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 IXXA04000121OLanding Gear · malfunctionedAFTER TAKEOFF FROM KHRL TO KTOL, LANDING GEAR UNSAFE LIGHT ILLUMINATED WITH GEAR UP. UPLOCK CHECK UNSATISFACTORY, NOSE GEAR FALLS FREE. CREW LANDED IN KTOL WITHOUT INCIDENT. AN INSPECTION IS ON GOING. WHEN MORE INFORMATION IS AVAILABLE IT WILL BE PROVIDED.Nov 16, 2004 · N821BX · Doug DC871F · Main Landing GearSDR UPS04843552Angle · corrodedVERTICAL STIFFENER CORRODED BEYOND LIMITS ON AFT SIDE OF WING REAR SPAR, RT W/W, STA 857 BULKHEAD XCW46. FABRICATED REPLACEMENT ANGLE FROM ACA41283 7075T6 EXT REF DWG 5643433. NDT PER DPS4.707, NO CRACKS NOTED. REMOVED AND REPLACED ANGLE PER SRM 51-1-21, 51Nov 15, 2004 · N798UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS04843572Fitting · crackedINTERCOSTAL TO FRAME ATTACH FITTING CRACKED AT STA 1140 LONG 35R. REMOVED AND REPLACED FITTING REF SRM 51-1-21, 51-1-20D, 51-1-8.Nov 14, 2004 · N744UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS04843503Life Vest · tornINSPECTION TYPE:N/A, F/O'S LIFE VEST WORN. REMOVED AND REPLACED F/O'S LIFE VEST. TAG# 956523.Nov 14, 2004 · N700UP · Doug DC871F · Life JacketSDR UPS04843606Longeron · crackedINSPECTION TYPE:C3 LONGERON 16R AT FS 1728 IS CRACKED AT FRAME ATTACHMENTS, LENGTH OF CRACKS IS APPROX 1.5 INCH. REPAIRED LONGERON AT 16R STA1728 IAW DWG 5644130, DC-8 53-2-2 FIG 10, SRM 53-02-02-0, SRM 51-1-20D.Nov 11, 2004 · N744UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA060009SRepair · scheduled maintDURING ROUTINE C-CHECK REMOVE EXISTING FUSELAGE SKIN REPAIR LOCATED AT STATION 220 LONGERON 35 RIGHT DUE TO DTA REQUIREMENTS. REMOVED NECESSARY FASTENERS, AND EXISTING DOUBLER, REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, REMOVED, TERATED, PRIMNov 10, 2004 · N825BX · Doug DC871F · Aircraft StructuresSDR IXXA060008SDoubler · damagedDURING ROUTINE C-CHECK REMOVED EXISTING FUSELAGE SKIN REPAIR DT STATION 410 LONGERON 35 RT DUE TO DTA REQUIREMENTS. REMOVED AFFECTED FASTENERS AND DOUBLER. FABRICATED NEW REPAIR PARTS, LOCATED, DRILLED, REMOVED, TREATED, PRIMED, INSTALLED NEW REPAIR PARTS AND Nov 10, 2004 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA0500206SRepair · temporaryDURING ROUTINE C-CHECK, TO COMPLY WITH DTA REQUIREMENTS REMOVE EXISTING FASTENERS AND EXISTING FUSELAGE DOUBLER AT STATION 107 LONGERON 35 RIGHT. INSTALL REPAIR AT FUSELAGE SKIN SECTION FROM STATION 98.5 TO STATION 114.5 BETWEEN LONGERON 34 LEFT TO LONGERON 3Nov 10, 2004 · N825BX · Doug DC871F · Fuselage Structure (General)SDR IXXA0500237SFrame · corrodedDURING ROUTINE C-CHECK FOUND LOWER CHORD AT STATION 70 BETWEEN LONGERONS 35 RIGHT AND 34 LEFT CORRODED. