N691WN

Part: LENS — MISSING (CABIN) · airframe 81,308 hrs · 66,915 cycles

LEFT OVERWING EXIT LENS COVER MISSING. INSTALLED LENS ASSEMBLY IAW AMM.

Part: FLAP — DELAMINATED (RT WING) · airframe 81,308 hrs · 66,915 cycles

RIGHT WING OTBD AFT FLAP DELAMINATED ON INBD END. R & R AFT FLAP IAW MM.

Part: ENGINE — OVERHEATED (NR 1) · airframe 81,069 hrs · 66,732 cycles

DIVERSION ON TAKEOFF NR 1 ENG OVERHEATED 973 DEGREES FOR 8-10 SECONDS. R & R NR 1 ENG IAW MT.

Part: WIRE — BROKEN (CABIN) · airframe 80,543 hrs · 66,349 cycles

EMERGENCY EXIT LIGHT WIRE BROKEN CONNECTOR, BS 332 & LBL 7. R & R WIRE IAW SWPM & MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 80,543 hrs · 66,349 cycles

STUB FRAME CRACKED AT BS 960, WL 255. R & R STUB FRAME IAW SRM & DWG.

Part: PLATE — CRACKED (FUSELAGE) · airframe 80,543 hrs · 66,349 cycles

CLOSEOUT PLATE CRACKED AT BS 947, BETWEEN STRINGER 14L TO STRINGER 11L. R & R PLATE IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,543 hrs · 66,349 cycles

FUSELAGE SKIN CRACKED AT BS 950, STRINGER 11L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,543 hrs · 66,349 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 951 TO BS 953, STRINGER 4R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,543 hrs · 66,349 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 931 TO BS 932, STRINGER 4R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,543 hrs · 66,349 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 500+3.5- TO BS 500+4.5, STRINGER 16R. REPAIRED SKIN IAW SRM.

Part: LENS — BROKEN (CABIN) · airframe 80,038 hrs · 66,002 cycles

RT EMERGENCY EXIT LIGHT BROKEN. R & R LENS IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 79,968 hrs · 65,949 cycles

FWD ENTRY WALL MOUNTED EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS IAW MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 79,536 hrs · 65,663 cycles

STRINGER CRACKED AT BS 897 STRINGER 4R. R & R STRINGER IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 79,536 hrs · 65,663 cycles

FRAME CRACKED STATION 947, STRINGER 24R. REPAIRED FRAME IAW EA.

Part: GROUND WIRE — DAMAGED (CABIN) · airframe 79,536 hrs · 65,663 cycles

FWD ENTRY DOOR EMERGENCY EXIT LIGHT GND WIRE DAMAGED. R & R WIRE IAW AMM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 79,536 hrs · 65,663 cycles

FWD CARGO RT INTERCOSTAL ATTACH ANGLE CRACKED AT STATION 400, RBL24. R & R ANGLE IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 79,536 hrs · 65,663 cycles

FRAME CRACKED AT STATION 380, STRINGER 16R. REPAIRED FRAME IAW SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,536 hrs · 65,663 cycles

STRINGER CLIP CRACKED AT STATION 947, STRINGER 25R. R & R CLIP IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 79,536 hrs · 65,663 cycles

AFT CARGO PIT FRAME CUTOUT CORNER CRACKED AT STATION 787, STRINGER 20R. REPAIRED WEB IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,536 hrs · 65,663 cycles

STRINGER CLIP CRACKED AT STATION 787, STRINGER 22R. R & R CLIP IAW DRAWING & SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 79,536 hrs · 65,663 cycles

SKIN CORRODED BETWEEN STATION 500C TO STATION 500D, STRINGER 28L. REPAIRED SKIN IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,536 hrs · 65,663 cycles

STRINGER CLIP CRACKED AT BS 380, STRINGER 21L. R & R CLIP IAW SRM & DRAWING.

Part: WEB — CORRODED (FUSELAGE) · airframe 79,536 hrs · 65,663 cycles

VERTICAL WEB CORRODED AT STATION 500B, BETWEEN STRINGER 28R & STRINGER 27R. R & R WEB IAW SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 79,536 hrs · 65,663 cycles

STRINGER SPLICE CHANNEL CRACKED AT BS 907 STRINGER 4R. REPAIRED CHANNEL IAW EA.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 79,536 hrs · 65,663 cycles

ATTACH ANGLE CRACKED AT STATION 380, STRINGER 21L. R & R ANGLE IAW DRAWING.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,536 hrs · 65,663 cycles

STRINGER CLIP CRACKED AT STATION 380, STRINGER 26R. R & R CLIP IAW DRAWING & SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 79,536 hrs · 65,663 cycles

STRINGER SPLICE CHANNEL CRACKED AT STATION 360, STRINGER 4L. REPAIRED SPLICE IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,536 hrs · 65,663 cycles

STRINGER CLIP CRACKED AT STATION 380, STRINGER 22L. R & R CLIP IAW SRM & DRAWING.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,536 hrs · 65,663 cycles

STRINGER CLIP CRACKED AT STATION 500A, STRINGER 23R. R & R CLIP IAW DRAWING.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,536 hrs · 65,663 cycles

STRINGER CLIP CRACKED AT BS 500C, STRINGER 27L. R & R CLIP IAW SRM & DRAWING.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 79,536 hrs · 65,663 cycles

SHEAR TIE CORRODED AT STATION 500C, BETWEEN STRINGER 27R TO STRINGER 28R. R & R SHEAR TIE IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,536 hrs · 65,663 cycles

STRINGER CLIP CRACKED AT STATION 500B, STRINGER 27L. R & R CLIP IAW SRM & DRAWING.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,536 hrs · 65,663 cycles

STRINGER CLIP CRACKED AT STATION 500A, STRINGER 22R. R &R CLIP IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 79,536 hrs · 65,663 cycles

LOWER SHEAR TIE LOWER ANGLE CRACKED AT BS 520, STRINGER 22L. REPAIRED FRAME IAW EA.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 79,536 hrs · 65,663 cycles

L CHORD CORRODED AT STATION 227.8, BETWEEN RBL 8 TO LBL 8. REPAIRED CHORD IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,536 hrs · 65,663 cycles

SKIN CRACKED BETWEEN STATION 812 TO STATION 816, STRINGER 19L. REPAIRED SKIN IAW SRM.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 79,536 hrs · 65,663 cycles

RT WING FUEL ACCESS PANEL 7412 CORRODED ON UPPER SURFACE AROUND DOME NUTS. REPAIRED PANEL IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 79,536 hrs · 65,663 cycles

PRESSURE BULKHEAD VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17.1. R & R WEB IAW EA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 79,536 hrs · 65,663 cycles

AFT PRESSURE BULKHEAD FWD SIDE Z STIFFENER AT 12:30 POSITION, FWD FLANGE ON STIFFENER, CRACKED IN FLANGE AT OUTER FLANGE TO DOME PAN ATTACH FASTENER. REPAIRED Z STIFFENER IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,536 hrs · 65,663 cycles

SKIN CRACKED BETWEEN STATION 500D + 15.5 TO STATION 540, BETWEEN STRINGER 27R TO STRINGER 27L. REPAIRED SKIN IAW EA.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 79,536 hrs · 65,663 cycles

OVERHEAD A/C BRACKET CRACKED AT STATION 887, STRINGER 1. R & R BRACKET IAW SRM & DRAWING.

