N14788

Part: CONNECTOR — SHORTED (CABIN)

INSPECTION FOUND LT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE FOUND THE CANNON PLUG SHORTED AT POWER SUPPLY. THE PLUG WAS REPLACED AND EXIT LIGHT OPERATION WAS RESTORED.

Part: WEB — CRACKED (RT MLG DOOR)

INSPECTION FOUND A 1 INCH CRACK IN RT MLG FLYING DOOR WEB FORWARD OF AFT HINGE FITTING. THE HINGE WEB WAS REMOVED IAW SRM 51-30-2. A NEW HINGE WEB WAS INSTALLED IAW SRM 52-80-1, 51-10-2, 51-30-2, AND MM 51-20-11.

Part: SKIN — LIGHTNING STRIKE (BS 500)

INSPECTION FOUND LIGHTNING STRIKE DAMAGE TO STATIC PORT SKIN ON RT FUSELAGE FORWARD OF FORWARD PIT DOOR AT STA 500. THE DAMAGE WAS REPAIRED IAW SRM 53-30-03.

Part: FITTING — CORRODED (NR 6 FLAP TRACK)

INSPECTION FOUND RT WING NR 6 FLAP TRACK FORWARD ATTACH FITTING CORRODED. THE FLAP TRACK FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 1166)

INSPECTION FOUND UPPER SURFACE OF FLOORBEAM CORRODED AT BS 1166, RBL 50 TO RBL 66. THE CORROSION WAS REMOVED AND A REPAIR STRAP WAS INSTALLED IAW SRM 51-30-5, 51-10-2, 51-30-2, AND ECRA 5321-01029.

Part: ANGLE — CORRODED (BS 178)

INSPECTION FOUND NOSE RADOME AREA LOWER L-ANGLE CORRODED AT FS 178, LBL 6 TO RBL 6. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-40-3, 51-30-2, 51-10-2 AND MM 51-20-0.

Part: ANGLE — CORRODED (BS 303.9)

INSPECTION FOUND ANGLE CORRODED BELOW FORWARD FLIGHT ATTENDANT'S SEAT AT STA 303.9 FROM LBL 12 TO LBL 50. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-40-3, 51-30-5, 53-10-2, AND MM 51-20-11.

Part: SPLICE — CORRODED (BS 720-730)

INSPECTION FOUND LT FORWARD CARGO BUTT SPLICE NR 6 AND BUTT SPLICE AT BS 720 TO 730 CORRODED. NEW BUTT SPLICES WERE INSTALLED IAW SRM 51-20-1, FIGURE 7, 51-10-2, MM 51-20-11.

Part: SEAT TRACK — CORRODED (BS 1132-1136)

INSPECTION FOUND RT SEAT TRACK CORRODED AT STA 1132-113 TO , RBL 48. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-10-5, FIGURE 7, 51-30-5, 51-10-2, 53-10-4, AND MM 51-20-11.

Part: RIB — CRACKED (NR 5 LE SLAT)

INSPECTION FOUND A .5 INCH CRACK IN RT WING NR 5 SLAT INBOARD AND OUTBOARD RIBS AT ACTUATOR ROD END ATTACH POINT. BOTH THE INBOARD AND OUTBOARD RIBS WERE REMOVED AND REPLACED IAW SRM 51-30-2.

Part: FRAME — CRACKED (CARGO DOORWAY)

INSPECTION FOUND C-3 CARGO DOOR CUTOUT FORWARD FRAME LOWER CORNER CRACKED OUT OF BOTTOM STOP FITTING UPPER INBOARD BOLT HOLE AND LOWER PART OF FRAME WAS CORRODED. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-40-3. THE CRACK WAS 1.75 INCH LONG.

Part: FITTING — CORRODED (VERT STAB)

INSPECTION FOUND TOP OF VERTICAL STABILIZER LT HORIZONTAL HINGE ATTACH FITTINGS CORRODED. THE FITTINGS WERE REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-4, AND ECRA 5550-01033.

Part: STRINGER — CRACKED (BS 900)

INSPECTION FOUND A 4 INCH CRACK IN STRINGER 14L AT STA 900. THE CRACKED SECTION OF STRINGER WAS REPLACED IAW SRM 51-30-2.

Part: WEB — CORRODED (LAVATORY)

INSPECTION FOUND RT AFT LAV FLOOR WEB CORRODED VANITY PLUMBING FITTING. THE FLOOR WEB WAS REMOVED, A NEW LAV FLOOR WEB, DOUBLER, AND FILLER WERE INSTALLED IAW SRM 51-40-2, 51-30-2, 51-10-2 AND MM 51-20-11.

Part: FLOOR — CORRODED (COCKPIT)

INSPECTION FOUND COCKPIT LT SIDE FLOOR PANEL CORRODED. A NEW FLOOR PANEL WAS INSTALLED IAW SRM ECRA 5320-01448.

Part: FRAME — CORRODED (BS 720)

INSPECTION FOUND SIDE WALL SUPPORT FRAME CORRODED AT STA 720D ABOVE STRINGER 26R. THE CORRODED SECTION OF SUPPORT FRAME WAS REMOVED. A REPAIR ANGLE AND DOUBLER WERE INSTALLED IAW SRM 51-40-3, 51-10-2, 51-50-2 AND MM 51-20-11.

Part: PRESS PANEL — CRACKED (BS 271)

INSPECTION FOUND A .1875 INCH CRACK IN NLG RT SIDE PRESSURE PANEL OUT OF FASTENER HOLE AT BS 271, WL 185. THE EXISTING DOUBLER WAS REMOVED IAW SRM 51-30-2. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1, PAGE 6A. A DOUBLER WAS INSTALLED IAW SRM 51-30-2, 51-10-2 AND MM 51-20-11.

Part: FLOORBEAM — CORRODED (BS 1130)

INSPECTION FOUND FLOORBEAM CORRODED AT STA 1130, RBL 26 TO RBL 34 AND LBL 62. THE FLOORBEAM AREAS WERE REPAIRED IAW ECRA 5321-01028 AND ECRA 5321-01027.

Part: ANGLE — CRACKED (BS 1166)

INSPECTION FOUND 8 INCH CRACK IN L-ANGLE AT STA 1166, STRINGER 26L TO 26R. THE ANGLE WAS REMOVED, A REPAIR ANGLE, NUT PLATES, AND RADIUS BLOCK WERE INSTALLED IAW SRM 51-40-3, 51-10-2, 51-30-2 AND MM 51-20-11.

Part: CHANNEL — CRACKED (CARGO DOOR)

INSPECTION FOUND C-1 CARGO DOOR UNDER LOWER LIGHT HAD A PIECE OF PAN CRACKED OUT. THE PAN CHANNEL WAS REMOVED, A REPAIR WAS INSTALLED IAW SRM 52-30-1, 51-10-2, 51-30-2 AND MM 51-20-12.

Part: PANEL — CRACKED (FUSELAGE)

INSPECTION FOUND A .5 INCH CRACK IN PANEL NR 3338. THE CRACKED AREA WAS CUT OUT, A WEB AND DOUBLER REPAIR WAS INSTALLED IAW SRM 51-20-1, 51-30-2, 51-10-2 AND MM 51-20-11.

Part: CHORD — CORRODED (BS 292)

INSPECTION FOUND LT UPPER CHORD CORRODED INSIDE NOSE WHEEL WELL AT STA 292, LBL 20. THE CHORD WAS REMOVED AND A NEW CHORD WAS INSTALLED IAW SRM 51-30-2.

Part: STRINGER — CORRODED (BS 1140-1183)

INSPECTION FOUND STRINGER 25R CORRODED AT STA 1140 TO 1183. THE STRINGER WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-10-3.

Part: STIFFENER — CORRODED (BS 340)

INSPECTION FOUND VERTICAL STIFFENER CORRODED AT RT FUSELAGE STA 340. A NEW STIFFENER WAS INSTALLED IAW ECRA 5300-01196 AND SRM 51-30-2.