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND NEW FASTENERS IAW COOPESA EO COO-Nov 9, 2004 · N825BX · Doug DC871F · Fuselage Main, FrameSDR UPS04843463Light · inoperativeINSPECTION TYPE:N/A EMERGENCY LIGHTS INOP OVER COURIER SEAT & IN COCKPIT CEILING. RELAMPED PER MM 33-50-02-2, CK'S OK.Nov 9, 2004 · N772UP · Doug DC871F · Emergency LightingSDR UPS04843524Skin · corrodedRT WING UPPER SKIN CORRODED AROUND HILOCK AT XRS554, ABOVE S54. NDT VERIFIED MATERIAL THICKNESS AT CORROSION REMOVAL SITE RANGED FROM .090-0.125. CUT OUT CORROSION SITE REF SRM 57-2-1 FIG28. FABRICATED DOUBLER AND FILLER FROM SHT7075T6-.190, MACHINED FILLERNov 3, 2004 · N798UP · Doug DC871F · Wing, Plate/SkinSDR 872SJ008Gusset · crackedRT UPPER GUSSET CRACKED AT STA XW5.000 GBAMC NR#04187. STOP DRILLED, FAB`D DOUBLER IAW DC-8 SRM. INSTALLED TOP AND BOTTOM DOUBLER IAW DC-8 SRM 51-1-21 AT STA XW5.000Nov 2, 2004 · N872SJ · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS04843551Attach Fitting · crackedTAILCONE ATTACH FITTING CRACKED AT CROWN (L1) ON FWD SIDE OF STA 1890 FRAME IN 62 COMP'T. REMOVED FITTING REF 51-1-20D. FABRICATED REPLACEMENT FITTING FROM PLATE 7075T6 REF DWG 3652562. NDT PER DPS4.707, NO CRACKS NOTED. INSTALLED FITTING REF SRM 51-1-8, 5Nov 1, 2004 · N798UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS04843560Spar · crackedINSPECTION TYPE: C1, CENTER WING REAR SPAR LOWER CORD CRACKED IN RT W/W, STA 857, OB CORNER. NDT MAPPED CRACK REF SPMSPM06-10-01.001. STOP DRILLED AND VERIFIED BY NDT. FABRICATED AND INSTALLED REPAIR PARTS PER SRO8570009Oct 30, 2004 · N798UP · Doug DC871F · Wing SparSDR UPS04843558Fitting · crackedINSPECTION TYPE:C1 SHEAR WEB FITTING CRACKED IN RT MLG W/W AT STA 857 APPROX RBL12. REMOVED CRACKED FITTING REF SRM51-3-0. FABRICATED REPLACEMENT FITTING FROM PLATE7050T7 PER SAA SK798-657, BOEING SERVICE ID 1-48219038 AND DAC DWG3646874. INSTALLED FITTINGOct 30, 2004 · N798UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS04843550Fitting · crackedBATH-TUB FITTING CRACKED AT STA 320, LONG 27L. REMOVED CRACKED FITTING REF 51-3-0, 51-1-21. FABRICATED REPLACEMENT FITTING FROM PLT7075T6 PER DWG3755822. NDT FITTING REF DPS7.707 NO CRACKS NOTED. FABRICATE SPLICE ANGLES FROM BAC1503-100163 AND INSTALLED ALOct 30, 2004 · N798UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS04843523Floorbeam · corrodedFLOORBEAM AT STA 55 RBL40 CORRODED BEYOND LIMITS. CUT OUT CORRODED AREA, NDT VERIFIED REF NDT SPM06-10-01.001 FABRICATED 2 FILLERS FROM 7075T6-.071. REPAIR ANGLE FROM AND 10136-2403, SPACER FROM 2024T3-.032. INSTALLED ALL REPAIR PARTS REF SRM 53-2-0 FIG1 F,Oct 30, 2004 · N798UP · Doug DC871F · Fuselage Main, Floor BeamSDR UPS04843518Longeron · crackedLONGERON 34L CRACKED AT STA 1260-1280. REMOVED LONG SPLICES AT STA 1270 STA 1350 PER SRM 51-1-20D OPENED SKIN FROM STA 1250-1350 FOR ACCESS REF SRM 51-1-21, 51-1-20D. REMOVED, FABRICATED, AND REPLACED LONG 34L FROM STA 1270-1350 REF DWG3758593, AND CLOSED SOct 30, 2004 · N798UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS04843511Fitting · crackedC1 BATH-TUB FITTING CRACKED AT STA300 L27L-L28L. REMOVED CRACKED FITTING AND FABRICATED REPAIR PARTS REF SRM53-2-0 FIG 2D. INSTALLED REPLACEMENT FITTING AND SPLICE ANGLES REF SRM 53-2-0 FIG2D AND SRM 51-1-20D.Oct 30, 2004 · N798UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS04843516Fitting · crackedINTERCOSTAL ATTACH FITTING CRACKED ON FWD SIDE