Douglas DC-8-71F

Service difficulty reports · 8,938

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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 = 'DC871F'
  ORDER BY difficulty_date DESC"

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SDR UPS02838561Fitting · crackedINSPECTION TYPE:C1 LT WW FITTING AT STA 880 L4L HAS CORROSION. REMOVED FITTING, CUT NEW FITTING AND FABRICATED SPLICE PARTS IAW DC8 SRM 53-2-0 FIG 8. INSTALLED FITTING IAW DC8 SRM 53-2-0 FIG 8 AND DC8 SRM 51-1-20D.May 10, 2002 · N700UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02838569Skin · damagedINSPECTION TYPE:C1 FUSELAGE SKIN BLENDOUT AT BS 550 RIGHT HAND SIDE ABOVE CARGO COMP DOOR EO DC8-5330-15732A, REPAIR AT C-CHECK. FABBED REPAIR DOUBLERS IAW DC8 SRM 53-2-0 FIG 20. INSTALLED REPAIR DOUBLER IAW DC8 SRM 53-2-0 FIG 20.May 9, 2002 · N700UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02838183Battery Pack · dischargedINSPECTION TYPE:PFLT EMERGENCY EXIT LIGHT INOP. REPLACED EMERGENCY BATTERY PACK, CHECKED WORKED OK.May 9, 2002 · N744UP · Doug DC871F · Emergency LightingSDR IXXA0200040SStructure · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE LOWER SECTION AFT OF THE NOSE WHEEL WELL STATION 16 AND LONGERON 35R. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF EXTERNAL DOUBLER IN ACCORDANCE WITH DOUGLAS STRUCMay 8, 2002 · N830BX · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02838113Engine · flamed outINSPECTION TYPE:N/A NR 1 ENGINE FLAMED OUT DURING CLIMB THROUGH 210 ENGINE ANTI-ICE WAS ON LIGHT TURBULENCE COMPLETED FLAME-OUT CHECKLIST. SUCCESSFUL RESTART AT 6 T/S IAW MM 71-00-00 ALL PROCEDURES PERFORMED BY PHL MX, SECURED CDP PS 3 LINE AT THE MED. REPLMay 2, 2002 · N709UP · Doug DC871F · Engine (Turbine/Turboprop)SDR UPS02838100Connector · not seatedINSPECTION TYPE:N/A DURING PREFLIGHT FOUND EMERGENCY LIGHT DISARM ARM SWITCH LIGHT DID NOT WORK. FOUND CONNECTOR P1-1344 AT DIMMING BOX B5-60 NOT FULLY SEATED. SEATED CONNECTOR P1-1344 LIGHT OPS CK NORMAL REF WDM 33-50-01.Apr 30, 2002 · N744UP · Doug DC871F · Emergency LightingSDR UPS02838099Wire · brokenINSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS REMAINED ON AFTER SWITCHING TO SHIPS POWER. REPAIRED BROKEN WIRE AT EMERGENCY BATTERY PACK CANNON PLUG, OPS CHECK GOOD PER MM 33-50-02.Apr 26, 2002 · N703UP · Doug DC871F · Light System WiringSDR UPS02838092Connector · burnedINSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS REMAINED ON. FOUND BURNT CONTACTS ON CANNON PLUGS. AIRCRAFT 779 COVERED FLIGHT PARTS ON ORDER.Apr 26, 2002 · N703UP · Doug DC871F · Emergency LightingSDR IXXA0200039SDoor · misdrilledDURING ROUTINE C-CHECK INSPECTION, MISDRILLED HOLES WERE DETECTED IN THE RIGHT HAND AFT SERVICE DOOR JAMB LOWER EDGE EXTERNAL SKIN FROM FUSELAGE STATION 1636 TO STATION 1648. REPAIR ACCOMPLISHED REMOVAL OF DEFECTIVE DOUBLER, FABRICATION AND