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 IXXA05SMN133SAngle · crackedDURING ROUTINE C CHECK INSPECTION, RT IB FLAP INTERNAL ANGLE CRACKED 3 INCH, STA XW 129.000. REMOVED CRACKED ANGLE IAW SRM 51-1-21. FABRICATED NEW ANGLE (A EXTRUSION S-1656396) IAW SRM 57-2-0 PAGE 1. CLEANED, TREATED AND PRIMED AREA + NEW ANGLE IAW SRM 51-SDR IXXA05SMN132SLongeron · corrodedDURING ROUTINE C CHECK INSPECTION, MAIN CARGO CMPT.- L-36 CORRODED, STA. 1690.00 - STA. 1700.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 53-2-2 FIG. 4A, EO SEMAN Nº 2005937 DATE 06-22-05. REMOVED CORROSION IAW DC-8 SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAWSDR IXXA05SMN131SLongeron · corrodedDURING ROUTINE C CHECK INSPECTION, MAIN CARGO CMPT.- L-28R CORRODED, STA. 1726.000. REMOVED CORROSION IAW SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PAGE 2. REMOVED CORRODED LONGERON IAW SRM 51-1-20D PAGE 1, DC-8 SRM 51-1-21 PAGE 1. CLEANED, TSDR IXXA05SMN130SFitting · crackedDURING ROUTINE C CHECK INSPECTION, NOSE SECTION FITTING CRACKED 5 INCHES, STA. 8.000 L-33L. REMOVED CRACKED FITTING IAW SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING IAW DWG NR 4645453 (ALCLAD 7075 T6 51), EO SEMAN NR 2005939. PERFORMED HEAT TREATMENT IAW SRMSDR IXXA05SMN129SFitting · crackedDURING ROUTINE C CHECK INSPECTION, NOSE SECTION STA. 8.000 RT SIDE FITTING CRACKED 5 INCHES (L-33R) REMOVED CRACKED FITTING IAW SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING IAW DWG DOUGLAS NR 4645453 (ALCLAD 7075 T6 51), EO SEMAN NR 2005938. PERFORMED HEAT TRESDR IXXA05SMN128SFitting · corrodedDURING ROUTINE C CHECK INSPECTION, MAIN CARGO CMPT. FITTING CORRODED AT STA. 1690.00, L-36 REMOVED CORROSION IAW SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PAGE 21. REMOVED CORRODED FITTING IAW SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING IAWSDR IXXA05SMN127SFitting · corrodedDURING ROUTINE C CHECK INSPECTION, AFT. LWR. CARGO BILGE INTERIOR. NR 3 DOOR HOUSING LWR FITTING CORRODED (INTERNAL STRUCTURE), STA. 1215.000, L-31LREMOVED CORROSION IAW SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PAGE 2P. REMOVED CORRODED FITTISDR IXXA05SMN126SSkin Panel · corrodedDURING ROUTINE C CHECK INSPECTION, EXTERNAL FUS CORRODED, STA. 70.000 STA. 115.000, L-35L - L-35R. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PAGE 1, SRM 53-3-1 FIG. 1 ITEM A, EO NR 2005864 DATE 06-13-05. REMOVED CORROSION IAW SRM 51-1-8 PAGES 17, 18, FOUND OUT OSDR IXXA05SMN125SLongeron · crackedDURING ROUTINE C CHECK INSPECTION, AFT ACCESSORY COMPARTMENT, L -34R CRACKED STA 1690.000. