N675AA

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,989 hrs · 62,461 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 23R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,989 hrs · 62,461 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 967, STR 21L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,989 hrs · 62,461 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 304, UPPER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,989 hrs · 62,461 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT LOWER HINGE CUTOUT, BS 304 ABOVE CUTOUT CENTER LINE. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,989 hrs · 62,461 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,989 hrs · 62,461 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT LOWER HINGE CUTOUT, BS 304 BELOW CUTOUT CENTER LINE. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,989 hrs · 62,461 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT, AT BS 304. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,989 hrs · 62,461 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 23R. REPAIRED SKIN PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 72,989 hrs · 62,461 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 908 TO BS 927, STR 24R. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,989 hrs · 62,461 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,989 hrs · 62,461 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,989 hrs · 62,461 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 932, STR 21R. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,989 hrs · 62,461 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,989 hrs · 62,461 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, AT BS 304 ABOVE CUTOUT CENTER LINE. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,989 hrs · 62,461 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 967, STR 21L. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,989 hrs · 62,461 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,989 hrs · 62,461 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, AT BS 304 BELOW CUTOUT CENTER LINE. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,017 hrs · 62,480 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER PAE ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,017 hrs · 62,480 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 23R. REPAIRED SKIN PER PAE ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,017 hrs · 62,480 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 967, STR 21L. REPAIRED SKIN PER PAE ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,985 hrs · 62,460 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,985 hrs · 62,460 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 967, STR 21L. REPAIRED SKIN PER ER.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 72,989 hrs · 62,461 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CORRODED AT BS 767, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 72,988 hrs · 62,461 cycles

DURING SCHEDULED HC1 CHECK, FOUND FWD CARGO DOOR SKIN CRACKED AT DOOR HANDLE CUTOUT. REPAIRED SKIN PER EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 72,921 hrs · 62,410 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED SPLICE PER SRM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 72,988 hrs · 62,461 cycles

DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 72,921 hrs · 62,410 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED SPLICE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,656 hrs · 61,486 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 348, STR 18R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,625 hrs · 61,455 cycles

DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503C, STR 15L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 500A S26L) · airframe 71,309 hrs · 61,229 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500A, STR 26L. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (RT WING LE SLAT) · airframe 71,309 hrs · 61,229 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED SLAT PER MM.

Part: SKIN — CRACKED (BS 370 S26L) · airframe 71,309 hrs · 61,229 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 370, STR 26L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 400 S26L) · airframe 71,309 hrs · 61,229 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 400, STR 26L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,050 hrs · 61,042 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 275 TO BS 279, STR 16L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,450 hrs · 59,871 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT UPPER AFT CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,441 hrs · 59,865 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 516 AND BS 487, STR 26L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,441 hrs · 59,865 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 19R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,441 hrs · 59,865 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT UPPER CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,966 hrs · 59,502 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 513B, STR 15R. REMOVED AND REPLACED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,765 hrs · 59,341 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 513D, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,765 hrs · 59,341 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 513D, STR 15L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,765 hrs · 59,341 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 733E, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,765 hrs · 59,341 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 769, STR 18L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,741 hrs · 59,319 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 19R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 68,339 hrs · 58,993 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (BS 382 S26L) · airframe 68,291 hrs · 58,957 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 382, STR 26L. REPAIRED SKIN PER SWA EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 67,692 hrs · 58,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 360, STR 27L. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 67,692 hrs · 58,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CRACKED AT BS 400, STR 17L. REPAIRED SHEAR TIE PER SRM.

Part: FLAP — CRACKED (LT WING) · airframe 67,692 hrs · 58,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND LEFT WING INBOARD FORE FLAP CRACKED AT LOWER AFT END. REPAIRED FLAP PER SRM.

Part: BEARING — WORN (LT ELEVATOR) · airframe 67,692 hrs · 58,483 cycles

DURING SCHEDULED 22Y CHECK, LEFT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED CONTROL ROD BUSHING AND BEARING PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 67,692 hrs · 58,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 19 DEF. REMOVED AND REPLACED STRIP PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 67,692 hrs · 58,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 21 ABC. REMOVED AND REPLACED STRIP PER MM.

