Douglas DC-8-62F

Service difficulty reports · 1,163

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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 = 'DC862F'
  ORDER BY difficulty_date DESC"

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SDR IXXA9800001Socket · shortedEN ROUTE, A BURNT ODOR WAS SENSED WHEN THE COCKPIT WHITE LIGHTING WAS TURNED ON. THE COCKPIT LIGHTING WAS TURNED OFF FOR THE REMAINDER OF THE FLIGHT. MAINTENANCE INVESTIGATED AND FOUND A GLARESHIELD FLUORESCENT LIGHT SOCKET SHORTED. MAINTENANCE DEACTIVATED Jan 4, 1998 · N41CX · Doug DC862F · Flight Compartment LightingSDR RRXA97323Prox Sensor · dirtyNOSE GEAR GREEN LIGHTS WENT OUT AT 200 FEET AURAL WARNING CAME ON, INITIATED GO AROUND, GEAR LIGHTS CAME BACK ON. ALL SYSTEM CHECKED NORMAL, LANDED. INSPECTED NOSE GEAR DOWN LOCK ASSY CLEANED AND ADJUSTED DOWN AND LOCKED PROX SENSOR IAW 32-20.Dec 19, 1997 · N996CF · Doug DC862F · Landing Gear Position and WarningSDR IXXA9700169Fan · failedEN ROUTE, A BURNT ODOR WAS SENSED IN THE COCKPIT WITH THE LEFT RECIRCULATION FAN OPERATING. THE FAN WAS SHUT OFF FOR THE REMAINDER OF THE FLIGHT. MAINTENANCE FOUND THE FAN DEFECTIVE. MAINTENANCE DEFERRED THE LEFT RECIRCULATION FAN.Dec 19, 1997 · N41CX · Doug DC862F · Air Distribution FanSDR RRXA97253Switch Wire · frayedAPPROACH AT KDAY WAS MISSED, DID NOT HAVE LIGHT INDICATION FOR LEFT MAIN LANDING GEAR DOWN LOCK. CREW TRIED RE-CYCLING GEAR AGAIN NO LIGHT INDICATION. CREW NOTIFIED KDAY FOR FLY-BY FOR LEFT MAIN LANDING GEAR IN DOWN POSITION. CREW WAS GIVEN APPROVAL TO LANSep 3, 1997 · N998CF · Doug DC862F · Landing Gear Position and WarningSDR TC8A97045Power Lever · lack of lubeUPON START OF TAXI OUT, UNABLE TO MOVE NR 1 THROTTLE FOWARD OF IDLE. SHUT DOWN ENGINE, POWER LEVER BINDING. LUBRICATED POWER CONTROL DRUM IN NR 1 PYLON. CHECKED PYLON CABLES AND COCKPIT MECHANISM AND CABLES FOR DEBRIS, NO DISCREPANCIES NOTED. AFTER LUBE, NAug 28, 1997 · N183SK · Doug DC862F · Power LeverSDR TC8A97044Microwave · failedWHEN OPERATING MICROWAVE, SMOKE CAME FROM UNIT, SMELL OF MELTING WIRES. PULLED ALL CIRCUIT BREAKERS, SMELL AND SMOKE STOPPED. REMOVED MICROWAVE OVEN.Aug 22, 1997 · N183SK · Doug DC862F · Buffet/GalleysSDR TC8A97037Release Trigger · lack of lubeKMIA - AFTER TAKEOFF AND GEAR RETRACTION, EXCESSIVE VIBRATION AND NOISE IN NOSE SECTION. RECYCLED GEAR, SAME CONDITIONS AS ABOVE. DUMPED FUEL FOR 3 MIN TO SATISFY LANDING WEIGHT, NORMAL LANDING AND TAXI. FOUND RT NOSE GEAR DOOR OPENED. FOUND RELEASE TRIGGERJul 25, 1997 · N183SK · Doug DC862F · Landing Gear Door Retract SectionSDR RRXA97194Oil Press Sw · failedDURING DESCENT, NR 2 ENGINE OIL PRESSURE LIGHT CAME ON. OIL PRESSURE WAS 36 PSI, OIL QUANTITY AND TEMP WERE NORMAL. SHUT DOWN ENGINE IAW QRH. REMOVED AND REPLACED NR 2 ENGINE LOW OIL PRESSURE WARNING SWITCH. OPS AND LEAK CHECK OK PER MM 79-32-2.Jul 4, 1997 · N996CF · Doug DC862F · Engine Oil PressureSDR IXXA9700121Panel · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS FOUND ON THE LEFT HORIZONTAL STABILIZER UPPER PANEL, INNER BEADED SKIN BETWEEN STATION XE150 TO 250. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF AN INTERNAL FILLER AND AN INTERJun 6, 1997 · N41CX · Doug DC862F · Horizontal Stabilizer, Plate/SkinSDR IXXA9700122Slot Door · crackedDURING ROUTINE C-CHECK INSPECTION, TWO CRACKS WERE FOUND ON THE RIGHT WING INBOARD LEADING EDGE SLOT DOOR. REPAIR ACCOMPLISHED STOP DRILLING THE ENDS OF THE CRACKS, FABRICATION AND INSTALLATION OF AN EXTERNAL REPAIR DOUBLER IN ACCORDANCE WITH DER APPROVED DRAMay 27, 1997 · N41CX · Doug DC862F · Wing Miscellaneous StructureSDR IXXA9700129Plating · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND ON THE EXTERNAL PLATING AT FUSELAGE STATION 1730, LONGERON 36. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR FILLER AND AN EXTERNAL REPAIR DOUBLER IN ACCORDANCE WITH May 21, 1997 · N41CX · Doug DC862F · Fuselage Main, Plate/SkinSDR IXXA9700128Plating · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND ON THE EXTERNAL PLATING JUST FORWARD OF OUTFLOW VALVE OPENING AT FUSELAGE STATION 1500, BETWEEN LONGERON 35 AND 36 LEFT. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF AN EXTERMay 20, 1997 · N41CX · Doug DC862F · Fuselage Main, Plate/SkinSDR IXXA9700130Plating · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS FOUND ON THE EXTERNAL PLATING AT FUSELAGE STATION 185, LONGERON 31 LEFT. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF AN INTERNAL FILLER AND AN EXTERNAL REPAIR DOUBLER IN ACCORDAMay 15, 1997 · N41CX · Doug DC862F · Fuselage Main, Plate/SkinSDR IXXA9700127Plating · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS FOUND ON THE LEFT WING LOWER LEADING EDGE AT STATION XFS 710. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR FILLER AND AN EXTERNAL REPAIR DOUBLER IN ACCORDANCE WITH DER AMay 14, 1997 · N41CX · Doug DC862F · Wing, Plate/SkinSDR IXXA9700126Beam · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS FOUND ON THE FLOOR SUPPORT BEAM AT RIGHT BUTT LINE 45.0, AT FUSELAGE STATION 1440. REPAIR ACCOMPLISHED CORROSION REMOVAL, FABRICATION AND INSTALLATION OF TWO REPAIR DOUBLERS IN ACCORDANCE WITH DER APPROVED SKETMay 13, 1997 · N41CX · Doug DC862F · Fuselage Miscellaneous StructureSDR IXXA9700125Plating · crackedDURING ROUTINE C-CHECK INSPECTION, THE LOWER FORWARD CORNER OF LEFT AFT PASSENGER ENTRY DOOR WAS FOUND TO BE CRACKED AT FUSELAGE STATION 1460. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF AN INTERNAL FILLER AND AN EXTERNAL REPAMay 12, 1997 · N41CX · Doug DC862F · Fuselage Main, Plate/SkinSDR IXXA9700124Plating · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS FOUND ON THE EXTERNAL PLATING AT FUSELAGE STATION 211, LONGERON 28 RIGHT. REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED AREAS, FABRICATION AND INSTALLATION OF INTERNAL FILLERS AND AN EXTERNAL REPAIR DOUBLER IN ACCMay 12, 1997 · N41CX · Doug DC862F · Fuselage Main, Plate/SkinSDR IXXA9700123Plating · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND PROTRUDING TO A RIVET HOLE FROM STATION 1530, LONGERON 31 RIGHT. REPAIR ACCOMPLISHED VERIFICATION THAT THE CRACK DID NOT PROGRESS PASS RIVET HOLE, FABRICATION AND INSTALLATION OF AN EXTERNAL REPAIR DOUBLER May 12, 1997 · N41CX · Doug DC862F · Fuselage Main, Plate/SkinSDR IXXA9700131Pressure Panel · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND ON THE RIGHT LOWER PRESSURE WEB PANEL AT FUSELAGE STATION 680. REPAIR ACCOMPLISHED REMOVAL AND INSTALLATION OF A NEW WEB PANEL IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY SRM 53-1-0, 51-1-20D, AND 51-1-21.May 8, 1997 · N41CX · Doug DC862F · Fuselage Miscellaneous StructureSDR IXXA9700132Attach Fitting · crackedDURING ROUTINE C-CHECK INSPECTION, THE NR 3 PYLON FOOTSTOOL FITTING WAS FOUND TO BE CRACKED. THE FITTING WAS REMOVED AND REPLACED IN ACCORDANCE WITH THE DOUGLAS STRUCTURE REPAIR MANUAL 51-3-0, 51-1-20D AND 51-1-21.May 6, 1997 · N41CX · Doug DC862F · Nacelle/Pylon, Attach FittingsSDR TC8A97022Vertical Gyro · failedCAPTAINS ADI DURING ROTATION AND INITIAL CLIMB SHOWED ABNORMAL INDICATION GOING THROUGH 16,000. CAPTAINS ADI GYRO FLAGS ERRECTED, RESET BREAKER AND AFTER 1 MINUTE, ADI GYRO FLAG CAME ON AGAIN. RETURN TO KMIA, NORMAL LANDING. REMOVED AND REPLACED NR 1 VERTICApr 29, 1997 · N183SK · Doug DC862F · Attitude Gyro and Indicating SystemSDR IXXA9700041Fan · failedIN FLIGHT, WHEN THE LEFT HAND RECIRCULATION FAN WAS TURNED ON, A BURNING ODOR WAS VERY NOTICEABLE, THE FAN WAS TURNED OFF FOR THE REMAINDER OF THE FLIGHT. AFTER AN UNEVENTFUL LANDING, MAINTENANCE DEFERRED THE FAN AND THE AIRCRAFT WAS RETURNED TO SERVICE.Apr 15, 1997 · N41CX · Doug DC862F · Air Distribution FanSDR TC8A97019Dc Buss · smokingSVMI-KMIA, FLT 00091 - DISCREPANCY: AT TOP OF DESCENT, ELECTRICAL SMOKE OF UNKNOWN ORIGIN, PROCEED AS GOM-8. ISOLATE DC BUS, NR 1 GENERATOR AND NR 4 GENERATOR TO STOP SMOKE.Apr 2, 1997 · N183SK · Doug DC862F · DC Power Distribution SystemSDR RRXA97070Uplatch Switch · broken wireAT 0840 HOURS, EASTERN TIME, AIRCRAFT COMPLETED TAKEOFF. DURING ASCENT, LANDING GEAR RETRACTION GEAR NOT LATCH LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. PERFORMED UPLATCH CHECK AND NOSE GEAR FAILED CHECK. RECYCLED GEAR WITH NO CHANGE. PILOT RADIO FMar 4, 1997 · N996CF · Doug DC862F · Landing Gear Position and WarningSDR IXXA9700027Water Heater · failedDURING