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 UPS98826656Seat Track · corrodedINSPECTION TYPE:C, STA 45 TRACK A CORROSION REMOVED FLOOR PANEL 1 AFS 70 TO FS 280. REMOVED CORRODED SEAT TRACK A FS 570 TO FS 280. PUT NEW SEAT TRACK, DRILLED HOLES IAW DC8 SRM 5 1 1 24. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED NEW SEAT TRACKSDR UPS98826653Angle · crackedINSPECTION TYPE:C, RIGHT HAND WING REAR SPAR I/B AILERON I/B CENTER HINGE FITTING ATTACH ANGLE BENT AND CRACKED. REMOVED CRACKED ANGLE FABBED NEW ONE ON TPA 1003 REV A INSTALLED IAW DC8 SRM 51 3 0.SDR UPS98826647Fitting · corrodedINSPECTION TYPE:C/CK, STA 1230 LONGERON 35 RIGHT TO LONGERON 36 Z FITTING CORRODED. REMOVED FITTING CUT AND INSTALLED NEW FITTING WITH SPLICES IAW DC8 SRM 53 2 0 AND 51 1 8 AND 51 1 20D.SDR UPS98826646Former · corrodedINSPECTION TYPE:C, AFT PIT FORMER CORRODED STA 1080, L36 TO 35L. REMOVED CORROSION, FABBED STRAP REPAIR AND SAM IAW REO 04666 AND DC.SDR UPS98826629Fitting · crackedINSPECTION TYPE:C/CK, Z FITTING CRACKED STA 1150 LONGERON 33 RIGHT TO 34 RIGHT. REMOVED Z FITTING CUT NEW FITTING AND FABBED SPLICES IAW DC8 SRM 53 2 0 FIG 2G. INSTALLED IAW DC8 SRM 51 1 20D.SDR UPS98826623Seat Track · corrodedINSPECTION TYPE:C/CK CORROSION IN SEAT TRACK D BETWEEN FS 480 AND 500. REMOVED 4 HOLE PLUG AND ROUTED OUT FOR NEW 5 HOLE PLUG IAW DC8 SRM 53 2 3. ALODINED AND PRIMED IAW DC8 SRM 51 1 8 PUT 5 HOLE PLUG IAW DC8 SRM 53 2 3. INSTALLED FASTENERS IAW DC8 SRM 51 SDR UPS98826617Fitting · crackedINSPECTION TYPE:C/CK MAIN CABIN STA 900 TO 920 LONGERON 7L END FITTING CRACKED. REMOVED OLD FITTING FROM AC LOCATED AND DRILLED NEW FITTING IAW DC 8 SRM 51 3 2. INSTALLED NEW FITTING IAW DC8 SRM, 51 3 0.SDR UPS98826608Former · corrodedINSPECTION TYPE:C/CK AFT PIT STA 1060 AND LONGERON 36 FORMER CORRODED. REMOVED FORMER FABRICATED NEW ONE IAW DWG DC8 53 0229 AND DC8 SRM 51 1 8. INSTALLED IAW DAC DWG 53 0229.SDR UPS98826595Skin · crackedINSPECTION TYPE:C/CK CRACKED SKIN AT RIGHT WING LEADING EDGE AUX FUEL TANK LOWER SURF XFS 157.5. FABRICATED NEW DOUBLER AND FILLER IAW DC8 SRM 57 2 0. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED NEW DOUBLER AND FILLER IAW DC8 S RM 51 1 20D.SDR UPS98826594Angle · crackedINSPECTION TYPE:C/CK FLOOR SUPPORT ANGLE AT FS 46 IS CRACKED IN AREA BETWEEN LBL 50 TO LBL 62. FABRICATED FLOOR SUPPORT ANGLE AND ANGLE REPAIR IAW DC8 SRM 53 7 1. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED IAW DC8 SRM 51 1 2 0D.SDR UPS98826678Fitting · crackedINSPECTION TYPE:C/CK, LONGERON END FITTING CRACKED, 27 LEFT AT AFT PRODUCTION SPLICE. INSTALLED NEW FITTING IAW DC8 SRM 51 1 24 AND 51 1 20D AND 51 1 21 A ND 51 3 0.SDR UPS98826677Skin · crackedINSPECTION TYPE:C/CK, LEFT ELEVATOR UPPER SKIN HAS 1 CRACK 2 INCHES AFT OF SPAR AT STA XE77 STOP DRILLED CRACK. FAB REPAIR IAW DC8 SRM 55 2 1 FIG 7. ALODINED AND PRIMED IAW DC8 SRM 51 1 8 AND INSTALLED IAW DC8 SRM 51 1 21A.SDR UPS98826654Skin · corrodedINSPECTION TYPE:C, LT ELEVATOR LOWER SKIN CORRODED AROUND FASTENER AT CLOSING CHANNEL STA XE 310. MRR FILED OPEN NO CORECTIVE ACTION.SDR UPS98826628Skin · crackedINSPECTION TYPE:C/CK, RIGHT WING LEADING EDGE SKIN CRACKED AT XFS 219.5. CUT OUT DAMAGED AREA IN SKIN AND FABRICATED REPAIR FILLER AND DOUBLER IAW DC8 SRM 57 2 1. ALODINED AND PRIMED REPAIR PART A/C STRUCTURE IAW DC8 SRM 51 1 8. INSTALLED REPAIR IAW DC8 SRMSDR UPS98826627Skin · crackedINSPECTION TYPE:C/CK, OUTBOARD SIDE OF PYLON NR 1 CRACKED. REPAIRED PER EO 04609 AND DC8 SB 54 95 BY INSTALLING REPAIR DOUBLERS.SDR UPS98826593Angle · crakcedINSPECTION TYPE:C/CK RIGHT HAND FWD EMERGENCY EXIT DOOR INNER SUPPORT ANGLE CRACKED. FABRICATED NEW ANGLE IAW DC8 SRM 52 7 1 HEAT TREATED 0807075-0 TO 0 80 7075 T6 IAW DC8 TPS 1003 REV A. ALODINED AND PRIMED IAW DC8 SRM 51 1 8 INSTALLED IAW DC8 SRM 51 3 0.SDR UPS98826655Rib · crackedINSPECTION TYPE:C, INNER RIB BETWEEN MLG DOORS FS 960 HAS CRACKS. REMOVED RIB FABBED NEW ONE ON DAC DWG 5616306, INSTALLED IAW DC8 SRM 51 1 4 AND 51 1 20D.SDR UPS98826609Fitting · crackedINSPECTION TYPE:C/CK ZEE FITTING AT FS 1160, LONGERON 34 RIGHT TO LONGERON 33 RIGHT CRACKED. REMOVED FITTING DRILLED NEW ONE IAW DC8 SRM, 53 2 0 FIG 2G WITH SPLICES. INSTALLED IAW DC8 SRM 51 1 20D.SDR UPS98826616Bracket · crackedINSPECTION TYPE:C/CK PERMANENT REPAIR TO LEFT HAND WING INBBOARD SPOILER BRACKET PER REO DC8 5720 6998. FABRICATED REPAIR ANGLES ALODINED AND PRIMED AND INSTALLED REPAIR IAW REO DC8 5720 6998, DC8 SRM 57 2 0 FIG 2 AND DC8 SRM 51 1 8.SDR UPS98826361Doubler · corrodedCORROSION ON INNER DOUBLER BELOW EXT AIR CONDITIONING RECEPTACLE ON RT SIDE ABOVE FWD E/E COMP. REMOVED CORROSION ON INNER DOUBLER. ACCOMPLISHED EO DC8-5330-8942-D INTERM REPAIR.SDR RRXA98075Resistor · overheatedON LANDING, NR 4 GEN UNPARL'D LIGHT AND BUS POWER FAIL LIGHT ON, SMOKE IN COCKPIT. FOUND NR 4 25 WATT RESISTOR OVERHEATED, ENTERED AS DMI NR 803339 IAW MEL 24-1 CAT C DUE DATE 4-6-98 PLACARD INSTALLED. *S/D* SERVICED OIL CAVITIES ON NR 4 CSD/GEN ASSY. RESESDR UPS98826178Engine · failedNR 4 ENGINE FLAMEOUT AT FL350, SUCCESSFUL RESTART WITH MILD VIBRATION. FLAMEOUT WITH THROTTLE ADVANCE. FIRE TEST INDICATED SHORT CIRCUIT, MA N-O-TEMP(270DEG. C). NR 4 BLEED OFF, TEMP DECREASE ENG FIRE, SEVERE DAMAGE CHECKLIST ACCOMPLISHED. DISCHARGED BOTH SDR UPS98826173Support Frame · crackedINSPECTION TYPE-N/A, STEP PLATE SUPPORT FRAME IS CRACKED IN 3 PLACES AT NR 4 PIT DOOR OPENED FOR OTHER MAINT, SEE CONTROL ITEM UPS98826172. TRANS TO N\R CARD 75992. FABRICATED NEW CHANNEL SUPPORT FRAME AND INSTALLED PER SRM 53-1-0 COMPLETED NON-ROUTINE 