Part: ANGLE — CORRODED (WS 491)

INSPECTION FOUND LT WING NR 3 SPOILER L-ANGLE CORRODED AT INBOARD SIDE OF TRANSMISSION, WS 491. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-2 AND 51-10-3.

Part: MECHANISM — OUT OF ADJUST (LT EMER EXIT DR)

THE LT FORWARD OVERWING EMERGENCY EXIT DOOR FAILED PULL CHECK. THE PULL FORCE ON THE DOOR WAS ADJUSTED TO SPECIFICATION IAW MM 52-21-0.

Part: SKIN — CORRODED (BS 560-580)

INSPECTION FOUND CORROSION IN FUSELAGE SKIN UNDER RIVET HEAD AT BS 560 TO 580, STRINGER 5R. THE CORRODED AREA OF SKIN WAS CUT OUT AND A DOUBLER STRAP REPAIR WAS INSTALLED IAW SRM 53-30-8, 51-10-6, 51-20-4, AND 51-30-2.

Part: CHANNEL — CRACKED (NR 3 PYLON)

INSPECTION FOUND A 1.75 INCH CRACK IN NR 3 ENGINE PYLON UPPER FIXED COWL FORWARD END U-CHANNEL. THE CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW SRM 51-40-3.

Part: SEAT TRACK — CORRODED (BS 1136)

INSPECTION FOUND LT SEAT TRACK CORRODED AT STA 1136, LBL 46. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-10-2, 51-10-2, 51-30-2, AND MM 51-20-12.

Part: STRINGER — CORRODED (BS 294.5)

INSPECTION FOUND STRINGER 23R CORRODED AT LOWER NOSE WHEEL WELL RT LAP SEAM STA 294.5. A STRINGER REPAIR WAS INSTALLED IAW SRM 53-10-3, FIGURE 1.

Part: FLOORBEAM — CORRODED (BS 344)

INSPECTION FOUND FLOORBEAM CORRODED AT STA 344, RBL 65 TO LBL 65. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-30-2, 53-10-2, 53-10-8, FIGURE 9, AND MM 51-20-12.

Part: CHORD — CORRODED (BS 351.5)

INSPECTION FOUND SHEAR TIE T-CHORD CORRODED AT STA 351.5, BL 0, WL 148.5. THE T-CHORD WAS REMOVED AND A NEW T-CHORD WAS INSTALLED IAW SRM 51-10-02.

Part: STRAP — CORRODED (BS 1050)

INSPECTION FOUND AFT CARGO PIT LT LOWER SIDE WALL PANEL STRAP CORRODED AT STA 1050. A NEW STRAP WAS INSTALLED IAW SRM 51-10-6.

Part: SKIN — DAMAGED (BS 380-451)

INSPECTION FOUND LIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN AT STA 448 TO 451, STRINGER 25R, AND AT STA 380, STRINGER 23R. DOUBLERS WERE INSTALLED IAW SRM 53-30-3.

Part: SKIN — IMPACTED (CARGO DOOR)

INSPECTION FOUND LIGHTNING STRIKE DAMAGE TO C-1 DOOR SKIN. DOUBLER WAS INSTALLED IAW SRM 52-00-3, FIGURE 4 AND ECRA 5232-01004.

Part: FLOOR PAN — CORRODED (BS 1173)

INSPECTION FOUND CABIN INTERIOR CENTER AISLE FLOOR PAN CORRODED AT BS 1173, RBL 22. THE FLOOR PAN WAS REMOVED AND A NEW FLOOR PAN WAS INSTALLED IAW SRM 51-30-2, 51-10-6, MM 51-20-11.

Part: PANEL — CORRODED (BS 720)

INSPECTION FOUND FLOOR TRANSITION PANEL CORRODED AT BS 720A-720D, STRINGER 26R. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-12.

Part: PANEL — CORRODED (STA 660-720)

INSPECTION FOUND LT TRANSITION PANEL CORRODED IN FORWARD CARGO PIT AT FS 660 TO 720D. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-12.

Part: PANEL — CORRODED (BS 620-720D)

INSPECTION FOUND RT TRANSITION PANEL CORRODED AROUND NUT PLATES IN FORWARD CARGO COMPARTMENT AT STA 620-720D. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-10-2, 51-30-2, AND MM 51-20-12.

Part: SUBFLOOR — CORRODED (BS 340)

INSPECTION FOUND FORWARD LAV SUBFLOOR CORRODED AT STA 340, RBL 42-60. THE LAV SUBFLOOR WAS REMOVED AND REPLACED IAW SRM 51-20-1.

Part: FRAME — CORRODED (BS 1183)

INSPECTION FOUND CORROSION AT HOLE OF LT UPPER DOOR FRAME STA 1183, WL 273, LBL 19.22. REPAIRED IAW ECRA 5310-03765.

Part: BRACKET — CRACKED (BS 303.9)

INSPECTION FOUND A 2 INCH AND 1.5 INCH CRACK IN CABIN FLOOR SUPPORT BRACKET AT STA 303.9, LBL 12. THE FLOOR SUPPORT BRACKET WAS REMOVED AND NEW BRACKET WAS INSTALLED IAW SRM 51-30-2.

Part: INTERCOSTAL — CORRODED (BS 303.9)

INSPECTION FOUND INTERCOSTAL CORRODED AT FS 303.9, LBL 0 TO 12. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-30-2.

Part: SKIN — CORRODED (BS 227-360)

INSPECTION FOUND LT AND RT NOSE SKIN CORRODED AT STA 227-360, STRINGERS 24-29L AND 24-29R. NEW SKIN SECTIONS WERE INSTALLED IAW SRM 51-30-2 AND BOEING DRAWING 65C15724.

Part: PANEL — CORRODED (BS 530-550)

INSPECTION FOUND FORWARD CARGO PIT LT TRANSITION PANEL CORRODED FROM STA 530-550. THE PANEL WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-12.

Part: ANGLE — CRACKED (BS 1213)

INSPECTION FOUND A .5 INCH CRACK IN RT RIB TO SKIN ATTACH ANGLE OF CENTER ENGINE AIR DUCT HOUSING AT STA 1213. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-3 AND MM 51-20-11.

Part: RIB — CRACKED (NR 4 LE SLAT)

INSPECTION FOUND A .5 INCH CRACK IN BOTH INBOARD AND OUTBOARD RIBS OF NR 4 SLAT AT ACTUATOR ROD END ATTACH POINT. THE ACCESS PANEL ON NR 4 SLAT WAS REMOVED IAW SRM 51-30-2. THE CRACKED RIBS WERE REMOVED IAW SRM 51-30-2. NEW RIBS WERE INSTALLED IAW SRM 51-30-4 AND 51-30-2. THE ANTI-ICE DUCTS AND ACCESS PANEL WERE REINSTALLED IAW MM 30-11-81 AND SRM 51-30-2.

Part: SUPPORT — CORRODED (BS 344-360)

INSPECTION FOUND DRAG BRACE SUPPORT DECK AND SIDE T-CHORDS CORRODED AT STA 344-360. THE SUPPORT DECK AND CHORDS WERE REMOVED AND REPLACED IAW SRM 51-30-2 AND BOEING DRAWING 65C15724.

Part: FLOORBEAM — CORRODED (BS 380)

INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 380, RBL 44 TO RBL 60. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A NEW SECTION OF FLOORBEAM AND SPLICE ANGLES WERE INSTALLED IAW SRM 53-10-8, FIGURE 9, 51-20-4, AND 51-10-2.

Part: T-CHORD — CORRODED (BS 259-360)

INSPECTION FOUND LT AND RT FUSELAGE T-CHORDS CORRODED AT STA 259-360. THE T-CHORDS WERE REMOVED AND REPLACED IAW SRM 51-30-2 AND BOEING DRAWING 65C15724.

