N374SW

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 69,873 hrs · 57,603 cycles

L1 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,803 hrs · 57,543 cycles

EMERGENCY LIGHT BATTERY PACK M1137, VOLTAGE LOW. R & R BATTERY PACK IAW AMM.

Part: RETAINING CLIP — BROKEN (EXIT SIGN) · airframe 69,803 hrs · 57,543 cycles

RIGHT SIDE OVERWING EMER EXIT SIGN HOUSING RETAINER CLIP BROKEN. R & R CLIP IAW AMM.

Part: SKIN — CRACKED (RT WING) · airframe 69,803 hrs · 57,543 cycles

RIGHT WING FOUND CRACKED HOLE ON UPPER AFT CHORD, UPPER WING SKIN AT RSS 255. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,803 hrs · 57,543 cycles

SKIN CRACKED AT BS 500D+5, STRINGER 2R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT WING) · airframe 69,803 hrs · 57,543 cycles

RIGHT WING UPPER SKIN ABOVE AFT WING SPAR, AFT ROW OPEN HOLE FASTENER CRACKED AT RSS 267. REPAIRED SKIN IAW ER & EA.

Part: SPAR — CRACKED (RT WING) · airframe 69,803 hrs · 57,543 cycles

RIGHT WING AFT SPAR WEB, LABELED NR 6 ON INBD SIDE OF RSS 224.14, CRACKED. REPAIRED WEB IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 69,803 hrs · 57,543 cycles

RIGHT WING UPPER SKIN CRACKED AT REAR SPAR AT WBL 251. REPAIRED SPAR WEB IAW ER & EA.

Part: SKIN — CRACKED (RT WING) · airframe 69,803 hrs · 57,543 cycles

RIGHT WING UPPER SKIN CRACKED AT AFT SPAR RSS 253. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (RT WING) · airframe 69,803 hrs · 57,543 cycles

RIGHT WING UPPER SKIN CRACKED ABOVE AFT WING SPAR, AFT ROW OPEN HOLE FASTENER CRACKED AT RSS 261. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (RT WING) · airframe 69,803 hrs · 57,543 cycles

RIGHT WING UPPER SKIN ABOVE AFT WING SPAR, AFT ROW OPEN HOLE FASTENER CRACKED AT RSS 255. REPAIRED SKIN IAW ER & EA.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 69,803 hrs · 57,543 cycles

RIGHT WING FWD SUPPORT FITTING LOCATED ON FWD SIDE OF AFT SPAR WEB RSS 224.14, CRACKED ON HOLE 5. R & R FITTING IAW SRM.

Part: SKIN — CRACKED (RT WING) · airframe 69,803 hrs · 57,543 cycles

RIGHT WING UPPER SKIN ABOVE AFT WING SPAR, FWD ROW OPEN HOLE FASTENER CRACKED AT RSS 267. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (RT WING) · airframe 69,803 hrs · 57,543 cycles

RIGHT WING UPPER SKIN ABOVE AFT WING SPAR, FWD ROW OPEN HOLE FASTENER CRACKED AT RSS 285. REPAIRED SKIN IAW ER & EA.

Part: SPAR — CRACKED (LT WING) · airframe 69,803 hrs · 57,543 cycles

LEFT WING CRACKED ON THE INBD SIDE OF RSS 224.14, UPPER SIDE OF SPAR WEB. REPAIRED SPAR WEB IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 69,803 hrs · 57,543 cycles

LEFT WING UPPER SIDE OF SPAR WEB AT FASTENER HOLE NR 7 CRACKED AT RSS 224.14. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 69,803 hrs · 57,543 cycles

LEFT WING, UPPER SKIN FASTENER HOLE CRACKED, APPROX RSS 229, .750" FWD OF TE. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (LT WING) · airframe 69,803 hrs · 57,543 cycles

LEFT WING UPPER SKIN FASTENER HOLE CRACKED AT APPROX RSS 206, 3.5" FWD OF TE EA1-357-T1243. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (LT WING) · airframe 69,803 hrs · 57,543 cycles

LEFT WING, UPPER SKIN FASTENER HOLE CRACKED, APPROX RSS 216, .750" FWD OF TE. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (LT WING) · airframe 69,803 hrs · 57,543 cycles

LEFT WING, UPPER SKIN FASTENER HOLE CRACKED, APPROX RSS 267, .750" FWD OF TE. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (LT WING) · airframe 69,803 hrs · 57,543 cycles

LEFT WING, UPPER SKIN FASTENER HOLE CRACKED, APPROX RSS 214, 2.5" FWD OF TE. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (LT WING) · airframe 69,803 hrs · 57,543 cycles

LEFT WING, UPPER SKIN FASTENER HOLE CRACKED, APPROX RSS 250, .750" FWD OF TE. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (LT WING) · airframe 69,803 hrs · 57,543 cycles

LEFT WING, UPPER SKIN FASTENER HOLE CRACKED, APPROX RSS 254, .750" FWD OF TE. REPAIRED SKIN IAW ER & EA.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 69,803 hrs · 57,543 cycles

RIGHT WING REAR SPAR MLG AFT SUPPORT FITTING, CRACKED AT UPPER INBD FASTENER HOLE. REPAIRED FITTING IAW ER.

Part: SKIN — CRACKED (RT WING) · airframe 69,803 hrs · 57,543 cycles

RIGHT WING UPPER SKIN CRACKED AFT EDGE FASTENER HOLE AT RSS 237. REPAIRED SKIN IAW ER & EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 69,803 hrs · 57,543 cycles

FRAME FORGING CORRODED AT BS 665, RBL 70.8. REPAIRED FRAME IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 69,803 hrs · 57,543 cycles

LEFT WING PLANK SKIN CRACKED ON UPPER SURFACE AT RSS 237. REPAIRED SKIN IAW EA.

Part: BRACKET — CRACKED (LT WING) · airframe 69,803 hrs · 57,543 cycles

LEFT WING MLG BEAM ATTACHMENT FITTING BRACKET CRACKED, UPPER SPAR CHORD. R & R BRACKET IAW SRM & DWG.

Part: STRUCTURE — CRACKED (RT WING) · airframe 69,803 hrs · 57,543 cycles

RIGHT WING EXTERIOR REAR SPAR, UPPER CHORD CRACKED AT WING STATION RSS 222.14. REPAIRED CHORD IAW EA.

Part: STRUCTURE — CRACKED (LT WING) · airframe 69,803 hrs · 57,543 cycles

LEFT WING EXTERIOR REAR SPAR UPPER CHORD, CRACKED AT WING STATION RSS 222.14. REPAIRED CHORD IAW EA.

Part: TIP CAP — DELAMINATED (RT HORIZ STAB) · airframe 69,803 hrs · 57,543 cycles

RIGHT HORIZONTAL STABILIZER TIP DELAMINATED AT LE. REPAIRED TIP IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,803 hrs · 57,543 cycles

SKIN CRACKED AT BS 834, STRINGER 1L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,803 hrs · 57,543 cycles

CROWN SKIN CRACKED AT BS 540-14, STRINGER 2R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,803 hrs · 57,543 cycles

CROWN SKIN CRACKED AT BS 480+2, STRINGER 2R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,803 hrs · 57,543 cycles

SKIN CRACKED AT BS 360+2.5, STRINGER 1R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,803 hrs · 57,543 cycles

CROWN SKIN CRACKED AT BS 520+3, STRINGER 2L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,803 hrs · 57,543 cycles

SKIN CRACKED AT BS 500D+15, STRINGER 5R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,803 hrs · 57,543 cycles

SKIN CRACKED AT BS 480+3, STRINGER 2L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,803 hrs · 57,543 cycles

SKIN CRACKED AT BS 500C+5, STRINGER 7R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,803 hrs · 57,543 cycles

SKIN CRACKED AT BS 807-4, STRINGER 2R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,835 hrs · 57,567 cycles

FUSELAGE SKIN CRACKED AT BS 827+3, STRINGER 2R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,802 hrs · 57,542 cycles

FUSELAGE SKIN CRACKED AT BS 827+3, STRINGER 2R. REPAIRED SKIN IAW EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 69,461 hrs · 57,298 cycles

RIGHT WING INBD FORE FLAP UPPER SKIN DELAMINATED. REPAIRED SKIN IAW SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 69,461 hrs · 57,298 cycles

LEFT WING NR 2 LE SLAT INBD WEDGE DELAMINATED. REPAIRED WEDGE IAW SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 69,461 hrs · 57,298 cycles

