N382SW

Part: MOUNT — MISSING (R1 DOOR) · airframe 71,251 hrs · 57,572 cycles

R1 DOOR EMERGENCY EVAC SLIDE MOUNT MISSING. R&R SLIDE CONTAINER MOUNT ASSEMBLY PER MT.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 70,950 hrs · 57,357 cycles

FORWARD OUTBOARD FLASHLIGHT INOP. R&R BATTERY PER AMM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 70,751 hrs · 57,206 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT BS 96.0, 1.5 INCHES AFT OF FORWARD LEADING EDGE. REPAIRED SKIN PER EA.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 70,544 hrs · 57,058 cycles

FORWARD EMERGENCY EXIT LENS CRACKED. R & R THE LENS IAW AMM.

Part: LENS — BROKEN (EXIT SIGN) · airframe 70,409 hrs · 56,966 cycles

AFT CABIN OVERHEAD AISLE EXIT SIGN CLEAR LENS BROKEN. R & R LENS IAW MM.

Part: LENS — MISSING (CABIN) · airframe 69,600 hrs · 56,420 cycles

FORWARD OVERHEAT EMER LIGHT LENS MISSING. INSTALLED LENS IAW SIP.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 60,133 hrs · 47,289 cycles

DIVERSION AT CRUISE, FIRE WARNING LIGHT ILLUMINATED & BELL SOUNDED FOR APPROX 5 SECONDS. ALL LIGHTS & INDICATIONS ON THE FIRE PANEL WERE ILLUMINATED DURING THE WARNING AS IF THE LAMP TEST BUTTON HAD BEEN PUSHED. R & R CARGO FIRE PANEL.

Part: STIFFENER — CRACKED (LT AILERON) · airframe 69,174 hrs · 56,144 cycles

LEFT WING AILERON STIFFENER CRACKED AT NR 2 HINGE FROM INBD. R & R STIFFENER IAW SRM.

Part: PLATE — CRACKED (LT WING) · airframe 68,323 hrs · 55,596 cycles

LEFT WING WIGGLE PLATE ATTACHED TO LOWER WING SKIN TE AT APPROX RSS 248 CRACKED. R & R WIGGLE PLATE IAW SRM.

Part: SPAR — CRACKED (LT WING) · airframe 68,323 hrs · 55,596 cycles

LEFT WING LOWER REAR SPAR, LOWER FASTENER ROW AT RSS 204, FASTENER HOLE CRACKED COMMON TO THE WEB. REPAIRED WEB IAW ER & EA.

Part: SKIN — CRACKED (RT WING) · airframe 68,323 hrs · 55,596 cycles

RIGHT WING UPPER SKIN, CRACKED AT 4 FASTENER HOLES, AFT ROW COMMON TO NUTPLATE ATTACH STRIP, BETWEEN RSS 254 - 267.5. REPAIRED SKIN IAW ER & EA.

Part: FITTING — CRACKED (RT MLG) · airframe 68,323 hrs · 55,596 cycles

RIGHT MLG BEAM, FWD FITTING CRACKED AT FASTENER HOLE, SECOND ROW FROM INBD, THIRD FROM TOP. R & R FITTING IAW ER & EA.

Part: SPAR — CRACKED (LT WING) · airframe 68,323 hrs · 55,596 cycles

LEFT WING REAR SPAR WEB CRACKED, COMMON TO LG SUPPORT BEAM, AFT SUPPORT FITTING RSS 225.54, UPPER ROW FASTENER 5. REPAIRED WEB IAW EA.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 68,323 hrs · 55,596 cycles

ATTACH ANGLE, CORRODED AT BS 727E, STRINGER 27L, OTBD ANGLE. R & R ANGLE IAW SRM & ER.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 68,323 hrs · 55,596 cycles

STRINGER SPLICE CRACKED AT BS 360, STRINGER 8L. R & R SPLICE IAW SRM & DWG.

Part: SPAR — CRACKED (RT WING) · airframe 68,323 hrs · 55,596 cycles

RIGHT WING REAR SPAR, CRACKED UPPER ROW 1ST INBD & 1ST OTBD OF RSS 224.14. REPAIRED SPAR IAW EA.

Part: WEB — CRACKED (RT WING) · airframe 68,323 hrs · 55,596 cycles

RIGHT WING WEB CRACKED, UPPER ROW 1ST INBD & 1ST OTBD OF RSS 224.14. REPAIRED WEB IAW EA & ER.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,323 hrs · 55,596 cycles

FLOORBEAM VERTICAL STIFFENER ANGLE CRACKED AT BS 328, RBL 34. R & R ANGLE IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,323 hrs · 55,596 cycles

STRINGER CLIP CRACKED AT BS 360, STRINGER 11L. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,323 hrs · 55,596 cycles

STRINGER CLIP CRACKED AT BS 360, STRINGER 8L. R & R CLIP IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 68,323 hrs · 55,596 cycles

FORWARD ENTRY DOOR MOPSILL SUPPORT WEB LOWER SURFACE CORRODED, BETWEEN BS 344 - 350. REPAIRED WEB IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,323 hrs · 55,596 cycles

STRINGER CLIP CRACKED AT BS 277, STRINGER 15R. R & R CLIP IAW SRM.

Part: SPAR — CRACKED (LT WING) · airframe 68,323 hrs · 55,596 cycles

LEFT WING UPPER REAR SPAR CHORD CRACKED AT RSS 224.14. REPAIRED CHORD IAW ATS ER & EA.

Part: LENS — MISSING (CABIN) · airframe 68,014 hrs · 55,371 cycles

MID CABIN CEILING EMER EXIT LIGHT, LOWER LENS COVER ASSEMBLY MISSING. R & R COVER ASSEMBLY IAW SRM.

Part: LENS — MISSING (CABIN) · airframe 67,844 hrs · 55,248 cycles

LEFT BULLNOSE EMER LIGHT LENS MISSING AT ROW 14. INSTALLED LENS IAW SIP.

Part: COVER — LOOSE (CABIN) · airframe 67,708 hrs · 55,149 cycles

RIGHT OVERWING EMER EXIT LIGHT COVER LOOSE AT ROW 12. SECURED COVER IAW SIP.

Part: SKIN — CRACKED (L1 DOOR) · airframe 67,474 hrs · 54,982 cycles

L1 DOOR INNER SKIN VERTICALLY CRACKED. REPAIRED SKIN IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 67,082 hrs · 54,711 cycles

FUSELAGE CHORD CRACKED AT STATION 1066, BETWEEN STRINGER 6L & 7L. REPAIRED CHORD IAW SRM.