INSTALLATION OF NEApr 23, 2002 · N830BX · Doug DC871F · Service DoorsSDR IXXA0200038SDoor · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DISCOVERED ON THE LEFT HAND PASSENGER DOOR CUT OUT LOWER CORNER. REPAIR ACCOMPLISHED DAMAGED AREA CUT OUT, FABRICATION AND INSTALLATION OF FILLER AND REPAIR DOUBLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIApr 21, 2002 · N830BX · Doug DC871F · DoorsSDR UPS02838078Skin · crackedINSPECTION TYPE:C1 L1 FWD ENTRY DOOR LWR AFT CORNER HAS CRACK INDICATION. ROUTED OUT CRACKS IN FUSELAGE SKIN & INNER DOUBLER IAW DC8 SRM 53-2-0 FIG 15.Apr 17, 2002 · N709UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02838082Intercostal · crackedINSPECTION TYPE:C1, L1 DOOR JAMB INTERCOSTAL IS CRACKED ON BOTH ENDS. FABBED NEW INTERCOSTAL IAW DAC DWG 5597646. INSTALLED DOOR PANS AND INTERCOSTAL IAW DC8 SRM 51-1-20D, 51-1-21 AND 51-3-0.Apr 16, 2002 · N709UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02838049Battery Pack · dischargedINSPECTION TYPE:PFLT EMERGENCY LIGHTS BATTERY PACK INOP. EMERGENCY LIGHTS BATTERY PACK REMOVED AND REPLACED AS PER MM 33-50-00.Apr 15, 2002 · N730UP · Doug DC871F · Emergency LightingSDR UPS02838034Skin · crackedINSPECTION TYPE:C1 REMOVED STEEL DOUBLER FROM R1 DOOR UPPER FWD CORNER. REMOVED STEEL DOUBLER RAIN GUTTER UPPER DOOR STOP GILLINER ATTACH ANGLE AND WEB FABBED DOUBLERS IAW DC8 SRM 53-2-0 FIG 14. REMOVED CRACK IAW DC 8 SRM 53-2-0 FIG 14. ALODINED & PRIMED IAApr 4, 2002 · N709UP · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA0200013OHarness · crackedAFTER TAKEOFF FROM TOL, THE FLIGHT CREW NOTICED AN ABNORMALLY HIGH ENGINE GAS TEMPERATURE INDICATION ON THE NUMBER FOUR ENGING. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURE AND THE ENGINE WAS SECURED AS PERCAUTIONARY MEASURE AND DISCHARGED ONE FIRE AGENT BOTTLE.Apr 3, 2002 · N820BX · Doug DC871F · Engine Temperature Indicating SystemSDR UPS02837958Odor · detectedINSPECTION TYPE:N/A ODOR IN COCKPIT FROM A/C UNIT. RAN BOTH PACKS WITH GROUND CART AND OFF ENGINE BLEEDS, COULD NOT DUPLICATE ODOR. OK FOR CONTINUED SERVICE.Mar 30, 2002 · N706UP · Doug DC871F · Air Distribution SystemSDR UPS02837962Life Vest · tornINSPECTION TYPE:N/A CAPTS LIFE VEST TORN. REPLACED CAPT LIFE VEST.Mar 30, 2002 · N715UP · Doug DC871F · Life JacketSDR UPS02837973Light · inoperativeINSPECTION TYPE:N/A EMERGENCY EXIT LIGHT INOP. SECURED GROUND IAW DC8 MM 20-00. REMOVED AND REPLACED LIGHT BULB IN EMERGENCY EXIT ASSY AT ENTRY DOOR IAW DC8 MM 33-50, OPS CHECK GOOD.Mar 29, 2002 · N772UP · Doug DC871F · Emergency LightingSDR UPS02838062Fitting · crackedINSPECTION TYPE:C1 AFT PIT FS 1200 ZEE FITTING AT L34R - L33R IS CRACKED. REMOVED FITTING IAW DC8 SRM 51-1-20D. LOCATED & DRILLED NEW FITTING I AW DC8 SRM 51-1-24, INSTALLED IAW DC8 SRM 51-1-20D.Mar 28, 2002 · N709UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02838042Clip · crackedINSPECTION TYPE:C1 O/B SKATE ANGLE CLIP BETWEEN STRINGER 62 AND STRINGER 63 CRACKED NR 1 PYLON NR 1 ALT. REMOVED AND REPLACED CLIP IAW DC8 SRM 51-1-20D.Mar 28, 2002 · N709UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS02838053Doubler · gougedINSPECTION TYPE:C1 REPAIR AT BS 25.5 TO 39.25, L21L TO L22L FALLS INTO THE D CAT PER UPS EO DC8-5330-12800 AND REQUIRED FURTHER EVAL BY ENGINEERING BY REPAIR GOUGED BEYOND LIMITS. REMOVE OLD DOUBLER, FABBED NEW REPAIR DOUBLERS AND FILLER PER 53-2-1 FIG 7, INSMar 27, 2002 · N709UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02838058Floorboard · damagedINSPECTION TYPE:C1 FLOORBOARD STA 340-460 POS 7 SOFT SPOT. FABRICATED FLOOR PANEL IAW UPS EO DC8-5320-9691C.Mar 26, 2002 · N709UP · Doug DC871F · Fuselage Floor PanelSDR UPS02838057Floor Panel · damagedINSPECTION TYPE:C1 CABIN FLOORBOARD STA 1480-1580 POS NR 7 HAS SOFT SPOT. FABRICATED FLOOR PANEL IAW UPS EO DC8-5320-9691C.Mar 26, 2002 · N709UP · Doug DC871F · Fuselage Floor PanelSDR UPS02838079Longeron · crackedINSPECTION TYPE:C1 STA 320 LONG 7R CRACKED. REMOVED CRACKED LONGERON FAB NEW LONG & SPLICES IAW DC8 SRM 53-2-2 AND DAC DWG 5755649. INSTALLED NEW LONGERON AND SPLICES IAW DC8 SRM 51-1-20D & 53-2-2.Mar 25, 2002 · N709UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS02838056Longeron · crackedINSPECTION TYPE:C1 STA 240 LONG 9R CRACKED. CUT OUT DAMAGED SECTION OF LONG & FABBED NEW SECTION IAW DAC DWG 5755 649-509 & DC8 SRM 53-2-2. INSTALLED SPLICES & NEW LONGERON SECTION IAW DC8 SRM 51-1-20D.Mar 25, 2002 · N709UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS02838052Door · damagedINSPECTION TYPE:C1 PERMANENT REPAIR ON SECOND AIRSTART DOOR IAW EO DC8-5330-12800. REPAIRED AREA IAW UPS EO DC8-5330-0793 AND DAC DRWG 08530020.Mar 25, 2002 · N709UP · Doug DC871F · Service DoorsSDR UPS02838039Angle · crackedINSPECTION TYPE:C1 AFT PIT STA 1270 INSULATE PAD IS CRACKED AT TORQUE BOX. REMOVED ANGLE IAW DC8 SRM 51-1-21 & 51-1-20D AND INSTALLED ANGLE IAW DC8 SRM 51-1-120D.Mar 25, 2002 · N709UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02838080Fitting · crackedINSPECTION TYPE:C1 KEEL BEAM FITTING RT AT STA 854 CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-3-0.Mar 24, 2002 · N709UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02838063Frame · crackedINSPECTION TYPE:C1 FRAME AT FS 720 AND BETWEEN L35L AND 36 IS CRACKED. REMOVED AND REPLACED DAMAGED FRAME SPLICES IAW DAC DWG 9753750.Mar 24, 2002 · N709UP · Doug DC871F · Fuselage Main, FrameSDR UPS02838045Fitting · corrodedINSPECTION TYPE:C1 AFT PIT IN TORQUE BOX STA 1220-1228 BETWEEN LONG 33R TO 32R IS CORRODED. REMOVED AND REPLACED CORRODED ANGLE IAW DC8 SRM 53-2-0 FIG 2D. FABBED SPLICE ANGLE IAW DC8 SRM 563-2-0, INSTALLED Z-ANGLES & SPLICES IAW DC8 SRM 53-2-0 FIG 2D.Mar 24, 2002 · N709UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02838043Fitting · crackedINSPECTION TYPE:C1 AFT CARGO PIT AT FS 1230 BETWEEN L34R - L35R Z-FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DC SRM 53-2-0 FIG 2D. FABBED SPLICE ANGLES IAW DC8 SRM 53-2-0, INSTALLED FITTING AND REPAIR ANGLES IAW DC8 SRM 53-2-0.Mar 24, 2002 · N709UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02838061Bulkhead · crackedINSPECTION TYPE:C1 RT APB CRACKED STA 1766 L11R. REPAIRED AREA IAW REO G08569.Mar 23, 2002 · N709UP · Doug DC871F · Fuselage Main, BulkheadSDR UPS02838055Frame · corrodedINSPECTION TYPE:C1 A/C COMPT AT FS 24 ABOVE LONG 35R FRAME IS CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8, OUT OF LIMITS. FABBED REPAIR PART IAW DWG DC8-53A-0II. INSTALLED PART IAW DC8 SRM 51-1-20D.Mar 23, 2002 · N709UP · Doug DC871F · Fuselage Main, FrameSDR UPS02838064Skin · damagedINSPECTION TYPE:C1 REMOVED STEEL DOUBLER FROM L2 LOWER AFT CORNER. REMOVED DOUBLER, PERFORMED HFEC AND NO CRACKS NOTED. FABBED AND INSTALLED DOUBLER TRIPLER AND FILLER IAW REO G08571. SEALED AREA IAW DC8 SRM 51-1-11.Mar 22, 2002 · N709UP · Doug DC871F · Passenger/Crew DoorsSDR UPS02838060Skin · crackedINSPECTION TYPE:C1 REMOVED STEEL DOUBLER FROM R1 DOOR UPPER FWD CORNER. FABBED DOUBLERS IAW DC8 SRM 53-2-0 FIG 14. REMOVED CRACK IAW DC8 SRM 53- 2-0 FIG 14. INSTALLED DOUBLERS & FILLER IAW DC8 SRM 51-1-20D.Mar 22, 2002 · N709UP · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA0200010OSkin · crackedDURING A ROUTINE MAINTENANCE PREFLIGHT INSPECTION, A CRACK WAS DETECTED ON THE OUTER PLATING AT FUSELAGE STATION 25, LONGERON 33 RIGHT. THE REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION A REPAIR FILLER AND A EXTERNAL REPAIR DOUBMar 22, 2002 · N822BX · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02838081Fitting · crackedINSPECTION TYPE:C1 KEEL BEAM FITTING RT AT STA 854 CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-3-0.Mar 21, 2002 · N709UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02837925Switch · failedINSPECTION TYPE:N/A NUMBER 2 INS FAILED ON THE WAY TO DFW, RED FLAG APPEARED BUT NO FAULT CODE. IN ATTITUDE REF MODE SMELLED SMOKE TURNED INS OFF AND PULLED CIRCUIT BREAKER. REMOVED AND REPLACED INU BATTERY AND BLOWER VANE SWITCH REF L/P 722257 ITEM 1 AND 72Mar 21, 2002 · N729UP · Doug DC871F · Inertial Guidance SystemSDR UPS02837935Fitting · corrodedINSPECTION TYPE:C1 STA 70 FWD SIDE LONG 31R UPPER FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 4614397, AND SRM 51-1-20D, 51-1-21.Mar 11, 2002 · N706UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02837853Fitting · crackedINSPECTION TYPE:C BATHTUB FITTING CRACKED, STA 1200 L34R-L35R. REMOVED AND REPLACED FITTING PER SRM 53-2-0 FIG 2D.Mar 9, 2002 · N707UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02837932Doubler · corrodedINSPECTION TYPE:C1 STA 25 TO 60 INTERNAL DOUBLER IS CORRODED BEYOND LIMITS BETWEEN LONG 26R TO 31R. REMOVED AND