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 UPS06847942Skin · crackedINSPECTION TYPE:C3 CRACK AT STA 1741 L17R OUTER SKIN SURFACE. REPAIRED CRACKED SKIN AT STA 1741 L17R IAW SAA EA NR 008-5320-01-A0401 UPS EO DC8-5330-25029-A, BAC SERV REQUEST NR 1-223199646-2, DACO DWG 5649327 REV P, AND FAA FORM 8100-9.Aug 8, 2006 · N802UP · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2006809512Attach Fitting · crackedAFT CARGO COMPT FITTING CRACKED STA 1240.000 L-35L (INTERCOSTAL ATTACH FITTING). REMOVED CRACKED FITTING IAW SRM 51-1-20D AND INSTALLED A NEW ONE IAW SRM 51-1-20D, SRM 51-3-1.Aug 8, 2006 · N809DH · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06847625Boot · disconnectedATB - A/C WOULD NOT MAINTAIN PRESSURIZATION ABOVE FL 310. FLOWS ON BOTH SIDES WERE SET TO MAX PRESSURE CONTROL WAS TRIED IN BOTH AUTO AND MANUAL MODES. LT MANIFOLD TEMP READ 195 AND RIGHT TEMP WAS 235. MANIFOLD PRESSURE FOR BOTH SIDES. OPENED PNLS 697,91D Aug 7, 2006 · N811UP · Doug DC873F · Humidity Control SystemSDR DHL2006809510Intercostal · crackedFWD CARGO COMPT INTERCOSTAL 0.500" CRACK (STA 8.000 - 25.000, L-28R TO L-29R). REMOVED CRACKED INTERCOSTAL IAW SRM 51-1-21. CLEANED AREA IAW SRM 51-1-8B. INSTALLED NEW INTERCOSTAL IAW SRM 51-1-21. REFER TO JC EA53000007-001-D (WO 600016595) AND BOEING MESSAug 5, 2006 · N809DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2006809509Stiffener · crackedMAIN CARGO COMPT FLOORBEAM STIFFENER 0.500" CRACK STA 980.000 RBL 25" TO RBL 26". REMOVED AND REPLACED FLOORBEAM STIFFENER AT STA 980.000 RBL 25" TO RBL 26" IAW SRM 51-1-20D, SRM 51-3-1. REFER TO JC EA53000006-001-D W/O NR 600016595 FOR FABRICATION.Aug 5, 2006 · N809DH · Doug DC873F · Fuselage Miscellaneous StructureSDR IXXA06SMN279SLongeron · crackedDURING ROUTINE C-CHECK INSPECTION FOUND LONGERON 36 CRACKED AT STATION 1350.000. REMOVED FASTENERS. TRIMMED OUT CRACKED LONGERON SEGMENT. FABRICATED NEW LONGERON FROM EXTRUSION P/N 2641455, (AL 7075 T651). FABRICATED SPLICE (AL 7075 T651). PERFORMED NDT IAug 4, 2006 · N605AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR IXXA06SMN278SLongeron · crackedDURING ROUTINE C-CHECK INSPECTION FOUND LONGERON 35 RT CRACKED AT STA 1350.000. REMOVED FASTENERS IAW SRM 51-1-20D. REMOVED CRACKED LONGERON SEGMENT. FABRICATED NEW LONGERON FROM EXTRUSION P/N 2641455/ 7075 T651. FABRICATED SPLICE. PERFORMED NDT INSPECTION. CLAug 4, 2006 · N605AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR IXXA06SMN277SSkin · crackedDURING ROUTINE C-CHECK INSPECTION FOUND EXTERNAL FUSELAGE SKIN CRACKED. AT STATION 1746.000, BETWEEN LONGERON 14 LT AND LONGERON 15 LT. REMOVED FASTENERS. REMOVED DAMAGED AREA. FABRICATED EXTERNAL REPAIR DOUBLER (AL 7075 T6 0.071) AND INTERNAL FINGER DOUBLERSAug 4, 2006 · N605AL · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA06SMN276SFitting · crackedDURING ROUTINE C-CHECK