Douglas DC-8-71F
Service difficulty reports · 8,938
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 = '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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR UPS05844415Strap · corrodedCORROSION ON SKIN SPLICE STRAP STA 450 LONG 30R. ENGINEERING SUBMITTED PROPOSAL TO BOEING FOR REPAIR. REMOVED ALL FASTENERS IN AREA OF CORROSION WS 05577521. REMOVED CORROSION AS NEEDED FOR REPAIR REF N/R 680150.SDR IXXA05SMN53SCargo Track · corrodedDURING ROUTINE C-CHECK INSPECTION, AFT CARGO BAY LT TRACK STA 980.000 - 1160.000 CORRODED. REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-3 FIG 12. REMOVED CORRODED TRACK IAW DC-8 SRM 51-3-0 PAGE 1. CLEANED, SDR IXXA05SMN52SSkin · dentedDURING ROUTINE C-CHECK INSPECTION, EVALUATE FOR REPAIR DENT OF RT HORIZ STAB. PERFORMED MAJOR REPAIR IAW DC-8 SRM 55-2-1 FIG 4. FABRICATED REPAIR DOUBLER IAW DC-8 SRM 55-2-1 FIG 4. CLEANED, TREATED AND PRIMED REPAIR DOUBLE INTERNAL PART IAW DC-8 SRM 51-1-8BSDR IXXA05SMN24SFitting · crackedDURING ROUTINE C-CHECK INSPECTION, MAIN CARGO BAY STA 781.000 L-14R AFT FITTING CRACKED 1 IN STA 781.000. REMOVED CRACKED FITTING IAW DC-8 SRM 53-1-0 PAGE 1, DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING IAW DWG NR 3779970. PERFORMED NDT INSPECTION IAW SDR IXXA05SMN23SAttach Fitting · crackedMAIN CARGO BAY FWD SERVICE DOOR INTERNAL JAMB FITTING CRACKED, STA 474.000 L-11R. REMOVED CRACKED FITTING IAW DC-8 SRM 53-1-0 PAGE 1, DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING IAW DWG NR 9755586. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02 TSDR IXXA05SMN22SAttach Fitting · crackedMAIN CARGO BAY RT WING SECTION INTERIOR FITTING CRACKED, STA 781.000 - RBL 23. REMOVED CRACKED FITTING IAW DC-8 SRM 53-1-0 PAGE 1, DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING IAW DWG NR 4646547. PERFORMED HEAT TREATMENT IAW DC-8 SRM 51-1-1 PAGES 1, 1SDR IXXA05SMN21SAttach Fitting · crackedMAIN CARGO BAY RT WING CTR SECTION FITTING CRACKED, STA 759.000 RBL 23. REMOVED CRACKED FITTING IAW DC-8 SRM 53-1-0 PAGE 1, DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING IAW DWG NR 4646547. PERFORMED HEAT TREATMENT IAW DC-8 SRM 51-1-1 PAGES 1, 13, 17. SDR IXXA05SMN20SAttach Fitting · crackedMAIN CARGO BAY STA 680.000 L-11L AFT FITTING CRACKED. REMOVED CRACKED FITTING IAW DC-8 SRM 53-1-0 PAGE 1, DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING IAW DWG NR 4751625. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02 TO 07. CLEANED, TREATED AND PRISDR IXXA05SMN19SAttach Fitting · crackedMAIN CARGO BAY, STA 857.000 L-19L AFT FITTING CRACKED. REMOVED CRACKED FITTING IAW DC-8 SRM 53-1-0 PAGE 1, DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING IAW DWG NR 4750423. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02 TO 07. CLEANED, TREATED AND SDR IXXA05SMN18STee Fitting · crackedMAIN CARGO BAY FWD TYPE I DOOR INNER JAMB FITTING CRACKED, STA 384.000 L-11 AND L-12R. REMOVED DAMAGED TEE IAW DC-8 SRM 53-1-0, DC-89 SRM 51-1-20D PAGE 21. FABRICATED NEW TEE IAW DGW 9755815. PERFORMED NDT INSPECTION TO TEE IAW NDT SPM PART 08-00-02/07. CLSDR IXXA05SMN17SRib · crackedLT NR 1 STUB WING FORMER CRACKED, STA XFS 526.000. PERFORMED MAJOR REPAIR IAW DWG 9753247. REMOVED CRACKED RIB IAW DC-8 SRM 54-1-0 PAGE 1, DC-8 SRM 51-1-21 PAGE 1, DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW RIB IAW DWG 9753297, DC-8 SRM. DPS 369-4 REV AM. PESDR IXXA05SMN34SAttach Fitting · corrodedMAIN CARGO BAY INTERNAL FUSELAGE FITTING CORRODED, STA 41520.000 L-21L. REMOVED CORROSION IAW DC-8 SRM 51-1-8 PAGE 17-18. FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0 PAGE 2P. REMOVED CORRODED FITTING IAW DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING IAW DWSDR IXXA05SMN33SAttach Fitting · crackedMAIN CARGO BAY END FITTING CRACKED, STA 680.000, L-4R. REMOVED CRACKED FITTING IAW DC-8 SRM 53-1-0 PAGE 1, DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING IAW DWG NR 3779762. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02 TO 07. CLEANED, TREATED AND SDR IXXA05SMN32SAttach Fitting · corrodedMAIN CARGO BAY INTERNAL FUSELAGE FITTING CORRODED, STA 1614.000 L-21L. REMOVED CORROSION IAW DC-8 SRM 51-1-8 PAGE 17-18. FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0 PAGE 2P. REMOVED CORRODED FITTING IAW DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING IAW DWGSDR IXXA05SMN31SFitting · crackedMAIN CARGO BAY FITTING INTERNAL SKIN CRACKED, STA 700.000 L-21 - L-22R. REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING IAW DWG NR 3616948. PERFORMED HEAT TREATMENT IAW DC-8 SRM 51-1-1 PAGES 1, 13, 17. PERFORMED NDT INSPECTIONSDR IXXA05SMN30SFitting · crackedNOSE SECTION RT TUNNEL FITTING CRACKED STA 8.000. REMOVED CRACKED FITTING IAW DC-8 SRM 53-1-0 PAGE 1, DC-8 SRM 51-3-0 PAGE 1. FABRICATED NEW FITTING IAW DWG NR 4640117. PERFORMED HEAT TREATMENT IAW DC-8 SRM 51-1-1 PAGES 1, 13, 17. PERFORMED NDT INSPECTIONSDR IXXA05SMN29SAttach Fitting · crackedLT HORIZ STAB FAIRING SUPPORT AFT FITTING CRACKED STA 1870.000. REMOVED CRACKED FITTING IAW DC-8 SRM 51-3-0 PAGE 1. FABRICATED NEW FITTING IAW DWG NR 3702408. PERFORMED HEAT TREATMENT IAW DC-8 SRM 51-1-1 PAGES 1, 13, 17. PERFORMED NDT INSPECTION IAW NDT SSDR IXXA05SMN28SAttach Fitting · crackedLT HORIZONTAL STABILIZER FAIRING SUPPORT AFT FITTING CRACKED STA 1880.000 LT. REMOVED CRACKED FITTING IAW DC-8 SRM. FABRICATED NEW FITTING IAW DWG NR 3702464. PERFORMED HEAT TREATMENT IAW DC-8 SRM. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02 TO 07. SDR IXXA05SMN27SSkin · crackedRT WING CTR L/E LOWER OUTER PLATING CRACKED. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, SEMAN DWG ED-3944. REMOVED FASTENERS FROM REPAIR AREA IAW DC-8 SRM. REMOVED DAMAGED AREA IAW SEMAN DWG ED-3944. PERFORMED NDT INSPECTION IAW DC-8 NDT SPM PART 06-10-01-SDR IXXA05SMN26SSkin · crackedRT WING CTR L/E OUTER PLATING UPPER SURFACE CRACKED STA. XFS 430.