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 UPS96821265Rib · crackedINSPECTION TYPE: CS2. RT WING LEADING EDGE UPPER RIB CRACK AT STA XFS560. REPAIRED RIB PER MM 57-00-00 FIG 801.SDR UPS96821264Rib · crackedINSPECTION TYPE: CS2. LT WING LEADING EDGE 9 EA RIBS CRACKED AT WS XFS730, XFS750, XFS755 , XFS760, XFS765, XFS775, XFS780, XFS785 AND XFS800. REPAIRED RIBS PER MM 57-00-00 FIG 801.SDR UPS96821262Fitting · crackedINSPECTION TYPE: CS2. LT WS XRS410 CANOE FITTING OUTBOARD SIDE BRACE FITTING CRACKED INSIDE CHANNEL. REPLACED FITTING PER SRM 51-1-20D.SDR UPS96821239Web · crackedINSPECTION TYPE-CS2, WEB CRACKED FS 340 RBL 48 ABOVE A BIN DOOR JAMB. REPAIRED WEB PER UPS EO.SDR UPS96821235Skin · delaminatedINSPECTION TYPE-CS2, RT WING NR 4 SPOILER DELAMINATED. REPLACED SPOILER PER MM 27-61-01.SDR UPS96821234Rib · crackedINSPECTION TYPE-CS2, RT WING LEADING EDGE 4 RIBS CRACKED AT STA XFS820, XFS800, XFS695 AND XFS680. REPAIRED RIBS PER MM 57-00-00, FIG 801.SDR UPS96821232Longeron · crackedINSPECTION TYPE-CS2, LONGERON 24R AT FS 857, CRACKED AT BOTTLE BOLT HOLE. REPLACED LONGERON PER DRAWING NR 5750198 DAC.SDR UPS96821140Skin · corrodedINSPECTION TYPE-C, AFT FUSELAGE SKIN LT SIDE STA 1766 TO 1790 L10L AT LAP SEAM HAS CORROSION. REMOVED CORROSION IAW DC8 SRM 51-1-8, MATERIAL LOSS EXCEED 20 PERCENT. REMOVED DAMAGE IAW DC8 SRM 53-2-1, MATERIAL ID FOR REPAIRS ARE IAW DC8 53-5-3 FIG 1 AND 53-21SDR UPS96821283Fitting · crackedINSPECTION TYPE: CS2. LT AFT ENTRY DOOR FITTING CRACKED INSIDE 2ND LIGHTNING HOLE FROM TOP FWD SIDE. REPLACED FITTING PER SRM 51-1-20D.SDR UPS96821280Trim Tab · delaminatedINSPECTION TYPE: CS2. LT AILERON TRIM TAB DELAMINATED. REPLACED TAB PER MM 27-13-01.SDR UPS96821236Skin · delaminatedINSPECTION TYPE-CS2, LT WING NR 4 SPOILER DELAMINATED. REPLACED SPOILER ASSY PER MM 27-61-01.SDR UPS96821263Skin · delaminationINSPECTION TYPE: CS2. NR 3 SPOILER PANEL DELAMINATED ON RT WING. REPLACED SPOILER PER MM 27-61-01.SDR UPS96821139Panel · crackedINSPECTION TYPE-C, 506A RT WING CRACKED PNL LAND NR 4 MAIN. REMOVED CRACKED AREA OF PNL AND FABRICATED INTERNAL AND EXTERNAL DOUBLERS, FILLERS IAW SRM 57-2-1, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED ALL REPAIR PARTS IAW DC8 SRM 51-1-20D AND 51-1-20ASDR UPS96821112Floor Beam · crackedINSPECTION TYPE-CS2, WEBBING ON TOP OF FLOOR BEAM IS CRACKED FS 8, RBL 1. REPAIRED WEB PER SRM DC8-5350-7876.SDR UPS96821111Support · crackedINSPECTION TYPE-CS2 FLOOR BEAM SUPPORT CRACKED AT FS 717 UNDER SEAT TRACK NR 5. REPLACED SUPPORT ASSY PER SRM 51-1-20D.SDR UPS96821446Skin · corrosionINSPECTION TYPE: CS2. HEAVY CORROSION AT FUSELAGE SKIN PANEL FS 120-140 BETWEEN LONGERONS 3 5L-35R. REPAIRED PER UPS EO.SDR UPS96821444Lanyard · frayedINSPECTION TYPE: CS2. EVACUATION SLIDE LANYARD ASSY CABLE FRAYED. REPLACED LANYARD PER MM 25-60-01.SDR UPS96821104Fitting · crackedINSPECTION TYPE-CS2, FITTING CRACKED AT FS 1690 LONGERON 26L. REPLACED FITTING PER SRM 51-1-20D AND SRM 51-1-21.SDR UPS96821187Doubler · corrosionINSPECTION TYPE-CS2, HEAVY CORROSION DAMAGE AT 2 SEAT TRACK SPLICE DOUBLERS FS 1470 LBL 33 AND FS 1500 TO 1520, BL 0. REPLACED DOUBLERS PER SRM 53-2-3.SDR UPS96821186Web · corrosionINSPECTION TYPE-CS2, HEAVY CORROSION ON COCKPIT SUBFLOOR WEB UPPER HORIZONTAL SURFACE FS 20 TO 8 LONGERON 22L. REPAIRED PER UPS EO.SDR UPS96821174Longeron · corrosionINSPECTION TYPE-CS2, HEAVY CORROSION ON LONGERON 28L FS 1765 OUTBOARD LEG. REPAIRED PER UPS EO.SDR UPS96821173Longeron · corrosionINSPECTION TYPE-CS2, HEAVY CORROSION ON LONGERON 26R, FS 1706. REPAIRED PER UPS EO.SDR UPS96821172Fitting · crackedINSPECTION TYPE-CS2, HEAVY CORROSION AND CRACKED FITTING AT FS 1692 LONGERON 28R. REPLACED FITTING PER SRM 51-1-20D.SDR UPS96821171Fitting · corrosionINSPECTION TYPE-CS2, MODERATE CORROSION DAMAGE ON C-DOOR LOWER JAMB T-BOLT BACK UP FITTING FS 1210. REPLACED FITTING PER SRM 53-2-0, FIG 2D.SDR UPS96821128Longeron · crackedINSPECTION TYPE CS2, LONGERON 5R CRACKED AT THE VERTICAL STAB FS 1740. REPAIRED PER UPS EO.SDR UPS96821059Ribs · crackedINSPECTION TYPE CS2, 4 RIBS CRACKED LT WING LEADING EDGE AT WS XFS780, XFS800, XFS740 AND XFS 710. REPAIRED RIBS PER MM 57-00-00 FIG 801.SDR UPS96821202Spar · crackedINSPECTION TYPE: CS2. LEFT HORIZONTAL STABILIZER REAR SPAR WEB CRACKED AROUND FASTENER HOLD STA XE119.52. REPAIRED PER UPS EO.SDR UPS96821201Bulkhead Frame · crackedINSPECTION TYPE: CS2. HEAVY CORROSION ON BULKHEAD FRAME FS 980 LONGERON 25R, AND A 3 INCH LONG CRACK BETWEEN LONGERONS 23R-24R. REPAIRED PER UPS EO.SDR UPS96821129Spar Web · crackedINSPECTION TYPE CS2, RT HORIZONTAL STAB CLOSING REAR SPAR WEB HAS CRACKED HOLE AT STA XE 142. REPAIRED PER UPS EO.SDR UPS96821107Panel · delaminatedINSPECTION TYPE-CS2, RIGHT HAND WING NR 4 SPOILER PANEL DELAMINATED. REPLACED SPOILER PANEL PER MM 27-61-01.SDR UPS96821060Ribs · crackedINSPECTION TYPE CS2, 4 RIBS CRACKED AT LT WING LEADING EDGE WS XFS 623, XFS 633, XFS 648 AND XFS 653. REPAIRED RIBS PER MM 57-00-00 FIG 801.SDR UPS96821009Lights · inoperativeINSPECTION TYPE: DLY. EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK. OPS CHK, PART NR ON 60-1223-5, S/N 286, OFF 5708458-503, OFF A056.SDR RRXA96147Skin · corrodedDURING A MAINTENANCE VISIT, FOUND INTERNAL DOUBLER CORRODED PAST LIMITATIONS IAW DC-8 SRM, AT Y=1580 BETWEEN LONGERON 31 RIGHT TO LONGERON 31 LEFT. SKIN HAD TO CUT AND REMOVED FOR ACCESS AT Y=1580 TO Y=1690 FROM LONGERON 31 RIGHT TO LONGERON 31 LEFT. REMOVEDSDR UPS96821175Fitting · crackedINSPECTION TYPE-CS2, CRACKED FLOORBEAM ATTACH FITTING FS 1640 LONGERON 21R. REPLACED FITTING PER SRM 51-1-20D.SDR UPS96821169Track · corrosionINSPECTION TYPE-CS2, LT WING STA 3 FLAP TRACKS PITTED. REPLACED TRACKS PER MM 27-51-03.SDR