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 UPS02837895Fitting · corrodedINSPECTION TYPE:C1 MAIN CARGO DOOR JAMB NR 7 LATCH SPOOL FITTING HAS LOWER JAMB FITTINGS FWD AND AFT OF LATCH SPOOL FITTING HAVE INTERGRANULAR CORROSION AT STA 280 LONG 21L. REMOVED AND REPLACED FITTINGS IAW DWG 4773295 AND SRM 51-3-0, 51-1-20D.Mar 6, 2002 · N706UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02837878Door Frame · crackedINSPECTION TYPE:C1 L1 DOOR UPPER FWD PAN IS CRACKED IN CORNER, STA 25 LONG 10L. CUT OUT CRACK, NDT VERIFIED NO CRACK. FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 1D.Mar 6, 2002 · N706UP · Doug DC871F · Fuselage Main, StructureSDR UPS02837873Skin · crackedINSPECTION TYPE:C1 REPAIR AT STA 280 FWD LOWER CORNER OF A PIT DOOR CUTOUT IS A CATEGORY D PER EO DC8-5330-12800 AND SKIN IS CRACKED BETWEEN LONG 31R AND 32R. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 53-2-0 FIG 22.Mar 6, 2002 · N706UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02837905Fitting · crackedINSPECTION TYPE:C1 STA 822 LONG 12R FRAME FITTING IS CRACKED AT EMERGENCY EXIT FRAME, AFT FITTING. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 4751643 AND SRM 51-1-20D, 51-3-0.Mar 5, 2002 · N706UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02837915Skin · crackedINSPECTION TYPE:C1 R-2 DOOR UPPER AFT CORNER FUSELAGE SKIN, INTERNAL DOUBLER, AND LONG 11R ARE CRACKED AT STA 1654 AND LONG 11R. CUT OUT CRACKED AREA ON SKIN AND INTERNAL DOUBLER, STOPDRILLED CRACK ON LONG 11R. NDT VERIFIED NO CRACKS AT STOPDRILL AND CUTOUT.Mar 4, 2002 · N706UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02837909Rib · crackedINSPECTION TYPE:C1 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 822.5. STOP DRILLED CRACK, NDT VERIFIED CRACK IS TERMINATED. FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 57-2-0 FIG 2.Mar 4, 2002 · N706UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS02837906Skin · crackedINSPECTION TYPE:C1 FUSELAGE SKIN CRACKED AT L-1 DOOR FWD UPPER CORNER STA 25 BETWEEN LONG 10L-11L. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SRM 53-2-0 FIG 15.Mar 4, 2002 · N706UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02837875Skin · crackedINSPECTION TYPE:C1 SKIN CRACKED STA 160 LONG 10R-11R. REMOVED EXISTING, CUTOUT CRACKED AREA, NDT VERIFIED NO CRACKS. AT CUTOUT, FABRICATED AND INSTALLED REPAIR FILLER, AND DOUBLERS IAW SRM 53-2-0 FIG 14.Mar 4, 2002 · N706UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02837992Splice · crackedINSPECTION TYPE:C1 STA 388 LONG 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754473, AND SRM 53-1-0, 51-1-20D.Mar 3, 2002 · N707UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02837917Stringer · crackedINSPECTION TYPE:C1 LEFT WING STRINGER 66 IS CRACKED AT APPROX XRS 370 AT FRONT SPAR. REMOVED STRINGER 66 SECTION, AND END FITTING, FABRICATED AND INSTALLED STRINGER, END FITTING, AND SPLICES IAW DWG 5751406, AND SRM 57-2-2 FIG 3D.Mar 3, 2002 · N707UP · Doug DC871F · Wing, Longeron/StringerSDR UPS02837901Rib · crackedINSPECTION TYPE:C1 LT WING T/E UPPER RIB IS CRACKED AT XRS 247. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 57-2-0 FIG 2.Mar 3, 2002 · N706UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS02837860Splice · crackedINSPECTION TYPE:C STRINGER 51 SPLICE FITTING CRACKED APPROX 10 INCHES OUTBOARD OF XRS74, LT WING. REMOVED AND REPLACED SPLICE FITTING PER SRM 51-1-20D AND 51-3-0.Mar 3, 2002 · N707UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS02837859Splice · crackedINSPECTION TYPE:C STRINGER 51 SPLICE CRACKED APPROX 12 INCHES OUTBOARD OF XRS 74, NR 3 ALT TANK, RT WING, FIRST STRINGER FWD OF REAR SPAR CAP. REMOVED AND REPLACED STRINGER 51 SPLICE PER SRM 51-1-20D AND 51-3-0.Mar 3, 2002 · N707UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS02837754Battery Pack · dischargedINSPECTION TYPE:N/A, A/C FAILS STANDBY POWER CHECK (NO EMERGENCY LIGHTS). REPLACED EMERGENCY BATTERY PACK, EMERGENCY LIGHTS OPS CHECK GOOD.Mar 3, 2002 · N702UP · Doug DC871F · Emergency LightingSDR UPS02837907Skin · crackedINSPECTION TYPE:C1 FUSELAGE SKIN IS CRACKED AT L-2 DOOR LOWER AFT CORNER STA 1660 BETWEEN LONG 20L-21L. CUT OUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SRM 53-2-0 FIG 18.Mar 1, 2002 · N706UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02837902Doubler · crackedINSPECTION TYPE:C23 MOULD-LINE DOUBLER AT NR 1 PYLON HAS PREVIOUSLY INSTALLED REPAIR DOUBLER ON THE I/B SIDE THATS CRACKED AT FASTENER HOLE. REMOVED DOUBLER, PERFORMED HFEC AND BOLT HAVE HFEC IAW NDT SPM 06-10.001 AND 06-10.003. CRACKS PRESENT IN 5 EA HOLES,Mar 1, 2002 · N748UP · Doug DC871F · Wing, Plate/SkinSDR UPS02837884Web · crackedINSPECTION TYPE:C23 RG I/B FLAP CLOSEOUT WEB CRACKED AROUND BEADED AREA. REMOVED AND REPLACED IAW REO G08529.Mar 1, 2002 · N748UP · Doug DC871F · Trailing Edge FlapsSDR UPS02837874Longeron · corrodedINSPECTION TYPE:C1 BELLY SKIN BULGING APPROX 2 FT FWD TO THE RIGHT OF THE VHF ANTENNA, NO CORROSION FOUND. REMOVED FASTENER TO INSPECT AND REPLACED WITH BLIND. FOUND LONG 36 CORRODED BEYOND LIMITS STA 1260-1350. REMOVED AND REPLACED LONGERON SECTION IAW DWGMar 1, 2002 · N706UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS02837824Web · crackedINSPECTION TYPE:C23 LT WING I/B FLAP I/B END CLOSEOUT WEB IS CRACKED AND HAS LOOSE FASTENERS. REMOVED AND REPLACED WEB IAW REO G08529.Mar 1, 2002 · N748UP · Doug DC871F · Trailing Edge FlapsSDR UPS02838041Intercostal · crackedINSPECTION TYPE:C1 FWD ACCESSORY COMPT AT FS 660 RBL 12 MAIN CABIN FLOOR INTERCOSTAL IS CRACKED. FABRICATED DOUBLER IAW DC8 SRM 53-2-0, INSTALLED IAW DC8 SRM 51-1-21 & 51-1-20D.Feb 28, 2002 · N709UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02837994Skin · crackedINSPECTION TYPE:C1 REPAIR AT AFT UPPER CORNER OF D-PIT DOOR IS CATEGORY D BECAUSE OF SCREWS AND BLIND FASTENERS PER EO DC8-5330-12800, AND HAS CRACKED SKIN STA 1440 LONG 23R APPROX. REMOVED EXISTING REPAIR, CUT OUT DAMAGED AREA. NDT VERIFIED NO CRACKS AT CUTFeb 28, 2002 · N707UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02837889Fitting · corrodedINSPECTION TYPE:C23 AFT PIT FS 1200 ZEE FITTING AT L34R - L33R IS CORRODED. REMOVED CORRODED ANGLE LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24, INSTALLED ZEE FITTING REPAIR ANGLE IAW DC8 SRM 51-1-20D.Feb 28, 2002 · N748UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02837851Structure · crackedINSPECTION TYPE:C LT AFT ENTRY DOOR STRUCTURE CRACKED AT LOWER HINGE CUTOUT. STOP DRILLED CRACK PER SRM 52-2-0 FIG 6. NDT VERIFIED CRACK TERM PER SPM 06-10-01.001. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 52-2-0 FIG 2.Feb 28, 2002 · N707UP · Doug DC871F · Passenger/Crew DoorsSDR UPS02837730Finger Doubler · corrodedINSPECTION TYPE:PFLT CORROSION UNDER FINGER DOUBLER AT STA 24 LONGERON 31R AT E/E COMPARTMENT. INSPECTED OUTER SKIN FOR CORROSION LOSS USING LOW FREQUENCY E/E PER NDT STANDARD PRACTICE MANUAL 06-10-02 PROCEDURE NR 2 LOSS OF SKIN INDICATED AT 10 PERCENT C/W EOFeb 27, 2002 · N718UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02837775Fitting · crackedINSPECTION TYPE:C23 AFT PIT BILGE Z-FITTING CRACKED I/B OF L34R AT STA 1200. INSTALLED NEW FITTING AND SPLICES IAW DC8 SRM 53-2-0.Feb 26, 2002 · N748UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02837770Longeron · crackedINSPECTION TYPE:C LOWER FUSELAGE SKIN BULGING AT L36, STA 380 TO 400. REMOVED SPLICE FITTING AT L36, STA 380 TO 400. REMOVED CORROSION ON L36 PER SRM 51-1-8. NO CORROSION FOUND ON SKIN. NDT REVEALED CRACK ON L36 FROM STA 390-394. FABRICATED AND INSTALLED Feb 26, 2002 · N707UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS02837735Longeron · corrodedINSPECTION TYPE:C L22R CORRODED BEYOND LIMITS. REMOVED L22R FROM STA 80 TO 130 IAW SRM 51-1-20D AND 51-1-21. INSTALLED LONGERON PER SRM 51-1-20D.Feb 26, 2002 · N707UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS02837855Longeron · corrodedINSPECTION TYPE:C L34R CORRODED BEYOND LIMITS AT STA 1220. REPAIRED PER DHSK 707-819 AND SRM 53-2-2 FIG 10.Feb 25, 2002 · N707UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS02837746Finger Doubler · corrodedINSPECTION TYPE:C FINGER DOUBLER CORRODED BEYOND LIMITS AT STA 1350 L31L TO L31R. FABRICATED AND INSTALLED DOUBLER PER SRM 51-1-21 AND 51-1-20D.Feb 25, 2002 · N707UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02837738Longeron · crackedINSPECTION TYPE:C L34L CRACKED AND CORRODED BEYOND LIMITS AT STA 1270. REMOVED L34L FROM STA 1270 TO STA 1350 PER SRM 51-1-20D. INSTALLED NEW LONGERON PER SRM 51-1-20D.Feb 25, 2002 · N707UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS02837737Longeron · crackedINSPECTION TYPE:C L35L CORRODED AND CRACKED AT STA 1270. REMOVED AND REPLACED DAMAGED LONGERON 35L FROM STA 1270 TO STA 1350 IAW SRM 51-1-20D.Feb 25, 2002 · N707UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS02837733Intercostal · damagedINSPECTION TYPE:C HOLES IN INTERCOSTAL BEND RADIUS AT STA 1100-1120 L33R TO L34R. FABRICATED REPLACEMENT INTERCOSTAL PER DAC DWG 9754949. INSTALLED SAME PER SRM 51-1-20D.Feb 25, 2002 · N707UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02837732Intercostal · damagedINSPECTION TYPE:C INTERCOSTAL HAS HOLES IN RADIUS AT STA 1100-1120, L33R-L34R. FABRICATED REPLACEMENT INTERCOSTAL PER DAC DWG 9754949. INSTALLED IAW SRM 51-1-20D.Feb 25, 2002 · N707UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02837817Shear Tie · brokenINSPECTION TYPE:C1 SHEAR TIE BROKEN AT STA 1140 BETWEEN LONG 34L TO 35L. REMOVED, FABRICATED, AND REPLACED SHEAR TIE SECTION IAW SRM 53-4-1, 51-1-20D, 53-1-0.Feb 24, 2002 · N707UP · Doug DC871F · Fuselage Main, StructureSDR UPS02837748Finger Doubler · crackedINSPECTION TYPE:C FINGER DOUBLER CRACKED AT STA 1329 L31R. FABRICATED AND INSTALLED DOUBLER PER SRM 51-1-21 AND 51-1-20D.Feb 24, 2002 · N707UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02837743Longeron · crackedINSPECTION TYPE:C L34R CRACKED AT STA 1350. REMOVED DAMAGED LONGERON FROM STA 1290 TO STA 1350 PER SRM 51-1-20D. INSTALLED REPLACEMENT LONGERON IAW SRM 51-1-20D.Feb 24, 2002 · N707UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS02837742Angle · corrodedINSPECTION TYPE:C LONGERON SUPPORT T-ANGLE HEAVILY CORRODED AT STA 1250 BETWEEN L33R AND L34R. REMOVED CORRODED ANGLE PER SRM 51-1-21. FABBRICATED REPLACEMENT AND INSTALLED PER SRM 51-1-20D.Feb 24, 2002 · N707UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02837741Finger Doubler · crackedINSPECTION TYPE:C FINGER DOUBLER CRACKED AT STA 1130 TO 1250 AT L31L. REMOVED DAMAGED FINGER DOUBLER FROM STA 1130 TO 1250 IAW SRM 51-1-20 