKHEAD WAS CRACKED APPROXIMATELY 63 INCHES ABOVE THE FLOOR BETWEEN THE LEFT BUTT LINE 28 TO LEFT BUTT LINE 40. REPAIRED AREA IAW DAC DWG SRO 8530007, DC-8 SRM 51-1-8, 51-1-20D, 51-3-0, 51-3-1, AND 53-8-5.Jun 9, 2001 · N818AX · Doug DC863 · Fuselage Main, BulkheadSDR ABXA010322Skin · corrodedAFT CARGO AT FUSELAGE 1180 - 1220 AT LONGERON 29 LEFT SKIN WAS CORRODED UNDER AND BESIDE L-ANGLE.Jun 8, 2001 · N818AX · Doug DC863 · Fuselage Main, Plate/SkinSDR ABXA010321Fitting · crackedAFT CARGO AT FUSELAGE 1180 BETWEEN LONGERON 27 LEFT - 28 LEFT Z-FITTING WAS CRACKED.Jun 8, 2001 · N818AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA010320Fitting · corrodedAFT CARGO AT FUSELAGE 1160 BETWEEN LONGERON 27 LEFT - 28 LEFT Z-FITTING WAS CORRODED.Jun 8, 2001 · N818AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA010319Angle · crackedNR 4 PYLON INTERIOR INBOARD VERTICAL ANGLE STATION YN 298 UNDER UPPER SPAR WEB CRACKED.Jun 8, 2001 · N818AX · Doug DC863 · Nacelle/Pylon, Main FrameSDR ABXA010318Angle · corrodedFS 980 LONGERON 35 LEFT BULKHEAD ATTACH ANGLE WAS CORRODED.Jun 8, 2001 · N818AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA010317Skin · corrodedAFT LOWER CARGO SKIN CORRODED AROUND SEVERAL FASTENERS FROM STATION FS 980 TO STATION FS 1040 BETWEEN LONGERON 35 LEFT AND LONGERON 35 RIGHT.Jun 8, 2001 · N818AX · Doug DC863 · Fuselage Main, Plate/SkinSDR ABXA010316Longeron · corrodedAFT LOWER CARGO LONGERON 36 CORRODED AT STATION FUSELAGE 1021.Jun 8, 2001 · N818AX · Doug DC863 · Fuselage Main, Longeron/StringerSDR ABXA010315Fitting · corrodedFORWARD LOWER CARGO FITTING CORRODED AT FUSELAGE 70 LONGERON 36.Jun 8, 2001 · N818AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA010314Fitting · corrodedAFT LOWER CARGO BATHTUB FITTING CORRODED AT FUSELAGE 1050 LONGERON 28 LEFT.Jun 8, 2001 · N818AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA010313Frame · corrodedAFT LOWER CARGO FRAME CORRODED AT FUSELAGE 1500 LONGERON 36.Jun 8, 2001 · N818AX · Doug DC863 · Fuselage Main, FrameSDR ABXA010312Frame · corrodedAFT LOWER CARGO FRAME CORRODED AT STATION FS 1050 LONGERON 35 LEFT.Jun 8, 2001 · N818AX · Doug DC863 · Fuselage Main, FrameSDR ABXA010311Shear Tie · corrodedAFT LOWER CARGO SHEAR TIE CORRODED AT STATION FS 1020 BETWEEN LONGERON 35 RIGHT - LONGERON 36.Jun 8, 2001 · N818AX · Doug DC863 · Fuselage Main, StructureSDR ABXA010310Longeron · corrodedAFT LOWER CARGO LONGERON 35 LEFT CORRODED AT STATION FS 1020.Jun 8, 2001 · N818AX · Doug DC863 · Fuselage Main, Longeron/StringerSDR ABXA010309Shear Tie · corrodedAFT LOWER CARGO, FUSELAGE 1040, LONGERON 35 RIGHT - 36, SHEAR TIE CORRODED.Jun 8, 2001 · N818AX · Doug DC863 · Fuselage Main, StructureSDR ABXA010308Longeron · corrodedFS 1000 LONGERON 35 LEFT CORRODED ON INBOARD SIDE.Jun 8, 2001 · N818AX · Doug DC863 · Fuselage Main, Longeron/StringerSDR ABXA010565Skin · corrodedRIGHT HORIZONTAL STABILIZER LOWER SKIN WAS CORRODED AND BULGED, XE 149. REPAIRED AREA AND REPLACED SKIN IAW TSRM 95T0345001, DC-8 SRM 51-1-8, 51-1-21, AND 51-1-20D.Jun 7, 2001 · N818AX · Doug DC863 · Horizontal Stabilizer, Plate/SkinSDR ABXA010559Skin · damagedREMOVED AND REPLACED THE AFT LOWER SKIN, STATION 1350-1490. REPLACED THE AFT LOWER SKIN IAW DC-8 SRM 51-1-21, 51-3-2, 51-1-11, 51-1-26, 51-3-1, AND 51-3-3.Jun 7, 2001 · N818AX · Doug DC863 · Fuselage Main, Plate/SkinSDR ABXA010387Frame · corrodedMAIN CABIN BETWEEN STA 1180 TO 1160, FRAME 1180 AT LONGERON 4 LEFT WAS CORRODED. REMOVED CORROSION, ALODINED AND PRIMED IAW DC-8 SRM 51-1-8. CORROSION WITHIN LIMITS IAW DC-8 SRM 53-2-0.Jun 7, 2001 · N818AX · Doug DC863 · Fuselage Main, FrameSDR ABXA010386Longeron · crackedLONGERON 36 WAS CRACKED UNDER SPLICE FITTING AT STA 1350. RECEIVED LONGERON, DRILLED AND REAMED LONGERON IAW DC-8 SRM 51-3-2. INSTALLED IAW DC-8 SRM 51-1-20D.Jun 7, 2001 · N818AX · Doug DC863 · Fuselage Main, Longeron/StringerSDR ABXA010334Fitting · corrodedAIR COND/PRESSURIZATION COMPARTMENT AT FS 70, LONGERON 35 LEFT, END FITTING WAS CORRODED.Jun 7, 2001 · N818AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA010333Fitting · corrodedAIR COND/PRESSURIZATION COMPARTMENT AT FS 70, LONGERON 34 LEFT, END FITTING WAS CORRODED.Jun 7, 2001 · N818AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA010332Fitting · corrodedAIR COND/PRESSURIZATION COMPARTMENT AT FS 70, LONGERON 31 LEFT, END FITTING WAS CORRODED.Jun 7, 2001 · N818AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA010331Fitting · corrodedAIR COND/PRESSURIZATION COMPARTMENT AT FS 70, BETWEEN LONGERON 30 LEFT - 31 LEFT, PRODUCTION SPLICE FITTING WAS CORRODED.Jun 7, 2001 · N818AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA010330Fitting · corrodedAIR COND/PRESSURIZATION COMPARTMENT AT FS 70, LONGERON 29 LEFT, END FITTING WAS CORRODED.Jun 7, 2001 · N818AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA010329Skin · corrodedAIR COND/PRESSURIZATION COMPARTMENT AT FS 36 - 54, BETWEEN LONGERON 30 LEFT - 31 LEFT, WAS CORRODED FROM UNDER FINGER DOUBLER.Jun 7, 2001 · N818AX · Doug DC863 · Fuselage Main, Plate/SkinSDR ABXA010328Frame · corrodedAIR COND/PRESSURIZATION COMPARTMENT AT FS 24, LONGERON 35 LEFT AND 35 RIGHT, FRAME WAS CORRODED AROUND ATTACH FASTENER TO LONGERON.Jun 7, 2001 · N818AX · Doug DC863 · Fuselage Main, FrameSDR ABXA010327Frame · corrodedMAIN CABIN BETWEEN STATION 1260 TO 1240 FRAME 1260 WAS CORRODED AT CUSP.Jun 7, 2001 · N818AX · Doug DC863 · Fuselage Main, FrameSDR ABXA010326Frame · corrodedMAIN CABIN BETWEEN STATION 1180 TO 1160 FRAME 1180 AT LONGERON 4 LEFT WAS CORRODED.Jun 7, 2001 · N818AX · Doug DC863 · Fuselage Main, FrameSDR ABXA010325Longeron · corrodedMAIN CABIN BETWEEN STATION 1120 TO 1100 LONGERON 16 LEFT WAS CORRODED.Jun 7, 2001 · N818AX · Doug DC863 · Fuselage Main, Longeron/StringerSDR ABXA010324Frame · corrodedMAIN CABIN BETWEEN STATION 1360 TO 1347 FRAME AT STATION 1360 BETWEEN LONGERON 12 LEFT TO 5 A WAS CORRODED.Jun 7, 2001 · N818AX · Doug DC863 · Fuselage Main, FrameSDR ABXA010323Spar · corrodedLEFT HORIZONTAL STABILIZER LEADING EDGE LOWER SPAR XE 114 WAS CORRODED INSIDE AROUND A RIVET BUCKTAIL.Jun 7, 2001 · N818AX · Doug DC863 · Horizontal Stabilizer, Spar/RibSDR ABXA010300Shear Tie · corrodedAFT CARGO AT STATION 1140 BETWEEN LONGERON 34 RIGHT AND 35 RIGHT, SHEAR TIE AND FRAME CORRODED.Jun 6, 2001 · N818AX · Doug DC863 · Fuselage Main, StructureSDR ABXA010299Shear Tie · crackedAFT CARGO AT STATION 1120 BETWEEN LONGERON 35 LEFT AND 36 LEFT, SHEAR TIE CRACKED.Jun 6, 2001 · N818AX · Doug DC863 · Fuselage Main, StructureSDR ABXA010298Frame · corrodedAFT FUSELAGE AT STATION 1734 BETWEEN LONGERON 6 LEFT TO 7 LEFT FRAME WAS CORRODED.Jun 6, 2001 · N818AX · Doug DC863 · Fuselage Main, Frame
Back to N818AX, cancelled Apr 7, 2004