Douglas DC-8-63F

Service difficulty reports · 1,883

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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 aircraft_model_key = 'DC863F'
  ORDER BY difficulty_date DESC"

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SDR ARWA981048Skin · corrodedLAP - FOUND CORROSION ON FUSELAGE SKIN SPLICE DOUBLER FINGER STATION 610.00 LONGERON 34L. CUT OUT AREA OF CORROSION, FABRICATED DOUBLER AND SHIM AND INSTALLED IAW EO JOSSAIR, CO NR 18R5311018. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B CPCP CONTROL 5074A. Oct 20, 1998 · N661AV · Doug DC863F · Fuselage Main, Plate/SkinSDR ARWA981047Floorbeam · corrodedLAP - FOUND CORROSION ON FLOORBEAM UPPER FORWARD FLANGE, MAIN CABIN STATION 1040 RBL 43.5 TO RBL 55. CUT OUT AREA OF CORROSION, FABRICATED ANGLE AND INSTALLED IAW EO JOSSAIR, CO NR 18R5371030. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B CPCP CONTROL 5994. (Oct 20, 1998 · N661AV · Doug DC863F · Fuselage Main, Floor BeamSDR ARWA981046Web · corrodedLAP - FOUND CORROSION ON PATH RT MLG WW STATINO 857 THROUGH STATION 879. REMOVED CORROSION (BEYOND LIMITS). REMOVED PATCH FABRICATED DOUBLER AND REPLACED IAW DOUGLAS ROD SKETCH 98-08-20-001 WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B CPCP CONTROL 5997. (M)Oct 20, 1998 · N661AV · Doug DC863F · Fuselage Miscellaneous StructureSDR ARWA981045Skin · damagedLAP - IMPROPER REPAIR ON SKIN FUSELAGE EXTERNAL STATION 35, LONGERON 8L TO LONGERON 10L. REMOVED IMPROPER REPAIR FABRICATED DOUBLER AND REPLACED IAW SRM 53-2-0 FIG 15. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A CONTROL 5071A. (M)Oct 20, 1998 · N661AV · Doug DC863F · Fuselage Main, Plate/SkinSDR ARWA981044Skin · crackedLAP - NR 1 CRACK AND 3 INCH, 1.5 INCH RUPTURES AND INADEQUATE REPAIR CUT OUT DAMAGED AREA FABRICATED FILLERS, DOUBLER AND TRIPLER AND INSTALLED IAW SRM 51-1-20D AND BOEING ROD SKETCH 98-08-18-005. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A CONTROL 5679. (M)Oct 20, 1998 · N661AV · Doug DC863F · Fuselage Main, Plate/SkinSDR ARWA981043Skin · corrodedLAP - FOUND CORROSION ON FUSELAGE EXTERIOR SKIN STATION 902.125 LONGERON 13L TO 15L. REMOVED CORROSION (BEYOND LIMITS). FABRICATED DOUBELR AND INSTALLED IAW EO SEMAN NR 1024. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B CPCP CONTROL 5117A. (M)Oct 20, 1998 · N661AV · Doug DC863F · Fuselage Main, Plate/SkinSDR ARWA981042Floorbeam · corrodedLAP - FOUND CORROSION ON FLOORBEAM CARGO COMPARTMENT STATION 55, RBL 12 TO RBL 12. REMVOED CORROSION, BEYOND LIMITS. FABRICATED ANGLES TWO AND INSTALLED IAW EO JOSSAIR, CO NR 18R5371031 WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B CPCP CONTROL 4392. (M)Oct 20, 1998 · N661AV · Doug DC863F · Fuselage Main, Floor BeamSDR ARWA981041Floorbeam · corrodedLAP - FOUND CORROSION