Douglas DC-8-71F

Service difficulty reports · 8,938

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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 = 'DC871F'
  ORDER BY difficulty_date DESC"

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SDR IXXA0500162SSkin · corrodedDURING ROUTINE C-CHECK, FOUND CORROSION ON EXTERIOR FUSELAGE SKIN FROM STATION 680 TO STATION 780 BETWEEN LONGERON 32 LEFT AND LONGERON 32 RIGHT. REMOVED FASTENERS, AND ANTENNA TO GAIN ACCESS. REMOVED CORROSION. ORIGINAL SKIN THICKNESS .125 AFTER CORROSION Jan 26, 2005 · N820BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA0500201SSeat Track · wornDURING ROUTINE C-CHECK FOUND MAIN CABIN SEAT TRACK AT STATION 1220 -F- WORN. REMOVED DAMAGE FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-3, AND 51-1-8Jan 25, 2005 · N820BX · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA0500200SBracket · crackedDURING ROUTINE C-CHECK FOUND AIRSTART NOZZLE BRACKET CRACKED AT 3 LOCATIONS. STOP DRILLED CRACKS, FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND FASTENERS IAW DC8 SRM 53-2-0, 51-9-0, AND 51-1-8.Jan 25, 2005 · N820BX · Doug DC871F · Elevator Tab Control SystemSDR IXXA050199STrim Tab · dentedDURING ROUTINE C-CHECK FOUND LEFT ELEVATOR TAB DENTED AT MID SKIN. REMOVED TAB, DISASSEMBLED, CLEANED INSPECTED, AND REPLACED TRAILING EDGE WEDGE. REINSTALLED TAB ON LEFT ELEVATOR IAW DC8 SRM 51-1-21, 51-1-22, 51-1-8B, 51-4-5, 51-3-0, DC8 DRAWING 5702579 ANDJan 25, 2005 · N820BX · Doug DC871F · Elevator Tab Control SystemSDR IXXA050198STrim Tab · delaminatedDURING ROUTINE C-CHECK FOUND LEFT ELEVATOR TAB DELAMINATED. REMOVED TAB, DISASSEMBLED, CLEANED INSPECTED, AND REPLACED TRAILING EDGE WEDGE. REINSTALLED TAB ON LEFT ELEVATOR IAW DC8 SRM 51-1-21, 51-1-22, 51-1-8B, 51-4-5, 51-3-0, DC8 DRAWING 5702579 AND DC8 OHJan 25, 2005 · N820BX · Doug DC871F · Elevator Tab Control SystemSDR IXXA0500195SSkin · crackedDURING ROUTINE C-CHECK FOUND EXTERNAL FUSELAGE SKIN CRACKED AT STATION 45 LONGERON 28 LEFT IN AREA OF EXISTING REPAIR. PERFORMED HFEC TO VERIFY CRACK. VERIFIED, GAINED ACCESS, REMOVED FASTENERS, EXISTING DOUBLER, AND REMOVED DAMAGE. FABRICATED FILLER AND DOJan 25, 2005 · N820BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA0500194SHinge · gougedDURING ROUTINE C-CHECK FOUND RIGHT HAND INBOARD FLAP, INBOARD HINGE, OUTBOARD ARM GOUGED AND CHAFED. REMOVED DAMAGE, ORIGINAL THICKNESS WAS .250, REMOVED .081 MATERIAL, REMAINING THICKNESS .169, OUT OF LIMITS. FABRICATED REPAIR PARTS, LOCATED, DRILLED, PRIMEJan 25, 2005 · N820BX · Doug DC871F · Trailing Edge FlapsSDR IXXA0500193SSkin · gougedDURING ROUTINE C-CHECK FOUND RIGHT HAND OUTBOARD