N375SW

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,383 hrs · 57,068 cycles

SKIN CRACKED AT BS 500A+17, STRINGER 2L. REPAIRED SKIN IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,147 hrs · 56,897 cycles

RIGHT LOWER EMER EXIT LIGHT COVER INOPERATIVE. R & R LIGHT ASSEMBLY IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,147 hrs · 56,897 cycles

LEFT LOWER EMER EXIT LIGHT COVER INOPERATIVE. R & R LIGHT ASSEMBLY IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,149 hrs · 56,898 cycles

LEFT OVERWING EMER EXIT LIGHT INOPERATIVE. R & R LIGHT ASSEMBLY IAW MM.

Part: O-RING — LEAKING (HYDRAULIC SYS) · airframe 69,097 hrs · 56,856 cycles

AIR TURN BACK & DECLARED EMER. LOSE OF SYS A HYD SYS. R & R O RING IAW AMM.

Part: WINDOW — ARCED (COCKPIT) · airframe 68,878 hrs · 56,704 cycles

L1 CAPTAINS FWD WINDSHIELD ARCED IN CTR OF L1, ABOUT 3/4 WAY DIAGONAL. R & R L1 WINDOW IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,777 hrs · 56,638 cycles

FUSELAGE CROWN SKIN CRACKED AT BS 500B+3, STRINGER 1L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,777 hrs · 56,638 cycles

FUSELAGE CROWN SKIN CRACKED AT BS 500C+3, STRINGER 2R. REPAIRED SKIN IAW SRM.

Part: SIGN — LOOSE (CABIN) · airframe 68,101 hrs · 56,143 cycles

RIGHT OVERWING EMER EXIT SIGN LOOSE. SECURED SIGN IAW AMM.

Part: LENS — LOOSE (CABIN) · airframe 67,883 hrs · 55,974 cycles

RIGHT OVERWING EMER EXIT LIGHT PANEL LENS LOOSE. SECURED LENS IAW AMM.

Part: LENS — MISSING (EXIT SIGN) · airframe 67,874 hrs · 55,967 cycles

OVERWING EXIT SIGN LENS MISSING. REINSTALLED LENS IAW SIP.

Part: COVER — DEBONDED (CABIN) · airframe 67,807 hrs · 55,916 cycles

RIGHT DOOR OVERHEAD EMER EXIT LIGHT COVER DISBONDED. BONDED COVER IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 67,807 hrs · 55,916 cycles

L1 DOOR EMER EXIT LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,807 hrs · 55,916 cycles

RIGHT DOOR LOWER EMER EXIT LIGHT BULB INOPERATIVE. R & R BULB IAW AMM.

Part: BRACKET — DAMAGED (L2 DOOR) · airframe 67,807 hrs · 55,916 cycles

L2 DOOR EMER EVAC SLIDE FLOOR BRACKET DAMAGED. R & R BASE IAW AMM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

SHEAR TIE CRACKED AT BS 967, BETWEEN STRINGER 26L - 27L. R & R SHEAR TIE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

SUPPORT ANGLE CRACKED BETWEEN BS 291.5 TO 294, STRINGER 17R. R & R ANGLE IAW SRM & DWG.

Part: SLAT — DELAMINATED (RT WING) · airframe 67,807 hrs · 55,916 cycles

RIGHT WING NR 4 SLAT ON INBD END AT LE DELAMINATED A UPPER TE AREA. REPAIRED NR 4 SLAT IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

TIE CLIP CRACKED AT BS 986.5, STRINGER 20L. R & R TIE CLIP IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

WEB CRACKED BETWEEN BS 277 - 294.5, STRINGER 17L. R & R WEB IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

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

Part: GLOWSTRIP — DETERIORATED (CABIN) · airframe 67,807 hrs · 55,916 cycles

LEFT EEPLS PHOTO LUMINESCENT STRIPS DETERIORATED. R & R STRIP IAW MM.

Part: GLOWSTRIP — DETERIORATED (CABIN) · airframe 67,807 hrs · 55,916 cycles

RIGHT EEPLS PHOTO LUMINESCENT STRIPS DETERIORATED. R & R STRIP IAW MM.

Part: WEB — CORRODED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

WEB CORRODED AT BS 348, STRINGER 17L. R & R WEB IAW SRM & DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

RIGHT STRINGER CORRODED BETWEEN BS 1116 TO 1128. R & R STRINGER IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

CLIP CRACKED AT BS 348.2, STRINGER 15L. R & R CLIP IAW SRM & DWG.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 67,807 hrs · 55,916 cycles

LEFT WING INBD FORE FLAP DELAMINATED ON UPPER SURFACE AT 48 INCHES OTBD END. REPAIRED FORE FLAP IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

RIGHT STRINGER CORRODED BETWEEN BS 1113 - 1124. R & R STRINGER IAW SRM & DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

SPLICE STRAP CRACKED AT BS 360, STRINGER 3R. REPAIRED STRAP IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

FRAME CORRODED AT BS 992.8, BETWEEN STRINGER 17A - 17R. REPAIRED FRAME IAW EO & EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

AFT PRESS BULKHEAD Z ANGLE CRACKED AT BS 1016, BETWEEN LBL 8.5 - 17. R & R Z ANGLE IAW SRM & DWG.

Part: LUG — CORRODED (TE FLAP) · airframe 67,807 hrs · 55,916 cycles

LEFT WING NR 4 FLAP TRACK INBD LUG CORRODED. REPAIRED LUG IAW CMM.

Part: LUG — CORRODED (TE FLAP) · airframe 67,807 hrs · 55,916 cycles

RIGHT WING NR 5 FLAP TRACK LUG CORRODED. REPAIRED LUG IAW CMM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

CENTER WING BOX DOUBLER CRACKED AT BS 639, RBL 45.5+7. R & R DOUBLER IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

FLOORBEAM UPPER CHORD CORRODED AT BS 328, LBL 26.75. REPAIRED CHORD IAW EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 67,807 hrs · 55,916 cycles

LEFT WING INBD FORE FLAP DELAMINATED ON UPPER SURFACE. REPAIRED FORE FLAP IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

FLOORBEAM CORRODED AT BS 986.5 LBL 14.5. REPAIRED FLOORBEAM IAW EO & EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

WEB CRACKED BETWEEN BS 312 - 328, RBL 31.6. R & R WEB IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

CLIP CRACKED AT BS 303.9+8, STRINGER 8L. R & R CLIP IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 67,807 hrs · 55,916 cycles

RIGHT WING NR 6 FLAP OTBD TRACK SUPPORT ANGLE CRACKED AT INBD CORNER. R & R ANGLE IAW SRM & DWG.

Part: WEDGE — DEBONDED (TE FLAP) · airframe 67,807 hrs · 55,916 cycles

RIGHT WING INBD MID FLAP SKIN LOWER SURFACE OF WEDGE PANEL DEBONDED. REPAIRED MID FLAP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

FUSELAGE SKIN CRACKED AT BS 967+12.5, STRINGER 21L. REPAIRED SKIN IAW EA.

Part: FLAP TRACK — CORRODED (RT WING) · airframe 67,807 hrs · 55,916 cycles

RIGHT WING NR 5 FLAP TRACK CORRODED ON INBD HOLE AFT POSITION. REPAIRED FLAP TRACK IAW CMM.

Part: FLAP TRACK — CORRODED (LT WING) · airframe 67,807 hrs · 55,916 cycles

LEFT WING NR 4 FLAP TRACK CORRODED ON INBD HOLE AFT POSITION. REPAIRED FLAP TRACK IAW CMM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

AFT CARGO COMPARTMENT ANGLE CRACKED BETWEEN BS 927 - 947.5. R & R ANGLE IAW SRM & DWG.

Part: ACCESS PANEL — CRACKED (RT PYLON) · airframe 67,807 hrs · 55,916 cycles

RIGHT PYLON NACELLE STRUT ACCESS PANEL 5864R CRACKED. REPAIRED PANEL IAW EO.

