N816AX, cancelled Jun 19, 2008

Service difficulty reports · 165

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 = 'N816AX' AND deregistration_id = 'N816AX-2008-06-19'
  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 ABXA070184Battery · dischargedEMERGENCY EXIT LIGHT BATTERY PACK DEAD UNABLE TO CHANGE. REMOVED AND REPLACED EMERGENCY LIGHT PACK ASSEMBLY IAW DC8 AMM 33-50-01.Jun 12, 2007 · N816AX · Doug DC863F · Emergency LightingSDR ABXA070072Wire · damagedDURING SERVICE CHECK FOUND ELECTRICAL ODOR COMING FROM OVERHEAD LIGHT. FOUND ONE FLUORESCENT LIGHT RECEPTACLE CORRODED AT TERMINAL ENDS AND SHORTING. CLEANED RECEPTACLE AND REPLACED BOTH TERMINAL ENDS ON WIRES COMING TO RECEPTACLE. REPLACED LAMP AND OPS CHEMar 15, 2007 · N816AX · Doug DC863F · Light System WiringSDR ABXA070069Wire · chafedACRID ODOR OF ELECTRICAL SMOKE BY ALL 3 CREW MEMBERS, SOURCE NOT IDENTIFIED. ODOR COMES AND GOES. FOUND LOAD CALCULATOR WIRES CHAFING ON PANEL. ROUTED PANEL AREA OUT AND REPAIRED WIRES IAW DC8 MM CHAPTER 20. NO OTHER DEFECTS NOTED AT THIS TIME.Mar 13, 2007 · N816AX · Doug DC863F · Navigation System WiringSDR ABXA070051Drive Link · crackedLEFT INBOARD FLAP DRIVE LINK AT STA XW 98.00 FOUND CRACKED WHILE COMPLYING WITH JC 8020401 AND ASB 27-269, AD 088-10-7. REMOVED AND REPLACED LINK, DETAILS IN WORK PACK 600264601.Feb 21, 2007 · N816AX · Doug DC863F · Trailing Edge Flap ActuatorSDR ABXA060233Door · missingNR 4 ENGINE RIGHT COWL DOOR BLOWOUT PANEL MISSING. REPLACED NR 4 ENGINE RIGHT COWL BLOWOUT PANEL AND DOOR FORWARD DOOR LATCH IAW DC8 MM 71-10 AND DC8 MM CHAPTER 20. OPS CHECKED GOOD.Aug 22, 2006 · N816AX · Doug DC863F · Engine Cowling SystemSDR ABXA060161Engine · fodIMMEDIATELY AFTER TAKEOFF FROM ILN, NR 3 FIRE WARNING LIGHT AND BELL CAME ON. AFTER APPROXIMATELY 5 SECONDS, THEN LIGHT WENT OUT. FIRE WARNING TESTED GOOD. SECURED NR 3 ENGINE AND LANDED. POSITIVE OIL PRESSURE INDICATED. FOUND CHARRED BIRD NEST NEXT TO AFApr 12, 2006 · N816AX · Doug DC863F · Fire DetectionSDR ABXA060126Pin · corrodedFORWARD TRUNNION MAIN LANDING GEAR PIN CORRODED BEYOND LIMITS (LEFT). LEFT MAIN GEAR FORWARD TRUNNION PIN REMOVED AND REPLACED IAW DC8 MM 32-11-01-4.Feb 18, 2006 · N816AX · Doug DC863F · Main Landing GearSDR ABXA060125Pin · shearedLEFT MAIN LANDING GEAR ACTUATOR LOWER ATTACH POINT PIN SHEARED DURING RETRACTION. REMOVED AND REPLACED LEFT MAIN LANDING GEAR ACTUATOR LOWER PIN AS PER AAR FORM 0909-02, REV 3. OPS CHECKED GOOD IAW DC8 AMM 