RIGHT WING INBD FORE FLAP DELAMINATED ON UPPER SURFACE. REPAIR FORE FLAP IAW EA.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 69,461 hrs · 57,298 cycles

LEFT WING NR 2 SLAT INBD WEDGE DELAMINATED ON UPPER & LOWER SURFACE. REPAIRED WEDGE IAW EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 69,461 hrs · 57,298 cycles

RIGHT WING INBD FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,461 hrs · 57,298 cycles

CORROSION BULGE AT FUSELAGE SKIN STATION 787+5, STRINGER 26R. REPAIRED SKIN IAW EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 69,327 hrs · 57,192 cycles

LEFT WING INBD AFT TE FLAP DELAMINATED. R & R FLAP ASSEMBLY IAW MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,327 hrs · 57,192 cycles

FUSELAGE FRAME CRACKED AT STATION 986, STRINGER 20R. REPAIRED FRAME IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,327 hrs · 57,192 cycles

LEFT CREASE BEAM WEB CORRODED BETWEEN BS 787 - 807. R & R WEB IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,327 hrs · 57,192 cycles

RIGHT CREASE BEAM WEB CORRODED BETWEEN BS 500A - 500B. REPAIRED CREASE BEAM IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 69,327 hrs · 57,192 cycles

LONGITUDINAL FLOORBEAM LOWER CHORD CRACKED BETWEEN BS 660 - 666, LBL 24.5. REPAIRED CHORD IAW SRM.

Part: FRAME — CRACKED (BS 348) · airframe 69,327 hrs · 57,192 cycles

FRAME CRACKED AT BS 348.2, STRINGER 16L. REPAIRED FRAME IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,327 hrs · 57,192 cycles

R1 DOOR EXTERNAL SKIN CRACKED AT LOWER HINGE ARM CUT OUT LOWER AFT CORNER DRAIN HOLE. REPAIRED SKIN IAW EA.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 69,327 hrs · 57,192 cycles

L1 DOOR THRESHOLD ATTACH ANGLE CORRODED BETWEEN BS 312 - 344, STRINGER 17L. R & R ANGLE IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,327 hrs · 57,192 cycles

CABIN FLOORBEAM CORRODED AT STATION 985.5, LBL 51. REPAIRED BEAM IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,327 hrs · 57,192 cycles

CABIN FLOORBEAM CORRODED AT STATION 985.5, RBL 15 - 35. REPAIRED BEAM IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,327 hrs · 57,192 cycles

FORWARD ENTRY DOOR WAY FLOOR ATTACH CREASE BEAM CORRODED BETWEEN BS 303 - 348. R & R CREASE BEAM IAW DWG & SRM.

Part: BRACKET — CRACKED (L1 DOOR) · airframe 69,327 hrs · 57,192 cycles

L1 DOOR ESCAPE SLIDE GIRT BAR FLOOR FITTING CRACKED UNDER FLOOR SUPPORT. R & R BRACKET IAW AMM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,327 hrs · 57,192 cycles

AFT R2 DOOR WET CREASE BEAM CORRODED BETWEEN BS 947 - 986, RBL 40, STRINGER 17. R & R BEAM IAW DWG & SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 69,327 hrs · 57,192 cycles

STRINGER 5L CRACKED AT STATION 1016. REPAIRED STRINGER IAW EA.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 69,327 hrs · 57,192 cycles

MAIN CABIN CREASE BEAM WEB CRACKED BETWEEN BS 616 - 639, INBD AFT FASTENER HOLE AT LT SIDE. R & R CREASE BEAM IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,327 hrs · 57,192 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 360 TO 380, STRINGER 17R. R & R WEB IAW SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 69,327 hrs · 57,192 cycles

LEFT CREASE BEAM INBD INNER CHORD HORIZONTAL FLANGE CRACKED AT BS 639. REPAIRED FLANGE IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,327 hrs · 57,192 cycles

RIGHT FRAME INNER CHORD CRACKED AT BS 616, LOWER FASTENER. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,327 hrs · 57,192 cycles

FUSELAGE FRAME CRACKED AT STATION 360, STRINGER 21R - 20R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,327 hrs · 57,192 cycles

FRAME CRACKED AT BS 500B, STRINGER 21L. REPAIRED FRAME IAW SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 69,327 hrs · 57,192 cycles

CHORD CRACKED AT STATION 727, STRINGER 18A LT. REPAIRED CHORD IAW EA.

Part: LATCH — BROKEN (COCKPIT) · airframe 68,936 hrs · 56,913 cycles

CAPTAIN ROPE ACCESS DOOR LATCH BROKEN. R & R LATCH IAW SIP.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,780 hrs · 56,792 cycles

STRINGER CLIP CRACKED AT BS 420, STRINGER 1L. R & R CLIP IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,780 hrs · 56,792 cycles

SKIN CRACKED AT BS 500B+2, STRINGER 2L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,780 hrs · 56,792 cycles

FUSELAGE SKIN CRACKED AT BS 500A+15, STRINGER 8R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,780 hrs · 56,792 cycles

FUSELAGE SKIN CRACKED AT BS 500C+16, STRINGER 8R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,780 hrs · 56,792 cycles

SKIN CRACKED AT BS 400+15, STRINGER 2R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,780 hrs · 56,792 cycles

FUSELAGE SKIN CRACKED AT BS 400+12, STRINGER 26L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,780 hrs · 56,792 cycles

SKIN CRACKED AT BS 500C+1, STRINGER 2L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,780 hrs · 56,792 cycles

SKIN CRACKED AT BS 948+15, STRINGER 5R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,780 hrs · 56,792 cycles

SKIN CRACKED AT BS 727C+13, STRINGER 2R. REPAIRED SKIN IAW SRM.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 68,488 hrs · 56,583 cycles

L1 WINDOW ARCED & CRACKED. R & R WINDSHIELD IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,116 hrs · 56,323 cycles

RIGHT BULLNOSE EMER LIGHT INOPERATIVE AT ROW 4. RELAMPED LIGHT IAW AMM.

Part: PANEL — DELAMINATED (LE SLAT) · airframe 67,273 hrs · 55,664 cycles

RIGHT WING LOWER LE WING PANEL 65C26278-9022 UNDER THE NR 6 SLAT DELAMINATED ALONG THE OTBD LE. REPAIRED NR 6 SLAT IAW SRM.

Part: ACTUATOR — BROKEN (LT SPOILER) · airframe 67,027 hrs · 55,490 cycles

LEFT WING NR 4 GND SPOILER INBD ACTUATOR BROKEN. R & R SPOILER IAW AMM.

Part: ACTUATOR — OUT OF ADJUST (LT SPOILER) · airframe 67,027 hrs · 55,490 cycles

LEFT WING NR 4 GND SPOILER OTBD ACTUATOR OUT OF ADJUSTMENT. R & R ACTUATOR IAW AMM.

Part: LUG — BROKEN (LT SPOILER) · airframe 67,027 hrs · 55,490 cycles

LEFT WING INBD GND SPOILER LUG BROKEN. R & R SPOILER IAW AMM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 66,556 hrs · 55,160 cycles

R2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE IAW MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,443 hrs · 55,085 cycles

STRINGER CLIP CRACKED AT BS 380, STRINGER 9L. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,443 hrs · 55,085 cycles

STRINGER CLIP CRACKED AT BS 380, STRINGER 8L. R & R CLIP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,443 hrs · 55,085 cycles

FRAME CHORD CRACKED AT BS 348.2, STRINGER 16L. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,443 hrs · 55,085 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 375 TO BS 376, STRINGER 8L. REPAIRED SKIN IAW SRM & EA.

Part: PLATE — CRACKED (LT NACELLE) · airframe 66,139 hrs · 54,870 cycles

LT NACELLE SPLICE PLATE CRACKED AT BS 234, UPPER PYLON FRAME. R & R PLATE IAW SRM.

Part: TRACK — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

TRACK TIE DOWN CRACKED AT BS 500, LBL 18.2. REPAIRED TRACK TIE IAW EA.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 63,682 hrs · 53,088 cycles

LEFT WING I/B MID FLAP LOWER SURFACE WEDGE PANEL DELAMINATED. REPAIRED MID FLAP IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

INTERNAL STRAP CORRODED AT BS 986.5, BETWEEN STR 27L TO STR 27R. REPAIRED STRAP IAW EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 63,682 hrs · 53,088 cycles

RIGHT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED AT STAB STA 101.90. REMOVED AND REPLACED RIB IAW SRM AND DRAWING.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

SHEAR TIE CORRODED AT BS 987, BETWEEN STR 27R TO STR 27L. REMOVED AND REPLACED SHEAR TIE IAW SRM AND EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

STRINGER CORRODED AT BS 987, STR 27L. REPAIRED STRINGER IAW SRM.