Part: LENS — BROKEN (CABIN) · airframe 67,692 hrs · 58,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT LENS BROKEN AT ROW 2. REMOVED AND REPLACED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,409 hrs · 58,281 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 445, STR 26L. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 66,722 hrs · 57,782 cycles

DURING SCHEDULED A1 CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,277 hrs · 57,415 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 65,891 hrs · 57,114 cycles

FOUND LT OVERWING EMERGENCY EXIT LIGHT ASSY LOOSE. SECURED LIGHT ASSY PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 65,785 hrs · 57,026 cycles

DURING SCHEDULED SERVICE CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT BROKEN AT L2 DOOR. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (BS 508D S16R) · airframe 65,515 hrs · 56,801 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 508D, STR 16R. REPAIRED SKIN PER SWA EA.

Part: PRESSURE PANEL — CRACKED (MGL WW) · airframe 65,515 hrs · 56,801 cycles

DURING SCHEDULED PM CHECK, FOUND LT MLG W/W BEADED PRESSURE WEB CRACKED AT BS 664, LBL 42. REPAIRED PRESSURE WEB PER SWA EA.

Part: SKIN — CRACKED (BS 757 S19R) · airframe 65,515 hrs · 56,801 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 757, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 516D S16R) · airframe 65,515 hrs · 56,801 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 516D, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 65,508 hrs · 56,794 cycles

DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 65,497 hrs · 56,786 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT RT AFT FUSELAGE. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 65,368 hrs · 56,691 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 10 ABC. REMOVED AND REPLACED EEPLS PHOTOLUMINESCENT STRIP PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 64,877 hrs · 56,328 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT FRAME CRACKED AT BS 495, NR 5 DOOR STOP FITTING. REPAIRED FRAME PER SB.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,877 hrs · 56,328 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 794, RBL 48. REPAIRED FRAME SECTION PER SB.

Part: SKIN — CRACKED (BS 732 S14L) · airframe 64,877 hrs · 56,328 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 732, STR 14L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (BS 733 S20L) · airframe 64,877 hrs · 56,328 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 733, STR 20L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,877 hrs · 56,328 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 793, STR 18L. REPAIRED SKIN PER SRM.

Part: STRIP — LOOSE (CABIN) · airframe 64,716 hrs · 56,206 cycles

DURING SCHEDULED A2 CHECK, FOUND EEPLS STRIP LOOSE BETWEEN ROW 1 TO ROW 5 ABC. REMOVED AND REPLACED STRIP PER MM.

Part: SKIN — CRACKED (BS 426-446) · airframe 63,516 hrs · 55,270 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 426 TO BS 446, STR 28L TO STR 28R. REPAIRED SKIN PER SWA EA.

Part: WEB — CRACKED (BS 243.7) · airframe 63,242 hrs · 55,067 cycles

DURING SCHEDULED A1 CHECK, FOUND NLG W/W RT FWD SIDE WEB CRACKED AT BS 243.7, WL 168.5. REPAIRED WEB PER SWA EA.

Part: SKIN — CRACKED (BS 939.75) · airframe 63,009 hrs · 54,884 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 939.75, STR 21L. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 791) · airframe 62,531 hrs · 54,514 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 791, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,604 hrs · 53,785 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D + 6, STR 15R. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,077 hrs · 53,381 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 24R. REPAIRED FRAME PER PAE ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,555 hrs · 52,979 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN AT BS 760, STRINGER 18R, CRACKED. REPAIRED SKIN PER SRM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,664 hrs · 52,275 cycles

DURING SCHEDULED C3 CHECK, FOUND EMERGENCY EXIT LIGHT AT ROW 19 DEF, INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 59,345 hrs · 53,023 cycles

DURING SCHEDULED D-CHECK, FOUND KEEL BEAM CHORD AT BS 500C, STRINGER 28R, CORRODED. REPAIRED CHORD PER ER.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 59,347 hrs · 52,025 cycles

DURING SCHEDULED D-CHECK, FOUND VERTICAL STABILIZER SPAR ATTACH FITTINGS AIRCRAFT SIDE, FWD LT FITTING AFT LUG AFT FACE CORRODED. REPAIRED VERTICAL STAB FITTINGS PER ER.