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PAGE 1, SRM 53-5-1 FIG. 7, EO SEMAN NR 2005863 DATE 06-18-05. REMOVED CRACKED LONGERON SEGMENT + EXISTING SPLICES IAW SRM 51-1SDR IXXA05SMN124SFitting · crackedDURING ROUTINE C CHECK INSPECTION, AFT ACCESSORY COMPARTMENT BATHTUB FITTING CRACKED, STA 1690.000 L-34R. REMOVED CRACKED BATHTUB FITTING IAW SRM 51-1-20D PAGE 21. FABRICATED NEW BATHTUB FITTING (ALCLAD 7075 T6 51) IAW DWG 4641324. PERFORMED HEAT TREATMENT IASDR IXXA05SMN123SFitting · crackedDURING ROUTINE C CHECK INSPECTION, AFT ACCESSORY COMPARTMENT BATHTUB FITTING CRACKED, STA 1690.000 L - 30L. REMOVED CRACKED BATHTUB FITTING IAW SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING (ALCLAD 7075 T6 51) IAW DWG 4641324. PERFORMED HEAT TREATMENT IAW SRSDR IXXA05SMN122SFitting · crackedDURING ROUTINE C CHECK INSPECTION, AFT ACCESSORY COMPARTMENT BATHTUB FITTING, CRACKED STA 1690.000 L-34L. REMOVED CRACKED BATHTUB FITTING IAW SRM 51-1-20D PAGE 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW BATHTUB FITTING IAW SRM 51-1-20SDR IXXA05SMN121SFitting · crackedDURING ROUTINE C CHECK INSPECTION, AFT. ACCESSORY COMPARTMENT FITTING CRACKED L-28R, STA 1766.000 REMOVED CRACKED FITTING IAW SRM 51-1-20D PAGE 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PAGE 1. TORQUED IASDR IXXA05SMN120SFitting · corrodedDURING ROUTINE C CHECK INSPECTION, ACND. CMPT. LT FITTING CORRODED STA 70.000, L-31R. REMOVED CORROSION IAW SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PAGE 2P. REMOVED CORRODED FITTING IAW SRM 51-1-20D PAGE 21. CLEANED, TREATED AND PRIMED SDR IXXA05SMN119SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FWD CARGO COMPT, FITTING CRACKED 1 INCH AT STA 220.000 - 240.000 L-31R. REMOVED DAMAGED FITTING IAW SRM 51-1-20D PAGE 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PAGE 1. TSDR IXXA05SMN118SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, LT OB FLAP, NON STANDARD REPAIR, XF 345.000 (UPPER PART) PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PAGE 1, SRM 57-7-1 FIG. 4, TR NR 57-94, EO SEMAN NR 2005856 DATE 06-18-05. REMOVED PLATING WITH IMPROPER REPAIR IAW SRM 51-1-21 SDR IXXA05SMN117SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, LT OB FLAP NON STANDARD REPAIR, XF 304.000 -XF 309.000 (UPPER PART). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PAGE 1, SRM 57-7-1 FIG. 4, TR NR 57-94, EO SEMAN NR 2005854 DATE 06-18-05. REMOVED PLATING WITH IMPROPER REPAIR IAW SSDR IXXA05SMN116SFlap · improperDURING ROUTINE C CHECK INSPECTION, LT OB FLAP L/E REPAIR IMPROPER, XF 333.000 (UPPER PART) PERFORMED MAJOR REPAIR IAW NR 05259 DATE 06-24-05, DWG NR ED 3988, EO NR 2005855 DATE 06-24-05. REMOVED FASTENERS IAW SRM. REMOVED DAMAGED PLATING SEGMENT IAW DWG ED 39SDR IXXA05SMN115SSkin · nickedDURING ROUTINE C CHECK INSP, LT OB FLAP L/E NICKED, XF 226.000 (UPPER PART) PERFORMED MAJOR REPAIR, DWG NR ED 3987 DATE 06-20-05, EO. REMOVED FASTENERS IAW SRM. REMOVED DAMAGED PLATING SEGMENT IAW DWG ED 3987. PERFORMED NDT INSP IAW SPM. NO CRACK, CORROSION FSDR IXXA05SMN114SSkin Panel · dentedDURING C CHECK INSPECTION, LT OTBD FLAP L/E DENTED, XF 213.000 (UPPER PART. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-1-0 PG 1, DC-8 SRM 57-7-1 FIG 4, TR NR 57-94, EO SEMAN NR 2005852 DATE 06-18-05. REMOVED DAMAGED PLATING IAW DC-8 SRM 51-1-21 PG 1, DC-8 SRM 51SDR IXXA05SMN113SSkin · improperDURING ROUTINE C CHECK INSPECTION, LT IB FLAP REPAIR IMPROPER, XF 415.000 (UPPER PART) PERFORMED MAJOR REPAIR IAW SRM 57-2-5 FIG. 1. EO SEMAN NR 2005858 DATE 06-18-05. REMOVED DAMAGED PLATING IAW SRM 57-2-5 FIG. 1(SHEET 1,2). PERFORMED DETAILED VISUAL INSPECTISDR IXXA05SMN112SSkin · improperDURING C CHECK INSPECTION, LT OTBD FLAP L/E UPPER PART NON STANDARD REPAIR, XF 415.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-1-0 PG 1, DC-8 SRM 57-7-1 FIG 4, TR # 57-94, EO SEMAN NR 2005857 DATE 06-18-05. REMOVED PLATING WITH IMPROPER REPAIR IAW DC-8 SRM 5SDR IXXA05SMN111SWing · crackedDURING ROUTINE C CHECK INSPECTION, RT WING UPPER SKIN CRACKED 1INCH, STA. XRS 74. 869, S-10. REMOVED EXISTING REPAIR DOUBLERS SRM 51-1-20D PAGE 21. REMOVED DAMAGED AREA IAW SEMAN DWG ED 3981. PERFORMED NDT INSPECTION IAW SPM PART 06-10-01-001. FABRICATED EXTESDR IXXA05SMN110SSkin · crackedDURING C CHECK INSPECT, RT WING UPPER SKIN HAS 2 CRACKS OF 1" EACH AT XRS 74. 869, S-15 AND S-16. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05280 DATE 07-04-05, SEMAN DWG # ED 3981 DATE 06-29-05, EO SEMAN NR 2005834 DATE 07-04-05. REMOVED EXISTING REPAIR SDR IXXA05SMN109SWing · elongatedDURING C CHECK INSPECT, LT WING, NR 2 STUB WING VANE SLOT HOLE ELONGATED, XS 247.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05270 DATE 06-29-05, SEMAN DWG # 3986 DATE 06-28-05, EO SEMAN # 2005849 DATE 06-29-05. REMOVED DAMAGED AREA IAW SEMAN DWG ED 398SDR IXXA05SMN108SWing · corrodedDURING C CHECK INSPECT, LT WING NR 2 STUB WING UPPER PART CORRODED, XFS 212.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-2-1 FIG 38. TR NR 57-85, EO SEMAN NR 2005848 DATE 06-18-05. REMOVED FASTENERS IAW DC-8 SRM 51-1-21 PG 1, DC-8 SRM 51-1-20D PG 21. REMOVED SDR IXXA05SMN107SSkin · improperDURING ROUTINE C CHECK INSPECTION, LH INBD FLAP UPPER PART SKIN NON STANDARD REPAIR, XW 132.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-1-0 PAGE 1, DC-8 SRM 57-7-1 FIG. 1, EO SEMAN NR 2005851 DATE 06-18-05. REMOVED PLATING WITH IMPROPER REPAIR IAW DC-8 SRM 51SDR IXXA05SMN106SSkin · wornDURING ROUTINE C CHECK INSPECTION, LH INBOARD FLAP UPPER PART SKIN WORN, XW 104.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-1-0 PAGE 1, DC-8 SRM 57-7-1 FIG. 1, EO SEMAN NR 2005850 DATE 06-18-05. REMOVED DAMAGED PLATING IAW DC-8 SRM 51-1-21 PAGE 1. FABRICATED SDR IXXA05SMN105SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FWD CARGO CMPT.- SPLICE FITTING CRACKED 2", STA 440.000 - 460.000 L-31R. REMOVED CRACKED SPLICE FITTING IAW DC-8 SRM 51-1-20D PAGES 21. CLEANED, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8B. INSTALLED SPLICE FITTING IAW DC-8SDR IXXA05SMN104SFitting · crackedDURING ROUTINE C CHECK INSPECTION, AFT LWR CARGO BILGE INTERIOR.