ON FLOORBEAM MAIN CARGO COMPARTMENT STATION 1300 RBL 17 CUT OUT AREA OF CORROSION. FABRICATED FILLER AND ANGLE AND INSTALLED IAW EO JOSSAIR, CO NR 18R5371032. WORK ACCOMPLISHED UNDER ARROW AIR JW3B CPCP CONTROL 5990. (M)Oct 20, 1998 · N661AV · Doug DC863F · Fuselage Main, Floor BeamSDR ARWA981040Skin · corrodedLAP - FOUND CORROSION ON REPAIR FUSELAGE STATION 660 TO 720, LONG 34 LEFT TO LONG 34 RT. REMOVED OLD REPAIR FABRICATED DOUBLER AND TRIPLER AND INSTALLED IAW DOUGLAS ROD SKETCH 98-08-25-008. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B CPCP CONTROL 5363. (M)Oct 20, 1998 · N661AV · Doug DC863F · Fuselage Main, Plate/SkinSDR ARWA981039Skin · corrodedLAP - FOUND CORROSION ON FUSELAGE EXTERIOR SKIN STATION 879 THROUGH 902 LONGERON 13R TO LONGERON 15R. REMOVED CORROSION (BEYOND LIMITS). FABRICATED DOUBELR IAW BOEING ACTION NR 378231 AND 379978. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B CPCP CONTROL 5116Oct 20, 1998 · N661AV · Doug DC863F · Fuselage Main, Plate/SkinSDR ARWA981038Floorbeam · corrodedLAP - FOUND CORROSION ON FLOORBEAM MAIN CARGO COMPARTMENT STATION 70, RBL 29. REMOVED CORROSION SRM 51-1-8. FABRICATED ANGLE AND INSTALLED IAW EO JOSSAIR, CO NR 18R5371033. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B CPCP CONTROL 5091A. (M)Oct 20, 1998 · N661AV · Doug DC863F · Fuselage Main, Floor BeamSDR ARWA981037Skin · damagedLAP - FOUND REPAIR IMPROPER ON SKIN FUSELAGE EXTERIOR STATION 1364, LONGERON 23R. REMOVED IMPROPER REPAIR. FABRICATED DOUBLER AND FINGER DOUBLERS AND REPLACED IAW SRM 53-2-1 FIG 7. WORK ACCOMPLISHED UNDER ARROW FORM M3A CONTROL 5063A. (M)Oct 20, 1998 · N661AV · Doug DC863F · Fuselage Main, Plate/SkinSDR ARWA981036Skin · damagedLAP - INADEQUATE REPAIR ON FUSELAGE EXTERIOR SKIN STATION 175 LONGERON 28R TO LONGERON 29R. INADEQUATE DOUBLER AND FINGER DOUBLERS AND REPLACED IAW SRM 53-2-1 FIG 7. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A CONTROL 5062A. (M)Oct 20, 1998 · N661AV · Doug DC863F · Fuselage Main, Plate/SkinSDR ARWA981035Floorbeam · corrodedLAP - FOUND CORROSION ON FLOORBEAM, UPPER AFT MAIN CARGO COMPARTMENT STATION 600 RBL 33 CUT OUT AREA OF CORROSION. FABRICATED FILLER AND ANGLE AND INSTALLED IAW WITH EO JOSSAIR, CON NR 18R5371011. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B CPCP CONTROL 5090Oct 20, 1998 · N661AV · Doug DC863F · Fuselage Main, Floor BeamSDR ARWA981034Floorbeam · corrodedLAP - FOUND CORROSION ON FLOORBEAM UPPER AFTR FLANGE STATION 160 RBL 25, CUT OUT AREA OF CORROSION. FABRICATED FILLERS AND ANGLES AND INSTALLED IAW EO JOSSAIR, CO NR 18R5371017. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B CONTROL 5081A. (M)Oct 20, 1998 · N661AV · Doug DC863F · Fuselage Main, Floor BeamSDR ARWA981033Floorbeam · corrodedLAP - FOUND CORROSION ON FLOORBEAM MAIN CARGO COMPARTMENT STATION 180, CUT OUT AREA OF CORROSION. FABRICATED FILLERS ANGLE AND INSTALLED IAW EO JOSSAIR, CO NR 18R5371014. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B CPCP CONTROL 5082A. (M)Oct 20, 1998 · N661AV · Doug DC863F · Fuselage Main, Floor BeamSDR ARWA981032Skin · damagedLAP - FOUND PATCH DETERIORATED ON FORWARD DOOR EXTERNAL FUSELAGE. FORWARD CARGO COMPARTMENT STATION 280. REMOVED PATCH AND FABRICATED DOUBLER AND REPLACED IAW SRM 53-2-0. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A CONTROL 5973. (M)Oct 20, 1998 · N661AV · Doug DC863F · Fuselage Main, Plate/SkinSDR ARWA981031Floorbeam · corrodedLAP - FOUND CORROSION ON FLOORBEAM MAIN CARGO COMPARTMENT STATION 140, REMOVED CORROSION SRM 51-1-8. FABRICATED BEAM AND INSTALLED IAW EO JOSS AIR , CO NR 18R5371013 WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B CPCP CONTROL 5080A. (M)Oct 20, 1998 · N661AV · Doug DC863F · Fuselage Main, Floor BeamSDR ARWA981030Floorbeam · corrodedLAP - FOUND CORROSION ON FLOORBEAM FLIGHT COMPARTMENT STATION 55, LBL 29 TO LBL 47, CUT OUT OF CORROSION. FABRICATED BEAM UPPER CHORD AND INSTALLED IAW EO JOSSAIR, CO NR 18R5371001, WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B CPCP CONTROL 4420. (M)Oct 20, 1998 · N661AV · Doug DC863F · Fuselage Main, Floor BeamSDR ARWA981029Floorbeam · corrodedLAP - FOUND CORROSION ON FLOORBEAM UPPER AFTER FLANGE MAIN CABIN STATION 100 RBL 34 CUT OUT AREA OF CORROSION FABRICATED ANGLE AND INSTALLED IAW EO JOSSAIR, CO NR 18R5371016, WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B CPCP CONTROL 5078A. (M)Oct 20, 1998 · N661AV · Doug DC863F · Fuselage Main, Floor BeamSDR ARWA981028Floorbeam · corrodedLAP - FOUND CORROSION ON FLOORBEAM FLIGHT COMPARTMENT STATION 55, RBL 12 TO RBL 29 CUT OUT AREA OF CORROSION. FABRICATED BEAM UPPER CHORD AND INSTALLED IAW EO JOSS AIR NR 18R5371004, WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B CPCP CONTROL 4419. (M)Oct 20, 1998 · N661AV · Doug DC863F · Fuselage Main, Floor BeamSDR ARWA981027Floorbeam · corrodedLAP - FOUND CORROSION ON FLOORBEAM MAIN CARGO COMPARTMENT STATION 80. CUT OUT AREA OF CORROSION, FABRICATED ANGLE AND INSTALLED IAW EO JOSSAIR, CO NR 18R5371002 WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B CPCP CONTROL 5077A. (M)Oct 20, 1998 · N661AV · Doug DC863F · Fuselage Main, Floor BeamSDR ARWA981026Skin · corrodedLAP - FOUND CORROSION ON UPPER SKIN LEFT WING STATION XW 204.125 STRINGER 13 REMOVED CORROSION BEYOND LIMITS. FABRICATED FILLERS AND DOUBLER AND INSTALLED IAW DOUGLAS ROD SKETCH 98-08-04-008 WORK ACCOMPLISHED UNDER ARROW FORM JW3B CPCP CONTROL 1625. (M)Oct 20, 1998 · N661AV · Doug DC863F · Wing, Plate/SkinSDR ARWA981025Skin · corrodedLAP - IMPROPER PATCHES AND CORROSION ON UPPER SKIN LEFT OUTBOARD FLAP STATION XF 213 TO XF 169. REMOVED UPPER SKIN FABRICATED NEW