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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR UPS97824422Floorbeam · corrodedINSPECTION TYPE-C, MODERATE CORROSION ON FLOORBEAM FS 1660 LBL 48. REPAIRED IAW DHC SK 701-044.Aug 29, 1997 · N701UP · Doug DC871F · Fuselage Main, Floor BeamSDR UPS97824412Doubler · corrodedINSPECTION TYPE:C, AFT ACCY COMPARTMENT HEAVY INTERGRANULAR CORROSION ON SKIN DOUBLER F/S 1615 L-26L TO 27L. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21, 51-1-20D, AND DWG 5779934.Aug 29, 1997 · N701UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS97824409Membrane · crackedINSPECTION TYPE:C, AFT ACCY COMPARTMENT SUB FLOOR MEMBRANE CRACKED F/S 1615 JUST INBD OF L-21R. FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-0 AND 53-4-1 PG 55 AND 56.Aug 29, 1997 · N701UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS97824421Frame · crackedINSPECTION TYPE-C, FS 940 LBL 65 FRAME HAS 3.5 IN RADIUS. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-20D AND DHC SK-701-894.Aug 28, 1997 · N701UP · Doug DC871F · Fuselage Main, FrameSDR UPS97824414Seat Track · corrodedINSPECTION TYPE:C, MAIN CABIN F/S 1306-1310 LBL 24, SEAT TRACK HAS HEAVY CORROSION, LOCK TANGS ARE SEPARATING. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF TRACK IAW SRM 53-2-3, 51-3-0, AND 51-1-11.Aug 28, 1997 · N701UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS97824413Seat Track · corrodedINSPECTION TYPE:C, F/S 942 LBL 24, SEAT TRACK HAS HEAVY CORROSION. REPAIRED TRACK IAW SRM 53-2-3, 53-1-0.Aug 28, 1997 · N701UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS97824398Fitting · corrodedINSPECTION TYPE:C, FRAME 900 FWD SIDE BELOW PRESSURE FLOOR JOGGLED PLATE FITTING EXFOLIATED, RT W/W. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-20D, 51-1-21, 51-3-0, AND DWG 2646348.Aug 28, 1997 · N701UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS97824395Seat Track · corrodedINSPECTION TYPE:C, F/S 586 LBL 44 SEAT TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF TRACK IAW SRM 51-1-21, 53-2-3, AND 53-3-0.Aug 28, 1997 · N701UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS97824394Fitting · crackedINSPECTION TYPE:C, F/S 980 RBL 65 ON SUB FLOOR, TIE FITTING IS CRACKED IN HALF. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-20D, AND DWG 4647365.Aug 28, 1997 · N701UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS97824392Seat Track · corrodedINSPECTION TYPE:C, F/S 563 AND 586 LBL 59, SEAT TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF TRACK IAW SRM 53-2-3, 51-1-11, 51-1-20.Aug 28, 1997 · N701UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS97824390Seat Track · corrodedINSPECTION TYPE:C, F/S 680, 635-642 RBL 59, SEAT TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF TRACK FROM F/S 610-730 IAW SRM 51-3-0, 51-1-11, 53-2-3, 51-1-21, AND 51-1-20.Aug 28, 1997 · N701UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS97824388Doubler · corrodedINSPECTION TYPE:C, F/S 920-940 RBL 59-65 - SUB FLOOR FINGER DOUBLER IS BULDING AND HAS NUMEROUS SHEARED RIVETS. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21, 53-7-3 FIG 4, AND DWG 5645332.Aug 28, 1997 · N701UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS97824387Doubler · corrodedINSPECTION TYPE:C, F/S 940-960 RBL 59-65 - SUB FLOOR FINGER DOUBLER IS BULDGING AND HAS NUMEROUS SHEARED RIVETS. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW SRM 53-7-3 FIG 4, 51-1-21, 51-1-14, AND DWG 5645332.Aug 28, 1997 · N701UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS97824386Doubler · corrodedINSPECTION TYPE:C, F/S 960-980 RBL 59-65 - FINGER DOUBLER IS BULGING AND HAS SEVERAL SHEARED RIVETS. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21, 53-7-3, AND DWG 5645332.Aug 28, 1997 · N701UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS97824385Doubler · corrodedINSPECTION TYPE:C, F/S 880-900 RBL 59-65 - SUBFLOOR FINGER DOUBLER IS CORRODED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW SRM 53-7-3, 51-1-21, AND DWG 5645332.Aug 28, 1997 · N701UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS97824384Rib · crackedINSPECTION TYPE:C, RT WING L/E AT STA XFS 821.00 - THE L/E RIB IS CRACKED AT THE AFT UPPER END. REPAIRED L/E RIB IAW SRM 57-3-1 FIG 7 AND 51-1-20D.Aug 28, 1997 · N701UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS97824383Rib · crackedINSPECTION TYPE:C, RT WING L/E AT STA XFS 636.00 - THE UPPER L/E RIB IS CRACKED AT THE AFT END. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0, 51-1-20D.Aug 28, 1997 · N701UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS97824420Floorbeam · corrodedINSPECTION TYPE-C, FS 59 FLOORBEAM TOP FLANGE LWR SURFACE HAS SEVERE CORROSION AT RBL 36. REPAIRED IAW DHC SK 701-539.Aug 26, 1997 · N701UP · Doug DC871F · Fuselage Main, Floor BeamSDR UPS97824411Frame · crackedINSPECTION TYPE:C, F/S 55 FRAME AT STR 24L HAS 2 CRACK IN RADIUS. REPAIRED IAW SRM 53-2-0.Aug 26, 1997 · N701UP · Doug DC871F · Fuselage Main, FrameSDR UPS97824410Support · crackedINSPECTION TYPE:C, FLOORBEAM SUPPORT LWR SUPPORT FITTING CRACKED AT F/S 1220 RT SIDE. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-3-0 51-1-20D, AND DWG 3754025.Aug 26, 1997 · N701UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS97824389Rib · crackedINSPECTION TYPE:C, LT WING CENTER L/E RIB AT STA XS478.897 IS CRACKED AT THE AFT UPPER END. FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.Aug 26, 1997 · N701UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS97824382Rib · crackedINSPECTION TYPE:C, LT WING CENTER L/E RIB AT XFS 322.75 IS CRACKED AT THE AFT UPPER END. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0, 51-1-20D, AND 51-1-21.Aug 26, 1997 · N701UP · Doug DC871F · Wing, Rib/BulkheadSDR RRXA97237Frame · missdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLE THUR FRAME RADIUS AT STA 1701 AND LONGERON 21 RIGHT. *S/D* FABRICATED AND INSTALLED REPAIR ANGLE FROM 1.0 X 1.0 X .050 7075-T6 ALCLAD IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-03517 AND DAC DWG 561214Aug 15, 1997 · N8079U · Doug DC871F · Fuselage Main, FrameSDR RRXA97236Skin · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO SKIN AT STA 55 AND LONGERON 31 LEFT. *S/D* FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-1 FIG 7 CLASS 1 REPAIR WITH DEVIATIONS IAW FAA APPROVED DER TIMCO REO-03515 AND DAC DWG 5613862. TREATAug 15, 1997 · N8079U · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA97234Frame · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FRAME AT STA 1168. *S/D* FOUND CORROSION DAMAGE TO FRAME WEB AND LWR LEG BEYOND LIMITATIONS IAW DC-8 SRM. FABRICATED AND INSTALLED REPAIR STRIP FROM .080 7075-T6 IAW FAA APPRVED DER TIMCO ENGINEERING SKAug 15, 1997 · N8079U · Doug DC871F · Fuselage Main, FrameSDR RRXA97235Frame · gougedDURING A MAINTENANCE VISIT, FOUND GOUGED TO FRAME AT STA 511 RIGHT SIDE. *S/D* FABRICATED AND INSTALLED REPAIR STRIP FROM .090 7075-T6 ALCLAD IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-03509 AND DAC DWG 5616521-507.Aug 14, 1997 · N8079U · Doug DC871F · Fuselage Main, FrameSDR RRXA97233Frame · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FRAME AT