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 UPS01836636Splice · crackedINSPECTION TYPE:C1,3 STA 440-460 LONG 17L, SPLICE FITTING IS CRACKED. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 3887799, AND SRM 51-1-20D.SDR UPS01836635Longeron · crackedINSPECTION TYPE:C1,3 STA 1735 LONG 15L IS CRACKED. REPAIRED LONGERON IAW SRM 53-2-2 FIG 10.SDR UPS01836624Fitting · crackedINSPECTION TYPE:C1,3 STA 680-700 LONG 7L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779762, AND SRM 51-1-20D, 51-1-21.SDR UPS01836620Fitting · crackedINSPECTION TYPE:C1,3 STA 857 LONG 18L INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779498, AND SRM 51-1-20D.SDR UPS01836618Fitting · crackedINSPECTION TYPE:C1,3 STA 320 BANANA FITTING IS CRACKED AT LONG 26L. REMOVED AND REPLACED FITTING IAW DWG 3754041, AND SRM 51-1-20D, 51-1-21.SDR UPS01836617Fitting · crackedINSPECTION TYPE:C1,3 STA 822 LONG 18R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4751640, AND SRM 51-1-20D.SDR UPS01836616Fitting · crackedINSPECTION TYPE:C1,3 STA 680-700 LONG 8L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779762, AND SRM 51-1-20D.SDR UPS01836597Rib · crackedINSPECTION TYPE:C1,3 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 797.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS01836531Skin · crackedINSPECTION TYPE:IN LEADING EDGE CRACKED O/B OF NR 3 ENGINE. CRACK LOWER RT LEADING EDGE JUST OUTBD NR 3 ENG, BELOW INBD FIRE BOTTLE ACCESS DOOR. COMING FROM SCREW HOLE APPROX 1/2 INCH LONG. VIS AND PAGE PEN INSP CONFIRMS CRACK APPROX 1/2 INCH AS NOTED. HFEC COSDR DHL2001804502Rib · crackedRT WING L/E UPPER RIB CRACKED .50 INCH AT XFS 633.00STOP DRILLED CRACKED, FABRICATED DOUBLER, AND INSTALLED DOUBLER IAW SRM 52-2-0, FIG 2 AND SRM 51-1-21 PG 1.SDR DHL2001804500Rib · crackedD-CHECK-RT WING L/E UPPER RIB CRACKED .50 INCH AT XFS 608.00. STOP DRILLED CRACK IAW SRM 57-2-0 FIG.2. FABRICATE DOUBLER AND INSTALLED DOUBLER ON RIB IAW SRM 57-2-0.FIG2 AND SRM 5101-21, PG1.SDR DHL2001806008Bracket · out of positionF/O SIDE WINDOW WILL NOT OPEN FULLY. REPOSITIONED WINDOW BRACKET OPS CK OK IAW MM 56-20-2.SDR UPS01836730Rib · crackedINSPECTION TYPE:C1,3 RT WING L/E UPPER RIB CAP IS CRACKED AT XS 467. REMOVED,FABRICATED,AND REPLACED RIB CAP IAW SRM 57-3-3 FIG 4, 51-1-21, 51-1-20D, 57-1-0.SDR RRXA11449Floor Panel · crackedDURING A MAINTENANCE VISIT FOUNDSUB FLOOR PANEL UNDER PILOTS SEAT CRACKED 2EA PLACES. ***CORRECTIVE ACTION *** STOP DRILLED CRACKS, TERMINATED, FABRICATED AND INSTALLED DOUBLERS IAW SRM 53-2-0 FIG 1D AND 1B, 51-1-8, 51-1-21,51-1-20D AND 06-10-001SDR UPS01836638Doubler · crackedINSPECTION TYPE:C1,3 RIGHT WING L/E NR 3 STUBWING LOWER DOUBLER IS CRACKED AT OPENING ABOVE PYLON CUTOUT. REMOVED, FABRICATED, AND REPLACED REPAIR DOUBLER IAW SRM 57-2-1A.SDR UPS01836637Rib · crackedINSPECTION TYPE:C1,3 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 410.25. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS01836633Skin · corrodedINSPECTION TYPE:C1,3 LT HORIZ STAB L/E UPPER SKIN IS CORRODED BEYOND LIMITS AT XFS 178. REPAIRED SKIN IAW SRM 55-2-1 FIG 4.SDR UPS01836632Skin · corrodedINSPECTION TYPE:C1,3 RT HORIZ STAB L/E LOWER SKIN IS CORRODED BEYOND LIMITS AT XFS 178. REPAIRED SKIN IAW SRM 55-2-1 FIG 4.SDR UPS01836631Floor Support · corrodedINSPECTION TYPE:C1,3 STA 1710 RBL 10, MAIN CABIN FLOOR SUPPORT IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED FLOOR SUPPORT IAW DWG 5755032.SDR UPS01836625Doubler · brokenINSPECTION TYPE:C1,3 RIGHT WING LOWER FRONT SPAR HAS DOUBLER BROKEN AT XS 520. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW SRM 57-2-1 FIG 14A, AND DWG 5802736.SDR DHL2001804526Skin · dentedRT OUTBOARD AILERON UPPER SKIN SURFACE DENTED AT STA XRS 659. CUT DAMAGED AREA IAW 57-2-1 PAR 16. FABRICATED DOUBLER AND INSTALLED ON RT OUTBOARD AILERON UPPER SKIN SURFACE IAW SRM 57-2-1 PAR 16, SRM 51-1-21 PG 1.SDR UPS01836601Doubler · crackedINSPECTION TYPE:C1,3 RIGHT WING OB SLOT VANE INTERNAL DOUBLER IS CRACKED AT XS 520. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769933, AND SRM 51-1-21,51-1-21A.SDR UPS01836600Skin · crackedINSPECTION TYPE:C1,3 RIGHT WING L/E UPPER SKIN IS CRACKED AT XFS 710. REPAIRED SKIN IAW DC8-5720-7767-A.SDR UPS01836599Rib · crackedINSPECTION TYPE:C1,3 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 772.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS01836596Rib · crackedINSPECTION TYPE:C1,3 RIGHT WING L/E LOWER RIB IS CRACKED AT XFS 603. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS01836593Skin · crackedINSPECTION TYPE:C1,3 RIGHT WING L/E SKIN IS CRACKED AT XFS 878. REPAIRED SKIN IAW SRM 57-2-1 FIG 2B.SDR UPS01836592Rib · crackedINSPECTION TYPE:C1,3 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 329. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS01836591Rib · crackedINSPECTION TYPE:C1,3 LEFT WING L/E RIB IS CRACKED AT XFS 615. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS01836590Rib · crackedINSPECTION TYPE:C1,3 RIGHT WING L/E LOWER RIBS ARE CRACKED AT XFS 822.5, XFS 828.75. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.SDR UPS01836589Rib · crackedINSPECTION TYPE:C1,3 LEFT WING L/E RIB IS CRACKED AT XFS 760. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS01836588Rib · crackedINSPECTION TYPE:C1,3 LEFT WING L/E RIB IS CRACKED AT XFS 585. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS01836587Skin · crackedINSPECTION TYPE:C1,3 RIGHT WING L/E LOWER SKIN IS CRACKED AT XFS 597.5. REPAIRED SKIN IAW DC8-5720-7767-A.SDR UPS01836586Skin · crackedINSPECTION TYPE:C1,3 RIGHT WING L/E SKIN IS CRACKED 2 PLACES AT XW 485. REPAIRED SKIN IAW DC8-5720-7767-A, AND SRM 57-2-1 FIG 2H.SDR UPS01836584Rib · crackedINSPECTION TYPE:C1,3 RIGHT WING L/E. LOWER RIBS ARE CRACKED AT XFS 791.25,XFS 797.5, XFS 803.75. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.SDR UPS01836583Skin · crackedINSPECTION TYPE:C1,3 RIGHT WING L/E. LOWER SKIN IS CRACKED AT XFS 841.25. REPAIRED SKIN IAW DC8-5720-7767-A.SDR UPS01836582Rib · crackedINSPECTION TYPE:C1,3 RIGHT WING L/E. LOWER RIB IS CRACKED AT XFS 778.75. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS01836581Rib · crackedINSPECTION TYPE:C1,3 RIGHT WING CENTER L/E. UPPER RIB IS CRACKED AT XFS 379. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR DHL2001804520Angle · crackedEXTERIOR FUSELAGE REINFORCING ANGLE .5 INCH CRACK AT STA 761 LBL 22.0 (LOWER SECTION)REMOVED AND REPLACED CRACKED REINFORCING ANGLE PER SRM 51-1-20D PG 21.SDR RRXA11448Web · misdrilledDURING A MAINTENANCE VISIT FOUND C PIT TORQUE BOX FS 1180 WEB FRAME MISDRILLED L29R L30R. REMOVED WEB, FABRICATED REPLACEMENT WEB AND INSTALLED IAW DWG 5753893 AND SRM 51-1-8, 51-1-21, 51-1-20D AND 51-9-01.SDR UPS01836615Fitting · crackedINSPECTION TYPE:C1,3 STA 1160 LONG 19R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4750418, AND SRM 51-1-20D.SDR UPS01836598Doubler · crackedINSPECTION TYPE:C1,3 LEFT WING L/E INTERNAL DOUBLER IS CRACKED AT XW 485. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769600, AND SRM 51-1-21,51-1-21A.SDR RRXA11447Web · misdrilledDURING A MAINTENANCE VISIT FOUND D PIT DOOR TORQUE BOX FWD LWR WEB HAS 4 EACH MISDRILLED NUTPLATES AND DRILLED RIVIT HEADS. *** CORRECTIVE ACTION *** REMOVED WEB, FABRICATED REPAIR AND INSTALLED IAW SRM 53-2-0 FIG 53, 53-4-1 FIG 51, 51-1-8, 53-2-0 FIG 2, 53-2SDR UPS01836626Spar Cap · crackedINSPECTION TYPE:C1,3 RIGHT WING REAR SPAR LOWER CAP IS CRACKED AT XCW 0. REPAIRED SPAR IAW 8110-3 APPROVED DK SK 809-649.SDR DHL2001804519Web · crackedEXTERIOR FUSELAGE WEB 1 INCH CRACKED STA 680 L-30L.STOP DRILLED CRACK, FABRICATED DOUBLER, AND INSTALLED DOUBLER PER SRM 53-2-0.SDR DHL2001804518Angle · crackedFUSELAGE EXTERIOR ANGLE CRACKED 1 INCH AT STA 630 BETWEEN L31 AND L32R. REMOVED AND REPLACED CRACKED ANGLE PER SRM 51-1-21 PG 7.SDR DHL2001804517Rib · crackedRT HORIZ STABILIZER L/E INNER RIB CRACKED .5 INCH AT XFS 47.5. STOP DRILLED CRACK, FABRICATED REINFORCING ANGLE, AND INSTALLED ANGLE PER SRM 55-2-0 FIG 2 &51-1-21 PG 1.SDR RRXA11446Longeron · corrodedDURING A MAINTENANCE VISIT FOUND LONGERON 23L AT FS 550 FWD OF APU EXHAUST IS CORRODED BEYOND LIMITS. *** CORRECTIVE ACTION *** REMOVED, FABRICATED AND INSTALLED REPLACEMENT LONGERON SECTION PER DWG 5779912 AND DC8 SRM 51-1-20D AND 53-1-0SDR UPS01836595Rib · crackedINSPECTION TYPE:C1,3 LEFT WING L/E LOWER RIB IS CRACKED AT XRS 162. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR DHL2001804501Rib · crackedRT WING L/E UPPER RIB CRACKED .50 INCH AT XFS 741.00STOP DRILLED CRACK, FABRICATED DOUBLER, AND INSTALLED DOUBLER IAW SRM 52-2-0, FIG 2 AND SRM 51-1-21 PG 1.SDR RRXA11445Angle · crackedDURING A MAINTENANCE VISIT FOUND LT I/B FLAP I/B END AT T/E RT MAIN ANGLE CRACKED. REMOVED CRACKED DOUBLER, FABRICATED AND INSTALLED RT MAIN ANGLE IAW SRM 57-2-0 FIG 2, SRM 51-1-21 AND DWG 5642060
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