N667SW

Part: VALVE — DISCONNECTED (RT WING) · airframe 75,872 hrs · 51,871 cycles

DIVERSION / DECLARED EMERGENCY. EN ROUTE TO LAS CROSSFEED VALVE STUCK IN OPEN POSITION. FUEL USED FROM NR 1 TANK ONLY. INSPECTED AND FOUND CROSSFEED VALVE DISCONNECTED. RECONNECTED VALVE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,575 hrs · 51,653 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,575 hrs · 51,653 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 739E, STR 18L. REPAIRED SKIN PER SRM.

Part: PIN — MISSING (L2 DOOR GIRT BAR) · airframe 75,566 hrs · 51,643 cycles

L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR GUIDE PIN MISSING. INSTALLED PIN PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,898 hrs · 51,111 cycles

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

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 74,898 hrs · 51,111 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT KEEL BEAM CORRODED BETWEEN BS 500D AND BS 545. REMOVED AND REPLACED KEEL BEAM PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,898 hrs · 51,111 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,898 hrs · 51,111 cycles

DURING SCHEDULED 22Y CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,898 hrs · 51,111 cycles

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

Part: SPOILER — DELAMINATED (RT WING) · airframe 74,898 hrs · 51,111 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING NR 9 GROUND SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: SPOILER — DELAMINATED (LT WING) · airframe 74,898 hrs · 51,111 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING 0 GROUND SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: SPOILER — DELAMINATED (RT WING) · airframe 74,898 hrs · 51,111 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING NR 6 FLIGHT SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: SPOILER — DELAMINATED (LT WING) · airframe 74,898 hrs · 51,111 cycles

DURING SCHEDULED 22Y CHECK, FOUND LEFT WING NR 1 GROUND SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: SKIN — DELAMINATED (HORIZ STAB) · airframe 74,898 hrs · 51,111 cycles

DURING SCHEDULED 22Y CHECK, FOUND LEFT HORIZONTAL STAB OUTBOARD T/E LOWER SKIN SURFACE DELAMINATED. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,898 hrs · 51,111 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 22L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (AFT CARGO DOOR) · airframe 74,573 hrs · 50,853 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT CARGO DOOR SKIN CRACKED AT DOOR HANDLE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: LENS — MISSING (CABIN) · airframe 74,573 hrs · 50,853 cycles

DURING SCHEDULED C1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT MISSING LENS AT ROW 2 ABC. INSTALLED LENS PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 73,594 hrs · 50,093 cycles

MID CABIN EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED EXIT SIGN PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 72,502 hrs · 49,277 cycles

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

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 72,147 hrs · 48,997 cycles

R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,121 hrs · 48,978 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CRACKED AT LOWER FWD CORNER. REMOVED AND REPLACED FRAME SECTION PER BOEING DRAWING AND SRM.

Part: SKIN — CORRODED (BS 492 S25R) · airframe 72,121 hrs · 48,978 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CORRODED AT FWD CARGO DOOR CUTOUT AFT LOWER CORNER BS 492, STR 25R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (NR 5 SLAT) · airframe 72,121 hrs · 48,978 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING NR 5 L/E SLAT LOWER SKIN CRACKED. REPAIRED NR 5 L/E SLAT SKIN PER SRM.

Part: SKIN — CRACKED (BS 430) · airframe 72,121 hrs · 48,978 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER CUTOUT BS 430, RBL 1. REPAIRED SKIN PER BOEING SB AND ER.

Part: STRINGER — CRACKED (BS 824 S23L) · airframe 72,121 hrs · 48,978 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 23L CRACKED AT BS 824. REPAIRED STRINGER PER SRM.

Part: LIGHT — CRACKED (CABIN) · airframe 72,121 hrs · 48,978 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — CRACKED (CABIN) · airframe 72,121 hrs · 48,978 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHT CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: STRINGER — CRACKED (BS 540 S4L) · airframe 72,121 hrs · 48,978 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 4L CRACKED AT BS 540. REPAIRED STRINGER PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 72,121 hrs · 48,978 cycles

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

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 72,121 hrs · 48,978 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,121 hrs · 48,978 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 13R. REPAIRED FRAME SECTION PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,121 hrs · 48,978 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 13L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,121 hrs · 48,978 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 500C, STR 14L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,121 hrs · 48,978 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,121 hrs · 48,978 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,121 hrs · 48,978 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 15R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: CREASE BEAM — CRACKED (BS 635) · airframe 72,121 hrs · 48,978 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 635, LBL 70. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM.

