N302SW

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM CORRODED AT BS 767 STR 27R. REPAIRED BEAM PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,811 hrs · 72,930 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 76,811 hrs · 72,930 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 20L. REPAIRED FRAME PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 5 DEF. RELAMPED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 6 ABC. RELAMPED LIGHT PER MM.

Part: HINGE FITTING — CRACKED (L2 DOOR) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND L2 DOOR LOWER HINGE FITTING CRACKED. REMOVED AND REPLACED FITTING PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, BETWEEN STR 23L TO STR 22L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500, BETWEEN STR 27R TO STR 28R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 500 BETWEEN STR 27R TO STR 28R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — BROKEN (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP BROKEN AT BS 727E, STR 18R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 986, STR 20L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 440, BETWEEN STR 26L TO 27L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 24R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM CORRODED BETWEEN BS 727 TO BS 727A, STR 27R. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 20R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 23R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 22L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500B, STR 20L. REPAIRED FRAME PER SRM.

Part: LENS — BROKEN (CABIN) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 986, STR 20L. REPAIRED STRINGER PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 460, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 500C, BETWEEN STR 26L TO STR 28L. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM CORRODED AT BS 927 STR 27L. REPAIRED BEAM PER SWA EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 788, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 540, STR 21L. REPAIRED STRINGER PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 24L. REPAIRED STRINGER PER SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND LOWER CHORD CORRODED AT BS 219 LBL 6 TO WL 156. REPAIRED CHORD PER PAE ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, BETWEEN STR 23L TO STR 22L. REPAIRED FRAME PER SRM.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND RIGHT WING I/B MID FLAP T/E WEDGE O/B END DELAMINATED. REMOVED AND REPLACED WEDGE PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 857, STR 27R, RBL 8. REMOVED AND REPLACED BEAM PER DHN EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 857, STR 27R, RBL 3. REPAIRED BEAM PER DHN EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 867, STR 20R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 927, STR 23R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 22L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 24R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 19L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 727C, STR 21R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 747, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 907, STR 22R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 727C, STR 22R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 907, BETWEEN STR 27L TO 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,811 hrs · 72,930 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 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 19L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 18L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 907, STR 24R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 18L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 927, BETWEEN STR 27L TO 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 18L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500B, STR 20L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 20R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 76,811 hrs · 72,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND FWD CARGO FRAME CORRODED AT BS 440, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED FRAME PER SRM.

Part: SKIN — CRACKED (BS 912 S10L) · airframe 75,788 hrs · 72,214 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 912, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 75,788 hrs · 72,214 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,081 hrs · 71,682 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,081 hrs · 71,682 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 75,081 hrs · 71,682 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 75,011 hrs · 71,627 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 74,822 hrs · 71,481 cycles

R2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 73,945 hrs · 70,814 cycles

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

Part: LENS — MISSING (CABIN) · airframe 73,484 hrs · 70,448 cycles

BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 23 ABC. INSTALLED LENS PER MM.

Part: ACTUATOR — FAULTY (MLG) · airframe 73,338 hrs · 70,324 cycles

AIR TURNBACK. CLIMBING OUT OF TUS WITH LANDING GEAR HANDLE IN UP POSITION NLG UNSAFE LIGHT ILLUMINATED. CYCLED GEAR SEVERAL TIMES THEN GOT THREE GREEN LIGHTS. REMOVED AND REPLACED NLG RETRACT ACTUATOR AND FUSE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 402, STR 5L. REPAIRED SKIN PER ER.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 26R CORRODED AT BS 867. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, BETWEEN RBL 3 AND LBL 3. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 1016, STR 20L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 555, STR 10R. REPAIRED SKIN PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 23L. REPAIRED STRINGER SPLICE PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 73,280 hrs · 70,280 cycles

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

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 24R CORRODED AT BS 357. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 420, STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727, STR 23L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,280 hrs · 70,280 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 380, STR 13R. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8R. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 582, STR 10L. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,280 hrs · 70,280 cycles

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

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 26R CORRODED AT BS 360. REMOVED AND REPLACED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,280 hrs · 70,280 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 22L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SHEAR TIE — CRACKED (BS 847 S13R) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 847, STR 13R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (BS 1006-1016) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 26R CORRODED BETWEEN BS 1006 AND BS 1016. REPAIRED STRINGER PER SRM.

Part: STRINGER — CRACKED (BS 380 S15R) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 15R CRACKED AT BS 380. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (BS 380 S8R) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 706 S4L) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727D S4L) · airframe 73,280 hrs · 70,280 cycles

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

Part: STRINGER CLIP — CRACKED (BS 767 S10L) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 747 S6L) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 867 S4L) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 400 S8R) · airframe 73,280 hrs · 70,280 cycles

