Douglas DC-8-71F
Service difficulty reports · 8,938
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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 IXXA06RNG027SSkin · crackedDURING ROUTINE C CHECK, FOUND A CRACK ON THE RUDDER FAIRING SKIN DRAIN HOLE AT STATION ZR 81.625 LEFT HAND. DAMAGED SKIN SECTION WAS REPAIRED IAW EWO ATI 55-017 AND DOUGLAS DRAWING 5655074. THIS REPAIR CONSTITUTES A MINOR REPAIR.SDR IXXA06RNG019SVane · elongatedDURING ROUTINE C CHECK, FOUND ELONGATED HOLES ON EXTENDED LEADING EDGE OUTBOARD VANE, STATION XOLDI 6.224 RIGHT HAND. DAMAGED WAS REMOVED, REPAIR DOUBLER AND FILLERS WERE FABRICATED AND INSTALLED IAW EWO ATI 57-072. FAA FORM 8110-3 WAS ISSUED APPROVING THIS SDR IXXA06RNG005SSkin · crackedDURING ROUTINE C CHECK FOUND A CRACK ON CENTER EXTENDED LEADING EDGE AROUND LOWER SKIN STATION XOLDI 6.225 - RIGHT HAND. RIGHT HAND WING CENTER LEADING EDGE WAS REMOVED IAW DC8 AMM 57-20-02 PAGE 203, REPAIRED OUTER SKIN IAW EWO ATI 57-069 AND INSTALLED RT WINSDR IXXA06RNG017SSkin · canningDURING INSPECTION CHECK FOUND A OIL CAN ON RT ELEVATOR LOWER SURFACE, STA XE 246.875 TO XE 258.896. REMOVED AND REPLACED RT ELEVATOR LOWER SKIN IAW DOUGLAS DRAWING 5654970. ACCOMPLISHED WEIGHT AND BALANCE IAW DC8 SRM 51-4-4 TR 51-116 PAGE 2.SDR IXXA06RNG012SSkin · corrodedDURING INSPECTION CHECK FOUND CORROSION ON FUSELAGE SKIN BETWEEN STA 340 TO 360, LONGERON 32 RT TO 32 LT. CORRODED AREA WAS REMOVED AND EXTERNAL DOUBLER, FILLER DOOR JAMB INNER SKIN AND SPLICE WERE FABRICATED AND INSTALLED IAW EWO ATI 53-042. FAA FORM 8110-3SDR IXXA06RNG004SSkin · crackedDURING A C-CHECK INSPECTION FOUND A CRACK ON CENTER EXTENDED LEADING EDGE AROUND LOWER SKIN XFS 341.000 RT. REPAIR DOUBLER AND ALUMINUM FILLER WERE FABRICATED AND INSTALLED IAW EWO ATI 57-068. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.SDR IXXA06RNG003SSkin · crackedDURING A CHECK INSPECTION FOUND TWO CRACKS ON CENTER EXTENDED LEADING EDGE AROUNG LOWER SKIN A STA XFS 304.000 RT. REPAIR DOUBLER AND ALUMINUM FILLER WER FABRICATED AND INSTALLED IAW EWO ATI 57-067. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.SDR IXXA06RNG002SSkin Panel · crackedDURING C-CHECK INSPECTION FOUND A CRACK ON INBOARD PYLON STUD EXTENDED EDGE UPPER, AROUND STA XS 250.089 LT. DAMAGED AREA WAS REMOVED AND REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW EWO ATI 57-066 & EWO DRAWING ATI 57-066. FAA FORM 8110-3 WAS ISSUED APPROSDR IXXA06RNG043SFitting · crackedDURING ROUTINE C CHECK, FOUND A CRACK ON RIGHT MAIN LANDING GEAR FITTING, LONGERON 24, STATION 879.000. FITTING WAS FABRICATED IAW DOUGLAS DRAWING 3641004 AND INSTALLED IAW SRM 51-3-0 PAGE 1-4 AND SRM 51-1-20D.SDR IXXA06RNG020SSupport Bracket · corrodedDURING ROUTINE C CHECK, FOUND CORROSION AND ONE SCRATCH ON MAIN LANDING GEAR RETRACT BRACKET LEFT HAND. CORRODED AREA WAS REPAIRED IAW EWO ATI 57-073 AND AMM 57-40-1 PAGE 801. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.SDR IXXA06RNG015SSkin · corrodedDURING ROUTINE C CHECK, FOUND TWO AREAS OF CORROSION OUT OF LIMITS ON OUTER OUTBOARD EXTENDED LEADING EDGE UPPER SKIN, STATION XFS 722 - 835, LEFT HAND. DAMAGED AREA WAS REMOVED AND REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW EWO ATI 57-071 AND SRM 57-2-1SDR IXXA06RNG001SSkin · misrepairedDURING A ROUTINE C-CHECK INSPECTION FOUND A TEMPORARY REPAIR ON INBOARD EXTENDED LEADING EDGE AROUND STA XFS 51.250 TO 57.500 LT. IMPROPER REPAIR WAS REMOVED AND NEW REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW EWO ATI 57-065. FAA FORM 8110-3 WAS ISSUED ASDR UPS06846679Door Frame · crackedINSPECTION TYPE:C3 VISUAL AND HFEC INSP DETECTED A CRACK APPROX .125" ON THE L-2 DOOR UPPER FWD DOOR JAMB CORNER EXTENDING FROM FASTENER. CUT OUT DAMAGE AT L-2 DOOR UPPER FWD DOOR JAMB CORNER IAW SRM 53-02-00 FIG 18. FABRICATED AND INSTALLED FILLER, DOUBLER,SDR UPS06846711Fairing · corrodedINSPECTION TYPE:C3 LT STA 98 CANOE CORRODED UNDER BOTH FLAP TRACKS. REMOVED LT STA 98 FLAP CANOE IAW DC8-MM 27-51-12. REMOVED CORROSION BY MACHINING IAW SB 27-164. FABRICATED AND INSTALLED SHIMS IAW SB 27-164. INSTALLED FLAP CANOE AT STA 98 LT IAW DC8- MM SDR UPS06846718Stringer Clip · crackedINSPECTION TYPE:C2 CRACKED STRINGER CLIP ON OTBD SKATE ANGLE C/S-STRINGER 62 NR 4 MAIN TANK. REMOVED CRACKED CLIP AT OTBD SKATE ANGLE C/S STRINGER 62 NR 4 MAIN TANK IAW SRM 51-01-20D. FABRICATED AND INSTALLED CLIP ON O/B SKATE ANGLE C/S STRINGER 62 34 MAIN TSDR UPS06846598Longeron · crackedFOUND LONGERON SPLICE L36 STA 1260-1280 IS CRACKED. REMOVED AND REPLACED LONGERON SPLICE FITTING AT STA 1260-1280 L36 IAW SRM 51-1-20D, AND 51-1-8.SDR UPS06846491Light · no testFOUND EMERG EXIT LIGHTS WILL NOT TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM 33-50-01-2.SDR UPS06846719Fitting · crackedINSPECTION TYPE:C3 STA 98 FLAP ACTUATOR REAR SPAR FITTING O/B LUG FOR SUPPORT LINK ARM IS BROKEN. FABRICATED AND INSTALLED NEW FITTING FROM 7050-T7451 PER AMS 4050 PLATE IAW UPS ENG FILE # DC8-57-20160, SAA EA#008-2760-01- A0133 REV A, DOUGLAS PSAMSL DWG 7981SDR UPS06846709Fairing · corrodedINSPECTION TYPE:C3 