Douglas DC-8-72

Service difficulty reports · 201

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'DC872'
  ORDER BY difficulty_date DESC"

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SDR IXXA05RNG086SSkin · corrodedDURING INSPECTION CHECK, FOUND CORROSION ON LOWER CARGO DOOR AFT JAMB STA 560 LONGERON 25 TO 33 RT. CORROSION WAS REMOVED IAW DC8 SRM 51-1-8 PAGE 20, THICKNESS MEASUREMENT WAS PERFORMED IAW ASTM 797-0 AND IT WAS FOUND OUT OF LIMITS IAW SRM 53-2-0 PAGE 2P. DASep 28, 2005 · N721CX · Doug DC872 · Fuselage Main, Plate/SkinSDR IXXA05RNG082SSkin · corrodedDURING INSPECTION CHECK, CORROSION WAS FOUND ON LOWER SKIN STA 1530-1536 LONGERON 31RH-31LH.CORROSION WAS REMOVED IAW SRM 51-1-8 PAGE 20, THICKNESS WAS MEASURED IAW ASTME 767-01 AND IT WAS FOUND OUT OF LIMITS. DAMAGE WAS REPAIRED, FABRICATION AND INSTALLATIONSep 26, 2005 · N721CX · Doug DC872 · Fuselage Main, Plate/SkinSDR IXXA05RNG117SSkin · corrodedDURING INSPECTION CHECK WAS FOUND A CORROSION AND BONDED DOUBLERS IN LT OB AILERON UPPER INNER SKIN, STA XA 621 TO XA 724. UPPER SKIN IN LT OB AILERON WAS FABRICATED AND INSTALLED IAW MFG DRAWING 5763133, AND RIVETS WERE INSTALLED IAW SRM 51-1-21 PAGE 1-7.Sep 26, 2005 · N721CX · Doug DC872 · Wing, Plate/SkinSDR IXXA05RNG087SSkin · corrodedDURING INSPECTION CHECK, FOUND A CORROSION ON FORMER STA 1530 LONGERON 28 - RT. CORROSION WAS REMOVED IAW DC8 SRM 51-1-8 PAGE 20, THICKNESS MEASUREMENT WAS PERFORMED IAW ASTME 797-01 AND IT WAS FOUND OUT OF LIMITS. DAMAGE WAS REPAIRED IAW SRM 53-2-5 FIG 8C-1Sep 26, 2005 · N721CX · Doug DC872 · Fuselage Main, Plate/SkinSDR IXXA05RNG111SPanel · corrodedDURING INSPECTION CHECK WAS FOUND A CORROSION ON RT WING FLAP IB INTERIOR TRAILING EDGE PANEL PLATING. SKIN WAS REPLACED IAW MFG DRAWING 5652277 AND RIVETS WERE INSTALLED IAW SRM 51-1-21 PAGE 1-7.Sep 25, 2005 · N721CX · Doug DC872 · Trailing Edge FlapsSDR IXXA05RNG110SSkin · corrodedDURING INSPECTION CHECK WAS FOUND A CORROSION AND BONDED DOUBLER DELAMINATED ON LT WING INTERIOR UPPER SURFACE T/E, STA XW 700 - XW 736.500.SKIN WAS REPLACED IAW MFG DRAWING 5644654, RIVETS WERE INSTALLED IAW SRM 51-1-21 PAGE 1-7 AND ANTI-CORROSIVE TREATMENT WSep 24, 2005 · N721CX · Doug DC872 · Wing, Plate/SkinSDR IXXA05RNG095SRivet · looseDURING INSPECTION CHECK, A LOOSE RIVET WAS FOUND ON MAIN CARGO DOOR SKIN BETWEEN STA 420-440-LT. AS TEMPORARY REPAIR BLIND RIVETS WILL BE INSTALLED IAW BOEING MESSAGE 1-136637626 AND EWO ATI 52-004. SOLID RIVETS OR HI-LOCKS MUST BE INSTALLED WITHIN 6000 CYCLSep 24, 2005 · N721CX · Doug DC872 · Cargo/Baggage DoorsSDR IXXA05RNG069SPlate · temporaryDURING INSPECTION CHECK, FOUND AN INTERIM REPAIR ON INBOARD