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

Part: FRAME — CRACKED (BS 440 S8R) · airframe 73,280 hrs · 70,280 cycles

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

Part: STRINGER CLIP — CRACKED (BS 787 S4L) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED RON, FOUND FUSELAGE STR CLIP CRACKED AT BS 727A, STR 5L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED RON, FOUND FUSELAGE STR CLIP CRACKED AT BS 727B, STR 6L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED RON, FOUND FUSELAGE STR CLIP CRACKED AT BS 500C, STR 7R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED RON, FOUND FUSELAGE STR CLIP CRACKED AT BS 500, STR 7L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED RON, FOUND FUSELAGE STR CLIP CRACKED AT BS 727A, STR 7L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED RON, FOUND FUSELAGE STR CLIP CRACKED AT BS 500D, STR 8R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED RON, FOUND FUSELAGE STR CLIP CRACKED AT BS 727C, STR 5L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED RON, FOUND FUSELAGE STR CLIP CRACKED AT BS 727A, STR 10L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED RON, FOUND FUSELAGE STR CLIP CRACKED AT BS 727C, STR 4L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED RON, FOUND FUSELAGE STR CLIP CRACKED AT BS 727A, STR 6L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED RON, FOUND FUSELAGE STR CLIP CRACKED AT BS 727E, STR 9R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED RON, FOUND FUSELAGE STR CLIP CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED RON, FOUND FUSELAGE STR CLIP CRACKED AT BS 520, STR 7R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED RON, FOUND FUSELAGE STR CLIP CRACKED AT BS 727A, STR 3L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED RON, FOUND FUSELAGE STR CLIP CRACKED AT BS 727A, STR 9L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 685 S2L) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500D S5R) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 597 S8R) · airframe 73,280 hrs · 70,280 cycles

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

Part: STRINGER CLIP — CRACKED (BS 616 S3R) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 706 S2L) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 685 S3L) · airframe 73,280 hrs · 70,280 cycles

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

Part: STRINGER CLIP — CRACKED (BS 597 S7R) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 706 S3L) · airframe 73,280 hrs · 70,280 cycles

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

Part: STRINGER CLIP — CRACKED (BS 639 S3L) · airframe 73,280 hrs · 70,280 cycles

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

Part: STRINGER — DAMAGED (BS 500B-510A) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE STRINGER 9R DAMAGED BETWEEN BS 500B TO BS 510A. REPAIRED STR PER SRM.

Part: STRINGER — DAMAGED (BS 360-460) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE STRINGER 9L DAMAGED BETWEEN BS 360 TO BS 460. REPAIRED STR PER SRM.

Part: FRAME — CRACKED (BS 360 S8L) · airframe 73,280 hrs · 70,280 cycles

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

Part: FRAME — CRACKED (BS 520 S8R) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 727E S7R) · airframe 73,280 hrs · 70,280 cycles

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

Part: STRINGER CLIP — CRACKED (BS 706 S3R) · airframe 73,280 hrs · 70,280 cycles

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

Part: FRAME — CRACKED (BS 480 S8R) · airframe 73,280 hrs · 70,280 cycles

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

Part: FRAME — CRACKED (BS 500A S8R) · airframe 73,280 hrs · 70,280 cycles

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

Part: STRINGER CLIP — CRACKED (BS 706 S10R) · airframe 73,280 hrs · 70,280 cycles

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

Part: STRINGER CLIP — CRACKED (BS 706 S2R) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 440 S8L) · airframe 73,280 hrs · 70,280 cycles

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

Part: STRINGER CLIP — CRACKED (BS 385 S2R) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 639 S3R) · airframe 73,280 hrs · 70,280 cycles

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

Part: STRINGER CLIP — CRACKED (BS 685 S3R) · airframe 73,280 hrs · 70,280 cycles

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

Part: STRINGER CLIP — CRACKED (BS 747 S5R) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 767 S8R) · airframe 73,280 hrs · 70,280 cycles

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

Part: STRINGER CLIP — CRACKED (BS 727B S9R) · airframe 73,280 hrs · 70,280 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 767 S8L) · airframe 73,280 hrs · 70,280 cycles

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

Part: FRAME — CRACKED (BS 727E S8L) · airframe 73,280 hrs · 70,280 cycles

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

Part: TORQUE TUBE — WORN (RT WING TE FLAP) · airframe 73,267 hrs · 70,272 cycles

DURING SCHEDULED HC2 CHECK, FOUND RIGHT WING 90 DEGREE TORQUE TUBE WORN AT NR 6 TRANSMISSION. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: SKIN — CRACKED (BS 271) · airframe 73,267 hrs · 70,272 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 271, STR 15L. REPAIRED SKIN PER SWA EA.

Part: TORQUE TUBE — WORN (LT WING TE FLAP) · airframe 73,267 hrs · 70,272 cycles

DURING SCHEDULED HC2 CHECK, FOUND LEFT WING OUTBOARD T/E FLAP TORQUE TUBE WORN OUTBOARD OF 120 DEGREE GEARBOX. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 73,255 hrs · 70,265 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (BS 800 S19L) · airframe 73,002 hrs · 70,062 cycles

DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 800, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 782 S20L) · airframe 73,002 hrs · 70,062 cycles

DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 782, STR 20L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,824 hrs · 69,932 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 384, STR 15L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,824 hrs · 69,932 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 924, STR 23R. REPAIRED SKIN PER SWA EA.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 72,613 hrs · 69,770 cycles

EEPLS PHOTOLUMINESCENT STRIP MISSING AT ROW 5 DEF. INSTALLED STRIP PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 72,571 hrs · 69,742 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 72,571 hrs · 69,742 cycles

DURING SCHEDULED HC1 CHECK, FOUND RIGHT WING INBOARD FORE FLAP UPPER AFT SURFACE DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 72,571 hrs · 69,742 cycles

DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: HYDRAULIC LINE — LEAKING (RT MLG) · airframe 72,123 hrs · 69,399 cycles

