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 UPS08853736Repair · crackedINSPECTION TYPE:SV PERMANENT REPAIR TO PIT 32 DOOR INNER PAN CRACKED. REPAIRED 52-02-00.SDR IXX2008F00098Hydraulic System · lowDURING CRUISE FROM KSJC TO KRFD, FLT ENGINEER NOTICED HYDRAULIC QUANTITY INDICATOR WAS AT THE BOTTOM OF NORMAL QUANTITY, DID NOT DROP ANY FURTHER DURING THE REST OF THE FLT. THE CREW LANDED IN KTOL WITHOUT FURTHER INCIDENT. MX SERVICED HYDRAULIC SYS, OPS CHESDR UPS08853347Panel · crackedINSPECTION TYPE:N/A LEFT WING TRAILING EDGE PANEL CRACK.SDR IXX2008F00097Engine · flamed outDURING CRUISE, AT 36,000 FT WITH POWER REDUCTION NR 2 ENGINE FLAMED OUT WITH 1-2 PSI OIL PRESSURE ATTEMPTED INFLIGHT RESTART, NO FUEL FLOW AND NO IGNITION. THE CREW PERFORMED INFLIGHT ENGINE SHUTDOWN PROCEDURE. THE CREW LANDED WITHOUT FURTHER INCIDENT. MAINT ISDR IXX2008F00096Engine · flamed outDURING CRUISE AT 36,000 FT WITH POWER REDUCTION NR 2 ENGINE FLAMED OUT, WITH 1-2 PSI OIL PRESSURE ATTEMPTED INFLIGHT RESTART, NO FUEL FLOW AND NO IGNITION. THE CREW PERFORMED INFLIGHT ENGINE SHUTDOWN PROCEDURE. THE CREW LANDED WITHOUT FURTHER INCIDENT. OPEN (SDR UPS08853339Unknown · odorINSPECTION TYPE:N/A ATB - RETURNED TO YHM AFTER SMOKE SMELL IN C/P AT 2,000 FEET. COMPLIED WITH GENERAL INSPECTION AS PER DC8 MM CH 5-00-00, WITH NO DEFECT NOTED AT THIS TIME. ENG RUNS CARRIED OUT WITH GENERATORS AND PACKS ON. A/C OK FOR SERVICE. COULD NOTSDR IXX2008F00095Fire Warning · malfunctionedDURING CRUISE, NR 2 FIRE WARNING CAME ON INTERMITTENTLY. THE CREW SHUTDOWN NR 2 ENGINE, WAS UNABLE TO ACCOMPLISH FIRE WARNING TEST. THE CREW DISCHARGED 1 FIRE BOTTLE, ACCOMPLISHED FIRE WARNING TEST. SEVERAL MINUTES LATER NR 2 FIRE WARNING CAME ON AGAIN, THE SDR IXX2008F00094Connector · damagedDURING CRUISE, NR (2) FIRE WARNING LIGHT CAME ON STEADY, THE CREW SHUTDOWN NR (2) ENGINE AND DISCHARGED (1) FIRE BOTTLE, LIGHT WENT OUT. (20 MINUTES OUT, NR (2) FIRE WARNING LIGHT CAME BACK ON MOMENTARILY AND FIRE LOOPS WOULD ONLY TEST INTERMITTENTLY, THE CRSDR UPS08853314Stringer · crackedINSPECTION TYPE:C2 4ALT- STRINGER 51 CRACKED BETWEEN XM 408 AND XRS 463 ACESS THRU 505B. REMOVED AND REPLACED STRINGER SECTION IAW SRM 51-1-20D, 57-2-2 FIG 3D, 51-3-0.SDR IXX2008F00091Hose · leakingAT TOP OF DECENT, THE ACFT LOST HYDRAULIC FLUID DOWN TO THE STAND PIPE. MAINT INSPECTED AND FOUND NR 3 ENGINE HYDRAULIC PUMP HOSE LEAKING, REPLACED NR 3 ENGINE HYDRAULIC PUMP HOSE. OPS CHECK GOOD IAW MM 29-16. AC WAS RETURNED TO SERVICE. (K)SDR IXX2008F00090Hydraulic System · failedAT TOP OF DECENT, THE ACFT LOST HYDRAULIC FLUID DOWN TO THE STAND PIPE. OPEN. (K)SDR U2R2008F00009Skin · corrodedDURING C-CHECK INSP, FOUND FUSELAGE EXTERIOR FS 