N332SW

Part: LENS — LOOSE (CABIN) · airframe 73,553 hrs · 65,933 cycles

RT OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 19. SECURED LENS PER MM.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 73,231 hrs · 65,690 cycles

DURING SCHEDULED HC1 CHECK, FOUND NLG WHEEL WELL UPPER WEB CRACKED AT BS 277. REPAIRED WEB PER EA.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 73,068 hrs · 65,552 cycles

L1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MT.

Part: LENS — LOOSE (CABIN) · airframe 72,365 hrs · 64,969 cycles

RT WING OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED LENS PER MM.

Part: COVER — BROKEN (CABIN) · airframe 72,146 hrs · 64,814 cycles

L1 DOOR LOWER EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: LENS — BROKEN (CABIN) · airframe 71,849 hrs · 64,585 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR OVERHEAD EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: ANGLE — CRACKED (R1 DOOR) · airframe 71,632 hrs · 64,437 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND R1 DOOR FWD LOWER MOUNT BOLT FRAME ANGLE CRACKED AT HANDLE MECHANISM. REMOVED AND REPLACED R1 DOOR PER MM.

Part: CONTROL PANEL — FAULTY (FIRE WARNING) · airframe 71,590 hrs · 64,401 cycles

AIR TURNBACK / DECLARED EMERGENCY. APU FIRE INDICATION APPROX 5 MIN APU SHUTDOWN AND DEPARTURE ALARM CONTINUED INTERMITTENTLY UNTIL LANDING. APU DET INOP, ILLUMINATED AT GATE. REMOVED AND REPLACED P8-1 ENG & APU FIRE CONTROL PNL.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 71,180 hrs · 64,093 cycles

DURING SCHEDULED 22Y CHECK, FOUND KEEL BEAM CRACKED AT BS 500D, BETWEEN STR 12L TO STR 13L. REPAIRED BEAM PER AEM EO.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 71,180 hrs · 64,093 cycles

DURING SCHEDULED 22Y CHECK, CABIN EMERGENCY LIGHT BATTERY CHARGE LOW. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,180 hrs · 64,093 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 518B, STR 19R. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,180 hrs · 64,093 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED BETWEEN BS 705 TO BS 715, LBL 24.5. REPAIRED BEAM PER AEM EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,180 hrs · 64,093 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AFT EDGE FRAME AFT LOWER CORNER R1 DOOR CUTOUT AT LEVEL STR 17R. REPAIRED FRAME PER AEM EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,180 hrs · 64,093 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED BETWEEN BS 520 TO BS 540, BETWEEN STR 27L TO STR 27R. REPAIRED SKIN PER AEM EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,180 hrs · 64,093 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 328, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER AEM EO.

Part: WEB — CRACKED (FUSELAGE) · airframe 71,180 hrs · 64,093 cycles

DURING SCHEDULED 22Y CHECK, FOUND WEB CRACKED BETWEEN BS 394.5 TO BS 303.9, STR 12L. REMOVED AND REPLACED WEB PER DWG.

Part: FLAP — CORRODED (LT WING) · airframe 71,180 hrs · 64,093 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING INBOARD FLAP CORRODED. REPAIRED FLAP PER AEM EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,180 hrs · 64,093 cycles

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

Part: LENS — MISSING (CABIN) · airframe 71,180 hrs · 64,093 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 71,180 hrs · 64,093 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 71,180 hrs · 64,093 cycles

DURING SCHEDULED 22Y CHECK, FOUND FWD CARGO COMPARTMENT ANGLE CORRODED AT BS 540, STR 27R. REMOVED AND REPLACED ANGLE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,180 hrs · 64,093 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 344, STR 6L. REPAIRED FRAME PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 71,180 hrs · 64,093 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,180 hrs · 64,093 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 312, STR 19R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,180 hrs · 64,093 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 799, STR 17L. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 71,180 hrs · 64,093 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,180 hrs · 64,093 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 320, STR 20L. REMOVED AND REPLACED FRAME PER SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 71,180 hrs · 64,093 cycles

DURING SCHEDULED 22Y CHECK, FOUND CHANNEL STRAP CRACKED BETWEEN BS 312 TO BS 344, STR 18L. REMOVED AND REPLACED STRAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,180 hrs · 64,093 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 13L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,180 hrs · 64,093 cycles

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

Part: FLAP — DELAMINATED (LT WING) · airframe 71,180 hrs · 64,093 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: SLAT — DELAMINATED (RT WING) · airframe 71,180 hrs · 64,093 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING NR 5 SLAT DELAMINATED. REPAIRED NR 5 SLAT PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,180 hrs · 64,093 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277 STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 71,180 hrs · 64,093 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,180 hrs · 64,093 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,180 hrs · 64,093 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 71,180 hrs · 64,093 cycles

