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 UPS99830766Rib · crackedINSPECTION TYPE:C123, LT WING L/E RIB ATV STA XFS 772.50 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS99830765Rib · crackedINSPECTION TYPE:C123, LT WING L/E RIB AT STA XFS 816.25 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS99830762Rib · crackedINSPECTION TYPE:C123, LT WING L/E RIB AT STA XFS 810 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS99830761Rib · crackedINSPECTION TYPE:C123, LT WING L/E RIB AT STA XFS 753.750 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS99830760Rib · crackedINSPECTION TYPE:C123, LT WING L/E RIB AT STA XFS 722.50 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR RRXA991791Floorbeam · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL AT STA 70 AND BL 18R. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FLOOR PANEL IAW DC-8 SRM 53-2-3. CORROSION DAMAGSDR RRXA991777Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LEFT WING, INBOARD FLAP, TOP SKIN AT XW=5. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 57-7-0. CORROSISDR IXXA9900023Ballast · defectiveEN ROUTE FROM JFK TO TOL, AN ODOR WAS SENSED IN THE COCKPIT WHEN THE GLAIR SHIELD LIGHTING WAS ILLUMINATED. THE CREW TURNED THE LIGHTS OFF AND THE ODOR SUBSIDED. MAINTENANCE INSPECTED THE LIGHTING SYSTEM, WHICH REVEALED A DEFECTIVE LIGHT BALLAST. MAINTENANSDR UPS99830887Rib · crackedINSPECTION TYPE:C123 LT WING L/E RIB AT XILD O.7095 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0.SDR UPS99830855Fitting · crackedINSPECTION TYPE:C123 FS 1180, AT LONGERON 33R, THE BANANA FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.SDR UPS99830854Ingercostal · crackedINSPECTION TYPE:C123 LT WING L/E AT XFS 115.0, JUST AFT OF THE ACCESS PANEL, THE INTERCOSTAL IS CRACKED AT THE 2ND FROM THE INBOARD FASTENER. REMOVED, FABRICATED, AND REPLACED THE INTERCOSTAL IAW DWG 3653679 AND SRM 51-1-20D.SDR UPS99830853Fitting · crackedINSPECTION TYPE:C123 LONGERON SPLICE FITTING IS CRACKED AT FS 1050, LONGERON 31L. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-21.SDR UPS99830852Fitting · crackedINSPECTION TYPE:C123 BATHTUB FITTING CRACKED INSIDE WEB AT FS 1210, LONGERON 33R. REMOVED AND REPLACED THE FITTING IAW SRM 51-2-0 FIG 2D.SDR UPS99830851Rib · crackedINSPECTION TYPE:C123 LT WING L/E AT XS 250.089, ABOVE THE WIRE BUNDLES. THE RIB IS CRACKED. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0 FIG 2.SDR UPS99830850Angle · crackedINSPECTION TYPE:C123 LT WING L/E, INBD SIDE OF THE XS 250.089 RIB, THE INBD SLOT AFT BULKHEAD OTBD VERTICAL ANGLE IS CRACKED AT THE LWR END. REMOVED, FABRICATED, AND REPLACED THE ANGLE IAW DWG 9753293 AND SRM 51-1-20D AND 51-3-0.SDR UPS99830849Angle · crackedINSPECTION TYPE:C123 LT INBD L/E UPPER AFT ATTACH ANGLE IS CRACKED. REMOVED, FABRICATED AND REPLACED THE ANGLE IAW DWG 5769646 AND SRM 51-3-0.SDR UPS99830848Rib · crackedINSPECTION TYPE:C123 LT WING L/E STUB WING RIB AT XS 520.168 IS CRACKED ABOVE THE ELECT CONDUIT. STOP DRILL THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0 FIG 2.SDR UPS99830847Longeron · corrodedINSPECTION TYPE:C123 LONGERON 31L BELOW THE FRAME AT FS 