Part: SUPPORT — CRACKED (TE FLAP) · airframe 67,807 hrs · 55,916 cycles

RIGHT WING NR 7 FLAP TRACK AROUND SUPPORT STRUCTURE CRACKED. REPAIRED SUPPORT IAW EO & EA.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 67,807 hrs · 55,916 cycles

LEFT WING SUPPORT ANGLE CRACKED AT RSS 537.806 INTERNAL STRUCTURE TE. R & R ANGLE IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

FUSELAGE SKIN CRACKED AT BS 927+7, STRINGER 23L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

FUSELAGE SKIN CRACKED AT BS 967+4.25, STRINGER 21L. REPAIRED SKIN IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

FRAME INNER CHORD CRACKED AT BS 616, STRINGER 17R, THE LOWEST FASTENER POSITION. REPAIRED CHORD IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

FUSELAGE SKIN CRACKED AT BS 907+14.5, STRINGER 25L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

FUSELAGE SKIN CRACKED AT BS 927+13.750, STRINGER 23R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

SKIN CRACKED AT BS 520+4.0, STRINGER 8L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

FUSELAGE SKIN CRACKED AT BS 360+14, STRINGER 8L. REPAIRED SKIN IAW EO & EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

ANGLE CRACKED BETWEEN BS 277 - 291.5, STRINGER 10R. R & R ANGLE IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

FUSELAGE SKIN CRACKED AT BS 927+6.5, STRINGER 24R. REPAIRED SKIN IAW EO & EA.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

AFT CARGO COMPARTMENT CROSS BEAM E T CHORD CRACKED AT BS 827+13. REPAIRED T CHORD IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

INTERCOSTAL CRACKED BETWEEN BS 277 - 291.5, STRINGER 10R. R & R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

INTERCOSTAL CRACKED BETWEEN BS 277 - 291.5, STRINGER 14R. R & R INTERCOSTAL IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

FRAME INNER CHORD CRACKED BETWEEN BS 348.2 - 351.2, BETWEEN STRINGER 14L - 17L. REPAIRED FRAME IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

SKIN CRACKED AT BS 500D+4.5, STRINGER 8L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

FUSELAGE SKIN CRACKED AT BS 500B+5, STRINGER 8L. REPAIRED SKIN IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

FRAME CRACKED AT BS 520, BETWEEN STRINGER 19L - 21L. REPAIRED FRAME IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

FORWARD ENTRY DOOR FUSELAGE SKIN CUT OUT CRACKED BETWEEN BS 328 - 360, BETWEEN STRINGER 15L TO 19L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

SKIN CRACKED AT BS 360+14, STRINGER 8L. REPAIRED SKIN IAW EO & EA.

Part: FAIRING — CRACKED (LT AILERON TAB) · airframe 67,807 hrs · 55,916 cycles

LEFT WING AILERON TAB MAST FAIRING CRACKED. R & R FAIRING IAW DWG.

Part: LENS — DETERIORATED (CABIN) · airframe 67,807 hrs · 55,916 cycles

LEFT OVERWING EXIT SIDEWALL LIGHT LENS DETERIORATED. R & R LENS IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

L2 DOOR SKIN CUT OUT CRACKED AT BS 986.5+2, STRINGER 7L. REPAIRED SKIN IAW SRM.

Part: LENS — DETERIORATED (CABIN) · airframe 67,807 hrs · 55,916 cycles

RIGHT OVERWING EXIT SIDEWALL LIGHT LENS DETERIORATED. R & R LENS IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,807 hrs · 55,916 cycles

LEFT EMER EXIT SIDEWALL PANEL SIGN BULB INOPERATIVE. R & R BULB IAW AMM.

Part: LENS — BROKEN (EXIT SIGN) · airframe 67,807 hrs · 55,916 cycles

LEFT EMER EXIT SIGN LENS BROKEN. R & R LENS IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

L2 DOOR SKIN CUT OUT UPPER AFT CORNER CRACKED AT BS 986.5+2, STRINGER 7L. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

FRAME OTBD CHORD CRACKED AT BS 727, BETWEEN STRINGER 18R - 27R, FWD LOWER HOLE. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,807 hrs · 55,916 cycles

FRAME OTBD CHORD CRACKED AT BS 7, STRINGER 18A LT. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,879 hrs · 55,243 cycles

FUSELAGE CROWN SKIN CRACKED AT BS 807 STRINGER 2R. R & R SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,879 hrs · 55,243 cycles

FUSELAGE CROWN SKIN CRACKED AT BS 827 STRINGER 2R. R & R SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,879 hrs · 55,243 cycles

FUSELAGE CROWN SKIN CRACKED AT BS 727B STRINGER 2L. R & R SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,879 hrs · 55,243 cycles

FUSELAGE CROWN SKIN CRACKED AT BS 787 STRINGER 2R. R & R SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,879 hrs · 55,243 cycles

FUSELAGE CROWN SKIN CRACKED AT BS 801 STRINGER 2R. R & R SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,879 hrs · 55,243 cycles

FUSELAGE CROWN SKIN CRACKED AT BS 847 STRINGER 1L. R & R SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,879 hrs · 55,243 cycles

FUSELAGE CROWN SKIN CRACKED AT BS 727A STRINGER 2L. R & R SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,879 hrs · 55,243 cycles

FUSELAGE CROWN SKIN CRACKED AT BS 801 STRINGER 1L. R & R SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,879 hrs · 55,243 cycles

FUSELAGE CROWN SKIN CRACKED AT BS 847 STRINGER 1L. R & R SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,879 hrs · 55,243 cycles

FUSELAGE CROWN SKIN CRACKED AT BS 807 STRINGER 1L. R & R SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,879 hrs · 55,243 cycles

FUSELAGE CROWN SKIN CRACKED AT BS 807 STRINGER 2L. R & R SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,879 hrs · 55,243 cycles

FUSELAGE CROWN SKIN CRACKED AT BS 727C STRINGER 26. R & R SKIN IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,876 hrs · 55,241 cycles

STRINGER CLIP CRACKED AT BS 727E STRINGER 8R. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,876 hrs · 55,241 cycles

STRINGER CLIP CRACKED AT BS 727D STRINGER 5R. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,876 hrs · 55,241 cycles

CRACKED STRINGER CLIP CRACKED AT BS 907 STRINGER 8L. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,876 hrs · 55,241 cycles

STRINGER CLIP CRACKED AT BS 727C STRINGER 4L. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,876 hrs · 55,241 cycles

STRINGER CLIP CRACKED AT BS 807 STRINGER 3R. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,876 hrs · 55,241 cycles

STRINGER CLIP CRACKED AT BS 887 STRINGER 2L. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,876 hrs · 55,241 cycles

STRINGER CLIP CRACKED AT BS 847 STRINGER 2R. REPAIRED CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,876 hrs · 55,241 cycles

STRINGER CLIP CRACKED AT BS 847 STRINGER 1. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,876 hrs · 55,241 cycles

STRINGER CLIP CRACKED AT BS 787 STRINGER 1. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,876 hrs · 55,241 cycles

STRINGER CLIP CRACKED AT BS 867 STRINGER 2R. REPAIRED CLIP IAW SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 66,876 hrs · 55,241 cycles

STRINGER CRACKED AT BS 900 STRINGER 3L. REPAIRED STRINGER IAW SRM.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 66,876 hrs · 55,241 cycles

SHEAR TIE DAMAGED AT BS 887, BETWEEN STRINGER 1 TO 2L. R & R SHEAR TIE IAW SRM & DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 66,876 hrs · 55,241 cycles

STRINGER CRACKED AT BS 841 STRINGER 1. REPAIRED STRINGER IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,876 hrs · 55,241 cycles

STRINGER CLIP CRACKED AT BS 727C STRINGER 1L. R & R CLIP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,876 hrs · 55,241 cycles

FUSELAGE CROWN SKIN CRACKED AT BS 727B+13, STRINGER 2L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,875 hrs · 55,241 cycles

FUSELAGE CROWN SKIN CRACKED AT BS 727A + 12 STRINGER 2L. REPAIRED SKIN IAW ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,876 hrs · 55,241 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,876 hrs · 55,241 cycles

SKIN CRACKED AT BS 807 STRINGER 2R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,876 hrs · 55,241 cycles

SKIN CRACKED AT BS 847 STRINGER 1L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,974 hrs · 55,315 cycles

FUSELAGE CROWN SKIN CRACKED AT BS 727C+7, STRINGER 2L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,876 hrs · 55,241 cycles

SKIN CRACKED AT BS 807 STRINGER 2L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,974 hrs · 55,315 cycles

FUSELAGE CROWN SKIN CRACKED AT BS 807, STRINGER 1L. REPAIR SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,876 hrs · 55,241 cycles

SKIN CRACKED AT BS 847 STRINGER 1L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,875 hrs · 55,241 cycles

FUSELAGE CROWN SKIN CRACKED AT BS 847 STRINGER 1L. REPAIRED SKIN IAW ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,974 hrs · 55,315 cycles

FUSELAGE CROWN SKIN CRACKED AT BS 801, STRINGER 1L. REPAIR SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,876 hrs · 55,241 cycles

SKIN CRACKED AT BS 787 STRINGER 2R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,876 hrs · 55,241 cycles

SKIN CRACKED AT BS 827 STRINGER 2R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,876 hrs · 55,241 cycles

SKIN CRACKED AT BS 727B STRINGER 2L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,876 hrs · 55,241 cycles

SKIN CRACKED AT BS 801 STRINGER 2R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,876 hrs · 55,241 cycles

SKIN CRACKED AT BS 807 STRINGER 2L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,876 hrs · 55,241 cycles

SKIN CRACKED AT BS 801 STRINGER 2R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,876 hrs · 55,241 cycles

SKIN CRACKED AT BS 827 STRINGER 2R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,876 hrs · 55,241 cycles

SKIN CRACKED AT BS 787 STRINGER 2R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,871 hrs · 55,239 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,871 hrs · 55,239 cycles

SKIN CRACKED AT BS 727B STRINGER 2L. REPAIRED SKIN IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,871 hrs · 55,239 cycles

FUSELAGE CROWN SKIN CRACKED AT BS 801, STRINGER 1L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,871 hrs · 55,239 cycles

FUSELAGE CROWN SKIN CRACKED AT BS 727C+7, STRINGER 2L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,871 hrs · 55,239 cycles

FUSELAGE CROWN SKIN CRACKED AT BS 807, STRINGER 1L. REPAIRED SKIN IAW SRM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,664 hrs · 54,385 cycles

R2 DOOR EMERGENCY EXIT LIGHT BULB INOPERATIVE. REPLACED BULB IAW MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 65,664 hrs · 54,384 cycles

L2 DOOR EMERGENCY EXIT LIGHT DAMAGED. R & R LIGHT ASSEMBLY IAW AMM.

