N686SW

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 76,329 hrs · 63,276 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED SLIDE PER MM.

Part: BALLAST — INOPERATIVE (CABIN) · airframe 76,329 hrs · 63,276 cycles

RT READING LIGHT AT ROW 19 BURNED OFF. SMOKING POWER TO LIGHT TURNED OUT FIRST OFFICERS SIDE. REMOVED AND REPLACED BALLAST PER MM.

Part: SKIN — WORN (FUSELAGE) · airframe 75,714 hrs · 62,802 cycles

DURINGS SCHEDULED 26Y CHECK, FOUND LT DORSIL FIN SKIN WORN BETWEEN BS 965 TO BS 1006. REPAIRED SKIN IAW ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,714 hrs · 62,802 cycles

DURING SCHEDULED 26Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR AFT LOWER CORNER. REPAIRED SKIN PER ER AND EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 75,714 hrs · 62,802 cycles

DURINGS SCHEDULED 26Y CHECK, FOUND SPLICE ANGLE CRACKED AT BS 540, BETWEEN STR 21L TO STR 22L. REMOVED AND REPLACED ANGLE IAW ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,714 hrs · 62,802 cycles

DURING SCHEDULED 26Y CHECK FOUND FRAME CRACKED AT BS 639, LBL 66. REPAIRED FRAME IAW ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,714 hrs · 62,802 cycles

DURING SCHEDULED 26Y CHECK FOUND FRAME CRACKED AT BS 639, RBL 66. REPAIRED FRAME IAW ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,714 hrs · 62,802 cycles

DURING SCHEDULED 26Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT LOWER CORNER. REPAIRED SKIN IAW EA AND ER.

Part: SKIN — WORN (FUSELAGE) · airframe 75,714 hrs · 62,802 cycles

DURING SCHEDULED 26Y CHECK, FOUND DORSIL FIN SKIN DOUBLER WORN BETWEEN BS 875 TO BS 885, STR 1L. REPAIRED SKIN IAW ER AND EA.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 75,714 hrs · 62,802 cycles

DURING SCHEDULED 26Y CHECK, FOUND L1 DOOR EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 75,714 hrs · 62,802 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED SPLICE IAW EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 75,714 hrs · 62,802 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 807, STR 21L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,714 hrs · 62,802 cycles

DURING SCHEDULED 26Y CHECK, FOUND AFT CARGO BAY SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,714 hrs · 62,802 cycles

DURING SCHEDULED 26Y CHECK, FOUND AFT CARGO BAY SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,714 hrs · 62,802 cycles

DURING SCHEDULED 26Y CHECK, FOUND SKIN CRACKED AT BS 685+3, STR 10R. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 7,514 hrs · 62,802 cycles

DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 7,514 hrs · 62,802 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 807, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 7,514 hrs · 62,802 cycles

DURING SCHEDULED 26Y CHECK, FOUND SKIN CRACKED AT BS 266, STR 9L. REPAIRED SKIN IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,714 hrs · 62,802 cycles

DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN STR 28L TO STR 28R. REPAIRED SHEAR TIE IAW SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 75,714 hrs · 62,802 cycles

DURING SCHEDULED 26Y CHECK, FOUND LT WING I/B AFT FLAP O/B TRAILING EDGE DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,714 hrs · 62,802 cycles

DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,714 hrs · 62,802 cycles

DURING SCHEDULED 26Y CHECK, FOUND L2 DOOR EMERGENCY EXIT FUSELAGE SKIN CRACKED AT LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: COVER — BROKEN (CABIN) · airframe 75,477 hrs · 62,620 cycles

DURING SCHEDULED MV2 CHECK FOUND, R1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 73,671 hrs · 61,273 cycles

DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR UPPER DOOR HINGE CUTOUT LOWER I/B CORNER OF DOOR FRAME SKIN CRACKED. REMOVED AND REPLACED DOOR PER SRM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 73,645 hrs · 61,253 cycles

DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED CHARGER PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 73,645 hrs · 61,253 cycles

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

Part: BUSHING — CORRODED (VERTICAL STAB) · airframe 73,645 hrs · 61,253 cycles

DURING SCHEDULED SPV CHECK, FOUND VERTICAL FIN LT PRIMARY LUG BUSHING CORRODED. REMOVED AND REPLACED BUSHING PER BAC DWG.

Part: COVER — MISSING (CABIN) · airframe 72,992 hrs · 60,745 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT COVER MISSING AT ROW 10. INSTALLED COVER PER MM.

Part: LENS — LOOSE (CABIN) · airframe 72,942 hrs · 60,711 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS LOOSE AT ROW 8. REMOVED AND REPLACED LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 72,942 hrs · 60,711 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS LOOSE AT ROW 10. REMOVED AND REPLACED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,023 hrs · 60,006 cycles

DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER FWD CORNER. REPAIRED SKIN PER SRM.

