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 UPS06848343Longeron · crackedINSPECTION TYPE:C2 LONGERON CRACKED AT STA 1734 L15R. REMOVED LONGERON SECTION 15R AT STA 1734 IAW SRM 53-02-02 FIG 10. FABRICATED AND INSTALLED LONGERON SECTION AT STA 1734 L15R IAW SRM 53-2-2 FIG 10, AND SRM 53-02-02-0 FIG 10Oct 13, 2006 · N755UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS06848329Longeron Splice · crackedINSPECTION TYPE:C2 STA 1260 L36 SPLICE FITTING CRACKED ON RT SIDE FACING FWD REMOVED AND REPLACED LONGERON SPLICE SECTION AND END FITTINGS FROM STA 1270-1350 L36 IAW SRM 51-1-20D, 51-3-2 AND SRM 51-3-0.Oct 13, 2006 · N755UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS06848322Fitting · crackedINSPECTION TYPE:C2 LONGERON END FITTING CRACKED AT STA 1760 L10L. REMOVED, AND REPLACED LONGERON END FITTING AT STA 1760 L10L IAW SRM 51-1-24, 51-1-21, AND SRM 51-1-20D.Oct 13, 2006 · N755UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS06848321Fitting · crackedINSPECTION TYPE:C2 CRACKED LONGERON END FITTING AT L33R FS 8. REMOVED AND REPLACED LONGERON END FITTING AT STA 8 L33R IAW SRM 51-1-20D, AND SRM 51-03-01-0, 51-01-20D-0.Oct 13, 2006 · N755UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS06848391Shear Web · corrodedINSPECTION TYPE:C2 HEAVY CORROSION ON PRESSURE WEB DOUBLER, STA 857, LT W/W, LBL 25. REPAIRED SHEAR WEB AT STA 857, XW=23, LBL 25 IAW SAA EA NR 008-5320-01 A0492, UPS RAA NR DC8-53-20600, BAC MSG NR 1-237059319, AND FAA FORM 8100-9.Oct 11, 2006 · N755UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS06848318Attach Fitting · crackedINSPECTION TYPE:C2 AFT PRESS BULKHD TO LONGERON ATTACH FITTING CRACKED AT STA 1766 L6R. REMOVED, FABRICATED, AND INSTALLED REPAIR ATTACH FITTING IAW DWG 5773844, AND SRM 51-1-20D AT STA 1766 L6R.Oct 11, 2006 · N755UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS06848317Fitting · crackedINSPECTION TYPE:C2 L34R AT STA 1690 HAS BULGE UNDER SPLICE END. REMOVED FASTENERS AT L34R STA 1690 UNDER SPLICE, NO CORROSION NOTED IAW SRM 51-1-21. FOUND SPLICE END CRACKED AT STA 1690 L34R. REMOVED AND REPLACED LONGERON SPLICE END AT STA 1690, L34R IAW SROct 11, 2006 · N755UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS06848445Angle · crackedINSPECTION TYPE:C2 RT HORIZ STAB UPPER BULLNOSE "L" ANGLE IS CRACKED, INBD END OF STAB NEXT TO FUSELAGE FWD OF FRONT SPAR. REMOVED AND REPLACED "L" ANGLE AND CAP ON RT HORIZ STAB UPPER BULL NOSE FWD OF FRONT SPAR IAW DWG 5654549, AND SRM 51-01-21, 51-03-00, 5Oct 10, 2006 · N755UP · Doug DC871F · Horizontal Stabilizer StructureSDR UPS06848332Attach Angle · crackedINSPECTION TYPE:C2 LT HORIZ STAB LWR AFT H-ANGLE HAS 6" CRACK FOR BANANA FAIRING ATTACHMENT. REMOVED H-ANGLE FROM LT HORIZ STAB LWR AFT BANANA FAIRING ATTACHMENT BEAM IAW SRM 51-03-00. FABRICATED AND INSTALLED BEAM ASSY AT LWR AFT LT HORIZ STAB BANANA FAIRINOct 10, 2006 · N755UP · Doug DC871F · Horizontal Stabilizer, Attach FittingsSDR UPS06848320Intercostal · crackedINSPECTION TYPE:C2 LT HORIZ STAB 2 CRACKS INBD END ON TEE ANGLE, FWD OF FRONT SPAR (PNL 64J). REMOVED