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 DHL9980125CSeat Track · wornAT C-CHECK, SEAT TRACK NR 4 PLUG WORN BETWEEN STA 326 TO 329. FABRICATED AND REPLACED SEAT TRACK PLUGS PER SRM 53-2-3.Oct 14, 1998 · N801DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL9980124CSeat Track · damagedAT C-CHECK, SEAT TRACK NR 4 PLUG ELONGATED BETWEEN STA 409 TO 420. REMOVED, FABRICATED AND INSTALLED NEW SECTION PER SRM 53-2-3.Oct 14, 1998 · N801DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL9980123CSeat Track · damagedAT C-CHECK, SEAT TRACK NR 3 ELONGATED STA 1310. REMOVED AND REPLACED DAMAGED SECTION PER SRM 53-2-3.Oct 14, 1998 · N801DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA99766Floor · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1400 TO 1440 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 Oct 13, 1998 · N795FT · Doug DC873F · Fuselage Floor PanelSDR RRXA99765Floor · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1500 TO 1580 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-Oct 13, 1998 · N795FT · Doug DC873F · Fuselage Floor PanelSDR RRXA99764Floor · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1500 BL 0 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 AND FILLER IAW DOct 13, 1998 · N795FT · Doug DC873F · Fuselage Floor PanelSDR RRXA99763Floor · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1520 BL 30R. 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 IAW DC-8 Oct 13, 1998 · N795FT · Doug DC873F · Fuselage Floor PanelSDR RRXA99762Floor · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1500 BL 0 TO 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 IAW DOct 13, 1998 · N795FT · Doug DC873F · Fuselage Floor PanelSDR RRXA99758Floor · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1400 TO 1420 BL 26R. 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 13, 1998 · N795FT · Doug DC873F · Fuselage Floor PanelSDR RRXA99753Floor · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1480 BL 24R. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. BLEND OUT WITHIN LIMITS. (CORROSION DAMAGE RECORDED IN EWA Oct 13, 1998 · N795FT · Doug DC873F · Fuselage Floor PanelSDR RRXA99752Floor · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1560 TO 1580 BL O TO 6R. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR PART IAW DC-8 SROct 13, 1998 · N795FT · Doug DC873F · Fuselage Floor PanelSDR RRXA99714Floor · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1540 BL 0. 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, FOct 13, 1998 · N795FT · Doug DC873F · Fuselage Floor PanelSDR RRXA99656Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 280 AND LONGERON 32 LEFT TO 35 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-2-2. (COROct 13, 1998 · N602AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA99653Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING BETWEEN STA 200 TO STA 280 AND LONGERONS 28 LEFT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DAC DWG 3755822. Oct 13, 1998 · N602AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA99643Longeron · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 33 RIGHT BETWEEN STA 8 TO STA 70, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR SPLICE IAW DC-8 SRM 53-2-2. (CORROSION DAOct 13, 1998 · N602AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA99642Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 280 AND LONGERON 29 LEFT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-2-0 FIGURE 1F. (CORROSOct 13, 1998 · N602AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA99627Pressure Panel · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO PRESSURE PANEL BETWEEN STA 950 TO STA 970 AND LONGERON 21 LEFT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVE TIMCOct 13, 1998 · N602AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA99647Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO 2 EACH FITTINGS AT STA 280 AND LONGERON 33 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTINGS IAW DC-8 SRM 53-2-0 FIGURE 1Oct 12, 1998 · N602AL · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS98827922Skin · corrodedINSPECTION TYPE-N/A, FOUND HI-LOK PULLED THROUGH SKIN AT LOWER BELLY NEAR PIT 33 DOOR. ALSO, FOUND 12 X 20 AREA OF CORRISION IN AREA AS ABOVE. REPAIRED AREA BY REMOVING AND REPLACING SKIN PER EO DC8-5330-10798-A.Oct 11, 1998 · N866UP · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL9980119CSkin · dentedAT C-CHECK, RT WING T/E UPPER I/B AREA STA 19 HAS DENTS. REMOVED AND REPAIRED DENTED PANEL PER SRM 51-1-21.Oct 11, 1998 · N801DH · Doug DC873F · Wing, Plate/SkinSDR DHL9980118CSkin · delaminatedAT C-CHECK, RT WING T/E UPPER I/B AREA AT STA 19 AFT T/E PANEL DELAMINATED. REMOVED AND REPAIRED PANEL AND REINSTALLED PER SRM 51-1-8.Oct 11, 1998 · N801DH · Doug DC873F · Trailing Edge FlapsSDR DHL9980117CSkin · delaminatedAT C-CHECK, RT WING T/E UPPER AREA NR 5 SPOILER PANEL DELAMINATED. REMOVED, REPAIRED AND REINSTALLED PANEL.Oct 11, 1998 · N801DH · Doug DC873F · SpoilersSDR DHL9980116CSkin · damagedAT C-CHECK, RT WING UPPER T/E AREA STA 535 UPPER PANEL TEMPORARY REPAIR. REMOVED, REPAIRED AND INSTALLED PER SRM 51-1-24.Oct 11, 1998 · N801DH · Doug DC873F · Wing, Plate/SkinSDR DHL9980115CSkin · delaminatedAT C-CHECK, RT WING UPPER T/E AREA STA 624 DELAMINATED. REMOVED, REPAIRED AND REINSTALLED PER SRM 51-1-21.Oct 11, 1998 · N801DH · Doug DC873F · Wing, Plate/SkinSDR DHL9980113CSkin · delaminatedAT C-CHECK, RT WING T/E SPOILER PANEL DELAMINATED. REMOVED AND REPLACED SPOILER PER MM 27-61-1.Oct 11, 1998 · N801DH · Doug DC873F · SpoilersSDR DHL9980112CVane · delaminatedAT C-CHECK, RT WING NR 4 VANE FLAP DELAMINATED. REMOVED AND REPLACED VANE PER MM 27-51-14.Oct 11, 1998 · N801DH · Doug DC873F · Trailing Edge FlapsSDR DHL9980111CSkin · delaminatedAT C-CHECK, RT WING T/E LOWER AREA STA 120 FUEL CHUTE PANEL DELAMINATED. REPAIRED AND REINSTALLED PER SRM 51-1-21.Oct 11, 1998 · N801DH · Doug DC873F · Wing, Plate/SkinSDR DHL9980110CSkin · delaminatedAT C-CHECK, RT WING T/E LOWER AREA STA 120 DELAMINATED. REMOVED, REPAIRED AND REINSTALLED PER SRM 51-1-8.Oct 11, 1998 · N801DH · Doug DC873F · Wing, Plate/SkinSDR DHL9980106CSkin · delaminatedAT C-CHECK, LEFT WING T/E LOWER AREA PANEL STA 178 CRACKED. REMOVED, REPAIRED AND REINSTALLED PER SRM 51-1-8.Oct 11, 1998 · N801DH · Doug DC873F · Wing, Plate/SkinSDR DHL9980105CSkin · delaminatedAT C-CHECK, LEFT WING T/W LOWER AREA AT STA 554 PANEL DELAMINATED. REMOVED, REPAIRED AND REINSTALLED PER SRM 51-1-8.Oct 11, 1998 · N801DH · Doug DC873F · Wing, Plate/SkinSDR DHL9980104CPanel · delaminatedAT C CHECK, LT WING T/E LOWER AREA AT STA 519 ACCESS PANEL DELAMINATED. REMOVED, REPAIRED AND REINSTALLED PER SRM 51-1-21.Oct 11, 1998 · N801DH · Doug DC873F · Wing, Plate/SkinSDR DHL9980103CTrim Tab · delaminatedAT C-CHECK, LT WING INBOARD AILERON TRIM TAB PANEL DELAMINATED. REMOVED, REPAIRED AND REINSTALLED PER MM 27-31-0.Oct 11, 1998 · N801DH · Doug DC873F · Aileron TabsSDR DHL9980102CSkin · delaminatedAT C-CHECK, LT WING UPPER I/B AREA AT STA 19 FWD T/E PANEL DELAMINATED. REMOVED AND REPAIRED PANEL, INSTALLED PER SRM 51-1-24.Oct 11, 1998 · N801DH · Doug DC873F · Wing, Plate/SkinSDR DHL9980101CHardware · wornAT C-CHECK, LT WING T/E UPPER AREA NR 5 SPOILER PANEL PRESENTS PLAY AT ATTACH POINTS. REMOVED AND REPLACED WORN HARDWARE PER MM 27-61-1.Oct 11, 1998 · N801DH · Doug DC873F · Drag Control SystemSDR RRXA99657Frame · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FRAME BETWEEN STA 1150 TO STA 1160 AND BETWEEN LONGERONS 24 LEFT TO 25 LEFT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER Oct 8, 1998 · N602AL · Doug DC873F · Fuselage Main, FrameSDR RRXA99637Floor · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FLOOR