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 UPS05845054Fitting · crackedMAIN CABIN INTERIOR LT SIDE FS 860 AFT SIDE L18L ATTACH FITTING CRACKED. REMOVED AND REPLACED ATTACH FITTING IAW SRM 51-1-20D.Jun 28, 2005 · N851UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05844979Fitting · crackedINSPECTION TYPE: C1, MAIN CABIN STA 900 LONGERON 3L FITTING CRACKED APPROX. 4 INCHES. REMOVED AND REPLACED LONGERON FITTING IAW DC-8 SRM 51-1-20D AND 51-1-2 1.Jun 28, 2005 · N851UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05844928Fitting · crackedINSPECTION TYPE: C1, STA 1220 BETWEEN L27R-L26R SPIDER FITTING HAS A CRACK RUNNING FROM BOLT HOLE TO LOWER RIVET. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.Jun 28, 2005 · N851UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05844927Fitting · crackedDURING X-RAY INSPECTION AND VERIFIED BY HFEC, A CRACK WAS FOUND ON ZEE FITTING, STA 340, BETWEEN LONG 30-31R. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.Jun 28, 2005 · N851UP · Doug DC873F · Fuselage Internal Mounting StructureSDR UPS05844926Longeron · crackedC1 LONG 15L AT APPROX STA 1744 HAS A CRACK AT UPPER FRAME ATTACH POINT. REMOVED DAMAGED SECTION OF LONGERON, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 53-2-2 FIG 10.Jun 28, 2005 · N851UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS05844925Longeron · crackedC1 LONG 14L AT APPROX STA 1743 IS CRACKED AT BOTH UPPER AND LOWER FRAME ATTACH POINTS. REMOVED DAMAGED SECTION OF LONGERON, FABRICATED, AND INSTALLED IAW DC- 8 SRM 53-2-2 FIG 10.Jun 28, 2005 · N851UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS05844924Longeron · crackedC1 LONG 16 AT APPROX STA 1745 IS CRACKED AT LWR FRAME TO LONG ATTACH POINT AT RADIUS, (LT CANTED FRAME). REMOVED DAMAGED SECTION OF LONGERON, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 53-2-2 FIG 10.Jun 28, 2005 · N851UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS05844923Longeron · crackedC1 CRACKED APPROX .5 ON LONG 14 UPPER FLANGE 2ND CANTED FRAME FROM STA 1766 INSIDE MAIN CABIN RT SIDE WALL. REMOVED DAMAGED SECTION OF LONGERON, FABRICATED, AND INSTALLED IAW DC-8 SRM 53-2-2 FIG 10.Jun 28, 2005 · N851UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS05844921Longeron · crackedINSPECTION TYPE: C1, CRACKED APPROX .5 INCH ON LONG 15 UPPER FLANGE 2ND CANTED FRAME FROM STA 1766 INSIDE MAIN CABIN RH SIDEWALL. REMOVED DAMAGE SECTION OF LONGERON, FABRICATED, AND INSTALLED REPAIR I AW DC-8 SRM 53-2-2 FIG 10.Jun 28, 2005 · N851UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS05844905Fitting · crackedINSPECTION TYPE C-1, MAIN CABIN STA 900 LONGERON 9R FITTING CRACKED APROX 3.0 IN. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D AND 51-1-21.Jun 28, 2005 · N851UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS05844904Fitting · crackedINSPECTION TYPE C-1, MAIN CABIN INTERIOR LT SIDE F/S 900 LONG 6L SPLICE FITTING CRACKED. REMOVED CRACKED SPLICE FITTING AND INSTALLED REPLACEMENT FITTING IAW DC-8 SRM 51-120D.Jun 28, 2005 · N851UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS05844903Fitting · crackedINSPECTION TYPE C-1, LT MAIN CABIN INTERIOR LONGERON 10L SPLICE FITTING CRACKED AT FS 860. REMOVED CRACKED SPLICE FITTING AND INSTALLED REPLACEMENT FITTING IAW DC-8 SRM 51-1-20D.Jun 28, 2005 · N851UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS05844902Fitting · crackedINSPECTION TYPE C-1, CRACKED FITTING AT F/S 760 BETWEEN LONGERONS 17 AND 18L. REMOVED CRACKED FITTING AND INSTALLED REPLACEMENT FITTING IAW DC-8 51- 1-20D.Jun 28, 2005 · N851UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS05844978Rib · crackedINSPECTION TYPE:C1 RH WING L/E UPPER RIB CRACKED AT XFS 728. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 57-3-3 AND 57-2-0 FIG 2.Jun 27, 2005 · N851UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05844919Skin · crackedC1 RT WING LE LWR SKIN CRACKED 1 INCH LONG AROUND FASTENER HOLE AT XW 257. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR IAW EO DC8-5720 -4087-B APPENDIX C.Jun 27, 2005 · N851UP · Doug DC873F · Wing, Plate/SkinSDR UPS05844918Skin · crackedINSPECTION TYPE: C1, LW NR 2 STUBWING UPPER OB CORNER HAS A CRACK IN SKIN. STOP DRILLED THREE CRACKS, FABRICATED, AND INSTALLED REPAIR IAW DC-8 S RM 57-2-0, 57-5-0, AND 57-2-1 FIG 18.Jun 27, 2005 · N851UP · Doug DC873F · Wing, Plate/SkinSDR UPS05844917Skin · scratchedC1 DEEP SCRATCHS IN SKIN L/W UPPER SPAR CAP IB CORNER OF NR 2 STUB WING. SCRATCHS FOUND OUT OF LIMITS, CUT OUT DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1 FIG 26.Jun 27, 2005 · N851UP · Doug DC873F · Wing, Plate/SkinSDR UPS05844901Rib · crackedINSPECTION TYPE C-1, RT WING L/E UPPER RIB CRACKED AT XFS 671. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR ANGLE DOUBLER IAW DC-8 SRM 57-2-0 FIG 2 AND 57-3-3 FIG 7.Jun 27, 2005 · N851UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05844900Rib · crackedINSPECTION TYPE C-1, RT WING L/E UPPER RIB CRACKED AT XFS 721. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR ANGLE DOUBLE IAW DC-8 SRM 57-2-0 FIG 2 AND 57-3-3 FIG 7.Jun 27, 2005 · N851UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05844899Rib · crackedINSPECTION TYPE C-1, RT WING L/E UPPER RIB CRACKED AT XFS 734. STOP DRILL CRACK, FABRICATED, AND INSTALLED REPAIR ANGLE DOUBLER IAW DC -8 SRM 57-2-0 FIG 2 AND 57-3-3 FIG 7.Jun 27, 2005 · N851UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05844897Pressure Blkhd · crackedINSPECTION TYPE C-1, AFT PRESSURE BULKHEAD IS CRACKED 0.5 IN LONG AT LBL 35 AND 66 IN FROM FLOOR. CUT OUT DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR FILLER IAW DC-8 SRM 53-2-5 FIG 14. THE -27 AND -25 DOUBLERS INSTALLED BY PREVIOUS REPAIR.Jun 26, 2005 · N851UP · Doug DC873F · Fuselage Main, BulkheadSDR UPS05844896Pressure Blkhd · crackedINSPECTION TYPE C-1, AFT PRESSURE BULKHEAD CRACKED 1.75 IN LONG AT RBL 26 AND 66 IN FROM FLOOR. CUT OUT DAMAGE SECTION, FABRICATED REPAIR DOUBLER, FINGER DOUBLER, AND FILLER AND INSTALLED IAW SRM 53-2-5 FIG 14A.Jun 26, 2005 · N851UP · Doug DC873F · Fuselage Main, BulkheadSDR UPS05845055Fitting · crackedSTA 759 BOOT FITTING CRACKED BETWEEN L17L AND L18L. REPAIRED BOOT FITTING IAW UPS EO DC8-53-2048 AND SAA SK 851-856307.Jun 25, 2005 · N851UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05844982Attach Fitting · corrodedINSPECTION TYPE: C1, FLOORBEAM VERTICAL ATTACH FITTING HAS HEAVY CORROSION. ALSO APPEARS TO BE CRACKED. STA 69 RBL 48. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-3-0.Jun 25, 2005 · N851UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05844977Fitting · crackedINSPECTION TYPE:C1 LWR FLOOR BEAM CRACKED ABOVE A-CARGO DOOR FRAME AT CUSP SAT 340. REMOVED AND REPLACED FLOORBEAM TO CUSP FITTING IAW DC-8 SRM 51-3-0.Jun 25, 2005 · N851UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05844916Bulkhead · crackedINSPECTION TYPE:C1 683 BULKHEAD CRACKED LBL 10 - RBL 24. CUT OUT DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 53 -2-5 FIG 13.Jun 25, 2005 · N851UP · Doug DC873F · Fuselage Main, BulkheadSDR UPS05844895Fitting · crackedINSPECTION TYPE C-1, VERTICAL LEG CRACKED BETWEEN FASTENERS STA 1220 AT LONGERON 27R. REMOVED CRACKED VERT LEG FITTING AND REPLACED IAW DC-8 SRM 51-1-20D AN D 51-1-21.Jun 25, 2005 · N851UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05844894Longeron · crackedINSPECTION TYPE C-1, LONG 11L CRACKED STA 670. REMOVED CRACKED LONGERON FITTING, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW DWG 5750540 AND DC-8 SRM 51-1-20D.Jun 25, 2005 · N851UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS05844893Fitting · crackedFLOORBEAM VERT ATTACH FITTING CRACKED STA 64 RBL 48. REMOVED CRACKED FITTING AND REPLACED IAW DC-8 SRM 51-1-21D.Jun 25, 2005 · N851UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS05844892Rib · crackedINSPECTION TYPE C-1, RT WING UPPER L/E RIB CRACKED 0.5 IN LONG AT XFS 584. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR ANGLES IAW DC-8 SRM 57-2-0 FIG 2.Jun 25, 2005 · N851UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05844915Skin · crackedINSPECTION TYPE:C1 C-4 DOOR UPPER FWD CORNER HAS A STEEL DOUBLER REPAIR AND MUST BE REPLACED WITH AN APPROVED REPAIR. REMOVED DOUBLER AND FILLER, FOUND CRACK AT PREVIOUS CUT OUT, CUT OUT DAM AGED AREA, FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0 FIG 2Jun 23, 2005 · N851UP · Doug DC873F · Cargo/Baggage DoorsSDR UPS05844891Skin · crackedINSPECTION TYPE C-1, LT FUSELAGE EXTERIOR SKIN CRACKED 1 IN LONG AT STA 1746 BETWEEN L14L TO L15L. REMOVED DAMAGED AREA OF SKIN, FABRICATED, AND INSTALLED REPAIR DOUBLER, FINGER DOUBLERS, AND FILLERS IAW DC-8 SRM 53-2-1 FIG 7.Jun 23, 2005 · N851UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS05844684Battery Pack · inoperativeEMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK IAW DC8 MM 33-50-01-2. TEST OK.Jun 8, 2005 · N851UP · Doug DC873F · Emergency LightingSDR DHL2005801012Mec · malfunctionedAT FL.360. NR 1 ENGINE FLAMED OUT. NR 1 MAIN FUEL QUANTY GUAGE WAS SHOWING 2000 LBS. W/INTERMITTED FUEL SELECTED. THERE WAS NO MASTER CAUTION OR NR 1QT.LOW LIGHT. REPLACED NR 1 ENGINE MEC PER CFM 56 M/M CH. 73-21-10. OPS CHECKS NORMAL ON ENGINE RUN. FAULT 5Jun 6, 2005 · N801DH · Doug DC873F · Engine (Turbine/Turboprop)SDR UPS05844758Skin · gougedINSPECTION TYPE:C-3. RT FS 70 L31R AND L32R, DEEP GOUGES ON EXTERIOR SKIN. REMOVED DAMAGED SKIN SECTION. FABRICATED AND INSTALLED REPAIR DOUBLER, TRIPLER AND FILLER IAW EO DC8-53-20473 AND SAA SK840-808375.Jun 3, 2005 · N840UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS05844748Longeron · corrodedAFTER REMOVAL OF L33R END FITTING STA 8 FOUND L33R CORRODED OUT OF LIMITS STA 8. REF N/R 807385. REMOVED AND REPLACED LONGERON 33R STA 8 TO 70 IAW SRM 51-1-21, 1-1-21D AND 51-3-2.Jun 2, 2005 · N840UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS05844700Rib · crackedLT WING CENTER L/E AT XFS 335 RIB CRACKED ON L/E LOWER SURFACE. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2 -0 FIG 2, 51-1-20D, AND 51-1-21.Jun 1, 2005 · N840UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05844743Frame · corrodedDEEP CORROSION AROUND SHEAR TIE FASTENER HEADS AFT SIDE OF FRAME, STA 1300 LONGERON 36. REMOVED CORROSION AND FOUND FRAME OUT OF LIMITS. REMOVED DAMAGED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0 FIG 2.May 29, 2005 · N840UP · Doug DC873F · Fuselage Main, FrameSDR UPS05844757Fitting · crackedINSPECTION TYPE:C-3. WING BOX BOOT FITTING CRACKED APPROX 5 IN LONG STA 759 BETWEEN L17L-L18L. CUT OUT