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"

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SDR 00FDEA00064Blade · damagedON T/O, FLEW THROUGH FLOCK OF BIRDS, NR 1 ENG START TO VIB. VIB SUBSIDE BELOW 65 DEG N1. RETURN TO SFS. *S/D* REMOVED AND REPLACED DAMAGED BLADES (5) PER MM 72-21-06-81. PERF VIB SURVEY CK AND TRIM BALANCING PER MM 72-00-00 AND DC 10 JRH. OK A/C OK FOR Feb 8, 2000 · N312FE · Doug DC1030F · Engine (Turbine/Turboprop)SDR 00FDEA00137Seat Track · crackedSNRM 246 - UPPER FUSELAGE SEAT TRACK BASE CRACKED AT BS 965, RBL 28.0. REWORKED AND SPLICE PLATES FABRICATED, PAINT AND WET INSTALLED PER SRM 53-70-00 FIG VOL 1.Feb 5, 2000 · N312FE · Doug DC1030F · Fuselage, Seat/Cargo Attach FittingsSDR 00FDEA0025Connector · failedNR 751 - RT W/W FWD INBD ELECT HYD PUMP CANNON PLUG WAS A SHORTED WIRE. PUMP HAD 2 EA SHORT WIRES CAUSING ELECTRICAL FIRE.Jan 18, 2000 · N314FE · Doug DC1030F · Hydraulic Pump (Electric/Engine), MainSDR 00FDEA00025Connector · failedNR 751 - RT W/W FWD INBD ELECT HYD PUMP CANNON PLUG WAS A SHORTED WIRE. PUMP HAD 2 EA SHORT WIRES CAUSING ELECTRICAL FIRE. REPLACED WIRE HARNESS, PLUG CONNECTOR PER WD/M 29-21-01, 29-21-02. REPLACED HYD PUMP AND ELECT MOTOR PER MM 29-21-01-2. OPS AND LEAK Jan 18, 2000 · N314FE · Doug DC1030F · Hydraulic Pump (Electric/Engine), MainSDR 99FDEA00494Warning Light · illuminatedNR 3 PNEUMATIC FAIL LIGHT ILLUM. COMPLETED RED TABS.Dec 1, 1999 · N310FE · Doug DC1030F · Airfoil Anti/De-ice SystemSDR 99ZZZX4541Girt Assy · unapproved partGIRT ASSY (LOWER) WAS MADE FROM AN UNKNOWN FABRIC AND IDENTIFIED WITH THE MANUFACTURER'S (BFG) P/N SWD230305-102 AND WITHOUT THE MANUFACTURER'S INSPECTION STAMP AND INSPECTION DATE. THIS PART IS NOT PER THE MANUFACTURER'S DRAWING AND IS CONSIDERED A SUSPECTEDNov 29, 1999 · Doug DC1030F · Emergency EquipmentSDR 99ZZZX4540Girt Assy · unapproved partGIRT BAR FLAP ASSY WAS MADE FROM AN UNKNOWN FABRIC AND IDENTIFIED WITH THE MANUFACTURER'S (BFG) P/N SWD230105-103, AND WITHOUT THE MANUFACTURER'S INSPECTION STAMP AND INSPECTION DATE. THIS PART IS NOT PER THE MANUFACTURER'S DRAWING AND IS CONSIDERED A SUSPECTENov 29, 1999 · Doug DC1030F · Emergency EquipmentSDR 99ZZZX4539Girt Assy · unapproved partGIRT ASSY WAS MADE FROM AN UNKNOWN FABRIC AND IDENTIFIED WITH THE MANUFACTURER'S (BFG) P/N SWD230305-100, AND WITHOUT THE MANUFACTURER'S INSPECTION STAMP AND INSPECTION DATE. THIS PART IS NOT PER THE MANUFACTURER'S DRAWING AND IS CONSIDERED A SUSPECTED UNAPPRNov 29, 1999 · Doug DC1030F · Emergency EquipmentSDR G60A038Elevators · damagedTCAS MADE CONTACT WHILE