Douglas DC-8-73F

Service difficulty reports · 15,471

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 = '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 RRXA99645Bulkhead Web · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO BULKHEAD WEB AND FITTING BETWEEN STA -12 TO STA -32 AND LONGERON 23 LEFT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW WEB AND FITTIOct 19, 1998 · N602AL · Doug DC873F · Fuselage Main, BulkheadSDR DHL9980176CPanel · crackedAT C-CHECK, LEFT WING TRAILING EDGE I/B LOWER AREA AT XW 5, JUST ABOVE I/B FLAP HINGE CRACKS ON WEB COVER PANEL. REMOVED AND FABRICATED NEW COVER PLATE AND INSTALLED PER SRM 51-3-0, 15 X 5.25.Oct 19, 1998 · N801DH · Doug DC873F · Wing, Plate/SkinSDR DHL9980175CPanel · crackedAT C-CHECK, LT WING TRAILING EDGE I/B LOWER AREA AT STA XW 5, JUST ABOVE FLAP I/B HINGE AREA FOUND CRACK AT WEB PANEL. REMOVED, FABRICATED AND INSTALLED PANEL PER SRM 51-1-21.Oct 19, 1998 · N801DH · Doug DC873F · Wing, Plate/SkinSDR DHL9980174CStrip · crackedAT C-CHECK, RIGHT WING LEADING EDGE I/B EXT LOWER AREA AT STA 69 METAL RUB STRIP CRACKED. REMOVED DAMAGED STRIP, FABRICATED NEW STRIP AND INSTALLED PER SRM 51-1-1.Oct 19, 1998 · N801DH · Doug DC873F · Wing Miscellaneous StructureSDR DHL9980173CSkin · bentAT C-CHECK, LT WING O/B FLAP LOWER CORNER TIP IS BENT. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED NEW T/E PER SRM 51-1-4 AND 51-1-21, 5 X 8.Oct 19, 1998 · N801DH · Doug DC873F · Trailing Edge FlapsSDR DHL9980171CRib · crackedAT C-CHECK, RT WING O/B LEADING EDGE INTERIOR LOWER AREA AT STA 785 RIBS CRACKED. STOP DRILLED HOLE AND FABRICATED DOUBLER REPAIR 6 X 1/25 PER SRM 57-2-0.Oct 19, 1998 · N801DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL9980169CFitting · crackedAT C-CHECK, LEFT WING HINGE FITTING BOLT AT STA NR 3B BOLT HOLE CRACKED I/B SIDE STA 97. REAMED BOLT HOLE .0312 OVERSIZE PER SRM 51-3-2.Oct 19, 1998 · N801DH · Doug DC873F · Trailing Edge FlapsSDR DHL9980168CHinge Fitting · crackedAT C-CHECK, LEFT WING FLAP HINGE FITTING STA 97 NR 3A BOLT HOLE O/B SIDE CRACKED. REMOVED FITTING, INSTALLED NEW FITTING PER S/B 27-249 AND SRM 51-1-21.Oct 19, 1998 · N801DH · Doug DC873F · Trailing Edge FlapsSDR DHL9980167CCowl · crackedAT C-CHECK, ENGINE NR 4 O/B TRANSLATING COWL INNER PANEL SECTION SHOWS CRACK DAMAGE TO INTERIOR SURFACE. STOP DRILLED END OF CRACK, FABRICATED REPAIR PER SRM 71-2-8, 3 X 3.5.Oct 19, 1998 · N801DH · Doug DC873F · Engine Cowling SystemSDR DHL9980166CCowl · chafedAT C-CHECK, ENGINE NR 4 INTERIOR PANEL OF O/B TRANSLATING COWL ON INTERIOR SURFACE CHAFED. CUT OUT CHAFING AND INSTLALLED DOUBLER PER 70 SERIES SRM 71-2-8, 2 X 2.Oct 19, 1998 · N801DH · Doug DC873F · Engine Cowling SystemSDR DHL9980198CRib · crackedAT C-CHECK, RT WING CENTER L/E LOWER INTERIOR AREA AT STA 347 FOUND CRACK ON LOWER RIB. STOP DRILLED HOLE, FABRICATED REPAIR DOUBLER PER SRM 57-2-0 AND INSTALLED PER SRM 51-1-21, 6 X 1.25.Oct 18, 1998 · N801DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL99801102Strip · wornAT C-CHECK, RT WING O/B FLAP UPPER AREA CENTER ICE BREAKER