N826AX, cancelled Nov 21, 2007

Service difficulty reports · 217

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 = 'N826AX' AND deregistration_id = 'N826AX-2007-11-21'
  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 ABXA020095Floorbeam · corrodedAFT CARGO AT STA. 1300, RBL 16, FLOORBEAM WAS CORRODED. FABRICATED NEW REPAIR PARTS AND FLOORBEAM IAW ABX REA D853-43926-MR, 51-1-8, 53-2-0, 51-1-20D, 51-3-0, AND 51-1-21.Jul 5, 2002 · N826AX · Doug DC863 · Fuselage Main, Floor BeamSDR ABXA020105Fitting · crackedCABIN UNDER FLOOR FRAME STIFFENER WAS CRACKED AT FS 780, LEFT BUTT LINE 47.0. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D, 51-3-2 AND 51-3-0.Jul 2, 2002 · N826AX · Doug DC863 · Fuselage Structure (General)SDR ABXA020094Longeron · corrodedAIR COND/PRESS COMPARTMENT AT FS 36, LONGERON 31 RIGHT, AT OUTBOARD SIDE WAS CORRODED AROUND FASTENERS. FABRICATED REPAIR STRAP AND REPAIRED AREA IAW REA D853-43733-MR, SRM 53-2-0, 51-1-8, 51-1-20D.Jun 27, 2002 · N826AX · Doug DC863 · Fuselage Structure (General)SDR ABXA020103Fitting · cracked#4 ALT HAD A CRACKED STRINGER END FITTING AT XRS 408. SPLICE - STRINGER 59 AFT SIDE. INSTALLED NEW END FITTING AND BOOST PUMP BRACKET IAW DC-8 SRM 51-1-24, 51-1-8, AND 51-1-20D.Jun 21, 2002 · N826AX · Doug DC863 · Wing StructureSDR ABXA020107Frame · corrodedAFT CARGO FRAME HAD CORROSION AROUND NUTPLATE AT FS 1140, LONGERON 30 LEFT. CORROSION WAS OUT OF LIMITS. TRIMMED OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC-8 SRM 51-1-8, 53-2-0, 51-1-20D, AND REA D853-43923-MR.Jun 18, 2002 · N826AX · Doug DC863 · Fuselage Main, StructureSDR ABXA020106Fitting · crackedAFT ACCESSORY COMPARTMENT LONGERON END FITTING CRACKED AT FS 1690, LONGERON 32 LEFT. FABRICATED LONGERON AND FRAME REPAIRS, INSTALLED REPAIRS IAW DC-8 SRM 53-2-0, 53-2-2, 51-1-8, 51-1-20D, 51-3-0, AND REA D853-43934-MR.Jun 18, 2002 · N826AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA020096Pressure Panel · corrodedMAIN CABIN, STATION 857 TO 880, BUTT LINE 0, CORROSION FOUND UNDER FINGER DOUBLER AND UNDER CABLE SUPPORT BRACKET. REPAIRED AREA IAW REA D853-43928-MR.Jun 18, 2002 · N826AX · Doug DC863 · Fuselage Main, BulkheadSDR ABXA020104Flap Track · corrodedRIGHT WING INBOARD FLAP, INBOARD FLAP TRACK SHOWED EVIDENCE OF WEAR AND CORROSION. REPLACED THE RIGHT WING INBOARD FLAP, INBOARD FLAP TRACKS IAW DC-8 MM 27-51-03.Jun 17, 2002 · N826AX · Doug DC863 · Nacelle/Pylon StructureSDR ABXA020102Frame · crackedRIGHT NOSE TUNNEL STATION 32, FRAME WAS CRACKED. FABRICATED NEW FRAME AND REPAIRED AREA IAW DC-8 SRM 51-1-20D, 53-3-1, 53-2-0, AND 51-1-8.Jun 17, 2002 · N826AX · Doug DC863 · Fuselage Main, FrameSDR ABXA020112Track · corrodedAFT CARGO COMPARTMENT STATION 1440 TO 1540, RIGHT BUTT LINE 60, CORROSION UNDER FLOOR BOARD CLIP NUTS. FABRICATED 8 EACH SPLICES AND