Douglas DC-8-71F

Service difficulty reports · 8,938

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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 = 'DC871F'
  ORDER BY difficulty_date DESC"

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SDR UPS98828042Fitting · crackedINSPECTION TYPE-C, STA 1220 RT SIDE, THE FLOORBEAM SUPPORT FITTING HAS A 5 INCH CRACK. REMOVED AND REPLACED FITTING IAW DWG 9754024 AND SRM 51-1-20D.Oct 13, 1998 · N729UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98828039Longeron · crackedINSPECTION TYPE-C, STA 290 AT STR 35L O/B LEG IS CRACKED. REPAIRED AREA IAW SRM 53-2-2 FIG 10.Oct 13, 1998 · N729UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS98828038Fitting · crackedINSPECTION TYPE-C, STA 1280 AT STR 21L, THE FRAME TO CUSP LWR TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 9755536 AND SRM 51-1-20D.Oct 13, 1998 · N729UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98828030Skin · crackedINSPECTION TYPE-C, AFT SERVICE DOOR NR 17 FWD LWR CORNER CRACK ON INNER SKIN FROM EDGE TO FASTENER .625 INCH LONG. REPAIRED IAW UPS EO DC8-5330-10839-A.Oct 13, 1998 · N729UP · Doug DC871F · Service DoorsSDR UPS98828017Cargo Track · corrodedINSPECTION TYPE:C LOWER CARGO TRACK CORRODED F/S 1330-1410 L-34L. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT TRACK IAW SRM 51-3-0 AND DWG 5779223.Oct 13, 1998 · N729UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS98828016Floorbeam · crackedINSPECTION TYPE:C F/S 1160 AT THE RT CUSP, THE FLOORBEAM TO CUSP FITTING IS CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-21 AND DWG 3754946.Oct 13, 1998 · N729UP · Doug DC871F · Fuselage Main, Floor BeamSDR UPS98827971Fitting · crackedINSPECTION TYPE-C, FS 1288 AT LONG 21R, THE FRAME TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-2OD AND SRM 51-3-0.Oct 13, 1998 · N729UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98827970Fitting · crackedINSPECTION TYPE-C, FS 1334 AT LONG 21R, THE FRAME TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0.Oct 13, 1998 · N729UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98827969Fitting · crackedINSPECTION TYPE-C FS STA 270 AT LONG 33R TO 30R THE TORQUE BOX FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.Oct 13, 1998 · N729UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98827968Web · crackedINSPECTION TYPE-C, FWD ENTRY DOOR INNER SKIN AT THE BAYONET CUTOUT IS CRACKED. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 52-2-0.Oct 13, 1998 · N729UP · Doug DC871F · Passenger/Crew DoorsSDR UPS98827967Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB AT XS 250.089 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Oct 13, 1998 · N729UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS98827966Angle · crackedINSPECTION TYPE-C, LT WING L/E VERTICAL FWD ANGLE CRACKED AT O/B END OF THE I/B SLOT. REMOVED, FABRICATED AND REPLACED VERTICAL ANGLE IAW DWG 9753293 AND SRM 51-1-20D AND 51-3-0.Oct 13, 1998 · N729UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS98827965Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB AT XFS 385.25 IS CRACKED 16 FWD OF THE T/E. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Oct 13, 1998 · N729UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS98827964Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB AT XFS 691.250 IS CRACKED AT THE AFT LWR END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Oct 13, 1998 · N729UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS98828051Fitting · crackedINSPECTION TYPE-C, THE RT LWR AUX SPAR TO REAR SPAR STA 98 TIE FITTING IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW DHC SK- 729-846 AND SRM 51-3-0.Oct 12, 1998 · N729UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS98828032Skin · crackedINSPECTION TYPE-C, RT WING L/E SKIN INTERNAL DOUBLER AT THE NR 3 PYLON CUTOUT IS CRACKED AT THE OPENING. REPAIRED IAW SRM 57-2-1.Oct 11, 1998 · N729UP · Doug DC871F · Wing, Plate/SkinSDR UPS98828031Skin · crackedINSPECTION TYPE-C, THE RT I/B AILERON UPPER L/E SKIN AT THE ACTUATOR IS CRACKED AT ONE SCREW HOLE. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SKIN IAW SRM 51-1-21 AND DWG 5705334.Oct 11, 1998 · N729UP · Doug DC871F · AileronsSDR UPS98828026Rib · crackedINSPECTION TYPE-C, RT WING L/E RIB AT STA 691.25 IS CRACKED AT THE AFT LWR END. REPAIRED IAW SRM 57-2-0.Oct 11, 1998 · N729UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS98827963Fitting · corrodedINSPECTION TYPE-C, FITTING LT W/W AT LONG 23L FS 960 HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 FIG 8.Oct 11, 1998 · N729UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98827962Angle · crackedINSPECTION TYPE-C, RT WING L/E VERTICAL ANGE JUST I/B OF XS 250.089 AND AFT OF THE SLOT IS CRACKED AT THE LWR END. REMOVED, FABRICATED AND REPLACED VERTICAL ANGLE IAW DWG 9753293 AND SRM 51-1-20D AND 51-3-0.Oct 11, 1998 · N729UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS98827961Rib · crackedINSPECTION TYPE-C, RT WING L/E RIB AT XFS 653.75 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Oct 11, 1998 · N729UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS98827960Skin · crackedINSPECTION TYPE-C, RT WING L/E LWR SKIN AT XFS 163.75 IS CRACKED JUST FWD OF THE REPAIR DOUBLER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2A.Oct 11, 1998 · N729UP · Doug DC871F · Wing, Plate/SkinSDR UPS98827959Skin · crackedINSPECTION TYPE-C, RT WING L/E UPPER SKIN XFS 622.5 AND 628.75 IS CRACKED. STOP DRILLED CRACKS AND REPAIRED IAW SRM 57-2-1 FIG 38.Oct 11, 1998 · N729UP · Doug DC871F · Wing, Plate/SkinSDR UPS98827958Skin · crackedINSPECTION TYPE-C, RT WING L/E SKIN AT THE L/E XW 258 IS CRACKED AT A FASTENER HOLE. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-1 FIG 2H.Oct 11, 1998 · N729UP · Doug DC871F · Wing, Plate/SkinSDR UPS98827957Skin · crackedINSPECTION TYPE-C, TR WING UPPER SKIN AT XRS 74 AND STR 12 HAS A STRESS CORROSION CRACK. CUT OUT DAMAGE AND REPAIRED IAW SRM 57-2-1 FIG 10.Oct 11, 1998 · N729UP · Doug DC871F · Wing, Plate/SkinSDR UPS98828006Doubler · corrodedINSPECTION TYPE:C FWD EXTERNAL RT FUSELAGE CORROSION ON PANEL LAND AT DEACTIVATED LAVATORY SERVICE PANEL. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21, DWG 5755443, AND DHC SK-729-598.Oct 10, 1998 · N729UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98828004Longeron · corrodedINSPECTION TYPE:C LONGERON 35L CORRODED F/S 285-295. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON IAW SRM 53-2-2.Oct 10, 1998 · N729UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS98827956Stiffener · corrodedINSPECTION TYPE-C, A/C COMPT FS 8 AT LONG 28R, THE VERTICAL STIFFENER IS CORRODED. REMOVED, FABRICATED AND REPLACED VERTICAL STIFFENER IAW DWG 5615530 AND SRM 51-1-21 AND 51-1-20D.Oct 10, 1998 · N729UP · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA9800078Plating · corrodedDURING ROUTINE PREFLIGHT INSPECTION, FOUND THE FUSELAGE EXTERNAL PLATING WITH CORROSION BULGE, TWO MISSING RIVET HEADS AND THREE CRACKS MIGRATING FROM ONE MISSING RIVET HEADS BETWEEN FUSELAGE STATION -21.0 TO 30.0 BETWEEN LONGERON 31 RIGHT AND 35 LEFT. THE AOct 8, 1998 · N824BX · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS98827880Battery Pack · dischargedINSPECTION TYPE-N/A, EMERGENCY LIGHTS DID NOT ILLUMINATE DURING PREFLIGHT TEST. REPLACED EMERGENCY LIGHTING BATTERY PACK.Oct 7, 1998 · N709UP · Doug DC871F · Emergency LightingSDR UPS98827894Skin · corrodedINSPECTION TYPE:C2 RT WING LEADING EDGE LWR SURFACE BULGED XFS 590-582/FWD OF FWD SPAR. REMOVED CORROSION ALODINED AND PRIMED IAW DC8 SRM 51-1-8. FABBED INNER DOUBLER IAW DC8 ADDENDIUM 5720-4087-B. FABRICATED OUTER DOUBLER IAW DAC DWG 5641225. INSTALLED DOSep 28, 1998 · N798UP · Doug DC871F · Wing, Plate/SkinSDR UPS98827866Doubler · corrodedINSPECTION TYPE-C, FINGER DOUBLER BLOWN OUT AT RBL 65 AT FS 940 TO 960. REMOVED, FABRICATED AND INSTALLED FINGER DOUBLER IAW SRM 53-7-1 FIG 10, 51-1-9, 51-1-20D AND 51-1-21.Sep 27, 1998 · N748UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98827865Doubler · corrodedINSPECTION TYPE-C, FINGER DOUBLER BULGING AND POPPED FASTENER AT RBL 65 AT FS 920 TO 940. REMOVED, FABRICATED AND INSTALLED FINGER DOUBLER IAW SRM 57-7-1 FIG 10, 51-1-9, 51-1-20D AND 51-1-21.Sep 27, 1998 · N748UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98827864Longeron · corrodedINSPECTION TYPE-C, LONG 34L AT FS 1745 IS CORRODED OUT OF LIMITS. REMOVED, FABRICATED AND REPLACED LONG 34L FROM FS 1720 TO 1766 IAW SRM 53-5-1 FIG 7, 51-1-20D AND 51-1-21.Sep 27, 1998 · N748UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA9800077Connector · corrodedDURING CLIMBOUT FROM A MISSED APPROACH, THE CREW RETRACTED THE LANDING GEAR, THE LANDING GEAR DOOR WARNING REMAINED ILLUMINATED. THE CREW CYCLED THE GEAR WITH THE DOOR WARNING INDICATION REMAINING THE SAME. MAINTENANCE INSPECTED THE LANDING GEAR DOOR SWITCHESep 25, 1998 · N822BX · Doug DC871F · Landing Gear Position and WarningSDR IXXA9800076Fire Loop · defectiveEN ROUTE, THE NUMBER ONE ENGINE FIRE WARNING SOUNDED WITH THE MASTER FIRE WARNING LIGHT ILLUMINATED. THE FLIGHT CREW SECURED THE ENGINE FOLLOWING COMPANY PROCEDURES AND DISCHARGED ONE FIRE BOTTLE. THE FIRE WARNING LIGHT EXTINGUSHED FOLLOWING FIRE BOTTLE DISCSep 25, 1998 · N825BX · Doug DC871F · Fire DetectionSDR UPS98827930Intercostal · corrodedINSPECTION TYPE:C2 INTERCOSTAL, FS 680-702 CORRODED RBL 20. REMOVED CORRODED WEB FABBED AND INSTALLED IAW DAC DWG 5773275, DC8 SRM 51-1-21, 51-1-8.Sep 23, 1998 · N798UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98827937Skin · corrodedINSPECTION TYPE:C2 TAILCONE LT LOWER SKIN CORRODED. REMOVED SKIN, FABBED NEW SKIN IAW DAC DWG 5764650. INSTALLED SKIN IAW DC8 SRM 51-1-21.Sep 22, 1998 · N798UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS98827924Floorbeam · crackedINSPECTION TYPE:C2 FLOORBEAM, STA 902 CRACKED AT RT O/B FLANGE. ROUTED OUT DAMAGE, FABBED FILLER AND SHIM IAW REO-05489 REV A FABBED. REPAIR STRAP ON UPS N/R 809637, DRILLED AND INSTALLED IT, FILLER AND SHIM IAW DC8 SRM 51-1-20D, 51-1-24 AND REO 05489 REV