Part: BRACKET — BROKEN (CABIN) · airframe 71,864 hrs · 59,894 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHT BRACKET BROKEN O/B SIDE OF FORWARD JUMPSEAT. SECURED BRACKET PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,553 hrs · 59,662 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500D, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 71,508 hrs · 59,631 cycles

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

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 71,192 hrs · 59,407 cycles

FWD GALLEY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 70,729 hrs · 59,087 cycles

DURING SCHEDULED 24Y CHECK, FOUND R2 DOOR LOWER EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 70,729 hrs · 59,087 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 15L TO STR 14L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,729 hrs · 59,087 cycles

DURING SCHEDULED 24Y CHECK, FOUND R2 DOOR OVERHEAD EMERGENCY EXIT SIGN FAULTY. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,729 hrs · 59,087 cycles

DURING SCHEDULED 24Y CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 70,729 hrs · 59,087 cycles

DURING SCHEDULED 24Y CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: FLAP — CORRODED (LT WING) · airframe 70,729 hrs · 59,087 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 2 O/B FLAP CORRODED. REMOVED AND REPLACED O/B FLAP PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,729 hrs · 59,087 cycles

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

Part: FITTING — CORRODED (GIRT BAR) · airframe 70,729 hrs · 59,087 cycles

DURING SCHEDULED 24Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING INSERT CORRODED. REMOVED AND REPLACED FITTING ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,729 hrs · 59,087 cycles

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

Part: FITTING — CORRODED (GIRT BAR) · airframe 70,729 hrs · 59,087 cycles

DURING SCHEDULED 24Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT FITTINGS CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 70,729 hrs · 59,087 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM CORRODED AT BS 732D, LBL 8. REPAIRED BEAM PER EA.

Part: SKIN — CRACKED (NR 2 SLAT) · airframe 70,729 hrs · 59,087 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 2 SLAT LOWER SURFACE CRACKED. REPAIRED SLAT PER SRM.

Part: FLOORBEAM — CORRODED (BS 772) · airframe 70,729 hrs · 59,087 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO BAY FLOORBEAM CORRODED AT BS 772, RBL 8. REPAIRED BEAM PER AAR EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 70,729 hrs · 59,087 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED BETWEEN BS 706 TO BS 712, BBL .070. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 70,729 hrs · 59,087 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM CORRODED AT BS 732D, RBL 8. REPAIRED BEAM PER EA.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 70,729 hrs · 59,087 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 1 SLAT O/B WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 70,729 hrs · 59,087 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 70,729 hrs · 59,087 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM CORRODED AT BS 734C, LBL 8. REPAIRED BEAM PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,729 hrs · 59,087 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 16R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,729 hrs · 59,087 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 15L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 70,729 hrs · 59,087 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 500, STR 28R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,729 hrs · 59,087 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 16R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,729 hrs · 59,087 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,729 hrs · 59,087 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,729 hrs · 59,087 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 16R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,729 hrs · 59,087 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 70,729 hrs · 59,087 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO BAY FLOORBEAM CORRODED AT BS 772, RBL 3. REPAIRED BEAM PER AAR EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,729 hrs · 59,087 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,729 hrs · 59,087 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 70,729 hrs · 59,087 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT BACKUP INTERCOSTAL CRACKED AT BS 333. REPAIRED INTERCOSTAL PER SWA EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 70,729 hrs · 59,087 cycles

DURING SCHEDULED 24Y CHECK, FOUND NR 5 L/E SLAT LOWER SKIN CRACKED. REPAIRED SLAT PER SRM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 70,729 hrs · 59,087 cycles

DURING SCHEDULED 24Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: SKIN — CRACKED (LE SLAT) · airframe 70,729 hrs · 59,087 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING O/B LEADING EDGE NR 6 SLAT LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: LENS — MISSING (CABIN) · airframe 70,090 hrs · 58,607 cycles

DURING SCHEDULED 2HC1, FOUND BULLNOSE EMERGENCY LIGHT LENS MISSING AT 21 ABC. INSTALLED LENS PER MM.

Part: COVER — MISSING (CABIN) · airframe 69,074 hrs · 57,885 cycles

OVERHEAD EMERGENCY EXIT SIGN LIGHT BULB COVER MISSING AT ROW 2. INSTALLED COVER PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 68,401 hrs · 57,404 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CORRODED AT BS 500D, BETWEEN STR 25R TO STR 26R. REPAIRED FRAME PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,401 hrs · 57,404 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,401 hrs · 57,404 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,401 hrs · 57,404 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 24R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,401 hrs · 57,404 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,401 hrs · 57,404 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,401 hrs · 57,404 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED SHEAR TIE PER ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 68,401 hrs · 57,404 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CORRODED AT BS 360, STR 26L. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 68,401 hrs · 57,404 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 727B, BETWEEN STR 20R TO STR 21R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: LENS — CRACKED (EXTERIOR) · airframe 68,401 hrs · 57,404 cycles

DURING SCHEDULED SPV CHECK, FOUND EXTERNAL EMERGENCY EXIT LIGHT LENS CRACKED AT BS 727D, BETWEEN STR 22L TO STR 23L. REMOVED AND REPLACED LIGHT ASSY PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 68,401 hrs · 57,404 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CORRODED AT BS 540, STR 26L. REPAIRED SKIN PER ER.

