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 UPS04842444Skin · dentedINSPECTION TYPE:C-2 JUST BELOW LOWER CUTOUT OF MAIN CARGO DOOR, FUSELAGE SKIN HAS TWO DENTS. REMOVED FASTENER IN SKIN FS 200-220, RMVD DAMAGE SECTION OF SKIN AT FS 210 MATERIAL ID FOR DOUBLER REPAIR EXTERNAL DOUBLER 7075-T6.080 PO 43557 21 FILLER 2024-T-3,071May 13, 2004 · N818UP · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2004805004Battery Pack · dischargedA/C EMERGENCY POWER BATTERY PACK DISCHARGED. REMOVED AND REPLACED A/C EMERGENCY BATTERY PACK, OPS CHECKED GOOD IAW DC-8 MM.May 13, 2004 · N805DH · Doug DC873F · Emergency LightingSDR UPS04842479Longeron · corrodedINSPECTION TYPE: C-2, CORROSION ON FUSELAGE SKIN AND AROUND FASTENER HOLES FS 300-320 L29L. REMOVED CORROSION AND FOUND OUT OF LIMITS ORIG THICKNESS .063 THINNEST SPOT .034 720 IAW DC8 SRM 51-1-8 AND 53-2-0. FAB, ALODINED, PRIMED AND INSTALLED 31 REPAIR ANGLMay 12, 2004 · N818UP · Doug DC873F · Fuselage Main, StructureSDR UPS04842450Frame · corrodedINSPECTION TYPE:C-2 CORROSION ON FRAME AT FS 180 L35L-35R. REMOVED CORROSION, FOUND BLENDOUT BEYOND ALLOWABLE LIMITS IAW SRM 53-2-0 FIG 1F. FAB -9 DOUBLER, -11 FILLER IAW EO 11728-B AND UPS DWG 53A-011A. INSTALLED PARTS IAW EO AND DWG. ALODINED AND PRIMED IAWMay 12, 2004 · N818UP · Doug DC873F · Fuselage Main, FrameSDR UPS04842544Seat Track · corrodedINSPECTION TYPE:C-2 ALC, CORROSION AROUND FASTENERS, HOLE ON CABIN, FLOORBOARD PANEL FS 1040 RBL 45. REMOVED CORROSION FOUND OUT OF LIMITS. REMOVED FLOORBOARD FROM 840 TO 1060 RT RBL 45, CUT SEAT TRACK FROM 870-1050 IAW EO DC853205167C, MAT ID SEAT TRACK ANDMay 10, 2004 · N818UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS04842482Shear Tie · corrodedINSPECTION TYPE: C-2, MAIN CABIN L-2 DOOR TORQUE BOX AFT EDGE INT STRUCTURE SHEAR TIE GOUGED. BLENDED GOUGED AREA. ORIG MAT THICKNESS .080 DAC DWG 5616606. REMOVED INTERCOSTAL 8 & 9. REC'D PART FROM HEAT TREAT IN T6 CONDITION IAW DAC DWG 5616666 AND FAB NEMay 10, 2004 · N818UP · Doug DC873F · Fuselage Main, StructureSDR UPS04842481Doubler · corrodedINSPECTION TYPE: C-2, AREA AROUND LOWER TAIL NAV LIGHT CORROSION & NUT PLATES BAD. REMOVED DOUBLER P/N 5704650-21 IAW DC8 SRM 51-1-21. LOCATED AND DRILLED NEW DOUBLER P/N 5704650-21 IAW DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-21.May 10, 2004 · N818UP · Doug DC873F · Fuselage Main, StructureSDR UPS04842540Skin · corrodedINSPECTION TYPE:C-2, FS 1400 D PIT EXTERIOR CUTOUT SKIN CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. FAB REPAIRED DOUBLER IAW REO GO9822. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED DOUBLERS IAW DC8 SRM 51-1-20D AND REO GMay 9, 2004 · N818UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS04842539Spar · crackedINSPECTION TYPE:C-2, RIGHT WING FWD SPAR AT XFS 520.00 HAS 500 HOLE WITH CRACK INDICATED. REPAIRED RIGHT WING FWD IAW DWG J060232-532 CONF AND REO GO9802May 9, 2004 · N818UP · Doug DC873F · Wing SparSDR DHL2004801005Drive Link · crackedDURING NDT INSPECTION OF RT IB FLAP DRIVE LINK FOUND CRACK OUT OF LIMITS ON LINK. REMOVED AND REPLACED RT IB FLAP DRIVE LINK IAW M/M 27-51-4. OPS CHECKED OK.May 9, 2004 · N801DH · Doug DC873F · Trailing Edge Flap Control SystemSDR IXXA060134SSkin · tornDURING ROUTINE C CHECK, FOUND RIGHT HAND OUTBOARD FLAP OUTBOARD TRAILING EDGE WEDGE LOWER SKIN GOUGED AND TORN. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTMay 8, 2004 · N605AL · Doug DC873F · Trailing Edge FlapsSDR UPS04842545Fitting · corrodedINSPECTION TYPE: C-2, FWD OF AFT PRESSURE BULKHEAD AT BS 1766 LONGERON 30 SPLICE FITTING HAS CORROSION (DOT E 2880). REMOVED CRACKED FITTING. FOUND OUT OF LIMITS. REC'D LONGERON END FITTING P/N 4772398-1 PO 446277.2 IAW DWGS 4772398. LOCATED, DRILLED & DEBMay 8, 2004 · N818UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS04842538Fitting · crackedINSPECTION TYPE:C-2, AFT PIT LOWER BILGE BETWEEN STA 1040-1080 L35L HAS CORROSION INSIDE CHANNEL. REMOVED CORROSION FOUND TO BE WITHIN LIMITS. REMOVED LONGERON SPLICE CLIP AND INTERCOSTAL STA 1040-1060. LONGERON SPLICE FOUND TO BE CRACKED, REC'D LOCATED ANMay 8, 2004 · N818UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS04842451Splice · crackedINSPECTION TYPE:C-2 FWD OR AFT PRESSURE BULKHEAD AT BS 1766 30L SPLICE FITTING HAS CORROSION. REMOVED FITTING. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS AND CRACKED. REC'D FITTING P/N 4772398-1 PO 446277. LOCATED AND DRILLED AND DEBURR FITTING INSTALLED FMay 8, 2004 · N818UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS04842448Splice · crackedINSPECTION TYPE:C-2 AFT PIT LOWER BILGE BETWEEN STA 1040-1080 L35R HAS CORROSION INSIDE CHANNEL. REMOVED CORROSION STA 1040-1080. NO MATERIAL LOSS IAW SRM 53-4-1 AND DAC DWG 9758507. FOUND WITHIN LIMITS. LONGERON SPLICE FOUND TO BE CRACKED. REC'D LOCATED ANDMay 8, 2004 · N818UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS04842537Frame · corrodedINSPECTION TYPE:C-2 AFT PIT LOWER BILGE FWD WALL AREA FRAME STA 1000 BETWEEN L27R AND 27L EXFOLIATED ON FWD SIDE IN NUMEROUS AREAS. REMOVED CORROSION OUT OF LIMITS. CUT OFF DAMAGED SECTION FROM L34L-L34R IAW DC8 SRM 53-2-0. LOCATED AND DRILLED FRAME SECTIONMay 7, 2004 · N818UP · Doug DC873F · Fuselage Main, FrameSDR UPS04842484Seat Track · corrodedINSPECTION TYPE: C-2, FWD PIT STA 260-280, RBL, WL 0, CORROSION EMINATING, FROM BENEATH NUT PLATES AND NUT PLATES CORRODED FLOOR PLK B6014. REMOVED CORROSION FROM SEAT TRACK. FOUND TO BE OUT OF LIMITS MAT ID FOR SEAT TRACK IS 52772660 7075-T6 EXT PO SP091664May 7, 2004 · N818UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS04842483Fitting · corrodedINSPECTION TYPE: C-2, FLOORBEAM END FITTING AT STA 260 RT CUSP EXFOLIATED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-8, 51-1-20D, 51-1-21, 51-1- 24.May 7, 2004 · N818UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS04842447Clip · corrodedINSPECTION TYPE:C-2 MAIN CABIN RT CUSP AT LWR FWD CORNER OF R2 DOOR (FS 1620) EXFOLIATION CORROSION. REMOVED CORROSION ON CLIP IAW DC8-SRM 51-1-8, OUT OF LIMITS. MAT ID AND FAB CUSP CLIP IAW DAC DWG 4773150 