32-32-0.Feb 17, 2006 · N816AX · Doug DC863F · Landing Gear Position and WarningSDR ABXA060127Pin · corrodedAFT TRUNNION MAIN LANDING GEAR PIN HAD PITTING THROUGH OUT PIN. LEFT MAIN GEAR AFT TRUNNION PIN REMOVED AND REPLACED IAW DC8 MM 32-11-01-4.Feb 10, 2006 · N816AX · Doug DC863F · Main Landing GearSDR ABXA060124Splice · crackedRIGHT SIDE CABIN STA. 680, LONGERON 11 RIGHT, AFT UPPER SPLICE FITTING HAD A CRACK. REMOVED AND REPLACED SPLICE FITTING AT RIGHT SIDE MAIN CABIN, STA 680, LONGERON 11 RIGHT AFT IAW DC8 SRM 51-1-20 AND 51-3-0.Jan 22, 2006 · N816AX · Doug DC863F · Fuselage Miscellaneous StructureSDR ABXA060123Fitting · crackedLEFT CENTER WING FLOOR AREA AT FS 759, LEFT BUTT LINE 48, SUPPORT FITTING HAD CORROSION AT BASE ATTACH NUTS. CLEANED AREA IAW DC8 MM 12-06-00, FITTING FOUND CRACKED. REMOVED AND REPLACED WITH NEW FITTING IAW DC8 SRM 51-1-20D.Jan 22, 2006 · N816AX · Doug DC863F · Fuselage Main, Attach FittingsSDR ABXA060121Fitting · corrodedAFT CARGO COMPARTMENT AREA BELOW C-3 DOOR HAD CORROSION ON FITTING APPROXIMATELY FS 1195, RIGHT BUTT LINE 19. REMOVED AND REPLACED FITTING AT C-3 DOOR AREA FS 1195, RIGHT BUTT LINE 19 IAW DC8 SRM 51-1-20D AND 53-2-0.Jan 21, 2006 · N816AX · Doug DC863F · Fuselage Main, Attach FittingsSDR ABXA060122Fitting · corrodedAFT CARGO COMPARTMENT AREA BELOW C-3 DOOR HAD FITTINGS (2 EACH) CORRODED IN BOX SECTION FS 1176, RIGHT BUTT LINE 20. REMOVED AND REPLACED FITTINGS AT AFT CARGO COMPARTMENT BELOW C-3 DOOR IAW DC8 SRM 51-1-20 AND 53-2-00.Jan 21, 2006 · N816AX · Doug DC863F · Fuselage Miscellaneous StructureSDR ABXA060120Fitting · crackedAFT LOWER CARGO COMPARTMENT FITTINGS (3 EACH) CRACKED, BETWEEN FS 1200 - 1220, RIGHT BUTT LINE 20, LOWER DOOR CUT OUT BOX SECTION. REMOVED AND REPLACED FITTINGS AT AFT CARGO COMPARTMENT BELOW C-3 DOOR IAW DC8 SRM 51-1-20D.Jan 20, 2006 · N816AX · Doug DC863F · Fuselage Main, Attach FittingsSDR ABXA050379Transmitter · defectiveNR 3 ENGINE OIL PRESSURE WAS 37 TO 39 PSI IN CRUISE. RETARDED THROTTLE TO IDLE TO COMPLY WITH ABNORMAL PROCEDURES, OIL PRESSURE WAS 35 PSI. OIL PRESSURE DROPPED TO 34 PSI, SECURED NR 3 ENGINE AT 0850 HRS - 10 PSI WINDMILLING OIL PRESSURE. 