FLAP UPPER SKIN IS GOUGED AT PREVIOUS REPAIR. REMOVED DAMAGED REPAIR, FABRICATED, NEW REPAIR PART, ALODINED, PRIMED AND INSTALLED NEW REPAIR PART IAW DC8 SRM 57-2-0, 51-1-20D, AND 51-1-8.Jan 25, 2005 · N820BX · Doug DC871F · Trailing Edge FlapsSDR IXXA0500189SDoubler · tornDURING ROUTINE C-CHECK FOUND LEFT WING INBOARD FLAP OUTBOARD FORWARD HINGE FAIRING PANEL DOUBLER TORN. REMOVED FASTENERS AND DAMAGED DOUBLER. FABRICATED NEW DOUBLER, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED NEW DOUBLER WET WITH SEALANT, AND INSTALLED FASJan 25, 2005 · N820BX · Doug DC871F · Trailing Edge FlapsSDR IXXA0500187SSupport Angle · crackedDURING ROUTINE C-CHECK FOUND RIGHT WING OUTBOARD FLAP INBOARD EDGE AT STATION XW 129 TRAILING EDGE SUPPORT ANGLE CRACKED. REMOVED FASTENERS, AND DAMAGED SUPPORT ANGLE. FABRICATED NEW SUPPORT ANGLE. LOCATED, DRILLED, TREATED, PRIMED AND INSTALLED NEW SUPPORTJan 25, 2005 · N820BX · Doug DC871F · Trailing Edge FlapsSDR IXXA0500184SSeat Track · wornDURING ROUTINE C-CHECK FOUND FLIGHT DECK COURIER SEAT TRACKS FORWARD AND AFT WORN. REMOVED FASTENERS, AND DAMAGED SEAT TRACKS. RECEIVED NEW SEAT TRACKS, LOCATED, DRILLED AND INSTALLED NEW SEAT TRACKS IAW DC8 SRM 51-1-24 AND 51-3-1.Jan 25, 2005 · N820BX · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA0500183SSeat Track · wornDURING ROUTINE C-CHECK FOUND FLIGHT DECK FLIGHT ENGINEER FORWARD AND AFT SEAT TRACKS WORN. REMOVED FASTENERS AND DAMAGED SEAT TRACKS. RECEIVED NEW SEAT TRACKS, LOCATED, DRILLED AND INSTALLED NEW SEAT TRACKS IAW DC8 SRM 51-3-0, 51-3-1, AND 51-1-21.Jan 25, 2005 · N820BX · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA0500181SSeat Track · damagedDURING ROUTINE C-CHECK FOUND FLIGHT DECK FIRST OFFICER SEAT TRACKS AFT SET HOLES ELONGATED. REMOVED SEAT TRACKS. ORIGINAL THICKNESS WAS .125, REMOVED .040 MATERIAL, .080 REMAINING, OUT OF LIMITS. FABRICATED STRAPS FROM .040 THICK 301 STAINLESS STEEL. LOCATJan 25, 2005 · N820BX · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS05843745Battery Pack · inoperativeEMERGENCY EXIT LIGHT INOP. REPLACED EMERG LIGHT BATTERY PACK PER WDM 33-50-01. OPS CK OK.Jan 25, 2005 · N755UP · Doug DC871F · Emergency LightingSDR IXXA0500182SFrame · chafedDURING ROUTINE C-CHECK FOUND FLIGHT DECK AT STATION 12.00 TO STATION 20.00 LEFT BUTT LINE 10 FRAME CHAFED THROUGH. REMOVED LOWER L-ANGLE WIRE BUNDLE ATTACH ANGLE, STIFFENERS, AND INTERCOSTAL. FABRICATED INTERCOSTAL AND DOUBLER. LOCATED INTERCOSTAL AND DOUBLJan 24, 2005 · N820BX · Doug DC871F · Fuselage Main, FrameSDR IXXA0500180SClip · crackedDURING ROUTINE C-CHECK, FOUND LEFT WING OUTBOARD FLAP INBOARD SUPPORT HINGE TRAILING EDGE UPPER WING SUPPORT