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 IXXA0500034SFitting · corrodedDURING A ROUTINE C CHECK INSPECTION, FOUND FUSELAGE AT SECTION FITTING CORROSION DAMAGE BETWEEN STA 1680.00 AND 1690.00, L-36. REPAIR ACCOMPLISHED, REMOVED CORRODED FITTING AND THE CORROSION. FOUND OUT OF LIMITS. CLEANED, TREATED AND PRIMED AREA AND INSTALLAug 30, 2004 · N606AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA0500020SSkin · damagedDURING A ROUTINE C CHECK INSPECTION, LT WING OUTBOARD FLAP LOWER PLATING HAS INTERIM REPAIR AT STA XF 1340.000. MAJOR REPAIR ACCOMPLISHED. REMOVED SKIN WITH INTERIM REPAIR ON IT IAW DC8 SRM 51-1-21 PG 1 DC8 SRM 51-3-0 PG1. FABRICATED NEW SKIN (AL2024130.050Aug 30, 2004 · N606AL · Doug DC873F · Leading Edge DevicesSDR IXXA0500023SSkin · crackedDURING A ROUTINE C CHECK INSPECTION, RT WING TOP PANEL PLATING HAS CRACK DAMAGE STA XRS 74.000, S-9. MAJOR REPAIR ACCOMPLISHED IAW DC8 SRM 57-2-1 FIG 17 PG 87, 88 1. REMOVED FASTENERS IAW DC8 SRM 51-1-20D PG 21. REMOVED DAMAGED AREA IAW DC8 SRM 57-2-1 PAGESAug 29, 2004 · N606AL · Doug DC873F · Wing, Plate/SkinSDR DHL2004801501Rib · crackedLEFT INNER WING OUTBOARD L/E FORMER CRACKED 0.750, STA XFS 703.750. PERFORMED STOP HOLE AND FABRICATED (2EA) REINFORCING ANGLES (AL2024-T3 0.032) IAW DC8 SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW DC8 SRM 51-1-8B. INSTALLED REINFORCING ANGLES IAW DAug 28, 2004 · N801DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2004806002Warning Light · illuminatedBELL FIRE DETECTOR CODE AD13477 B ILLUMINATED. TRANSFERRED TO DMI 17690 IAW MEL 26-10-1-A-1 CAT-C. PLACARDS INSTALLED, SYS OK LIGHT ILLUMINATED.Aug 28, 2004 · N806DH · Doug DC873F · Fire DetectionSDR IXXA0500024SFloorbeam · corrodedDURING A ROUTINE C CHECK INSPECTION A CORRODED BEAM WAS FOUND AT STA FS 1360.00 RBL 47". REPAIR WAS ACCOMPLISHED, CORROSION WAS REMOVED. FABRICATED FILLER & REPAIR ANGLE. CLEANED, TREATED AND PRIMED AREA. APPLIED PRC SEALANT ON FAYING SURFACES AND INSTALLAug 27, 2004 · N606AL · Doug DC873F · Fuselage Main, Floor BeamSDR IXXA0500022SFloorbeam · corrodedDURING A ROUTINE C CHECK INSPECTION, FOUND FLOORBEAM CORROSION ON RT FUSELAGE AFT CENTER SECTION AT STA 15000.000 RBL 48 INCH. MAJOR REPAIR ACCOMPLISHED IAW DC8 SRM 51-2-1 FIG 1 PAGES 8-14 (SHEET 7,12) TR NR 51-1-30. REMOVED CORROSION IAW DC8 SRM 51-1-8 PG 1Aug 27, 2004 · N606AL · Doug DC873F · Fuselage Main, Floor BeamSDR IXXA0500021SFloorbeam · corrodedDURING A ROUTINE C CHECK INSPECTION, THE RT FUSELAGE AFT CENTER SECTION FLOORBEAM HAS CORROSION DAMAGE AT STA 1300.000 RBL 48 INCH. MAJOR REPAIR WAS ACCOMPLISHED. REMOVED CORROSION IAW DC8 SRM 51-1-8 PGS 17-18. FOUND OUT OF LIMITS IAW EC8 SRM 53-2-0 PAGE 2PAug 27, 2004 · N606AL · Doug DC873F · Fuselage Main, Floor BeamSDR DHL2004805010Carbon Seal · deterioratedNR 1 ENGINE LOOSES APROX. 