REPAIR TRACK, INSTALLED AND REPAIRED AREA IAW DC-8 SRM 51-3-0, 53-2-0, 53-2-3, AND 51-1-8.Jun 17, 2002 · N826AX · Doug DC863 · Fuselage Main, StructureSDR ABXA020111Floorbeam · corrodedFORWARD CARGO TEE CHORD AT FS 70 WAS CORRODED BETWEEN LONGERON 29 LEFT - LONGERON 31 LEFT. FABRICATED REPAIR DOUBLER AND REPAIRED AREA IAW DC-8 SRM 51-1-27 AND REA D853-43935-MR.Jun 17, 2002 · N826AX · Doug DC863 · Fuselage Main, Floor BeamSDR ABXA020093Doubler · corrodedRIGHT WHEEL WELL UPPER PRESSURE DECK REPAIR DOUBLER EXFOLIATED ABOVE LONGERON 24, FS 879. REPAIRED AREA IAW ABX REA D853-43932-MR.Jun 17, 2002 · N826AX · Doug DC863 · Fuselage Main, BulkheadSDR ABXA020110Spar Cap · crackedRIGHT WING FORWARD LOWER SPAR CAP HAD CRACK INDICATIONS IN FASTENER HOLES #2 AND #4 FROM THE INBOARD SIDE. FABRICATED REPAIR PARTS AND REPAIRED AREA IAW ABX DC-8 JOB CARD J060232, DC-8 SRM 51-1-8, 51-1-20D, AND 51-1-25.Jun 16, 2002 · N826AX · Doug DC863 · Wing, Attach FittingsSDR ABXA020109Fitting · corrodedAIR COND/PRESS COMPARTMENT BETWEEN FS 56-70, LONGERON 36, END FITTING WAS CORRODED. REPLACED END FITTING IAW DC-8 SRM 51-1-20D.Jun 16, 2002 · N826AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA020108Longeron · corrodedAIR COND/PRESS COMPARTMENT AT FS 24, LONGERON 31 RIGHT WAS CORRODED AT ATTACH ANGLE ATTACHING FASTENERS. REMOVED CORRODED CLIP LONGERON TO FRAME. INSTALLED NEW ATTACH P/N 2643619-1 IAW DC-8 SRM 51-1-21A AND 51-1-24.Jun 16, 2002 · N826AX · Doug DC863 · Fuselage Main, StructureSDR ABXA010694Link · brokenRIGHT INBOARD FLAP DRIVE LINK BROKEN. REPLACED RIGHT STATION 98 FLAP DRIVE LINK ASSEMBLY IAW DC8 MM 27-51-04-3-0001. OPS CHECKED GOOD.Jan 26, 2002 · N826AX · Doug DC863F · Trailing Edge Flap Control SystemSDR ABXA010499Control Unit · defectiveANTI-SKID CONTROL PANEL RIGHT AND LEFT INBOARD LIGHTS ILLUMINATED ON LANDING. REDUCED BRAKING WAS EXPERIENCED ON LANDING ROLL OUT. MAINTENANCE INSPECTED AND DEFERRED THE ANTI-SKID SYSTEM IAW DC-8 MEL 32-1. LATER ON 09/15/01 THE ANTI-SKID CONTROL UNIT WAS REPLASep 14, 2001 · N826AX · Doug DC863 · Brake Anti-Skid SectionSDR ABXA010394Fitting · crackedFRAME TO LONGERON FITTING WAS CRACKED AFT SIDE, STA 820, ABOVE LONGERON 22 RIGHT. REPLACED FITTING IAW DC-8 DWG 4753360, SRM 53-1-0 AND 51-1-20D.Jul 2, 2001 · N826AX · Doug DC863F · Fuselage Miscellaneous StructureSDR ABXA010395Spar Cap · crackedRIGHT WING AFT UPPER SPAR CAP WAS CRACKED BETWEEN XCW 69.5 AND XCW 46. REPLACED RIGHT WING UPPER SPAR CAP BETWEEN XCW 0 TO XRS 74.8 IAW REA D857-41242MR.Jun 20, 2001 · N826AX · Doug DC863F · Wing SparSDR ABXA010122Spar · corrodedTHE RIGHT WING SPAR AFT FACE AT UPPER DIHEDRAL HAD CORROSION EXTENDING DOWN FROM THE TOP OF AFT FACE TO BOTTOM OF THE REAR SPAR. MAINTENANCE INSPECTED AND REPLACED THE SPAR WEB.Dec 13, 2000 · N826AX · Doug DC863 · Wing SparSDR ABXA00373Pressure