Part: ANGLE — CRACKED (BS 1203)

INSPECTION FOUND A .5 INCH CRACK IN LEFT RIB TO SKIN ATTACH ANGLE AND A 2.5 CRACK IN RIGHT RIB TO SKIN ATTACH ANGLE OF CENTER ENGINE AIR DUCT HOUSING AT STA 1203. THE ATTACH ANGLES WERE REMOVED AND REPLACED IAW SRM 51-40-3 AND MM 51-20-11.

Part: DOUBLER — SEPARATED (AFT AIRSTAIR)

INSPECTION FOUND LEFT AFT AIRSTAIR EXTERNAL SKIN REPAIR DOUBLER SEPARATING WITH A LOOSE RIVET. THE SEPARATING AREA WAS REMOVED. DOUBLER, FILLER, AND AN ANGLE WERE INSTALLED IAW SRM 51-10-2.

Part: ANGLE — CRACKED (RT WING)

INSPECTION FOUND A 1 INCH CRACK IN OUTBOARD TRAILING EDGE ATTACH ANGLE AT RT WING NR 8 FLAP TRACK. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-40-3, 51-10-2, AND MM 51-20-11.

Part: FRAME — CRACKED (BS 930)

INSPECTION FOUND A .75 INCH CRACK IN RT FUSELAGE FRAME AT STA 930, WL 230 AND 234. THE FRAME WAS REPAIRED IAW ECRA 5310-01397, SRM 51-10-2, 51-30-2, AND MM 51-20-11.

Part: PANEL — CORRODED (BS 530-560)

INSPECTION FOUND RT TRANSITION PANEL CORRODED IN FORWARD CARGO COMPARTMENT AT STA 530-560. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-20-1, 51-10-2, 51-30-2, AND MM 51-20-11.

Part: BRACKET — CRACKED (C2 DOORWAY)

INSPECTION FOUND C2 DOOR FRAME AFT SIDEWALL ATTACH BRACKET CORRODED WITH A .25 INCH CRACK AT RIVET. A REPAIR WAS INSTALLED IAW SRM 51-30-2.

Part: SKIN — CRACKED (LT HORIZ STAB)

INSPECTION FOUND A 2.5 CRACK IN LT HORIZONTAL STABILIZER UPPER AFT TRAILING EDGE SKIN AT HS STA 195. A DOUBLER WAS INSTALLED IAW SRM 51-20-1, 51-40-5, 51-30, AND 51-20-4.

Part: STRAP — CRACKED (BS 930)

INSPECTION FOUND A 1 INCH CRACK IN LT FUSELAGE SPLICE STRAP AT STA 930, WL 228. THE SPLICE STRAP WAS REMOVED AND A NEW STRAP WAS INSTALLED IAW SRM 51-30-2.

Part: SKIN — CRACKED (LT WING)

INSPECTION FOUND A 1 CRACK IN LEADING EDGE SKIN AT LT WING NR 3 SLAT TRACK. THE CRACK WAS STOP DRILLED. A REPAIR WAS INSTALLED IAW SRM 51-30-2.

Part: SPAR — CRACKED (BS 1218)

INSPECTION FOUND A 1.5 CRACK IN BRACKET AT RT LOWER VERTICAL STABILIZER FRONT SPAR, FS 1218 AN ANGLE WAS INSTALLED IAW SRM 51-40-3, FIGURE 1 AND MM 51-20-11.

Part: SUPPORT — CORRODED (BS 1166)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 1166, STRINGER 29R. THE CORRODED AREA WAS CUT OUT. A REPAIR WAS INSTALLED IAW SRM 53-10-5, 51-10-2, AND MM 51-20-11.

Part: ANGLE — CORRODED (BS 1166)

INSPECTION FOUND FLOORBOARD SUPPORT ANGLE CORRODED AT STA 1166 IN AFT PIT, LT SIDE. THE CORRODED SECTION OF SUPPORT ANGLE WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-10-5, FIGURE 6, 51-10-2, 51-30-2, AND MM 51-20-11.

Part: ANGLE — CRACKED (CARGO DOOR)

INSPECTION FOUND A 1 INCH CRACK IN ATTACH ANGLE AT C-1 DOOR FRAME. THE ATTACH ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 360)

INSPECTION FOUND FLOORBEAM CORRODED AT STA 360, RBL 24.75. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-10-08 AND 51-30-02.

Part: SUPPORT — CORRODED (BS 1166)

INSPECTION FOUND FLOORBOARD SUPPORT ANGLE IN AFT PIT CORRODED AT STA 1166, LT SIDE. THE CORRODED AREA OF FLOORBOARD SUPPORT ANGLE WAS REMOVED AND REPAIR PARTS WERE INSTALLED IAW SRM 53-10-5, FIGURE 6, 51-10-2, 51-30-2, AND MM 51-20-11.

Part: BRACKET — CRACKED (BS 1218 & 1228)

INSPECTION FOUND CRACKED BRACKETS AT LT LOWER VERTICAL STABILIZER FRONT SPAR FITTING AT FS 1218 AND STA 1228. THE CRACKS WERE 1.5 AND 1 INCH LONG. ANGLES WERE INSTALLED AT BOTH LOCATIONS IAW SRM 51-40-3, FIGURE 1 AND MM 51-20-11.

Part: STRAP — BROKEN (VERT STAB)

INSPECTION FOUND RT VERTICAL STABILIZER SPAR ATTACH STRAP BROKEN IN HALF AT STA 1213. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-40-2 AND MM 51-20-11.

Part: ANGLE — CORRODED (BS 294.5)

INSPECTION FOUND L-ANGLE ON TOP OF DOGHOUSE CORRODED AT STA 294.5, LBL 12. THE L-ANGLE WAS REMOVED IAW SRM 51-30-2. A NEW L-ANGLE WAS INSTALLED IAW SRM 51-30-2.

Part: SUPPORT — CORRODED (BS 535)

INSPECTION FOUND FORWARD PIT FLOOR SUPPORT ANGLE CORRODED AT STA 535, RBL 20. THE CORROSION WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-40-3, 51-30-2, 51-10-2, AND MM 51-20-11.

Part: FRAME — CRACKED (BS 804.5)

INSPECTION FOUND A 1 INCH CRACK IN FRAME AT STA 804.5, STRINGER 14L. A 1.5 INCH CRACK WAS FOUND IN FRAME AT STA 804.5, STRINGER 14R. AN ANGLE WAS INSTALLED AT EACH LOCATION IAW SRM 51-30-2.

Part: INTERCOSTAL — GOUGED (BS 950)

INSPECTION FOUND INTERCOSTAL WEB GOUGED AT RT FUSELAGE STA 950B BETWEEN STRINGER 29L AND 30L. THE INTERCOSTAL WEB WAS REMOVED. A NEW INTERCOSTAL AND THREE EACH L-ANGLE STIFFENERS WERE INSTALLED IAW SRM 51-40-3, 51-30-2, 51-10-2, AND MM 51-20-0.

Part: SEAT TRACK — CORRODED (BS 1030-1136)

INSPECTION FOUND LT FUSELAGE SEAT TRACK CORRODED AT STA 1030 TO 1136. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-10-5.

Part: FLOORBEAM — CORRODED (BS 1070)

INSPECTION FOUND RT FUSELAGE FLOORBEAM CORRODED AT STA 1070. THE CORRODED AREA WAS CUT OUT, TWO ANGLES AND FILLER WERE INSTALLED IAW SRM 53-10-8, FIGURE 8.

Part: ANGLE — CRACKED (BS 620)

INSPECTION FOUND CORROSION AND A .75 INCH CRACK IN L-ANGLE IN FORWARD PIT AFT OF DOOR AT STA 620, STRINGER 27R. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-20-1, 51-10-2, AND MM 51-20-12.

Part: STRINGER — CORRODED (BS 1166)

INSPECTION FOUND STRINGER 24R CORRODED AT STA 1166. THE CORRODED AREA WAS CUT OUT, A REPAIR WAS INSTALLED IAW SRM 53-10-3, 51-10-2, AND MM 51-20-11.

