Douglas DC-8-73F
Service difficulty reports · 15,471
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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 = '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 DHLA201000007Door · gougedRT OTBD WING SLOT DOOR HAS A DEEP GOUGE IN OUTER PLATING LOWER SURFACE APPROX AT WS XS 493.0. ACCOMPLISHED EXTERNAL DOUBLER REPAIR TO PN 5769946-502 SLOT DOOR IN AFFECTED AREA IAW EVA D857-00321 REV IR AND SRM 57-2-0, FIG 2A TR 57-84. REFERENCE ASSOCIATED FASDR DHLA201000015Tire · failedON LANDING, SIGNIFICANT ACFT VIBRATION NOTED. AFTER CLEARING RUNWAY GROUND CONFIRMED 2 LT TIRES WERE BLOWN. NOTE ANTI-SKID ON DMI NR 35939 AT THE TIME OF INCIDENT. LT INBD FLAP FOUND WITH 12" X 10" X .5" DENT. TIRE AND WHEEL ASSEMBLES REPLACED ON LT GEAR. LSDR DHLA2010804001Skin · corrodedCORROSION CRACK DISCOVERED ON FUSELAGE EXTERIOR SKIN AT FS 120, AND LONGERON 36, EMANATING FROM FWD ADF ANTENNA. ACCOMPLISHED FUSELAGE SKIN EXTERNAL DOUBLER AND FILLER REPAIR IAW EVA D853-00319, DWG ES D853-00319-001-D, SRM, AMM, AND NDT MANUAL. REF 8110-3SDR IXXA100010OWire Harness · brokenDURING CLIMBOUT, NR 1 ENG SHORT CIRCUIT LIGHT CAME ON. NR ONE ENG FIRE WARNING WOULD NOT TEST. CREW SHUTDOWN NR 1 ENG AND LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED AND FOUND LT LWR NINTH STAGE BLEED AIR DUCT BROKEN AT ENG CASE FLANGE AND CORE WIRING HARNESDR IXXA10SMN028SWeb · crackedDURING ROUTINE C-CHECK INSP FOUND LT WING INBD LOWER SLOT DOOR WEB BROKEN. REMOVED DAMAGED WEB. FABRICATED NEW WEB. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW SRM 51-3-0, SRM 57-1-0 PAGE 1, SRM 57-3-3 FIGURE 22 ITEM "G", DPS 4.7SDR IXXA10SMN24SSkin · damagedDURING ROUTINE C-CHECK INSP FOUND RT WING NR 3 INBD SLOT VANE HOLES ELONGATED AT STA XW 257.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED REPAIR DOUBLER, FILLERS, INTERNAL DOUBSDR IXXA10SMN027SWeb · crackedDURING ROUTINE C-CHECK INSP FOUND RUDDER WEB INTERIOR CRACKED AT STA ZR 163.000. REMOVED CRACKED WEB. FABRICATED WEB. PERFORMED HEAT TREATMENT. CLEANED, TREATED, PRIMED AREA AND REPAIR PART. APPLIED SEALANT TO FAYING SURFACES. PERFORMED RUDDER BALANCE. FSDR IXXA10SMN26SSkin · corrodedDURING ROUTINE C-CHECK INSP FOUND RUDDER LT EXTERNAL SKIN CORRODED AT STA ZR 155.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLERS. BONDED PARTS AS NEEDED SDR IXXA10SMN023SDoubler · crackedDURING ROUTINE C-CHECK INSP FOUND NR 2 MAIN TANK TOP ACCESS DOOR NR 505F DOUBLER CRACKED AT STA XRS 22.270 STR 6. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO CRACK, NO CORROSION FOUND. FABRICATED EXTERNAL, INTSDR IXXA10SMN022SDoubler · crackedDURING ROUTINE C-CHECK INSP FOUND NR 2 MAIN TANK TOP ACCESS DOOR NR 506C DOUBLER CRACKED AT STA XRS 22.750 STR 13. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED INTERNAL AND EXTERNAL DSDR IXXA10SMN021SDoor Frame · crackedDURING ROUTINE C-CHECK INSP, FOUND FUSELAGE EXTERIOR "D" CARGO DOOR FWD UPPER JAMB CORNER CRACKED AT STA 1400.000 LONGERON 26 RT LONGERON 27 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRSDR IXXA10SMN025SSkin · crackedDURING ROUTINE C-CHECK INSP, FOUND LT WING INBD FLAP T/E PANEL CRACKED AT STA XW 35.000 REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLERS. BONDED PARTS AS NEEDED WITH ADHESIVE. CLEANED, TREATED, PRIMEDSDR IXXA10SMN017SSkin · misrepairedDURING ROUTINE C-CHECK INSP, FOUND IMPROPER REPAIR AT STATION FS 668 LONGERON 36. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED REPAIR DOUBLER, REPAIR TRIPLER, FILLERS AND FINGER DOUBLERS. PERFORMED NDT INSP. NO DISCREPANCYSDR IXXA10SMN018SSkin · misrepairedDURING ROUTINE C-CHECK INSP FOUND IMPROPER REPAIR AT STA FS 1447 LONGERON 29 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. PERFORMED INSP. NO DISCREPANCY FOUND. FABRICATED REPAIR DOUBLER, FILLERS. CLEANED, TREATED, PRIMED AREA SDR IXXA10SMN016SSkin · misrepairedDURING ROUTINE C-CHECK INSP FOUND IMPROPER REPAIR AT STA FS 615 LONGERON 36. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. PERFORMED INSP. NO DISCREPANCY FOUND. FABRICATED REPAIR DOUBLER, FILLERS. CLEANED, TREATED, PRIMED AREA AND RSDR IXXA10SMN015SSkin · misrepairedDURING ROUTINE C-CHECK INSP, FOUND IMPROPER REPAIR AT STA FS 36.5 LONGERON 30.5 LT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. PERFORMED INSP. NO DISCREPANCY FOUND. FABRICATED REPAIR DOUBLER, FILLERS. CLEANED, TREATED, PRIMED ARESDR IXXA10SMN020SSkin · misrepairedDURING ROUTINE C-CHECK INSP FOUND IMPROPER REPAIR AT STA FS 1765 LONGERON 17.5 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED INTERNAL, EXTERNAL, DOUBLERS AND FILLER. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTSDR DHLA201000001Battery Pack · dischargedEMERGENCY LIGHTING DIM DURING TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK ASSY. OPS CHECK OK IAW MM 33-50-00 & 33-50-1. ACFT WAS GROUNDED.SDR DHLA2009873002Skin · corrodedREF N/R 8696-06: EXFOLIATION CORROSION DISCOVERED ON FUSELAGE SKIN AT APPROXIMATE FS 1464 AND LONGERON 36. ACCOMPLISHED FUSELAGE SKIN DOUBLER AND FILLER REPAIR IAW SRM 53-2-1, FIG 7 TR 53-203, SHEET 13, EVA D853-00315 AND NDT MANUAL. HFEC OF REPAIR PARTS ANSDR IXXA090075OGenerator · failedDURING CLIMB