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 UPS07850655Fitting · gougedINSPECTION TYPE:C2 LEFT I/B FLAP CANOE FITTING I/B SIDE GOUGED. REPAIRED LEFT I/B FLAP CANOE FITTING IAW UPS EA 008-2750-01-A1062 AND UPS RAA DC8-57-20229.Aug 16, 2007 · N801UP · Doug DC873F · Trailing Edge FlapsSDR UPS07850633Attach Angle · corrodedINSPECTION TYPE:C2 ATTACH ANGLE CORRODED AT RIGHT END OF CENTER J-BEAM ON STA 8 BULKHEAD IN A/C COMPARTMENT. REMOVED, FABRICATED AND INSTALLED A/C COMPARTMENT RIGHT CENTER J-BEAM ATTACH ANGLE ON STA 8 BULKHEAD IAW SRM 51-01-21, SRM 51-1-8, SRM 53-2-0 FIG 1F AAug 16, 2007 · N801UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS07850457Floor Panel · damagedINSPECTION TYPE:N/A PIT 31 HAS HOLE IN FLOOR PANEL. A .375 INCH HOLE IN PIT 31 FLOOR PANEL IS LOCATED 33 INCHES AFT OF DOORSILL AND 41 INCHES LEFT OF CENTERLINE. ACCOMPLISHED INTERIM REPAIR PER EO DC8-5320-8724, APPROX A. DEFERRAL OPENED FOR PERMANENT REPAIAug 16, 2007 · N812UP · Doug DC873F · Fuselage Floor PanelSDR UPS07850657Panel · gougedINSPECTION TYPE:C2 RIGHT ELEVATOR PANEL 75 CHAFED AND GOUGED. REPAIRED RIGHT ELEVATOR PANEL 75 IAW EO DC8-5720-7767 APPX A.Aug 15, 2007 · N801UP · Doug DC873F · Elevator, Plate/SkinSDR UPS07850656Doubler · gougedINSPECTION TYPE:C2 RIGHT I/B FLAP STA 98 UPPER SURFACE EXISTING REPAIR DOUBLER GOUGED. REPAIRED RIGHT I/B FLAP STA 98 UPPER SURFACE IAW EO DC8-5720-7720-A.Aug 15, 2007 · N801UP · Doug DC873F · Trailing Edge FlapsSDR UPS07850471Fitting · crackedINSPECTION TYPE:C2 CRACKED END FITTING AT STA 1240 L35R. REMOVED AND REPLACED LONGERON END FITTING AT STA 1240 L35R IAW SRM 51-1-20D AND SRM 51-3-2.Aug 15, 2007 · N851UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS07850712Fitting · crackedINSPECTION TYPE:C2 UPPER AFT BANANA FAIRING ATTACH FITTING CRACKED AT RIGHT HORIZ STAB. REMOVED, FABRICATED, AND INSTALLED UPPER AFT BANANA FAIRING ATTACH FITTING ON RIGHT HORIZ STAB IAW DWG 4701959, AND SRM 51-3-0.Aug 14, 2007 · N801UP · Doug DC873F · Horizontal Stabilizer Miscellaneous StructureSDR UPS07850708Structure · corrodedINSPECTION TYPE:C2 LEFT WING FLAPWELL FUEL DUMP CHUTE FWD AREAS CORRODED. REPAIRED LEFT WING FLAPWELL FUEL DUMP CHUTE FWD AREAS IAW SRM 51-01-08- 0, 57-02-00 FIG 007, DWG 5649654, AND SRM 51-01-21.Aug 14, 2007 · N801UP · Doug DC873F · Wing Miscellaneous StructureSDR UPS07850661Spar Cap · corrodedINSPECTION TYPE:C2 HEAVY CORROSION ON INBOARD FACE OF VERTICAL STAB REAR SPAR LEFT CAP ABOVE NR 2 RUDDER HINGE ARM. REPAIRED DAMAGED VERTICAL STAB SPAR CAP ABOVE NR 2 RUDDER HINGE ARM IAW SAA EA 008-5520-01-A1073, UPS RAA DC8-55-20109, AND FAA FORM 8100-9.Aug 14, 2007 · N801UP · Doug DC873F · Vertical Stabilizer, Spar/RibSDR UPS07850660Spar Cap · corrodedINSPECTION TYPE:C2 CORROSION ON INBOARD