Part: FITTING — CRACKED (FUSELAGE) · airframe 59,347 hrs · 52,025 cycles

DURING SCHEDULED D-CHECK, FOUND SPAR FITTING AT BS 1016, LBL 1, WL 247, CRACKED. REPAIRED FITTING PER ER.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 59,345 hrs · 52,023 cycles

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

Part: SKIN — CORRODED (FUSELAGE) · airframe 59,345 hrs · 52,023 cycles

DURING SCHEDULED D-CHECK, FOUND AFT CARGO COMPARTMENT SKIN AT BS 949, LBL 3, CORRODED. REPAIRED FUSELAGE SKIN PER BAC DRAWING AND SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 59,345 hrs · 52,023 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CHORD AT BS 947, LBL 54, CORRODED. REMOVED AND REPLACED CHORD SECTION PER ER.

Part: FRAME — CORRODED (FUSELAGE) · airframe 59,345 hrs · 52,023 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 847, STRINGER 27R, CORRODED. REMOVED AND REPLACED FRAME SECTION PER ER.

Part: DRAG BRACE — CORRODED (LT VERT STAB) · airframe 59,345 hrs · 52,023 cycles

DURING SCHEDULED D-CHECK, FOUND LT VERTICAL STABILIZER AFT DRAG BRACE, CORRODED. REMOVED AND REPLACED LT VERTICAL STABILIZER DRAG BRACE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 59,345 hrs · 52,023 cycles

DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOORBEAM AT BS 727B, LBL 24, CRACKED. REPAIRED FLOORBEAM PER ER.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 59,345 hrs · 52,023 cycles

DURING SCHEDULED D CHECK, FOUND AFT CARGO COMPARTMENT STRINGER 27L AT BS 949, CORRODED. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 59,345 hrs · 52,023 cycles

DURING SCHEDULED D CHECK, FOUND VERTICAL STIFFENER AT BS 663, RBL 6, CRACKED. REMOVED AND REPLACED VERTICAL STIFFENER PER SRM.

Part: LINK — CORRODED (RT WING) · airframe 59,345 hrs · 52,023 cycles

DURING SCHEDULED D CHECK, FOUND RT WING STABILIZER LINK BETWEEN MAIN GEAR BEAM AND REAR SPAR, CORRODED. REMOVED AND REPLACED RT WING STABILIZER LINK PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 59,345 hrs · 522,020 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 727E, RBL 9, WL, 149, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,345 hrs · 52,023 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME CHORD AT BS 727, LBL 11, CRACKED. REPAIRED FRAME CHORD PER SB, ER.

Part: SHEAR TIE — CORRODED (BS 500) · airframe 59,345 hrs · 52,023 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE AT BS 500 RBL 1, WL 148, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 59,345 hrs · 52,023 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 827, STRINGER 26L, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 59,345 hrs · 52,023 cycles

DURING SCHEDULED D-CHECK, FOUND RT & LT HORIZONTAL STAB FITTING, FWD & AFT SPARS CLEVIS LUGS CORRODED. REPAIRED HORIZONTAL STAB PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 59,345 hrs · 52,023 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 867, STRINGER 27L TO STRINGER 27R, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,345 hrs · 52,023 cycles

DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 188, STRINGER 17R, STRINGER 17L, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 59,345 hrs · 52,023 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 328, STRINGER 21L, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 59,345 hrs · 52,023 cycles