AREA I/B AND O/B METAL RUB STRIPS WORN. REMOVED AND REPLACED RUB STRIPS PER SRM 51-1-7, 1 X 7.Oct 18, 1998 · N801DH · Doug DC873F · Trailing Edge FlapsSDR DHL99801101Strip · wornAT C-CHECK, RT O/B FLAP UPPER AREA O/B ICE BREAKER AFT AREA HAS RUB STRIPS WORN OUT. REMOVED AND FABRICATED NEW RUB STRIP AND INSTALLED PER SRM 51-1-21, 1 X 7.Oct 18, 1998 · N801DH · Doug DC873F · Trailing Edge FlapsSDR DHL9980197CFloor Panel · crackedAT C-CHECK, FWD LOWER CARGO COMPT STA 180 RT UNDER BRACKET SUPPORT ATTACHING TO FLOOR PANEL CRACKED. REMOVED DAMAGED SECTION, FABRICATED DOUBLER AND INSTALLED PER SRM 53-2-0, 5 X 7.Oct 17, 1998 · N801DH · Doug DC873F · Fuselage Floor PanelSDR DHL9980164CFrame · crackedAT C-CHECK, AFT FWD CARGO COMPT METAL AFT SIDE OF C2 DOOR JAMBS WALL CRACKED LOWER SIDE DAMAGED. STOP DRILLED CRACK, FABRICATED AND INSTALLED ANGLE REPAIR AND INSTALLED PER SRM 51-1-8, 4 X 4.Oct 17, 1998 · N801DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL9980162CSkin · crackedAT C-CHECK, RT WING T/E AREA STA 106 JUST BELOW I/B FLAP ACTUATOR LT SIDE LOWER AREA CRACKED AT FAIRING CUTOUT. REPAIRED AND REINSTALLED PANEL PER SRM 51-3-0.Oct 17, 1998 · N801DH · Doug DC873F · Wing, Plate/SkinSDR DHL9980161CSkin · crackedAT C-CHECK, RT WING I/B TRAILING EDGE AREA AT STA XWS 5 CRACK ON WEB PANEL JUST ABOVE I/B FLAP I/B HINGE AREA. REMOVED CRACKED PANEL, FABRICATED NEW WEB PER SRM 51-1-21, 15 X 5.5.Oct 17, 1998 · N801DH · Doug DC873F · Wing, Plate/SkinSDR DHL9980160CPanel · crackedAT C-CHECK, RT WING L/E LOWER AREA STA XW 485 SMALL SQUARE ACCESS PANEL CRACKED. REMOVED, FABRICATED AND INSTALLED NEW PANEL PER SRM 51-1-4, 7 X 7.Oct 17, 1998 · N801DH · Doug DC873F · Wing, Plate/SkinSDR DHL9980159CRub Strip · brokenAT C-CHECK, RT WING T/E LOWER AREA STA 311 METAL RUB STRIP AT STA 311. FABRICATED NEW RUB STRIP AND INSTALLED PER SRM 51-1-21, 2 X 10.Oct 17, 1998 · N801DH · Doug DC873F · Trailing Edge FlapsSDR DHL9980158CCover · crackedAT C-CHECK, RT WING O/B FLAP I/B HINGE O/B FACE METAL COVER BROKEN. REMOVED DAMAGED COVER AND FABRICATED NEW AND INSTALLED PER SRM 51-121.Oct 17, 1998 · N801DH · Doug DC873F · Trailing Edge FlapsSDR DHL9980154CBracket · crackedAT C-CHECK, MAIN CARGO COMPT FS 360 CEILING RT SIDE ATTACH BRACKET BROKEN. REMOVED AND FABRICATED NEW BRACKET PER SRM 51-1-21, 2 X 2.Oct 17, 1998 · N801DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL9980153CBracket · crackedAT C-CHECK, RT WING O/B LEADING EDGE INTERIOR AT STA 603 FOUND PNEUMATIC SUPPORT CRACKED. FABRICATED REPAIR DOUBLER PER SRM 51-1-21, 2 X 6.Oct 17, 1998 · N801DH · Doug DC873F · Wing Miscellaneous StructureSDR DHL99801109Structure · crackedAT C-CHECK, RT CENTER LOWER INT AREA AT STA 337 CRACKED. REMOVED CENTER L/E, FABRICATED REPAIR DOUBLER PER SRM 57-3-3, 25 X 16. INSTALLED PER SRM 51-1-8, INSTALLED CENTER L/E PER 57-20-2.Oct 17, 1998 · N801DH · Doug DC873F · Wing Main, Frame StructureSDR DHL99801108Rib · crackedAT C-CHECK, LEFT WING LOWER INT AREA AT STA 337 HAS CRACK 12 INCHES LONG ON LOWER INT RIB WEB AREA. REMOVED CENTER L/E LEFT WING. REMOVED CRACKED