Part: STIFFENER — CORRODED (BS 1016) · airframe 65,664 hrs · 54,384 cycles

CHANNEL STIFFENER CORRODED AT BS 1016, RBL 1. REPAIRED STIFFENER IAW EA.

Part: STIFFENER — CORRODED (BS 1016) · airframe 65,664 hrs · 54,384 cycles

STIFFENER CORRODED AT BS 1016+1, LBL 1. REPAIRED STIFFENER IAW EA.

Part: STRINGER — CORRODED (BS 1006-1016) · airframe 65,664 hrs · 54,384 cycles

STRINGER 26R CORRODED BETWEEN BS 1006 - 1016. R & R STRINGER IAW SRM.

Part: ANGLE — CRACKED (RT WING) · airframe 65,664 hrs · 54,384 cycles

RIGHT WING LOWER TE PANEL SUPPORT CRACKED JUST OTBD OF NR 6 FLAP TRACK FAIRING. REPAIRED ANGLE IAW EA.

Part: SKIN — CRACKED (BS 341) · airframe 65,664 hrs · 54,384 cycles

FUSELAGE SKIN CRACKED AT BS 341, STRINGER 2L. REPAIRED SKIN IAW SRM.

Part: LENS — LOOSE (CABIN) · airframe 65,566 hrs · 54,315 cycles

RT OVERWING EXIT LIGHT LENS LOOSE. REINSTALLED RT OVERWING EXIT LIGHT LENS IAW MM.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 65,357 hrs · 54,176 cycles

R1 DOOR LOWER FRAME CRACKED AT AFT LOWER STOP ATTACH POINT. R & R R1 DOOR ASSEMBLY IAW MM.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 65,357 hrs · 54,176 cycles

FWD ENTRY DOOR UPPER AFT STOP POST CRACKED IN UPPER RADIUS. R & R POST IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,293 hrs · 54,126 cycles

R2 DOOR EMERGENCY EXIT SLIDE LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: SUPPORT FITTING — CORRODED (TE FLAP) · airframe 64,243 hrs · 53,376 cycles

LT WING NR 2 FLAP TRACK AFT SUPPORT FITTING OTBD HOLE CORRODED. R & R FITTING IAW SRM.

Part: LENS — LOOSE (CABIN) · airframe 63,509 hrs · 52,804 cycles

LEFT OVERWING DOOR EMERGENCY EXIT LENS LOOSE. SECURED LENS IAW MM.

Part: ACTUATOR — LEAKING (RT SPOILER) · airframe 62,939 hrs · 52,374 cycles

RIGHT WING INBOARD GROUND SPOILER LEAKED. REMOVED AND REPLACED GROUND SPOILER ACTUATOR PER MM.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 62,858 hrs · 52,322 cycles

RIGHT WING LOWER AREA TRAILING EDGE SUPPORT ANGLE CRACKED. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: PAN — CRACKED (LT PYLON) · airframe 62,858 hrs · 52,322 cycles

LEFT PYLON HEAT SHIELD STRUT FAIRING PAN CRACKED. REPAIRED PAN IAW EA.

Part: FITTING — CRACKED (LT PYLON) · airframe 62,858 hrs · 52,322 cycles

LEFT PYLON NACELLE TO FLAP TRACK FAIRING INTERFACE FITTING CRACKED. REPAIRED FITTING IAW EA.

Part: SKIN — DELAMINATED (NR 7 SPOILER) · airframe 62,858 hrs · 52,322 cycles

RIGHT WING NR 7 FLIGHT SPOILER UPPER SURFACE DELAMINATED. REPAIRED SPOILER IAW SRM.

Part: ANGLE — CRACKED (RT WING) · airframe 62,858 hrs · 52,322 cycles

RIGHT WING ANGLE CRACKED. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: ANGLE — CRACKED (TE FLAP) · airframe 62,858 hrs · 52,322 cycles

INTERNAL ANGLE OF THE NR 8 O/B FLAP TRACK FAIRING SUPPORT CRACKED. REMOVED AND REPLACED ANGLE PER SRM.

Part: SUPPORT — CRACKED (TE FLAP) · airframe 62,858 hrs · 52,322 cycles

INTERNAL ANGLE OF THE NR 7 O/B FLAP TRACK FAIRING SUPPORT CRACKED. REMOVED AND REPLACED ANGLE PER SRM.

Part: ANGLE — CRACKED (FLAP TRACK) · airframe 62,858 hrs · 52,322 cycles

NR 6 FLAP TRACK ANGLE, INTERNAL AREA SIDE OF THE DOOR, RIGHT WING CRACKED. REMOVED AND REPLACED ANGLE PER SRM.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 62,858 hrs · 52,322 cycles

CRACK ON SUPPORT ANGLE LOCATED ON INTERNAL AREA FLAP TRACK NR 3 AT LEFT WING. REMOVED AND REPLACED SUPPORT ANGLE PER SRM.

Part: SKIN — CRACKED (LT WING) · airframe 62,858 hrs · 52,322 cycles

LEFT WING LEADING EDGE SKIN AT WBL 208 CRACKED. REPAIRED LEADING EDGE PER EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

SUPPORT ANGLE CRACKED AT BS 341, BETWEEN STR 16L AND STR 17L. REMOVED AND REPLACED ANGLE IAW SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 62,858 hrs · 52,322 cycles

LEFT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: WEB — CRACKED (RT NLG WW) · airframe 62,858 hrs · 52,322 cycles

RIGHT NLG WHEEL WELL WEB CRACKED AT BS 243.7+3.5, WL 169.1. REPAIRED WEB IAW EO AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

FUSELAGE SKIN CRACKED AT BS 500D + 4, STR 16L. REPAIRED SKIN IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

SHEAR TIE FRAME AT BS 344, STR 27R CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

SUPPORT ANGLE AT BS 351, E/E COMPARTMENT CRACKED. REMOVED AND REPLACED SUPPORT ANGLE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

SKIN CRACKED AT BS 727B+4, STR 1R. REPAIRED SKIN IAW EA.

Part: WEB — CRACKED (NLG WW) · airframe 62,858 hrs · 52,322 cycles

RIGHT NLG WHEEL WELL WEB CRACKED AT BS 243.7+4.5, WL 169.1. REPAIRED WEB IAW EO AND EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

ANGLE AT BS 294.5, STR 23L CRACKED. REMOVED AND REPLACED ANGLE PER SRM.

Part: FLAP — CORRODED (RT WING) · airframe 62,858 hrs · 52,322 cycles

RIGHT WING O/B MID FLAP CORRODED. REMOVED AND REPLACED MID FLAP IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

SKIN CRACKED AT BS 727C+4, STR 1R. REPAIRED SKIN IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

CRACK ON TIE CLIP LOCATED BS 380 AND STR 22L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

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

Part: STIFFENER — CRACKED (LT WING) · airframe 62,858 hrs · 52,322 cycles

LEFT WING FUEL TANK STRUCTURE STIFFENER CRACKED AT WBL 114.00+6. REPAIRED STIFFENER IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

SKIN CRACKED AT BS 328, STR 17R. REPAIRED SKIN IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

SUPPORT ANGLE CRACKED AT BS 540, BETWEEN STR 28L TO STR 24L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

CRACK ON WEB BETWEEN BS 312 TO BS 328, LBL 47. REMOVED AND REPLACED WEB IAW SRM.

Part: CABLE — FRAYED (EVAC SLIDE) · airframe 62,858 hrs · 52,322 cycles

R2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED CABLE IAW AMM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

STRAP BETWEEN BS 312 AND BS 344, LBL 11.10 UPPER STRUCTURE E/E COMPARTMENT CRACKED. REMOVED AND REPLACED STRAP PER SRM.

Part: FITTING — CRACKED (LT WING) · airframe 62,858 hrs · 52,322 cycles

LEFT WING TRAILING EDGE FITTING CRACKED AT WBL 84.64. REMOVED AND REPLACED FITTING IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

WEB BETWEEN BS 328 AND BS 344, LBL 47 UPPER STRUCTURE E/E COMPARTMENT CRACKED. REMOVED AND REPLACED WEB PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

SUPPORT ANGLE AT BS 328, RBL 37 UPPER STRUCTURE E/E COMPARTMENT CRACKED. REMOVED AND REPLACED SUPPORT ANGLE PER SRM.