PANEL SKIN AND REPLACED IAW REPAIR INFORMATION JOSSAIR, CO NR 18R5751031 AND SRM 51-3-0 WORK ACCOMPLISHED UNDER ARROW AIR FORM M3Oct 20, 1998 · N661AV · Doug DC863F · Trailing Edge FlapsSDR ARWA981024Web · corrodedLAP - FOUND CORROSION ON TAPERED DOUBLER NLG W/W RIGHT AT STATION 8, CUT OUT AREA OF CORROSION. FABRICATED FILLERS AND DOUBLER AND INSTALLED IAW EO JOSSAIR, CO NR 18R5361009 WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B CPCP CONTROL 4318. (M)Oct 20, 1998 · N661AV · Doug DC863F · Fuselage Miscellaneous StructureSDR ARWA981023Skin · crackedLAP - NR 1 CRACK ON LEADING EDGE RIGHT WING STATION XFS 178 PERFORMED STOP DRILL AND FABRICATED DOUBLER AND INSTALLED IAW EO SEMAN NR 1014 WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A CONTROL 1363. (M)Oct 20, 1998 · N661AV · Doug DC863F · Wing, Plate/SkinSDR ARWA981022Skin · dentedLAP - DENTS, DEFORMATION AND CORROSION ON RT OUTBOARD FLAP T/E LOWER SKIN STATION XRS 367 TO XRS 400. REMOVED LOWER SKIN, FABRICATED NEW SKIN REPLACED IAW REPAIR INFORMATION JOSSAIR, CO NR 18R5751030 AND SRM 51-3-0 WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A COct 20, 1998 · N661AV · Doug DC863F · Trailing Edge FlapsSDR ARWA981021Skin · corrodedLAP - FOUND CORROSION ON L/E UPPER SKIN RIGHT WING CUT OUT AREA OF CORROSION FABRICATED DOUBLER AND INSTALLED IAW EO JOSSAIR, CO NR 18R5781019 WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B CPCP CONTROL 1703. (M)Oct 20, 1998 · N661AV · Doug DC863F · Wing, Plate/SkinSDR ARWA981020Skin · corrodedLAP - FOUND CORROSION ON RIGHT WING TOP AT STATION XFS 175 CUT OUT AREA OF CORROSION FABRICATED DOUBLER, FILLER AND INSTALLED IAW EO SEMAN NR 1028. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A CONTROL 1702. (M)Oct 20, 1998 · N661AV · Doug DC863F · Wing, Plate/SkinSDR CKSA98542Air Distr · odorDURING CLIMB-OUT, EXPERIENCED BAD SMELL IN THE COCKPIT. RAN NASI SYSTEM THROUGH ALL SETTINGS AND VISUALLY CHECKED INSTALLATION OF SYSTEM. NO DEFECTS NOTED.Sep 29, 1998 · N811CK · Doug DC863F · Air Distribution SystemSDR IXXA9800069Retract Mech · out of adjustAFTER TAKEOFF WHEN THE LANDING GEAR WAS RETRACTED, THE FLIGHT CREW NOTICED A NOISE AND VIBRATION COMING FROM THE NOSE WHEEL WELL AREA. THE CREW CYCLED THE GEAR BUT THE VIBRATION CONDITION WAS STILL PRESENT. THE AIRCRAFT RETURNED TO TOL FOR AN UNEVENTFUL LANDSep 2, 1998 · N867BX · Doug DC863F · Landing Gear Door Retract SectionSDR ARWA980813Heat · inoperativeSJU - FLT 759 - GROUND TURN BACK, F/O'S PITOT HEAT INOP. REMOVED AND REPLACED PITOT TUBE ASSY. OPS NORMAL IAW MM 30-30-0. SATISFACTORY LEAK CHECK IAW MM 34-12-0. (M)Aug 26, 1998 · N441J · Doug DC863F · Pitot/Static Anti-Ice SystemSDR IXXA9800065Mechanism · misriggedAFTER TAKEOFF, WHEN THE FLIGHT CREW RETRACTED THE LANDING GEAR, THE CONTROL HANDLE WOULD NOT POSITION TO THE