Douglas DC-8-71F

Service difficulty reports · 8,938

Newest first. General aviation reporting is voluntary.

Query with SQL
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 RRXA98064Seal · cutDURING CLIMBOUT LOST OIL QUANTITY ON NR 3 WITH OIL PRESSURE FLUCTUATING. PUT NR 3 THROTTLE TO IDLE, AFTER 2 MINUTES LOW OIL PRESSURE LIGHT ILLUMINATED. ACCOMPLISHED INFLIGHT SHUTDOWN CHECKLIST. ON GROUND CHK FOUND STARTER CASE SEAL LEAKS. REMOVED STARTER AFeb 28, 1998 · N8091U · Doug DC871F · Turbine Engine Accessory DriveSDR UPS98826162Frame · corrodedINSPECTION TYP-C, STA 260 BTWN LONGERON 34R 33L, THE FWD FACE OF THE FRAME IS CORRODED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FRAME AND ASSOCIATED PARTS IAW DWG 5754671 AND SRM 53-4-1.Feb 27, 1998 · N707UP · Doug DC871F · Fuselage Main, FrameSDR UPS98826086Splice · corrodedINSPECTION TYPE-C, AFT PIT FS 1350 LONG, 28L SPLICE FITTING CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-20D AND DWG 4646163.Feb 27, 1998 · N707UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98826002Cusp · corrodedINSPECTION TYPE:C F/S 453 CORROSION REMOVAL RT CUSP BEYOND LIMITS. REPAIRED IAW SRM ADDN DC8-5330-2159-B.Feb 27, 1998 · N707UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98825994Fitting · crackedINSPECTION TYPE:D/CK, STA 300 L27 TO 28 L 'Z' FITTING CRACKED. REMVOED FITTING FABBED ANGLES IAW DC8 SRM 53 2 0. ALODINED AND PRIMED AS REQUIRED IAW DC8 SRM 51 1 8. INSTALLED FITTING AND SPLICE ANGLES IAW DC8 SRM 51 1 20D AND 53 2 0.Feb 27, 1998 · N703UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98825988Seat Track · crackedINSPECTION TYPE:D/CK FUSELAGE MAIN CABIN INTERIOR FLOOR BOARD SUPPORT CHANNEL HAVE CORROSION AND SEAT TRACK E AT STA 1758 BLO IS CRACKED. REMOVED CRACKED HAT CHANNEL. REMOVED CORROSION FROM LEFT HAND FLOOR BOARD OUT OF LIMITS IAW DC8 SRM 53 2 0, LOCATED AND Feb 27, 1998 · N703UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS98826161Doubler · corrodedINSPECTION TYPE-C, STA 1160 TO 1220 BTWN STR 33R TO 34L. THE INTERNAL DOUBLER HAS MANY AREAS OF MODERATE CORROSION. REPAIRED AREA IAW 8110-3 APPROVED DHC SH 707-569.Feb 26, 1998 · N707UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98826159Skin · corrodedINSPECTION TYPE-C, STA 1650 BTWN STR 28L TO 32L THE INTERNAL SKIN IS CORRODED AND EXTENDS UNDER THE TEAR STRAP AT EACH BAY. REPAIRED THE AREA IAW 8110-3 APPROVED DHC SK707-590.Feb 26, 1998 · N707UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS98826123Frame · crackedINSPECTION TYPE-C, NOSE SECTION LT SIDE AT STA 99 FRAME IS CRACKED IN TWO PLACES UPPER AND LWR SECTION OF SPLICE. STOP DRILLED CRACK ON UPPER FLANGE AND REMOVED DAMAGE ON LWR FLANGE AND REPAIRED IAW DHC SK 707-600 AND REFERENCE TO EO DC8 5310- 10296.Feb 26, 1998 · N707UP · Doug DC871F · Fuselage Main, FrameSDR UPS98826116Splice · crackedINSPECTION TYPE-C, FS 1260 TO 1280 STR 35R SPLICE FITTING HAS 4 INCH CRACK. REMOVED, FABRICATED, AND REPLACED FITTING IAW SRM 51-1-20D AND DWG 3759258.Feb 26, 1998 · N707UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98826094Shear Tie · corrodedINSPECTION TYPE-C, FS 1161 BTWN STR 27L-28L SHEAR TIE FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.Feb 26, 1998 · N707UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98826091Longeron · crackedINSPECTION TYPE:C F/S 1280-1300 STR 31L IS CRACKED BTWN 5 FASTENERS. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON IAW SRM 51-1-21 AND DWG 5753744.Feb 26, 1998 · N707UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS98826062Fitting · damagedINSPECTION TYPE-C, 505-E XRS 74.9. STRINGER 51 END FITTING HAS ELONGATED HOLE THROUGH FITTING'S WING SKIN. INSTALLED BUSHING IAW DC8-SRM 51-1-25 AND REO 04389. ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED NEW FITTING IAW 51-1-20D, DC8 SRM 51-1-11 ANFeb 26, 1998 · N703UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98826026Splice · crackedINSPECTION TYPE-C, FS 1040 TO 1060 STR 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.Feb 26, 1998 · N707UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98826164Skin · corrodedINSPECTION TYPE-C, STA 1346 TO 1354 STR 24L TO 31L, THE SKIN AND THE FINGER DOUBLER HAVE MODERATE CORROSION. REMOVED CORROSION FROM SKIN, FOUND WITHIN LIMITS IAW SRM 53-2-0. FABRICATED AND REPLACED FINGER DOUBLER IAW DWG 5779914.Feb 25, 1998 · N707UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS98826163Skin · corrodedINSPECTION TYPE-C, STA 1346 TO 1354 STR 24L TO 31L, THE SKIN AND THE FINGER DOUBLER HAVE MODERATE CORROSION. REMOVED CORROSION FROM SKIN, FABRICATED AND INSTALLED REPLACEMENT FINGER DOUBLER IAW DWG 5779914 AND SRM 51-1-21.Feb 25, 1998 · N707UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS98826127Fitting · crackedINSPECTION TYPE-C, STA 1180 AT STR 26L, THE DOOR OPEN STOP FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.Feb 25, 1998 · N707UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98826126Fitting · crackedINSPECTION TYPE-C, STA 1200 AT STR 26L, THE DOOR OPEN STOP FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.Feb 25, 1998 · N707UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98826125Fitting · crackedINSPECTION TYPE-C, STA 300 AT STR 26L, THE DOOR OPEN STOP FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.Feb 25, 1998 · N707UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98826124Fitting · crackedINSPECTION TYPE-C, STA 320 AT STR 26L, DOOR OPEN STOP FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.Feb 25, 1998 · N707UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98826095Splice · crackedINSPECTION TYPE-C, FS 440 TO 460 STR 34L SPLICE FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW SRM 51-1-20D.Feb 25, 1998 · N707UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98826058Cusp · corrosionINSPECTION TYPE-C, FS 240 TO 260 RT CUSP UPPER SURFACE HAS SEVERE CORROSION. REPAIRED IAW SRM 53-2-5.Feb 25, 1998 · N707UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98826003Cargo Track · corrodedINSPECTION TYPE:C NR 2 PIT, CARGO TRACK AFT DOOR RT SIDE HAS HEAVY CORROSION. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT TRACK IAW SRM 51-3-0. AND DWG 5750726.Feb 25, 1998 · N707UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS98826057Fitting · crackedINSPECTION TYPE-C, LT WING T/E, THE LWR REAR SPAR TO AUX SPAR TIE FITTING AT THE STA 98 FLAP HINGE IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-3-0 AND DWG 5642205.Feb 24, 1998 · N707UP · Doug DC871F · Wing, Control Surface Attach FittingsSDR UPS98825989Fitting · crackedINSPECTION TYPE:D/CK STA 320 AT LONG 35 L FITTING IS CRACKED. REMVOED EXISTING FITTING FABRICATED SPLICES IAW DC8 SRM 53 2 0. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED FITTING IAW DC8 SRM 5 1 1 20D.Feb 24, 1998 · N703UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98826121Rib · crackedINSPECTION TYPE-C, LT WING RIB AT STA.XOLDI 6.225 I/B SIDE IS CRACKED. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Feb 23, 1998 · N707UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS98826072Rib · crackedINSPECTION TYPE-C, LT WING L/E LWR RIB AT STA XFS 360.25 IS CRACKED AT AFT DOUBLER FSTR HOLE. REMOVED, FABRICATED AND INSTALLED REPLACEMENT RIB IAW SRM 51-1-21 AND DWG 5769530.Feb 23, 1998 · N707UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS98826001Rib · crackedINSPECTION TYPE:C LT WING L/E RIB AT STA XFS 379.0 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0.Feb 23, 1998 · N707UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS98826000Rib · crackedINSPECTION TYPE:C LT WING L/E RIB AT STA XFS 372.75 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0.Feb 23, 1998 · N707UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS98826005Intercostal · corrodedINSPECTION TYPE-D/CK, FLOORBEAM INTERCOSTAL AT STA 1710 TO 1730 RBL 12 HAS CORROSION. FABRICATED SUPPORT IAW DAC DWG 5755032, ALODINED AND PRIMED NEW SUPPORT. INSTALLED NEW SUPPORT IAW DC8 SRM 51-1-21 AND 51-1-20D AND 51-3-0.Feb 19, 1998 · N703UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98825863Support · corrodedINSPECTION TYPE-C, FS 1040 TO 1060 ABOVE STR 33R FLOOR SUPPORT ANGLE HAS CORROSION REMOVAL WENT OUT OF LIMITS. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT ANGLE IAW SRM 53-11-0 AND 51-1-21.Feb 17, 1998 · N752UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98825884Fitting · corrodedINSPECTION TYPE-C, LONG 33R FITTING FS 8 CORROSION REMOVAL BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.Feb 16, 1998 · N752UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98825812Smoke Curtain · tornINSPECTION TYPE:SV, MAIN CABIN SMOKE CURTAIN TORN. REMOVED AND REPLACED SMOKE CURTAIN IAW DC8-25-50-02.Feb 16, 1998 · N718UP · Doug DC871F · Emergency EquipmentSDR RRXA98074Spar Web · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE BEYOND LIMITATIONS TO RIGHT WING, AUX SPAR WEB AT STA 879 TO STA 902. AUX SPAR WEB CORROSION REMOVED MATERIAL LOSS WAS MINIMAL USING DC-8 SRM 57-2-0 FIGURE 6 SHEET 1. THE MAJOR MATERIAL REMOVED WAS AT THE EDFeb 12, 1998 · N8177U · Doug DC871F · Wing SparSDR RRXA98042Fitting · oversize holesDURING A MAINTENANCE VISIT, FOUND OVERSIZE HOLE TO LT FLAP LINK SUPPORT FITTING AT STA XF 339. REWORK TO 0.874/0.8762 B/P DAI HOLES. OPEN SUBJECT HOLES TO REMOVE MINIMUM MATERIAL, ENLARGE BOTH HOLES. FABRICATED AND INSTALLED 2 EACH BUSHINGS IAW FAA APPROVEDFeb 12, 1998 · N8177U · Doug DC871F · Trailing Edge Flap Control SystemSDR IXXA980004Engine · damagedEN ROUTE FROM TOL TO ATL, DURING CRUISE THE FLIGHT ENGINEER NOTICED A MARKED DECLINE IN THE NUMBER ONE ENGINE OIL QUANTITY. THE CREW PERFORMED A PRECAUTIONARY INFLIGHT SHUTDOWN IAW COMPANY PROCEDURES, AND CONTINUED TO ATL MAKING AN UNEVENTFUL LANDING. MAINTFeb 12, 1998 · N824BX · Doug DC871F · Engine (Turbine/Turboprop)SDR UPS98825885Fitting · crackedINSPECTION TYPE-C, MAIN CARGO DECK UPPER SURFACE WING CTR SECTION FS 781 RBL 62 CORROSION BETWEEN 2 FASTENERS AND CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.Feb 11, 1998 · N752UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98825881Tie Fitting · crackedINSPECTION TYPE-C, FS 1232 AT STR 33R INTERCOSTAL TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.Feb 11, 1998 · N752UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98825880Shear Tie · corrodedINSPECTION TYPE-C, SHEAR TIE FITTING AT FS 300 LONG 30L HAS MODERATE CORROSION AROUND FASTENERS. REMOVED AND REPLACED SHEAR TIE FITTING IAW SRM 53-2-0.Feb 11, 1998 · N752UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98825842Fitting · crackedINSPECTION TYPE-C, NR 1 PIT AFT LWR T-BOLT STOP FITTING IS CRACKED ON THE LWR LEG. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 FIG 2D.Feb 11, 1998 · N752UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98825796Splice · crackedINSPECTION TYPE-C, FS 600 TO 620 STR 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.Feb 11, 1998 · N752UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98825793Fitting · corrosionINSPECTION TYPE-C, LONGERON END FITTING AT FS 274 STR 31R HAS HEAVY CORROSION AROUND FASTENERS. REMOVED AND REPLACED FITTING IAW SRM 51-1-210D.Feb 11, 1998 · N752UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98825790Splice · crackedINSPECTION TYPE-C, FS 440 TO 460 STR 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-21D.Feb 11, 1998 · N752UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98825788Splice · crackedINSPECTION TYPE-C, FS 440 TO 460 STR 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.Feb 11, 1998 · N752UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98825895Seat Track · corrodedINSPECTION TYPE:C F/S 1024 LBL 59 - SEAT TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF TRACK IAW SRM ADDN DC8-5320-5167-C.Feb 10, 1998 · N752UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS98825894Seat Track · corrodedINSPECTION TYPE:C F/S 1207 LBL 59, SEAT TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF TRACK IAW SRM 53-7-2.Feb 10, 1998 · N752UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS98825893Seat Track · corrodedINSPECTION TYPE:C F/S 260 RBL 48 - SEAT TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF TRACK IAW SRM ADDM DC8-5320-8309.Feb 10, 1998 · N752UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS98825892Bulkhead Angle · corrodedINSPECTION TYPE:C AFT SIDE OF F/S 70 O/B OF 33R LOWER BULKHEAD L ANGLE HAS HEAVY CORROSION AROUND BOLT AND BETWEEN IT AND LONGERON FITTING. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR CHORD IAW SRM 53-2-5 51-1-20D, AND DWG 5613064.Feb 10, 1998 · N752UP · Doug DC871F · Fuselage Main, BulkheadSDR UPS98825888Fitting · corrodedINSPECTION TYPE-C, LONGERON 33R END FITTING AFT SIDE OF FS 70 IS EXFOLIATED (HEAVY CORROSION). REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.Feb 10, 1998 · N752UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS98825805Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XOLDI 6.225 THE UPPER L/E RIB HAS A 2 INCH CRACK AT MID SPAN. REPAIRED IAW SRM 57-2-0.Feb 10, 1998 · N752UP · Doug DC871F · Wing, Rib/Bulkhead
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