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 UPS05845565Longeron · corrodedINSPECTION TYPE:SP L27R FS 70 TO FS 8.0 LONGERON 27R HAS EXFOLIATION CORROSION. REMOVED AND REPLACED LONGERON 27R AT FS 70 TO FS 8.0 IAW SRM 51-1-21 AND SRM 51-1-20D.Sep 20, 2005 · N718UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS05845585Doubler · corrodedINSPECTION TYPE:SP A/C DOUBLER BETWEEN L26R - L31R FS 30 TO 65 INTERNAL DOUBLER IS EXFOLIATED AT FS 55 TO FS 35. REMOVED AND INSTALLED INTERNAL DOUBLER IAW SRM 51-1-21 & 51-3-0.Sep 20, 2005 · N718UP · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA0500107OBolt · out of adjustDURING TAKEOFF FROM KTOL, GEAR UPLATCH CHECK UNSATISFACTORY DOORS LIGHT AND LANDING GEAR UNSAFE LIGHT CAME ON IN UPLATCH POSITION. CYCLED GEAR DOWN AND UP, SAME RESULTS CREW RETURNED AIRCRAFT TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND STRUT TO UNSep 15, 2005 · N822BX · Doug DC871F · Main Landing GearSDR UPS05845573Skin · corrodedINSPECTION TYPE:SP TRANSFERRED FROM LOG PAGE 442150, REF DMI LOG D-309966 SKIN CORRODED AT STA 25 - 74 LONG 28R - 31L. REMOVED AND REPLACED BELLY SKIN AT STA -21.92 TO 70 LONG 31R TO L31L IAW EO DC8-5330-8942-D.Sep 14, 2005 · N718UP · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA0500106OEngine · flamed outDURING DESCENT FROM BIKF TO KNGU, NR 4 ENGINE EXPERIENCED VIBRATION AND A FLAME OUT. CREW LANDED AIRCRAFT IN KNGU WITHOUT INCIDENT. MAINTENANCE COMPLIED WITH FAULT 53, FAN VIBRATION AND NO DEFECTS WERE NOTED. FAULT 51 COMPLIED WITH AND MAINTENANCE SUMPED WASep 12, 2005 · N823BX · Doug DC871F · Engine (Turbine/Turboprop)SDR UPS05845402Adc · failedINSPECTION TYPE:N/A ATB - AFTER T/O LOST NR 1 ADC, PULLED C/B COULD NOT RESTORE, XFRD TO NR 2 ADC ON CAPT SIDE. ATB DUE TO SLIGHT ELEC BURNING SMELL. REMOVED AND REPLACED AIR DATA COMP IAW MM 34-11-01-4 AND NR 1 ADC SELECT XFR RELAY IAW MM 20-50-16-2. CHECKSep 12, 2005 · N703UP · Doug DC871F · Air Data ComputerSDR UPS05845475Shear Tie · corrodedINSPECTION TYPE:SP, AT STA 35 IN BETWEEN L34L AND L34R HAS CORROSION BEYOND LIMITS ON SHEAR TIE. REMOVED, FABRICATED AND INSTALLED SHEER TIE IAW SRM 53-03-01 FIG 003, 51-3-2, 51-1-21 AND 51-1-21.Sep 11, 2005 · N772UP · Doug DC871F · Fuselage Internal Mounting StructureSDR UPS05845474Shear Tie · corrodedINSPECTION TYPE:SP AT STA 55 IN BETWEEN L34L AND L34R HAS CORROSION BEYOND LIMIT ON SHEER TIE. REMOVED, FABRICATED AND INSTALLED SHEER TIE IAW SRM 53-03-01, 51-3-2, 51-1-21 AND 51-1-20D.Sep 11, 2005 · N772UP · Doug DC871F · Fuselage Internal Mounting StructureSDR UPS05845400Longeron · corrodedLONGERON CORROSION BELLY 30, 31 & 34. LOG PAGES REFERENCED 442142/2,3 & 4441243 REMOVED 52 RIVETS/HI LOKS AT F.S. 70. STA 28R-30R TO VERIFY CORR PERFO RMED LOW FQY, VERIFY MATL LOSS 10-12 SO 05571 QC REF DC8-5330-22862 RE MOVE RIVETS F.S. 35. STA 30R TO VESep 10, 2005 · N718UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS05845476Skin · corrodedINSPECTION TYPE:SP REMOVE AND REPLACE LOWER FWD SKIN STA -21.92 TO STA 70 L31L- L31R. REMOVED AND REPLACED LWR FWD SKIN STA -21.92 TO STA 70 L31L-L31R IAW EO DC8-5330-8942-D.Sep 9, 2005 · N772UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS05845354Skin · crackedSKIN BULGE AND CRACK. ASSIGNED FERRY PERMIT NR 9148 TO SAA. PER NRC 788843 REPAIRED ON NRC 788844. PERFORMED LOW FREQ EDDY CURRENT INSP IN AREA OF SKIN BULGE AT FS 35 PER NDT SPM 06-10-2.002. MAT LOS S DETECTED AT FS 35 IN AREA BTWN L36 & L34R APPX 8". SKIN Sep 2, 2005 · N772UP · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA0500105OLanding Gear · failedWHEN LANDING GEAR LEVER IS SELECTED TO UPLATCH CHECK POSITIONS, DOOR LIGHTS AND LANDING GEAR UNSAFE LIGHTS ILLUMINATE. SAME RESULTS AFTER GEAR RECYCLE. THE NOSE GEAR DOOR STAYED CLOSED WHEN GEAR LEVER IS RETURNED TO UP POSITION BOTH LIGHTS GO OUT. ALSO THESep 1, 2005 · N822BX · Doug DC871F · Landing Gear Retraction/Extension SystemSDR IXXA0500104OBlade · leakingNR 2 ENG SHUTDOWN FOR LOSS OF OIL QTY. OIL PRESS DROPPED. OIL TEMP STABLE. SHUTDOWN NR 2 ENG. WINDMILL OIL PRESS DROPPED & QTY INCREASED. TEMP STABLE. NO WINDMILLING PRESS. LOW PRESS LIGHT ILLUM. LANDED W/OUT INCIDENT. R&R NR 2 ENG, OPS & LEAK CHK GOOD. ACFT Aug 23, 2005 · N828BX · Doug DC871F · Turbine Engine Oil SystemSDR UPS05845283Doubler · crackedNOSE SECTION FUSELAGE SKIN HAS 3/8" CRACK AT AFT HINGE ACCESS DOOR. REMOVED CRACKED DOUBLER AT NOSE EXTERIOR AFT SKIN IAW SRM 51-1-21. FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW DWG56126127 AND SRM 51-1-20E.Aug 19, 2005 · N750UP · Doug DC871F · Landing Gear DoorsSDR IXXA0500103OEngine · malfunctionedDURING CRUISE FROM KPHL TO KTOL THE NR 2 ENGINE FLUCTUATED EGT FOLLOWED BY A INSTANTANEOUS EGT TEMPERATURE INCREASE. OIL PRESSURE FLUCTUATED BUT NO LOSS. THE CREW PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN THEN LANDED IN KTOL WITHOUT INCIDENT. AN INSPECTION IS Aug 19, 2005 · N828BX · Doug DC871F · Engine (Turbine/Turboprop)SDR IXXA0500097OTube · broken!DURING CLIMBOUT FROM KTOL TO KPHL THE NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. PRESSURE WAS AT 14 PSI AND FLUCTUATING AND OIL QUANTITY DEPLETING SLOWLY. THE CREW PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN. CREW LANDED IN KPHL WITHOUT INCIDENT. MAINTENAAug 18, 2005 · N828BX · Doug DC871F · Engine Oil System (Airframe Furnished)SDR IXXA0500096OLine · brokenDURING CRUISE FROM KBFI TO KTOL THE NR 2 ENGINE HAD LOSS OF OIL QUANTITY FOLLOWED BY LOSS OF OIL PRESSURE. CREW PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN. AIRCRAFT MAINTAINED OIL PRESSURE DURING DURATION OF FLIGHT AND THE CREW LANDED IN KTOL WITHOUT INCIDENT. Aug 18, 2005 · N828BX · Doug DC871F · Turbine Engine Oil SystemSDR IXXA0500095OLine · brokenDURING CRUISE FROM KDFW TO KTOL CREW SHUTDOWN THE #2 ENGINE DUE TO LOSS OF OIL QUANTITIY PRESSURE. CREW LANDED IN KTOL WITHOUT INCIDENT. MAINTENANCE