STA 520 AND BETWEEN LONGERONS 25 RIGHT AND 29 RIGHT. *S/D* FABRICATED AND INSTALLED 3 EACH Z DOUBLERS FROM .071 2024-T6 ALCLAD IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-03484 AND DAC DWG'Aug 11, 1997 · N8079U · Doug DC871F · Fuselage Main, FrameSDR RRXA97231Skin · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO INTER SKIN AT STA 485 BETWEEN LONGERONS 34 RIGHT AND 35 RIGHT. *S/D* FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-1 FIG 7. OMITTED FINGER DOUBLER FOR REPAIR IAW FAA APPROVED DER TIMCO ENGINEAug 11, 1997 · N8079U · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS97824086Light · inoperativeINSPECTION TYPE-N/A, ON PREFLIGHT EMERGENCY EXIT LIGHTS WOULD NOT TEST, NO LIGHT ILLUMINATION. REMOVED AND REPLACED EMERGENCY BATTERY PACK, OPS CHECKED OK PER MM 33-50-01.Aug 10, 1997 · N715UP · Doug DC871F · Emergency LightingSDR RRXA97232Spar · crackedDURING ACCOMPLISHMENT OF DAC SB 57-88, ON LEFT WING, HOLES 1 THUR 5 AND A, B AND C HAD CRACKS INDICATED. HOLES WERE ABOVE SIZE ALLOWED IAW SB 57-88. *S/D* IDENTIFIED CRACKS AND REAMED OUT DAMAGE IAW FAA APPROVED DER TIMCO REO-03479. FABRICATED AND INSTALLEAug 8, 1997 · N8079U · Doug DC871F · Wing SparSDR RRXA97213Fire Wire · barePERFORMED PRECAUTIONARY SHUTDOWN NR 4 ENGINE DUE TO INTERMITTENT FIRE BELL AT TOD 0:22Z DISCONNECTED CSD WINDMILL OIL PRESSURE 3 PSI. REPAIRED BARE WIRE TO LOOP AT 1 O'CLOCK POSITION TO TURBINE SECTION. RAN NR 4 ENGINE FOR 20 MINUTES AT CRUISE POWER, SYSTEM Jul 24, 1997 · N8087U · Doug DC871F · Fire DetectionSDR RRXA97211Fire Wire · bareNR 4 ENGINE FIRE WARNING COMES ON INTERMITTENTLY IN SHORT BURSTS, SYSTEM TESTS OK. REMOVED BARE WIRE TO LOOP IN CORE SECTION, 1 O'CLOCK POSITION ADEL CLAMP, OPS CHECK GOOD IAW MM CH 26.Jul 22, 1997 · N8087U · Doug DC871F · Fire DetectionSDR RRXA97205Fire Bottle · low pressureAGENT LOW PRESS LIGHT ON IN FLT. REPLACED RT INBD FIRE BOTTLE.Jul 12, 1997 · N8087U · Doug DC871F · Fire Bottle, FixedSDR UPS97823724Battery Pack · dischargedINSPECTION TYPE:N/A, EMERGENCY BATTERY PACK BAD, NO TEST ON EMERGENCY LIGHT SWITCH. REMOVED AND REPLACED EMERGENCY BATTERY PACK, OPS CHECK NORMAL IAW 33-50-01.Jul 10, 1997 · N702UP · Doug DC871F · Emergency LightingSDR RRXA97196Engine · malfunctionedNR 4 ENGINE VERY SLOW TO SPOOL AT TAKEOFF AND COULD NOT MAINTAIN MAX POWER DUE HIGH EGT. IN CRUISE EGT AVERAGED 46DEG HIGHER. DURING GROUND RUN OF NR 4 ENGINE, ALL INDICATIONS WERE NORMAL. NO DEFECTS NOTED AT TAKEOFF POWER OR OTHER ENGINE SETTINGS. OKAY FOJul 10, 1997 · N8076U · Doug DC871F · Engine (Turbine/Turboprop)SDR UPS97823576Battery Pack · dischargedINSPECTION TYPE:N/A, EMERG EXIT LIGHT DIM WHEN TESTED. SHELF LIFE ON NEW ASSY DUE 7\28. ALSO, DIM WHEN TESTED AOG BATTERY RACK.Jun 30, 1997 · N752UP · Doug DC871F · Emergency LightingSDR UPS97823574Transformer · failedINSPECTION TYPE:N/A, CREW SMELLED SMOKE FUMES BEFORE DESCENT. REPLACED OVERHEAD GLARESHIELD POWER TRANSFORMER.Jun 27, 1997 · N701UP · Doug DC871F · Flight Compartment LightingSDR UPS97823664Rib · crackedINSPECTION TYPE:C/CK, RIGHT HAND AFT SERVICE DOOR, UPPER AFT RIB INSIDE DOOR CRACKED. REMOVED RIB, FABBED NEW RIB IAW DC8 SRM 52-3-1 AND 52-1-24, INSTALLED RIB IAW DC8 SRM 51-1-21 AND 51-1-20. RIB REQUIRED HEAT TREATED, DONE IAW DC8 SRM 51-1-1.Jun 18, 1997 · N713UP · Doug DC871F · Service DoorsSDR UPS97823662Doubler · crackedINSPECTION TYPE:C/CK, LEFT HAND WING AFT SPAR FUEL DUMP CHUTE SHROUD DOUBLER FOR CUTOUT IS CRACKED AND GOUGED. REMOVED DOUBLER, FABRICATED NEW ONE IAW DAC DWG 5765045 AND INSTALLED IAW DC8 SRM 51-3-0.Jun 18, 1997 · N713UP · Doug