Douglas DC-10-30F

Service difficulty reports · 1,152

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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 = 'DC1030F'
  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 00FDEA00775Floor Support · corrodedCABIN - CORROSION ON FLOOR PANEL SUPPORT STRUCTURE AT BS 450, BL 0 TO LBL 28. *S/D* BLENDED OUT AS PER SRM 51-21-01 VOL II. REMOVED AND REPLACED PER SRM 51-31-01 VOL II. TOUCH UP PAINT PER SRM 51-21-01 VOL II.Nov 9, 2000 · N305FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR 00FDEA00774Plate · corrodedCABIN - CORROSION ON FLOOR PANEL PLATE AT BS 420, LBL 35 TO 75. *S/D* BLENDED OUT PER SRM 51-21-01 VOL II. REMOVED AND REPLACED PER SRM 51-31-01 VOL II.Nov 9, 2000 · N305FE · Doug DC1030F · Fuselage Floor PanelSDR 00FDEA00773Floor Support · corrodedCABIN - CORROSION ON FLOOR PANEL SUPPORT HAT SECTION AT BS 450 TO 460, LBL 55. *S/D* REMOVED AND REPLACED PER SRM 51-31-01 VOL II.Nov 8, 2000 · N305FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR 00FDEA00772Seat Track · corrodedCABIN - CORROSION ON SEAT TRACK CROWN AT BS 460 TO 468, LBL 28. *S/D* REMOVED AND REPLACED PER MM 53-21-04-2, 53-70-00 FIG 1 SHT 4 VOL I.Nov 8, 2000 · N305FE · Doug DC1030F · Fuselage, Seat/Cargo Attach FittingsSDR 00FDEA00771Floor Support · corrodedCABIN - CORROSION ON FLOOR PANEL SUPPORT HAT SECTION AT BS 425 TO 460, LBL 28. *S/D* REMOVED AND REPLACED PER SRM 51-31-01 VOL II. PAINT TOUCHED UP PER SRM 51-21-02 VOL II.Nov 8, 2000 · N305FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR 00FDEA00770Skin · crackedLEFT HAND WING - RIVETS LOOSE (APPROX 30 EA) AND SKIN CRACK AT OUTBOARD FLAP UPPER SURFACE INBOARD MIDDLE SEGMENTS AS MARKED. *S/D* REMOVED AND REPLACED PER SRM 51-35-01, 57-10-00 VOL I. PAINT TOUCHED UP PER SRM 51-21-01 VOL II.Nov 7, 2000 · N305FE · Doug DC1030F · Trailing Edge FlapsSDR 00FDEA00758Switch · failedON T/O AFT GEAR HANDLE RAISED. UNSAFE GEAR LIGHTS REMAIN ILLUM. REMOVED AND REPLACED S1-341 IN THE THROTTLE SWITCH ASSY NR 2 PER IAW 76-11-04-2 PG 201. OPS CK NORMAL.Nov 4, 2000 · N307FE · Doug DC1030F · Landing Gear Position and WarningSDR RRXA001075Packing · leakingHYDRAULIC SYSTEM 3 ELEVATOR OFF LIGHT CAME ON, SYSTEM 3 QTY DECREASING. REPLACED PACKING ON NR 3 SYSTEM HYDRAULIC PRESSURE TRANSMITTER. OPS CKS AND LEAK CHECKS GOOD IAW MM 29-31-03. NO OTHER LEAKS NOTED, SERVICED HYDRAULICS.Oct 24, 2000 · N831LA · Doug DC1030F · Hydraulic Indicating SystemSDR 00FDEA00729Controller · malfunctionedDURING CLIMB HAD UNCOMMANDED AUTO SLAT EXTENSION.Oct 21, 2000 · N314FE · Doug DC1030F · Leading Edge Slat Control SystemSDR 00FDEA00722Structure · damagedON POSTFLIGHT FOUND NR 2 SPOILER