Douglas DC-8-71F

Service difficulty reports · 8,938

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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 = 'DC871F'
  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 UPS03840134Rod · corrodedRT MAIN LANDING GEAR RETRACT ACTUATOR HAS CORROSION ON ROD END, JAM NUT & LOCK TAB WASHER ROD END CONDITION UNKNOWN. REPAIR PER EO DC8-3230-3958-D PARTS ON ORDER, ACTUATOR AND ROD END ASSY. REMOVED AND REPLACED MLG ACTUATOR IAW MM 32-32-02.Feb 2, 2003 · N744UP · Doug DC871F · Landing Gear ActuatorSDR UPS03840131Slide · deployedINSPECTION TYPE: B, WHILE ADJUSTING SIGHT GAUGE ON L1, EVAC-SLIDE INADVERTENTLY DEPLOYED SLIDE. ALL PROCEDURES WHILE ADJUSTING WERE DONE IAW MM 25-60-04. SLIDE WAS PUNCTURED ON CREW ENTRY STAIRS WHILE INFLATING. REMOVED EVAC-SLIDE FROM ACFT.Feb 2, 2003 · N730UP · Doug DC871F · Escape SlideSDR IXXA300010OShutoff Valve · looseUPON TAKEOFF ROLL FROM CLT WITH INTENTION TO FLY TO TOL. CREW NOTED NR 4 ENGINE WAS NOT PRODUCING SELECTED POWER. CREW REJECTED TAKEOFF WHEN GROUND SPEED REACHED 80 KNOTS. CREW RETURNED TO BLOCKS. UPON INSPECTION, MAINTENANCE DISCOVERED NR 4 ENG FUEL SHUT Jan 31, 2003 · N825BX · Doug DC871F · Fuel Selector/Shut-Off ValveSDR IXXA0300009OConnector · dirtyAFTER DEPARTURE FROM LRD IN CRUISE EN ROUTE TO DFW, CREW NOTED ABNORMAL RISE IN NR 1 ENGINE EGT. POWER WAS RETARDED ON NR 1 ENGINE AND TEMP RISE STOPPED. DURING DESCENT INTO DFW NR 1 EGT AGAIN BEGAN TO RISE ABNORMALLY, AS A PRECAUTIONARY ACTION NR 1 ENGINE WJan 30, 2003 · N823BX · Doug DC871F · Turbine Engine System WiringSDR IXXA060478SPanel · chafedDURING ROUTINE C CHECK, FOUND LEFT WING UPPER TRAILING EDGE PANEL AFT OF TRUNNION PANEL CHAFED ON INBOARD UPPER SKIN. REMOVED DAMAGED AREA, FABRICATED REPAIR DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED DOUBLER. IAW 57-2-0, 57-2-1, 57-3-Jan 29, 2003 · N820BX · Doug DC871F · Wing, Plate/SkinSDR IXXA060479SLongeron · crackedDURING ROUTINE C CHECK, FOUND LONGERON 11 RIGHT CRACKED AT AFT SERVICE DOOR JAMB UPPER AFT CORNER. FABRICATED NEW LONGERON AND NEW SPLICES, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED AND INSTALLED NEW LONGERON AND SPLICES IAW DOUGLAS DRAWING 3773512, DC8 SRM Jan 28, 2003 · N820BX · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA060482SPlate · gougedDURING ROUTINE C CHECK, FOUND THE LEFT NR 4 FLAP VANE CENTER OUTBOARD FLAP ATTACH PLATE GOUGED. REMOVED DAMAGED PLATE, FABRICATED NEW PLATE, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED AND INSTALLED NEW PLATE IAW DOUGLAS DRAWING 565-37552 DC8 SRM 51-3-0, AND 5Jan 27, 2003 · N820BX · Doug DC871F · Trailing Edge FlapsSDR IXXA060481SIntercostal · crackedDURING ROUTINE C CHECK, FOUND INTERCOSTAL CRACKED FROM STATION 1140 TO STATION 1160, AT LONGERON 33 LEFT. REMOVED DAMAGE, FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS. IAW DC8 SRM 53-2-0, 51-1-8, AND 51-1-21.Jan 27, 2003 · N820BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA060484SFrame · crackedDURING ROUTINE C CHECK, FOUND A CRACKED FRAME AT STATION 280 LONGERON 29 RIGHT. REMOVED DAMAGED FRAME, FABRICATED NEW FRAME, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW FRAME IAW DOUGLAS DRAWING 9779487, DC8 SRM 51-1-8, AND 51-1-20D.Jan 26, 2003 · N820BX · Doug DC871F · Fuselage Main, FrameSDR IXXA060483SStringer · corrodedDURING ROUTINE C CHECK, FOUND THE CENTER WING LOWER STRINGER 76 LEFT CORRODED AT STATION XCW50.0. REMOVED CORROSION. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW TIMCO REPAIR ENGINEERING ORDER REO-G09014Jan 26, 2003 · N820BX · Doug DC871F · Wing, Longeron/StringerSDR IXXA0300007OBellcrank · crackedAFTER TAKEOFF SPOILER EXTENDED LIGHT ILLUM. ACFT EXHIBITED INAPROPRIATE FLT CHARACTERISTICS. RETURNED FOR UNEVENTFUL LANDING. MX NOTED SPOILER HYD RESERVOIR LOW. MX SERVICED SPOILER RESERVOIR, INSPECTED SPOILER PANELS, CABLES, ACTUATORS AND ALL NORMAL. REJan 26, 2003 · N823BX · Doug DC871F · Drag Control SystemSDR IXXA060485SPlate · wornDURING ROUTINE C CHECK, FOUND RIGHT OUTBOARD FLAP BOILER PLATE KNIFE EDGED AT STATION 410. REMOVED DAMAGED BOILER PLATE, FABRICATED REPAIR PARTS, LOCATED, DRILED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DOUGLAS DRAWINGS 5719443, 5719445, DC8 Jan 25, 2003 · N820BX · Doug DC871F · Trailing Edge FlapsSDR IXXA060493SStructure · crackedDURING ROUTINE C CHECK, FOUND RIGHT AFT SERVICE DOOR AFT CORNER CRACKED, EXTENDING PAST STOP DRILL AT LIGHTNING HOLE. REMOVED DAMAGE, FABRICATED, REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-0, 52-2-0, Jan 24, 2003 · N820BX · Doug DC871F · Service DoorsSDR IXXA060492SSkin · crackedDURING ROUTINE C CHECK FOUND RIGHT AFT SERVICE DOOR CUTOUT UPPER AFT CORNER CRACKED AT FASTENER HOLE. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS WITH NEW FASTEJan 24, 2003 · N820BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA060489SFloor Support · corrodedDURING ROUTINE C CHECK, FOUND COCKPIT FLOOR PANEL 674A ATTACH ANGLE CORRODED. REMOVED DAMAGED ATTACH ANGLE. FABRICATED NEW ATTACH ANGLE, LOCATED, DRILLED TRIMMED, TREATED, PRIMED AND INSTALLED NEW ATTACH ANGLE IAW DC8 SRM 51-1-8, 53-2-0, 53-7-3 51-9-0, AND 5Jan 24, 2003 · N820BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA060488SBeam · crackedDURING ROUTINE C CHECK, FOUND L-1 DOOR FORWARD INTERNAL TOP SIDE CORNER ON FIRST HORIZONTAL BEAM FROM TOP FORWARD SIDE CRACKED IN RADIUS. STOP DRILLED CRACKED, FABRICATED REPAIR DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR DOUBLERJan 24, 2003 · N820BX · Doug DC871F · Passenger/Crew DoorsSDR IXXA060486SSkin · crackedDURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE SKIN CRACKED AT STATION XW291. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED, REPAIR PARTS. IAW DC8 SRM 51-1-8, 51-2-1, 51-1-20D, AND 51-3-0.Jan 24, 2003 · N820BX · Doug DC871F · Wing, Plate/SkinSDR IXXA060497SAngle · crackedDURING ROUITNE C CHECK FOUND RIGHT HAND ELEVATOR DRAIN PAN INSIDE OF TAIL CONE CRACKED. REMOVED DAMAGE, FABRICATED REPAIR ANGLE, LOCATED, DRILLED, TREATED, PRIMED AND INSTALLED REPAIR ANGLE. IAW DC8 SRM 53-2-0, 51-1-8, AND 51-1-21.Jan 23, 2003 · N820BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA060500SFitting · crackedDURING ROUTINE C CHECK, FOUND A CRACKED END FITTING FROM STATION 1767 TO 1772 AT LONGERON 10 LEFT. REMOVED CRACKED END FITTING. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW END FITTING IAW DC8 SRM 51-1-20D, 51-1-21, 21-3-0, AND 51-1-24.Jan 23, 2003 · N820BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA060499SFitting · crackedDURING ROUTINE C CHECK, FOUND A CRACKED END FITTING FROM STATION 1767 TO 1770 AT LONGERON 17 RIGHT. REMOVED CRACKED END FITTING. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW END FITTING IAW DC8 SRM 51-1-20D, 51-1-21, AND 51-3-0.Jan 23, 2003 · N820BX · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA060498SFrame · crackedDURING ROUTINE C CHECK, FOUND EMPENNAGE FRAME CRACKED AT STATION 1960 LEFT SIDE WHERE HORIZONTAL STIFFENER FASTENS TO FRAME. REMOVED DAMAGE. FABRICATED REPAIR DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 53-2-0Jan 23, 2003 · N820BX · Doug DC871F · Fuselage Main, FrameSDR IXXA060496SDoubler · damagedDURING ROUTINE C CHECK, FOUND FORWARD LOWER AIR CONDITIONER ACCESS DOOR INTERNAL DOUBLER REQUIRES REPLACEMENT DUE TO MANY PREVIOUS REPAIRS. REMOVED EXISTING DOUBLER. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED AND INSTALLED REPAIR PARJan 23, 2003 · N820BX · Doug DC871F · Fuselage Main, StructureSDR IXXA060495SSeat Track · gougedDURING ROUTINE C-CHECK, FOUND SEAT TRACK "B" GOUGED AT STATION FS 400. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, LOCATED, DRILLED TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-3, AND 51-1-8.Jan 23, 2003 · N820BX · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA060494SIntercostal · crackedDURING ROUTINE C-CHECK, FOUND RIGHT AFT SERVICE DOOR MID INTERCOSTAL CRACKED. REMOVED DAMAGED INTERCOSTAL. FABRICATED NEW INTERCOSTAL, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW INTERCOSTAL IAW DC8 SRM 51-1-20, 51-1-8, 51-1-21, AND DOUGLASJan 23, 2003 · N820BX · Doug DC871F · Service DoorsSDR IXXA060491SSkin · crackedDURING ROUTINE C CHECK, FOUND AFT PASSENGER DOOR CUTOUT UPPER AFT CORNER CRACKED. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND NEW FASTENERS IAW DC8 SRM 53-2Jan 23, 2003 · N820BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA060487SAngle · corrodedDURING ROUTINE C CHECK, FOUND ANGLE CORRODED AT STATION FS 70 LONGERON 32 LEFT. REMOVED DAMAGE, FABRICATED, REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-8, 51-2-0, AND 53-2-5.Jan 23, 2003 · N820BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA060502SSeat Track · wornDURING ROUTINE C CHECK, FOUND SEAT TRACK WORN AND GOUGED AT STATION 240 BL-0. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS, IAW,DC8 SRM 53-2-3, AND 51-1-8.Jan 23, 2003 · N820BX · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA060501SSeat Track · gougedDURING ROUTINE C CHECK, FOUND SEAT TRACK GOUGED AT STATION 250 BL-0. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS, IAW DC8 SRM 53-2-3, AND 53-2-3.Jan 23, 2003 · N820BX · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA060511SCover · wornDURING ROUTINE C CHECK, FOUND RIGHT WING TRAILING EDGE FLAP SPRING COVER WORN AT STATION 255. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW DC8 SRM 51-3-0, DOUGLAS DRAWING NUMBER 5719443, AND TIMCO RE[AIR ENGINJan 22, 2003 · N820BX · Doug DC871F · Trailing Edge FlapsSDR IXXA060510SWeb · corrodedDURING ROUTINE C CHECK, FOUND WEB CORRODED AT STATION FS 1165, LONGERON 35 RIGHT. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW DC8 SRM 1-1-8, 53-2-0, 51-1-21, 51-3-0, AND DOUGLAS DRAWJan 22, 2003 · N820BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA060509SSkin · misrepairedDURING ROUTINE C CHECK, FORWARD ENTRY DOOR CUTOUT LOWER AFT EXISTING REPAIR DOES NOT MEET THE INTENT OF AD 2000-20-08. REMOVED EXISTING DOUBLER. REMOVED EXISTING DOUBLER. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW Jan 22, 2003 · N820BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA060508SSkin · bentDURING ROUTINE C CHECK, FOUND LEFT ELEVATOR UPPER SKIN IS BENT AT OUTBOARD HINGE CUTOUT. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW DC8 SRM 51-1-8, 51-1-24, 51-1-21 AND DOUGLAS DRAWJan 22, 2003 · N820BX · Doug DC871F · Elevator, Plate/SkinSDR IXXA060507SSkin · crackedDURING ROUTINE C CHECK, FOUND RIGHT WING LOWER LEADING EDGE OUTBOARD OF PANEL 522A EXISTING REPAIR CRACKED. REMOVED EXISTING REPAIR. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW DC8 Jan 22, 2003 · N820BX · Doug DC871F · Wing, Plate/SkinSDR IXXA060506SSkin · crackedDURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE OUT BOARD SKIN SPLICE REPAIR, OUTER SKIN CRACKED. REMOVED EXISTING REPAIR. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW DC8 SRM Jan 22, 2003 · N820BX · Doug DC871F · Wing, Plate/SkinSDR IXXA060505SWeb · damagedDURING ROUTINE C CHECK, FOUND LEFT AFT PASSENGER DOOR CUTOUT JAMB WEB HAS IMPACT DAMAGE. REMOVED DAMAGE, FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW DOUGLAS DRAWIMG 9751069, TIMCO REPAIR ENGENEERING ORDERJan 22, 2003 · N820BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA060504SStructure · crackedDURING ROUTINE C CHECK, FOUND AFT PIT BASKET DOOR ATTACHMENT HOLE CRACKED. REMOVED DAMAGE, FABRICATED DOUBLER AND FILLER, LOCATED, DRILLED TRIMMED, TREATED, PRIMED, AND INSTALLED DOUBLER AND FILLER, IAW DC8 SRM 53-2-0, 51-1-8, AND 51-1-21.Jan 22, 2003 · N820BX · Doug DC871F · Cargo/Baggage DoorsSDR IXXA060503SSeat Track · gougedDURING ROUTINE C CHECK FOUND A SEAT TRACK GOUGED AT STATION 275 RBL 45.5. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS.IAW DC8 SRM 53-2-3, 51-1-8, AND 53-2-3.Jan 22, 2003 · N820BX · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA060515SWeb · gougedDURING ROUTINE C CHECK, FOUND LEFT MAIN LANDING GREA STRUT CUTOUT AFT VERTICAL WEB GOUGED. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW DC8 SRM 51-1-21, 51-1-8, AND DOUGLAS DRAWING 5651221.Jan 21, 2003 · N820BX · Doug DC871F · Wing Miscellaneous StructureSDR IXXA060513SDoubler · gougedDURING ROUTINE C CHECK, FOUND AIR START DOOR CUTOUT DOUBLER GOUGED. REMOVED EXISTING DOUBLER. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW DC8 SRM 51-1-8, 51-1-21 AND DOUGLAS DRAWING NUMBER 5614438.Jan 21, 2003 · N820BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA060512SFitting · crackedDURING ROUTINE C CHECK, FOUND FITTING CRACKED ON INSIDE OF L1 DOOR UPPER AFT EDGE, BACK SIDE OF DOOR STOP. REPLACED FITTING IAW DC8 SRM 51-1-21 AND 51-1-21D.Jan 21, 2003 · N820BX · Doug DC871F · Passenger/Crew DoorsSDR UPS03840037Intercostal · corrodedINSPECTION TYPE: C2, STA 1400 INTERCOSTAL IS CORRODED BEYOND LIMITS AT RBL 49. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 53-2-0 FIG 23.Jan 15, 2003 · N701UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS03840026Fitting · crackedINSPECTION TYPE: C2, RT WING STRINGER END FITTING IS CRACKED I/B OF XRS 74 AT STRINGER 51. REMOVED AND REPLACED FITTING IAW DWG 3704841, AND SRM 51-1-20D.Jan 9, 2003 · N701UP · Doug DC871F · Wing Main, Frame StructureSDR UPS03840000Battery Pack · inoperativeINSPECTION TYPE: PFLT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK. OPS CHECK'S GOOD IAW MM 33-50-01. S/N ON 10886, S/N OFF 348.Jan 7, 2003 · N798UP · Doug DC871F · Emergency LightingSDR UPS04841698Shear Tie · crackedINSPECTION TYPE: C3, STA 1766 AFT SIDE SHEAR TIE IS CRACKED AT LOWER END BETWEEN LONGERON 9L AND 10L. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 53-2-0 FIG 1B.Jan 6, 2003 · N702UP · Doug DC871F · Fuselage Main, StructureSDR UPS03840063Skin · crackedINSPECTION TYPE:C2 RADIOGRAPHIC (X-RAY) INSPECTION DETECTED A CRACK ON THE R-1 DOOR LOWER AFT CORNER APPROX .700 INCHES IN LENGTH, STA190 APPROX AT LONG 20R. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER IAW SRM 53-2-0 FIG 14.Jan 3, 2003 · N701UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS03840036Skin · crackedINSPECTION TYPE: C2, RADIOGRAPHIC (X-RAY) INSPECTION DETECTED 4 CRACKS ON THE R-2 DOOR UPPER AFT CORNER APPROX .406, 1.11, 1.64, 1.74 INCHES IN LENGTH, AT STA 1660 LONG 10R APPROX. CUT OUT CRACKED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTAJan 3, 2003 · N701UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS03840031Fitting · crackedINSPECTION TYPE: C2, RT HORIZONTAL STAB L/E LOWER T-ANGLE IS CRACKED AT XFS 47. REMOVED AND REPLACED FITTING IAW DWG SE08550009, AND SRM 51-1-20D.Jan 3, 2003 · N701UP · Doug DC871F · Horizontal Stabilizer StructureSDR UPS03840033Web · crackedINSPECTION TYPE: C2, D-PIT DOOR AFT TORQUE BOX WEB IS CRACKED AND TORN AT HOLES AT STA 1440 LONG 33R. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUTS. FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 23.Jan 2, 2003 · N701UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS03840029Floorbeam · crackedINSPECTION TYPE: C2, FLOORBEAM TO VERTICAL STIFFENER ATTACH ANGLE IS CRACKED AT STA 680 AT RBL 48. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 5773275, AND SRM 51-1-20.Jan 2, 2003 · N701UP · Doug DC871F · Fuselage Main, Floor BeamSDR UPS03840030Skin · crackedINSPECTION TYPE:C2 LEFT WING L/E LOWER SKIN REPAIR DOUBLER SCREW HOLES HAVE COUNTERSUNK TOO DEEP AT STA XFS 307, AND IS CRACKED. REMOVED DOUBLER, STOPDRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW DC8-5720-4087-B.Dec 30, 2002 · N701UP · Doug DC871F · Leading Edge Devices
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