1.5 QT/HR OF OIL. OIL PRESSURE STABLE AT 50 PSI OIL LOSS STOPPED AT 2 QT. PERFORMED T/S IAW M/M 71-00-00 FAULT 60 FOUND EVIDENCE OF OIL LEAKAGE ON LWR PORTION OF T/R AND DRAIN MAST. FOUND CARBON SEAL AT STARTER PAD DETERIORATED, REAug 26, 2004 · N805DH · Doug DC873F · Turbine Engine Oil SystemSDR IXXA0500048SFitting · damagedDURING A ROUTINE C-CHECK INSPECTION, LT FUSELAGE LONGERON 24 FITTING FRAME WAS REMOVED AND INSTALLED TO COMPLY WITH N/R 3484 SID 960.000L-24 TO L-23L. REPAIR ACCOMPLISHED, REMOVED FRAME FITTING, CLEANED, TREATED AND PRIMED AREA. FABRICATED SPLICES AND DOUBLEAug 25, 2004 · N606AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA0500026SFloorbeam · corrodedDURING A ROUTINE C CHECK INSPECTION, FOUND FLOORBEAM CORRODED AT STA 1400.00 RBL 45". REPAIR WAS ACCOMPLISHED, CORROSION WAS REMOVED. FABRICATED FILLER & REPAIR ANGLE. CLEANED, TREATED AND PRIMED. APPLIED PRC SEALANT TO FAYING SURFACES. INSTALLED FILLER &Aug 23, 2004 · N606AL · Doug DC873F · Fuselage Main, Floor BeamSDR DHL2004801500Torque Link · crackedPERFORM NDT OF RT MLG UPPER TORQUE LINK AND ATTACH BOLT. PERFORMED MAGNETIC PARTICLES METHOD NDT OF RT MLG UPPER TORQUE LINK AND ATTACH BOLT IAW DC8 NDT SPM PART 07-00-01/08. REFER TO NR 1481 FOR DISCREPANCY FOUND CRACK IN RT TORQUE LINK ATTACH BOLT THREAD, Aug 23, 2004 · N801DH · Doug DC873F · Main Landing Gear Strut/Axle/TruckSDR IXXA0500012SFloorbeam · corrodedDURING A ROUTINE C-CHECK INSPECTION FOUND FLOORBEAM CORRODED AFT CARGO COMPARTMENT AT STA FS 1520.000. A MAJOR REPAIR WAS PERFORMED. REMOVED THE CORRODED AREA AND FOUND OUT OF LIMITS IAW DC8 SRM 51-1-8 PG 17, 18 AND SRM 53-2-0 PG 2P. FABRICATED FILLER ( AL Aug 22, 2004 · N606AL · Doug DC873F · Fuselage Main, Floor BeamSDR IXXA0500011SFloorbeam · corrodedDURING A ROUTINE C-CHECK INSPECTION RT FUSELAGE AFT CENTER SECTION FLOORBEAM CORROSION DAMAGE STA 1480.000, RBL 47. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION IAW DC8 SRM 51-1-8 PAGES 17, 18. FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0 PG 2P. REMOVED CORRODEDAug 22, 2004 · N606AL · Doug DC873F · Fuselage Main, Floor BeamSDR IXXA0500010SFloorbeam · corrodedDURING ROUTINE C-CHECK INSPECTION RT FUSELAGE AFT CENTER SECTION FLOORBEAM CORRSION DAMAGE STA 1460.000, RBL 48 WAS FOUND. REMOVED CORROSION IAW DC8 SRM 51-1-1 PAGES 17, 18, FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0 PGS 20. REMOVED CORRODED AREA IAW DC8 SRM 51-Aug 22, 2004 · N606AL · Doug DC873F · Fuselage Main, Floor BeamSDR IXXA0500006SDoor Frame · crackedDURING A ROUTINE C-CHECK INSPECTION, EXTERNAL FUSELAGE AFT PASSENGER DOOR UPPER CORNER DOOR JAMB CRACKED .5 INCH AT STA 1660.000 L-9 TO L-101. PERFORMED MAJOR REPAIR. REMOVED FASTENER, DAMAGED AREA AND FABRICATED