# Service difficulty reports: N820AX, cancelled May 15, 2007 A list on [N820AX, cancelled May 15, 2007](https://openairdocs.org/deregistered/N820AX-2007-05-15.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 99 reports - [SDR ABXA040235](https://openairdocs.org/sdr/ABXA040235.md): Fuel Control · defective · Jun 30, 2004 · N820AX · Doug DC863 · Fuel Control/Turbine Engines > PASSING FL 200 ON DESCENT 320 KTS, AS THROTTLE ADVANCED NR 1 ENG FLAMED OUT. IMMEDIATE ACTION ITEM COMPLETED & ENG RESTARTED NORMALLY. MX INSPECTED FUEL TANK BOOST PUMP AND OUTPUT PRESSURE, NO EVIDENCE OF FOD, NO DEFECTS. CHECKED FORWARD PUMP OUTPUT, 190 PS - [SDR ABXA040173](https://openairdocs.org/sdr/ABXA040173.md): Skin · damaged · Apr 28, 2004 · N820AX · Doug DC863 · Rudder, Plate/Skin > RUDDER TRAILING EDGE TIP HAS METAL MISSING. REPAIRED ARE IAW DC-9 SRM 55-2-0, 51-1-2, 51-1-21A, 51-4-8 AND REA D855-49316MR. - [SDR ABXA030386](https://openairdocs.org/sdr/ABXA030386.md): Brake Assy · broken · Oct 7, 2003 · N820AX · Doug DC863 · Brake > NR 8 BRAKE COMPENSATING LINK ATTACH POINT BROKE. REMOVED AND REPLACED BRAKE AND TIRE ASSEMBLY IN THE NR 8 POSITION IAW DC-8 MM 32-40-0. - [SDR ABXA030172](https://openairdocs.org/sdr/ABXA030172.md): Mechanism · broken · May 23, 2003 · N820AX · Doug DC863 · Trailing Edge Flap Control System > WHEN FLAPS WERE EXTENDED TO THE 12 DEG POSITION, THE LEFT FLAP POSITION INDICATED 12 DEG AND THE RIGHT FLAP INDICATED 7 DEG. THE AIRCRAFT ROLLED TO THE LEFT. RETRACTED FLAPS AND RE-EXTENDED, OPS NORMAL. VERIFIED, FOUND RIGHT INBOARD FLAP ACTUATOR MECH ASSEMB - [SDR ABXA030133](https://openairdocs.org/sdr/ABXA030133.md): Uplock · lack of lube · Apr 9, 2003 · N820AX · Doug DC863 · Landing Gear Retraction/Extension System > GEAR UPLATCH FAILED TWICE. RECYCLED AND FOLLOWED ABNORMAL PROCEDURES. SUSPECT CABLE TO NOSE GEAR. TRIED AGAIN ON FINAL APPROACH AND UPLATCH CHECK WAS NORMAL. AIRCRAFT FERRIED TO ILN. INSPECTED UPLATCH ASSEMBLY. GROUND OPS SEVERAL TIMES. LUBRICATED UPLAT - [SDR ABXA020067](https://openairdocs.org/sdr/ABXA020067.md): Longeron · cracked · May 20, 2002 · N820AX · Doug DC863 · Fuselage Main, Structure > FORWARD CARGO STATION 520, LONGERON 35 RIGHT, INBOARD FLANGE WAS CRACKED. REPAIRED AREA IAW REA D853-43899-MR. - [SDR ABXA020065](https://openairdocs.org/sdr/ABXA020065.md): Fitting · corroded · May 20, 2002 · N820AX · Doug DC863 · Fuselage Main, Attach Fittings > FORWARD CARGO, FS 300, BETWEEN LONGERON 33 RIGHT - LONERON 34 RIGHT, "Z" FITTING WAS CORRODED. REPLACED "Z" FITTING AND REPAIRED AREA IAW DC-8 SRM 51-3-2, 51-1-20D AND DAC DRAWING #3755824. - [SDR ABXA020063](https://openairdocs.org/sdr/ABXA020063.md): Strap · corroded · May 20, 2002 · N820AX · Doug DC863 · Fuselage Main, Structure > FORWARD CARGO STATION 485, LONGERON 34 RIGHT, DOUBLER ON BACKSIDE OF LONGERON WAS CORRODED. REPLACED STRAP IAW DC-8 SRM 51-1-24 AND 51-1-20D. - [SDR ABXA020062](https://openairdocs.org/sdr/ABXA020062.md): Shear Tie · corroded · May 20, 2002 · N820AX · Doug DC863 · Fuselage Main, Attach Fittings > AFT CARGO AT STATION 1520, BETWEEN LONGERON 35 RIGHT AND LONGERON 36, SHEAR TIE WAS CORRODED. REPAIRED AREA, FABRICATED AND INSTALLED NEW CLIP IAW DC-8 SRM 51-1-21, 53-2-0, 51-9-0, 53-4-1, 51-1-8 AND 51-1-20D. - [SDR ABXA020061](https://openairdocs.org/sdr/ABXA020061.md): Shear Tie · corroded · May 20, 2002 · N820AX · Doug DC863 · Fuselage Main, Attach Fittings > AFT CARGO AT STATION 1520, BETWEEN LONGERON 35 LEFT AND LONGERON 36, SHEAR TIE WAS CORRODED. REPAIRED AREA, FABRICATED AND INSTALLED NEW CLIP IAW DC-8 SRM 51-1-21, 53-2-0, 51-9-0, 53-4-1, 51-1-8 AND 51-1-20D. - [SDR ABXA020060](https://openairdocs.org/sdr/ABXA020060.md): Fitting · corroded · May 20, 2002 · N820AX · Doug DC863 · Fuselage Structure (General) > FORWARD CARGO AT STA. 70, STRING 25 LEFT, LONGERON END FITTING WAS CORRODED. REPLACED FITTING IAW DC-8 SRM 51-1-21, 51-1-20D AND 51-3-0. - [SDR ABXA020066](https://openairdocs.org/sdr/ABXA020066.md): Attach Angle · corroded · May 19, 2002 · N820AX · Doug DC863 · Fuselage Main, Plate/Skin > AFT LOWER CARGO STATION 986, FLOOR ATTACH ANGLE, BETWEEN LONGERON 33 RIGHT AND LONGERON 34 RIGHT, WAS CORRODED. REPAIRED AREA AND INSTALLED NEW FLOOR ATTACH ANGLE IAW DC-8 SRM 51-1-21, 51-1-20D AND REA D853-43896-MR. - [SDR ABXA020064](https://openairdocs.org/sdr/ABXA020064.md): Skin · cracked · May 17, 2002 · N820AX · Doug DC863 · Wing, Plate/Skin > RIGHT WING, INBOARD OF THE #4 PYLON, STATION XFS 515.00 - 526.76, HAD CRACK INDICATION AT HOLES 2 AND 4 GOING OUTBOARD. REPAIRED AREA AND INSTALLED NEW FILLER AND DOUBLER IAW DC-8 SRM 53-2-0, 51-1-8, 51-1-21, 51-3-0, 51-1-20D AND REA D857-43890-MR. - [SDR ABXA010514](https://openairdocs.org/sdr/ABXA010514.md): Drive Link · broken · Sep 25, 2001 · N820AX · Doug DC863 · Drag Control System > THE LEFT MID FLIGHT SPOILER INBOARD DRIVE LINK FOUND BROKEN DURING SERVICE CHECK INSPECTION. MAINTENANCE INSPECTED AND REPLACED THE INBOARD DRIVE LINK CRANK ASSY AND COMPLETED OPERATIONAL CHECKS IAW DC-8 MM 27-61-01-2. - [SDR ABXA010522](https://openairdocs.org/sdr/ABXA010522.md): Capacitor · blown · Sep 14, 2001 · N820AX · Doug DC863 · Ground Proximity System > #1 RADIO ALTEMETER CIRCUIT BREAKER OPENED. THE BREAKER WAS RESET ONCE AND OPENED AGAIN. MAINTENANCE REPLACED THE #1 RADIO ALTIMETER IAW DC8 MAINTENANCE MANUAL 34. INSPECTION