FLAP UPPER FWD PLATING BETWEEN STA XW91-80, RT. EXISTING DOUBLER WAS REMOVED AND A NEW REINFORCEMENT DOUBLER WAS INSTALLED IAW EO ATI-091105 AND EWO ATI 57-047.Sep 24, 2005 · N721CX · Doug DC872 · Wing Miscellaneous StructureSDR IXXA05RNG074SSkin · corrodedDURING INSPECTION CHECK, FOUND CORROSION ON INTERNAL SKIN OF PASSENGER WINDOW STA 360 AND 380 LH. CORRODED AREA WAS REMOVED AND REPAIR DOUBLER WAS INSTALLED IAW EWO ATI 53-024, SRM 53-2-0 FIGURE 22A AND BOEING SERVICE REQUEST 1-129925991.Sep 24, 2005 · N721CX · Doug DC872 · Fuselage Main, Plate/SkinSDR IXXA05RNG109SSkin · corrodedDURING INSPECTION CHECK, FOUND A CORROSION ON LT INBOARD FLAP LWD EXTERIOR SURFACE. SKIN ON LT INBOARD FLAP EXTERIOR SURFACE WAS REPLACED IAW DOUGLAS DRAWING 5642960, AND RIVETS WERE INSTALLED IAW SRM 51-1-21 PAGE 1-7.Sep 21, 2005 · N721CX · Doug DC872 · Trailing Edge FlapsSDR IXXA05RNG108SSkin · corrodedDURING INSPECTION CHECK, FOUND A CORROSION ON RT ELEVATOR UPPER SURFACE, STA XE 246.875-XE 272. SKIN WAS REPLACED IAW DOUGLAS DRAWING 5654970 AND RIVETS WERE INSTALLED IAW DC8 SRM 51-1-21 PAGE 1-7.Sep 17, 2005 · N721CX · Doug DC872 · Elevator, Plate/SkinSDR IXXA05RNG084SSkin · corrodedDURING INSPECTION CHECK, FOUND A CORROSION ON AFT LOWER CARGO FWD DOOR SKIN, STA 1140 - RT. CORROSION WAS REMOVED IAW DC8 SRM 51-1-8 PAGE 20, THICKNESS MEASUREMENT WAS PERFORMED IAW ASTME 797-01 AND IT WAS FOUND OUT OF LIMITS IAW DC8 SRM 52-2-0 PAGE 22. DAMASep 17, 2005 · N721CX · Doug DC872 · Cargo/Baggage DoorsSDR IXXA05RNG081SSkin · deformedDURING INSPECTION CHECK WAS FOUND A OIL CAN ON LOWER SURFACE SKIN STA XE 89.718 TO 108.843-LT. REPAIR DOUBLER WAS INSTALLED IAW EWO ATI 55-013 AND SRM 55-2-1 FIG 2A.Sep 16, 2005 · N721CX · Doug DC872 · Empennage StructureSDR IXXA05RNG080SSkin · deformedDURING INSPECTION CHECK WAS FOUND A OIL CAN ON LOWER SURFACE SKIN STA XE 279.125 TO 288.957 - LT. SKIN WAS REPLACED IAW DRAWING 5654970 ZONE 17 TO 21, RIVETS WERE INSTALLED IAW SRM 51-1-21 PAGE 1-7 AND PROTECTIVE TREATMENT WAS APPLIED IAW SRM 51-1-8 PAGE 13-16Sep 16, 2005 · N721CX · Doug DC872 · Empennage StructureSDR IXXA05RNG107SFairing · crackedDURING INSPECTION CHECK, FOUND A CRACK ON LT ELEVATOR LOWER SURFACE, STA XE 149.000. FAIRING WAS FABRICATED AND REPLACED IAW DOUGLAS DRAWING 5655694 VIEW C-C, AND RIVETS WERE INSTALLED IAW DC8 SRM 51-1-21 PAGE 1-7.Sep 16, 2005 · N721CX · Doug DC872 · Wing Miscellaneous StructureSDR IXXA05RNG067SSkin · corrodedDURING INSPECTION CHECK WAS FOUND CORROSION ON INTERNAL SKIN OF PASSENGER WINDOW STA 1120-1140, LEFT. CORRODED AREA WAS REMOVED AND REPAIR DOUBLER WAS INSTALLED IAW EWO ATI-53-021 AND SRM 53-2-0 FIGURE 22A, TR 53-170.Sep 