Part: WEB — CRACKED (L1 DOOR) · airframe 63,682 hrs · 53,088 cycles

L1 DOOR UPPER SILL WEB CRACKED. REMOVED AND REPLACED WEB IAW SRM AND DRAWING.

Part: ANGLE — CRACKED (NR 1 PYLON) · airframe 63,682 hrs · 53,088 cycles

NR 1 ENGINE STRUT FAIRING ANGLE CRACKED AT STA 363.65. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.

Part: PAN — CRACKED (LT PYLON) · airframe 63,682 hrs · 53,088 cycles

CRACK ON PAN LOCATED OUTBOARD SIDE ASSY AFT STRUT FAIRING ENGINE NR 1. REPAIRED PAN IAW EA.

Part: ANGLE — CRACKED (LT WING) · airframe 63,682 hrs · 53,088 cycles

LEFT WING I/B ANGLE CRACKED AT 355 WBL. REPAIRED ANGLE IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

ANGLE CRACKED AT BS 328, LBL 46. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.

Part: STIFFENER — CRACKED (RT PYLON) · airframe 63,682 hrs · 53,088 cycles

NR 6 INBD SIDE RT PYLON STIFFENER CRACKED AT ON FLAP TRACK FAIRING. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.

Part: STIFFENER — CRACKED (LT PYLON) · airframe 63,682 hrs · 53,088 cycles

STIFFENER CRACKED LOCATED AFT STRUT FAIRING LOWER SURFACE OF ENGINE NR 1. REMOVED AND REPLACED STIFFENER IAW SRM AND DRAWING.

Part: ANGLE — CRACKED (RT WING) · airframe 63,682 hrs · 53,088 cycles

RIGHT WING FRONT SPAR ANGLE CRACKED AT WBL 71.24. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: ANGLE — CRACKED (TE FLAP) · airframe 63,682 hrs · 53,088 cycles

NR 1 FLAP TRANSMISSION SUPPORT INTERNAL ANGLE CRACKED. REMOVED AND REPLACED ANGLE IAW EA AND EO.

Part: ANGLE — CRACKED (TE FLAP) · airframe 63,682 hrs · 53,088 cycles

NR 8 FLAP TRANSMISSION SUPPORT INTERNAL ANGLE CRACKED. REMOVED AND REPLACED ANGLE IAW EA AND EO.

Part: WEB — CRACKED (RT HORIZ STAB) · airframe 63,682 hrs · 53,088 cycles

RIGHT HORIZONTAL STABILIZER WEB CRACKED BETWEEN STAB STA 184.70 TO STA 193.90. REPAIRED WEB IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

TIE CLIP CRACKED AT BS 480, STR 16R. REMOVED AND REPLACED TIE CLIP IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

WEB CRACKED AT BS 827, STR 25R. REMOVED AND REPLACED WEB IAW SRM AND DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

FRAME CRACKED AT BS 847, BETWEEN STR 23R TO STR 24R. REPAIRED FRAME IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

STRAP CRACKED AT BS 847, BETWEEN STR 23R TO STR 24R. REMOVED AND REPLACED STRAP IAW SRM AND DRAWING.

Part: PAN — CRACKED (LT PYLON) · airframe 63,682 hrs · 53,088 cycles

CRACK ON LOWER PAN LOCATED ASSY AFT STRUT FAIRING OUTBOARD SIDE ENGINE NR 1. REPAIRED PAN IAW EA.

Part: FITTING — CRACKED (LT PYLON) · airframe 63,682 hrs · 53,088 cycles

LEFT PYLON NACELLE TO FLAP TRACK FAIRING INTERFACE FITTING CRACKED. REMOVED AND REPLACED FITTING IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

ANGLE CRACKED AT BS 665, RBL 24. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.

Part: STRUCTURE — WORN (LE SLAT) · airframe 63,682 hrs · 53,088 cycles

LEFT WING NR 3 SLAT CAN I/B POSITION WORN. REMOVED AND REPLACED SLAT CAN IAW EA.

Part: BRACKET — CRACKED (L1 DOOR) · airframe 63,682 hrs · 53,088 cycles

L1 DOOR FWD UPPER BRACKET CRACKED. REMOVED AND REPLACED BRACKET IAW SRM AND DRAWING.

Part: BRACKET — CRACKED (L1 DOOR) · airframe 63,682 hrs · 53,088 cycles

L1 DOOR AFT UPPER BRACKET CRACKED. REMOVED AND REPLACED BRACKET IAW SRM AND DRAWING.

Part: ANGLE — CRACKED (RT WING) · airframe 63,682 hrs · 53,088 cycles

RIGHT WING ANGLE LOCATED ON INTERNAL CAVITY AT LEVEL RSS 535 TRAILING EDGE AREA CRACKED. REMOVED AND REPLACED CHORD IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

TIE CLIP CRACKED AT BS 380, STR 22L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

SUPPORT ANGLE CRACKED BETWEEN BS 344 TO BS 360, LBL 10. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

ANGLE CRACKED BETWEEN BS 259.5 TO BS 312, STR 27L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

STRINGER CLIP CRACKED AT BS 294.5, STR 23L. REMOVED AND REPLACED CLIP IAW SRM AND DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

SUPPORT ANGLE CRACKED AT BS 380, STR 20L. REMOVED AND REPLACED ANGLE IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

TIE CLIP CRACKED AT BS 927, STR 21L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

STRAP CRACKED AT BS 328+ 2, LBL 45.5. REMOVED AND REPLACED STRAP IAW SRM AND DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

WEB CRACKED BETWEEN BS 312 AND BS 328, LBL 46. REMOVED AND REPLACED WEB IAW SRM AND DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

WEB CRACKED BETWEEN BS 500A TO BS 500B, STR 26R. REMOVED AND REPLACED WEB IAW SRM AND DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

TIE CLIP CRACKED AT BS 380, STR 21L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DRAWING.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

STRINGER SPLICE CORRODED AT BS 360+4, STR 27L. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

SHEAR TIE CORRODED AT BS 360, BETWEEN STR 27L AND STR 28L. REMOVED AND REPLACED SHEAR TIE IAW SRM & DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

WEB CRACKED BETWEEN BS 344 TO BS 360, BL 0. REMOVED AND REPLACED WEB IAW SRM AND DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

STRAP CRACKED AT BS 328, BL 0. REMOVED AND REPLACED STRAP IAW SRM AND DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

ANGLE CRACKED AT BS 320, STR 21L. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

ANGLE CRACKED AT BS 336, STR 21L. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

WEB CRACKED BETWEEN BS 259.5 TO BS 312, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: PANEL — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

AFT WING TO BODY FAIRING PANEL 3578L CRACKED. REPAIRED PANEL IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

STRAP CRACKED AT BS 328, RBL 45.5. REMOVED AND REPLACED STRAP IAW SRM AND DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

TIE CLIP CRACKED AT BS 380, STR 26R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DRAWING.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

FLOORBEAM UPPER CHORD LOCATED AT BS 312, RBL 21. REPAIRED CHORD IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

SUPPORT ANGLE CRACKED AT BS 351.5, STR 26R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: SKIN — CRACKED (TE FLAP) · airframe 63,682 hrs · 53,088 cycles

LEFT WING INBOARD FORE FLAP CRACKED AT 16IN OF INBOARD END ON LOWER SURFACE. REPAIRED FORE FLAP IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

ANGLE CRACKED AT BS 380, BETWEEN STR 20L AND STR 21L. REMOVED AND REPLACED ANGLE IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

FLOORBEAM UPPER CHORD CRACKED AT BS 312, RBL 34. REPAIRED CHORD IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

WEB CRACKED BETWEEN BS 747 TO BS 767, STR 25R. REMOVED AND REPLACED WEB IAW SRM.

Part: STRUCTURE — CRACKED (RT WING) · airframe 63,682 hrs · 53,088 cycles

RIGHT WING UPPER CHORD CRACKED AT BS 114.00, S-2. REPAIRED CHORD IAW EO AND EA.

