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 UPS08852741Stringer Clip · crackedINSPECTION TYPE-C2, L6R ATTACH CLIP CRACKED AT APB, STA 1766, MAIN CABIN. REMOVED, FABRICATED AND INSTALLED REPLACEMENT CLIP IAW DWG 5773844 AND 5191-20D.Jul 1, 2008 · N752UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS08852739Frame · gougedINSPECTION TYPE-C2, GOUGE ON THE STA 360 LT FRAME JUST ABOVE THE UPPER SURFACE OF THE L21. REPAIRED GOUGE IAW SRM 53-02-00-0 FIG 001F.Jul 1, 2008 · N752UP · Doug DC871F · Fuselage Main, FrameSDR UPS08852738Frame · gougedINSPECTION TYPE-C2, GOUGE ON THE STA 702.875 LT FRAME JUST ABOVE THE UPPER SURFACE OF CUSP EXTRUSION(LONGERON 210 IN MAIN CABIN). DRILLED HOLE TO REMOVE DAMAGE AND PLUGGED HOLE. IAW SRM 53-02-00 FIG 0 01F.Jul 1, 2008 · N752UP · Doug DC871F · Fuselage Main, FrameSDR UPS08852730Torque Box · damagedINSPECTION TYPE-C2, MAIN CABIN, RT AFT SERVICE DOOR FRAME (TORQUE BOX) WEB HAS DOUBLE DRILLED AND EXTRA HOLES STA 1660 L-19R. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-02-00-0 FIG 001D, 5 1-01-21.Jul 1, 2008 · N752UP · Doug DC871F · Fuselage Main, StructureSDR UPS08852902Doubler · crackedINSPECTION TYPE-C2, EXTERIOR FUSELAGE HOLD OPEN RECEPTACLE FOR L1 DOOR HAS CRACKED REPAIR DOUBLER. REMOVED, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM, 51-1-8, 51-1-5, 51-3-0.Jun 30, 2008 · N752UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS08852899Seat Track · wornINSPECTION TYPE-C2, OBSERVERS FWD SEAT TRACK HAS ELONGATED HOLES REMOVED AND REPLACED SEAT TRACK IAW, SRM, 51-3-2, 51-1-8, 51-3-0.Jun 30, 2008 · N752UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS08852893Doubler · crackedINSPECTION TYPE-C2, POSSIBLE CRACK IN RADIUS OF REPAIR DOUBLER ON BOTTOM OF J-BEAM, APB, 60 COMPT. STA 1766 BL0. REMOVED CRACKED DOUBLER,FABBED AND INSTALLED REPAIR DOUBLER IAW, SRM. 51-1-8, 53-2-5, 51-1-24, 51-1-20D, 51-3-1.Jun 30, 2008 · N752UP · Doug DC871F · Fuselage Main, StructureSDR UPS08852791Stringer · crackedINSPECTION TYPE-C2, L 17R CRACKED UNDER END FITTING , STA. 1766-1772, 60 COMPT. REMOVED AND INSTALLED NEW END FITTING IAW SRM, 51-1-8, 51-3-0, 53-5-1 FIG.F.Jun 30, 2008 · N752UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS08852788Skin · dentedINSPECTION TYPE-C2, FUSELAGE SKIN AROUND TAIL-STAND HANGER FIN IN VERY POOR CONDITION, NUMEROUS DENTS, SKIN DEFORMED,PUSHED IN, DAMAGED REPAIR DOUBLER, BAD PAINT STA. 1870-1885. REMOVED AND INSTALLED REPAIR DOUBLER IAW SRM,51-1-20 FIG.45, 51-1-8, 5 2-3-0 FIG.Jun 30, 2008 · N752UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS08852757Seat Track · wornINSPECTION TYPE-C2, F/O'S BOTH LT AND RT SEAT TRACKS HAVE ELONGATED HOLES. REMOVED AND REPLACED SEAT TRACKS IAW SRM, 51-1-20D, 51-1-24, 51-3-1.Jun 30, 2008 · N752UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS08852753Shear Tie · crackedINSPECTION