PERFORMED DYE PEN TEST. ALODINE AND PRIME CUSP CLIMay 7, 2004 · N818UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS04842445Doubler · gougedINSPECTION TYPE:C-2 LW OB FLAP UPPER SURFACE DOUBLER GOUGED AT I/B ICE BREAKER GUIDE TRACK STA XF219. REMOVED DAMAGED DOUBLER FAB NEW DOUBLER ALODINED AND PRIMED INSTALLED NEW DOUBLER.May 6, 2004 · N818UP · Doug DC873F · Trailing Edge FlapsSDR UPS04842536Structure · bentINSPECTION TYPE:C-2, RIGHT WING I/B FLAP I/B END (LIP) BENT AT AFT AREA, CHAFING FILLET PANEL 192 U. FABBED NEW WEB AND DOUBLER REPAIR IAW REO G09806.May 5, 2004 · N818UP · Doug DC873F · Trailing Edge FlapsSDR UPS04842443Skin · corrodedINSPECTION TYPE: C-2 FUSELAGE SKIN CORRODED ALONG LONGERON 21R AT FS 8 AND FS55 EO DC8-5330-19540-A INSTALLED TEMP REPAIR, INSTALL PERMANENT REPAIR AT NEXT C- CHECK. GEN AND RECEIVED RFTS N818UP-1-20760. REMOVED FASTENERS STA-9 TO STA-70 L2OR -L24 RMVD TEMPMay 4, 2004 · N818UP · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2004805003Switch · malfunctionedTAKEOF WARNING HORN SOUNDED AFTER ADVANCING THRUST FOR TAKEOFF. REJECTED TAKEOFF PER S.O.P. A/C WEIGHT 206200, IAS 0, OAT CEL 10, PRESS ALTITUDE 833, BRAKE ENERGY ZONE NORMAL FOUND BUILDUP OF DEBRIS ON FLAP/SWITCH FOLLOWUP CAM. CLEANED AND OPS CHECKED May 2, 2004 · N805DH · Doug DC873F · Trailing Edge Flap Control SystemSDR UPS04842308Screw · corrodedTWENTY SCREWS & NUTPLATES CORRODED OUT OF BOTTOM OF LEFT REAR L1 TYPE DOOR. REPAIRED LEFT REAR TYPE 1 EXIT DOOR PER DC8 EO DC8-5220-19783F.Apr 28, 2004 · N840UP · Doug DC873F · FastenersSDR DHL2004873004Windshield · crackedRT WINDSHIELD (R1) HAS A 6 INCHES CRACK IN THE LOWER LT CORNER. CRACK IS IN OUTER PANE. CRACK DOES NOT OBSTRUCT VIEW. R & R RT WINDSHIELD IAW M/M 56-10-2. WINDSHIELD HEAT TESTED OK.Apr 23, 2004 · N873SJ · Doug DC873F · Flight Compartment WindowsSDR UPS04842168Seat Track · corrodedINSPECTION TYPE:C3 STATION 786 TO 798 BL 0 SEAT TRACK IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED SEAT TRACK SECTION BETWEEN STATION 750 TO 810 IAW SRM 53-2-3 FIG 14.Apr 8, 2004 · N812UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004807006Switch · malfunctionedDOORS NOT LATCHED LIGHT FLICKER INTERMITTENT IN FLIGHT WITH GEAR RETRACTED. DOOR NOT LATCHED INDICATING LIGHT MAY BE INOPERATIVE PER MEL -B- 32-8 DMI 16255 PLACARD INSTALLED. DMI 16255 DOORS NOT LATCHED LIGHT FLICKERS INTERMITTENT IN FLIGHT WITH GEAR RETRACTApr 7, 2004 · N807DH · Doug DC873F · Door Warning SystemSDR IXXA0500062OWarning Light · illuminatedDURING TAKEOFF FROM TAPA CREW REJECTED TAKEOFF DUE TO NR 1 ENGINE OIL LOW PRESSURE LIGHT ILLUMINATING AT 110KNTS. CREW RETURNED TO REMOTE PARKING WITHOUT INCIDENT. BRAKE ENERGY CHART CHECKED. MAINTENANCE DEFERRED IN ACCORDANCE WITH MEL 79-7 CAT "D".Apr 6, 2004 · N606AL · Doug DC873F · Engine Oil PressureSDR UPS04842125Web · corrodedINSPECTION TYPE: C3, STATION 1190 LONG 33L UPPER WEB IS CORRODED BEYOND LIMITS, WEB BELOW C-PIT DOOR. BLENDED OUT CORROSION, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 25.Apr 6, 2004 · N812UP · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2004805002Pump · faultyNR 3 ENGINE FLAMED OUT AT 35,000, MACH .84. COMPLETED IN-FLIGHT ENGINE FAILURE CHECK LIST. COMPLETED IN-FLIGHT ENGINE START ABNORMAL PROCEDURE, AND IN-FLIGHT ENGINE SHUTDOWN CHECK LIST (5 PSI OIL). TROUBLESHOT PER CFM 56 M/M 71-00-00, FAULT 51. NO DEFECTS Apr 6, 2004 · N805DH · Doug DC873F · Fuel Boost PumpSDR IXXA0400064SPanel · corrodedDURING ROUTINE C-CHECK INSPECTION RT WING INBD L/E SLANT PANEL UPPER SKIN SURFACE CORRODED, STA XCW 69.000 AND XFS 207.000. REPAIR ACCOMPLISHED BY PERFORMING MAJOR REPAIR IAW DC8 SRM 57-1-0 PG 1, FAX TIN-N 043, BOEING MESSAGE DATE 03/31/2004. REMOVED CORROSIApr 4, 2004 · N603AL · Doug DC873F · Wing, Plate/SkinSDR UPS04842121Fitting · corrodedINSPECTION TYPE: C3, LEFT WING FLAP HINGE 219 CANOE FITTING HAS PITTING CORROSION. MILLED OUT CORROSION, FABRICATED AND INSTALLED REPAIR FILLERS IAW SB 27-164.Apr 4, 2004 · N812UP · Doug DC873F · Wing, Attach FittingsSDR UPS04842224Intercostal · crackedINSPECTION TYPE:C3 STATION 25 AT LONG 21L ANGLE IN FWD ENTRY DOOR FWD JAMB IS CRACKED. REMOVED, CRACKED INTERCOSTAL, FABRICATED AND INSTALLED INTERCOSTAL IAW DWG 5597646 AND SRM 51-1-20D, 51-1-21.Apr 3, 2004 · N812UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS04842237Frame · corrodedINSPECTION TYPE: C3, STATION 1040 FRAME AND FRAME CAP ARE CORRODED BEYOND LIMITS AT LONG. 35L CUTOUT DAMAGED FRAME AT STATION 1040 LONG. 35L, FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW DC8-53A-010 AND REPLACED FRAME CAP IAW SRM. 53-1-0,51-1-20D,51-1Apr 2, 2004 · N812UP · Doug DC873F · Fuselage Main, FrameSDR UPS04842231Splice · crackedINSPECTION TYPE:C3 LONG 35L SPLICE FITTING IS CRACKED STATION 1040-1060. REMOVED AND REPLACED FITTING IAW DWG 3750545 AND SRM 51-1-20D.Apr 2, 2004 · N812UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS04842230Attach Fitting · crackedINSPECTION TYPE:C3 INTERCOSTAL ATTACH FITTING IS CRACKED AT STATION 1150 AT LONG 33R. REMOVED AND REPLACED INTERCOSTAL IAW DWG 4758514 AND SRM 51-1-20D.Apr 2, 2004 · N812UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS04842229Attach Fitting · crackedINSPECTION TYPE:C3 INTERCOSTAL ATTACH FITTING IS CRACKED AT STATION 1140 AT LONG 35R. REMOVED AND REPLACED FITTING IAW DWG 3758497 AND SRM 51-1-20D.Apr 2, 2004 · N812UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS04842226Bracket · crackedINSPECTION TYPE:C3 CIRCUMFERENTIAL TIE BRACKET IS CRACKED AT LONG 3L AND 3R AT APPROX STATION 1790. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW DWG 5612148 AND SRM 51-1-21, 51-1-20D.Apr 2, 2004 · N812UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS04842167Frame · corrodedINSPECTION TYPE:C3 STATION 1060 FRAME IS CORRODED BEYOND LIMITS AT LONG 35L. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC8-53A-010.Apr 2, 2004 · N812UP · Doug DC873F · Fuselage Main, FrameSDR UPS04842166Shear Tie · corrodedINSPECTION TYPE:C3 STATION 1000 BETWEEN LONG 28L TO 29L SHEAR TIE IS CORRODED. REMOVED, FABRICATED AND REPLACED SPLICE PLATE AND FILLER IAW SRM 53-2-0 FIG 2A AND 2B.Apr 2, 2004 · N812UP · Doug DC873F · Fuselage Main, StructureSDR UPS04842124Frame · corrodedINSPECTION TYPE: C3, STATION 1040 FRAME IS CORRODED AT LONG 36. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC8-53A-010.Apr 2, 2004 · N812UP · Doug DC873F · Fuselage Main, FrameSDR UPS04842266Fitting · corrodedINSPECTION TYPE: C3, RT WING FLAP HINGE 98 CANOE FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED CANOE FITTING I.A.W. DWG. 5614372,M/M.27-51-12, SAA SK 812-411,AND UPS ENGINEERING FILE NUMBER DC8-57-20109Apr 1, 2004 · N812UP · Doug DC873F · Trailing Edge FlapsSDR UPS04842238Rib · crackedINSPECTION TYPE: C3, LEFT WING INBOARD STUB WING UPPER RIB IS CRACKED AT XS 250. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED 2 ANGLE DOUBLERS IAW SRM. 57-2-0 FIG. 2Apr 1, 2004 · N812UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS04842235Support Angle · corrodedINSPECTION TYPE: C3, TORQUE BOX SUPPORT ANGLE IS CORRODED BEYOND LIMITS AT STATION 280 LONG. 33R. REMOVED, FABRICATED AND REPLACED SUPPORT ANGLE IAW DWG. 9754020 AND SRM. 51-1-20D.Apr 1, 2004 · N812UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS04842228Longeron · crackedINSPECTION TYPE:C3 STATION 1734 LONG 15L IS CRACKED. CUT OUT DAMAGE LONGERON BETWEEN STATION 1710 TO 1760, FABRICATED AND INSTALLED LONGERON, STRAPS AND SPLICE FITTINGS IAW SRM 53-2-2 FIG 10.Apr 1, 2004 · N812UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS04842227Attach Angle · crackedINSPECTION TYPE:C3 STATION 1766 LEFT SIDE THE LOWER ATTACH ANGLE AT UPPER CANTED BULKHEAD IS CRACKED BETWEEN LONGERON 9L AND 10L. REMOVED, FABRICATED AND INSTALLED ANGLE IAW DWG 5772706 AND SRM 51-1-20D, 51-1-21.Apr 1, 2004 · N812UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS04842225Longeron · crackedINSPECTION TYPE:C3 STATION 1746 LONG 15R IS CRACKED. CUT OUT DAMAGED LONGERON SECTION BETWEEN STATION 1736-1760, FABRICATED AND INSTALLED LONGERON SECTION, STRAPS AND INSTALLED LONG SPLICE REPAIR IAW SRM 53-2-2 FIG 10.Apr 1, 2004 · N812UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS04842170Attach Angle · crackedINSPECTION TYPE:C3 AFT PRESSURE BULKHEAD CENTER POST UPPER ATTACH ANGLE IS CRACKED STATION 1766 BL 0. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 5773844 AND SRM 51-1-21, 51-1-20D.Apr 1, 2004 · N812UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS04842169Web · corrodedINSPECTION TYPE:C3 STATION 922 BLB 63 FINGER DOUBLER AND PRESSURE WEB IS CORRODED BEYOND LIMITS. REMOVED FINGER DOUBLER, CUT OUT DAMAGE, FABRICATED AND INSTALLED FINGER DOUBLERS, FILLER SPLICE STRAP AND REPAIR DOUBLER IAW SRO8530026.Apr 1, 2004 · N812UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS04842162Angle · crackedINSPECTION TYPE:C3 LEFT WING I/B STUB WING VERTICAL ANGLE IS CRACKED AT LOWER END AT XS 246.5. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753293 AND SRM 51-3-0, 51-1-20D.Apr 1, 2004 · N812UP · Doug DC873F · Wing Miscellaneous Structure
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