FILLER, DOUBLER, AND TRIPLER. CLEANED, TREATAug 22, 2004 · N606AL · Doug DC873F · Fuselage Main, StructureSDR IXXA0500004SDoubler · crackedDURING ROUTINE C-CHECK INSPECTION PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-1 FIG 36 PG 133-134. REMOVED FASTENERS IAW DC8 SRM 51-1-21 PG 1, PERFORMED STOP HOLE ON CRACK END IAW DC8 SRM 57-2-1 PAGES 133, 134 FIG 36. FABRICATED EXTERNAL DOUBLER (AL 707576 0-160Aug 22, 2004 · N606AL · Doug DC873F · Wing Miscellaneous StructureSDR UPS04842990Fastener · brokenINSPECTION TYPE:N/A FWD LIFE RAFT OPEN AND ONE SNAP BROKEN. REPAIRED SNAP AND CLOSED LIFE RAFT CORNER.Aug 21, 2004 · N813UP · Doug DC873F · Life RaftSDR UPS04842983Precooler · overtempAT FL 370 ENGINE ANTI ICE WAS TURNED ON, SHORTLY AFTER MANIFOLD OVER TEMP LIGHT ILLUMINATED MANIFOLD TEMP (RT) REACHED RED ARC. COCKPIT FILLED WITH SMOKE AND FUMES. COMPLIED WITH CHECKLIST AND TURNED NR 3 ENG ANTI-ICE OFF. MANIFOLD TEMP RETURNED TO NORMAL. Aug 21, 2004 · N802UP · Doug DC873F · Pneumatic Indicating SystemSDR UPS04843021Battery Pack · inoperativeEMERGENCY LIGHTS WILL NOT CAME ON. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW MM 33-50-01-2. ALL OPS CHECK NORMAL.Aug 20, 2004 · N880UP · Doug DC873F · Emergency LightingSDR UPS04842991Slide · deterioratedGIRT BAR CABLE UNHOOKED FROM RAFT. UPON FURTHER INSPECTION FOUND SEVERAL AREAS OF DETERIORATION ON SLIDE. REMOVED AND REPLACED DOOR SLIDE IAW MM 25-60-01-2.Aug 20, 2004 · N812UP · Doug DC873F · Escape SlideSDR IXXA0500077SSkin · damagedDURING A ROUTINE C-CHECK INSPECTION FOUND LT INBOARD FLAP WITH TEMP REPAIR ON UPPER SURFACE STA XW 90.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF PLATING WITH THE TEMP REPAIR ON IT. FABRICATED NEW PLATING. CLEANED, TREATED AND PRIMED AREA AND THE INNER FACE OAug 19, 2004 · N606AL · Doug DC873F · Trailing Edge FlapsSDR IXXA0500009SSkin · corrodedDURING A ROUTINE C-CHECK INSPECTION MAINTENANCE PERFORMED A MAJOR REPAIR ON VERTICAL STABILIZER L/E UPPER SKIN. FOUND CORROSION AT STA ZFS 179.000. REMOVED CORROSION FROM VERTICAL STABILIZER L/E UPPER SKIN STA ZFS 179.000 IAW DC8 SRM 51-1-8 PGS 17, 18. FOUNAug 18, 2004 · N606AL · Doug DC873F · Vertical Stabilizer, Plate/SkinSDR IXXA0500008SSkin · damagedDURING A ROUTINE C-CHECK MAINTENANCE FOUND RT OUTBOARD FLAP L/E HAS INTERIM REPAIR ON UPPER SKIN, STA XF 418.000. PERFORMED MAJOR REPAIR IAW DCI SRM 57-1-0 PG 1 DC8, SRM 57-7-1 FIG 4 (TR 5794). REMOVED PLATING WITH INTERIM REPAIR ON IT, IAW DC8 SRM 51-1-21 PAug 18, 2004 · N606AL · Doug DC873F · Trailing Edge FlapsSDR IXXA0500030SPanel · damagedDURING A ROUTINE C CHECK INSPECTION, FOUND RT INNER WING EXTENDED LEADING EDGE SLANT PANEL UPPER CAP INTERIM REPAIRS BETWEEN STATIONS XFS. 32.500 AND XFS. 182.500. REPAIR ACCOMPLISHED. REMOVED DAMAGED SLANT