Douglas DC-8-73F

Service difficulty reports · 15,471

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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 = 'DC873F'
  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 RRXA001840Seat Track · wornDURING A MAINTENANCE VISIT FOUND A WORN NR 7 SEAT TRACK AT STA 1580 TO 1575 AND RBL 59, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED TRACK IAW DC-8 SRM 53-2-3.Mar 28, 2000 · N961R · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA001839Seat Track · wornDURING A MAINTENANCE VISIT FOUND A WORN NR 6 SEAT TRACK AT STA 1480 AND 1494 RT AND RBL 45, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED TRACK IAW DC-8 SRM 53-2-3.Mar 28, 2000 · N961R · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA001838Seat Track · wornDURING A MAINTENANCE VISIT FOUND A WORN SEAT TRACK NR 6 AT RBL 45 STA 1388, 1393 & 1400 RT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PLUG IAW DC-8 SRM 53-2-3.Mar 28, 2000 · N961R · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA001837Seat Track · wornDURING A MAINTENANCE VISIT FOUND A WORN SEAT TRACK NR 4 TRACK STA 1400 AND 1435 AND RBL 25, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED TRACK IAW DC-8 SRM 53-2-3.Mar 28, 2000 · N961R · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA001835Fitting · elongatedDURING A MAINTENANCE VISIT FOUND A CRACK INDICATION TO THE STRINGER END FITTING AT THE LT WING LWR WING AT STA 64, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. OVERSIZED FASTENER HOLES AND INSTALLED SMar 28, 2000 · N961R · Doug DC873F · Wing Miscellaneous StructureSDR RRXA001823Seat Track · damagedDURING A MAINTENANCE VISIT FOUND SEVERAL ELONGATED HOLES IN THE SECOND OBS FWD SEAT TRACK, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED TRACK IAW DC-8 SRM 51-3-0.Mar 28, 2000 · N961R · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA001822Seat Track · elongatedDURING A MAINTENANCE VISIT FOUND SEVERAL ELONGATED LOCK HOLES IN THE SECOND O/B AFT SEAT TRACK, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED TRACK IAW DC-8 SRM 51-3-0.Mar 28, 2000 · N961R · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA001818Seat Track · damagedDURING A MAINTENANCE VISIT FOUND ELONGATED HOLES IN THE AFT SEAT TRACK FOR F/E SEAT LOCK, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW SEAT TRACK IAW DC-8 SRM 51-3-0.Mar 28, 2000 · N961R · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA001817Seat Track · damagedDURING A MAINTENANCE VISIT FOUND ELONGATED LOCK HOLES IN THE FWD SEAT TRACK FOR F/E''S SEAT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW TRACK IAW DC-8 SRM 51-3-0.Mar 28, 2000 · N961R · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA001814Seat Track · wornDURING A MAINTENANCE VISIT FOUND A WORN NR 4 SEAT TRACK PLUG AT STA 280 AND LBL 0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PLUG IAW DC-8 SRM 53-2-3.Mar 28, 2000 · N961R · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA001792Skin · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE LT IB FLAP OB OF STA 98, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED DOUBLER AND INSTALLED IAW DC-8 SRM 51-1-21, 57-2-0 AND E.Mar 28, 2000 · N961R · Doug DC873F · Trailing Edge FlapsSDR RRXA001791Skin · damagedDURING A MAINTENANCE VISIT, FOUND SCREWS LOOSE AND PULLING THROUGH SKIN AT LT OB FLAP IB WEDGE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SKIN IAW DC-8 SRM 51-3-0, Mar 28, 2000 · N961R · Doug DC873F · Trailing Edge FlapsSDR DHL2000804135Fitting · crackedTAIL CONE INTERIOR NR 62 ACCESS DOOR ELEVATOR CONTROL LT FITTING LOWER PART INTERNAL PANEL CRACKED 1.5 INCH. REMOVED FASTENERS PER SRM 51-1-21. STOP DRILLED PER SRM 53-2-0. FABRICATED DOUBLER PER SRM 53-2-0. CLEANED, TREATED AND PRIMED PER SRM 51-1-8. INSMar 28, 2000 · N804DH · Doug DC873F · Tail Cone DoorsSDR UPS00832318Skin · corrodedINSPECTION TYPE:C1 LEFT WING L/E CORRODED BEYOND LIMITS AT XFS 900. REMOVED, FABRICATED AND REPLACED L/E SKIN IAW DWG 9751896 AND SRM 51-1-21.Mar 28, 2000 · N812UP · Doug DC873F · Wing, Plate/SkinSDR