FLT GCO7580 WAS DEPARTING PHNL, AT APPROXIMATELY 3800 FT. FLIGHT CREW INITIATED EVASIVE MANEUVER WHICH RESULTED IN STRUCTURAL DAMAGE TO BOTH LT AND RT ELEVATORS. (M)Nov 7, 1999 · N602GC · Doug DC1030F · Elevator StructureSDR 2000ZZZM12Elevators · damagedTCAS MADE CONTACT WHILE FLT GCO7580 WAS DEPARTING PHNL, AT APPROXIMATELY 3800 FT. FLIGHT CREW INITIATED EVASIVE MANEUVER WHICH RESULTED IN STRUCTURAL DAMAGE TO BOTH LT AND RT ELEVATORS. (M)Nov 7, 1999 · N602GC · Doug DC1030F · Elevator StructureSDR WRLA99019Windshield · crackedDURING CRUISE FLIGHT CREW NOTICE CRACK IN F/O WINDSCREEN STARTED SLIGHT 'ARCING' W/RIGHT ANTI-ICE IN NORM ABOUT 2 MIN AFTER START OF DESCENT. FLIGHT CREW SECURED RIGHT WINDSHIELD ANTI-ICE. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. (M) MAINTENANCE PERSONNEL Oct 27, 1999 · N107WA · Doug DC1030F · Flight Compartment WindowsSDR 99FDEA00458Bolt · looseLT WING INBD FLAP HINGE BOLT TO REAR SPAR FND LOOSE AND ABOUT A QTR OF THE NUT MATERIAL MISSING.Oct 21, 1999 · N301FE · Doug DC1030F · Trailing Edge FlapsSDR 99FDEA00447Tee · crackedLT HOR-STAB LEAD EDGE PNL 2ND FROM I/B (CTR I/B) FOUND TOP CAP CRACKED (XFS.166.161) APPROX 46 .375 LONG. *S/D* REMOVED AND REPLACED NEW CAP PER SRM 51-35-01 VOL II.Oct 21, 1999 · N301FE · Doug DC1030F · Horizontal Stabilizer StructureSDR 99FDEA00446Strap · crackedRT HORIZ STAB LEADING EDGE PNL 3RD FROM I/B (CENTER) FOUND TOP TEE BRACKET CRACKED (XFS 172.161) APPROX 26 .75 LONG. *S/D* NEW STRAP FAB PER DWG ALC7506, REMOVED AND REPLACED PER SRM 51-33-01 VOL II.Oct 21, 1999 · N301FE · Doug DC1030F · Horizontal Stabilizer StructureSDR 99FDEA00440Actuator · looseLT MAIN LANDING GEAR DOWNLOCK ACTUATOR FOUND ACTUATOR END WITH BOLT LOOSE AND NUT MISSING. *S/D* REPLACED AND TIGHTENED BUSHING AND NUT PER MM 20-50-02-2.Oct 20, 1999 · N301FE · Doug DC1030F · Landing Gear Retraction/Extension SystemSDR 99FDEA00436Warning · activatedAIR COND DOOR LIGHT ON S/O PNL ILLUM IN FLT DURING CLIMB. VERIFIED AND RECORDED IN AML. AC DOORS ARE CLOSED BY VISUAL INSP PRIOR TO EACH DEPARTURE.Oct 19, 1999 · N309FE · Doug DC1030F · Door Warning SystemSDR G6OA037Door · looseON GEAR RETRACTION ON DEPARTURE FROM KLAX, FELT SEVERE VIBRATIONIN NOSE GEAR AREA. ON ARRIVAL AT KSAN, FOUND RIGHT NOSE GEAR DOOR OPEN. INSPECTED NOSE GEAR DOORS AND LOCKING MECHANISMS IAW MM 32-21-00. RESECURED NOSE GEAR DOORS AND LOCKING MECHANISMS. NOSEOct 12, 1999 · N600GC · Doug DC1030F · Landing Gear Door Retract SectionSDR 99FDEA00418Hardware · loose12 OFF MOUNTING BOLTS LOOSE AND 3 OFF NUTS MISSING FROM SHEAR WEB FORGINGS ON AFT NR 1 