N33785

Part: FRAME — BENT (BS 640)

INSPECTION FOUND FRAME BENT AT FS 640 BETWEEN LONGERON 26 AND 27R. THE FRAME WAS REPAIRED IAW EA 27-5311-2-A0538 AND ECRA 5310-03968.

Part: SUPPORT — CORRODED (FUSELAGE)

INSPECTION FOUND RT AFT LAV FORWARD WALL FLOOR SUPPORT CORRODED. A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-2, 51-30-2, AND MM 51-20-0.

Part: FLOORBEAM — CORRODED (BS 1130)

INSPECTION FOUND FLOORBEAM CORRODED ON UPPER T-CHORD AT STA 1130, BL 0 TO O/B RT SIDE. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-03965 AND EA 27-5310-2-A0548.

Part: ANGLE — CORRODED (BS 643)

INSPECTION FOUND FORWARD CARGO FLOOR SUPPORT ANGLE CORRODED UNDER NUTPLATES AT STA 643, LBL 9. THE CORRODED SECTION OF FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT AND ANGLES WERE INSTALLED IAW SRM 51-40-4 AND 51-30-2.

Part: SUPPORT — BENT (BS 650)

INSPECTION FOUND FORWARD CARGO FLOOR SUPPORT BENT AT STA 650, LBL 3. THE BENT SECTION WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 51-40-4, FIGURE 1.

Part: SUPPORT — CORRODED (BS 643)

INSPECTION FOUND FORWARD CARGO FLOOR SUPPORT ANGLE CORRODED UNDER NUTPLATE AT FS 643, LBL 13. THE FLOOR SUPPORT ANGLE WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-30-2, 51-10-2, 51-40-4, AND MM 51-20-0.

Part: WEB — CRACKED (BS 1188)

INSPECTION FOUND A 4 INCH CRACK IN CUSP WEB AT TOP OF BULKHEAD AT VERTICAL SUPPORT, FS 1188, RBL 20. THE CUSP WEB WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: FRAME — CRACKED (BS 880)

INSPECTION FOUND A 2 INCH CRACK IN FRAME AT FS 880 BETWEEN STRINGER 18R AND 17R. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A REPAIR ANGLE WAS INSTALLED IAW SRM 51-30-2 AND 51-40-3, FIGURE 1.

Part: DOOR PAN — CRACKED (PAX DOOR)

INSPECTION FOUND A 1 INCH CRACK IN L-2 CABIN DOOR AT UPPER PAN AREA NEAR HINGE FITTING. THE AREA WAS REPAIRED IAW SRM 51-40-2.

Part: PANEL — CORRODED (SPOILER)

INSPECTION FOUND LT WING NR 6 SPOILER PANEL UPPER SURFACE CORRODED. THE SPOILER PANEL WAS REMOVED, REPAIRED, AND REINSTALLED IAW SRM 57-50-6 AND MM 27-62-1.

Part: ANGLE — CRACKED (BS 113 0)

INSPECTION FOUND A 3 INCH CRACK IN RT FLOOR SUPPORT ANGLE AT CUSP WEB, FS 1130, STRINGER 17R. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-0.

Part: SEAT TRACK — CORRODED (BS 1110 - 1130)

INSPECTION FOUND SEAT TRACK CORRODED AT FS 1110-1130, RBL 22. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-10-2, 51-30-2, AND MM 51-20-0.

Part: FLOORBEAM — CORRODED (BS 1166)

INSPECTION FOUND FLOORBEAM UPPER T-CHORD CORRODED AT STA 1166, BL O TO O/B RT SIDE. THE CORROSION WAS REMOVED IAW SRM 51-10-6. AN ANGLE REPAIR WAS INSTALLED IAW ECRA 5310-03961.

Part: BULKHEAD — CRACKED (BS 1183)

INSPECTION FOUND A 4 CRACK IN WEB AT AFT PRESSURE BULKHEAD STA 1183, STRINGER 2L FITTING. THE CRACK WAS STOP DRILLED IAW ECRA 5310-03958 AND A DIP WAS ISSUED TO REINSPECT THE REPAIR EVERY 3000 CYCLES.

Part: FAIRING SUPPORT — CORRODED (BS 720F)

INSPECTION FOUND RT LOWER BODY FAIRING 3441 SUPPORT NR 7 CORRODED AT STA 720F, S26R. THE CORROSION WAS REMOVED IAW SRM 51-10-6. A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-2 AND 51-30-2.

Part: FLOORBEAM — CORRODED (BS 380 - 400)

INSPECTION FOUND FLOORBOARD SUPPORT CORRODED AT STA 380-400, RBL 15. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2.

Part: SUPPORT — CRACKED (BS 600)

INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT FS 600, LBL 12. THE CRACK WAS STOP DRILLED AND REPAIR PARTS WERE INSTALLED IAW SRM 51-40-4.

Part: FRAME — CORRODED (BS 1070)

INSPECTION FOUND FRAME CORRODED ON TOP LEG IN AFT CARGO AREA AT STA 1070, S27R. THE CORRODED DOUBLER, GUSSET, AND STIFFENER WERE REMOVED IAW SRM 51-30-2. A NEW DOUBLER, GUSSET, AND STIFFENER WERE INSTALLED IAW SRM 51-30-2.

Part: RIB — CRACKED (NLG DOOR)

INSPECTION FOUND A 1 INCH CRACK IN RADIUS OF RIB AT RT FORWARD NLG DOOR FORWARD UPPER EDGE, SIX INCHES BELOW THE DOOR LATCH. THE RIB WAS REMOVED AND A NEW RIB WAS INSTALLED IAW SRM 51-10, FIGURE 1, 52-10-2, 51-30-1, AND MM 51-20-0.

Part: SKIN — CRACKED (NR 2 ENG COWL)

INSPECTION FOUND A 2 INCH CRACK IN UPPER FORWARD CORNER SKIN OF LT AFT NR 2 ENGINE COWL. THE CRACKED AREA WAS CUT OUT, A DOUBLER AND FILLER WERE INSTALLED IAW SRM 54-30-3, 51-10-2, AND 51-30-2.

Part: SUPPORT — CORRODED (BS 420 - 440)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 420-440, RBL 18. THE FLOOR SUPPORT WAS REMOVED AND A NEW PART WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-0.

Part: HINGE — CRACKED (AILERON)

INSPECTION FOUND A .5 INCH CRACK IN CENTER HINGE BRACKET OF RT WING I/B AILERON TAB. THE HINGE WAS REMOVED AND REPLACED IAW SRM 57-50-01.

Part: LONGERON — CORRODED (BS 560 - 600)

INSPECTION FOUND LONGERON 20L CORRODED AT FS 560-600. REPAIR ANGLES WERE INSTALLED IAW SRM 53-10-3, FIGURE 2, 51-10-2, AND 51-20-3.

Part: SUPPORT — CORRODED (BS 1148)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1148, BL 0. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-1 AND 51-10-2.