Part: HINGE — CRACKED (L1 DOOR) · airframe 63,682 hrs · 53,088 cycles

L1 DOOR SHIELD HINGE ON FLAP ASSY CRACKED. REMOVED AND REPLACED SHIELD HINGE IAW SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

STIFFENER CRACKED AT BS 947.5+10, BETWEEN STR 24L TO STR 26L. REMOVED AND REPLACED STIFFENER IAW SRM AND DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

WEB CRACKED AT BS 794.3, STR 25R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

WEB CRACKED AT BS 718, BL 0. REMOVED AND REPLACED WEB IAW SRM AND DRAWING.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

ATTACH CLIP CRACKED AT BS 348.2, STR 15L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

STIFFENER CRACKED AT BS 947.5+6, BETWEEN STR 24L TO STR 26L. REMOVED AND REPLACED STIFFENER IAW SRM AND DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

TIE CLIP CRACKED AT BS 727A, STR 26L. REMOVED AND REPLACED TIE CLIP IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

FRAME CORRODED AT BS 727E, BETWEEN 27R TO STR 27L. REPAIRED FRAME IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

TIE CLIP CRACKED AT BS 927, STR 25R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: RUB STRIP — CRACKED (NR 1 NACELLE) · airframe 63,682 hrs · 53,088 cycles

NR 1 ENGINE NACELLE STRUT ACCESS PANEL 57700L RUB STRIP CRACKED. REMOVED AND REPLACED RUB STRIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

TIE CLIP CRACKED AT BS 420, STR 27L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: STRUCTURE — CRACKED (LT HORIZ STAB) · airframe 63,682 hrs · 53,088 cycles

LEFT HORIZONTAL STABILIZER LOWER CHORD CRACKED AT STA 120.30. REPAIRED CHORD IAW EO AND EA.

Part: RUB STRIP — CRACKED (NR 1 NACELLE) · airframe 63,682 hrs · 53,088 cycles

NR 1 ENGINE NACELLE STRUT ACCESS PANEL 5747L RUB STRIP CRACKED. REMOVED AND REPLACED RUB STRIP IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

WEB CRACKED AT BS 712, LBL 4. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: RETAINER — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

RIGHT AIR CONDITIONING ACCESS PANEL 3403R SEAL RETAINER CRACKED. REMOVED AND REPLACED RETAINER IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

SKIN CRACKED AT BS 500C+5, STR 8R. REPAIRED SKIN IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

TIE CLIP CRACKED AT BS 947.5, STR 25R. REMOVED AND REPLACED TIE CLIP IAW EA.

Part: LENS — BROKEN (CABIN) · airframe 63,682 hrs · 53,088 cycles

FWD EMERGENCY EXIT LENS BROKEN. REMOVED AND REPLACED LENS IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

SKIN CRACKED BETWEEN BS 837 TO BS 847, STR 2R. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

FRAME CRACKED AT BS 500B, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

BULKHEADS FITTING CRACKED AT BS 727, STR 27R. REMOVED AND REPLACED FITTING IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

BULKHEAD FITTING CRACKED AT BS 727, STR 27L. REMOVED AND REPLACED FITTING IAW SRM AND DRAWING.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

WEB CORRODED BETWEEN BS 420 TO BS 440, STR 17R. REMOVED AND REPLACED WEB IAW SRM AND DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

FRAME CRACKED AT BS 500B, BETWEEN STR 20R AND STR 21R. REPAIRED FRAME IAW SRM.

Part: PANEL — CRACKED (NLG WW) · airframe 63,682 hrs · 53,088 cycles

NLG WHEEL WELL SIDE PANEL CRACKED AT BS 258.5, RBL 16. REPAIRED NLG WHEEL WELL SIDE PANEL IAW SRM.

Part: RETAINER — BROKEN (RT WING) · airframe 63,682 hrs · 53,088 cycles

BROKEN RETAINER OF BARREL NUT LOCATED ON ROOT RIB OF RIGHT WINGLET. REMOVED AND REPLACED RETAINER IAW SRM.

Part: PANEL — CRACKED (NLG WW) · airframe 63,682 hrs · 53,088 cycles

NLG WHEEL WELL CRACKED AT BS 258.5, RBL 16. REPAIRED PANEL IAW SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

STRINGER CRACKED AT BS 480+6, STRINGER 16R. REPAIRED STRINGER IAW SRM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

BULKHEAD CHANNEL CRACKED AT BS 727, WL 162. REMOVED AND REPLACED CHANNEL IAW SRM AND DRAWING.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

STRINGER CRACKED AT BS 294.5, STR 10L. REPAIRED STRINGER IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

FUSELAGE SKIN CRACKED AT BS 480+4.75, STR 16R. REPAIRED SKIN IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

TIE CLIP CRACKED AT BS 727B, STR 25R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DRAWING.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

CHANNEL ASSY CRACKED AT BS 540, BETWEEN BL 0 TO LBL 24.5. REMOVED AND REPLACED CHANNEL ASSY IAW SRM AND DRAWING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

CLIP CRACKED AT BS 380, STR 26L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

TIE CLIP CRACKED AT BS 787, STR 21R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: WEB — CRACKED (LT NLG WW) · airframe 63,682 hrs · 53,088 cycles

LEFT SIDE OF THE NLG WHEEL WELL CRACKED BETWEEN BS 243.7 TO BS 251.6. REPAIRED WEB IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

TIE CLIP CRACKED AT BS 787, STR 20R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

SKIN CRACKED AT BS 440, STR 16R. REPAIRED SKIN IAW SRM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

CHANNEL ASSY CRACKED AT BS 540, BETWEEN BL 0 TO RBL 24.5. REMOVED AND REPLACED CHANNEL ASSY IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

ANGLE CRACKED AT BS 500D BETWEEN STR 27L TO STR 28L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

FRAME CORRODED AT BS 500C, BETWEEN STR 28L TO STR 28R. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

FRAME CORRODED AT BS 500C, BETWEEN STR 26L AND STR 27L. REPAIRED FRAME IAW SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 63,682 hrs · 53,088 cycles

MAIN WHEEL WELL PRESSURE DECK CRACKED AT BS 663.5 + 1, LBL 24.5. REPAIRED DECK IAW SRM.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 63,682 hrs · 53,088 cycles

LOWER CORNER OF AFT CARGO DOOR AFT FRAME CRACKED. REMOVED AND REPLACED DOOR IAW AMM AND EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 63,682 hrs · 53,088 cycles

MAIN WHEEL WELL PRESSURE DECK CRACKED AT BS 663.5 + 1, LBL 17. REPAIRED DECK IAW EO AND EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 63,682 hrs · 53,088 cycles

MAIN WHEEL WELL PRESSURE DECK CRACKED AT BS 673.5, LBL 19.3. REPAIRED DECK IAW SRM.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 63,682 hrs · 53,088 cycles

MAIN WHEEL WELL PRESSURE DECK CRACKED AT BS 663.5 + 2, RBL 24.5. REPAIRED WEB IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,682 hrs · 53,088 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 667, LBL 24.5. REPAIRED CHORD IAW EO.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 63,559 hrs · 53,003 cycles

PANEL SEAL BRACKET AFT OF RIGHT W/W CRACKED. REMOVED AND REPLACED BRACKET PER MM.

Part: PANEL — BULGED (RT HORIZ STAB) · airframe 63,680 hrs · 53,087 cycles

RIGHT HORIZONTAL STABILIZER UPPER T/E PANEL BULGING AT STA 162. REPAIRED PANEL IAW EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 63,141 hrs · 52,703 cycles

RIGHT WING O/B AFT FLAP I/B END DELAMINATED. REMOVED, REPLACED, ADJUSTED AND OP'S TEST GOOD ON RIGHT O/B AFT FLAP IAW MM 27-51-39-404-002. (POS:RT; P/N OFF:65-46435-334; S/N OFF:2268; P/N ON: 65-46435-370; S/N ON:2424)

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 63,141 hrs · 52,703 cycles

RIGHT WING UPPER TRAILING EDGE PANEL AFT ATTACH ANGLE I/B OF PYLON CRACKED. REMOVED AND REPLACED ANGLE IN RT WING UPPER T/E PANEL AFT I/B SIDE OF NR 2 PYLON IAW SRM 51-21-99-307-001, SRM 51-40-02-0G-0.

Part: SPINDLE — FAULTY (TE FLAP) · airframe 62,970 hrs · 52,584 cycles

FLAPS 5 AIRCRAFT MADE UNUSUAL RUMBLE NOISE. REMOVED AND REPLACED SPINDLE IAW AMM.

Part: BUMPER — DETERIORATED (COCKPIT) · airframe 62,970 hrs · 52,584 cycles

FIRST OFFICERS GLARESHIELD BUMPER PAD DETERIORATED. REMOVED AND REPLACED BUMPER PER AMM.

