Douglas DC-8-73F

Service difficulty reports · 15,471

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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 = 'DC873F'
  ORDER BY difficulty_date DESC"

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SDR UPS05845655Longeron · crackedINSPECTION TYPE:C2 FS 1790 TO FS 1880 L36 IS CRACKED AND HAS ELONGATED HOLES. REMOVED LONGERON 26 AT FS 1790 TO 1880 IAW SRM 51-1-20D FABRICATED AND INSTALLED LONGERON 36 AND SPLICE REPAIR IAW S1415997 AND SRM 51-1-20D, AND 51-1-20.Oct 11, 2005 · N866UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS05845640Angle · corrodedC-PIT AT STA 1190 RBL 39 L-ANGLE HAS INTERGRANULAR CORROSION. REMOVED ANGLE IAW SRM 51-1-20D, FABRICATED AND INSTALLED ANGLE AT STA 1190 RBL 39 IAW DWG 5711283, SAA SK 866-833103, UPS EO FILE NUMBER DC8-53-20512, AND BOEING MESSAGE NR 1-134429123-2 DATED 10-1Oct 11, 2005 · N866UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05845639Fitting · crackedFS 1880 L36 END FITTING IS CRACKED AT FASTENER HOLE. REMOVED AND REPLACED LONGERON END FITTING IAW SRM 51-1-20D AND SRM 51-1-21.Oct 11, 2005 · N866UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05845636Fitting · corrodedC2 BS 1890 L32L END FITTING HAS CORROSION AND ELONGATED HOLES. REMOVED AND REPLACED END FITTING AT FS 1890 L32L IAW SRM 51-1-20D, AND SRM 51-3-2.Oct 11, 2005 · N866UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05845633Longeron · corrodedINSPECTION TYPE:C2 LONGERON L32L CORRODED AND HAS ELONGATED HOLES AT FS 1880. REMOVED LONGERON 32L AT FS 1880 IAW SRM 51-3-0. FABRICATED AND INSTALLED LONGERON AND SPLICE FITTING AT FS 1880 L32L IAW SRM 53-02-02 AND SRM 51-1-20D.Oct 11, 2005 · N866UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS05845618Doubler · corrodedAT 60 HOLE INTERNAL SUPPORT DOUBLER HAS CORROSION OUT OF LIMITS AND DOUBLE DRILLED HOLES. REMOVED INTERNAL SUPPORT DOUBLER AT THE 60 HOLE IAW SRM 51-3-0. FABRICATED AND INSTALLED INTERNAL SUPPORT DOUBLER AT THE 60 HOLE IAW DWG 5649329.Oct 11, 2005 · N866UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS05845661Skin · crackedINSPECTION TYPE: C2 FUSELAGE SKIN HAS A .5 INCH CRACK AT MCD LWR AFT CORNER, UNDER REMOVED SCUFF PLATE, AT PREVIOUS CUT OUT. TRIMMED OUT CRACK AT MCD LWR AFT CORNER IAW DWG SR 08530027, FABRICATED AND INSTALLED -11 FILLERS, -4 DOUBLER AND -7 DOUBLER IAW DWG Oct 7, 2005 · N866UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS05845598Fitting · corrodedINSPECTION TYPE:C2 C PIT INTERGRANULAR CORROSION ON BATH TUB FITTING AT STA 1180 L35L . REMOVED BATHTUB FITTING AT STA 1180 L35L IAW SRM 51-1-20D AND 51-1-21. REPLACED BATH TUB FITTING AT STA 1180 L35L IAW SRM 53-2-0 FIG 2D AND SRM 51-1-8.Oct 6, 2005 · N866UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05845779Fitting · corrodedINSPECTION TYPE:C2 A-CROSS SLIDE DOOR TORQUE BOX, CORROSION ON LONGERON 35R FS 278. REMOVED BATHTUB FITTING AT STA 279 L35R-L36 IAW SRM 51-1-20D. INSTALLED NEW BATHTUB FITTING AT FS 279 L35R-L35 IAW SRM 53-04-01.Oct 5, 2005 · N866UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05845774Finger