Douglas DC-8-71F

Service difficulty reports · 8,938

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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 UPS00832568Rib · crackedINSPECTION TYPE:C-2, LEFT WING LEADING EDGE LWR RIB CRACKED STA XFS 360.250. STOP DRILLED CRACKED IAW SRM 57-2-0 FIG 2. FAB AND INSTALLED ANGLE DOUBLER IAW SRM 51-1-20D.Apr 25, 2000 · N700UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS00832567Rib · crackedINSPECTION TYPE:C-2, RIGHT WING L/E UPPER RIB CRACKED STA XS 467.233. STOP DRILLED CRACKED IAW SRM 57-2-0 FIG 2. FAB AND INSTALLED REPAIR DOUBLER IAW SRM 51-1-21 & 51-1-20D.Apr 25, 2000 · N700UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS00832566Angle · crackedINSPECTION TYPE:C-2, RIGHT WING L/E STIFFENER ANGLE CRACKED STA XOLDI 6.225. STOP DRILLED CRACKED IAW SRM 57-2-0. FAB AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0 & 51-1-20D.Apr 25, 2000 · N700UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS00832563Rib · crackedINSPECTION TYPE:C-2, LEFT WING LEADING EDGE THE I/B UPPER RIB CRACKED STA XS 520.1. STOP DRILLED CRACKED IAW SRM 57-2-0. FAB AND INSTALLED REPAIR ANGLES IAW 51-1-20 & 57-2-0 FIG 2.Apr 25, 2000 · N700UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS00832560Rib · crackedINSPECTION TYPE:C-2, RIGHT WING L/E AT STA XOLDI 6.225 THE LWR RIB CRACKED. STOP DRILLED CRACK IAW SRM 57-2-0. FAB AND INSTALLED 2 REPAIR DOUBLERS IAW SRM 51-1-11, 57-3-1 & 51-1-20D.Apr 25, 2000 · N700UP · Doug DC871F · Wing, Rib/BulkheadSDR RRXA003703Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE UPPER PANEL RT HORIZ STAB AT STA XE 248, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED NEW PANEL. (CORROSION DAMAGE RECORDEDApr 24, 2000 · N8084U · Doug DC871F · Horizontal Stabilizer, Plate/SkinSDR RRXA003501Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE T/E RT HORIZ STAB AT STA XE99, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-2-0, 51-1-21 AND 51-3-Apr 24, 2000 · N8084U · Doug DC871F · Horizontal Stabilizer, Plate/SkinSDR RRXA003487Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE T/E OF THE RT HORIZONTAL STABILIZER AT STA XE 278, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-2-Apr 24, 2000 · N8084U · Doug DC871F · Horizontal Stabilizer, Plate/SkinSDR UPS00832556Frame · corrodedINSPECTION TYPE:C-2, FRAME CAP FS 1040 CORRODED OUT OF LIMITS. REMOVED AND REPLACED FRAME CAP FS 1040 IAW SRM 51-1-20 AND 51-1-20D.Apr 24, 2000 · N700UP · Doug DC871F · Fuselage Main, FrameSDR RRXA003705Attach Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LOWER GILLINER ATTACH ANGLE AT STA 1540 AND L27L-L27R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0 ANApr 22, 2000 · N8084U · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS00832538Rib · crackedINSPECTION TYPE:C2, RT WING L/E RIB IS CRACKED AT STA XFS 385.00. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Apr 22, 2000 · N700UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS00832537Rib · crackedINSPECTION TYPE:C2, RT WING L/E RIBS ARE CRACKED AT STA XFS 283.00 AND XFS 401.00. STOP DRILLED CRACK AND REPAIRED BOTH RIBS IAW SRM 57-2-0 FIG 2.Apr 22, 2000 · N700UP · Doug DC871F · Wing, Rib/BulkheadSDR RRXA003701Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE DOME NUTS ON L30R & L27R AT STA 35-70, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-2-0 AND 52-1-21. (CORROSIApr 21, 2000 · N8084U · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS00832570Seat Track · crackedINSPECTION TYPE:C-2 SEAT TRACK CRACKED STA 380 RBL48. REMOVED, FABBED AND INSTALLED SEAT TRACK SECTION IAW EODC8-53-20- 8309 APPENDIX-B AND SRM 51-3-0.Apr 21, 2000 · N700UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS00832569Fitting · crackedINSPECTION TYPE:C-2, STA 380 TO 400 LONG 31L SPLICE FITTING CRACKED. REMOVED AND REPLACED SPLICE FITTING IAW SRM 51-1-20D.Apr 21, 2000 · N700UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00832564Frame · corrodedINSPECTION TYPE:C-2, STA 280 FRAME RAIL ABOVE LONG 34L - 35L