Part: FLOOR PANEL — CORRODED (BS 290 - 300)

INSPECTION FOUND BLUE WATER STAINS AND CORROSION ON FLOOR PANEL AT STA 290-300. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-10-4, PAGE 4, 51-10-2, AND MM 51-20-0.

Part: SUPPORT — CORRODED (BS 1075)

INSPECTION FOUND AFT CARGO FLOOR SUPPORT CORRODED AT FS 1075, RBL 12. THE CORRODED AREA WAS CUT OUT, NEW PARTS AND NUT PLATES WERE INSTALLED IAW SRM 51-40-4, 51-30-1, 51-10-2, 51-20-0, AND 51-20-4.

Part: SUPPORT — CORRODED (BS 312 - 344)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 312-344, LBL 30. THE UPPER STRAP OF FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT STRAP WAS INSTALLED IAW SRM 51-30-2 AND 53-10-2.

Part: SKIN — GOUGED (BS 348)

INSPECTION FOUND FUSELAGE SKIN GOUGED AT FS 348, S26L. THE GOUGED AREA WAS CUT OUT, REPAIR FILLER AND DOUBLER WERE INSTALLED IAW SRM 53-30-3, FIGURE 24, 51-30-2, 51-20-4.

Part: SUPPORT — CORRODED (BS 1130)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1130, RBL 24. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 53-10-1, 51-10-2, 51-30-2, AND MM 51-20-2.

Part: STIFFENER — CRACKED (PANEL 1104)

INSPECTION FOUND A 1 INCH CRACK AT EACH END OF PANEL 1104 STIFFENER. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-0.

Part: WEB — CORRODED (FUSELAGE)

INSPECTION FOUND WEB CORRODED AT AFT CARGO DOOR JAMB. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2 AND 51-20-1.

Part: STRINGER — CORRODED (BS 480)

INSPECTION FOUND STRINGER 28L CORRODED AT STA 480. THE STRINGER WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-10-3, 51-10-2, 51-30-2, AND MM 51-20-0.

Part: ANGLE — CRACKED (BS 303)

INSPECTION FOUND A 1 INCH IN COCKPIT FLOOR SUPPORT ANGLE AT FS 303, LBL 5. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-20-1.

Part: SEAT TRACK — CORRODED (BS 1030 - 1070)

INSPECTION FOUND RT O/B SEAT TRACK CORRODED FROM STA 1030-1070. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: ANGLE — CRACKED (BS 623)

INSPECTION FOUND A 2 INCH CRACK IN NUT PLATE STRIP ANGLE AT STA 623, LONGERON 23R. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2 AND 53-10-2.

Part: FLOORBEAM — CORRODED (BS 344)

INSPECTION FOUND FLOORBEAM CORRODED ON UPPER AND LOWER SURFACES AT STA 344, LBL 20 TO LBL 60. A REPAIR WAS INSTALLED IAW SRM 53-10-8, FIGURE 9.

Part: SEAT TRACK — CORRODED (BS 950B - 1030)

INSPECTION FOUND RT O/B SEAT TRACKS CORRODED AT STA 990-1030 AND 950B-970. THE SEAT TRACK SECTIONS WERE REMOVED AND REPLACED IAW SRM 51-30-2.

Part: PANEL — CORRODED (BS 950E)

INSPECTION FOUND RT TRANSITION PANEL CORRODED AT STA 950E. THE CORROSION WAS REMOVED IAW SRM 51-10-6. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-30-2, 51-10-6, AND 51-40-3.

Part: SUPPORT — CORRODED (BS 950D - 990)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 950D-990, BL 0. THE CORROSION WAS REMOVED IAW SRM 51-10-6. A REPAIR WAS INSTALLED IAW SRM 51-10-4, FIGURE 3.

Part: SUPPORT — BENT (BS 660 - 800)

INSPECTION FOUND FLOOR SUPPORT CORRODED AND BENT AT FS 660-800, BL 0. THE CORROSION WAS REMOVED IAW SRM 53-10-1. THE BENT SECTION OF FLOOR SUPPORT WAS REMOVED AND REPLACED USING SPLICES IAW SRM 51-40-2 AND 51-30-1.

Part: ANGLE — CORRODED (BS 790)

INSPECTION FOUND WEB SUPPORT ANGLE CORRODED WING CENTER SECTION FS 790 LOWER TORQUE BOX AT KEEL AREA. THE CORROSION WAS REMOVED IAW SRM 51-10-6. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, PAGE 7.

Part: PANEL — CORRODED (BS 1110 - 1166)

INSPECTION FOUND LEFT TRANSITION PANEL CORRODED AT FS 1110-1166 IN AFT PIT. THE PANEL WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: PANEL — CORRODED (VERTICAL STAB)

INSPECTION FOUND VERTICAL STABILIZER RT ACCESS PANEL NR 5216 AND STIFFENER CORRODED. A NEW PANEL AND NUT PLATES WERE INSTALLED IAW SRM 51-20-1, FIGURE 7, 51-30-2, 51-10-2, AND MM 51-20-0.

Part: WEB — CORRODED (BS 1090)

INSPECTION FOUND AFT CARGO C-3 DOOR CUTOUT FORWARD WEB LOWER SURFACE CORRODED AROUND NUT PLATES FROM STRINGER 27R TO 19R AT FS 1090. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 53-10-1, 51-20-1, AND 51-30-2.

Part: WEB — CORRODED (BS 770)

INSPECTION FOUND WEB CORRODED AT WING CENTER SECTION, FS 770 LOWER TORQUE BOX AT KEEL AREA. THE CORRODED SECTION OF WEB WAS CUT OUT AND A NEW WEB SECTION WAS INSTALLED IAW SRM 51-30-2, 51-10-2, 51-40-2, AND MM 51-20-0.

Part: FRAME — CRACKED (BS 540)

INSPECTION FOUND A .75 INCH CRACK IN FRAME AT STA 540, S27R. THE CRACKED SECTION OF FRAME WAS REMOVED AND A REPAIR DOUBLER, FRAME, AND ANGLE WERE INSTALLED IAW SRM 51-40-3, FIGURE 1 AND 51-30-2.

Part: ANGLE — CRACKED (BS 720F)

INSPECTION FOUND A .5 INCH CRACK IN INTERCOSTAL ATTACH ANGLE AT STA 720F, BL 0. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-0.

Part: WEB — CRACKED (TE FLAP)

INSPECTION FOUND A 2 INCH CRACK IN LEFT WING SLAT NR 1 O/B TRACK TO SLAT WEB. THE SLAT AND TRACK WERE REMOVED IAW MM 27-81-11. A NEW WEB, TRACK FITTING, AND LOWER SKIN WERE INSTALLED IAW SRM 51-30-2. THE SLAT AND TRACK WERE INSTALLED IAW MM 27-81-11.

Part: INTERCOSTAL — CORRODED (BS 1050 - 1070)

INSPECTION FOUND INTERCOSTAL CORRODED AT STA 1050-1070, LONGERON 27L. THE CORROSION WAS REMOVED IAW SRM 51-10-6. AN ANGLE WAS INSTALLED IAW SRM 51-40-4, 51-10-2, AND 51-30-2.