Part: FUEL CAP — LEAKING (RT WING) · airframe 66,724 hrs · 54,458 cycles

DIVERSION, FUEL LEAK OFF RT WING. R & R FUEL CAP IAW SIP.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 66,450 hrs · 54,281 cycles

NUMBER 2 LE SLAT DELAMINATED AT UPPER SKIN. REPAIRED NR 2 SLAT IAW EA.

Part: SLAT — DELAMINATED (LT WING) · airframe 66,450 hrs · 54,281 cycles

LEFT WING NR 2 LE SLAT DELAMINATED AT OTBD UPPER TE. REPAIRED NR 2 SLAT IAW SRM.

Part: SIGN — LOOSE (CABIN) · airframe 66,342 hrs · 54,213 cycles

RIGHT EMER EXIT SIGN LOOSE. SECURED SIGN IAW SIP.

Part: LENS — LOOSE (EXIT SIGN) · airframe 66,264 hrs · 54,163 cycles

RIGHT OVERWING EXIT EMER SIGN LENS ABOVE DOOR LOOSE. SECURED LENS IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 66,112 hrs · 54,053 cycles

FORWARD PAX DOOR LOWER EXIT LIGHT LENS COVER MISSING. R & R COVER IAW AMM.

Part: PLATE — LOOSE (CABIN) · airframe 66,040 hrs · 54,006 cycles

RIGHT EMER EXIT LIGHT COVER PLATE LOOSE. R & R PLATE IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 66,023 hrs · 53,995 cycles

RIGHT OVERWING EXIT SIGN LOOSE. SECURED SIGN IAW SIP.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,810 hrs · 53,858 cycles

FUSELAGE SKIN CRACKED AT L1 DOOR, UPPER HINGE CUT OUT, APPROX STATION 315, STRINGER 10L. REPAIRED SKIN IAW EA.

Part: WINDOW — DELAMINATED (COCKPIT) · airframe 65,694 hrs · 53,779 cycles

R2 COCKPIT WINDOW AFT CORNER DELAMINATED AROUND BURN MARK. R & R NR 2 WINDOW ASSEMBLY IAW MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 65,246 hrs · 53,477 cycles

FUSELAGE FRAME CRACKED AT STATION 348 STRINGER 16L, L1 DOOR CUT OUT. REPAIRED FRAME IAW EA.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 65,246 hrs · 53,477 cycles

L1 DOOR CUT OUT AFT LOWER SCUFF PLATE ATTACH ANGLE CRACKED STATION 351. R & R ANGLE IAW SRM.

Part: PLATE — CRACKED (TE FLAP) · airframe 65,246 hrs · 53,477 cycles

LEFT WING INBD FLAP OTBD CARRIAGE GIMBLE CLOCKING PLATE CRACKED AT LOWER BOLT. R & R PLATE IAW CMM.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 65,246 hrs · 53,477 cycles

STATION 1016 FWD SIDE OF PRESS WEB CORRODED AT LOWER 2 FASTENER ROWS RBL 12 TO LBL 12. REPAIRED WEB IAW AE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,246 hrs · 53,477 cycles

LEFT FUSELAGE FRAME CRACKED AT STATION 727 STRINGER 18A. R & R FRAME ASSEMBLY IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,246 hrs · 53,477 cycles

RIGHT FUSELAGE FRAME CRACKED AT STATION 727 STRINGER 18A. R & R FRAME ASSEMBLY IAW EA.

Part: WINDOW — ARCED (COCKPIT) · airframe 63,278 hrs · 52,081 cycles

DIVERSION DECLARED, EMERGENCY L1 WINDOW ARCED IN FLIGHT. R & R WINDOW IAW MM.

Part: DOOR — OUT OF ADJUST (L1) · airframe 62,853 hrs · 51,802 cycles

L1 DOOR OUT OF ADJUSTMENT. ADJUSTED DOOR IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,709 hrs · 51,701 cycles

EMERGENCY EXIT BULLNOSE LIGHT INOPERATIVE AT 2 DEF. RELAMPED IAW MM.

Part: ANGLE — CRACKED (FLAP TRACK) · airframe 62,709 hrs · 51,701 cycles

LT WING NR 3 FLAP TRACK FAIRING INTERNAL AREA ANGLE CRACKED. R & R ANGLE IAW SRM & DRAWING.

Part: PLATE — WORN (R2 DOOR) · airframe 62,709 hrs · 51,701 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR PLATE WORN. R &R PLATE ASSEMBLY IAW MM.

Part: PLATE — WORN (L2 DOOR) · airframe 62,709 hrs · 51,701 cycles

L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR PLATE WORN. R & R PLATE ASSEMBLY IAW MM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

AFT CARGO FLOOR ANGLE CRACKED AT BS 787 TO BS 807, STRINGER 17R. R & R ANGLE IAW SRM.

Part: PLATE — CRACKED (KRUEGER FLAP) · airframe 62,709 hrs · 51,701 cycles

LT WING KRUGER FLAP INTERNAL AREA PLATE CRACKED. R & R PLATE IAW SRM.

Part: ACCESS PANEL — CRACKED (VERTICAL STAB) · airframe 62,709 hrs · 51,701 cycles

VERTICAL STABILIZER ACCESS PANEL 9501L CRACKED. R & R PANEL IAW SRM & DRAWING.

Part: SLAT — DELAMINATED (RT WING) · airframe 62,709 hrs · 51,701 cycles

RT WING NR 4 SLAT TE DELAMINATED INBD END. REPAIRED NR 4 SLAT IAW SRM.

Part: DOUBLER — CRACKED (TE FLAP) · airframe 62,709 hrs · 51,701 cycles

RT WING INBD SIDE FORE FLAP OTBD INTERNAL DOUBLER CRACKED AT LEVEL WBL 220.00. R & R DOUBLER IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

ANGLE CRACKED AT BS 947.5, STRINGER 22R. R & R ANGLE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (LT WING) · airframe 62,709 hrs · 51,701 cycles

LT WING TE ANGLE CRACKED AT LEVEL WBL 183.40. R & R ANGLE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

EE COMPARTMENT ANGLE CRACKED AT BS 328, STRINGER 21L. R & R ANGLE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

EE COMPARTMENT ANGLE CRACKED AT BS 336, STRINGER 21L. R & R ANGLE IAW SRM & DRAWING. .