HAS HEAVY CORROSION. REMOVED AND REPLACED FRAME RAIL IAW SRM 51-1-20D.Apr 21, 2000 · N700UP · Doug DC871F · Fuselage Main, FrameSDR UPS00832553Frame · corrodedINSPECTION TYPE:C2, STA 1120 FRAME IS CORRODED BEYOND LIMITS LONG 35L-35R. REPAIRED IAW SRM 53-2-0 FIG 2.Apr 21, 2000 · N700UP · Doug DC871F · Fuselage Main, FrameSDR UPS00832451Fitting · crackedINSPECTION TYPE:C2, STA 1241 LONG 35R INTERCOSTAL TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3758498, AND SRM 51-1-20D.Apr 21, 2000 · N700UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00832450Spar Cap · corrodedINSPECTION TYPE:C2, LEFT WING AUX TANK UPPER SPAR CAP IS CORRODED BEYOND LIMITS AT XFS 20. REPAIRED IAW SRM 57-2-1 FIG 37.Apr 21, 2000 · N700UP · Doug DC871F · Wing SparSDR UPS00832449Intercostal · crackedINSPECTION TYPE:C2, STA 1746 LBL 29 INTERCOSTAL IS CRACKED AT AFT END. REMOVED, FABRICATED, AND REPLACED INTERCOSTAL IAW DWG 5755032 AND SRM 51-1-21.Apr 21, 2000 · N700UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00832448Fitting · corrodedINSPECTION TYPE:C2, STA 200 - 220 LONG 31R SPLICE FITTING IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 3755217 AND SRM 51-1-20D.Apr 21, 2000 · N700UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00832539Frame · corrodedINSPECTION TYPE:C2, STA 1040 FRAME AT STR 36 HAS HEAVY CORROSION ON UPPER FLANGE UNDER SIDE. REPAIRED AREA IAW SRM 53-2-0 FIG 2.Apr 21, 2000 · N700UP · Doug DC871F · Fuselage Main, FrameSDR RRXA003496Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FRAME FITTING AFT SIDE AT STA 1240 LT BELOW LONGERON 1, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8 SRM Apr 20, 2000 · N8084U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA000453Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO AFT CARGO COMP SKIN AT STA 1050 TO 1130 AND LONGERON 36. DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED SKIN IAW DC8 SRM 53-4-0, 51-1-2 AND EAPD 01-53-029. TREATED AREA IAW DC8 SRM 51-1-8. Apr 20, 2000 · N8177U · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA000405Frame · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO TOP OF FRAME AT STA 1140 AND LONGERON 35L - 32R. DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGED FRAME, TREATED AREA IAW DC8 SRM 51-1-8, AND INSTALLED IAW DC8 SRM 53-4-0, 51-1-21 FIG PD08-53-036.Apr 20, 2000 · N8177U · Doug DC871F · Fuselage Main, FrameSDR UPS00832606Skin · crackedINSPECTION TYPE:C2, LEFT WING L/E LOWER SKIN IS CRACKED AT FASTENER HOLES BETWEEN XFS 640 - 649. REPAIRED IAW EO DC8-5720-4087-B.Apr 20, 2000 · N700UP · Doug DC871F · Leading Edge DevicesSDR UPS00832584Fitting · crackedINSPECTION TYPE:C-2, RT UPPER CUSP FITTING CRACKED STA 324. REMOVED, FABBED AND INSTALLED CUSP FITTING IAW DWG NR 3754031 & SRM 51-1- 20D.Apr 20, 2000 · N700UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00832565Rib · crackedINSPECTION TYPE:C-2, RIGHT WING L/E UPPER RIB CRACKED STA XS 250.089. STOP DRILLED CRACKED IAW SRM 57-2-0 FIG 2. FAB AND INSTALLED ANGLE DOUBLERS IAW SRM 51-1-20D & 51-3-0.Apr 20, 2000 · N700UP · Doug DC871F · Leading Edge DevicesSDR UPS00832558Rib · crackedINSPECTION TYPE:C-2, LEFT WING CENTER L/E RIB CRACKED STA XOLDI 6.225. STOP DRILLED CRACK IAW SRM 57-2-0 FIG 2. FAB AND INSTALLED DOUBLER IAW 57-2-0 FIG-2.Apr 20, 2000 · N700UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS00832557Skin · crackedINSPECTION TYPE:C-2, LEFT WING CENTER L/E LWR SKIN CRACKED STA XW 257. STOP DRILLED CRACK IAW ADDUM DC8-5720-4087-B. FAB AND INSTALLED DOUBLER IAW DC8-5720-4087-B.Apr 20, 2000 · N700UP · Doug DC871F · Leading Edge DevicesSDR UPS00832546Doubler · corrodedINSPECTION TYPE:C2, RIGHT WING L/E BETWEEN STA 772.500 TO XFS 760.00. THE INTERNAL DOUBLER HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 3641257.Apr 20, 2000 · N700UP · Doug DC871F · Leading Edge DevicesSDR UPS00832545Skin · crackedINSPECTION TYPE:C2, RIGHT WING L/E (NR 3 STUB WING) AT STA XS207.500. THE L/E SKIN IS CRACKED AT FRONT SPAR. REPAIRED AREA IAW DC8-5720-7767-A.Apr 20, 2000 · N700UP · Doug DC871F · Leading Edge DevicesSDR UPS00832536Rib · crackedINSPECTION TYPE:C2, RIGHT WING L/E EXTERIOR SKIN IS CRACKED AT STA XFS288.00 ON THE L/E. REPAIRED AREA IAW SRM 57-2-1 FIG 2H.Apr 20, 2000 · N700UP · Doug DC871F · Leading Edge DevicesSDR UPS00832534Rib · crackedINSPECTION TYPE:C2, RIGHT WING L/E AT STA XFS.792.250. THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Apr 20, 2000 · N700UP · Doug DC871F · Leading Edge DevicesSDR UPS00832532Rib · crackedINSPECTION TYPE:C2, LEFT WING L/E UPPER RIB IS CRACKED AT STA XS.00. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Apr 20, 2000 · N700UP · Doug DC871F · Leading Edge DevicesSDR UPS00832531Skin · corrodedINSPECTION TYPE:C2, RIGHT WING L/E SKIN HAS INTERNAL CORROSION AT STA XFS710.00. REPAIRED AREA IAW 8110-3 APPROVED DH SK 700-025.Apr 20, 2000 · N700UP · Doug DC871F · Leading Edge DevicesSDR UPS00832434Rib · crackedINSPECTION TYPE:C2, LEFT WING L/E UPPER RIB IS CRACKED AT XFS 647. REPAIRED IAW SRM 57-2-0 FIG 2.Apr 20, 2000 · N700UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS00832433Rib · crackedINSPECTION TYPE:C2, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 785. REPAIRED IAW SRM 57-2-0 FIG 2.Apr 20, 2000 · N700UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS00832432Rib · crackedINSPECTION TYPE:C2, RIGHT WING L/E LOWER RIB IS CRACKED AT XFS 341.5. REPAIRED IAW SRM 57-2-0 FIG 2.Apr 20, 2000 · N700UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS00832429Skin · crackedINSPECTION TYPE:C2, LT WING EXTERNAL SKIN IS CRACKED AT STA XFS 310.250 (LOWER SURFACE). REPAIRED AREA IAW SRM 57-3-3 FIG 5.Apr 20, 2000 · N700UP · Doug DC871F · Wing, Plate/SkinSDR UPS00832428Fitting · crackedINSPECTION TYPE:C2, STA 440 - 460 AT STR 31R, THE STRINGER SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257 AND SRM 51-1-20D.Apr 20, 2000 · N700UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00832426Rib · crackedINSPECTION TYPE:C2, RT WING L/E AT STA XFS 792.25, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Apr 20, 2000 · N700UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS00832421Rib · crackedINSPECTION TYPE:C2, LEFT WING L/E UPPER RIB IS CRACKED AT XFS 646. REPAIRED IAW SRM 57-2-0 FIG 2.Apr 20, 2000 · N700UP · Doug DC871F · Leading Edge DevicesSDR UPS00832420Rib · crackedINSPECTION TYPE:C2, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 283.25. REPAIRED IAW SRM 57-2-0 FIG 2.Apr 20, 2000 · N700UP · Doug DC871F · Leading Edge DevicesSDR UPS00832417Rib · crackedINSPECTION TYPE:C2, LEFT WING L/E UPPER RIB IS CRACKED AT XFS 660. REPAIRED IAW SRM 57-2-0 FIG 2.Apr 20, 2000 · N700UP · Doug DC871F · Leading Edge DevicesSDR RRXA003499Intercostal · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FWD LOWER CARGO BILGE INTERCOSTAL ANGLE TO CIRCUMFERENTIAL FRAME AT STA 380 AND L29R, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AApr 19, 2000 · N8084U · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00832582Skin · crackedINSPECTION TYPE:C-2, UPPER LT FUSELAGE SKIN AT CANTED FRAME 1746.621 AT LONG 15L SKIN CRACKED. CUT OUT CRACKED AREA IAW SRM 53-2-1 FIG 7. FABBED AND INSTALLED DOUBLER AND FINGER DOUBLER IAW SRM 53-2-1 FIG 7 & 51-1-20D.Apr 19, 2000 · N700UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS00832555Fitting · crackedINSPECTION TYPE:C-2, A- PIT STA 280 LONG 27R TORQUE BOX FITTING CRACKED. REMOVED AND INSTALLED FITTING IAW SRM 51-1-21D.Apr 19, 2000 · N700UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS00832554Seat Track · crackedINSPECTION TYPE:C-2, SEAT TRACK CRACKED AND HAS HEAVY CORROSION STA 1160 RBL 48. REMOVED DAMAGED SEAT TRACK IAW SRM 51-1-20D. FAB SEAT TRACK AND SPLICE, INSTALLED IAW EO DC8-5320-8309C.Apr 19, 2000 · N700UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS00832452Longeron · crackedINSPECTION TYPE:C2, STA 80 LONG 24L IS CRACKED. REPAIRED IAW SRM 53-2-2 FIG 10.Apr 19, 2000 · N700UP · Doug DC871F · Fuselage Main, Longeron/Stringer
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