0855 HRS OIL PRESSUREDec 21, 2005 · N816AX · Doug DC863F · Engine Oil Indicating SystemSDR ABXA050126Fitting · crackedDURING LINE MAINTENANCE, FOUND THE CENTER WING TANK FRONT SPAR LT SUPPORT FITTING CRACKED AT STA XCW 67. REPLACED FITTING IAW DC-8 SRM 51-3-0.May 18, 2005 · N816AX · Doug DC863F · Wing, Center BoxSDR ABXA040221Hinge · crackedMAIN CARGO DOOR AFT HINGE HAD AFT ATTACHMENT FASTENER HOLE SHOWING CRACK INDICATION. REPAIRED AREA IAW REA D852-49168MR.Jun 8, 2004 · N816AX · Doug DC863F · Cargo/Baggage DoorsSDR ABXA040220Mount · wornMAIN CARGO DOOR LOWER LATCH MOUNT HOLES WORN. REPAIRED AREA IAW REA D852-49174MR.Jun 8, 2004 · N816AX · Doug DC863F · Fuselage Main, Attach FittingsSDR ABXA040224Skin · damagedSTA 1440, LONGERON 29 RIGHT REQUIRED PERMANENT REPAIR. PERMANENT REPAIR ACCOMPLISHED IAW REA D853-49148MR.Jun 4, 2004 · N816AX · Doug DC863F · Fuselage Main, Plate/SkinSDR ABXA040223Floorbeam · corrodedFLOORBEAM WEB AT BS 180 WAS CORRODED AT 3 ATTACH FASTENERS FOR SPLICE PLATE LEFT BUTTLINE 57. REPAIRED AREA IAW REA D853-49182MR.Jun 4, 2004 · N816AX · Doug DC863F · Fuselage Main, Floor BeamSDR ABXA040222Floorbeam · crackedFLOORBEAM WEB AT BS 240 HAD 4 CRACK INDICATIONS AT SPLICE PLATE ATTACH FASTENERS LEFT BUTTLINE 57. REPAIRED AREA IAW REA D853-49184MR.Jun 4, 2004 · N816AX · Doug DC863F · Fuselage Main, Floor BeamSDR ABXA040219Finger Doubler · corrodedAFT CARGO STA 1480, LONGERON 31 LEFT, FINGER DOUBLER, CORRODED. REPAIRED FUSELAGE SKIN IAW DC-8 SRM 53-2-1 AND REPAIRED FRAME SECTION IAW DWG K04888 AND REA D853-49146, SRM 53-2-0, 51-1-21, 51-1-20D, AND 51-3-1.Jun 4, 2004 · N816AX · Doug DC863F · Fuselage Main, Plate/SkinSDR ABXA040036Wire · burnedNR 3 GENERATOR UNPARALLED LIGHT ILLUMINATED IN FLIGHT, NO VOLTS, NO FREQS. RESET, NO VOLTS, NO FREQS, DISCONNECTED. REPLACED NR 3 ENGINE GENERATOR IAW 24-20-01-4-0002. DURING OPS CHECK, NOTED SPARKS COMING FROM THE TOP OF ENGINE. FOUND T1, T2, AND T3 WIRESDec 29, 2003 · N816AX · Doug DC863F · Electrical Power System WiringSDR ABXA030473Cylinder · leakingHYDRAULIC QUANTITY GRADUALLY DECREASED DOWN TO 7 GALLONS. LOSS OF HYDRAULICS EMERGENCY PROCEDURE FOLLOWED. MAINTENANCE FOUND RT BOGIE TRIM CYLINDER LEAKING. REPLACED RT BOGIE TRIM CYLINDER IAW MM 32-33-01-2.Dec 12, 2003 · N816AX · Doug DC863F · Landing Gear Steering SystemSDR ABXA030323Engine · overheatedDURING TAKEOFF, NR 3 ENGINE EGT WENT TO 600 DEGREES. RETARDED THROTTLE AND EGT DECREASED INTO NORMAL RANGE. OTHER INSTRUMENTS DECREASED AS WELL. SECURED ENGINE PER ABNORMAL PROCEDURES. EGT AT 600 DEGREES FOR APPROXIMATELY 15 SECONDS. NR 3 ENGINE WAS SHUTDAug 4, 2003 · N816AX · Doug DC863F · Engine (Turbine/Turboprop)SDR ABXA020246Ground Wire · looseWHEN HOT CUP WAS TURNED ON, EMERGENCY EXIT LIGHTS IN COCKPIT INTERMITTENTLY