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

EE COMPARTMENT ANGLE CRACKED AT BS 320, STRINGER 21L. R & R ANGLE IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

FUSELAGE SKIN CRACKED AT BS 951+10.250, STRINGER 17L. REPAIRED SKIN IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

SUPPORT STRUCTURE ANGLE CRACKED BETWEEN BS 294.5 TO BS 312, LBL 24.5. R & R ANGLE IAW SRM & DRAWING.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

BULKHEAD DOME CAP CRACKED AT BS 1016, STRINGER 6L INBD SIDE. REPAIRED CAP IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

SUPPORT ANGLE CRACKED AT BS 294.5, STRINGER 23L. R & R ANGLE IAW SRM & DRAWING.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

MAIN WW ANGLE CRACKED BETWEEN BS 663 TO BS 675, RBL 36. R & R CHANNEL IAW SRM & DRAWING.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 62,709 hrs · 51,701 cycles

MLG WW PRESSURE WEB CRACKED AT BS 665.75, LBL 32. REPAIRED WEB IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

FUSELAGE SKIN CRACKED AT BS 951+8.5, STRINGER 17L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

FUSELAGE SKIN CRACKED AT BS 951+8.5, STRINGER 17L. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

STUD FRAME CRACKED AT BS 951 + 20, STRINGER 17L. R & R STUD FRAME IAW SRM & DRAWING.

Part: FLAP — DELAMINATED (RT WING) · airframe 62,709 hrs · 51,701 cycles

RT WING INBD FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: ATTACH FITTING — CRACKED (L1 DOOR) · airframe 62,709 hrs · 51,701 cycles

L1 DOOR ATTACH CLIP CRACKED AT BS 348.2, STRINGER 15L. R & R CLIP IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

FUSELAGE SKIN STRAP CRACKED AT BS 951+10.250 TO BS 951+3.250, STRINGER 17L. REPAIRED SKIN IAW SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

STRINGER SPLICE CORRODED AT BS 360+7, STRINGER 27L. R & R SPLICE IAW SRM & DRAWING.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

INTERCOSTAL CRACKED AT BS 348.2, STRINGER 16L. R & R INTERCOSTAL IAW SRM & DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

STRAP CRACKED BETWEEN BS 312 TO BS 344, LBL 45. R & R STRAP IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

FUSELAGE FRAME CRACKED AT BS 947.5, STRINGER 19L. REPAIRED FRAME IAW SWA EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

WEB ANGLE CRACKED AT BS 947.5, BETWEEN STRINGER 24R TO STRINGER 25R. R & R ANGLE IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

SUPPORT ANGLE CRACKED BETWEEN BS 927 TO BS 947, BBL 0. R & R ANGLE IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

SUPPORT ANGLE CRACKED AT BS 947.5, BETWEEN STRINGER 24R TO STRINGER 25R. R & R ANGLE IAW SRM & DRAWING.

Part: RIB — CRACKED (LT WING) · airframe 62,709 hrs · 51,701 cycles

LT WING UPPER RIB CHORD CRACKED AT WBL 114, STRINGER 2. REPAIRED RIB IAW SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

FUSELAGE FRAME CRACKED AT BS 947.5, STRINGER 24R. REPAIRED FRAME IAW SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

STRINGER CLIP CRACKED AT BS 947.5, STRINGER 25R. R & R CLIP IAW SRM C

Part: WEB — CORRODED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

WEB CORRODED BETWEEN BS 420 TO BS 440, STRINGER 17R. R & R WEB IAW DRAWING.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

BULKHEAD DOME CAP BULKHEAD CRACKED AT BS 1016, STRINGER 1. REPAIRED CAP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

SKIN CRACKED AT BS 500 +6.8, STRINGER 17L. REPAIRED SKIN IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

STRAP CRACKED AT BS 540, STRINGER 22L. R & R STRAP IAW SRM & DRAWING.

Part: WEB — CORRODED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

WEB CORRODED BETWEEN BS 500A TO BS 500B, STRINGER 17L. R & R WEB IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

TIE CLIP CRACKED AT BS 727A, STRINGER 20L. R & R TIE CLIP IAW SRM & DRAWING.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

DOME CAP BULKHEAD WEB CRACKED AT BS 1016, STRINGER 15L. REPAIRED WEB IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

RT WING TO BODY FAIRING AFT LOWER STRUCTURE ANGLE CRACKED BETWEEN BS 700 & BS 727. R & R ANGLE IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

FUSELAGE SKIN BEAR STRAP CRACKED AT BS 947.5, STRINGER 17L. REPAIRED SKIN IAW SWA EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

WEB CORRODED AT BETWEEN BS 500A TO BS 500B, STRINGER 17L. R & R WEB IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

TIE CLIP CRACKED AT BS 727B, STRINGER 25R. R & R TIE CLIP IAW SRM & DRAWING.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

BRACKET CRACKED AT BS 540, BL 0. R & R BRACKET IAW SRM & DRAWING.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

FWD ENTRY DOOR SURROUND STRUCTURE SUPPORT BRACKET CRACKED AT BS 360, STRINGER 8L. R & R BRACKET IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

SUPPORT ANGLE CRACKED AT INSTRUMENT COMPARTMENT AT RACK AT E3-4 SHELF EE COMPARTMENT. R & R ANGLE IAW SRM & DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

LT SIDE NLG WW CRACKED AT BS 251.6, WL 169+7. REPAIRED WEB IAW SRM.

Part: WEB — CRACKED (NLG WW) · airframe 62,709 hrs · 51,701 cycles

LT SIDE NLG WW CRACKED FOUND AROUND FASTENER AT BS 243.7+4, WL 169.1. REPAIRED WEB IAW SRM.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

SUPPORT BRACKET CRACKED AT BS 360, STRINGER 9L, AT FWD ENTRY DOOR SURROUND STRUCTURE. R & R BRACKET IAW SRM & DRAWING.

Part: WEB — CRACKED (NLG WW) · airframe 62,709 hrs · 51,701 cycles

LT SIDE NLG WW CRACKED AT BS 243.7+3, WL 169.1. REPAIRED WEB IAW SRM.

Part: ATTACH FITTING — CRACKED (RT HORIZ STAB) · airframe 62,709 hrs · 51,701 cycles

RT HORIZONTAL STABILIZER LOWER OTBD ATTACH FITTING CRACKED. R & R FITTING IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

SUPPORT ANGLE CRACKED AT BS 380, STRINGER 26L. R & R CLIP IAW SRM & DRAWING.

Part: ATTACH FITTING — CRACKED (RT HORIZ STAB) · airframe 62,709 hrs · 51,701 cycles

RT HORIZONTAL STABILIZER CENTER SECTION UPPER OTBD ATTACH FITTING CRACKED. R & R FITTING IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (NR 1 PYLON) · airframe 62,709 hrs · 51,701 cycles

NR 1 ENG STRUT AFT SUPPORT ANGLE CRACKED AT STRUT TORQUE BOX. R & R ANGLE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

SUPPORT ANGLE CRACKED AT BS 500B, STRINGER 26L. R & R ANGLE IAW SRM & DRAWING.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 62,709 hrs · 51,701 cycles

MLG WW PRESSURE WEB UPPER CHORD CRACKED AT BS 663.75+2, LBL 24.8. REPAIRED WEB IAW SWA EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

SUPPORT ANGLE CRACKED AT BS 380, STRINGER 26R. R & R CLIP IAW SRM & DRAWING.