Part: SUPPORT — CRACKED (BS 760)

INSPECTION FOUND A 3 INCH CRACK IN FLOOR SUPPORT AT FS 760, RBL 3. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-30, 51-10-2, AND MM 51-20-0.

Part: FLOORBEAM — CORRODED (BS 277)

INSPECTION FOUND FLOORBEAM CORRODED AT FS 277, RBL 12. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A REPAIR WAS INSTALLED USING SUPPORT ANGLES AND STIFFENERS IAW SRM 51-30-2 AND 51-40-4, FIGURE 1.

Part: SUPPORT — CORRODED (FAIRING)

INSPECTION FOUND RT LOWER BODY FAIRING SUPPORT NR 10 CORRODED. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2.

Part: SKIN — CORRODED (FUSELAGE)

INSPECTION FOUND SKIN OF RT ACCESS PANEL AT FUSELAGE BELLY BETWEEN HEAT EXCHANGERS CORRODED WITH PULLED RIVETS. THE SKIN WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-10-2.

Part: SUPPORT — CRACKED (BS 848)

INSPECTION FOUND A 1 INCH CRACK ON EACH END OF FLOOR SUPPORT AT STA 848, BL 0 AND LBL 25. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2.

Part: FITTING — CORRODED (CARGO DOOR)

INSPECTION FOUND C1 CARGO DOOR LOWER FORWARD SILL FITTING CORRODED. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 950 - 1038)

INSPECTION FOUND LT O/B SEAT TRACK CORRODED FROM STA 950-1038. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-2, 51-30-2.

Part: SKIN — CRACKED (MLG DOOR)

INSPECTION FOUND A 3 INCH CRACK IN LEFT MLG O/B DOOR SKIN INNER SURFACE. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-40-2.

Part: SHEAR TIE — CORRODED (BS 480)

INSPECTION FOUND SHEAR TIE CORRODED AT STA 480, LONGERON 27R-27L. THE SHEAR TIE WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-10-4, FIGURE 12.

Part: ANGLE — CORRODED (BS 380 - 420)

INSPECTION FOUND R-1 DOOR THRESHOLD ATTACH ANGLES CORRODED AT STA 380-420. THE CORROSION WAS REMOVED IAW SRM 51-10-6. THE ATTACH ANGLES WERE REMOVED AND NEW ANGLES WERE INSTALLED IAW SRM 51-30-2, 51-10-2, 51-20-1, 51-40-3, FIGURE 1, AND MM 51-20-0.

Part: PANEL — CORRODED (BS 480 - 1090)

INSPECTION FOUND RT TRANSITION PANELS AT FS 480-560 AND FS 1070-1090 CORRODED. THE PANELS WERE REMOVED AND REPLACED IAW SRM 51-30-2, 51-20-1, 51-10-2, AND MM 51-20-0.

Part: ANGLE — BROKEN (BS 560)

INSPECTION FOUND ATTACH ANGLE FOR RT TRANSITION WEB AT FS 560, LONGERON 27R BELOW TORQUE BOX BROKEN OFF. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2 AND 51-10-2.

Part: PAN — CRACKED (PAX DOOR)

INSPECTION FOUND A 4 INCH CRACK IN L-1 DOOR INNER PAN FORWARD LOWER CORNER. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW ECRA 5265-01005.

Part: FRAME — BENT (BS 560)

INSPECTION FOUND FRAME UPPER FLANGE BENT AT STA 560, LONGERON 25L. THE BENT AREA WAS REMOVED AND AN ANGLE WAS INSTALLED IAW SRM 53-10-4, 51-10-2, AND 51-30-2.

Part: STIFFENER — CRACKED (COWL)

INSPECTION FOUND A 1 INCH CRACK IN NR 3 ENGINE COWL NR 10 STIFFENER. THE STIFFENER WAS REMOVED AND REPLACED IAW SRM 51-20-1 AND 51-30-2.

Part: ANGLE — CORRODED (BS 810)

INSPECTION FOUND WEB SUPPORT ANGLE CORRODED AT WING CENTER SECTION LOWER TORQUE BOX AT KEEL AREA, FS 810. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-1, PAGE 4 AND 51-10-2.

Part: FITTING — CORRODED (SPOILER)

INSPECTION FOUND NR 6 SPOILER CENTER HINGE POINT LEFT AND RIGHT FITTINGS CORRODED. THE FITTINGS WERE REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-20-3, PAGE 5.

Part: FRAME — CRACKED (NLG DOOR)

INSPECTION FOUND A .75 INCH CRACK IN LT FORWARD NLG DOOR SIXTH FRAME. THE FRAME WAS REMOVED AND A NEW FRAME WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-0.

Part: FITTING — CORRODED (CARGO DOOR)

INSPECTION FOUND CENTER CARGO DOOR FORWARD PRESSURE RELIEF DOOR SKIN FITTING CORRODED. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: SKIN — CORRODED (FAIRING)

INSPECTION FOUND RT BODY FAIRING 3441 INNER SKIN AND SUPPORT NR 22 CORRODED. THE CORROSION WAS REMOVED IAW SRM 51-10-6. AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-0. THE SUPPORT WAS REMOVED AND A DOUBLER AND BRACKET WERE INSTALLED IAW SRM 51-10-6, 51-30-2, AND 51-40-3, FIGURE 1.

Part: SEAT TRACK — CORRODED (BS 380 - 1030)

INSPECTION FOUND SEAT TRACK SECTIONS CORRODED AT STA 380-420, RBL 40 AND STA 990-1030, RBL 48. THE SEAT TRACK SECTIONS WERE REMOVED AND REPLACED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-0.

Part: SKIN — DENTED (COWL)

INSPECTION FOUND BOTTOM OF NR 3 ENGINE COWL SKIN DENTED AND SCRATCHED BETWEEN STIFFENERS 9 & 10. THE DAMAGED AREA WAS CUT OUT AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 54-30-3.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION FOUND EMERGENCY EXIT SIGNS AT L2 AND R2 DOORS INOPERATIVE. THE BATTERY WAS REMOVED AND REPLACED IAW MM 33-50-22.

Part: FRAME — CRACKED (BS 930)

INSPECTION FOUND A .75 INCH CRACK IN LT FRAME AT FS 930 BELOW WINDOW. REPAIRED IAW ECRA 5310-01397.

Part: FRAME — CRACKED (BS 380)

INSPECTION FOUND A 2 INCH CRACK IN FRAME AT STA 380, LONGERON 8R. THE CRACKED AREA WAS CUT OUT IAW SRM 53-10-4. A REPAIR WAS INSTALLED IAW SRM 53-10-4, FIGURE 1.

Part: BEAM — CRACKED (SPOILER)

INSPECTION FOUND A 2 INCH CRACK IN BEAM BEHIND WEB AFTER REMOVAL OF NR 8 SPOILER FITTING. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1, PAGE 6A. A REPAIR WAS INSTALLED IAW SRM 51-30-2.