DURING SCHEDULED 22Y CHECK, FOUND WEB CRACKED BETWEEN BS 277 TO BS 291.5, BETWEEN STR 8R TO STR 10R. REMOVED AND REPLACED WEB PER SRM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 71,180 hrs · 64,093 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL BEAM CRACKED BETWEEN BS 698 TO BS 717, BBL 0.07. REPAIRED BEAM PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,180 hrs · 64,093 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,180 hrs · 64,093 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,180 hrs · 64,093 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,180 hrs · 64,093 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,180 hrs · 64,093 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,180 hrs · 64,093 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,180 hrs · 64,093 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,180 hrs · 64,093 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,180 hrs · 64,093 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,180 hrs · 64,093 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,180 hrs · 64,093 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,180 hrs · 64,093 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 343, BETWEEN STR 21R TO STR 22R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,135 hrs · 64,061 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 515C, STR 8L. REPAIRED SKIN PER SRM.

Part: ACM — FAULTY (AC BAY) · airframe 70,824 hrs · 63,851 cycles

LOSS PRESSURE AT 14,000 FT ALT WARNING HORN SOUNDED. MASKS DIDN'T FALL. REMOVED AND REPLACED BELLY DRAINS, FWD OUTFLOW VALVE, AND LEFT ACM PER MM.

Part: ACTUATOR — BROKEN (SPOILER) · airframe 66,630 hrs · 60,757 cycles

CONTROL YOKE STICKS 6 UNITS DURING LEFT TURN. FOUND NR 5 GRND SPOILER ACT ATTACH BRACKET BROKEN. REMOVED AND REPLACED SPOILER ACT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,063 hrs · 63,286 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,063 hrs · 63,286 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,063 hrs · 63,286 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 303.5, WL 238 LT. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,063 hrs · 63,286 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,998 hrs · 63,237 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 384, STR 15R. REPAIRED SKIN PER SWA EA.

Part: COVER — MISSING (EXTERIOR) · airframe 69,943 hrs · 63,193 cycles

R2 DOOR EXTERNAL EMERGENCY EXIT LIGHT LENS COVER MISSING. REPAIRED LIGHT PER EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 69,697 hrs · 63,008 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,932 hrs · 62,427 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 792, STR 18L. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 68,863 hrs · 62,375 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED I/B. REMOVED AND REPLACED AFT FLAP PER MM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 68,863 hrs · 62,375 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 1 SLAT DELAMINATED ON T/E WEDGE. REMOVED AND REPLACED SLAT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,738 hrs · 62,282 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 760, STR 19L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,738 hrs · 62,282 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 727D, STR 19L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,738 hrs · 62,282 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 763, STR 19L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,738 hrs · 62,282 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 747, STR 20L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,738 hrs · 62,282 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 500D, STR 16L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,738 hrs · 62,282 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 440, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,738 hrs · 62,282 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 779, STR 18L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,738 hrs · 62,282 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 500D, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,738 hrs · 62,282 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 779, STR 19L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,738 hrs · 62,282 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 750, STR 18L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,738 hrs · 62,282 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 749, STR 19L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,738 hrs · 62,282 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 759, STR 18L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,738 hrs · 62,282 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 445, STR 16R. REPAIRED SKIN PER SWA EA.

Part: LENS — MISSING (CABIN) · airframe 68,526 hrs · 62,128 cycles

BULLNOSE LIGHT LENS MISSING AT ROW 6. INSTALLED LENS PER MM.

Part: STRIP — MISSING (CABIN) · airframe 67,723 hrs · 61,567 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS STRIP MISSING AT MID CABIN. INSTALLED STRIP PER MM.

Part: STRIP — MISSING (CABIN) · airframe 67,722 hrs · 61,567 cycles

FOUND EEPLS STRIP MISSING AT MID CABIN. INSTALLED STRIP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,150 hrs · 61,147 cycles

DURING SCHEDULED HC1 CHECK, FOUND AFT SERVICE DOOR SKIN CRACKED AT LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 67,032 hrs · 61,058 cycles

RIGHT AFT CABIN EMERGENCY EXIT LIGHTS REMAIN ILLUMINATED. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 66,298 hrs · 60,507 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,220 hrs · 60,451 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 506A, STR 20R. REPAIRED SKIN PER SRM.

