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.
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
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 UPS01837114Rib · crackedINSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 316.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS01837113Rib · crackedINSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XS 515.72. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS01837112Rib · crackedINSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 335.25. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS01837111Rib · crackedINSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 834. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS01837107Fitting · crackedINSPECTION TYPE:C23 STA 280 LONG 21R FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754032, AND SRM 51-1-20D.SDR UPS01837096Fitting · crackedINSPECTION TYPE:C23 STA 610 LONG 26R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750330 AND SRM 51-1-20D, 53-1-0.SDR UPS01837032Doubler · corrodedINSPECTION TYPE:C23 RIGHT WING L/E STALL WARNING DOUBLER IS CORRODED BEYOND LIMITS AT XFS 373. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769589, AND SRM 51-1-21 APPROX SIZE 5 X 7 INCHES.SDR UPS01837027Splice · crackedINSPECTION TYPE:C23 STA 600-620 LONG 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257, AND SRM 51-1-20D, 51-3-0.SDR UPS01837026Angle · crackedINSPECTION TYPE:C23 NR 2 STUB WING VERTICAL ATTACH ANGLE IS CRACKED AT XS 250. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 9753293, AND SRM 51-1-20D, 51-3-0.SDR UPS01837021Doubler · crackedINSPECTION TYPE:C23 LEFT WING L/E INBOARD WRAP-AROUND DOUBLER IS CRACKED AT XFS 304. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769589, AND SRM 51-1-20D, 51-1-21.SDR UPS01837013Clip · crackedINSPECTION TYPE: C23, LEFT WING L/E. INTERCOSTAL ATTACH CLIP IS CRACKED AT XOLDI 6.225. REMOVED,FABRICATED,AND REPLACED CLIP I.A.W.DWG. 5769589,AND SRM. 51- 1-20DSDR UPS01837011Rib · crackedINSPECTION TYPE: C23, LEFT WING L/E. UPPER RIBS ARE CRACKED AT XFS 354 AND XFS 379 REPAIRED RIBS I.A.W. SRM. 57-2-0 FIG. 2SDR UPS01837010Rib · crackedINSPECTION TYPE: C23, RIGHT WING L/E. UPPER RIB IS CRACKED AT XFS 297.5 REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2SDR UPS01837007Fitting · crackedINSPECTION TYPE: C23, STA. 440-460 LONG. 31R SPLICE FITTING IS CRACKED REMOVED AND REPLACED FITTING I.A.W. DWG. 3750257,AND SRM. 51-1-20DSDR UPS01837006Doubler · crackedINSPECTION TYPE: C23, LEFT WING L/E. LOWER INTERNAL DOUBLER IS CRACKED AT DRAIN HOLE AT XFS 335.25 REMOVED,FABRICATED,AND REPLACED DOUBLER I.A.W. DWG. 5769589,AND SRM. 51-1-21,51-1-20DSDR UPS01837155Skin · crackedINSPECTION TYPE:C23 R-2 DOOR UPPER AFT CORNER OF OPENING SKIN, INTERNAL DOUBLER, AND LONGERON 11R ARE CRACKED AT STA 1654. REPAIRED SKIN AND INTERNAL DOUBLER, AND LONGERON IAW 8110-3 APPROVED DH SK 936-267, AND DC8-5330-15557-A.SDR UPS01837139Rib · crackedINSPECTION TYPE:C23 RIGHT WING L/E LOWER RIBS ARE CRACKED AT XFS 822.5, XFS 828.75, XFS 835. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.SDR UPS01837138Splice · crackedINSPECTION TYPE:C23 STA 210 LONG 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754220, AND SRM 51-1-20D.SDR UPS01837137Rib · crackedINSPECTION TYPE:C23 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 628.75. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS01837136Rib · crackedINSPECTION TYPE:C23 LEFT WING L/E UPPER RIBS ARE CRACKED AT XFS 578.75, XFS 585. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.SDR DHL2001801545Attach Angle · crackedAFT CARGO COMPT FLOOR LINING ATTACH ANGLE CRACKED 1 INCH BETWEEN STA 1480.000 AND L35L. STOP DRILLED CRACK PER SRM 53-2-0 PG 2E-2F. FABRICATED REINFORCING ANGLE PER SRM 53-2-0 PG 2E-2F. INSTALLED ANGLE PER SRM 53-2-0 PG 2E-2F.SDR DHL2001801544Attach Angle · crackedAFT CARGO COMPT FLOOR LINING ATTACH ANGLE CRACKED 1 INCH BETWEEN STA 1340.000 AND L-31R. STOP DRILLED CRACK PER SRM 53-2-0 PG 2E. FABRICATED REINFORCING ANGLE PER SRM 53-2-0 PG 2E-2F. INSTALLED ANGLE PER SRM 53-20 PG 2E-2F.SDR DHL2001801520Rib · crackedRIGHT WING CENTER LEADING EDGE INTERIOR RIB CRACKED .5 INCH AT XFS 310. STOP DRILLED CRACK PER SRM 57-2-0 PG 1-2. FABRICATED REINFORCING ANGLE PER SRM 57-2-0 PG 1-2. INSTALLED ANGLE PER SRM 57-2-0 PG 1-2.SDR DHL2001801506Seat Track · wornMAIN CARGO SEAT TRACK LUG WORN BETWEEN STA 500.000 AND STA 580.000. CUT DAMAGED AREA PER SRM 53-2-3 PG 49-50. FABRICATED 3 SPLICES. CONDITIONED NEW TRACK PER SRM 53-2-3 PG 40-50. INSTALLED SPLICES AND NEW TRACK PER SRM 53-2-3 PG 49-50.SDR DHL2001801505Fitting · crackedAFT CARGO COMPT-SPLICE FITTING 2 IN CRACKED , BETWEEN STA 1040.000 AND STA 1060 , L31R.REMOVED CRACKED FITTING PER SRM 51-120D PG 21.CLEANED, TREATED AND PRINED PER SRM 51-1-20B.INSTALLED NEW FITTING PER SRM 51-1-20D PG 9.SDR DHL2001801504Frame · crackedFWD CARGO COMPT-FRAME AT STA 220.000, L-35L SHOWS .5 INCH CRACK. STOP DRILLED CRACK PER SRM 53-2-0 FIG 2. FABRICATED DOUBLER PER SRM 53-2-0-FIG 2. INSTALLED DOUBLER PER SRM 53-2-0 FIG 2.SDR DHL2001801501Attach Angle · crackedAFT CARGO COMPT - FLOOR LINING ATTACH ANGLE CRACKED 1 INCH BETWEEN STA 1360.000 AND L-35R. STOP DRILLED CRACK PER SRM 53-2-0 PG 2E-2F. FABRICATED ANGLE PER SRM 53-2-0 PG 2E-2F. INSTALLED ANGLE PER SRM 53-2-0 PG 2E-2F.SDR UPS01837104Doubler · crackedINSPECTION TYPE:C23 LEFT WING L/E INTERNAL WRAP AROUND DOUBLER IS CRACKED AT XFS 566.25. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769600, AND SRM 51-1-20D, 51-1-21.SDR UPS01837101Doubler · crackedINSPECTION TYPE:C23 LEFT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 585. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769600 AND SRM 51-1-20D, 51-1-21.SDR UPS01837100Rib · crackedINSPECTION TYPE:C23 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 660. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS01837099Rib · crackedINSPECTION TYPE:C23 LEFT WING L/E UPPER RIBS ARE CRACKED AT XFS 747.5, XFS 753.75, XFS 760. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.SDR UPS01837098Rib · crackedINSPECTION TYPE:C23 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 847.5. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.SDR UPS01837097Finger Doubler · crackedINSPECTION TYPE:C23 STA 130 LONG 31L FINGER DOUBLER IS CRACKED. TRIMMED OFF CRACKED FINGER ON FINGER DOUBLER IAW ENGINEERING RESPONSE AND SRM CHAPTER 51 GUIDELINES.SDR UPS01837019Rib · crackedINSPECTION TYPE:C23 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 772.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS01837033Angle · corrodedINSPECTION TYPE:C23 STA 1766 LONG 10R AFT SIDE OF AFT PRESSURE BULKHEAD HAS TWO SEAL ANGLES CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED ANGLES IAW DWG 5772638, AND SRM 51-1-20D, 51-3-0.SDR UPS01837031Skin · corrodedINSPECTION TYPE:C23 LEFT WING L/E LOWER SKIN HAS INTERGRANULAR CORROSION AT XFS 341. CUT OUT CORRODED AREA, FABRICATED DOUBLER AND FILLER APPROX SIZE 6 X 2.5 INCH. REPAIRED SKIN IAW EO DC8-5720-7767-A.SDR UPS01837030Doubler · corrodedINSPECTION TYPE:C23 RIGHT WING L/E LOWER INTERNAL DOUBLER IS CORRODED BEYOND LIMITS BETWEEN XFS 722.25 TO XFS 735 (PANEL 518C). REMOVED AND REPLACED DOUBLER IAW DWG 3641257, AND SRM 51-1-20D, 51-1-21.SDR UPS01837029Angle · crackedINSPECTION TYPE:C2,3 STA -99 PILOTS WINDOW FRAME HAS A CRACKED ANGLE AT FWD LOWER CORNER AFT OF SPLICE. REMOVED, FABRICATED, AND REPLACED ANGLE IAW SRM 53-2-3 FIG 3, 53-1-0.SDR UPS01837020Rib · crackedINSPECTION TYPE:C23 RIGHT WING L/E LOWER RIB IS CRACKED AT XFS 772.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS01837018Rib · crackedINSPECTION TYPE: C23, RIGHT WING L/E. UPPER RIB IS CRACKED AT XFS 672.5 REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2SDR UPS01837017Rib · crackedINSPECTION TYPE: C23, RIGHT WING L/E. LOWER RIBS ARE CRACKED AT XFS 747.5 TO XFS 760 REPAIRED RIBS I.A.W. SRM. 57-2-0 FIG. 2SDR UPS01837016Rib · crackedINSPECTION TYPE: C23, RIGHT WING L/E. UPPER RIBS ARE CRACKED AT XFS 635 AND XFS 647.5. REPAIRED RIBS I.A.W. SRM. 57-2-0 FIG. 2SDR UPS01837015Rib · crackedINSPECTION TYPE: C23, RIGHT WING L/E. UPPER RIBS ARE CRACKED AT XFS 722.5,XFS 728.75, XFS 735. REPAIRED RIBS I.A.W. SRM. 57-2-0 FIG. 2SDR UPS01837014Rib · crackedINSPECTION TYPE: C23, RIGHT WING L/E. LOWER RIBS ARE CRACKED AT XFS 616.25 AND XFS 622.5 REPAIRED RIBS I.A.W. SRM. 57-2-0 FIG. 2SDR UPS01837012Rib · crackedINSPECTION TYPE: C23, LEFT WING L/E. LOWER RIBS ARE CRACKED AT XFS 616.25 AND XFS 622.5 REPAIRED RIBS I.A.W. SRM. 57-2-0 FIG. 2SDR UPS01837009Rib · crackedINSPECTION TYPE: C23, RIGHT WING L/E. LOWER RIBS ARE CRACKED AT XFS 653.75 AND XFS 660 REPAIRED RIBS I.A.W. SRM. 57-2-0 FIG. 2SDR UPS01837008Rib · crackedINSPECTION TYPE: C23, LEFT WING L/E. UPPER RIBS ARE CRACKED AT XFS 722.5 AND XFS 728.75 REPAIRED RIBS I.A.W. SRM. 57-2-0 FIG. 2SDR UPS01837005Skin · crackedINSPECTION TYPE: C23, RIGHT WING UPPER SKIN IS CRACKED AT XRS 74 AT STRINGER 9 REPAIRED SKIN I.A.W. SRM. 57-2-1 FIG. 10SDR UPS01837004Rib · crackedINSPECTION TYPE: C2,3, RIGHT WING L/E. UPPER RIB IS CRACKED AT XFS 766.25 REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2SDR DHL2001801541Floor Support · crackedFWD CARGO COMPT-FLOOR SUPPORT ANGLE CRACKED .75 INCH AT STA 380.000 AND L-31L. STOP DRILLED CRACK PER SRM 53-2-0 FIG 1B. FABRICATED SUPPORT ANGLE WITH STEEL PER SRM 53-2-0 FIG 1B. INSTALLED SUPPORT ANGLE PER SRM 53-2-0 FIG 1B.
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