PYLON FRAME, ADJACENT TO SPHERICAL BEARING FITTING. REMOVED AND REPLACED PER MM 70-00-00-2.Oct 6, 1999 · N317FE · Doug DC1030F · Nacelle/Pylon StructureSDR 99FDEA00423Control Cable · brokenLT WING NR 6 SLAT EXTEND CABLE FOUND SNAPPED OFF. REMOVED AND REPLACED IAW MM 27-89-11-4. CABLES RE-RIGGED AND FUNCTIONAL TEST CARRIED OUT IAW MM 27-80-00-05. FOUND SATISFACTORY.Oct 5, 1999 · N317FE · Doug DC1030F · Leading Edge Slat Control SystemSDR G60A035Audio Control · failedF/E AUDIO CONTROL PANEL INOPERATIVE AND STARTED SMOKING. DISCONNECTED CONTROL PANEL. REMOVED AND REPLACED AUDIO CONTROL PANEL AND SYSTEM OPS CHECK NORMAL IAW MM 23-44-00. (M)Sep 27, 1999 · N600GC · Doug DC1030F · Audio Integrating SystemSDR 99FDEA00388Seat Track · crackedMAIN DECK UPPER CARGO, SEAT TRACK CRACKED AT BS 635 X=27.5-242. UPPER CARGO SEAT CRACK AT BS Y=755 INTERSECTING X=8.5. *S/D* REPAIRED MDUC PER SRM 53-70-00 VOL 1-242 & UCST PER SRM 53-70-00 VOL 1-243.Sep 14, 1999 · N310FE · Doug DC1030F · Fuselage, Seat/Cargo Attach FittingsSDR 99FDEA00384Skin · crackedRT WING LOWER SURFACE OF LEADING EDGE ALONG XORS 402 FOUND WITH 2 INCH CRACK. *S/D* REPAIR CARRIED OUT PER SRM 57-10-00 FIG 68 VOL 1.Sep 10, 1999 · N310FE · Doug DC1030F · Wing, Plate/SkinSDR 99FDEA00369Tr Cowl · departedNR 2 ENGINE THRUST REVERSER TRANSLATING COWL DEPARTED THE A/C ON LANDING. *S/D* REMOVED AND REPLACED NR 2 RT T/R FAN IAW MM 78-32-11-2.Sep 6, 1999 · N310FE · Doug DC1030F · Engine Thrust ReverserSDR 99FDEA00365Fillet · missingPIECE OF AC LOST ON T/O ROTATION. LEFT SLAT TO FUSELAGE FILLET DEPARTED A/C. INSP FUSELAGE AFT OF MISSING PERFORMANCE FAIRING NO DAMAGE NOTED. ALSO INSPECTED NR 2 ENG INTAKE WITH NO DAMAGE NOTED. REMOVED AND REPLACED CLOSE-OUT STRIP OF I/B 1L SLAT UPON INSSep 1, 1999 · N311FE · Doug DC1030F · Aerodynamic FairingsSDR 99FDEA00368Seat Track · crackedMAIN DECK UPPER FUSELAGE, CRACK FOUND ON SEAT TRACK AT BS 635 X=27.5 LH-687. MAIN DECK UPPER FUSELAGE CRACK ON SEAT TRACK AT BS 635 X=75.25 RH-688. MAIN DECK CRACK ON SEAT TRACK AT BS 775X=8.5 RH-700. *S/D* REPAIRED SEAT TRACKS 687, 688, 700 AS PER SRM 53-Aug 31, 1999 · N321FE · Doug DC1030F · Fuselage, Seat/Cargo Attach FittingsSDR 99FDEA00331Controller · malfunctionedON TAKEOFF, PNEUMATIC TEMP HI LIGHT FLICKERED INTERM ON PILOT ANNUNCIATOR PANEL. REMOVED AND REPLACED OVERHEAD WARN AND CAUTION ANNUN, SYS LOGIC CONTROLLER UNIT, UNIT PER MM 33-15-03-2. OPS CK GOOD.Aug 12, 1999 · N303FE · Doug DC1030F · Overheat DetectionSDR 99FDEA00297Fuse · cracked99-182 - AFT GEAR RETRACTION, HYD QUAN AND PRESSURE ON NR 3 SYS DROPPED TO 0. REPLACED