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 UPS00832822Skin · gougedINSPECTION TYPE:C123, STA 520 AT LONG 31R EXTERIOR IS GOUGED BEYOND LIMITS. REPAIRED IAW 8110-3 APPROVED DH SK 730-037.May 23, 2000 · N730UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS00832633Odor · detectedINSPECTION TYPE:N/A, AIRCRAFT HAS BURNING SMELL WHEN ANTI ICE IS SELECTED ON. SMELL WENT AWAY WHEN ANTI ICE SELECTED OFF. PACK TEMPS WERE BOTH AT 25 DEGREE C AND BOTH MANIFOLD TEMPS WERE AT 200 DEGREES C. REPEAT WRITE UP, STILL TROUBLESHOOTING AT THIS TIME.May 23, 2000 · N707UP · Doug DC871F · Air Distribution SystemSDR UPS00832794Shear Tie · crackedINSPECTION TYPE:C123, STA 702.85 SHEAR TIE FITTING IS CRACKED BETWEEN LONG 35L AND 36. REMOVED AND REPLACED FITTING IAW DWG 3753757 AND SRM 51-1-20D.May 22, 2000 · N730UP · Doug DC871F · Fuselage Main, StructureSDR UPS00832770Angle · crackedINSPECTION TYPE:C123, RIGHT WING L/E VERTICAL ANGLE IS CRACKED AT XS 520. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 9753297 AND SRM 51-1-20D.May 22, 2000 · N730UP · Doug DC871F · Leading Edge DevicesSDR UPS00832674Battery · inoperativeINSPECTION TYPE:N/A, ON PRE-DEPARTURE CHECK, FOUND EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY BATTERY ASSY, OPS CK GOOD.May 22, 2000 · N718UP · Doug DC871F · Emergency LightingSDR UPS00832887Angle · crackedINSPECTION TYPE:C123, LEFT WING L/E VERTICAL ANGLE IS CRACKED AT XS 250.089. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753293 AND SRM 51-1-20D, 51-1-21.May 21, 2000 · N730UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS00832883Fitting · crackedINSPECTION TYPE:C123, STA 70 LONG 35L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4610355 AND SRM 51-1-20D.May 21, 2000 · N730UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS00832833Keelbeam · corrodedINSPECTION TYPE:C123, KEEL BEAM IS CORRODED BEYOND LIMITS AT STA 660 - 680 AT LONG 36. REPAIRED IAW 8110-3 APPROVED DH SK 730-934.May 21, 2000 · N730UP · Doug DC871F · Fuselage Main, KeelSDR UPS00832829Shear Tie · corrodedINSPECTION TYPE:C123, STA 660 SHEAR TIE BETWEEN LONG 34L-34R IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED IAW DWG 5616509 AND SRM 51-1-21.May 21, 2000 · N730UP · Doug DC871F · Fuselage Main, StructureSDR UPS00832824Longeron · corrodedINSPECTION TYPE:C123, STA 70 LONG 35L IS CORRODED BEYOND LIMITS. REPAIRED IAW SRM 53-2-2 FIG 10.May 21, 2000 · N730UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS00832819Angle · crackedINSPECTION TYPE:C123, LEFT WING L/E ANGLE IS CRACKED AT XS 520. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 5769589 AND SRM 51-1-20D.May 21, 2000 · N730UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS00832814Rib · crackedINSPECTION TYPE:C123, LEFT WING L/E UPPER RIBS ARE CRACKED AT XFS 366.5 AND 372.75. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.May 21, 2000 · N730UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS00832806Doubler · crackedINSPECTION TYPE:C123, RIGHT WING L/E INTERNAL DOUBLER IS CRACKED AT XFS 341. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769589 AND SRM 51-1-20D, 51-1-21.May 21, 2000 · N730UP · Doug DC871F · Wing, Plate/SkinSDR UPS00832788Rib · gougedINSPECTION TYPE:C123, LEFT WING L/E RIB XS 510 IS GOUGED BEYOND LIMITS. REPAIRED RIB IAW SRM 57-2-0 FIG 2.May 21, 2000 · N730UP · Doug DC871F · Leading Edge DevicesSDR UPS00832779Rib · crackedINSPECTION TYPE:C123, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 379. REPAIRED RIB IAW SRM 57-2-0 FIG 2.May 21, 2000 · N730UP · Doug DC871F · Leading Edge DevicesSDR UPS00832778Rib · crackedINSPECTION TYPE:C123, RIGHT WING L/E RIB IS CRACKED AT XS497.491. REPAIRED RIB IAW SRM 57-2-0 FIG 2.May 21, 2000 · N730UP · Doug DC871F · Leading Edge DevicesSDR UPS00832776Rib · crackedINSPECTION TYPE:C123, LEFT WING L/E UPPER RIB IS CRACKED AT XFS 647.