CLIP CRACKED. REMOVED FASTENERS, FABRICATED NEW CLIP, TREATED, PRIMED, AND INSTALLED NEW CLIP AND FASTENERS IAW DC8 SRM 57-2-0, 51-1-21, AND 51-1-8.Jan 24, 2005 · N820BX · Doug DC871F · Trailing Edge FlapsSDR IXXA0500178SSkin · dentedDURING ROUTINE C-CHECK FOUND LEFT WING INBOARD FLAP LOWER SKIN DENTED SEVERAL PLACES. BLENDED TWO DENTS WITHIN LIMITS ONE DENT OUT OF LIMITS. REPAIRED OUT OF LIMIT DENT IAW DC8 SRM 57-2-0. TREATED AND PRIMED ALL DENTS IAW DC8 SRM 51-1-8.Jan 24, 2005 · N820BX · Doug DC871F · Trailing Edge FlapsSDR IXXA0500176SBracket · wornDURING ROUTINE C-CHECK FOUND LEFT WING OUTBOARD FLAP AT OUTBOARD FLAP TRACK UPPER SURFACE HAS BRACKET WORN / CHAFED THROUGH AND BAD FASTENERS. REMOVED BAD FASTENERS, FABRICATED NEW BRACKET, TREATED, PRIMED, INSTALLED NEW BRACKET AND FASTENERS IAW DC8 DRAWING Jan 24, 2005 · N820BX · Doug DC871F · Trailing Edge FlapsSDR IXXA0500174SHeat Shield · damagedDURING ROUTINE C-CHECK FOUND NUMBER 1 ENGINE THRUST REVERSER INBOARD INNER HEAT SHIELD HAS A HOLE WORN THROUGH. RECEIVED NEW HEAT SHIELD, LOCATED, DRILLED AND INSTALLED HEAT SHIELD IAW CFM56 MM 78-31-10.Jan 24, 2005 · N820BX · Doug DC871F · Engine Thrust ReverserSDR IXXA0500173SStructure · gougedDURING ROUTINE C-CHECK FOUND NUMBER 2 ENGINE THRUST REVERSER INBOARD SHELL HAS GOUGES. REMOVED DAMAGE, RECEIVED REPAIR DOUBLER, LOCATED, DRILLED, TREATED, PRIMED AND INSTALLED DOUBLER IAW CFM MM 78-31-10.Jan 24, 2005 · N820BX · Doug DC871F · Engine Thrust ReverserSDR IXXA0500177SFloor Panel · corrodedDURING ROUTINE C-CHECK FOUND FLOORING IN COURIER AREA CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED FASTENERS, FABRICATED NEW FLOOR PANEL, ALODINED, PRIMED, INSTALLED NEW FLOOR PANEL AND FASTENERS IAW DC8 DRAWING 564827, DC8 SRM 51-1-8, 53-Jan 23, 2005 · N820BX · Doug DC871F · Fuselage Floor PanelSDR IXXA0500175SShroud · wornDURING ROUTINE C-CHECK FOUND NUMBER 1 ENGINE FAN ABRADABLE SHROUD WORN BEYOND LIMITS AT 12:00, AND 1:00 POSITIONS. REMOVED ACCOUSTICAL PANELS, POTTED REPAIR AREAS, APPLIED FIBERGLASS OVERLAYS, CLEANED AND SEALED AREAS. REINSTALLED ACCOUSTICAL PANELS IAW CFM Jan 23, 2005 · N820BX · Doug DC871F · Engine (Turbine/Turboprop)SDR IXXA0500172SFrame · crackedDURING ROUTINE C-CHECK FOUND FRAME CRACKED IN THE AFT PIT STATION 1120 AT LONGERON 30 RIGHT. REMOVED DAMAGE, FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-0, 51-1-8, AND 51-1-20D.Jan 23, 2005 · N820BX · Doug DC871F · Fuselage Main, FrameSDR IXXA0500171SCowling · crackedDURING ROUTINE C-CHECK FOUND NUMBER 1 ENGINE NOSE COWL EXTERNAL SKIN CRACKED BEYOUND STOP DRILL AT INBOARD ANTI-ICE CUTOUT LOWER FORWARD CORNER. REMOVED FASTENERS. PERFORMED HFEC TO