16, 2005 · N721CX · Doug DC872 · Fuselage Main, Plate/SkinSDR IXXA05RNG065SSkin · corrodedDURING INSPECTION CHECK WAS FOUND A CORROSION ON UPPER SKIN AT LEADING EDGE STA XW 408 TO 454, LT.CORROSION ON UPPER SKIN AT LEADING EDGE STA XW 408 TO 454-LT WAS REPAIRED IAW SRM 57-2-1 FIGURE 38 AND EWO ATI 57-043.Sep 16, 2005 · N721CX · Doug DC872 · Wing, Plate/SkinSDR IXXA05RNG075SDoubler · corrodedDURING INSPECTION CHECK WAS FOUND A CORROSION ON DOUBLER AT LEADING EDGE OB SLOT UPPER DOOR LT. CORRODED DOUBLER WAS REMOVED AND NEW REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-2-1 FIG 12 AND EWO ATI-57-050.Sep 15, 2005 · N721CX · Doug DC872 · Leading Edge DevicesSDR IXXA05RNG063SSkin · misrepairedDURING INSPECTION CHECK, FOUND A IMPROPER REPAIR ON FUSELAGE SKIN LOWER DOOR JAMB STA 340-360, LT. DAMAGE WILL BE REPAIRED IAW EWO ATI-53-016 AND FAA FORM 8110-3 MUST BE ISSUED.Sep 15, 2005 · N721CX · Doug DC872 · Fuselage Main, Plate/SkinSDR IXXA05RNG076SSkin · corrodedDURING INSPECTION CHECK, CORROSION WAS FOUND ON LOWER SKIN STA 208-270 LONGERON 32RH-32 LT. CORROSION WAS REMOVED IAW SRM 51-1-8 PAGE 20, THICKNESS WAS MEASURED IAW ASTME 79701 AND IT WAS FOUND OUT OF LIMITS IAW SRM 53-2-0 PAGE2P. SKIN WAS REPLACED IAW DRAWINGSep 14, 2005 · N721CX · Doug DC872 · Fuselage Main, Plate/SkinSDR IXXA05RNG071SSkin · corrodedDURING INSPECTION CHECK, FOUND A CORROSION ON INNER SKIN STA 1440-1460, LONGERON 22 - RT. CORROSION WAS REMOVED IAW DC8 SRM 51-1-8 PAGE 20, THICKNESS MEASUREMENT WAS PERFORMED IAW ASTM 797-01, AND IT WAS FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0 PAGE 2P. DAMAGESep 14, 2005 · N721CX · Doug DC872 · Fuselage Main, Plate/SkinSDR IXXA05RNG106SSkin · corrodedDURING INSPECTION CHECK, FOUND TWO IMPROPER PATCHES AND CORROSION ON RT WING INBOARD FLAP TOP SURFACE, STA XW 31 - XW 92. SKIN ON RT WING INBOARD FLAP WAS REPLACED IAW DOUGLAS DRAWING 5642960 AND RIVETS WERE INSTALLED IAW DC8 SRM 51-1-21 PAGE 1-7.Sep 13, 2005 · N721CX · Doug DC872 · Wing, Plate/SkinSDR IXXA05RNG085SSkin · chafedDURING INSPECTION CHECK, FOUND CHAFING ON CENTER SECTION AT WHEEL WELL VERTICAL WEB, AROUND STA 1060 LH. CHAFING DAMAGE WAS REMOVED, NEW WEB SEGMENT AND REPAIR DOUBLER STRAP WERE INSTALLED IAW EO ATI-091705 AND EWO ATI-53-029. FAA FORM 8110-3 WAS ISSUED APPRSep 13, 2005 · N721CX · Doug DC872 · Fuselage Main, Plate/SkinSDR IXXA05RNG083SSkin · chafedDURING INSPECTION CHECK, FOUND CHAFING ON CENTER SECTION AT WHEEL WELL VERTICAL WEB, AROUND STA 1060 RT. CHAFING DAMAGE WAS TRIMMED OUT, NEW WEB SEGMENT AND REPAIR DOUBLER STRAP WERE INSTALLED IAW EO ATI-091405 AND EWO ATI-53-025.Sep 13, 2005 · N721CX · Doug DC872 · Fuselage