Part: SKIN — CRACKED (LT AILERON TAB) · airframe 79,536 hrs · 65,663 cycles

LT AILERON TAB NOSE CAP SKIN CRACKED AT SECOND FROM OTBD HINGE CUTOUT. R & R TAB IAW MM.

Part: PAD — CORRODED (FLAP TRACK) · airframe 79,536 hrs · 65,663 cycles

RT WING NR 8 FLAP TRACK UPPER SURFACE AFT MOUNT PAD CORRODED. REPAIRED PAD IAW EA.

Part: FLAP TRACK — CORRODED (LT WING) · airframe 79,536 hrs · 65,663 cycles

LT WING NR 1 FLAP TRACK UPPER SURFACE CORRODED AT AFT MOUNT PAD. REPAIRED PAD IAW EA.

Part: SUPPORT FITTING — CRACKED (FLAP FAIRING) · airframe 79,536 hrs · 65,663 cycles

LT WING NR 3 FLAP FAIRING SUPPORT CLIP CRACKED. R & R CLIP IAW DRAWING.

Part: SUPPORT ANGLE — CRACKED (TE FLAP) · airframe 79,536 hrs · 65,663 cycles

LT WING NR 3 FLAP FAIRING AFT SUPPORT ANGLE CRACKED ON INBD SIDE. R & R ANGLE IAW SRM & DRAWING.

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 79,536 hrs · 65,663 cycles

LT WING NR 1 BOOST PUMP ACCESS PANEL 7203 CRACKED FASTENER INSERT. R & R PANEL IAW AMM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 79,536 hrs · 65,663 cycles

STRINGER CLIP CORRODED AT STATION BS 827, STRINGER 26L. R & R CLIP IAW SRM & DRAWING.

Part: SKIN — DELAMINATED (EMERGENCY EXIT) · airframe 79,536 hrs · 65,663 cycles

LT EMERGENCY EXIT DOOR HATCH LT EXTERNAL OUTER SKIN AT TOP AFT CORNER DELAMINATED. R & R SKIN IAW MM & DRAWING.

Part: HOLDER — CRACKED (GIRT BAR) · airframe 79,536 hrs · 65,663 cycles

R1 DOOR EVAC GIRT BAR FWD HOLDER CRACKED. R & R HOLDER IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 79,536 hrs · 65,663 cycles

AFT CARGO COMPARTMENT RT UPPER INTERCOSTAL FLANGE CORRODED AT STATION 767, BETWEEN STRINGER 25R & STRINGER 26R. R & R INTERCOSTAL IAW SRM & DRAWING.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,536 hrs · 65,663 cycles

STRINGER CLIP CRACKED AT STATION 947.5, STRINGER 26L. R & R CLIP IAW EA.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 79,536 hrs · 65,663 cycles

AFT CARGO COMPARTMENT STRINGER ANGLE BRACKET CRACKED AT STATION 947.5, BETWEEN STRINGER 25L TO STRINGER 24L. R & R BRACKET IAW SRM & DRAWING.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 79,536 hrs · 65,663 cycles

FWD CARGO AT MAIN DISTRIBUTION BAY FWD CENTER WING BOX HORIZONTAL U CHANNEL CRACKED AT STATION 540, RBL14.75. REPAIRED U CHANNEL IAW SWA EA.

Part: SLAT — DELAMINATED (LT WING) · airframe 79,536 hrs · 65,663 cycles

LT WING NR 2 SLAT TOP INBD CORNER DELAMINATED. REPAIRED SLAT IAW SRM.

Part: GUSSET — CRACKED (RT WING) · airframe 79,536 hrs · 65,663 cycles

RT WING TE REAR SPAR STATION 501, RIB BETWEEN OTBD FLAP & AILERON GUSSET CRACKED. R & R GUSSET IAW SRM & DRAWING.

Part: SKIN — CHAFED (TE FLAP) · airframe 79,536 hrs · 65,663 cycles

RT WING INBD FORE FLAP UPPER SURFACE CHAFED AT PREVIOUS REPAIR. R & R REPAIR IAW SRM.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 79,536 hrs · 65,663 cycles

RT WW UPPER PRESSURE DECK CRACKED AT STATION 663, RBL 38. REPAIRED DECK IAW SRM.

Part: WEB — DAMAGED (RT WING) · airframe 79,536 hrs · 65,663 cycles

RT WING TE CLOSE-OUT WEB AT OTBD END OF OTBD FLAP DAMAGED. REPAIRED WEB IAW SWA EA.

Part: COVER — MISSING (CABIN) · airframe 79,469 hrs · 65,608 cycles

LT OVERWING EMERGENCY EXIT AISLE LIGHT COVER MISSING AT ROW 2. INSTALLED COVER IAW AMM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,877 hrs · 65,144 cycles

STRINGER CLIP DAMAGED AT BS 480, STRINGER 16R. R&R CLIP IAW SWA EA.

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 78,877 hrs · 65,144 cycles

BAFFLE CRACKED BETWEEN BS 440 TO BS 460, STRINGER 26L. R&R BAFFLE IAW SRM & DRAWING.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 78,877 hrs · 65,144 cycles

SHEAR TIE CRACKED AT BS 500B, BETWEEN STRINGER 15L & STRINGER 16L. REPAIRED SHEAR TIE IAW SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 78,877 hrs · 65,144 cycles

STRINGER SPLICE CRACKED AT BS 908, STRINGER 4L. R&R CLIP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,877 hrs · 65,144 cycles

SKIN CRACKED AT BS 500+17, STRINGER 23R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,877 hrs · 65,144 cycles

FS SKIN CRACKED AT BS 424 TO BS 427, STRINGER 26L. REPAIRED SKIN IAW SWA EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 78,877 hrs · 65,144 cycles

LT CREASE BEAM WEB CORRODED BETWEEN BS 787-BS 807, WL 208. R&R WEB IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,877 hrs · 65,144 cycles

SKIN CRACKED BETWEEN BS 507-BS 508.6, STRINGER 26L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,877 hrs · 65,144 cycles

SKIN CRACKED BETWEEN BS 475.5-BS 476.5, STRINGER 26L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,877 hrs · 65,144 cycles

SKIN CRACKED AT BS 906, BETWEEN STRINGER 2R-STRINGER 3R. REPAIRED SKIN IAW EA & ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,877 hrs · 65,144 cycles

FS SKIN CRACKED AT BS 355, STRINGER 23R. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,877 hrs · 65,144 cycles

FS SKIN CRACKED AT BS 906, BETWEEN STRINGER 3L & 4L. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,877 hrs · 65,144 cycles

SKIN CRACKED AT BS 485, STRINGER 16R. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,877 hrs · 65,144 cycles

SKIN CRACKED AT BS 942, STRINGER 4R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,877 hrs · 65,144 cycles

CHEM MILL SKIN CRACKED BETWEEN BS 360 TO BS 540, BETWEEN STRINGER 14L TO STRINGER 19L. REPAIRED SKIN IAW EA & ER.

