N811AX, cancelled Mar 20, 2007

Service difficulty reports · 85

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 = 'N811AX' AND deregistration_id = 'N811AX-2007-03-20'
  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 ABXA060157Rotary Switch · faultyAFTER TAKEOFF AND GEAR RETRACTED (FROM ILN TO MEM) THE RED GEAR UNSAFE LIGHT REMAINED ILLUMINATED ALONG WITH THE AMBER RIGHT DOOR LIGHT ON F/E'S PANEL. RECYCLED GEAR WITH NO EFFECT. PERFORMED AN UPLATCH CHECK AND ALL LIGHTS EXTINGUISHED WITH A NORMAL UPLATCHApr 5, 2006 · N811AX · Doug DC863F · Landing Gear Position and WarningSDR ABXA060132Warning Light · illuminatedAFTER TAKEOFF WHEN GEAR WAS RETRACTED, RED UNSAFE LIGHT STAYED ON, LEFT MAIN GEAR DOOR LIGHT WAS ON. CYCLED GEAR, OPS CHECKED NORMAL. REMOVED AND REPLACED LEFT MAIN LANDING GEAR DOOR UPLATCH AND INDICATION IAW DC8 MM 32-60-00 AND ALSO CHECKED MIN ROLLER CLEAMar 16, 2006 · N811AX · Doug DC863F · Landing Gear Position and WarningSDR ABXA060059Skin · corrodedFUSELAGE SKIN LOWER SIDE OF NR 3 CARGO DOOR HAD A SPOT OF CORROSION. REPAIRED NR3 CARGO DOOR JAMB SKIN IAW SRM 53-2-1, FIG. 9. PARTIAL WORK NR1-102 FOR WORK ACCOMPLISHED (W.O. 600239852) COI 50853 INITIATED FOR REPAIR REPLACEMENT IN 1000 CYCLES.Jan 20, 2006 · N811AX · Doug DC863F · Fuselage Main, Plate/SkinSDR ABXA050004Transmitter · defectiveNR 4 ENGINE OIL PRESSURE BEGAN FLUXUATING IN CRUISE AND THEN WENT TO '0' PSI. NO LOW OIL PRESSURE LIGHT CAME ON. ALL OTHER ENG PARAMETERS NORMAL. SECURED NR 4 ENGINE AT 0340Z. REMOVED AND REPLACED ENGINE OIL STRAINER. NO CONTAMINATES NOTED. REPLACED MAIN Jan 11, 2005 · N811AX · Doug DC863F · Engine Oil PressureSDR ABXA040363Skin · corrodedFUSELAGE EXTERIOR SKIN BULGED AND FASTENERS HEAD SHEARED LEFT SIDE OF TAILSKID FAIRING. CUT OUT DAMAGED AREA AND INSTALLED FABRICATED DOUBLER REPAIR, TREATED, ALODINED AND PRIMED IAW DC-8 SRM 51-1-21, 53-2-1, 51-1-8, 51-1-20, AND REA D853-50297-MR.Oct 31, 2004 · N811AX · Doug DC863F · Fuselage Main, Plate/SkinSDR ABXA040362Skin · corrodedEXTERIOR LOWER FUSELAGE SKIN CRACKED AND BULGED AT LONGERON 35 RIGHT, FS 102. REMOVED END FITTING, SHEAR TIES AND DOUBLER IAW DC-8 SRM 51-1-21. REINSTALLED END FITTING, SHEAR TIES AND DOUBLER IAW DC-8 SRM 51-1-21 AND 51-1-20D. REPAIRED SKIN IAW REA D853-502Oct 31, 2004 · N811AX · Doug DC863F · Fuselage Main, Plate/SkinSDR ABXA040366Skin · corrodedFORWARD CARGO RIGHT SIDE FROM STA 200 - 220, BETWEEN LONGERON 33 RIGHT - 34 RIGHT, SKIN CORRODED WITH BROKEN RIVETS. REMOVED SHEAR TIES, INSTALLED FINGER DOUBLERS, EXTERNAL DOUBLERS, FILLER AND INTERNAL DOUBLERS AND SHEAR TIES IAW REA D853-50304-MR AND DC-8 SOct 30, 2004 · N811AX · Doug DC863F · Fuselage