DAMAGED. REMOVED AND REPLACED NR 2 SPOILER.Oct 14, 2000 · N320FE · Doug DC1030F · SpoilersSDR 00FDEA00721Door · missingON POST FLIGHT FOUND LEFT WING REFUEL DOOR MISSING. REPLACED REFUELING DOOR ASSY.Oct 13, 2000 · N305FE · Doug DC1030F · Fluid Service DoorsSDR 00FDEA00716Spar Cap · crackedHFEC INSP FOUND CRACK ON RHS OF THE UPPER SURFACE OF THE UPPER OUTER REAR SPAR CAP''S AFT BARREL NUT HOLES. *S/D* REPAIRED PER FEDEX EA 8-5510-52866.Oct 7, 2000 · N317FE · Doug DC1030F · Horizontal Stabilizer, Spar/RibSDR 00FDEA00714Harness · shortedEXTERNAL PWR FEEDER CABLES FOUND SHORTED AND BURNT WHICH CAUSED FIRE AT FWD CARGO BULKHEAD AREA. *S/D* REMOVED AND REPLACED PER WDM STANDARD MAINTENANCE PRACTICES 20-10-01, 20-20-01 & WDM 24-41-01. EXT PWR OPS CK SAT PER 24-53-01.Oct 6, 2000 · N317FE · Doug DC1030F · External Power SystemSDR G60A055Extinguisher · dischargedNR 1 ENGINE FIRE WARNING. DISCHARGED NR 1 FIRE BOTTLE. REMOVED AND REPLACED NR 1 ENGINE FIRE BOTTLE IAW 26-21-02. (M)Oct 5, 2000 · N601GC · Doug DC1030F · Fire Bottle, FixedSDR G60A054Panel · damagedL/W PANEL HAS SEVERAL LENGTH WISE CUTS, PANEL NR 541EB, DUE TO ENGINE FAILURE. REMOVED AND ROUTED PANEL TO ALITALIA FOR REPAIRS. INSTALLED SERVICEABLE PANEL IAW 20-52-00. (M)Oct 5, 2000 · N601GC · Doug DC1030F · Wing, Plate/SkinSDR G60A053Skin · damagedLOWER SURFACE OF INBOARD AILERON, STATION XW 060 HAS 24 INCHES CORDWISE TEAR IN SKIN DUE TO ENGINE FAILURE. REMOVED AND REPLACED LEFT INBOARD AILERON IAW 27-10-01. (M)Oct 5, 2000 · N601GC · Doug DC1030F · Wing StructureSDR G60A052Skin · damagedLEFT WING OUTBOARD FLP, INBOARD RIB STATION XW380 HAS 4 INCH HOLE IN CENTER OF RIB AND THE FLAP SKIN IS PEELED UPWARD 24 INCHES LONG ON UPPER SURFACE DUE TO ENGINE FAILURE. REMOVED AND REPLACED LEFT INBOARD FLAP PANEL MM 20-52-02. (M)Oct 5, 2000 · N601GC · Doug DC1030F · Trailing Edge FlapsSDR G60A051Case · damagedBOTH LEFT AND RIGHT REVERSER HALVES DAMAGED DUE TO ENGINE FAILURE, P/N 536L411904, 536L411905. REMOVED AND REPLACED LEFT AND RIGHT THRUST REVERSER HALVES IAW 78-32-11. (M)Oct 5, 2000 · N601GC · Doug DC1030F · Engine Thrust ReverserSDR 20010112SG020Structure · damagedLOWER SURFACE OF INBOARD AILERON, STATION XW 060 HAS 24 INCHES CHORDWISE TEAR IN SKIN DUE TO ENGINE FAILURE. REMOVED AND REPLACED LEFT INBOARD AILERON IAW 27-10-01. (M)Oct 5, 2000 · N601GC · Doug DC1030F · AileronsSDR 00FDEA00622Proximity Switch · malfunctionedAFT RAISING LAND GEAR, LIGHT ON PILOTS LAND GEAR LIGHT PANEL REMAINED ILLUM. TROUBLESHOOTING PER TAFI 32-30-00 FAULT CODE AF, NO FAULT FOUND. PRECAUTIONARY REMOVED AND REPLACED PROXIMITY ELECTRONICS UNIT PER DC 10-30 MM 32-61-01-2. OK FOR SERVICE.Sep 4, 2000 · N303FE · Doug DC1030F · Landing Gear Position and WarningSDR 00FDEA00762Bearing · corrodedRT AND LT HORIZONTAL STAB PIVOT BEARINGS CORRODED DUE TO LACK OF GREASE CAUSED BY PLUGGED GREASE PARTS AROUND BEEPING SURFACE AREA.Aug 30, 2000 · N312FE · Doug DC1030F · Horizontal Stabilizer StructureSDR 00FDEA00607Bracket · crackedLEFT NR 3 DOOR FWD FROM THE TOP NR 5 MOUNTING TOP-STUD BRACKET FOUND CRACKED. *S/D* REMOVED AND REPLACED PER DC10 SRM 51-35-02 VOL II.Aug 28, 2000 · N321FE · Doug DC1030F · Passenger/Crew DoorsSDR 00FDEA00459Control Cable · damagedDURING DESCENT, NR 2 THROTTLE STUCK AT 88 PERCENT N2. THROTTLE WILL MOVE BUT N2 REMAINS AT 88 PERCENT N2 AND THROTTLE RETURNS TO ORIG POS. REMOVED AND REPLACED NR 2 ENG PUSH PULL CABLE REF MM 76-11-01-2. RIGGED PER DC-10 MM 76-11-01-2 AND SECURED ALL ROD ENJul 13, 2000 · N306FE · Doug DC1030F · Power LeverSDR 00FDEA00455Door · corrodedAVIONICS COMP DOOR NR 115AZ FOUND CORRODED INTERIOR. *S/D* REMOVED AND REPLACED PER DRAWING NR ACA 3777, MM 52-41-01-2.Jul 11, 2000 · N319FE · Doug DC1030F · Electrical/Electronic Compartment DoorsSDR 00FDEA00445Control Cable · brokenLT WING LEAD EDGE SLAT NR 7 EXTEND CABLE NR 65 FOUND BROKEN DURING ACCESS PANELS OPEN UP. *S/D* REMOVED AND REPLACED PER MM 27-89-13-4.Jul 7, 2000 · N319FE · Doug DC1030F · Leading Edge Slat Control SystemSDR 00FDEA00444Control Cable · brokenLT WING LEAD EDGE SLAT NR 6 EXTEND CABLE NR 63 FOUND BROKEN DURING ACCESS PANELS OPEN UP. *S/D* REMOVED AND REPLACED PER MM 27-89-11-4.Jul 7, 2000 · N319FE · Doug DC1030F · Leading Edge Slat Control SystemSDR 00FDEA00400Stiffener · corrodedSNRM 0327 LOWER AUX FUEL TANK AFT BULKHEAD, LT MOST VERTICAL STIFFNER FOUND WITH CORROSION. R&R PER 51-31-01, 21-11-06-2.Jun 20, 2000 · N322FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR 00FDEA00399Support Bracket · crackedSNRM 0338 RT WING PANEL SUPPORT FOR PANEL NR 618GB WAS CRACKED, LOCATED APPROX 4 INCHES OB OF SLAT DRIVE MECH ACCESS PANEL. R&R PER SRM 51-31-01.Jun 20, 2000 · N322FE · Doug DC1030F · Wing Miscellaneous StructureSDR 00FDEA00403Skin · crackedSNRM 0196 LT WING OB FLAP UPPER SKIN SURFACE FOUND CRACKED APPROX 3 5/32 INCHES. R&R PER SRM 51-31-01, 57-10-00, 57-52-02.Jun 19, 2000 · N322FE · Doug DC1030F · Trailing Edge FlapsSDR 00FDEA00402Skin · crackedSNRM 0198 LT WING IB FLAP UPPER SKIN FOUND PATCH REPAIR CRACKED APPOX 6 INCHES. R&R PER CMM 57-52-01.Jun 19, 2000 · N322FE · Doug DC1030F · Trailing Edge FlapsSDR 00FDEA00401Skin · crackedSNRM 0222 LT WING L/E LOWER ACCESS PANEL CUTOUT NR 526AB FWD SIDE FOUND CRACKED. R&R PER SRM 51-31-01.Jun 19, 2000 · N322FE · Doug DC1030F · Wing, Plate/SkinSDR 00FDEA00398Channel · corrodedSNRM 0252 AFT FUSELAGE