Part: CABLE — FRAYED (EVAC SLIDE) · airframe 62,858 hrs · 52,322 cycles

L2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED CABLE IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

CRACK ON ANGLE AT BS 807 BETWEEN STR 26R AND STR 25R AFT. REMOVED AND REPLACED ANGLE PER SRM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

GUSSET CRACKED AT STA 887, BETWEEN STR 20R & STR 21R. REMOVED AND REPLACED GUSSET APR SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

CRACK ON SUPPORT ANGLE LOCATED BS 328, LBL 47. REMOVED AND REPLACED ANGLE IAW SRM.

Part: PLATE — CRACKED (MLG WW) · airframe 62,858 hrs · 52,322 cycles

CRACK ON PLATE LOCATED ON STRUCTURE OF THE MAIN WHEEL WELL AREA, BETWEEN BS 695 TO BS 727, BBL 70 APPROX. REMOVED AND REPLACED PLATE IAW SRM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

CRACK ON BRACKET BETWEEN BS 727A TO BS 727B, BETWEEN STR 21L TO STR 20L. REMOVED AND REPLACED BRACKET IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

L2 DOOR SKIN CUTOUT CRACKED. REPAIRED SKIN IAW SRM.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

SUPPORT CLIP AT BS 360, STR 11L CRACKED. REMOVED AND REPLACED SUPPORT CLIP PER SRM.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 62,858 hrs · 52,322 cycles

LEFT HORIZONTAL STABILIZER STIFFENER CRACKED AT STA 121.50. REMOVED AND REPLACED STIFFENER IAW EA.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

SHEAR WEB CRACKED BETWEEN BS 348.2 TO BS 351.2, BETWEEN STR 15L TO STR 17L. REMOVED AND REPLACED SHEAR WEB IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

SUPPORT ANGLE AT BS 344, BETWEEN STR 7L TO STR 10L FWD CABIN CRACKED. REMOVED AND REPLACED SUPPORT ANGLE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

FRAME CRACKED AT BS 312, BETWEEN STR 4L TO STR 6L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

FRAME CRACKED AT BS 344, STR 17L. REMOVED AND REPLACED FRAME IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

CRACK ON SUPPORT ANGLE LOCATED ON BS 380, STR 26L. REMOVED AND REPLACED ANGLE PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

CRACK ON STIFFENER BETWEEN BS 294.5 TO BS 303.9, STR 16L. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

SUPPORT ANGLE CRACKED AT STA 328 TO STA 344, STR 6L. REMOVED AND REPLACED ANGLE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

SKIN CRACKED AT BS 727B+4, STR 1L. REPAIRED SKIN IAW EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

STRINGER CORRODED BETWEEN BS 380 TO BS 400, STR 17L. REMOVED AND REPLACED STRINGER IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

FRAME CORRODED AT BS 727D, BETWEEN STR 27R AND STR 27L. REPAIRED FRAME IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

ANGLE CRACKED AT BS 787 + 2.5, STR 18R. REMOVED AND REPLACED ANGLE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

SKIN CRAKCED AT BS 727B+4, STR 1L. REPAIRED SKIN IAW EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

WEB CORRODED BETWEEN BS 420 TO BS 440, STR 17L. REPAIRED WEB IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

WEB CRACKED AT BS 787+1, STR 18R. REPAIRED ANGLE IAW EO AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

SKIN CRACKED AT BS 727C+4, STR 1. REPAIRED SKIN IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

FRAME CORRODED AT BS 767, BETWEEN STR 27R AND STR 27L. REPAIRED FRAME IAW SRM AND DWG.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 62,858 hrs · 52,322 cycles

MAIN WHEEL WELL PRESSURE DECK CRACKED AT BS 663.75+1, LBL 24.5+6". REMOVED ANAD REPLACED WEB IAW EO AND EA.

Part: SKIN — CRACKED (L1 DOOR) · airframe 62,858 hrs · 52,322 cycles

CRACK ON EDGE OF INTERNAL SKIN ON FWD ENTRY DOOR. REPAIRED SKIN IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 669, RBL 24.5. REPAIRED CHORD IAW EO AND EA.

Part: SUPPORT ANGLE — CRACKED (ENTRY DOOR) · airframe 62,858 hrs · 52,322 cycles

CRACK ON SUPPORT ANGLE LOWER AREA OF THE AFT ENTRY DOOR INTERNAL STRUCTURE. REMOVED AND REPLACED ANGLE IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 669, RBL 24.5. REPAIRED CHORD IAW EA.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 62,858 hrs · 52,322 cycles

CRACK ON INTERNAL DOUBLER LOCATED EXTERNAL POWER ACCESS PANEL BETWEEN BS 227 TO BS 235, WL 176 RT. REPAIRED DOUBLER IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,707 hrs · 52,208 cycles

4 INCH CRACK IN FUSELAGE SKIN LOCATED AT BS 500D & 15 ABOVE STR 16R. REPAIRED PER SRM 53-00-01-2R-31 EA 1-353-21579. REF TO EA'S FOR SIGNOFFS. FACT AS A RESULT OF POST REPAIR INSPECTION

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,707 hrs · 52,208 cycles

4 INCH CRACK IN FUSELAGE SKIN LOCATED AT BS 500D & 15 ABOVE STR 16R. REPAIRED PER SRM 53-00-01-2R-31 EA 1-353-21579. REF TO EA'S FOR SIGNOFFS.

Part: SKIN — CRACKED (LE SLAT) · airframe 62,411 hrs · 51,986 cycles

RIGHT WING NR 6 SLAT LWR SKIN CRACKED AT O/B END. REPAIRED RIGHT WING NR 6 SLAT LWR SKIN O/B END PER B737 SRM 57-43-01-2R-6.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,411 hrs · 51,986 cycles

STA 947 AT S24L INTERCOSTAL O/B SIDE OF WATER SERVICE PAN, FWD CLIP IS CRACKED. REMOVED AND REPLACED CLIP ON FWD END OF INTERCOSTAL AT STA 947 STR 24L PER B737 SRM 51-40-02.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 62,411 hrs · 51,986 cycles

AFT FLOOR LEFT CARGO TRACK APPROX STA 947 HAS CORROSION AROUND NUT PLATES. REMOVED AND REPLACED AFT CARGO FLOOR TIE DOWN TRACK IAW B737-300 SRM 51-40-02, AND B737-300 DWG 69-36682, PO 762014.1

Part: STRINGER — CORRODED (FUSELAGE) · airframe 62,411 hrs · 51,986 cycles

STR 26L AT STA 947 HAS CORROSION ON BOTTOM RADIUS. CUT AND REMOVED CORRODED STRINGER 26L FROM STA 937 TO 967+5 IAW B373 SRM 53-00-03-2R-1. REPAIRED BY SPLICING IN NEW STRINGER SECTION IAW B737 SRM 53-00- 03-2R-1.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,411 hrs · 51,986 cycles

FRAME 947 AT STR 26L HAS CORROSION ON SHEAR TIE. REMOVED AND REPLACED SHEAR TIE AT STA 947 STA 25L TO STR 26L PER BAC DWG 65-46560 REV F. REMOVED AND RE-INSTALLED INTERCOSTAL AT STA 927 TO STA 947.5 PER B377 SRM 51-40-02.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 62,411 hrs · 51,986 cycles

STRINGER 27L BS 967 IS CORRODED JUST AFT OF THE STRINGER CLIP. REPAIRED BY SPLICING IN NEW STRINGER SECTION FROM STA 947.5+10 TO STA 967+10 IAW B737 SRM 53-00-03-2R-1.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,411 hrs · 51,986 cycles

BS 947 AT S25R STRINGER CLIP IS CRACKED. REMOVED AND REPLACED STRINGER CLIP PER DWG 65-46560 & REO G15685 REV IR AND EA 1-353-21280.

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 62,411 hrs · 51,986 cycles

BS 967 BETWEEN AT S19R FAILSAFE CHORD IS CRACKED. REMOVED AND REPLACED CRACKED FAILSAFE CHORD P/N 65-46563-8 PO 760882.1 BS 967 UPPER SECTION AT STRINGER 19R IAW BAC DWG 65-46563 AND B737-300 SRM 51-40-02.