FLAP STA 98FH, CORROSION FOUND ON CANOE UNDER FLAP TRACKS. REMOVED STA 98 RH FLAP CANOE IAW DC8-MM 27-51-12. REMOVED CORROSION FROM FLAP CANOE IAW SB 27-164. FABRICATED AND INSTALLED SHIMS IAW SB 27-164. INSTALLED FLAP CANOE AT STA 98 RTSDR UPS06846680Splice · corrodedA-PIT TORQUE BOX STA 280-270 LONGERON 34L-35L FITTING HAS CORROSION. REMOVED BATH TUB FITTING AT STA 280, AND REMOVED LONGERON SPLICE FITTING AT STA 270-280 L35L IAW SRM 51-1-20, AND SRM 53-2-2 FIG 10 LOCATED AND DRILLED AND INSTALLED NEW LONGERON SPLICE FITTSDR UPS06846597Longeron · crackedINSPECTION TYPE:C3 LONGERON 15R IS CRACKED WHERE VERTICAL STAB ATTACHES STA 1740. REMOVED CRACKED LONGERON SECTION AT STA 1730-1750 15R IAW SRM 51-01-21-0 AND SRM 53-02-02-0. FABRICATED AND INSTALLLED LONGERON SPLICE SECTION AT STA 1730-1750 L15R IAW SRM 53-SDR UPS06846518Rib · crackedINSPECTION TYPE:C3 LT CENTER LE XRS 323 RIB IS CRACKED AT AFT UPPER END. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-02-0, 57-3-1 AND 51-01-20D.SDR IXXA060173OSensor · inoperativeAPPROX 2 HRS INTO FLT ACFT ENCOUNTERED MOUNTAIN WAVE EFFECT AND INCREASING AIRSPEED WHEN POWER WAS REDUCED. NR 4 ENGINE POWER ROLLED BACK TO IDLE AND WOULD NOT RESPOND TO THROTTLE. PERFORMED PRECAUTIONARY SHUTDOWN AND DESCENDED. ON DESCENT PERFORMED IN FLIGSDR IXXA060172OFire Detector · shortedAT CRUISE FL 36.0 NR 3 ENGINE SHORT CIRCUIT LIGHT BEGAN FLASHING. FIRE WARNING WOULD NOT TEST, ENGINE SHUTDOWN PER COM PROCEDURE. THE CREW ELECTED TO RETURN THE AIRCRAFT TO TOL AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED CONNECTOR FROM FORWARD SIDE OF SDR UPS06846415Bulb · inoperativeEMERGENCY LIGHT OVER MAIN ENTRY DOOR HAS BULBS INOP. RELAMPED. OPS CK'S GOOD.SDR UPS06846411Trim Tab · crackedINSPECTION TYPE:N/A RT ELEV TRIM TAB CRACKED/DAMAGED ABOUT 1' OB OF PREVIOUS REPAIR. REMOVED RT ELEV GEAR TAB REF MM 27-30-03-2. OK TO INSTALL. TRIMMED OTBD EDGE OF RT ELEVATOR GEARED TRIM TAB PER EO DC8-5520-23895A AND INSTALLED TRIM TAB IAW MM 27-30-03. OPS SDR UPS06846442Repair · misinstalledC-2 DOOR JAMB UPPER AFT CORNER REPAIR DOES NOT MEET REQUIREMENTS OF SRM 53-2-0, AND DWG SRO 8530019. REMOVED EXISTING DOUBLER ON C-2 DOOR JAMB UPPER AFT CORNER IAW SRM 53-2-0 FIG 20, FABRICATED AND INSTALLED FILLERS DOUBLER AND TRIPLER IAW SRM53-02-00 FIG 20 SDR UPS06846327Light · inoperativeEMERGENCY EXIT LIGHTS INOP. TRANSFERRED TO UPS NRC 814597. R&R EMERG BATT PACK IAW MM 33-50-01-2. OPS CK FAILED. OPENED EMER LT BATT ACCESS PNL. REPAIRED 2 BROKEN WIRES AT CONNECTOR. OPS CK FAILED R&R BATT PACK