Part: ANGLE — CORRODED (BS 304-280)

INSPECTION FOUND COCKPIT FLOOR PANEL ATTACH ANGLE CORRODED AT BS 304-280, WL 208.1, LBL 40. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2.

Part: STRINGER — CORRODED (BS 360-380)

INSPECTION FOUND STRINGER 21R CORRODED BETWEEN STA 360 AND 380. THE CORRODED AREA WAS CUT OUT AND A STRINGER REPAIR WAS INSTALLED IAW SRM 53-10-3 AND 53-10-4.

Part: FAIRING — CRACKED (FUSELAGE)

INSPECTION FOUND A 1 INCH CRACK AT NUT PLATE HOLE OF LT BODY FAIRING PANEL NR 3337. THE CRACKED SECTION WAS REMOVED. A REPAIR WAS INSTALLED IAW SRM 53-40-3, FIGURE 1, 51-10-2, 51-30-2, AND MM 51-20-12.

Part: SKIN — CRACKED (RT TE MIDFLAP)

INSPECTION FOUND A 1 INCH CRACK AT FASTENER ON OUTBOARD SKIN APPROXIMATELY 28 INCHES FROM AFT END OF RT OUTBOARD MID FLAP OUTBOARD JACKSCREW FAIRING. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A REPAIR WAS INSTALLED IAW SRM 51-40-2.

Part: LONGERON — CRACKED (BS 965)

INSPECTION FOUND A 1 INCH CRACK LONGERON 13R AT ATTACH ANGLE, STA 965. THE CRACKED AREA WAS CUT OUT IAW SRM 53-02, FIGURE 18. A REPAIR LONGERON AND TWO SPLICES WERE INSTALLED IAW SRM 51-30.

Part: ANGLE — CRACKED (LT ELEVATOR)

INSPECTION FOUND A 1.5 INCH CRACK IN LT ELEVATOR ATTACH ANGLE. AN ANGLE WAS INSTALLED IAW SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 328)

INSPECTION FOUND TOP OF FLOORBEAM CORRODED AT FS 328, LBL 29.5. THE CORRODED SECTION OF FLOORBEAM WAS CUT OUT. REPAIR PARTS WERE INSTALLED IAW SRM 53-10-8, 51-10-2, 51-30-2, AND MM 51-20-11.

Part: FRAME — CORRODED (BS 340)

INSPECTION FOUND RT FUSELAGE FRAME CORRODED AT STA 340. THE CORRODED AREA WAS REMOVED. REPAIR PARTS WERE INSTALLED IAW SRM 51-40-3, 51-10-2, 51-30-02, AND MM 51-20-11.

Part: SEAT TRACK — CRACKED (BS 344)

INSPECTION FOUND A 1 INCH CRACK IN FORWARD END OF LT OUTBOARD SEAT TRACK AT STA 344. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-10-5, FIGURE 7.

Part: COWL — CRACKED (NR 3 ENGINE)

INSPECTION FOUND A 1 BY .25 INCH PIECE OF SKIN CRACKED OUT BY NOSE COWL OF NR 3 ENGINE UPPER FORWARD END OF FIXED COWL. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-40-2, 51-10-2, 51-20-4, 51-30-2, AND MM 51-20-11.

Part: WEB — CRACKED (LT TE MIDFLAP)

INSPECTION FOUND LT WING O/B MID FLAP INBOARD WEB CRACKED AT INBOARD JACKSCREW FAIRING MOUNT BRACKET. THE CRACK WAS .75 LONG. THE CRACKED AREA WAS REMOVED. A DOUBLER WAS INSTALLED IAW SRM 51-40-2, 57-50-1, 51-10-2, 51-30-2, AND MM 51-20-11.

Part: SEAT TRACK — CORRODED (BS 1030)

INSPECTION FOUND CABIN SEAT TRACK CORRODED AT BS 1030, RBL 24. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED. A REPAIR WAS INSTALLED IAW SRM 51-30-2 AND MM 51-20-12.

Part: SKIN — DAMAGED (BS 373)

INSPECTION FOUND LIGHTNING STRIKE ON FUSELAGE SKIN AT BS 373 BETWEEN STRINGER 22R AND 23R. THE DAMAGED AREA WAS CUT OUT IAW SRM 53-30-3. A REPAIR WAS INSTALLED IAW SRM 51-30-2.

Part: SKIN — DAMAGED (STA 389)

INSPECTION FOUND LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN AT STA 389 BETWEEN STRINGERS 23R AND 24R. THE DAMAGED AREA WAS REMOVED IAW SRM 53-30-3. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-30-1 AND 51-20-4.

Part: FRAME — CRACKED (BS 375)

INSPECTION FOUND A 1 AND 1.5 INCH CRACK IN DOOR FRAME AT FS 375 JUST FORWARD OF R-1 DOOR CUTOUT STRINGER 17R ABOVE FLOOR LINE. A DOUBLER, TRIPLER, AND FILLERS WERE INSTALLED IAW SRM 51-40-3, FIGURE 1, 51-30, 51-10-2, AND MM 51-20.

Part: SUPPORT — CRACKED (CARGO COMPT)

INSPECTION FOUND A 1.5 INCH CRACK IN SIDEWALL SUPPORT ON RT SIDE AFT OF C-1 DOOR. THE CRACKED SECTION OF SUPPORT WAS REMOVED. A REPAIR WAS INSTALLED IAW SRM 51-30-0.

Part: PANEL — CRACKED (VERT STAB)

INSPECTION FOUND A .5 INCH CRACK IN LT VERTICAL STABILIZER SLIDER PANEL AND A .75 INCH CRACK IN RT VERTICAL STABILIZER SLIDER PANEL. BOTH PANELS WERE REPLACED IAW SRM 51-20-1, FIGURE 7, 51-10-2, AND MM 51-20-2.

Part: FRAME — CRACKED (BS 910)

INSPECTION FOUND A .5 INCH CRACK IN LT INTERIOR FUSELAGE FRAME AT FS 910 AT STRINGER 15L. THE CRACKED AREA WAS TRIMMED OUT, A REPAIR WAS INSTALLED IAW SRM 51-30-2.

Part: ANGLE — CRACKED (BS 970-990)

INSPECTION FOUND .5 TO 1 INCH CRACKS IN INTERCOSTAL UPPER ANGLE AT FS 970 TO 990, BL 0. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 312)

INSPECTION FOUND FLOORBEAM CORRODED AT STA 312, LBL 29.5. THE CORRODED AREA OF FLOORBEAM WAS CUT OUT. DOUBLERS AND A TEE WERE INSTALLED IAW SRM 53-10-8, 51-10-2, 51-40-3, 51-30-2, AND MM 51-20-1.

Part: STRINGER — CORRODED (BS 477)

INSPECTION FOUND STRINGER 23R CORRODED AT STA 477. THE CORRODED AREA OF STRINGER WAS REMOVED IAW SRM 53-10-3. A REPAIR WAS INSTALLED IAW SRM 51-30-2, 51-10-2 AND MM 51-20-11.

Part: TRACK GUIDE — GOUGED (NR 3 LE SLAT)

INSPECTION FOUND THE OUTBOARD TRACK GUIDE FOR NR 3 SLAT INBOARD TRACK GOUGED. THE TRACK GUIDE WAS REMOVED AND A NEW GUIDE WAS INSTALLED IAW SRM 51-30-2.

Part: FRAME — CORRODED (BS 372)

INSPECTION FOUND FUSELAGE FRAME CORRODED ON FORWARD SIDE AT STA 372 BETWEEN STRINGER 17R AND 20R. THE CORRODED SECTION WAS REMOVED AND A FORMED SECTION REPAIR WAS INSTALLED IAW SRM 51-40-3 AND 51-30-2.