Part: SKIN — CRACKED (LE SLAT) · airframe 78,877 hrs · 65,144 cycles

PREVIOUS REPAIR CRACKED AT NR 3 LE SLAT ACTUATOR CUTOUT. REPAIRED SKIN IAW SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 78,221 hrs · 64,664 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER TASK CARD.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 77,959 hrs · 64,474 cycles

MAIN E/E FLOORBEAM LOWER SUPPORT CRACKED AT BS 328, RBL 36. REPAIRED SUPPORT PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,959 hrs · 64,474 cycles

SKIN CRACKED AT BS 586, STR 10R. REPAIRED SKIN PER EA.

Part: LOCK PIN — INOPERATIVE (EVAC SLIDE) · airframe 77,875 hrs · 64,422 cycles

L2 DOOR SLIDE LOCK PIN INOP. RE-INSTALLED SLIDE LOCK PIN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,808 hrs · 64,375 cycles

FUSELAGE SKIN CRACKED AT STA 500A + 6, STR 16 RIGHT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 77,808 hrs · 64,375 cycles

LEFT WING 3 SLAT FIXED LEADING EDGE HAS 10.6" CRACK 1" OUTBOARD OF SLAT ACTUATOR MOD. REPAIRED SKIN IAW EA.

Part: WINDOW — ARCED (COCKPIT) · airframe 77,793 hrs · 64,364 cycles

CAPT'S NR 2 WINDOW HAD ARCING IN THE LOWER LEFT CORNER. REMOVED AND REPLACED NR 2 WINDOW PER M/M.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,436 hrs · 64,117 cycles

SUBSURFACE SKIN CRACKED AT STA 760 BELOW STA 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,436 hrs · 64,117 cycles

SUB SURFACE SKIN CRACKED AT STA 862 ABOVE STA 17R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,436 hrs · 64,117 cycles

SUB SURFACE SKIN CRACKED AT STA 760 BELOW STA 19R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 76,331 hrs · 63,327 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,234 hrs · 63,249 cycles

R2 DOOR EMERGENCY EXIT LIGHT ASSEMBLY BULBS INOP. REMOVED AND REPLACED BULBS PER AMM.

Part: SKIN — CRACKED (L1 DOOR) · airframe 76,116 hrs · 63,159 cycles

L1 DOOR FUSELAGE SKIN CRACKED AT UPPER HINGE CUTOUT AT AFT UPPER CORNER. REMOVED AND REPLACED DOOR IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,116 hrs · 63,159 cycles

FUSELAGE SKIN CRACKED AT BS 931.5, STR 21R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,116 hrs · 63,159 cycles

SKIN CRACKED AT BS 500B - 5, STR 16L. REPAIRED SKIN PER EA.

Part: LIGHT — LOOSE (CABIN) · airframe 75,401 hrs · 62,604 cycles

OVERWING CEILING EMERGENCY EXIT LIGHT ASSY LOOSE. SECURED LIGHT ASSY PER M/M.

Part: SPOILER — DELAMINATED (LT WING) · airframe 75,168 hrs · 62,435 cycles

LEFT WING I/B GROUND SPOILER DELAMINATED AT TRAILING EDGE. REMOVED AND REPLACED SPOILER IAW MM.

Part: SUPPORT FITTING — CRACKED (NR 5 SPOILER) · airframe 75,130 hrs · 62,407 cycles

LEFT WING NR 5 GROUND SPOILER I/B ACTUATOR ATTACH POINT UPPER BOLT CRACKED. REMOVED AND REPLACED GROUND SPOILER SUPPORT FITTING PER SRM.

Part: HOUSING — BROKEN (CABIN) · airframe 75,016 hrs · 62,325 cycles

L1 DOOR EMERGENCY EXIT LIGHT HOUSING BROKEN. REMOVED AND REPLACED LIGHT ASSY IAW MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 74,767 hrs · 62,139 cycles

BULLNOSE EMERGENCY EXIT LIGHT INOPERATIVE AT 5 DEF. RELAMPED LIGHT PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 74,570 hrs · 61,991 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT OF CONTAINER, DID NOT DEPLOY, STILL OPERATIONAL. RE-INSTALLED SLIDE IAW MM.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 74,511 hrs · 61,944 cycles

DURING SCHEDULED 14Y CHECK, FOUND BEAR STRAP CORRODED AT BS 494, STR 27R. REPAIRED STRAP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,511 hrs · 61,944 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED BETWEEN BS 444.5 TO BS 445.5, STR 26L. REPAIRED SKIN PER ER.

Part: WEB — DAMAGED (RT WING) · airframe 74,511 hrs · 61,944 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT MLG SUPPORT BEAM VERTICAL WEB DAMAGED. REPAIRED WEB PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,511 hrs · 61,944 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER ER.

Part: KEELBEAM — PUNCTURED (FUSELAGE) · airframe 74,511 hrs · 61,944 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT KEEL BEAM PUNCTURED BETWEEN BS 684 TO BS 727+14. REPAIRED BEAM IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,511 hrs · 61,944 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT FWD LT CORNER. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,511 hrs · 61,944 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 488.5, STR 25R. REPAIRED SKIN IAW ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,511 hrs · 61,944 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 663, STR 1. REPAIRED FRAME IAW EA.

Part: BEAM — CRACKED (FUSELAGE) · airframe 74,511 hrs · 61,944 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL BEAM UPPER CHORD CRACKED AT BS 727A+17, LBL 24.8. REPAIRED CHORD IAW ER AND EA.

Part: BEAM — CORRODED (LT MLG) · airframe 74,511 hrs · 61,944 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT MLG ACTUATOR WALKING BEAM CORRODED. REMOVED AND REPLACED BEAM PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,511 hrs · 61,944 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 663, STR 3R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,511 hrs · 61,944 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 663, STR 3L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,511 hrs · 61,944 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED BETWEEN BS 464.5 TO BS 466, STR 16L. REPAIRED SKIN IAW SM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,511 hrs · 61,944 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 663, STR 2L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,511 hrs · 61,944 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED BETWEEN BS 679 TO BS 681, STR 10R. REPAIRED SKIN IAW SM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 74,511 hrs · 61,944 cycles

DURING SCHEDULED 24Y CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178 BETWEEN RBL 21 TO RBL 22.25. REPAIRED WEB IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,511 hrs · 61,944 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 663, STR 2R. REPAIRED FRAME PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 74,511 hrs · 61,944 cycles

DURING SCHEDULED 24Y CHECK, FOUND WEB CRACKED AT BS 295, STR 15L. REPAIRED WEB IAW ER AND EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 74,511 hrs · 61,944 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED BETWEEN BS 708 TO BS 712, RBL 24.8. REPAIRED WEB IAW ER.