Switch · malfunctionedAFTER LEVEL-OFF AT FL 350, NR 4 ENGINE OIL PRESSURE LIGHT STARTED FLICKERING WITH SHORT PERIODS OF BEING ON STEADY. RETARDED NR 4 THROTTLE AND LOW PRESSURE LIGHT REMAINED ONSTEADY. SHUT NR 4 ENGINE DOWN. REPLACED OIL DIFFERENTIAL PRESSURE SWITCH. OPS CHECKAug 9, 2000 · N826AX · Doug DC863 · Engine Oil PressureSDR ABXA9900867Light · inoperativeEMERGENCY EXIT LIGHT DID NOT ILLUMINATE WHEN TURNED ON. RELAMPED IAW DC8 MM 33-10-00. OPS CHECKED GOOD.Dec 21, 1999 · N826AX · Doug DC863 · Emergency LightingSDR ABXA9900456Rib · crackedLEFT WING LEADING EDGE UPPER RIB CRACKED AT FASTENER END AT STATION XFS 195. REPAIRED IAW DC8 SRM 57-2-0.Apr 29, 1999 · N826AX · Doug DC863 · Wing, Rib/BulkheadSDR ABXA9800616Window · lack of lubeFIRST OFFICER'S SLIDING WINDOW (EMERG EXIT) WOULD NOT OPEN. CLEANED LATCH AND LUBRICATED AS REQUIRED, OPS CHECKED GOOD.Jul 13, 1998 · N826AX · Doug DC863 · Flight Compartment WindowsSDR ABXA9800450Valve Assy · bypassingAFTER TAKEOFF AND GEAR RETRACTED, GEAR UNSAFE LIGHT WAS ILLUMINATED. RECYCLED GEAR WITH SAME RESULTS. PERFORMED GEAR UPLATCH CHECK AND LEFT AND RIGHT MAIN GEAR AND DOORS, 'NOT LATCHED' LIGHT WAS ILLUMINATED. REPLACED SYSTEM SELECTOR VALVE FOR BYPASSING. OPMay 13, 1998 · N826AX · Doug DC862 · Landing Gear Retraction/Extension SystemSDR ABXA9800924Rib · crackedNR 4 PYLON UPPER RIB HAD CRACK AT END. REPAIRED IAW DC8 SRM.May 12, 1998 · N826AX · Doug DC863F · Nacelle/Pylon StructureSDR ABXA9800040Mfd · malfunctionFAINT BURNING ODOR WAS REPORTED BY CREW DURING FLIGHT AND ON GROUND. PROBLEM WAS DETERMINED TO BE MULTI-FUNCTION DISPLAY (MFD). REPLACED DISPLAY UNIT IAW DC8 MM 34-20, OPS CHECKED GOOD.Jan 22, 1998 · N826AX · Doug DC863F · Independent Position Determining SystemSDR ABXA9800034Filter · defectiveDURING DESCENT WITH THROTTLE AT IDLE, NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED WITH AN OIL PRESSURE READING OF 25 PSI. SECURED NR 2 ENGINE. WINDMILLING OIL PRESS 7 PSI, N2-23 PERCENT, N1-14 PERCENT, EGT-70 DEG, AND EPR-1.00. REPLACED MAIN OIL FILTER Jan 18, 1998 · N826AX · Doug DC863F · Turbine Engine Oil SystemSDR ABXA9701978Connector · dirtyAFTER UPLATCH CHECK, UNSAFE GEAR LIGHT CAME ON. RECYCLED GEAR. SUBSEQUENT UPLATCH CHECK WAS GOOD. GEAR WELL AREA WAS FOUND TO BE SATURATED WITH DE-ICE FLUID. CLEANED FLUID FROM CONNECTORS. NO DEFECTS NOTED.Dec 12, 1997 · N826AX · Doug DC863F · Landing Gear Position and WarningSDR ABXA9701408Skin · excessive gapDURING PREFLIGHT, FOUND EXCESSIVE GAP AT LEADING EDGE OF NR 3 PYLON. INSTALLED SEAL AND STAINLESS STEEL STRIP IAW ABX REA D854-20655.Aug 18, 1997 · N826AX · Doug DC863F · Nacelle/Pylon, Plate/SkinSDR ABXA9701404Fitting · crackedFORWARD LOWER CARGO COMPARTMENT RIGHT SIDE FS 280 LONGERON 21R AT CROSS SLIDE DOOR CUTOUT, FORWARD UPPER CORNER FRAME TO FLOOR SUPPORT