DURING SCHEDULED D-CHECK, FOUND FLOOR WEB AT BS 188 TO BS 196, STRINGER 17R, STRINGER 17L, CRACKED. REMOVED AND REPLACED FLOOR WEB SECTIONS PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 59,345 hrs · 52,023 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER 2L AT BS 380, CRACKED. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,345 hrs · 52,023 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 907, STRINGER 9R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 59,345 hrs · 52,023 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER 7L AT BS 1010, CRACKED. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 59,345 hrs · 52,023 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 500B, RBL 3, WL 148, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727D) · airframe 59,345 hrs · 52,023 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 727D, STRINGER 7R CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,345 hrs · 52,023 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 907, STR 9L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 59,345 hrs · 52,023 cycles

DURING SCHEDULED D-CHECK, FOUND ANGLE AT BS 360, STR 8L, CRACKED. REMOVED AND REPLACED ANGLE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 59,345 hrs · 52,023 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 328, RBL 20 TO RBL 50, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM.

Part: FRAME — CRACKED (BS 727C) · airframe 59,345 hrs · 52,023 cycles

DURING SCHEDULED D CHECK, FOUND FRAME AT BS 727C TO BS 727D, STR 9L CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,345 hrs · 52,023 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 787, STRINGER 9L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727C) · airframe 59,345 hrs · 52,023 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 727C, STR 4R TO STR 7R CRACKED. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,345 hrs · 52,023 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 727A, STR 9L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (BS 747) · airframe 59,345 hrs · 52,023 cycles

DURING SCHEDULED D CHECK, FOUND FRAME AT BS 747 TO BS 767, STR 9R TO STR 13R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 59,345 hrs · 52,023 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 500B, LBL 17, WL 150, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,257 hrs · 51,951 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 315, STRINGER 19R, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,247 hrs · 51,944 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 315, STRINGER 19R, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,491 hrs · 51,319 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN AT BS 765, STRINGER 19L, CRACKED. REPAIRED SKIN PER SRM.

Part: WIRE — SHORTED (JUNCTION BOX) · airframe 57,808 hrs · 50,774 cycles

AIRTURN BACK, SHORTLY AFTER TAKEOFF FELT A LIGHT VIBRATION AND THEN SMOKE AND FUMES IN COCKPIT. SMOKE SMELLED ELECTRICAL AND DISIPATED ALMOST IMMEDIATELY. VIBRATION ALSO CEASED. FOUND DISCONNECT D970 SHORTED TO GROUND AND WIRES W388-010-20 AND W388-027-20 BURNED IN JUNTION BOX AT BS 720R. SPLICED NEW WIRES AND REPLACED D970 CONNECTOR PER MM. ALSO, REMOVED AND REPLACED P5-2 FUEL SYSTEM MODULE PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 57,808 hrs · 50,774 cycles

DURING SCHEDULED C1 CHECK, FOUND BULKHEAD WEB CRACKED AT BS 1016, BETWEEN STRINGER 3R AND STRINGER 5R. REPAIRED WEB PER EA.

Part: FITTING — INOPERATIVE (GIRT BAR) · airframe 57,767 hrs · 50,738 cycles

L2 DOOR EVAC SLIDE GIRT BAR BRACKET SPRING INOP. REMOVED AND REPLACED L2 DOOR EVAC SLIDE BRACKET PER MM.

Part: FAN — DAMAGED (E/E BAY) · airframe 56,922 hrs · 50,073 cycles

ACRID SMELL IN COCKPIT. REMOVED AND REPLACED REC FAN PER MM AND OPS CK GOOD PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,822 hrs · 49,994 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 854, STR 20L. REPAIRED SKIN PER SRM.

Part: INDICATOR — OUT OF LIMITS (ESCAPE SLIDE) · airframe 56,607 hrs · 49,820 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: MOTOR — FAULTY (FLAP DRIVE) · airframe 56,492 hrs · 49,744 cycles

DECLARED EMERGENCY, T/E FLAPS WOULD NOT EXTEND PASS 1 PERCENT. REMOVED AND REPLACED FLAP DRIVE MOTOR (HYD AND ELECT) AND FLAP DRIVE UNIT PER MM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 56,363 hrs · 49,643 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 908, STRINGER 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 56,363 hrs · 49,643 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 360 BEAR STRAP CRACKED AT STRINGER 4R. REPAIRED BEAR STRAP PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 56,363 hrs · 49,643 cycles

DURING SPECIAL VISIT, FOUND 2 EA STRINGER SPLICES CRACKED, BS 540, STR 10R, AND BS 908, STR 4. REMOVED AND REPLACED BOTH STRINGER SPLICES PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,363 hrs · 49,643 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED, BS 360, BETWEEN STRINGERS 13R AND 15R. REPAIRED SHEAR TIE PER SRM.