ON SHORT FINAL -A- SYSTEM HYDRAULIC FLUID LOSS AND SYSTEM FAILURE. FOUND HYDRAULIC LINE LEAKING AT RT MLG RETRACT ACTUATOR. REMOVED AND REPLACED HYDRAULIC LINE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,846 hrs · 69,184 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 909, STR 3L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,846 hrs · 69,184 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 924, STR 4R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,846 hrs · 69,184 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 851, STR 18L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,846 hrs · 69,184 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 494, STR 17L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,846 hrs · 69,184 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 804, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,846 hrs · 69,184 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 972, STR 23L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,846 hrs · 69,184 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 765, STR 19L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 582 S10L) · airframe 71,266 hrs · 68,762 cycles

DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 582, STR 10L. REPAIRED PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 573 S10R) · airframe 71,266 hrs · 68,762 cycles

DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 573, STR 10R. REPAIRED PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 370 S14R) · airframe 71,266 hrs · 68,762 cycles

DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 370, STR 14R. REPAIRED PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 917 S22R) · airframe 71,266 hrs · 68,762 cycles

DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 917, STR 22R. REPAIRED PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 787 S18L) · airframe 71,266 hrs · 68,762 cycles

DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 18L. REPAIRED PER SWA EA & SRM.

Part: ACTUATOR — FAULTY (NLG) · airframe 71,095 hrs · 68,619 cycles

LANDING HANDLE MOVED TO OFF POSITION, NLG DROPPED. CYCLED GEAR HANDLE ALL INDICATIONS NORMAL, MOVED HANDLE TO OFF POSITION. REMOVED AND REPLACED M983 LOGIC CARD AND NLG RETRACT ACTUATOR PER MM.

Part: SKIN — CORRODED (BS 523-538) · airframe 70,822 hrs · 68,395 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CORRODED FROM BS 523 TO BS 538, RBL 7. REPAIRED SKIN PER ER.

Part: SKIN — CORRODED (BS 533 S28R) · airframe 70,822 hrs · 68,395 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 533, STR 28R. REPAIRED SKIN PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 70,822 hrs · 68,395 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 275, STR 22R. REPAIRED SKIN PER ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 70,822 hrs · 68,395 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 285, STR 24R. REPAIRED SKIN PER ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 70,822 hrs · 68,395 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 326, STR 28R. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,822 hrs · 68,395 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 360, STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 70,822 hrs · 68,395 cycles

DURING SCHEDULED 22Y CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 5 DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 70,822 hrs · 68,395 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER 28R CORRODED AT BS 320. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 70,822 hrs · 68,395 cycles

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

Part: FITTING — CORRODED (L1 DOOR) · airframe 70,822 hrs · 68,395 cycles

DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED GIRT BAR FITTING PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 70,822 hrs · 68,395 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 328, BL 0 TO RBL 42. REPAIRED FLOORBEAM CHORD PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,822 hrs · 68,395 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 986, STR 2L. REPAIRED FRAME SECTION PER SRM.

Part: SHEAR TIE — CRACKED (BS 294 S12L) · airframe 70,822 hrs · 68,395 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CRACKED AT BS 294, STR 12L. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: GIRT BAR — LOOSE (R1 DOOR) · airframe 70,822 hrs · 68,395 cycles

DURING SCHEDULED 22Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED DOOR HOOK PER SRM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 70,822 hrs · 68,395 cycles

DURING SCHEDULED 22Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,607 hrs · 68,217 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 832, STR 20L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 70,457 hrs · 68,086 cycles

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

Part: ACTUATOR — FAULTY (NLG) · airframe 70,244 hrs · 67,897 cycles

NOSE GEAR WOULD NOT LOCK IN THE UP POSITION. CYCLED GEAR HANDLE OFF/UP GEAR LOCKED. REMOVED AND REPLACED NLG RETRACT ACTUATOR PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 70,531 hrs · 67,748 cycles

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

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 68,983 hrs · 66,971 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,056 hrs · 66,233 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 910, STR 4L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,056 hrs · 66,233 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 12R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (BS 941) · airframe 67,563 hrs · 65,830 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 941, STR 4R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 67,255 hrs · 65,589 cycles

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

Part: ROD — WORN (RT AILERON) · airframe 67,196 hrs · 65,530 cycles

DURING SCHEDULED C2 CHECK, RT WING AILERON FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED RT AILERON CONTROL ROD PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,196 hrs · 65,530 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 912, STR 4R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,944 hrs · 65,357 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727C + 8, STR 14R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,944 hrs · 65,357 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500A + 17, STR 8R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,944 hrs · 65,357 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT BS 500D + 18, STR 7R & STR 8R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,527 hrs · 65,030 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 26R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,527 hrs · 65,030 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 16R. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,527 hrs · 65,030 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 440 TO BS 446, STR 16R. REPAIRED SKIN PER SRM.

Part: ACCESS PANEL — CRACKED (NLG WW) · airframe 66,527 hrs · 65,030 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 4 EA CRACKS BELOW NLG W/W FWD ACCESS PANELS, LT & RT SIDE, BS 236 TO BS 243 + 1. REPAIRED WEB PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,939 hrs · 63,763 cycles

DURING WALKAROUND INSPECTION FOUND FUSELAGE SKIN CRACKED AT BS 727D+6, STR 14R. REPAIRED SKIN PER SWA EA.