FITTING IS CRACKED. REPAIRED CRACKED FLOOR SUPPORT FITTING IAW DAC DWG 97540022 AND DC-8 SRM 51-1-24.Aug 13, 1997 · N826AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA9701341Angle · crackedNR 3 PYLON LOWER FORWARD SUPPORT ANGLE AT TOMBESTONE IS CRACKED AT OUTBOARD FASTENER. INSTALLED NEW ANGLE IAW DC-8 SRM 51-3-0 AND DAC DWG NR 9753018.Aug 6, 1997 · N826AX · Doug DC863 · Nacelle/Pylon StructureSDR ABXA9701340Longeron · crackedLONGERON 24, RT HAS AN 8 INCH CRACK, EMANATING FROM BOTTLE BOLT AT 6 O'CLOCK POSITION. *S/D* REPAIRED IAW DC8 SRM 53-2-2 AND 51-1-20.Aug 6, 1997 · N826AX · Doug DC863 · Fuselage Main, Longeron/StringerSDR ABXA9701278Panel · crackedLT WING PANEL 505F HAS 12 CRACKS AT FASTENER HOLES. *S/D* REPAIRED IAW ABX REA D857-19869MR AND DC 8 SRM 51-1-8.Jul 21, 1997 · N826AX · Doug DC863 · Wing, Plate/SkinSDR ABXA9700012Brake Valve · defectiveDURING TAXI THE LEFT MAIN LANDING GEAR BRAKES HAD NO EFFECT IN STOPPING THE AIRCRAFT. REPLACED INBOARD BRAKE CONTROL VALVE, PERFORMED PRESSURE CHECK AND ADJUSTMENT OF BRAKE CONTROL VALVE, OPS CHECKED GOOD AND NO LEAKS NOTED IAW DC-8 MM.Jan 21, 1997 · N826AX · Doug DC863 · Master Cylinder/Brake ValveSDR ABXA9700048Connector · dirtyNR 2 ENGINE LOW OIL PRESSURE LIGHT CAME ON, OIL PRESSURE 50 PSI. RETARDED THROTTLE TO IDLE, LIGHT STAYED ON. SHUT DOWN ENGINE AT 1210 Z. WINDMILLED WITH 34 PSI OIL PRESSURE, 34 PERCENT N-1, 38 PERCENT N-2. VERIFIED LOW OIL PRESSURE LIGHT ON WITH OIL PRESSUJan 1, 1997 · N826AX · Doug DC863F · Engine Oil PressureSDR ABXA9600629Battery Rack · dischargedEMERGENCY LIGHTS WEAK. REPLACED EMERGENCY LIGHT BATTERY RACK IAW DC-8 MM 33-50-1, OPS CHECKED GOOD.Sep 20, 1996 · N826AX · Doug DC863F · Emergency LightingSDR ABXA9600604Power Supply · defectiveEMERGENCY LIGHTING TEST FAILED. REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY IAW DC8 M.M. 33-50-2. OPS CHECK GOOD.Jul 30, 1996 · N826AX · Doug DC863 · Emergency LightingSDR ABXA9600507Battery Rack · dischargedEMERGENCY EXIT LIGHTS EXTINGUISHED AFTER APPROXIMATELY 3 SECONDS OF OPERATION. REPLACED EMERGENCY LIGHT BATTERY RACK ASSEMBLY IAW DC8 MM, OPS CHECK OF EMERGENCY LIGHTING SYSTEM WAS GOOD.Jun 12, 1996 · N826AX · Doug DC863 · Emergency LightingSDR ABXA9600460Hinge Fitting · chafedDURING 826AX MOD, DISCOVERED LEFT HAND INBOARD FLAP INBOARD HINGE ARM CHAFED. REPAIRED HINGE FITTING ON INBOARD FLAP, INBOARD HINGE THAT WAS CHAFED IAW ABX REA D857-12329MR.Dec 27, 1995 · N826AX · Doug DC863 · Trailing Edge FlapsSDR ABXA9600459Tip Cap · dentedDURING 826AX MOD, DISCOVERED LEFT HAND ELEVATOR OUTBOARD TIP CAP DENTED. REPAIRED LEFT HAND ELEVATOR OUTBOARD TIP CAP THAT WAS DENTED IAW ABX REA D853-12346MR.Dec 27, 1995 · N826AX · Doug DC863 · Elevator StructureSDR ABXA9600458Door Jamb · bentDURING 826AX MOD, DISCOVERED R-2 DOOR JAMB LOWER FOWARD CORNER AT