FLICKERED ON AND OFF RANDOMLY. FOUND LOOSE WIRING AT GROUND STUD FOR EMERGENCY POWER SUPPLY. TIGHTENED LOOSE CONNECTION AT GROUND STUD. NO DEFECTS NOTED WITH HOT CUP. SYSTEM OPS CHOct 11, 2002 · N816AX · Doug DC863F · Light System WiringSDR ABXA020212Torque Link · disconnectedGROUND SHIFT FAILED AFTER TAKEOFF, UNABLE TO RAISE GEAR HANDLE, AUTO PRESSURIZATION INOPERATIVE. TAKEOFF WARNING HORN SOUNDED. RAN ABNORMAL. PULLED GROUND CONTROL CIRCUIT BREAKERS. SYSTEMS RESTORED. AFTER LANDING, AND NOSE WHEEL TOUCH DOWN, A LOUD POP WASSep 19, 2002 · N816AX · Doug DC863F · Nose/Tail Landing Gear Strut/AxleSDR ABXA030221Frame · corrodedFORWARD LOWER CARGO STA 280, LONGERON 36, UPPER FRAME FLANGE WAS CRACKED AND CORRODED. CUT OUT DAMAGED SECTION OF FRAME. FABRICATED FILLER, DOUBLER, ALODINED, PRIMED, AND INSTALLED FASTENERS IAW REA D853-43982MR, DC-8 SRM 51-1-8, 51-1-20D, AND 51-1-20E.Aug 12, 2002 · N816AX · Doug DC863F · Fuselage Main, FrameSDR ABXA030217Skin · crackedAFT PASSENGER DOOR UPPER AFT CORNER OUTER SKIN HAD 2 CRACKS. REMOVED DAMAGED, NO CRACKS NOTED AFT OF CUTOUTS. FABRICATED DOUBLER AND FILLERS, INSTALLED IAW DC-8 SRM 53-2-0, NDT SPM 06-10-001, DC-8 SRM 51-1-8, 51-1-20D AND SRM 51-1-21.Aug 10, 2002 · N816AX · Doug DC863F · Fuselage Main, Plate/SkinSDR ABXA030227Skin · crackedFORWARD SERVICE DOOR LOWER AFT CORNER SKIN HAD A CRACK. CUT OUT DAMAGE IAW DC-8 SRM 53-2-0. FABRICATED DOUBLERS AND FILLERS IAW DC-8 SRM 53-2-0. INSTALLED DOUBLERS AND FILLERS IAW DC-8 SRM 53-2-0. REINSTALLED INNER TORQUE BOX WEB IAW DC-8 SRM 51-1-20E AND 51-3Aug 7, 2002 · N816AX · Doug DC863F · Service DoorsSDR ABXA030220Door Frame · crackedL1 DOOR JAMB LOWER AFT CORNER HAD STAINLESS STEEL REPAIR. REMOVED DOOR CLOSE OUT PANEL TO FOM. FABRICATED 3 DOUBLER, 5 DOUBLER AND FILLERS, INSTALLED ALL IAW DC-8 SRM 53-2-0, 51-1-21 AND 51-3-0.Aug 7, 2002 · N816AX · Doug DC863F · Fuselage Main, StructureSDR ABXA030222Structure · corrodedLT WING LEADING EDGE UPPER SECTION APPROXIMATELY, STA. XFS 126.250, CORROSION AROUND FASTENERS. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REPAIRED IAW REA D857-43958MR.Aug 6, 2002 · N816AX · Doug DC863F · Leading Edge DevicesSDR ABXA030219Doubler · crackedFORWARD LOWER CARGO C1 DOOR, FUSELAGE INNER DOUBLER WAS CRACKED AT FUSELAGE STA. 320, OUTER EDGE AND HAD AN IMPROPER REPAIR. CUT OUT DAMAGED SECTION OF DOUBLER, FABRICATED FILLER, REPAIR DOUBLER SPLICES, AND INSTALLED ALL REPAIRS PARTS IAW DC-8 SRM 51-1-20D, DJul 22, 