Douglas DC-8-73F

Service difficulty reports · 15,471

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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 = 'DC873F'
  ORDER BY difficulty_date DESC"

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SDR UPS07849592Doubler · corrodedINSPECTION TYPE:C3 HEAVY CORROSION ON INTERNAL DOUBLER AT FS 220 BETWEEN L35L AND L35R A-PIT. REMOVED CORROSION AND REPAIRED INTERNAL DOUBLER AT STA 220 BETWEEN LONGERONS 35L AND 35R IAW SAA EA 008-5310-01-A0747, UPS RAA DC8- 53-20613, AND FAA FORM 8100-9.Mar 15, 2007 · N811UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS07849568Longeron · corrodedINSPECTION TYPE:C3 L30R AT STA 1700 HAS CORROSION. CORROSION EXTENDS UNDER END FITTING. REMOVED EXFOLIATED AND CRACKED END FITTING AT STA 1700 L30R IAW SRM 51-1-21. FABRICATED AND INSTALLED REPLACEMENT LONGERON SEGMENT AT STA 1700 L30R IAW SRM 53-02-002 FIGMar 15, 2007 · N811UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS07849501Bulb · burned outPILOTS OVERHEAD PANEL EMERGENCY LIGHTS DISARMED LIGHT INOP. FOUND BULB BURNED OUT. REPLACED BULB, CHECKS OK.Mar 15, 2007 · N807UP · Doug DC873F · Emergency LightingSDR UPS07849593Intercostal · corrodedINSPECTION TYPE:C3 INTERCOSTAL UNDER SEAT TRACK STA 70-80 RBL 48 HAS CORROSION. REMOVED INTERCOSTAL AT STA 65-80 IAW SRM 51-1-20D. FABRICATED INTERCOSTAL AND INSTALLED AT STA 65-80 IAW DWG 4888755, AND SRM'S 51-3-2, AND 51-1-20D.Mar 14, 2007 · N811UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS07849569Fitting · crackedINSPECTION TYPE:C3 LONGERON END FITTING CRACKED AT STA 1260 TO 1280 L34L. REMOVED LONGERON SPLICE FITTING AT STA 1260-1280 L34L IAW SRM 51-1-20D. LOCATED, DRILLED AND INSTALLED LONGERON SPLICE FITTING AT STA 1260-1280 L34L IAW SRM 51-3-2, AND SRM 51-1-20D.Mar 14, 2007 · N811UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS07849577Shear Tie · corrodedINSPECTION TYPE:C3 SHEAR TIE CORRODED AT STA 660 L35R TO L35L. REMOVED SHEAR TIE AT STA 660 L35R-L35L IAW SRM 51-1-21. FABRICATED AND INSTALLED SHEAR TIE AT STA 660 L35L-L35R IAW DWG 5616509, AND SRM'S 51-1-20D, AND 51-1-21.Mar 13, 2007 · N811UP · Doug DC873F · Fuselage Internal Mounting StructureSDR UPS07849540Finger Doubler · corrodedINSPECTION TYPE:C3 CENTER WING BOX SUBFLOOR FINGER DOUBLER CORRODED AT STA 960-980 RBL 65. REMOVED FINGER DOUBLER AT STA 960-980 RBL 65 IAW SRM 51-1-21. FABRICATED AND INSTALLED FINGER DOUBLER AT STA 960-980 RBL 65 IAW SRM 53-7-3, AND SRM 53-07-03-0.Mar 13, 2007 · N811UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS07849535Finger Doubler · corrodedINSPECTION TYPE:C3 SUBFLOOR FINGER DOUBLER HEAVY CORRODED AT STA 935 RBL 65. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FINGER DOUBLER IAW SRM 53-2-0 FIG 1F, 53-07-03 AND 51-3-02.Mar 13, 2007 · N811UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS07849551Skin · damagedINSPECTION TYPE:C3 DEEP CREASED DENT 3 INCHES LONG ON LEADING EDGE O/B RIGHT WING. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-02-01-00 FIG 002H.Mar 12, 2007 · N811UP · Doug DC873F · Wing, Plate/SkinSDR UPS07849431Rib · crackedINSPECTION TYPE:C3 LEFT WING OUTBOARD LWR RIB CRACKED AT XFS 790. CRACK TERMINATES AT FASTENER HOLE PER HFEC INSP NDTSPM 06-10-01-001 FABRICATED AND INSTALLED REPAIR DOUBLERS AND ANGLES AT LEFT WING OUTBOARD LEADING EDGE STA XFS 790 IAW SRM 57-03-03 FIG 7, ANMar 9, 2007 · N811UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS07849411Skin · corrodedSKIN CORROSION/PULLED FASTENER FWD OF PIT 32 DOOR OPENING. CLASS II REPAIR CARRIED OUT TO LOWER BELLY SKIN AT STATION 498 (LONGERON 36) IAW DC8 SRM 53-02-01-0.Mar 9, 2007 · N801UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS07849599Longeron · corrodedINSPECTION TYPE:C3 L36 HEAVILY CORRODED AT STA 662. REPAIRED LONGERON 36 AT STA 662 IAW SAA EA 008-5310-01-A0734, UPS EO DC8-5310-26461-A, AND FAA FORM 8100-9.Mar 8, 2007 · N811UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS07849550Stiffener · corrodedINSPECTION TYPE:C3 HEAVY CORROSION AT BASE OF VERTICAL STIFFENER ON STA 8 BULKHEAD IN A/C COMP'T, LEFT SIDE, ABOVE L28. REMOVED, FABRICATED AND INSTALLED STIFFENER AND SPLICE REPAIR IAW SRM 51-1-21, 51-1-20D AND DWG 5615530.Mar 8, 2007 · N811UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS07849598Pressure Panel · crackedINSPECTION TYPE:C3 CRACK IN NLG WHEEL WELL CEILING (PRESSURE WEB) STA -13 LBL 2. REPAIRED PRESSURE WEB IN NLG WHEEL WELL CEILING AT STA -13 LBL 2 IAW SAA EA008-5330-01-A0745, UPS EO DC8-5330-26455-A, AND FAA FORM 8100-9.Mar 7, 2007 · N811UP · Doug DC873F · Fuselage Main, BulkheadSDR UPS07849521Skin · corrodedINSPECTION TYPE:C3 BULGING SKIN ON EXTERNAL FUSELAGE AT STA 1710 L20L. CUT OUT DAMAGED AREA ON SKIN AT STA 1710 L20L IAW SRM 53-02-01-0 FIG 7. FABRICATED & INSTALLED REPAIR DOUBLER, FILLER, AND FINGER DOUBLER AT STA 1710 L20L IAW SRM 53-02-01-0 FIG 7.Mar 7, 2007 · N811UP · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA070012OCable · out of adjustDURING TAKEOFF ROLL AT ABOUT 90 KNOTS, THE CREW HEARD TWO LOUD POPPING NOISES. THE CREW ABORTED THE TAKEOFF. ENGINE ANTI-ICE WAS ON. MAX POWER WAS SET 87 PERCENT N1. THE CREW RETURNED TO PARKING. MAINTENANCE INSPECTED THE AIRCRAFT AND COMPLIED WITH CFM56 Mar 7, 2007 · N605AL · Doug DC873F · Engine Fuel and ControlSDR UPS07849409Web · corrodedINSPECTION TYPE:C1 EXFOLIATED CORROSION ON WEB AT STA -99 - -80 RBL 30-50. REMOVED CORROSION ON WEB AT STA -99 TO -80 RBL 30-50 IAW SRM 51-1-8 FABRICATED AND INSTALLED SPLICE DOUBLER AND REPAIR DOUBLER AT STA -80 TO -90 RBL 30-50 IAW SRM 51-1-20D, AND DWG 561Mar 6, 2007 · N868UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS07849329Light · illuminatedINSPECTION TYPE:N/A DURING FLIGHT - EMERGENCY LIGHTS ILLUMINATED, UNABLE TO RESET. TRIED RESETTING ALL 3 CIRCUIT BREAKERS WITHOUT SUCCESS, TURNED EMERGENCY LIGHTS TO DISARM THEN OFF. RESET EMERGENCY EXIT LIGHT CONTROL C/B, ELIMINATED DISCREPANCY. ALL SYSTEMMar 6, 2007 · N852UP · Doug DC873F · Emergency LightingSDR UPS07849518Splice · crackedINSPECTION TYPE:C1 CRACK AT NR 4 ALT LWR FRONT SPLICE PLATE BETWEEN XRS 428 AND XRS 463. REMOVED CRACKED SPLICE FITTING AT NR 4 ALT TANK LWR FRONT SPAR CAP BETWEEN XRS 428-XRS 463 IAW SRM 