THE CRACKED LOCK OUT FUSE PER MM 32-31-06-2 ALSO NR 3 HYD SYS CASE DRAIN FILTER CK IS OK PER MM 29-12-02-2 AND MM 29-12-17-2. LEAK CK IS OK CLOSED SECURED AND NR 3 ENG COJul 29, 1999 · N320FE · Doug DC1030F · Hydraulic System, MainSDR 99FDEA00273Clip · crackedSNRM 308,309,310 LT WING TO FUSELAGE UPPER FAIRING SUPPORT RIBS ATTACH CLIP CRACKED AT BS 1225, BS 1289, BS 1300, BS 1310, BS 1341 AND BS 1375. L/H WING TO SELAGE FARIR BOTTOM SUPT RIBS CRACKED. CARRIED OUT REPAIRS PER AEA 0553, ANB 7140, ANB 7139, AEA 0552,Jul 19, 1999 · N319FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR 99FDEA00266Trim Cylinder · malfunctioned99-162 - GEAR HANDLE WOULD NOT RAISE AFT T/O. RED TAB RAN BUT STILL DID NOT WORK. GOOD HYDS ON ALL 3 SYS. NO PINS FND. BLED/RESET TRIM CYLINDER INTERLOCK FUSE PRECAUTIONARY PER DC-10 MM 32-31-06-2. A/C OK FOR RETURN TO SERVICE.Jul 18, 1999 · N308FE · Doug DC1030F · Landing Gear Retraction/Extension SystemSDR 99FDEA00248Tail Cone · damagedIN FLT HAD LOUD BANG FOLLOWED BY AIRFRAME VIBRATIONS. ON POST FLT PATIO DOORS UNDER NR 2 ENGINE HAD OPENED IN FLT. *S/D* REMOVED AND REPLACED LT AND RT DROOP ELEVATORS AND TAIL CONE ASSY PER MM 27-30-03-4, MM 53-52-00. REPAIRED TAIL MISMATCH COVER ON EA 8-Jun 29, 1999 · N303FE · Doug DC1030F · Aerodynamic FairingsSDR G6OA033Mount · looseDURING C-CHECK INSPECTION, NR 1 ENGINE FORWARD MOUNT WAS FOUND SLIGHTLY SEPARATED. FURTHER INVESTIGATION FOUND NUT/BOLT LOOSENED FROM EACH OTHER WHICH ALLOWED THE MOUNTING BRACKET TO SEPARATE. INSPECTED AND RE-WORKED PER EO 99-5415-026. RE-INSTALLED ENGINE, Jun 24, 1999 · N600GC · Doug DC1030F · Engine Mount SectionSDR G6OA034Aoa Sensor · badDURING CLIMB-OUT, AUTO SLAT SYSTEM DEPLOYED. AFTER TROUBLESHOOTING, REMOVED AND REPLACED NR 2 AOA SENSOR IAW 22-31-01. SLAT SYSTEM TESTED OK IAW 22-33-00. (M)Jun 16, 1999 · N607GC · Doug DC1030F · Stall Warning SystemSDR 99ZZZX3012Mount · looseC-CHECK - PYLONS DURING ROUTINE INSPECTION. REF: J/C 0834, FOUND FORWARD ENGINE MOUNT BOLTS WITH LOCKWIRE BROKEN AND CAP BETWEEN FORWARD PYLON ENGINE MOUNT AND FORWARD ENGINE MOUNT, LT SIDE 0.065 INCH. RT SIDE 0.085 INCH.May 28, 1999 · N600GC · Doug DC1030F · Engine Mount SectionSDR 99ZZZX3011Mount · looseC-CHECK - PYLONS DURING ROUTINE INSPECTION. REF: J/C 0834, FOUND FORWARD ENGINE MOUNT BOLTS WITH LOCKWIRE BROKEN AND CAP BETWEEN FORWARD PYLON ENGINE MOUNT AND FORWARD ENGINE MOUNT, LT SIDE 0.065 INCH. RT SIDE 0.085 INCH.May 28, 1999 · N600GC · Doug DC1030F · Engine Mount SectionSDR 99FDEA00181Vane · failedBUFFET ENCOUNTERED AS FLAPS SEL TO 35 DEG EXT BUFFET INCREASED