8.000, L-21R SKIN WITH BULGING AND CHERRY MAX RIVETS. (K)SDR U2R2008F00008Structure · crackedDURING C-CHECK INSP, FOUND LWR CARGO COMPARTMENT, STA 560.000 RT CUSP EXTRUSION WITH 2 INCH CRACK. (K)SDR U2R2008F00007Strap · crackedDURING C-CHECK INSPECTION, FOUND AFT SERVICE DOOR (R2) AFT UPPER JAMB CORNER WITH CRACK OF 0.800 LENGTH ON BEAR STRAP (AFTER ACCOMPLISHED X-RAY INSPECTION). (K)SDR U2R2008F00006Frame · corrodedDURING C-CHECK INSP, FOUND FWD CARGO COMPARTMENT F3 8.00 BTW L-24R FRAME WITH CORROSION. (K)SDR U2R2008F00005Stringer · crackedDURING C-CHECK INSP, FOUND RT WING X RS 202 NR 4 MAIN FUEL TANK STRINGER 67 HAS 2 INCH CRACK BY ACCESSORY PANEL NR 5050. (K)SDR U2R2008F00004Stringer · crackedDURING C-CHECK INSP, FOUND RT WING X RS NR 4 MAIN FUEL TANK STRINGER 58 HAS 2 INCH TRANSVERSAL CRACK BY ACCESSORY PANEL NR 5050. (K)SDR U2R2008F00003Support Angle · crackedDURING C-CHECK INSP, FOUND LT WING X RS 71, 5-52 NR 2 MAIN FUEL TANK INTERIOR LOWER SUPPORT ANGLE CRACKED. (K)SDR U2R2008F00002Bracket · crackedDURING C-CHECK INSP, FOUND LT WING NR 1 ALTERNATE FUEL TANK INTERIOR BOOST PUMP BRACKET FITTING (2) CRACKS. (K)SDR U2R2008F00001Skin · dentedDURING C-CHECK INSP, FOUND RT ELEVATOR XE117-594 LOWER SURFACE DENTED. (K)SDR IXX2008F00109Skin · misrepairedDURING ROUTINE C-CHECK INSPECTION, FOUND LOWER AFT FUSELAGE BELLY FWD OF AFT BASKET DOOR HAS IMPROPER REPAIR AT STA FS1142 LONGERON 35.5 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTSDR UPS08853297Fitting · crackedINSPECTION TYPE:C2 STRINGER 65 TO FRONT SPAR Z-FITTING CRACK AT NR 1 ALT THRU ACCESS PANEL 505B. REMOVE AND REPLACE Z-FITTING IAW SRM 51-1-8, 51-3-1, 51-1-24, 51-1-20 D.SDR UPS08853229Shear Tie · crackedINSPECTION TYPE:C2 AFTER REMOVAL OF EXISTING DOUBLER PER EO DC8-5330-27215 FOUND SHEAR TIE CRACKED AT STA 12 L21L-22L, HIDDEN UNDER DOUBLER. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-1-8, 51-1-20D, 51-1-21, 51- 3-1.SDR UPS08853334Doubler · crackedINSPECTION TYPE:C2 FUSELAGE EXTERIOR SKIN REPAIR DOUBLER IS CRACKED AT L1 DOOR HOLD OPEN PIN RECEPT 8. REMOVED, FABRICATED, AND INSTALLED REPAIR DOUBLER AT L1 DOOR HOLD OPEN PIN RECEPT IAW DC8 SRM 51-1-21, 51-1-8.SDR UPS08853276Longeron · corrodedINSPECTION TYPE:C2 D PIT CARGO COMPT STA 1540 RT LONG 30 HAS EXFOLIATING CORROSION. CUT OUT DAMAGED SECTION OF LONGERON AND SPLICED IN REPAIR SECTION OF LONGERON IAW SRM 53-02-02 FIG 10.SDR UPS08853275Longeron · corrodedINSPECTION TYPE:C2 D PIT CARGO COMP STA 1540, L30R HAS EXFOLATED CORROSION AT L30. REMOVED AND REPLACED LONGERON SECTION IAW SRM 51-1-8, 53-4-1, 53-2-2 FIG 10.SDR UPS08853263Web · corrodedINSPECTION TYPE:C2 STA -80 WEB EXFOLIATED ON FORE AND AFT SIDES IN COCKPIT SUBFLOOR, AT FUSE