Part: HINGE — WORN (ELEVATOR TAB) · airframe 55,847 hrs · 49,216 cycles

DURING SCHEDULED C3 CHECK, SWA SI 11139-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB PER MM.

Part: SLIDE — OUT OF ADJUST (ENTRY DOOR) · airframe 55,846 hrs · 49,214 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 54,909 hrs · 48,442 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE ASSY LOOSE. ADJUSTED SLIDE PER MM.

Part: LENS — LOOSE (CABIN) · airframe 54,243 hrs · 47,911 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,982 hrs · 47,686 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 440 AND BS 459, STR 10R. REPAIRED SKIN PER SRM.

Part: ACTUATOR — FAILED (SPOILER) · airframe 53,083 hrs · 46,954 cycles

DURING SCHEDULED C4 CHECK, NR 2 FLIGHT SPOILER WILL NOT RETRACT. REMOVED AND REPLACED SPOILER ACTUATOR PER MM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 51,386 hrs · 45,557 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL CHORD CRACKED .50 INCH LONG AT BS 178, WL 183 AND LBL 5.7. REPAIRED CHORD PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,386 hrs · 45,557 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED .25 INCH LONG AT BS 183, WL 233 AND LBL 17.1. REMOVED AND REPLACED VERTICAL BEAM WEB WEB PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,386 hrs · 45,557 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 179, WL 227 AND RBL 17.1. REPAIRED WEB PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,386 hrs · 45,557 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED .25 INCH LONG AT BS 181.5, WL 182 AND RBL 17.1. REPAIRED WEB PER SRM.

Part: BRACKET — LOOSE (AFT SVC DOOR) · airframe 51,386 hrs · 45,557 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LOOSE FASTENER, AT AFT SVC DOOR EMERGENCY EVAC SLIDE ATTACH BRACKET. SECURED BRACKET PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 51,386 hrs · 45,557 cycles

DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM SPLICE FITTING CORRODED AT BS 500D, FROM STR 28R TO 28L. REPAIRED KEEL BEAM PER SWA RA.

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 51,386 hrs · 45,557 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 767+5, RBL 3. REPAIRED FLOORBEAM PER SWA RA.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,386 hrs · 45,557 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED (3 EA) AT BS 178, WL 207 AND LBL 5, WL 207 AND LBL 6.75, WL 217 AND RBL 17.1. REPAIRED WEB PER SRM.

Part: WEB — CRACKED (LT MLG W/W) · airframe 51,386 hrs · 45,557 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB CRACKED AT BS 665, LBL 65. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 31,357 hrs · 45,529 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED 1.7 INCHES LONG AT BS 500D, STR 12L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (FWD ENTRY DOOR) · airframe 31,357 hrs · 45,529 cycles

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

Part: SPOILER — DELAMINATED (RT WING) · airframe 51,357 hrs · 45,529 cycles

DURING SCHEDULED C2 CHECK, FOUND NR 6 SPOILER DELAMINATED ON TOP SIDE. REMOVED AND REPLACED NR 6 SPOILER PER MM.

Part: LENS — MISSING (CABIN FLOOR) · airframe 51,329 hrs · 45,506 cycles

EEPLS LENS COVERS MISSING AT ROWS 3, 17, AND 20. DEFERRED PER MEL. LATER AT TPA DURING RON, INSTALLED LENSES PER MM.

Part: COVER — LOOSE (CABIN FLOOR) · airframe 51,024 hrs · 45,243 cycles

EEPLS TRACK COVER LOOSE AT ROW 2. SECURED COVER PER MM.