Part: WEB — CRACKED (FUSELAGE)

INSPECTION FOUND A 3 INCH CRACK IN AFT CARGO DOOR JAMB UPPER AFT WEB. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2 AND 51-20-1.

Part: STRINGER — CORRODED (BS 700 - 750)

INSPECTION FOUND STRINGER 26R CORRODED FROM STA 700-750. A REPAIR WAS INSTALLED IAW SRM 51-30-2.

Part: PANEL — CORRODED (BS 540 - 670)

INSPECTION FOUND LT TRANSITION PANEL AT FS 540-670 CORRODED. THE PANEL WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: SKIN — WORN (TE FLAP)

INSPECTION FOUND THE RT I/B FOREFLAP UPPER SKIN WORN THROUGH. THE FOREFLAP WAS REPAIRED IAW SRM 51-40-6.

Part: ANGLE — CORRODED (BS 216 - 219)

INSPECTION FOUND TWO ATTACH ANGLES CORRODED FROM FS 216-219, RBL 15, L27R. THE ANGLES WERE REMOVED AND NEW ANGLES WERE INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-0.

Part: WEB — CRACKED (BS 720E)

INSPECTION FOUND RT WING ROOT L/E TO BODY LOWER SUPPORT WEB CRACKED AT NUT PLATE HOLE, FS 720E, STRINGER 21R. THE CRACK WAS 1 INCH LONG. THE CRACKED AREA WAS CUT OUT, FILLER AND DOUBLER WAS INSTALLED IAW SRM 51-40-2 AND 51-30-2.

Part: FRAME — CRACKED (BS 312)

INSPECTION FOUND A 1.25 INCH CRACK IN RT FUSELAGE FRAME AT STA 312, LONGERON 13R. THE CRACKED AREA WAS CUT OUT IAW SRM 53-10-4, FIGURE 1. REPAIR ANGLES WERE INSTALLED IAW SRM 53-10-4, 51-10-2, AND 51-30-0.

Part: SUPPORT — CORRODED (BS 400 - 420)

INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 420, RBL 20-40 AND AT STA 400-420, RBL 10. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-30-2.

Part: SUPPORT — CORRODED (BS 1110 - 1130)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1110-1130, LBL 15. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-30-0, PAGE 3.

Part: SUPPORT — CORRODED (BS 420)

INSPECTION FOUND FLOORBOARD SUPPORT CORRODED AT STA 420, RBL 12-25. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-0.

Part: SUPPORT — CRACKED (BS 760)

INSPECTION FOUND A 3 INCH CRACK IN FLOOR SUPPORT AT FS 760, RBL 56. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-30-5, 51-10-2, AND 51-20-0.

Part: ANGLE — CORRODED (BS 1148 - 1166)

INSPECTION FOUND TRANSITION PANEL ATTACH ANGLE AT STA 1148-1166 IN AFT PIT. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: SKIN — CORRODED (FAIRING)

INSPECTION FOUND LEFT LOWER BODY FAIRING 3341 SKIN AND NR 7 SUPPORT CORRODED. THE SKIN WAS REMOVED AND NEW SKIN, DOUBLER, AND STRAPS WERE INSTALLED IAW SRM 53-30-3 AND 51-20-4. THE SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: SKIN — GOUGED (AILERON)

INSPECTION FOUND LEFT O/B AILERON LOWER EDGE GOUGED. THE GOUGED AREA WAS REPAIRED IAW SRM 57-50-5, FIGURE 2 AND 51-20-0.

Part: ANGLE — CRACKED (BS 1193)

INSPECTION FOUND A 2 INCH CRACK IN ATTACH ANGLE AT FS 1193, RBL 20. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2.

Part: PANEL — CORRODED (BS 620 - 800)

INSPECTION FOUND TRANSITION PANELS AT FS 620-660, S24R AND AT STA 660-800, S23L CORRODED. THE PANELS WERE REMOVED AND NEW PANELS WERE INSTALLED IAW SRM 51-10-2 AND 51-30-2.

Part: STIFFENER — CRACKED (BS 1183)

INSPECTION FOUND A 1 INCH CRACK IN STIFFENER AT STA 1183, LBL 60. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-0.

Part: SKIN — CRACKED (PAX DOOR)

INSPECTION FOUND A 2 INCH CRACK IN L-1 DOOR INNER SKIN AT CUTOUT FOR HANDLE ON LOWER FORWARD SIDE. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1, PAGE 6D, 51-40-2, AND 51-30-1.

Part: FLOOR PANEL — CORRODED (CARGO BAY)

INSPECTION FOUND AFT PIT FLOOR PANEL CORRODED. A NEW FLOOR PANEL WAS INSTALLED IAW SRM 51-30-5, 51-10-2, AND MM 51-20-0.

Part: WEB — CORRODED (BS 800)

INSPECTION FOUND WEB CORRODED AROUND FASTENERS ON LEFT AND RIGHT SIDES AT WING CENTER SECTION FS 800 LOWER TORQUE BOX KEEL AREA, S29L-29R. THE WEB WAS CUT OUT AND A NEW WEB SECTION AND SPLICE WERE INSTALLED IAW SRM 51-40-2, FIGURE 1, 51-30-6, AND MM 51-20-0.

Part: WEB — CORRODED (BS 790)

INSPECTION FOUND WEB OUTER SURFACE CORRODED AROUND FASTENERS ON LEFT AND RIGHT SIDES AT WING CENTER SECTION, FS 790 LOWER TORQUE BOX AT KEEL AREA. THE CORRODED WEB SECTION WAS CUT OUT AND A NEW WEB SECTION WAS INSTALLED IAW SRM 51-40-2.

Part: ANGLE — CRACKED (BS 1070)

INSPECTION FOUND A 2 INCH CRACK IN FLOORBOARD SUPPORT ANGLE AT STA 1070, LBL 28. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-2, MM 51-20-0.

Part: RIB — CRACKED (RUDDER)

INSPECTION FOUND A 1 CRACK IN UPPER RUDDER AFT UPPER LEFT T/E RIB. A DOUBLER WAS INSTALLED IAW SRM 51-40-2.

Part: ANGLE — CORRODED (BS 760)

INSPECTION FOUND WEB SUPPORT ANGLE CORRODED AT WING CENTER SECTION, STA 760 LOWER TORQUE BOX KEEL AREA. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-10-2.

Part: FLOORBEAM — CORRODED (BS 1030)

INSPECTION FOUND CABIN FLOORBEAM UPPER CHORDS CORRODED AT FS 1030 FROM LBL 12 TO RBL 40. A REPAIR WAS INSTALLED IAW SRM 53-10-8, 51-10-2, 51-30-1, AND MM 51-20-0.

Part: SUPPORT — CRACKED (BS 555)

INSPECTION FOUND A 3 INCH CRACK IN FORWARD CARGO COMPARTMENT FLOOR SUPPORT AT FS 555 BETWEEN STRINGER 23L AND 27L. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2.