Part: BEAM — CORRODED (RT MLG) · airframe 74,511 hrs · 61,944 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT MLG ACTUATOR WALKING BEAM CORRODED. REMOVED AND REPLACED BEAM PER MM.

Part: SKIN — CHAFED (FUSELAGE) · airframe 74,511 hrs · 61,944 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT SKIN CHAFED BETWEEN BS 1006 TO BS 1007. REPAIRED SKIN IAW SRM.

Part: LENS — DIRTY (EXTERIOR) · airframe 74,511 hrs · 61,944 cycles

DURING SCHEDULED 24Y CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT LENS DIRTY. CLEANED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,511 hrs · 61,944 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED BETWEEN BS 444 TO BS 445.5, STR 16L. REPAIRED SKIN IAW SM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,511 hrs · 61,944 cycles

DURING SCHEDULED 24Y CHECK FOUND, SHEAR TIE CORRODED AT BS 500B, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 74,511 hrs · 61,944 cycles

DURING SCHEDULED 24Y CHECK FOUND, STRINGER SPLICE CORRODED AT BS 537, STR 27R. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,511 hrs · 61,944 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, BETWEEN STR 28L TO STR 28R. REPAIRED SHEAR TIE IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 74,511 hrs · 61,944 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED BETWEEN BS 666 TO BS 674, LBL 24.8. REPAIRED BEAM IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,511 hrs · 61,944 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 74,511 hrs · 61,194 cycles

DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 500 TO BS 500A, STR 17L. REMOVED AND REPLACED WEB PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 74,511 hrs · 61,944 cycles

DURING SCHDULED 24Y CHECK, FOUND RT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED IAW MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,511 hrs · 61,944 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8R. R&R CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 74,511 hrs · 61,944 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP DAMAGED AT BS 500C, STR 15R. R&R CLIP IAW SRM AND DWG.

Part: LENS — LOOSE (CABIN) · airframe 74,511 hrs · 61,944 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS LOOSE AT ROW 5. SECURED LENS IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 74,511 hrs · 61,944 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS LOOSE AT ROW 9. SECURED LENS IAW MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 74,511 hrs · 61,944 cycles

DURING SCHEDULED 24Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT AND MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 74,511 hrs · 61,944 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT HORIZONTAL STABILIZER LOWER INSPAR SKIN CRACKED AT STA 126. REPAIRED SKIN IAW SWA EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 74,511 hrs · 61,944 cycles

DURING SCHEDULED 24Y CHECK, FOUND BULKHEAD WEB AT "Y" CHORD CRACKED AT AFT FASTENER BUCKTAILS, STR 6L. REPAIRED PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 74,511 hrs · 61,944 cycles

DURING SCHEDULED 24Y CHECK, FOUND VERTICAL BEAM CRACKED BS 178, RBL 17.0, WL 230-233 AT AFT CHORD. REPAIRED PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 74,511 hrs · 61,944 cycles

DURING SCHEDULED 24Y CHECK, FOUND O/B CREASE BEAM CORROSION BS 889 TO 892 AND 896 TO 899, STR 17L, WL 208. REPAIRED PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,202 hrs · 60,927 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EXTERNAL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,606 hrs · 60,491 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 624, STR 1. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,606 hrs · 60,491 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 941.5 TO BS 943, STR 21R. REPAIRED SKIN PER ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,609 hrs · 60,492 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 780 TO 781, STR 19R. REPAIRED SKIN PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 72,606 hrs · 60,491 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR ACTUATOR AFT SUPPORT WEB CORRODED AT BS 821, WL 200. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,609 hrs · 60,492 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 624, STR 1. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,606 hrs · 60,491 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 727E+11, STR 18R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,609 hrs · 60,492 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 727E+11, STR 18R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,609 hrs · 60,492 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 727D+7 TO 727D+8, STR 20R. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,609 hrs · 60,492 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 639, WL 203.5. REMOVED AND REPLACED FRAME PER SRM AND BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,606 hrs · 60,491 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 624, STR 1. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,606 hrs · 60,491 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 727E+11, STR 18R. REPAIRED SKIN PER SRM.

Part: TAB — DELAMINATED (AILERON) · airframe 72,606 hrs · 60,491 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING AILERON TAB DELAMINATED. REMOVED AND REPLACED TAB PER MM.

Part: GASPER FAN — FAULTY (CARGO BAY) · airframe 72,542 hrs · 60,439 cycles

DIVERSION/DECLARED EMERGENCY. FLIGHT ATTENDANTS AND PASSENGERS REPORTED A BURNING ELECTRICAL SMELL IN THE MID CABIN AREA. REMOVED AND REPLACED GASPER FAN PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 72,361 hrs · 60,307 cycles

L1 DOOR EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,762 hrs · 59,870 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 801, STR 17L. REPAIRED SKIN PER EA.

Part: SIGN — BROKEN (CABIN) · airframe 71,353 hrs · 59,560 cycles

LT EMERGENCY EXIT SIGN BROKEN AT ROW 11. REMOVED AND REPLACED SIGN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,837 hrs · 59,142 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 911, STR 23L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,837 hrs · 59,142 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 951, STR 23L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,837 hrs · 59,142 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 465, STR 16R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,837 hrs · 59,142 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 731D, STR 19R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,842 hrs · 59,143 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 465, STR 16R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,842 hrs · 59,143 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 908 TO BS 1016, BETWEEN STR 20L TO STR 25L. REPAIRED SKIN PER EA.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 70,842 hrs · 59,143 cycles

DURING SCHEDULED OTS CHECK, FOUND BULKHEAD LOWER ANGLE SUPPORT CLIP CRACKED AT BS 947, STR 22L. REMOVED AND REPLACED CLIP PER BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,837 hrs · 59,142 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 908 TO BS 1016, STR 20L. REPAIRED SKIN PER EA.

Part: ACTUATOR — FAULTY (NLG) · airframe 70,701 hrs · 59,025 cycles

ABORTED TAKEOFF, DUE TO AIRCRAFT STEERING HARD RIGHT. NOT ABLE TO BRING BACK TO THE LEFT. REMOVED AND REPLACED ROTARY NOSE STEERING ACTUATOR PER MM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 70,617 hrs · 58,960 cycles

DURING SCHEDULED OTS CHECK, FOUND STRINGER CHANNEL CORRODED AT BS 369, STR 26L. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,617 hrs · 58,960 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 371, STR 26L. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,617 hrs · 58,960 cycles

DURING SCHEDULED OTS CHECK, FOUND FRAME CRACKED AT BS 380, STR 26L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,617 hrs · 58,960 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 371, STR 26L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,650 hrs · 58,985 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 471, STR 26L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 70,232 hrs · 58,673 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: WEB — CRACKED (NLG WW) · airframe 69,365 hrs · 58,023 cycles

DURING SCHEDULED MV2 CHECK, FOUND NOSE WHEEL WELL RT WEB CRACKED AT BS 259, WL 174. REPAIRED WEB PER EA.