Part: FRAME — CRACKED (BS 400 S16L) · airframe 72,121 hrs · 48,978 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 16L. REPAIRED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (BS 380 S13L) · airframe 72,121 hrs · 48,978 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 13L. REPAIRED FRAME SECTION PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 71,947 hrs · 48,836 cycles

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

Part: KEELBEAM — CORRODED (BS 500D) · airframe 71,742 hrs · 48,672 cycles

DURING SCHEDULED C2 CHECK, FOUND RIGHT KEEL BEAM CORRODED AT BS 500D, STR 28R. REPAIRED KEEL BEAM PER SWA EA.

Part: BATTERY — DISCHARGED (CABIN) · airframe 71,667 hrs · 48,604 cycles

DURING SCHEDULED MV1 CHECK, FOUND AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (BS 750) · airframe 71,445 hrs · 48,426 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 19L. REPAIRED SKIN PER SWA EA AND SRM.

Part: SKIN — CRACKED (BS 753) · airframe 71,445 hrs · 48,426 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 753, STR 20L. REPAIRED SKIN PER SWA EA AND SRM.

Part: SKIN — CRACKED (BS 742) · airframe 71,445 hrs · 48,426 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 742, STR 24L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 750) · airframe 71,445 hrs · 48,426 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 23L.REPAIRED SKIN PER SWA EA.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,187 hrs · 48,233 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT EMERGENCY EXIT EXTERIOR LIGHT AFT OF RT WING INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BULB PER MM.

Part: SKIN — CRACKED (BS 767 S24L) · airframe 70,788 hrs · 47,923 cycles

DURING SCHEDULED C1CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (LT WING SPOILER) · airframe 69,953 hrs · 47,226 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: SKIN — CRACKED (BS 500D) · airframe 69,953 hrs · 47,226 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 12L. REPAIRED SKIN PER SWA EA.

Part: BATTERY PACK — INOPERATIVE (AFT CABIN) · airframe 68,714 hrs · 46,250 cycles

DURING SCHEDULED RON CHECK, FOUND LT & RT AFT CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,044 hrs · 45,718 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, BELOW STR 12R. REPAIRED SKIN PER SRM & SWA EA.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,995 hrs · 44,882 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD GALLEY LOWER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 66,886 hrs · 44,796 cycles

DURING SCHEDULED 1/4D CHECK, FOUND PRESSURE BULKHEAD WEB AT BS 1016, LBL 1, CORRODED. REPAIRED WEB PER ACO.

Part: TEE FITTING — CRACKED (AFT CARGO DOOR) · airframe 66,886 hrs · 44,796 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO DOOR LOWER OUTBOARD TEE CHORD CRACKED. REPAIRED DOOR CHORD PER RO 0520018-74R.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,886 hrs · 44,796 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,886 hrs · 44,796 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 727D + 13, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,886 hrs · 44,796 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE INNER SKIN AT BS 989.5 BETWEEN STRINGER 24L AND STRINGER 25L, CORRODED. REMOVED AND REPLACED SKIN SECTION PER SRM.

Part: FLOORBEAM — CORRODED (AFT CARGO COMPT) · airframe 66,886 hrs · 44,796 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM AT BS 772, LBL 8, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,886 hrs · 44,796 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 500D, STRINGER 26L, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 66,886 hrs · 44,796 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 23L, AT BS 500C, CORRODED. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 66,886 hrs · 44,796 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 26R, BETWEEN BS 1006 AND 1016, CORRODED. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: SKIN — DELAMINATED (LT WING SPOILER) · airframe 66,886 hrs · 44,796 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT WING NR 3 SPOILER DELAMINATED. REMOVED AND REPLACED LT WING NR 3 SPOILER PER MM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 66,886 hrs · 44,796 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 26R AT BS 500D + 2, CORRODED. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 66,886 hrs · 44,796 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 27L, AT BS 1016, CRACKED. REPAIRED STRINGER SECTION PER SRM.