Part: BATTERY — DISCHARGED (CABIN) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CABIN EMERGNECY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 68,390 hrs · 57,395 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,389 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 291, WL 259 RT SIDE. REPAIRED SKIN PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,389 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 1006, STR 25R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,389 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 950, STR 27R. REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 25R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, BETWEEN STR 21L TO STR 22L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM CRACKED AT BS 617, STR 17R. REPAIRED BEAM PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 727C, STR 10R. REPAIRED STRINGER PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CRACKED AT BETWEEN BS 616 TO BS 639, RBL 65, WL 208. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED BETWEEN BS 360 TO BS 440, STR 22R. REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED BETWEEN BS 360 TO BS 440, STR 21R. REMOVED AND REPLACED STRINGER PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND VERTICAL WEB CRACKED AT BS 227, BL 0. REPAIRED WEB PER PAE DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 19L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 986, STR 25R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

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

Part: STRINGER — CORRODED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BETWEEN BS 360 TO BS 440, STR 23R. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 914, STR 25L. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 3L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

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

Part: STRINGER — CORRODED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 520, STR 23L. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BETWEEN BS 967 TO BS 987, STR 25L. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 18L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BETWEEN BS 360 TO BS 440, STR 24R. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 460, BETWEEN STR 14R TO STR 15R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, BETWEEN STR 23L TO STR 24L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 26L TO 27L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 767, RBL 3, WL 149. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 3L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STR 26L CORRODED AT BS 936. REPAIRED STRINGER PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STR 25L CORRODED AT BS 985. REPAIRED STRINGER PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STR 26L CORRODED AT BS 980. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 867B, BETWEEN RBL 1 TO RBL 4. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, BETWEEN STR 15R TO 16R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 727B, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 1006, STR 23R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE DAMAGED AT BS 500D, BETWEEN STR 16R TO STR 17R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 947, BETWEEN STR 26R TO 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 986, STR 26R. REMOVED AND REPLACED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 727A, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 987, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE DAMAGED AT BS 520, BETWEEN STR 16R TO STR 17R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 947, BETWEEN STR 27L TO 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 907, STR 25R. REMOVED AND REPLACED SPLICE PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND NR 2 SLAT T/E WEDGE DELAMINATED AT UPPER SURFACE. REPAIRED WEDGE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 3L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727, STR 2R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 907, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,390 hrs · 57,395 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,389 hrs · 57,395 cycles

DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 21L. REPAIRED SKIN PER SWA EA.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,131 hrs · 57,204 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (BS 747 S24L) · airframe 68,082 hrs · 57,164 cycles

DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 24L. REPAIRED SKIN PER SWA EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,082 hrs · 57,164 cycles

DURING SCHEDULED MV3 CHECK, FOUND LT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,082 hrs · 57,164 cycles

DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,082 hrs · 57,164 cycles

DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 24L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,082 hrs · 57,164 cycles

DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 20L. REPAIRED SKIN PER SWA EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,082 hrs · 57,164 cycles

DURING SCHEDULED MV3 CHECK, FOUND LT FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,082 hrs · 57,164 cycles

DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 21L. REPAIRED SKIN PER SWA EA.

Part: MEC — FAULTY (NR 1 ENGINE) · airframe 67,790 hrs · 56,937 cycles

DURING DESCENT NR 1 ENGINE HANG UP AT 50% FOR TWO TO THREE MINUTES, THEN ROLLS BACK. R&R NR 1 MEC PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,759 hrs · 56,214 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,759 hrs · 56,214 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,488 hrs · 56,016 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 773, STR 22L. REPAIRED SKIN PER SWA EA.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 66,411 hrs · 59,954 cycles

DURING SCHEDULED MV2 CHECK, RT FWD CABIN EMERGENCY BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: CONNECTOR — DIRTY (CABIN) · airframe 66,317 hrs · 55,882 cycles

DURING SCHEDULED MV3 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INTERMITTENT. FOUND LIGHT ASSY CONNECTOR DIRTY. CLEANED CONNECTOR PER MM.

Part: CONNECTOR — DIRTY (CABIN) · airframe 66,317 hrs · 55,882 cycles

DURING SCHEDULED MV3 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INTERMITTENT. FOUND LIGHT ASSY CONNECTOR DIRTY. CLEANED CONNECTOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,876 hrs · 55,548 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,975 hrs · 54,836 cycles

DURING SCHEDULED 22Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 5 DEF. REPAIRED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,975 hrs · 54,836 cycles

DURING SCHEDULED 22Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 8 DEF. REPAIRED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,975 hrs · 54,836 cycles

DURING SCHEDULED 22Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 1 DEF. REPAIRED LIGHT ASSY PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,925 hrs · 54,836 cycles

DURING SCHEDULED 22Y CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,925 hrs · 54,836 cycles

DURING SCHEDULED 22Y CHECK, FOUND FWD RIGHT CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,925 hrs · 54,836 cycles

DURING SCHEDULED 22Y CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,925 hrs · 54,836 cycles

DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: GLOWSTRIP — DELAMINATED (CABIN) · airframe 64,975 hrs · 54,836 cycles

DURING SCHEDULED 22Y CHECK, FOUND MID CABIN EEPLS PHOTOLUMINESCENT STRIPS DELAMINATED. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,975 hrs · 54,836 cycles

DURING SCHEDULED 22Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 23 DEF. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,975 hrs · 54,836 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 20R. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 64,975 hrs · 54,836 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 312, LBL 12. REPAIRED FLOORBEAM PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,975 hrs · 54,836 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT EQUIPMENT COOLING DUCT EXHAUST BS 378, BL 0. REPAIRED SKIN PER EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 64,975 hrs · 54,836 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER 8R CRACKED AT BS 344. REPAIRED STRINGER PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 64,975 hrs · 54,836 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 312, LBL 12. REPAIRED FLOORBEAM PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,975 hrs · 54,836 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT CRACKED BS 450, BL 0. REPAIRED SKIN PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,975 hrs · 54,836 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 28R AND STR 28L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 64,975 hrs · 54,836 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT PRESSURE BULKHEAD CORRODED AT BS 1016, BETWEEN STR 26L AND STR 26R. REPAIRED BULKHEAD PER ACO.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 64,975 hrs · 54,836 cycles

DURING SCHEDULED 22Y CHECK, FOUND LEFT WING INBOARD T/E AFT FLAP DELAMINATED AT INBOARD LOWER END. REPAIRED FLAP PER SRM.