DESCENT, THE FLIGHT ATTENDANT REPORTED VIA INTERPHONE TO COCKPIT, THAT THE RIGHT AFT LAVATORY SMOKE DETECTOR WAS SOUNDING AND A SMELL OF SMOKE. THE FLIGHT ENGINEER WAS DISPATCHED TO INVESTIGATE. THE FLIGHT ATTENDANT DISCHARGED A PORTABLE FIRE EXTINGUIMar 1, 1997 · N41CX · Doug DC862F · Wash Water SystemSDR TC8A97015Connector · failedNR 1 ENGINE PRECAUTIONARY SHUTDOWN DUE TO HIGH ENGINE OIL TEMP, HIGH ENGINE OIL PRESSURE AND ERRATIC N2, CHECKLIST COMPLETED. REPAIRED WIRING AND CHANGED CANNON PLUG AT OIL TEMP-OIL PRESSURE AND N2 INDICATOR. NR 1 ENGINE CHECKED RUN-UP NORMAL IAW 77-0-0.Feb 15, 1997 · N183SK · Doug DC862F · Engine Oil TemperatureSDR TC8A97012Valve Relief · failedUNABLE TO PRESSURIZE ACFT DURING CLIMB. REMOVED AND REPLACED SAFETY RELIEF VALVE, SYSTEM OPS CHECKS NORMAL ON RUN-UP MM 21-30-2.Feb 8, 1997 · N183SK · Doug DC862F · Cabin Pressure Control SystemSDR TC8A97011Engine · out of trimKMIA, FLT 03603. ABORTED TAKEOFF NR 3 ENGINE. WILL NOT REACH MAX POWER OF 1.87. PERFORMED ENGINE TRIM RUN ON ALL FOUR ENGINES, TRIMMED ALL FOUR ENGINES, OPS CHECKED GOOD IN ALL THROTTLE SETTINGS I/A/W TCA DC-8 MIP, CHAPTER 2, PAGES 96-104.Feb 5, 1997 · N183SK · Doug DC862F · Fuel Controlling SystemSDR TC8A97010Engine · out of trimKMIA, FLT 03603. ABORTED TAKEOFF. NR 2 ENGINE WILL NOT REACH MAX POWER OF 1.87. PERFORMED ENGINE TRIM RUN ON ALL FOUR ENGINES, TRIMMED ALL FOUR ENGINES, OPS CHECKED GOOD IN ALL THROTTLE SETTINGS I/A/W TCA DC-8 MIP, CHAPTER 2, PAGES 96-104.Feb 5, 1997 · N183SK · Doug DC862F · Fuel Controlling SystemSDR TC8A97006Engine · out of trimNR 1 AND 4 ENGINES NOT PRODUCING TAKEOFF POWER. POWER LEVERS AGAINST STOP, NR 1 EPR 1.64, NR 4 EPR 1.60. TRIMMED NR 1 AND NR 4 ENGINES. NR 1 AND NR 4 OPS NORMAL ON RUN-UP, M/M JT3D-7.Jan 16, 1997 · N183SK · Doug DC862F · Fuel Controlling SystemSDR TC8A96071Indication · malfunctionedKOAK TO KIND - FLT 35404 - DISCREPANCY: CYCLED LANDING GEAR IN-FLIGHT DUE TO UNSAFE WARNING, AFTER RECYCLED, ALL INDICATIONS NORMAL. CORRECTIVE ACTION: INSPECTED DOWNLOCK WARNING TRIGGERING MECHANISM ON SWITCHES ASSY. FREED SPRING IAW MM 32-60-0, SYSTEMDec 19, 1996 · N183SK · Doug DC862F · Landing Gear Position and WarningSDR RRXA96171O-Ring · failedHYDRAULIC LOW LIGHT CAME ON AFTER TAKEOFF WITH A LOSS OF HYDRAULIC QUANTITY. REPLACED O-RING AT NR 2 ENGINE THRUST REVERSER, CHECK VALVE IN PYLON AND LEAK CHECKS GOOD.Dec 13, 1996 · N996CF · Doug DC862F · Engine Thrust ReverserSDR RRXA96167Turbo Comp · failedNR 2 TURBO COMPRESSOR HAD LOUD GRINDING NOISE AND SENT BURNING ODOR INTO COCKPIT. MAINTENANCE REMOVED AND REPLACED NR 2 TC, OPERATIONAL CHECK OF THE TC SYSTEM WAS GOOD.Nov 27, 1996 · N996CF · Doug DC862F · Cabin Compressor SystemSDR TC8A96067Connector · looseNR 2 COMPASS OFF FLAG APPEARED ON TAXI OUT. CLEANED AND RESECURED