Part: TRIM TAB — DELAMINATED (LT ELEVATOR) · airframe 62,198 hrs · 52,022 cycles

LEFT ELEVATOR TAB UNDER TAB MAST FAIRING DELAMINATED. REMOVED AND REPLACED TRIM TAB PER AMM.

Part: ACTUATOR — LEAKING (LT SPOILER) · airframe 62,068 hrs · 51,924 cycles

LEFT WING NR 0 GROUND SPOILER ACTUATOR LEAKED. REMOVED AND REPLACED ACTUATOR PER M/M.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,351 hrs · 51,389 cycles

FUSELAGE SKIN CRACKED AT BS 360+12, ABOVE STR 2L. REPAIRED SKIN PER EA.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 61,308 hrs · 51,355 cycles

RIGHT KEEL BEAM CORRODED AT BS 500D. REMOVED AND REPLACED BEAM IAW SRM & DWG.

Part: DOWNLOCK SENSOR — FAULTY (RT MLG) · airframe 61,222 hrs · 51,290 cycles

AIR TURNBACK -- AFTER T/O WITH FLAPS UP WHEN LANDING GEAR HANDLE WAS PLACED TO "OFF" POSITION THE RED UNSAFE LIGHT CAME ON FOLLOWED BY GREEN RIGHT GEAR LIGHT ON. ALL HYD PRESSURES AND QUANTITY WERE NORMAL. FOLLOWING QRH WITH GEAR HANDLE IN UP POSITION RIGHT GEAR RETRACTED AND ALL LIGHTS OFF. LANDING WAS NORMAL. REMOVED AND REPLACED RIGHT MAIN GEAR DOWNLOCK SENSOR NR 73 AND PERFORMED LANDING GEAR WARNING SYSTEM TEST IAW M/M.

Part: PANEL — DELAMINATED (RT SPOILER) · airframe 61,182 hrs · 51,258 cycles

RIGHT WING INBOARD FLIGHT SPOILER PANEL O/B SIDE DELAMINATED. REMOVED AND REPLACED SPOILER AS PER M/M.

Part: FUEL LINE — FAILED (NR 2 ENGINE) · airframe 61,153 hrs · 51,239 cycles

INFLIGHT SHUT DOWN -- UPON INITIAL DESCENT NR 2 ENGINE FLAMED OUT. NO COMPRESSOR STALL. REMOVED AND REPLACED NR 2 ENGINE FUEL SUPPLY LINE PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 60,358 hrs · 50,634 cycles

R-2 DOOR ESCAPE SLIDE PRESSURE GAUGE OUT OF POSITION. REPOSITIONED SLIDE PER MT#G25-61-06SA AND MM.

Part: LENS — BROKEN (CABIN) · airframe 60,318 hrs · 50,602 cycles

L2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS ASSY PER MM.

Part: ACTUATOR — BROKEN (SPOILER) · airframe 60,265 hrs · 50,561 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING NR 4 O/B ACTUATOR MOUNT SUPPORT LUG BROKEN. REMOVED AND REPLACED ACTUATOR IAW MM.

Part: SUPPORT BRACKET — BROKEN (EVAC SLIDE) · airframe 59,603 hrs · 50,066 cycles

R2 DOOR EMERGENCY EVAC SLIDE SUPPORT BRACKET FOR GIRT BAR BROKEN. REMOVED AND REPLACED SLIDE IAW MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 58,868 hrs · 49,514 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CENTER OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER IAW MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 58,868 hrs · 49,514 cycles

DURING SCHEDULED 12Y CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,698 hrs · 49,389 cycles

DURING SCHEDULED 18Y CHECK, FOUND SKIN CRACKED BETWEEN BS 969 TO BS 970.5, STR 21L. REPAIRED SKIN PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 58,698 hrs · 49,389 cycles

DURING SCHEDULED 18Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 639, LBL 45. REPAIRED WEB PER EA AND ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,698 hrs · 49,389 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,698 hrs · 49,389 cycles

DURING SCHEDULED 18Y CHECK FOUND, SHEAR TIE CORRODED AT BS 807, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,698 hrs · 49,389 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 27R TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,698 hrs · 49,389 cycles

DURING SCHEDULED 18Y CHECK FOUND, SHEAR TIE CORRODED AT BS 727D, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,698 hrs · 49,389 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 927, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 58,698 hrs · 49,389 cycles

DURING SCHEDULED 18Y CHECK, FOUND FAIL SAFE CHORD CRACKED AT BS 380, BETWEEN STR 14L TO STR 24L. REMOVED AND REPLACED CHORD PER SRM AND DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 58,698 hrs · 49,389 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 14R TO STR 15R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 58,698 hrs · 49,389 cycles

DURING SCHEDULED 18Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 882 TO BS 887, WL 208. REMOVED AND REPLACED BEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,698 hrs · 49,389 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 25R TO STR 26R. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 58,698 hrs · 49,389 cycles

DURING SCHEDULED 18Y CHECK, FOUND FRAME CORRODED AT BS 767, BETWEEN STR 26L TO STR 26R. REMOVED AND REPLACED FRAME SECTION IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 58,698 hrs · 49,389 cycles

DURING SCHEDULED 18Y CHECK, FOUND AFT CARGO BAY FLOOR SUPPORT CORRODED BETWEEN BS 774 TO BS 827, RBL 3. REPAIRED SUPPORT PER EA.

Part: FAILSAFE — CORRODED (FUSELAGE) · airframe 58,698 hrs · 49,389 cycles

DURING SCHEDULED 18Y CHECK, FOUND FAIL SAFE CHORD CORRODED AT BS 767, BETWEEN STR 27L TO STR 26R. REMOVED AND REPLACED CHORD PER CHORD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 58,698 hrs · 49,389 cycles

DURING SCHEDULED 18Y CHECK, FOUND AFT CARGO BAY FLOOR SUPPORT CORRODED BETWEEN BS 774 TO BS 827, RBL 8. REPAIRED SUPPORT PER EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 58,698 hrs · 49,389 cycles

DURING SCHEDULED 18Y CHECK, FOUND CREASE BEAM SHEAR WEB CORRODED BETWEEN BS 400 TO BS 420, STR 17L. REMOVED AND REPLACED WEB PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,698 hrs · 49,389 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 25R TO STR 26R. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,698 hrs · 49,389 cycles

DURING SCHEDULED 18Y CHECK FOUND, SKIN CRACKED BETWEEN BS 487 TO BS 487.5, STR 4R. REPAIRED SKIN PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,698 hrs · 49,389 cycles

DURING SCHEDULED 18Y CHECK FOUND, SKIN CRACKED AT BS 873, STR 4L. REPAIRED SKIN PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,698 hrs · 49,389 cycles

DURING SCHEDULED 18Y CHECK FOUND, SKIN CRACKED AT BS 500C+3.5-6, STR 4L. REPAIRED SKIN PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,698 hrs · 49,389 cycles

DURING SCHEDULED 18Y CHECK FOUND, SKIN CRACKED BETWEEN BS 727E+16.25 TO BS 727E+17.5, STR 4L. REPAIRED SKIN PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,698 hrs · 49,389 cycles

DURING SCHEDULED 18Y CHECK FOUND, SKIN CRACKED AT BS 500C+4.25-7, STR 4R. REPAIRED SKIN PER ACO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 58,698 hrs · 49,389 cycles

DURING SCHEDULED 18Y CHECK FOUND, FRAME CORRODED AT BS 767, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,698 hrs · 49,389 cycles

DURING SCHEDULED 18Y CHECK FOUND, SKIN CRACKED BETWEEN BS 500B+12.5 TO BS 500B+14.5, STR 4R. REPAIRED SKIN PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,698 hrs · 49,389 cycles

DURING SCHEDULED 18Y CHECK FOUND, SKIN CRACKED BETWEEN BS 382 TO BS 385, STR 4R. REPAIRED SKIN PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,698 hrs · 49,389 cycles

DURING SCHEDULED 18Y CHECK FOUND, SKIN CRACKED AT BS 444.5 TO BS 445, STR 4L. REPAIRED SKIN PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,698 hrs · 49,389 cycles

DURING SCHEDULED 18Y CHECK FOUND, SKIN CRACKED BETWEEN BS 727A+3.5 TO BS 727A+16.5, STR 4R. REPAIRED SKIN PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,698 hrs · 49,389 cycles

DURING SCHEDULED 18Y CHECK FOUND, SKIN CRACKED AT BS 500D+5-6, STR 4R. REPAIRED SKIN PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,698 hrs · 49,389 cycles

DURING SCHEDULED 18Y CHECK FOUND, SKIN CRACKED BETWEEN BS 750.5 TO BS 751.75, STR 4L. REPAIRED SKIN PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,697 hrs · 49,389 cycles

DURING SCHEDULED SPV CHECK FOUND, SKIN CRACKED AT BS 500C+5, STR 10R. REPAIRED PER ACO.