TYPE-C2, LARGE SHEER TIE BRACKET CRACKED AT LT END, 60 COMPARTMENT CEILING STA, 1800,L3L. REMOVED AND REPLACED SHEER TIE IAW SRM 51-1-8, 53-2-0 FIG F ,51-1-20D.Jun 30, 2008 · N752UP · Doug DC871F · Fuselage Internal Mounting StructureSDR UPS08852744Seat Track · damagedINSPECTION TYPE-C2 F/E'S AFT SEAT TRACK HAS ELONGATED HOLES. REMOVED AND REPLACED F/E'S AFT SEAT TRACK IAW SRM 51-01-24.Jun 30, 2008 · N752UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS08852743Seat Track · damagedINSPECTION TYPE-C2 CAPT BOTH LT AND RT SEAT TRACKS HAVE ELONGATED HOLES. REMOVED AND REPLACED CAPT'S LT AND RT SEAT TRACKS IAW SRM 51-01-24 AN AND 51-01-20D.Jun 30, 2008 · N752UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS08852749Fitting · gougedINSPECTION TYPE-C2, LT WING FLAPWELL FITTING BENT AND GOUGED BELOW FLAP STA 98 ACTUATOR. REMOVED AND INSTALLED FITTING AT FLAP STA 98 IAW SRM 51-3-0, 51-1-8, 5 1-3-1.Jun 29, 2008 · N752UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS08852737Rib · crackedINSPECTION TYPE-C2, AFT END OF RIB CRACKED IN RT HORIZ STAB L/E STA. XFS 47.5. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 5 1-3-02, 55-02-00 FIG 2.Jun 29, 2008 · N752UP · Doug DC871F · Horizontal Stabilizer, Spar/RibSDR UPS08852731Seat Track · corrodedINSPECTION TYPE-C2, MCC FLOOR SEAT TRACK LBL 59 CORROSION AND WEAR MARKS BS 1306 TO 1350. INSTALLED 1EA PLUG AND 1 CHANNEL BS 1320-1326 LBL 59 IAW SRM 51-03- 01 (AREAS STA 1306-1319 AND 1326-1350 BLENDED AND WITHIN LIMITS IAW SRM 53-02-03 FIG 012).Jun 28, 2008 · N752UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS08852728Seat Track · brokenINSPECTION TYPE-C2, BROKEN SEAT TRACK LUG ON MAIN CARGO FLOOR STA 260 BL 0. CUT OUT DAMAGE IAW 53-02-03 FIG 006D INSTALLED 2EA PLUGS AND 2EA CHANN ELS IAW 51-03-00.Jun 28, 2008 · N752UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS08852752Skin · corrodedINSPECTION TYPE-C2, CORRODED LOWER ATC-2 ANTENNA INSTALLATION AREA EXTERNAL SKIN AT STA. Y 427-5 RBL3. FABBED AND INSTALLED REPAIR DOUBLER IAW SRM, 51-1-8, 53-2-00 FIG 1F51- 3-2, 51-1-22.Jun 27, 2008 · N752UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS08853099Bulkhead · crackedINSPECTION TYPE:C2 FWD ACCESSORY COMPT BULKHEAD AT STA 683 LBL 21 BELOW FASTENER PATTERN ATTACHING BULKHEAD DOME TO WING LOWER FRONT SPAR WEB HAS 3 INCH CRACK. REMOVED WEB, REPLACED WEB IAW SRM 51-1-21.Jun 26, 2008 · N752UP · Doug DC871F · Fuselage Main, BulkheadSDR UPS08852904Longeron · corrodedINSPECTION TYPE-C2, AC COMPT. STA 62, HAS L31R WITH EXFOLIATION CORROSION. REMOVED DAMAGE AND FABBED AND INSTALLED REPAIR DOUBLER IAW, SRM, 51-1- 8, 53-2-0 FIG. 1F, 51-1-21.Jun 26, 2008 · N752UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS08852901Floorbeam · corrodedINSPECTION TYPE-C2, A/C COMPT. BS 55, RBL 38, FLOORBEAM HAS EXFOLIATION CORROSION. REMOVED CORROSION, FABBED