Main, Plate/SkinSDR IXXA05RNG072SSkin · corrodedDURING INSPECTION CHECK WAS FOUND A CORROSION ON RT INBOARD FLAP EXTERIOR SURFACE, BETWEEN STA XW3-XW92 (VIEW LOOKING UP). RT WING INBOARD FLAP SKIN WAS REMOVED AND REPLACED IAW DOUGLAS DRAWING 5642960. RIVETS WERE INSTALLED IAW DC8 SRM 51-1-21 PAGE 1 TO 7.Sep 13, 2005 · N721CX · Doug DC872 · Trailing Edge FlapsSDR IXXA05RNG064SSkin · misrepairedDURING INSPECTION CHECK, FOUND A IMPROPER REPAIR ON FUSELAGE SKIN STA 1500-1530, LONG 17-21, LT. DAMAGE WILL BE REPAIRED IAW EWO ATI-53-017 AND FAA FORM 8110-3 MUST BE ISSUED.Sep 13, 2005 · N721CX · Doug DC872 · Fuselage Main, Plate/SkinSDR IXXA05RNG062SSkin · corrodedDURING INSPECTION CHECK, FOUND A CORROSION ON INTERNAL SKIN OF PASSENGER WINDOW STA 1160-1180, LT. DAMAGE WILL BE REPAIRED IAW EWO ATI-53-020 AND SRM 53-2-0 FIGURE 22A, TR-53-170.Sep 12, 2005 · N721CX · Doug DC872 · Fuselage Main, Plate/SkinSDR IXXA05RNG061SSkin · corrodedDURING INSPECTION CHECK, FOUND A CORROSION ON INTERNAL SKIN OF PASSENGER WINDOW STA 560-580, LT. DAMAGE WILL BE REPAIRED IAW EWO ATI-53-019 AND SRM 53-2-0 FIGURE 22A TR 53-170.Sep 12, 2005 · N721CX · Doug DC872 · Fuselage Main, Plate/SkinSDR IXXA05RNG060SSkin · corrodedDURING INSPECTION CHECK, FOUND A CORROSION ON INTERNAL SKIN OF PASSENGER WINDOW STA 640-660, RT. DAMAGE WILL BE REPAIRED IAW EWO ATI-53-018 AND SRM 53-2-0 FIGURE 22A TR-53-170.Sep 12, 2005 · N721CX · Doug DC872 · Fuselage Main, Plate/SkinSDR IXXA05RNG105SSkin · corrodedDURING INSPECTION CHECK, FOUND CORROSION ON LT RUDDER STA´S ZR 335.250, ZR 327 - 319, ZR 310.688, ZR 300 - 290. SKIN WAS REMOVED AND REPLACED IAW DOUGLAS DRAWING 5655077 VIEW A-B&C AND RIVETS WERE INSTALLED IAW DC8 SRM 51-1-21 PAGE 1-7.Sep 10, 2005 · N721CX · Doug DC872 · Rudder, Plate/SkinSDR IXXA05RNG104SSkin · corrodedDURING INSPECTION CHECK, FOUND A CORROSION ON LT WING OUTBOARD AILERON LWD SKIN, STA XW 565 TO XA 638. SKIN IN LT WING OUTBOARD AILERON WAS REMOVED AND REPLACED IAW DRAWING 5763133 AND RIVETS WERE INSTALLED IAW DC8 SRM 51-1-21 PAGE 1-7.Sep 10, 2005 · N721CX · Doug DC872 · Wing, Plate/SkinSDR IXXA05RNG078SSkin · corrodedDURING INSPECTION CHECK, FOUND CORROSION ON RT HORIZONTAL STABILIZER UPPER PLATING AT OUTBOARD CENTER SECTION AROUND STA XE 173.656 BETWEEN AUXILIARY AND AFT UPPER SPAR CAP. CORRODED AREA WAS BLEND OUT AND REPAIR DOUBLER WAS INSTALLED IAW EO ATI 091505 AND EWSep 10, 2005 · N721CX · Doug DC872 · Horizontal Stabilizer, Plate/SkinSDR IXXA05RNG077SPlate · corrodedDURING INSPECTION CHECK,CORROSION WAS FOUND ON STABILIZER UPPER TRAILING EDGE PLATING STA XE 28-RH. REPAIR ACCOMPLISHED, REMOVAL PANEL AND STIFFENER, FABRICATION AND INSTALLATION