FACE OF VERTICAL STAB REAR SPAR CAP RIGHT SIDE AT 6 BOLTS ABOVE 2ND HINGE ARM. REPAIRED DAMAGED AREA OF THE VERTICAL STAB REAR SPAR CAP IAW SAA EA 008-5520-01-A1073, UPS RAA DC8-55-20109, AND FAA FORM 8100-9.Aug 14, 2007 · N801UP · Doug DC873F · Vertical Stabilizer, Spar/RibSDR UPS07850589Skin · looseINSPECTION TYPE:C2 OUTER SKIN LOOSE AROUND COUNTERSINKS AT TOP OF VERTICAL STAB L/E LWR SECTION. REMOVED EXISTING FASTENERS AND FABRICATED AND INSTALLED REPAIR DOUBLER AT TOP OF VERT STAB L/E LWR SECTION IAW SRM 55-2-1 AND SRM 51-1-21.Aug 14, 2007 · N801UP · Doug DC873F · Vertical Stabilizer, Plate/SkinSDR UPS07850539Stiffener · corrodedINSPECTION TYPE:C2 SMALL HORIZ STIFFENER CORRODED/EXFOLIATED INSIDE VERT STAB REAR SPAR, THROUGH ACCESS PNL 55. REMOVED DAMAGED STIFFENER ON VERT STAB INSIDE ACCESS PNL 55 IAW SRM 51-01-21. FABRICATED AND INSTALLED REPAIR STIFFENER IAW SRM 51-01-21 AND DWG 5Aug 14, 2007 · N801UP · Doug DC873F · Vertical StabilizerSDR UPS07850825Skin · dentedINSPECTION TYPE:C2 SEVERAL DENTS ON EXT FUSELAGE SKIN AT STA 1600 L22R AND L23R. REPAIRED FUSELAGE SKIN AT STA 1600 L22R AND L23R IAW SAA EA 008-5330- 01-A1086, UPS EO DC8-5330-27794-A, AND FAA FORM 8100-9.Aug 13, 2007 · N801UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS07850658Fitting · gougedINSPECTION TYPE:C2 LEFT FLAP STA 219 I/B CANOE FITTING GOUGED. REPAIRED LEFT FLAP CANOE FITTING STA 219 I/B CANOE FITTING IAW EA 008- 2750-01-A1064.Aug 13, 2007 · N801UP · Doug DC873F · Trailing Edge FlapsSDR UPS07850585Flap Track · damagedINSPECTION TYPE:C2 FLAP TRACK CHROME MISSING LEFT FLAP STA 410 O/B. REMOVED AND REPLACED LEFT STA 410 FLAP TRACK IAW AMM DC8 27-51-03-2.Aug 13, 2007 · N801UP · Doug DC873F · Trailing Edge FlapsSDR DHL2007804528Structure · crackedFUSELAGE EXTERIOR PRIMARY HEAT EXCHANGER AFT UPPER CORNER ACS MODIFICATION DOUBLER 0.375" CRACK STA -12.000 L-24L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 08-13-07, ASTAR EVA D853-00007 DATED 07-10-07, ASTAR DWG ES D853-00007-001 DATEDAug 13, 2007 · N804DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2007804527Longeron · damagedPERFORMED DETAILED VISUAL INSPECTION OF REPAIR AND FOUND IT TO BE NOT IN ACCORDANCE WITH SRM. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 08-13-07, EVA D853-00014 REV IR DATED 08-07-07. DRAWING AD79-23-104 REV IR DATED 08-03-07. REMOVED EXISTING NON STAug 13, 2007 · N804DH · Doug DC873F · Fuselage Main, Longeron/StringerSDR DHL2007804526Longeron · crackedPERFORMED DETAILED VISUAL INSPECTION OF REPAIR AND FOUND IT TO BE NOT IN ACCORDANCE WITH SRM. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 08-13-07, ASTAR EVA D853-00013-001-D REV IR DATED 08-08-07. REMOVED NON STANDARD REPAIR IAW SRM 51-1-21, SRM 51-1-2Aug 13, 2007 · N804DH · Doug DC873F · Fuselage Main, Longeron/StringerSDR IXXA07SMN209SSkin · dentedDURING ROUTINE C CHECK INSPECTION, RT ELEVATOR OIL CANNING LOWER PANEL, PLATING AT STA XE 279.000 STA XE 306.000.Aug 13, 2007 · N606AL · Doug DC873F · Elevator, Plate/SkinSDR IXXA07SMN208SSkin · dentedDURING ROUTINE C CHECK INSPECTION, HORIZ STABILIZER EMPENNAGE INBD L/E EXT SKIN SHOWS (01EA) DENTS AT STA XFS 97.500 AND STA XFS 103.000.Aug 13, 2007 · N606AL · Doug DC873F · Horizontal Stabilizer, Plate/SkinSDR IXXA07SMN207SFloorbeam · crackedDURING ROUTINE C CHECK INSPECTION, FWD BELLY PIT UPPER FLANGE OF FLOORBEAM, CRACKED AT STA BS 180.000, RBL 46".Aug 13, 2007 · N606AL · Doug DC873F · Fuselage Main, Floor BeamSDR IXXA07SMN206SBulkhead · crackedDURING ROUTINE C CHECK INSPECTION, AFT BULKHEAD.-TEE CAP OF LT SIDE PRESS WALL UPPER PART BETWEEN L-9L AND L-10L, STA 1766.000 SHOWS CRACK 1".Aug 13, 2007 · N606AL · Doug DC873F · Horizontal Stabilizer StructureSDR IXXA07SMN205SStructure · crackedDURING ROUTINE C CHECK INSPECTION, RT AFT NLG DOOR, AFT DOOR STRUCTURE ATTACH ARM HAS CRACK FWD UPPER AREA (CRACKS IN FILLER PNL NOT DOOR HINGE) FILLER PNL REMOVED.Aug 13, 2007 · N606AL · Doug DC873F · Landing Gear DoorsSDR IXXA07SMN210SBeam · dentedDURING ROUTINE C CHECK INSPECTION, ACCESS CMPT CORROSION ON BEAM AT STA 50.000 AND RBL 35".Aug 13, 2007 · N606AL · Doug DC873F · Fuselage Main, StructureSDR UPS07850435Battery Pack · dischargedINSPECTION TYPE:N/A EMERGENCY BATTERY PACK INOP. REPLACED EMERGENCY BATTERY PACK. OPS CHECKED NORMAL.Aug 13, 2007 · N894UP · Doug DC873F · Emergency LightingSDR UPS07850481Floorbeam · corrodedINSPECTION TYPE:C1 FLOORBEAM AT STA 240 BL-0 HAS CORROSION OUT OF LIMITS. CUT OUT DAMAGED AREA OF FLOORBEAM AT STA 240 BL 0 IAW SRM 53-02-00 FIG 001. FABRICATED AND INSTALLED REPAIR ANGLES AND STRAP AT STA 240 BL 0 IAW SRM 53-02-00 FIG 001.Aug 11, 2007 · N874UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS07850462Intercostal · crackedINSPECTION TYPE:C1 INTERCOSTAL CRACKED AT STA 1650 LBL 3. STOP DRILLED CRACKED INTERCOSTAL AT STA 1650 LBL 3 IAW SRM 51-1-21, FABRICATED AND INSTALLED REPAIR DOUBLER ON INTERCOSTAL AT STA 1650 LBL 3 IAW DWG 3704315, AND SRM 53-02-00-0 FIG 001B.Aug 11, 2007 · N874UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS07850587Skin · dentedINSPECTION TYPE:C2 TRANSFERRED FROM LP 749931 ITEM 2: MINOR FUSELAGE SKIN DENT DMG AT STA 1867 L32R. CUT OUT DAMAGED AREA AT STA 1867 L32R IAW SRM 53-02-01 FIG 7. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER AT STA 1867 L32R IAW SRM 53-05-03-0, AND 53Aug 10, 2007 · N801UP · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA070038OActuator · out of adjustDURING CLIMB-OUT FROM KTOL, THE GEAR DOORS NOT LATCHED LIGHT ILLUMINATED. THE CREW PERFORMED AN UP-LATCH CHECK AND THE LEFT MAIN GEAR DOOR OPEN YELLOW LIGHT ILLUMINATED. THE CREW RECYCLED GEAR AND HAD A SUCCESSFUL UPLATCH CHECK BUT DOOR NOT LATCHED LIGHT REMAug 10, 2007 · N603AL · Doug DC873F · Landing Gear ActuatorSDR UPS07850664Fitting · crackedINSPECTION TYPE:C1 MAIN CABIN FRAME FITTING CRACKED AT STA 980 L19L. REPAIRED MAIN CABIN FRAME FITTING AT STA 980 L19L IAW SAA EA 008- 5310-01-A1020, UPS RAA DC8-53-20655, AND FAA FORM 8100-9.Aug 9, 2007 · N874UP · Doug DC873F · Fuselage Main, FrameSDR UPS07850611Fitting · corrodedINSPECTION TYPE:C1 MAIN CABIN FRAME FITTING HAS EXFOLIATION CORROSION AND CRACK AT STA 940 L21L. REPAIRED FRAME FITTING AT STA 940 L21L IAW SAA EA 008-5310-01-A1016 UPS RAA DC8-53-20651, AND FAA FORM 8100-9.Aug 9, 2007 · N874UP · Doug DC873F · Fuselage Main, FrameSDR UPS07850504Longeron Splice · crackedINSPECTION TYPE:C1 .25 INCH CRACK LWR ROW STA 1749 ON L28R SPLICE AND EXISTING REPAIR THAT IS NOT PER SRO8530032. REMOVED EXISTING REPAIR AND CUT OUT DAMAGED AREA OF L28R SPLICE AT STA 1749 IAW SRO8530032. FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERSAug 9, 2007 · N874UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR IXXA07SMN199SSkin · dentedDURING ROUTINE C CHECK INSPECTION, LT WING OTBD FLAP LWR SKIN PANEL SHOWS (04EA) DENTS BETWEEN STA XF 415.000 AND STA XF 453.000.Aug 9, 2007 · N606AL · Doug DC873F · Trailing Edge FlapsSDR IXXA07SMN200SSkin · dentedDURING ROUTINE C CHECK INSPECTION, LT WING NON STANDARD REPAIR ON INBD SLOT VANE AT STA XS 247.000.Aug 9, 2007 · N606AL · Doug DC873F · Wing, Plate/SkinSDR IXXA07SMN204SSkin · dentedDURING ROUTINE C CHECK INSPECTION, EXT FUSELAGE UPPER SKIN WITH DENT AT STA FS 980.000 AND L-7 LT.Aug 9, 2007 · N606AL · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA07SMN203SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, RUDDER EXT SKIN WITH CORROSION AT STA ZR -253.000 RT SIDE.Aug 9, 2007 · N606AL · Doug DC873F · Rudder, Plate/SkinSDR IXXA07SMN202SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, RUDDER EXT SKIN WITH CORROSION AT STA ZR -162.000 RT SIDE.Aug 9, 2007 · N606AL · Doug DC873F · Rudder, Plate/SkinSDR UPS07850503Skin · corrodedINSPECTION TYPE:C1 MAJOR CORROSION BETWEEN STA 1620 - 1640 L31L - L31R, BETWEEN SKIN AND INTERNAL DOUBLER, CORROSION AROUND OUTFLOW VALVE. REMOVED AND REPLACED BELLY SKIN FROM STA 1490 - 1690 L31L - L31R IAW SRM 51-1-20D AND SRM 51-1-21.Aug 8, 2007 · N874UP · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA07SMN198SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, RT WING INBD FLAP UPPER SKIN SHOWS NON STANDARD REPAIR AND DENT BETWEEN STA XW 2.000 AND STA XW 92.000.Aug 8, 2007 · N606AL · Doug DC873F · Trailing Edge FlapsSDR IXXA07SMN197SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, RT WING INB FLAP