FOUND A BROKEN LINE AT THE OIL PRESSURE TRANSMITTER. THEY REMOVED AND REPLACED THE PRESSURE TRANSMITTER LINE ANAug 17, 2005 · N828BX · Doug DC871F · Engine Oil System (Airframe Furnished)SDR UPS05845421Spar · crackedINSPECTION TYPE:C1 RIGHT KEEL BEAM AT FS 857 2.5 INCH CRACK ON LWR SPAR. STOP DRILLED CRACK AT XCW 4.0 IAW SRM 51-1-20D NDT HFEC IAW NDTSPM 06-10-01.001 NO CRACKS NOTED BEYOND STOP DRILL. FABRICATED FILLERS VERTICAL FILLERS AND -136 ANGLE AND STIFFENERS AND IAug 16, 2005 · N750UP · Doug DC871F · Fuselage Main, FrameSDR UPS05845275Finger Doubler · corrodedCOCKPIT SUBFLOOR FINGER DOUBLER HAS SEVERAL SHEAR HEAD RIVETS AND CORRODED AT STA -67 TO -80 RBL 60. REMOVED FINGER DOUBLER IAW SRM 51-1-21 AND 51-3-0. REMOVED CORROSION FROM WEB IAW SRM 51-1-8, FABRICATED AND INSTALLED REPLACEMENT FINGER DOUBLER AT STA -67 Aug 16, 2005 · N750UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS05845241Frame · crackedFRAME ON 62 DOOR OPENING IS CRACKED INSIDE OPENING RT SIDE. FAB`D DOUBLER AND REPAIRED IAW SRM 53-05-01 AND 51-1-21A.Aug 16, 2005 · N750UP · Doug DC871F · Fuselage Main, FrameSDR UPS05845236Fitting · corrodedHEAVY CORROSION ON SPLICE FITTING STA 210 L7R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.Aug 16, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS05845369Floorbeam · crackedINSPECTION TYPE:C1 FLOORBEAM CRACKED AT FS 55 LBL 12. CUT OUT DAMAGED AREA OF FLOORBEAM IAW SRM 53-2-0 TEMP REV 53-152, FABRICATED DOUBLER AND FILLER AND INSTALLED REPAIR PARTS IAW SRM 53-2-0 TEMP REV 53-152 AND 51-1-20D.Aug 15, 2005 · N750UP · Doug DC871F · Fuselage Main, Floor BeamSDR UPS05845285Fitting · crackedFS -8 AT L33L BULKHEAD HAS CRACKED END FITTING A/C COMPT. REMOVED AND REPLACED END FITTING AT FS -8 L33L IAW SRM 51-3-0,51-3-2 PG 1 AND 51-1-21.Aug 15, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS05845282Fitting · crackedSTA 280 RBL 50 END FITTING CRACKED. REMOVED AND REPLACED END FITTING AT STA 280 RBL 50 IAW DWG 9754022 AND SRM 51-1-20D.Aug 15, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS05845256Fitting · crackedEND FITTING CRACKED LONG 17R FS 1768. REMOVED AND REPLACED END FITTING AT STA 1768 LONG 17R IAW DWG 4772397 AND SRM51-1-20D.Aug 15, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA05000940Wire · damagedDURING CLIMB & CRUISE NR 2 ENGINE FUEL FLOW & EGT FLUCUATED FROM 811 TO 875, OTHER ENGINES AT 830 TO 835. EGT THEN PEAKED AT 1000 (FLASHING). ALSO WITH STANDARD POWER SET FOR CLIMB, THE EGT & FF FOLLOWED THE THROTTLE & THEN THE FUEL FLOW & EGT WENT HIGH & DIAug 15, 2005 · N828BX · Doug DC871F · Engine Indicating System WiringSDR UPS05845383Splice · crackedINSPECTION TYPE:C1 CRACKED SPLICE ANGLE INSIDE CHANNEL AT FS 450 L33R. REMOVED CRACKED SPLICE ANGLE IAW SRM 51-1-21D, MACHINED AND INSTALLED LONGERON SPLICE AT STA 450 L33R IAW DWG 3750330.Aug 14, 2005 · N750UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS05845368Splice · crackedINSPECTION