FUSELAGE STATION 1620, STRUCTURE IS BENT. REPAIRED R-2 DOOR JAMB FORWARD CORNER FRAME AT FUSELAGE STATION 1620 THAT WAS BENT IAW ABX REA D853-12345MR.Dec 27, 1995 · N826AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA9600454Frame · bentDURING 826AX MOD, DISCOVERED L-2 DOOR JAMB LOWER TORQUE BOX FRAME IS BENT AT FUSELAGE STATION 1613. REPAIRED FUSELAGE STATION 1613 FRAME ON L-2 DOOR THAT WAS BENT IAW ABX REA D853-12374MR.Dec 27, 1995 · N826AX · Doug DC863 · Fuselage Main, FrameSDR ABXA9600453Frame · crackedDURING 826AX MOD, DISCOVERED STATION 1580 AT APPROXIMATELY LONGERON 8L, FROM STATION 25 TO AFT PRESSURE BULKHEAD, STATION 1580 AT CUSP AREA FRAMES OF .100 INCH THICKNESS OR LESS, HAVE NUMEROUS DRILLED HOLES, FRAME END IS CRACKED AND CORRODED. REPAIRED FUSELAGDec 27, 1995 · N826AX · Doug DC863 · Fuselage Main, FrameSDR ABXA9600452Frame · corrodedDURING 826AX MOD, DISCOVERED FRAME SECTION, GUSSET PLATE AND VERTICAL FLOOR SUPPORT FRAME AT STATION 460 BETWEEN LONGERON 27R AND LONGERON 25R HAS AREAS ON CORROSION. REPAIRED FUSELAGE STATION 460 FRAME SECTION, GUSSET PLATE AND VERTICAL FLOOR SUPPORT FRAME ADec 27, 1995 · N826AX · Doug DC863 · Fuselage Main, FrameSDR ABXA9600451Skin · gougedDURING 826AX MOD, DISCOVERED STATION 340, LONGERON 31R, LONGERON 24R-25R, LONGERON 27R FUSELAGE SKIN, STATION 180 LONGEON 25R C1 DOOR AFT BOTTOM CUTOUT HAS GOUGE. REPAIRED FUSELAGE SKIN AT STATION 340, LONGERON 31R, LONGERON 24R-25R, LONGERON 27R AND STATION Dec 27, 1995 · N826AX · Doug DC863 · Fuselage Main, Plate/SkinSDR ABXA9600450Skin · misrepairedDURING 826AX MOD, DISCOVERED STATION 360, LONGERON 27R-29R, BOTH REPAIRS HAVE NO FINGER DOUBLERS. REPAIRED FUSELAGE SKIN AT FUSELAGE STATION 360, LONGERON 27R-29R, THAT HAD NO FINGER DOUBLERS IAW ABX REA D853-12442MR.Dec 27, 1995 · N826AX · Doug DC863 · Fuselage Main, Plate/SkinSDR ABXA9600446Skin · crackedDURING 826AX MOD, DISCOVERED AT STATION 1400, LONGERON 29R TO 33R, C-4 DOOR CUTOUT HAS CRACKS. REPAIRED LOWER FUSELAGE EXTERIOR SKIN AT C-4 DOOR, STATION 1400, LONGERON 29R TO 33R IAW ABX REA D853-12449MR.Dec 27, 1995 · N826AX · Doug DC863 · Fuselage Main, Plate/SkinSDR ABXA9600445Longeron · corrodedDURING 826AX MOD, DISCOVERED LONGERON 27L WAS CORRODED AT STATION 1070 TO 1085 AT AFT CARGO PIT. REPAIRED CORRODED LONGERON 27L AT STATION 1070 TO 1085 IAW ABX REA D853-12471MR.Dec 27, 1995 · N826AX · Doug DC863 · Fuselage Main, Longeron/StringerSDR ABXA9600444Barrier Door · crackedDURING 826AX MOD, DISCOVERED THAT THE AFT ACCESSORY COMPARTMENT DOOR WAS CRACKED AT BOTH LEFT HAND AND RIGHT HAND SIDES. REPAIRED AFT LOWER PIT, AFT BARRIER COMPARTMENT DOOR THAT WAS CRACKED ON BOTH LEFT HAND AND RIGHT HAND SIDES IAW ABX REA D853-12475MR.Dec 27, 1995 · N826AX · Doug DC863 · Cargo Compartments
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