CRACKS, FABRICATED AND INSTALLED REPAIR PARTS IAW SAASK 840-808203 AND EO DC853-20469.May 28, 2005 · N840UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS05844559Case · leakingINSPECTION TYPE:N/A EMERGENCY DECLARED, NR 3 ENGINE HYDRAULIC CASE DRAIN FILTER DUE INSPECTION DUE TO LOSS OF HYDRAULIC PRESSURE. LANDED UNEVENTFUL AND TOWED TO RAMP TWO. REMOVED AND REPLACED NR 3 ENGINE HYDRAULIC CASE DRAIN FILTER IAW MM 29-1 0-15-2, FILTERMay 28, 2005 · N880UP · Doug DC873F · Hydraulic System, MainSDR UPS05844705Longeron · crackedCRACK APPROX 3 INCHES LONG ON LONGERON 35R AT FS 1270. REMOVED DAMAGED SECTION OF LONGERON. FABRICATED AND INSTALLED REPLACEMENT SECTION OF LONGERON IAW DC-8 SRM 51-1-20D AND DWG'S 3758593 AND 575 0322.May 27, 2005 · N840UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS05844703Fitting · crackedCRACKED FITTING ON TORQUE BOX AT CARGO DOOR AT FS 1160 BETWEEN L31 AND L32 R. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.May 27, 2005 · N840UP · Doug DC873F · Fuselage Main, StructureSDR UPS05844698Splice · crackedLONGERON SPLICE FITTING CRACKED AT STA 1260 TO 1280 L36. REMOVED AND REPLACED LONGERON SPLICE FITTING IAW DC-8 SRM 51-1-20D.May 27, 2005 · N840UP · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2005801011Actuator · faulty"DOORS NOT LATCHED" LIGHT (UPPER LEFT) REMAINED ON FOR EXTENDED PERIOD AFTER TAKEOFF/GEAR RETRACTION (ABOUT 1 MIN) THEN FLASHED INTERMITTENTLY FOR 2-3 MINS BEFORE STAY ON,GO OUT, ALSO HAD RT. R & R RT MLG DOOR ACTUATING CYLINDER AND CONTROL VALVE IAW MM 32-3May 27, 2005 · N801DH · Doug DC873F · Landing Gear Door ActuatorSDR DHL200580110Wire · looseDOOR NOT LATCHED LIGHT VERY SLOW TO GO OUT AFTER GEAR RETRACTION DOOR NOT LATCHED LIGHT BRIEFLY ILLUMINATED WHEN FLAPS REACHED UP POSITION NORMAL GEAR UPLATCH CHECK NO LIGHTS ON S/O PANEL. INSPECTED TERMINAL ENDS AND FOUND LOOSE CONNECTIONS AT TERMINAL STRIP May 27, 2005 · N801DH · Doug DC873F · Landing Gear System WiringSDR UPS05844515Window · failedCREW REPORTED WINDOW WAS ARCING AND TURNED OFF WINDOW HEAT. 30 SECONDS LATER, WINDOW SHATTERED (CAPTAIN'S SIDE WINDOW). REMOVED AND REPLACED LEFT SIDE WINDOW PER MM 56-10-02-2. OPERATIONAL A ND LEAK CHECK NORMAL.May 26, 2005 · N802UP · Doug DC873F · Flight Compartment WindowsSDR DHL2005801009Switch · out of adjustAFTER TAKEOFF UPON GEAR RETRACTION, THE RED DOORS NOT LATCHED LIGHT AND THE RIGHT DOOR UNSAFE LIGHT ILLUMINATED WITH THE GEAR HANDLE UP. BOTH LIGHTS EXTINGUISHED AFTER 10 SECONDS. ADJUSTED RIGHT MAIN GEAR DOOR SWITCH. PERFORMED OPERATIONS CK SYSTEM, OP CHECMay 26, 2005 · N801DH · Doug DC873F · Landing Gear Position and WarningSDR UPS05844759Panel · corrodedHEAVY CORROSION ON LT WW CEILING STA 860 LBL 61. CUT OUT DAMAGE AND INSTALLED REPAIR PARTS IAW EO DC8-5310-22401-A AND SAA SK 840-807868.May 25, 2005 · N840UP · Doug DC873F · Fuselage Main, BulkheadSDR UPS05844755Skin · crackedINSPECTION TYPE:C-3. EXTERNAL FUSELAGE L1 DOOR CUTOUT UPPER AFT CORNER, SKIN VISUALLY CRACKED. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER IAW EO DC8 5330-22342-A AND SAA SK 840-807798.May 25, 2005 · N840UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS05844701Fuel Tank · damagedRT AUX TANK UPPER SURFACE FASTENER HOLE ELONGATED AT XW 208. FABRICATED REPAIR DOUBLER, INSTALLED CONICAL WASHERS AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 57-2-1 FIG 37, 51-1-26, 51-1-20D, AND 51-1-21.May 25, 2005 · N840UP · Doug DC873F · Fuel Storage
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