Part: FRAME — CRACKED (CARGO DOORWAY)

INSPECTION FOUND A 1 CRACK AT FASTENER HOLE OF WEB AT NR 2 CARGO DOORWAY FORWARD FRAME BS 950E. A REPAIR WAS INSTALLED IAW SRM 51-30-2.

Part: SUPPORT — CORRODED (BS 1166)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 1166 ABOVE STRINGER 29R. THE CORRODED AREA WAS CUT OUT. A REPAIR WAS INSTALLED IAW SRM 53-10-5, 51-10-2, AND MM 51-20-11.

Part: RIB — CRACKED (LT WING TIP)

INSPECTION FOUND A .5 INCH CRACK IN LT WING TIP RIB AT PANEL NR 8110. THE RIB WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 480)

INSPECTION FOUND FLOORBEAM CORRODED AT STA 480, RBL 24-65. A CHORD, ANGLES, STRAPS, AND STIFFENERS WERE INSTALLED IAW SRM 53-10-8, FIGURE 1.

Part: SUPPORT — CORRODED (BS 1010)

INSPECTION FOUND FLOORBOARD SUPPORT CORRODED WITH TWO .5 INCH CRACKS AT BS 1010 BETWEEN STRINGERS 27R AND 28R. A DOUBLER WAS INSTALLED IAW SRM 51-40-3, FIGURE 1.

Part: SKIN — CRACKED (PAX DOOR)

INSPECTION FOUND L-1 DOOR INNER SKIN CRACKED JUST AFT OF WINDOW OPENING. THE CRACKED AREA WAS CUT OUT. A REPAIR WAS INSTALLED IAW SRM 51-40-2 FIGURE 1, 51-30-2, 52-10-1 FIGURE 1, 51-30-6, 51-30-8, AND 51-40-2 FIGURE 1.

Part: ANGLE — CRACKED (RT WING)

INSPECTION FOUND TWO .625 INCH CRACKS IN RT WING TRAILING EDGE SUPPORT ANGLE UNDER NR 13 SPOILER OUTBOARD END AT SUPPORT ROD LOWER ATTACH POINT. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-40-3, 51-10-2 AND 51-30-2.

Part: SEAT TRACK — CORRODED (BS 460-480)

INSPECTION FOUND SEAT TRACK CORRODED AT STA 460 TO 480, RBL 45. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 53-10-5, FIGURE 1, 51-10-2, AND MM 51-20-12.

Part: FLOORBEAM — CORRODED (BS 950)

INSPECTION FOUND AFT PIT FLOORBEAM CRACKED AT BS 950E ABOVE STRINGER 29L. THE CRACKED SECTION OF FLOORBEAM WAS REMOVED. A REPAIR WAS INSTALLED IAW SRM 51-40-4, 51-30-2, 51-10-2, AND MM 51-20-0.

Part: ANGLE — CORRODED (BS 294.5)

INSPECTION FOUND FLOOR SUPPORT ANGLE CORRODED AT DOGHOUSE, STA 294.5. THE FLOOR SUPPORT ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2.

Part: FRAME — CRACKED (BS 312)

INSPECTION FOUND A 1 INCH CRACK IN FRAME AT STA 312 BELOW SRTINGER 13R. THE CRACKED SECTION OF FRAME WAS REMOVED. A REPAIR WAS INSTALLED IAW SRM 53-10-4, FIGURE 4 AND 51-30-2.

Part: FRAME — CORRODED (BS 340)

INSPECTION FOUND LT FUSELAGE FRAME CORRODED AT STA 340. A REPAIR WAS INSTALLED IAW SRM 51-40-3, FIGURE 1 AND 51-30-2.

Part: SEAT TRACK — CORRODED (BS 410-430)

INSPECTION FOUND SEAT TRACK CORRODED AT STA 410 TO 430, RBL 24. THE SEAT TRACK WAS REPLACED IAW SRM 53-10-5, FIGURE 7.

Part: FRAME — GOUGED (BS 560)

INSPECTION FOUND LT FUSELAGE FRAME GOUGED AT STA 560, WL 294. A REPAIR WAS INSTALLED IAW SRM 53-10-4, FIGURE 1, 51-30-2, 51-10-2, AND MM 51-20-0.

Part: ANGLE — CRACKED (WS 92.8)

INSPECTION FOUND LT WING FORWARD RIB ATTACH ANGLE CRACKED AT WS 92.8. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 57-20-2, 51-10-2, AND 51-30-2.

Part: ANGLE — CRACKED (BS 950)

INSPECTION FOUND RT UPPER WING TO BODY FAIRING SUPPORT STRUCTURE CRACKED ON LOWER ANGLE AND WEB AT FS 950. THE CRACK WAS 2 INCHES LONG. THE ANGLE WAS REMOVED AND THE CRACK WAS STOP DRILLED. A REPAIR WAS INSTALLED IAW SRM 51-30-2, 51-40-3, 51-10-2, 51-00-0 FIGURE 23 AND MM 51-20-1.

Part: ANGLE — CORRODED (BS 1180)

INSPECTION FOUND LT AFT LAV FLOOR LEVEL ANGLE CORRODED AT FS 1180. A NEW ANGLE WAS INSTALLED IAW SRM 51-10-2, 51-30-2, AND 51-20-4.

Part: WEB — CRACKED (BS 740)

INSPECTION FOUND A 3 AND 4 INCH CRACK IN LT CABIN ATTACH WEB AT STA 740, LBL 45. THE CRACKS WERE STOP DRILLED, A DOUBLER WAS INSTALLED IAW SRM 51-10-1, 51-40-2, 53-10-2, AND 51-30-2.

Part: SKIN — CRACKED (RT TE FOREFLAP)

INSPECTION FOUND TWO 2.5 INCH CRACKS AT RIVET HEADS FORWARD OF OUTBOARD SEQUENCE CARRIAGE ATTACH POINT OF RT INBOARD FOREFLAP. A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-30.

Part: SUPPORT — CORRODED (R-1 DOOR)

INSPECTION FOUND R-1 DOOR FORWARD SUPPORT CORRODED. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 52-10-1 AND MM 51-20-11.

Part: SEAT TRACK — CORRODED (BS 950)

INSPECTION FOUND SEAT TRACK CORRODED AT STA 950A-950B, LBL 46. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-5, FIGURE 1, 51-10-2, AND MM 51-20-11.

Part: SEAT TRACK — CORRODED (BS 990-1030)

INSPECTION FOUND RT OUTBOARD SEAT TRACK CORRODED AT STA 990-1030. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 53-10-5, 51-10-2, AND MM 51-20-11.

Part: STIFFENER — CRACKED (LT WING)

INSPECTION FOUND STIFFENER CRACKED AT LT WING TRAILING EDGE FALSE SPAR WHERE FLAP TRACK NR 3 IS LOCATED. THE STIFFENER WAS REMOVED IAW SRM 51-30-2. A NEW STIFFENER WAS FABRICATED AND INSTALLED IAW SRM 51-20-1, 51-10-2, AND 51-30-2.

Part: SEAT TRACK — CORRODED (BS 1050-1060)

INSPECTION FOUND LT SEAT TRACK CORRODED AT STA 1050-1060. A NEW SEAT TRACK WAS FABRICATED AND INSTALLED IAW SRM 53-10-5, FIGURE 1.

Part: SEAT TRACK — CORRODED (BS 950)

INSPECTION FOUND RT OUTBOARD SEAT TRACK CORRODED AT STA 950-950A. THE SEAT TRACK WAS REMOVED. A NEW SEAT TRACK WAS FABRICATED AND INSTALLED IAW SRM 53-10-5, FIGURE 1 AND 7, 51-30-2, 51-10-2, AND MM 51-20-0.

Part: ANGLE — CORRODED (BS 560)

INSPECTION FOUND FLOOR ATTACH ANGLE IN FORWARD CARGO PIT CORRODED AT STA 560, RBL 20. THE CORRODED AREA WAS CUT OUT, AN ANGLE AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-40-4, FIGURE 1.