Part: STIFFENER — CORRODED (PRESSURE BLKHD) · airframe 66,886 hrs · 44,796 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RADIAL STIFFENER AT AFT PRESSURE BULKHEAD BS 1016, 6 O'CLOCK POSITION CORRODED. REPAIRED STIFFENER PER ACO.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,886 hrs · 44,796 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT AFT CARGO COMPARTMENT BS 927, RBL 3, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 66,886 hrs · 44,796 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 3 EACH CRACKS ON BEADED PRESSURE WEB AT BS 663, BETWEEN LBL 33 AND RBL 39. REPAIRED WEB PER SRM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 66,886 hrs · 44,796 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REPAIRED FLAP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,868 hrs · 44,778 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 752 AND BS 769, BETWEEN STRINGERS 23L AND 24L. REPAIRED SKIN SECTIONS PER EA.

Part: WARNING HORN — MALFUNCTIONED (MLG) · airframe 66,708 hrs · 44,657 cycles

COULD NOT SILENCE LANDING GEAR WARNING HORN ON APPROACH WITH FLAPS 30, 3 GREEN LANDING GEAR LIGHTS SHOWING. CYCLED ALL SYSTEMS, COULD NOT SILENCE HORN. INSPECTED LANDING GEAR AND FLAPS, NO DISCREPANCIES NOTED. C/W FLAP POSITION AND LANDING GEAR WARNING TEST PER MM, NO DEFECTS NOTED.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 65,404 hrs · 43,666 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 65,347 hrs · 43,631 cycles

L1 DOOR EVAC SLIDE LOOSE. SECURED L1 DOOR EVAC SLIDE PER MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 65,338 hrs · 43,624 cycles

L1 DOOR EVAC SLIDE LOOSE. SECURED L1 DOOR EVAC SLIDE PER MM.

Part: FAN — OVERHEATED (E&E BAY) · airframe 65,084 hrs · 43,427 cycles

DURING LAST 15 MINUTES OF FLIGHT, REPORTS OF SMOKE ODOR IN CABIN. TURNED OFF GASPER FAN AND RECIRCULATION FAN ODOR CONTINUED. REMOVED AND REPLACED GASPER FAN PER MM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 64,953 hrs · 43,325 cycles

L1 DOOR FRAME LOWER HINGE STRAP UPPER CORNER, CRACKED. REPAIRED L1 DOOR FRAME HINGE STRAP PER EA.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 64,527 hrs · 42,980 cycles

DURING SCHEDULED C2 CHECK, FOUND LT KEEL BEAM AT BS 510 TO BS 520, CORRODED. REPAIRED KEEL BEAM PER EA.

Part: HOSE — LEAKING (B HYD SYSTEM) · airframe 64,232 hrs · 42,757 cycles

DIVERSION, HYD B-SYSTEM LOW PRESSURE LIGHT ILLUMINATED, QUANTITY ALMOST ZERO. REMOVED AND REPLACED HYD-B SYSTEM PRESSURE HOSE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,051 hrs · 41,046 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 749, STR 18R. REPAIRED SKIN PER SRM.

Part: SPOILER — DELAMINATED (LT WING) · airframe 60,657 hrs · 39,944 cycles

DURING SCHEDULED C2 CHECK, FOUND NR 0 GROUND SPOILER DELAMINATED AT ACTUATOR ATTACH POINT. REMOVED AND REPLACED NR 0 GROUND SPOILER PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 59,729 hrs · 39,206 cycles

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

Part: FRAME — CORRODED (AFT CARGO) · airframe 58,683 hrs · 38,373 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 867, WL 165 AND RBL 18. REPAIRED FRAME PER SRM.

Part: STRINGER — CORRODED (AFT CARGO) · airframe 58,683 hrs · 38,373 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CORRODED AT BS 795, STR 26R. REPAIRED STR PER BFG ER.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 58,683 hrs · 38,373 cycles

DURING SCHEDULED D CHECK, FOUND KEEL BEAM CORRODED AT BS 540, WL 149 AND RBL 7. REPAIRED KEEL BEAM PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,683 hrs · 38,373 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,683 hrs · 38,373 cycles

DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 767, BETWEEN STR'S 8R AND 9R. REPAIRED FRAME PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 58,683 hrs · 38,373 cycles