OF STA 1000 FRAME AT L30L. REMOVED 2 GUSSETS AT STA 1000 AND REMOVED CRACKED FITTING REF SRM 51-1-21, 51-1-20D, 51-3-0. INSTALLED REPLACEMENT FITTING AND 2 GUSSETS REF SRM 51-1-20D, 51-1-8.Oct 29, 2004 · N798UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS04843513Frame · corrodedCORROSION ON FRAME AT STA 1080 ABOVE L36. REMOVAL EXCEEDED ALLOWABLE LIMITS. NDT VERIFIED MAT`L THICKNESS FROM 0.111- 0.154 REMOVED FRAME CAP AND 3 GUSSETS FROM L33R TO L35L REF SRM 51-1-21, 51-1-20D. FABRICATED AND INSTALLED REPAIR STRAP FROM 7075T7-.080 POct 29, 2004 · N798UP · Doug DC871F · Fuselage Main, FrameSDR IXXA0400116OLink Assy · bindingWHEN THE GEAR UPLATCH CHECK WAS ACCOMP WITH THE HANDLE IN THE UPLATCH CHECK POSITION. AT THE SAME TIME THE NOSE GEAR SEEMED TO FALL HARD ONTO THE NOSE DOORS CAUSING INCREASED NOISE. THE GEAR WAS CYCLED DOWN AND UP. THE UPLATCH CHECK REPEATED AND THE NOISE FROOct 29, 2004 · N830BX · Doug DC871F · Nose/Tail Landing GearSDR IXXA060082SRib · crackedDURING ROUTINE C CHECK, FOUND RIGHT WING RIB WEB CRACKED AT STATION XRS6. REMOVED DAMAGE. FABRICATED DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR DOUBLER, AND FASTENERS AT RIGHT HAND WING STATION XRS6 IAW DC8 SRM 57-2-0, 51-1-21, 57-Oct 28, 2004 · N825BX · Doug DC871F · Wing, Rib/BulkheadSDR UPS04843519Support Fitting · corrodedRT FUSELAGE FLAP HINGE STA 3 SUPPORT FITTING CORRODED BEYOND LIMITS. REMOVED AND REPLACED SUPPORT ASSY REF SRM 51-1-20D, 51-1-21, UPS EO DC8-5740-21256A.Oct 28, 2004 · N798UP · Doug DC871F · Trailing Edge FlapsSDR UPS04843437Spring · failedNR 1 & 4 ENGINE REVERSERS WENT INTO REVERSE IN FLIGHT. REINSTALLED NR 1 & 4 T/R LOCKOUT SPRINGS PER MM 76-11-00, OPS CHECK GOOD. REINSTALLED PNLS 573A AND 573B PER MM 53-21-01 AND REINSTALLED CAPT AND CO-PILOTS SEATS PER MM 25-11-01. RESET STALL WARNING C/BOct 28, 2004 · N729UP · Doug DC871F · Engine Thrust ReverserSDR IXXA0400115OControl Valve · leakingON DESCENT FROM KPDX TO KBFI, RUDDER CONTROL LIGHT ILLUMINATED WITH HYDRAULIC SYSTEM PRESS READ ZERO AND HYDRAULIC QUANTITY DOWN TO 6 GALS. COMPLETED QR4 PROCEDURE (LOSS OF HYDRAULIC). CREW ABORTED DESCENT AND RETURNED TO KPDX. LANDED WITHOUT INCIDENT. AN IOct 28, 2004 · N822BX · Doug DC871F · Rudder Control SystemSDR COOSDR040053Skin · delaminatedRT WING, SPOILER PN 56551671, SN 2740 UPPER SKIN DELAMINATED AT STA XRS 218. (K)Oct 27, 2004 · N825BX · Doug DC871F · SpoilersSDR UPS04843549Support · crackedRT FUSELAGE FLAP HINGE SUPPORT FITTING CRACKED. DISSASEMBLED FLAP BUSS DRUM ASSY TO FOM PER MM27-51-06. REMOVED AND REPLACED SUPPORT ASSEMBLY REF SRM 51-1-21, 51-1-20D, 51-3-0 51-1-8, 51-1-15. REASSEMBLED AND RIGGED FLAP BUS PER 27-51-06. OPS CHK GOOD.Oct 27, 2004 · N798UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS04843527Fitting · crackedFITTING CRACKED ON FRAME AT STA 1180, LONG 19R. REMOVED AND REPLACED FITTING REF SRM 51-1-20D, 51-1-8.Oct 27, 2004 · N798UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS04843522Longeron · crackedLONGERON 15R CRACKED AT STA 1750. REMOVED DAMAGED LONG SECTION FROM