Part: STIFFENER — CORRODED (BS 1016) · airframe 64,975 hrs · 54,836 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT PRESSURE BULKHEAD STIFFENER CORRODED AT BS 1016, BL 0. REMOVED AND REPLACED STIFFENER PER SRM.

Part: FRAME — CRACKED (BS 727A S8R) · airframe 64,975 hrs · 54,836 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 400 S8R) · airframe 64,975 hrs · 54,836 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 277 S15R) · airframe 64,975 hrs · 54,836 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 294 S11L) · airframe 64,975 hrs · 54,836 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 64,975 hrs · 54,836 cycles

DURING SCHEDULED 22Y CHECK, FOUND LEFT WING INBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,975 hrs · 54,836 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,975 hrs · 54,836 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,975 hrs · 54,836 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,975 hrs · 54,836 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,975 hrs · 54,836 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,851 hrs · 53,954 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 24R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,851 hrs · 53,954 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 760, STR 21L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,851 hrs · 53,954 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 794, STR 19L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,851 hrs · 53,954 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 787 S18L) · airframe 63,188 hrs · 53,444 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 18L. REPAIRED SKIN PER SWA EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,847 hrs · 53,191 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 312, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,847 hrs · 53,191 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 62,847 hrs · 53,191 cycles

DURING SCHEDULED SPV CHECK, FOUND MID CABIN EMERGENCY EXIT BATTERIES INOP. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 62,847 hrs · 53,191 cycles

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

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 62,847 hrs · 53,191 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 25L, BS 360. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,847 hrs · 53,191 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 492, STR 22R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,773 hrs · 53,129 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 964, STR 21L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 62,773 hrs · 53,129 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 61,850 hrs · 52,377 cycles

DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 61,850 hrs · 52,377 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING OUTBOARD AFT FLAP DELAMINATED AT INBOARD LOWER END. REMOVED AND REPLACED AFT FLAP PER MM.

Part: LINE — LEAKING (MLG WW) · airframe 61,488 hrs · 52,086 cycles

AIR TURN BAC, DECLARED EMERGENCY MASTER CAUTION AND "B" HYDRAULIC SYSTEM LOW PRESSURE LIGHT ILLUMINATED FOLLOWED BY "B" HYDRAULIC SYSTEM QUANTITY GAUGE DROPPING. REMOVED AND REPLACED HYDRAULIC LINE AT "B" SYSTEM ACOUSTIC FILTER AND "B" SYSTEM CASE DRAIN FILTER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,243 hrs · 51,879 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 847, STR 25L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,243 hrs · 51,879 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 803, STR 26L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,234 hrs · 51,871 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 760, STR 23L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,234 hrs · 51,871 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 765, STR 23L. REPAIRED SKIN PER SWA EA.

Part: CABLE — MISROUTED (EVAC SLIDE) · airframe 60,897 hrs · 51,623 cycles

DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EMERGENCY EXIT EVAC SLIDE CABLE MISROUTED. REROUTED EVAC SLIDE CABLE PER MM.

Part: COFFEEMAKER — FAULTY (FWD GALLEY) · airframe 60,611 hrs · 51,401 cycles

BURNING SMELL IN FWD GALLEY. REMOVED AND REPLACED FWD COFFEEMAKER PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 59,951 hrs · 50,890 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 8 ABC. REMOVED AND REPLACED STRIP PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,951 hrs · 50,890 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT CABIN RT LOWER EMERGENCY EXIT LIGHTS INOP. RELAMPED LIGHTS PER MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 59,021 hrs · 50,195 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 360, STR 25R. REPAIRED SKIN PER SRM.

Part: WINDOW — ARCED (COCKPIT) · airframe 59,021 hrs · 50,195 cycles

R1 COCKPIT WINDOW ARCED & CRACKED. REMOVED AND REPLACED R1 WINDOW PER MM.

Part: STRINGER — CORRODED (E & E COMPART) · airframe 59,021 hrs · 50,195 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 360, STR 26R. REPAIRED STRINGER PER SRM.

Part: LIGHT — LOOSE (MAIN CABIN) · airframe 58,976 hrs · 50,153 cycles

DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT LOOSE AT ROW 16 DEF. SECURED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF LIMITS (R1 DOOR) · airframe 58,474 hrs · 49,740 cycles

R1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATED OUT OF LIMITS. REMOVED AND REPLAECD SLIDE PER MM.

Part: WIRE — BROKEN (EXIT SIGN) · airframe 57,992 hrs · 49,348 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND AFT CABIN CENTER EMERGENCY EXIT SIGN WIRES BROKEN. REPAIRED WIRES PER SWPM & SOPM.

