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 UPS05845547Fitting · crackedC3 C PIT DOOR JAMB FITTING CRACKED I/B OF NR 2 TEE BOLT FITTING AT FWD SIDE. REMOVED AND REPLACED FITTING IAW DC-8 SRM 53-2-0 FIG 2D AND 51-1-20D.Sep 2, 2005 · N801UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05845504Fitting · crackedINSPECTION TYPE:C3 L26L END FITTING APPEARS CRACKED AT STA 1688. REMOVED AND REPLACED LONGERON END FITTING IAW DC-8 SRM 51-1-20D.Sep 2, 2005 · N801UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05845503Longeron · corrodedINSPECTION TYPE:C3 A/C COMPARTMENT STA 25 LONGERON 31R, LONGERON HAS HEAVY CORROSION. REMOVED LONGERON, FABRICATED, AND INSTALLED REPLACEMENT LONGERON IAW DC-8 SRM 51-1-20D AND 51-1-21.Sep 2, 2005 · N801UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS05845456Fitting · crackedLWR CARGO STA 1140 L35R FWD FITTING CRACKED 2 INCHES LONG. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.Sep 2, 2005 · N801UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05845399Fitting · crackedINSPECTION TYPE:C3 C-PIT DOOR JAMB FITTING CRACKED I/B OF NR 6 T-BOLT FITTING AT FWD SI DE. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.Sep 2, 2005 · N801UP · Doug DC873F · Cargo/Baggage DoorsSDR UPS05845353Motor · overheatedLAV FLUSH MOTOR OVERHEATED CAUSING SMOKE IN CABIN. REMOVED AND REPLACED LAV TIMER AND FLUSH MOTOR PER MM 20-10-03, 20-16-00-2. OPS CK NORMAL PER MM 38-30-00-1. NO LEAKS NOTED.Sep 2, 2005 · N818UP · Doug DC873F · Waste Disposal SystemSDR DHL2005806525Cap · corrodedRT SLANT PANEL UPPER CAP CORRODED, STA XFS 95. PERFORMED MAJOR REPAIR. REMOVED FASTENERS, REMOVED CORROSION FROM RT SLANT PANEL UPPER CAP STA XFS 95 IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 37. PERFORMED DETAIL VISUAL INSP OF REWORKESep 1, 2005 · N806DH · Doug DC873F · Wing Main, Frame StructureSDR DHL2005806514Doubler · crackedITEM REF. NR. 040957: PRIMARY HEAT EXCHANGER AFT LWR CORNER ACS STRUCTURAL MODIFICATION DOUBLER CRACKED 0.750 IN STA -12.000 L-27R. DWG U80-R18 REV. IR DATED 08-08-05. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW DWG U80-R18. PSep 1, 2005 · N806DH · Doug DC873F · Fuselage Main, StructureSDR DHL2005806517Doubler · crackedPRIMARY HEAT EXCHANGER AFT LWR CORNER ACS STRUCTURAL MODIFICATION DOUBLER CRACKED 0.75 IN STA -12.000 L-27L (MAJOR REPAIR). REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGE SECTION IAW DWG NR U80-R19. PERFORMED DETAIL VISUAL INSP OF REWORKED AREA. NO CRACK ORSep 1, 2005 · N806DH · Doug DC873F · Fuselage Main, StructureSDR DHL2005806522Longeron · crackedFWD ACCY COMPT LONGERON 28R CRACKED 1 INCH STA 8.000-35.000 MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 53-3-3 FIG 2 SHEET 1, SRM 51-2-0 FIG 52 SHEET 1. REMOVED DAMAGED LONGERON IAW SRM 53-1-0 PG 1, SRM 51-1-21. FABRICATED NEW LONGERON IAWAug 31, 2005 · N806DH · Doug DC873F · Fuselage Main, Longeron/StringerSDR DHL2005806521Door Frame · crackedD-BELLY DOOR FRAME UPPER AFT CORNER CRACKED 1.000. PERFORMED STOP HOLE IAW SRM 52-2-0 PG 1. FABRICATED DOUBLER IAW SRM 52-4-1 FIG 4, SRM 51-1-4 PG 1. HEAT TREATED FROM 2024T3 TO 2024T4 IAW SRM 51-1-1 PG 1, 13, 17. CLEANED, TREATED AND PRIMED IAW SRM 51-1-Aug 31, 2005 · N806DH · Doug DC873F · Fuselage