Douglas DC-8-61

Service difficulty reports · 942

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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 = 'DC861'
  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.

SDR ABXA010833Doubler · corrodedAFT CARGO, LONGERON 32 RIGHT, B/S 1200, WAS CORRODED. REPAIRED AREA IAW DC-8 SRM 51-1-20D, 51-1-21 AND REA D853-43071MR.Mar 27, 2002 · N849AX · Doug DC861 · Fuselage Structure (General)SDR ARWA20020312Proximity SwitchLOG PAGE # 108372. DISCREPANCY: GEAR NOT LATCHED, DOOR NOT LATCHED, LIGHTS ILLUMINATED. ON LEFT MAIN LANDING GEAR NO DOWN LIGHTS. CORRECTIVE ACTION: REMOVED AND INSTALLED LEFT MAIN GEAR PROXIMITY SWITCH SENSOR. ACCOMPLISHED ADJ & TEST POSITION & WARNING SYMar 26, 2002 · N29UA · Doug DC861 · Landing Gear Position and WarningSDR ABXA010801Fitting · cracked#3 PYLON V-BLOCK SUPPORT FITTING HAD A CRACK IN IT. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D, 51-3-0, 51-1-23 AND 56-3-0.Mar 23, 2002 · N849AX · Doug DC861 · Nacelle/Pylon StructureSDR ABXA010800Strap · corroded#1 PYLON "T" CAP STRAP HAD CORROSION AT WING STATION 485.00, LOWER SPAR CAP, FORWARD SPAR. REMOVED AND REPLACED THE FORWARD SPAR STRAP, REMOVED AND REINSTALLED THE #1 PYLON "T" DOUBLER IAW DC-8 SRM 51-1-20D, 51-1-8.Mar 22, 2002 · N849AX · Doug DC861 · Nacelle/Pylon StructureSDR ABXA010789Seat Track · crackedFORWARD CARGO AT F.S. 340 - 360, LEFT BUTT LINE 50, SEAT TRACK WAS CRACKED. REPLACED SEAT TRACK IAW DC-8 SRM 51-1-8, 51-3-0, 51-1-21 AND ZANTOP DWG. #86302.Mar 20, 2002 · N849AX · Doug DC861 · Fuselage Structure (General)SDR ABXA010788Fitting · crackedFORWARD CARGO AT F.S. 200 - 220, LONGERON 31 LEFT, SPLICE FITTING WAS CRACKED. REPLACED FITTING IAW DC-8 SRM 51-1-20D.Mar 19, 2002 · N849AX · Doug DC861 · Fuselage Structure (General)SDR ABXA010787Frame · crackedFORWARD CARGO AT F.S. 180, ABOVE LONGERON 36 FRAME, UPPER CHORD WAS CRACKED AND BENT. REPAIRED AREA IAW DC-8 SRM STD-5310-002 AND SRM 51-1-8.Mar 19, 2002 · N849AX · Doug DC861 · Fuselage Structure (General)SDR ABXA010786Seat Track · crackedFORWARD CARGO AT F.S. 580 - 600, LEFT BUTT LINE 50, SEAT TRACK WAS CRACKED. REPLACED SEAT TRACK IAW DC-9 SRM 51-3-0, 51-1-8 AND ZANTOP DWG. #86302.Mar 19, 2002 · N849AX · Doug DC861 · Fuselage Structure (General)SDR ABXA010830Longeron · corrodedFORWARD ACCESSORY COMPARTMENT AT F.S. 640 - 660, LONGERON 31 RIGHT, WAS CRACKED. FABBED REPAIR STRAP AND REPAIRED AREA IAW DC-8 SRM 53-2-0, 53-4-1, 51-1-20D AND REA D853-43068MR.Mar 18, 2002 · N849AX · Doug DC861 · Fuselage Structure (General)SDR ABXA010785Fitting · crackedFORWARD CARGO, F.S. 380 - 400, LONGERON 31 LEFT, SPLICE FITTING WAS CRACKED. REMOVED AND REPLACED FITTING AT STA. 390, LONGERON 31 LEFT IAW DC-8 SRM 51-1-24 AND 51-1-20D.Mar 16, 2002 · N849AX · Doug DC861 · Fuselage Structure (General)SDR ABXA010791Strap · crackedT-CAP DOUBLER STRAP AT WS 485.00, FORWARD SPAR, LOWER CRACKED NR 4 ALT. REMOVED AND REPLACED DOUBLER STRAP IAW DC-8 SRM 51-1-20D, 51-1-24 AND DAC DWG 5803958.Mar 15, 2002 · N849AX · Doug DC861 · Wing Miscellaneous StructureSDR ABXA010790Fitting · crackedFORWARD LOWER CARGO, STATION 272, FITTING WAS CRACKED FORWARD OF C1 DOOR. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D, 51-3-1 AND 51-1-24.Mar 15, 2002 · N849AX · Doug DC861 · Fuselage Structure (General)SDR ABXA010784Fitting · crackedSPLICE FITTING CRACKED AT LONGERON 27 RIGHT, STATION 450, FORWARD LOWER CARGO. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D AND 51-1-21.Mar 15, 2002 · N849AX · Doug DC861 · Fuselage Main, StructureSDR ABXA010834Spar Cap · crackedRIGHT WING, FORWARD LOWER SPAR CAP HAD 9 EACH FASTENERS HOLES SHOWING CRACK INDICATIONS. REPAIRED DAMAGED HOLES IAW REA D857-43058.Mar 12, 2002 · N849AX · Doug DC861 · Wing StructureSDR ABXA010792Seat Track · crackedFORWARD CARGO AT F.S. 580 - 600, AT LEFT BUTT LINE 55, SEAT TRACK WAS CRACKED. REMOVED AND REPLACED SEAT TRACK IAW DC-8 SRM 51-3-0, 51-1-24 AND 51-1-8.Mar 10, 2002 · N849AX · Doug DC861 · Fuselage Structure (General)SDR ABXA010777Splice · crackedAFT LOWER CARGO COMPARTMENT, LONGERON SPLICE TIE CRACKED BETWEEN B.S. 1300 - 1320, LONGERON 31 LEFT. REPLACED SPLICE IAW DC-8 SRM 51-1-20D AND 51-3-2.Mar 10, 2002 · N849AX · Doug DC861 · Fuselage Main, StructureSDR ARWA20020205Spar · crackedDURING C-CHECK, LEFT WING STA XW 60 AUXILIARY SPAR LUG WITH CRACK, ADJACENT TO MLG TRUNNION FITTING. REMOVED AND REPLACED AUXILIARY SPAR IAW DRAWING 5616128.Feb 14, 2002 · N29UA · Doug DC861 · Wing SparSDR ABXA010799Longeron · corrodedFORWARD ACCESSORY COMPARTMENT LONGERON 36 WAS CORRODED AT FS 662. REPAIRED AREA AND INSTALLED NEW REPAIR ANGLE IAW DC-8 SRM 53-2-0, 51-1-20D, 51-1-8 AND REA D853-40966MR.Feb 5, 2002 · N847AX · Doug DC861 · Fuselage Main, Longeron/StringerSDR ABXA010797Longeron · crackedRIGHT WHEEL WELL, LONGERON 24 RIGHT WAS CRACKED AND CORRODED AT STATION 980. REPAIRED AREA AND INSTALLED NEW DOUBLER AND ANGLE IAW DC-8 SRM 51-1-21, 51-1-8, 51-1-20D AND REA D853-40964MR.Feb 5, 2002 · N847AX · Doug DC861 · Fuselage Main, Longeron/StringerSDR ABXA010798Web · corrodedFORWARD CARGO, AT FS 80, RIGHT CUSP AT LONGERON 21 RIGHT, ATTACH ANGLE WAS CORRODED. REPAIRED AREA IAW DC-8 SRM 51-1-8 AND REA D853-40960MR.Jan 30, 2002 · N847AX · Doug DC861 · Fuselage Miscellaneous StructureSDR ABXA010795Thrust Link · chafed#2 PYLON THRUST LINK CHAFED ON BOTTOM SIDE FROM PNEUMATIC DUCT CLAMP (REF. EA 5403277MR) REPAIR OR REPLACEMENT PER CARD 8821016, STEP 02.A) REPAIRED AREA IAW DC-8 SRM 51-1-8, MM 71-00-00, SB 54-92 AND REA D854-40959MR.Jan 28, 2002 · N847AX · Doug DC861 · Nacelle/Pylon StructureSDR ABXA010739Fitting · crackedRIGHT WING REAR SPAR, XRS 340, ACTUATOR ATTACH FITTING TO REAR SPAR WAS