DURING SCHEDULED D CHECK, FOUND BULKHEAD WEB CRACKED AT BS 180, WL 234 AND LBL 17.1. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,683 hrs · 38,373 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, BETWEEN STR'S 8R AND 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,683 hrs · 38,373 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (2 EA) BETWEEN STR'S 8L AND 9L, BS 887 AND BS 827. REPAIRED FRAMES PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 58,683 hrs · 38,373 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 287, WL 208, RT SIDE. REMOVED AND REPLACED WEB SECTION PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 58,683 hrs · 38,373 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM CRACKED AT BS 520, WL 208 LT SIDE. REPAIRED CREASE BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,683 hrs · 38,373 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, WL 202 AND RBL 65. REPAIRED FRAME PER SWA T1.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,683 hrs · 38,373 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED (5 EA), BS 380 AT STR 22L, BS 500D AT STR 19R, BS 500D AT STR 19L, BS 807 AT STR 26R AND BS 500D AT STR 21R. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,683 hrs · 38,373 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 493, WL 161 AND RBL 35. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,683 hrs · 38,373 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED (3 EA) , BS 578 AND BS 706 AT STR 10R, AND BS 663 AT STR 10R. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,683 hrs · 38,373 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 787, WL 151 AND LBL 9. REPAIRED SHEAR TIE PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 58,683 hrs · 38,373 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 340, WL 208 AND LBL 55. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 58,683 hrs · 38,373 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM CORRODED AT BS 913,WL 208 AND LBL 58. REPAIRED CREASE BEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,683 hrs · 38,373 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 500, WL 149 RH SIDE. REPAIRED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 58,683 hrs · 38,373 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM CORRODED AT BS 287, WL 208 AND RBL 53. REPAIRED CREASE BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,683 hrs · 38,373 cycles

DURING SCHEDULED D CHECK, FOUND STR CLIPS CRACKED (7 EA) AT BS 500D AND STR 21R, BS 807 AND STR 26R, BS 380 AND STR 22L, BS 500D AND STR'S 19L AND 19R, BS 578 AND STR 10L, BS 706 AND STR 10L. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,683 hrs · 38,373 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 294, WL 209 AND RBL 55. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,683 hrs · 38,373 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (2 EA) AT BS 493, WL 161 RT AND BS 616, WL 202 RT. REPAIRED FRAMES PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,683 hrs · 38,373 cycles

DURING SCHEDULED D CHECK, FOUND STR CLIPS CRACKED (7 EA) AT BS 500D AND STR 21R, BS 807 AND STR 26R, BS 380 AND STR 22L, BS 500D AND STR'S 19L AND 19R, BS 578 AND STR 10L, BS 706 AND STR 10L. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,683 hrs · 38,373 cycles

DURING SCHEDULED D CHECK, FOUND STR CLIPS CRACKED (7 EA) AT BS 500D AND STR 21R, BS 807 AND STR 26R, BS 380 AND STR 22L, BS 500D AND STR'S 19L AND 19R, BS 578 AND STR 10L, BS 706 AND STR 10L. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 58,683 hrs · 38,373 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM CRACKED AT BS 520, WL 280 AND LBL 65. REPAIRED CREASE BEAM PER SRM.

Part: FLOORBEAM — CORRODED (FWD CABIN) · airframe 58,683 hrs · 38,373 cycles

DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 294, WL 208 AND LBL 38. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,683 hrs · 38,373 cycles

DURING SCHEDULED D CHECK, FOUND STR CLIPS CRACKED (7 EA) AT BS 500D AND STR 21R, BS 807 AND STR 26R, BS 380 AND STR 22L, BS 500D AND STR'S 19L AND 19R, BS 578 AND STR 10L, BS 706 AND STR 10L. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,683 hrs · 38,373 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIES CORRODED (2 EA) AT BS 460, BETWEEN STR 26L AND 27L AND BS 787, BETWEEN STR'S 26L AND 27L. REPAIRED SHEAR TIES PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,683 hrs · 38,373 cycles

DURING SCHEDULED D CHECK, FOUND STR CLIPS CRACKED (7 EA) AT BS 500D AND STR 21R, BS 807 AND STR 26R, BS 380 AND STR 22L, BS 500D AND STR'S 19L AND 19R, BS 578 AND STR 10L, BS 706 AND STR 10L. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,683 hrs · 38,373 cycles