STA 1740-1766, SHEARTIE AT STA 1750, AND END FITTING AT STA 1766 PER SRM 53-2-2 FIG10, 51-1-20D, 51-1-21. FABRICATED AND INSTALLED REPLACEMENT LONGERON SECTION FROM S1616757 EXT AND 2 STRAPSOct 27, 2004 · N798UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS04843515Longeron · crackedLONGERON 15L CRACKED AT STA 1750. REMOVED CRACKED LONGERON SECTION FROM 1740-1760, 2 SHEAR TIES AT STA 1750 END FITTING AT STA 1760 REF SRM 51-1-21 AND 53-2-3. FABRICATED REPLACEMENT LONG SECTION FROM S1616757 EXT AND STRAPS FROM 7075T6-.080 PER SRM 53-2-3.Oct 27, 2004 · N798UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS04843512Fitting · crackedEND FITTING CRACKED ON L13L STA 840. REMOVED FITTING REF SRM 51-1-20D. FABRICATED REPLACEMENT FITTING PER DWG 3779874 FROM 7075-T6 PLATE ON SAA TRAVELER NR 0072. NDT C/W ON FINISHED PART PER DPS4.707, NO CRACKS NOTED. INSTALLED FITTING REF SRM 51-1-20D.Oct 27, 2004 · N798UP · Doug DC871F · Fuselage Main, Attach FittingsSDR 872SJ006Finger Doubler · corrodedLT OB TOP SIDE OF WHEEL WELL PRESSURE DOGHOUSE BETWEEN STA 960 AND 980, FINGER DOUBLER HAS CORROSION ON FWD UNDERSIDE. GBAMC NR304186 -OPEN-Oct 27, 2004 · N872SJ · Doug DC871F · Fuselage Main, Plate/SkinSDR COOSDR040052Skin · corrodedFUSELAGE AFT CENTER SECTION, LOWER PLATING (PN 57799293) CORRODED FROM STA 980 TO STA 1040 BETWEEN LONGERON 35L AND 35R. (K)Oct 26, 2004 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA060011SSkin · dentedDURING ROUTINE C CHECK, FOUND EMPENNAGE RIGHT HAND ELEVATOR UPPER AND LOWER SKIN DENTED IN SEVERAL AREAS. REMOVED RIGHT HAND ELEVATOR. REMOVED RIGHT HAND ELEVATOR UPPER AND LOWER SKIN SECTION FROM STATION XE 132.531 TO XE251.562. FABRICATED REPAIR PARTS, LOOct 25, 2004 · N825BX · Doug DC871F · Elevator, Plate/SkinSDR COOSDR040051Skin · corrodedLOWER FUSELAGE SKIN WITH CORROSION AT Y STA 622.0, BETWEEN LONG 27L AND LONG 30L. (K)Oct 25, 2004 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS04843526Frame · crackedCORROSION ON FRAME AT STA -99 AT DOOR 90A NEAR L23L. REMOVED LIGHT CORROSION AT SITE. REMOVED .003 MAT FROM .088 THICK RIB, WITH IN LIMITS PER SRM53-2-0 FIG 1F, TREATED PER SRM 51-1-8. FOUND RIB CRACKED. CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLER (707Oct 25, 2004 · N798UP · Doug DC871F · Fuselage Main, FrameSDR UPS04843517Fitting · crackedLONGERON 11R END FITTING CRACKED AT STA 680. REMOVED AND REPLACED CRACKED FITTING PER SRM 51-1-20D.Oct 25, 2004 · N798UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS04843510Fitting · crackedC1 LONGERON 19 RT END FITTING CRACKED AT STA 860. REMOVED AND REPLACED L19R END FITTING REF SRM 51-1-20D.Oct 25, 2004 · N798UP · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA060047SWeb · crackedDURING ROUTINE C-CHECK FOUND WEB CRACKED ST STATION 30 -X48. REMOVED DAMAGE. FABRICATED REPAIR DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR DOUBLER AND FASTENERS AT STATION 30 TO 33.5 AT -X48. IAW SRM 53-2-0, 51-1-4, 51-1-5, AND 51-1-8Oct 22, 2004 · N825BX · Doug DC871F · Fuselage Structure (General)SDR