Main, Plate/SkinSDR ABXA040367Cusp Web · corrodedMAIN CABIN AT FS 1164 - 1170 AND LONGERON 21 RIGHT (CUSP) HAD CORROSION. REPAIRED AREA IAW DC-8 SRM 51-1-8 AND REA D853-50301-MR.Oct 30, 2004 · N811AX · Doug DC863F · Fuselage Miscellaneous StructureSDR ABXA040365Doubler · corrodedAREAS OF CORROSION NOTED ON LOWER SKIN AROUND OUTFLOW VALVE (AFT ACCESSORY COMPARTMENT) FROM FLOOR FRAME 1620 - 1640, LONGERON 34 RIGHT TO 34 LEFT. REMOVED ALL SUBSTRUCTURE AND FASTENERS COMMON TO REPAIR AREA TO FACILITATE REPAIR. REMOVED ALL CORROSION IAW DOct 30, 2004 · N811AX · Doug DC863F · Fuselage Main, Plate/SkinSDR ABXA040364Support · corrodedRIGHT FUSELAGE STA 915 - 935, SUPPORT BRACE OUTBOARD OF LONGERON 24 RIGHT, EXFOLIATED. REPAIRED AREA IAW REA D853-50298-MR.Oct 30, 2004 · N811AX · Doug DC863F · Fuselage Miscellaneous StructureSDR ABXA040334Wire Harness · burnedDURING LINE MAINTENANCE INVESTIGATION OF NR 3 ENGINE EPR PROBLEM, FOUND THE EPR WIRING HARNESS, THRUST BRAKE WIRING AND THRUST REVERSER EMERGENCY DUMP VALVE WIRING CHARRED AND FRAYED DUE TO A PREVIOUS PNEUMATIC DUCT LEAK. REPLACED WIRE NR 3H406E24, 3H2156B24,Sep 27, 2004 · N811AX · Doug DC863F · Engine Indicating System WiringSDR ABXA040333Wire · frayedDURING LINE MAINTENANCE, FOUND NR 3 ENGINE EPR WIRING HARNESS CHARRED AND FRAYED DUE TO PREVIOUS PNEUMATIC LEAK. REPLACED NR 3 ENGINE EPR WIRES 7E57SA24N AND 3E573A24N BETWEEN CONNECTOR P1-1449 AND GROUND 825.Sep 27, 2004 · N811AX · Doug DC863F · Engine Indicating System WiringSDR ABXA040207Escape Rope · mismanufacturedCHECK EMERGENCY ROPE AT MAIN CABIN DOOR FOR PROPER LENGTH. ROBBED EMERGENCY ROPE FROM 826AX, CHECKED FOR PROPER LENGTH AND INSTALLED ON 811AX IAW DC-8 MM 25-60-02-0002. CANNIBALIZATION FORM WAS FILLED OUT.Jun 13, 2004 · N811AX · Doug DC863F · Emergency EquipmentSDR ABXA040200Jackscrew · bindingDURING APPROACH TO GUA, STABILIZER JAMMED, WOULD NOT MOVE BOTH ELECTRIC OR HYDRAULIC. INDICATOR AT 5.2 DEGREES. FOUND GEARBOX SPROCKET SHEAR PINS SHEARED AND RIGHT JACKSCREW BINDING. INSTALLED NEW SHEAR PINS IAW DC8 OVHL MM 27-10-1. REPLACED LEFT AND RIGHTJun 2, 2004 · N811AX · Doug DC863F · Stabilizer Control SystemSDR ABXA040116Engine · defectiveUPON INITIAL CLIMBOUT, NR 2 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED. NR 2 ENGINE OIL PRESSURE WAS NOTED TO BE 28 PSI AND OIL QUANTITY DECREASING. SHUT DOWN ENGINE AT 0424Z. N1 AND N2 RPM'S NOTED: 22/35. ENGINE OIL PRESSURE IN CRUISE: 3 PSI. REPLACEDMar 24, 2004 · N811AX · Doug DC863F · Engine (Turbine/Turboprop)SDR ABXA040107Actuator · bypassingON CLIMBOUT, THE AIRCRAFT EXPERIENCED A VIOLENT LATERAL FLUTTER. THE AUTOPILOT WAS OFF, YAW DAMPER ENGAGED. THE YAW DAMPER