UPS96821168Track · corrosionINSPECTION TYPE-CS2, LT WING STA 98 FLAP TRACKS PITTED. REPLACED TRACKS PER MM 27-51-03.SDR UPS96821167Track · corrosionINSPECTION TYPE-CS2, LT WING STA 219 FLAP TRACKS PITTED. REPLACED TRACKS PER MM 27-51-03.SDR UPS96821113Skin · crackedINSPECTION TYPE-CS2, LT WING UPPER SKIN HAS A 3.25 INCH LONG CRACK AT STA 69.5 REAR SPAR. REPAIRED SKIN PER SRM 57-2-1, FIG 20.SDR UPS96821105Angle · crackedINSPECTION TYPE-CS2, NR 4 PYLON DRAG ANGLE CRACKED .25 INCH LONG PAST STOP DRILL. REPAIRED ANGLE PER TASK CARD 8040-01, STEP 4.SDR UPS96821062Ribs · crackedINSPECTION TYPE CS2, THREE RIBS CRACKED AT RT WING LEADING EDGE ST XFS 304, XFS 310 AND XFS 341. REPAIRED RIBS PER MM 57-00-00 FIG 801.SDR RRXA96139Web · corrodedDURING A MAINTENANCE VISIT, FOUND TORQUE BOX WEB CORRODED PAST LIMITATIONS IAW DC-8 SRM, AT Y=275 TO Y=280 AND LONGERON 27 RIGHT. INSTALLED REPAIR IAW DER APPROVED ENGINEERING SKETCH B21-R24, TREATED AREA IAW DC-8 SRM 51-1-8.SDR RRXA96138Skin · corrodedDURING A MAINTENANCE VISIT, FOUND SKIN CORRODED PAST LIMITATIONS IAW DC-8 SRM, AT Y=678 TO Y=680 AND BETWEEN LONGERON 30 RIGHT TO 31 RIGHT. INSTALLED REPAIR IAW DER APPROVED ENGINEERING SKETCH B21-R20, TREATED AREA IAW DC-8 SRM 51-1-8.SDR RRXA96137Skin · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO SKIN PAST LIMITATIONS IAW DC-8 SRM, AT Y=640 BETWEEN LONGERON 30 RIGHT AND LONGERON 32 RIGHT. INSTALLED REPAIR IAW DER APPROVED ENGINEERING SKETCH B21-R06, TREATED AREA IAW DC-8 SRM 51-1-8.SDR UPS96821166Track · corrosionINSPECTION TYPE-CS2, LT WING FLAP STA 410 TRACKS PITTED. REPLACED TRACKS PER MM 27-51-03.SDR UPS96821063Ribs · crackedINSPECTION TYPE CS2, LT WING LEADING EDGE ASSY 1 EA RIBS CRACKED AT WS XFS 580, XFS 620, 4 EA RIBS CRACKED AT WS XFS 766, 3 EA RIBS CRACKED AT WS XFS 800 AND 2 EA RIBS CRACKED AT WS XFS 820. REPAIRED RIBS PER MM 57-00-00 FIG 801.SDR UPS96821057Track · corrosionINSPECTION TYPE CS2, NR 3 SEAT TRACK AT FS 1342 HAS MODERATE CORROSION. REPAIRED SEAT TRACK PER SRM 53-2-3.SDR RRXA96146Frame · corrodedDURING A MAINTENANCE VISIT, FOUND FRAME CORRODED PAST LIMITATIONS IAW DC-8 SRM, AT Y=1020 AND BETWEEN LONGERON 35 LEFT TO 35 RIGHT. INSTALLED REPAIR IAW DER APPROVED ENGINEERING SKETCH B21-R09.SDR RRXA96129Frame · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE UNDER NUTPLATES ON FRAME PAST LIMITATIONS IAW DC-8 SRM, AT Y=1140 BETWEEN LONGERON 33 LEFT AND LONGERON 33 RIGHT. INSTALLED REPAIR IAW DER APPROVED ENGINEERING SKETCH, TREATED AREA IAW DC-8 SRM 51-1-8.SDR DHL96804011Yaw Damper · malfunctionedAFTER TAKEOFF, RUDDER BEGAN EXTREME OSCILLATION. AFTER YAW DAMPER DISENGAGED, OSCILATION STOPPED. DEFERRED PER MEL.SDR UPS96821170Track · corrosionINSPECTION TYPE-CS2, MODERATE CORROSION DAMAGE ON RT WING STA 219 FLAP TRACKS. REPLACED TRACKS PER MM 27-51-03.
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