VERIFY CRACK STOPS AT FASTENER HOLE. FABRICATED DOUBLER, LOCATED, DRILLED, Jan 22, 2005 · N820BX · Doug DC871F · Engine Cowling SystemSDR IXXA0500169SDoubler · crackedDURING ROUTINE C-CHECK FOUND AIR START ENCLOSURE GOUGED AND CRACKED. REMOVED FASTENERS, INNER AND OUTER DOUBLER. FABRICATED INNER AND OUTER DOUBLER. LOCATED, DRILLED, TREATED PRIMED, AND INSTALLED NEW INNER AND OUTER DOUBLER IAW DAC DRAWING 5614438, DC8 SRMJan 21, 2005 · N820BX · Doug DC871F · Fuselage Main, StructureSDR UPS05843742Battery Pack · inoperativeINSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS WILL NOT TEST. REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK, CHECKS OK MM 33-50-01-2.Jan 21, 2005 · N755UP · Doug DC871F · Emergency LightingSDR IXXA0500167SSkin · gougedDURING ROUTINE C-CHECK FOUND EXTERNAL FUSELAGE GOUGED AT STATION 280 LONGERON 30 RIGHT. REMOVED GOUGE. ORIGINAL MATERIAL THICKNESS IS .071 AFTER DAMAGED REMOVED MATERIAL THICKNESS IS .051 OUT OF LIMITS. FABRICATED DOUBLER, LOCATED, DRILLED, ALODINED, PRIMEDJan 20, 2005 · N820BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA0500166SAngle · crackedDURING ROUTINE C-CHECK FOUND SUPPORT ANGLE CRACKED AT THE RIGHT WHEEL WELL STATION 785 LONGERON 23 RIGHT SWING DOWN PANEL. MANUFACTURED REPAIR ANGLES. LOCATED, DRILLED, TRIMMED, ALODINED, PRIMED, AND INSTALLED REPAIR ANGLES IAW DC8 DRAWING 5643404, DC8 SRM 5Jan 20, 2005 · N820BX · Doug DC871F · Wing Miscellaneous StructureSDR IXXA0500164SStiffener · crackedDURING ROUTINE C-CHECK FOUND THREE CRACKED STIFFENERS IN THE FORWARD PIT RIGHT HAND FORWARD BULKHEAD. REMOVED FASTENERS, AND DAMAGED PARTS. MANUFACTURED REPLACEMENT PARTS. LOCATED, DRILLED, ALODINED, PRIMED, AND INSTALLED REPLACEMENT PARTS IAW DC8 SRM 53-2-Jan 20, 2005 · N820BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA0500163SSkin · crackedDURING ROUTINE C-CHECK FOUND LEFT WING JUST ABOVE NUMBER 2 PYLON UPPER SKIN CRACKED. REPLACED UPPER SLOT DOOR WITH NEW, IAW DC8MM 20-12-0, AND 27-81-02.Jan 20, 2005 · N820BX · Doug DC871F · Wing, Plate/SkinSDR IXXA0500161SAttach Fitting · corrodedDURING ROUTINE C-CHECK FOUND ATTACH FITTING CORRODED AT RIGHT WHEEL WELL STATION XCW44.00 LONGERON 24 RIGHT. CLEANED AREA, UPON FURTHER INSPECTION SEVERAL CRACKS NOTED VERIFIED BY INSPECTION. REMOVED FASTENERS AND DAMAGED FITTING. RECEIVED NEW ATTACH FITTINGJan 20, 2005 · N820BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA0500159SAttach Fitting · corrodedDURING A ROUTINE C-CHECK FOUND LONGERON ATTACH FITTING AT STATION 870 LONGERON 24 LEFT CORRODED. ORIGINAL THICKNESS .125 REMOVED .025 MATERIAL, FITTING OUT OF LIMITS. DURING CORROSION REMOVAL FOUND LONGERON 24 LEFT CRACKED