Part: BRACKET — CORRODED (BS 251.8)

INSPECTION FOUND CORROSION ON TWO L-ANGLE BRACKETS AT AFT SIDE OF STA 251.8, UP SIX INCHES AND TWELVE INCHES FROM FLOOR LEFT SIDE OF COCKPIT. TWO NEW L-ANGLE BRACKETS WERE FABRICATED AND INSTALLED IAW SRM 53-10-2, 51-10-2, AND MM 51-20-11.

Part: FRAME — CORRODED (BS 219.8)

INSPECTION FOUND WEB CORRODED AT FLIGHT DECK FS 219.8, RT FRAME, DIRECTLY BELOW R-2 SLIDING WINDOW. THE WEB WAS REMOVED IAW SRM 51-30-2. A NEW WEB WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-30-2, 51-10-2, AND MM 51-20-11.

Part: WEB — CRACKED (CARGO DOOR)

INSPECTION FOUND A 1.5 INCH CRACK AT AFT LIGHTENING HOLE OF C-1 CARGO DOOR WEB. THE CRACK WAS STOP DRILLED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, PAGE 6B, 51-40-2, 51-10-2, 51-30-2, AND MM 51-20-11.

Part: SPLICE — CORRODED (CARGO COMPT)

INSPECTION FOUND BUTT SPLICE CORRODED, DENTED, AND GOUGED AT NR 3 RT CARGO AREA. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-10-2.

Part: SEAT TRACK — CORRODED (BS 1136)

INSPECTION FOUND SEAT TRACK CORRODED AT STA 1136, RBL 25. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS FABRICATED AND INSTALLED IAW SRM 53-10-5, 51-30-5, 51-10-2, 51-30-2, AND MM 51-20-11.

Part: SILL — CORRODED (R-2 DOOR)

INSPECTION FOUND R-2 DOOR LOWER SILL CORRODED AT BS 1065. THE CORRODED AREA WAS CUT OUT IAW SRM 51-40-3. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, 51-30-2, AND MM 51-20-11.

Part: ANGLE — CORRODED (BS 360)

INSPECTION FOUND FUSELAGE FRAME ANGLE CORRODED AT STA 360 BETWEEN STRINGER 17R AND 20R. THE ANGLE WAS REMOVED IAW SRM 51-30-2. THE CORROSION WAS REMOVED IAW SRM 51-10-6. AN ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, AND 51-30-2.

Part: ANGLE — CRACKED (WS 130)

INSPECTION FOUND A CRACK ON THE INBOARD SIDE OF L/E CAVITY BULKHEAD LOWER ANGLE APPROXIMATELY TWENTY INCHES AFT OF KRUEGER FLAP HINGE LINE AT LT WING LEADING EDGE STA 130. THE ANGLE WAS REMOVED AND A NEW REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-30, 51-10-2, AND MM 51-20-11.

Part: SEAT TRACK — CORRODED (BS 344-384)

INSPECTION FOUND FORWARD END OF LT INBOARD SEAT TRACK CORRODED AT STA 344 TO 384. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS FABRICATED AND INSTALLED IAW SRM 53-10-5, 51-10-2, 51-30-2, AND MM 51-20-0.

Part: ANGLE — CRACKED (RT WING)

INSPECTION FOUND TWO ATTACH ANGLES CRACKED UNDER OUTBOARD END OF NR 12 SPOILER AT SUPPORT ROD LOWER ATTACH POINT OF RT WING TRAILING EDGE. THE ATTACH ANGLES WERE REMOVED. TWO NEW ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, 51-30-2, AND MM 51-20-0.

Part: INTERCOSTAL — CRACKED (BS 720)

INSPECTION FOUND THREE CRACKS IN UPPER FLANGE OF INTERCOSTAL BETWEEN FS 720 AND 720A. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, 51-30-2, AND MM 51-20-11.

Part: PAN WEB — CORRODED (LT AFT LAVATORY)

INSPECTION FOUND LT AFT LAV PAN WEB CORRODED. THE CORRODED AREA WAS REMOVED IAW SRM 51-10-6. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-10-2, 51-30-2, AND MM 51-20-11.

Part: ACCESS PLATE — CORRODED (CENTER WING)

INSPECTION FOUND WING CENTER SECTION LOWER SKIN PLENUM ASSEMBLY INSPECTION ACCESS PLATE CORRODED ON FORWARD RT SIDE. A NEW ACCESS PLATE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-2, 51-20-1, AND MM 51-20-11.

Part: ANGLE — CRACKED (NR 8 TE FLAP)

INSPECTION FOUND APPROXIMATELY A 2 CRACK IN RT WING NR 8 FLAP TRACK INBOARD TRAILING EDGE ATTACH ANGLE. A NEW ATTACH ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, 51-30-2, AND MM 51-20-11.

Part: ANGLE — CRACKED (NR 2 LE SLAT)

INSPECTION FOUND APPROXIMATELY A 2 CRACK IN LT WING LEADING EDGE SLAT NR 2 INBOARD SLAT TRACK OUTBOARD SIDE L ANGLE. THE ANGLE WAS REPLACED IAW SRM 57-30-4, 51-20-12, AND 51-30-2.

Part: SUPPORT — CRACKED (BS 760)

INSPECTION FOUND A 5/8 CRACK IN OUTBOARD END OF FLOORBOARD SUPPORT AT BS 760, RBL 45.5. THE FLOORBOARD SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-5 AND 51-30-2.

Part: SUPPORT — CRACKED (BS 760)

INSPECTION FOUND A 2 INCH CRACK IN RT INBOARD END OF FLOOR SUPPORT AT BS 760, BL 0. THE CRACKED SECTION OF FLOOR SUPPORT WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, FIGURE 1 AND 51-30-2.

Part: BRACKET — CRACKED (NR 7 FLAP TRACK)

INSPECTION FOUND APPROXIMATELY A 2 INCH CRACK IN RT WING INBOARD NR 7 FLAP TRACK TRAILING EDGE ATTACH BRACKET. THE ATTACH BRACKET WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-30-2, 51-10-2, AND MM 51-20-0.

Part: SPAR CHANNEL — CRACKED (LT WING)

INSPECTION FOUND U-CHANNEL AT REAR SPAR OF LT WING LOWER SURFACE JUST INBOARD OF SECOND OUTBOARD FLAP TRANSMISSION WORN AND CRACKED OUT OF NUT PLATE HOLE. THE CHANNEL WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, FIGURE 1 AND 51-30-2.

Part: PAN — CRACKED (BS 740-760)

INSPECTION FOUND AFT EDGE OF PRESSURE PAN CRACKED APPROXIMATELY TWO INCHES AT FASTENER HOLE STA 740-760, LT SIDE. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-10-2, 51-30-2, AND MM 51-20-11.

Part: SKIN — CRACKED (BS 1183)

INSPECTION FOUND A 1.25 INCH CRACK IN FUSELAGE SKIN AT STA 1183, WL 189, RBL 30. A DOUBLER AND TRIPLER WERE FABRICATED AND INSTALLED IAW BOEING 727 DRAWING NR 65C31446-3.

Part: STRAP — CORRODED (BS 555-630)

INSPECTION FOUND BUTT STRAP IN FORWARD CARGO PIT CORRODED AT LT STA 555-630. A NEW BUTT STRAP WAS FABRICATED AND INSTALLED IAW SRM 51-20-1, FIGURE 7, 51-10-2, AND MM 51-20-12.

Part: STRAP — CORRODED (BS 950)

INSPECTION FOUND BUTT STRAP CORRODED IN AFT PIT AT STA 950A. A NEW STRAP WAS FABRICATED AND INSTALLED IAW SRM 51-20-1, PAGE 7, 51-10-2, PAGE 4, AND MM 51-20-12, PAGE 710.