Part: STRINGER — CORRODED (AFT CARGO BAY) · airframe 57,259 hrs · 48,763 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON STR 24L, BS 908. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (AFT CARGO) · airframe 57,259 hrs · 48,763 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON SHEAR TIE AT BS 747, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 57,259 hrs · 48,763 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL BEAM UPPER T-CHORD CRACKED AT BS 660.5, BL 0. REPAIRED T-CHORD PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,259 hrs · 48,763 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 445, STR 24R. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 57,259 hrs · 48,763 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON STRINGER CLIP AT BS 767, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,259 hrs · 48,763 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON STR 25L, BS 767. REPAIRED STRINGER PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 57,259 hrs · 48,763 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE WEB CRACKED AT BS 1016 BULKHEAD, 1 O'CLOCK POSITION. REPAIRED WEB PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,259 hrs · 48,763 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 375, ABOVE STR 15L. REPAIRED SKIN PER SWA EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 57,259 hrs · 48,763 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 787, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (AFT CARGO) · airframe 57,259 hrs · 48,763 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO BELTFRAME CORRODED AT BS 887, LBL 1. REPAIRED BELTFRAME PER SRM.

Part: SKIN — CRACKED (R1 DOOR) · airframe 57,259 hrs · 48,763 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR SKIN CRACKED AT UPPER DOOR HINGE CUTOUT. REPAIRED SKIN PER SRM & SWA ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,259 hrs · 48,763 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 760, BELOW STR 18R. REPAIRED SKIN PER SWA EA & SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 57,259 hrs · 48,763 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BEADED WEB CRACKED AT BS 664.5, BETWEEN LBL 30.5 TO LBL 32.0. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,122 hrs · 48,648 cycles

DURING SCHEDULED C3 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS FROM BS 500D, BS 520, STRINGER 12R. REPAIRED SKIN PER EA.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 57,122 hrs · 48,648 cycles

DURING SCHEDULED C3 CHECK, FOUND R2 DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS, BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,904 hrs · 48,477 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 482, STRINGER 10R, CRACKED. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 55,383 hrs · 47,312 cycles

DURING SPV, FOUND BS 1016, BULKHEAD WEB AT STR 7R AND STR 8R, CRACKED. REPAIRED BULKHEAD WEB PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,366 hrs · 47,299 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 500, STRINGER 10L, CRACKED. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 55,366 hrs · 47,599 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,079 hrs · 47,069 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 513, STRINGER 10L, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,079 hrs · 47,069 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 316, STRINGER 18R, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,072 hrs · 47,061 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 513, STRINGER 10L, CRACKED. REPAIRED SKIN PER SRM.

Part: WEDGE — DELAMINATED (L/E SLAT) · airframe 54,522 hrs · 46,613 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING NR 4 L/E SLAT UPPER WEDGE PANEL DELAMINATED. REMOVED AND REPLACED NR 4 L/E SLAT PER MM.

Part: WEDGE — DEBONDED (T/E FLAP) · airframe 54,522 hrs · 46,613 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING INBOARD MID FLAP T/E WEDGE PANEL DISBONDED. REMOVED AND REPLACED LT WING INBOARD MID FLAP PER MM.

Part: WEDGE — DELAMINATED (L/E SLAT) · airframe 54,522 hrs · 46,613 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING NR 5 L/E SLAT UPPER WEDGE PANEL DELAMINATED. REMOVED AND REPLACED NR 5 L/E SLAT PER MM.

Part: WEDGE — DELAMINATED (L/E SLAT) · airframe 54,522 hrs · 46,613 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING NR 6 L/E SLAT UPPER WEDGE PANEL DELAMINATED. REMOVED AND REPLACED NR 6 L/E SLAT PER MM.

Part: SLIDE — UNSERVICEABLE (R2 DOOR) · airframe 53,851 hrs · 46,105 cycles

R2 DOOR EVAC SLIDE LOW PRESSURE INDICATION. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,467 hrs · 45,765 cycles

DURING SCHEDULED C3 CHECK, FOUND SKIN CRACKED BETWEEN BS 500C TO BS 500D, ABOVE STRINGER 10L. REPAIRED SKIN CRACK PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,512 hrs · 45,050 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) BS 780, STR 18L AND STR 18 R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,855 hrs · 44,510 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 4R, BS 697 AT BS 717. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,742 hrs · 43,595 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED ( 3 EA ) AT BS 500 + 4 @ STR 10R, BS 500A @ STR 10R & BS 500D + 10 BETWEEN STR 10L & STR 13L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,805 hrs · 42,867 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,805 hrs · 42,867 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 735, STR 20L. REPAIRED SKIN PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 49,235 hrs · 42,415 cycles

DURING SCHEDULED D CHECK, FOUND KEEL BEAM CORRODED AT BS 727, STR 27L. REPAIRED KEEL BEAM PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 49,235 hrs · 42,415 cycles

DURING SCHEDULED D CHECK, FOUND KEEL BEAM CORRODED FROM BS 690 TO BS 722, RBL 8. REPAIRED KEEL BEAM PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 49,235 hrs · 42,415 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500D, STR 27L. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 49,235 hrs · 42,415 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 787, WL 148 AND BL O. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,235 hrs · 42,415 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 8R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,235 hrs · 42,415 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (4 EA) BETWEEN STR 8R AND STR 9R, BS 440, BS 480, BS 747 AND BS 827. REPAIRED FRAMES PER BFG ER.