Part: ANGLE — CRACKED (RT WING)

INSPECTION FOUND A .25 INCH CRACK IN SUPPORT ANGLE FOR BODY TO FUSELAGE FAIRING AT RT WING AFT VERY I/B T/E PANEL. THE SUPPORT ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-1, 51-30-2, AND 51-10-3.

Part: FRAME — CRACKED (BS 540)

INSPECTION FOUND FRAME BENT AND CRACKED AT UPPER FLANGE, STA 540, L25L. THE FRAME WAS REFORMED AND THE CRACKED AREA WAS TRIMMED OUT IAW SRM 51-40-4. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-40-4.

Part: FLOORBEAM — GOUGED (BS 344)

INSPECTION FOUND FLOORBEAM GOUGED AT STA 344, RBL 45. A REPAIR WAS INSTALLED IAW SRM 51-10-2, 51-20-4, 51-30-2, MM 51-20-0, ECRA 5310-03955, AND EA 27-5310-2-A0532.

Part: CUSP — CORRODED (BS 1090 - 1110)

INSPECTION FOUND CUSP WEB SECTION CORRODED ON BOTTOM SIDE AT FS 1090-1110, RBL 58. THE CUSP WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW 51-10-1, 53-10-2, 51-10-6, 51-30-0, AND MM 51-20-2.

Part: SKIN — DAMAGED (VERTICAL STAB)

INSPECTION FOUND LEADING EDGE ACCESS PANEL SKIN OF VERTICAL STABILIZER WITH FASTENERS PULLING THROUGH AT STA 134. A DOUBLER WAS INSTALLED IAW SRM 55-30-7, 51-10-6, 51-20-0, AND 51-30-2.

Part: PANEL — CORRODED (BS 1030 - 1090)

INSPECTION FOUND LT TRANSITION PANELS AT FS 1030-1065 AND FS 1065-1090 CORRODED. THE PANELS WERE REMOVED AND REPLACED IAW SRM 51-30-2.

Part: SUPPORT — CORRODED (BS 660 - 800)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 660-800, RBL 12. SUPPORT ANGLES WERE INSTALLED IAW SRM 51-40-4 AND 51-30-3.

Part: BRACKET — CRACKED (LT WING)

INSPECTION FOUND A 3 INCH CRACK IN SUPPORT BRACKET AT LEFT WING L/E PANEL NR 6215. THE SUPPORT BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: STRINGER — CRACKED (BS 580 - 600)

INSPECTION FOUND A .5 INCH CRACK IN STRINGER 4R AT STA 580-600. THE CRACKED SECTION OF STRINGER WAS CUTOUT AND A REPAIR WAS INSTALLED IAW SRM 51-10-3, 51-10-2, 53-10-3, AND MM 51-20-0.

Part: WEB — CORRODED (BS 760)

INSPECTION FOUND WEB OUTER SURFACE CORRODED AROUND FASTENERS AT WING CENTER SECTION, FS 760 LOWER TORQUE BOX KEEL AREA. THE CORRODED WEB SECTION WAS CUT OUT AND A NEW SECTION WAS INSTALLED IAW SRM 51-40-2.

Part: INTERCOSTAL — CRACKED (BS 480 - 500)

INSPECTION FOUND A 3 INCH CRACK IN INTERCOSTAL AT STA 480-500, S28L. THE CRACKED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 51-40-3 AND 51-30-2.

Part: INTERCOSTAL — CORRODED (BS 950A - 950B)

INSPECTION FOUND AFT CARGO INTERCOSTAL CORRODED UNDER AND ON TOP OF NUTPLATES AT FS 950A-950B, S26R-27R. A REPAIR WAS INSTALLED IAW SRM 51-30-1.

Part: SEAT TRACK — CORRODED (BS 950 - 1110)

INSPECTION FOUND LT I/B SEAT TRACK CORRODED FROM STA 950-990, LBL 24 AND FROM STA 1070-1110, LBL 24. THE SEAT TRACK SECTIONS WERE REMOVED AND REPLACED IAW SRM 51-30-2, 51-20-0, AND 51-10-2.

Part: SUPPORT — CRACKED (NR 2 ENG COWL)

INSPECTION FOUND A 1 INCH CRACK IN SECOND FRAME SUPPORT FROM AFT OF LT FORWARD NR 2 ENGINE COWL. THE FRAME SUPPORT WAS REMOVED AND A NEW FRAME SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-30-1, AND 51-10-1.

Part: SUPPORT — CORRODED (BS 660 - 800)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 660-800, LBL 12. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-40-4 AND 51-30-0.

Part: ANGLE — CORRODED (BS 780)

INSPECTION FOUND LOWER WEB SUPPORT ANGLE CORRODED AT FS 780. A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2.

Part: PANEL — CORRODED (HORIZONTAL STAB)

INSPECTION FOUND RT HORIZONTAL STABILIZER LE PANEL 9202 CORRODED. A NEW PANEL WAS INSTALLED IAW SRM 51-10-5, 51-10-2, AND MM 51-20-0.

Part: SKIN — CRACKED (WING)

INSPECTION FOUND A 3 INCH CRACK IN RT I/B FLAP TRACK FAIRING SKIN. A DOUBLER WAS INSTALLED IAW SRM 51-30-0, 51-10-2, 51-30-2, AND MM 51-20-0.

Part: INTERCOSTAL — CORRODED (BS 1148 - 1166)

INSPECTION FOUND INTERCOSTAL CORRODED AT STA 1148-1166, L26L. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: ANGLE — CRACKED (LT MLG DOOR)

INSPECTION FOUND A 2 INCH CRACK IN LEFT MLG WING DOOR ANGLE AT T/E LOWER CORNER. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-0.

Part: STIFFENER — CRACKED (BS 1183)

INSPECTION FOUND A 1.4 INCH CRACK IN STIFFENER AT STA 1183, LBL 35. REPAIR DOUBLERS WERE INSTALLED IAW SRM 51-30-2, 51-10-2, MM 51-20-0, AND ECRA 5310-01600.

Part: SUPPORT — CRACKED (BS 760)

INSPECTION FOUND A .5 INCH CRACK IN O/B FLOOR SUPPORT AT RT FUSELAGE WALL FS 760. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-0.

Part: SUPPORT — CORRODED (BS 1050 - 1130)

INSPECTION FOUND FLOOR SUPPORT ANGLES AT FS 1070-1050, LBL 55 AND AT FS 1130, BL 0 CORRODED. THE FLOOR SUPPORT ANGLES WERE REMOVED AND REPLACED IAW SRM 51-10-1, 51-30-2, 51-10-2, AND 51-20-02.

Part: WEB — CORRODED (BS 1090 - 1130)

INSPECTION FOUND AFT DOOR AFT TORQUE BOX WEB CORRODED WITH A 1 INCH CRACK AT RIVET, FS 1090-1130, S27R. THE CORROSION WAS REMOVED IAW SRM 51-10-6. A WEB AND NUT PLATES WERE INSTALLED IAW SRM 51-10-4, 51-30-2, AND 53-10-4.