Part: CABLE — MISROUTED (AFT ENTRY DOOR) · airframe 50,858 hrs · 45,121 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINING CABLE IMPROPERLY ROUTED. REROUTED CABLE PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 50,673 hrs · 44,977 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,509 hrs · 44,018 cycles

DURING SCHEDULED BC4 CHECK, FOUND EEPLS COVER MISSING AND EEPLS INOP AT OVERWING EXIT. INSTALLED COVER, REMOVED AND REPLACED BATTERY PACK PER MM.

Part: TAB — CRACKED (LH ELEVATOR) · airframe 49,509 hrs · 44,018 cycles

DURING SCHEDULED C4 CHECK, FOUND LH ELEVATOR TAB INBD HINGE CUTOUT AREA CRACKED & DELAMINATED 1/8 X 1/2 . R&R TAB PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 49,345 hrs · 43,873 cycles

DURING SCHEDULED PMC CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT LT OVERWING. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM.

Part: COVER — MISSING (CABIN) · airframe 49,038 hrs · 43,629 cycles

EEPLS COVER MISSING AT ROW 10. INSTALLED EEPLS COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,871 hrs · 43,489 cycles

EEPLS INOP AND LENS MISSING AT MID CABIN. RELAMPED AND REPLACED LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 48,815 hrs · 43,437 cycles

EEPLS LENS MISSING AT MID CABIN. DEFERRED PER MEL. LATER AT LAX INSTALLED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,824 hrs · 43,443 cycles

DURING RON, FOUND EEPLS INOP AT ROW 17. RELAMPED EEPLS PER MM.

Part: LENS — MISSING (CABIN) · airframe 48,824 hrs · 43,443 cycles

DURING RON, FOUND EEPLS LENS MISSING AT ROW 9. INSTALLED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,500 hrs · 43,172 cycles

DURING SCHEDULED A1 CHECK, FOUND EEPLS INOP AT ROW 9. RELAMPED PER MM.

Part: BOTTLE — DISCHARGED (ESCAPE SLIDE) · airframe 47,806 hrs · 42,607 cycles

DURING SCHEDULED RON CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED AFT SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,594 hrs · 42,423 cycles

DURING SCHEDULED C2 CHECK, FOUND 2 EXTERNAL FUSELAGE SKIN CRACK AT BS 765, STR 19R. REPAIRED SKIN PER SRM.

Part: BALLAST — MALFUNCTIONED (CABIN) · airframe 47,311 hrs · 42,188 cycles

ELECTRICAL SMELL IN CABIN AT ROW 8 DEF. R&R SIDEWALL LIGHT BALLAST PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,916 hrs · 41,844 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 RT SIDE CHORD CRACKED AT WL 207. REMOVED AND REPLACED RT SIDE CHORD PER ACO 7342-53.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 46,916 hrs · 41,844 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND CRACK AT BS 178 BULKHEAD, WL 213. REPAIRED BULKHEAD PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 46,906 hrs · 41,832 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 180 HORIZONTAL WEBS CRACKED AT WL 207, RBL AND LBL 26. REMOVED AND REPLACED WEBS PER SRM.

Part: LIGHT — INOPERATIVE (CABIN)

EEPLS INOP AT OVERWING EXIT. REPAIRED BROKEN WIRING PER MM.

Part: SKIN — DELAMINATED (TE FLAP)

DURING SCHEDULED SERVICE CHECK, FOUND LT INBD AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED A1 CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SLIDE — LOOSE (CABIN)

AFT ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (RT LE SLAT)

DURING SCHEDULED C1 CHECK, FOUND RT WING NR 5 L/E SLAT LOWER SKIN CRACKED AT 3 EACH PLACES. REMOVED AND REPLACED L/E SLAT ASSY PER MM.

Part: MECHANISM — NOT LOCKED (SERVICE DOOR)

AIR TURNBACK, AFT SERVICE DOOR LIGHT ILLUMINATED DURING CLIMB (DOOR HANDLE WOULD NOT LOCK DOWN). ADJUSTED AND TESTED AFT SERVICE DOOR PER MM.