Part: SMOKE DETECTOR — INOPERATIVE (AFT CARGO BAY) · airframe 65,477 hrs · 59,912 cycles

DURING SCHEDULED BRDG CHECK, AFT CARGO COMPARTMENT RT FWD SMOKE DETECTOR INOP. REMOVED AND REPLACED SMOKE DETECTOR PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,477 hrs · 59,912 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,477 hrs · 59,912 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, BETWEEN STR 3L AND STR 2R. REPAIRED FRAME PER SWA EA.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 65,477 hrs · 59,912 cycles

DURING SCHEDULED BRDG CHECK, FOUND BELTFRAME CRACKED AT BS 380, STR 16R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,477 hrs · 59,912 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,477 hrs · 59,912 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,477 hrs · 59,912 cycles

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

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 65,477 hrs · 59,912 cycles

DURING SCHEDULED BRDG CHECK, FOUND KEEL BEAM CORRODED BETWEEN BS 520 AND BS 540, LBL 11. REPAIRED KEEL BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,477 hrs · 59,912 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,477 hrs · 59,912 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,477 hrs · 59,912 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,477 hrs · 59,912 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,477 hrs · 59,912 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,477 hrs · 59,912 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,477 hrs · 59,912 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,477 hrs · 59,912 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,477 hrs · 59,912 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,477 hrs · 59,912 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SUPPORT ANGLE — CRACKED (CENTER WING) · airframe 65,477 hrs · 59,912 cycles

DURING SCHEDULED BRDG CHECK, FOUND WING CENTER SECTION FRONT SPAR STIFFENER SUPPORT ANGLE CRACKED AT BS 540, LBL 57. REMOVED AND REPLACED SUPPORT ANGLE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 65,477 hrs · 59,912 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 16R CORRODED AT BS 485. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,477 hrs · 59,912 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 14R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (L/E SLAT) · airframe 65,477 hrs · 59,912 cycles

DURING SCHEDULED BRDG CHECK, FOUND LT WING NR 2 L/E SLAT LOWER SURFACE CRACKED. REMOVED AND REPLACED SLAT PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,477 hrs · 59,912 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 294.5, STR 7L. REPAIRED FRAME PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 65,477 hrs · 59,912 cycles

DURING SCHEDULED BRDG CHECK, FOUND ZEE CHORD CORRODED AT BS 270, LBL 11 TO RBL 11. REMOVED AND REPLACED ZEE CHORD PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 65,477 hrs · 59,912 cycles

DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD DOME CAP WEB CRACKED AT BS 1016, 12 O'CLOCK POSITION. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,477 hrs · 59,912 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 65,477 hrs · 59,912 cycles

DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, 9 O'CLOCK POSITION. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,477 hrs · 59,912 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,477 hrs · 59,912 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 2R. REPAIRED FRAME PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 65,477 hrs · 59,912 cycles

DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 400 AND BS 420, STR 17L. REMOVED AND REPLACED WEB PER SWA EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 65,477 hrs · 59,912 cycles

DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 360 AND BS 400, STR 17R. REMOVED AND REPLACED WEB PER SWA EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 65,477 hrs · 59,912 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 1006, STR 24L. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,477 hrs · 59,912 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM UPPER TEE CAP CRACKED AT BS 727B, LBL 45. REPAIRED FLOORBEAM TEE CAP PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,477 hrs · 59,912 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 1006, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,477 hrs · 59,912 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 988, STR 20L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 65,477 hrs · 59,912 cycles

DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR FRAME CUTOUT AFT FRAME CRACKED AT NR 5 DOOR STOP. REPAIRED FRAME PER SRM.

Part: BRACKET — CORRODED (BIRT BAR) · airframe 65,477 hrs · 59,912 cycles

DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR BRACKET CORRODED. REMOVED AND REPLACED BRACKET PER SRM.

Part: BRACKET — CORRODED (GIRT BAR) · airframe 65,477 hrs · 59,912 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,477 hrs · 59,912 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16R. REPAIRED FRAME PER BOEING DRAWING.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 65,477 hrs · 59,912 cycles

DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 616 TO BS 639, RBL 70. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,477 hrs · 59,912 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 928, STR 23L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,477 hrs · 59,912 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 928, STR 12L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 65,411 hrs · 59,868 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 65,411 hrs · 59,868 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,358 hrs · 59,828 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 971, STR 21L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 503D S16R) · airframe 65,252 hrs · 59,756 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503D, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,241 hrs · 59,748 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503D, STR 16R. REPAIRED SKIN PER SWA EA.

Part: LIGHT — BROKEN (CABIN) · airframe 64,912 hrs · 59,491 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 64,844 hrs · 59,440 cycles

DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: BULKHEAD — CRACKED (BS 1016 S5R) · airframe 64,844 hrs · 59,440 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT PRESSURE BULKHEAD CRACKED AT BS 1016, STR 5R. REPAIRED BULKHEAD PER SRM.