WATER TANK BAY STA 1996, FUSELAGE FRAME AFT LWR CHANNEL TOP SURFACE CORRODED, LONGERON 50 RT TO LT. R&R CHANNEL & STRAP PER SRM 53-30-00 FIG 8, VOL 1.Jun 19, 2000 · N322FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR 00FDEA00359Skin · damagedFWD CARGO DOOR CUTOUT FWD SIDE FOUND EXTERIOR SKIN AT L 39-40 DAMAGED. *S/D* REMOVED DAMAGED AREA PER SRM 53-50-00 FIG 9 SHEET 3 VOL 1 AND 51-21-01 VOL II. REPAIRS ARE REPAINTED PER SRM 51-21-02 VOL II. FASTENERS INSTALLED PER 51-33-01 VOL II.May 29, 2000 · N315FE · Doug DC1030F · Fuselage Main, Plate/SkinSDR G6OA047Harness · arcedWHILE TROUBLESHOOTING MEL CONTROL NR M607-4435 FOUND WIRE BUNDLE TO FE PANEL LIGHT CONTROL PANEL BETWEEN P1-299 AND R5-299 CHAFED THROUGH CAUSING ELECTRICAL ARCING ON OUTFLOW VALVE CABLE. REPAIRED WIRES L3850C22 AND L725B22 PER MM 20-30-13. OPERATIONAL CHECKMay 26, 2000 · N607GC · Doug DC1030F · Flight Compartment LightingSDR G6OA048Harness · arcedARCING OF WIRE BUNDLE TO FE PANEL LIGHT CONTROL PANEL BETWEEN P1-299 AND R5-299 CAUSED OUTFLOW VALVE CABLE (CABLE RUN 129) TO BREAK. FABRICATED NEW CABLE PER MM 20-20-00 AND REPLACED PER MM 21-30-00. OPERATIONAL CHECKS OK. (M)May 26, 2000 · N607GC · Doug DC1030F · Pressure Regulator/Outflow ValveSDR 00FDEA00330Seat Track · corrodedSEAT TRACK CROWN AND FLANGE AREA CORRODED BS 1917 TO BS 1987, RBL 88. SEAT TRACK CROWN AND FLANGE AREA CORRODED BS 415 TO BS 465, RBL 28. *S/D* REMOVED AND REPLACED PER SRM 51-35-01 & 51-32-02 VOL II & 53-70-00 FIG 1 VOL I. REMOVED AND REPLACED PER SRM 53-May 10, 2000 · N311FE · Doug DC1030F · Fuselage, Seat/Cargo Attach FittingsSDR 00FDEA00331Angle · crackedRIGHT HORIZONTAL STABILIZER CTR LEAD EDGE TEE ANGLE CRACKED. LEFT HORIZONTAL STAB CTR LEAD EDGE TEE ANGLE CRACKED. *S/D* REMOVED AND REPLACED PER 51-31-01 VOL II.May 9, 2000 · N311FE · Doug DC1030F · Horizontal Stabilizer StructureSDR 00FDEA00332Bulkhead · corrodedCENTER LAND GEAR WHEEL WELL FWD BULKHEAD AFT FACE CORRODED ON 1 STIFFENER LT & RT O/B. CENTER LANDING GEAR WHEEL WELL FOUND CORRODED ON L-ANGLE FWD BULKHEAD AFT FACE LWR EDGE. *S/D* REMOVED AND REPLACED PER 51-21-01 VOL LLL & 53-00-01 FIG IA VOL I. SNRM 15May 9, 2000 · N311FE · Doug DC1030F · Fuselage Main, BulkheadSDR 00FDEA00307Valve · failedLOUD BANG FROM REAR OF A/C PRESS BUMP FELT. REMOVED AND REPLACED AIR CONDITIONING SYS AIR CK VALVE IN REF TO AMM 21-22-03-2. OPS CK NORM.May 1, 2000 · N314FE · Doug DC1030F · Cabin Cooling SystemSDR 00FDEA00213Skin · crackedA/C ARRIVED TO EWR WITH DAMAGE TO LH WING OUTBD FORE FLAP. ** S/D ** R&R LT OTBD VANE ASSY PER MM 27-50-03-2. PER OPS CK NO DEFECT NOTED.Apr 8, 2000 · N311FE · Doug DC1030F · Leading Edge DevicesSDR 00FDEA00220Block · corrodedLT MAIN LANDING GEAR FIXED BRACE PILLOW BLOCK HAS CORROSION IN I/B & O/B HOLES ON TRAPEZOIDAL FITTING. REMOVED AND REPLACED CORROSION PER SRM 57-20-003 EA 8-5710-49631.Apr 7, 2000 · N303FE · Doug DC1030F · Landing Gear Retraction/Extension SystemSDR 00FDEA00210Block · corrodedRT GEAR FIXED BRACE PILLOW BLOCK I/B HOLE CORRODED. *S/D* REMOVED CORROSION PER SRM 57-20-003 EA 8-5710-49631.Apr 4, 2000 · N303FE · Doug DC1030F · Landing Gear Retraction/Extension SystemSDR 00FDEA00211Floorbeam · damagedUPPER CARGO COMP SEAT TRACK SUPPORT BEAM AT BS 919, 939, 959, 999 & 1019 FOUND TRACK ATTACH HOLES ELONGATED AFT SEAT TRACK REMOVED (LBL 47.5). *S/D* REMOVED AND REPLACED PER EA 8-5310-49609 THRU 49612.Mar 31, 2000 · N307FE · Doug DC1030F · Fuselage Main, Floor BeamSDR 00FDEA00201Rib · crackedLT WING NR 3 SLAT I/B RIB FOUND CRACKED, LENGTH 6 INCHES.Mar 30, 2000 · N307FE · Doug DC1030F · Leading Edge DevicesSDR G60A046Valve · failedAT FL33, AC PACK NR 1 FLOW VALVE WAS SURGING WITH PACK SELECT SWITCH IN AUTO. COCKPIT FILLED WITH SMOKE. RAN PROCEDURES FROM FOM VOLUME I, PAGE I-110 AND SECURED THE NR 1 AC PACK. SMOKE STOPPED AS SOON AS PACK WAS TURNED OFF. ENTERED IN MEL LOG AS MEL 21-1Mar 29, 2000 · N602GC · Doug DC1030F · Heating SystemSDR 00FDEA00145Fire Bottle · dischargedNR 2 ENGINE SHOWING LOW PRESSURE ON FIRE BOTTLE. (PER CREW DEBRIEF - AGENT NR 2). REMOVED AND REPLACED NR 2 ENGINE FIRE BOTTLE IAW 26-21-02-2.Mar 11, 2000 · N303FE · Doug DC1030F · Extinguishing SystemSDR 00FDEA00143Skin · damagedON PUSHBACK AT GATE 3 EWR, HEARD LOUD NOISE ON LEFT SIDE OF ACFT, DETERMINED THAT ACFT HAD BEEN PUSH INTO LOAD DOCK. PULL CVR D/B. ACFT TOWED TO GATE, INTERIM REPAIR WAS COMPLETED PER EA 8-5320-49721. *S/D* REPAIR PER EA 8-5310-46689.Mar 7, 2000 · N302FE · Doug DC1030F · Fuselage Main, Plate/SkinSDR 00FDEA00081Warning Light · illuminated00-46 - CAB PRESS RELIEF OPEN LIGHT ILLUMINATED. RAN RED TABS. REMOVED INSULATION MATERIAL FROM UPPER FWD POSITIVE VALVE. PERF ADJUST TEST PER DC10-30 MM 21-34-01-2, CK GOOD. OK FOR SERVICE.Feb 15, 2000 · N304FE · Doug DC1030F · Cabin Pressure Control SystemSDR 00FDEA00075Switch · failedALL 4 GEAR IND STAY RED ON BOTH PNLS. RAN RED TAB PROC WITH NO RESULTS. REMOVED AND REPLACED NR 3 SUBPEDESTAL THROTTLE SWITCH ASSY PER DC10 MM 76-11-04-2. OPS CHECK GOOD.Feb 12, 2000 · N304FE · Doug DC1030F · Power LeverSDR 00FDEA00074Prox Sensor · malfunctioned00-41 - IMMEDIATELY AFTER T/O, LG HORN SOUNDED WITH GEAR HANDLE RAISED. REMOVED AND REPLACED PROX ELECTRONIC UNIT PER MM 32-61-01-2 BOX CK GOOD.Feb 11, 2000 · N304FE · Doug DC1030F · Landing Gear Position and Warning
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