WAS DISENGAGED BY PILOT WITH NO NOTEABLE DIFFERENCE. DEPOWERED THE RUDDER HYDRAULICS AND THE FLUTTER STOPPED. FURTHER TROUBLESHOOTINGMar 12, 2004 · N811AX · Doug DC863F · Autopilot SystemSDR ABXA040065Uplock · damagedGEAR UPLATCH CHECK FAILED. RIGHT MAIN LANDING GEAR DOOR NOT LATCHED LIGHT ILLUMINATED WITH LANDING GEAR RED UNSAFE LIGHT. IAS DID NOT EXCEED 230 KTS. DEFERRED MAIN LANDING GEAR DOOR UPLATCH SYSTEM IAW DC-8 MEL 32-14, CAT A, CODE 1. PLACARD INSTALLED. MUSTFeb 14, 2004 · N811AX · Doug DC863F · Landing Gear Retraction/Extension SystemSDR ABXA040039Link · looseUPLATCH CHECK FAILED ON INITIAL CHECK. GEAR WAS CYCLED THROUGH ONCE THEN UPLATCH CHECK WAS ACCOMPLISHED. UPLATCH CHECK WAS SATISFACTORY. FOUND LEFT MAIN LANDING GEAR LOWER SIDE BRACE LOWER LINK AND LOWER SIDE BRACE UPPER LINK WITH EXCESSIVE PLAY. REPLACE UJan 23, 2004 · N811AX · Doug DC863F · Landing Gear Retraction/Extension SystemSDR ABXA030475Arm · wornRED GEAR UNSAFE LIGHT CAME ON AFTER GEAR RETRACTION WITH RT GEAR DOOR LIGHT ON FLIGHT ENGINEER'S PANEL. RECYCLED GEAR, ALL INDICATIONS NORMAL. MAINTENANCE FOUND DOOR ROLLER OUT OF ADJUSTMENT AND AFT ARM WORN. REPLACED ARM, ADJUSTED MAIN GEAR DOOR UPLATCH MEDec 13, 2003 · N811AX · Doug DC863F · Landing Gear Door Retract SectionSDR ABXA030474Proximity Sensor · dirtyLANDING GEAR UNSAFE LIGHT ILLUMINATED IN CRUISE. NOT LATCHED LIGHT ON FLIGHT ENGINEER'S PANEL ILLUMINATED WITH SELECTION RT GEAR POSITION. PERFORMED ABNORMAL. LIGHTS EXTINGUISHED WHEN LANDING GEAR WAS CYCLED. MAINTENANCE FOUND RT MAIN LANDING GEAR DOOR NOTDec 12, 2003 · N811AX · Doug DC863F · Landing Gear Position and WarningSDR ABXA030308Spring · wornTHE GEAR UNSAFE LIGHT ILLUMINATED INTERMITTENTLY ACCOMPANIED WITH LEFT DOOR NOT LATCHED LIGHT AT FLIGHT ENGINEER'S PANEL. PERFORMED ABNORMAL CHECK, UNSAFE LIGHT WOULD NOT REMAIN ILLUMINATED LONG ENOUGHT TO DETERMINE WHICH SWITCH MAY BE MALFUNCTIONING. REPLACJul 22, 2003 · N811AX · Doug DC863 · Landing Gear Retraction/Extension SystemSDR ABXA030170Seal · tornGEAR UNSAFE LIGHT REMAINED ILLUMINATED WITH GEAR RETRACTED. CYCLED GEAR AND LIGHT WENT OUT. RIGHT MAIN LANDING GEAR DOOR IDENTIFIED ON FLIGHT ENGINEER'S LANDING GEAR AND DOOR LATCHING PANEL. CLEANED UP LATCH SWITCH. OPS CHECKED GOOD IAW DC-8 AMM 32-60-00-2May 24, 2003 · N811AX · Doug DC863F · Landing Gear Position and WarningSDR ABXA030137Battery · dischargedMAINTENANCE FOUND EMERGENCY LIGHT VERY WEAK IN TEST. REPLACED EMERGENCY LIGHTS BATTERY RACK ASSEMBLY. OPS CHECKED GOOD IAW DC-8 MM.Apr 16, 2003 · N811AX · Doug DC863F · Emergency LightingSDR ABXA030109Proximity Switch · dirtyON CLIMBOUT, GEAR UNSAFE LIGHT STAYED ILLUMINATED AFTER GEAR