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 62,411 hrs · 51,986 cycles

BS 967 BETWEEN STR 23-24R FAILSAFE CHORD CRACKED. REMOVED AND REPLACED CHORD IAW BAC DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 62,411 hrs · 51,986 cycles

STRINGER 25R AT STA 967+10 HAS CORROSION ON THE BOTTOM FLANGE. PERFORMED STRINGER SPLICE REPAIR ON STGR 25R AT STA 950-1016 PER B737 SRM 53-00-03-2R-1, REO G15685 AND EA.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 62,411 hrs · 51,986 cycles

S23R BACK SIDE OF FRAME STA 967 BRACKET IS CRACKED. REMOVED AND REPLACED BRACKET ON S23R STA 967 BACKSIDE PER BAC DWG.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 62,411 hrs · 51,986 cycles

S23R FRONT SIDE OF FRAME STA 967 BRACKET IS CRACKED. REMOVED AND REPLACED BRACKET P/N ON FRONT SIDE PER BAC DWG 65-51627.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 62,411 hrs · 51,986 cycles

S24R BACK SIDE OF FRAME STA 967 BRACKET IS CRACKED. REMOVED AND REPLACED BRACKET ON BACKSIDE OF STA 967, S24R PER BAC DWG.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 62,411 hrs · 51,986 cycles

S24R FRONT SIDE OF FRAME STA 967 BRACKET IS CRACKED. REMOVED AND REPLACED BRACKET FRONT SIDE OF STA 967 S24R PER ABC DWG.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 62,408 hrs · 51,985 cycles

A/C HAS DAMAGE FUSELAGE FRAME AND SHEAR TIE AT BS 965 TO BS 967 BETWEEN STR 23R AND 24R. REMOVED AND REPLACED PER EA REO. (SUBMITTED AS A SUPPLEMENTAL, COULDN`T FIND ORIGINAL RECORD.)

Part: FLAP — DELAMINATED (RT WING) · airframe 62,349 hrs · 51,941 cycles

RIGHT WING O/B AFT FLAP DELAMINATED INBOARD END. REMOVED AND REPLACED AFT FLAP PER AMM.

Part: LIGHT — LOOSE (CABIN) · airframe 62,349 hrs · 51,941 cycles

LEFT EEPLS LOOSE BETWEEN ROWS 6 TO ROW 7. SECURED EEPLS PER MM.

Part: FLAP — CHAFED (RT WING) · airframe 62,349 hrs · 51,941 cycles

RIGHT WING O/B FORE FLAP L/E CHAFED AT INBOARD END. REMOVED AND REPLACED FORE FLAP IAW THE AMM.

Part: LENS — LOOSE (CABIN) · airframe 62,212 hrs · 51,852 cycles

LEFT EMERGENCY EXIT ROW LIGHT LOOSE. SECURED LENS PER AMM.

Part: LENS — LOOSE (CABIN) · airframe 61,863 hrs · 51,588 cycles

LEFT EMERGENCY EXIT ROW SIGN LOOSE. SECURED LENS PER EA.

Part: LIGHT — BROKEN (CABIN) · airframe 61,115 hrs · 51,036 cycles

L1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER M/M.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,539 hrs · 50,588 cycles

FUSELAGE SKIN CRACKED AT BS 390 + 1, STR 1L. REPAIRED SKIN PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 60,394 hrs · 50,481 cycles

AT CRUISE FLIGHT FL 370 EMERGENCY EXIT TRACK LIGHT LOOSE. SECURED LIGHT PER AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,887 hrs · 49,050 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE WINDOW SKIN CRACKED AT BS 420+10, UPPER FWD CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 59,828 hrs · 50,068 cycles

DURING SCHEDULED CV CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,828 hrs · 50,068 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 907+35.0, STR 24L. REPAIRED SKIN IAW EA.

Part: LIGHT — BROKEN (CABIN) · airframe 59,418 hrs · 49,754 cycles

LEFT EEPLS BROKEN BETWEEN ROW 6 TO ROW 8. REMOVED AND REPLACED EEPLS PER MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 58,783 hrs · 49,283 cycles

DURING SCHEDULED 12Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 72E+5, STR 17R. REPAIRED WEB IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 58,783 hrs · 49,283 cycles

DURING SCHEDULED 12Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 807, STR 17L. REPAIRED WEB IAW SRM AND DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 58,783 hrs · 49,283 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,783 hrs · 49,283 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 500D+12 TO BS 500D+14, STR 16L. REPAIRED SKIN IAW EA.

Part: WIRE — DAMAGED (CABIN) · airframe 58,783 hrs · 49,283 cycles

DURING SCHEDULED SPV CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 8. REPAIRED WIRE PER WDM.

Part: LIGHT — BROKEN (EXTERIOR) · airframe 58,783 hrs · 49,283 cycles

DURING SCHEDULED SPV CHECK, FOUND L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT BULB BROKEN. REMOVED AND REPLACED BULB PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 58,783 hrs · 49,283 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME INNER CHORD CORRODED AT BS 639, LBL 65. REMOVED AND REPLACED CHORD PER SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,783 hrs · 49,283 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 894 TO BS 895.5, STR 2L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,783 hrs · 49,283 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN AT CHEM MILL CRACKED BETWEEN BS 832.5 TO BS 833.25, STR 4R. REPAIRED SKIN PER DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,783 hrs · 49,283 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN AT CHEM MILL CRACKED BETWEEN BS 752 TO BS 753, STR 4R. REPAIRED SKIN PER DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,783 hrs · 49,283 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN AT CHEM MILL CRACKED BETWEEN BS 840.5 TO BS 843.5, STR 4L. REPAIRED SKIN PER DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,783 hrs · 49,283 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN AT CHEM MILL CRACKED BETWEEN BS 727B+15.5 TO BS 727B+16.75, STR 4R. REPAIRED SKIN PER DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,783 hrs · 49,283 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN AT CHEM MILL CRACKED AT BS 727E+14.5+15, STR 4L. REPAIRED SKIN PER DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,783 hrs · 49,283 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN AT CHEM MILL CRACKED BETWEEN BS 727+16.5 TO BS 727+17, STR 4R. REPAIRED SKIN PER DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,783 hrs · 49,283 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 851 TO BS 854, STR 4R. REPAIRED SKIN PER ACO AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,783 hrs · 49,283 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 727D+14, STR 4L. REPAIRED SKIN PER ACO AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,783 hrs · 49,283 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 727C+14.5, STR 4L. REPAIRED SKIN PER ACO AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,783 hrs · 49,283 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 840 TO BS 841.5, STR 4R. REPAIRED SKIN PER ACO AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,783 hrs · 49,283 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 727A+13, STR 4L. REPAIRED SKIN PER ACO AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,067 hrs · 48,746 cycles

DURING SCHEDULED 18Y CHECK, FOUND AFT CARGO DOOR SKIN CUTOUT, LOWER FORWARD CORNER INNER BEARSTRAP CRACKED. REPAIRED SKIN PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,067 hrs · 48,746 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, BETWEEN STR 28R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,067 hrs · 48,746 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,067 hrs · 48,746 cycles

DURING SCHEDULED 18Y CHECK, FOUND SKIN CRACKED AT BS 400, BETWEEN STR 25R TO STR 26R. REPAIRED SKIN PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,067 hrs · 48,746 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 23R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,067 hrs · 48,746 cycles

DURING SCHEDULED 18Y CHECK, FOUND FRAME CRACKED AT BS 500B, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 58,067 hrs · 48,746 cycles

DURING SCHEDULED 18Y CHECK, FOUND FWD CARGO COMPARTMENT Z-ANGLE CRACKED BETWEEN BS 500A TO BS 500, STR 26R. REMOVED AND REPLACED Z-ANGLE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,067 hrs · 48,746 cycles

DURING SCHEDULED 18Y CHECK, FOUND FRAME CRACKED AT BS 500B, BETWEEN STR 20 TO STR 21R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,067 hrs · 48,746 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,067 hrs · 48,746 cycles

DURING SCHEDULED 18Y CHECK, FOUND AFT CARGO COMPARTMENT FRAME CORRODED AT BS 794, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (CABIN) · airframe 58,067 hrs · 48,746 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 27R TO STR 26R. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,067 hrs · 48,746 cycles

DURING SCHEDULED 18Y CHECK, FOUND AFT CARGO COMPARTMENT FRAME CORRODED AT BS 794, LOWER DOOR SILL WEB ATTACH ANGLE. REPAIRED FRAME PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,067 hrs · 48,746 cycles

DURING SCHEDULED 18Y CHECK, FOUND AFT CARGO COMPARTMENT FRAME CORRODED AT BS 794, STR 25R. REPAIRED FRAME PER SRM AND BAC DWG.

Part: FUSE — INOPERATIVE (BATTERY PACK) · airframe 58,067 hrs · 48,746 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT FWD EEPLS BATTERY PACK FUSE INOP. REMOVED AND REPLACED FUSE PER SWPM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,067 hrs · 48,746 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26L TO STR 25L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,067 hrs · 48,746 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED CLIP PER SI.