AT STATIION 870. REMOVED FASTENERSJan 20, 2005 · N820BX · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS05843690Door · openNR 3 PIT DOOR OPENED ON LANDING A/C OOS. 11832 ASSIGNED TO THIS WRITE UP 0557984 C/W ALL ITEMS ON ECA FORM 11832, SYS OPS CK OK.Jan 20, 2005 · N729UP · Doug DC871F · Cargo/Baggage DoorsSDR UPS05843682Pump · leakingINSPECTION TYPE:N/A ON CLIMBOUT HYD FLUID QTY LOSS. FOLLOWED EMERGENCY PROCEDURE CHECK LIST. ON LANDING REMOVED AND REPLACED EMERGENCY STBY RUDDER PUMP. SERVICED & RAN AND OPS CHECKED NORMAL.Jan 20, 2005 · N772UP · Doug DC871F · Hydraulic System, AuxiliarySDR UPS05843668Battery Pack · inoperativeINSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS DO NOT CHECK. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK. OPS CHECK OK IAW 33-50-00.Jan 19, 2005 · N750UP · Doug DC871F · Emergency LightingSDR UPS05843662Engine · flamed outNR 2 ENGINE FLAMED OUT IN FLIGHT. A/C IS OOS. PERFORMED STEP 4 UP TO FUEL FILTER REPLACEMENT ON FIGURE 139 SHEET 1 OF MM 71 00 00. TS (558010) PERFORMED ENG MAINT RUN PER MM 71-00-00-1, NO DEFECTS NOTED. A/C OK FOR SERVICE.Jan 18, 2005 · N708UP · Doug DC871F · Engine (Turbine/Turboprop)SDR IXXA0500205SSpar · crackedDURING ROUTINE C-CHECK COMPLY WITH AD 2001-06-02, INSPECT LOWER FRONT SPAR CAPS. REMOVED FASTENERS AND PHENOLIC FAIRINGS AS REQUIRED TO FACILITATE INSPECTION OF FRONT LOWER SPAR CAPS. PERFORMED HFEC ON LEFT WING NO CRACKS INDICATED. PERFORMED HFEC ON RIGHT WJan 17, 2005 · N820BX · Doug DC871F · Wing SparSDR IXXA0500160SCloseout Panel · corrodedDURING ROUTINE C-CHECK FOUND RIGHT HAND GEAR OVERHEAD TRUNNION PANEL CORRODED, DELAMINATED. REMOVED FASTENER AND DAMAGED PANEL. RECEIVED OVERHAULED TRUNNION PANEL. LOCATED, DRILLED AND INSTALLED TRUNNION PANEL IAW DC8 SRM 51-1-24, 51-3-0, AND 51-3-1.Jan 15, 2005 · N820BX · Doug DC871F · Fuselage Main, StructureSDR UPS06846160Fitting · corrodedHEAVY CORROSION ON AFT SIDE OF FITTING BETWEEN LT W/W CIELING AND L24L AT STA 920. REMOVED AND REPLACED FITTING AND REPAIR SPLICE IAW SRM 53-2-0 FIG 008 AND 51-03-01.Jan 13, 2005 · N702UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS05843782Fitting · crackedINSPECTION TYPE:C1 INTERCOSTAL-TO-FRAME ATTACH FITTING CRACKED AT STA 1140 LONGERON 35R. REMOVED AND REPLACED FITTING REF SRM 51-1-20D, 51-1-8, 51-1-15.Jan 13, 2005 · N701UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS05843781Fitting · crackedINSPECTION TYPE:C3, CLIP CRACKED IN NR 1 ALT TANK AT NR 1 PYLON SKATE ANGLE BETWEEN STR 62 & 63 XRS508.997 LT WING INT. FAB REPLACEMENT CLIP PER DWG5804007 FROM BAR7075T6. DYE-PEN INSP PER DPS 4.707; NO CRACKS NOTED. REMOVED AND REPLACED FITTING REF SRM 51-Jan 