PANEL UPPER CAP IAW EC8 SRM 51-1-20D PG 21, DC8 SRMAug 17, 2004 · N606AL · Doug DC873F · Wing, Plate/SkinSDR IXXA0500007SSkin · crackedDURING A ROUTINE C-CHECK INSPECTION, EXTERNAL FUSELAGE CRACKED .75 INCH FROM STA 1718.000 TO STA 1719.000. MAINTENANCE PERFORMED MAJOR REPAIR IAW DC8 DRM 53-2-1 FIG 7. REMOVED FASTENERS IAW DC8 SRM 51-1-21 PG 1. REMOVED CRACKED AREA IAW DC8 SRM 51-1-21 PG 1Aug 17, 2004 · N606AL · Doug DC873F · Fuselage Structure (General)SDR IXXA0500005SSkin · corrodedDURING A ROUTINE C-CHECK INSPECTION FOUND RT FUSELAGE AFT CENTER SECTION LOWER PLATING CORROSION DAMAGE AROUND STA 1340.000, L-31 RT. PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW DC8 SRM 51-1-21 PG 1 DC8, SRM 51-1-20D PG 21. REMOVED CORROSION IAW DC8 51-1-Aug 17, 2004 · N606AL · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA0500029SSkin · damagedDURING A ROUTINE C CHECK INSPECTION, FOUND LT FUSELAGE FWD CENTER SECTION LOWER PLATING HAS INTERIM REPAIR BETWEEN STA FS 470.00 AND 480.00, L-31LH. REPAIR WAS ACCOMPLISHED. REMOVED DAMAGED SECTION, FABRICATED FINGER DOUBLERS AND FILLER AND DOUBLER. CLEANEDAug 16, 2004 · N606AL · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA060135SHinge Fitting · crackedDURING ROUTINE C CHECK FOUND LEFT WING INBOARD AILERON UPPER INBOARD HINGE FITTING CRACKED. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED HINGE FITTING. RECEIVED NEW PART, LOCATED, DRILLED, DEBURRED, PRIMED, INSTALLED NEW FITTING AND NEW FASTENERS. RIGGED AAug 14, 2004 · N605AL · Doug DC873F · AileronsSDR IXXA0500028SSkin · crackedDURING A ROUTINE C CHECK INSPECTION, FOUND RT FUSELAGE AFT CENTER SECTION LOWER SKIN, REMOVED DOUBLER, FOUND SKIN CRACKED 4.500" STA 1520.00, L-29R AT FRAME AND ATTACH CLIP. REPAIR WAS ACCOMPLISHED. REMOVED DOUBLER IAW DC8 SRM 51-1-21 PG 1. REMOVED THE DAMAAug 14, 2004 · N606AL · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2004804004Engine · leakingACFT EXPERIENCED A SUDDEN LOSS OF OIL QUANTITY AND PRESSURE THAT CAUSED THE FLIGHT CREW TO PERFORM EN ROUTE ENGINE SHUTDOWN OF THE NR 2 ENGINE.Aug 12, 2004 · N804DH · Doug DC873F · Turbine Engine Oil SystemSDR DHL2004804Engine · leakingAIRCRAFT EXPERIENCED A SUDDEN LOSS OF OIL QUANTITY AND PRESSURE THAT CAUSED THE FLIGHT CREW TO PERFORM ENROUTE ENGINE SHUTDOWN OF THE NR 2 ENGINE.Aug 12, 2004 · N804DH · Doug DC873F · Turbine Engine Oil SystemSDR DHL2004801008Blower · failedRADIO RACK OVERHEAT LIGHT ILLUMINATED IN FLIGHT ABNORMAL PROCEDURE PERFORMED HOT ELECTRICAL ODOR NOTICEABLE IN COCKPIT RADIO RACK OVERHEAT LIGHT EXTINGUISHED AND ODOR WENT AWAY AFTER VENTURI VALVE OPENED. DEFERRED RADIO RACK BLOWER IWA MEL 21-27 PLACARD INSTAAug 12, 2004 · N801DH · Doug DC873F · Air Distribution FanSDR IXXA0500033SDoor Frame · damagedDURING A ROUTINE C CHECK INSPECTION, LT