Part: SLIDE — DISLODGED (R2 DOOR) · airframe 64,002 hrs · 58,757 cycles

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

Part: SLIDE — DISLODGED (R2 DOOR) · airframe 63,992 hrs · 58,746 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,878 hrs · 58,649 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 19L. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,538 hrs · 58,376 cycles

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

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,012 hrs · 57,970 cycles

DURING SCHEDULED C3 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 63,012 hrs · 57,970 cycles

DURING SCHEDULED C3 CHECK, R2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (BS 970 S22L) · airframe 62,152 hrs · 57,296 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 970, STR 22L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,036 hrs · 57,191 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 969, STR 22L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 740 S18L) · airframe 62,036 hrs · 57,191 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740, STR 18L. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,447 hrs · 56,720 cycles

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

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 61,447 hrs · 56,720 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,447 hrs · 56,720 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 21R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 61,447 hrs · 56,720 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 359, STR 16L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 61,178 hrs · 56,488 cycles

DURING SCHEDULED C1 CHECK, FOUND NLG W/W CEILING PANEL CUTOUT CRACKED AT RIGHT BS 250 AND LEFT BS 250. REPAIRED CEILING PANEL CUTOUT PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,178 hrs · 56,488 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 770, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,167 hrs · 56,482 cycles

FOUND FUSELAGE SKIN CRACKED AT BS 504C, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,167 hrs · 56,482 cycles

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

Part: SKIN — CRACKED (L1 DOOR) · airframe 60,436 hrs · 55,900 cycles

DURING SCHEDULED A2 CHECK, FOUND L1 DOOR SKIN CRACKED AT UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 59,880 hrs · 55,458 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 59,561 hrs · 55,223 cycles

R1 DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 58,243 hrs · 54,190 cycles

DURING SCHEDULED C2 CHECK, FOUND NR 1 L/E SLAT SKIN CRACKED NEAR INBOARD END. REPAIRED SLAT PER SRM.

Part: SKIN — CRACKED (BS 947) · airframe 58,243 hrs · 54,190 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, BETWEEN STR 23L & STR 24L. REPAIRED SKIN PER SWA EA.

Part: LINE — CHAFED (MLG WW) · airframe 57,768 hrs · 53,833 cycles

AIR TURNBACK/DECLARED EMERGENCY, LOST A-SYSTEM HYDRAULICS. REMOVED AND REPLACED A-SYSTEM HYDRAULIC SUPPLY LINE PER MM.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 57,767 hrs · 53,831 cycles

DIVERSION, LOST A-SYSTEM HYDRAULIC PRESSURE & FLUID. REMOVED AND REPLACED A-SYSTEM HYDRAULIC HEAT EXCHANGER LINE & HYDRAULIC CASE DRAIN FILTER PER MM.

Part: BUSHING — WORN (LT ELEVATOR TAB) · airframe 57,296 hrs · 53,458 cycles

DURING SCHEDULED C1 CHECK, LT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TAB NR 1 HINGE BUSHING & HARDWARE PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,296 hrs · 53,458 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,285 hrs · 53,448 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 777, STR 24R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,285 hrs · 53,448 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D + 10, STR 19R. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,257 hrs · 53,422 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C + 18, STR 13L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,257 hrs · 53,422 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 57,257 hrs · 53,422 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BEADED WEB CRACKED AT BS 664, RBL 40. REPAIRED WEB PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 57,257 hrs · 53,422 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE KEELBEAM CORRODED AT BS 520, RBL 7. REPAIRED KEEL BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,257 hrs · 53,422 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 24R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,257 hrs · 53,422 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CABIN LONGITUDINAL FLOORBEAM CRACKED AT BS 663, BL 0. REPAIRED FLOORBEAM PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 727A) · airframe 57,257 hrs · 53,422 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25R & STR 26L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,257 hrs · 53,422 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500, BL 0. REPAIRED SHEAR TIE PER SRM.

Part: WEB — CRACKED (LT MLG WW) · airframe 57,257 hrs · 53,422 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BEADED WEB CRACKED AT BS 664, LBL 33. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,257 hrs · 53,422 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 25L. REMOVED AND REPLACED CLIP PER SRM.