Part: ANGLE — CORRODED (BS 750)

INSPECTION FOUND LOWER WEB ATTACH ANGLE CORRODED AT STA 750. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2 AND 51-30-1, PAGE 7.

Part: PANEL — CORRODED (BS 990 - 1070)

INSPECTION FOUND LT AND RT TRANSITION PANELS AT FS 990-1030, S27L AND RT TRANSITION PANEL AT FS 1030-1070 CORRODED. THE PANELS WERE REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-10-01.

Part: BRACKET — CRACKED (BS 1193)

INSPECTION FOUND A 1 INCH CRACK IN VERTICAL SUPPORT LOWER END ATTACH BRACKET AT STA 1193, LBL 20. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 360)

INSPECTION FOUND FLOORBEAM CORRODED AT STA 360, BL 0 TO RBL 35. REPAIR ANGLES, FILLER, AND EXTRUSION WERE INSTALLED IAW SRM 53-10-8, FIGURE 8.

Part: STRAP — CRACKED (BS 328 - 344)

INSPECTION FOUND A 2.5 CRACK IN STRAP UNDER FLOORBEAM IN FORWARD CABIN AREA AT STA 328-344, LBL 50. THE STRAP WAS REPAIRED BY INSTALLING A DOUBLER IAW SRM 51-30-2 AND 51-40-3.

Part: BRACKET — CORRODED (BS 700B)

INSPECTION FOUND BRACKET CORRODED AT FS 700B, S27R. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: ANGLE — CORRODED (BS 540)

INSPECTION FOUND ATTACH ANGLE CUT AND CORRODED AT C-1 DOOR CUTOUT LOWER FORWARD SECTION, STA 540, STRINGER 26R. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2.

Part: BRACKET — CRACKED (BS 720C)

INSPECTION FOUND A .75 INCH CRACK IN BRACKET AT FS 720C, S27R. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: STRAP — CRACKED (BS 720)

INSPECTION FOUND A 6 INCH CRACK IN TRANSITION PANEL STRAP AT FS 720, RT FORWARD PIT. A NEW STRAP WAS INSTALLED IAW SRM 51-10-2.

Part: WEB — CRACKED (BS 400 - 420)

INSPECTION FOUND A 3 INCH CRACK IN WEB ANGLE AT STA 400-420, RBL 45. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-10-1, PAGE 4, 51-30-0, PAGE 3, 51-20-0, AND 51-10-2.

Part: SUPPORT — CRACKED (BS 848)

INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT STA 848, BL 0 TO RBL 25. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: INTERCOSTAL — CRACKED (BS 620)

INSPECTION FOUND AN 8 INCH CRACK IN INTERCOSTAL UNDER FLOOR SUPPORT FITTING AT FS 620. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-30-5 AND 51-30-2.

Part: PAN — CRACKED (PAX DOOR)

INSPECTION FOUND A .5 INCH CRACK IN RADIUS OF UPPER AFT CORNER OF L-1 DOOR PAN. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 51-40-2.

Part: FLOORBEAM — CORRODED (BS 312)

INSPECTION FOUND UPPER SURFACE OF FLOORBEAM CORRODED AT STA 312, LBL 30. A REPAIR DOUBLER AND FLOOR SUPPORT WERE INSTALLED IAW SRM 53-10-8, 51-30-1, AND 51-30-2.

Part: SEAT TRACK — CORRODED (BS 380 - 420)

INSPECTION FOUND SEAT TRACK CORRODED AT STA 380-420, RBL 25. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 420 - 440)

INSPECTION FOUND SEAT TRACK CORRODED AT STA 420-440, RBL 50. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: ANGLE — CORRODED (BS 1166)

INSPECTION FOUND UPPER ATTACH ANGLE CORRODED AT FS 1166 FALSE BULKHEAD, BL 0. THE CORRODED AREA WAS REMOVED IAW SRM 51-40-3. A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW SRM 51-40-3.

Part: ANGLE — CRACKED (RT WING)

RIGHT WING I/B OF I/B AILERON ANGLE IS CRACKED (.5) LOCATED ABOVE JACK SCREW AREA. REMOVED FASTENERS, FABRICATED AND INSTALLED NEW BRACKET PER SRM 51-30-2 AND 57-20-4.

Part: RIB — CRACKED (WING)

TWO RIBS ATTACHED TO NR 7 SPOILER ACTUATOR CASTING ARE CRACKED (1). REPLACED RIBS PER SRM 51-10-1 AND 51-30-2.

Part: BRACKET — CRACKED (NR 1 LE FLAP ACT)

LEFT WING NR 1 L/E KRUEGER FLAP ACTUATOR I/B MOUNT BRACKET IS CRACKED .375 INCH. REMOVED BRACKET, FABRICATED AND INSTALLED NEW BRACKET PER SRM 51-10-1.

Part: TIP — CRACKED (RT WING)

LEFT WING LOWER WING TIP SURFACE HAS .5 INCH LONG HOLE WORK THROUGH AND .5625 INCH CRACK. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER PER SRM 57-30-2.

Part: TIP — CRACKED (RT WING)

RIGHT WING TIP AT LOWER SURFACE AFT OF MOUNT SCREWS HAS A 1 INCH LONG CRACK. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER PER SRM 51-40-2 AND 51-30-2.

Part: ANGLE — CRACKED (LT WING)

A 2.875 PIECE OF ANGLE BROKEN OFF AT TOP OF LEFT WING JUST FWD OF O/B AILERON L/E AT I/B END. REMOVED FASTENERS AND DAMAGED T ANGLE. FABRICATED AND INSTALLED NEW T ANGLE PER SRM 51-30-2 AND 57-10-7.

Part: BRACKET — CRACKED (LT WING)

BRACKET HAS .3125 INCH CRACK AT INBOARD SIDE AT LEFT WING NR 1 SLAT WHERE INBOARD TRACK MOUNTS TO LOWER SKIN. REMOVED AND REPLACED CRACKED BRACKET PER SRM 51-30-2.

Part: MOUNT — CRACKED (NR 2 LE FLAP ACT)

LEFT WING NR 2 KRUEGER FLAP ACTUATOR INBOARD MOUNT CRACKED AT TOP (1). REMOVED, FABRICATED AND INSTALLED BRACKET PER SRM 51-10-1.

Part: CHANNEL — CRACKED (C2 DOOR)

INBOARD SIDE OF C2 DOOR UPPER AFT CORNER METAL CHANNEL IS CRACKED (1) AT SEAL DEPRESSOR AREA. REMOVED CRACKED SECTION, FABRICATED, TREATED, PRIMED INSTALLED PER SRM 51-30-2, 51-10-6, AND 51-20-1.

Part: MEGAPHONE — INOP (CABIN)

AFT MEGAPHONE INOPERATIVE (NO SOUND). CLEANED CONTACTS AND OPS CHECK NORMAL PER MM 25-62-00.