INSPECTION FOUND A CRACKED FITTING AT STATION 978.000 LONGERON 18 RT. REMOVED DAMAGED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW SRM 51-3-0, SRM 51-3-1, AND SRM 51-3-0.Aug 4, 2006 · N605AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA06SMN273STorque Tube · wornDURING ROUTINE C CHECK INSPECTION FOUND CONTROL COLUMN TORQUE TUBE WITH DEEP WEAR. REPLACED DAMAGED TORQUE TUBE. CLEANED, TREATED AND PRIMED AREA. IAW SRM 51-1-21, SRM 51-1-20D. SRM 51-1-8B. SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1, AND SRM 27-267 REV. 2 DATE 0Aug 4, 2006 · N605AL · Doug DC873F · Control Column SectionSDR IXXA06SMN275SLongeron · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND LONGERON 36 CORRODED FROM BS 200-180. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SPLICE FITTING. FABRICATED NEW SPLICE FITTING (AL 7075 O 0.071). HEAT TREATED 7075 O TO 7075 T6. CLEANED, TREATED AND PAug 4, 2006 · N605AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR IXXA06SMN274SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LONGERON 19 RT FITTING CRACKED AT STATION STA 822.500. REMOVED CRACKED END FITTING IAW SRM 51-1-20D. FABRICATED NEW END FITTING (AL PLATE 7075-T651) IAW ATI REPAIR SPECIFICATION NR 2003-05, MFG DRAWING NR 4751640. PERFAug 4, 2006 · N605AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS06847595Light · inoperativeINSPECTION TYPE:NA EMERGENCY EXIT/DISARM LIGHT INOP. RELAMPED, OPS CHECKED GOOD.Aug 4, 2006 · N880UP · Doug DC873F · Emergency LightingSDR DHL2006809511Intercostal · crackedRT MLG W/W INTERCOSTAL DOUBLER 1" CRACK STA 875.000. REMOVED INTERCOSTAL IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51--1-8B. INSTALLED INTERCOSTAL IAW SRM 51-1-21. REFER TO JC EA52000003-001-D (WO 600016595) FOR FABRICATION.Aug 2, 2006 · N809DH · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06847587Connector · damagedON UPLATCH, GEAR NOT LATCHED LIGHT IS ILLUMINATED. SAT DOING REPAIR, XFRD TO NRC 996802. DURING T/S FOUND NLG UP LIMIT SWITCH INOP. INSTALLED JUMPER WIRE CONNECTOR P1-218 PINS 7 AND 5 LIGHT CAME ON. REMOVED JUMPER WIRE AND GEAR NOT LATCH LIGHT WENT OFF. TAug 2, 2006 · N803UP · Doug DC873F · Landing Gear System WiringSDR DHL2006809513Doubler · crackedFUS EXTERIOR EXTERNAL POWER RECEPTACLE DOOR, INTERNAL DOUBLER CRACKED 0.500" STA -32.000 STA -40.000 L-31.5R. PERFORMED MAJOR REPAIR IAW SRM 53-3-3 FIG 1. REMOVED EXISTING INTERNAL DOUBLER IAW SRM 53-1-0, SRM 51-1-21, SRM 51-1-20D. FABRICATED INTERNAL DOUBLAug 1, 2006 · N809DH · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS06847552Slide · unwanted deployMAIN CARGO DOOR EXIT SLIDE FELL OUT OF HOLDER, BROKEN CLIP ON COVER EMERG ESCAPE SLIDE INOP. SLIDE REMOVED FROM DOOR AND DEFERRED IAW MEL 52-07-4 AND ASSIGNED DEFERRAL NR M330482. REPLACED DMGD CLIP ON ESCAPE SLIDE COVER PER SMR 51-01-21. RE- INSTALLED SLIDEAug 1, 2006 · N808UP · Doug DC873F · Escape SlideSDR UPS06847665Fitting · crackedINSPECTION TYPE-C1-3 BOTH STRINGER END FITTINGS ON STRINGER 51 AT XRS 74 ARE CRACKED NR 2 MAIN TANK. REMOVED BOTH STRINGER END FITTINGS AT STR 51 XRS 74 NR 2 MAIN TANK IAW SRM 51-1-20D. LOCATED AND DRILLED UP, AND INSTALLED 2 END FITTINGS AT STR 51 AT STA XRJul 31, 2006 · N806UP · Doug DC873F · Wing, Longeron/StringerSDR UPS06847530Battery Pack · inoperativeDURING PRE-DEPARTURE CHECK, FOUND EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW AMM 33-50-01-2. OPS CK GOOD.Jul 31, 2006 · N852UP · Doug DC873F · Emergency LightingSDR UPS06847494Actuator · crackedWHEN FLAPS EXTENDED TO 23 DEGREES OUTER NEEDLE INDICATED 12 DEGREES INNER NEEDLE INDICATED 23 DEGREES, REQUIRED 4 UNITS OF RT AILERON TRIM FOR LEVEL FLIGHT. UPON INSPECTION FOUND LT STA 98 FLAP ACTUATOR PISTON ROD CRACKED IN TWO. REMOVED AND REPLACED STA 98 Jul 30, 2006 · N803UP · Doug DC873F · Trailing Edge Flap ActuatorSDR UPS06847663Fitting · corrodedBATH TUB FITTING EXFOLIATED OUT OF LIMITS AT A-PIT TORQUE BOX STA 280 L33L-L34L. REMOVED BATHTUB FITTING AT STA 280 L33L-L34L IAW SRM 53-02-00, AND SRM 51-1-20D. DRILLED UP AND INSTALLED BATHTUB FITTING AT STA 280 L33L-L34L IAW SRM 53-02-00-0.Jul 29, 2006 · N806UP · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA06SMN269SSkin · misrepairedDURING ROUTINE C-CHECK INSPECTION FOUND LT ELEVATOR LOWER SKIN WITH A NON STANDARD REPAIR FROM STA XE301.656 TO STA XE312.500. REMOVED SKIN WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKIN AND FINGER DOUBLER WITH (AL 2024 T3 0.016”). BONDED BOTH PARTS WJul 28, 2006 · N605AL · Doug DC873F · Elevator, Plate/SkinSDR IXXA06SMN268SSkin · misrepairedDURING ROUTINE C-CHECK INSPECTION FOUND LT ELEVATOR LOWER SKIN WITH A NON STANDARD REPAIR FROM STA XE55.062 TO STA XE60.125. REMOVED SKIN WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKIN AND FINGER DOUBLER WITH (AL 2024 T3 0.016). BONDED BOTH PARTS WITJul 28, 2006 · N605AL · Doug DC873F · Elevator, Plate/SkinSDR IXXA06SMN267SSkin · dentedDURING ROUTINE C-CHECK INSPECTION FOUND LT ELEVATOR UPPER SKIN DENTED FROM STATION XE74.469 TO STATION XE104.031. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND FINGER DOUBLER WITH (AL 2024 T3 0.016”). BONDED BOTH PARTS WITH HYSOL. CLEANED, TREATED AND PRIMED AJul 28, 2006 · N605AL · Doug DC873F · Elevator, Plate/SkinSDR IXXA06SMN266SSkin · misrepairedDURING ROUTINE C-CHECK INSPECTION FOUND LT. ELEVATOR UPPER SKIN HAS A NON STANDARD REPAIR AT STATION XE312.500. REMOVED SKIN WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKIN AND FINGER DOUBLER (AL 2024 T3 0.016”). BONDED BOTH PARTS WITH HYSOL. CLEANED,Jul 28, 2006 · N605AL · Doug DC873F · Elevator, Plate/SkinSDR IXXA06SMN264SSkin · misrepairedDURING ROUTINE C-CHECK INSPECTION FOUND EXTERNAL FUSELAGE FORWARD PASSENGER DOOR UPPER CORNER HAS NON STANDARD