AND REPLACED T-ANGLE FITTING, LWR HORIZ STAB L/E INTERCOSTAL FWD OF FRONT SPAR INSIDE PNL 64J IAW SRM 51-03-02-0, 51-1-21, AND SRM 51-1-20D.Oct 10, 2006 · N755UP · Doug DC871F · Horizontal Stabilizer StructureSDR UPS06848256Angle · crackedINSPECTION TYPE:C2 RT HORIZ STAB 2 CRACKS INBD END ON T-ANGLE, FWD OF FRONT SPAR, 9PNL 64J. REMOVED AND REPLACED T-ANGLE IAW SRM 51-01-21, 51-03-00 AND 51-1-20D.Oct 10, 2006 · N755UP · Doug DC871F · Horizontal Stabilizer Miscellaneous StructureSDR UPS06848255Skin · bulgedINSPECTION TYPE:C2 BULGING SKIN FS 465 L32L EXTERNAL FUSELAGE. CUT OUT DAMAGE. FABRICATED AND INSTALLED FILLER, DOUBLER AND FINGER DOUBLER IAW SRM 53-02-01 FIG 007, 53-04-01-0 FIG 002, 51-10-00-0 FIG 002, 51-1-21 AND 51-1-20D.Oct 10, 2006 · N755UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS06848222Battery Pack · malfunctionedEMERGENCY LIGHTING WILL NOT STAY ON WHEN TESTED. EMERGENCY BATT PACK REPLACED IAW AMM 33-50-01-2 AND EMERGENCY LIGHTING SYSTEM CK SERVICEABLE.Oct 10, 2006 · N715UP · Doug DC871F · Emergency LightingSDR UPS06848311Finger Doubler · corrodedINSPECTION TYPE:C1 FINGER DOUBLER UNDER FWD LT CORNER OF EPC RACK HAS 4 POPPED RIVETS AND CORROSION AT STA FS -5 LBL 60. REMOVED CORROSION AND FINGER DOUBLER AT STA -5 LBL60 IAW SRM 51-1-21. FABRICATED AND INSTALLED FINGER DOUBLER AT STA -5 LBL 60 IAW SRM 53Oct 7, 2006 · N772UP · Doug DC871F · Fuselage Main, StructureSDR UPS06848449Boss · out of limitsINSPECTION TYPE:C1 L/MLG RETRACT PIN BOSS REQUIRES BUSHING, MAX OD IS 1.800" ACTUAL MEASUREMENT IS 1.831". FABRICATED AND INSTALLED REPAIR BUSHING TO L/MLG RETRACT PIN BOSS BORE IAW SAA EA NR 008-3230-01-A0469 REV.A, UPS EO DC8-3230-25374-A, SB DC8-32-102, ADOct 6, 2006 · N772UP · Doug DC871F · Main Landing GearSDR UPS06848333Attach Angle · crackedINSPECTION TYPE:C2 UPPER SURFACE CLIP IS CRACKED AT XRS 139 STRINGER 1 AND 2 NR 2 ALT TANK. REMOVED AND REPLACED UPPER SURFACE CLIP AT XRS 139 STRINGER 1 AND 2 NR 2 ALT TANK IAW SRM 51-1-20D, AND SRM 51-3-2.Oct 6, 2006 · N755UP · Doug DC871F · Wing, Attach FittingsSDR UPS06848312Fitting · crackedINSPECTION TYPE:C1 STRINGER END FITTINGS FOR STRINGER 51 ARE CRACKED AT XRS 74 NR 3 MAIN TANK. REMOVED AND REPLACED 2 STRINGER END FITTINGS AT STA XRS 74 NR 3 MAIN TANK IAW SRM 51-1-20D, 51-03-02.Oct 6, 2006 · N772UP · Doug DC871F · Wing, Longeron/StringerSDR UPS06848310Stringer · crackedINSPECTION TYPE:C1 STRINGER 64 IS CRACKED BET XRS428 AND XRS463 NR 4 ALT REMOVED STRINGER 64 AND CLIP AT STA 428 IN NR 4 ALT TANK IAW SRM 51-01-20D. FABRICATED AND INSTALLED STRINGER IAW DWG 3644045, AND SRM 51-03-02, 51-1-20D AT STA XRS 428 AND XRS 463.Oct 6, 2006 · N772UP · Doug DC871F · Wing, Longeron/StringerSDR IXXA06SMN329SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP UPPER SKIN HAS NON STANDARD REPAIR AT STATION XW104.000. REMOVED EXISTING SKIN WITH NON STANDARD REPAIR. FABRICATED NEW SKIN (AL 2024 T3 0.040”). CLEANED, TREATED AND PRIMED AREA AND NEW SKIN INTERNOct 6, 2006 · N825BX · Doug DC871F · Trailing Edge FlapsSDR UPS06848204Linkage · stuckPILOTS SLIDING WINDOW