Part: SEAT TRACK — CORRODED (BS 1090)

CORROSION AT BOTTOM OF SEAT TRACK STA 1090 RBL 47. REMOVED AND REPLACED CORRODED SEAT TRACK FROM STA 1090 TO STA 1130 RBL 47 PER SRM 51-10-1.

Part: TAB — DELAMINATED (RT AILERON)

RIGHT WING OUTBOARD AILERON TAB IS DELAMINATED AT BOTH T/E'S (10). REMOVED AND REPLACED RIGHT WING OUTBOARD AILERON TAB PER MM 27-10-41.

Part: WIRE — DISCONNECTED (EMERGENCY EXIT)

ESCAPE PATH LIGHTS AT MID CABIN OVERWING EXITS ARE LOOSE AND DISCONNECTED. REPAIRED AND SECURED PATH WIRING. OPS CHECK PER MM 33-51-0.

Part: WIRE — DISCONNECTED (ROW 28-30)

ESCAPE PATH WIRE DAMAGED AT SEAT 24 TO 30. DISCONNECTED OUT OF TRACKS. REPAIRED AND CONNECTED WIRE AT ROWS 28 TO 30. OPS CHECK GOOD PER MM 33-51-01.

Part: SKIN — CORRODED (RT HORIZ STAB)

RIGHT HORIZONTAL STAB HAS BULGE IN UPPER SKIN AT AFT SPAR APPROX 12 INCHES FROM OUTBOARD END AT FIRST RIB FROM END. CUT OUT DAMAGE AND ACCOMPLISHED REPAIR PER 55-10-5 AND 12-30-8 MM.

Part: BATTERY PACK — DISCHARGED (PAX DOORWAY)

AFT ENTRY OVERHEAD EMERGENCY LIGHT INOPERATIVE WHEN TESTED. REMOVED AND REPLACED BATTERY PACK AND OPS CHECK NORMAL PER MM 33-60-01.

Part: DOOR — GOUGED (CARGO COMPT)

BOTTOM EDGE OF C2 DOOR AFT 25 HOLES AND GOUGES IN LIP. REMOVED AND REPLACED NEW BOTTOM EDGE PER SRM 51-10-1 AND 51-30-2.

Part: BULKHEAD — CRACKED (VERT STAB)

INSPECTION FOUND VERTICAL STABILIZER LEADING EDGE LOWER PANEL UPPER ATTACH BULKHEAD CRACKED AT ATTACH HOLES. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-30-3.

Part: ANGLE — CRACKED (BS 1263)

INSPECTION FOUND A 2 INCH CRACK IN REPAIR ANGLE ON FORWARD SIDE OF RT BS 1263 TORQUE BOX WEB BELOW HORIZONTAL DECK. THE CRACKED AREA WAS REMOVED AND A REPAIR KIT WAS INSTALLED IAW BOEING DRAWING 65C27136.

Part: PLATE — CRACKED (VERT STAB)

INSPECTION FOUND VERTICAL STABILIZER UPPER LT REINFORCEMENT PLATE JUST FOWARD OF TENSION TIE FORWARD ATTACH BOLT AREA CRACKED. THE CRACK WAS 1.5 INCH LONG. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 55-30-3.

Part: SIDEWALL — CRACKED (BS 290)

INSPECTION FOUND A CRACK BETWEEN TWO FASTENERS IN RIGHT SIDEWALL PANEL OF NLG WHEEL WELL, FS 290. THE CRACKED AREA WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW EA 5362-01016.

Part: STRINGER — CRACKED (WS 686.5)

INSPECTION FOUND LT WING UPPER AFT VENT BOX STRINGER FORWARD MOUNT EAR CRACKED OUT AT WS 66.50. A REPAIR WAS FABRICATED AND INSTALLED IAW EA 5762-01050.

Part: CIRCUMFERENTIAL — CORRODED (BS 740)

INSPECTION FOUND CORROSION ON CIRCUMFERENTIAL IN AIR CONDITIONING DISTRIBUTION BAY AT STA 740 FROM STRINGER 26L TO S26R. THE CIRCUMFERENTIAL WAS REMOVED AND REPLACED IAW SRM 51-40-3.

Part: STRINGER — CRACKED (WS 686.5)

INSPECTION FOUND A CRACK AT LT WING FORWARD VENT BOX STRINGER FORWARD AND AFT MOUNT EARS AT WS 686.50. REPAIRS WERE FABRICATED AND INSTALLED IAW EA 5762-01050.

Part: TAB — CRACKED (BS 601.50)

INSPECTION FOUND STIFFENER TAB CRACKED INSIDE OF NR 3 TANK TOP OF RIB AT STA 601.50 AT OUTBOARD SIDE. THE TAB WAS CUT OFF AND A REPAIR WAS INSTALLED IAW EA 5762-01050.

Part: FRAME — CORRODED (BS 1030)

INSPECTION FOUND FRAME AT FS 1030 BETWEEN STRINGER 18L AND 19L CORRODED. A DOUBLER AND SHEAR TIE WERE FABRICATED AND INSTALLED IAW SRM 53-10-4.

Part: FITTING — CORRODED (NR 13 ACT FTG)

INSPECTION FOUND NR 13 SPOILER ACTUATOR SUPPORT FITTING CORRODED. THE SUPPORT FITTING WAS REMOVED AND REPLACED IAW MM 27-61-81.

Part: SIDEWALL — CRACKED (BS 272)

INSPECTION FOUND A CRACK AT FASTENER HEAD IN LEFT SIDEWALL PANEL OF NLG WHEEL WELL, FS 272. THE CRACKED AREA WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW EA 5362-01016.

Part: SIDEWALL — CRACKED (BS 272)

INSPECTION FOUND A CRACK AT FASTENER HEAD IN LT SIDEWALL PANEL OF NLG WHEEL WELL FS 272. THE CRACKED AREA WAS CUT OUT, A REPAIR WAS INSTALLED IAW ECRA 5310-03599.

Part: SIDEWALL — CRACKED (BS 286)

INSPECTION FOUND A CRACK AT FASTENER HEAD IN LT CEILING PANEL OF NLG WHEEL WELL AT FS 286. THE CRACKED AREA WAS CUT OUT, FILLER, DOUBLER AND STRAP WERE FABRICATED AND INSTALLED IAW EA 5362-01016.

Part: SIDEWALL — CRACKED (BS 259)

INSPECTION FOUND A CRACK BETWEEN TWO FASTENER HEADS IN RIGHT SIDEWALL PANEL OF NLG WHEEL WELL FS 259. THE CRACKED AREA WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5310-03600.

Part: SIDEWALL — CRACKED (BS 286)

INSPECTION FOUND A CRACK AT FASTENER HEAD IN RT SIDEWALL PANEL OF NLG WHEEL WELL AT FS 286. THE CRACKED AREA WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW EA 5362-01016.

Part: SKIN — DISBONDED (LT TE AFT FLAP)

INSPECTION FOUND AN 8 AREA OF LEFT AFT INBOARD FLAP DISBONDED BETWEEN SPAR AND LOWER SKIN AT INBOARD END. THE AFT FLAP SEGMENT WAS REMOVED AND REPLACED IAW MM 27-51-1.