Part: ATTACH FITTING — CRACKED (RT HORIZ STAB) · airframe 62,709 hrs · 51,701 cycles

RT HORIZONTAL STABILIZER UPPER INBD ATTACH FITTING CRACKED. R & R FITTING IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

SUPPORT ANGLE CRACKED AT BS 500C, STRINGER 26L. R & R ANGLE IAW SRM & DRAWING.

Part: PLATE — CRACKED (FUSELAGE) · airframe 62,709 hrs · 51,701 cycles

LT WING TO BODY FAIRING ACCESS PANEL 33578L PLATE CRACKED. R & R PLATE IAW SRM & DRAWING.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 62,709 hrs · 51,701 cycles

MLG WW PRESSURE WEB CRACKED AT BS 664.+1.75, LBL 24.5+7.75. REPAIRED WEB IAW SWA EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 62,709 hrs · 51,701 cycles

MLG WW PRESSURE WEB UPPER CHORD CRACKED AT BS 663.75+3, LBL 24.8. REPAIRED WEB IAW SWA EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 62,709 hrs · 51,701 cycles

MLG WW PRESS WEB CRACKED AT BS 663.75, LBL 24.5. REPAIRED WEB IAW SWA EA.

Part: SKIN — CRACKED (RT WING) · airframe 62,709 hrs · 51,701 cycles

RT WING INBD FIXED LE SKIN CRACKED AT LE STATION 208. REPAIRED SKIN IAW EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 62,709 hrs · 51,701 cycles

MLG WW PRESSURE WEB UPPER CHORD CRACKED AT BS 663.75 TO BS 686, LBL 24.8. REPAIRED WEB IAW SWA EA.

Part: SKIN — CRACKED (LT WING) · airframe 62,709 hrs · 51,701 cycles

LT WING INBD FIXED LE SKIN CRACKED AT LE STATION 208. REPAIRED SKIN IAW EA.

Part: DOOR — CRACKED (L1) · airframe 62,182 hrs · 51,288 cycles

L1 DOOR AFT UPPER CORNER CRACKED. REPAIRED DOOR IAW SRM.

Part: COVER — INOPERATIVE (R2 DOOR) · airframe 62,160 hrs · 51,269 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINING BRACKET INOPERATIVE. R&R COVER IAW MM & MT.

Part: HOOK — OUT OF ADJUST (GIRT BAR) · airframe 62,101 hrs · 51,221 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK OUR OF ADJUSTMENT. ADJUSTED HOOKS PER SIP.

Part: COVER — BROKEN (EXIT SIGN) · airframe 61,813 hrs · 51,008 cycles

FWD ENTRY EMERGENCY EXIT SIGN LIGHT BROKEN. R&R COVER IAW MM.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 61,685 hrs · 50,915 cycles

LEFT AFT INTERIOR EMERGENCY EXIT BATTERY INOPERATIVE. R & R BATTERY IAW MM.

Part: WEB — CHAFED (FUSELAGE) · airframe 61,685 hrs · 50,915 cycles

BEADED WEB CHAFED BETWEEN BS 663 TO BS 675, BETWEEN RBL 12 TO RBL21. REPAIRED WEB IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,017 hrs · 50,397 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER M/M.

Part: SUPPORT BRACKET — BROKEN (NR 2 PYLON) · airframe 60,732 hrs · 50,201 cycles

SUPPORT BRACKET ON AFT END OF AFT STRUT LOWER FAIRING BROKEN. REMOVED AND REPLACED SUPPORT BRACKET PER SRM 51-40-02.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 60,732 hrs · 50,201 cycles

AFT GALLEY DOOR SLIDE INDICATOR GAUGE - OUT OF POSITION. REPOSITIONED AFT GALLEY DOOR SLIDE GAUGE AS PER M/M.

Part: DOOR — OUT OF ADJUST (L1) · airframe 60,732 hrs · 50,201 cycles

FWD ENTRY DOOR DRAGGING UPPER AFT CORNER DURING OPEN AND CLOSE. ADJUSTED DOOR PER MM

Part: STRUCTURE — DELAMINATED (LT ELEVATOR) · airframe 60,732 hrs · 50,201 cycles

LT ELEVATOR DELAMINATED AFT EDGE FROM INBD EDGE. REPAIRED ELEVATOR IAW SRM.

Part: LENS — LOOSE (CABIN) · airframe 60,636 hrs · 50,125 cycles

ROW 8 BULLNOSE LENS LOOSE. REMOVED AND REPLACED EMERGENCY LIGHT BULL NOSE LENSE AT SEAT ROW 8DEF PER AMM CL 90348 CLOSING LP 8962150.

Part: LIGHT — BROKEN (CABIN) · airframe 60,447 hrs · 50,000 cycles

R1 DOOR EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER M/M. OPS CHECK GOOD.

Part: LENS — CRACKED (CABIN) · airframe 59,640 hrs · 49,448 cycles

R2 DOOR EMERGENCY LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT ASSY PER M/M.

Part: LENS — LOOSE (CABIN) · airframe 59,172 hrs · 49,089 cycles

RIGHT EMERGENCY EXIT LIGHT LENS LOOSE ON AFT SIDE. REMOVED AND REPLACED LIGHT ASSY PER AMM.

Part: FLAP — WORN (RT WING) · airframe 59,172 hrs · 49,089 cycles

RIGHT WING O/B FORE FLAP I/B LEADING EDGE WORN. REMOVED AND REPLACED FORE FLAP PER AMM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 59,027 hrs · 48,980 cycles

INBOARD F/A FORWARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 58,627 hrs · 48,674 cycles

L2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATOR LOW. REMOVED & REPLACED SLIDE PER MT.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 58,216 hrs · 48,362 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW AMM.

Part: CONNECTOR — NOT SEATED (EXTERIOR) · airframe 58,216 hrs · 48,362 cycles

R2 DOOR EXTERIOR EMERGENCY LIGHT INOP. RESEATED CONNECTOR IAW MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 58,215 hrs · 48,362 cycles

RIGHT EXTERIOR EMERGENCY EXIT LIGHT AFT RIGHT WING INOP. RELAMPED LIGHT IAW MM.