Part: STRINGER — CRACKED (BS 360)

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 14L CRACKED, BS 360. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: FLOORBEAM — CORRODED (BS 772)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FLOORBEAM UPPER FACE, BS 772, LBL 3 - LBL 12. REPAIRED BEAM PER SWA RA NR 1-A53-2021.

Part: FLOORBEAM — CORRODED (BS 928)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT FLOORBEAM FWD FLANGE, BS 328, RBL 49. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER — CORRODED (BS 827-847)

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 25L HAS HEAVY CORROSION BETWEEN BS 827-847. REPAIRED STRINGER PER SRM.

Part: BRACKET — CORRODED (PAX DOOR)

DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR GIRT BAR FWD AND AFT ATTACH BRACKETS CORRODED. REMOVED AND REPLACED ATTACH BRACKETS PER MM.

Part: FLOORBEAM — CORRODED (BS 312)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FLOORBEAM, BS 312, RBL 36. REPAIRED BEAM PER SWA RA NR 1-353-2136.

Part: FLOORBEAM — CORRODED (BS 947.5)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FLOORBEAM, BS 947.5, LBL 50. REPAIRED BEAM PER SWA RA NR 1-353-2135.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND AFT SECTION OF EMERGENCY ESCAPE FLOOR TRACK LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CORRODED (BS 947-1006)

DURING SCHEDULED RON CHECK, FOUND CORROSION AT FUSELAGE SKIN, BS 947-1006, STRINGER 28L. REPAIRED SKIN PER SRM.

Part: STRINGER — CORRODED (BS 1016)

DURING SCHEDULED RON CHECK, FOUND CRACKS THROUGH EDDY CURRENT INSPECTION AT STRINGERS 6L, AND 6R, AT BULKHEAD STA 1016. REPAIRED STRINGERS PER SWA RA NR 1-353-2086.

Part: FLOORBEAM — CORRODED (BS 986.5)

DURING SCHEDULED RON CHECK, FOUND CORROSION AT FLOORBEAM, BS 986.5, FROM CENTER TO RT END. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM.

Part: STRINGER — CORRODED (BS 947-1006)

DURING SCHEDULED RON CHECK, FOUND CORROSION AT STRINGER 28L, BETWEEN BS 947-1006. REPAIRED STRINGER PER SRM.

Part: LIGHT — INOPERATIVE (ROW 1 & 2)

EMERGENCY EXIT LIGHTS OUT ON ROWS 1 AND 2. RESECURED LIGHTS PER MM.

Part: SKIN — CORRODED (BS 500)

DURING SCHEDULED SC CHECK, FOUND FUSELAGE SKIN WITH 6 RIVETS POPPED AND ANTENNA DOUBLER CORRODED THROUGH, BETWEEN BS 500B AND C AND BETWEEN S28L AND R. REPAIRED PER BOEING SRM.

Part: BATTERY CHARGER — INOPERATIVE (ROW 19-23)

DURING WALKAROUND CHECK, FOUND EMERGENCY FLOOR PATH LIGHTING INOPERATIVE IN ROWS 19 THROUGH 23. REMOVED AND REPLACED EMERGENCY FLOOR PATH LIGHTING BATTERY CHARGER AND BATTERY PACK PER BOEING MM.

Part: LIGHT — LOOSE (CABIN)

DURING WALKAROUND CHECK, FOUND EMERGENCY EXIT LIGHT SECOND WHITE FROM FWD LOOSE IN FLOOR TRACK. REMOVED AND REPLACED TRACK ASSEMBLY, FWD 8 FEET OF CABIN PER BOEING MM.

Part: BATTERY CHARGER — INOP (ROW 19)

DURING WALKAROUND CHECK, FOUND ALL EMERGENCY FLOOR TRACK LIGHTING AFT OF ROW 19 APPEAR INOPERATIVE. REPLACED BATTERY CHARGER CONTROL HOUSING FOR AFT FLOOR TRACK LIGHTING PER BOEING MM.