51-01-20D. FABRICATED AND INSTALLED REPAIR SPLICE FITTING IAW DWG 3644Mar 5, 2007 · N868UP · Doug DC873F · Wing Main, Frame StructureSDR UPS07849300Engine · flamed outINSPECTION TYPE:N/A AT FL370, NR 4 ENGINE FLAMED OUT. NOTED NR 4 BOOST PUMP OFF. RESTARTED AFTER SECOND ATTEMPT. REMOVED AND REPLACED NR 4 MAIN FUEL FILTER IAW DC8 MM 73-10-02-4. FILTER WAS CLEAN. INSP CHIP DETECTOR IAW DC8 MM 79-20-05-2. RAN ENG. STARTMar 1, 2007 · N852UP · Doug DC873F · Engine (Turbine/Turboprop)SDR UPS07849341Longeron Splice · crackedINSPECTION TYPE:C1 LONGERON SPLICE FITTING CRACKED AT STA 1050 L31R. REMOVED AND REPLACED SPLICE FITTING IAW SRM 51-3-0, 51-1-20D.Feb 26, 2007 · N868UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS07849408Attach Fitting · crackedINSPECTION TYPE:C1 MAIN CABIN ATTACH FITTING CRACKED AT STA 857.125 L19R. REMOVED FITTING AT STA 857.125 L19R IAW SRM 51-1-20D. FABRICATED AND INSTALLED REPAIR FITTING AT STA 857.125 L19R IAW SRM 51-03-02 SRM 51-1-20D.Feb 22, 2007 · N868UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS07849271Control Unit · inoperativeINSPECTION TYPE:N/A COCKPIT EMERGENCY LIGHTS INOP. REPLACED EMERGENCY LIGHT BATTERY PACK CONTROL UNIT PER MM 33-50-02-2.Feb 22, 2007 · N813UP · Doug DC873F · Emergency LightingSDR UPS07849517Longeron Splice · corrodedINSPECTION TYPE:C1 HEAVY CORROSION UNDER SPLICE FITTING, L24R STA 45. REMOVED CORRODED LONGERON SPLICE FITTING AT STA 45-55 L24R IAW SRM 51-1-21. FABRICATED AND INSTALLED L24R SPLICE FITTING AND STIFFENER AT STA 45-55 IAW SRM 53-3-3 FIG 2, 51-3-2, AND SRM 51Feb 21, 2007 · N868UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS07849414Frame · damagedINSPECTION TYPE:C1 MAIN CABIN LONGERON FRAME AND SHEAR TIE HAS DRILLED STOP MARK AND FRAME HAS SEVERAL OPEN HOLES AT STA 80 L20R. REMOVED DAMAGED SECTION OF FRAME. FABRICATED 2 EACH REPAIR SPLICES, 1 FRAME SECTION AND 1 SHEAR TIE. INSTALLED IAW SRM 53-02-00Feb 21, 2007 · N868UP · Doug DC873F · Fuselage Main, FrameSDR UPS07849405Skin · crackedINSPECTION TYPE:C1 EXTERIOR FUSELAGE, L-1 DOOR HOLD OPEN RECEPTICAL CUTOUT HAS .375 INCH CRACKED IN AFT LWR CORNER. TRIMMED OUT DAMAGED AREA L-1 DOOR HOLD OPEN CUTOUT AFT LWR CORNER IAW SRM ADDENDUM DC8-5330-19684-A. FABRICATED AND INSTALLED REPAIR DOUBLER AFeb 21, 2007 · N868UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS07849342Seat Track · corrodedINSPECTION TYPE:C1 SEAT TRACK HEAVILY CORRODED STA 1510 RBL 45. REMOVED SEAT TRACK FROM STA 1490-1550 RBL 45. FABRICATED AND INSTALLED REPLACEMENT SEAT TRACK IAW SRM 51-3-0, 53-07-03 FIG 7-3 FIG 003.Feb 21, 2007 · N868UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS07849332Door Frame · crackedINSPECTION TYPE:C1 HFEC INSPECTED DETECTED A CRACK ON THE D-PIT UPPER FWD CORNER APPROX .156" ON LWR SIDE OF FASTENER AND .156" UPPER SIDE OF FASTENERS. CUT OUT DAMAGED AREA AT STA 1400 L23R IAW SRM 53-2-0 FIG 21. FABRICATED AND INSTALLED REPAIR DOUBLER, FILFeb 21, 2007 · N868UP · Doug DC873F · Fuselage Main, StructureSDR UPS07849331Rib · crackedINSPECTION TYPE:C3 CRACKED UPPER RIB INSIDE PANEL 518A ON LEFT WING OUTBOARD LEADING EDGE. STOP