CANNON PLUG AT CAPTAINS RADIO MAGNETIC DIRECTION INDICATOR, SYSTEM OPS CHECKS GOOD.Nov 14, 1996 · N183SK · Doug DC862F · Visual Omnirange (VOR) SystemSDR RRXA96124Generation Syst · malfunctionedDURING CRUISE, NR 2 GENERATOR LOCKED OUT. BUS RESET, VOLTS AND FREQS NORMAL, GEN RELAY OPEN, LT EMERGENCY BUS POWER FAILURE LIGHT ILLUM AND LOST ASSOCIATED BUS. 996CF DIVERTED TO KORD. *S/D* MAINTENANCE TRANSFERED THE NR 2 GEN TO THE DMI LIST. NR 2 BUS OPOct 18, 1996 · N996CF · Doug DC862F · AC Generation SystemSDR RRXA96118Bulkhead · holeWHILE PREFORMING CONSTANT SECTION INSPECTION FOUND A 3 INCH HOLE IN AFT PRESSURE BULKHEAD WEB AT Y=1606 RT. REPAIRED BY DOUBLER REPAIR IAW DALFORT AVIATION EXPEDITE ENGINEERING AUTHORIZATION XEA: X8-53-866.Oct 11, 1996 · N996CF · Doug DC862F · Fuselage Main, BulkheadSDR TC8A96060R1Bulkhead Web · damagedKOSC - COMPLIED WITH AD 90-16-05 AFT PRESSURE BULKHEAD WEB MODIFICATION. REPAIRED AFT PRESSURE BULKHEAD WEB IAW SB 53-53. REF DAC FAX FILE NR GLP1813/96-07-23-010. TASK CARD NR 79494. REPORT GENERATED BY AMERICAN INTERNATIONAL AIRWAYS, INC. (B4MR) FOR TRANSep 24, 1996 · N183SK · Doug DC862F · Fuselage Main, BulkheadSDR TC8A96060Bulkhead Web · damagedCOMPLIED WITH AD 90-16-05 AFT PRESSURE BULKHEAD WEB MODIFICATION. REPAIRED AFT PRESSURE BULKHEAD WEB IAW SB 53-53 REF DAC FAX FILE NR GLP1813/96-07-23-010. TASK CARD NR 79494. REPORT GENERATED BY AMERICAN INTERNATIONAL AIRWAYS, INC B4MR FOR TRANS CONTINENTISep 24, 1996 · N183SK · Doug DC862F · Fuselage Main, BulkheadSDR TC8A96059R1Longeron · crackedKOSC - DURING BASE MODIFICATION FOUND: LONGERON SPLICE CRACKED AT LONGERON 31 LEFT HAND BETWEEN STA 600-620 (CRACK .25 INCH). REMOVED AND REPLACED LONGERON SPLICE IAW DC8 SRM 51-1-20D AND 51-1-8. TASK CARD NR 81712. REPORT GENERATED BY AMERICAN INTERNATIONSep 24, 1996 · N183SK · Doug DC862F · Fuselage Main, Longeron/StringerSDR TC8A96059Longeron · crackedDURING BASE MODIFICATION, FOUND LONGERON SPLICE CRACKED AT LONGERON 31 LEFT HAND BETWEEN STA 600 TO 620 CRACKED .25 INCH. REMOVED AND REPLACED LONGERON SPLICE IAW DC8 SRM 51-1-20D AND 51-1-8. TASK CARD NR 81712. REPORT GENERATED BY AMERICAN INTERNATIONAL AISep 24, 1996 · N183SK · Doug DC862F · Fuselage Main, Longeron/StringerSDR IXXA96105Fire Detect Amp · malfunctionedEN ROUTE QPG TO OKO, THE NR 3 ENGINE FIRE WARNING LIGHTS ILLUMINATED. CREW SHUT THE ENGINE DOWN AND SEQUENCED THE FIRE BOTTLE FOR THAT ENGINE ON A PRECAUTIONARY BASIS. AIRCRAFT RETURNED QPG WITH AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE ENGINE FOR EVJul 6, 1996 · N41CX · Doug DC862F · Fire DetectionSDR CKSA96049Stiffener · chafedKOSC - FLT 72016 - DURING 'C-1' CHECK INSPECTION FOUND, TASK NR 61961 RUDDER, STIFFENER CHAFED AT TOP OF NR 2 HINGE CUT-OUT. REPAIRED CHAFED STIFFENER PER AIA SKETCH AIA/E/2315 