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 UPS98826977Rib · crackedINSPECTION TYPE-C, RT WING L/E RIB AT STA XFS 810.0 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED PER SRM 57-2-0 FIG 2.SDR UPS98826976Skin · crackedINSPECTION TYPE-C, RT WING L/E SKIN ON BOTTOM, ABOVE THE NR 3 PYLON HAS A CRACKED REPAIR DOUBLER. REMOVED EXISTING REPAIR DOUBLER, FABRICATED AND INSTALLED A NEW REPAIR DOUBLER PER SRM 51-1-20D AND 57-2-0.SDR UPS98826932Fitting · crackedINSPECTION TYPE-C, LONG SPLICE FITTING AT STA 450 AT LONG 32R IS CRACKED. REMOVED AND REPLACED THE LONG SPLICE FITTING PER SRM 51-1-20D.SDR UPS98826927Fitting · crackedINSPECTION TYPE-C, FS 450 AT LONG 36 THE LONG SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING PER SRM 51-1-20D.SDR UPS98826923Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XS484.895, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS98826922Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XFS603.750, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS98826901Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XFS597.500, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS98826900Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XFS603.750, THE LWR L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS98826898Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XFS876.00, THE LWR L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS98826897Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XFS747.500, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS98826896Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XFS766.250, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS98826895Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XFS791.250, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS98826894Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XFS828.750, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS98826893Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XFS828.750, THE LWR L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS98826892Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XFS797.500, THE LWR L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS98826891Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XFS822.800, THE LWR L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS98826890Rib · crackedINSPECTION TYPE-C, RT WING L/E STA XFS776.00, THE LWR L/E RIB IS CRACKED. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS98826889Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XFS810.000, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS98826888Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XFS.822.800, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS98826887Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XFS.610.00, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS98826886Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XFS.622.500, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS98826885Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XFS635.000, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS98826884Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XFS 653.750, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS98826883Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XFS.653.750, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS98826882Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XFS.660.000, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS98826881Rib · crackedINSPECTION TYPE-C, RT WING L/E UPPER RIB IS CRACKED AT THE AFT END AT STA XFS672.500. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS98826880Rib · crackedINSPECTION TYPE-C, RT WING LWR L/E RIB IS CRACKED AT THE AFT END AT STA XFS.735.000. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS98826879Rib · crackedINSPECTION TYPE-C, RT WING L/E RIB UPPER ARM IS CRACKED AT THE AFT END AT STA XFS741, 250. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS98826855Battery Pack · dischargedINSPECTION TYPE N/A, EMERG EXIT LIGHTS INOP. REMOVED AND REPLACED EMERG LIGHT BATT PACK (P/N 5708458-503) ON, (P/N 60-1223-5) OFF, (S/N 588) ON, (S/N 219) OFF.SDR UPS98826928Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB AT STA XFS 616.250 IS CRACKED AT THE AFT LOWER END. STOP DRILLED CRACK AND REPAIRED PER SRM 57-2-0 FIG 2.SDR UPS98826854Circuit Breaker · failedINSPECTION TYPE N/A, EMERGENCY EXIT LIGHTS ARE ON CONTINUOUSLY IN THE ARM POSITION AND WILL NOT DISARM CHECK. REMOVED AND REPLACED EEL CIRCUT BREAKER REF 20-50-00, OPS CHECK GOOD W/REF TO MM 33-50-01.SDR RRXA98307Frame · corrosionDURING A MAINTENANCE VISIT, FOUND FRAME WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM, AT STA 1520 AND LONGERON 8 RIGHT. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED TIMCO DER ENGINEERING SKETSDR RRXA98304Frame · corrodedDURING A MAINTENANCE VISIT, FOUND FRAME WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM, AT STA 200 AND LONGERON 17 RIGHT. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TIMCO DER ENGINEERSDR RRXA98303Frame · corrodedDURING A MAINTENANCE VISIT, FOUND FRAME WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM, AT STA 100 AND LONGERON 30 RIGHT. FABRICATED AND INSTALLED REPAIR STRAP IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-04788.SDR RRXA98299Frame · corrodedDURING A MAINTENANCE VISIT, FOUND FRAME WITH CORROSION DAMAGE BEYOND LIMITS, AT STA 1260 AND LONGERON 4 RIGHT. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TIMCO DER REO-04779.SDR RRXA98298Frame · corrodedDURING A MAINTENANCE VISIT, FOUND FRAME WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM, AT STA 300 BETWEEN LONGERONS 5 LEFT AND 6 LEFT. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRCATED AND INSTALLED REPAIR IAW FAA APPROVED TIMCO DER ENGSDR RRXA98290Frame · corrodedDURING A MAINTENANCE VISIT, FOUND FRAME WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM, AT STA 430 AND LONGERON 13 LEFT. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TIMCO DER ENGINEERISDR RRXA98289Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND FRAMES WITH MISS-DRILLED HOLES, AT STA 190 ALSO STA 200, BETWEEN LONGERONS 7 RIGHT TO 16 RIGHT AND LONGERON 6 LEFT. REMOVED DAMAGED SECTIONS, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR STRAPS IAW FAA ASDR UPS98827092Longeron · corrodedINSPECTION TYPE:C/CK CORROSION AND CRACK LONGERON 33 LEFT STATION 1540. REMOVED DAMAGED SECTION AND FABRICATED STRAPS AND LONGERON. ALODINED AND PRIMED AND INSTALLED IAW DC8 SRM 53-2-2, 51-1-8, 51-1-20D.SDR UPS98826930Fitting · corrodedINSPECTION TYPE-C, FS 960 ABOVE LONG 24R THE FITTING IS CORRODED. REMOVED AND REPLACED FITTING PER DWG 3647117 AND SRM 51-1-20D, 51-1-3, 53-2-0 FIG 8.SDR UPS98826929Rib · crackedINSPECTION TYPE-C, LT WING I/B SLOT O/B Z-ANGLE CLOSE OUT RIB IS CRACKED. REMOVED AND REPLACED Z-ANGLE PER DWG 5769859 AND SRM 51-1-20D AND 51-1-21.SDR UPS98826838Control Valve · failedCREW EVACUATED AIRCRAFT DUE TO SMOKE IN COCKPIT. CREW FOLLOWED EVACUATION CHECKLIST, FIRED ALL BOTTLES, SHUTDOWN ALL ENGINES AFTER AIRCRAFT WAS REPOSITIONED TO UPS RAMP, THEN MOVED A/C TO MERCURY CARGO RAMP. DETERMINED LEFT PACK WILL NOT SHUT OFF, SUSPECT FLSDR RRXA98309Frame · crackedDURING A MAINTENANCE VISIT, FOUND FRAME DENTED/CRACKED BEYOND LIMITS IAW DC-8 SRM, STA 300 AND LONGERON 15 RIGHT. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-048SDR UPS98826904Fitting · crackedINSPECTION TYPE-C, STA 1200 AT LONG 34R, THE BACK-UP FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755841.SDR UPS98826903Skin · corrodedINSPECTION TYPE-C, FUSELAGE SKIN AT STA 450 TO 610 STR 33R-33L IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SKIN IAW DWG 5779913 AND SRM 51-1-20D.SDR DHL98804001Rt Unit · malfunctionedRADAR ANTENNA TILT WENT TO FULL NOSE UP ON DEPARTURE. REPLACED RADAR R/T AND CONTROL PANEL.SDR RRXA98308Jamb · cutDURING A MAINTENANCE VISIT, L-2 DOOR JAMB PAN, AFT LOWER CORNER NEEDS TO BE REMOVED TO FACILITATE OTHER MAINTENANCE. REPLACED PANEL BY SPLICE REPAIR IAW FAA APPROVED TIMCO ENGINEERING SKETCH REO-04810.SDR RRXA98306Spar Cap · corrodedDURING A MAINTENANCE VISIT, FOUND RIGHT WING, AFT SPAR CAP WITH CORROSION BEYOND LIMITS IAW DC-8 SRM, AT STA 63. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-0480SDR RRXA98305Angle · cutDURING A MAINTENANCE VISIT, STA 70, FWD CAP ANGLE REQUIRES SPLICE REPAIR, BETWEEN LONGERONS 25 LEFT TO 26 LEFT, AND RIGHT SIDE. DC-8 SRM 53-2-5, FIGURE 8C GIVES INSTRUCTIONS TO ACCOMPLISH THE SPLICE AT LOWER LOCATION. FAA APPROVED TIMCO DER REO-04801, ALSO PSDR RRXA98223Frame · cutDURING A MAINTENANCE VISIT, FOUND FRAME CAP CUT AT STA 70 BETWEEN LONGERONS 25 LEFT AND 26 LEFT. FABRICATED AND INSTALLED REPAIR SPLICE IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH RE0-04801.
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