Part: FRAME — CORRODED (FUSELAGE) · airframe 49,235 hrs · 42,415 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500, STR 27L. REPAIRED FRAME PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 49,235 hrs · 42,415 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: FLOORBEAM — CRACKED (MID CABIN) · airframe 49,235 hrs · 42,415 cycles

DURING SCHEDULED D CHECK, FOUND LONGITUDINAL FLOORBEAMS CRACKED (2 EA) BETWEEN BS 706 AND BS 711, WL 202 AT RBL 25 AND LBL 25. REPAIRED FLOORBEAMS PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,235 hrs · 42,415 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (6 EA) BETWEEN STR 8L AND STR 9L, BS 480, BS 727, BS 807, BS 847, BS 867 AND BS 887. REPAIRED FRAMES PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,235 hrs · 42,415 cycles

DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 312, STR 5L. REPAIRED FRAME PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 49,235 hrs · 42,415 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 49,235 hrs · 42,415 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 747, BETWEEN STR 25R AND STR 26R. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (AFT CABIN) · airframe 49,235 hrs · 42,415 cycles

DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 986, WL 208 AND RBL 2. REPAIRED FLOORBEAM PER BFG ER.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 49,235 hrs · 42,415 cycles

DURING SCHEDULED D CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727A + 17, WL 208 AND LBL 25. REPAIRED FLOORBEAM PER BFG ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,235 hrs · 42,415 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 20R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,235 hrs · 42,415 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 19L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: FRAME — CRACKED (FWD CARGO) · airframe 49,235 hrs · 42,415 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 460, RBL 2. REPAIRED FRAME PER SRM.

Part: SKIN — BULGED (FUSELAGE) · airframe 49,235 hrs · 42,415 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN BULGED AT BS 500D TO BS 526, STR 28L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,235 hrs · 42,415 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17R. REPAIRED FRAME PER SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 49,235 hrs · 42,415 cycles

DURING SCHEDULED D CHECK, FOUND LT HORIZONTAL STABILIZER UPPER RIB CHORD CRACKED (2 EA) AT STA 166.30 AND STA 193.9. REPAIRED UPPER RIBS PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 49,235 hrs · 42,415 cycles

DURING SCHEDULED D CHECK, FOUND PRESSURE BULKHEAD CRACKED (2 EA) AT BS 1016, STR 6R AND STR 6L. REPAIRED BULKHEAD PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 49,235 hrs · 42,415 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB CRACKED BETWEEN BS 616 AND BS 639, STR 17L. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,822 hrs · 42,083 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 820, STR 20L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 47,287 hrs · 40,817 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER WHEN DOOR CLOSED. REINSTALLED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 47,287 hrs · 40,817 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,094 hrs · 40,663 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 727D AND BS 727E, STR 20L. REPAIRED SKIN PER SRM AND SWA RA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,094 hrs · 40,663 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D + 8, STR 10R. REPAIRED SKIN PER SWA RA.

Part: SLIDE — OUT OF ADJ (ENTRY DOOR) · airframe 46,533 hrs · 40,202 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 46,379 hrs · 40,073 cycles

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

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 49,552 hrs · 35,841 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM.

Part: FITTING — CORRODED (LT & RT MLG) · airframe 45,758 hrs · 39,545 cycles

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

Part: SKIN — CRACKED (FUSRLAGE) · airframe 44,961 hrs · 38,897 cycles

DURING WALKAROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT UPPER RIGHT CORNER OF AFT CARGO BIN OPENING. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,961 hrs · 38,897 cycles

DURING WALKAROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 963, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,961 hrs · 38,897 cycles

DURING WALKAROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT STR 19R, BS 767, BS 759 AND BS 727D+3. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,961 hrs · 38,897 cycles

DURING WALKAROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 722, STR 20L. REPAIRED SKIN PER SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 43,882 hrs · 37,983 cycles

FWD SECTION OUTBOARD EMERGENCY FLASHLIGHT HAS LOW BATTERY INDICATION. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,573 hrs · 37,716 cycles

DURING SCHEDULED C4 CHECK, FOUND APPROX 4 EXTERNAL FUSELAGE SKIN CRACK AT BS 500D, STR 10R. REPAIRED SKIN PER SRM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 43,428 hrs · 37,588 cycles

FORE & AFT VERTICAL FLASHLIGHTS INOP. R&R FLASHLIGHTS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,383 hrs · 37,553 cycles

RT OVERWING EMERGENCY EXIT LIGHT INOP. R&R EXIT LIGHT ASSY PER MM.

Part: BATTERY PACK — INOPERATIVE (CABIN FLOOR) · airframe 43,330 hrs · 37,508 cycles

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

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 43,289 hrs · 37,473 cycles

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

Part: BATTERY — INOPERATIVE (CABIN) · airframe 42,684 hrs · 36,968 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: STRAP — CRACKED (FWD ENTRY) · airframe 42,542 hrs · 36,838 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR LOWER HINGE CUTOUT STRAP CRACKED. REMOVED AND REPLACED STRAP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,542 hrs · 36,838 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD RT SIDE CHORD CRACKED, RBL 28. REMOVED AND REPLACED CHORD SECTION PER ACO.

Part: SHEAR TIE — CRACKED (CARGO BAY) · airframe 42,542 hrs · 36,838 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 727E SHEAR TIE CRACKED NEXT TO KEEL BEAM, RBL 9. REPAIRED SHEAR TIE PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,542 hrs · 36,838 cycles

DURING SCHEDULED 1/4D CHECK, FOUND EEPLS INOP AT MID CABIN. REMOVED AND REPLACED LAMP HOLDERS PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 42,542 hrs · 36,838 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, RBL 28. REPAIRED BULKHEAD PER SRM.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 42,478 hrs · 36,775 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP. REMOVED AND REPLACED BATTERY ASSY PER MM.

Part: SLIDE — DISLODGED (PAX DOOR)

FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER WHEN DOOR CLOSED AT SLC AND AGAIN AT LAS. REINSTALLED FWD ENTRY DOOR SLIDE ASSY AFTER THE TWO INCIDENTS PER MM.