DC871F · Fuselage Miscellaneous StructureSDR SRAA970610Fire Loops · malfunctionedON DESCENT, NR 1 ENGINE SHORT CIRCUIT LIGHT FLICKERED ON. REMOVED AND REPLACED ALL FIRE LOOPS ON NR 1 ENGINE. PERFORMED ENGINE RUN, OPS CHECKED GOOD IAW ATA CH 26.Jun 15, 1997 · N872SJ · Doug DC871F · Fire DetectionSDR UPS97823667Structure · corrodedINSPECTION TYPE:C/CK, INTERIM REPAIR TO FWD CORNER NR 4 PIT DOOR OPENING. REPAIRED PER TIMCO REO 03320 REV IR.Jun 14, 1997 · N713UP · Doug DC871F · Fuselage Main, StructureSDR SRAA970608Fire Control · inoperativeDURING FLIGHT, NR 1 ENGINE FIRE LOOP SHORT CIRCUIT LIGHT FLICKERS ON AND OFF. UPON TAXI IN FIRE WARNING ON NR 1 ENGINE CAME ON AND SHORT CIRCUIT LIGHT CAME ON STEADY. REMOVED AND REPLACED NR 1 FIRE WARNING CONTROL, SYSTEM OPS CHECKED GOOD PER MM CH 26-00.Jun 14, 1997 · N872SJ · Doug DC871F · Fire DetectionSDR RRXA97186Hyd Line · failedAIR TURNBACK, LOSS OF HYDRAULIC FLUID AND PRESSURE AFTER T/O AND GEAR RETRACTION. RETURNED TO MMGL. REMOVED AND REPLACED BOGIE TRIM FLEXIBLE LINE. REPLENISHED HYD SYSTEM TO PROPER LEVEL, LEAKS CHECK GOOD.Jun 13, 1997 · N8091U · Doug DC871F · Hydraulic System, MainSDR SRAA970605Connector · dirtyDURING FLIGHT, NR 1 ENGINE FIRE WARNING SHORT CIRCUIT LIGHT FLICKERS ON AND OFF. VISUALLY OBSERVED NR 1 ENGINE, NO FIRE CONDITION EXISTS. AIRCRAFT CONTINUED TO DESTINATION WITHOUT INCIDENT. REMOVED AND CLEANED CANNON PLUG ON NR 1 FIRE CONTROL BOX, OPS CHECKJun 8, 1997 · N872SJ · Doug DC871F · Fire DetectionSDR UPS97823313Precooler · dirtyINSPECTION TYPE:C, AIR TURNBACK DUE TO FUMES IN THE COCKPIT. TROUBLESHOT SYSTEM FOUND DEBRIS IN THE NR 2 PRECOOLER. REMOVED AND REPLACED THE NR 2 ENG PRECOOLER AND THE LT WATER SEPARATOR COALESCER BAG IAW MM 36-13-05 AND 21-55-02.Jun 7, 1997 · N779UP · Doug DC871F · Pneumatic Distribution SystemSDR UPS97823288Air Distr · smokeINSPECTION TYPE:C, AIR TURNBACK DUE TO SMOKE AND FUMES IN COCKPIT (FROM LOG PG 773468 ITEM 1). TROUBLESHOT PROBLEM, RAN PACKS WITH RECIRC FAN ON AND OFF WITH GROUND AIR AND ENGINES RUNNING. PRESSURIZED AIRCRAFT, ONLY DEFECT NOTED WAS CLOSE PROXIMITY OF INSULJun 6, 1997 · N779UP · Doug DC871F · Air Distribution SystemSDR RRXA97180Switches · dirtyON LANDING GEAR DOWN LOCK, ON GREEN LIGHTS WERE NOT ON. ALSO, ANTI-SKID LIGHT REMAINED ON. GEAR RED WARNING LIGHTS WERE ALSO OUT. GPWS SOUNDED ON SHORT FINAL WITH AIRCRAFT IN PROPER LANDING CONFIG. CLEANED ALL SWITCH CONTACTS, RESET LANDING GEAR WARNING AJun 5, 1997 · N8177U · Doug DC871F · Landing Gear Position and WarningSDR IXXA9700113Spar Cap · crackedDURING ROUTINE C-CHECK INSPECTION, THE LEFT WING UPPER AUXILIARY SPAR CAP WAS FOUND CRACKED. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED CAP, FABRICATION AND INSTALLATION OF NEW SPAR CAP IN ACCORDANCE WITH DER APPROVED DRAWING 853-239-97, DOUGLAS AIRCRAFT DRAWING Jun 4, 1997 · N822BX · Doug DC871F · Wing SparSDR IXXA9700112Doubler · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND ON AN INTERNAL REPAIR DOUBLER BETWEEN FUSELAGE STATION 1160 AND 1680, LONGERON 27 AND 28 RIGHT. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF NEW REPAIR DOUBLER IN ACCORDANCE Jun 4, 1997 · N822BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA9700110Fitting · crackedDURING ROUTINE C-CHECK INSPECTION, LONGERON 32 RIGHT WAS FOUND CRACKED AT FUSELAGE STATION 345. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A LONGERON FILLER AND SPLICE FITTING IN ACCORDANCE WITH DER APPROVED DRAWING 853-218-9Jun 4, 1997 · N822BX · Doug DC871F · Fuselage Miscellaneous Structure
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