Part: WINDOW POST — CRACKED (L1 COCKPIT) · airframe 57,257 hrs · 53,422 cycles

DURING SCHEDULED 1/4D CHECK, FOUND L1 COCKPIT WINDOW POST CRACKED AT UPPER OUTBOARD CORNER. REPAIRED POST PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,050 hrs · 53,248 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 312, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,803 hrs · 53,052 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 973, STR 24L. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,594 hrs · 52,877 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY BULLNOSE LIGHT INOP AT ROW 20. RELAMPED PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,567 hrs · 52,852 cycles

L2 & R2 DOOR EMERGENCY EXIT SIDE LIGHTS INTERMITTANT. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: COVER — LOOSE (CABIN) · airframe 55,641 hrs · 52,133 cycles

EEPLS FLOOR TRACK COVER, LOOSE. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: SKIN — WORN (FUSELAGE) · airframe 55,521 hrs · 52,039 cycles

DURING SCHEDULED SERVICE CHECK, FOUND UPPER FUSELAGE SKIN BETWEEN BS 857 AND BS 907, BL 0, WORN. REPAIRED SKIN PER EA.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,384 hrs · 51,930 cycles

DURING SCHEDULED A1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT AT ROW 6 DEF, INOP. RELAMPED PER MM.

Part: SKIN — DELAMINATED (LT WING FOREFLAP) · airframe 54,552 hrs · 51,271 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED OUTBOARD T/E FOREFLAP PER MM.

Part: LINE — LEAKING (A-HYD SYSTEM) · airframe 54,530 hrs · 51,246 cycles

AIR TURNBACK, NR 1 ENGINE HYDRAULIC A-SYSTEM LOW PRESSURE LIGHT ILLUMINATED. REMOVED AND REPLACED NR 1 ENGINE A-SYSTEM HYDRAULIC PRESSURE LINE PER MM.

Part: BOLT — SHEARED (RT WING SLAT) · airframe 53,963 hrs · 50,773 cycles

ON APPROACH NR 4 L/E SLAT INDICATED INTRANSIT, RECYCLED PER QRH WITH NORMAL DEPLOYMENT. UPON LANDING CYCLE FLAPS/SLATS AND NOTED A LOUD BANG AND ASYMMETRICAL RATE OF DEPLOYMENT ON NR 4 L/E SLAT, NR 4 L/E SLAT OUTBOARD SIDE STICKS. REMOVED AND REPLACED NR 4 L/E SLAT DETENT BOLT PER MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 53,951 hrs · 50,762 cycles

L1 DOOR EVAC SLIDE GIRT BAR LOOSE. REMOVED AND REPLACED L1 DOOR EVAC SLIDE PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 53,580 hrs · 50,473 cycles

DURING SCHEDULED RON, FOUND LOWER KEELBEAM CHORD AT BS 727 + 2, STRINGER 27R, CORRODED. REMOVED AND REPLACED LOWER KEELBEAM CHORD PER EA.

Part: WEDGE — DELAMINATED (L/E SLAT) · airframe 52,757 hrs · 49,822 cycles

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

Part: WARNING SYSTEM — FAULTY (NR 2 ENGINE) · airframe 51,367 hrs · 48,704 cycles

IN FLT SHUTDOWN, AIR TURNBACK, DECLARED EMERGENCY, NR 2 ENG OIL FILTER BYPASS LIGHT ILLUMINATED. REMOVED NR 2 ENG OIL FILTER. NO DEFECTS FOUND. DEFERRED NR 2 ENG OIL FILTER WARN SYS PER MEL. LATER AT LAS, REMOVED AND REPLACED NR 2 ENG OIL FILTER AS PRECAUTIONARY.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 50,832 hrs · 48,273 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BEAR STRAP CRACKED AT BS 360, ABOVE STR 14R. REPAIRED BEAR STRAP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 50,832 hrs · 48,273 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 14L AND STR 15L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,832 hrs · 48,273 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIP CRACKED AT BS 827, STR 16R. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 50,832 hrs · 48,273 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 540, STR 10L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,832 hrs · 48,273 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 16L. REPAIRED FRAME PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 50,832 hrs · 48,273 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICES CRACKED (4 EA) AT BS 540 AT STR 4R, BS 908 AT STR 4R, BS 908 AT STR 4L AND BS 360 AT STR 4L. REMOVED AND REPLACED STRINGER SPLICES PER SRM.

Part: ROD END — WORN (RT ELEVATOR) · airframe 49,979 hrs · 47,602 cycles

DURING SCHEDULED C1 CHECK, SWA SI 11139-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB ROD ENDS ON OUTBOARD ROD PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,973 hrs · 47,597 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 24L. REPAIRED SKIN PER SRM.

Part: FITTING — CORRODED (BOTH LT/RT MLG) · airframe 49,718 hrs · 47,388 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BOTH LT/RT MLG FWD OTBD FITTINGS CORRODED. REMOVED AND REPLACED BOTH LT AND RT MLG OTBD FITTINGS PER MM.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 49,464 hrs · 47,186 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR LOWER BEAM CRACKED AT NR 2 STOP FITTING. REMOVED AND REPLACED LOWER BEAM WEB PER SRM.