DURING SCHEDULED D CHECK, FOUND STR CLIPS CRACKED (7 EA) AT BS 500D AND STR 21R, BS 807 AND STR 26R, BS 380 AND STR 22L, BS 500D AND STR'S 19L AND 19R, BS 578 AND STR 10L, BS 706 AND STR 10L. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,683 hrs · 38,373 cycles

DURING SCHEDULED D CHECK, FOUND STR CLIPS CRACKED (7 EA) AT BS 500D AND STR 21R, BS 807 AND STR 26R, BS 380 AND STR 22L, BS 500D AND STR'S 19L AND 19R, BS 578 AND STR 10L, BS 706 AND STR 10L. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 58,683 hrs · 38,373 cycles

DURING SCHEDULED D CHECK, FOUND Z-CHORD CORRODED AT BS 270, WL 208 AND RBL 2. REPAIRED Z-CHORD PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,683 hrs · 38,373 cycles

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

Part: WEB — CRACKED (FUSELAGE) · airframe 58,380 hrs · 38,129 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 201 AND RBL 5.0. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,752 hrs · 37,603 cycles

DURING OUT OF SERVICE MAINTENANCE, FOUND FUSELAGE SKIN CRACKED 3 INCHES LONG AT BS 730 D, BELOW STR 19R. REPAIRED SKIN PER SRM.

Part: GUARD — DEFECTIVE (COCKPIT) · airframe 56,964 hrs · 36,988 cycles

DURING SCHEDULED C2 CHECK, FOUND COCKPIT EMERGENCY EXIT LIGHT SWITCH GUARD NOT ARMING THE SWITCH. REMOVED AND REPLACED SWITCH GUARD PER MM.

Part: DOUBLER — UNSECURE (ENTRY DOOR) · airframe 56,791 hrs · 36,834 cycles

FWD ENTRY DOOR SCAB PATCH ON FWD LOWER CORNER COMING OFF. MX FERRY TO DAL. REMOVED OLD REPAIR AND INSTALLED REPAIR PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,249 hrs · 35,570 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELGE SKIN CRACKED AT AFT SVC DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: STIFFENER — CRACKED (MLG WW) · airframe 55,094 hrs · 35,443 cycles

DURING SCHEDULED SERVICE CHECK, FOUND VERTICAL STIFFENER CRACKED, AT MLG WHEEL WELL, BS 663, RBL 6.4. REPAIRED PER SWA RA.

Part: STIFFENER — CRACKED (MLG WW) · airframe 54,900 hrs · 35,279 cycles

DURING SCHEDULED SERVICE CHECK, FOUND VERTICAL STIFFENER CRACKED IN MLG WW BULKHEAD AT BS 663 RBL 6.4. REPAIRED STIFFENER PER SWA RA.

Part: COVER — LOOSE (CABIN) · airframe 54,310 hrs · 34,797 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK COVER LOOSE AT MID CABIN. REMOVED AND REPLACED TRACK COVER PER MM.

Part: FIRE DETECTOR — MALFUNCTIONED (AFT CARGO BAY) · airframe 54,147 hrs · 34,664 cycles

DECLARED EMERGENCY, AFT CARGO FIRE WARNING INDICATION DURING CRUISE. BOTH BOTTLES DISCHARGED. VERIFIED NO SIGN OF FIRE IN AFT CARGO COMPARTMENT. FIRE DETECTION/SUPPRESSION SYSTEM DEACTIVATED PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,083 hrs · 34,607 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 3 EXTERNAL LT FUSELAGE SKIN CRACK BETWEEN BS 727C & BS 747, WL 208.1. REPAIRED SKIN PER SRM.

Part: SLIDE — DETACHED (FWD PAX DOOR) · airframe 53,899 hrs · 34,448 cycles

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

Part: SLIDE — OUT OF ADJ (PAX DOOR) · airframe 53,870 hrs · 34,424 cycles

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

Part: BRACKET — LOOSE (GIRT BAR) · airframe 53,251 hrs · 33,944 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE COVER FWD RETAINING BRACKET RIVETS LOOSE. REPLACED RIVETS PER SRM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 52,361 hrs · 33,179 cycles

DURING SCHEDULED C1 CHECK, FOUND LEFT WING O/B TRAILING EDGE AFT FLAP DELAMINATED AT LOWER SURFACE. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,454 hrs · 32,383 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED AT AFT SERVICE DOOR FWD LOWER CUT OUT. REPAIRED SKIN PER SWA RA NR 1-353-2258.

