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 DHL2004804523Bracket · crackedNR 4 ALT FWD BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED BRACKET ON NR 4 ALT FWD BOOSTER PUMP IAW SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 21-9.Jul 7, 2004 · N804DH · Doug DC873F · Wing Miscellaneous StructureSDR DHL2004804522Bracket · crackedNR 4 ALT TANK AFT BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED BRACKET ON NR 4 ALT TANK AFT BOOSTER PUMP IAW SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 21-9.Jul 7, 2004 · N804DH · Doug DC873F · Wing Miscellaneous StructureSDR UPS04842655Window · stiffINSPECTION TYPE:N/A CAPTAINS CLEARVIEW WINDOW HARD TO OPEN. OPENED AND CLOSED CAPTAIN'S SLIDING WINDOW THROUGH CYCLES. WINDOW OPENS AND CLOSES NORMALLY. NO DEFECTS NOTED. OK FOR CONTINUOUS SERVICE.Jul 7, 2004 · N818UP · Doug DC873F · Flight Compartment WindowsSDR DHL2004804510Cargo Track · wornMAIN CARGO COMPT NR 6 TRACK LUG WORN, STA 248.000 TO STA. 275.000. TRIMMED OUT DAMAGED SEGMENT IAW SRM 53-2-3 PG 49-50 FIG 14. FABRICATED SPLICES (AL 7075-T6 0.100, 0.125, 0.160) IAW SRM 53-2-3 PG 49-50 FIG 14. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B (AJul 5, 2004 · N804DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004804509Skin · crackedITEM REF. NR. 1071: EXTERNAL FUSELAGE PLATING WITH CRACKS 0.250, 0.750 AT STA. FS 1742.000, FS 1747.000, L-15L TO L-17L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG.7. REMOVED RIVETS IAW SRM 51-1-21 PG.1. TRIMMED OUT IAW SRM 53-2-1 PG.107-108 FIG.Jul 2, 2004 · N804DH · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS04842699Rib · crackedINSPECTION TYPE: C-3, RT CENTER L/E HAS CRACKED RIB AT APPROX STA 304.600. REMOVED EXISTING REPAIR IAW DC8 SRM 51-1-211. MAT ID FOR REPAIR ANGLE BAC 1503-100147 EXTRUSION 7075-T6 PO 437138. STOP DRILLED CRACKED. LOCATED, DRILLED & DEBURRED REPAIR ANGLE. Jul 2, 2004 · N803UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS04842698Rib · crackedINSPECTION TYPE: C-3, RT CENTER 4E HAS CRACKED RIB AT APPROX STA 448.00. REMOVED FASTENERS IN REPAIR AREA RT CENTER L/E AT STA 448.00 & STOP DRILL CRACK. MAT ID FOR REPAIR ANGLE 9751065-33 EXTRUSION 7075-T6 PO 387706. PERFORMED HFEC IAW MD NDT SPM 06-10-01.Jul 2, 2004 · N803UP · Doug DC873F · Wing, Rib/BulkheadSDR DHL2004807012Warning Light · illuminatedYELLOW MX LIGHT ILLUMINATED ON LWR CARGO SMOKE DETECTOR CODE AD16242{B} SYS OK LIGHT ILLUMINATED ALSO. TRANSFERRED TO DMI 17083 IAW MEL 26-10-1,CAT C PLACARD INSTALLED.Jul 2, 2004 · N807DH · Doug DC873F · Smoke DetectionSDR UPS04842697Rib · crackedINSPECTION TYPE:C-3, RIGHT CENTER L/E RIB CRACKED AT APPROX STA 379.000 VERIFIED BY NDT. STOP DRILL CRACK. MAT ID FOR RIB AT XFS 379 .063 7075-T6. MAT ID FOR REPAIR ANGLE 7075-T6 .080 PO 437138.5. ACCOMPLISHED HFEC INSP OF STOP DRILL IAW DAC NTSPM 06 10-01Jul 1, 2004 · N803UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS04842696Rib · crackedINSPECTION TYPE:C-3, RIGHT WING CTR L/E RIB CRACKED AT APPROX STA XFS 304 VERIFIED BY NDT. PERFORMED AFEC IAW DAC SPM NDT 06-10-001-01 TO VERIFY CRACK END AT FASTENER HOLE. MAT THICKNESS FOR RIB AT STA XFS 304 .063 7075-T6, MAT ID FOR REPAIR ANGLE 7075-T6 .0Jul 1, 2004 · N803UP · Doug DC873F · Wing, Rib/BulkheadSDR DHL2004807011Warning Light · illuminatedDURING CRUISE FLIGHT, LOWER CARGO FIRE "MX" LIGHT ILLUMINATED "SYS OK" LIGHT REMAINED ILLUMINATED. NO DEFECT NOTED, PERFORMED SYSTEM OPS CHECK IAW MM SUPP 26-15-00, OK FOR SERVICE.Jul 1, 2004 · N807DH · Doug DC873F · Fire DetectionSDR UPS04842691Seat Track · corrodedINSPECTION TYPE: C-3, FWD PIT FS 600 MIDDLE ROW OF FASTENERS IN SEAT TRACK SPLICE (AS SEEN FROM BELOW) LOCATED AT BC 60 R- CORROSION AROUND FASTENERS & SPACER. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-3. MAT ID FOR SEAT TRACK SPLICES A &Jun 30, 2004 · N803UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA060132SSkin · dentedDURING ROUTINE C CHECK, FOUND RIGHT WING DENTED AT STATION XFS-45 OUTBOARD OF LIFT ATTACH POINT. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGE. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPJun 29, 2004 · N605AL · Doug DC873F · Wing, Plate/SkinSDR DHL2004804507Cargo Track · wornMAIN CARGO COMPT NR 4 TRACK LUG WORN, STA 1696.000. TRIMMED OUT DAMAGED AREA IAW SRM 53-2-3 PG 17 FIG 6D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW CHANNEL AND TRACK PLUG IAW SRM 51-3-0 PG 1.Jun 28, 2004 · N804DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004804506Frame · crackedRIGHT WING CTR L/E UPPER FORMER CRACKED 1.000, XFS 316.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END AND FABRICATED ANGLE DOUBLER (AL 2024-T3 0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER IAW SRM 51Jun 27, 2004 · N804DH · Doug DC873F · Wing SparSDR DHL2004804508Cargo Track · wornMAIN CARGO COMPT NR 2 TRACK PLUG LUG WORN, STA 1133.000. REMOVED WORN NR 2 TRACK PLUG, STA 1133.000 IAW DC8 SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW PLUG IAW SRM 51-3-0 PG 1.Jun 27, 2004 · N804DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004804505Rib · crackedRT WING CTR. LE UPPER FORMER CRACKED 0.500, XFS 347.750. CORR.: REMOVED FASTENER IAW SRM 51-1-21 PG.1. PERFORMED STOP HOLE ON CRACK END AND FABRICATED ANGLE DOUBLER (AL2024-T3 0.040) IAW SRM 57-2-0 PG.9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER IAW SRM 51-Jun 27, 2004 · N804DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2004804504Rib · crackedITEM REF. NR. 1514: RT WING CTR. LE UPPER FORMER CRACKED 0.500 AT XFS 354.000. REMOVED FASTENER IAW SRM 51-1-21 PG.1. PERFORMED STOP HOLE ON CRACK END AND FABRICATED ANGLE DOUBLER (AL 2024-T3 0.040) IAW SRM 57-2-0 PG.9-10. CLEANED TREATED AND PRIMED ANGLE DOJun 27, 2004 · N804DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2004805006Warning Light · false indicationDURING UPLATCH CHECK RT GEAR UNSAFE LIGHT ILLUMINATED. PERFORMED ABNORMAL PROCEDURE CYCLED GEAR TWICE UPLATCH CHECKED, OK. DEFER IAW MEL32-16-1 CAT A ITEM DMI NR 17038, COMPLIED WITH S/P 32-16,MAIN LANDING GEAR UPLATCH SYS. PLACARD INSTALLED.Jun 27, 2004 · N805DH · Doug DC873F · Landing Gear Position and WarningSDR IXXA060131SAngle · crackedDURING ROUTINE C CHECK, FOUND RIGHT WING INBOARD FLAP OUTBOARD ANGLE CRACKED. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED ANGLE. FABRICATED NEW ANGLE, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED NEW ANGLE, AND FASTENERS AT RIGHT WING INJun 26, 2004 · N605AL · Doug DC873F · Trailing Edge FlapsSDR IXXA060130SSkin · crackedDURING ROUTINE C CHECK, FOUND RIGHT WING INBOARD AILERON TP SIDE ABOVE AILERON TRIM LINKAGE SKIN CORRODED. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, DEBURRED. TREATED, PRIMED, INSTALLED REPAIR PARTS ANJun 26, 2004 · N605AL · Doug DC873F · AileronsSDR UPS04842742Fitting · crackedINSPECTION TYPE:C-3 MAIN CABIN FS 25 LONGERON 22 END FITTING CRACKED. REMOVED FITTINGS IAW DC8 SRM 51-3-0, LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-3-2. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FITTINGS IAW DC8 SRM 51-1-20D, 51-3-0, 51-3-1.Jun 26, 2004 · N803UP · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2004807010Smoke Detector · will not testMAIN CABIN SMOKE DETECTOR NR 2 WILL NOT TEST. NR 2 MAIN CABIN SMOKE DETECTOR OPS CHECK NORMAL IAW DC 8 MM 26-10-6, THIS CLEARS DMI 17026.Jun 26, 2004 · N807DH · Doug DC873F · Smoke DetectionSDR DHL2004804515Frame · crackedLEFT INNER WING L/E OUTBOARD SECTION FORMER CRACKED 0.500, STA XFS 641.250. REMOVED FASTENERS IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 21. PERFORMED STOP HOLE IAW DC8 SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024-T3 0.032) IAW DC8 SRM 57-2-0 PJun 25, 2004 · N804DH · Doug DC873F · Wing SparSDR DHL2004804514Frame · crackedLEFT OUTER WING L/E OUTBOARD SECTION FORMER CRACKED 0.500, STA XFS 860.000. REMOVED FASTENERS IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 21. PERFORMED STOP HOLE IAW DC8 SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024-T3 0.032) IAW DC8 SRM 57-2-0 PJun 25, 2004 · N804DH · Doug DC873F · Wing SparSDR UPS04842610Seat · malfunctionedINSPECTION TYPE:N/A CAPTAINS SEAT WILL NOT LOCK IN PLACE, IT SLID OUT OF POSITION AT BEGINNING OF T/O ROLL AND SETTING THE BRAKES AT ENGINE SHUTDOWN. SEAT WAS IN FALSE LOCK POSITION. REPLACED CAPTAIN'S SEAT ASSY IAW 25-11-01-2. OPS CHECK GOOD.Jun 25, 2004 · N802UP · Doug DC873F · Flight Compartment EquipmentSDR DHL2004804502Cargo Track · wornMAIN CARGO COMPT NR 7 TRACK PLUG LUG WORN, STA 320.000. REMOVED WORN PLUG IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PLUG IAW SRM 51-3-0 PG 1.Jun 24, 2004 · N804DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004804503Frame · crackedLEFT JOINT FLAP FORMER CRACK, STA XW 122.000. FABRICATED ANGLE DOUBLER (2024T3 0.050) IAW DC8 SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW DC8 SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW DC8 SRM 57-2-0 PG 9-10, DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-21A PG Jun 24, 2004 · N804DH · Doug DC873F · Wing SparSDR DHL2004804501Cargo Track · wornMAIN CARGO COMPT NR 2 TRACK PLUG LUG WORN, STA 1215.000. REMOVED DETERIORATED PLUG IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PLUG IAW SRM 51-3-0 PG 1.Jun 24, 2004 · N804DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004804500Cargo Track · wornMAIN CARGO COMPT NR 3 TRACK PLUG LUG WORN, STA 689.000. REMOVED NR 3 TRACK PLUG, STA 689.000 IAW DC8 SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW PLUG IAW DC8 SRM 51-3-0 PG 1.Jun 24, 2004 · N804DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA060120SSupport Channel · brokenDURING ROUTINE C-CHECK FOUND HAT CHANNEL BROKEN AT STATION 1586 LONGERON 21 RIGHT. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED HAT CHANNEL SECTION. FABRICATED REPAIR PARTS. LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND NJun 22, 2004 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR IXXA060119SFrame · crackedDURING ROUTINE C-CHECK FOUND FRAME CRACKED AT STATION 1580 LONGERON 21 LEFT. REMOVED FASTENER AS NEEDED TO REMOVE DAMAGED FRAME SECTION. FABRICATED REPAIR PARTS, LOCATED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS AT STATIONJun 22, 2004 · N605AL · Doug DC873F · Fuselage Main, FrameSDR IXXA060118SFrame · crackedDURING ROUTINE C-CHECK FOUND FRAME CRACKED AT STATION 1580 LONGERON 21 RIGHT. REMOVED FASTENER AS NEEDED TO REMOVE DAMAGED FRAME SECTION. FABRICATED REPAIR PARTS, LOCATED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS AT STATIOJun 22, 2004 · N605AL · Doug DC873F · Fuselage Main, FrameSDR IXXA04000930Warning Light · will not testDURING DESCENT, NR 1 ENG FIRE WARNING SYSTEM SHORT LIGHT ILLUMINATED AND FIRE WARNING WOULD NOT TEST. NR 1 ENGINE SHUT DOWN IN FLIGHT. MAINTENANCE NOTED ENGINE IS WITHIN LIMITS PER ALL APPLICABLE MANUALS. MAINTENANCE CLEANED AND RESECURED WIRING CONNECTORS Jun 22, 2004 · N606AL · Doug DC873F · Smoke DetectionSDR UPS04842625Doubler · damagedINSPECTION TYPE: C, EXISTING REPAIR DOUBLER AT EXT PWR RECEPTICAL FOUND TO HAVE PREVIOUS DAMAGE ON FAYING SURFACE (GOUGE). REMOVED DOUBLER. MAT ID FOR NEW DOUBLER 7075-T6 .063 PO 442690.4 IAW DC8 SRM 53-2-0 & 51-9-0 FIG 68A. FAB DOUBLER IAW DC8 SRM 51-1-8, Jun 21, 2004 · N803UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS04842624Doubler · brokenINSPECTION TYPE:C, NOSE EXT PWR RECEPTICAL DOOR PNL CUTOUT HAS BROKEN SECTION. REMOVED INNER DOUBLER IAW DC8 SRM 51-1-21. MAT ID FOR NEW DOUBLER 7075-T6 .063 PO 428102.3 IAW DC8 DWG 5613862 & DC8 SRM 51-9-0 FIG 68A. FAB NEW DOUBLER, ALODINED AND PRIMED IAW Jun 21, 2004 · N803UP · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA060129SFlap Track · gougedDURING ROUTINE C CHECK, FOUND RIGHT OUTBOARD FLAP OUTBOARD HINGE ICE DOOR TRACK GOUGED. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED TRACK. FABRICATED NEW TRACK, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED INSTALLED NEW TRACK AND FASTENERS AT RIGHTJun 18, 2004 · N605AL · Doug DC873F · Trailing Edge FlapsSDR IXXA060128SFlap Track · gougedDURING ROUTINE C CHECK, FOUND RIGHT HAND OUTBOARD FLAP LEADING EDGE INBOARD HINGE AT FLAP STATION XRS-230.000 ICE DOOR INBOARD TRACK GOUGED. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED TRACK. FABRICATED NEW TRACK, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATJun 18, 2004 · N605AL · Doug DC873F · Trailing Edge FlapsSDR IXXA060127SSupport Angle · crackedDURING ROUTINE C CHECK, FOUND RIGHT WING RIGHT OUTBOARD FLAP INBOARD TRAILING EDGE SUPPORT ANGLE CRACKED. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS, ANDJun 18, 2004 · N605AL · Doug DC873F · Trailing Edge FlapsSDR IXXA060126SVane · gougedDURING ROUTINE C CHECK, FOUND RIGHT WING FLAP NUMBER 2 FIXED VANE OUTBOARD UPPER EDGE GOUGED. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, LOCATED, TRIMMED, ALODINED, INSTALLED AND CURED ALL REPAIR PARTS ON RIGHT WING FLAP NUMBER 2 FIXED VANE, PRIMED AND SJun 18, 2004 · N605AL · Doug DC873F · Trailing Edge FlapsSDR IXXA060125SVane · delaminatedDURING ROUTINE C CHECK, FOUND RIGHT WING FLAP NUMBER 1 VANE LOWER INBOARD SECTION DELAMINATED. REPLACED RIGHT WING FLAP NUMBER 1 VANE WITH OVERHAULED UNIT.Jun 18, 2004 · N605AL · Doug DC873F · Trailing Edge FlapsSDR IXXA060154SAngle · crackedDURING ROUTINE C CHECK, FOUND NUMBER 1 ENGINE PYLON LOWER AFT SECTION HAS CRACKED RIB ANGLE VERY AFT RIB. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED RIB ANGLE. FABRICATED NEW RIB ANGLE, LOCATED, DRILLED, TRIMMED, DEBURRED, PRIMED. INSTALLED NEW RIB ANGLJun 17, 2004 · N605AL · Doug DC873F · Nacelle/Pylon Miscellaneous StructureSDR IXXA060144SSkin · corrodedDURING ROUTINE C CHECK, FOUND AFT CARGO DOOR INTERIOR SKIN AT UPPER FORWARD STOP CORRODED. REMOVED FASTENERS AS NEEDED TO REMOVE EXISTING DOUBLER. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLEDJun 17, 2004 · N605AL · Doug DC873F · Cargo/Baggage DoorsSDR IXXA060124SWedge · crackedDURING ROUTINE C-CHECK FOUND RT WING OUTBOARD AILERON OUTBOARD WEDGE TRAILING EDGE GOUGED. PERFORMED HFEC, FOUND WEDGE CRACKED. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED. FABRICATED REPAIR PARTS, LOCATED, DRILLED, DEBURRED, TRIMMED, TREATED, PRIMED, INSJun 17, 2004 · N605AL · Doug DC873F · AileronsSDR UPS04842662Rib · gougedINSPECTION TYPE: C-3, RT WING OUT BOUND L/E INBOARD END RIB HAS DEEP GOUGE. BLENDED GOUGE AREA, FOUND OUT OF LIMITS IAW DC8 SRM 57-2-1 FIG 2G. FAB DOUBLER REPAIR IAW DC8 SRM 57-2-0 AND 51-1-4. LOCATED & DRILLED DOUBLER IAW DC8 SRM 51-1-24 & 51-2-0. ALODINJun 17, 2004 · N803UP · Doug DC873F · Wing, Rib/BulkheadSDR IXXA060148SAccess Panel · wornDURING ROUTINE C CHECK, FOUND NUMBER 3 PYLON FOOTSTOOL ACCESS PANEL HAS SEVERAL AREAS WITH DEEP FRETTING WEAR. FABRICATED NEW FOOTSTOOL ACCESS PANEL, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, AND PRIMED NEW FOOTSTOOL ACCESS PANEL IAW DC8 SRM 53-2-0, 51-1-Jun 16, 2004 · N605AL · Doug DC873F · Nacelle/Pylon, Plate/SkinSDR IXXA060115SWeb · crackedDURING ROUTINE C CHECK FOUND A CRACKED WEB AT LIGHTNING HOLE AT STATION 1164 LBL 68 LONGERON 21 LT. REMOVED DAMAGED. FABRICATED DOUBLER, LOCATED, DRILLED, DEBURRED, PRIMED, INSTALLED DOUBLER AND NEW FASTENERS AT STATION 1164 LBL 68. IAW SRM 51-1-21, 53-4-1, ANJun 16, 2004 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR IXXA060112SPanel · gougedDURING ROUTINE C-CHECK FOUND NR 4 PYLON WRAP AROUND PANEL HAS 2 EACH DEEP GOUGES. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, LOCATED, DRILLED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS ON NR 4 PYLON WRAP AROUND PANEL. IAW SRM 54-2Jun 16, 2004 · N605AL · Doug DC873F · Nacelle/Pylon Miscellaneous StructureSDR UPS04842745Frame · corrodedINSPECTION TYPE: C-3, STA 35 AT LONGERON 22R CORRODED AT FRAME. REMOVED FRAME SECTION TO FOM FAB NEW FRAME SECTION AND SPLICES INSTALLED NEW FRAME SECTION AND SPLICES IAW DAC DWG 5613836 AND REO GO9859 AND DC8 SRM 51-1-21, 51-1-20D, 51-1-8.Jun 16, 2004 · N803UP · Doug DC873F · Fuselage Main, FrameSDR IXXA060165SDoubler · gougedDURING ROUTINE C-CHECK, FOUND LEFT WING INBOARD FLAP UPPER OUTBOARD REPAIR DOUBLER GOUGED. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED DOUBLER. FABRICATED NEW DOUBLER, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED. INSTALLED NEW DOUBLER AND NEW FASJun 15, 2004 · N605AL · Doug DC873F · Trailing Edge Flaps
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