IXXA060046SWeb · crackedDURING ROUTINE C-CHECK FOUND WEB CRACKED ST STATION 30 -X48. REMOVED DAMAGE. FABRICATRED REPAIR DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR DOUBLER AND FASTENERS AT STATION 30 AND 33.5 AT -X48. IAW SRM 53-2-0, 51-1-4, 51-1-5, AND 51-Oct 22, 2004 · N825BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA0500240SSkin · corrodedDURING ROUTINE C-CHECK FOUND EXTERNAL FUSELAGE SKIN CORRODED FROM STATION 660 TO STATION 662 AT LONGERON 33 LEFT. REMOVED DAMAGED SKIN. FABRICATED FILLER, DOUBLER, AND TRIPLER. LOCATED DRILLED TRIMMED TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND NEW FASTOct 22, 2004 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA0500239SSkin · corrodedDURING ROUTINE C-CHECK FOUND EXTERNAL FUSELAGE SKIN FROM STATION 620 TO 630 AT LONGERONS 29 LEFT AND 30 LEFT. REMOVED DAMAGED SKIN AREA. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND NEW FASTENERS IAW COOOct 22, 2004 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR 872SJ005Finger Doubler · corrodedCARGO AREA RT SIDE STA 960 HAS CORROSION UNDER FINGER DOUBLER UNDER FLOORBOARD. GBAMC NR04182 -OPEN-Oct 22, 2004 · N872SJ · Doug DC871F · Fuselage Main, Plate/SkinSDR 872SJ007Structure · corrodedLT WW UPPER LT SIDE FWD AND AFT OF NR 6 FLOOR SUPPORT HAS CORROSION. GBAMC NR04178 -OPEN-Oct 22, 2004 · N872SJ · Doug DC871F · Fuselage Main, StructureSDR 872SJ004Floor Support · corrodedLT W/W LT SIDE UPPER, SECOND FLOOR SUPPORT HAS CORROSION ON LOWER SIDE. GBAMC NR04176 -OPEN-Oct 22, 2004 · N872SJ · Doug DC871F · Fuselage Miscellaneous StructureSDR 872SJ003Door · corrodedD-PIT, AFT BULKHEAD DOOR 645 CORRODED GBAMC NR#04172 CUT OUT DAMAGED MATERIAL ON D PIT DOOR AFT BULKHEAD DOOR 645 IAW DC-8 SRM 52-2-0 FIG 4 SHEET 2. FABRICATED DOUBLER PATCH OUT OF 7075T6 .032 AND INSTALLED DOUBLER PATCH ON D-PIT BULKHEAD DOOR IAW DC-8 SRM 52Oct 22, 2004 · N872SJ · Doug DC871F · Tail Cone DoorsSDR 872SJ001Skin · corrodedLAV ACCESS SERVICE PANEL HAS CORROSION UNDER PAINT GBAMC NR 04161 AND NR 04185 UPON INVESTIGSTION FOUND SKIN TO BE OUT OF LIMITS BELOW LIP ON ACCESS DOOR, REMOVED DAMAGED SKIN AREA OF 1.75X9.00 FABED FILLER,FABED FINGER DOUBLER FOR BACK, FAB DOUBLER FOR EXTERNOct 21, 2004 · N872SJ · Doug DC871F · Fuselage Main, Plate/SkinSDR 872SJ002Skin · corrodedA/C COMP AREA INTERIOR A/C OUTFLOW DUCT HAS CORROSION GBAMC NR 04160 CLEANED CORRISON ON INTERIOR A/C OUTFLOW DUCT PANEL IAW DC-8 SRM 51-1-8,CORRISON FOUND TO BE OUT OF LIMITS IAW DC-8 SRM 53-2-0. MATERIAL THICKNESS.130,MATERIAL LOSS .104 FABED DOUBLER IAW COTOct 21, 2004 · N872SJ · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA060084SIntercostal · crackedDURING ROUTINE CHECK, FOUND A CRACKED INTERCOSTAL FROM STATION 1140 TO STATION 1160 AT LONGERON 14 RT. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED INTERCOSTAL. FABRICATED NEW INTERCOSTAL, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW INTERCOSTAOct 20, 2004 · N825BX · Doug DC871F · Fuselage Miscellaneous Structure
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