AND INSTALLED REPAIR IAW, SRM, 51-1-8, 51-2- 00, 51-1-21A, 51-3-0.Jun 26, 2008 · N752UP · Doug DC871F · Fuselage Main, Floor BeamSDR IXX2008F00009Switch · brokenDURING CLIMB-OUT, OVER RIDE TOGGLE SWITCH BROKE OFF. AIRCRAFT RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED OVER RIDE SWITCH; OPS CHECK GOOD IAW UAL MM 74-20-36. (K)Jun 26, 2008 · N825BX · Doug DC871F · Electrical Power SystemSDR UPS08852755Attach Bracket · gougedINSPECTION TYPE-C2, RT WING REAR SPAR AT IB HINGE OF NR4 SPOILER PARTITION RIB ATTACH BRACKET GOUGED AND BENT. REMOVED AND REPLACED GUSSET IAW SRM, 51-1-21,57-2-0, 51-1-8.Jun 26, 2008 · N752UP · Doug DC871F · Wing, Attach FittingsSDR UPS08852895Skin · damagedINSPECTION TYPE-C2, DRILL START IN LOWER SKIN OF R/W OB, L/E, FWD OF 3RD. PANEL FROM OB END. REMOVED DAMAGE, FAB AND INSTALLED REPAIR DOUBLER IAW SRM 51-1-8, 57-2- 0 FIG.7 51-1-21.Jun 24, 2008 · N752UP · Doug DC871F · Wing, Plate/SkinSDR UPS08852732Fitting · crackedINSPECTION TYPE-C1, NR 4 ALT. STRINGER 65 TO FRONT SPAR FITTING CRACKED. REMOVED, FABRICATED AND INSTALLED FRONT SPAR FITTING. IAW DWG. 3644046 SRM 51-01-20D AND 51-03-01-0.Jun 19, 2008 · N700UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS08852582Fitting · crackedINSPECTION TYPE:C1 FS 834 L22L INTERCOSTAL END FITTING CRACKED. REPLACED INTERCOSTAL END FITTING AT FS 834 AND L22L IAW SRM 51-01-24-0, SRM 51-01-20D.Jun 19, 2008 · N700UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS08852550Slide · inoperativeMAIN ENTRY DOOR SLIDE INOP 378344. REMOVED MAIN ENTRY DOOR SLIDE AND ROUTED TO S/M. RIVET INSTALLED ON LOOSE BRACKET SRM 51-1-21 AND FWD ENTRY SLIDE REINSTALLED IAW MM 25- 60-01-2. THIS CLEARS M378344.Jun 19, 2008 · N701UP · Doug DC871F · Escape SlideSDR G412008F00002Control Unit · defectiveDURING CRUISE FROM KRFD NUMBER ONE ENGINE FIRE BELL AND LIGHT CAME ON, THE CREW ACCOMPLISHED RUN ENGINE FIRE CHECK LIST, THE CREW DISCHARGED ONE AGENT, AND DISCHARGED THE SECOND AGENT AND THE SECOND AGENT WOULD NOT DISCHARGE, THE CREW LANDED IN KTOL WITHOUT INJun 17, 2008 · N830BX · Doug DC871F · Fire DetectionSDR MAS2008F00009Control Valve · leakingON CLIMBOUT FROM KPHL HYDRAULIC PRESSURE WENT TO ZERO, HYDRAULIC FLUID LEVEL TO STANDPIPE, THE CREW DECLARED EMERGENCY AND LANDED INTO KTOL WITHOUT INCIDENT. MAINTENANCE INSPECTED HYDRAULIC SYSTEM AND FOUND SLOT CONTROL VALVE LEAKING, MAINTENANCE REPLACED SLOTJun 17, 2008 · N820BX · Doug DC871F · Hydraulic System, MainSDR UPS08853000None · noneINSPECTION TYPE-C2, COMPLY WITH MPI 19584 REGARDING REPLACEMENT OF EXISTING REPAIR AT AT L28R IAW WAN3 1369154 AND EO DC8-5330-20248-E APPX.E FABBED AND INSTALLED REPAIR DOUBLER IAW, EA NR 008-5330-01-A1449, SRO 853 0032. NOT AN SDR.Jun 16, 2008 · N752UP · Doug DC871F · Standard Practices/StructuresSDR UPS08852916Angle · crackedINSPECTION TYPE-C1 RUDDER "L" ANGLE CRACKED AT LT SIDE OF TOAD STOOL. (RUDDER TORQUE TUBE) REMOVED FABRICATED AND REPLACED "L" ANGLE IAW SRM 51-3-0.Jun 15, 2008 · N700UP · Doug DC871F · Rudder StructureSDR UPS08852635Skin · bulgedINSPECTION TYPE-C1 VERTICAL FIN, RT SIDE AFT OF ISOLATION STRIP HAS SKIN BULGING AND FASTENERS PULLING. REMOVED FASTENERS FOR ACCESS IAW SRM 51-01-21. NO CORROSION NOTED ON A REA. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 55-02-00, AND 51-01-21.Jun 15, 2008 · N700UP · Doug DC871F · Vertical Stabilizer, Plate/SkinSDR UPS08852748Seat Track · brokenINSPECTION TYPE-C1, SEAT TRACK AT LBL 45 BS 1600 MAIN CABIN HAS SEVERAL TANGS BROKEN OFF. FABRICATED NEW SEAT TRACK SECTION BS 1530-1610 LBL45 AND INSTALLED IA IAW SRM 53-02-03-0 FIG 008A, 51-01-08,51-03-00,51-03-01Jun 14, 2008 · N700UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS08852658Attach Bracket · damagedINSPECTION TYPE-C1, CABIN STA. 690 LONG 17L INTERCOSTAL ATTACH BRACKET HAS DRILL START. REMOVED, FABRICATED AND INSTALLED NEW "T" SUPPORT ANGLE IAW SRM 53-2-0 FIG 1F, DWG 3768038, 51-01-20D.Jun 14, 2008 · N700UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS08852637Attach Fitting · missingINSPECTION TYPE-C1, CABIN BS 1260 L15R, INTERCOSTAL CLIP MISSING FABRICATED AND INSTALLED CLIP IAW SRM 53-04-01 FIG 051, AND 51-1 -20D.Jun 13, 2008 · N700UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS08852627Torque Box · chafedINSPECTION TYPE-C1, C-PIT AT BS 1220, TORQUE BOX BENEATH CROSS-SLIDE DOOR HAS REPAIR DOUBLER WITH DEEP CHAFE WEAR, GOUGES FABRICATED AND REPLACED REPAIR DOUBLER IAW DWG 3753772 AND SRM 53- 02-00 FIG 025, 51-01-20D.Jun 13, 2008 · N700UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS08852584Web · chafedINSPECTION TYPE:C1 C-PIT CROSS SLIDE DOOR INTERIOR SURFACE AT AFT UPPER AREA, INTERNAL WEB HAS REPAIR DOUBLER WITH SEVERE CHAFE WEAR. FABRICATED AND REPLACED C-PIT DOOR INTERIOR WEB REPAIR DOUBLER IAW SRM 52-02-00 FIG 002, SRM 52-04-01 FIG 001.Jun 13, 2008 · N700UP · Doug DC871F · Cargo/Baggage DoorsSDR UPS08852581Longeron · crackedINSPECTION TYPE:C1 MAIN CABIN AT STA 1748 LONGERON 15R CRACKED WHERE LONGERON ATTACHES TO CANTED FRAME. REPAIRED LONGERON 15R FROM STA 1741 TO 1766 IAW SRM 53-02-02 FIG 10, SRM 51-03-02, SRM 51-01-21 AND SRM 51-01-20D.Jun 13, 2008 · N700UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS08852580Longeron · crackedINSPECTION TYPE:C1 MAIN CABIN AT STA 1753 HAS LONGERON 14R CRACKED WHERE LONGERON ATTACHES. REPAIRED L14R FROM STA 1745 TO 1766 IAW SRM 51-01-21, SRM 51-01-20D, SRM 53-02-02 FIG 10 AND SRM 51-03-01.Jun 13, 2008 · N700UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS08852543Web · puncturedINSPECTION TYPE:C1 B-PIT DOOR INTERIOR WEB IS PUNCTURED AT FWD UPPER LIGHTENING HOLE. REPAIRED B-PIT DOOR INTERIOR WEB IAW DWG 5645357 AND SRM 51-1-21.Jun 13, 2008 · N700UP · Doug DC871F · Cargo/Baggage DoorsSDR UPS08852542Floor Panel · corrodedINSPECTION TYPE:C1 COURIER AREA FLOOR PNL F25 SKIN CORRODED. REPAIRED CABIN FLOOR PNL F25 IAW SRM 53-1-21, SRM 53-02-00 FIG 1F, AND DWG 5777814.Jun 13, 2008 · N700UP · Doug DC871F · Fuselage Floor PanelSDR UPS08852747Door Frame · gougedINSPECTION TYPE-C1, RT FWD SERVICE DOOR AFT JAMB WEB HAS 5 AREAS OF DRILL STARTS, GOUGES AND HOLES. STA 190 BETWEEN L-21R AND L-10R. PLUGGED TOP 3 AREA HOLES IAW SRM 53-02-00 FIG 1F. FABRICATED AND INSTALLED REPAIR DOUBLER AT BOTTOM 2 AREA IAW SRM 53-02-00 Jun 12, 2008 · N700UP · Doug DC871F · Fuselage Main, StructureSDR UPS08852664Frame · corrodedINSPECTION TYPE-C1, AREA OF CORROSION EXFOLIATON ON AFT SIDE OF STA 70 FRAME, A PIT, BETWEEN L29L AND L30L. REMOVED DAMAGE AND FABRICATED DOUBLER IAW SRM 53-02-05 FIG 008C.Jun 12, 2008 · N700UP · Doug DC871F · Fuselage Main, FrameSDR UPS08852661Floor Panel · crackedINSPECTION TYPE-C1, FLOOR PANEL F87 HAS 3 EA SCREW HOLES CRACKED. REMOVED DAMAGE, FABRICATED AND INSTALLED 2EA. DOUBLERS IAW SRM 53-2-3 FIG 010, AND SRM 51-1-21.Jun 12, 2008 · N700UP · Doug DC871F · Fuselage Floor PanelSDR UPS08852660Frame · crackedINSPECTION TYPE-C1, RT FWD TYPE 1 EMERGENCY EXIT DOOR HAS CRACKED FRAME IN 2 PLACES, IB & OB ENDS OF DOOR TORQUE TUBE. REMOVED, FABRICATED, AND INSTALLED 2 REPLACEMENT WEBS IAW SRM 52-02 -00 FIG2, 51-01-21, AND 52-07-01.Jun 12, 2008 · N700UP · Doug DC871F · Emergency ExitsSDR UPS08852659Strap · damagedINSPECTION TYPE-C1, RT FWD SERVICE DOOR, FWD JAMB HAS RIVET INSTALLED THROUGH EDGE OF STRAP STA. 165 L20R. REMOVED STRAP, FABRICATED AND INSTALLED NEW STRAP IAW SRM 51-01-21 53-02-00.Jun 12, 2008 · N700UP · Doug DC871F · Service DoorsSDR UPS08852657Door Frame · damagedINSPECTION TYPE-C1, RT FWD SERVICE DOOR, FWD JAMB WEB HAS HOLE DRILLED OVER FRAME STA 165 ABOVE L21R. INSTALLED PLUG IAW SRM 53-02-00 AND 51+01-21.Jun 12, 2008 · N700UP · Doug DC871F · Fuselage Main, StructureSDR UPS08852656Door Frame · corrodedINSPECTION TYPE-C1, LT AFT ENTRY DOOR, FWD LWR JAMB HAS INTERGRANULAR CORROSION AND IS CRACKED BS 1620 L21L (DOOR PAN). CUT OUT DAMAGED AREA IAW SRM 53-02-00 FIG 001F. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-00-2 FIG 1D AND 51-1-20D.Jun 12, 2008 · N700UP · Doug DC871F · Fuselage Main, StructureSDR UPS08852638Seat Track · damagedINSPECTION TYPE-C1, F/E SEAT TRACKS BOTH FWD & AFT HOLES ARE ELONGATED. REMOVED AND REPLACED F/E SEAT TRACKS IAW SRM 51-03-01.Jun 12, 2008 · N700UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS08852622Fitting · damagedINSPECTION TYPE-C1, RT FWD TYPE 1 DOOR, FWD LWR JAMB BELT FRAME END FITTING HAS DOUBLE DRILLED HOLES STA 390 L-21R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D, 51-1-21,AND 51-01-2.Jun 12, 2008 · N700UP · Doug DC871F · Fuselage Main, Attach Fittings
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