Part: STIFFENER — CRACKED (LT MLG W/W) · airframe 49,464 hrs · 47,186 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BULKHEAD STIFFENER CRACKED AT LT MLG W/W, BS 663 AND LBL 6.15. REMOVED AND REPLACED STIFFENER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,464 hrs · 47,186 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 942, ABOVE STR 24L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,464 hrs · 47,186 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIPS CRACKED (2 EA) AT BS 663, STR 10L AND STR 10R. REMOVED AND REPLACED STRINGER CLIPS PER SRM

Part: VALVE — MALFUNCTIONED (A/C BAY) · airframe 48,725 hrs · 46,597 cycles

DURING FLIGHT SMELLED ELECTRICAL SMELL IN COCKPIT AND CABIN. FOUND ODOR ASSOCIATED WITH RT PACK WHEN TEMP SELECTED IN FULL HOT. REMOVED AND REPLACED RT PACK VALVE PER MM.

Part: COVER — LOOSE (CABIN) · airframe 48,529 hrs · 46,439 cycles

EEPLS COVER LOOSE BETWEEN ROW NR 7 AND ROW NR 9. SECURED COVER PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 48,100 hrs · 46,088 cycles

DURING SCHEDULED C3 CHECK, FOUND RT T/E OTBD AFT FLAP DELAMINATED. REMOVED AND REPLACED RT T/E OTBD AFT FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,653 hrs · 45,700 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D PLUS 5, ABOVE STR 10R. REPAIRED SKIN PER SRM.

Part: ROD END — WORN (ELEVATOR TAB) · airframe 47,201 hrs · 45,328 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED TAB ATTACH ROD END ASSY'S PER MM.

Part: FASTENER — LOOSE (FWD SVC DOOR) · airframe 47,087 hrs · 45,228 cycles

DURING SCHEDULED BC2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE CONTAINER UPPER FWD FASTENER LOOSE. REMOVED AND REPLACED EMERGENCY EVAC SLIDE CONTAINER FASTENER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,941 hrs · 44,280 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 3 INCHES LONG AT BS 961, BELOW STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (UPPER FUSELAGE) · airframe 45,295 hrs · 43,740 cycles

DURING SCHEDULED BC4 CHECK, FOUND FUSELAGE SKIN CRACKED 3.75 INCHES, BS 522, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (AFT ENTRY DOOR) · airframe 44,400 hrs · 42,997 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR UPPER HINGE CUTOUT, CRACK IS 5/32. REPAIRED SKIN PER SWA RA.

Part: LIGHT — LOOSE (CABIN) · airframe 44,400 hrs · 42,997 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,286 hrs · 46,334 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 980, STRINGER 22L. REPAIRED SKIN PER SWA RA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,286 hrs · 46,334 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STRINGER 10R. REPAIRED SKIN PER BOEING SB & SWA RA.

Part: SLIDE — OUT OF TOLERANCE (SERVICE DOOR) · airframe 43,312 hrs · 42,070 cycles

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

Part: CONTROL PANEL — FAILED (COCKPIT) · airframe 42,677 hrs · 41,545 cycles

AIR TURNBACK, MCP FAILED. RESET ALL FMC C/B AND RESEATED ALL DIGITAL FLIGHT COMPUTERS. RESEATED CONNECTORS AT MCP. PERFORMED DFCS BITE TEST. ALL INDICATIONS AND BITE TEST GOOD. AT PHX, REPLACED A FCC FOR MX CONVENIENCE.

Part: COVER — LOOSE (CABIN) · airframe 42,164 hrs · 41,087 cycles

EEPLS TRACK COVER LOOSE AT MID CABIN. R&R EEPLS ASSY PER MM.

Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 41,983 hrs · 40,921 cycles

DURING LINE CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE CABLE END LOOP EXCESSIVE PER SI 11036-25. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 41,410 hrs · 40,430 cycles

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

Part: SKIN — CRACKED (LT WING SLAT) · airframe 41,251 hrs · 40,307 cycles

DURING SCHEDULED 1/4D CHECK, FOUND NR 2 L/E SLAT LOWER SKIN CRACKED I/B OF PREVIOUS REPAIR. REPAIRED SKIN PER BAC DRAWING AND SRM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 41,251 hrs · 40,307 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RIGHT WING T/E INBOARD FORE FLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: STRAP — CRACKED (FUSELAGE SKIN) · airframe 41,251 hrs · 40,307 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE EXTERNAL SKIN STRAP CRACKED, BS 1138 BELOW LT HORIZONTAL STAB ATTACH LUG. REMOVED AND REPLACED FUSELAGE SKIN STRAP PER SRM AND BOEING DRAWING.