WILL NOT OPEN. ADJUSTED PILOT SLIDING WINDOW UPPER ACTUATING LINKAGE ROD PER AMM 56-10-03-56, OPS OK.Oct 6, 2006 · N752UP · Doug DC871F · Flight Compartment WindowsSDR UPS06848492Skin · dentedINSPECTION TYPE:C2 TRANSFERRED FROM LP 325899/2: REF D-308181, FUSELAGE SKIN DENT FWD OF PIT 32 DOOR CUT OUT. REPAIRED FUSELAGE SKIN DENT FWD OF PIT 32 DOOR CUT OUT LWR FWD DOOR CORNER IAW SAA EA# 008-5320-01-A0477, UPS EO DC8-5330-25373-A, AND FAA FORM 8100-Oct 5, 2006 · N755UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS06848313Fitting · crackedINSPECTION TYPE:C1 CRACK BETWEEN UPPER VERTICAL BOLTS IN CUSP/FLOORBEAM FITTING A-PIT STA 340, L21R. REMOVED FITTING AT CUSP/FLOORBEAM IN A-PIT STA 340 L21R IAW SRM 51-3-0, AND SRM 51-1-21. FABRICATED AND INSTALLED FITTING, T-ANGLE AND INTERCOSTAL AT STA 340Oct 5, 2006 · N772UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS06848308Longeron Splice · crackedINSPECTION TYPE:C1 CRACKED LONGERON STA 1746 L16L. REMOVED AND REPLACED LONGERON SPLICE AT STA 1766-1738 L16L IAW SRM 51-01-21-0, AND SRM 53-02-02-0 FIG 10.Oct 5, 2006 · N772UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS06848307Skin · crackedINSPECTION TYPE:C1 MISSING RIVETS, SKIN CRACKED ON RT ELEVATOR UPPER SKIN STA XE 84.96. REMOVED AND REPLACED SKIN ON RT ELEVATOR UPPER STA XE 84.96 IAW SRM 55-2-1, AND SRM 55-2-1 FIG 8.Oct 5, 2006 · N772UP · Doug DC871F · Elevator, Plate/SkinSDR UPS06848205Slide · unsecureESCAPE SLIDE NOT SECURED TO DOOR ON ONE SIDE. RESECURED ESCAPE SLIDE TO MAIN ENTRY DOOR AS REQUIRED.Oct 5, 2006 · N755UP · Doug DC871F · Escape SlideSDR UPS06848402Longeron · crackedINSPECTION TYPE:C1 CRACKED LONGERON STA 1748 L15L BEHIND CANTED FRAME REMOVED AND REPLACED LONGERON SPLICE SECTION AT STA 1766-1742 L15L IAW SRM 53-02-02-0 FIG 10, AND SRM 53-05-02-0.Oct 4, 2006 · N772UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS06848306Longeron Splice · crackedINSPECTION TYPE:C1 CRACKED LONGERON STA 1734 L15R. REMOVED AND REPLACED LONGERON SPLICE AT STA 1734 L15R IAW SRM 51-1-21, AND SRM 51-1-20D.Oct 4, 2006 · N772UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS06848305Longeron · crackedINSPECTION TYPE:C1 CRACKED LONGERON STA 1754 L14L BEHIND CANTED FRAME. REMOVED LONGERON SECTION FROM STA 1766-1746 L14L IAW SRM 51-01-21-0. FABRICATED AND INSTALLED LONGERON AND REPAIR SPLICES IAW SRM 53-05-02-0, AND SRM 53-02-02.Oct 4, 2006 · N772UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS06848304Fitting · crackedINSPECTION TYPE:C1 CRACKED LONGERON END FITTING STA 857 L6R. REMOVED AND REPLACED LONGERON END FITTING AT STA 857 L6R IAW SRM 51-1-21, AND SRM 51-1-20D.Oct 4, 2006 · N772UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS06848303Fitting · crackedINSPECTION TYPE:C1 CRACKED LONGERON END FITTING STA 902 L5R. REMOVED AND REPLACED LONGERON END FITTING AT STA 902 L5R IAW SRM 51-03-02-0, AND SRM 51-01-23-0.Oct 4, 2006 · N772UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS06848188Window · inoperativeCAPTAIN'S SLIDING WINDOW WOULD NOT OPEN. COMPLIED W/ALERT K 134429 REGARDING CAPTAIN & F/O'S