Part: FRAME — CRACKED (BS 344 S22L) · airframe 68,807 hrs · 57,588 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 344, STR 22L. REPAIRED FRAME PER AEO.

Part: SKIN — CRACKED (BS 395 S16L) · airframe 68,807 hrs · 57,588 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 395, STR 16L. REPAIRED SKIN PER AEM.

Part: BULB — MISSING (EMERGENCY LIGHT) · airframe 68,807 hrs · 57,588 cycles

DURING SCHEDULED 22Y CHECK, FOUND OVERHEAD R1 DOOR EMERGENCY EXIT LIGHT BULB MISSING. INSTALLED BULB PER MM.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 68,807 hrs · 57,588 cycles

DURING SCHEDULED 22Y CHECK, FOUND LENS CRACKED RT AFT GALLEY LOWER SIDE. REMOVED AND REPLACED LENS ASSY PER MM.

Part: FITTING — CORRODED (R1 DOOR GIRT BAR) · airframe 68,807 hrs · 57,588 cycles

DURING SCHEDULED 22Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE BASE OF GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM.

Part: FRAME — CRACKED (BS 500B S20-21L) · airframe 68,807 hrs · 57,588 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 500B, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: LIGHT — CRACKED (CABIN) · airframe 68,807 hrs · 57,588 cycles

DURING SCHEDULED 22Y CHECK, FOUND EMERGENCY LIGHT CRACKED AT R2 DOOR. REMOVED AND REPLACED EMERGENCY LIGHT PER MM.

Part: LIGHT — CRACKED (CABIN) · airframe 68,807 hrs · 57,588 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT EMERGENCY LIGHT CRACKED. REMOVED AND REPLACED EMERGENCY LIGHT PER MM.

Part: FRAME — CRACKED (BS 500B 20-21L) · airframe 68,807 hrs · 57,588 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 500B, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: BULB — MISSING (EMERGENCY LIGHT) · airframe 68,807 hrs · 57,588 cycles

DURING SCHEDULED 22Y CHECK, FOUND R1 DOOR LOWER EMERGENCY EXIT LIGHT BULB MISSING. INSTALLED BULB PER MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,807 hrs · 57,588 cycles

DURING SCHEDULED 22Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 947.5 TO BS 990. REPAIRED BEAM PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,807 hrs · 57,588 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 294 BETWEEN STR 5L TO STR 6L. REPAIRED FRAME PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 68,807 hrs · 57,588 cycles

DURING SCHEDULED 22Y CHECK, FOUND PRESSURE BULKHEAD WEB CRACKED AT BS 178, BETWEEN RBL 5.7 TO RBL 17. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,807 hrs · 57,588 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 457, STR 16L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,807 hrs · 57,588 cycles

DURING SCHEDULED 22Y CHECK, FOUND EMERGENCY EXIT LIGHT BULB INOP AT UPPER AFT GALLEY AREA. REMOVED AND REPLACED BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,807 hrs · 57,588 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: COVER — CRACKED (CABIN) · airframe 68,807 hrs · 57,588 cycles

DURING SCHEDULED 22Y CHECK, FOUND EMERGENCY EXIT LIGHT COVER CRACKED AT UPPER AFT GALLEY. REPAIRED COVER PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,807 hrs · 57,588 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 270, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,807 hrs · 57,588 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED BETWEEN BS 348 TO BS 360, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,807 hrs · 57,588 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 13R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 68,807 hrs · 57,588 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CRACKED AT BS 708, BBL 0.07. REPAIRED BEAM PER SI.

Part: WEB — CRACKED (FUSELAGE) · airframe 68,807 hrs · 57,588 cycles

DURING SCHEDULED 22Y CHECK, FOUND WEB CRACKED BETWEEN BS 270 TO BS 291, STR 14R. REMOVED AND REPLACED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,876 hrs · 65,144 cycles

FS SKIN CRACKED AT BS 395, STRINGER 16L. REPAIRED SKIN IAW EO.

Part: LENS — BROKEN (CABIN) · airframe 68,755 hrs · 57,546 cycles

DURING SCHEDULED CV CHECK, FOUND FWD ENTRY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,755 hrs · 57,546 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 701, STR 10R. REPAIRED SKIN PER SRM.

Part: LENS — MISSING (CABIN) · airframe 68,646 hrs · 57,469 cycles

LEFT EEPLS LENS MISSING AT ROW 21. INSTALLED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,497 hrs · 57,341 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 16. RELAMPED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,141 hrs · 57,067 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 473, STR 16L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,901 hrs · 56,888 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE BEAR STRAP SKIN CRACKED AT UPPER HINGE CUTOUT, BS 291, WL 256. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,901 hrs · 56,888 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,901 hrs · 56,888 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR CUTOUT BETWEEN BS 291 TO BS 304, BETWEEN WL 233 TO WL 261. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,901 hrs · 56,888 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,901 hrs · 56,888 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 67,901 hrs · 56,888 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING O/B FORE FLAP I/B TRAILING EDGE DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,901 hrs · 56,888 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,901 hrs · 56,888 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 67,901 hrs · 56,888 cycles

DURING SCHEDULED 6Y CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,901 hrs · 56,888 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 692, STR 10R. REPAIRED SKIN PER SWA EA.

Part: LENS — LOOSE (CABIN) · airframe 67,360 hrs · 56,481 cycles

OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,066 hrs · 56,271 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 911, STR 20L. REPAIRED SKIN PER SRM.

Part: SLAT — CRACKED (LT WING) · airframe 66,523 hrs · 55,878 cycles

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

Part: GIRT BAR — LOOSE (L1 DOOR) · airframe 66,523 hrs · 55,878 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR LOOSE. SECURED GIRT BAR PER MM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 64,985 hrs · 54,805 cycles

AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,831 hrs · 54,691 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,831 hrs · 54,691 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 400, STR 26L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,831 hrs · 54,691 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 797, STR 26L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,831 hrs · 54,691 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 920 AND BS 943, STR 21L AND STR 23L. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,507 hrs · 54,457 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,455 hrs · 53,696 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 512D, STR 26R. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 63,089 hrs · 53,432 cycles

DURING SCHEDULED MV2 CHECK, FOUND RIGHT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,031 hrs · 53,386 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 20R. REPAIRED FRAME PER SRM.