Part: CABLE — MISROUTED (L2 DOOR SLIDE) · airframe 64,833 hrs · 63,673 cycles

DURING SCHEDULED A2 CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED L2 DOOR CABLE PER MM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 64,332 hrs · 63,264 cycles

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

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 64,294 hrs · 63,224 cycles

BULLNOSE EMERGENCY EXIT LIGHT COVER AT ROW 4ABC, BROKEN. REMOVED AND REPLACED LIGHT COVER PER MM.

Part: HINGE BRACKET — CRACKED (ELEVATOR TAB) · airframe 63,404 hrs · 62,496 cycles

DURING SCHEDULED THRU CHECK, FOUND RT AND LT ELEVATOR TAB CONTROL ROD HINGE ATTACH EAR CRACKED. REMOVED AND REPLACED RT AND LT ELEVATOR TABS PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,631 hrs · 61,821 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT EMERGENCY EXIT LIGHT INOP. RELAMPED AFT EMERGENCY EXIT LIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 52 TO RBL 52, WL 208. REPAIRED FLOORBEAM SECTION PER SRM.

Part: SUPPORT BEAM — CORRODED (RT MLG) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D CHECK, FOUND RT MLG SUPPORT BEAM CORRODED ON LOWER SURFACE. REPAIRED BEAM PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 887, STRINGER 21R. REPAIRED FRAME SECTION PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D CHECK, FOUND CORROSION ON STRINGER 27L, BS 380 TO BS 391 AND BS 400B + 15 TO BS 495. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 480, BS 787, 907, STRINGER 9L ALSO AT BS 867, STRINGER 9R. REPAIRED FRAMES PER ER.

Part: ATTACH FITTING — CORRODED (VERTICAL STAB) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D CHECK, FOUND VERTICAL STAB AFT SPAR PRIMARY LUG AND AFT FACE CHAMFER CORRODED. REPAIRED VERTICAL STAB LUG PER ER.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 360 TO BS 380, LBL 65, WL 208. REPAIRED WEB PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D CHECK, FOUND PRESSURE BULKHEAD CRACKED AT BS 1016, LAP SPLICE 3 AND LAP SPLICE 4. REPAIRED BULKHEAD PER ER.

Part: BOLT — CORRODED (LT MLG) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D CHECK, FOUND LT MLG SIDE STRUT TO UNIVERSAL ATTACHMENT BOLT CORRODED. REMOVED AND REPLACED BOLT PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 708, LBL 25, WL 203, BS 947, LBL 52, WL 208. REPAIRED WEB PER ER.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D CHECK, FOUND FLOOR ZEE CHANNEL CORRODED AT BS 270, FROM LBL 10 TO RBL 10, WL 208. REMOVED AND REPLACED CHORD SECTION PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOORBEAMS UPPER CHORD CRACKED AT BS 664, BL 0, WL 208, BS 727A, RBL 45.5, WL 208. REPAIRED CHORDS PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 706, STRINGER 11R, BS 616, STRINGER 7L. REPAIRED FRAMES SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STRINGER 16L. REPAIRED FRAME PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 360, STRINGER 10L, BS 277, WL 25, RBL 60 AND BS 727C, STRINGER 8L. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D CHECK, FOUND DOUBLER CORRODED AT BS 442, BETWEEN STRINGERS 27R AND 28R. REPAIRED DOUBLER PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN STRINGERS 26L AND 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT THE FOLLOWING LOCATIONS BS 460, STRINGER 14L AND BS 887, STRINGER 9L. REPAIRED FRAMES PER ER.

Part: CLIP — CRACKED (FUSELAGE) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 727B, STRINGERS 5R, 2R. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 727C, STRINGERS 5L, 6L, 7L, 8L. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 727A, STRINGERS 8L, 6L, 4L, 2L. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: SKIN — BULGED (FUSELAGE) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN BULGED AT BS 795, BETWEEN STRINGER 26R AND STRINGER 27R. REPAIRED SKIN PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 727D, STRINGERS 7R, 3R. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 460, STRINGER 14L, BS 595, STRINGER 7L, BS 597, STRINGER 8L, BS 706, STRINGER 11L, BS 616, STRINGER 2L. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT THE FOLLOWING LOCATIONS STRINGER 9R, BS 837, BS 807, BS 787, BS 907. REPAIRED FRAMES PER ER.

Part: CLIP — CRACKED (FUSELAGE) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 727E, STRINGERS 7L, 5L, 4L. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 747, STRINGERS 10R, 5R. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 727A, STRINGERS 7R, 6R, 4R, 2R. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 727B, STRINGERS 9L, 8L, 5L, 2L. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 727C, STRINGERS 8R, 7R, 6R, 3R. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 878, STRINGER 10R, BS727E, STRINGER 5R, BS 578, STRINGER 8R. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 727D, STRINGERS 8L, 7L, 6L. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 259, LBL 11 AND RBL 11, WL 208. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 492, STRINGER 24R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN STRINGER 28 L AND STRINGER 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 500, BETWEEN STRINGERS 28L TO 28R. REPAIRED FRAME SECTION PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D-CHECK, FOUND BS 500 + 17, STRINGER 28L AND BS 493, STRINGER 28R, CORRODED. REPAIRED STRINGERS PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D CHECK, FOUND KEEL BEAM CORRODED AT THE AFT CARGO COMPARTMENT BS 745, LBL 8, WL 148. REPAIRED KEEL BEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,494 hrs · 61,744 cycles

DURING SCHEDULED D CHECK, FOUND AFT CARGO COMPT SHEAR TIE CORRODED AT BS 727C, RBL 6, WL148. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (RT WING) · airframe 62,472 hrs · 61,729 cycles

DURING SCHEDULED C1 CHECK, FOUND RT WING FIXED L/E SKIN CRACKED AT WING STATION 213. REPAIRED WING SKIN CRACK PER EA.