Main, StructureSDR UPS05845502Fitting · crackedINSPECTION TYPE: C3, LONG END FITTING CRACKED AT STA 1760 L17R. REMOVED AND REPLACED LONGERON END FITTING IAW DC-8 SRM 51-1-21.Aug 31, 2005 · N801UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05845500Fitting · corrodedINSPECTION TYPE:C3 MAIN CABIN BELT FRAME END FITTING CORRDED AT STA 1040 L21R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0.Aug 31, 2005 · N801UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05845499Longeron · crackedINSPECTION TYPE:C3, L15R CRACKED AT STA 1749. REMOVED CRACKED SECTION OF LONGERON, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF LONGERON IAW DC-8 SRM 53-2-2 FIG 10.Aug 31, 2005 · N801UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS05845498Skin · crackedINSPECTION TYPE:C3 LT UPPER WING NR 2 MAIN TANK ACCESS PANEL 505F UNDER LANDING HAS 1" LONG POSSIBLE CRACK. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1 FIG 36.Aug 31, 2005 · N801UP · Doug DC873F · Wing, Plate/SkinSDR UPS05845455Longeron · crackedLONG 15 LT CRACKED AT STA 1728 TOP AND BOTTOM. REMOVED DAMAGED SECTION OF LONGERON, FABRICATED REPLACEMENT SECTION OF LONGERON, AND INSTALLED IAW DC-8 SRM 53-2-2 FIG 10.Aug 31, 2005 · N801UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS05845298Microphone · inoperativeCAPTAINS O2 MASK MIC INOP.Aug 31, 2005 · N812UP · Doug DC873F · Audio Integrating SystemSDR UPS05845296Window · jammedF/O'S SLIDING WINDOW JAMMED.Aug 31, 2005 · N840UP · Doug DC873F · Flight Compartment WindowsSDR UPS05845613Skin · corrodedINSPECTION TYPE:C3 EXFOLIATING CORROSION AROUND FASTENER HOLE ON THE LT HORIZONTAL L/E AS MARKED ON TOP SURFACE. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW SAA SK 801-804772 .Aug 30, 2005 · N801UP · Doug DC873F · Horizontal Stabilizer, Plate/SkinSDR UPS05845612Longeron · crackedINSPECTION TYPE:C3 LONGERON 24L CRACKED IN BATHTUB STA 863-871. REMOVED AND REPLACED LONGERON 24L IAW UPS EO DC8-5310-22823-A AND SAA SK 801-804705.Aug 30, 2005 · N801UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS05845593Structure · corrodedINSPECTION TYPE:C3 EXFOLIATION TYPE CORROSION AROUND FASTENER HOLES FOR THE RT HORIZONTAL L/E TOP SURFACE FROM STA XFS 78.750 TO XFS 266.250. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SAA SK 801-804773.Aug 30, 2005 · N801UP · Doug DC873F · Horizontal Stabilizer StructureSDR UPS05845611Pressure Panel · corrodedINSPECTION TYPE:C3 CORROSION UNDER STIFFENER ON RIGHT W/W CEILING STA 902 RBL 50-55. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW UPS EO DC8-5310- 23036-A AND SAA SK 801-804599.Aug 29, 2005 · N801UP · Doug DC873F · Fuselage Main, BulkheadSDR UPS05845546Bulkhead · corrodedHEAVY CORROSION ON VERTICAL STIFFENER ON FWD BULKHEAD RT W/W STA 857, RBL 45, 12" BELOW CEILING. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DWG 5643433 AND SRM TR 51-2-1 FIG 1.Aug 29, 2005 · N801UP · Doug DC873F · Fuselage Main, BulkheadSDR UPS05845545Bulkhead · corrodedHEAVY CORROSION ON AFT 980 BULKHEAD LT WW OB CORNER ABOVE LONG 24 LT. REMOVED CORROSION, FABRICATED, AND INSTALLED SHIM IAW SAA SK 801-80457 2.Aug 29, 2005 · N801UP · Doug DC873F · Fuselage Main, BulkheadSDR UPS05845497Skin · crackedINSPECTION TYPE: C3, RT UPPER WING SKIN CRACKED AT XCW 69.500 REAR SPAR SKIN, (4 INCHES LONG CRACK). REMOVED DAMAGED SECTION OF SKIN, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1 FIG 20.Aug 29, 2005 · N801UP · Doug DC873F · Wing, Plate/SkinSDR UPS05845398Skin · corrodedINSPECTION TYPE:C3 LT WING L/E UPPER SKIN HAS INTERGRANULAR CORROSION UNDER REPAIR DOUBLER AT XFS 410.250. REMOVED REPAIR DOUBLER, CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1.Aug 29, 2005 · N801UP · Doug DC873F · Wing, Plate/SkinSDR UPS05845397Rib · corrodedINSPECTION TYPE:C3 LT WING L/E LOWER RIB HAS INTERGRANULARR CORROSION AT XFS 366.500, RIB IS ALSO CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT RIB IAW DC-8 SRM 51-1-2 0D, 51-1-21, AND DWG 5769530.Aug 29, 2005 · N801UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05845349Rib · crackedLT WING LE UPPER RIB IS CRACKED AT XS 435.789. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2 -0 FIG 2.Aug 29, 2005 · N801UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05845348Skin · corrodedLT WING LE HAS INTERGRANULAR CORROSION IN SKIN AT XW 257. SKIN IS SPLIT T ALONG EDGE. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1.Aug 29, 2005 · N801UP · Doug DC873F · Wing, Plate/SkinSDR UPS05845347Rib · corrodedLT WING LE LOWER RIB IS BULGED AND HAS INTERGRANULAR CORROSION AT XFS 372.750. CUT OUT DAMAGE, FABRICATED, INSTALLED REPAIR IAW DC-8 SRM 57-2-0 FIG. 2.Aug 29, 2005 · N801UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05845346Rib · crackedLEFT WING LE LOWER RIB IS CRACKED AT XFS 341.500. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2 -0 FIG 2.Aug 29, 2005 · N801UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05845345Rib · crackedLEFT WING LE LOWER RIB PREVIOUS REPAIR IS CRACKED AT XFS 360.250. REMOVED, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-0 FIG 2.Aug 29, 2005 · N801UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05845344Rib · crackedLT WING LE LOWER RIB PREVIOUS REPAIR IS CRACKED AT XFS 347.750. REMOVED, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-0 FIG 2.Aug 29, 2005 · N801UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05845343Rib · crackedLT WING LE LOWER RIB IS CRACKED AT XFS 335.250. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2 -0 FIG 2.Aug 29, 2005 · N801UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05845338Rib · crackedRT WING LE UPPER RIB CRACKED .375 LONG AT XFS 322 (MID CENTER LE). STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2 -0 FIG 2.Aug 29, 2005 · N801UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05845337Rib · crackedRT WING LE UPPER RIB CRACKED .3750 LONG AT XFS 312 (MID CENTER LE). STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-0 FIG 2.Aug 29, 2005 · N801UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05845336Rib · crackedRT WING LE UPPER RIB CRACKED .3450 LONG AT XFS 379 (MID CENTER LE). STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-0 FIG 2.Aug 29, 2005 · N801UP · Doug DC873F · Wing, Rib/BulkheadSDR DHL2005873002Battery · dischargedEMERGENCY LIGHTS BATTERY DISCHARGED DUE TO LEFT IN ARMED POS. ALLOWED EMERGENCY LIGHT BATTERIES TO CHARGE TO PEAK AND TESTED PER DACO M/M 33-50-0. OP CHECKS SERVICE.Aug 29, 2005 · N873SJ · Doug DC873F · Emergency LightingSDR