Part: BOLT — CORRODED (LT MLG) · airframe 63,031 hrs · 53,386 cycles

DURING SCHEDULED BRDG CHECK, FOUND LT MLG BOTTLE BOLT CORRODED. REMOVED AND REPLACED BOTTLE BOLT PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 63,031 hrs · 53,386 cycles

DURING SCHEDULED BRDG CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER AND DIODES PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,031 hrs · 53,386 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 20L. REPAIRED FRAME PER SRM.

Part: BOLT — CORRODED (RT MLG) · airframe 63,031 hrs · 53,386 cycles

DURING SCHEDULED BRDG CHECK, FOUND RT MLG BOTTLE BOLT CORRODED. REMOVED AND REPLACED BOTTLE BOLT PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 63,030 hrs · 53,385 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 967, STR 7L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: RIB — CRACKED (RT WING) · airframe 63,030 hrs · 53,385 cycles

DURING SCHEDULED BRDG CHECK, FOUND RT WING LOWER RIB CHORD CRACKED AT STA 135.5, STR 2. REPAIRED CHORD PER ACO.

Part: RIB — CRACKED (LT WING) · airframe 63,030 hrs · 53,385 cycles

DURING SCHEDULED BRDG CHECK, FOUND LT WING LOWER RIB CHORD CRACKED AT STA 135.5, STR 2. REPAIRED CHORD PER ACO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,030 hrs · 53,385 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: ATTACH FITTING — CORRODED (VERTICAL STAB) · airframe 63,030 hrs · 53,385 cycles

DURING SCHEDULED BRDG CHECK, FOUND RT VERTICAL STABILIZER PRIMARY FITTING ATTACH LUGS CORRODED. REPAIRED FITTING PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,030 hrs · 53,385 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,030 hrs · 53,385 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 14L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,030 hrs · 53,385 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,030 hrs · 53,385 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,030 hrs · 53,385 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 807, STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,030 hrs · 53,385 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,030 hrs · 53,385 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,030 hrs · 53,385 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 14L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,030 hrs · 53,385 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,030 hrs · 53,385 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 14L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,030 hrs · 53,385 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 14L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,030 hrs · 53,385 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 14L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 63,030 hrs · 53,385 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 13R CRACKED AT BS 500D. REPAIRED STRINGER PER SRM.

Part: CAP — CRACKED (BULKHEAD) · airframe 63,030 hrs · 53,385 cycles

DURING SCHEDULED DAL CHECK, FOUND AFT PRESSURE BULKHEAD DOME CAP CRACKED AT BS 1016, BETWEEN 12 O'CLOCK AND 6 O'CLOCK POSITION. REPAIRED DOME CAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,030 hrs · 53,385 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,030 hrs · 53,385 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,030 hrs · 53,385 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,030 hrs · 53,385 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,030 hrs · 53,385 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,030 hrs · 53,385 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,030 hrs · 53,385 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,030 hrs · 53,385 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,030 hrs · 53,385 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,030 hrs · 53,385 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 1042, STR 25R. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,030 hrs · 53,385 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 336, STR 18L. REMOVED AND REPLACED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,030 hrs · 53,385 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 320, STR 18L. REMOVED AND REPLACED FRAME PER SRM.

Part: HINGE FITTING — CORRODED (HORIZ STAB) · airframe 63,030 hrs · 53,385 cycles

DURING SCHEDULED BRDG CHECK, FOUND LT HORIZONTAL STABILIZER CENTER SECTION HINGE FITTING CORRODED AT BEARING FACE. REPAIRED FITTING PER SWA EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,030 hrs · 53,385 cycles

DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500D, STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 63,030 hrs · 53,385 cycles

DURING SCHEDULED BRDG CHECK, FOUND RT VERTICAL STABILIZER AFT INBOARD FAIL SAFE FITTING CORRODED. REMOVED AND REPLACED FITTING PER SWA EA.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 63,030 hrs · 53,385 cycles

DURING SCHEDULED BRDG CHECK, FOUND LT VERTICAL STABILIZER AFT INBOARD FAIL SAFE FITTING CORRODED. REMOVED AND REPLACED FITTING PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,030 hrs · 53,385 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,030 hrs · 53,385 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,030 hrs · 53,385 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 14R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,030 hrs · 53,385 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 63,030 hrs · 53,385 cycles

DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD STIFFENER CORRODED AT BS 1016, LBL 0.5. REPAIRED STIFFENER PER SRM.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 63,030 hrs · 53,385 cycles

DURING SCHEDULED BRDG CHECK, FOUND RT VERTICAL STABILIZER LUG FITTING CORRODED. REPAIRED FITTING PER SWA EA.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 63,030 hrs · 53,385 cycles

DURING SCHEDULED BRDG CHECK, FOUND LT VERTICAL STABILIZER LUG FITTING CORRODED. REPAIRED FITTING PER SWA EA.

Part: FLAP TRACK — CORRODED (NR 7 TE FLAP) · airframe 63,030 hrs · 53,385 cycles

DURING SCHEDULED BRDG CHECK, FOUND RT WING NR 7 OUTBOARD FLAP INBOARD TRACK FITTING CORRODED. REPAIRED FLAP TRACK PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 727B S14L) · airframe 63,030 hrs · 53,385 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 14L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: ATTACH FITTING — CRACKED (NLG WW) · airframe 63,030 hrs · 53,385 cycles

DURING SCHEDULED BRDG CHECK, FOUND NLG W/W LT SNUBBER ATTACHMENT CRACKED AT LBL 7.75. REPAIRED ATTACHMENT PER ACO.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 63,030 hrs · 53,385 cycles

DURING SCHEDULED BRDG CHECK, FOUND NLG W/W VERTICAL WEB CRACKED AT FWD TEE CHORD. REPAIRED WEB PER SRM.

Part: CREASE BEAM — CORRODED (BS 660) · airframe 63,030 hrs · 53,385 cycles

DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM CORRODED AT BS 660, LBL 70. REMOVED AND REPLACED CREASE BEAM PER SRM.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 63,030 hrs · 53,385 cycles

DURING SCHEDULED BRDG CHECK, FOUND AFT CARGO DOOR FWD FRAME CORRODED AT LOWER FWD CORNER. REPAIRED FRAME PER ACO.

Part: TIRE — SEPARATED (RT MLG) · airframe 61,585 hrs · 52,264 cycles

NR 1 MAIN TIRE TREAD SEPARATED. R&R NR 1 MAIN WHEEL AND TIRE ASSY PER MM. R&R NR 4 GROUND SPOILER AND LT INBOARD FWD FLAP PER MM.

Part: SKIN — CRACKED (BS 415) · airframe 61,513 hrs · 52,198 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 415, STR 16L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 925) · airframe 61,513 hrs · 52,198 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 925, STR 24L. REPAIRED SKIN PER SRM.