CLEARVIEW WINDOW IAW WAN 1166862 & ALERT REPORT PGS. 1 & 2. NRC'S 962085 & 962041 GENERATED.Oct 4, 2006 · N755UP · Doug DC871F · Flight Compartment WindowsSDR UPS06848175Line · leakingDURING CLIMB, LOST MAIN SYS HYD PRES AND QTY TO AUX POS. RAN "LOSS OF HYD FLUID OR PRES" CK LIST. LANDED W/FULL FLAPS ON AUX PUMP. FOUND NR 3 ENG PRESS LINE CHAFED THROUGH. REMOVED AND REPLACED LINE AND CLAMP LEAK CK GOOD REF LP 625876/ITEM 2/3.Oct 3, 2006 · N702UP · Doug DC871F · Hydraulic System, MainSDR UPS06848334Skin · corrodedINSPECTION TYPE:C2 CORROSION ON EXTERNAL SKIN MARKER BEACON ANTENNA MATING SURFACE STA 660 L35L. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-2-0 AT STA 660 L35L. REPAIRED FUSELAGE SKIN AT STA 660 L35L IAW SAA EA NR 008-5320-01-A0461, UPS RAA DOct 1, 2006 · N755UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS06848099Skin · delaminatedRT WING SPOILER AT XRS 247 TO 351 HAS TEAR AT RT. MID HINGE ON TOP AND WORN THIN UNDERNEATH NR 4 SPOILER. INSTALLED NEW NR 4 SPOILER PER MM 27-61-01-2 TO STEP B6. INSTALLED IAW MM 27-61-01-2. OPS CHECK NORMAL.Sep 29, 2006 · N752UP · Doug DC871F · SpoilersSDR UPS06848092Battery Pack · dischargedFOUND EMERGENCY LIGHT BATTERY PACK DEAD ON PRE-FLIGHT. EMERGENCY LIGHT BATTERY PACK REPLACED IAW AMM 33-50-01-2 AND SYSTEM CHECK SERVICEABLE.Sep 28, 2006 · N851UP · Doug DC871F · Emergency LightingSDR IXXA06SMN320SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND NR 4 ALTERNATE TANK CRACKED AT STATION XW485.000, CONFIRMED WITH NDT. REMOVED FASTENERS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND. FABRICATED REPAIR PARTS. CLEANED TREATED AND PSep 25, 2006 · N825BX · Doug DC871F · Wing, Plate/SkinSDR IXXA06SMN321SFitting · crackedDURING ROUTINE C-CHECK INSPECTION FOUND FITTING CRACKED AT STA 1212.000 LONGERON 29 RT. REPLACED FITTING AT STA 1212.000 LONGERON 29 RT. IAW SRM 51-1-20D.Sep 25, 2006 · N825BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA06SMN323SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT ELEVATOR UPPER SKIN HAS NON STANDARD REPAIR FROM STATION XE116.000 TO STATION XE79.000. REMOVED SKIN WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKIN AND FINGER DOUBLER. BONDED BOTH PARTS WITH HYSOL IAW DSep 25, 2006 · N825BX · Doug DC871F · Elevator, Plate/SkinSDR IXXA06SMN325SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING OUTBOARD FLAP LEADING EDGE UPPER SKIN WITH NON STANDARD REPAIR AT STATION XF211.000. REMOVED SKIN WITH NON STANDARD REPAIR. FABRICATED NEW SKIN. CLEANED TREATED AND PRIMED AREA AND NEW SKIN INTERNAL SURFACSep 25, 2006 · N825BX · Doug DC871F · Trailing Edge FlapsSDR IXXA06SMN326SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION FOUND RIGHT WING OUTBOARD FLAP UPPER SKIN WITH NON STANDARD REPAIR AT STATION XF445.000. REMOVED SKIN WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKIN AND DOUBLER. BONDED BOTH PARTS WITH HYSOL. CLEANED, TREATED AND PSep 25, 2006 · N825BX · Doug DC871F · Trailing Edge FlapsSDR IXXA06SMN327SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING OUTBOARD FLAP UPPER SKIN WITH NON STANDARD REPAIR AT STATION XF360.000. REMOVED SKIN WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKIN, AND DOUBLER. BONDED BOTH PARTS WITH HYSOL. CLEANED, TREATED ANDSep 25, 2006 · N825BX · Doug DC871F · Trailing Edge FlapsSDR IXXA06SMN319SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING INBOARD AILERON LEADING EDGE SKIN CRACKED AT STATION XD525.000. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN INTERNAL SURFACE. APPLIED SEALANT TO FAYING SURFACESep 25, 2006 · N825BX · Doug DC871F · Aileron Control SystemSDR UPS06848254Fitting · crackedINSPECTION TYPE:C3 LONGERON END FITTING CRACKED AT STA 70 L32R FWD SIDE. REMOVED AND REPLACED LONGERON END FITTING IAW SRM 51-1-21 AND 51-1-20 D.Sep 25, 2006 · N708UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA06SMN328SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT INBOARD FLAP UPPER SKIN HAS NON STANDARD REPAIR AT STATION XW105.000. REMOVED EXISTING SKIN WITH NON STANDARD REPAIR. FABRICATED NEW SKIN (AL 2024 T3 0.050”), AND DOUBLER (AL 2024 T3 0.032”). BONDED SKIN AND DOSep 25, 2006 · N825BX · Doug DC871F · Trailing Edge FlapsSDR IXXA06SMN318SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND EXISTING DOUBLER IMPROPER AT STATION 600.000 LONGERON 30 RIGHT. REMOVED EXISTING DOUBLER. TRIMMED OUT DAMAGED AREA. FABRICATED EXTERNAL REPAIR DOUBLER (AL 7075 T6 0.125), INTERNAL FINGER DOUBLER (AL 7075 T6 0.050”), Sep 25, 2006 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS06848095Fitting · crackedINSPECTION TYPE:C3 FITTING CRACKED AT RT STA 70 L30R. REMOVED AND REPLACED FITTING IAW SRM 51-3-0,51-1-20D AND 51-3-2.Sep 25, 2006 · N708UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS06848199Fitting · crackedINSPECTION TYPE:C3 C-PIT STA 1160 INSIDE OF DOOR, SPYDER FITTING IS CRACKED AT THE BOLT. REMOVED CRACKED SPYDER FITTING AT STA 1160 IAW SRM 51-1-21, FABRICATED AND INSTALLED SPYDER FITTING AT STA 1160 INSIDE OF DOOR IAW SRM 51-3-0, 51-1-21, AND DWG 3754025Sep 24, 2006 · N708UP · Doug DC871F · Cargo/Baggage DoorsSDR UPS06848193Finger Doubler · corrodedINSPECTION TYPE:C3 STA 440-460 L34L-L34R FUSELAGE DOUBLER AND FINGER DOUBLER HAVE CORROSION. REMOVED FUSELAGE SKIN DOUBLER AND FINGER DOUBLER AT STA 440-460 L34L-L34R IAW SRM 53-2-0. FABRICATED AND INSTALLED SKIN DOUBLER AND FINGER DOUBLER AT STA 440-46- L34Sep 23, 2006 · N708UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS06848191Stringer Splice · crackedINSPECTION TYPE:C3 STA 440 TO STA 460 L36 SPLICE FITTING IS CRACKED. REMOVED AND REPLACED SPLICE FITTING AT STA 440-460 L36 IAW SRM 51-1-20D, AND SRM 51-03-02-0.Sep 23, 2006 · N708UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS06848220Doubler · corrodedINSPECTION TYPE:C3 AFTER SKIN REMOVAL A/C BAY FOUND INTERNAL DOUBLER CORROSION OUT OF LIMITS STA 8-70 BETWEEN L30L-32L. REMOVED INTERNAL DOUBLER FROM STA 8-70 L30L-32L IAW SRM 51-1-21. FABRICATED AND INSTALLED INTERNAL DOUBLER AT STA 8-70 L30L-32L IAW SRM 53Sep 22, 2006 · N708UP · Doug DC871F · Fuselage Main, Plate/Skin
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