72559SDR UPS98826172Skin · crackedINSPECTION TYPE-N/A, FOUND SKIN BULGED AND CRACKED 2 INCHES FWD OF NR 4 PIT DOOR LOWER FWD CORNER DOUBLER. ALSO, BULGE IN SKIN WITH RIVET PULLED THROUGH AFT CORNER NR 4 PIT DOOR SCUF GAURD AREAS MARKED. NR OPENED AGAINST THIS ITEM. COMPLETED NON ROUTINE 725SDR UPS98826165Battery Pack · dischargedINSPECTION TYPE-W/E, EMERGENCY EXIT LIGHTS INOP ON WEEKEND CHECK. REPLACED RECHARGEABLE BATTERY PACK ASSY.SDR RRXA98069Controls · malfunctionedIN FLIGHT THERE WAS A LARGE DEAD SPOT IN THE AILERONS IN THE CENTER/NEUTRAL POSITION. IN FLIGHT THE AIRPLANE ROLLS LEFT AND RIGHT. TO STOP OR CONTROL THE ROLL YOU HAVE TO DO A DUTCH ROLL TYPE OF MANUVER TO CONTROL THE ROLL. INSPECTED CONTROL SURFACES, CABLESDR RRXA98068Switch · out of adjustON FINAL APPROACH, LT MAIN GEAR LIGHTS DIDN'T COME ON. RECYCLED GEAR NO LIGHTS, REPLACED BULBS, STILL NO LIGHTS, RECYCLED GEAR NO LIGHTS, REPLACED BULBS A SECOND TIME AND LT MAIN GEAR LIGHTS WORKED. EMERGENCY EQUIPMENT STANDING BY. ON GROUND TEST OF OLD BULSDR IXXA9800017Cowl · damagedDURING LANDING, THE NUMBER ONE ENGINE SUSTAINED A GROUND STRIKE WITH MINOR DAMAGE TO THE FORWARD FAN COWLINGS, DRAIN MAST AND THE ACCESSORY GEARBOX COVER. A MANUFACTURER SUPPORT TEAM WAS CALLED IN TO PERFORM AN ENGINE BORESCOPE AND GEARBOX FPI INSPECTION, WHISDR UPS98826160Angle · corrodedINSPECTION TYPE-C, FLOORBEAM ATTACH ANGLE AT STA 780 HAS HEAVY CORROSION AND IS CRACKED. REMOVED AND REPLACED ATTACH ANGLE AT STA 780 RBL 45 TO 69 IAW DWG 3643111 AND SRM 51-1-20D.SDR UPS98826092Fitting · corrodedINSPECTION TYPE:C F/S 1690 LONGERON 28L. LONGERON TO FRAME FITTING IS EXFOLIATED. REMOVED AND REPLACED FITTING IAW SRM 51-1-21.SDR UPS98826122Fitting · crackedINSPECTION TYPE-C, STA 1160 AND STR 33R AND 34R SHEAR TIE IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 FIG 2D.SDR UPS98826120Fitting · crackedINSPECTION TYPE-C, AFT FUSELAGE TAIL SKID FITTING IS CRACKED AT BOTH END BOLT HOLES AT STA 1750 BL 0. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.SDR UPS98826118Fitting · crackedINSPECTION TYPE-C, BOTH TAIL SKID BACKUP FITTINGS CRACKED AT FS 1766. REMOVED, FABRICATED, AND REPLACED FITTINGS IAW SRM 51-3-0 AND DWG 3750866.SDR UPS98826115Frame · corrodedINSPECTION TYPE-C, FS 1480 LWR FRAME CORRODED BEYOND LIMITS BETWEEN LONG 35R TO 36. REPAIRED IAW SRM 53-2-0.SDR UPS98826071Shear Tie · crackedINSPECTION TYPE-C, SHEAR TIE CRACKED FS 1200 STR 33R TO 34R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.SDR UPS98826004Skin · crackedNR 4 PIT DOOR FRAME SKIN CRACKED IN UPPER AFT CORNER EO DC8-5330-4067A ISSUED. INSTALLED TEMP REPAIR TO DOOR JAM CORNER PER EO DC-8 5330-4067.SDR UPS98825982Angle · corrodedINSPECTION TYPE-C, RT WING T/E SPAR AT XW 408 LOWER SPLICE ANGLE IS EXFOLIATED. REMOVED