Part: TAB — WORN (RT AILERON) · airframe 61,513 hrs · 52,198 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING AILERON TAB OUTBOARD HINGE FITTING WORN. REMOVED AND REPLACED AILERON TAB PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 60,647 hrs · 51,495 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RIGHT FWD FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: STRUCTURE — DELAMINATED (T/E FLAP) · airframe 60,514 hrs · 51,393 cycles

DURING SCHEDULED C3 CHECK, FOUND LEFT WING INBOARD FORE FLAP DELAMINATED AT UPPER INBOARD END. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,427 hrs · 51,329 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 376, STR 14L. REPAIRED SKIN PER SWA EA.

Part: LIGHT — BROKEN (CABIN) · airframe 59,147 hrs · 50,342 cycles

EMERGENCY EXIT LIGHT BROKEN AT L1 DOOR. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (BS 520 S15L) · airframe 589,090 hrs · 50,142 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 15L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,197 hrs · 49,581 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SERVICE DOOR CUTOUT FWD UPPER CORNER. REPAIRED SKIN PER ER.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 58,197 hrs · 49,581 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT FWD CARGO DOOR CUTOUT FWD FRAME INBOARD CORNER. REPAIRED FRAME WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,197 hrs · 49,581 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 58,197 hrs · 49,581 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 58,197 hrs · 49,581 cycles

DURING SCHEDULED SPV CHECK, FOUND BULKHEAD VERTICAL CHORD CRACKED AT BS 178, LBL 5.7. REPAIRED BULKHEAD CHORD PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 58,197 hrs · 49,581 cycles

DURING SCHEDULED SPV CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, RBL 10 TO LBL 12. REMOVED AND REPLACED WEB SECTION PER SRM.

Part: LENS — MISSING (CABIN) · airframe 57,684 hrs · 49,199 cycles

DURING SCHEDULED C4 CHECK, FOUND RT FWD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,684 hrs · 49,199 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 851, STR 10R. REPAIRED SKIN PER SWA EA.

Part: LENS — LOOSE (CABIN) · airframe 57,684 hrs · 49,199 cycles

DURING SCHEDULED C4 CHECK, FOUND LT FWD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,684 hrs · 49,199 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 518, STR 12L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 500C) · airframe 57,241 hrs · 48,857 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 10L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 500C) · airframe 57,241 hrs · 48,857 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 15R. REPAIRED SKIN PER SWA EA AND SRM.

Part: SKIN — CRACKED (BS 729D) · airframe 57,241 hrs · 48,857 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 729D, STR 19R. REPAIRED SKIN PER SWA EA AND SRM.

Part: SKIN — CRACKED (BS 981) · airframe 56,720 hrs · 48,455 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 981, STR 21L. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 930-940) · airframe 56,720 hrs · 48,455 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 930 TO BS 940, STR 23R. REPAIRED SKIN PER SRM.

Part: WEB — CRACKED (LT MLG WW) · airframe 55,442 hrs · 47,429 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BEADED WEB CRACKED AT BS 663, BETWEEN LBL 39.5 & LBL 42. REPAIRED BEADED WEB PER SWA EA.

Part: FITTING — LOOSE (GIRT BAR) · airframe 55,442 hrs · 47,429 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FLOOR FITTING LOOSE. SECURED FITTING PER MM.

Part: FITTING — WORN (GIRT BAR) · airframe 55,442 hrs · 47,429 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD AND AFT GIRT BAR FLOOR FITTINGS WORN. REMOVED AND REPLACED FITTINGS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,442 hrs · 47,429 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C + 17, STR 10L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,442 hrs · 47,429 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SWA EA & SRM.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 55,442 hrs · 47,429 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN BEAR STRAP CORRODED AT BS 493, RBL 13. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,442 hrs · 47,429 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 498, STR 16L. REPAIRED SKIN PER SWA EA & SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,442 hrs · 47,429 cycles

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

Part: STRINGER CLIP — CRACKED (BS 767) · airframe 55,442 hrs · 47,429 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 767, STR 25L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOOR SUPPORT — CRACKED (BS 658-672) · airframe 55,442 hrs · 47,429 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CRACK ON NR 2 LONGITUDINAL FLOOR SUPPORT BETWEEN BS 658 TO BS 672. REPAIRED FLOOR SUPPORT PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,830 hrs · 46,915 cycles

DURING SCHEDULED C1 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT BS 496 & BS 500D + 12, STR 10L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,278 hrs · 46,467 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D + 10, STR 14R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,890 hrs · 46,160 cycles

DURING SCHEDULED CHECK, FOUND FUSELAGE SKIN AT BS 941, STRINGER 21L, CRACKED. REPAIRED SKIN PER SRM.

Part: MOTOR — FAULTY (TE FLAPS) · airframe 53,746 hrs · 46,047 cycles

AIR TURNBACK, DECLARED EMERGENCY. AFTER TAKEOFF FLAPS WOULD NOT RETRACT OR EXTEND. REMOVED AND REPLACED FLAP DRIVE MOTOR PER MM.

Part: LIGHT — BROKEN (FWD CABIN) · airframe 53,168 hrs · 45,578 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS HOLDER CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,879 hrs · 45,347 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 500C, STRINGER 10R, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,870 hrs · 45,338 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 500C, STRINGER 10R, CRACKED. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF LIMITS (L2 DOOR) · airframe 52,612 hrs · 45,130 cycles

L2 DOOR EVAC SLIDE PRESSURE IND OUT OF LIMITS. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM.

Part: SKIN — DELAMINATED (LT WING SLAT) · airframe 51,588 hrs · 44,316 cycles

DURING SCHEDULED A1 CHECK, FOUND LT WING L/E NR 2 L/E SLAT DELAMINATED. REMOVED AND REPLACED NR 2 L/E SLAT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,157 hrs · 43,966 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 908, STRINGER 21L, CRACKED. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 50,338 hrs · 43,320 cycles

DURING SCHEDULED SC, FOUND L1 AND R1 DOOR EXIT LIGHTS WILL NOT ILLUMINATE. REMOVED AND REPLACED EXIT LIGHTS BATTERY PACK PER MM.

Part: WEDGE — DELAMINATED (RT WING SLAT) · airframe 50,105 hrs · 43,138 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING T/E MID FLAP OUTBOARD SIDE OF THE INBOARD T/E WEDGE PANEL DELAMINATED. REMOVED AND REPLACED WEDGE PANEL PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,334 hrs · 40,869 cycles

DURING SCHEDULED C1 CHECK, FOUND OVERHEAD BIN EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 21 ABC. RELAMPED EMERGENCY EXIT LIGHT PER MM.