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, SEMAN DWG ED-3937. REMOVED FASTENERS IAW DC-8 SRM. REMOVED DAMAGED AREA IAW SEMAN ED-3937. PERFORMED NDT INSPECTION IAW NDT SPM PART 06-10-01-001SDR IXXA05SMN25SDoubler · crackedRT WING CTR L/E INTERNAL DOUBLER CRACKED. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 AND SEMAN DWG ED-3953. REMOVED FASTENERS FROM REPAIR AREA IAW DC-8 SRM. REMOVED DAMAGED AREA IAW SEMAN ED-3953. PERFORMED NDT INSPECTION TO AREA IAW NDT SPM PART 06-10-01-SDR IXXA05SMN43SSkin · crackedDURING ROUTINE C-CHECK INSPECTION, CARGO DOOR EXTERNAL SKIN HAS 0.25 IN. CRACKS ON EDGES STA 1160.000 TO STA 1220.000, L-31R TO L-31L. PERFORMED MAJOR REPAIR IAW DC-8 SRM 52-1-0 PAGE 1, DC-8 SRM 52-4-1 FIG 1. REMOVED EXISTING DAMAGED SKIN IAW DC-8 SRM 51-1-21SDR IXXA05SMN42SLongeron · corrodedDURING ROUTINE C-CHECK INSPECTION, AFT CARGO COMPARTMENT CORROSION ON LONGERON 36 BETWEEN STA FS 1380.000 AND 1420.000. PERFORMED BLEND OUT 0.015, MATERIAL THICKNESS 0.150, REMAINING MATERIAL 0.135 ON LWR RADIO AREA AND BLEND OUT 0.011, MATERIAL THICKNESS 0.1SDR IXXA05SMN41SSkin · corrodedFUSELAGE SKIN CORRODED, STA 722.000 781.000, L-35L TO L-35R. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05163 DATE 04-28-05; SEMAN DWG ED-3961 DATED 04-20-05. REMOVED DAMAGED PLATING SEGMENT IAW SEMAN DWG ED-3961. PERFORMED NDT INSPECTION IAW DC-8 NDT SPSDR IXXA05SMN40SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, FUSELAGE L-35L CORRODED, STA 690.000 STA 781.000. REMOVED LEVEL I CORROSION IAW DC-8 SRM 51-1-8 PAGES 17-18. PERFORMED BLEND OUT 0.003”. MATERIAL THICKNESS 0.160”, REMAINING MATERIAL 0.157 FOUND WITHIN ALLOWABLE LIMITS IAWSDR IXXA05SMN39SSkin · corrodedFUSELAGE SKIN CORRODED STA 700.00 STA 708.000 L-32L. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05163 DATE 04-28-05; SEMAN DWG ED-3961 DATED 04-20-05. REMOVED DAMAGED PLATING SEGMENT IAW SEMAN DWG ED-3961. PERFORMED NDT INSPECTION IAW DC-8 NDT SPM PART 0SDR IXXA05SMN38SSkin · corrodedFUSELAGE EXTERIOR SKIN LOCAL CORROSION, STA 700.000 STA 708.000, L-32R. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05163 DATE 04-28-05; SEMAN DWG ED-3961 DATED 04-20-05. REMOVED DAMAGED PLATING SEGMENT IAW SEMAN DWG ED-3961. PERFORMED NDT INSPECTION IAW SDR IXXA05SMN37SFitting · brokenDURING ROUTINE C-CHECK INSPECTION, FWD CARGO COMPARTMENT FITTING BROKEN, 70.000 L-31L. REMOVED BROKEN FITTING IAW DC-8 SRM 51-120D PAGE 21. CLEANED, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8B. INSTALLED NEW FITTING DC-8 SRM 51-1-20D PAGE 9. TORQUED IAW DSDR IXXA05SMN36SSkin · corrodedEXT FS RT FUSELAGE FWD CTR SECTION PLATING CORRODED AND HOLES ELONGATED, STA 260.000 L-3. MAJOR REPAIR IAW FAA 8110-3 NR 05168 AND SEMAN DWG ED-3951. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0. REMOVED EXISTING DOUBLER DC-SDR IXXA05SMN35SSkin · corrodedEXT FUSELAGE RT FUSELAGE CTR SECTION PLATING TCAS DOUBLER MOD CORRODED. ELONGATED HOLES AND DENT DAMAGE (STA 220.000 - 260.000, L-29R TO L-31R). PERFORMED MAJOR REPAIR IAW FAA 8110-3 NR 05168, SEMAN DWG ED-3951. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FOUND OSDR IXXA05SMN16SFitting · crackedDURING ROUTINE C-CHECK INSPECTION, FWD CARGO BAY FITTING CRACKED 1 IN., STA 240.000. L-31R. REMOVED CRACKED FITTING IAW DC-8 SRM 53-1-0 PAGE 1. CLEANED, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D PAGE 9. TORQUSDR IXXA05SMN14SSkin · crackedRT WING, LE LWR SKIN WITH 03 CRACKS , XW 422.750. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3. REMOVED EXISTING REPAIR DOUBLER IAW SEMAN DWG ED-3950, DC-8 SRM. REMOVED DAMAGED AREA IAW SEMAN DWG ED-3950. PERFORMED NDT INSPECTION IAW DC-8 NDT SPM PART 06-10-SDR IXXA05SMN13SSkin · crackedRT WING INBD AILERON UPPER SKIN CRACKED 0.5 IN., STA. XA 610.000. MAJOR REPAIR IAW DC-8 SRM 57-1-0 PAGE 1 IAW DC-8 SRM 57-8-1 FIG 1, DWG DACO 5705334. REMOVED DAMAGED PANEL IAW DC-8 SRM 57-1-0 PAGE 1, DC-8 SRM 51-1-21 PAGE 1. REMOVED DAMAGED AREA IAW DC-8 SSDR IXXA05SMN12SMount · crackedDURING ROUTINE C-CHECK INSPECTION, 2 CRACKS ON DOPPLER ANTENNA FRAME, STA -99.000 TO STA -131.000. REMOVED CRACKED CAP IAW DC-8 SRM 53-1-0 PAGE 1, DC-8 SRM 51-1-21 PAGE 1, IAW DWG 5616101. PERFORMED HEAT TREATMENT IAW DC-8 SRM 51-1-1 PAGES 1, 13, 17. CLEASDR IXXA05SMN11SFitting · crackedDURING ROUTINE C-CHECK INSPECTION, RT HORIZONTAL STABILIZER FITTING CRACKED 1 IN., XFS 47.000 - XFS 60.000 (LWR PART). REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-20D PAGE 21. CLEANED, TREATED AND PRIMED IAW DC-8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC-8 SRSDR IXXA05SMN10SFitting · crackedDURING ROUTINE C-CHECK INSPECTION, LT HORIZONTAL STABILIZER FITTING CRACKED 1 IN., XFS 47.000 - XFS 60.000 (LWR PART). REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-20D PAGE 21. CLEANED, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC-SDR IXXA05SMN09SFitting · crackedDURING ROUTINE C-CHECK INSPECTION, AFT CARGO COMPARTMENT SPLICE FITTING CRACKED 3 IN., STA 1040.000, STA 1060.00, L-31R. REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING IAW DWG 3750330. PERFORMED NDT INSPECTION TO FITTING IAW NSDR IXXA05SMN08SFitting · crackedDURING ROUTINE C-CHECK INSPECTION, AFT CARGO COMPT SPLICE FITTING CRACKED 9 IN., L-31L , STA 1040.00 - STA 1060.000. REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING IAW DWG 3750257. PERFORMED NDT INSPECTION TO FITTING IAW NDT SSDR IXXA05SMN55SFitting · crackedDURING ROUTINE C-CHECK INSPECTION, FWD CARGO COMPT - INTERIOR SPLICE FITTING CRACKED, STA 440.000 - STA 460.00, L-34L 3. REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING (ALCLAD 7075 T6 51) IAW DWG 3750330. PERFORMED NDT INSPECTSDR IXXA05Fitting · crackedDURING ROUTINE C-CHECK INSPECTION, RT WING L/E INBOARD STUB WING UPPER SURFACE SCREWS OXIDIZED, XW 257.000. REMOVED OXIDIZED SCREWS