OUT FROM DEPARTURE NR 3 GENERATOR BUSS FAILURE, VOLTS AND FREQUENCIES AT ZERO. THE CREW ACCOMPLISHED COM PROCEDURES AND RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX RESET NR 3 GENERATOR BUS FAULT RESET SWITCH. OPS CHECK GOOD IAW MM 24-20-0. SDR DHLA2010807501Keelbeam · crackedMLG W/W KEEL BEAM TEE ANGLE CRACKED 1/4" AT STA 940.000. REMOVED AND REPLACED TEE ANGLE AT STA 940.000 IAW JC EC-01874-001 AND DWG NR 4645516 AND IAW SRM 51-1-20D.SDR IXXA090071OConnector · dirtyON FINAL APPROACH, WHEN MLG WAS EXTENDED THE LT MLG LIGHT STAYED OUT. THE CREW RECYCLED MAIN GEARS AND ALL WAS NORMAL. THEY LANDED WITHOUT FURTHER INCIDENT. MX REMOVED, CLEANED AND INSPECTED THE LT MAIN GEAR DOWN LOCK LIMIT SWITCH CONNECTOR. OPS CHECK GOOD ISDR DHLA2010807502Doubler · crackedFUSE NOSE SECTION ACCESS DOOR NR 2 INLET INTERNAL DOUBLER CRACKED 1 3/4". PERFORMED MAJOR REPAIR IAW 8110-3 DTD 12-04-09 EVA D853-00286 REV IR DTD 11-20-09 REMOVED EXISTING REPAIR IAW SRM 51-1-21 INSTALLED REPAIR PARTS IAW SMN-DWG ED-5017.SDR DHLA2009806001Skin · corrodedINTERGRANULAR CORROSION DISCOVERED ON FUSE. EXTERIOR SKIN, FS 59.0, LONG 34L TO 35L. ACCOMPLISHED EXTERNAL DOUBLER REPAIR, FS 53.5 TO 70.0, LONG 34L TO 34R, IAW D857-00297 REV IR DATED 12/4/09, DWG NR D85300297-001-D REV IR DATED 12/4/09, AND SRM CHPT'S 51 & SDR DHLA2010807504Beam · corrodedFWD CARGO COMPT, BEAM CORRODED STA 180.000 LBL 5. PERFORMED MAJOR REPAIR IAW SRM 51-2-1 SHEET 9,12 TR NR 51-130, DTD 01-26-04.SDR DHLA2010807508Skin · crackedLT INBD FLAP LWR SKIN CRACKED STA XCW 64.000. PERFORMED MAJOR REPAIR IAW SRM 57-7-1-FIG1 PG2.SDR DHLA2010807503Skin · crackedLEFT WING UPPER SKIN CRACKED STA XRS 74.000 S-9. PERFORMED MAJOR REPAIR ON LT WING UPPER SKIN AT STA XRS 74.000 S-9 IAW SRM 57-2-1, FIG 17.SDR DHLA200900055Fire Detector · false activationNR 2 ENG FIRE WARNING LIGHT AND BELL. COMPLETED ENG FIRE PHASE ONE ITEMS COMPLETED ENG FIRE CHECK LIST FIRE LIGHT OUT. INSPECTED ENG NR 2 INLET AND EXHAUST INCLUDING FAN AND CORE SECTION NO DAMAGE OR EVIDENCE OF FIRE NOTED. T/S IAW MMS 26-10-01 AND W/D 26-01SDR DHLA2010807505Skin · scratchedREMOVE PAINT AND INSPECT FUSELAGE SKIN FOR DEEP SCRATCHES AT STA 1360 L-24L. PERFORMED MAJOR REPAIR IAW SRM 53-2-1-FIG 7 SHEET 2,23,24 AND TR NR 53-203 DTD 01/21/08. THIS IS A CLASS 1 REPAIR INITIAL INSP 4,000 LC, REPETITIVE 4,000 LC NEXT REINSPECTION DUE 33.SDR IXXA090066OSwitch · brokenDURING CLIMBOUT, MLG DOOR NOT LATCHED LIGHT CAME ON, THE CREW RECYCLED LANDING GEAR AND ACCOMPLISHED UPLATCH CHECK THE DOOR NOT LATCHED LIGHT STAYED ON. THEY LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED MLG AND FOUND RT GEAR DOOR SWITCH BROKEN. MX REPLACED SDR DHLA200900053A/C Pack · odorCHEMICAL OIL ODOR COMMING FROM LT PACK. RAN LT PACK, SUSPECT WAS FROZE UP PACK. OPS CK GOOD NO DEFECT NOTED IAW MM 36-10-0.SDR DHLA2009804002Skin · corrodedREFERENCE ASTAR N/R 8285-39: DURING "B" CHECK, FOUND CRACK IN FUSE SKIN AT FS 1442, BETWEEN LONGERON 35R AND 36. ACCOMPLISHED CLASS II EXTERNAL DOUBLER REPAIR FOR CORROSION REMOVAL IAW SRM 53-2-1 FIG 7 TEMP REV. 53-203, 53-2-0, AND 51-1-8. THIS IS A LIFE LISDR DHLA2000900052Bleed Valve · malfunctionedDURING CRUISE, AT 360FL, ODOR OF SMOKE IN COCKPIT. PERFORMED SMOKE SOURCE IDENTIFICATION CHECKLIST. HAD DIFFICULT TIME CONTROLLING CABIN PRESSURE IN AUTO AT ALT PRESSURE SWING 2000 FT/M UP AND DOWN EVERY 10. TRANSFERRED NR 1 ENG HP REG VALVE TO DMI NR 3567SDR DHLA200900051Battery Pack · dischargedON PRE-DEPARTURE CHECK FOUND EMERGENCY LIGHT INOP. R & R BATTERY PACK IAW MM 33-51-1 CHECKED OPERATION OK. AIRCRAFT WAS GROUNDEDSDR IXXA090059OOxygen System · lowDURING CLIMB OUT, CREW NOTICED OXYGEN REGULATOR AT JUMP SEAT HAD FLOW LEVER IN EMERGENCY POSITION, OXYGEN SYS DEPLETED DOWN TO 75 PSI. THEY RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX SERVICED OXYGEN SYS, OPS CHECK GOOD IAW MM 35-10-0. ACFT WAS RETURNESDR IXXA090056OSteering Sys · lack of lubeDURING TAKEOFF FROM KLRD THE NOSE WHEEL CONTROL DID NOT RESPOND TO CONTROL WHEEL OR RUDDER. THE CREW ABORTED TAKEOFF AND RETURNED TO BLOCKS WITHOUT FURTHER INCIDENT. MAINTENANCE LUBRICATED NOSE GEAR SREERING SYSTEM. OPERATIONAL CHECK GOOD IAW DACO DC8 MAINTENASDR 2009F00101Skin · misrepairedREMOVE EXTERNAL REPAIR DOUBLER AT FUSELAGE STATION 1750 LONGERON 34L AND REPLACE WITH REPAIR IAW APPROVED DATA. INDICATE TYPE OF REPAIR AND REINSPECTION INTERVAL IF KNOWN (MAJOR REPAIR). REMOVED EXISTING DOUBLER REPAIR, CUT OUT DAMAGED AREA AND FABRICATED RESDR 2009FA0000946Skin · damagedREMOVE EXTERNAL REPAIR AT LT MAIN LANDING GEAR DOOR CUT OUT (CRACKS IN INBD FWD CORNER) AND REPLACE WITH REPAIR IAW APPROVED DATA. INDICATE TYPE OF REPAIR AND REINSPECTION INTERVAL IF KNOWN (MAJOR REPAIR). REMOVED EXISTING REPAIR, FABRICATED REPAIR DOUBLER ASDR DHLA2009873001Skin · damagedEVIDENCE OF A LIGHTNING STRIKE FOUND DURING SERVICE CHECK ON RUDDER RT SIDE JUST BELOW 2CD STATIC WICK FROM THE TOP: REF L.P. A017576 FOR ORIGINAL DISCREPANCY. ACCOMPLISHED REPAIR TO RUDDER RT SIDE, STA XR306.5 CANT IAW EVA D855-00275. REFERENCE W/O 8403 ASDR DHLA20098051Door Frame · crackedFWD SVC DOOR FWD UPPER JAMB CORNER CRACKED 1/4 INCH. C/A INSTALLED DOUBLER REPAIR IAW DWG SR08530021, SRM 