Part: LIGHT — BROKEN (CABIN) · airframe 58,216 hrs · 48,362 cycles

FORWARD LAVATORY EMERGENCY EXIT LIGHT BASE BROKEN. REMOVED AND REPLACED LIGHT BASE ASSY IAW & MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,216 hrs · 48,362 cycles

STRINGER CLIP CRACKED AT BS 360, STR 2L. REMOVED & REPLACED CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,216 hrs · 48,362 cycles

STRINGER CLIP AT BS 360, STR 1 CRACKED. REMOVED AND REPLACED CLIP IAW BAC DWG & SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,216 hrs · 48,362 cycles

STRINGER CLIP CRACKED AT BS 500A+18, STR 8L. REPAIRED CLIP IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,216 hrs · 48,362 cycles

RT FUSELAGE SKIN CRACKED AT BS 400+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,216 hrs · 48,362 cycles

RT FUSELAGE SKIN CRACKED AT BS 380+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,216 hrs · 48,362 cycles

RT FUSELAGE SKIN CRACKED AT BS 520+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW IR AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,216 hrs · 48,362 cycles

RT FUSELAGE SKIN CRACKED AT BS 500C+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW REO AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,216 hrs · 48,362 cycles

RT FUSELAGE WINDOW SKIN CRACKED AT BS 500+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,216 hrs · 48,362 cycles

RT FUSELAGE SKIN CRACKED AT BS 480+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW REO AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,216 hrs · 48,362 cycles

RT FUSELAGE SKIN CRACKED AT BS 420+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,216 hrs · 48,362 cycles

RT FUSELAGE SKIN CRACKED AT BS 380+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,216 hrs · 48,362 cycles

RT FUSELAGE WINDOW SKIN CRACKED AT BS 480+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,216 hrs · 48,362 cycles

RT FUSELAGE SKIN CRACKED AT BS 440+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,216 hrs · 48,362 cycles

LT FUSELAGE SKIN CRACKED AT BS 500A+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,216 hrs · 48,362 cycles

RT FUSELAGE SKIN CRACKED AT BS 360+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW REO AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,216 hrs · 48,362 cycles

RT FUSELAGE SKIN CRACKED AT BS 400+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIR SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,216 hrs · 48,362 cycles

RT FUSELAGE SKIN CRACKED AT BS 500B+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,216 hrs · 48,362 cycles

RT FUSELAGE SKIN CRACKED AT BS 500C+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,216 hrs · 48,362 cycles

RT FUSELAGE WINDOW SKIN CRACKED AT BS 460+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,216 hrs · 48,362 cycles

RT FUSELAGE SKIN CRACKED AT BS 360+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW REO AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,216 hrs · 48,362 cycles

RT FUSELAGE SKIN CRACKED AT BS 440+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,216 hrs · 48,362 cycles

RT FUSELAGE SKIN CRACKED AT BS 787+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,216 hrs · 48,362 cycles

LT FUSELAGE SKIN CRACKED AT BS 767+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,216 hrs · 48,362 cycles

LT FUSELAGE SKIN CRACKED AT BS 807+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW REO AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,216 hrs · 48,362 cycles

RT FUSELAGE SKIN CRACKED AT BS 807+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,216 hrs · 48,362 cycles

LT FUSELAGE SKIN CRACKED AT BS 727C+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW REO AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,216 hrs · 48,362 cycles

RT FUSELAGE WINDOW SKIN CRACKED AT BS 827+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,216 hrs · 48,362 cycles

LT FUSELAGE SKIN CRACKED AT BS 807+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,216 hrs · 48,362 cycles

LT FUSELAGE SKIN CRACKED AT BS 887+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,216 hrs · 48,362 cycles

LT FUSELAGE SKIN CRACKED AT BS 727B+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW REO AND EA.

Part: LIGHT — CRACKED (CABIN) · airframe 58,216 hrs · 48,362 cycles

RT BULLNOSE EMERGENCY EXIT LIGHT CRACKED AT ROW 14. REPAIRED LIGHT IAW AMM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,108 hrs · 48,283 cycles

STRINGER CLIP CRACKED AT STA 727B, STR 6L. REMOVED AND REPLACED CLIP PER SRM AND BAC DRAWING.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 58,108 hrs · 48,283 cycles

RT WING I/B FORE FLAP IS DELAMINATED AT O/B END UPPER SURFACE. REPAIRED FORE FLAP PER SRM.

Part: COVER — OUT OF POSITION (EXIT SIGN) · airframe 58,108 hrs · 48,283 cycles

FWD OVERHEAD EMERGENCY EXIT SIGN COVER FELL OFF. RE-INSTALLED COVER PER MM.

Part: COVER — OUT OF POSITION (EXIT SIGN) · airframe 58,108 hrs · 48,283 cycles

FWD OVERHEAD EMERGENCY EXIT SIGN COVER FELL OFF. RE-INSTALLED COVER PER MM.

Part: MOTOR — SHEARED (NR 1 ENGINE) · airframe 57,792 hrs · 48,060 cycles

ABORTED TAKEOFF, NR 1 ENGINE WOULD NOT PRODUCE TAKEOFF POWER. FOUND NR 1 ENGINE VBV MOTOR OUTPUT SHAFT SHEARED. REMOVED AND REPLACED NR 1 VBV MOTOR AND FLEXIBLE DRIVE SHAFT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,733 hrs · 48,017 cycles

DURING SCHEDULED 18Y CHECK, FOUND SKIN CRACKED AT BS 500C+7, STR 4L. REPAIRED SKIN PER SWA EA

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,733 hrs · 48,017 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT AFT UPPER CORNER. REPAIRED SKIN IAW SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,733 hrs · 48,017 cycles

DURING SCHEDULED 18Y CHECK, FOUND LONGITUDINAL FLOOR BEAM UPPER CHORD CRACKED BETWEEN 666 TO BS 671, LBL 24.5. REPAIRED CHORD PER ER.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,733 hrs · 48,017 cycles

DURING SCHEDULED 18Y CHECK, FOUND LONGITUDINAL FLOOR BEAM WEB CRACKED AT BS 639, RBL 45. REPAIRED WEB PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,733 hrs · 48,017 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT FWD LOWER CORNER. REPAIRED SKIN IAW SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,733 hrs · 48,017 cycles

DURING SCHEDULED 18Y, CHECK FOUND INNER FRAME CHORD CRACKED AT BS 615, WL 202. REPAIRED CHORD IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,733 hrs · 48,017 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE IAW EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 57,733 hrs · 48,017 cycles

DURING SCHEDULED 18Y CHECK, FOUND AFT CARGO COMPARTMENT SKIN CORRODED AT BS 986.5, BETWEEN STR 26L TO STR 27L. REPAIRED SKIN PER ER AND EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,733 hrs · 48,017 cycles

DURING SCHEDULED 18Y CHECK, FOUND FLOORBEAM CORRODED AT BS 727C+5, RBL 3. REPAIRED BEAM IAW SRM AND EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,733 hrs · 48,017 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 57,733 hrs · 48,017 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 794.3, STR 26R. REMOVED AND REPLACED CLIP PER DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,733 hrs · 48,017 cycles