LOWER DOUBLER FROM CENTER L/E AT 337. FABRICATED REPAIR DOUBLER PER SRM 57-3-3, 25 X 16. INSTALLED DOUBLER PEROct 17, 1998 · N801DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL99801107Angle · crackedAT C-CHECK, RIGHT WING T/E INBOARD LOWER STA 5.00 AT I/B FLAP I/B HINGE SUPPORT FWD AREA FOUND CRACK ON ANGLE REINFORCEMENT. REMOVED CRACKED ANGLE, FABRICATED NEW ANGLE 12 X 2.5 PER SRM 51-1-21.Oct 17, 1998 · N801DH · Doug DC873F · Wing Miscellaneous StructureSDR DHL99801106Angle · crackedAT C-CHECK, RT WING T/E AREA AT STA XW 5 CRACKED ON ANGLE NEXT TO WEB PANEL. STOP DRILLED, FABRICATED ANGLE REPAIR PER DC-8 SRM 51-1-4, 6 X 2.Oct 17, 1998 · N801DH · Doug DC873F · Wing Miscellaneous StructureSDR RRXA99736Floor · corrodedDURING A MAINTENANCE VISIT, FOUND BULGE IN MAIN CABIN FLOOR PANEL AT STA 300 BL 36R. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAOct 16, 1998 · N795FT · Doug DC873F · Fuselage Floor PanelSDR DHL9980157CCowling · delaminatedAT C-CHECK, ENG NR 4 I/B COWLING INTERIOR AFTER SECTION DELAMINATION AT APPROX 10 O' CLOCK POSITION. REPAIRED PER SRM 51-1-19.Oct 16, 1998 · N801DH · Doug DC873F · Engine Cowling SystemSDR DHL9980156CFairing · crackedAT C-CHECK, LT WING I/B UPPER AREA WING TO FUS FAIRING SUPPORT BRACKET AT FUSE 910 SUPPORT CRACKED. INSTALLED REPAIR PER SM 51-1-21, 2 X 6.5.Oct 16, 1998 · N801DH · Doug DC873F · Wing, Control SurfacesSDR RRXA99767Angle · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO TOP SIDE OF LONGERON 24L AT STA 960 TO 980, Z-18.560, LONG 24L. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 5Oct 15, 1998 · N795FT · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA99750Floor · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 410 TO 470 BL 40L TO 2L. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR PARTS IAW DC-8 SOct 15, 1998 · N795FT · Doug DC873F · Fuselage Floor PanelSDR RRXA99749Floor · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 375 TO 400 BL 20L TO 44L. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-Oct 15, 1998 · N795FT · Doug DC873F · Fuselage Floor PanelSDR RRXA99748Floor · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 480 TO 520 BL 2L TO 10L. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8Oct 15, 1998 · N795FT · Doug DC873F · Fuselage Floor PanelSDR RRXA99747Floor · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 550 TO 590 BL 2L TO 40L. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR PARTS IAW DC-8 SOct 15, 1998 · N795FT · Doug DC873F · Fuselage Floor PanelSDR RRXA99745Floor · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 798 TO 820 BL 6L. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-3, FIOct 15, 1998 · N795FT · Doug DC873F · Fuselage Floor PanelSDR RRXA99744Floor · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 530 TO 540 BL 4R. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR PARTS IAW DC-8 SRM 53-2Oct 15, 1998 · N795FT · Doug DC873F · Fuselage Floor PanelSDR RRXA99743Floor · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 857 BL 44R. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR PARTS IAW DC-8 SRM 53-2-3, FIOct 15, 1998 · N795FT · Doug DC873F · Fuselage Floor PanelSDR RRXA99742Floor · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 857 TO 781 BL 48R. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR PARTS IAW DC-8 SRM 53-Oct 15, 1998 · N795FT · Doug DC873F · Fuselage Floor PanelSDR RRXA99741Floor · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 510 BL 2R. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-3, FIG 10. Oct 15, 1998 · N795FT · Doug DC873F · Fuselage Floor PanelSDR RRXA99740Floor · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 310 BL 4R TO 44R. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53Oct 15, 1998 · N795FT · Doug DC873F · Fuselage Floor PanelSDR RRXA99739Floor · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 320 BL 44R TO 2R. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53Oct 15, 1998 · N795FT · Doug DC873F · Fuselage Floor PanelSDR RRXA99729Floor · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 680 TO 660 BL 4L TO 34L. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR PARTS IAW DC-8 SOct 15, 1998 · N795FT · Doug DC873F · Fuselage Floor PanelSDR DHL9980152CSkin · missingAT C-CHECK, RT WING T/E UPPER AREA STA 120 PIECE OF METAL MISSING ON SKIN NEXT TO NR 1 SPOILER O/B HINGE AREA 2060. CUT OUT DAMAGED AREA AND FABRICATED DOUBLER AND FILLER 1 X 4 PER SRM 51-1-21.Oct 15, 1998 · N801DH · Doug DC873F · Wing, Plate/SkinSDR DHL9980151CBracket · crackedAT C-CHECK, RT WING UPPER AREA WING TO FUS SUPPORT BRACKET STA 640 CRACKED. FABRICATED AND INSTALLED NEW BRACKET PER SRM 51-3-0, 6 X 6.Oct 15, 1998 · N801DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL9980149CStrap · missingAT C-CHECK, AFT CARGO COMPT RT STA 980 TO 1010 O/B STRAP OF SEAT TRACK MISSING SECTION. FABRICATED STRAP PER SRM 51-1-4 AND INSTALLED PER SRM 51-3-0, 1 X 60.Oct 15, 1998 · N801DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL9980147CStrap · damagedAT C-CHECK, AFT CARGO COMPT RT STA 1060 LOWER AREA HAS DAMAGED STRAP. REMOVED DAMAGED STRAP, FABRICATED NEW STRAP AND INSTALLED PER SRM 51-3-0.Oct 15, 1998 · N801DH · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA99761Floor · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1020 TO1060 BL 6R. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 5Oct 14, 1998 · N795FT · Doug DC873F · Fuselage Floor PanelSDR RRXA99760Floor · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1060 BL 0R TO 6R. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53Oct 14, 1998 · N795FT · Doug DC873F · Fuselage Floor PanelSDR RRXA99759Floor · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1140 BL 18R. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLES, DOUBLER, AND FILLER Oct 14, 1998 · N795FT · Doug DC873F · Fuselage Floor PanelSDR RRXA99757Floor · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1400 TO 1420 BL 6L. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAOct 14, 1998 · N795FT · Doug DC873F · Fuselage Floor Panel
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