RETRACTION. RIGHT GEAR DOOR INDICATED. RECYCLED GEAR TWICE. LIGHT WENT OUT. INSPECTED RIGHT GEAR DOOR AND INDICATING SYSTEM COMPONENTS. NO DEFECTS NOTED. DOOR FAIRED ON GROUND WITH HYDRAULIC PRESSUREMar 5, 2003 · N811AX · Doug DC863F · Landing Gear Position and WarningSDR ABXA030067Transmitter · failedDURING CLIMBOUT, WHEN NR 1 ENGINE ANTI-ICE WAS TURNED OFF, NR 1 ENGINE COMPRESSOR STALLED ACCOMPANIED BY NR 1 OIL PRESSURE WENT TO 100 PSI AND OIL QUANTITY FLUCTUATED +/-2 GALLONS. SECURED ENGINE. ENGINE WINDMILLED ABOVE 25 PERCENT FOR 45 MINUTES. FOUND NR 1 Feb 11, 2003 · N811AX · Doug DC863F · Engine Oil PressureSDR ABXA030062Eyebolt · wornLT MLG WAS MAKING LOUD NOISE DURING RETRACT. ON SERVICE CHECK, FOUND LT MLG RETRACT CYLINGER EYE BOLT HAD EXCESSIVE PLAY. REWORKED PIN IAW 32-13-0001-001 NEA ON SHOP TRAVELER 5816-01.Feb 7, 2003 · N811AX · Doug DC863F · Landing Gear Retraction/Extension SystemSDR ABXA030187Skin · corrodedCLEAN, TREAT AND PRIME SKIN UNDER C4 SCUFF PLATE. CLEANED CORROSION, TREATED, PRIMED SKIN. FABRICATED AND INSTALLED FILLERS, DOUBLERS AND TRIPLERS IAW DC-8 REA D853-46013-MR, AND THE SRM.Feb 4, 2003 · N811AX · Doug DC863F · Fuselage Main, Plate/SkinSDR ABXA030186Longeron · crackedLONGERON 24 RIGHT CRACKED JUST UNDER BOTTLE BOLT IN BATH TUB AREA. ACCOMPLISHED LONGERON 24 RIGHT REPLACEMENT IAW ABX REA D853-46001-MR AND JOB CARD 90453100 (TIMCO).Jan 5, 2003 · N811AX · Doug DC863F · Fuselage Main, Longeron/StringerSDR ABXA030185Skin · crackedAFT PAX DOOR UPPER AFT CORNER HAD 4 CRACKS FOUND WITH NDT L-2. REMOVED DAMAGE IAW DC-8 SRM 53-2-0, FABRICATED AND INSTALLED DOUBLERS AND FILLERS IAW DC-8 SRM 53-2-0, 51-1-20D, AND 51-1-21.Jan 5, 2003 · N811AX · Doug DC863F · Fuselage Main, Plate/SkinSDR ABXA020305Actuator · brokenHYD QTY LOSS ON LANDING. MAINTENACE FOUND THE RT INBOARD FLAP ACTUATOR CRANK ASSEMBLY BROKEN ALONG WITH A BROKEN HYD LINE TO THE ACTUATOR AND ASSOCIATED ATTACHING HARDWARE BROKEN. OPEN: CORRECTIVE ACTION IS NOT COMPLETE.Nov 12, 2002 · N811AX · Doug DC863F · Trailing Edge Flap ActuatorSDR ABXA020306Warning System · malfunctionedDURING CLIMB, AFTER GEAR UPLATCH CHECK, AIRCRAFT HAD LIGHT TURBULANCE. THE RED GEAR UNSAFE LIGHT CAME ON CAUSED BY THE RT MAIN GEAR DOOR UPLATCH LIGHT ILLUMINATED. RECYCLED GEAR TWICE BEFORE LIGHT WENT OUT. PERFORMED ADJUSTMENT ON UPLATCH. OPS CHECKED UPLATCHNov 10, 2002 · N811AX · Doug DC863F · Landing Gear Position and WarningSDR ABXA020278Pump · defectiveMANUAL REVERSION LIGHTS CAME ON DURING FINAL APPROACH. RAN LOSS OF HYDRAULIC PROCEDURES. REPLACED BOTH LT AND RT ENGINE DRIVEN HYDRAULIC PUMPS IAW DC-8 MM 29-10-12-02 AND 29-10-12. SERVICED SYSTEM IAW DC-8 AMM 12-00. LEAK AND