UP POSITION. THE CREW RETURNED THE GEAR HANDLE TO THE DOWN POSITION, RECEIVING THREE DOWN AND LOCK INDICATIONS. A SECOND ATTEMPT TO RETRACT THE GEAR Aug 12, 1998 · N867BX · Doug DC863F · Landing Gear Retraction/Extension SystemSDR IXXA9800108Plating · damagedDURING ROUTINE C CHECK INSPECTION, HEAT STRESS WAS DETECTED ON NUMBER THREE PYLON INBOARD AND OUTBOARD PLANK PLATING. REPAIR ACCOMPLISHED REMOVAL OF AFFECTED AREAS, FABRICATION AND INSTALLATION OF NEW PLANK PLATINGS IN ACCORDANCE WITH DOUGLAS DRAWING 5753265 Aug 6, 1998 · N786AL · Doug DC863F · Nacelle/Pylon, Plate/SkinSDR CKSA98493Fire Loop · out of adjustENGINE FIRE INDICATION NR 1, BOTTLE NR 1 DISCHARGED, HANDLE LIGHT REMAINED ILLUMINATED, BOTTLE NR 2 DISCHARGED, LIGHT REMAINED ILLUMINATED, ON POST FLIGHT, NO VISABLE INDICATION OF FIRE. REMOVED AND REPLACED NR 1 ENGINE FIRE LOOP AS PER MM 26-10-1 GROUND GOODJul 30, 1998 · N815CK · Doug DC863F · Fire DetectionSDR RRXA98270Wheel · broke offON LANDING, THE NR 1 MLG WHEEL AND TIRE ASSEMBLY BROKE FROM AXLE. TIRE ASSEMBLY ROLLED INTO PARKED EQUIPMENT. AIRCRACFT WAS TOWED TO RAMP FOR INSPECTION. *S/D* REMOVED AND REPLACED NR 1 MAIN WHEEL AND TIRE ASSEMBLY, REPLACED NR 1 MAIN BRAKE ASSEMBLY, REPLAJul 20, 1998 · N921R · Doug DC863F · Wheel/Ski/FloatSDR ARWA9807128Buss Panel · failedWHILE PERFORMING PRE-FLIGHT, COCKPIT FILLED WITH SMOKE. POWER SHUT DOWN, PROBLEM FOUND TO BE, SHORTED BUSS PROTECTION PANEL AND ASSOCIATED WIRING. REMOVED AND REPLACED BUSS PROTECTION PANEL AND BURNT WIRING SYSTEM; TESTED IAW MM 24-20-7. FOUND NOTE: SWISPORJul 17, 1998 · N441J · Doug DC863F · AC Power Distribution SystemSDR CKSA98505Switch · not securedAFTER TAKEOFF FROM MIA, LANDING GEAR FAILED UPLATCH CHECK. MX NOTE: COMPLETED UPLATCH CHECK LIST AND FOUND WHEN LOWERING LANDING GEAR RIGHT MAIN GEAR GREEN LIGHT INTERMITTENTLY ON. TROUBLESHOT AND FOUND RT MAIN GEAR DOOR SWITCH NOT SECURED. SECURED DOOR SWIJul 12, 1998 · N811CK · Doug DC863F · Landing Gear Position and WarningSDR IXXA9800105Mount · chafedDURING ROUTINE C CHECK INSPECTION, CHAFING WAS DETECTED ON NUMBER THREE PYLON FORWARD ENGINE MOUNT. REPAIR BLENDS AFFECTED AREA AND DETERMINES THAT THE WEAR IS ACCEPTABLE FOR STRENGTH IN ACCORDANCE WITH DOUGLAS FAX ACTION NUMBER 374208 AND ENGINEERING ORDER 7Jul 10, 1998 · N786AL · Doug DC863F · Engine Mount SectionSDR IXXA9800095Bulkhead Fitting · crackedDURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED ON AFT PRESSURE BULKHEAD LOWER SUPPORT FITTING AT FUSELAGE STATION 1744, LONGERON 36. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED FITTING, FABRICATION AND INSTALLATION A NEW FITTING IN ACCORDANCE WITH DOUGLASJul 9, 1998 · N867BX · Doug DC863F · Fuselage Main, BulkheadSDR 98ZZZX2958Spar Cap · crackedFOUND LT WING INBD LOWER AUXILIARY SPAR CAP CRACKED ON VERTICAL FLANGE AT XRS22. SUSPECT CAUSE OF THE CRACK WAS VIBRATION.Jul 9, 1998 · N867BX · Doug DC863F · Wing SparSDR 98ZZZX2957Plank · crackedPYLON PLANK HAS CRACK LOCATED AT 19.5 INCHES AFT FROM YN190. SUSPECT CAUSE OF THE CRACK WAS VIBRATION.Jul 9, 1998 · N867BX · Doug DC863F · Nacelle/Pylon StructureSDR 98ZZZX2956Plank · crackedPYLON PLANK CRACK LOCATED AT YN226. SUSPECT CAUSE OF THE CRACK IS VIBRATION.Jul 9, 1998 · N867BX · Doug DC863F · Nacelle/Pylon StructureSDR ABXA9800614Switch · defectiveON DEPARTURE, DURING GEAR UPLATCH CHECK, GEAR UNSAFE LIGHT ILLUMINATED. PERFORMED ALTERNATE UPLATCH CHECK AND CONFIRMED TO BE LEFT MAIN GEAR UPLATCH. RECYCLED GEAR, SAME RESULTS. REPLACED LEFT MAIN LANDING GEAR UPLATCH SWITCH IAW DC8 MM 32-60-00. OPS CHECKJul 8, 1998 · N815AX · Doug DC863F · Landing Gear Position and WarningSDR IXXA9800059Wire · chafedEN ROUTE MGUM TO KFLL, THE GEAR UPLATCH CHECK FAILED WITH THE GEAR NOT LATCHED WARNING LIGHT ILLUMINATED. THE CREW CYCLED THE GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TO KFLL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED TJun 24, 1998 · N906R · Doug DC863F · Landing Gear System WiringSDR IXXA9800094Plating · corrodedDURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON LOWER FUSELAGE EXTERNAL PLATING FROM FUSELAGE STATIONS 1752 AND 1766, BETWEEN LONGERONS 35 LEFT AND 35 RIGHT. REPAIR ACCOMPLISHED CORROSION REMOVAL IN ACCORDANCE WITH DOUGLAS FAX ACTION NUMBER 37266Jun 16, 1998 · N867BX · Doug DC863F · Fuselage Main, Plate/SkinSDR IXXA9800090Angle · corrodedDURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED BETWEEN FUSELAGE STATION 380 AND 400, LONGERON 27 LEFT. REPAIR ACCOMPLISHED REMOVAL OF CORRODED ANGLE, FABRICATION AND INSTALLATION A NEW LONGERON ANGLE IN ACCORDANCE WITH FAA DER APPROVED DRAWING COO-Jun 11, 1998 · N867BX · Doug DC863F · Fuselage Miscellaneous StructureSDR IXXA9800071Frame · corrodedDURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON THE FUSELAGE FRAME AT FUSELAGE STATION 70, BETWEEN LONGERON 32 AND 34 RIGHT. REPAIR ACCOMPLISHED CORROSION REMOVAL, FABRICATION AND INSTALLATION AN INTERNAL REPAIR ANGLE IN ACCORDANCE WITH THE DOUGLJun 10, 1998 · N867BX · Doug DC863F · Fuselage Main, FrameSDR IXXA9800092Doubler · corrodedDURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON CENTER WING UPPER JOINT DOUBLER AT FUSELAGE STATION 816, STRINGER 6. REPAIR ACCOMPLISHED BLENDED OUT CORROSION IN ACCORDANCE WITH FAA DER APPROVED DRAWINGS, COO-SJO-98-0393DDAC, COO-SJO-98-0394DAC, Jun 8, 1998 · N867BX · Doug DC863F · Wing Miscellaneous StructureSDR ABXA9800498Angle · crackedRIGHT WING INBOARD SLOT BOX, OUTBOARD AFT VERTICAL ANGLE IS CRACKED AT THE BOTTOM. REPAIRED IAW DC8 SRM 51-1-20D.Jun 6, 1998 · N819AX · Doug DC863F · Wing Miscellaneous Structure
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