AND REPLACED SPLICE ANGLE IAW SRM 51-3-0.SDR UPS98826117Skin · corrodedINSPECTION TYPE-C, FS 1690 TO 1890 REMOVE AND REPLACE TAIL SKID LWR SKIN DUE TO CORROSION. REMOVED AND REPLACED SKIN IAW SRM 51-1-21.SDR UPS98826114Doubler · crackedINSPECTION TYPE-C, FS 640 BETWEEN LONG 35R AND 35L INTERNAL DOUBLER IS CRACKED. REPAIRED IAW DHC SK-707-712.SDR UPS98826085Splice · crackedINSPECTION TYPE-C, SPLICE FITTING AT LONG 24L FS 1350 CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT IAW SRM 51-1-20D AND DWG 4646163.SDR UPS98826078Seat Track · corrodedINSPECTION TYPE-D/CK, SEAT TRACK F FUSELAGE STATION 1440 CORRODED. REMOVED SEAT TRACK SECTION FUSELAGE STATION 1430 TO 1450, CUT AND DRILLED NEW SECTION AND INSTALLED SECTION IAW DC8 SRM 51-1-8, 51-3-0, 53-1-2 AND EO DC8 5320 5167.SDR UPS98826073Shear Tie · crackedINSPECTION TYPE-C, AFT PIT FS 1520 SHEAR TIE BETWEEN LONGERONS 31L TO 32L LEFT SIDE IS CRACKED. REPAIRED IAW SRM 53-2-0.SDR IXXA9800044Frame · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS FOUND ON FUSELAGE FRAME AT FUSELAGE STATION 70 BETWEEN LONGERONS 32 AND 33 RIGHT. REPAIR WAS ACCOMPLISHED BY CORROSION REMOVAL, FABRICATION AND INSTALLATION OF A NESTED ANGLE REPAIR DOUBLER IN ACCORDANCE WITH FSDR UPS98826113Fitting · corrodedINSPECTION TYPE-C, CORROSION BETWEEN BATHTUB FITTING AND SKIN AT STA 1160 BETWEEN STR 34R AND 35R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.SDR UPS98826068Doubler · corrodedINSPECTION TYPE-C, LWR INTERNAL DOUBLER CORRODED FS 1766 LBL 3. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21 AND DWG 5649329.SDR UPS98826061Fitting · crackedINSPECTION TYPE-C, BATHTUB FITTING IS CRACKED AT FS 1200 BETWEEN STR 34R AND 35R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.SDR UPS98825999Rib · crackedINSPECTION TYPE:C LT WING L/E RIB AT STA XS 435.0 CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0.SDR IXXA9800047Plating · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON FUSELAGE EXTERNAL PLATING BETWEEN FUSELAGE STATIONS 30 AND 61 LONGERON 34 RIGHT. REPAIR ACCOMPLISHED BY REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR FILLER AND REPAIR DOUBLERS ISDR IXXA9800046Plating · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED AT THE LEFT FORWARD EMERGENCY EXIT DOOR LOWER AFT JAMB CORNER AT FUSELAGE STATION 418. REPAIR WAS ACCOMPLISHED BY REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF AN EXTERNAL REPAIR DOUBLER AND ASDR IXXA9800045Plating · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS FOUND ON THE FUSELAGE EXTERNAL PLATING AT FUSELAGE STATION 340 LONGERON 31 LEFT. REPAIR WAS ACCOMPLISHED BY CORROSION REMOVAL, FABRICATION AND INSTALLATION OF AN EXTERNAL REPAIR DOUBLER IN ACCORDANCE WITH FAA D
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