Part: SKIN — CRACKED (LT HORIZ STAB)

INSPECTION FOUND A .5 INCH CRACK IN LT HORIZONTAL STABILIZER OUTBOARD TRAILING EDGE JUST BELOW ELEVATOR OUTBOARD HINGE. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-10-6, FIGURE 2.

Part: SKIN — DENTED (NR 6 LE FLAP)

INSPECTION FOUND LEADING EDGE OF NR 6 SLAT DENTED. THE DENTED AREA WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-50-3, FIGURE 1.

Part: SKIN — CORRODED (BS 420)

INSPECTION FOUND RT FUSELAGE SKIN CORRODED AT STA 420 JUST FORWARD OF STATIC PORT AREA. THE CORRODED AREA WAS CUT OUT, A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 5 AND ECRA 5330-02592.

Part: SKIN — DENTED (RT TE FLAP)

INSPECTION FOUND LOWER CENTER LEADING EDGE OF RIGHT OUTBOARD TRAILING EDGE FLAP DENTED. THE DENTED AREA WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-50-4.

Part: SKIN — CORRODED (BS 480)

INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 480, STRINGER 29L. THE STRINGER AND SPLICES WERE REMOVED AND THE SKIN CORROSION WAS CLEANED. STRINGER, SPLICE AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-10-3 AND 53-30-3.

Part: BEAM — CORRODED (HORIZ STAB)

INSPECTION FOUND RT HORIZONTAL STABILIZER UPPER SKIN TRAILING EDGE BEAM CORRODED. THE TRAILING EDGE BEAM WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: ENGINE — FAILED (NR 2)

THE NR 2 ENGINE EGT APPROACHED HIGH END LIMITS WHILE EN ROUTE TO EWR. THE NR 2 ENGINE WAS SHUT DOWN AS A PRECAUTIONARY MEASURE. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. THE NR 2 ENGINE WAS REMOVED AND REPLACED. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION.

Part: FOLLOW-UP CABLES — BROKEN (LT TE FLAP)

EWR - FLT 0654 - AIRCRAFT REQUIRED 25-30 UNITS RIGHT AILERON TO MAINTAIN LEVEL FLIGHT WHILE ON FINAL APPROACH TO EWR. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LT INBD T/E FLAP FOLLOW-UP CABLES BROKEN WITH RESULTANT DAMAGE TO THE MID-FLAP. THE MID-FLAP AND FOLLOW-UP CABLES WERE REMOVED AND REPLACED. AN ADJUSTMENT TEST OF THE INBOARD MID-FLAP WAS PERFORMED IAW MM 27-51-1, PAGES 409-415. THE FLAPS WERE CYCLED SEVERAL TIMES WITH OPERATION CHECKING GOOD. (X)

Part: SUPPORT — CORRODED (BS 1072-1092)

INSPECTION FOUND CORROSION ON THE OUTBOARD FLOOR SUPPORT AT BS 1072-BS 1092, RBL 60. THE CORRODED SECTION WAS REMOVED. AN L-ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3. (X)

Part: FRAME — CORRODED (BS 560)

INSPECTION FOUND CORROSION ON THE FORWARD FRAME AT BS 560 IN THE FORWARD BILGE INTERIOR. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. (X)

Part: STRINGER — CORRODED (LAV SERVICE DOOR)

INSPECTION FOUND CORROSION ON STRINGER AT LOWER FORWARD AND AFT CORNERS OF AFT LAV SERVICE DOOR. THE CORRODED SECTION OF STRINGER WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-3. (X)

Part: FRAME — CORRODED (BS 540)

INSPECTION FOUND CORROSION ON FRAME AT BS 540, STR 26R. THE CORRODED SECTION OF FRAME WAS REMOVED. A NEW SECTION OF FRAME WAS FABRICATED AND INSTALLED IAW SRM 53-10-4. (X)

Part: SUPPORT — CORRODED (BS 345)

INSPECTION FOUND FLOOR SUPPORT CORRODED ON THE FLANGE IN THE FORWARD GALLEY AREA AT BS 345, RBL 18. THE CORRODED SECTION WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8. (X)

Part: STRINGER — CORRODED (BS 442)

INSPECTION FOUND CORROSION ON STR 24R AND STR 28R AT BS 442. THE CORRODED SECTION OF STRINGER WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 AND SRM 53-10-3. (X)

Part: SKIN — CORRODED (BS 296)

INSPECTION FOUND SKIN BULGED DUE TO CORROSION AT BS 296L. THE CORRODED AREA OF SKIN WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. (X)

Part: CARBON SEAL — BROKEN (NR 2 ENGINE)

FLL - FLT 0443 - THE NR 2 ENGINE OIL TEMPERATURE CLIMBED INTO THE RED ZONE WHILE EN ROUTE FROM EWR TO FLL. THE TEMPERATURE RISE WAS ACCOMPANIED BY A DROP IN OIL PRESSURE AND QUANTITY AND ILLUMINATION OF THE NR 2 ENGINE OIL BYPASS LIGHT. THE NR 2 ENGINE WAS SHUT DOWN AND THE AIRCRAFT LANDED AT FLL WITHOUT INCIDENT. THE NR 2 ENGINE REMOVED AND REPLACED. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION. SUPPLEMENT - SHOP FINDINGS REVEALED NR 5 CARBON SEAL, SEAL RING, AND HEATSHIELD BROKEN AND WORN. (X)

Part: HYD LINE — CRACK ('A' HYD SYSTEM)

FLT NR 0134 - EWR - AIRCRAFT DECLARED EMERGENCY LANDING DUE TO 'A' SYSTEM LOST HYD PRESSURE AND FLUID. DURING INSPECTION FOUND 'A' SYSTEM PRESSURE LINE CRACK, CHANGE LINE AND PUMP. LEAK CHECKED SYSTEM ALL OK. 95ZZZW713.

Part: PUMP — FAILED ('A' HYD SYSTEM)

FLT NR 0134 - EWR - AIRCRAFT DECLARED EMERGENCY LANDING DUE TO 'A' SYSTEM LOST HYD PRESSURE AND FLUID. DURING INSPECTION FOUND 'A' SYSTEM PRESSURE LINE CRACK, CHANGE LINE AND PUMP. LEAK CHECKED SYSTEM ALL OK. REFERENCE CAL950340.

Part: SWITCH — CRACKED (RT MLG DOOR)

IAH - FLT 148 - THE RT MLG DOOR DID NOT INDICATE UP AND LOCKED DURING GEAR RETRACTION AFTER TAKEOFF FROM IAD. THE GEAR WAS CYCLED AND THE RT MLG DOOR INDICATED UP AND LOCKED. MAINTENANCE FOUND THE S399 RT GEAR DOOR SWITCH CRACKED. THE GEAR DOOR SWITCH WAS REMOVED AND REPLACED. GEAR OPERATION AND INDICATIONS CHECKED GOOD. (W)