N842AX, cancelled May 15, 2007

Service difficulty reports · 72

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 = 'N842AX' AND deregistration_id = 'N842AX-2007-05-15'
  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 ABXA060160Wire · crushedNR 4 CTC CAUSED VERY LOUD HOWL, VIBRATION AND SMOKE ODOR IN COCKPIT. FOUND NR 4 CTC WIRING METAL OVERBRAID CRUSHED 1/2" FROM UPPER CONNECTOR. REPAIRED WIRING IAW REA D821-53653 AS REQUIRED. SYSTEM OPS CHECKED GOOD.Apr 14, 2006 · N842AX · Doug DC863F · Electrical Power System WiringSDR ABXA060143Frame · corrodedFOUND CORROSION ON AFT SIDE OF FRAME CAP, STA 70, BETWEEN LONGERON 29 RIGHT AND LONGERON 30 RIGHT IS OUT OF LIMITS. REMOVED EXISTING EXTERNAL DOUBLER AT STA 70 - 101, LONGERON 28 RIGHT - 30 RIGHT. FABRICATED/INSTALLED NEW DOUBLER TO EXTEND PAST STA 70. FABRMar 11, 2006 · N842AX · Doug DC861 · Fuselage Main, FrameSDR ABXA060144Fitting · corrodedWHILE ADDRESSING CORROSION ON AFT SIDE OF FRAME CAP, STA 70, BETWEEN LONGERON 29 RIGHT AND 30 RIGHT, CORROSION WAS FOUND ON THE LONGERON 30 RIGHT END TIE FITTING. IT WAS OUT OF LIMITS. FABRICATED NEW FITTING IAW ABX REA D853-53464, ON ITEM VY-067. FITTING WMar 11, 2006 · N842AX · Doug DC861 · Fuselage Main, Attach FittingsSDR ABXA060135Floorbeam · corrodedFOUND STA 25, RIGHT BUTT LINE 55, MAIN CABIN FLOORBEAM HAD CORROSION. FLOORBEAM IN AREA OF STA 25, RIGHT BUTT LINE 55 REPLACED IAW DC8 SRM 51-1-21 AND 51-1-20D.Feb 28, 2006 · N842AX · Doug DC861 · Fuselage Main, Floor BeamSDR ABXA060133Skin · corrodedFOUND STA 1623 TO 1630, LONGERON 32 RIGHT TO 33 RIGHT, SKIN MATERIAL CORRODED OUT OF LIMITS 36% MATERIAL LOSS (NOTED ON ITEM YY-783, STEP 17). INSTALLED REPAIR DOUBLER IAW DC8 SRM 53-2-0, FIG 1D, 51-2-1, 51-1-8 AND 53-2-1, REF PARTIAL WORKSHEET NR 99.Feb 24, 2006 · N842AX · Doug DC861 · Fuselage Main, Plate/SkinSDR ABXA060142Seat Track · corrodedFOUND CORROSION ON SEAT TRACK MAIN CARGO BAY AT STA 960 - 970, RIGHT BUTT LINE 24, AROUND FASTENERS. OUT OF LIMITS. FIT AND DRILLED TWO NEW SECTIONS OF SEAT TRACK FORM STA 890 TO 990 (PO# 1123125) AND STA 990 TO 1030 (PO# 1068063). TREATED, PRIMED AND INSTAFeb 24, 2006 · N842AX · Doug DC861 · Fuselage, Seat/Cargo Attach FittingsSDR ABXA060115Skin · corrodedSTA 22, OUTBOARD OF LONGERON 31 RIGHT, SKIN AREA WAS OUT OF LIMITS DUE TO CORROSION BLEND OUT, 27% MATERIAL LOSS. FABRICATED SKIN DOUBLER. TREATED, PRIMED AND INSTALLED DOUBLER IAW DC8 SRM 51-1-21, 51-1-8, 53-2-0 AND LWR 20030215.Feb 24, 2006 · N842AX · Doug DC861 · Fuselage Main, Plate/SkinSDR ABXA060134Longeron · corrodedCORROSION