OPS CHECKED GOOD.Oct 30, 2002 · N811AX · Doug DC863F · Hydraulic Pump (Electric/Engine), MainSDR ABXA020074Warning System · malfunctionedGEAR UNSAFE LIGHT ILLUMINATED AFTER GEAR RETRACTION. CYCLED GEAR, LIGHT WENT OUT. LOUD GRINDING NOISE HEARD ON 2ND ROTATION.Aug 11, 2002 · N811AX · Doug DC863F · Landing Gear Position and WarningSDR ABXA010915Connector · looseAIR RETURN TO MIA DUE TO LOSS OF HYDRAULIC FLUID. AIRCRAFT DUMPED FUEL IN PREPARATION FOR RETURN TO MIA. FOUND CONNECTOR ON HYDRAULIC QUANTITY TRANSMITTER LOOSE. CLEANED AND RESECURED. SYSTEM OPS CHECKED GOOD. CHECKED FUEL DUMP SYSTEM AFTER USE, FOUND ALLJun 20, 2002 · N811AX · Doug DC863F · Hydraulic Pressure SensorSDR ABXA010897Flap · out of rigON TAKEOFF WITH FLAPS SELECTED TO 18 DEG, THE INDICATOR INDICATED 15 DEG, THEN INCREASED TO 20 DEGREES. ON APPROACH, FLAP INDICATION WAS AS FOLLOWS, 12 SELECTED, 10 INDICATED - 23 SELECTED, 23 INDICATED - 35 SELECTED, 40 INDICATED. AIRCRAFT WAS FERRIED FROM May 23, 2002 · N811AX · Doug DC863F · Trailing Edge Flap Control SystemSDR ABXA010707Fuel Control · failedDURING DESCENT, THE NR 4 ENGINE FAILED TO ACCELERATE. EPR, EGT, RPM AND F/F DECAYED. OIL PRESSURE WAS NORMAL (WINDMILLING). PERFORMED CHECKLIST - NO HELP. DURING LEVEL OFF WITH INCREASED AIRSPEED - NEGATIVE RELIGHT. PERFORMED ENGINE SHUTDOWN ACTIONS CHECKFeb 8, 2002 · N811AX · Doug DC863F · Fuel Control/Turbine EnginesSDR ABXA010655Actuator · brokenON SERVICE CHECK, FOUND BOTH CRANK ASSEMBLIES TO THE RIGHT WING INBOARD SPOILER RODS BROKEN. REPLACED BOTH INBOARD SPOILER REAR SPAR ACTUATOR CRANK ASSEMBLIES IAW DC-8 MM 27-61-01-2-0001.Dec 24, 2001 · N811AX · Doug DC863F · Drag Control ActuatorSDR ABXA010397Seat Track · dirtyAFTER MOVING THE CAPTAIN'S SEAT FORWARD OR AFT, THE HANDLE DID NOT LOCK DOWN ALLOWING THE SEAT TO MOVE. CLEANED AND LUBRICATED THE SEAT TRACK. CHECKED GOOD IAW DC-8 MM 25-11-01.Jul 8, 2001 · N811AX · Doug DC863F · Fuselage, Seat/Cargo Attach FittingsSDR ABXA010398Brake · malfunctionedON LANDING, 5 MAIN LANDING GEAR TIRES BLEW. MECHANICS FOUND THAT THE EMERGENCY AIR BRAKE BOTTLE WENT OFF. REPLACED AFT AIR BRAKE MECHANICAL CONTROL CABLE. REF CABLE RUN 81B, 82B, IAW DC-8 MM 32-45-00. SERVICED AIR BRAKE BOTTLE. OPS CHECK OF AIR BRAKE SYSTJul 2, 2001 · N811AX · Doug DC863F · BrakeSDR ABXA010339Lock · lack of lubeCAPTAIN'S SEAT WOULD NOT REMAIN IN SELECTED POSITION. INTERMITTENTLY CAUSED SEAT TO SLIDE BACK ON TRACK. LUBRICATED CAPTAIN'S SEAT TRACKS AND LOCKING MECHANISM. SEAT NOW STAYS IN SELECTED POSITION.Jun 8, 2001 · N811AX · Doug DC863F · Flight Compartment EquipmentSDR ABXA010303Door · faultyCOCKPIT DOOR WAS DIFFICULT TO KEEP CLOSED. UNSAFE AS IS