Part: FLAP — DELAMINATED (LT WING) · airframe 58,159 hrs · 45,980 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING I/B MID FLAP I/B UPPER EDGE DELAMINATED. REMOVED AND REPLACED MID FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,647 hrs · 48,591 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 394, STR 4L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,523 hrs · 48,502 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 6R. REMOVED AND REPLACED CLIP PER SI AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,523 hrs · 48,502 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7R. REMOVED AND REPLACED CLIP PER SI AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,523 hrs · 48,502 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 10R. REMOVED AND REPLACED CLIP PER SI AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,523 hrs · 48,502 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 8R. REMOVED AND REPLACED CLIP PER SI AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,523 hrs · 48,502 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7L. REMOVED AND REPLACED CLIP PER SI AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,523 hrs · 48,502 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 5L. REMOVED AND REPLACED CLIP PER SI AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,535 hrs · 48,513 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 4L. REMOVED AND REPLACED CLIP PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 57,535 hrs · 48,513 cycles

EEPLS LOOSE BETWEEN ROW 9 TO ROW 11. REPAIRED EEPLS PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,535 hrs · 48,513 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 2R. REMOVED AND REPLACED CLIP PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,535 hrs · 48,513 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 1. REMOVED AND REPLACED CLIP PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,535 hrs · 48,513 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED CLIP PER MM.

Part: LIGHT — BROKEN (COCKPIT) · airframe 57,378 hrs · 48,391 cycles

NOSE LANDING GEAR INDICATED UNSAFE SHORT FINAL. MISSED APPROACH. VERIFIED GEAR DOWN VISUALLY. FOUND NLG GREEN DOWN KORRY LIGHT BROKEN. REMOVED AND REPLACED GREEN DOWN KORRY LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,293 hrs · 48,330 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 787+15, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,160 hrs · 48,226 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 432 TO BS 445, STR 1L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,160 hrs · 48,226 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 441 TO BS 445, STR 1L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,160 hrs · 48,226 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 426 TO BS 427, STR 1L. REPAIRED SKIN PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,883 hrs · 48,012 cycles

DURING SCHEDULED OTS CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 15R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,883 hrs · 48,012 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 507, STR 15R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,883 hrs · 48,012 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 942, STR 24L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,883 hrs · 48,012 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 507, STR 15R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,883 hrs · 48,012 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 942, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,436 hrs · 47,669 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 762, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,436 hrs · 47,669 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 486, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,436 hrs · 47,669 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 393, STR 4R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 56,439 hrs · 47,670 cycles

DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: HINGE — CRACKED (SPOILER) · airframe 55,488 hrs · 46,950 cycles

DURING SCHEDULED CV CHECK, FOUND RT WING GROUND SPOILER O/B HINGE CRACKED. REMOVED AND REPLACED SPOILER PER MM.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 55,267 hrs · 46,797 cycles

DURING SCHEDULED MV4 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: LENS — MISSING (CABIN) · airframe 55,024 hrs · 46,620 cycles

RT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,703 hrs · 46,384 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 504D, STR 16L. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 53,680 hrs · 45,612 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT OVERWING EMERGENCY EXIT SIGN LENS LOOSE. SECURED LENS PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 52,988 hrs · 45,080 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,988 hrs · 45,080 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,945 hrs · 45,048 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE BELLY SKIN CRACKED UNDER NR 3 VHF ANTENNA, BS 727D. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,896 hrs · 45,014 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT LOWER HINGE CUTOUT, BS 305, BETWEEN WL 240 TO WL 261. REPAIRED SKIN PER EA.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 52,896 hrs · 45,014 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR UPPER HINGE SUPPORT FITTING CRACKED AT BEAR STRAP CUTOUT. REMOVED AND REPLACED FITTING PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,896 hrs · 45,014 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT, BS 305, WL 261. REPAIRED SKIN PER EA.

Part: FUSE — BLOWN (CABIN) · airframe 52,895 hrs · 45,014 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED FUSE PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 52,896 hrs · 45,014 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CRACKED AT BS 277, BETWEEN STR 12R AND STR 13R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 52,896 hrs · 45,014 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT STRINGER CORRODED AT BS 947, STR 26L. REPAIRED STRINGER PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 52,896 hrs · 45,014 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD LAV EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT PER SRM.

Part: LENS — BROKEN (CABIN) · airframe 52,896 hrs · 45,014 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,896 hrs · 45,014 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 306 TO BS 340, BETWEEN LBL 56 TO LBL 61, WL 208. R&R BEAM PER SRM.

Part: SLAT — DELAMINATED (LT WING) · airframe 52,896 hrs · 45,014 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 2 SLAT O/B UPPER CORNER DELAMINATED. REPAIRED SLAT PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,896 hrs · 45,014 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,896 hrs · 45,014 cycles

DURING SCHEDULED 1/6Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2R. REMOVED AND REPLACED CLIP PER SRM.

Part: ATTACH FITTING — CORRODED (GIRT BAR) · airframe 52,896 hrs · 45,014 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH BRACKET MOUNT FITTINGS CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 52,896 hrs · 45,014 cycles

DURING SCHEDULED 16Y CHECK, FOUND NLG RT SIDE SNUBBER ATTACH POINT CEILING WEB CRACKED. REPAIRED PER ACO.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,896 hrs · 45,014 cycles

DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR CREASE BEAM CORRODED BETWEEN BS 283 TO BS 332, WL 208. REMOVED AND REPLACED BEAM PER BAC DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,896 hrs · 45,014 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM CORRODED BS 344, BETWEEN LBL 13 TO RBL 13, WL 208. REMOVED AND REPLACED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,896 hrs · 45,014 cycles

DURING SCHEDULED 1/6Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 3R. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,896 hrs · 45,014 cycles

DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR CREASE BEAM CORRODED BETWEEN BS 299 TO BS 332, WL 20. REMOVED AND REPLACED BEAM PER BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,896 hrs · 45,014 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 3R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,896 hrs · 45,014 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,896 hrs · 45,014 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 3L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,896 hrs · 45,014 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,896 hrs · 45,014 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,896 hrs · 45,014 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 3L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,896 hrs · 45,014 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: SIGN — OUT OF POSITION (CABIN) · airframe 52,652 hrs · 44,845 cycles

RT OVERWING EMERGENCY EXIT SIGN FELL OFF. INSTALLED SIGN PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 52,359 hrs · 44,642 cycles

L2 DOOR EMERGENCY EXIT LIGHT LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,289 hrs · 44,594 cycles

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 465 TO BS 505C, STR 10R. REPAIRED SKIN PER SRM AND EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,026 hrs · 44,398 cycles

DURING SCHEDULED MV3 CHECK, FOUND L1 DOOR EMERGENCY EVACUATION SLIDE LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 50,793 hrs · 43,521 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT ASSY LOOSE. SECURED LIGHT PER MM.

Part: SKIN — CRACKED (BS 504C S15R) · airframe 50,700 hrs · 43,447 cycles

DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 504C, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 506B S10R) · airframe 50,700 hrs · 43,447 cycles

DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 506B, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 922 S24L) · airframe 50,511 hrs · 43,312 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 922, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 922 S24L) · airframe 50,511 hrs · 43,312 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 922, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,088 hrs · 42,283 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 516D, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 48,228 hrs · 41,632 cycles

DURING SCHEDULED 14Y CHECK, FOUND LEFT WING OUTBOARD AFT FLAP OUTBOARD T/E DELAMINATED. REMOVED AND REPLACED LEFT WING AFT FLAP PER MM.