FOUND LONGERON 31 RIGHT AROUND OUTBOARD RIVET ROW STA 21.5 WHILE OPENING AREA FOR ITEM YY-882. REMOVED LONGERON 31 RIGHT FROM STA. 10 TO 70. FABRICATED NEW, PO NR 112478, TREATED, PRIMED AND INSTALLED REF. DC8 SRM 51-1-21, 51-1-20D, 51-3-0, 51-1-8 Feb 20, 2006 · N842AX · Doug DC861 · Fuselage Main, Longeron/StringerSDR ABXA060117Finger Doubler · corrodedFOUND FORWARD ACCESSORY COMPARTMENT, STA 20, LONGERON 31 RIGHT, FINGER DOUBLER CORRODED. CORROSION REMOVED FROM INTERNAL FINGER DOUBLER BY BLENDING, RESULTING IN LOCALIZED AREAS THAT EXCEEDED ALLOWABLE SRM LIMITS. REPAIR ACCOMPLISHED IAW REA D853-53187.Feb 16, 2006 · N842AX · Doug DC861 · Fuselage Main, Plate/SkinSDR ABXA060104Frame · corrodedCORROSION ON FRAME IN AFT CARGO BAY AT STA 1020, LONGERON 35 LEFT. OUT OF LIMITS. FABRICATED T-BRACKET USING 7075-T6 0.120" X 0.090" THK. FABRICATED DOUBLER USING 7075-T6 0.100" THK. TREATED PRIMED REPAIR PARTS AND INSTALLED IAW DC8 SRM 51-2-0, PG 49, 53-4Feb 16, 2006 · N842AX · Doug DC861 · Fuselage Main, FrameSDR ABXA060139Fitting · corrodedWHILE REMOVING LONGERON 24 RIGHT AT STA 5 - 25 THE END FITTING AT STA 70 WAS NOTED TO HAVE CORROSION. REMOVED AND REPLACED END FITTING. FITTING FABRICATED IAW ABX REA D853-53189 ON ITEM YY-985.Feb 14, 2006 · N842AX · Doug DC861 · Fuselage Main, Attach FittingsSDR ABXA060138Stiffener · corrodedLONGERON STIFFENER INSIDE LONGERON 23 RIGHT, STA 5 - 25 CORRODED BEYOND LIMITS. REMOVED AND REPLACED STIFFENER. FABRICATED NEW STIFFENER FOR LONGERON 23 RIGHT, STA 5 - 25 IAW REA D853-53185 ON CARD YY-977.Feb 14, 2006 · N842AX · Doug DC861 · Fuselage Miscellaneous StructureSDR ABXA060140Stiffener · corrodedWHILE REMOVING LONGERON 24 RIGHT AT STA 5 - 25, A STIFFENER AT STA 8 WAS NOTED TO HAVE CORROSION. REMOVED AND REPLACED STIFFENER AT STA 8 STIFFENER FABRICATED IAW ABX REA D853-53186 ON ITEM YY-978.Feb 14, 2006 · N842AX · Doug DC861 · Fuselage Miscellaneous StructureSDR ABXA060145Skin · corrodedFOUND SHEARED RIVET HEADS STA 95 - 100, RIGHT SIDE ON LONGERON 29. FOUND CORROSION ON SKIN OUT OF LIMITS. REMOVED DAMAGED SKIN AREA, 3" WIDE CENTERED ON LONGERON 29 RIGHT AND FROM STA 84 TO 101. FABRICATED FILLER, DOUBLER AND FINGER DOUBLERS. TREATED AND PFeb 14, 2006 · N842AX · Doug DC861 · Fuselage Main, Plate/SkinSDR ABXA060141Longeron · corrodedFOUND SHEARED RIVET HEADS STA 95 - 100, RIGHT SIDE ON LONGERON 29. FOUND CORROSION ON LONGERON OUT OF LIMITS. REMOVED LONGERON 29 RIGHT FROM STA 86 TO 107. REMOVED PREVIOUSLY REPAIRED SECTION FROM STA 72 TO 86. FIT NEW LONGERON SECTIONS FROM STA 72 TO 