2002 · N816AX · Doug DC863F · Cargo/Baggage DoorsSDR ABXA030223Seat Track · corrodedSEAT TRACK AT BUTT LINE 25 LEFT WAS CORRODED, FS 70 - 260. REMOVED WEB AND FLOORBOARDS FS 70 - 260, LEFT BUTT LINE 0 - 45 TO FOM. REMOVED SEAT TRACK SECTION. FABRICATED SECTION IAW ZANTOP DWG 86302. ALODINED AND PRIMED IAW DC-8 SRM 51-1-8. INSTALLED SEAT Jul 22, 2002 · N816AX · Doug DC863F · Fuselage, Seat/Cargo Attach FittingsSDR ABXA030231Pan · crackedFORWARD PASSENGER DOOR LOWER AFT CORNER AT THE CUSP CHORD SHOWED CRACK INDICATION. STOP DRILLED CRACKED DOOR PAN, FABRICATED REPAIR AND SPLICE PARTS AND PLATES FOR DOOR PAN AND TORQUE BOX WEB IAW DAC 5597646, DC-8 SRM 53-2-0, 51-9-0, 51-1-21, 53-3-1, AND 51-1Jul 22, 2002 · N816AX · Doug DC863F · Fuselage Miscellaneous StructureSDR ABXA030229Longeron · corrodedREMOVE AND REPLACE LONGERON 32 LEFT INBOARD CHANNEL STA. 190 - 385. REMOVED CORRODED SECTION, FABRICATED LONGERON AND SPLICES. INSTALLED IAW DC-8 SRM 51-1-20D, 53-2-2, AND 51-1-8.Jul 20, 2002 · N816AX · Doug DC863F · Fuselage Main, Longeron/StringerSDR ABXA030228Longeron · corrodedLONGERON 32 LEFT OB CHANNEL AT STA. 370 WAS CORRODED. REMOVED CORRODED SECTION OF LONGERON, FABRICATED LONGERON AND SPLICES. INSTALLED IAW SRM 51-1-20D, 51-1-24, AND 53-2-2.Jul 20, 2002 · N816AX · Doug DC863F · Fuselage Main, Longeron/StringerSDR ABXA030230Longeron · corrodedLONGERON 35 RIGHT INBOARD CHANNEL WAS CORRODED AT STA 340. CUT AND REMOVED DAMAGED SECTION, FABRICATED NEW SECTION AND REPAIR SPLICES. INSTALLED IAW DC-8 SRM 53-2-2 AND 51-1-20D.Jul 20, 2002 · N816AX · Doug DC863F · Fuselage Main, Longeron/StringerSDR ABXA030226Skin · corrodedREMOVE AND REPLACE FORWARD LOWER CARGO SKIN FROM F.S. 190 - 450 LONGERON 31 LEFT - 31 RIGHT. (COI NR 41207-001). REPLACED FORWARD LOWER CARGO SKIN IAW DC-8 SRM.Jul 19, 2002 · N816AX · Doug DC863F · Fuselage Main, Plate/SkinSDR ABXA030225Door Frame · corrodedAFT CARGO, BS 1220, FUSELAGE FRAME CORRODED JUST INBOARD OF SLIDING DOOR, LOWER AFT CUTOUT. REPLACED DOOR FRAME ZEE FITTING, FABRICATED REPAIR SPLICE ANGLES AND FILLERS. INSTALLED IAW DC-8 SRM 53-2-0, 51-1-8, AND 51-3-0.Jul 17, 2002 · N816AX · Doug DC863F · Fuselage Main, StructureSDR ABXA030218Structure · crackedFORWARD SERVICE DOOR UPPER FORWARD CORNER HAD A CRACK IN OUTER SKIN. CUT OUT CRACKED AREA, FABRICATED DOUBLER, TRIPLER, FILLER, AND INSTALLED EACH IAW SRM 53-2-0, 51-1-8, 51-1-21, 51-1-20D, 51-3-0 AND 51-1-14.Jul 16, 2002 · N816AX · Doug DC863F · Fuselage Main, Attach FittingsSDR ABXA030216Frame · corrodedAFT CARGO BS 1010, BETWEEN LONGERON 35 LEFT AND 35 RT, FUSELAGE FRAME CORRODED ON UPPER CAP, UPPER AND LOWER SURFACES. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, REMOVED (1 EA) FRAME CAP, (6 EA) GUSSETS, CUT OUT DAMAGED AREA, FABRICATED REPAIR ANGLE, FILLERJul 16, 2002 · N816AX · Doug DC863F · Fuselage Main, FrameSDR ABXA030224Shear Tie · corrodedAFT LOWER CARGO, SHEARTIE CORRODED AT STA. 1200, LONGERON 28 - 29 LEFT. REMOVED CORROSION, OUT OF LIMITS. REMOVED FITTING AND FABRICATED SPLICE, INSTALLED NEW FITTING IAW DC-8 SRM 51-1-8, 53-2-0, AND 51-1-20D.Jul 15, 2002 · N816AX · Doug DC863F · Fuselage Main, StructureSDR ABXA020058Warning System · malfunctionedGEAR UNSAFE LIGHT REMAINED ILLUMINATED ON RETRACTION. LEFT GEAR DOWN INDICATED NOT LATCHED. RECYCLED ONCE, NO HELP. RUNNING ABNORMAL TO UPLATCH CHECK POSITION LIGHT EXTINGUISHED.Jul 13, 2002 · N816AX · Doug DC863F · Landing Gear Position and WarningSDR ABXA020032Fitting · crackedRIGHT WHEEL WELL AREA, STATION 920, FITTING WAS CRACKED AT CENTER KEEL. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-21 AND 51-1-20.Jun 25, 2002 · N816AX · Doug DC863F · Fuselage Miscellaneous StructureSDR ABXA020031Skin · corrodedSKIN CORROSION OUT OF LIMITS JUST AFT OF GYRO COMPARTMENT. INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-0.Jun 25, 2002 · N816AX · Doug DC863F · Fuselage Main, Plate/SkinSDR ABXA020030Skin · corrodedCORROSION OUT OF LIMITS ON FUSELAGE SKIN, STATION 280, LONGERON 35 LEFT AND STATION 335, LONGERON 35 RIGHT. INSTALLED REPAIR DOUBLER IAW REA D853-44492.Jun 25, 2002 · N816AX · Doug DC863F · Fuselage Main, Plate/SkinSDR ABXA010889Battery Pack · dischargedDURING MAINTENANCE INSPECTION, FOUND EMERGENCY EXIT LIGHTS DIM. REPLACED EMERGENCY EXIT LIGHTS BATTERY PACK IAW DC-8 MM 33-50-01.May 29, 2002 · N816AX · Doug DC863F · Emergency LightingSDR ABXA010888Battery Pack · dischargedEMERGENCY LIGHTS WERE COMING ON INTERMITTENTLY. REPLACED EMERGENCY LIGHT BATTERY PACK IAW DC-8 MM.May 28, 2002 · N816AX · Doug DC863F · Emergency LightingSDR ABXA010900Nut · missingUPON FLAP EXTENSION FOR LANDING, SPLIT FLAPS WERE INDICATED. CONFIRMED BY ROLL TENDENCY. LEFT FLAP WAS APPROXIMATELY 6 DEGREES BEHIND RIGHT FLAP. RIGHT FLAP AT 35 DEGREES, LEFT FLAP AT 29 DEGREES. FOUND LEFT INBOARD FLAP ACTUATOR IDLER ARM TRACK MISSING NUMay 23, 2002 · N816AX · Doug DC863F · Fasteners
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