A.Sep 22, 1998 · N798UP · Doug DC871F · Fuselage Main, Floor BeamSDR UPS98827938Frame · corrodedINSPECTION TYPE:C2 TAILCONE FRAME, STA 1971 CORR, BLO TO RBL 6. REMOVED FRAME SECTION, FABBED NEW SECTION, AND SPLICES IAW DC8 SRM 5 3-2-0 AND DAC DWG 5704650. INSTALLED REPAIR IAW DC8 SRM 51-1-20D.Sep 21, 1998 · N798UP · Doug DC871F · Fuselage Main, FrameSDR UPS98827697Engine · flamed outINSPECTION TYPE-N/A AT FL 310, SET UP SUCTION FEED OFF OF NR 4 ALT TANK FUEL PRESSURE WAS INTIALLY AT 30 PSI THEN PRESSURE FLUCTUATED FROM 30 PSI TO 0 PSI. FUEL PRESSURE STAYED AT 0 PSI AND THEN NR 4 ENG FLAMED OUT. ENGINE RESTARTED, OTHER INDICATIONS NORMASep 19, 1998 · N702UP · Doug DC871F · Engine (Turbine/Turboprop)SDR UPS98827872Skin · corrodedINSPECTION TYPE-C2, FUSELAGE EXTERIOR SKIN CORRODED STA 1190 AND LONG 22R. REPAIRED AREA IAW DC8 SRM 53-2-1 FIG 7. REMOVED CORROSION PER DC8 SRM 51-1-8. BLEND OUT WAS BEYOND LIMITS PER DC8 SRM 53-2-0. TRIMMED OUT DAMAGE, FABBED FILLER AND DOUBLER PER DC8 SSep 18, 1998 · N798UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS98827867Fitting · corrodedINSPECTION TYPE-C, NR 1 PIT AT STR 32L STA 270, DOOR OPEN STOP/FRAME FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.Sep 18, 1998 · N748UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98827941Skin · corrodedINSPECTION TYPE:C2 TAILCONE RT SKIN CORRODED, L33R TO L36 FS 1912-1950. REMOVED SKIN, FABBED AND INSTALLED NEW ONE IAW DAC DWG 5644500 AND DC8 SRM 51-1-8, 51-1-21.Sep 17, 1998 · N798UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS98827939Frame · crackedINSPECTION TYPE:C2 CRACKED TAIL CONE FRAME, STA 1933 RIGHT OF L36. REMOVED DAMAGE, FABBED REPAIR FRAME AND SPLICES IAW DC8S RM 53-2-0 FI G 2, 51-3-2. INSTALLED REPAIR IAW DC8 SRM 53-2-0 FIG 2, 51-1-20D AND 51-1-8.Sep 17, 1998 · N798UP · Doug DC871F · Fuselage Main, FrameSDR UPS98827936Extrusion · corrodedINSPECTION TYPE:C2 TAIL CONE, L36 EXTRUSION CORRODED, STA 1890-1940. REMOVED AND REPLACED EXTRUSION IAW DC8 SRM 51-1-24.Sep 17, 1998 · N798UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98827877Frame · crackedINSPECTION TYPE-C2, TAIL CONE FRAME STA 1919 RT SIDE OF LONGERON 36 CRACKED. REMOVED DAMAGED SECTION OF FRAME, FORMED FRAME SECTION IAW DAC DWG 5 704650. HEAT TREATED ANGLES, SPLICES, FORMED FRAME IAW TPS-1003 AND DC8 SRM 51-1-1. FAB FRAME AND SPLICE ANGLESSep 17, 1998 · N798UP · Doug DC871F · Fuselage Main, FrameSDR UPS98827876Fitting · crackedINSPECTION TYPE-C2, RT SIDE CENTER WING, STA 795 AND XCW46R FITTING IS CRACKED. REMOVED FITTING CRACKED AT RT CENTER WING STA 759 AND XCW46R. RECEIVED NEW FITTING 3641125-507 PO 270648. DRILLED HOLES IAW DC8 SRM 51-1 -24. ALODINED AND PRIMED IAW DC8 SRM 51Sep 17, 1998 · N798UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98827931Floorbeam · gougedINSPECTION TYPE:C2 FWD LWR CARGO STA 160 RBL 50 FLOORBEAM HAS GOUGE AROUND THE HI-LOK REPAIRED IAW REO5465.Sep 15, 1998 · N798UP · Doug DC871F · Fuselage Main, Floor BeamSDR UPS98827928Fitting · crackedINSPECTION TYPE:C2 AFT PIT AFT SIDE OF TORQUE BOX BOTTOM AFT CORNER OF CARGO DOOR FRAME, TORQUE BOX FITTING CRACKED AT 2 PLACES (BANANA FTGS). REMOVED AND REPLACED FITTINGS, STA 1220 AND 1228 IAW DC8 SRM 51-1-20 D, 51-1-21 AND 51-3-0.Sep 15, 1998 · N798UP · Doug DC871F · Fuselage Miscellaneous Structure
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