Part: BEAM — CRACKED (CARGO BAY) · airframe 41,251 hrs · 40,307 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 787 FLOORBEAM CRACKED AT RADIUS, RBL 14. REPAIRED BEAM PER SRM.

Part: CONTROL BOX — INOPERATIVE (E&E BAY) · airframe 40,963 hrs · 40,063 cycles

DIVERSION, ANTI-SKID LIGHT ILLUMINATED. REMOVED AND REPLACED ANTI-SKID CONTROL UNIT AND LT I/B WHEEL SPEED TRANSDUCER PER MM.

Part: LINE — LEAKING (B-HYD SYST)

DURING FLIGHT LOST ALL B-SYSTEM HYDRAULIC FLUID. A/C MADE AN UNEVENTFUL LANDING. FOUND PRESS LINE LEAKING AT B-ELECT PUMP REPLACED LINE, LEAK CK'D PER BOEING MM. REPLACED B-CASE DRAIN AND B-SYSTEM RETURN FILTERS PER BOEING MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED C3 CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOP AT ROW 22DEF. RELAMPED PER BOEING M/M.

Part: ANGLE — CORRODED (BS 948)

DURING SCHEDULED D-CHECK, FOUND AFT CARGO FLOORBEAM ANGLE CORRODED AT BS 948. REPLACED PER BOEING SRM.

Part: SKIN — GOUGED (LT WING)

DURING SCHEDULED D-CHECK, FOUND LEFT WING FIXED L/E SKIN INTERNAL SURFACE GOUGED AT NR 1 SLAT I/B AUX TRACK CUTOUT. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 294.5)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 294.5, RBL 1 TO LBL 1, WL 208. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND A 1 INCH CRACK AT BS 178 BULKHEAD AT WL 187, RBL 1. REPAIRED PER BOEING SRM AND TYPICAL REPAIR T1-353-057.

Part: LONGERON — CRACKED (NR 1 PYLON)

DURING SCHEDULED D-CHECK, FOUND NR 1 PYLON LONGERON CRACKED JUST FWD OF BUBBLE FAIRING. REMOVED AND REPLACED PER BOEING SRM.

Part: CREASE BEAM — CRACKED (BS 177)

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM CRACKED AT BS 177 STR 17 WL 208. REPAIRED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 312-348)

DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOORWAY LOWER SILL I/B SUPPORT ANGLE CORRODED AT BS 312 TO 348, WL 209, LBL 61. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 947.5)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 947.5, WL 208, LBL 53 CRACKED AT FASTENER HOLE. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 986.5)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 986.5, LBL 45 TO RBL 50, WL 208 CORRODED ON UPPER AND LOWER SURFACES. REMOVED AND REPLACED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND 1 INCH CRACK AT BS 178 BULKHEAD, WL 187, RBL 1. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (GALLEY DOORWAY)

DURING SCHEDULED D-CHECK, FOUND GALLEY DOORWAY UPPER FWD STUB FRAME CRACKED. REPAIRED PER BOEING SRM.

Part: ANGLE — CORRODED (GALLEY DOORWAY)

DURING SCHEDULED D-CHECK, FOUND AFT GALLEY DOORWAY LOWER SILL SUPPORT Z-ANGLES CORRODED. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 616)

DURING SCHEDULED D-CHECK, FOUND RT FRAME AT BS 6616, RBL 60, WL 201 CRACKED. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 328)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT 328, RBL 30, WL 208 CORRODED AT FASTENER HOLE LOWER SURFACE. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND SUPPORT BEAM AT BS 1010 LBL 34 WL 208, BS 959 RBL 18 WL 208, BS 995 LBL 18 TO BS 1004 LBL 7 WL 208 AND BS 957 RBL 25 WL 208 CORRODED AT FASTENER HOLE. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 967)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 967, RBL 28, WL 208 ON UPPER AND LOWER SURFACE. REPAIRED PER BOEING SRM.

Part: SHEAR TIE — CRACKED (BS 1107)

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 1107 BETWEEN STRINGERS 2R AND 3R. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (GALLEY DOORWAY)

DURING SCHEDULED D-CHECK, FOUND FWD GALLEY DOOR CUTOUT LOWER AFT CORNER OUTER SKIN CRACKED. REPAIRED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 1140)

DURING SCHEDULED D-CHECK, FOUND STRINGER 5L CRACKED AT BS 1140. REMOVED AND REPLACED PER BOEING SRM.