Part: CABLE — BROKEN (ESCAPE SLIDE)

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE GIRT BAR ATTACH CABLE ASSY BROKEN. REMOVED AND REPLACED CABLE ASSY PER MM.

Part: SLIDE — DISLODGED (CABIN)

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

Part: SKIN — CRACKED (BS 867)

DURING SCHEDULED SC CHECK, FOUND A 1 INCH FUSELAGE SKIN CRACK AT BS 867, AT S18R. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 775)

DURING SCHEDULED BC4 CHECK, FOUND A 2.5 FUSELAGE SKIN CRACK AT BS 775, S23. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 986-1006)

DURING SCHEDULED 1/2D CHECK, FOUND INTERCOSTAL CORRODED BETWEEN BS 986.5 AND 1006 BL 0 AND BETWEEN BS 967 AND 986.5 LBL 17. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 615-640)

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED SHEAR TIE WEB AT BS 615 STR 15R AND BS 640 STR 15R. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 2865)

DURING SCHEDULED 1/2D CHECK, FOUND INTERCOSTAL CORRODED BETWEEN BS 286.5 AND BS 1006 LBL 36. REPAIRED PER BOEING SRM.

Part: TIE CLIP — CRACKED (BS 663)

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED TIE CLIP AT BS 663 STR 10L. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 967-986.5)

DURING SCHEDULED 1/2D CHECK, FOUND INTERCOSTAL CORRODED BETWEEN BS 967 AND 986.5 RBL 18. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 986.5-1006)

DURING SCHEDULED 1/2D CHECK, FOUND INTERCOSTAL CORRODED TOP AND BOTTOM SURFACE BETWEEN BS 986.5 AND 1006 LBL 15. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 747-772)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED FLOORBEAM AT BS 772 RBL 12, BS 774 RBL 3 AND BS 747-767 RBL 3. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 312)

DURING SCHEDULED 1/2D CHECK, FOUND UPPER FLANGE OF FLOORBEAM CORRODED AT PANEL HOLES TOP AND BOTTOM AT BS 312 LBL 15 TO RBL 22. REPAIRED PER BOEING SRM.

Part: BULKHEAD — DAMAGED (GALLEY)

DURING SCHEDULED 1/2D CHECK, FOUND FWD LAV FWD BULKHEAD COMPOSITE DAMAGED SEVERAL AREAS. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (GALLEY)

DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED ANGLE BELOW TORQUE BOX FWD I/B CORNER. REPAIRED PER BOEING SRM.

Part: BULKHEAD PANEL — CRACKED (BS 380)

DURING SCHEDULED 1/2 D-CHECK, FOUND BULKHEAD PANEL AT BS 380 RT SIDE GOUGED AND CRACKED. REPAIRED PER BOEING SRM.

Part: LIGHT — BROKEN (CABIN)

DURING SCHEDULED 1/2 D CHECK, FOUND EMERGENCY LIGHT LENSE OVER AFT ENTRY DOOR BROKEN. REMOVED AND REPLACED PER BOEING MM.

Part: FLOORBEAM — CORRODED (BS 9475)

DURING SCHEDULED 1/2 D CHECK, FOUND CORROSION IN AND AROUND SCREW HOLES AT FLOORBEAM BS 947.5 RBL 3 TO NR 3 SEAT TRACK. REPAIRED PER BOEING MM.

Part: TIE DOWN — CORRODED (BS 854)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED CARGO TIE DOWN AT BS 854 RBL 14. REMOVED AND REPLACED PER BOEING SRM.

Part: TIEDOWN — CORRODED (CARGO COMPT)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED CARGO TIE DOWN AT BS 787 RBL 14, BS 792 TO 847 RBL 21 AND BS 792 RBL 14. REMOVED AND REPLACED PER BOEING SRM.

Part: STRINGER — CORRODED (FUSELAGE)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED STRINGER 25L AT BS 850 LBL 23, BS 871, BS 864 AND STR 28L BS 503. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 294.5-312)

DURING SCHEDULED 1/2D CHECK, FOUND INTERCOSTAL CORRODED AT FLOOR PANEL HOLES LBL 11 AT BS 294.5 TO 312. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 907)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORROSION AROUND HOLE IN FLOORBEAM AT BS 907 RBL 8. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 380-400)

DURING SCHEDULED 1/2 D-CHECK, FOUND WEB UPPER ANGLE CRACKED AT BS 380 TO 400 BL 0. REPAIRED PER BOEING SRM.

Part: STRINGER — CORRODED (BS 794-847)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED STRINGER 25L BS 787 TO 791. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 837)

DURING SCHEDULED 1/2 D CHECK, FOUND CORRODED FLOORBEAM AT BS 837 STR 25L LBL 22. REMOVED AND REPLACED PER BOEING MM.

Part: TIE DOWN — CORRODED (BS 867)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED HOLE IN CARGO TIE DOWN AT BS 867 RBL 14. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 590)

DURING SCHEDULED 1/2D CHECK, FOUND INTERCOSTAL AT BS 950 POS 25-40L CORRODED AND WORN SCREW HOLES; BS 950 POS 18L-20L AND BS 947-967 POS 17L. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 294-305)

DURING SCHEDULED 1/2 D-CHECK, FOUND SUPPORT ANGLE ON STRINGER 11L CRACKED AT BS 294 TO 305. REPAIRED PER BOEING SRM.