AND 8110-3. (X)May 2, 1996 · N3931A · Doug DC862F · Rudder StructureSDR CKSA96048Skin · corrodedKOSC - FLT 72016 - DURING 'C-1' CHECK INSPECTION FOUND TASK NR 59699 FS 490 L35R, BULGE IN SKIN. REMOVED FASTENERS AND CUT OUT CORROSION. REPAIRED IAW SKETCH NR A1A/3/2180 PER 8110-3. (X)May 2, 1996 · N3931A · Doug DC862F · Fuselage Main, Plate/SkinSDR CKSA96047Fillet Panel · delaminatedDOSC - FLT 72016 - DURING 'C-1' CHECK INSPECTION FOUND, TASK NR 59644 PANEL 262F DELAMINATION. FABRICATED NEW PANEL IAW AIA SKETCH AIA/E/2188 AND INSTALLED. (X)May 2, 1996 · N3931A · Doug DC862F · Aerodynamic FairingsSDR CKSA96046Angle · corrodedKOSC - FLT 72016 - DURING 'C-1' CHECK INSPECTION FOUND, CARD NR 6000-0551 AREA, AFT FUSELAGE/VERTICAL STABILIZER. VERTICAL STABILIZER TO FUSELAGE ATTACH LEVEL 2 TASK NR 74798. REPAIRED VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE IAW DC-8 SRM 53-2-5, FIGURE May 2, 1996 · N3931A · Doug DC862F · Vertical StabilizerSDR CKSA96045Angle · corrodedDURING 'C-1' CHECK INSPECTION FOUND, CARD NR 6000-0551 AREA, AFT FUSELAGE/VERTICAL STABILIZER. VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE RIGHT SIDE HAS STRESS CRACKS AND CORROSION. LEVEL 2 TASK NR 74799. CLEANED CORROSION AND FOUND TO BE OUT OF LIMITS. May 2, 1996 · N3931A · Doug DC862F · Vertical StabilizerSDR CKSA96044Skin · corrodedKOSC - FLT 72016 - DURING 'C-1' CHECK INSPECTION FOUND, CARD NR 6000-0551 AREA, AFT FUSELAGE/VERTICAL STABILIZER SKIN SEPARATING AND CORRODED, VERTICAL STABILIZER RIGHT SIDE APPROXIMATELY STA XR284 TO XR230 AFT SPAR AREA. LEVEL 2 TASK NR 61999. REPLACED UPPEMay 2, 1996 · N3931A · Doug DC862F · Vertical Stabilizer, Plate/SkinSDR CKSA96043Skin · corrodedKOSC - FLT 72016 - DURING 'C-1' CHECK INSPECTION FOUND, CARD NR 6000-0551 AREA, AFT FUSELAGE/VERTICAL STABILIZER, VERTICAL STABILIZER SKIN LEFT SIDE APPROXIMATELY STA XR230 TO XR310 AFT SPAR AREA CORRODED AND SEPARATING. LEVEL 2 TASK NR 61998. RESEALED BONDEMay 2, 1996 · N3931A · Doug DC862F · Vertical Stabilizer, Plate/SkinSDR CKSA96042Floor Plank · corrodedKOSC - FLT 72016 - DURING 'C-1' CHECK INSPECTION FOUND, CARD NR 5670-0551 AREA, GALLEY (ANY LOCATION) FS 255 LBL 29 FLOOR PLANK CORRODED. LEVEL 2 TASK NR 61940. REMOVED CORROSION, TREATED AND PRIMED AS IT REQUIRED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-8 ANDMay 2, 1996 · N3931A · Doug DC862F · Fuselage Floor PanelSDR CKSA96041Floor Plank · corrodedKOSC - FLT 72016 - DURING 'C-1' CHECK INSPECTION FOUND, CARD NR 5670-0551 AREA, GALLEY (ANY LOCATION) FS 255 LBL FLOOR PLANK CORROSION LEVEL 2 TASK NR 61938. REMOVED CORROSION, TREATED AND PRIMED AS IT REQUIRED PER IAW DC-8 SRM 51-1-8, AND INSTALLED REPAIR ACMay 2, 1996 · N3931A · Doug DC862F · Fuselage Floor Panel
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