Part: SIGN — LOOSE (EMERGENCY EXIT) · airframe 65,472 hrs · 61,729 cycles

DURING SCHEDULED C1 CHECK, FOUND CEILING OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED OVERWING EMERGENCY EXIT SIGN PER MM.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 62,472 hrs · 61,729 cycles

DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT LIGHT AT ROW 7 INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,472 hrs · 61,729 cycles

DURING SCHEDULED C1 CHECK, FOUND 4 EACH SKIN CRACKS AT BS 480, STRINGER 16R, BS 270, STRINGER 9C, BS 500D, STRINGER 15L AND BS 578, STRINGER 10R. REPAIRED SKIN CRACKS PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,368 hrs · 61,641 cycles

DURING PREFLIGHT CK, FOUND FUSELAGE SKIN CRACKED AT BS 804, STR 20L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,494 hrs · 60,942 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) STR 8R, BS 500 AND BS 500D. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 60,616 hrs · 60,203 cycles

DURING SCHEDULED C3 CHECK, FOUND BS 1016 BULKHEAD CRACKED AT STR 5L. REPAIRED BULKHEAD PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,616 hrs · 60,203 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 1016, BETWEEN STR 3R AND 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,262 hrs · 59,925 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 970, STR 21R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,262 hrs · 59,925 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D + 3, ABOVE STR 16R. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,693 hrs · 59,491 cycles

DURING SCHEDULED C2 CHECK, FOUND BOTH SEVERAL LAMPS INOP AT AFT CABIN DOOR EMERGENCY EXIT LIGHTS. RELAMPED BOTH EXIT LIGHTS PER MM.

Part: CABLE — MISROUTED (AFT ENTRY DOOR) · airframe 59,693 hrs · 59,491 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: SLIDE — OUT OF ADJUST (FWD CABIN DOORS) · airframe 59,633 hrs · 59,491 cycles

DURING SCHEDULED C2 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED SLIDES PER MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 59,693 hrs · 59,491 cycles

DURING SCHEDULED C2 CHECK, FOUND NR 2 L/E SLAT DELAMINATED AT OTBD END. REMOVED AND REPLACED NR 2 L/E SLAT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,693 hrs · 59,491 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR VERTICAL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,370 hrs · 59,220 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT FWD LOWER CORNER OF FWD SVC DOOR. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,370 hrs · 59,220 cycles

DURING SCHEDULED SPECIAL VIST, FOUND A 1.25 LONG FUSELAGE SKIN CRACK, BS 767+7, ABOVE STR 20L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,370 hrs · 59,220 cycles

DURING SCHEDULED SPECIAL VIST, FOUND A 7.0 LONG FUSELAGE SKIN CRACK, BS 727E+12, ABOVE STR 5R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (AFT CARGO DOOR) · airframe 58,822 hrs · 58,767 cycles

DURING SCHEDULED PM CHECK, FOUND AFT CARGO DOOR SKIN CRACKED AT LOWER FWD CORNER. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (AFT SVC DOOR) · airframe 58,809 hrs · 58,780 cycles

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

Part: SLIDE — OUT OF ADJUST (BOTH ENTRY DOOR) · airframe 58,809 hrs · 58,780 cycles

DURING SCHEDULED C1 CHECK, FOUND BOTH CABIN ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED SLIDES PER MM.

Part: SKIN — DELAMINATED (AILERON TAB) · airframe 58,747 hrs · 58,726 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT AILERON TAB DELAMINATED AT INBD UPPER SURFACE. REMOVED AND REPLACED RT AILERON TAB PER MM.

Part: SLIDE — OUT OF POSITION (CABIN DOOR) · airframe 58,530 hrs · 58,539 cycles

BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDES PRESS IND OUT OF VIEW. REPOSITIONED SLIDES PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,900 hrs · 58,040 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500A, ABOVE STR 26R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,900 hrs · 58,040 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT GROUND AIR CONDITIONING DOOR CUTOUT AT FWD CORNER. REPAIRED SKIN PER SRM.

Part: SLAT — CRACKED (LT WING) · airframe 57,900 hrs · 58,040 cycles

DURING SCHEDULED C4 CHECK, FOUND NR 3 L/E SLAT CRACKED IN AFT ROW OF RIVETS. REMOVED AND REPLACED NR 3 L/E SLAT PER MM.

Part: LENS — LOOSE (CABIN) · airframe 57,900 hrs · 58,040 cycles

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

Part: FITTING — LOOSE (ENTRY DOORS) · airframe 57,900 hrs · 58,040 cycles

DURING SCHEDULED C4 CHECK, FOUND BOTH CABIN ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTINGS LOOSE. SECURED FITTINGS PER MM.

Part: TRACK — CRACKED (CABIN) · airframe 57,900 hrs · 58,040 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS PHOTO LUMINESCENT TRACK STRIP CRACKED FROM ROW NR 7 TO OVERWING EXIT. REMOVED AND REPLACED STRIP PER MM.