UPS00832316Fitting · crackedINSPECTION TYPE:C1 STA 1766 AFT PRESSURE BULKHEAD ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4772398 AND SRM 51-1-21.Mar 28, 2000 · N812UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832315Spar Cap · corrodedINSPECTION TYPE:C1 LEFT WING AUX TANK UPPER SPAR CAP CORROSION REMOVAL IS BEYOND LIMITS BETWEEN XFS 116 - 126.25. REPAIRED IAW SRM 57-2-1 FIG 37.Mar 28, 2000 · N812UP · Doug DC873F · Wing SparSDR UPS00832313Seat Track · corrodedINSPECTION TYPE:C1 STA 1120 - 1140 LBL 24 SEAT TRACK HAS HEAVY CORROSION AROUND SEAT TRACK PLUGS. REPAIRED IAW SRM 53-2-3 FIG 12.Mar 28, 2000 · N812UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS00832308Frame · crackedINSPECTION TYPE:C1 STA 55 FRAME IS CRACKED BETWEEN LONG 23R AND 24R. REPAIRED IAW SRM 53-2-0 FIG 2.Mar 28, 2000 · N812UP · Doug DC873F · Fuselage Main, FrameSDR UPS00832306Skin · crackedINSPECTION TYPE:C1 RIGHT WING L/E LOWER SKIN IS CRACKED AT XFS 341.5. REPAIRED IAW SRM 57-3-3 FIG 5.Mar 28, 2000 · N812UP · Doug DC873F · Wing, Plate/SkinSDR UPS00832297Angle · crackedINSPECTION TYPE:C1 STA 717 FLOORBEAM SUPPORT ANGLE IS CRACKED AT BL 0. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 5773275 AND SRM 51-1-20D.Mar 28, 2000 · N812UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832277Fitting · crackedINSPECTION TYPE:C1 STA 759 RBL 24 FLOORBEAM ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755222 AND SRM 51-1-20D.Mar 28, 2000 · N812UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832276Fitting · crackedINSPECTION TYPE:C1 STA 280 AT LONG 27R VERTICAL SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 9754024 AND SRM 51-1-20D.Mar 28, 2000 · N812UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832275Fitting · crackedINSPECTION TYPE:C1 STA 717 LBL 24 FLOORBEAM ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755222, AND SRM 51-1-20D.Mar 28, 2000 · N812UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832269Rib · crackedINSPECTION TYPE:C1 RIGHT WING L/E LOWER RIB IS CRACKED AT XFS 610. REPAIRED IAW SRM 57-2-0 FIG 2.Mar 28, 2000 · N812UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS00832266Angle · crackedINSPECTION TYPE:C1 STA 781 RBL 50 FLOORBEAM ATTACH ANGLE IS CRACKED. REMOVED AND REPLACED ANGLE IAW DWG 3643111, AND SRM 51-1-20D.Mar 28, 2000 · N812UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832262Fitting · crackedINSPECTION TYPE:C1 LOWER FLOORBEAM TO CUSP FITTING CRACKED FS 280 AT LONG 21R. REMOVED, FAB AND REPLACED CUSP FITTING IAW SRM 51-1-21 & 51-3-0.Mar 28, 2000 · N812UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832260Seat Track · corrodedINSPECTION TYPE:C1 SEAT TRACK CORRODED BEYOND LIMITS AT FS 155 0 BL. REMOVED FAB REPLACED SEAT TRACK IAW SRM 53-2-3 FIG 8A.Mar 28, 2000 · N812UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA001922Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK IN THE SKIN UPPER SURFACE LT CENTER SECTION L/E AT STA XFS 366, 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 51-1-Mar 27, 2000 · N961R · Doug DC873F · Leading Edge DevicesSDR RRXA001786Skin · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK IN THE SKIN UPPER SURFACE AT THE LT CENTER SECTION LE AT STA XFS 366, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DCMar 27, 2000 · N961R · Doug DC873F · Leading Edge DevicesSDR UPS00832312Skin · corrodedINSPECTION TYPE:C1 LEFT WING L/E SKIN IS CORRODED BEYOND LIMITS AT XFS 710. REPAIRED IAW SRM 57-2-1 FIG 2H.Mar 27, 2000 · N812UP · Doug DC873F · Wing, Plate/SkinSDR UPS00832309Skin · crackedINSPECTION TYPE:C1 RIGHT WING L/E LOWER SKIN IS CRACKED AT NR 3 PYLON CUTOUT XS 220.190. REPAIRED IAW SRM 57-2-1A FIG 2.Mar 27, 2000 · N812UP · Doug DC873F · Wing, Plate/SkinSDR UPS00832301Fitting · crackedINSPECTION TYPE:C1 STA 680 LONG 11L INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4751625 AND SRM 51-1-20D.Mar 27, 2000 · N812UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832300Skin · crackedINSPECTION TYPE:C1 RIGHT WING L/E EXT SKIN IS CRACKED AT XFS 710. REPAIRED IAW SRM 57-2-1 FIG 2H.Mar 27, 2000 · N812UP · Doug DC873F · Wing, Plate/SkinSDR UPS00832299Skin · crackedINSPECTION TYPE:C1 LEFT WING L/E UPPER SKIN IS CRACKED BETWEEN XFS 647.5 AND XFS 655. REPAIRED IAW SRM 57-2-1 FIG 38.Mar 27, 2000 · N812UP · Doug DC873F · Wing, Plate/SkinSDR UPS00832295Fitting · crackedINSPECTION TYPE:C1 STA 781 LONG 18R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750025, AND SRM 51-1-20D.Mar 27, 2000 · N812UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832294Skin · crackedINSPECTION TYPE:C1 LEFT WING L/E UPPER SKIN IS CRACKED AT XFS 347.75. REPAIRED IAW SRM 57-2-1 FIG 38.Mar 27, 2000 · N812UP · Doug DC873F · Wing, Plate/SkinSDR UPS00832293Rib · crackedINSPECTION TYPE:C1 RIGHT WING L/E LOWER RIBS ARE CRACKED AT XFS 635.75 AND XFS 660. REPAIRED IAW SRM 57-2-0 FIG 2.Mar 27, 2000 · N812UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS00832274Rib · crackedINSPECTION TYPE:C1 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 285.25. REPAIRED IAW SRM 57-2-0 FIG 2.Mar 27, 2000 · N812UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS00832273Skin · crackedINSPECTION TYPE:C1 LEFT WING L/E UPPER SKIN IS CRACKED AT XFS 316.5. REPAIRED IAW SRM 57-2-1 FIG 38.Mar 27, 2000 · N812UP · Doug DC873F · Wing, Plate/SkinSDR UPS00832272Skin · crackedINSPECTION TYPE:C1 LEFT WING L/E UPPER SKIN IS CRACKED BETWEEN XFS 603.75 AND XFS 628.75. REPAIRED IAW SRM 57-2-1 FIG 38.Mar 27, 2000 · N812UP · Doug DC873F · Wing, Plate/SkinSDR UPS00832267Rib · crackedINSPECTION TYPE:C1 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 672.5. REPAIRED IAW SRM 57-2-0 FIG 2.Mar 27, 2000 · N812UP · Doug DC873F · Wing, Rib/BulkheadSDR RRXA000607Longeron · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE LONGERON AT STA 155 AND ''X'' LONGERON 35L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED IAW DC-8 SRM 51-1-20D, 5-1-21 AND 53-2-Mar 26, 2000 · N831AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA001977Track · wornDURING A MAINTENANCE VISIT FOUND A WORN NR 2 TRACK AT STA 1590, 1580 & 1572 AND LBL 45 INCHES, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED TRACK IAW DC-8 SRM 53-2-3.Mar 25, 2000 · N961R · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA001930Structure · damagedDURING A MAINTENANCE VISIT FOUND SCREWS PULLING THROUGH SKIN AT THE RIGHT LWR SURFACE I/B AUX TANK AT STA XFS 88 TO 132, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAMar 25, 2000 · N961R · Doug DC873F · Fuel StorageSDR RRXA001924Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AND SCREWS PULLING THROUGH SKIN AT THE LEFT I/B NR 2 STUB WING AT STA XFS 250 TO 291, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTMar 25, 2000 · N961R · Doug DC873F · Wing, Plate/SkinSDR RRXA001923Fitting · chafedDURING A MAINTENANCE VISIT FOUND CHAFING AT THE CANOE FITTING LEFT O/B FLAP O/B SLIDING HINGE COVER O/B FWD ROD END AT STA 410, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED REPAMar 25, 2000 · N961R · Doug DC873F · Trailing Edge FlapsSDR RRXA001907Skin · tornDURING A MAINTENANCE VISIT FOUND TORN SKIN 8 INCHES AFT OF AILERON L/E LEFT O/B AILERON UPPER SURFACE O/B EDGE AT STA XA 747, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBMar 25, 2000 · N961R · Doug DC873F · AileronsSDR RRXA001795Panel · damagedDURING A MAINTENANCE VISIT FOUND SCREWS PULLING THROUGH THE SKIN AT THE RT LWR SURFACE I/B AUX TANK AT STA XFS 88 TO 132, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 EOMar 25, 2000 · N961R · Doug DC873F · Wing, Plate/SkinSDR RRXA001789Skin · damagedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE AND SCREWS PULLING THROUGH SKIN AT LT IB NR 2 STUB WING AT STA XFS 250 TO 291, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTAMar 25, 2000 · N961R · Doug DC873F · Wing, Plate/SkinSDR RRXA001787Fitting · chafedDURING A MAINTENANCE VISIT, FOUND A CHAFED CANOE FITTING AT THE LT OB FLAP OB SLIDING HINGE COVER OB FWD ROD END AT STA 410, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. BLENDED CHAFED AREA AND REMar 25, 2000 · N961R · Doug DC873F · Trailing Edge Flaps
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