TYPE:C1 SPLICE FITTING AT FS 450 L31R IS CRACKED. REMOVED AND REPLACED SPLICE FITTING AT FS 450 L31R IAW DWG 5754814 AND SRM 51-1-20D.Aug 14, 2005 · N750UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS05845385Fitting · crackedINSPECTION TYPE:C1 C-PIT FS 1150 L33R I/B SIDE, FITTING HAS 2EA PLUGGED FASTENERS LOOSE. REMOVED INTERCOSTAL AT FS 1150 L33R IAW SRM 51-1-20D, FABRICATED AND INSTALLED FITTING AND INTERCOSTAL IAW DWG 4758514 AND DWG 9754949.Aug 13, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS05845292Fitting · corrodedLWR CARGO FS 1230 L32R ZEE FITTING CORRODED AND CRACKED .500 INCH LONG AROUND FASTNER HOLE. REMOVED ZEE FITTING IAW SRM 51-1-21 AND 51-1-20D. REPLACED ZEE FITTING AT FS 1230 L32R IAW SRM 51-3-2 AND 51-1-20D.Aug 13, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS05845255Skin · crackedLT WING AILERON LE UPPER SURFACE AROUND FASTENER HAS 1/4" LONG CRACK PCU AREA. STOP DRILLED CRACK NDT HFEC VERIFIED CRACK TERMINATES AT STOP DRILL. FABRICATED REPAIR DOUBLER IAW 57-02-00-0 AND INSTALLED REPAIR DOUBLER IAW SRM 57-02-00-0 AND 57-08-00-0. REPAAug 13, 2005 · N750UP · Doug DC871F · Aileron TabsSDR UPS05845242Rib · crackedLT LE UPPER RIB CRACKED AT XFS 766.250. FAB`D DOUBLER AND REPAIRED IAW DWG 5769470 AND SRM57-02-00 FIG 2.Aug 13, 2005 · N750UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS05845240Rib · crackedLT WING LE UPPER RIB CRACKED AT XFS 707. FABED DOUBLER AND REPAIRED RIB IAW DWG 5769466, AND SRM 57-2-0 FIG 2.Aug 13, 2005 · N750UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS05845239Finger Doubler · corrodedCOCKPIT SUBFLOOR FINGER DOUBLER HAS SHEARED HEAD FASTENERS AND POSSIBLE CORROSION UNDER DOUBLER AT FS -67 TO -52 LBL24. REMOVED AND REPLACED FINGER DOUBLER IAW SRM DWG 5612298 AND SRM 51-1-21 AND 51-1-20D.Aug 13, 2005 · N750UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS05845420Cusp Web · crackedINSPECTION TYPE:C1 CUSP CRACKED FS 1100 L21R. REMOVED CUSP DOUBLER AT FS 1100 L21R AND REMOVED DAMAGED SECTION OF L21R IAW SRM 51-1-20A AND SRM 53-2-5 FIG 15. FABRICATED AND INSTALLED SPLICE PLATE -3 AND -5, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53Aug 12, 2005 · N750UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS05845384Pan · crackedINSPECTION TYPE:C1 L1 DOOR LWR AFT CORNER JAMB INSIDE WEB CRACKED 2 INCHES LONG. REMOVED DOOR JAMB AND WEB CUT OUT DAMAGED AREA IAW DWG 5597646, FABRICATED DOUBLER AND SPLICE AND INSTALLED REPAIR PARTS IAW DWG 5597646.Aug 12, 2005 · N750UP · Doug DC871F · Passenger/Crew DoorsSDR UPS05845294Cusp Web · crackedCUSP HAS SHEAR HEAD FASTENER AND CRACK 1 INCH LONG FS 1420 L21R. REMOVED DAMAGED CUSP FROM BS 1390-1430 L21R IAW SRM 51-1-20D AND 51-1-2. FABRICATED AND INSTALLED REPAIR PARTS AND CUSP ANGLE IAW SRM 53-2-5 FIG 15 AND DWG 9754069 AT BS 1390-1430 L21R.Aug 12, 2005 · N750UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS05845257Longeron · crackedLONGERON 7R CRACKED AT FS 