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 57,845 hrs · 58,003 cycles

ON WALK AROUND INSPECTION, FOUND RT WING OTBD T/E FLAP DELAMINATED ON LOWER SIDE. REMOVED AND REPLACED RT OTBD T/E FLAP PER MM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 57,660 hrs · 57,827 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,544 hrs · 57,729 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACK AT BS 500B PLUS 14, ABOVE STR 15L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,443 hrs · 57,641 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 940, STR 23R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,690 hrs · 57,047 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 727D + 4, BELOW STR 19R AND BS 910, STR 22R. REPAIRED SKIN PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 55,824 hrs · 56,355 cycles

EEPLS LOOSE AT ROW NR 8. SECURED EEPLS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,333 hrs · 55,946 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 20R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,306 hrs · 55,922 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 912, STR 21L. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CRACKED (FWD CABIN) · airframe 55,306 hrs · 55,922 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FRAME SHEAR TIE CRACKED AT BS 360, ABOVE STR 14L. REPAIRED SHEAR TIE PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 55,306 hrs · 55,922 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REPAIRED STR SPLICE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,306 hrs · 55,922 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR UPPER AFT CUT OUT. REPAIRED SKIN PER SRM.

Part: TIE CLIP — CRACKED (FWD CABIN) · airframe 55,306 hrs · 55,922 cycles

DURING SCHEDULED 1/4D CHECK, FOUND TIE CLIP CRACKED AT BS 420, STR 14R. R&R TIE CLIP PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 55,306 hrs · 55,922 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4R. REPAIRED STR SPLICE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,306 hrs · 55,922 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 20R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,306 hrs · 55,922 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED ( 2 EA ) AT BS 328, STR 21R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (AFT CABIN) · airframe 55,306 hrs · 55,922 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 3L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,306 hrs · 55,922 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FRAME CRACKED AT BS 360, BELOW STR 14R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,306 hrs · 55,922 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 15L. R&R SHEAR TIE PER SRM.

Part: BELTFRAME — CORRODED (FUSELAGE) · airframe 55,306 hrs · 55,922 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BELT FRAME CORRODED AT BS 787, BL 0. REPAIRED BELT FRAME PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 55,306 hrs · 55,922 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STR SPLICE CRACKED AT BS 908, STR 4L. R&R STR SPLICE PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 55,306 hrs · 55,922 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SEVERAL TIE CLIPS CRACKED AT BS 616. R&R TIE CLIPS PER SRM.

Part: ANGLE — CRACKED (VERT STAB) · airframe 55,306 hrs · 55,922 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL STAB AFT RH ATTACH FITTING FWD DRAG ANGLE CRACKED. REPAIRED DRAG ANGLE PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 55,306 hrs · 55,922 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STR 4L SPLICE CRACKED AT BS 908. R&R SPLICE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,306 hrs · 55,922 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FRAME CRACKED AT BS 360, ABOVE STR 14R. REPAIRED FRAME PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 55,306 hrs · 55,922 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4R. R&R STR SPLICE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,907 hrs · 55,599 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED ( 2 EA ) AT STR 10R, BS 500, BS 524. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,907 hrs · 55,599 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED ( 6 EA ) AT STR 10L, BS 374 - 500 D. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,033 hrs · 54,835 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 500C & 500D AT STR 15L. REPAIRED SKIN PER SRM.

Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 53,754 hrs · 54,585 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. R&R EMERGENCY EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,482 hrs · 54,354 cycles

DURING SCHEDULED C3 CHECK, FOUND 1.5 EXTERNAL FUSELAGE SKIN CRACK AT BS 460, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,482 hrs · 54,354 cycles

DURING SCHEDULED C3 CHECK, FOUND 3 EXTERNAL FUSELAGE SKIN CRACKS AT BS 500A, STR 10R, 2 LONG, BS 480, STR 10L, 3 LONG & BS 380, STR 10L, 1.75 LONG. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,482 hrs · 54,354 cycles

DURING SCHEDULED C3 CHECK, FOUND 3.25 INCH LONG EXTERNAL FUSELAGE SKIN CRACK AT BS 727D, STR 19R. REPAIRED SKIN PER SRM.

Part: COVER — LOOSE (CABIN) · airframe 53,482 hrs · 45,354 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK COVER LOOSE AT AFT GALLEY. SECURED TRACK COVER PER MM.

Part: LENS — LOOSE (CABIN) · airframe 52,498 hrs · 53,543 cycles

DURING SCHEDULED C2 CHECK, FOUND EMERGENCY LIGHT LENS LOOSE AT BULLNOSE, ROW 9D. SECURED PROX LIGHT LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,470 hrs · 53,512 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACKS AT STR 10R BS 472, BS 482, BS 492 & BS 500C. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,289 hrs · 53,363 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT FUSELAGE SKIN CRACK AT BS 520, STR 12R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,220 hrs · 53,305 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT SIDE EXTERNAL FUSELAGE SKIN CRACK BETWEEN BS 500D AND 520, STR 10L. REPAIRED SKIN PER SRM.

Part: HANDLE — LACK OF LUBE (COCKPIT) · airframe 51,794 hrs · 52,931 cycles

ABORTED TAKEOFF, T/O WARNING HORN SOUNDED ON ROLLOUT WITH ALL SYSTEMS SET IN PROPER POSITION. FOUND SPEED BRAKE HANDLE STIFF, LUBRICATED SPEED BRAKE HANDLE AND SLIDER ASSY PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,605 hrs · 52,760 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD CRACKED WL 207, RBL 27 AND WL 207, LBL 12 - LBL 12.5. REPAIRED BULKHEAD PER SRM.