13, 2005 · N701UP · Doug DC871F · Wing, Attach FittingsSDR UPS05843780Fitting · corrodedINSPECTION TYPE:C3 RT WING STA XW97 CANOE SUPPORT FITTING ATTACH BOLT HOLES CORRODED & GOUGED. REMOVED AND REPLACED FITTING REF SRM 51-3-2, 51-1-20D, 51-3-0, MM 20-16-00, 27-51-12.Jan 13, 2005 · N701UP · Doug DC871F · Wing, Attach FittingsSDR UPS05843848Support Fitting · corrodedRT STA 98 FLAP SUPPORT FITTING (CANOE) HAS CORROSION UNDER FLAP TRACK AREA, O/B SURFACE .025 DEEP I/B SURFACE IS .006 DEEP. UNDERCUT AND REMOVED CORROSION .050 AND FABRICATED AND INSTALLED REPAIR FILLERS PER SB 27-164 PAGE 8.Jan 12, 2005 · N701UP · Doug DC871F · Trailing Edge FlapsSDR UPS05843789Web · crackedINSPECTION TYPE:C1, R1 DOOR JAMB TORQUE WEB CRACKED ABOVE UPPER DOOR HINGE ARM STA 150- 155, NEXT TO L14R. CUT OUT DAMAGE, NDT VERIFIED REF NDT/SPM06-10-01.001. FAB DOUBLER FROM SHT2024T3-.050, TREAT, PRIME & INSTALLED SAME REF SRM 53-2-0 FIG 1F, 51-1-8, 51-Jan 10, 2005 · N701UP · Doug DC871F · Fuselage Main, StructureSDR UPS05843787Fitting · crackedINSPECTION TYPE:C1, TAIL CONE ATTACH FITTING CRACKED ON L36, STA 1875. REMOVED AND REPLACED FITTING IAW SRM 51-1-21, 51-1-20D, 51-1-8, 51-3-0.Jan 10, 2005 · N701UP · Doug DC871F · Aerodynamic FairingsSDR UPS05843846Attach Fitting · crackedMAIN CABIN STA 835.5 L18L, FRAME ATTACH FITTING CRACKED. REMOVED AND REPLACED FRAME ATTACH FITTING AT STA 853.5 L18L, IAW SRM 51-1-20D.Jan 8, 2005 · N701UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS05843837Attach Fitting · crackedMAIN CABIN AT STA 702 LBL (LONGERON 13LH) FRAME ATTACH FITTING CRACKED. REMOVED, FABRICATED AND REPLACED FRAME ATTACH FITTING AT F/S 702 L13L IAW 51-1-20-D, DWG3779978 AND SAA TRAVELER 0035.Jan 8, 2005 · N701UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS05843835Longeron · crackedLONGERON 36 HAS 1 INCH CRACK ON RT UPPER FLANGE IN RADIUS BETWEEN F/S 1260-1280. REMOVED AND REPLACED DAMAGED LONGERON SECTION IAW DWG 5750322 AND SRM 51-1-20D FROM F/S 1260-1360 L36.Jan 8, 2005 · N701UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS05843786Fitting · crackedINSPECTION TYPE:C1, LONGERON 8R END FITTING CRACKED AT STA 676. REMOVED AND REPLACED END FITTING IAW SRM 51-1-20D, 51-1-8.Jan 8, 2005 · N701UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS05843867Frame · corrodedA-PIT FRAME CORRODED AND MISDRILLED AT STA 280 L32R. CUT OUT DAMAGE, NDT VERIFIED ALL DAMAGE REMOVED PER NDTSPM 06-10-01.001. FAB REPAIR ANGLE FROM SHT 7075-0-.080 HEAT TREAT TO T6 PER DPS7.00-1. FAB FILLERS FROM SHT 7075T6-.080. INSTALLED ALL PARTS REF'S Jan 7, 2005 · N701UP · Doug DC871F · Fuselage Main, Frame
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