- NR 4 DOOR INTERNAL SUPPORT CTR FITTING CRACKED, STA 1420.000. REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-21 PAGES 1 CLEANED, TREATED AND PRIMED AREA DC-8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DSDR IXXA05SMN103SFitting · corrodedDURING ROUTINE C-CHECK INSPECTION, AFT LOWER CARGO COMPT. INTERIOR.- FITTING CORRODED IN NR 3 DOOR HOUSING , STA 1215.000 NEAR TO L-31L. REMOVED CORROSION IAW DC-8 SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0 PAGE 2P. REMOVED CORRODED FITTINSDR IXXA05SMN102SVane · elongatedDURING ROUTINE C-CHECK INSPECTION, LT WING.- VANE SLOT REPAIR HOLE ELONGATED, XW 454.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, SEMAN DWG ED 3982, EO SEMAN 2005835. REMOVED FASTENERS IAW DC-8 SRM 51-1-21 PAGE 1, DC-8 SRM 51-1-20D PAGE 21. TRIMMED OUT SDR IXXA05SMN101SWeb · crackedDURING ROUTINE C CHECK INSPECTION, LT WING T/E WEB UPPER PART CRACKED 1/2, XCW 69.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-2-6 FIG. 15, EO SEMAN NR 2005836 DATE 06-25-05. REMOVED FASTENERS IAW DC-8 SRM 51-1-20D PAGE 21. REMOVED DAMAGED AREA IAW DC-8 SRM 57-SDR IXXA05SMN100SPanel · corrodedDURING ROUTINE C CHECK INSPECTION, LH WING.- SLANT PANEL UPPER PART CORRODED, XW 6.000 PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-2-1 FIG. 37, EO SEMAN Nº 2005847 DATE 06-16-05. REMOVED FASTENERS IAW DC-8 SRM 51-1-21 PAGE 1, DC-8 SRM 51-1-20D PAGE 21. SMOOTHED, PESDR IXXA05SMN99SSkin · crackedDURING C CHECK INSPECT, LT WING, SKIN UPPER PART WITH 02 CRACKS 1", 1/2", XRS 74.000 S-9 - S10. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-2-1 FIG 10, EO SEMAN NR 2005833 DATE 06-14-05. REMOVED DAMAGED AREA IAW DC-8 SRM 57-2-1 FIG 10 (SHEET 3). PERFORMED NDT INSPSDR IXXA05SMN98SLongeron · corrodedDURING C CHECK INSPECT, AFT CARGO CMPT L-36 CORRODED, STA 1540.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 53-2-2 FIG 4A, EO SEMAN NR 2005846 DATE 06-18-05. REMOVED CORROSION IAW DC-8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0 PAGE 2P. REMOVED SDR IXXA05SMN97SFrame · crackedDURING ROUTINE C CHECK INSPECTION, NOSE SECTION, DOUPLER ANTENNA FRAME WITH 02 CRACKS 2" EACH ONE. REMOVED DOUPLER ANTENNA FRAME (CRACKED) IAW DC-8 SRM 51-1-21 PAGE 1. FABRICATED NEW DOUPLER ANTENNA CAP IAW DWG DOUGLAS NR 561601 (ALCLAD 7075 T6 0.125). PERFOSDR IXXA05SMN96SSkin · crackedDURING ROUTINE C CHECK INSPECTION, LT WING NR 5 SPOILER LWR SKIN WITH 02 CRACKS 2", XRS 367.000 - XRS 421.000. REMOVED REPLACED NR 5 SPOILER PANEL ON LT WING XRS 367.000 XRS 421.000 IN ACCORDANCE WITH DC-8B MM 27-61-1 PAGES 201-205.SDR IXXA05SMN94SSkin · crackedDURING C CHECK INSPECTION, RT MLG REMOVE AND INSTALL CTR DOOR (LWR SKIN CRACKED). REMOVED AND REPLACED CTR MAIN PANEL ON RT MLG IN ACCORDANCE WITH DC-8 MM 32-12-1 PAGE 401. FOR OPS CHECK SEE J/C 74204.SDR IXXA05SMN95SSkin · delaminatedDURING ROUTINE C CHECK INSPECTION, LT LWR WING T/E NR 546 