89.2Feb 14, 2006 · N842AX · Doug DC861 · Fuselage Main, Longeron/StringerSDR ABXA060103Seat Track · corrodedSEAT TRACK SECTION, STA 1500, RIGHT BUTT LINE 46, CORRODED OUT OF LIMITS AROUND SCREW HOLES. REMOVED AND REPLACED SEAT TRACK SECTION IAW DC8 SRM 53-2-3, 51-3-0, 51-1-8, 53-2-0 AND LWR 200302015.Feb 11, 2006 · N842AX · Doug DC861 · Fuselage, Seat/Cargo Attach FittingsSDR ABXA060114Support Fitting · corrodedFOUND STA 25, MAIN CABIN RIGHT SIDE, CUSP LINE, FRAME SUPPORT FITTING CORRODED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D AND 51-3-0.Feb 9, 2006 · N842AX · Doug DC861 · Fuselage Miscellaneous StructureSDR ABXA060113Skin · corrodedFOUND CRACK ON AFT LOWER SKIN OF R1 DOOR CUTOUT, APPROXIMATE STA 190, RIGHT BUTT LINE 67. REMOVED DAMAGED AREA. FABRICATED FILLER 7075-T6 0.063". FABRICATED DOUBLERS, ONE FROM 7075-0, 0.063" AND THE OTHER FROM 7075-0, 0.080". HEAT TREATED DOUBLERS FROM -0 Feb 8, 2006 · N842AX · Doug DC861 · Fuselage Main, Plate/SkinSDR ABXA060137Fitting · corrodedFOUND LOWER AFT CARGO, STA 1230, LONGERON 28 RIGHT, LONGERON BATHTUB FITTING CORRODED OUT OF LIMITS. REMOVED AND REPLACED BATHTUB FITTING IAW DC8 SRM 51-1-21, 51-1-20D, 51-1-8, 51-3-1 AND LWR 200302015.Feb 7, 2006 · N842AX · Doug DC861 · Fuselage Main, Attach FittingsSDR ABXA060136Longeron · corrodedFOUND CORROSION ON OUTER HORIZONTAL LEG OF LONGERON 33 LEFT AT STA 1240. AFTER REMOVING CORROSION BY LOCALIZED BLENDING, THE AREA WAS OUT OF LIMITS. CUT OUT DAMAGED SECTION AND APPLIED SPLICE REPAIR TO LONGERON 33 LEFT AT STA 1240 IAW REA D853-53188.Feb 7, 2006 · N842AX · Doug DC861 · Fuselage Main, Longeron/StringerSDR ABXA060116Stiffener · gougedSTA 1160, LONGERON 32 RIGHT, AFT CARGO CROSS SLIDE DOOR, LOWER FORWARD DOOR JAMB STIFFENER GOUGED. REMOVED AND REPLACED STIFFENER IAW DC8 SRM 51-1-20D.Feb 7, 2006 · N842AX · Doug DC861 · Fuselage Miscellaneous StructureSDR ABXA060111Rib · corrodedTWO BROKEN RIVETS AND BULGED RIB ON TOP OF WING CENTER BOX SECTION STA 759, RIGHT BUTT LINE 50. WEB WAS DISCOVERED TO HAVE EXFOLIATION CORROSION AT 2 LOCATIONS BEHIND RIB. CUT OUT 2 AREAS OF CORROSION ON WEB STA 759, RIGHT BUTT LINE 50 AND RIGHT BUTT LINE 53Feb 7, 2006 · N842AX · Doug DC861 · Fuselage Main, StructureSDR ABXA060112Frame · corrodedLOWER AFT CARGO, STA 1040, BUTT LINE 0, LOWER FRAME SURFACE CORRODED. REMOVED FASTENERS AND CARGO TRACK TO ACCESS CORROSION SITE. FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR PARTS FOR FRAME AND SHEAR TIE IAW DC8 SRM 53-4-1, 53-2-0 AND DC8 SSRM DRAWING K048Feb 7, 2006 · N842AX · Doug DC861 · Fuselage