Part: SIGN — LOOSE (CABIN) · airframe 58,067 hrs · 48,746 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,067 hrs · 48,746 cycles

DURING SCHEDULED 18Y CHECK, FOUND L1 DOOR FUSELAGE CUTOUT, UPPER AFT CORNER SKIN CRACKED. REMOVED AND REPLACED SKIN PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,067 hrs · 48,746 cycles

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

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 58,067 hrs · 48,746 cycles

DURING SCHEDULED 18Y CHECK, FOUND FWD GALLEY DOORWAY CREASE BEAM CORRODED. REMOVED AND REPLACED BEAM PER BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,067 hrs · 48,746 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 28L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 58,067 hrs · 48,746 cycles

DURING SCHEDULED 18Y CHECK, FOUND AFT GALLEY DOORWAY CREASE BEAM CORRODED. REMOVED AND REPLACED BEAM PER BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,067 hrs · 48,746 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,067 hrs · 48,746 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,067 hrs · 48,746 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 1. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,067 hrs · 48,746 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,067 hrs · 48,746 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,067 hrs · 48,746 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 3L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,067 hrs · 48,746 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,067 hrs · 48,746 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 3R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,067 hrs · 48,746 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 8R. REMOVED AND REPLACED CLIP PER SI.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 58,067 hrs · 48,746 cycles

DURING SCHEDULED 18Y CHECK, FOUND FWD CARGO COMPARTMENT LOWER DOOR SILL WEB SUPPORT WEB CORRODED AT BS 492, BETWEEN STR 26R TO STR 25R. REPAIRED ANGLE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,067 hrs · 48,746 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 500C+12, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,686 hrs · 48,473 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 790, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,686 hrs · 48,473 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 825, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,682 hrs · 48,472 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 514D, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,682 hrs · 48,472 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 814, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,682 hrs · 48,472 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 727E + 4, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,682 hrs · 48,472 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 727C + 14, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,682 hrs · 48,472 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 770, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,682 hrs · 48,472 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 892, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,682 hrs · 48,472 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 730A, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,040 hrs · 48,005 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 810, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,040 hrs · 48,005 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 783, STR 10R. REPAIRED SKIN PER SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 57,040 hrs · 48,005 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT MAIN WHEEL WELL UPPER PRESSURE DECK WEB SURFACE CRACKED AT BS 706, RBL 59. REPAIRED WEB PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,040 hrs · 48,005 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 792, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,040 hrs · 48,005 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 739E, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,040 hrs · 48,005 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 822, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,040 hrs · 48,005 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 810, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,184 hrs · 47,326 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED BETWEEN BS 732D TO BS 733.5, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,184 hrs · 47,326 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED BETWEEN BS 452 TO BS 456, STR 10L. REPAIRED SKIN PER SRM.

Part: COVER — DISTORTED (EVAC SLIDE) · airframe 56,184 hrs · 47,326 cycles

DURING SCHEDULED CV CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE COVER DISTORTED. REMOVED AND REPLACED COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,184 hrs · 47,326 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED BETWEEN BS 771 TO BS 773, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,184 hrs · 47,326 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED BETWEEN BS 773 TO BS 775, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,184 hrs · 47,326 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED BETWEEN BS 503C TO BS 504.5, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,184 hrs · 47,326 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED BETWEEN BS 753 TO BS 754, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,184 hrs · 47,326 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED BETWEEN BS 831 TO BS 835, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,184 hrs · 47,326 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED BETWEEN BS 394 TO BS 397, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,184 hrs · 47,326 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED BETWEEN BS 763 TO BS 764, STR 10R. REPAIRED SKIN PER SRM.

Part: HOUSING — FAULTY (CABIN) · airframe 55,827 hrs · 47,049 cycles

AFT EMERGENCY EXIT LIGHTS FAULTY. REMOVED AND REPLACED BATTERY HOUSING PER MM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 55,416 hrs · 46,732 cycles

DURING SCHEDULED OTS CHECK, FOUND LT WING NR 4 SLAT I/B UPPER CORNER OF WEDGE SKIN DELAMINATED. REPAIRED SKIN PER EA.

Part: SUPPORT FITTING — CRACKED (R1 DOOR) · airframe 55,416 hrs · 46,732 cycles

DURING SCHEDULED OTS CHECK, FOUND R1 DOOR SKIN ON FRAME LOWER AFT STOP INNER SUPPORT FITTING CRACKED. REMOVED AND REPLACED R1 DOOR PER MM.

Part: SKIN — CRACKED (RT WING) · airframe 55,416 hrs · 46,732 cycles

DURING SCHEDULED OTS CHECK, FOUND RT WING SKIN CRACKED AT STA 238. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (LT WING) · airframe 55,413 hrs · 46,731 cycles

DURING SCHEDULED OTS CHECK, FOUND LT WING UPPER SKIN CRACKED AT STA RSS 238. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,416 hrs · 46,732 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787+16, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,416 hrs · 46,732 cycles

DURING SCHEDULED OTS, FOUND FUSELAGE SKIN CRACKED AT BS 493, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,416 hrs · 46,732 cycles

DURING SCHEDULED OTS, FOUND FUSELAGE SKIN CRACKED AT BS 727B+14, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 55,413 hrs · 46,731 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING I/B FORE FLAP SKIN DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,678 hrs · 46,207 cycles

DURING SCHEDULED SPV CHECK, FOUND LT AFT EMERGENCY EXIT LIGHT INOP AT BS 967. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 54,409 hrs · 46,015 cycles

AIR TURNBACK. PASSING FL 320 (32,000FT) CABIN ALT WARNING HORN SOUNDED AND NOTED CABIN PRESSURE PASSING 11,000FT. ALL PRESSURE SWITCHES WERE IN NORMAL POSITION WITH NO FAIL LIGHTS. CABIN MASKS DID NOT DEPLOY. PERFORMED EMERGENCY DESCENT, SWITCHED PRESS CONTROLLER TO STBY AND STOPPED CABIN ALT PRESSURIZATION CLIMB. AUTO FAIL LIGHT CAME ON SEVERAL MINUTES AFTER SWITCH WAS IN STBY. REMOVED AND REPLACED PRESSURE CONTROLLER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,902 hrs · 45,663 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 503C, STR 15R. REPAIRED SKIN PER EA.

Part: SIGN — LOOSE (CABIN) · airframe 53,410 hrs · 45,312 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT GALLEY OVERHEAD EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED SIGN PER MM.

Part: LENS — BROKEN (CABIN) · airframe 53,174 hrs · 45,140 cycles

AFT EMERGENCY EXIT SIGN COVER BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,064 hrs · 45,049 cycles

DURING SCHEDULED 16Y CHECK, FOUND EEPLS LIGHT INOP AT ROW 15. REMOVED AND REPLACED LAMP PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,064 hrs · 45,049 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO FRAME CORRODED AT BS 847, STR 27L TO STR 27R. REPAIRED FRAME PER AAR EA.

Part: FUSE — BLOWN (CABIN) · airframe 53,064 hrs · 45,049 cycles

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

Part: SKIN — CORRODED (FUSELAGE) · airframe 53,064 hrs · 45,049 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 440, STR 27R TO STR 28R. REPAIRED SKIN PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 53,064 hrs · 45,049 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,064 hrs · 45,049 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO LONGITUDINAL FLOORBEAM CORRODED AT BS 731D, LBL 3. REPAIRED BEAM PER SRM & EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,064 hrs · 45,049 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 827, STR 27L TO STR 27R. REPAIRED FRAME PER SRM & EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 53,064 hrs · 45,049 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING INBOARD AFT FLAP DELAMINATED AT OUTBOARD CORNER. REPAIRED FLAP PER EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 53,064 hrs · 45,049 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR FWD CUTOUT. REMOVED AND REPLACED FRAME ASSY PER SRM & ACO.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 53,064 hrs · 45,049 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 53,064 hrs · 45,049 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 867, STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,064 hrs · 45,049 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD CARGO DOOR LOWER AFT CUTOUT SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 53,064 hrs · 45,049 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CRACKED AT BS 493, STR 16R. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,064 hrs · 45,049 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR CUTOUT SKIN CRACKED AT BS 304, WL 260. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 53,064 hrs · 45,049 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING OUTBOARD AFT FLAP DELAMINATED AT T/E. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,064 hrs · 45,049 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,064 hrs · 45,049 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 27L TO STR 27R. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,064 hrs · 45,049 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM T-CAP CORRODED AT BS 986.5, BETWEEN LBL 16 TO LBL 19. REMOVED AND REPLACED BEAM PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 53,064 hrs · 45,049 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM CORRODED AT R1 DOORWAY, BETWEEN BS 294.5 TO BS 332.5. REMOVED AND REPLACED BEAM PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 53,064 hrs · 45,049 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 887 TO BS 867, STR 17L. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,064 hrs · 45,049 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,064 hrs · 45,049 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 53,064 hrs · 45,049 cycles

DURING SCHEDULED 16Y CHECK, FOUND BULKHEAD ANGLE BS 291.5 CRACKED AT BS 291.5, BETWEEN STR 10R TO STR 11R. REMOVED AND REPLACED ANGLE PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 53,064 hrs · 45,049 cycles

DURING SCHEDULED 16Y CHECK, FOUND BULKHEAD ANGLE BS 291.5 CRACKED AT BS 291.5, BETWEEN STR 11R TO STR 12R. REMOVED AND REPLACED ANGLE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 53,064 hrs · 45,049 cycles