IAW MM 33-50-01-2. OPS CK GOOD. CLOSED ACCESS SDR IXXA060171OConnector · corrodedDURING FLIGHT 834 FROM TOL TO SJC APROX 50 MIN INTO FLIGHT, NR 3 ENG SHORT CIRCUIT AMBER LIGHT CAME ON. PERFORMED ABNORMAL CHECK LIST. THE LIGHT DID NOT EXTINGUISH, NOR DID THE FIRE WARNING TEST. PERFORMED ENGINE SHUTDOWN OTHER THAN FIRE DAMAGE. THE CREW ESDR UPS06846401Door Frame · gougedINSPECTION TYPE:C1 D-PIT AFT LOWER DOOR SURROUND FRAME FITTING HAS DEEP GOUGE. REMOVED AND REPLACED FRAME FITTING IAW SRM 51-3-0.SDR UPS06846318Battery Pack · inoperativeINSPECTION TYPE:N/A DURING PREFLIGHT FOUND EMERGENCY LIGHTS INOP. REPLACED BATTERY/RELAY PACK IAW MM 33-50-01.SDR UPS06846438Spar Cap · crackedRT WW LWR SPAR CAP CRACKED 1/2" LONG AT STA 857.125. STOP DRILLED CRACK AT AT RT WW LWR SPAR CAP IAW SRO 8570009 INSTALLED -47 PLUG IN WING SKIN, FABRICATED AND INSTALLED REPAIR ANGLES, AND -66 SPACER IAW SRO 8570009, AND SRM 51-1-20D AT STA 857.125 RT WW LWRSDR UPS06846437Attach Fitting · crackedINSPECTION TYPE:C1 LONGERON ATTACH FITTING CRACKED AT STA 1240 L33R. REMOVED AND REPLACED LONGERON ATTACH FITTING AT STA 1240 L33R IAW SRM 51-1-20D, AND SRM 51-1-8.SDR UPS06846435Frame · gougedC-PIT STA 1140 FRAME UPPER FLANGE ABOVE LONGERON 34R HAS DEEP, LONG DRILL WALK. REMOVED AND REPLACED FRAME UPPER CAP IAW SRM 20-15-00-2,51-3-2 AND 51 -1-20D.SDR UPS06846439Bulkhead · corrodedINSPECTION TYPE:C1 IN 60 HOLE CORROSION ON WEB UNDER L-ANGLE OF BULKHEAD JUST AFT OF HOLE ENTRANCE. REMOVED CORRODED WEB AND ANGLE AT STA 1788 IAW SRM 53-02-00-0. FABRICATED AND INSTALLED REPAIR WEB AND ANGLE AT STA 1788 IAW SRM 53-02-00-0, 53-05-03-0, AND SSDR UPS06846405Fitting · corrodedINSPECTION TYPE:C1 IN 60 HOLE, FRAME FITTING ON FIRST LATERAL FRAME SUPPORT RT CENTER ABOVE ENTRANCE HAS BAD CORROSION AROUND FASTENERS. REMOVED AND REPLACED FITTING IAW SRM 51-1-21, 51-1-20D AND DWG 3753645.SDR UPS06846404Support Channel · brokenINSPECTION TYPE:C1 STA 360 L34L FLOOR SUPPORT CHANNEL BROKEN. REMOVED, FABRICATED AND INSTALLED SUPPORT CHANNEL IAW SRM 51-1-21 AND DWG 9759429.SDR UPS06846338Web · crackedFOUND PIT SLIDING CARGO DOOR TORQUE BOX UPPER WEB CRACKED STA 1220 L33L. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-02-00, AND 51-1-21.SDR UPS06846407Finger Doubler · corrodedINSPECTION TYPE:C1 AFTER SKIN REMOVAL FOUND FINGER DOUBLER CORRODED OUT OF LIMITS AND CRACKED STA 1350 - 1390 L31R. REMOVED, FABRICATED AND INSTALLED FINGER DOUBLER IAW SRM 53-04-01-0, 51-1-20D.SDR UPS06846406Shear Tie · corrodedINSPECTION TYPE:C1 AFTER REMOVAL OF SKIN FOUND