WHEN FLAPS 50 DEG EXT SEL. REMOVED AND REPLACED RT I/B AND O/B FLAP VANE ASSY AND OPS CK NORM PER MM 27-50-03-2.May 12, 1999 · N309FE · Doug DC1030F · Trailing Edge FlapsSDR 99FDEA00136Frame · corrodedMAIN CARGO DECK OVER MLG WHEEL WELL AREA, FUSELAGE FRAME AT BS 1521 HAS CORROSION. ** S/D ** REMOVED 3 FLOOR PNL FOR ACCESS TO CTR WHEEL WELL. REMOVED CORROSION, NDT CK HOLES AND THICKNESS. ALODINED AND PAINTED. INSTALLED FASTENERS PER 53-33-00. INSTALApr 6, 1999 · N307FE · Doug DC1030F · Fuselage Main, FrameSDR G6OA031Latches · failedON TRANSIT WALK AROUND INBOARD DETACHABLE ELEVATOR IN DETACHED POSITION. LATCH PINS FOUND SHEARED. REMOVED AND REPLACED LEFT DETACHABLE ELEVATOR LATCHES, TWO P/N H2188-1, AND INSTALLED ALL REQUIRED FASTENERS. RELATCHED ELEVATOR AND CHECKED FOR PROPER MOVEMEApr 4, 1999 · N600GC · Doug DC1030F · Elevator Control SystemSDR G60A031Latches · shearedON TRANSIT WALK AROUND, FOUND INBOARD DETACHABLE ELEVATOR IN DETACHED POSITION. LATCH PINS FOUND SHEARED. REMOVED AND REPLACED LEFT DETACHABLE ELEVATOR LATCHES, TWO P/N H2188-1, AND INSTALLED ALL REQUIRED FASTENERS. RELATCHED ELEVATOR AND CHECKED FOR PROPERApr 4, 1999 · N600GC · Doug DC1030F · Elevator Control SystemSDR 99ZZZX1375Cdp Line · contaminatedTEN MINUTES AFTER T/O OUT OF NARITA ON CLIMBING TO 10,000 FEET, CREWS NOTICED NR 3 ENGINE POWER LAGGING BEHIND COMPARED WITH ENG 1 AND ENG 2. ATTEMPTS TO RESTORE NORMAL POWER TO THAT ENGINE FAILED AND ACFT MADE AN ATB. DURING T/S, CHECKED MAIN FUEL FILTER ANMar 10, 1999 · N10MB · Doug DC1030F · Fuel Controlling SystemSDR 99FDEA00092Spar · corrodedLEFT AFT UPPER CORNER OF THE CENTER WING BOX AT BS 118 TO 112 TO INCLUDE THE CLOS RIB AND ATTACH UPPER SKIN PLATES AT BS 1370 TO 1358 WERE FOUND WITH EXFOLIATION CORROSION DURING C-CHECK INSP IN THE LT MLG WHEEL WELL. ALL CORROSION HAS BEEN REMOVED, WAITING FMar 9, 1999 · N320FE · Doug DC1030F · Wing SparSDR G60A045Structure · damagedDURING GROUND OPERATIONS LOADING AT SAN DIEGO, CA, THE AIRCRAFT WAS STRUCK BY A FORK LIFT. THE DAMAGE TO THE AIRCRAFT STRUCTURE CONSISTS OF A 48 INCH BY 6 INCH HOLE FORWARD OF THE FORWARD EQUIPMENT BAY. (M)Mar 7, 1999 · N607GC · Doug DC1030F · Fuselage Main, StructureSDR 99ZZZX2220Bulkhead · crackedIN NARITA AFTER UNLOADING LC5 PALLET CENTER CARGO COMPT, CARGO HANDLER FOUND IMPACT DAMAGE (CRACK) AT BLKHD STA 1841 BETWEEN CENTER CARGO AND AFT GARGO HOLD. CRACKS OF APPROX 7-8 INCHES FROM IMPACT POINT ABOUT 2 INCHES FROM FLOORBOARD LEVEL. DAMAGE CAUSED BYMar 5, 1999 · N10MB · Doug DC1030F · Fuselage Main, BulkheadSDR 99FDEA00089Wire · meltedAPU GENERATOR