ACCESS DOOR EXTERNAL SKIN DELAMINATED. REMOVED AND REPLACED EXTERNAL PANEL IN LT LWR WING T/E NR 546 ACCESS DOOR IN ACCORDANCE WITH DPS 367-15.SDR IXXA05SMN93SSkin · delaminatedDURING ROUTINE C CHECK INSPECTION, RT WING, T/E LWR PANEL EXTERNAL , INTERNAL SKIN DELAMINATED, XW 0.000 - XW 90.000. REMOVED AND REPLACED PANEL ON RT WING T/E, XW 0.000 XW 90.000 IAW DC-8 SRM 51-3-0 PAGE 1, DC-8 SRM 51-1-21 PAGE 14. TORQUED IAW DC-8 SRM 51-SDR UPS05844740Skin · corrodedSKIN BULGING AT SEAM APPROX 6 FT AFT OF NOSE GEAR LEFT SIDE OF FX MARKED. DAMAGED FINGER 5 INOP FOUND CORRODED. REMOVED DAMAGE, INSPECTED AREA TO INSTALL REPAIR. FABRICATED NEW FINGER DOUBLER SECTION IAW PRELIM EO DC8-5330-22410-A. INSTALLED 80 PERCENT SDR UPS05844805Intercostal · corrodedINSPECTION TYPE:C-2, INTERCOSTAL AT STA 980 HAS CORROSION. CORROSION OUT OF LIMITS PER SRM 53-2-0. FABRICATED AND INSTALLED INTERCOSTAL IAW SRM 51-1-21, AND SRM 51-1-20D.SDR IXXA05SMN62SSkin · damagedDURING ROUTINE C CHECK INSPECTION, RT AFT FUSELAGE STA FS 1346.000, L-35.5R. ONLY 2 ROWS OF RIVETS IN OLD ANTENNA DOUBLER ADD THIRD ROWS OF RIVETS UTILIZING SRM RIVET SPACING OR UPGRADE REPAIR DOUBLER, STA 1346.000 L-35.5R (REF 822BX-R14). PERFORMED MAJOR REPSDR IXXA05SMN92SSkin · delaminatedDURING ROUTINE C CHECK INSPECTION, RT WING UPPER T/E PANEL EXTERNAL SKIN DELAMINATED, XA 613.000 - XA 681.000. REMOVED AND REPLACED UPPER T/E PANEL ON RT WING XA 613.000 XA 681.000 IAW DC-8 SRM 51-3-0, DC-8 SRM 51-1-21 PAGE 1. TORQUED IAW DC-8 SRM 51-3-1.SDR IXXA05SMN91SSkin · damagedDURING ROUTINE C CHECK INSPECTION, LT AILERON REMOVE AND REINSTALL TRIM TAB (UPPER SKIN HAS HOLES). REMOVED TRIM TAB FROM LT ALEIRON IAW DC-8 MM 27-13-1 PAGES 201-203. INSTALLED TRIM TAB ON LT AILERON IAW DC-8 MM 27-13-1 PAGES 203-208 (REPAIRED CONDITION). SDR IXXA05SMN90SSkin · delaminatedDURING ROUTINE C-CHECK INSPECTION, RT ELEVATOR. REMOVE AND REINSTALL GEARED TAB (EXTERNAL SKIN DELAMINATED). REMOVED GEARED TAB FROM RT ELEVATOR IAW MM 27-30-3. INSTALLED GEARED TAB (OVERHAULED CONDITION) IAW MM 27-30-3. FOR OPS CHECK SEE NR 0818.SDR IXXA05SMN89SFitting · corrodedDURING C-CHECK INSPECT, MLG WW FRAME FITTING CORRODED, STA 940.000, L-24. PERFORMED MAJOR REPAIR IAW DC-8 SRM 53-2-0, EO SEMAN NR 2005844. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0. REMOVED CORRODED FRAME FITTING IAW DC-SDR IXXA05SMN88SFitting · crackedDURING ROUTINE C CHECK INSPECTION, MLG W/W FITTING CRACKED 4", STA 857.725 , RBL 46". 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-8 SRM 51-1-20D PAGE 9. TORQUED SDR IXXA05SMN87SStructure · crackedDURING C CHECK INSPECT, MLG W/W L-24 CRACKED 2", STA 980.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 53-2-2 FIG 5 TR NR 53-123 DATE 05-15-01, EO SEMAN NR 2005831 DATE 06-16-05. REMOVED FASTENERS IAW DC-8 SRM 51-1-20D PAGE 21. PERFORMED SLOP HOLE ON CRACK END I
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