Main, FrameSDR ABXA060102Frame · corrodedLOWER AFT CARGO STA 1100, LOWER FRAME RIGHT BUTT LINE 5 TO LEFT BUTT LINE 5, SURFACE CORROSION. REMOVED CORROSION IAW DC8 SRM 51-1-8 AND 53-2-0. OUT OF LIMITS. INSTALLED DOUBLER IAW DC8 SRM 51-1-20.Feb 7, 2006 · N842AX · Doug DC861 · Fuselage Main, FrameSDR ABXA060100Clip · corrodedLOWER AFT CARGO STA 1000 BETWEEN LONGERON 33 RIGHT AND 32 RIGHT, FRAME CLIP CORRODED OUT OF LIMITS. REMOVED CORROSION IAW DC8 SRM 51-1-8. MADE REPAIR IAW REA D853-53274, AND INSTALLED FASTENERS IAW DC8 SRM 51-1-20.Feb 7, 2006 · N842AX · Doug DC861 · Fuselage Main, Attach FittingsSDR ABXA060101Seat Track · corrodedSEAT TRACK SECTION, STA 1580 TO STA 1620, LEFT BUTT LINE 42, CORRODED OUT OF LIMITS. REMOVED SEAT TRACK SECTION, FABRICATED AND INSTALLED NEW SECTION IAW DC8 SRM 53-2-3, 51-3-0 AND 51-1-11.Feb 7, 2006 · N842AX · Doug DC861 · Fuselage, Seat/Cargo Attach FittingsSDR ABXA060110Doubler · corrodedHEAVY CORROSION IN FORWARD CARGO BILGE AT BASE OF FORWARD BULKHEAD STA. 70, BUTT LINE 0. REMOVED AND REPLACED NOSE JACK PAD DOUBLER AND VERTICAL FRAME ASSEMBLY FOR CORROSION AT STA 70, BUTT LINE 0 IAW DC8 SRM 53-0.Feb 6, 2006 · N842AX · Doug DC861 · Fuselage Main, Plate/SkinSDR ABXA060099Fitting · corrodedCORROSION ON LEFT UPPER SIDE WING BOX SECTION, BUTTERFLY FITTING AT STA 683, LEFT BUTT LINE 62. CORRODED OUT OF LIMITS. REMOVED AND REPLACED LEFT UPPER SIDE WING BOX SECTION BUTTERFLY FITTING AT STA 683, LEFT BUTT LINE 62 IAW DC8 SRM 51-1-20D.Feb 6, 2006 · N842AX · Doug DC861 · Fuselage Main, Attach FittingsSDR ABXA060098Pressure Panel · corroded3 RIVET HEADS WERE SHEARED AND METAL WAS BULGING UNDER REINFORCEMENT STRAP, UPPER SURFACE OF RIGHT MAIN LANDING GEAR WHEEL WELL FORWARD OUTBOARD CORNER JUST OUTBOARD OF CEILING SERVICE LIGHT. WEB OUT OF LIMITS AFTER CORROSION REMOVAL MATERIAL LOSS 35%. REMOVFeb 2, 2006 · N842AX · Doug DC861 · Fuselage Main, BulkheadSDR ABXA060097Skin · corrodedCORROSION AROUND FASTENERS ON RIGHT WING, LEADING EDGE, UPPER SURFACE AT XFS 356.00. CORROSION OUT OF LIMITS. FABRICATED REPAIR DOUBLERS AND FILLERS IAW DC8 SRM 57-2-1. INSTALLED REPAIR IAW ABX SSRM K08002.Feb 2, 2006 · N842AX · Doug DC861 · Leading Edge DevicesSDR ABXA050340Battery Pack · inoperativeEMERGENCY EXIT LIGHTS (UNDER GLARESHIELD, OVERHEAD AND CLOSET LIGHTS) VERY DIM. OPS CHECKED ALL LIGHTS, ALL OPS CHECKED GOOD AT THIS TIME IAW DC8 MM.Dec 7, 2005 · N842AX · Doug DC861 · Emergency LightingSDR ABXA050341Battery Pack · dischargedEMERGENCY EXIT LIGHTS STILL DIM AND EMERGENCY HORIZONTAL GYRO LIGHTS DON'T WORK. GYRO FLAGGED WITH BATTERY POWER ONLY. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS BATTERY PACK IAW DC8 MM. EMERGENCY EXIT LIGHTS OPS CHECKED GOOD. REMOVED AND REPLACED STANDBY Dec 7, 2005 · N842AX · Doug DC861 · Emergency LightingSDR ABXA040266Window · stickingFIRST OFFICER'S SLIDING WINDOW WOULD NOT OPEN. REPLACED FIRST OFFICER'S SLIDING WINDOW IAW DC8 56-10-0.Jul 29, 2004 · N842AX · Doug DC861 · Flight Compartment WindowsSDR ABXA040265Spring · brokenDURING MAINTENANCE, FOUND FIRST OFFICER'S WINDOW WAS STUCK. REPLACED SPRING, OPS CHECKED WINDOW. WINDOW DID NOT STICK. PRESSURIZED AIRCRAFT TO 5 PSI DIFF. CHECKED WINDOW AFTER DEPRESSURIZATION. OPENED AND CLOSED NORMALLY.Jul 12, 2004 · N842AX · Doug DC861 · Flight Compartment WindowsSDR ABXA040088Spar Cap · crackedSTA 857 LEFT BUTTLINE 24, SPAR CAP CRACKED. REPAIRED SPAR CAP IAW DC-8 SRM 53-2-5, 51-1-8, 51-1-21, AND 51-3-1.Feb 28, 2004 · N842AX · Doug DC861 · Fuselage Main, StructureSDR ABXA040089Fitting · crackedLEFT LONGERON 23 CRACKED AT STA 920. REPAIRED LONGERON IAW DC-8 SRM 53-2-2, 51-1-8, 51-1-20D, 51-3-1, AND 51-3-0.Feb 15, 2004 · N842AX · Doug DC861 · Fuselage Main, Longeron/StringerSDR ABXA040090Skin · corrodedFORWARD LOWER CARGO CORROSION FUSELAGE SKIN AT LONGERON 35 LEFT, FS 620. REPAIR ACCOMPLISHED IAW REA D853-48847MR AND DC-8 SRM 53-2-1, 51-1-20D, AND 51-1-8.Feb 14, 2004 · N842AX · Doug DC861 · Fuselage Main, Plate/SkinSDR ABXA040035Battery Pack · defectiveDURING MAINTENANCE INSPECTION, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE. OPS CHECKED EVERY EXIT LIGHT IAW DC8-1, STEP 7. OPS CHECKED GOOD. OPS CHECKED AGAIN, NO GOOD. REPLACED EMERGENCY LIGHT POWER PACK IAW DC8 WDM 33-51-01. OPS CHECKED GOOD IAW DC8-1, STEJan 15, 2004 · N842AX · Doug DC861 · Emergency LightingSDR ABXA040034Battery Pack · defectiveDURING MAINTENANCE INSPECTION, FOUND BATTERIES FOR THE EMERGENCY LIGHT EXPLODED W/O 600187843. REPLACED BATTERY PACK AND OPS CHECKED GOOD IAW DC-8 MM 33-50-02-2.Jan 6, 2004 · N842AX · Doug DC861 · Emergency LightingSDR ABXA030075Fan · defectiveLT RECIRCULATION FAN STALLED WITH ODOR OF WIRE BURNING AND ELECTRICAL SURGE ON AIRCRAFT. REMOVED AND REPLACED LT RECIRCULATION FAN IAW DC-8 MM 21-21-01-2. OPS CHECKED GOOD IAW DC-8 MM.Feb 18, 2003 · N842AX · Doug DC861 · Air Distribution FanSDR ABXA020364Link · brokenRT WING INBOARD SPOILER WOULD NOT DEPLOY. REMOVED AND REPLACED BROKEN ACTUATOR CRANK LINKS IN THE INBOARD AND OUTBOARD POSITIONS FOR THE RT INBOARD SPOILER PANEL IAW MM. OPS CHECKED GOOD.Dec 18, 2002 · N842AX · Doug DC861 · Drag Control SystemSDR ABXA010844Doubler · crackedRIGHT WING 505F PANEL LAND NUT CHANNEL REMOVED, SEALANT REMOVED, AND HOLES POLISHED TO FACILITATE NDT INSPECTION. REPAIRED AREA IAW DC-8 SRM 51-1-20D AND REA D857-43117MR.Apr 21, 2002 · N842AX · Doug DC861 · Wing StructureSDR ABXA010843Doubler · crackedLEFT WING PANEL LAND 505F, UPPER SURFACE, 3 EACH FASTENER HOLES CRACKED. REPAIRED AREA IAW REA D857-43118MR.Apr 21, 2002 · N842AX · Doug DC861 · Wing StructureSDR ABXA010840Rib · crackedF.S. 870, RIGHT WHEEL WELL, LOWER OUTBOARD RIB REPAIR WAS CRACKED. FABBED AND INSTALLED NEW REPAIR, AND REPAIRED AREA IAW DC-8 SRM 51-1-8, 53-2-0, 51-1-20D AND ABX DWG 5616306.Apr 18, 2002 · N842AX · Doug DC861 · Fuselage Structure (General)SDR ABXA010839Attach Angle · cracked#1 ENGINE PYLON FOOTSTOOL WAS CRACKED AT THE '6'O-CLOCK POSITION, CENTER BOLT AND NEXT BOLT OUTBOARD. REPAIRED AREA IAW D854-43106MR.Apr 18, 2002 · N842AX · Doug DC861 · Wing StructureSDR ABXA010838Spar Cap · corrodedF.S. 857, BUTT LINE 54 RIGHT, 16" BELOW THE RIGHT MAIN LANDING GEAR WHEEL WELL CEILING, FORWARD BULKHEAD SKIN WAS CORRODED. FABRICATED REPAIR DOUBLER AND SHIM IAW REA D857-43109MR. INSTALLED PARTS AND REPAIRED AREA IAW DC-8 SRM 51-1-8, 51-1-20D AND REA D857-43Apr 18, 2002 · N842AX · Doug DC861 · Fuselage Structure (General)SDR ABXA010837Fitting · crackedFORWARD CARGO AT F.S. 350, BETWEEN LONGERON 36 - 35 LEFT, 'Z' FITTING WAS CRACKED. REPLACED 'Z' FITTING AND REPAIRED AREA IAW DC-8 SRM 51-1-8, 51-1-20D, 51-3-2 AND 53-2-0.Apr 18, 2002 · N842AX · Doug DC861 · Fuselage Structure (General)SDR ABXA010836Fitting · corrodedFORWARD CARGO AT F.S. 330, 'T' BOLT LATCH ATTACH FITTING WAS CORRODED BETWEEN LONGERON 33 RIGHT. REMOVED AND REPLACED BACKUP FITTING IAW DC-8 MM.Apr 18, 2002 · N842AX · Doug DC861 · Fuselage Structure (General)SDR ABXA010835Fitting · crackedFUSELAGE STATION 1168, RIGHT SIDE UPPER CUSP LINE CORNER CASTING FROM CUSP EXTRUSION TO STATION 1168 VERTICAL SUPPORT, HAD A CRACK INDICATION FROM BOLT HEAD TO EDGE OF PART, INBOARD SIDE. REPLACED FITTING AND REPAIRED AREA IAW DC-8 SRM 51-3-2, 51-1-20D AND 51-Apr 18, 2002 · N842AX · Doug DC861 · Fuselage Main, StructureSDR ABXA010868Fitting · crackedLEFT WING STATION 340, FLAP SUPPORT FITTING WAS CRACKED. REMOVED AND REPLACED THE LEFT WING STATION 340 FLAP SUPPORT FITTING IAW DC-8 MM 20-14-00 AND 20-16-00. REMOVED AND REPLACED THE LEFT WING STATION 340 FLAP ACTUATOR CYLINDER AND OPS CHECKED GOOD IAW DC-8Apr 9, 2002 · N842AX · Doug DC861 · Flight Control System
Back to N842AX, cancelled May 15, 2007