IAW DC-8 SRM 51-3-0 PAGE 1. INSTALLED NEW SCREWS ON RT L/E INBOARD STUD WING UPPER SURFACE, XW 257.000 IAW DC-8 SRM 51-3-0 PAGSDR IXXA05SMN07SFitting · crackedDURING ROUTINE C-CHECK INSPECTION, FWD CARGO COMPT INTERIOR SPLICE FITTING CRACKED 3 IN., STA 440.000 - STA 460.000, L-31R. REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING IAW DWG 3750257. PERFORMED NDT INSPECTION TO FITTING IASDR IXXA05SMN05SFitting · crackedDURING ROUTINE C-CHECK INSPECTION, FWD CARGO COMPARTMENT INTERIOR SPLICE FITTING CRACKED 8 IN., STA 440.000 - STA 460.000 , L-31L. REMOVED CRACKED FITTING IAW DC-8 SRM 53-1-0 PAGE 1, DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING IAW DWG 3750257. PERFORMSDR IXXA05SMN03SFitting · crackedDURING ROUTINE C-CHECK INSP, FWD CARGO COMPARTMENT INTERIOR, SPLICE FITTING CRACKED 3 IN, STA 440.000 - STA 460.000 L-35L. REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING IAW DWG 3750330. PERFORMED NDT INSPECTION TO FITTING IAWSDR IXXA05SMN01SScrew · corrodedDURING ROUTINE C CHECK INSPECTION, RT WING, L/E INBD STUB WING UPPER SURFACE SCREWS OXIDIZED, XW 257.000. REMOVED OXIDIZED SCREWS IAW DC-8 SRM 51-3-0 PAGE 1. INSTALLED NEW SCREWS ON RT L/E INBD STUD WING UPPER SURFACE, XW 257.000 IAW DC-8 SRM 51-3-0 PAGE 1. SDR IXXA05SMN02SFitting · crackedDURING ROUTINE C-CHECK INSPECTION, FWD CARGO COMPT INTERIOR. SPLICE FITTING CRACKED, STA 600.00 - STA 620.000, L-31R. REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING (ALCLAD 7075 T6 51) IAW DWG 3750257. PERFORMED NDT INSPECTIOSDR IXXA05SMN055SFitting · crackedDURING ROUTINE C-CHECK INSPECTION, FWD CARGO COMPT - INTERIOR SPLICE FITTING CRACKED, STA 440.000 - STA 460.00, L-34L 3. REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING (ALCLAD 7075 T6 51) IAW DWG 3750330. PERFORMED NDT INSPECTSDR IXXA05SMN04SFitting · cockedDURING ROUTINE C-CHECK INSPECTION, FWD CARGO COMPT - INTERIOR SPLICE FITTING CRACKED, STA 440.000 - STA 460.00, L-34L 3. REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING (ALCLAD 7075 T6 51) IAW DWG 3750330. PERFORMED NDT INSPECTSDR UPS05844417Skin · corrodedINSPECTION TYPE:SP COMPLY WITH D 301309 REGARDING FUSELAGE SKIN CORROSION AT E/E DOOR STA 35. CUT OUT DAMAGED SKIN, FABRICATED AND INSTALLED REPAIR IAW EO DC8-5330- 22128-A AND SAA SK 708-911.SDR UPS05844380Skin · corrodedFUSELAGE SKIN DAMAGE RT JUST OUTBOARD OF FWD EQUIPMENT CENTER DOOR MARKED. REMOVED DAMAGED SKIN IN CORRODED AREA DIM APPX 2.9 X 2.5 INCHES. REMOVED ADDITIONAL DAMAGED SKIN APPROX 10 X 9 INCHES TOTAL UNABLE TO CLEAN UP ALL OF UNDERLYING CORROSION AT THIS TIMESDR IXXA0500158SSpar Cap · crackedDURING A ROUTINE C-CHECK INSPECTION FOUND RT WING UPPER FRONT SPAR CAP STRUCTURE HAS CRACK DAMAGE BETWEEN STA XFS -6 CAP. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS. REMOVED CORROSION FROM SLANT PANEL UPPER CAP AND FOUND OUT OF LIMITS. CLEANED, TREATED
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