Part: BEAM — CORRODED (FUSELAGE) · airframe 50,707 hrs · 51,967 cycles

DURING SCHEDULED C4 CHECK, FOUND KEEL BEAM CORRODED, BS 500, BS 520, BS 740, AND BS 810. REPAIRED KEEL BEAM PER SWA RA''S 1-353-2295 AND 1-353-2297.

Part: CONNECTOR — OUT OF POSITION (COCKPIT) · airframe 50,248 hrs · 51,571 cycles

ABORTED TAKE-OFF --- TAKE-OFF WARNING HORN SOUNDED DURING TAKE-OFF. REPOSITIONED SPEED BRAKE SWITCH CONNECTOR PER MM.

Part: NUT — BROKEN (NR 2 ENGINE)

DURING TAKEOFF, NR 2 ENG STARTED SURGING, AT ABOUT 3000 - 4000 FEET NR 2 FUEL TANK PUMP LIGHTS ILLUMINATED. FOUND COUPLING NUT BETWEEN NR 2 ENG SHUTOFF VALVE AND WING SPAR FEED THROUGH BROKEN. REMOVED AND REPLACED FUEL LINE AND COUPLING NUT PER MM.

Part: SWITCH — CONTAMINATED (LE FLAP)

ABORTED TAKEOFF, L/E FLAP/SLAT TRANSIT LIGHTS ILLUMINATED AND TAKEOFF WARNING HORN SOUNDED UPON THROTTLE ADVANCEMENT. CLEANED KRUEGER FLAP POSITION INDICATOR SWITCHES. OPS CK GOOD PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR)

AFT SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: SCREW — LOOSE (SRVC DOOR SLIDE)

DURING SCHEDULED C1 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE FWD HOOK LOOSE. TIGHTENED LOOSE SCREW PER MM.

Part: COVER — MISSING (CABIN)

DURING SCHEDULED C1 CHECK, FOUND EEPLS LIGHTS FWD NAD AFT END COVERS MISSING. REMOVED AND REPLACED END COVERS PER MM.

Part: SKIN — CRACKED (BS 350)

DURING SCHEDULED SERVICE CHECK, FOUND CRACKED FUSELAGE SKIN, BS 350 ABOVE STRINGER 15L. REPAIRED SKIN PER SRM.

Part: BULKHEAD CHORD — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND LT SIDE CHORD AT BS 178 BULKHEAD CRACKED, LBL 26. REPAIRED CHORD PER SRM.

Part: RIB — CRACKED (LT WING)

DURING SCHEDULED 1/2D CHECK, FOUND LT WING LOWER RIB CHORD CRACKED BETWEEN STRINGERS 2 AND 3. REPAIRED RIB PER SWA RA NR 1-357-0677.

Part: FITTING — CRACKED (LT MLG)

DURING SCHEDULED 1/2D CHECK, FOUND REAR SPAR ATTACH FITTING CRACKED AT LEFT MAIN LANDING GEAR BEAM STABILIZER LINK, FWD END. REMOVED AND REPLACED ATTACH FITTING PER SRM.

Part: FLOORBEAM — CRACKED (BS 667)

DURING SCHEDULED 1/2D CHECK, FOUND CRACK EXTENDING FROM OVAL CUTOUT OF FLOORBEAM, BS 667, LBL 24.75 UNDER SEAT TRACK. REPAIRED BEAM PER SWA RA NR 1-357-0680.

Part: SKIN — CRACKED (NLG WW)

DURING SCHEDULED 1/2D CHECK, FOUND CUT OUT FOR LH NOSE WHEEL WELL ACCESS PANEL CRACKED AT INBD CORNER. REPAIRED SKIN PER SWA RA NR 1-353-2068.

Part: FRAME — CRACKED (SERVICE DOOR)

DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR AFT LOWER CORNER OF FRAME CRACKED. REPAIRED FRAME PER MM.

Part: FRAME — CRACKED (SERVICE DOOR)

DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR AFT FRAME CRACKED AT NR 3 AND NR 4 STOP CUT-OUTS. REPAIRED FRAME PER SRM.

Part: BULKHEAD — CRACKED (BS 178.)

DURING SCHEDULED 1/2D CHECK, FOUND 9 EA CRACKS AT BS 178 BULKHEAD, BETWEEN LBL 17.5-RBL 17.5. REPAIRED BULKHEAD PER SWA RA NR 1-353-2067.

Part: FLOORBEAM — CORRODED (BS 772)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT FLOORBEAMS, BS 772, RBL 3, AND BS 857, LBL 12, AFT CARGO BIN. REPAIRED BEAMS PER SRM AND SWA RA NR 1-A53-2021.

Part: FLOORBEAM — CORRODED (BS 772)

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED FLOORBEAM, BS 772, LBL 17. REPAIRED BEAM PER SRM.

Part: SKIN — CRACKED (BS 500)

DURING WALKAROUND INSPECTION, FOUND A 3.1 INCH LONG CRACK AT FUSELAGE SKIN, BS 5OOB, STRINGER 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 500)

DURING SCHEDULED A2 CHECK, FOUND A 4 INCH LONG CRACK AT APPROX BS 500D STR 11R. REPAIRED PER SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING INSPECTION, FOUND SKIN CRACK IN CROWN RT SIDE ABOVE NR 3 WINDOW. REPAIRED SKIN PER SRM.