Part: SPLICE — CORRODED (CARGO COMPT)

INSPECTION FOUND BUTT SPLICE NR 3 IN FORWARD CARGO COMPARTMENT ON RT SIDE CORRODED. A NEW BUTT SPLICE WAS FABRICATED AND INSTALLED IAW MM 51-20-1, 51-10-2, AND 51-20-12.

Part: SPLICE — CORRODED (CARGO COMPT)

INSPECTION FOUND BUTT SPLICE NR 2 IN FORWARD CARGO COMPARTMENT ON RT SIDE CORRODED. A NEW BUTT SPLICE WAS FABRICATED AND INSTALLED IAW SRM 51-20-1, FIGURE 7, 51-10-2, AND MM 51-20-12.

Part: STRAP — CORRODED (BS 540)

INSPECTION FOUND FORWARD CARGO PIT FLOOR SUPPORT STRAP CORRODED WITH ELONGATED HOLES AT STA 540. A SUPPORT STRAP WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-10-2.

Part: FLOOR — PUNCTURED (BS 640-720)

INSPECTION FOUND A HOLE IN FORWARD PIT FLOOR PANEL AT STA 640-720. THE DAMAGED AREA WAS CUT OUT. TWO DOUBLERS AND REPAIR FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-10-7, 51-10-2, 51-30-2, AND MM 51-20-11.

Part: TIP — CRACKED (LT WING TIP)

INSPECTION FOUND LT WING TIP INBOARD ACCESS PANEL 8112 DEFORMED AND CRACKED. A NEW PANEL WAS FABRICATED AND INSTALLED IAW SRM 51-20-01.

Part: FLOOR — PUNCTURED (BS 950)

INSPECTION FOUND A PUNCTURE IN AFT CARGO FLOOR PANEL AT STA 950E. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-2, 53-10-7, 51-10-2, 51-30-2, AND MM 51-20-11.

Part: SKIN — DENTED (NLG DOOR)

INSPECTION FOUND A DENT IN AFT LOWER OUTBOARD SKIN OF NLG LT FORWARD DOOR. THE DOOR WAS REPAIRED IAW SRM 52-80-2 AND 51-30-2.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

INSPECTION FOUND BOTH INTERIOR LT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. THE LT OVERWING EMERGENCY EXIT LIGHT POWER SUPPLY WAS REMOVED AND REPLACED.

Part: BOLT — FAILED (LT TE FOREFLAP)

WHEN GEAR WAS EXTENDED WITH FLAPS AT 25 DEGREES ON FINAL APPROACH TO JAX, THE AIRCRAFT ROLLED LEFT. THE PILOT MAINTAINED LEVEL FLIGHT USING FULL RT AILERON AND ALMOST FULL RT RUDDER. THE AIRCRAFT LANDED AT JAX WITHOUT INCIDENT. MAINTENANCE FOUND AN EIGHT FOOT SECTION OF THE LT OUTBOARD TRAILING EDGE FOREFLAP MISSING. ENGINEERING FOUND AN ATTACHMENT BOLT FOR THE FOREFLAP HAD FAILED. THE REMAINING BOLTS WERE INSPECTED AND FOUND IN GOOD CONDITION. THE LOST SECTION OF FOREFLAP HAS NOT BEEN RECOVERED. THE AIRCRAFT WAS TAKEN OUT OF SERVICE FOR REPAIR.

Part: FUEL PANEL — LOOSE (LT WING)

A FUEL LEAK WAS REPORTED COMING FROM LT WING AFTER TAKEOFF FROM EWR. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LOOSE SCREWS AT THE NR 4 UNDERWING FUEL ACCESS PANEL OF THE LT WING. ALL SCREWS WERE RETORQUED AND LEAK CHECK WAS GOOD.

Part: SKIN — DENTED (HORIZ STAB)

RIGHT HORIZ STABILIZER DENT IN LOWER SKIN BY FRONT SPAR 30 FROM TIP. CUT OUT DENTED AREA. FABRICATED AND INSTALLED DOUBLER PER SRM 55-10-3.

Part: SKIN — CORRODED (BS 500)

SKIN BULGED AT RIGHT SIDE FUSELAGE STA 500 AND STR 27. REMOVED EXISTING DOUBLER. CUT OUT CORRODED SKIN. FABRICATED AND INSTALLED DOUBLER PER SRM 53-30-3.

Part: ANGLE — CRACKED (AFT AIRSTAIR)

STATION 1263 RT ANGLES CRACKED ON BOTH FACES BELOW AIRSTAIR ACTUATOR SUPPRT BRACKET. REMOVED AND REPLACED ANGLES PER SRM 51-10-1 AND 51-30-2.

Part: SKIN — CRACKED (LEFT WING)

APPROX .125 INCH CRACK COMING FROM TWO FLUSH RIVITS AT LEFT WING NR 3 SLAT UPPER SKIN 65 FROM O/B END. CUT OUT CRACKED SKIN. FABRICATED AND INSTALLED DOUBLER PER SRM 57-50-3.

Part: BATTERY — DISCHARGED (CABIN)

ESCAPE PATH LIGHT INOP AT ROW 24. REPAIRED SHORTED WIRING AND REPLACED BATTERY PACK.

Part: BATTERY — DIRTY (CABIN)

OVERHEAD EMERGENCY EXIT LIGHT ABOVE SEAT 17 INOP. CLEANED CONTACTS AT BATTERY PACK AND REINSTALLED.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHTS, OVERHEAD AT FORWARD CABIN INOP. REMOVED AND REPLACED BATTERY PACK.

Part: SKIN — CRACKED (LT ELEV TAB)

LEFT ELEVATOR CONTROL TAB SKIN LEADING EDGE CRACKED 1.5 INCH JUST ABOVE NUMBER 2 HINGE FROM INBOARD. REMOVED AND REPLACED TAB PER MM 27-30-0.

Part: SKIN — CRACKED (LT ELEVATOR)

LEFT ELEVATOR LOWER SKIN AT PANEL 9314 AND 9313 CRACKED (2 AND 3). FABRICATED AND INSTALLED REPAIR DOUBLERS PER SRM 55-20-3.

Part: SKIN — CRACKED (VERT STAB)

VERT STAB RT SKIN JUST BELOW PANEL 9524 CRACKED IN TWO PLACES (2 AND 3). CUT OUT CRACKED SKIN. FABRICATED AND INSTALLED FILLER AND DOUBLER PER EC/RA 5530-01190.

Part: HYD LINE — LEAKING (BHYD SYST)

THE AIRCRAFT LOST B-SYSTEM HYDRAULIC QUANTITY WHILE IN FLIGHT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LEAKAGE IN B-SYSTEM HYDRAULIC RETURN LINE AT CASE DRAIN TEE FITTING. A FLEX LINE WAS INSTALLED AND A DIP WAS ISSUED TO REPLACE THE FLEX LINE WITH A PERMANENT LINE. THE HYDRAULIC SYSTEM WAS SERVICED. LEAK AND OPERATIONAL CHECKS WERE GOOD.

Part: HYD LINE — LEAKING (B-HYD SYST)

BOTH B-SYSTEM LOW PRESSURE LIGHTS ILLUMINATED WITH B-SYSTEM SHOWING ONE GALLON IN RESERVOIR DURING CRUISE PORTION OF FLIGHT. THE A-SYSTEM SHOWED 3 GALLONS AND WENT TO 2.25 GALLONS OVER THE NEXT 1.5 HOURS. THE FLIGHT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUND HYDRAULIC RETURN LINE IN HYDRAULIC BAY LEAKING. THE HYDRAULIC RETURN LINE WAS REMOVED AND REPLACED. IN ADDITION, BOTH THE NR 1 AND NR 2 ELECTRIC B-PUMPS WERE REMOVED AND REPLACED. THE HYDRAULIC SYSTEM WAS SERVICED TO FULL, LEAK AND OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (COCKPIT)

TWO CEILING EXIT LIGHTS BEHIND FIRST CLASS PARTITION WERE FOUND INOPERATIVE. MAINTENANCE FOUND THE 28V POWER FAIL CIRCUIT BREAKER NOT FULLY ENGAGED. THE CIRCUIT BREAKER WAS RESET AND OPERATION CHECKED GOOD. THE COCKPIT EMERGENCY EXIT LIGHT WAS ALSO FOUND INOPERATIVE. THE LIGHT WAS REMOVED AND REPLACED.