Part: SKIN — DELAMINATED (NR 6 SLAT) · airframe 48,228 hrs · 41,632 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT WING NR 6 L/E SLAT OUTBOARD END DELAMINATED. REPAIRED SLAT PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500C S27R) · airframe 48,228 hrs · 41,632 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 27R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 380 S8L) · airframe 48,228 hrs · 41,632 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 520 S8L) · airframe 48,228 hrs · 41,632 cycles

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

Part: FRAME — CRACKED (BS 440 S8L) · airframe 48,228 hrs · 41,632 cycles

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

Part: FRAME — CRACKED (BS 380 S8L) · airframe 48,228 hrs · 41,632 cycles

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

Part: FRAME — CRACKED (BS 787 S8L/R) · airframe 48,228 hrs · 41,632 cycles

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

Part: FRAME — CRACKED (BS 747 S8L) · airframe 48,228 hrs · 41,632 cycles

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

Part: FRAME — CRACKED (BS 400 S8L/R) · airframe 48,228 hrs · 41,632 cycles

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

Part: FRAME — CRACKED (BS 360 S8R) · airframe 48,228 hrs · 41,632 cycles

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

Part: FRAME — CRACKED (BS 907 S8L/R) · airframe 48,228 hrs · 41,632 cycles

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

Part: FRAME — CRACKED (BS 827 S8L) · airframe 48,228 hrs · 41,632 cycles

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

Part: FRAME — CRACKED (BS 827 S8R) · airframe 48,228 hrs · 41,632 cycles

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

Part: FRAME — CRACKED (BS 867 S8R) · airframe 48,228 hrs · 41,632 cycles

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

Part: CABLE — FRAYED (L2 DOOR SLIDE) · airframe 48,228 hrs · 41,632 cycles

DURING SCHEDULED 14Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM.

Part: ATTACH FITTING — WORN (NR 4 SPOILER) · airframe 48,228 hrs · 41,632 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WING NR 4 SPOILER INBOARD ATTACH FITTING LOOSE. REPAIRED FITTING PER SRM.

Part: ATTACH FITTING — BROKEN (NR 4 SPOILER) · airframe 47,726 hrs · 41,227 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LEFT WING NR 4 SPOILER ATTACH LUG BROKEN. REMOVED AND REPLACED NR 4 SPOILER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,929 hrs · 40,586 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 490, STR 10R. REPAIRED SKIN PER SWA EA.

Part: GLOWSTRIP — WORN (CABIN) · airframe 46,346 hrs · 40,135 cycles

DURING SCHEDULED SPV CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 10 DEF. REMOVED AND REPLACED STRIP PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,346 hrs · 40,135 cycles

DURING SCHEDULED SPV CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,346 hrs · 40,135 cycles

DURING SCHEDULED SPV CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,346 hrs · 40,135 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (BS 520 S10R) · airframe 44,700 hrs · 38,896 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 10R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 520 S10R) · airframe 44,454 hrs · 38,173 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 10R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 932 S24L) · airframe 44,454 hrs · 38,173 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 932, STR 24L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 44,191 hrs · 38,503 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT EXTERIOR LIGHT INOP AT L1 DOOR. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: BOLT — WORN (LT MLG) · airframe 43,161 hrs · 37,708 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT MLG BEAM ARM CLEVIS TO LOCK DOWN ASSY BOLT WORN. REMOVED AND REPLACED BOLT PER MM.

Part: BOLT — WORN (LT MLG) · airframe 43,161 hrs · 37,708 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT MLG STRUT UPPER ATTACH BOLT WORN. REMOVED AND REPLACED UPPER BOLT PER MM.

Part: BOLT — WORN (LT MLG) · airframe 43,161 hrs · 37,708 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT MLG STRUT LOWER ATTACH BOLT WORN. REMOVED AND REPLACED LOWER BOLT PER MM.

Part: COVER — BROKEN (CABIN) · airframe 42,918 hrs · 37,516 cycles

L1 DOOR EMERGENCY EXIT SIGN COVER BROKEN. R&R LIGHT ASSY PER MM.

Part: SPLICE — CRACKED (BS 359) · airframe 41,409 hrs · 36,384 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STR SPLICE CRACKED AT BS 359, STR 14L. REPAIRED STR SPLICE PER SRM.

Part: SKIN — CRACKED (BS 303) · airframe 41,409 hrs · 36,384 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED R1 DOOR FWD LOWER CUT OUT, BS 303, STR 18R. REPAIRED SKIN.

Part: FRAME — CRACKED (BS 303) · airframe 41,409 hrs · 36,384 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303 AND L1 DOOR CUT OUT LOWER STOP FITTING. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (BS 518D) · airframe 41,409 hrs · 36,384 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 518D, STR 12R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 515D) · airframe 41,409 hrs · 36,384 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515D, STR 10R. REPAIRED SKIN PER SWA EA.

Part: SHEAR TIE — CORRODED (BS 867) · airframe 41,409 hrs · 36,384 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPT FUSELAGE SHEAR TIE CORRODED AT BS 867, LBL4 TO RBL 5. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,409 hrs · 36,384 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SRM.

Part: WINDOW POST — CRACKED (COCKPIT) · airframe 41,409 hrs · 36,384 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R1 COCKPIT WINDOW UPPER POST CRACKED. REPAIRED WINDOW POST PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,803 hrs · 35,111 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT EQUIPMENT COOLING EXHAUST AFT CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (R1 DOOR) · airframe 39,793 hrs · 35,100 cycles

DURING SCHEDULED C1 CHECK, FOUND R1 DOOR SKIN CRACKED AT AFT UPPER FASTENER HOLE. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 39,793 hrs · 35,100 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: GIRT BAR — CRACKED (R2 DOOR) · airframe 39,793 hrs · 35,100 cycles

DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FLOOR FITTING CRACKED. REMOVED AND REPLACED FLOOR FITTING PER MM.

Part: LENS — LOOSE (CABIN) · airframe 39,749 hrs · 35,060 cycles

LEFT OVERWING EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED LENS PER MM.

Part: SIGN — LOOSE (EMERGENCY EXIT) · airframe 39,360 hrs · 34,726 cycles

LT OVERWING DOOR EMERGENCY EXIT SIGN CAME LOOSE. REINSTALLED SIGN PER MM.

Part: SKIN — DEBONDED (RT WING SPOILER) · airframe 38,887 hrs · 34,366 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING NR 6 SPOILER DISBONDED. REMOVED AND REPLACED RT NR 6 SPOILER PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 37,883 hrs · 33,596 cycles

R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 37,877 hrs · 33,591 cycles

DURING SCHEDULED C3 CHECK, LT ELEVATOR NR 1 TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LEFT ELEVATOR TAB NR 1 HINGE BUSHING PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 37,877 hrs · 33,591 cycles

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

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 37,708 hrs · 33,461 cycles

FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: SLIDE — WILL NOT TEST (R2 DOOR) · airframe 37,146 hrs · 32,998 cycles

DURING SPV, R2 DOOR EVAC SLIDE FAILED DEPLOYMENT TEST. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 36,584 hrs · 32,557 cycles

L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM.

Part: BUSHING — WORN (ELEVATOR) · airframe 36,028 hrs · 32,117 cycles

DURING SCHEDULED C1 CHECK, FOUND LT ELEVATOR TAB FAILED FREEPLAY CHECK. REMOVED AND REPLACED NR 1 TO NR 4 ELEVATOR TAB HINGE BUSHINGS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 35,539 hrs · 31,739 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520L, STRINGER 12L. REPAIRED SKIN CRACK PER SRM.

Part: SENSOR — FAULTY (NLG) · airframe 35,213 hrs · 31,487 cycles

INFLIGHT AT CRUISE RED NOSE GEAR LIGHT ILLUMINATED, WENT OUT ON ITS OWN. ON SHORT FINAL AFTER GOOD 3 GREEN, GREEN LIGHT OUT RED LIGHT ON, LANDING GEAR WARNING HORN, GO AROUND RECONFIGURED, THIS TIME NOSE GEAR GREEN. REMOVED AND REPLACED LOCK SENSOR PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,205 hrs · 30,716 cycles

DURING SCHEDULED PM CHECK, FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 34,062 hrs · 30,595 cycles

DURING SCHEDULED C1 CHECK, FOUND LT INBD AFT T/E FLAP DELAMINATED ON LOWER SURFACE. REMOVED AND REPLACED LT INBD AFT T/E FLAP PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,912 hrs · 30,474 cycles

DURING SCHEDULED PM CHECK, FOUND AFT SVC DOOR EXTERIOR AND RT AFT LOWER EXTERIOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: FITTING — CORRODED (VERT STAB) · airframe 33,285 hrs · 29,955 cycles

DURING SCHEDULED D CHECK, FOUND VERTICAL STAB AFT SPAR PRIMARY LUG AFT FACE CORRODED ON BOTH LT/RT SIDES. REPAIRED VERT STAB PER BFG ER.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 33,285 hrs · 29,955 cycles

DURING SCHEDULED D CHECK, FOUND FLOORBEAM CRACKED AT BS 947, WL 208 AND LBL 53. REPAIRED FLOORBEAM PER BFG ER.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 33,285 hrs · 29,955 cycles

DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR FRAME CRACKED AT CUTOUT FOR NR 5 STOP FITTING. REPAIRED FRAME PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,285 hrs · 29,555 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 868, RT SIDE AND BS 727B, LT SIDE. REPAIRED CREASE BEAM WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,285 hrs · 29,955 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, BETWEEN STR 8R AND STR 9R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,285 hrs · 29,955 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SVC DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,285 hrs · 29,955 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 767, STRINGER 22R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,285 hrs · 29,955 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 26R & STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,285 hrs · 29,955 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 927, RBL 4 TO LBL 4. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,285 hrs · 29,955 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 992, WL 209 & RBL 45. REPAIRED FRAME PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,285 hrs · 29,955 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 727D + 19 & BS 794, LT SIDE. REPAIRED CREASE BEAM WEB PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,285 hrs · 29,955 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 722B + 9 & BS 752, RT SIDE. REPAIRED CREASE BEAM WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,285 hrs · 29,955 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 639, STR 1. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,285 hrs · 29,955 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17L. REMOVED AND REPLACED FUSELAGE FRAME PER SRM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 33,174 hrs · 29,874 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD SERVICE DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH FITTING FASTENERS LOOSE. SECURED ATTACH FITTING PER MM.