REPAIR. REMOVED EXISTING NON STANDARD REPAIR. PERFORMED NDT INSPECTION NO CRACKS OR CORROSION FOUND. FABRICATED REPAIR DOUBLER (AL 7075 T6 0.063), AJul 28, 2006 · N605AL · Doug DC873F · Passenger/Crew DoorsSDR IXXA06SMN260SSkin · misrepairedDURING ROUTINE C-CHECK INSPECTION, LT WING OB FLAP UPPER SKIN NO STANDARD REPAIR NEAR XF 169 TO XF 213.000. PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG. 4 T.R. 57-94 DATE 10-01-02. REMOVED PANEL PLATING WITH NO STANDARD REPAIR EXISTING IAW SRM 51-1-21. FABRICAJul 28, 2006 · N605AL · Doug DC873F · Leading Edge DevicesSDR IXXA06SMN256SSkin · damagedDURING ROUTINE C-CHECK INSPECTION FOUND LT WING OB LEADING EDGE LOWER SKIN HOLES AND DENTED, AT STATION XFS710.000. REMOVED FASTENERS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION NO CRACKS OR CORROSION FOUND. FABRICATED REPAIR DOUBLER, AND FILLERS.050). CLEJul 28, 2006 · N605AL · Doug DC873F · Wing, Plate/SkinSDR IXXA06SMN246SSkin · damagedDURING ROUTINE C-CHECK INSPECTION FOUND RT WING IB LEADING EDGE IB SLOT UPPER SKIN HOLES ELONGATED, AT STATION XS250.089. REMOVED FASTENERS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION, NO CRACKS, OR CORROSION FOUND. FABRICATED REPAIR DOUBLER, INTERNAL DOUBJul 28, 2006 · N605AL · Doug DC873F · Wing, Plate/SkinSDR IXXA06SMN270SSkin · misrepairedDURING ROUTINE C-CHECK INSPECTION FOUND D-PIT BELLY DOOR LOWER AFT CORNER HAS A NON STANDARD REPAIR IAW SB 53-078. REMOVED EXISTING SKIN WITH NON STANDARD REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN. APPLIED SEALANT TO FAYINGJul 28, 2006 · N605AL · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA06SMN271SBulkhead · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND HORIZONTAL PRESSURE WALL CORRODED AT STATION -12.000 LBL 50. REMOVED FASTENERS. REMOVED CORROSION, FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVED. FJul 28, 2006 · N605AL · Doug DC873F · Fuselage Main, BulkheadSDR IXXA06SMN253SSkin · nickedDURING ROUTINE C-CHECK INSPECTION FOUND LT WING OB FLAP LOWER SKIN TRAILING EDGE SKIN NICKED BETWEEN STATIONS XF415.000 AND XF435.000. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN (AL 2024 T3 0.025”) AND DOUBLER (AL 2024 T3 0.020”). BONDED BOTH PARTS WITH HYSOL. Jul 28, 2006 · N605AL · Doug DC873F · Leading Edge DevicesSDR IXXA06SMN252SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND LT WING IB LEADING EDGE UPPER SKIN WITH CORROSION AROUND FASTENERS FROM STA XFS7.500 TO STA XFS13.750. REMOVED CORROSION, FOUND OUT OF LIMITS FABRICATED REPAIR DOUBLER (AL 7075 T6 0.125”). CLEANED, TREATED AND PRIMED ARJul 28, 2006 · N605AL · Doug DC873F · Wing, Plate/SkinSDR IXXA06SMN251SSkin · misrepairedDURING ROUTINE C-CHECK INSPECTION FOUND RIGHT HAND INBOARD AILERON LOWER SKIN HAS NON STANDARD REPAIR BETWEEN STATIONS XA 578.000 AND XA 603.000. REMOVED SKIN WITH NON STANDARD REPAIR. FABRICATED NEW SKIN (AL 2024 T3 0.025) AND DOUBLER (AL 2024 T3 0.020). BJul 28, 2006 · N605AL · Doug DC873F · AileronsSDR IXXA06SMN250SSkin · crackedDURING ROUTINE C-CHECK INSPECTION, FOUND LT WING UPPER SKIN CRACKED, AT STATION 69.500. REMOVED FASTENERS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION, NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVED. FABRICATED DOUBLER, FILLER, HEAT TREATED DOUBLER. CLEAJul 28, 2006 · N605AL · Doug DC873F · Wing, Plate/SkinSDR IXXA06SMN245SSkin · damagedDURING ROUTINE C-CHECK INSPECTION FOUND RT WING CENTER LEADING EDGE OB SLOT UPPER SKIN HOLES ELONGATED AT STATION XOLDI6.225. REMOVED FASTENERS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVAL. FABRICATED REPAIJul 28, 2006 · N605AL · Doug DC873F · Wing, Plate/SkinSDR IXXA06SMN244SSkin · misrepairedDURING ROUTINE C-CHECK INSPECTION FOUND RT WING CENTER LEADING EDGE OB SLOT UPPER SKIN WITH NON STANDARD REPAIR AT STA XS520.168. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION, NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVED. FABRIJul 28, 2006 · N605AL · Doug DC873F · Wing, Plate/SkinSDR IXXA06SMN265SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION FOUND RIGHT HAND ELEVATOR LOWER SKIN WITH NON STANDARD REPAIR AT STATION XE39.188. REMOVED FASTENERS IAW SRM 51-1-21. REMOVED DAMAGED AREA. FABRICATED NEW REPAIR, AND FILLERS (AL 2024 T3 0.016”) IAW SRM 55-2-1 FIG. 11 (SHEET 4Jul 28, 2006 · N605AL · Doug DC873F · Elevator, Plate/SkinSDR IXXA06SMN259SSkin · dentedDURING ROUTINE C-CHECK INSPECTION FOUND LEFT HAND OUTER WING, OUTBOARD LEADING EDGE DENTED, FROM STATION XFS 885.000 TO STATION XFS 920.000. REMOVED DAMAGED SKIN IAW DC-8 SRM 57-1-0 PAGE 1, DC-8 SRM 51-1-21, DC-8 SRM 51-3-0. FABRICATED SKIN (AL 7075 T6 0.050Jul 28, 2006 · N605AL · Doug DC873F · Wing, Plate/SkinSDR IXXA06SMN258SFrame · crackedDURING ROUTINE C-CHECK INSPECTION FOUND FRAME CRACKED AT STATION 55.000, LONGERON 24 RIGHT. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21 (XFS 591.250). REMOVED CORROSION (XFS 566.250 – XFS 578.750) IAW SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW SRMJul 28, 2006 · N605AL · Doug DC873F · Fuselage Main, FrameSDR IXXA06SMN257SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND LT WING OB LEADING EDGE LOWER SKIN CORRODED FROM STA XFS566.250 TO STA XFS578.750. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21 (XFS591.250). REMOVED CORROSION IAW SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW SRM 5Jul 28, 2006 · N605AL · Doug DC873F · Wing, Plate/SkinSDR IXXA06SMN254SSkin · nickedDURING ROUTINE C CHECK INSPECTION FOUND LT WING IB FLAP UPPER SKIN REPAIR NICKED AT STATION XW104.000. REMOVED DAMAGED SKIN IAW SRM 51-1-0 PAGE 1, SRM 51-1-21. FABRICATED NEW SKIN (AL 2024 T3 0.040”) CLEANED, TREATED AND PRIMED AREA AND SKIN INTERNAL SURFACEJul 28, 2006 · N605AL · Doug DC873F · Trailing Edge FlapsSDR