FEEDER CABLE SHORTING OUT WHERE IT PASSES THRU BS 2007 - PRESSURE BULK HEAD. REMOVD AND REPLACED C PHASE CABLE AND THE PRESSURE SEAL FITTING ASSY.Mar 5, 1999 · N312FE · Doug DC1030F · Electrical Power System WiringSDR 99FDEA00045Retract Mech · malfunctionedLANDING GEAR WOULD NOT EXTEND, ALL LIGHTS STAYED RED, FRONT AND BACK PANEL. RAN CKLIST OK. *S/D* REMOVED AND REPLACED LANDING GEAR SEL VALVE PER DC10-30 MM 32-31-03-2, RIGGED CABLES BETWEEN LANDING GEAR CONTROL HANDLE AND SEL VALVE PER DCN -30 MM 32-31-01-5Feb 5, 1999 · N301FE · Doug DC1030F · Landing Gear Retraction/Extension SystemSDR G6OA042Bolt · looseNR 1 ENGINE FORWARD MOUNT TRUSS FITTING TO PYLON MOUNT BOLTS SHOWS SLIPPAGE ON TORQUE STRIPE INDEX. PERFORMED RE-WORK AS REQUIRED BY REF; DC-10 SB A54-99, REVISION 4 DATED FEB 15, 1995. (M)Feb 4, 1999 · N602GC · Doug DC1030F · Engine Mount SectionSDR G6OA041Bolt · looseNR 1 ENGINE FORWARD MOUNT TRUSS FITTING TO PYLON MOUNT BOLTS SHOWS SLIPPAGE ON TORQUE STRIPE INDEX. PERFORMED RE-WORK AS REQUIRED BY REF DC-10-SB A54-00, REVISION 4 DATED FEB 15, 1995. (M)Feb 4, 1999 · N602GC · Doug DC1030F · Engine Mount SectionSDR G6OA030Seat · smokingEN ROUTE FROM LSB TO SNN, THE FLIGHT CREW NOTICED A SMOKE ODOR AND SMOKE COMING FROM THE FLIGHT ENGINEER SEAT BASE. THE FLIGHT ENGINEER SEAT CONTROL CIRCUIT BREAKERS WERE OPENED. THE ODOR AND SMOKE CLEARED. AIRCRAFT CONTINUED ON MEL 25-1. (M)Jan 21, 1999 · N601GC · Doug DC1030F · Flight Compartment EquipmentSDR 99FDEA00013Transmitter · failed99-0013 - ON T/O FLAP LIMIT CHANNEL INOP AND SELECT FLAP LIMIT OVERRIDE LIGHT ILL IN READ 10 DEG LT SIDE AND 4 DEG RT SIDE. FOUND LT OTBD FLAP POS TRANSMITTER BAD. REMOVED AND REPLACED SAME PER MM 27-54-03-2. OPS CK GOOD. FOUND DUPLEX ACTUATOR INOP MM 27-5Jan 14, 1999 · N314FE · Doug DC1030F · Trailing Flap Position Indicating SystemSDR 99FDEA00011Switch · inopAT FL 180 AIR COND DOOR LIGHT CAME ON. A/C REMAIN PRESS, RETURN TO MEM. *S/D* REMOVED AND REPLACED BOTH LEFT SIDE ACCESS DOOR SWITCH IAW MM 52-70-07. REMOVED AND REPLACED RING TERMINAL, P1-1618 AND RE-TERMINATED WIRES IAW MM CHAPTER 20. AIR COND DOOR LIGHJan 13, 1999 · N317FE · Doug DC1030F · Door Warning SystemSDR G6OA029Fire Detector · malfunctionedWHILE ON FINAL APPROACH TO MIA, THE LOWER AFT CARGO COMPARTMENT FIRE WARNING LIGHT BECAME ILLUMINATED. THE NR 1 FIRE BOTTLE WAS DISCHARGED, THE LOWER AFT CARGO COMPARTMENT FIRE WARNING LIGHT WENT OUT. GROUND MAINTENANCE REMOVED AND REPLACED THE NR 1 FIRE BOTDec 31, 1998 · N607GC · Doug DC1030F · Fire Detection
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