DHL2005806512Floorbeam · corrodedAFT CARGO COMPT FLOORBEAM UPPER FLANGE CORRODED STA 1320.000 RBL 40 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 51-2-1 FIG 1 SHEET 9-12, TR 51-130. REMOVED FASTENERS IAW SRM 51-1-20D. REMOVED CORROSION ON FLOORBEAM UPPER FLANGE STA 1320 RBL 40 IAW SRAug 28, 2005 · N806DH · Doug DC873F · Fuselage Main, Floor BeamSDR DHL2005806520Skin · corrodedEXTERIOR AFT FUSELAGE DOUBLER REPAIR FASTENERS SHEARED, STA 1868 BETWEEN L-36 & L-32L AND CORROSION ON ADJACENT SKIN TO DOUBLER REPAIR. PERFORMED MAJOR REPAIR. REMOVED EXISTING REPAIR DOUBLER. REMOVED CORROSION FROM ADJACENT SKIN. FOUND OUT OF LIMITS. CUTAug 28, 2005 · N806DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2005806519Door · misrepairedAFT PASSENGER DOOR REPAIR ON AFT UPPER JAMB CORNER IS NOT IAW SR08530021 STA 1660.000 L-18L TO L-12L. PERFORMED MAJOR REPAIR IAW AD200-20-08, DWG NR SR08530021, 5750776 (S/B 53-075). REMOVED EXISTING REPAIR IAW SRM 51-1-21, SRM 51-1-20D. PERFORMED DETAIL VISUAug 28, 2005 · N806DH · Doug DC873F · Fuselage Main, StructureSDR DHL2005806539Doubler · crackedAFT SVC DOOR UPPER AFT CORNER INTERNAL DOUBLER CRACKED 1IN (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW AD2000-20-08, S/B 53-075, DWG NR SR08530021, 5750776. CUT OUT DAMAGED SECTION IAW DWG SR08530021. PERFORMED NDT INSP IAW NDT SPM PART 06-10-01-001. FABRICATEAug 28, 2005 · N806DH · Doug DC873F · Service DoorsSDR UPS05845544Rib · chafedRT WING LE LOWER RIB IS CHAFFED AT XFS 416.500. CHAF FOUND OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-0 FIG. 2.Aug 28, 2005 · N801UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05845412Skin · crackedINSPECTION TYPE: C3, RT WING L/E UPPER SKIN IS CRACKED O/B OF XFS 710.000. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1 FIG 38.Aug 28, 2005 · N801UP · Doug DC873F · Wing, Plate/SkinSDR UPS05845396Skin · crackedINSPECTION TYPE:C3 RIGHT WING L/E UPPER SKIN IS CRACKED IN THREE LOCATIONS (1ST XFS 310.250 ) (2ND 316.250) (3RD 322.750). CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1 FIG 38.Aug 28, 2005 · N801UP · Doug DC873F · Wing, Plate/SkinSDR UPS05845395Skin · crackedINSPECTION TYPE: C3, LEFT WING L/E UPPER SKIN IS CRACKED AT XW 485. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1 FIG 38.Aug 28, 2005 · N801UP · Doug DC873F · Wing, Plate/SkinSDR UPS05845364Skin · corrodedINSPECTION TYPE:C3 RIGHT WING L/E SKIN UPPER I/B OF XFS 710.000 HAS INTERGRANULAR CORROSION AND IS CRACKED. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1 FIG 38.Aug 28, 2005 · N801UP · Doug DC873F · Wing, Plate/SkinSDR UPS05845352Rib · crackedRT WING LE UPPER RIB IS CRACKED AT XFS 753.750. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2 -0 FIG 2.Aug 28, 2005 · N801UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05845351Skin · crackedRT WING LE SKIN IS CRACKED AT TWO LOCATIONS XW 257. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1.Aug 28, 2005 · N801UP · Doug DC873F · Wing, Plate/SkinSDR UPS05845342Skin · corrodedRT WING LE UPPER SKIN HAS INTERGRANULAR CORROSION AT XFS 622.500. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1 FIG 38.Aug 28, 2005 · N801UP · Doug DC873F · Wing, Plate/Skin
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