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2.May 21, 2000 · N730UP · Doug DC871F · Leading Edge DevicesSDR UPS00832775Angle · crackedINSPECTION TYPE:C123, LEFT WING L/E VERTICAL ANGLE IS CRACKED AT XS 256. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753294 AND SRM 51-1-20D.May 21, 2000 · N730UP · Doug DC871F · Leading Edge DevicesSDR UPS00832673Pan · corrodedINSPECTION TYPE:C123, FWD ACCY COMP DOOR PAN HAS AREA CORRODED BEYOND LIMITS. REPAIRED IAW SRM 53-2-0 FIG 23.May 21, 2000 · N730UP · Doug DC871F · Accessory Compartment DoorsSDR UPS00832885Rib · crackedINSPECTION TYPE:C123, RIGHT WING L/E LOWER RIB IS CRACKED AT XFS 335.250. REMOVED, FABRICATED AND REPLACED RIB IAW DWG 5769530 AND SRM 51-1-20D.May 20, 2000 · N730UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS00832884Fitting · crackedINSPECTION TYPE:C123, STA 280 LONG 34R TORQUE BOX SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 9754055 AND SRM 51-3-0.May 20, 2000 · N730UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS00832818Rib · crackedINSPECTION TYPE:C123, RIGHT WING L/E RIB IS CRACKED BEYOND LIMITS AT XS 503.789. REPAIRED RIB IAW SRM 57-2-0 FIG 2.May 20, 2000 · N730UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS00832811Doubler · crackedINSPECTION TYPE:C123, LEFT WING LOWER INTERNAL DOUBLER IS CRACKED AT XFS 250. REMOVED, FABRICATED AND REPLACED DOUBLER IAW 5769699 AND SRM 51-1- 21.May 20, 2000 · N730UP · Doug DC871F · Wing Main, Frame StructureSDR UPS00832803Doubler · crackedINSPECTION TYPE:C123, LEFT WING L/E INTERNAL DOUBLER IS CRACKED AT XFS 556.250. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769600 AND SRM 51-1-21.May 20, 2000 · N730UP · Doug DC871F · Wing, Plate/SkinSDR UPS00832774Doubler · crackedINSPECTION TYPE:C123, RIGHT WING L/E INTERNAL DOUBLER IS CRACKED AT XFS 250. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769859 AND SRM 51-1-20D, 51-1-21.May 20, 2000 · N730UP · Doug DC871F · Wing, Plate/SkinSDR UPS00832773Rib · crackedINSPECTION TYPE:C123, RIGHT WING L/E UPPER RIB IS CRACKED AT XOLDI 6.225. REPAIRED RIB IAW SRM 57-2-0 FIG 2.May 20, 2000 · N730UP · Doug DC871F · Leading Edge DevicesSDR UPS00832766Doubler · crackedINSPECTION TYPE:C123, LEFT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 304. REMOVED AND REPLACED DOUBLER IAW DWG 5641252 AND SRM 51-1-20D, 51-1-21.May 20, 2000 · N730UP · Doug DC871F · Wing, Plate/SkinSDR UPS00832764Doubler · crackedINSPECTION TYPE:C123, RIGHT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 341.5. REPAIRED IAW 8110-3 APPROVED DH SK 730-808.May 20, 2000 · N730UP · Doug DC871F · Wing, Plate/SkinSDR UPS00832891Skin · corrodedINSPECTION TYPE:C123, STA 620 - 640 LONG 35L-36 INTERNAL SKIN IS CORRODED BEYOND LIMITS. REPAIRED IAW 8110-3 APPROVED DH SK 730-651.May 19, 2000 · N730UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS00832888Rib · crackedINSPECTION TYPE:C123, RIGHT HORIZONTAL STAB L/E LOWER RIB IS CRACKED AT XFS 116.25. REPAIRED IAW SRM 55-2-0 FIG 2.May 19, 2000 · N730UP · Doug DC871F · Horizontal Stabilizer, Spar/RibSDR UPS00832835Rib · crackedINSPECTION TYPE:C123, LEFT HORIZONTAL STAB L/E RIB IS CRACKED AT XFS141.25. REPAIRED RIB IAW SRM 55-2-0 FIG 2.May 19, 2000 · N730UP · Doug DC871F · Horizontal Stabilizer, Spar/RibSDR UPS00832830Skin · crackedINSPECTION TYPE:C123, STA 1340 LONG 11L UPPER AFT CORNER OF CENTER LEFT SERVICE DOOR OPENING SKIN IS CRACKED. REPAIRED IAW SRM 53-2-0 FIG 18.May 19, 2000 · N730UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS00832827Shear Tie · corrodedINSPECTION TYPE:C123, STA 640 SHEAR TIE IS CORRODED BEYOND LIMITS BETWEEN LONG 34L AND 34R. REMOVED, FABRICATED AND REPLACED SHEAR TIE IAW DWG 5616509 AND SRM 51-1-21.May 19, 2000 · N730UP · Doug DC871F · Fuselage Main, StructureSDR UPS00832825Intercostal · corrodedINSPECTION TYPE:C123, STA 1746 AT RBL 16 FLOORBEAM INTERCOSTAL IS CORRODED BEYOND LIMITS. REPAIRED IAW SRM 53-2-0 FIG 1B AND 1D.May 19, 2000 · N730UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00832812Fitting · crackedINSPECTION TYPE:C123, STA 440 - 460 LONG 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257 AND SRM 51-1-20D.May 19, 2000 · N730UP · Doug DC871F · Fuselage Main, StructureSDR UPS00832780Intercostal · crackedINSPECTION TYPE:C123, STA -80 LBL 59 VERTICAL INTERCOSTAL IS CRACKED. REPAIRED INTERCOSTAL IAW SRM 53-2-0 FIG 1B.May 19, 2000 · N730UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00832777Floorbeam · crackedINSPECTION TYPE:C123 STA -23 BL 0 FLOORBEAM UPPER FLANGE IS CRACKED. REPAIRED FLOORBEAM IAW SRM 53-2-0 FIG 1B.May 19, 2000 · N730UP · Doug DC871F · Fuselage Main, Floor BeamSDR UPS00832767Rib · crackedINSPECTION TYPE:C123, RIGHT HORIZONTAL STAB L/E UPPER RIB IS CRACKED AT XFS 172.5. REPAIRED IAW SRM 55-2-0 FIG 2.May 19, 2000 · N730UP · Doug DC871F · Horizontal Stabilizer, Spar/RibSDR RRXA002764Retainer · crackedDURING A MAINTENANCE VISIT FOUND A CRACK IN SEAL RETAINER OUTBOARD CENTER ''C'' PIT DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0, 52-2-0 AND 5May 18, 2000 · N8084U · Doug DC871F · Cargo/Baggage DoorsSDR RRXA002737Doubler · looseDURING A MAINTENANCE VISIT FOUND PREVIOUS REPAIR DOUBLER SEPARATING, FASTENER HOLES ELONGATED AND SEALANT DETERIORATED ON THE RT WING MIDDLE L/E AT STA XW 408, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1May 18, 2000 · N8084U · Doug DC871F · Wing, Plate/SkinSDR RRXA002734Skin · bulgedDURING A MAINTENANCE VISIT FOUND BULGED AND SCRATCHED SKIN ON THE RT WING O/B LEADING EDGE EXTERIOR AT STA XFS 724, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NR 00-107 WITMay 18, 2000 · N8084U · Doug DC871F · Wing, Plate/SkinSDR RRXA002732Skin · damagedDURING A MAINTENANCE VISIT FOUND CREASED AND BILGED SKIN ON THE RT WING O/B LEADING EDGE EXTERIOR SKIN AT STA 714, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NR 00-107 WITHMay 18, 2000 · N8084U · Doug DC871F · Wing, Plate/SkinSDR RRXA002721Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE RT WING BOTTOM OF LEADING EDGE O/B NR 3 PYLON O/B OF PANEL 523 AT STA XFS 291.500, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLEDMay 18, 2000 · N8084U · Doug DC871F · Wing, Plate/SkinSDR RRXA002669Skin · wornDURING A MAINTENANCE VISIT FOUND THE SKIN WORN THROUGH ON THE AFT O/B END ON THE O/B WING L/E AT STA XRS 878, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW EO NR 00-May 18, 2000 · N8084U · Doug DC871F · Wing, Plate/SkinSDR RRXA002664Skin · crackedDURING A MAINTENANCE VISIT FOUND ABOUT A 1.5 INCH CRACK IN SKIN AND 9 FASTENERS BAD ON THE LEFT L/E AT STA XFS 422, 9 INCHES FROM FRONT SPAR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED ANMay 18, 2000 · N8084U · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA002663Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK EXTENDING FROM SCREW HOLE ON THE LEFT L/E AT STA X OLDI 6.225, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-0May 18, 2000 · N8084U · Doug DC871F · Wing, Plate/SkinSDR UPS00832894Longeron · corrodedINSPECTION TYPE:C123, STA 1560 LONG 34R IS CORRODED BEYOND LIMITS. REPAIRED LONGERON IAW SRM 53-2-0 FIG 10.May 18, 2000 · N730UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS00832889Floor Support · crackedINSPECTION TYPE:C123, STA 1520 AT LONG 27L VERTICAL FLOORBEAM SUPPORT IS CRACKED. REMOVED, FABRICATED AND REPLACED SUPPORT IAW DWG 3610417 AND SRM 51-1-20D.May 18, 2000 · N730UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00832886Rib · crackedINSPECTION TYPE:C123, LEFT WING L/E UPPER RIB IS CRACKED AT XFS 716.25. REPAIRED RIB IAW SRM 57-2-0 FIG 2.May 18, 2000 · N730UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS00832832Finger Doubler · corrodedINSPECTION TYPE:C123, STA 869 BL 0 FINGER DOUBLER IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5645332 AND SRM 51-1-20D.May 18, 2000 · N730UP · Doug DC871F · Fuselage Miscellaneous Structure
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