1746. REMOVED DAMAGED AREA IAW SRM 53-02-02 FIG 11, FABRICATED AND INSTALLED REPAIR SPLICE FILLER AND REPAIR ANGLES IAW SRM 53-02-02 FIG 11 AND SRM 51-1-20D.Aug 12, 2005 · N750UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS05845254Longeron · crackedLONG 15L CRACKED AT FS 1726. REMOVED DAMAGED AREA IAW SRM 53-2-2 FIG 11. FABRICATED REPAIR SPLICE FILLER AND REPAIR ANGLES AND INSTALLED IAW SRM 53-02-02 FIG 11 AND SRM 51-1-20D.Aug 12, 2005 · N750UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS05845252Angle · crackedC1 ANGLE CRACKED AT FS 1766 LONG 6L. REMOVED ANGLE IAW SRM 51-1-20D AT FS 1766 LONG 6L. FABRICATED AND INSTALLED ANGLE AT FS 1766 LONG 6L DWG 5773844 AND SRM 51-1-20D.Aug 12, 2005 · N750UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS05845251Angle · crackedC1 ANGLE CRACKED AT FS 1766 LONG 6R. REMOVED CRACKED ANGLE AT FS 1766 L6R IAW SRM 51-1-20D. FABRICATED AND INSTALLED ANGLE AT FS 1766 L6R IAW SRM DWG 5773844 AND SRM 51-1-20D.Aug 12, 2005 · N750UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS05845229Fitting · crackedMAIN CABIN LONGERON END FITTING CRACKED AFT SIDE OF STA 680 L2L. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D, 51-1-21, AND 51-3-0 .Aug 12, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS05845228Longeron · crackedLONGERON 14R CRACKED FS 1746. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 53-2-2 FIG 11.Aug 12, 2005 · N750UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS05845227Bulkhead · crackedAFT PRESSURE BULKHEAD CRACKED 1.5" LONG FS 1766 RBL 48 L11R. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAE DWG SRO 8530007.Aug 12, 2005 · N750UP · Doug DC871F · Fuselage Main, BulkheadSDR UPS05845219Fitting · crackedFITTING CRACKED AT FS 1150 L19R. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.Aug 12, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS05845371Fitting · crackedINSPECTION TYPE:C1 CENTER WING SUB FLOOR FS 759 LBL 48 L-FITTING CRACKED. REMOVED CRACKED L-FITTING IAW SRM 51-1-20D, FABRICATED AND INSTALLED L-FITTING IAW DWG 3643110 AND 51-1-20D.Aug 11, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS05845366Fitting · crackedINSPECTION TYPE:C1, FITTING CRACKED AT FS 759 L18R AFT SIDE. REMOVED AND REPLACED FITTING AT FS 759 L18R IAW SRM 51-1-20D,51-1-24, AND 51-1-8Aug 11, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS05845293Fitting · crackedFITTING CRACKED AT FS 857.125 L18R AFT SIDE. REMOVED AND REPLACED END FITTING AT FS 857.125 L18R IAW SRM 51-1-20D AND DWG 4750420.Aug 11, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS05845281Fitting · corrodedMAIN CABIN TEE FITTING CORRODED AT FS 980 LBL 40. REMOVED CORROSION ON TEE FITTING AND FOUND TO BE OUT OF LIMITS IAW SRM 53-2-0. REMOVED AND REPLACED TEE FITTING AT FS 980 LBL 40 IAW SRM 51-3-0, 51-1-21, AND 51-3-2.Aug 11, 2005 · N750UP · Doug DC871F · Fuselage Main, Attach Fittings
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