53-4-1 FIG 9 ITEM D, AND AD-2000-20-08 S/BDC8-53-075.SDR DHLA20098054Door Frame · crackedMAIN CARGO DOOR LWR. JAMB CRACKED 1/2 INCH STA. 200.000 L-21L TO 22L. REF N/R 229834: CUT OUT DAMAGED SECTION AND INSTALLED REPAIR IAW DWG ED-4987 AND SRM 51-1-11,SRM 51-1-21, SRM51-1-20D,SRM 51-3-1.SDR DHLA20098053Doubler · damagedAPPEARS THAT AIRSTART NOZZLE IS HITTING HARD ON INTERNAL DOUBLER FLANGE AT STA 156.000. REMOVED EXISTING REPAIR AND REWORK. REMOVED AND REPLACED DOUBLER IAW NR D853-00271 REV IR DATED 09-09-09, DWG ED-4985 DATED 9-05-09 AND SRM 51-1-1 PG 1,13,17.SDR DHLA20098052Longeron · damagedFUSELAGE STA 1749 LONGERON HAS RT EXISTING REPAIR IN POOR CONDITION. REM AND REP WITH PERMANENT TYPE REPAIR IAW APPROVED DATA. INDICATS REINSPECTION INTERVAL IF REQUIRED. REMOVED EXISTING REPAIR AND INSTALLED FABRICATED REPAIR DOUBLER IAW SRM 53-2-1, FIG 7 SDR DHLA200900050Light · burnedDURING ENGINE START, ODOR OF SMOKE IN COCKPIT, S/O OBSERVED SMOKE COMING FROM PANEL NEAR DOOR HANDLE, PANEL WAS HOT AND PAINT WAS BURNED. FOUND READ, ENTRY , INSIGNIA DIMMMING RESISTER OVERHEATING, PULLED AND COLLARD C/B CAP AND STOWED WIRES PER SWPM 20-10-04SDR DHLA20090049Unknown · unknownNUMBER 3 AND 4 ENG SLOW TO SPOOL UPON A ROLLING T/O. REJECTED T/O DUE TO DIRECTIONAL CONTROL. PERF ENG NR 3 AND 4 T/S IAW MM 71-00-00 ALL ENG INSPECTIONS AND PARAMETERS NORMAL. OK FOR SERVICE. ACFT GROUNDED. AT POWER UP AIRCRAFT PULLED OFF THE RUNWAY, SSDR DHLA200900048Pump · wornNR 4 ENG FLAMOUTED, PASSING FL350 IN CLIMB. ATTEMPTED RESTART AT FL350 UNSUCCESSFUL ATTEMPTED. ATTEMPED 2ND RESTART DURING DECENT TO CVG AT FL220. ATTEMPTED UNSECCESSFUL. OIL PRESSURE 3-5 PSI TIME OF FAILER 0430Z. LAND AT 0613. PERFORMED FAULT ISOL 51 IN MM 71SDR 2009F00103Door Frame · damagedFUSELAGE STATION 1660 LONGERON 15 RT. REMOVE AND REPLACE THIS REPAIR AT R-2 AFT DOOR JAMB WITH REPAIR IAW APPROVED DATA. INDICATE REINSPECTION INTERVAL IF REQUIRED. (MAJOR REPAIR)SDR 2009F00102Tab · delaminatedRT ELEVATOR GEARED TAB IS DELAMINATED.SDR DHLA200900047Connector · contaminatedON FINAL APPROACH FIRE BELL AND NR 2 ENGINE FIRE LIGHT INTERMITTENT CONTINUED ON ROLL OUT, PERFORMED ENGINE FIRE SHUTDOWN PROCEDURES FIRE LIGHT & BELL CONTINUED INTERMITTENTLY. COULD NOT DUPLICATE AT FIRST, RAN ENG AT 80 PERCENT N1 FOR 5 MIN AND LOOP RESISTANSDR DHLA200900046Engine · slowRTO ON RNWY 34R SLC DUE TO ENGINES SPOOLING UP UNEVENLY. SPEED 70 KTS, LIGHT BRAKING, PRESSURE ALTITUDE 4127 FT, FULL REVERSE, A/C WEIGHT 225,000 LBS. NR 3 & NR 4 SLOW TO SPOOL UP. INFO NOTED BY MX.
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