DURING SCHEDULED 16Y CHECK, FOUND RIGHT I/B CREASE BEAM CORRODED FROM BS 954 TO BS 992, STR 17R. REMOVED AND REPLACED BEAM PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 53,064 hrs · 45,049 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 3 I/B WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 53,064 hrs · 45,049 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 960 TO BS 984, LBL 54. REMOVED AND REPLACED BEAM PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 52,519 hrs · 44,654 cycles

DURING HC2 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (AFT CARGO DOOR) · airframe 52,519 hrs · 44,654 cycles

DURING HC2 CHECK, FOUND AFT CARGO DOOR SKIN CRACKED AT HANDLE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 52,519 hrs · 44,654 cycles

DURING HC2 CHECK, FOUND NR 2 L/E SLAT WEDGE DELAMINATED. REPAIRED SLAT PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,347 hrs · 44,525 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 514B, STR 10L. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,347 hrs · 44,526 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 513C, STR 10L. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,347 hrs · 44,526 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 514, STR 10L. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,347 hrs · 44,525 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 731E, STR 4L. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,347 hrs · 44,525 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 812, STR 4L. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,347 hrs · 44,525 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BS 554, STR 4L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 52,347 hrs · 44,525 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,347 hrs · 44,525 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BS 505C, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,347 hrs · 44,525 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BS 772, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,347 hrs · 44,525 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BS 475, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,347 hrs · 44,525 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 790, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,347 hrs · 44,525 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BS 730C, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,347 hrs · 44,525 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 750, STR 4L. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,347 hrs · 44,525 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 416 TO BS 446, STR 1L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,347 hrs · 44,525 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BS 513A, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,347 hrs · 44,525 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 727, STR 4R. REPAIRED SKIN PER SWA EA.

Part: LIGHT — BROKEN (CABIN) · airframe 51,959 hrs · 44,249 cycles

FWD ENTRY EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,465 hrs · 43,885 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 494, STR 10R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,465 hrs · 43,885 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 4R. REPAIRED SKIN PER SWA EA.

Part: LENS — LOOSE (CABIN) · airframe 50,989 hrs · 43,544 cycles

FOUND LT EMERGENCY EXIT SIGN LENS LOOSE. SECURED LENS PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,965 hrs · 42,800 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,965 hrs · 42,800 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 294.5, STR 14R. REPAIRED SKIN PER SWA EA.

Part: LENS — MISSING (CABIN) · airframe 49,571 hrs · 42,512 cycles

DURING SCHEDULED MV2 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,492 hrs · 42,450 cycles

DURING SCHEDULED MV1 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LENS — BROKEN (CABIN) · airframe 49,396 hrs · 42,375 cycles

DURING SCHEDULED 14Y CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,396 hrs · 42,375 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 435, STR 1. REPAIRED SKIN PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,396 hrs · 42,375 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 28L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,396 hrs · 42,375 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 320, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,396 hrs · 42,375 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 383, STR 28R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,396 hrs · 42,375 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 514, STR 10R. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,396 hrs · 42,375 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 328, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,396 hrs · 42,375 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 336, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,396 hrs · 42,375 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,396 hrs · 42,375 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,396 hrs · 42,375 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,396 hrs · 42,375 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,396 hrs · 42,375 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,396 hrs · 42,375 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,396 hrs · 42,375 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,396 hrs · 42,375 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,396 hrs · 42,375 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,396 hrs · 42,375 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,396 hrs · 42,375 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,396 hrs · 42,375 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,396 hrs · 42,375 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,396 hrs · 42,375 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,396 hrs · 42,375 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,396 hrs · 42,375 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,396 hrs · 42,375 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,396 hrs · 42,375 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 49,157 hrs · 42,197 cycles

DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 49,157 hrs · 42,197 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,157 hrs · 42,197 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR CUTOUT FWD LOWER CORNER. REPAIRED SKIN PER SRM.

Part: ACTUATOR — WORN (SPOILER) · airframe 48,132 hrs · 41,437 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD GROUND SPOILER OUTBOARD ACTUATOR WORN. REMOVED AND REPLACED ACTUATOR PER MM.

Part: ATTACH FITTING — CRACKED (NR 5 SPOILER) · airframe 47,137 hrs · 40,668 cycles

DURING SCHEDULED C1 CHECK, FOUND RIGHT WING NR 5 GROUND SPOILER INBOARD ACTUATOR FWD ATTACH LUG CRACKED. REMOVED AND REPLACED NR 4 SPOILER PER MM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 46,296 hrs · 40,003 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR SKIN CRACKED AT AFT LOWER CORNER. REMOVED AND REPLACED AFT CARGO DOOR PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 46,274 hrs · 39,982 cycles

LEFT OVERWING EMERGENCY EXIT SIGN LENS MISSING. INSTALLED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,625 hrs · 37,909 cycles

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

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 42,147 hrs · 36,767 cycles

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

Part: FRAME — CRACKED (BS 303) · airframe 41,426 hrs · 36,185 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303.9, STR 16L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CORRODED (BS 727) · airframe 41,426 hrs · 36,185 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BLKHD OTBD LOWER CHORD CORRODED AT BS 727, RBL 4.375. REPAIRED CHORD PER SWA EA AND SRM.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 41,426 hrs · 36,185 cycles

DURING SCHEDULED 1/4D CHECK, FOUND NR 1 L/E SLAT LOWER T/E SKIN CRACKED. REPAIRED SLAT PER SRM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 41,417 hrs · 36,173 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RIGHT WING T/E OUTBOARD AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,671 hrs · 35,556 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA & SRM.

Part: LIGHT — LOOSE (R1 DOOR) · airframe 40,671 hrs · 35,556 cycles

R1 DOOR EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,196 hrs · 35,179 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D + 17, STR 12R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 39,429 hrs · 34,570 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — DISLODGED (R2 DOOR) · airframe 39,093 hrs · 34,312 cycles

R2 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED R2 DOOR EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,475 hrs · 33,828 cycles

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

Part: SKIN — CRACKED (NR 1 SLAT) · airframe 37,999 hrs · 33,447 cycles

DURING SCHEDULED C3 CHECK, FOUND LT WING NR 1 L/E SLAT SKIN CRACKED. REPAIRED L/E SLAT SKIN PER EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 37,999 hrs · 33,447 cycles

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

Part: FITTING — CRACKED (FUSELAGE) · airframe 37,017 hrs · 32,640 cycles

DURING SCHEDULED C2 CHECK, FOUND L1 DOOR LOWER HINGE BOX FITTING CRACKED. REMOVED AND REPLACED HINGE BOX FITTING PER SAM FORM.

Part: SKIN — DELAMINATED (RT WING FOREFLAP) · airframe 36,163 hrs · 31,951 cycles

DURING SCHEDULED C1 CHECK, FOUND RT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED RT INBOARD T/E FOREFLAP PER MM.

Part: COVER — LOOSE (RT EMER EXIT) · airframe 35,524 hrs · 31,443 cycles

RT OVERWING EMERGENCY EXIT LIGHT AT DOOR HAS LOOSE COVER. REINSTALLED EXIT LIGHT COVER PER MM.

Part: BALLAST — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,453 hrs · 31,386 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BALLAST PER MM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 33,829 hrs · 30,067 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT LENS BROKEN. REPAIRED LENS AND REINSTALLED PER MM.

Part: SHEAR TIE — CRACKED (RT WING) · airframe 33,530 hrs · 29,822 cycles

DURING SCHEDULED D CHECK, FOUND RT WING SHEAR TIE CRACKED AT STA 135.5 LOWER REAR SPAR. REPAIRED SHEAR TIE PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 33,434 hrs · 30,087 cycles

DURING SCHEDULED D-CHECK, FOUND UPPER CHORD CRACKED AT BS 178, WL 233, LBL 25. REMOVED AND REPLACED UPPER CHORD PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 33,434 hrs · 30,087 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 1040, BETWEEN STR 2R AND STR 3R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: ATTACH FITTING — CORRODED (FWD ENTRY) · airframe 33,530 hrs · 29,822 cycles

DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT ATTACH FITTING CORRODED. REPAIRED FITTING PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,530 hrs · 29,822 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 33,530 hrs · 29,822 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 13L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: WEB — CRACKED (NOSE) · airframe 33,053 hrs · 29,624 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKED AT WL 196, RBL 5, AND WL 199, LBL 5. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,415 hrs · 32,458 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT RADIUS OF EQUIPTMENT COOLING CUTOUT. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (AFT SVC DOOR) · airframe 31,519 hrs · 28,240 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SWITCH — INOPERATIVE (COCKPIT) · airframe 31,000 hrs · 27,808 cycles

IN FLIGHT, MASTER FIRE WARNING LIGHT ILLUMINATED AND BELL SOUNDED FOR NEARLY 5 MINUTES, WOULD NOT CANCEL. REMOVED AND REPLACED FIRST OFFICER FIRE WARNING BELL CUTOUT SW PER MM.