Part: GUSSET — CRACKED (SERVICE DOOR) · airframe 47,315 hrs · 40,852 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR INTERNAL GUSSET CRACKED AT AFT DOOR HINGE. REMOVED AND REPLACED FWD SVC DOOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,310 hrs · 40,847 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED ON CAPTAINS UPPER WINDOW POST. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,315 hrs · 40,852 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED ON CO-PILOT'S UPPER WINDOW POST. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,310 hrs · 40,847 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 17L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLOORBEAM — CORRODED (AFT CARGO BAY) · airframe 47,310 hrs · 40,847 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT RBL 8, BS 845 AND BS 825. REPAIRED FLOORBEAM PER SWA RA.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 47,310 hrs · 40,847 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED AT REAR SPAR FWD OF INBD BALANCE BAY. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,310 hrs · 40,847 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLOORBEAM — CORRODED (AFT CARGO BAY) · airframe 47,310 hrs · 40,847 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAMS CORRODED AT BS 770 AT LBL 13, BS 860 AT RBL 8, BS 860 AT LBL 3, BS 847 AT LBL 6 AND BS 813 AT LBL 3. REPAIRED FLOORBEAMS PER SWA ER.

Part: BRACKET — CORRODED (FWD ENTRY DOOR) · airframe 47,310 hrs · 40,847 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET CORRODED. REMOVED AND REPLACED GIRT BAR BRACKET PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,913 hrs · 40,542 cycles

DURING SCHEDULED RON, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM.

Part: FIRE LOOP — FAULTY (APU) · airframe 46,367 hrs · 40,106 cycles

AIR TURNBACK, APU FIRE WARNING LIGHT AND BELL SOUNDED WHILE AIRBORNE, DISCHARGED ONE BOTTLE. INSPECTED, FOUND NO EVIDENCE OF FIRE. REMOVED AND REPLACED FIRE BOTTLE AND FIRE LOOP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,297 hrs · 40,053 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED 4 AFT OF BS 927, STR 23L. REPAIRED SKIN PER SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 44,989 hrs · 38,964 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 44,522 hrs · 38,587 cycles

DURING SCHEDULED C2 CHECK, FOUND OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW NR 20 DEF. SECURED LENS PER MM.

Part: SLIDE — OUT OF ADJUST (FWD ENTRY DOOR) · airframe 44,522 hrs · 38,587 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 43,201 hrs · 37,498 cycles

(DECLARED EMERGENCY) AT 29,000 FEET CABIN PRESS HORN SOUNDED AND CABIN PRESS CONTROL INOP. REMOVED AND REPLACED AFT OUTFLOW VALVE PER MM.

Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 42,745 hrs · 37,110 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: CONTROL VALVE — LEAKING (MLG W/W) · airframe 41,948 hrs · 36,432 cycles

DECLARED EMERGENCY, DURING CLIMB LOST A-SYSTEM HYDRAULIC FLUID, TOTAL A-HYD SYSTEM FAILURE. REMOVED AND REPLACED LANDING GEAR TRANSFER FLOW CONTROL VALVE AND PTU CONTROL VALVE PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 41,268 hrs · 35,872 cycles

EMERGENCY FLASHLIGHT INOP AT AFT CABIN. R&R FLASHLIGHT PER MM.

Part: FRAME — CRACKED (CARGO DOOR) · airframe 38,732 hrs · 33,762 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD CARGO DOOR LOWER O/B T-CHORD CRACKED. REMOVED AND REPLACED FWD CARGO DOOR PER MM.

Part: SKIN — CRACKED (FUSELGE) · airframe 38,732 hrs · 33,762 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT ENTRY DOOR UPPER HINGE FUSELAGE SKIN CUT OUT CRACKED. REPAIRED SKIN PER SWA RA.

Part: LIGHT — LOOSE (SEAT 2, 20, & 22) · airframe 38,732 hrs · 33,762 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BULLNOSE EGRESS LIGHTS LOOSE AT SEAT 2D, 20D, AND 22D. SECURED LIGHTS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,732 hrs · 33,762 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD RIGHT O/B CHORD ANGLE CRACKED, WL 207. REPAIRED CHORD ANGLE SECTION PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 38,732 hrs · 33,762 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 773 FLOORBEAM UPPER SURFACE CORRODED, RBL 8. REPAIRED BEAM PER T1-253-025.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 38,732 hrs · 33,762 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 17R AND CLIP CRACKED, BS 178. REPAIRED STRINGER SECTION AND REMOVED AND REPLACED CLIP PER SRM.

Part: BATTERY PACK — INOPERATIVE (CABIN)

DURING SCHEDULED RON CHECK, FOUND AFT SECTION OF EEPLS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — DELAMINATED (TE FLAP)

DURING SCHEDULED C1 CHECK, FOUND LT WING OUTBOARD AFT FLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER SWA RA NR 1-357-0769.

Part: LEAD — CORRODED (NR 1 ENGINE EGT)

AIR TURNBACK, AFTER TAKEOFF, NR 1 ENG EGT IND OVERTEMPED TO 955 DEGREES FOR APPROX 2 SECONDS. C/W HOT SECTION BORESCOPE INSPECTION, CALIBRATED EGT IND, TROUBLESHOT AND REMOVED AND REPLACED NR 1 ENG EGT SOFT LEAD AT ENG PER MM.

Part: BULB — FAILED (RT EMER EXIT)

DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EXIT SIGN INOP. RELAMPED SIGN PER MM.

Part: CONNECTOR — LOOSE (NR 2 ADC)

AIR TURNBACK--- UPON TAKE OFF, F/O'S AIR SPEED, ALTIMETER INDICATORS AND TRANSPONDER INSTRUMENTS BECAME INOP. FOUND QUICK DISCONNECT ON NR 2 ADC LOOSE. SECURED CONNECTOR PER MM.

Part: FAN — FAILED (AC BAY)

NOTED ELECTRICAL SMOKE SMELL. CREW TURNED OFF RECIRCULATION FAN, SMELL DISSAPATED. CONTINUED PER MEL 21-26. DURING OVERNIGHT CHECK, REPLACED RECIRCULATION FAN AND OP CHECKED PER BOEING M/M.

Part: GEAR LIGHT — ILLUMINATED (RT MLG)

INBOARD INTO DAL, RIGHT MAIN GEAR UNSAFE LIGHT ILLUMINATED. GEAR WAS RECYCLED AND RECEIVED NORMAL INDICATION. AIRCRAFT LANDED AT DAL WITHOUT INCIDENT. GEAR RETRACTION TESTED SEVERAL TIMES AND CHECKED SENSORS PER BOEING M/M.

Part: SKIN — CRACKED (RT WING)

DURING SCHEDULED 1/4 D-CHECK, FOUND RT WING LOWER SKIN CRACKED JUST I/B OF NUMBER 6 AUX TRACK. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 787)

DURING SCHEDULED 1/4 D-CHECK, FOUND RIGHT TRANSITION ANGLE CRACKED AT BS 787. REPAIRED PER BOEING SRM.

Part: CHANNEL — CRACKED (FWD CARGO)

DURING SCHEDULED 1/4 D-CHECK, FOUND CHANNEL CRACKED ABOVE VHF ANTENNA, IN FWD CARGO BIN. REPLACED CHANNEL PER BOEING SRM.