SHEAR TIE CORROSION OUT OF LIMITS AND CRACKED AT STA 1400 BETWEEN L35R- L36. REMOVED, FABRICATED AND INSTALLED SHEAR TIE IAW SRM 51-1-21, 51-1-20D, 53-02-33.SDR UPS06846398Shear Tie · crackedINSPECTION TYPE:C1 AFTER REMOVAL OF SKIN FOUND SHEAR TIE CORRODED OUT OF LIMITS AND CRACKED AT STA 1380 BETWEEN L31L-L32L. REMOVED, FABRICATED AND INSTALLED SHEAR TIE IAW SRM 53-04-01 FIG 51, 51-1-20D AND 51-1-21.SDR UPS06846397Shear Tie · crackedINSPECTION TYPE:C1 AFTER REMOVAL OF SKIN FOUND SHEAR TIE CORRODED OUT OF LIMITS AND CRACKED AT STA 1440 BETWEEN L33R-L34R. REMOVED, FABRICATED AND INSTALLED SHEAR TIE IAW 53-04-01 FIG 51, 51-1-20D AND 51-1-21.SDR UPS06846358Shear Tie · corrodedAFTER SKIN REMOVAL FOUND SHEAR TIE CORRODED OUT OF LIMITS AND CRACKED AT STA 1380 L35R-L36. REMOVED SHEAR TIE AT STA 1380 L35R-L36 IAW SRM 51-1-21. FABRICATED AND INSTALLED SHEAR TIE AT STA 1380 L35R-L36 IAW SRM 53-02-00-0, 51-1-8, SRM 51-1-21, 51-1-20D.SDR UPS06846357Shear Tie · corrodedAFTER REMOVAL OF SKIN FOUND SHEAR TIE CORRODED OUT OF LIMITS AND CRACKED AT STA 1380 L34L AND L35L. REMOVED SHEAR TIE AT FS 1380 L34L-L35L IAW SRM 51-01-20D. FABRICATED AND INSTALLED SHEAR TIES AT STA 1380 L34L-L35L IAW SRM 53-02-00-0, 51-1-8, AND SRM 51-1-2SDR UPS06846332Keelbeam · crackedFITTING CRACKED ON RT CORNER IN RADIUS OF KEEL BEAM STA 960. REMOVED AND REPLACED L ANGLE AT STA 960 RT IAW SRM 51-1-2OD, 51-1-15 AND SRM 51-3-0.SDR UPS06846436Floorbeam · corrodedINSPECTION TYPE:C1 IN A/C COMPT CEILING, FLOORBEAM STA 50 BETWEEN RBL 10-25 HAS CORROSION. REMOVED CORRODED UPPER FLANGE OF FLOORBEAM AT STA 50 RBL 10 -25 IAW SRM 51-1-8, AND SRM 53-2-0 FIG 1F. FABRICATED AND INSTALLED REPAIR FLANGE, REPAIR ANGLE AND REPAIR SDR UPS06846402Attach Fitting · corrodedINSPECTION TYPE:C1 FRAME ATTACH FITTING HEAVY CORRODED AT STA 834.500 L22R. REMOVED AND REPLACED FRAME ATTACH FITTING IAW SRM 51-1-20D.SDR UPS06846340Fitting · crackedFOUND FRAME ATTACH FITTING CRACKED AT STA 822.500 L22L AFT SIDE. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D, 53-1-0 AND 51-3-2.SDR UPS06846335Longeron · crackedFOUND POSSIBLE CRACK ON LONG 32L AT FS 1440. REMOVED DAMAGED LONGERON FROM STA 1350-1490, FABRICATE AND INSTALLED REPLACEMENT LONGERON SECTION IAW SRM 51-1-20D, 51-3-2 AND DWG 3645897.SDR UPS06846444Fitting · crackedFOUND FITTING CRACKED AT STA 700 L13R FWD SIDE. REMOVED CRACKED FITTING AT STA 700 L13R IAW SRM 51-1-20D. FABRICATED AND INSTALLED FITTING AT STA 700 L13R IAW DWG 3779978, AND SRM 51-1-20D.
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