Part: SLIDE — OUT OF ADJUST (AFT ENTRY DOOR) · airframe 30,315 hrs · 27,263 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLAT — CRACKED (LT WING) · airframe 29,741 hrs · 26,802 cycles

DURING SCHEDULED C2 CHECK, FOUND NR 1 L/E SLAT CRACKED (2 EA), 12 INCHES OTBD OF OTBD ACTUATOR STOP. REPAIRED L/E SLAT PER SRM.

Part: SLIDE — OUT OF ADJUST (AFT SVC DOOR) · airframe 29,741 hrs · 26,802 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 28,734 hrs · 25,966 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT PLAY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 27,057 hrs · 24,555 cycles

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

Part: FLAP — DELAMINATED (AFT FLAP) · airframe 26,871 hrs · 24,396 cycles

DURING SCHEDULED C3 CHECK, FOUND LH OTBD AFT FLAP DELAMINATED ON UPPER & LWR INBD SURFACES. R&R LH OTBD AFT FLAP PER MM.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 26,473 hrs · 24,047 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 26,416 hrs · 24,007 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. R&R EMERGENCY EVAC SLIDE PER MM.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 26,429 hrs · 24,014 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EMERGENCY EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 25,886 hrs · 23,566 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE ASSY PER MM.

Part: ACTUATOR — BROKEN (RT WING) · airframe 25,607 hrs · 23,332 cycles

DURING SCHEDULED 1/4D CHECK, FOUND NR 5 GROUND SPOILER OUTBOARD ACTUATOR ATTACH LUG BROKEN. REMOVED AND REPLACED SPOILER ACTUATOR PER MM.

Part: HINGE — LOOSE (LT AILERON) · airframe 25,607 hrs · 23,332 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT AILERON OUTBOARD CENTER TAB HINGE SHAFT LOOSE IN SUPPORT HOUSING. REMOVED AND REPLACED HINGE ASSY PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,607 hrs · 23,332 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAM WEB CRACKED AT LBL 17.1, WL 229. REPAIRED VERTICAL BEAM WEB PER BFG ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 25,607 hrs · 23,332 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIES CORRODED BETWEEN STR 26R & STR 27R, BS 727C, RBL 10, BS 727D, RBL 8 & BS 747 RBL 12. REPAIRED SHEAR TIES PER SRM.

Part: FLAP — CRACKED (RT WING) · airframe 25,607 hrs · 23,332 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT WING T/E INBOARD AFT FLAP CRACKED AND DELAMINATED ON OUTBOARD END. REPAIRED AFT FLAP PER BAC DWG & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 24,923 hrs · 22,744 cycles

DURING SCHEDULED C1 CHECK, FOUND .1875 INCH EXTERNAL FUSELAGE SKIN CRACK AT AFT ENTRY DOOR LWR SKIN CUTOUT. REPAIRED SKIN PER RA 1-353-2399.

Part: LIGHT — LOOSE (CABIN FLOOR) · airframe 24,633 hrs · 22,499 cycles

EEPLS LOOSE AT OVERWING EXIT. SECURED TRACK PER MM.

Part: SENSOR — OUT OF ADJ (AFT CARGO DOOR) · airframe 24,339 hrs · 22,242 cycles

ABORTED TAKEOFF, AFT CARGO DOOR LIGHT ILLUMINATED DURING TAKEOFF ROLL. ADJUSTED AFT CARGO DOOR PROX SENSOR PER MM.

Part: BULB — FAILED (ROW 14)

DURING SCHEDULED SC CHECK, FOUND EMERGENCY TRACK LIGHTING INOP AT ROW 14, RELAMPED PER M/M.

Part: LIGHT — MISSING (CABIN)

DURING SCHEDULED 1/2 D-CHECK, FOUND REMOVED EGRESS LIGHTING FOM. INSTALLED EGRESS LIGHTING AND OPS CHECKS GOOD PER BOEING MM.

Part: WINDOW POST — CRACKED (COCKPIT)

DURING SCHEDULED 1/2D CHECK, FOUND HFEC REVELS CRACKED TOP OF F/O CORNER WINDOW POST. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 986.5-1006)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED INTERCOSTAL AT BS 986.5 TO 1006, LBL 12. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 967-986.5)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED INTERCOSTAL AT BS 967 TO 986.5, LBL 18. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 344)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM AT BS 344, LBL 9. REPAIRED PER BOEING NR TIA53014.

Part: INTERCOSTAL — CRACKED (BS 294.5)

DURING SCHEDULED 1/2D CHECK, FOUND INTERCOSTAL CRACKED AT BS 294.5, STR 12L. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 927-947)

DURING SCHEDULED 1/2D CHECK, FOUND UPPER WEB ANGLE CRACKED AT BS 927-947, BL 0. REPAIRED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 277)

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 277 STR 24R. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 986.5)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED INTERCOSTAL AT BS 986.5 TO 1006 LBL 12. REPAIRED PER BOEING SRM.

Part: STANCHION — CRACKED (E & E COMP)

DURING SCHEDULED 1/2D CHECK, FOUND FWD RIGHT STANCHION CRACKED E-1 RACK. REPAIRED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 947)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED RT Z-ANGLE AT BS 947 TO 996. REMOVED AND RPLACED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 967-986.5)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED INTERCOSTAL AT BS 967 TO 986.5 LBL 18. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 727)

DURING SCHEDULED 1/2 D-CHECK, FOUND RT TRANSITION ANGLE ABOVE STRINGER 25R CORRODED AROUND FASTENER HOLES BETWEEN BS 727 AND 727B AND BETWEEN BS 727B AND 767. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED 1/2 D-CHECK, FOUND LOWER FWD CORNER DOOR FRAME CRACKED. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 727)

DURING SCHEDULED 1/2 D-CHECK, FOUND AFT AT BS 727 PRESS BULKHEAD BL 0, LOWER COMP BEAM CRACKED. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 767 & 787)

DURING SCHEDULED 1/2 D-CHECK, FOUND RT TRANSITION ANGLE WEB BETWEEN BS 767 AND 787 HEAVILY CORRODED AND DETERIORATED. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 986.5)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED FLOORBEAM CLIP NUT HOLE FWD FLANGE AT BS 986.5, RBL 28, RBL 36, RBL35, RBL 30, RBL 40 AND RBL 43. REPAIRED PER BOEING SRM.

Part: PLATE — GOUGED (CARGO DOORWAY)

DURING SCHEDULED 1/2 D-CHECK, FOUND WEB PLATE AFT DOOR CUTOUT ABOVE STRINGER 24R GOUGED/WORN. REPAIRED PER BOEING SRM.

Part: SKIN — DAMAGED (BS 494)

DURING SCHEDULED 1/2D CHECK, FOUND PANEL AFT OF FWD CARGO DOOR CUTOUT DAMAGED AT BS 494, RBL 22. REPAIRED PER BOEING MM.

Part: ANGLE — CORRODED (BS 500)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED ANGLE AT BS 500D, RBL 20, LBL 20. REMOVED AND REPLACED PER BOEING MM.

Part: ANGLE — CORRODED (BS 727 & 787)

DURING SCHEDULED 1/2D CHECK, FOUND LT TRANSITION ANGLE ABOVE STRINGER 25L SURFACE CORRODED BETWEEN BS 727C AND 787. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 540)

DURING SCHEDULED 1/2D CHECK, FOUND INTERCOSTAL CRACKED AT BS 540 LBL 0. REPAIRED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 500)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED LT TRANSITION ANGLE FROM BS 500 TO BS 500D LBL 20. REMOVED AND REPLACED PER BOEING SRM.

Part: WIRE — LOOSE (LT HSI)

AIRCRAFT DIVERTED, CAPT HSI HEADING FLAG DISPLAY INTERMITTENTLY, HEADING IS BAD AND HEADING SLEW BUG IS ERRATIC, PLACING COMPASS SWITCH TO BOTH ON NR 2 DOES NOT FIX THE PROBLEM. AIRCRAFT MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED CAPT HSI PER BOEING MM AND TIGHTENED LOOSE WIRE ON TRANSFER SWITCH, OPS OK AT THIS TIME.

Part: BLADE — FAILED (NR 1 ENGINE)

DURING CLIMBOUT, NR 1 ENGINE FAILED AT FL 370, NR 1 ENGINE THREW A FAN BLADE. SHUTDOWN ENGINE AND A/C WAS DIVERTED. AIRCRAFT MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED NR 1 ENGINE ASSY PER SRM 385, OPS CHECK NORMAL. ENGINE AND EQUIPMENT SENT FROM PHX. WORK IN PROGRESS.

Part: FAN — FAILED (CABIN)

DURING WALKAROUND CHECK, FOUND BURNING SMELL IN CABIN AND E/E FAN C/B TRIPPED. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — GOUGED (PAX DOORWAY)

DURING SCHEDULED A2 CHECK, FOUND GOUGED SKIN BELOW AFT ENTRY DOOR. REPAIRED PER BOEING SRM.

Part: BATTERY CHARGER — INOPERATIVE (FWD GAL)

DURING WALKAROUND CHECK, FOUND FWD GALLEY EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY CHARGER PER BOEING M/M.