OF THE RADIO ALTIMETER INDICATED THAT THE POWER SUPPLY INPUT CAPACITOR A6C1A EXPLODED, - [SDR ABXA010236](https://openairdocs.org/sdr/ABXA010236.md): Pin · sheared · May 16, 2001 · N820AX · Doug DC863 · Landing Gear Retraction/Extension System > AFTER TAKEOFF, THE LANDING GEAR HANDLE WOULD NOT MOVE TO THE RETRACT POSITION. THE JET PUMP WOULD NOT TURN OFF AND AUTO PRESSURIZATION CONTROL WOULD NOT WORK. MAINTENANCE INSPECTED AND REPLACED THE ANTI-RETRACTION SWIVEL PIN ON THE GROUND SHIFT MECHANISM. O - [SDR ABXA010079](https://openairdocs.org/sdr/ABXA010079.md): Intercostal · corroded · Jan 6, 2001 · N820AX · Doug DC863 · Fuselage Miscellaneous Structure > CORROSION WAS FOUND AT FUSELAGE STATION 1200 - 1180 L34R INSIDE THE TORQUE BOX. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW ABX REA D853-39259 AND DC-8 SRM 51-1-20. - [SDR ABXA000515](https://openairdocs.org/sdr/ABXA000515.md): Seal · leaking · Nov 22, 2000 · N820AX · Doug DC863 · Hydraulic System, Main > SLOW HYDRAULIC FLUID LOSS EN ROUTE; ARRESTED AT STANDPIPE DURING EMERGENCY CHECK LIST. VERIFIED LEAK AT SLOT CONTROL VALVE. REPLACED SEAL. COMPLIED WITH HYDRAULIC RESERVOIR SERVICE IAW DC8 29-16-00. LEAK CHECKED GOOD IAW DC8 MM. - [SDR ABXA000002](https://openairdocs.org/sdr/ABXA000002.md): Power Pack · discharged · Dec 15, 1999 · N820AX · Doug DC863 · Emergency Lighting > EMERGENCY LIGHTS WOULD NOT COME ON WHEN ELECTRICAL POWER WAS LOST. REPLACED EMERGENCY LIGHT PACK ASSY. OPS CHECKED GOOD. - [SDR ABXA9900856](https://openairdocs.org/sdr/ABXA9900856.md): Power Pack · discharged · Dec 14, 1999 · N820AX · Doug DC863 · Emergency Lighting > EMERGENCY LIGHTS DID NOT ILLUMINATE WHEN ELECTRICAL POWER WAS LOST. REPLACED EMERGENCY LIGHT POWER PACK IAW DC8 MM 33-50-00. - [SDR ABXA9900715](https://openairdocs.org/sdr/ABXA9900715.md): Bulb · corroded · Sep 15, 1999 · N820AX · Doug DC863 · Landing Gear Position and Warning > DID NOT GET RIGHT MAIN GEAR GREEN LIGHT WHEN GEAR HANDLE PLACED IN DOWN POSITION. RECYCLED GEAR, DID NOT CHANGE INDICATION. CONTACTS ON BULBS WERE CORRODED. REPLACED BOTH INDICATION BULBS. SYSTEM OPS CHECKED GOOD IAW DC8 MM. - [SDR ABXA9900321](https://openairdocs.org/sdr/ABXA9900321.md): Wheel · failed · Apr 23, 1999 · N820AX · Doug DC863 · Wheel/Ski/Float > BEAD FLANGE SEPARATED FROM NR 5 MAIN LANDING GEAR ASSEMBLY, DAMAGING NR 5 MAIN GEAR BRAKE ASSEMBLY. REPLACED NR 5 WHEEL ASSEMBLY AND NR 5 MAIN GEAR BRAKE ASSEMBLY. - [SDR ABXA9900272](https://openairdocs.org/sdr/ABXA9900272.md): Doubler · cracked · Apr 1, 1999 · N820AX · Doug DC863 · Fuselage Miscellaneous Structure > DOUBLER CRACKED AT STATION 1640 TO 1680. REPAIRED DOUBLER IAW ABX REA