DURING SCHEDULED 18Y CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM CORRODED AT BS 727B+3, LBL 3. REPAIRED BEAM IAW EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 57,733 hrs · 48,017 cycles

DURING SCHEDULED 18Y CHECK, FOUND WEB VERTICAL SUPPORT CORRODED BETWEEN BS 794 TO BS 847, RBL 19. REMOVED AND REPLACED SUPPORT IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,733 hrs · 48,017 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,733 hrs · 48,017 cycles

DURING SCHEDULED 18Y CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM CORRODED AT BS 727D+5, RBL 3. REPAIRED BEAM IAW AND SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,733 hrs · 48,017 cycles

DURING SCHEDULED 18Y CHECK, FOUND AFT CARGO COMPARTMENT FLOOR BEAM CORRODED AT BS 727D+5, LBL 3. REPAIRED BEAM IAW AND SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,733 hrs · 48,017 cycles

DURING SCHEDULED 18Y CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM CORRODED AT BS 727D+5, LBL 8. REPAIRED BEAM IAW SWA AND SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,733 hrs · 48,017 cycles

DURING SCHEDULED 18Y CHECK, FOUND FRAME CRACKED AT BS 500C, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,733 hrs · 48,017 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 500C+7, STR 4L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,728 hrs · 48,016 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 500C+7, STR 4L. REPAIRED SKIN IAW EA.

Part: LENS — BROKEN (CABIN) · airframe 57,733 hrs · 48,017 cycles

R1 DOOR LOWER EMERGENCY EXIT LIGHT LENS ASSY BROKEN. REMOVED AND REPLACED LENS ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,345 hrs · 47,733 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 727, STR 4L. REPAIRED SKIN IAW ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,345 hrs · 47,733 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 837, STR 1. REPAIRED SKIN IAW ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,345 hrs · 47,733 cycles

DURING SCHEDULED MV3 CHECK, FOUND SKIN CRACKED AT BS 837, STR 1. REPAIRED SKIN PER SRM.

Part: FLAP — PUNCTURED (LT WING) · airframe 56,433 hrs · 47,050 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING I/B AFT FLAP PUNCTURED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 55,871 hrs · 46,614 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 5 SLAT T/E WEDGE DELAMINATED. REPAIRED WEDGE PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,924 hrs · 45,931 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER AFT CORNER OF RADIUS. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 45,923 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT BS 767+13, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 45,923 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT BS 420+14.25, STR 1. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 45,923 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT BS 727C+10, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 45,923 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT BS 807+12.5, STR 4R. REPAIRED SKIN PER EA.

Part: LIGHT — LOOSE (CABIN) · airframe 54,616 hrs · 45,691 cycles

RT EEPLS LOOSE AT ROW 6. SECURED EEPLS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,383 hrs · 45,517 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 794, STR 19L. REPAIRED SKIN PER MT.

Part: LENS — LOOSE (CABIN) · airframe 54,152 hrs · 45,329 cycles

FWD EEPLS LENS LOOSE. SECURED LENS PER MM.

Part: COVER — LOOSE (CABIN) · airframe 53,569 hrs · 44,890 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT COVER LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,302 hrs · 44,702 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 736B, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,302 hrs · 44,702 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 735E, STR 4R. REPAIRED SKIN PER EA.

Part: LENS — LOOSE (CABIN) · airframe 52,907 hrs · 44,387 cycles

RT OVERWING EGRESS LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,601 hrs · 44,164 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN AT BS 760, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,601 hrs · 44,164 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 740A, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 52,468 hrs · 44,063 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 1 SLAT OUTER SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, LBL 5. REPAIRED BEAM PER AEM EO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 787, BETWEEN STR 27R TO STR 27L. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 727B, RBL 45.5. REPAIRED BEAM PER AEM EO.

Part: FLAP — DELAMINATED (LT WING) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 529, STR 28L. REPAIRED SKIN PER AEM EO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 787, BETWEEN STR 25L TO STR 26L. REPAIRED FRAME PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING I/B FORE FLAP LOWER SKIN DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 767, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 787, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 757, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND ZEE ANGLE CORRODED BETWEEN BS 737E TO BS 787, STR 25L. REPAIRED Z-ANGLE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 1006, BETWEEN STR 27R TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR SKIN CUTOUT UPPER CORNER FITTING CRACKED AT BS 304. REMOVED AND REPLACED FITTING PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, LBL 28.5. REPAIRED BEAM PER SRM.

Part: COVER — CRACKED (FUSELAGE) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND COVER CRACKED AT L2 DOOR CUTOUT AT BS 986.5, STR 10L. REPAIRED COVER PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 986.5, BETWEEN STR 27R TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: CABLE — FRAYED (EVAC SLIDE) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND UPPER INNER CHORD CORRODED BETWEEN BS 947.5 TO BS 1006, RBL 47. REMOVED AND REPLACED CHORD PER SRM.

Part: CABLE — FRAYED (EVAC SLIDE) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 1. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 26L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 20L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 21L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663.75, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 20L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,463 hrs · 44,060 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,404 hrs · 44,016 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 513D TO BS 517D, STR 8R. REPAIRED SKIN PER EA.

Part: PANEL — FAULTY (COCKPIT) · airframe 52,403 hrs · 44,016 cycles

DIVERSION - SMOKE COMING FROM FUEL PANEL AT 34,000 FT. SMOKE HAD ELECTRICAL SMELL AND STOPPED VISIBLY AFTER APPROX 60 SEC. DIVERTED TO ORF. NO CIRCUIT BREAKERS POPPED. REMOVED AND REPLACED FUEL SYSTEM P5-2 PANEL PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 50,737 hrs · 42,783 cycles

R2 DOOR EMERGENCY EXIT SIGN LENS LOOSE. REMOVED AND REPLACED SIGN ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,740 hrs · 42,106 cycles

DURING SCHEDULED 14Y CHECK, FOUND RADIO ALTIMETER CUTOUT SKIN CRACKED AT BS 433, LBL 4. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,740 hrs · 42,106 cycles

DURING SCHEDULED 14Y CHECK, FOUND RADIO ALTIMETER CUTOUT SKIN CRACKED AT BS 430, RBL 3. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,740 hrs · 42,106 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT, BETWEEN BS 209 TO BS 291, BETWEEN WL 255 TO WL 259. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,740 hrs · 42,106 cycles

DURING SCHEDULED 14Y CHECK, FOUND RADIO ALTIMETER CUTOUT SKIN CRACKED AT BS 434, LBL 2. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,740 hrs · 42,106 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, BS 304, WL 234. REPAIRED SKIN PER ER.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 49,740 hrs · 42,106 cycles