Part: WIRE — CHAFED (COCKPIT)

ON LAND ROLL, SPARKS AND SMOKE IN OVERHEAD PANEL BEHIND FUEL PANEL. SEVERAL LIGHTING CB'S POPPED (RT AND LT INBOARD, NORMAL POSITION AND LT TURN OFF). FUEL RECALL LIGHT ON MASTER CAUTION ON. FOUND SEVERAL CHAFED WIRES BEHIND GEN DRIVE PANEL. REPAIRED WIRES, ALL AFFECTED SYSTEMS CHECKED GOOD PER MM.

Part: SKIN — CRACKED (BS 727)

DURING SCHEDULED SPV CHECK, FOUND A 2 INCH FUSELAGE SKIN CRACKED AT BS 727A-727E, ON CREASE LINE. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT LEFT SIDE OF FUSELAGE 3 INCHES ABOVE AND 3 INCHES AFT OF WATER SERVICE PANEL. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT RT SIDE OF FUSELAGE 36 FWD OF OUT FLOW VALVE. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (BS 976 & 941)

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 976 ABOVE STR 22L AND AT BS 941 ABOVE 25R. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING WALKAROUND CHECK, FOUND APPROX 3 SKIN CRACK RIGHT TOP SIDE OF FUSELAGE BETWEEN CABIN WINDOWS 10 AND 11. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING WALKAROUND CHECK, FOUND APPROX 3 INCH CRACK TOP SIDE OF FUSELAGE BETWEEN CABIN WINDOWS 10 AND 11 RIGHT SIDE. REPAIRED PER BOEING SRM.

Part: CHORD — CRACKED (PYLON)

DURING SCHEDULED BC1 CHECK, FOUND OUTBOARD PYLON CHORD CRACKED AT NAC BS 319. REPAIRED PER SWA RA NR 1-354-192.

Part: SKIN — CRACKED (FUSELAGE)

DURING WALKAROUND CHECK, FOUND APPROX 4 SKIN CRACK RT SIDE ABOVE PASSENGER WINDOW NR 11. REPAIRED PER BOEING SRM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING TERMINAL CHECK, FOUND EGRESS TRACK LIGHTING INOP FWD CABIN TO MID CABIN. REMOVED AND REPLACED FWD CABIN EGRESS LIGHTING BATTERY PACK AS PER BOEING MM, OPS CHECK GOOD.

Part: SKIN — CRACKED (CABIN)

DURING WALKAROUND CHECK, FOUND APPROX 4 SKIN CRACKED AT RT SIDE ABOVE PASSENGER WINDOW NR 11. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (R2 DOORWAY)

DURING SCHEDULED C3 CHECK, FOUND R2 DOOR LOWER FUSELAGE HINGE CUTOUT FUSELAGE SIDE CRACKED 1.52. REPAIRED PER BOEING SRM.

Part: RIB — DAMAGED (WS 208)

DURING SCHEDULED C3 CHECK, FOUND L/E RIB AT WS 208 DAMAGED BY KRUEGER FLAP SCREW. GOUGE STARTS AT VERTICAL WEB AND CONTINUES .375 INCH ACROSS ANGLE. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED A2, FOUND 4 IN SKIN CRACK RT SIDE JUST AFT AND ABOVE NR 12 CABIN WINDOW. REPAIRED PER BOEING SRM.

Part: SLIDE — LOW PRESS (AFT SERV DOOR)

DURING SCHEDULED SERVICE CHECK, FOUND AFT DOOR SLIDE PRESSURE BELOW MINIMUM. REPLACED SLIDE ASSEMLY PER BOEING M/M.

Part: STRINGER — CRACKED (BS 967)

DURING SCHEDULED C4 CHECK, FOUND STRINGER 27L CRACKED, AT BS 967. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 517)

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 517 BETWEEN CABIN WINDOW BELOW S12L. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 969)

DURING SCHEDULED SERVICE CHECK, FOUND A 3 INCH FUSELAGE SKIN CRACK AT BS 969 AT S21L. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED SERVICE CHECK, FOUND A FUSELAGE SKIN CRACKS JUST AFT OF PREVIOUS REPAIR. REPAIRED PER BOEING SRM.

Part: RELAY — INOPERATIVE (COCKPIT)

DIVERTED TO PHX DUE TO NR 2 BUSS DROPPING OFF LINE IN FLIGHT. REPLACED R30 RELAY PER BOEING M/M, AND PERFORMED SWA ACO TO REPLACE BOTH NR 1 TRANSFER C/B'S.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK AND HOUSING PER BOEING M/M.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED SC CHECK, FOUND SKIN CRACKED 3 AT RT AFT FUSELAGE APPROX 48 FWD OF AFT OUTFLOW VALVE AND 2 ABOVE SKIN LAP. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 277)

DURING SPECIAL VISIT CHECK, FOUND FUSELAGE SKIN CRACK AT BS 277, AT S16L, APPROX 4 INCHES LONG. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 727)

DURING SCHEDULED 1/4 D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E S15R. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 750)

DURING SCHEDULED 1/4 D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, 1.5 INCH LENGTH. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (CARGO DOOR)

DURING SCHEDULED B/C3 CHECK, FOUND FWD CARGO DOOR FRAME CRACKED IN AFT LOWER CORNER. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.