D. FABRICATED DOUBLER AND INSTALLED PER SRM 53-4-1 FIG 51.Feb 24, 2002 · N707UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02837729Fabric · frayedINSPECTION TYPE:PFLT EMERGENCY ESCAPE SLIDE GIRT BAR HAS FABRIC ATTACHMENT FRAYING. REMOVED AND REPLACED SLIDE.Feb 24, 2002 · N772UP · Doug DC871F · Escape SlideSDR UPS02837891Skin · damagedINSPECTION TYPE:C L1 DOOR UPPER FWD CORNER, AND UPPER AFT CORNER REPAIRS DO NOT CONFORM TO EO DC8-5330-12073F. REPAIRED PER UPS EO DC8-5330-16381-A, DHSK707-694.Feb 23, 2002 · N707UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02837736Skin · crackedINSPECTION TYPE:C LOWER AFT CORNER OF R1 DOOR CUTOUT REQUIRES REPAIR IAW SRM 53-2-0 FIG 14. REMOVED EXISTING DOUBLER PER SRM 51-1-20D. CUT OUT DAMAGE, NDT VERIFIED ALL DAMAGE REMOVED PER NDT SPM 06-10-01. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-2-0Feb 23, 2002 · N707UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02837918Angle · crackedINSPECTION TYPE:C1 L-1 DOOR LOWER FWD CORNER SUPPORT ANGLE IS CRACKED AT STA 25 AT LONG 21L LOWER SIDE. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 5597646, AND SRM 51-1-20D, 51-1-21.Feb 22, 2002 · N707UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02837854Doubler · corrodedINSPECTION TYPE:C LOWER FUSE SKIN PILLOWED AT STA 80 L21R. FOUND L22R AND FINGER DOUBLER CORRODED BEYOND LIMITS. REMOVED DOUBLER SECTION FROM STA 70-80. FABRICATED REPLACEMENT AND INSTALLED PER SRM 51-1-21 AND 51-1-20D.Feb 22, 2002 · N707UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02837852Door Frame · crackedINSPECTION TYPE:C R2 DOOR FRAME UPPER AFT CORNER CRACKED NEAR STA 1655, L11. REPAIRED PER DHSK707-642.Feb 22, 2002 · N707UP · Doug DC871F · Fuselage Main, StructureSDR UPS02837768Door Frame · crackedINSPECTION TYPE:C CRACK DETECTED BY XRAY AT UPPER AFT CORNER OF L2 DOOR FRAME APPROX STA 1657. REMOVED DOUBLERS PER SRM 51-1-21 AND 51-1-20D. LOCATED AND REMOVED CRACKED FILLER BETWEEN SKIN AND DOUBLER. NDT C/W PER SPM 06-10-01.00 1 NO CRACKS NOTED ON SKIN Feb 22, 2002 · N707UP · Doug DC871F · Fuselage Main, StructureSDR UPS02837747Longeron · crackedINSPECTION TYPE:C L7R CRACKED AT STA 520. REMOVED L7R FROM STA 510 TO STA 530 PER SRM 53-2-2 FIG 4C. FABRICATED LONGERON AND INSTALLED PER SRM 53-2-2 FIG 10.Feb 22, 2002 · N707UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS02837893Web · damagedINSPECTION TYPE:C LT CUSP REPAIR DOES NOT CONFORM TO SRM AT LT STA 1328. REMOVED AND REPLACED LT CUSP EXTRUSION FROM STA 1190 TO STA 1370 PER SRM 53-2-5 FIG 15.Feb 21, 2002 · N707UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02837888Skin Panel · crackedINSPECTION TYPE:C23 LT HORIZONTAL STAB UPPER O/B FWD SKIN PANEL CRACKED AT 2ND BOLT IN AFT DIRECTION. REMOVED AND REPLACED HORIZ STAB PLANK IAW DAC SB55-16 AND DAC DWG SRO 8 550001.Feb 21, 2002 · N748UP · Doug DC871F · Horizontal Stabilizer, Plate/SkinSDR UPS02837887Door Frame · crackedINSPECTION TYPE:C23 L2 DOOR CORNER UPPER AFT SHOWS CRACK INDICATION IN REPAIR AREA GOING TO FASTENER HOLE. REMOVED EXISTING DOUBLERS, ROUTED OUT CRACK, FABBED AND INSTALLED REPAIR DOUBLERS IAW DC8 SRM 53-2-0 FIG 18.Feb 21, 2002 · N748UP · Doug DC871F · Fuselage Main, StructureSDR UPS02837858Skin · corrodedINSPECTION TYPE:C CORROSION FOUND ON INTERIOR OF BELLY SKIN, 1050-1350, L31L TO L31R. REMOVED AND REPLACED AFT BELLY SKIN AND C-PIT DOOR INTERNAL DOUBLER PER SRM 51-1-21 AND 51-1-20D.Feb 21, 2002 · N707UP · Doug DC871F · Fuselage Main, Plate/Skin
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