DURING SCHEDULED 14Y CHECK, FOUND FWD CARGO BAY LT KEEL BEAM CORRODED AT BS 520. REMOVED AND REPLACED BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,740 hrs · 42,106 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT, BETWEEN BS 292 TO BS 304, WL 257. REPAIRED SKIN PER ER.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 49,740 hrs · 42,106 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CRACKED AT BS 380, STR 15R. REPAIRED STRINGER PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 49,740 hrs · 42,106 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,740 hrs · 42,106 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 867 STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,740 hrs · 42,106 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 49,740 hrs · 42,106 cycles

DURING SCHEDULED 14Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 667, LBL 24. REPAIRED BEAM PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,740 hrs · 42,106 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,740 hrs · 42,106 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,740 hrs · 42,106 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,740 hrs · 42,106 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,740 hrs · 42,106 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,740 hrs · 42,106 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,740 hrs · 42,106 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,740 hrs · 42,106 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,740 hrs · 42,106 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,740 hrs · 42,106 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,740 hrs · 42,106 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,740 hrs · 42,106 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,740 hrs · 42,106 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,740 hrs · 42,106 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,740 hrs · 42,106 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,740 hrs · 42,106 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,740 hrs · 42,106 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,740 hrs · 42,106 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 500A STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,740 hrs · 42,106 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,740 hrs · 42,106 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,740 hrs · 42,106 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,740 hrs · 42,106 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SRM.

Part: LENS — BROKEN (L1 DOOR) · airframe 48,944 hrs · 41,561 cycles

FOUND L1 DOOR EGRESS LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: LENS — BROKEN (CABIN) · airframe 48,944 hrs · 41,561 cycles

FOUND L1 DOOR EGRESS LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: GIRT BAR — OUT OF ADJUST (EVAC SLIDE) · airframe 48,825 hrs · 41,481 cycles

DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EMERGENCY ESCAPE SLIDE GIRT BAR OUT OF ADJUST. ADJUSTED GIRT BAR PER MM.

Part: GIRT BAR — OUT OF ADJUST (EVAC SLIDE) · airframe 48,825 hrs · 41,481 cycles

DURING SCHEDULED C2 CHECK, FOUND L2 SLIDE DOOR GIRT BAR OUT OF ADJUST. ADJUSTED GIRT BAR PER MM.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 48,825 hrs · 41,481 cycles

DURING SCHEDULED C2 CHECK, FOUND PHOTOLUMINESCENT STRIP DAMAGED AT SEAT 9C. REMOVED AND REPLACED STRIP PER MM.

Part: SEAL — BROKEN (FLASHLIGHT) · airframe 48,825 hrs · 41,481 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT INBOARD FLASHLIGHT SEAL BROKEN. REMOVED AND REPLACED SEAL PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 46,618 hrs · 39,859 cycles

AFT CABIN OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY AND BATTERY CHARGER PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,595 hrs · 39,842 cycles

RIGHT AFT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 46,337 hrs · 39,651 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT BS NR 5 DOOR STOP. REMOVED AND REPLACED FRAME PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 46,337 hrs · 39,651 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CRACKED AT BS NR 5 DOOR STOP. REMOVED AND REPLACED FRAME PER SRM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 45,859 hrs · 39,268 cycles

DURING SCHEDULED C3 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 132. REPAIRED SKIN PER SRM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 45,517 hrs · 39,006 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 43,343 hrs · 37,295 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN COVER LOOSE. SECURED COVER PER MM.

Part: LENS — LOOSE (CABIN) · airframe 43,314 hrs · 37,274 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN LENS LOOSE. SECURED LENS PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 42,940 hrs · 36,978 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 15 DEF. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM.

Part: STRINGER CLIP — CRACKED (BS 927 S26R) · airframe 41,383 hrs · 35,766 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: DOOR FRAME — CRACKED (BS 797 S24R) · airframe 41,383 hrs · 35,766 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME WEB CRACKED AT BS 797, STR 24R. REPAIRED FRAME WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,383 hrs · 35,766 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR CUTOUT FUSELAGE SKIN PRESSURE SEAL LANDING CRACKED AT LOWER HINGE CUTOUT. REMOVED AND REPLACED PRESSURE SEAL LANDING PER SRM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 41,097 hrs · 35,530 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LT WING FLAP PER MM.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 40,300 hrs · 34,931 cycles

FOUND FWD LT CABIN EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 40,108 hrs · 34,792 cycles

LEFT OVERWING EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED EXIT SIGN PER MM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 39,056 hrs · 33,958 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING INBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,590 hrs · 33,603 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT UPPER & LOWER LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,072 hrs · 33,179 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 38,072 hrs · 33,179 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 37,620 hrs · 32,814 cycles

R2 COCKPIT WINDOW ARCED & CRACKED. REMOVED AND REPLACED R2 WINDOW PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,632 hrs · 31,246 cycles

DURING SCHEDULED RON, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 35,379 hrs · 31,056 cycles

DURING SCHEDULED C4 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN AT STATION 146, REAR SPAR, CRACKED. REPAIRED SKIN PER SRM.

Part: LENS — MISSING (CABIN) · airframe 34,648 hrs · 30,450 cycles

EMERGENCY EXIT LIGHT LENS MISSING AT RT OVERWING EXIT. REPLACED LIGHT LENS PER MM.

Part: HOOK — LOOSE (L1 DOOR) · airframe 34,380 hrs · 30,241 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EVAC SLIDE FWD HOOK LOOSE. SECURED L1 DOOR EVAC SLIDE FWD HOOK PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,024 hrs · 29,136 cycles

DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 360, STRINGER 8R. REPAIRED FRAME PER ER.

Part: WIRE — CHAFED (EMERGENCY SIGN) · airframe 33,015 hrs · 29,131 cycles

DURING SCHEDULED D CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT WIRES CHAFFING. REMOVED AND REPLACED WIRE PER WDM AND MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,015 hrs · 29,131 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM CORRODED AT BS 380 TO BS 400 LT, WL 208 AND BS 500 TO 500A LT, WL 208. REPAIRED CREASE BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,015 hrs · 29,131 cycles

DURING SCHEDULED D CHECK, FOUND FRAMES CRACKED AT BS 294, RBL 55 AND BS 303, WL 216. REPAIRED FRAMES PER ER.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,010 hrs · 29,127 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM CHORD CORRODED AT BS 363, WL 208, LBL 65. REPAIRED CREASE BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,010 hrs · 29,127 cycles

DURING SCHEDULED D CHECK, FOUND FRAMES CRACKED AT BS 787, STRINGER 8R AND BS 400, STRINGER 8R. REPAIRED FRAMES PER ER.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,010 hrs · 29,129 cycles

DURING SCHEDULED D CHECK, FOUND AFT PAX CABIN CREASE BEAM WEB CORRODED. REPAIRED BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,010 hrs · 29,127 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 1025, BETWEEN STR 16L AND STR 17L. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,010 hrs · 29,127 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION BS 294, RBL 33 TO 53, FLOORBEAM. REPAIRED FLOORBEAM PER SRM.