Doubler · crackedINSPECTION TYPE:C2 FINGER DOUBLER CRACKED AT STA 920-940 LBL 60. REMOVED FINGER DOUBLER AT STA 920-940 LBL 60 IAW SRM 51-1-20D AND 51-3-0. FABRICATED AND INSTALLED FINGER DOUBLER AT STA 920-940 LBL 60 IAW SRM 53-07-03 FIG 004 AND SRM 51-1-21 SRM 51-1-20D.Oct 5, 2005 · N866UP · Doug DC873F · Fuselage Main, StructureSDR UPS05845733Bulkhead · crackedFOUND CRACK ON AFT PRESS BULKHEAD LBL 26, 65 INCHES FROM FLOOR CUT OUT DAMAGED AREA AT FS 1766 LBL26 IAW SRM 53-2-5 FIG 14, NDT AREA IAW SPM 06-10-01-001, NO CRACKS NOTED AT CUT OUT AREA. FABRICATED -15, -17 DOUBLERS AND -9, -11, -13 AND -19 FILLERS IAW SRM 5Oct 5, 2005 · N866UP · Doug DC873F · Fuselage Main, BulkheadSDR UPS05845654Fitting · corrodedC2 C-PIT STA 1200 L26L BANANA FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED BANANA FITTING AT STA 1200 L26L IAW SRM 53-2-0, AND 51=1-20D,AND SRM 51-3-2.Oct 5, 2005 · N866UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05845649Fitting · corrodedC2 A- PIT BAG BIN, INTERGRANULAR CORROSION ON BATH TUB FITTING AT STA 280 L32L. REMOVED AND REPLACED BATH TUB FITTING AT STA 280, L32L IAW SRM 53-02-00 FIG 002D AND SRM 51-1-21.Oct 5, 2005 · N866UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05845635Door Frame · crackedA-PIT DOOR JAMB FWD LWR CORNER O/B OF L33R STA 280 ANGLE IS CRACKED APPROX 1". REMOVED AND REPLACED DOOR FRAME JAMB FITTING IAW SRM 51-1-20D AND SRM 51-1-8.Oct 5, 2005 · N866UP · Doug DC873F · Fuselage Main, StructureSDR UPS05845631Fitting · crackedC-PIT STA 1180 L26L BANANA FITTING CRACKED. REMOVED AND INSTALLED NEW BANANA FITTING AT STA 1180 L26L IAW SRM 51-3-2 AND SRM 51-1-20D.Oct 5, 2005 · N866UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05845619Fitting · crackedA-BAG BIN, L28L SPLICE FITTING CRACKED STA 210. REMOVED CRACKED SPLICE FITTING AT STA 210 L28L IAW SRM 51-1-20D. FABRICATED AND INSTALLED LONGERON SPLICE FITTING AT STA 210 L28L IAW DWG 4653726 ANG SRM 51-3-2, AND SRM 51-1-20D.Oct 5, 2005 · N866UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05845599Splice · crackedINSPECTION TYPE:C2 A PIT L31L SPLICE FITTING CRACKED BETWEEN STA 440 AND 460. REMOVED AND REPLACED SPLICE FITTING AT STA 440-460 L31L IAW SRM 51-1-20D, 51-3-2.Oct 5, 2005 · N866UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS05845597Angle · crackedINSPECTION TYPE:C2 ANGLE CRACKED ON FWD SIDE OF APB AT L6L. REMOVED ANGLE AT FWD SIDE OF AFT PRESS BULKHEAD IAW SRM 51-1-21. FABRICATED AND INSTALLED ANGLE ON FWD SIDE OF APB AT L6L IAW DWG 5773844 AND SRM 51-1-20D.Oct 5, 2005 · N866UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS05845554Battery Pack · weakEMERGENCY EXIT LIGHTS DIM. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK IAW MM 33-50-01.Oct 5, 2005 · N809UP · Doug DC873F · Emergency LightingSDR UPS05845783Spar · corrodedINSPECTION TYPE:C2 PRESSURE PANEL AT STA 857 RBL 26 TO 46 REAR SPAR TO FUSELAGE ANGLE EXFOLIATED. REMOVED ANGLE CHORD AT STA 857 RBL 26 TO 46 IAW SRM 51-1-20D. LOCATED AND DRILLED RT UPPER AFT SPAR CHORD AND INSTALLED SPAR CHORD IAW SRM 51-1-20D AND SRM 53-2Oct 4, 2005 · N866UP · Doug DC873F · Fuselage Main, FrameSDR UPS05845691Fitting · crackedFOUND L17L CRACKED AT END FITTING IN 60 COMPT, STA 1775. REMOVED END FITTING AT FS 1775 L17L IAW SRM 51-1-21. FABRICATED AND INSTALLED LONGERON AND END FITTING IAW SRM53-5-1 FIG 7 AND SRM 51-1-20D.Oct 4, 2005 · N866UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05845601Fitting · crackedINSPECTION TYPE:C2 FS 822.500 RBL 24 FWD FITTING CRACKED. REMOVED AND REPLACED FITTING AT FS 822.500 RBL 24 IAW SRM 51-1-20D, 51-3-2 AND SRM 51-3-0.Oct 4, 2005 · N866UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05845781Cusp Web · crackedINSPECTION TYPE:C2 CUSP CRACKED 3 INCH LONG STA 220 L21R. CUT OUT DAMAGED AREA OF CUSP AT FS 220 L21R IAW SRM 51-1-21D, FABRICATED AND INSTALLED REPAIR -25 ANGLES, CUSP SPLICE AND -21 DOUBLER IAW 53-2-5 FIG 1, 53-2-5 FIG 1 AND SRM 53-02-05 FIG 5.Oct 3, 2005 · N866UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS05845778Pressure Panel · corrodedINSPECTION TYPE:C2 FUSELAGE FLOORBEAM HEAVY CORROSION STA 940 RBL 65. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS AT STA 940 RBL 65 IAW UPS EO DC8-5330-23084-A, SAA SK 866-832597, BOEING MESSAGE 1-133200277-3 AND FAA FORM 8100-9.Oct 3, 2005 · N866UP · Doug DC873F · Fuselage Main, BulkheadSDR UPS05845776Shear Web · corrodedINSPECTION TYPE:C2 HEAVY CORROSION ON RT W/W FWD BULKHEAD STA 857, RBL 26. CUT OUT CORROSION IN SHEAR WEB AT STA 857 RBL 26 AND INSTALLED REPAIR PARTS IAW UPS ENG FILE DC8-53-20517 SAA SK 866-832582, BOEING MESSAGE 1-137210970-2, AND FAA FORM 8100-9.Oct 3, 2005 · N866UP · Doug DC873F · Fuselage Main, StructureSDR UPS05845718Spar Cap · crackedFOUND CRACK ON CENTER WING REAR SPAR LWR CAP, INSIDE KEEL BEAM BOX RT SIDE. STOP DRILLED CRACK AT REAR SPAR IAW SK SAA 866-832589, NDT VERIFIED CRACK TERMINATES AT STOP DRILL IAW NDT SPM 06-10-01.001 REPAIRED RT WING, REAR SPAR, LWR CAP CENTER LINE AT XCW-0 IOct 3, 2005 · N866UP · Doug DC873F · Wing, Center BoxSDR UPS05845690Floorbeam · crackedFOUND FLOORBEAM CRACKED 2" LONG AT FS 940 RBL 60 UPPER FLANGE AREA. CUT OUT DAMAGED AREA OF FLOORBEAM AT STA 940, RBL 60 IAW SRM TR# 53-152, FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW SRM TR# 51-1-21 FIG 1AND SRM 51-1-20D AT STA 940 RBL60.Oct 3, 2005 · N866UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS05845689Cusp Web · crackedFOUND CUSP CRACKED STA 1140 L21L. REMOVED CRACK CUSP AT FS 1140 L21L IAW SRM 53-2-5 FIG 15. FABRICATED AND INSTALLED -3 ANGLES, -7 DOUBLERS AND CUSP AT FS 1140 TO 1170 IAW SRM 53-2-5 FIG 15 AND 53-1-2 FIG 1.Oct 3, 2005 · N866UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS05845662Cusp Web · crackedINSPECTION TYPE: C2 C CUSP CRACKED 3 INCH LONG STA 1080 L21L. REMOVED DAMAGED AREA IAW SRM 53-02-05-0 AT FS 1080 L21L FABRICATED AND INSTALLED CUSP SPLICE,-7 DOUBLER, -3 AND -5 ANGLES AND -9 CUSP IAW 51-1-21, AND SRM 53-2-5 FIG 1.Oct 3, 2005 · N866UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS05845606Floorbeam · corrodedINSPECTION TYPE:C2 FLOORBEAM HEAVY CORROSION STA 940 LBL 60 UNDER THE SEAT TRACK. CUT OUT DAMAGED AREA OF