D853-27021MR. - [SDR ABXA9900238](https://openairdocs.org/sdr/ABXA9900238.md): Boss · corroded · Mar 22, 1999 · N820AX · Doug DC863 · Main Landing Gear > CORROSION FOUND IN LEFT MAIN LANDING GEAR PIN BOSS HOLE. REPAIRED IAW ABX REA D832-26975 MR. - [SDR ABXA9900237](https://openairdocs.org/sdr/ABXA9900237.md): Doubler · corroded · Mar 22, 1999 · N820AX · Doug DC863 · Fuselage Miscellaneous Structure > INNER DOUBLER AT STATION 1660 TO 1700 CORRODED. REPAIRED IAW ABX REA B853-26997MR. - [SDR ABXA9800866](https://openairdocs.org/sdr/ABXA9800866.md): Window Trim · loose · Oct 2, 1998 · N820AX · Doug DC863 · Flight Compartment Windows > CAPTAIN'S SLIDING WINDOW (EMERG EXIT) WOULD NOT OPEN FULLY. FOUND LOOSE WINDOW TRIM. RESECURED TRIM, WINDOW OPERATED FREELY. - [SDR ABXA9800363](https://openairdocs.org/sdr/ABXA9800363.md): Eadi · defective · Apr 16, 1998 · N820AX · Doug DC863 · Attitude Gyro and Indicating System > FIRST OFFICER'S EADI FAILED. DISPLAY UNIT WENT BLANK, ELECTRICAL SMELL/FUMES WERE NOTED IN THE COCKPIT. REPLACED FIRST OFFICER'S EADI IAW DC8 MM 34-21-0, OPS CHECKED GOOD. - [SDR ABXA9701474](https://openairdocs.org/sdr/ABXA9701474.md): Striker · worn · Sep 16, 1997 · N820AX · Doug DC863 · Landing Gear Door Retract Section > GEAR UNSAFE LIGHT ILLUMINATED AFTER TAKEOFF, WITH RT DOOR NOT LATCHED LIGHT ILLUMINATED. RECYCLED GEAR TWICE AND LIGHT EXTINGUISHED. FOUND RIGHT MAIN GEAR DOOR STRIKER WORN. REPLACED STRIKER AND RAN GEAR IAW DC8 MM 32-31-4, OPS CHECKED GOOD. - [SDR ABXA9701473](https://openairdocs.org/sdr/ABXA9701473.md): Uplatch · lack or lube · Sep 16, 1997 · N820AX · Doug DC863 · Landing Gear Door Retract Section > AFTER GEAR RETRACTION AND ALL GEAR INDICATION LIGHTS OUT, A FEW SECONDS LATER THE RED GEAR UNSAFE LIGHT CAME ON. CYCLED GEAR, LIGHTS WENT OUT. CLEANED AND LUBRICATED RIGHT GEAR DOOR UPLATCH ASSY. INSPECTED AND TESTED IAW DC8 MM 32-6. - [SDR ABXA9701471](https://openairdocs.org/sdr/ABXA9701471.md): Mechanism · out of adjust · Sep 15, 1997 · N820AX · Doug DC863 · Landing Gear Door Retract Section > GEAR UNSAFE LIGHT REMAINS ON AFTER GEAR RETRACTION. ASSOCIATED RT DOOR LIGHT ON FLIGHT ENGINEER PANEL WAS ALSO ILLUMINATED. LIGHTS EXTINGUISHED AFTER GEAR RECYCLE. FOUND LEFT GEAR DOOR MECHANISM OUT OF RIG. RIGGED AND CHECKED IAW DC8 MM 72-31-5. - [SDR ABXA9701593](https://openairdocs.org/sdr/ABXA9701593.md): Rib · cracked · Sep 8, 1997 · N820AX · Doug DC863 · Wing, Rib/Bulkhead > RT WING L/E AT STA XFS 660.00 THE UPPER L/E RIB IS CRACKED AT THE AFT END. INSTALLED REPAIR ANGLE IAW SRM 57-2-0, SRM 51-1-20D AND 51-1-21. - [SDR ABXA9701566](https://openairdocs.org/sdr/ABXA9701566.md): Rib · cracked · Sep 8, 1997 · N820AX · Doug DC863 · Vertical Stabilizer, Spar/Rib > VERTICAL STABILIZER L/E RIB CRACKED STA XFS 242.00 LT AFT END. REPAIRED SRM 55-2-0, SRM 51-1-20D, AND SRM 51-1-21. - [SDR ABXA9701565](https://openairdocs.org/sdr/ABXA9701565.md): Rib · cracked · Sep 8, 1997 · N820AX · Doug DC863 · Vertical Stabilizer, Spar/Rib > VERTICAL STABILIZER L/E RIB CRACKED, STA ZFS 111.00 RT END. REPAIRED IAW SRM 55-2-0, SRM 51-1-20D, AND SRM 51-1-21. - [SDR ABXA9701564](https://openairdocs.org/sdr/ABXA9701564.md): Rib · cracked · Sep 8, 1997 · N820AX · Doug DC863 · Vertical Stabilizer, Spar/Rib > VERTICAL STABILIZER L/E RIB CRACKED, STA ZRS 123.00 LT AFT END. REPAIRED IAW SRM 55-2-0, SRM 51-1-20D, AND SRM 51-1-21. - [SDR ABXA9701563](https://openairdocs.org/sdr/ABXA9701563.md): Rib · cracked · Sep 8, 1997 · N820AX · Doug DC863 · Vertical Stabilizer, Spar/Rib > VERTICAL STABILIZER L/E RIB CRACKED STA ZFS 104.00 LT AFT END. REPAIRED ANGLE IAW SRM 55-2-0, SRM 51-1-20D, AND SRM 51-1-21. - [SDR ABXA9701562](https://openairdocs.org/sdr/ABXA9701562.md): Rib · cracked · Sep 8, 1997 · N820AX · Doug DC863 · Vertical Stabilizer, Spar/Rib > VERTICAL STABILIZER L/E RIB CRACKED STA ZFS 92.00 LT AFT END. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 55-2-0, SRM 51-1-20D, AND SRM 51-1-21. - [SDR ABXA9701595](https://openairdocs.org/sdr/ABXA9701595.md): Rib · cracked · Sep 7, 1997 · N820AX · Doug DC863 · Wing, Rib/Bulkhead > RT WING L/E AT STA XFS 822.500, THE UPPER L/E RIB IS CRACKED AT THE AFT END. INSTALLED REPAIR ANGLE IAW SRM 57-2-10, 51-1-20D AND 51-1-21. - [SDR ABXA9701594](https://openairdocs.org/sdr/ABXA9701594.md): Rib · cracked · Sep 7, 1997 · N820AX · Doug DC863 · Wing, Rib/Bulkhead > RT WING L/E AT STA XFS 697.5 THE UPPER L/E RIB IS CRACKED AT THE AFT END. INSTALLED REPAIR ANGLE IAW SRM 57-2-0, 51-1-20D AND 51-1-21. - [SDR ABXA9701592](https://openairdocs.org/sdr/ABXA9701592.md): Rib · cracked · Sep 7, 1997 · N820AX · Doug DC863 · Wing, Rib/Bulkhead > RT WING L/E AT STA XFS 741.25, THE UPPER L/E RIB IS CRACKED AT THE AFT END. FABRICATED REPAIR ANGLE AND INSTALLED PER SRM 57-2-0 FIG 2, SRM 51-1-20D AND SRM 51-1-21. - [SDR ABXA9701591](https://openairdocs.org/sdr/ABXA9701591.md): Skin · corrosion · Sep 7, 1997 · N820AX · Doug DC863 · Wing, Plate/Skin > LT WING LEADING EDGE SKIN AT STA XW 761 CORROSION REMOVAL BEYOND LIMITS. REPAIRED LT WING L/E STA XW 761 IAW SRM 57-2-1, SRM 51-1-8 AND SRM 51-1-20. - [SDR ABXA9701578](https://openairdocs.org/sdr/ABXA9701578.md): Rib · cracked · Sep 7, 1997 · N820AX · Doug DC863 · Wing, Rib/Bulkhead > LT WING L/E RIB IS CRACKED AT XFS 578.75 AFT UPPER END. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0, SRM 51-1-21, AND SRM 51-1-21. - [SDR ABXA9701577](https://openairdocs.org/sdr/ABXA9701577.md): Rib · cracked · Sep 7, 1997 · N820AX · Doug DC863 · Wing, Rib/Bulkhead > LT WING L/E RIB IS CRACKED, XFS 585.00 AFT UPPER END. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0, SRM 51-1-21, AND SRM 51-1-21. - [SDR ABXA9701576](https://openairdocs.org/sdr/ABXA9701576.md): Rib · cracked · Sep 7, 1997 · N820AX · Doug DC863 · Wing, Rib/Bulkhead > LT WING L/E RIB IS CRACKED, XFS 591.25 AFT UPPER END. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0, SRM 51-1-21, AND SRM 51-1-21. - [SDR ABXA9701575](https://openairdocs.org/sdr/ABXA9701575.md): Rib · cracked · Sep 7, 1997 · N820AX · Doug DC863 · Wing, Rib/Bulkhead > LT WING L/E RIB IS CRACKED XFS 597.5 AFT UPPER END. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0, SRM 51-1-21, AND SRM 51-1-21. - [SDR ABXA9701574](https://openairdocs.org/sdr/ABXA9701574.md): Rib · cracked · Sep 7, 1997 · N820AX · Doug DC863 · Wing, Rib/Bulkhead > LT WING L/E RIB IS CRACKED XFS 603.75 AFT LWR END. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0, SRM 51-1-21, AND SRM 51-1-21. - [SDR ABXA9701567](https://openairdocs.org/sdr/ABXA9701567.md): Frame · corrosion · Sep 7, 1997 · N820AX · Doug DC863 · Fuselage Main, Frame > FUSELAGE FRAME STA 1100 LONG 33R TO 34R FWD UPPER FLANGE, LWR SURFACE HAS EXFOLIATION CORROSION AT NUTPLATES. - [SDR ABXA9701560](https://openairdocs.org/sdr/ABXA9701560.md): Fitting · corroded · Sep 7, 1997 · N820AX · Doug DC863 · Fuselage Miscellaneous Structure > LONGERON SPLICE FITTING HAS SEVERE CORROSION F/S 450 L-30L. REPAIRED LONGERON F/S 450 TO 465 IAW SRM 53-4-1, 51-1-20. - [SDR ABXA9701559](https://openairdocs.org/sdr/ABXA9701559.md): Skin · corrosion · Sep 7, 1997 · N820AX · Doug DC863 · Wing, Plate/Skin > LT WING LEADING EDGE SKIN AT STP XFS 786 CORRODED BEYOND LIMITS. REPAIRED IAW SRM 57-2-1. - [SDR ABXA9701558](https://openairdocs.org/sdr/ABXA9701558.md): Rib · cracked · Sep 7, 1997 · N820AX · Doug DC863 · Wing, Rib/Bulkhead > LT WING L/E RIB IS CRACKED AT XFS 610.00 AFT UPPER END. REPAIRED IAW SRM 52-2-0, SRM 51-1-21, AND SRM 51-1-21. - [SDR ABXA9701557](https://openairdocs.org/sdr/ABXA9701557.md): Rib · cracked · Sep 7, 1997 · N820AX · Doug DC863 · Wing, Rib/Bulkhead > LT WING L/E RIB IS CRACKED AT XFS 616.25 AFT UPPER END. REPAIRED IAW SRM 57-2-0, SRM 51-1-21, AND SRM 51-1-21. Next page: https://openairdocs.org/deregistered/N820AX-2007-05-15/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 = 'N820AX' AND deregistration_id = 'N820AX-2007-05-15' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N820AX-2007-05-15/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.