Part: LINE — RUPTURED (B-HYD SYST)

EN ROUTE, EXPERIENCED B-SYSTEM HYDRAULIC QUANTITY LOSS. AIRCRAFT DIVERTED TO ONT AND MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED RUPTURED LINE TO B-ACOUSTIC MUFFLER, CHECKED CASE DRAIN FILTERS AND OP CHECKED PUMP PER BOEING M/M.

Part: FIRE WARNING — MALFUNCTIONED (APU)

ON CLIMBOUT, APU FIRE WARNING LIGHT AND BELL SOUNDED, FIRE BOTTLE WAS DISCHARGED. AIRCRAFT RETURNED TO LAS AND MADE AN UNEVENTFUL LANDING. INSPECTED AIRCRAFT AND FOUND NO EVIDENCE OF FIRE OR OVERHEAT CONDITION. DEFERRED FIRE DETECT/EXTINGUISHING SYSTEMS AND CONTINUED PER MEL.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AROUND 3 FASTENERS, AT WL 234, RBL 7-10. REPAIRED PER TI T1-A53-015.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT RBL 6.7, WL 197.5-198.6, AT LBL 4.7, WL 197-198.6, AT LBL 4.7, WL 202.5-203.5, AND RBL 4.7, WL 197.5 -198.5. REPAIRED PER SWA EWO 97-0189.

Part: EEL BATTERY — DISCHARGED (CABIN)

AT GATE, FOUND AFT EMERGENCY FLASHLIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M.

Part: SKIN — DENTED (LT WING LE)

DURING SCHEDULED MAINT CHECK, FOUND LEFT WING L/E DENTED 15 INCHES OUTBOARD OF NUMBER 1 ENGINE, MEASURING 1.5 INCHES BY .5 INCH BY .012 INCH DEEP. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING SCHEDULED MAINT CHECK, FOUND FLOORBEAM CORROSION AT BS 294.5, AT BL 0 AND LBL 12, WL 208, AND AT BS 360, LBL 10 AND RBL 1, WL 208, AND AT BS 344, LBL 10 AND RBL 10. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — DENTED (FUSELAGE)

DURING SCHEDULED MAINT CHECK, FOUND FUSELAGE SKIN DENTED AT BS 312, BETWEEN 18 AND 19R, AT BS 320, BETWEEN S20 AND 21R, FROM BS 363 TO 364, S5L, AND AT BS 1128, BETWEEN S14 AND 15R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — DENTED (BS 328)

DURING SCHEDULED MAINT CHECK, FOUND FUSELAGE SKIN CRACKED 1 INCH AT FORWARD GALLEY DOORWAY LOWER AFT CORNER, BS 328, RBL 65, WL 211. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: STRINGER CLIP — CRACKED (FUSELAGE)

DURING SCHEDULED MAINT CHECK, FOUND STRINGER CLIPS CRACKED AT BS 400, S27L, AND 28L, AT BS 747, S10R, AT BS 500D, S3R AND 19R/L, AT BS 406, S3R, AT BS 380, S7L, AT BS 500A, S1, AT BS 727B, S14L, AT BS 663, S10R AND L, AND AT BS 727A, S16R. REPLACED ALL PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — BENT (AFT SERV DOOR)

DURING SCHEDULED MAINT CHECK, FOUND AFT SERVICE DOOR EXTERNAL SKIN BENT AT UPPER OUTER EDGE LOWER HINGE CUTOUT. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: FRAME — CRACKED (BS 492)

DURING SCHEDULED MAINT CHECK, FOUND FUSELAGE FRAME FLANGE CRACKED AT BS 492, S24R. REPAIRED PER TRAMCO EWO 95-0194.

Part: FLOORBEAM — CORRODED (BS 986.5)

DURING SCHEDULED MAINT CHECK, FOUND FLOORBEAM CORROSION AT BS 986.5, TOP AND BOTTOM OF UPPER T-CHORD FROM LBL 10 TO RBL 49. REPAIRED PER TRAMCO EWO 95-0172.