DRILLED CRACK ON UPPER RIB INSIDE PANEL 518A LEFT WING OUTBOARD LEADING EDGE IAW SRM 57-02-00 FIG 002. FABRICATED AND INSTALLED ANGLE DOUBLER ON RIB INSIDE PANEL Feb 21, 2007 · N868UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS07849519Frame · gougedINSPECTION TYPE:C1 CANTED FRAME CAP DENTED/GOUGED BEYOND LIMITS, MAIN CABIN STA 1707 L21R. REMOVED DAMAGED FRAME CAP AT STA 1707 L21R IAW SRM 51-1-21. FABRICATE AND INSTALLED FRAME CAP AT STA 1707 L21R IAW SRM 53-2-0, 51-1-20D AND DWG 5612146.Feb 20, 2007 · N868UP · Doug DC873F · Fuselage Main, FrameSDR UPS07849502Fitting · crackedINSPECTION TYPE:C1 MAIN CABIN LONGERON END FITTING CRACKED STA 900 L10L. REMOVED AND REPLACED END FITTING IAW SRM 51-1-20D AND 51-2-15.Feb 20, 2007 · N868UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS07849430Frame · crackedINSPECTION TYPE:C1 HOLE DRILLED THRU EDGE OF FRAME, INTO RADIUS, MAIN CABIN STA 1600 L9R. REMOVED SPLICE ANGLE AND CUT OUT DAMAGE, FABRICATED AND INSTALLED -J- DOUBLER AND FILLER IAW EO DC8-5310-11728B AND DWG DC-853A-011A.Feb 20, 2007 · N868UP · Doug DC873F · Fuselage Main, FrameSDR UPS07849410Door Frame · crackedINSPECTION TYPE:C1 R2 DOOR JAMB WEB CRACKED, 2 PLACES, AT DOOR SNUBBER, STA 1618 L15R TO L16R. REMOVED WEB FROM R2 DOOR JAMB AT FS 1618 L15R-L16R IAW SRM 51-1-21. FABRICATED AND INSTALLED WEB AT STA 1618 L15R-L16R IAW DWG 5772656 AND SRM 51-3-2 AND SRM 51-1-Feb 20, 2007 · N868UP · Doug DC873F · Fuselage Main, StructureSDR UPS07849340Bracket · crackedINSPECTION TYPE:C1 APB BRACKET CRACKED STA 1766 L6L MAIN CABIN. REMOVED, FABRICATED AND INSTALLED APB BRACKET IAW SRM 51-1-21, 51-1-2 0D AND DWG 5773844.Feb 20, 2007 · N868UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS07849339Fitting · crackedINSPECTION TYPE:C1 MAIN CABIN FWD OF THE 857.123 L6L END FITTING CRACKED. REMOVED AND REPLACED END FITTING IAW SRM 51-1-20D AND 51-3-0.Feb 20, 2007 · N868UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS07849323Fitting · crackedINSPECTION TYPE:C1 L10R END FITTING CRACKED AT STA 1763, MAIN CABIN. REMOVED CRACKED END FITTING AT STA 1763 L10R IAW SRM 51-1-20D. LOCATED, DRILLED UP, AND INSTALLED END FITTING AT STA 1763 L10R IAW SRM 51-3-2, AND SRM 51-1-20D.Feb 20, 2007 · N868UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS07849322Fitting · crackedINSPECTION TYPE:C1 CRACK IN END FITTING, L17R, STA 1763, MAIN CABIN. REMOVED L17R END FITTING AT STA 1763 IAW SRM 51-1-20D. LOCATED, DRILLED UP, AND INSTALLED L17R END FITTING AT STA 1763 IAW SRM 51-3-2, AND SRM 51-1-20D.Feb 20, 2007 · N868UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS07849225Light · faultyINSPECTION TYPE:N/A EMERGENCY LIGHTS WILL NOT DISARM. RELAMPED DISARM INDICATION LIGHT. OPS CHECK OK.Feb 20, 2007 · N802UP · Doug DC873F · Emergency LightingSDR UPS07849215Switch · stiffINSPECTION TYPE:N/A EMERGENCY EXIT LIGHT SWITCH HARD TO MOVE TO DISARM CHECK POSITION. REPLACED EMERGENCY EXIT LIGHT SWITCH PER IPC 33-50-00-003. OPS CHECK OK PER AMM 33-50-00-0.Feb 18, 2007 · N802UP · Doug DC873F · Emergency LightingSDR UPS07849597Spar Cap · crackedINSPECTION TYPE:C3 DURING WING FORWARD SPAR INSPECTION FOUND 1EA ATTACHMENT HOLE CRACKED. REPAIRED LEFT WING FRONT SPAR LWR CAP BETWEEN XFS 515 AND 526.76 IAW SAA EA 008-5710-01-A0733, UPS EO DC8-5710-26430-A, AND FAA FORM 8100-9.Feb 14, 2007 · N811UP · Doug DC873F · Wing SparSDR UPS07849192Battery Pack · inoperativeINSPECTION TYPE:N/A ON EMERGENCY EXIT LIGHTS TEST, NO LIGHTS WOULD OPERATE. STANDBY INSTRUMENTS OK. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY POWER PACK ASSY & SYS. OPS CHECKED NORMAL IAW MM 33-50-01-2.Feb 11, 2007 · N880UP · Doug DC873F · Emergency LightingSDR UPS07849158Battery Pack · inoperativeINSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. REPLACED EMERGENCY BATTERY PACK IAW 33-50-01-2.Feb 8, 2007 · N880UP · Doug DC873F · Emergency LightingSDR UPS07849138Girt Bar · stiffINSPECTION TYPE:N/A THE EMERGENCY ESCAPE SLIDE GIRT BAR IS VERY DIFFICULT TO ENGAGE & DISENGAGE. REPACKED EMERGENCY ESCAPE SLIDE IN ITS CONTAINER. GIRT BAR STOWS OK.Feb 7, 2007 · N874UP · Doug DC873F · Escape SlideSDR UPS07849137Lamp · burned outINSPECTION TYPE:N/A EMERGENCY EXIT DISARM LIGHT BURNED OUT. EMERGENCY EXIT DISARM LIGHT RELAMPED IAW DC8 AMM 33-50-02-2.Feb 7, 2007 · N867UP · Doug DC873F · Emergency LightingSDR IXXA070005OProximity Switch · defectiveAFTER GEAR RETRACTION,THE LANDING GEAR DOORS NOT LATCHED LIGHT ILLUMINATED. THE CREW RECYCLED THE GEAR AND THE LIGHT REMAINED ON, UNTIL THE GEAR WAS EXTENDED. THE CREW CONTINUED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE GEAR AND FOUND SEVERAL LOOSJan 30, 2007 · N606AL · Doug DC873F · Door Warning SystemSDR UPS07849069Battery · inoperativeFOUND COCKPIT COURIER AREA AND ENTRY DOORS LIGHT INOP DURING PREFLIGHT BATTERY SAI EMERGENCY LIGHTS CHECK. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT PER MM 33-50-01-2.Jan 30, 2007 · N811UP · Doug DC873F · Emergency LightingSDR 8012007001Seat Track · crackedDURING A "B" CHECK IN FT LAUDERDALE FL, THE FOLLOWING DISCREPANCIES WERE NOTED; A .500 CRACK WAS FOUND ON THE RT O/B SEAT TRACK AT FUSE STA 1690. PER DOUGLAS AIRCRAFT SRM, 53-2-3 THE FOLLOWING REPAIR WAS PERFORMED, REMOVED SEAT TRACK FROM STA 1690 TO 1696. IJan 29, 2007 · N801DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS07849041Wire · brokenFOUND EMERGENCY LIGHTS INOP. FOUND WIRE NR L610A20 BROKEN AT TOGGLE SWITCH. REPAIRED WIRE IAW DCI WDM 33-50-01. TOGGLE SWITCH REPLACED AS PRECAUTION IAW DC8 AMM 20-50-01-4. CHECKS SERVICEABLE IAW DC8 AMM 33-50-02-2.Jan 26, 2007 · N810UP · Doug DC873F · Light System WiringSDR UPS07848982Battery Pack · dischargedINSPECTION TYPE:N/A DURING PDC, EMERGENCY LIGHT INOP. REPLACED EMERGENCY LIGHT BATTERY PACK IAW DC8 AMM 33-50-01-2. CHECK SERVICEABLE.Jan 24, 2007 · N851UP · Doug DC873F · Emergency LightingSDR UPS07849680Attach Fitting · crackedINSPECTION TYPE:C1 ATTACH FITTING CRACKED AT STA 787 L13R. REMOVED FITTING AT STA 787 L13R IAW SRM 51-1-20D. FABRICATED AND INSTALLED LONGERON END FITTING AT STA 787 L13R IAW SRM 51-01-21-0, NAD SRM 51-1-20D.Jan 14, 2007 · N819UP · Doug DC873F · Fuselage Main, Attach Fittings
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