Part: BULKHEAD CHORD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD SIDE CHORD (RT) CRACKED IN RADIUS AT WL 207. REPAIRED PER BOEING SRM.

Part: BULKHEAD ANGLE — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND ATTACH ANGLE CRACKED AT BS BULKHEAD 178 WL 208 RBL 24 TO 20. REMOVED AND REPLACED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 1140)

DURING SCHEDULED D-CHECK, FOUND STRINGER 5R CRACKED AT BS 1140. REMOVED AND REPLACED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT WL 201 TO 202, LBL 6.5. REPAIRED PER BOEING SRM.

Part: CHORD — CORRODED (BS 270)

DURING SCHEDULED D-CHECK, FOUND Z-CHORD AT BS 270, WL 208 CORRODED BETWEEN LBL 11 TO RBL 11. REMOVED AND REPLACED PER BOEING SRM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AT BS BULKHEAD 178 TO 186 WL 208 RBL 24. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — DENTED (BS 385)

DURING SCHEDULED RON CHECK, FOUND DENT AT FUSELAGE RT SIDE BS 385. REPAIRED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 727)

DURING SCHEDULED D-CHECK, FOUND CORROSION ON FLOOR SUPPORT AT BS 727D+5 TO 860, LBL 12.75. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 248)

DURING SCHEDULED D-CHECK, FOUND NLG RETRACT ACTUATOR SUPPORT BEAM HAS CRACKED WEB AT BS 248. REPAIRED PER BOEING MM.

Part: BULKHEAD PANEL — DAMAGED (BS 727)

DURING SCHEDULED D-CHECK, FOUND AT BS 727 BULKHEAD PANEL IS DAMAGED. REPAIRED PER BOEING MM.

Part: BULKHEAD ANGLE — CORRODED (BS 947.5)

DURING SCHEDULED D-CHECK, FOUND CORROSION ON AFT BULKHEAD SUPPORT ANGLE AT BS 947.5. REPAIRED PER BOEING SRM.

Part: SUPPORT — CRACKED (BS 727)

DURING SCHEDULED D-CHECK, FOUND CORROSION ON FLOOR SUPPORT AT BS 727D+5 TO 860, LBL 7.5. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (CARGO DOORWAY)

DURING SCHEDULED RON, FOUND FUSELAGE DENTED BELOW AFT CARGO DOOR. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (RT WING)

DURING SCHEDULED SERVICE CHECK, FOUND RIGHT I/B FIXED L/E SKIN CRACKED .187 , 15 FROM PYLON. REPAIRED PER SWA RA 1-A57-0503.

Part: RT UNIT — INOPERATIVE (COCKPIT)

EN ROUTE, WEATHER RADAR BEGAN DISPLAYING FALSE RETURNS. AIRCRAFT DIVERTED TO BHM AND MADE AN UNEVENTFUL LANDING. REPLACED RADAR R/T UNIT PER BOEING M/M.

Part: PRIORTY VALVE — FAILED (NLG)

AFTER TAKEOFF, NOSE GEAR DID NOT RETRACT. RECYCLED GEAR AND NOSE GEAR RETRACTED. INSPECTED AND REPLACED NLG DOWNLOCK ACTUATOR, PRIORITY VALVE, AND RETRACTION TESTED PER BOEING M/M.

Part: VALVE — FAILED (NLG)

AFTER TAKEOFF, NOSE GEAR DID NOT RETRACT. CYCLED AND THEN GEAR RETRACTED. MADE AN UNEVENTFUL LANDING AT OAK. REMOVED AND REPLACED NOSE GEAR DOWNLOCK ACTUATOR, PRIORITY VALVE, AND PERFORMED GEAR RETRACTION TEST PER M/M.

Part: SKIN — GOUGED (ENTRY DR CUTOUT)

DURING SCHEDULED BC4 CHECK, FOUND A FUSELAGE SKIN GOUGED 12 INCHES AND 16 INCHES BELOW AFT ENTRY DOOR. REPAIRED PER BOEING SRM.

Part: SKIN — DAMAGED (FUSELAGE)

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN DAMAGED AFT OF AFT CARGO DOOR. REPAIRED PER BOEING SRM.

Part: SKIN — TORN (BS 847)

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN TEAR AT BS 847, BETWEEN STRINGERS 24 AND 25R. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (AFT GALLEY)

DURING SCHEDULED BC1 CHECK, FOUND AFT GALLEY DOOR UPPER HINGE CUTOUT ON FUSELAGE TOP FWD CORNER CRACKED. REPAIRED PER SWA RA 1-353-909.