FLOORBEAM IAW SRM 53-2-0 AND TEMP REV 53-152, FABRICATED AND INSTALLED REPAIR ANGLE AT STA 940 LBL 60 IAW SRM 53-2-0 TEMP REV 53-152, AND SRM 51-1-20D.Oct 3, 2005 · N866UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS05845603Finger Doubler · corrodedINSPECTION TYPE:C2 STA 880 RBL 65 SUBFLOOR FINGER DOUBLER HAS HEAVY CORROSION. REMOVED FINGER DOUBLER AT STA 880 RBL 65 IAW SRM 51-1-21, AND 51-3-0, FABRICATED AND INSTALLED FINGER DOUBLER AT FS 880 RBL 65 IAW SRM 53-7-3 FIG4, 51-9-0 FIG 68A, AND SRM 51-1-21.Oct 3, 2005 · N866UP · Doug DC873F · Fuselage Main, StructureSDR UPS05845602Fitting · corrodedINSPECTION TYPE:C2 CORROSION ON END FITTING AT L35L BS 70 A/C COMPT. REMOVED AND REPLACED END FITTING IAW SRM 51-1-21, 51-1-8 SRM 53-2-0 AND 51-1-20D.Oct 3, 2005 · N866UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05845600Fitting · corrodedINSPECTION TYPE:C2 STA 1500 L21R FUSELAGE FRAME TO CUSP FITTING HEAVY CORROSION. REMOVED FRAME FITTING TO CUSP AT FS 1500 L21R IAW 51-1-8 AND SRM 53-02-0 FIG 1F. REPLACED FUSELAGE FRAME TO CUSP FITTING IAW SRM 51-3-2, AND SRM 51-1-20D.Oct 3, 2005 · N866UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05845780Skin · damagedINSPECTION TYPE:C2 RUDDER RIGHT SIDE HAS 18EA CREASES JUST ABOVE UPS LOGO 2ND HINGE POINT FROM TOP. REMOVED AND REPLACED SKIN ON RUDDER STA ZR53-ZR71 IAW SRM 55-02-00 FIG 6 AND SRM 51-1-21.Oct 1, 2005 · N866UP · Doug DC873F · Rudder, Plate/SkinSDR UPS05845692Longeron · corrodedFOUND L31L CORRODED BEYOND LIMITS IN LT BELLY STRESS PNL STA 690-710. REMOVED LONGERN 31L FS 690-710 IAW SRM 53-02--02-0. FABRICATED AND INSTALLED LONGERON 31L AND -37. REPAIR SPLICES IAW DWG 3750575 AND SRM 53-02-02-0 AND SRM 51-1-20D.Oct 1, 2005 · N866UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS05845657Pressure Panel · corrodedC2 CORROSION UNDER DOUBLER ON LT W/W CEILING STA 960 LBL 57-62, CORROSION AT SAME LOCATION IN MAIN CABIN UNDER FLOORBEAM. REMOVED MLG LT WHEEL WELL HORIZ. PRESSURE PANEL WEB AT FS 960 LBL 57-62 IAW SAA SK 866-832452, AND UPS EO FABRICATED AND INSTALLED PRESSUOct 1, 2005 · N866UP · Doug DC873F · Fuselage Main, BulkheadSDR UPS05845693Skin · corrodedFOUND FUSELAGE SKIN HAS HEAVY CORROSION AND SEVERAL CRACKS AT AFT MANUFACTURING SPLICE AREA STA 1690 L32L TO L32R. REMOVED AND REPLACED SKIN FROM STA 1690 TO 1890 L28R TO L28L IAW SRM 51-1-21, 51-3-2, 51-20-00, 51-3-0 AND 51-1-20D.Sep 29, 2005 · N866UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS05845596Skin · crackedINSPECTION TYPE:C3 MCD NR 3 LATCH INTERNAL DOUBLER CUTOUT HOLE HAS TORN AND CRACKED SKIN A T 6 O`CLOCK POS. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW SAA SK 801-805297.Sep 22, 2005 · N801UP · Doug DC873F · Cargo/Baggage DoorsSDR DHL2005807004Switch · inoperativeBEGINNING OF TAKEOFF ROLL MASTER WARNING AND BELLY DOOR OPEN LIGHT ILLUMINATED RTO AT NO IND AIRSPEED. FOUND B PIT BELLY DOOR SWITH STUK, DISCONNECTED SWITCH, DEFERRED BY MEL 52-6 IN DMI NR 22471. TLATEMPA 999017. RE DMI 22471 BEGINNING OF TAKEOFF ROLL, MASTSep 17, 2005 · N807DH · Doug DC873F · Door Warning SystemSDR UPS05845457Smoke Goggles · scratched2ND OBSERVERS SMOKE GOGGLES SCRATCHED. REPLACED SMOKE GOGGLES.Sep 17, 2005 · N802UP · Doug DC873F · Emergency EquipmentSDR DHL2005806540Bracket · corrodedITEM REF NR 041577: RT ELEVATOR SYSTEM, 1EA BRACKET CORRODED, STA -90.000. REMOVED AND REPLACED RT ELEVATOR SYS BRACKET AT STA -90.000. TIGHTENED BOLT IAW MM 20-16-0 PG. 201. ADJUSTED CONTROL CABLES IAW MM 27-30-0 PG. 512-513. OPS CHECKED SEE NR 041920Sep 16, 2005 · N806DH · Doug DC873F · Elevator Control SystemSDR DHL2005806541Bracket · corrodedITEM REF NR 041572: RT ELEVATOR SYSTEM 1EA BRACKET CORRODED STA -141.000. REMOVED AND REPLACED RT ELEVATOR SYSTEM BRACKET STA -141.000. TIGHTENED BOLT IAW MM 20-16-0 PG. 201. ADJUSTED ELEVATOR CONTROL CABLES IAW MM 27-30-0 PG. 512-513. REFER TO NR 041920 FOR OSep 16, 2005 · N806DH · Doug DC873F · Elevator Control SystemSDR UPS05845461Skin · corrodedLT HORIZONTAL LE HAS INTERGRANULAR CORROSION AROUND FASTENER HOLES ON LOWER SURFACE AT IB END OF OB SECTION. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 55-2-1 FIG 4.Sep 15, 2005 · N801UP · Doug DC873F · Horizontal Stabilizer, Plate/SkinSDR UPS05845450Rib · crackedINSPECTION TYPE:C3 WHILE WORKING NR 808576, FOUND LT WING I/B FLAP LWR O/B SIDE 3RD RIB FROM LWR AT XW120 CRACKED. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 51-1-21, 57-2-0 FIG 2 SHT 2, 51-1-20D.Sep 13, 2005 · N874UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05845622Floorbeam · crackedPOSSIBLE CRACK AT FLOORBEAM LOWER AREA STA 902 RBL 50-55. NDT VERIFIED TWO CRACKS. CUT OUT DAMAGED SECTION OF FLOORBEAM, FABRICATED REPLACEMENT SECTION OF FLOORBEAM AND REPAIR PARTS IAW SAA SK 801-805214.Sep 12, 2005 · N801UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS05845595Fitting · crackedINSPECTION TYPE:C3 BATHTUB FITTING CRACKED AT LT L24L WW STA 960. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-3-0, 51-1-20D, AND DWG 56 43117.Sep 12, 2005 · N801UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05845541Fitting · corrodedINSPECTION TYPE: C3, DEEP CORROSION PITTING AROUND LOWER FASTENER THRU BATHTUB FITTING AT STA. 1153 ABOVE L33R. REMOVED BATHTUB FITTING, FABRICATED SPLICE ANGLES, INSTALLED FITTING AND SPLICE ANGLES IAW SRM 53-02-00 FIG 2D, 51-1-20D.Sep 12, 2005 · N874UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05845531Longeron · crackedC3 - CRACKED LONGERON AT STA 1736 L15R. CUT OUT DAMAGED LONGERON, FABRICATED AND INSTALLED REPLACEMENT LONGERON IAW SRM 51-1-21, 51-1-20D, 53-2-2 FIG 10 AND DWG 5894025.Sep 12, 2005 · N874UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS05845530Fitting · crackedC3 - D-PIT DOOR INTERIOR FWD UPPER ANGLE CRACKED JUST BELOW UPPER STOP. REMOVED AND REPLACED DOOR UPPER ANGLE SUPPORT FITTING IAW SRM 51-1-2 AND 51-3-0.Sep 12, 2005 · N874UP · Doug DC873F · Cargo/Baggage DoorsSDR UPS05845491Longeron · crackedFOUND CRACKED LONGERON AT STA 1756 L14L. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-3-0, 53-2-2 FIG 11 AND 51-1-20D.Sep 12, 2005 · N874UP · Doug DC873F · Fuselage Main, Longeron/Stringer
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