REPLACED DOUBLER IAW DWG 5649028, AND SRM 51-1-20D, 51- 1-21.Mar 8, 2002 · N706UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02837908Longeron · corrodedINSPECTION TYPE:C1 STA 1650 LONG 35L LONGERON AND END FITTINGS ARE CORRODED BEYOND LIMITS. REMOVED END FITTINGS, AND LONG 35L BETWEEN STA 1650-1680, FABRICATED AND REPLACED LONGERON SECTION AND END FITTINGS IAW DWG 3647110, AND SRM 51-1-20D, 51-3-0.Mar 8, 2002 · N706UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS02837897Fitting · crackedINSPECTION TYPE:C1 STA 1220 BATHTUB FITTING IS CRACKED BETWEEN LONG 34R-35R. REMOVED AND REPLACED FITTING IAW DWG 3755843 AND SRM 53-2-0 FIG 2D, 51-1-20D.Mar 8, 2002 · N706UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02837896Fitting · crackedINSPECTION TYPE:C1 STA 1200 BATHTUB FITTING IS CRACKED BETWEEN LONG 33R-34R. REMOVED AND REPLACED FITTING IAW DWG 3755841 AND SRM 51-1-20D, 53-2-0 FIG 2D.Mar 8, 2002 · N706UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02837802Hydraulic Line · failedINSPECTION TYPE:N/A, HYD FAILURE IN FLIGHT. EMERGENCY DECLARED. ON CLIMBOUT LOSS OF HYDRAULIC FLUID DOWN TO AUX QUANTITY POSITION. R&R MS ON AILERON RETURN LINE I/B RT WING BEHIND O/B FALSE PANEL. RAN NR 2 & 3 ENG, ALL SYS RAN AND NO LEAKS NOTED. REMOVED Mar 8, 2002 · N705UP · Doug DC871F · Hydraulic System, MainSDR UPS02837911Fitting · crackedINSPECTION TYPE:C1 STA 960 T-FITTING BETWEEN MAIN LANDING GEAR DOORS IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 5616306, AND SRM 51-1-20D.Mar 7, 2002 · N706UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02837914Skin · crackedINSPECTION TYPE:C1 LT MID GALLEY DOOR LOWER FWD CORNER CUTOUT SKIN IS CRACKED AT STA 1306 BETWEEN LONG 20L AND 21L. CUTOUT CRACKED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SRM 53-2-0 FIG 15A.Mar 6, 2002 · N706UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02837904Skin · crackedINSPECTION TYPE:C1 L2 DOOR JAMB LOWER FWD CORNER SKIN IS CRACKED BETWEEN LONG 20L AND 21L STA 1620. CUT OUT CRACKED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SRM 53-2-0 FIG 18.Mar 6, 2002 · N706UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02837900Skin · crackedINSPECTION TYPE:C1 L-1 LOWER AFT CORNER DOUBLER AND TRIPLER DOES NOT CONFORM TO SRM 53 -2-0 FIG 15 AND SRO8530021, AND SKIN IS CRACKED AT STA 60 BETWEEN LONG 20L AND 21L. CUTOUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLERMar 6, 2002 · N706UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02837899Skin · crackedINSPECTION TYPE:C1 REPAIR AT STA 1440, UPPER AFT CORNER D-PIT DOOR IS A CATEGORY D PER EO DC8-5330-12800, AND SKIN IS CRACKED AT LONG 22R APPROX. REMOVED EXISTING REPAIR, CUTOUT CRACKED AREA, NDT VERIFIED NO CRACKS. AT CUTOUT, FABRICATED AND INSTALLED DOUBLEMar 6, 2002 · N706UP · Doug DC871F · Fuselage Main, Plate/Skin
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