FUSELAGE FORWARD PASSENGER DOOR UPPER FORWARD JAMB CORNER INTERIM REPAIR AROUND STA 25.000, L-8L TO L-10L. REPAIR ACCOMPLISHED, REMOVED INTERIM REPAIR, FABRICATED DOUBLER AND TRIPLER. CLEANED, TREATED AND PRIMED AREA. Aug 11, 2004 · N606AL · Doug DC873F · Fuselage Main, StructureSDR IXXA4001040Door · openAFTER TAKE OFF WITH THE GEAR UP THE CREW HEARD EXCESSIVE NOISE COMING FROM THE NOSE GEAR AREA. CREW CYCLED GEAR AND SOUND CONTINUED UPON INVESTIGATING NOSE GEAR AREA FOUND LT FWD GEAR DOOR OPEN, RESET DOOR IAW DC-8. OPS CHECK NORMAL NO DAMAGE NOTED.Aug 11, 2004 · N603AL · Doug DC873F · Nose/Tail Landing GearSDR IXXA0500045SSkin Panel · corrodedDURING A ROUTINE C-CHECK INSPECTION, FOUND LT FUSELAGE FORWARD AND AFT CENTER SECTION PRESSURE PANEL CORROSION DAMAGE BETWEEN STA FS 980.000 AND FS 857.000. REPAIR ACCOMPLISHED. REMOVED FASTENERS, AND REMOVED CORROSION. FOUND OUT OF LIMITS. PERFORMED NDT IAug 10, 2004 · N606AL · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2004805009Control Valve · malfunctionedANTI SKID LIGHT ON DIM DURING T/O ROLL, T/O WARNING HORN CHIRPS AFTER V1 AND THRU ROTATION. REMOVED AND REPLACED LT MLG STRUT OUTBOARD ANTI SKID CONTROL VALVE PER MM 32-43-3, OPS CHECK GOOD.Aug 10, 2004 · N805DH · Doug DC873F · Brake Anti-Skid SectionSDR IXXA060136SAngle · crackedDURING ROUTINE C CHECK, FOUND RIGHT WING LOWER SURFACE INBOARD OF NUMBER 1 SPOILER PANEL ATTACH ANGLE CRACKED. REMOVED DAMAGE. FABRICATED REPAIR ANGLES, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR ANGLES AND NEW FASTENERS AT RIGHT Aug 9, 2004 · N605AL · Doug DC873F · SpoilersSDR IXXA0500044SSkin · damagedDURING A ROUTINE C-CHECK INSPECTION, RT WING OUTBOARD FLAP UPPER FORWARD PLATING INTERIM REPAIR AROUND STA XF. 226.000. REPAIR ACCOMPLISHED. REMOVED ALL FASTENERS WITHIN REPAIR AREA. REMOVED THE DAMAGED AREA. PERFORMED NDT INSPECTION, CLEANED, TREATED AND Aug 9, 2004 · N606AL · Doug DC873F · Wing, Plate/SkinSDR IXXA0500042SFitting · crackedDURING A ROUTINE C CHECK INSPECTION, FOUND LT FUSELAGE LONGERON 24 FITTING FRAME CRACK DAMAGE AT STA 879.000. REPAIR ACCOMPLISHED. REMOVED FITTING. FABRICATED SHIMS, DOUBLER AND SPLICES. HEAT TREATED SHIMS AND DOUBLER. CLEANED, TREATED AND PRIMED AREA ANDAug 7, 2004 · N606AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA0500041SAngle · corrodedDURING A ROUTINE C CHECK INSPECTION, RT FUSELAGE STRUCTURE FOWARD CENTER SECTION PRESSURE ATTACH ANGLE HAS CORROSION DAMAGE AT STA Y=857.125(XCW 44). REPAIR ACCOMPLISHED. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED THE CORRODED ANGLE, CLEANED TREATEDAug 7, 2004 · N606AL · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2004805008Control Box · failedINTERMITTENT ANTI-SKID LIGHT ON T/O, LIGHT FLICKERED DIMLY ON AND OFF. REMOVED AND REPLACED ANTI-SKID CONTROL BOX , OPERATIONAL CHECK OK PER M/M 32-43-0.Aug 7, 2004 · N805DH · Doug DC873F · Brake Anti-Skid SectionSDR IXXA0500031SSkin · damagedDURING A ROUTINE C CHECK INSPECTION, FOUND LOWER CARGO COMPARTMENT FORWARD DOOR OUTER SKIN DENT, NICK DAMAGES AND INTERIM REPAIR AT STA 320.0000. REPAIR ACCOMPLISHED, REMOVED DAMAGED PLATING IAW DC8 SRM 51-1-21 PG 1. FABRICATED NEW PLATING (2014T60 0.050"(P.Aug 6, 2004 · N606AL · Doug DC873F · Cargo/Baggage DoorsSDR IXXA0500032SSkin · damagedDURING A ROUTINE C CHECK INSPECTION, FOUND AFT LOWER CARGO COMPARTMENT FORWARD DOOR PLATING WERE DAMAGE AND INTERIM REPAIRS STA 1160.000 AT 1220.000. REPAIR ACCOMPLISHED, REMOVED EXTERNAL PLATING WITH INTERIM REPAIR, CLEANED, TREATED AND PRIMED AREA. APPLIEAug 5, 2004 · N606AL · Doug DC873F · Cargo/Baggage DoorsSDR DHL2004873005Warning Light · illuminatedUPON LANDING GEAR EXTENSION LEFT LANDING GEAR LIGHT CAME ON IMMEDIATELY UPON LOWERING LANDING GEAR HANDLE.Aug 3, 2004 · N873SJ · Doug DC873F · Landing Gear Position and WarningSDR DHL2004804534Clip · crackedITEM REF. NR. 2091: NR 1 ALT. TANK LWR SECTION INTERIOR CLIP CRACKED (STA. XRS 456.562 - 460.000, S-62L TO S-63L). REMOVED CRACKED CLIP IAW DC8 SRM 51-1-20D PG. 21. FABRICATED NEW CLIP (AL 7075-T651) IAW EA NR 5720-037, DWG 3864001. HEAT TREATED IAW DACO CP 7Jul 31, 2004 · N804DH · Doug DC873F · Wing Miscellaneous StructureSDR DHL2004804533Bracket · crackedAFT ACCY. COMPT. BRACKET CRACKED 0.500, L-35R TO L-36, STA. 660.000. REMOVED CRACKED BRACKET IAW SRM 51-3-0 PG. 1-2. FABRICATED NEW BRACKET (ALCLAD 7075-T651) IAW EA NR 5320-036, DWG 5755360. HEAT TREATED IAW DACO DPS 7.00. PERFORMED NDT INSP. IAW NDT SPM PARJul 31, 2004 · N804DH · Doug DC873F · Fuselage Miscellaneous StructureSDR IXXA060111SFrame · corrodedDURING ROUTINE C-CHECK FOUND CORRODED FRAME AT STATION 140 LONGERON 36. REMOVED CORROSION,. ORIGINAL THICKNESS, .080 REMOVED .040 MATERIAL, OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, LOCATED, DRILLED, DEBURRED, TREATED, PRIMED, INSTALLED REPJul 30, 2004 · N605AL · Doug DC873F · Fuselage Main, FrameSDR IXXA060109SFrame · corrodedDURING ROUTINE C-CHECK FOUND CORRODED FRAME AT STATION 180 LONGERON 36. REMOVED CORROSION, ORIGINAL THICKNESS .100 REMOVED .040 MATERIAL, OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, LOCATED, DRILLED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIJul 30, 2004 · N605AL · Doug DC873F · Fuselage Main, FrameSDR IXXA060110SFrame · corrodedDURING ROUTINE C CHECK FOUND CORRODED FRAME AT STATION 220 LONGERON 36. REMOVED CORROSION,. ORIGINAL THICKNESS .100 REMOVED .040 MATERIAL, OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTAJul 30, 2004 · N605AL · Doug DC873F · Fuselage Main, Frame
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