Part: WEB — CORRODED (BS 794-847)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED SURFACE WEB FROM BS 794 TO 847 RBL 25. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 792-827)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM EXFOLIATED BETWEEN AT BS 792 TO 827. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 827-847)

DURING SCHEDULED 1/2 D CHECK, FOUND CORRODED FLOORBEAM AT BS 827-847 RBL 14. REMOVED AND REPLACED PER BOEING MM.

Part: FLOORBEAM — CORRODED (BS 844)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORROSION AROUND HOLE IN FLOORBEAM AT BS 844 RBL 8 AND AT BS 844 RBL 3. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — CORRODED (BS 847)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED WEB AFT OF DOOR CUTOUT AT BS 847 RBL 25. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 277-294.5)

DURING SCHEDULED 1/2D CHECK, FOUND INTERCOSTAL CORRODED AT FLOOR PNL HOLES AT LBL 11 BS 277 TO 294.5. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 312)

DURING SCHEDULED 1/2D CHECK, FOUND LWR FLOOR BEAM FLANGE INTERCOSTAL CRACKED, LBL 12 AT BS 312 ON INBD AND O/B EDGES, AND LBL 12 AT BS 328 O/B EDGE. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (NR 1 LE SLAT)

DURING SCHEDULED C2 CHECK, FOUND CRACKED BOTTOM SKIN OF NR 1 SLAT IN ACTUATOR AREA. REPAIRED PER BOEING NR T1-A57-015.

Part: FIRE LOOP — FAILED (NR 2 ENGINE)

DURING WALKAROUND CHECK, FOUND NR 2 ENG FIRE LOOP WILL NOT TEST. REMOVED AND REPLACED NR 2 ENG FIRE LOOP UNIT PER BOEING MM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND R-2 EXTERIOR EMERGENCY LIGHT AND L-2 INTERIOR EMERGENCY LIGHT INOP. REPLACED BATTERY PACK PER BOEING MM.

Part: WEB — CRACKED (BS 727)

DURING SCHEDULED 1/2 D-CHECK, FOUND RT 18 A WEB AT BS 727 HAS CRACK AT I/B FASTENER HOLE. REPAIRED PER SWA RA 1-353-1767.

Part: FLOORBEAM — CORRODED (BS 772)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORRODED AT BS 772, RBL 14. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 857)

DURING SCHEDULED D-CHECK, FOUND CORROSION IN AND AROUND FLOORBEAM HOLE AT BS 857, RBL 14. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — EXFOLIATED (BS 792/872)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM IS EXFOLIATED BETWEEN BS 792 AND 872. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 862)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORRODED AT BS 862, RBL 14. REMOVED AND REPLACED PER BOEING SRM.

Part: SLIDE — DEPLOYED (R1 DOOR)

AT GATE, FWD SERVICE DOOR SLIDE ACCIDENTALLY DEPLOYED. REMOVED AND REPLACED SLIDE ASSEMBLY PER BOEING M/M.

Part: SKIN — CRACKED (BS 727B)

DURING SCHEDULED TERMINAL CHECK, FOUND A 1.75 INCH CRACK IN FUSELAGE SKIN AT BS 727B AT S16L. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (R2 DOORWAY)

DURING SCHEDULED CHECK, FOUND FUSELAGE SKIN DENTED ABOVE AND SLIGHTLY AFT OF R2 DOOR CUTOUT. REPAIRED PER SWA RA 1-353-1576.

Part: ENGINE — BIRD STRIKE (NR 1)

EXPERIENCED BIRD STRIKE TO NUMBER 1 ENGINE AFTER TAKEOFF, ACCOMPANIED BY EGT RISE AND ODOR IN CABIN. AIRCRAFT RETURNED TO OAK AND HAD AN UNEVENTFUL LANDING. PERFORMED BIRD STRIKE INSPECTION PER BOEING M/M, NO DEFECTS NOTED. ENGINE PLACED ON 10 CYCLE BORESCOPE INSPECTION.

Part: LINE — RUPTURED (NLG WW)

AFTER TAKEOFF, NOSE GEAR WOULD NOT RETRACT. RECYCLED GEAR, NO HELP. RETURNED TO BHM AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND HYDRAULIC FLUID AROUND SWIVEL. REMOVED AND REPLACED RETRACT LINE TO LOCK ACTUATOR, RESERVICED SYSTEM, AND RETRACTION TESTED NOSE GEAR PER BOEING M/M.

Part: HYD HOSE — LEAKING (NLG ACTUATOR)

AFTER TAKEOFF, NOSE GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO BHM AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND NOSE GEAR MAIN ACTUATOR HYD HOSE LEAKING. REPLACED PER BOEING M/M.

Part: BELT FRAME — CRACKED (BS 807)

DURING SCHEDULED 1/4 D-CHECK, FOUND BELT FRAME CRACKED AT BS 807 BL 0. REPAIRED PER BOEING SRM.

Part: POST — CRACKED (COCKPIT)

DURING SCHEDULED CHECK, FOUND CAPTAIN'S NUMBER 1 WINDOW POST CRACKED .156 INCH. REPAIRED PER SWA RA 1-A53-1156.

Part: POST — CRACKED (LT COCKPIT)

DURING SCHEDULED B/C CHECK, FOUND CAPTAIN'S NUMBER 1 WINDOW POST CRACKED .156 INCH. REPAIRED PER RA 1-A53-1156.