1340 IS CORRODED BEYOND LIMITS. CUT OUT THE DAMAGED LONGERON AND SPLICED IN A NEW SECTION OF LONGERON IAW DH SK718-829.SDR UPS99830846Fitting · crackedINSPECTION TYPE:C123 BETWEEN FS 1340 AND 1360, LONGERON 30L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED THE SPLICE FITTING IAW SRM 51-1-20D.SDR UPS99830844Longeron · corrosionINSPECTION TYPE:C123 BATH TUB FITTING AND BEAM HAVE HEAVY CORROSION INSIDE WEB AT FS 330 TO 340, LONGERON 36. REMOVED AND REPLACED THE FITTING AND THE BEAM (LONGERON) IAW SRM 51-1-20D AND 53-2-0 FIG 1F.SDR UPS99830835Doubler · corrodedINSPECTION TYPE:C123 STA 1460 LONG 31L FINGER DOUBLER IS CORRODED. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER IAW DWG 5615374.SDR UPS99830832Doubler · crackedINSPECTION TYPE:C123 LT WING L/E LWR SKIN DOUBLER AT STA XFS 305 IS CRACKED AT ACCESS PANEL 524B. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5641252 AND SRM 51-1-20.SDR UPS99830831Rib · crackedINSPECTION TYPE:C123 LT WING L/E RIB AT STA XFS347.75 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS99830802Rib · crackedINSPECTION TYPE:C123, LT WING L/E RIB AT FS 461.372 WAS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0 FIG 2.SDR UPS99830801Rib · crackedINSPECTION TYPE:C123, LT WING L/E RIB AT FS 466.651 WAS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0 FIG 2.SDR UPS99830799Splice · crackedINSPECTION TYPE:C123, THE LONGERON 34R SPLICE FITTING WAS CRACKED BETWEEN FS 1340 AND 1360. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.SDR UPS99830798Angle · crackedINSPECTION TYPE:C123, LT WING L/E, FWD OF THE NR 2 PYLON CUTOUT THE L/E RIB FWD ATTACH CLIP WAS CRACKED AT THE LWR END. REMOVED, FABRICATED AND REPLACED THE CLIP IAW DWG 9753294 AND SRM 51-1-20D.SDR UPS99830797Doubler · corrodedINSPECTION TYPE:C123, THE FINGER DOUBLER AT FS 1460 AND LONG 31L WAS CORRODED. REMOVED, FABRICATED AND REPLACED THE FINGER DOUBLER IAW DWG 5615374 & SRM 51-1-20D, 51-1-21.SDR UPS99830796Longeron · crackedINSPECTION TYPE:C123, LONGERON 35L FS 215 - 220 WAS CRACKED BEYOND THE STOP DRILL AND CORROSION WAS FORMING INSIDE THE CRACK. CUT OUT THE DAMAGED LONGERON, FS 190 - 230 AND SPLICED IN A NEW SECTION OF LONGERON IAW SRM 53-2-2 FIG 10.SDR UPS99830780Doubler · crackedINSPECTION TYPE:C123, LT WING L/E LWR SKIN INTERNAL DOUBLER AT FS 336.75 WAS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED AND REPLACED THE INTERNAL DOUBLER IAW DWG 5769589 AND SRM 51-1-20D & 51-1-21.SDR UPS99830776Rib · crackedINSPECTION TYPE:C123, LT WING L/E RIB AT FS 227.335 WAS CRACKED AT THE AFT UPPER END. STOP DRILLED THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0.SDR UPS99830775Rib · crackedINSPECTION TYPE:C123, LT WING L/E RIB AT FS 195.0 WAS CRACKED AT THE AFT LWR END. REPAIRED THE RIB IAW SRM 57-2-0.SDR UPS99830772Doubler · crackedINSPECTION TYPE:C123, LT WING L/E LWR SKIN DOUBLER AT STA XFS 304.0 IS CRACKED FWD OF THE DOUBLER T/E. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769589 AND SRM 51-1-20D.SDR UPS99830771Angle · crackedINSPECTION TYPE:C123, LT WING LEADING EDGE I/B SIDE OF THE XS520.168 RIB, THE SLOT AFT BULKHEAD VERTICAL ANGLE IS CRACKED AT THE LWR END. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753297 AND SRM 51-1-20D.SDR UPS99830768Rib · crackedINSPECTION TYPE:C123, LT WING L/E RIB AT STA XFS 435.789 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS99830767Rib · crackedINSPECTION TYPE:C123, LT WING L/E RIB AT STA XFS442.185 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS99830764Rib · crackedINSPECTION TYPE:C123, LT WING L/E RIB AT STA XFS 476.897 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS99830763Rib · crackedINSPECTION TYPE:C123, LT WING L/E RIB AT STA XOLDI6.225 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS99830759Rib · crackedINSPECTION TYPE:C123, LT WING L/E RIB AT STA XFS 448.501 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS99830631Fuel Dump · corrodedINSPECTION TYPE:N/A, CORROSION AND METAL DISTRESS FOUND ON LEFT FUEL DUMP. ACCOMPLISHED INTERIM REPAIR PER EO DC-8-5720-1158-A, ITEM DEFERRED PER EO DC8-5720-11858-A. SPEED TAPE APPLIED, OK FOR CONTINUED SERVICE.SDR UPS99830624Mechanism · out of adjustINSPECTION TYPE:N/A, AFTER TAKEOFF DURING GEAR RETRACTION DOOR NOT LATCHED (RIGHT) REMAINED ILLUMINATED. CHECKLIST FOLLOWED, AFTER THREE GEAR RETRACTION CYCLES LIGHT FINALLY EXTINGUISHED. ADJUSTED RIG ON RIGHT HAND MAIN GEAR DOOR ACTUATOR PER M/M 32-32-07. SDR UPS99830890Angle · crackedINSPECTION TYPE:C123 SIX INCH CRACK AT FS 1766, UPPER CABIN BULKHEAD ANGLE BETWEEN LONGERON 10L AND 11L. STOP DRILLED CRACK AND REPAIRED THE ANGLE IAW SRM 53-2-5 FIG 1F.SDR UPS99830888Fitting · corrodedINSPECTION TYPE:C123 CORROSION AROUND THE UPPER CUSP FITTING MOUNT BOLTS AT FS 1306 LT. REMOVED AND REPLACED THE CUSP FITTING IAW SRM 51-1-20D AND 51-3-0.SDR UPS99830845Fitting · corrodedINSPECTION TYPE:C123 CORROSION AROUND UPPER CUSP FITTING MOUNT BOLTS INBD, FWD, AND AFT AND ON FLOORBEAM FS 1306, LT SIDE. REMOVED AND REPLACED THE CUSP FITTING IAW SRM 51-1-20D AND 51-3-0.SDR UPS99830794Doubler · crackedINSPECTION TYPE:C123, THE LT I/B AILERON LOWER SURFACE INTERNAL DOUBLER FOR ACCESS PANEL 541 WAS BENT AND CRACKED. REPAIRED THE DOUBLER IAW DH SK718-668.SDR UPS99830792Skin · crackedINSPECTION TYPE:C123, AFT FUSELAGE SKIN AT FS 1717, BETWEEN LONG 35R & 36 WAS CRACKED AND HEAVILY CORRODED. REMOVED AND REPLACED THE SKIN FROM FS 1690 TO 1890 IAW SRM 51-1-21 AND 51-1-20D.SDR UPS99830791Fitting · crackedINSPECTION TYPE:C123, VERTICAL LEG OF ANGLE (P/N 3701427-2) CRACKED AT O/B END. ANGLE INSTALLED AT I/B END OF THE RT HORIZ STAB, FWD OF ACCESS PANEL 64I. REMOVED AND REPLACED THE ANGLE FITTING IAW SRM 51-1-20D, 51-1-21 AND 51-3-0.SDR UPS99830889Angle · crackedINSPECTION TYPE:C123 LT SIDE OF THE LWR KEEL BEAM AT FS 839, BL 0, BETWEEN THE MLG DOORS, INTERCOSTAL ANGLE IS CRACKED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-1-20D.SDR UPS99830843Fitting · crackedINSPECTION TYPE:C123 FLOOR SUPPORT BEAM CRACKED AND ANGLE FITTING CRACKED AT FS 240, LBL 42. REMOVED AND REPLACED THE ANGLE FITTING AND REPAIRED THE FLOOR SUPPORT BEAM IAW DH SK718-388.SDR UPS99830622Skin · crackedINSPECTION TYPE:N/A, 1 INCH CRACK UPPER AFT CORNER FUSELAGE PIT 34. *S/D* REPAIRED CRACK IAW SRM 53-02-00.
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