Part: RIVET — LOOSE (GIRT BAR FITTING) · airframe 30,695 hrs · 27,255 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EVACUATION SLIDE GIRT BAR HOOK ATTACH RIVET SHEARED. INSTALLED RIVET PER SRM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 30,628 hrs · 27,206 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: TRUNNION PIN — CORRODED (LT & RT MLG) · airframe 30,295 hrs · 26,950 cycles

DURING SCHEDULED A2 CHECK, FOUND BOTH LT & RT MLG TRUNNION PINS CORRODED. REMOVED AND REPLACED BOTH LT & RT MLG TRUNNION PINS PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 28,774 hrs · 25,765 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 25,764 hrs · 23,348 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 1.5 INCH CRACK AT CAPT'S FWD UPPER WINDOW POST. REPAIRED SKIN PER SRM.

Part: WEB — CRACKED (ACFT NOSE) · airframe 25,761 hrs · 23,344 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED, LBL 5, WL 201. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (R1 DOOR) · airframe 25,761 hrs · 23,344 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR AFT LOWER FRAME CRACKED. REPAIRED FRAME PER BAC DRAWING.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,761 hrs · 23,344 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO BIN FLOORBEAM CORRODED, BS 771 BETWEEN LBL 8-LBL 13. REPAIRED BEAM PER SWA RA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 25,761 hrs · 23,344 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD LT SIDE CHORD CRACKED AT WL 207. REMOVED AND REPLACED LT SIDE CHORD PER SWA ACO.

Part: WEB — CRACKED (FUSELAGE) · airframe 25,761 hrs · 23,344 cycles

DURING SCHEDULED 1/4D CHECK, FOUND WEB CRACKED AT BS 178, RBL 5, WL 201. REPAIRED WEB PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 25,761 hrs · 23,344 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 VERTICAL STIFFENER CRACKED, RBL 5.7, WL 184. REPAIRED STIFFENER PER SWA RA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,761 hrs · 23,343 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOOR BEAMS CORRODED ( 2 EA ) AT BS 910, RBL 14 & BS 945, LBL 17. REPAIRED FLOOR BEAMS PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 25,761 hrs · 23,343 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE FRAME CORRODED AT BS 747, BETWEEN STR 26R & 27R. REPAIRED SHEAR TIE FRAME PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 25,761 hrs · 23,344 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL STIFFENER WEB CRACKED AT BS 178, RBL 17.1, WL 234. REPAIRED STIFFENER PER SRM.

Part: FITTING — CORRODED (LT & RT MLG) · airframe 24,971 hrs · 22,659 cycles

DURING SCHEDULED SVC CHECK, FOUND LT & RT MLG WALKING BEAM HANGER FITTINGS CORRODED. REMOVED AND REPLACED LT AND RT HANGER FITTING'S PER ALM WORK CARDS AND MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,210 hrs · 21,127 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT HAS SEVERAL BULBS INOP AND LENS BROKEN. REMOVED AND REPLACED LENS AND REPLACED BULBS PER MM.

Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 23,210 hrs · 21,127 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. REPOSITIONED EVAC SLIDE ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN FLOOR) · airframe 22,954 hrs · 20,922 cycles

SECTION OF EEPLS INOP. REMOVED AND REPLACED SECTION OF EEPLS PER MM.

Part: LENS — MISSING (CABIN) · airframe 22,663 hrs · 20,691 cycles

AFT GALLEY EMERGENCY EXIT LIGHT LENS MISSING. REPLACED LENS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 21,351 hrs · 19,593 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS LOOSE AT ROW 15. R&R LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,711 hrs · 19,040 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT ROW 14. RELAMPED PER MM.

Part: LENS — BROKEN (CABIN) · airframe 20,483 hrs · 18,825 cycles

DURING SCHEDULED C2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. R&R LENS PER MM.

Part: GIRT BAR — WORN (ESCAPE SLIDE) · airframe 20,483 hrs · 18,825 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE GIRT ASSY WORN. R&R SLIDE ASSY PER MM.

Part: GIRT BAR — OUT OF ADJ (ESCAPE SLIDE) · airframe 20,483 hrs · 18,825 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE GIRT ASSY OUT OF ADJUSTMENT. REPOSITIONED SLIDE ASSY PER MM.

Part: AUTO PILOT — MALFUNCTIONED (E & E COMPT)

AIR TURNBACK, LOST F/O'S ROLL PITCH HEADING AFTER TAKEOFF. PERFORMED POWER CK OF ALL BUSES, APU, STANDBY, ENGS, AND ALL INSTRUMENTS CAME BACK TO NORMAL. POWER DOWN AIRCRAFT FOR SEVERAL MINUTES, POWERED AIRCRAFT BACK UP AGAIN, RAN BOTH ENGS. ALL F/O'S INSTRUMENTS OP CK GOOD.

Part: TR SLEEVE — MISSING (NR 2 ENGINE)

AFTER LANDING DURING THROUGH FLIGHT INPECTION DISCOVERED NR 2 ENG T/R OUTBOARD SLEEVE MISSING FROM AIRCRAFT. REPLACED NR 2 ENG T/R OUTBOARD SLEEVE ASSY PER MM AND LATER ON THE NR 2 ENG OUTBOARD T/R ASSY WAS REPLACED.

Part: FLOORBEAM — CORRODED (BS 294)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON TOP FLANGE OF FLOORBEAM, BS 294 , RBL 23-47. REPAIRED BEAM PER SRM.

Part: COVER — CRACKED (ROW 12C)

DURING SCHEDULED BC4 CHECK, FOUND 12-C FLOOR PROX LIGHT COVER CRACKED. REMOVED AND REPLACED COVER PER MM.

Part: SKIN — DAMAGED (CARGO DOORWAY)

DURING SCHEDULED C4 CHECK, FOUND DOORWAY SKIN INSIDE FWD LOWER CORNER OF DOOR DAMAGED. REPAIRED PER BOEING SRM.

Part: WIRE — DAMAGED (CABIN)

DURING WALKAROUIND CHECK, FOUND NUMEROUS FLOOR TRACK LIGHTS INOP. REPAIRED WIRING AND RELAMPED AS REQUIRED PER BOEING M/M.