CRACKED. REPLACED FITTING IAW DC-8 DAC DWG 5773254, MM 20-16-00, 20-14-00 AND 27-51-09.Jan 23, 2002 · N847AX · Doug DC861 · Wing Miscellaneous StructureSDR ABXA010738Fitting · crackedRIGHT WING AUX SPAR, LOWER "L" ANGLE, WAS CRACKED APPROXIMATELY 10 INCHES LONG AT XRS 47. REPLACED FITTING IAW DC-8 SRM 51-1-24, 51-1-8 AND 51-1-20D.Jan 23, 2002 · N847AX · Doug DC861 · Wing, Attach FittingsSDR ABXA010737Splice · crackedFORWARD CARGO AT FS 600 - 620, LONGERON 25 RIGHT, SPLICE FITTING WAS CRACKED. REPLACED FITTING IAW DC-8 SRM 51-3-2, 51-1-20D AND 51-1-11.Jan 22, 2002 · N847AX · Doug DC861 · Fuselage Miscellaneous StructureSDR ABXA010736Splice · crackedFORWARD CARGO AT FS 600 - 620, LONGERON 31 RIGHT, SPLICE FITTING WAS CRACKED, OUTBOARD SIDE. REPLACED FITTING IAW DC-8 SRM 51-1-24, 51-3-2 AND 51-1-20D.Jan 22, 2002 · N847AX · Doug DC861 · Fuselage Miscellaneous StructureSDR ABXA010796Link · chafedNR 3 PYLON THRUST LINK CHAFED ON LOWER SIDE FROM PNEUMATIC DUCT CLAMP (REF EA AD 54-03277MR) FOR REPAIR OR REPLACEMENT PER ABX CARD 8931015, STEP 02.A). REPAIRED AREA IAW DC-8 SB 54-92.Jan 21, 2002 · N847AX · Doug DC861 · Nacelle/Pylon Miscellaneous StructureSDR ABXA010679Battery · dischargedEMERGENCY LIGHTS WERE DIM. REPLACED EMERGENCY LIGHT BATTERY AND RELAY ASSEMBLY. OPS CHECKED GOOD IAW DC-8 MM 33-50-01-2-0001.Jan 21, 2002 · N843AX · Doug DC861 · Emergency LightingSDR ABXA010675Latch · out of adjCOCKPIT ENTRY DOOR LATCH MECHANISM WAS JAMMED. ADJUSTED DOOR LATCH AS NEEDED IAW DC-9 MM CHAPTER 51. OPS CHECKED GOOD.Jan 18, 2002 · N848AX · Doug DC861 · Fixed Inner DoorsSDR ABXA010670Fitting · corrodedRIGHT MAIN LANDING GEAR WHEEL WELL, LONGERON 24 RIGHT, FITTING HAD EXFOLIATION CORROSION AT STATION 879. REMOVED CORRODED FITTING. FABRICATED REPAIR PARTS IAW DC-8 SRM 53-2-0. INSTALLED NEW FITTING AND REPAIR PARTS IAW DC-8 SRM 53-2-0.Jan 15, 2002 · N853AX · Doug DC861 · Fuselage Miscellaneous StructureSDR ABXA010668Fitting · corrodedFORWARD CARGO, STATION LONGERON 29 LEFT AND LONGERON 30 LEFT Z-ANGLE CORRODED. REMOVED CORRODED FITTING. RECEIVED NEW FITTING P/N 3755822-505N. FABRICATED REPAIR ANGLES IAW DC-8 SRM 53-2-0. INSTALLED Z-FITTING AND REPAIR ANGLES IAW DC-8 SRM 53-2-0.Jan 12, 2002 · N853AX · Doug DC861 · Fuselage Miscellaneous StructureSDR ABXA010667Fitting · corrodedFORWARD CARGO, STATION 320, BETWEEN LONGERON 28 LEFT - LONGERON 29 LEFT, Z-ANGLE CORRODED. REMOVED OLD FITTING. RECEIVED NEW FITTING P/N 3155822-505N. FABRICATED REPAIR ANGLES IAW DC-8 SRM 53-2-0.Jan 12, 2002 · N853AX · Doug DC861 · Fuselage Miscellaneous StructureSDR ABXA010666Spar · corrodedLEFT WING, FORWARD SPAR CAP AT XFS 520.76 HOLE HAD A CRACK INDICATION WITH HFEC DETERMINE CRACK LENGH AND LOCATION IAW ES00046. REPAIRED CRACKED HOLE IAW DAC DWG 4709980 AND DC-8 SRM 51-1-25. ALODINED AND PRIMED IAW DC-8 SRM 51-1-8.Jan 10, 2002 · N853AX · Doug DC861 · Wing StructureSDR ABXA010665Skin · corrodedRIGHT WING, TOP SURFACE BY STATION XRS 172, CORROSION ON SKIN. REPAIRED IAW ABX REA D857-40949-MR AND DC8 SRM 57-2-0, 51-1-26, 51-1-8 AND 51-1-20D.Jan 9, 2002 · N853AX · Doug DC861 · Wing, Plate/SkinSDR ABXA010793Stringer · crackedUPPER LEFT STRINGER 1 WAS CRACKED AT FS 1870, ABOVE BULKHEAD IN TAIL CONE FORWARD AREA. REPAIRED AREA IAW DC-8 SRM 51-1-21, 51-1-20, 51-1-8, 53-2-0 AND REA D853-40948MR.Jan 8, 2002 · N853AX · Doug DC861 · Fuselage Main, Longeron/StringerSDR ARWA20020109Gcu · failedDURING APPROACH NR 4 GENERATOR UNPARALLEL LIGHT AND BUS POWER FAIL LIGHT ILLUMINATED. PERFORMED ABNORMAL CHECKLIST. AIRCRAFT LANDED AT DESTINATION UNEVENTFUL. RESET NR 4 GENERATOR SYSTEM IN ACCORDANCE WITH MM 24-5-1 ENTERED ON DMI 16156 PER MEL 24-1 GEN NR Jan 8, 2002 · N29UA · Doug DC861 · AC RegulatorSDR ARWA20011216Filter Housing · defectiveNR 4 ENGINE OIL PRESSURE ERRATIC FLUCTUATES BETWEEN 0 TO 20 PSI WITH OIL PRESSURE LIGHT ON. ENGINE SHUTDOWN AS PER ABNORMAL CHECKLIST AND PROCEDURES. AIRCRAFT LANDED UNEVENTFUL. REMOVED AND REPLACED GEARBOX IAW MM 72-00. ACCOMPLISHED RUN UP, NO LEAKS NOTEDDec 29, 2001 · N29UA · Doug DC861 · Engine Oil Distribution (Airframe Furnished)SDR ABXA010669Splice · crackedAFT CARGO, FS 1040 - 1060, LONGERON 31 RIGHT, SPLICE FITTING WAS CRACKED. RECEIVED NEW FITTING P/N 3750257-1. INSTALLED IAW DC-8 SRM 51-1-20D. REMOVED DAMAGED FITTING IAW DC-8 SRM 51-3-2.Dec 29, 2001 · N853AX · Doug DC861 · Fuselage Miscellaneous StructureSDR ARWA20011217Oil Cap · looseDURING PUSHBACK MECHANIC REPORTED OIL LEAK ON NR 3 ENGINE, SHUTDOWN NR 3 ENGINE AND RETURNED TO RAMP UNDER TOW. FOUND NR 3 STARTER OIL CAP LOOSE, SERVICED AND SECURED OIL CAP IAW MM 80-10-0. LEAK CK ON RUN UP, NO LEAKS NOTED DURING RUN UP IAW MM 71-00. AIRCDec 29, 2001 · N30UA · Doug DC861 · Engine StarterSDR ARWA20011214Transmitter · erraticNR 4 OIL PRESSURE WENT TO 0 PSI AFTER TOP OF DESCENT, NR 4 OIL PRESS LIGHT ILLUMINATED, ENGINE WAS SHUT DOWN. BLED NR 4 ENGINE OIL SYSTEM, REMOVED AND REPLACED MAIN OIL FILTER IAW P&W 72-0, FOUND OIL PRESS XMTR ERRATIC, R&R IAW MM 79-32-1, OPS CKD DURING ENGIDec 27, 2001 · N29UA · Doug DC861 · Engine Oil PressureSDR ARWA20011203Brake · seizedNR 2 MAIN LANDING GEAR BRAKE ASSEMBLY LOCKED-UP CAUSING NR 2 TIRE TO BLOW. BRAKE TEMPERATURE CHECK AND WITHIN LIMITS. REMOVED AND REPLACED NR 2 MAIN GEAR BRAKE ASSEMBLY IAW DC-8 MM 32-42-1. REMOVED AND REPLACED NR 2 MAIN GEAR WHEEL AND TIRE ASSEMBLY IAW MM Dec 5, 2001 · N29UA · Doug DC861 · BrakeSDR ARWA20011104Hydraulic Line · leakingAFTER T/O LOST HYDRAULIC FLUID TO STAND PIPE AND PRESS 0, PERFORMED LOSS OF HYDRAULIC FLUID AND PRESS CHECKLIST AND RETURNED TO MIAMI. LANDED IN MIAMI OVERWEIGHT AT 272,600 WITHOUT INCIDENT. FOUND LT MLG BUNGEE CYLINDER PRESSURE LINE LEAKING. REMOVED AND RENov 18, 2001 · N29UA · Doug DC861 · Hydraulic System, MainSDR ARWA0011013Thermocouple · faultyIN CRUISE AT FL 29.0 NR 1 ENGINE EGT FLUCTUATED FROM 210 C TO 380 C, ALL OTHER PARAMETERS AS FOLLOWS: EPR 1.74, N2 97.5 PERCENT, FF 4900 LBS, N1 102.5 PERCENT, OIL TEMP 76 C, OIL PRESS 52 PSI, OAT -19 C. PERFORMED IN-FLIGHT ENGINE SHUTDOWN ABNORMAL CHECKLISTOct 30, 2001 · N30UA · Doug DC861 · Engine EGT/TIT Indicating SystemSDR ABXA010529Hydraulic System · lowTHE GENERAL HYDRAULIC SYSTEM NEEDED SERVICED. THE SYSTEM INDICATED ZERO DURING APPROACH AND LANDING. MAINTENANCE SERVICED THE GENERAL HYDRAULIC SYSTEM IAW DC-8 MAINTENANCE MANUAL.Oct 6, 2001 · N853AX · Doug DC861 · Hydraulic System, MainSDR ABXA010495Skin · corrodedCORROSION WAS FOUND AT FUSELAGE STATION 300, LONGERON 33R THRU 34R ON WALK AROUND INSPECTION. MAINTENANCE REPAIRED THE AREA IAW ABX REA D853-36700MR. OPEN: CORRECTIVE ACTION IS NOT COMPLETE.Sep 15, 2001 · N850AX · Doug DC861 · Fuselage Main, Plate/SkinSDR ABXA010472Indicator · defectiveDURING GEAR DOWN EXTENTION INTO LAX, THE HYDRAULIC QUANTITY BEGAN TO RAPIDLY DECREASE. CREW DECLARED AN EMERGENCY INTO LAX. FOUND THE HYDRAULIC INDICATOR INTERMITTENTLY INOPERATIVE. REPLACED THE INDICATOR. BLED THE HYRDRAULIC SYSTEM AND CYCLED ALL FLIGHT CONTRSep 12, 2001 · N849AX · Doug DC861 · Hydraulic Quantity IndicatorSDR ABXA010471Tire · defectiveDURING DEPARTURE FROM ILN, UPON GEAR RETRACTION, WHEN THE NOSE GEAR ENTERED THE WELL, A VIBRATION WAS FELT IN THE THROTTLE QUADRANT AREA. CREW RECYCLED GEAR AND DID A TOWER FLYBY THEN CONTINUED ON TO LAX. FOUND THE LEFT NOSE TIRE DEFORMED AND OUT OF ROUND. REPSep 12, 2001 · N849AX · Doug DC861 · Landing Gear Retraction/Extension SystemSDR ABXA010594Fitting · misdrilledAFT LOWER CARGO FRAME WAS MISDRILLED AT STAION 1140 RIGHT AND LONGERON 30 RIGHT. INSTALLED NEW FILLER AND DOUBLER AND REPAIRED AREA IAW DC-8 SRM 51-1-8 AND REA D853-40922MR.Sep 6, 2001 · N848AX · Doug DC861 · Fuselage Main, Attach FittingsSDR ABXA010458Switch · malfunctionedMAIN CARGO DOOR, NON-DOUGLAS, SYSTEM A-LIGHT CAME ON IN FLIGHT WITH PRESSURIZATION HOLDING. PER ABNORMALS, CREW DESCENDED TO 10,000 FEET. DEPRESSURIZED AIRCRAFT AND INSPECTED DOOR. LIGHT WENT OUT BELOW 6.0 PSID. DOOR INSPECTION, ALL LATCHED APPEARED LOCKEDAug 30, 2001 · N849AX · Doug DC861 · Door Warning SystemSDR ABXA010593Fitting · crackedMAIN CABIN, STATION 682 AND LONGERON 10 RIGHT, LONGERON TIE FITTING WAS CRACKED. INSTALLED NEW FITTING AND REPAIRED AREA IAW DC-8 SRM 51-1-20D AND 51-1-23.Aug 27, 2001 · N848AX · Doug DC861 · Fuselage Main, Attach FittingsSDR ABXA010592Fitting · crackedMAIN CABIN, STATION 682 AND LONGERON 5 RIGHT, LONGERON TIE FITTING WAS CRACKED. INSTALLED NEW FITTING AND REPAIRED AREA IAW DC-8 SRM 51-1-24, 51-1-20D AND 51-1-23.Aug 27, 2001 · N848AX · Doug DC861 · Fuselage Main, Attach Fittings
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