NEW PANEL AND STIFFENER IAW DRAWINGS 55-05467-1, 55-05467-2, 55-05467-3, 55-05467Sep 9, 2005 · N721CX · Doug DC872 · Horizontal Stabilizer, Plate/SkinSDR IXXA05RNG066SDoubler · improperDURING INSPECTION CHECK, FOUND IMPROPER REPAIR ON RT HORIZONTAL STABILIZER L/E DOUBLER STA XFS 210-222.500. EXISTING DOUBLER WAS REMOVED AND A NEW REINFORCEMENT DOUBLER WAS INSTALLED IAW EO ATI 090805 AND EWO ATI-55-006.Sep 9, 2005 · N721CX · Doug DC872 · Horizontal Stabilizer, Plate/SkinSDR IXXA05RNG073SSkin · misrepairedDURING INSPECTION CHECK WAS FOUND A IMPROPER REPAIR ON WING LEADING EDGE, STA XW 257.50, RT. PERMANENT REPAIR WAS PERFORMED IAW EWO ATI 57-044 AND EO ATI-090905. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.Sep 9, 2005 · N721CX · Doug DC872 · Wing, Plate/SkinSDR IXXA05RNG102SPlate · crackedDURING INSPECTION CHECK, FOUND A CRACK ON CENTER L/E SLOT DOOR PLATING AROUND STA XFS 510.222-LT. DAMAGE WAS REPAIRED IAW EO ATI-092705 AND EWO ATI 57-052.Sep 8, 2005 · N721CX · Doug DC872 · Wing Miscellaneous StructureSDR IXXA05RNG101SSkin · unbondedDURING INSPECTION CHECK, FOUND LT WING UPPER SKIN PANEL AT STA XW 761.695 DISBONDED. SKIN WAS REMOVED AND REPLACED ON LT WING UPPER PANEL IAW DOUGLAS DRAWING 5644654, RIVETS WERE INSTALLED IAW DC8 SRM 51-1-21 PAGE 1-7 AND PROTECTIVE TREATMENT WAS APPLIED IAW Sep 8, 2005 · N721CX · Doug DC872 · Wing, Plate/SkinSDR IXXA05RNG059SFitting · crackedDURING INSPECTION CHECK WAS FOUND RT OUTBOARD FLAP, INBOARD FLAP HINGE FITTING AT STA XF339.7332 CRACKED. DAMAGE WILL BE REPAIRED IAW EWO ATI-57-042 AND FAA FORM 8110-3 MUST BE ISSUED APPROVING THIS REPAIR.Sep 8, 2005 · N721CX · Doug DC872 · Trailing Edge FlapsSDR IXAA05RNG058SFitting · crackedDURING MAINTENANCE CHECK, FOUND RT OUTBOARD FLAP, INBOARD FLAP HINGE FITTING STA XF 219.459 CRACKED. DAMAGE WILL BE REPAIRED IAW EWO ATI-57-041 AND FAA FORM 8110-3 MUST BE ISSUED APPROVING THIS REPAIR.Sep 8, 2005 · N721CX · Doug DC872 · Wing, Control Surface Attach FittingsSDR IXXA05RNG079SSkin · deformedDURING INSPECTION CHECK WAS FOUND A OIL CAN ON LOWER SURFACE SKIN STA XE 104.051 TO 108.815 - LT. REPAIR SKIN AND REPAIR SPLICE WERE FABRICATED AND INSTALLED IAW SRM 55-2-1 FIG 2A AND EWO ATI 55-011.Sep 7, 2005 · N721CX · Doug DC872 · Empennage StructureSDR IXXA05RNG103SSkin · corrodedDURING INSPECTION CHECK, FOUND A CORROSION ON LT WING EXTERIOR LWD SURFACE, REAR SPAR BETWEEN STA XW 736.500 - XW 761.0 AND STA XRS 700.000 - XW 736.000. SKIN WAS REMOVED AND REPLACED IAW DOUGLAS DRAWING 5644654, RIVETS WERE INSTALLED IAW DC8 SRM 51-1-21 PAGESep 7, 2005 · N721CX · Doug DC872 · Wing, Plate/SkinSDR IXXA05RNG070SSkin · corrodedDURING INSPECTION CHECK, FOUND