PANEL LWR SKIN SHOWS (03EA) NON STANDARD REPAIR FROM STA XW 2.000 TO STA XW 92.000.Aug 8, 2007 · N606AL · Doug DC873F · Trailing Edge FlapsSDR IXXA07SMN195SSkin · dentedDURING ROUTINE C CHECK INSPECTION, RT WING OTBD FLAP AFT PANEL LWR SKIN SHOWS (03EA) DENTS BETWEEN STA XF 375.000 AND STA XF 405.000.Aug 8, 2007 · N606AL · Doug DC873F · Trailing Edge FlapsSDR IXXA07SMN196SSkin · dentedDURING ROUTINE C CHECK INSPECTION, RT WING OTBD FLAP AFT PANEL PLATING LWR SKIN SHOWS (04EA) DENTS BETWEEN STA XF 415.000 AND STA XF 453.000.Aug 8, 2007 · N606AL · Doug DC873F · Trailing Edge FlapsSDR IXXA07SMN194SSkin · dentedDURING ROUTINE C CHECK INSPECTION, LT WING INBD FLAP UPPER FWD PLATING SHOWS DENT BETWEEN STA XW 28.000 TO STA XW 91.000.Aug 8, 2007 · N606AL · Doug DC873F · Trailing Edge FlapsSDR DHL2007804525Skin · delaminatedNR 2 RT FLAP VANE LWR SKIN DELAMINATED. REMOVED AND REPLACED NR 2 RT FLAP VANE IAW MM 27-51-14 PG 201-202. REFER TO NR 060653 FOR OPS CHECK.Aug 7, 2007 · N804DH · Doug DC873F · Trailing Edge FlapsSDR DHL2007804520Panel · delaminatedRT WING T/E UPPER PANEL DELAMINATED (STA XA 566.000 - 613.000). REMOVED AND REPLACED DELAMINATED RT WING T/E UPPER PANEL (STA XA 566.000 - 613.000) IAW SRM 51-3-0, SRM 51-3-1 (TORQUE).Aug 7, 2007 · N804DH · Doug DC873F · Wing, Plate/SkinSDR DHL2007804519Panel · delaminatedLT WING T/E LWR PANEL DELAMINATED (STA XW 0.000 - 90.000). REMOVED AND REPLACED DELAMINATED LT WING T/E LWR PANEL (STA XW 0.000 - 90.000) IAW SRM 51-3-0, SRM 51-3-1 (TORQUE).Aug 7, 2007 · N804DH · Doug DC873F · Wing, Plate/SkinSDR DHL2007804518Panel · delaminatedRT WING T/E LWR PANEL DELAMINATED (STA XRS 162.000 - XF 219.000). REMOVED AND REPLACED DELAMINATED RT WING T/E LWR PANEL (STA XRS 162.000 - XF 219.000) IAW SRM 51-3-0, SRM 51-3-1 (TORQUE).Aug 7, 2007 · N804DH · Doug DC873F · Wing, Plate/SkinSDR DHL2007804517Panel · delaminatedRT WING T/E LWR PANEL DELAMINATED (STA XW 0.0000 - 47.000). REMOVED AND REPLACED DELAMINATED RT WING T/E LWR PANEL (STA XW 0.000 - 47.000) IAW SRM 51-3-0, SRM 51-3-1 (TORQUE).Aug 7, 2007 · N804DH · Doug DC873F · Wing, Plate/SkinSDR DHL2007804516Panel · delaminatedRT WING T/E LWR PANEL DELAMINATED (STA XW 97.000 - XRS 162.000). REMOVED AND REPLACED RT WING T/E LWR PANEL (STA XW 97.000 - XRS 162.000) IAW SRM 51-3-0, SRM 51-3-1 (TORQUE).Aug 7, 2007 · N804DH · Doug DC873F · Wing, Plate/SkinSDR UPS07850477Support Angle · corrodedINSPECTION TYPE:C1 CORROSION UNDER NUT PLATES IN AFT CABIN SUBFLOOR, STA 1746-1756 ALONG RBL 17. REMOVED SUPPORT, REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED SUPPORT ANGLE SRM 51-1-8, 51-1-21, 53-02-00, 51-3-0 DWG 2652479-87. REF Aug 7, 2007 · N874UP · Doug DC873F · Fuselage Miscellaneous Structure
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