IXXA06SMN247SPanel · dentedDURING ROUTINE C CHECK INSPECTION, FOUND LT WING IB UPPER PANEL DENTED, AT STATION XW40.000. REMOVED DAMAGED SKIN IAW SRM 57-1-0 PAGE 1, SRM 51-1-21. FABRICATED SKIN WITH (AL 2024 T3 0.025) AND BONDED DOUBLER (AL 2024 T3 0.020) IAW SRM 57-7-1 FIG. 1 ITEM A, Jul 28, 2006 · N605AL · Doug DC873F · Wing, Plate/SkinSDR IXXA06SMN272SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND EXTERNAL FUSELAGE SKIN CORRODED AT STATION 902.000 LONGERON 13 RIGHT. REMOVED FASTENERS IAW DC-8 SRM 51-1-21, DC-8 SRM 51-3-0. REMOVED CORROSION IAW DC-8 SRM 51-1-8 PAGES 17-18 FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0 PJul 28, 2006 · N605AL · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA06SMN263SSkin · misrepairedDURING ROUTINE C-CHECK INSPECTION FOUND LEFT HAND WING CENTER LEADING EDGE UPPER SKIN WITH NON STANDARD REPAIR FROM STATION XFS 360.250 TO STATION XFS 410.250. REMOVED EXISTING REPAIR IAW DC-8 SRM 51-1-20D. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER (AJul 28, 2006 · N605AL · Doug DC873F · Wing, Plate/SkinSDR IXXA06SMN262SRepair · misrepairedDURING ROUTINE C-CHECK INSPECTION FOUND LEFT HAND WING INBOARD LEADING EDGE UPPER SKIN WITH A NON STANDARD REPAIR AT STATION XCW69.00. REMOVED EXISTING REPAIR, IAW DC-8 SRM 51-1-21, DC-8 SRM 51-3-0. FABRICATED REPAIR DOUBLER (AL 7075 T6 0.071) IAW SEMAN DRAWJul 28, 2006 · N605AL · Doug DC873F · Wing, Plate/SkinSDR IXXA06SMN261SSkin · crackedDURING ROUTINE C-CHECK INSPECTION FOUND LEFT HAND PASSENGER DOOR LOWER AREA CRACKED AT STATION 35.000. REMOVED FASTENERS IAW DC-8 SRM 51-1-21, REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER AND FILLER (AL 7075 T6 0.050”) IAW DC-8 SRM 52-2-0 FIG 4, (SHEET 3)Jul 28, 2006 · N605AL · Doug DC873F · Passenger/Crew DoorsSDR IXXA06SMN255SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND RIGHT HAND WING INBOARD LEADING EDGE UPPER SKIN CORRODED FROM STATION XW5.000 TO STATION XW22.000. REMOVED FASTENERS IAW DC-8 SRM 51-1-21, DC-8 SRM 51-3-0. REMOVED CORROSION IAW DC-8 SRM 1-1-8 FOUND OUT OF LIMITS. REMJul 28, 2006 · N605AL · Doug DC873F · Wing, Plate/SkinSDR IXXA06SMN249SSkin · misrepairedDURING ROUTINE C-CHECK INSPECTION FOUND RIGHT HAND WING OUTBOARD LEADING EDGE INTERNAL SURFACE UPPER SKIN WITH A NON STANDARD REPAIR FROM STATION XFS 560.000 TO STATION XFS 622.500. REMOVED EXISTING REPAIR IAW DC-8 SRM 57-1-0 PAGE 1, DC-8 SRM 51-1-21. FABRICJul 28, 2006 · N605AL · Doug DC873F · Wing, Plate/SkinSDR IXXA06SMN248SSkin · nickedDURING ROUTINE C-CHECK INSPECTION FOUND LEFT HAND WING OUTBOARD FLAP LOWER SKIN NICKED FROM STATION XF 415.000 TO STATION XF 425.000. REMOVED DAMAGED SKIN IAW DC-8 SRM 57-1-0 PAGE 1, DC-8 SRM 51-1-21. FABRICATED NEW SKIN (AL 2024 T3 0.032”) AND DOUBLER (AL 2Jul 28, 2006 · N605AL · Doug DC873F · Trailing Edge Flaps
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