PANEL AT STA 1664 AND BL 10 LEFT, 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 FIGURE 10. (CORROSION DAOct 8, 1998 · N602AL · Doug DC873F · Fuselage Floor PanelSDR RRXA99636Frame · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FRAME AT STA 1660 BETWEEN LONGERONS 29 LEFT TO 34 LEFT, 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 53-2-0 FIGURE 1FOct 8, 1998 · N602AL · Doug DC873F · Fuselage Main, FrameSDR RRXA99635Intercostal · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA1720 AND BL 12 LEFT, 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 53-2-0. (CORROSION DAMAGE RECOct 8, 1998 · N602AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA98439Harness · wornNR 2 ENG EGT GAUGE VERY ERRATIC BOTH THE DIGITAL AND ANILOG AT THE SAME TIME SECURED ENG NR 2 PER QRH. REMOVED AND REPLACED LT AND RT EGT HARNESS ON NR 2 ENG EGT IND NORMAL. OPS CK GOOD ON GRD RUN.Oct 8, 1998 · N795FT · Doug DC873F · Engine EGT/TIT Indicating SystemSDR RRXA99660Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 270 AND LONGERON 36, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 51-3-2. (CORROSION DAMAGE RECOct 6, 1998 · N602AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA99659Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 280 AND LONGERON 30 LEFT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DAC DWG 3755822. (CORROSION DAMAGOct 6, 1998 · N602AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA99658Frame · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO DOOR JAMB FRAME WEB AT STA 238, BL 78 LEFT AND WL -3, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FRAME WEB IAW DAC DWG 5772786. (COct 6, 1998 · N602AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA99654Longeron · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 36 BETWEEN STA 190 TO STA 375, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED LONGERON IAW DC-8 SRM 51-3-2. (CORROSION DAMAGE RECORDED IN EWA COOct 6, 1998 · N602AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA99650Skin · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO EXTERNAL SKIN PANEL BETWEEN STA 190 TO STA 440 AND BETWEEN LONGERONS 31 LEFT TO 31 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND INSTALLED NEW SOct 6, 1998 · N602AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA99649Angle · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO CROSS SLIDE CARGO DOOR, ATTACHMENT ANGLE AT STA 340 AND LONGERON 34 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DAOct 6, 1998 · N602AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA99646Skin · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO EXTERNAL SKIN PANEL BETWEEN STA 100 TO STA 110 AND BETWEEN LONGERONS 26 RIGHT TO 27 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NOct 6, 1998 · N602AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA99644Longeron · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 33 RIGHT AND FITTING AT STA 8, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-2-0 FIGURE 1F. (CORROSIOct 6, 1998 · N602AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA99641Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 280 AND LONGERON 34 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-2-0. (CORROSION DAMAGOct 6, 1998 · N602AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA99640Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING BETWEEN STA 1525 TO STA 1530 AND LONGERON 31 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-2-0.Oct 6, 1998 · N602AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA99639Floorbeam · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FLOORBEAM AT STA 1000 AND BL 23 LEFT, 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 53-2-0. (CORROSION DAMAGEOct 6, 1998 · N602AL · Doug DC873F · Fuselage Main, Floor Beam
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