REF, UNABLE TO KEEP CLOSED DURING EMERGENCY PROCEDURE. COCKPIT SMOKE REMOVAL, STEP 6. NOTE: DOOR CAME OPEN SEVERAL TIMES DURING FLIGHT. OPEN AND CLOSED COCKPIT DOOR SEVERAL TIMES BY USING THE COCKPIT DJun 8, 2001 · N811AX · Doug DC863F · Fixed Inner DoorsSDR ABXA010286Longeron · corrodedFORWARD CARGO COMPARTMENT LONGERON 28 LEFT CORRODED AT FS 280 INSIDE TORQUE BOX. REPAIRED AREA IAW DC-8 SRM 51-3-0, 51-1-21, 51-1-20D, AND REA D853-40780MR.Jun 4, 2001 · N811AX · Doug DC863F · Fuselage Main, Longeron/StringerSDR ABXA010292Longeron · corrodedLEFT MAIN LANDING GEAR WHEEL WELL LONGERON 24 HAD CORROSION ON UPPER SURFACE BETWEEN STATION 879 - 902. CORROSION ALSO RUNS UNDER FITTING AT STATION 902. REPLACED LEFT LONGERON 24 IAW DAC DWG 5750198.Jun 1, 2001 · N811AX · Doug DC863F · Fuselage Main, Longeron/StringerSDR ABXA010285Longeron · corrodedFORWARD CARGO COMPARTMENT CORROSION ON LONGERON 34 RIGHT AT FS 280 INSIDE TORQUE BOX. REPAIRED AREA IAW DC-8 SRM 51-3-0, 51-1-20D, 53-2-2, AND REA D853-40226MR.May 30, 2001 · N811AX · Doug DC863F · Fuselage Main, Longeron/StringerSDR ABXA010284Stiffener · crackedLEFT MAIN LANDING GEAR STATION 940 STIFFENER CRACKED ADJACENT TO CABLE PULLEY ON OUTBOARD WEB. REPAIRED AREA IAW DC-8 DAC DWG 5643402, DC-8 SRM 53-2-0, 51-1-8, 51-1-11, 51-1-21A, AND 51-1-20D.May 29, 2001 · N811AX · Doug DC863F · Fuselage Miscellaneous StructureSDR ABXA010234Fitting · crackedFITTING AT STA 980 IN LEFT MAIN LANDING GEAR WHEEL WELL ABOVE LONGERON 24 IS CRACKED. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW DC-8 SRM.May 23, 2001 · N811AX · Doug DC863F · Fuselage Miscellaneous StructureSDR ABXA010223Fitting · crackedCORROSION FOUND ON LONGERON 24 BACK UP FITTING AT STA 879, LEFT MAIN LANDING GEAR WHEEL WELL. FOUND TO BE CRACKED AFTER CORROSION REMOVAL.May 12, 2001 · N811AX · Doug DC863F · Fuselage Miscellaneous StructureSDR ABXA010291Skin · corrodedFS 660 - 680 LONGERON 36 - 35 RIGHT AIRCRAFT SKIN WAS CORRODED UNDER ACCELEROMETER BRACKET INSIDE AND OUTSIDE AIRCRAFT. REPAIRED AREA IAW DC-8 SRM 51-1-21, 51-1-8, 53-2-0, 51-1-20D, AND 53-2-1.Apr 30, 2001 · N811AX · Doug DC863F · Fuselage Main, Plate/SkinSDR ABXA010290Fitting · corrodedRIGHT MAIN LANDING GEAR WHEEL WELL HAD CORROSION ON INBOARD UPPER CHAMBER ON TRAP FITTING. BLENDED AND REMOVED CORROSION FOUND WITHIN LIMITS IAW DC-8 SRM 53-2-0, FIGURE 1, SHEET 3. ALODINED AND PRIMED IAW DC-8 SRM 51-1-8.Apr 26, 2001 · N811AX · Doug DC863F · Fuselage, Landing Gear Attach FittingsSDR ABXA010204Brake · defectiveTHE BRAKES WERE SPONGY AND INEFFECTIVE ON LANDING.Apr 25, 2001 · N811AX · Doug DC863F · Landing Gear Brake System
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