Part: SKIN — CRACKED (BS 720)

INSPECTION FOUND A .75 INCH CRACK ON FUSELAGE SKIN LAP JOINT AT STA 720, STRINGER 26R. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-6 AND 53-30-3.

Part: ACTUATOR — DAMAGED (NLG STEERING)

THE NOSE GEAR LOCKED UP IN 90 DEGREE POSITION AFTER TAKING RUNWAY AND CREW WAS UNABLE TO STEER AIRCRAFT. THE AIRCRAFT WAS TOWED BACK TO THE GATE. MAINTENANCE FOUND THE NOSE GEAR LT STEERING ACTUATOR ROD END STRIPPED. THE NOSE GEAR LT STEERING ACTUATOR WAS REMOVED AND REPLACED. THE RT STEERING ACTUATOR AND METERING VALVE WERE REPLACED AS A PRECAUTIONARY MEASURE. AN OPERATIONAL CHECK AND TEST OF THE STEERING SYSTEM WAS PERFORMED IAW MM 32-51-21 AND THE SYSTEM CHECKED GOOD WITH NO LEAKS NOTED.

Part: SKIN — CRACKED (LT TE FLAP)

INSPECTION FOUND A 1.5 INCH CRACK IN LT WING INBOARD FLAP INNER SKIN AT AFT END OF OPENING FOR UPPER ACCESS PANEL NR 8443. A NEW PART WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.

Part: RIB — CRACKED (LT WING)

INSPECTION FOUND A 10 INCH CRACK IN OUTBOARD RIB AT NR 5 SLAT ACTUATOR ATTACH POINT. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-3.

Part: RIB — CRACKED (RT WING TIP)

INSPECTION FOUND A 6 INCH CRACK IN FORWARD END CLOSURE RIB AND LOWER ANGLE OF RT WING TIP ASSEMBLY. THE CRACKED AREA WAS CUT OUT, REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-40-2.

Part: SKIN — PUNCTURED (RT TE MID FLAP)

INSPECTION FOUND RT WING INBOARD TRAILING EDGE MID FLAP PUNCTURED AT UPPER SURFACE OF TRAILING EDGE INBOARD END. THE DAMAGED AREA WAS CUT OUT AND A HOT BOND REPAIR WAS ACCOMPLISHED IAW SRM 51-40-6.

Part: FRAME — CRACKED (BS 1303)

INSPECTION FOUND A 1 INCH CRACK IN LEFT AND RIGHT CORNERS OF FRAME WEB ON AFT FACE OF STA 1303 FRAME, ABOVE S-DUCT. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2.

Part: RIB — CRACKED (RT WING TIP)

INSPECTION FOUND A 6 INCH CRACK IN FORWARD END CLOSURE RIB AND UPPER ANGLE OF RT WING TIP ASSEMBLY. THE CRACKED AREA WAS CUT OUT. REPLACEMENT PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-30-2.

Part: SKIN — DELAMINATED (RT TE FLAP)

INSPECTION FOUND RT WING TRAILING EDGE FLAP LOWER SKIN DELAMINATING IN TWO AREAS INBOARD OF INBOARD FAIRING. A FIBERGLASS OVERLAY REPAIR WAS ACCOMPLISHED IAW SRM 51-40-8.

Part: SKIN — CHAFED (RT WING)

INSPECTION FOUND A HOLE CHAFED IN SKIN FORWARD OF FLUX VALVE, RT WING TIP. THE DAMAGED AREA WAS CUT OUT, A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-20-5.

Part: STRINGER — CRACKED (WS 686.5)

INSPECTION FOUND A .5 INCH CRACK IN STRINGER INSIDE LT WING TANK AT STA 686.5. A REPAIR WAS FABRICATED AND INSTALLED IAW EA 576201050.

Part: FRAME — CORRODED (CARGO DOOR)

INSPECTION FOUND AFT CARGO C-3 FORWARD DOOR FRAME CORRODED IN AREA OF STRINGER 26. THE CORROSION WAS REMOVED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-30-2.

Part: SKIN — DENTED (BS 1243)

INSPECTION FOUND LT FUSELAGE SKIN DENTED JUST BELOW NR 1 ENGINE AT STA 1243. THE DENTED AREA WAS CUT OUT. A FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3.

Part: SKIN — DELAMINATED (LT TE MID FLAP)

INSPECTION FOUND THE OUTBOARD TRAILING EDGE OF LEFT OUTBOARD MID FLAP DELAMINATED. THE DELAMINATED CORE WAS CUT OUT AND A HOT BOND REPAIR WAS ACCOMPLISHED IAW SRM 51-40-6.

Part: FAIRING — PULLED LOOSE (AILERON TAB)

INSPECTION FOUND FAIRING PULLED LOOSE FROM BOTTOM OF LEFT INBOARD AILERON TAB. THE FASTENERS WERE REMOVED, THE FAIRING WAS REBONDED, AND THE FASTENERS WERE REINSTALLED IAW SRM 51-30-2.

Part: RIB — CRACKED (LT WING)

INSPECTION FOUND A .25 INCH CRACK IN RIB OF NR 5 SLAT ACTUATOR ATTACH POINT INBOARD SIDE. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 51-40-3.

Part: THRESHOLD — CRACKED (BS 1178)

INSPECTION FOUND CORROSION AND CRACKS ON THRESHOLD STRUCTURE BELOW CABIN FLOOR AT BS 1178, LBL 18 TO RBL 18. A NEW THRESHOLD WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.

Part: SKIN — CRACKED (LT TE FORE FLAP)

INSPECTION FOUND OUTBOARD LEADING EDGE OF LEFT INBOARD FOREFLAP SKIN CRACKED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-50-4.

Part: SKIN — CRACKED (LT TE FORE FLAP)

INSPECTION FOUND LEADING EDGE OF LEFT OUTBOARD FOREFLAP SKIN CRACKED AND GALLED IN TWO PLACES AT OUTBOARD SEQUENCE CARRIAGE POSITION. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-50-4.

Part: WIRE — DAMAGED (CABIN)

THE EMERGENCY PATH LIGHTING BETWEEN SEAT ROWS 6 ABC - 8 ABC WERE FOUND INOPERATIVE DURING AN EMERGENCY LIGHT OPERATIONAL CHECK. MAINTENANCE FOUND A FLOOR HARNESS FEEDER WIRE DAMAGED. THE WIRE WAS REPAIRED AND OPERATIONAL CHECKS WERE GOOD IAW MM 33-51-0.

Part: TIP — CRACKED (LT WING)

INSPECTION FOUND A .50 INCH CRACK IN LOWER OUTBOARD EDGE OF LT WING TIP. THE CRACKED AREA WAS CUT OUT. A DOUBLER AND FILLER REPAIR WERE FABRICATED AND INSTALLED IAW SRM 57-20-5.

Part: TIP — CRACKED (RT WING)

INSPECTION FOUND A .25 INCH CRACK IN RT WING TIP UPPER SURFACE, JUST FORWARD OF PANEL 6641. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.

Part: SKIN — CRACKED (BS 520)

INSPECTION FOUND A 5 INCH CRACK WITH CORROSION IN SKIN LAP JOINT AT STA 520, S24L. REPAIRED IAW SRM 53-30-03, FIGURE 5.

Part: FLOOR BEAM — CORRODED (BS 1130/1148)

INSPECTION FOUND FLOOR BEAM CORRODED AT CEILING OF AFT CARGO COMPARTMENT, STA 1130 AND 1148, RT SIDE OF AIRCRAFT. THE FLOOR BEAM WAS REPAIRED IAW ECRA 5310-03288.