SKIN, LT SIDE BELOW SIDE BELOW SIDE CONSOLE. REMOVED AND REPLACED -80 WEB IAW SRM 51-1-20D, 51-3-0, 51-1-24.SDR UPS08853235Seat Track · wornINSPECTION TYPE:C2 SEAT TRACK WORN AT SEVERAL LOCATIONS BETWEEN STA 200 TO STA 240 LBL 45 IN MAIN CABIN. REPAIRED SEAT TRACK IAW SRM 53-02-3 AND SRM 51-03-0.SDR UPS08853262Skin · crackedINSPECTION TYPE:C2 CRACKED EXISTING REPAIR DOUBLER AT STA 3 ON FLAP WELL SUPPORT FRAME. REMOVED AND INSTALLED REPAIR DOUBLER IAW SRM 51-1-21, 51-1-8, 57-2-00 FIG 2A, 51-1-21.SDR UPS08853210Bracket · crackedINSPECTION TYPE:C2 CRACK ON ANGLE BRACKET MAIN CABIN WING BOX ST 880 LBL 60. REMOVE AND REPLACE BRACKET IAW SRM, 51-1-21, 51-1-8, 51-3-2.SDR UPS08853209Floorbeam · damagedINSPECTION TYPE:C2 DEEP SCRATCH ABOUT 16 INCHES LONG MAIN CABIN WING BOX FLOORBEAM UPPER SURFACE STA 880 LBL 25-45. FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 51-1-8, 51-1-21, 51-1-20D.SDR UPS08853208Structure · corrodedINSPECTION TYPE:C2 CORROSION ON SUBFLOOR COURIER AREA SAT 55 LBL 17. REMOVED CORROSION, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 51-1- 2-1, 51-1-8, 52-3-2.SDR UPS08853075Inu · failedINSPECTION TYPE:N/A EN ROUTE - CAPTAIN'S INS WARNING LIGHT ON EADI AND EHSI - LOST MULTIPLE SYSTEMS. CREW DECLARED EMERGENCY AND LANDED UNEVENTFULLY. REMOVED AND REPLACED NR 1 INU IAW MM 34-44-03. ADJUSTMENT TEST DUE. NR 1 INU CHECKS OK IN REF TO AMM 34-44SDR UPS08853261Hinge · wornINSPECTION TYPE:C2 RIGHT I/B GEAR DOOR LOOSE ON HINGE PINS. REMOVED AND REPLACED HINGE ON MAIN GEAR DOOR IAW SRM 51-1-8, 51-1-20D, 51-1-3, 51-1-21, 51-1-21A, 51-3-1.SDR UPS08853130Skin · gougedINSPECTION TYPE:C1 2 EA GOUGES IN UPPER SKIN OF RT WING O/B FLAP, ON I/B & O/B SIDE OF FLAP STA 219. FABRICATED AND INSTALLED 2 EA REPAIR DOUBLERS IAW SRM 57-07-01 FIG 004, 57-02-00, AND 51-1-21A.SDR UPS08853212Longeron · crackedINSPECTION TYPE:C2 CRACKED LONGERON END FITTING ON L19R AT STA 1770 INSIDE DOOR PANEL 60 COMPARTMENT. REMOVED AND REPLACED FITTING IAW SRM, 51-1-8, 51-1-21, 51-3-1.SDR UPS08853211Fitting · corrodedINSPECTION TYPE:C2 CORRODED FUSELAGE FRAME FITTING ON THE UPPER SURFACE OF INTERIOR CUSP EXTRUSION SRA 25 L21R. REMOVED AND REPLACED FITTING IAW SRM, 51-3-1, 51-1-8.SDR UPS08853196Door Frame · gougedINSPECTION TYPE:C2 TOOL MARK ON INNER SKIN INSIDE FWD RT SERVICE DOOR AFT DOOR JAMB BOX LOWER CORNER STA 200. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER IAW, SRM, 51-1-8, 53-2-0, 51-1-21.SDR UPS08853195Attach Fitting · corrodedINSPECTION TYPE:C2 CORRODED FRAME LWR CLIP ON THE UPPER SURFACE OF INTERIOR CUSP EXTRUSION STA 1666 L21R. REMOVED AND REPLACED LOWER CLIP IAW SRM 51-1-8, 51-3-2, 51-1-20D.SDR IXX2008F00104Skin · corrodedDURING ROUTINE C-CHECK INSP, FOUND RT HORIZ STABILIZER AFT PANEL CORRODED AT STA XF 195.963. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTNERS AS NEEDED TO PERFORM REPAIR. REMOVED CORRODED SKIN. FABRICATED NEW SKIN, AND DOUBLER. BONDED PART AS NEESDR IXX2008F00116Skin · misrepairedDURING ROUTINE C-CHECK INSPECTION, FOUND RT OTBD FLAP EXHAUST GATE LOWER SKIN HAS IMPROPER REPAIR. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED TREATED AND PRIMED AREA AND REPAIR PART. INSTALLED NEW FSDR IXX2008F00114Skin · misrepairedDURING ROUTINE C-CHECK INSP, FOUND LT AFT CORNER OF A PIT DOOR OPENING HAS IMPROPER REPAIR AT STA FS340, LONGERON 31 LT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAISDR IXX2008F00112Skin · misrepairedDURING ROUTINE C-CHECK INSP, FOUND RT OTBD FLAP LOWER SKIN HAS IMPROPER REPAIR AT STA XF 238.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEWSDR IXX2008F00115Skin · misrepairedDURING ROUTINE C-CHECK INSP, FOUND AFT LOWER FUSELAGE AFT OF OUTFLOW VALVE HAS IMPROPER REPAIR AT STA FS1688, LONGERON 35.75 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO CRACK, NOSDR IXX2008F00111Skin · misrepairedDURING ROUTINE C-CHECK INSP, FOUND FWD LWR FUSELAGE AFT OF AFT ADF ANTENNA HAS IMPROPER REPAIR AT STA FS 172 LONGERON 35.5 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO CRACK AND NSDR IXX2008F00101Skin · misrepairedDURING ROUTINE C-CHECK, FOUND DOUBLER FWD OF A-PIT DOOR ON LWR CENTERLINE, HAS IMPROPER REPAIR AT FS220, LONGERON 36. REMOVED FASTNERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP, NO CRACK, NO CORROSION FOSDR IXX2008F00117Fitting · crackedDURING ROUTINE C-CHECK INSP, FOUND AFT CARGO COMPARTMENT SPLICE FITTING CRACKED AT STA 1040.00-1060.000 LONGERON 31 RIGHT. REMOVED CRACKED SPLICE FITTING. FABRICATED SPLICE FITTING. PERFORMED NDT INSP. NO CRACK, NO CORROSION FOUND. CLEANED, TREATED AND PRSDR IXX2008F00113Skin · misrepairedDURING ROUTINE C-CHECK INSP, FOUND LT OTBD FLAP UPPER SKIN HAS IMPROPER REPAIR AND AT STA XF420.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR, REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PSDR IXX2008F00110Fitting · crackedDURING ROUTINE C-CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT SPLICE FITTING CRACKED AT STA 1040.000-1060.000 LONGERON 31 LT. REMOVED CRACKED SPLICE FITTING. FABRICATED SPLICE FITTING. PERFORMED NDT INSP. NO CRACK, NO CORROSION FOUND. CLEANED, TREATED, ASDR IXX2008F00105Skin · crackedDURING ROUTINE C-CHECK INSPECTION, FOUND RT WING UPPER SKIN CRACKED AT STRINGER 8 STA XW 408.00. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFOMRED NDT INSP. NO CRACK AND NO CORROSION FOUND. FABRICATED REPAIR DOUBLER, AND FILLE
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