Part: STRIP — LOOSE (CABIN) · airframe 32,330 hrs · 29,197 cycles

EEPLS PHOTOLUMINESCENT STRIP LOOSE BETWEEN ROWS NR 8 AND NR 10 AT BOTH ABC AND DEF. SECURED PHOTOLUMINESCENT STRIP PER MM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 32,207 hrs · 29,096 cycles

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

Part: SLIDE — OUT OF ADJUST (FWD ENTRY DOOR) · airframe 32,207 hrs · 29,296 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 30,872 hrs · 28,024 cycles

AFT GALLEY AREA EMERGENCY EXIT LIGHTS ARE INTERMITTENT. REMOVED AND REPLACED BATTERY PER MM.

Part: ROD END — BROKEN (LT WING) · airframe 29,782 hrs · 27,139 cycles

ABORTED TAKEOFF, DURING TAKEOFF THE L/E FLAP TRANSIT LIGHT AND THE NR 1 KRUGER FLAP TRANSIT LIGHT ILLUMINATED. REMOVED AND REPLACED NR 1 KRUGER FLAP TAILGATE ACTUATING ROD END PER MM.

Part: CONNECTOR — FAULTY (NR 2 ENGINE) · airframe 29,564 hrs · 26,961 cycles

AIR TURNBACK, DURING CLIMB NR 2 ENGINE EGT WENT TO 1250 AND OVER TEMP LIGHT ILLUMINATED. REMOVED AND REPLACED ELECT DISCONNECT D3302 PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 28,679 hrs · 26,266 cycles

EEPLS LOOSE AT ROWS NR 8 AND NR 9. SECURED EEPLS PER MM.

Part: CABLE — FRAYED (L2 DOOR) · airframe 28,564 hrs · 26,166 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 25,592 hrs · 23,682 cycles

DURING SCHEDULED 1/4D CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT AFT SVC DOOR LOWER FWD CORNER CUTOUT. REPAIRED SKIN PER SRM.

Part: DOOR FRAME — CRACKED (FWD CARGO BAY) · airframe 25,592 hrs · 23,682 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD CARGO DOOR FRAME CRACKED AT LOWER STOP, BS 493. REPAIRED DOOR FRAME PER T1-653-044.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 25,592 hrs · 23,682 cycles

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

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,592 hrs · 23,682 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAM WEB CRACKED AT RBL 17.1, UPPER SECTION. REPAIRED VERTICAL BEAM WEB PER RA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 25,592 hrs · 23,682 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CRACKED AT BS 787, RBL 13. REPAIRED FLOORBEAM PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,592 hrs · 23,682 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAM WEB CRACKED AT RBL 17, WL 277. REPAIRED VERTICAL BEAM WEB PER RA.

Part: BEAM — CORRODED (RT MLG) · airframe 25,292 hrs · 23,426 cycles

DURING SCHEDULED SEVICE CHECK, FOUND RT MLG STABILIZER BEAM FWD LUGS CORRODED. R&R STABILIZER BEAM PER MM.

Part: LIGHT — INOPERATIVE (CABIN FLOOR) · airframe 24,941 hrs · 23,121 cycles

EEPLS INOP AT MID CABIN. REPLACED 2 LIGHT ASSYS PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 24,209 hrs · 22,487 cycles

EEPLS WIRES EXPOSED AND BROKEN AT ROW 11. RECONNECTED WIRES AND INSTALLED COVERS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 23,832 hrs · 22,179 cycles

EEPLS TRACK LOOSE AT ROW 14. SECURED LIGHT TRACK PER MM.

Part: BLADE — BIRD STRIKE (NR 1 ENGINE) · airframe 23,549 hrs · 21,938 cycles

AIR TURNBACK, BIRD STRIKE TO NR 1 ENG FAN SECTION. C/W ENG AND BORESCOPE INSPS FOUND FAN BLADES NR 1, 2, 3, 4, 27, 38, 20, 17, 11, 12, 13, 14, 15, 18, 24, 29, 30, 32, AND 37 DAMAGED. REMOVED AND REPLACED A TOTAL OF 25 FAN BLADES PER MM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 22,782 hrs · 21,276 cycles

FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: LIGHT — INOPERATIVE (ROW 23)

EMERGENCY LIGHT FLOOR TRACK INOPERATIVE AT ROW 23. REMOVED AND REPLACED TRACK SECTION PER MM.

Part: WIRE — LOOSE (CABIN)

CABIN EMERGENCY ESCAPE FLOOR TRACK LIGHTING INOP AT FWD SECTION. RESECURED LOOSE WIRE AT SECTION.

Part: COVER — MISSING (CABIN)

CREW REPORTS EGRESS LIGHT COVER MISSING IN REAR PAX CABIN. REMOVED AND REPLACEDR EGRESS LIGHT COVER PER MM.

Part: LAMPS — FAILED (CABIN)

DURING PREFLIGHT CHECK, FOUND 3 FLOOR EMERGENCY EXIT LIGHTS INOP AND WIRES EXPOSED LT SIDE CABIN. REPAIRED AND RELAMPED PER BOEING M/M.

Part: FLOORBEAM — CORRODED (BS 727)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM AT BS 727+13, RBL 3. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 767-797)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED RT TRANSITION ANGLE FROM BS 767-797 RBL 21. REMOVED AND REPLACED PER BOEING SRM.

Part: CHORD — CORRODED (BS 986)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORROSION AROUND CLIP NUT HOLE AT BS 986 RBL 36 FWD LEG BS 986 RBL 35 AFT LEG AND BS 986 RBL 30 AFT LEG. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — DAMAGED (BS 797)

DURING SCHEDULED 1/2D CHECK, FOUND DAMAGED WEB FWD OF CARGO CUTOUT AT BS 797 RBL 25. REPAIRED PER BOEING SRM.

Part: CHORD — CORRODED (BS 986)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORROSION AROUND CLIP NUT HOLE AT BS 986 LBL AFT LEG BS 986 LBL 14 AFT LEG AND BS 1016 RBL 6. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CRACKED (BS 767)

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED FLOORBEAM AT BS 767 RBL 13. REPAIRED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 727-767)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED RT TRANSITION ANGLE AT BS 727A-767 RBL 21. REPAIRED PER BOEING SRM.

Part: WEB — DAMAGED (CARGO DOORWAY)

DURING SCHEDULED 1/2D CHECK, FOUND DAMAGED WEB AFT OF DOOR CUTOUT. REPAIRED PER BOEING SRM.

Part: WEB — DAMAGED (BS 1016)

DURING SCHEDULED 1/2D CHECK, FOUND DAMAGED FLOOR WEB AT BS 1016 RBL 15. REPAIRED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 767-797)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON RT TRANSITION ANGLE FROM BS 767 TO 797 RBL 21. REMOVED AND REPLACED PER BOEING SRM.

Part: CLIP — CORRODED (BS 328 & 986)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AROUND CLIP NUT HOLE AT BS 328 RBL 49 FWD LEG AND BS 986 LBL 35 FWD LEG. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 358)

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN DENTED AT BS 358, BETWEEN S17L AND 16L. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED C1 CHECK, FOUND EXTERNAL POWER DOOR CUTOUT CRACKED AT LOWER HINGE AREA. REPAIRED PER SWA RA 1-353-1703.

Part: BATTERY PACK — DISCHARGED (CABIN)

FOUND AFT CABIN LOWER EMERGENCY FLASHLIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M.