CORROSION ON LH HORIZONTAL STABILIZER LOWER SURFACE SKIN, STATION XE 235. BLEND OUT IN CORRODED AREA WAS PERFORMED AND REPAIR DOUBLER WAS INSTALLED IAW EO ATI-091305 AND EWO ATI 55-007. FAA FORM 8110-3 WAS ISSUED APPROVING THISSep 7, 2005 · N721CX · Doug DC872 · Horizontal Stabilizer, Plate/SkinSDR IXXA05RNG053STail Cone · dentedDURING INSPECTION CHECK, FOUND SOME DENTS ON LT FUSELAGE TAIL CONE STA`S 1746, 1745 AND 1754. SKIN DENTS WILL BE REPAIRED IAW EWO ATI-53-013 AND FAA FORM 8110-3 MUST BE ISSUED APPROVING THIS REPAIR.Sep 7, 2005 · N721CX · Doug DC872 · Aerodynamic FairingsSDR IXXA05RNG054SSkin · crackedDURING INSPECTION CHECK, FOUND A CRACK (1.5 INCHES) ON TOP PANEL PLATING OUTBOARD OF STA XCW 69.5 AND STRINGER 1 RT. DAMAGE WILL BE REPAIRED IAW EWO ATI 57-039 AND SRM 57-2-1 FIG 18A.Sep 7, 2005 · N721CX · Doug DC872 · Wing, Plate/SkinSDR IXXA05RNG051SSkin · misrepairedDURING INSPECTION CHECK, FOUND A IMPROPER REPAIR ON SKIN STA 460 LONGERON 28-29 RT. PERMANENT REPAIR WILL BE MADE IAW SRM 53-2-1 FIGURE 7 AND EWO ATI-53-012. THIS REPAIR CONSTITUTES A MAJOR REPAIR.Sep 7, 2005 · N721CX · Doug DC872 · Fuselage Main, Plate/SkinSDR IXXA05RNG068SSkin · corrodedDURING INSPECTION CHECK WAS FOUND A CORROSION ON WING UPPER SKIN STA XRS 40.869 REAR SPAR TO AUX SPAR - LT. REPORTED AREA WAS BLENDED OUT AND REINFORCEMENT DOUBLER WAS FABRICATED AND INSTALLED IAW EO ATI-091005 AND EWO ATI 57-045. FAA FORM 8110-3 WAS ISSUED ASep 6, 2005 · N721CX · Doug DC872 · Wing, Plate/SkinSDR IXXA05RNG050SDoubler · misrepairedDURING INSPECTION CHECK WAS FOUND A TEMPORAL REPAIR ON SKIN STA 235 LONGERON 24-25-LT. DAMAGE WILL BE REPAIRED IAW EWO ATI-53-011 AND SRM 53-2-1 FIGURE 7. THIS REPAIR CONSTITUTES A MAJOR REPAIR.Sep 6, 2005 · N721CX · Doug DC872 · Fuselage Main, Plate/SkinSDR IXXA05RNG057SSkin · crackedDURING INSPECTION CHECK, FOUND A CRACK ON TOP PANEL PLATING AT CENTER SPAR AND STA XRS 74.869 LT. DAMAGE WILL BE REPAIRED IAW EWO ATI 57-040 AND SRM 57-2-1 FIG 17.Sep 6, 2005 · N721CX · Doug DC872 · Wing, Plate/SkinSDR IXXA05RNG056SFitting · crackedDURING INSPECTION CHECK, FOUND A CRACKED FITTING LONGERON 24 STA 857.125 BATH TUB RT. REPAIR WILL BE MADE IAW EWO ATI 53-015 AND SRM 53-2-2 FIGURE 5, TEMPORARY REVISION 53-123.Sep 4, 2005 · N721CX · Doug DC872 · Fuselage Main, Attach FittingsSDR IXXA05RNG052SSkin · corrodedDURING INSPECTION CHECK, FOUND STRESS CORROSION CRACK ON RT WING UPPER EXTERIOR SURFACE STA XRS74 STRINGERS 9 TO 15. DAMAGE WILL BE REPAIRED IAW EWO ATI 57-038 AND FAA FORM 8110-3 MUST BE ISSUED APPROVING THIS REPAIR.Sep 4, 2005 · N721CX · Doug DC872 · Wing, Plate/Skin
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