Part: ANGLE — CRACKED (HORZONTAL STAB) · airframe 51,454 hrs · 32,383 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT HORIZONTAL STAB VERTICAL T-ANGLE CRACKED, STA 230 AFT SIDE OF AFT SPAR. REMOVED AND REPLACED T-ANGLE PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,454 hrs · 32,383 cycles

DURING SCHEDULED 1/4D CHECK, FOUND THRU HFEC INSP BS 178 BULKHEAD CRACKED, LBL 9, LBL 10 AND LBL 12. REPAIRED BULKHEAD PER SRM.

Part: FRAME — CRACKED (SERVICE DOOR) · airframe 51,454 hrs · 32,383 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR AFT FRAME CRACKED AROUND NR 3 STOP. REPAIRED FRAME PER TYP REPAIR T1-152-003.

Part: FRAME — CRACKED (SERVICE DOOR) · airframe 51,454 hrs · 32,383 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR AFT FRAME CRACKED AT LOWER CORNER. REPAIRED FRAME PER BAC DRAWING.

Part: BEAM — CORRODED (CARGO) · airframe 51,454 hrs · 32,383 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAMS CORRODED, BS 860, LBL 8 - RBL 8 AND BS 770, LBL 3 - RBL 8. REPAIRED BEAMS PER SWA RA NR 1-A53-2021.

Part: SLIDE — LOOSE (PAX DOOR)

FWD ENTRY DOOR EVACUATION SLIDE GIRT SKIRT HANGING DOWN. REPOSITIONED SLIDE ASSY PER MM.

Part: GATE — LEAKING (SERVICE DOOR)

DIVERSION, LOUD NOISE AND VIBRATON AROUND AFT SERVICE DOOR. DURING DESCENT AT 7000 FEET, CABIN CLIMB RATE WENT TO 2000 FEET FOR ABOUT 10 SECONDS. ADJUSTED AFT SERVICE DOOR LOWER GATE. INSTALLED PRESS SEAL FILLER AROUND AFT SERVICE DOOR FWD THRESHOLD PLATE EDGE, AND REMOVED AND REPLACED AFT OUTFLOW VALVE AND PRESS RELIEF VALVES. OPS CK GOOD PER MM.

Part: SLIDE — LOOSE (PAX DOOR)

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

Part: SLIDE — LOOSE (PAX DOOR)

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

Part: SLIDE — DEPLOYED (PAX DOORWAY)

FWD ENTRY DOOR EVACUATION SLIDE INADVENTENTLY DEPLOYED. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (LT LE SLAT)

DURING SCHEDULED C2 CHECK, FOUND NR 2 L/E SLAT SKIN CRACKED BELOW OUTBOARD TRACK CUT OUT. REPAIRED SKIN PER SWA RA NR1-A57-0691.

Part: HTD LINES — LEAKING (NLG)

AIR TURNBACK, NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. FOUND NOSE LANDING GEAR LOCK ACTUATOR HYD LINES LEAKING. REMOVED AND REPLACED 2 EACH LINES PER MM. OPS CHECKED GOOD. P/N'S BACH8B04NN0166T AND 97934B04EE0207T.

Part: SLIDE — LOW PRESSURE (PASSENGER DOOR)

AFT ENTRY EVACUATION SLIDE PRESS LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: BATTERY — DISCHARGED (CABIN)

DURING PRE-FLIGHT CHECK, FOUND FWD I/B EMER FLASHLIGHT INOP. REPLACED BATTERY PER BOEING M/M.

Part: SLIDE BOTTLE — LOW (CABIN DOOR)

DURING SCHEDULED RON CHECK, FOUND EMERGENCY EVAC, FWD SLIDE BOTTLE LOW. REMOVED AND REPLACED PER BOEING MM.

Part: SKIN — CRACKED (WS 312)

DURING SCHEDULED C-3 CHECK, FOUND CRACK INBD WS 213 BETWEEN KRUEGER FLAPS. REPAIRED PER SWA RA 1-357-0503.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED 1/2 D CHECK, FOUND FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP\N\NREPLACED BATTERY PACK PER BOEING M/M

Part: FLOORBEAM — CORRODED (BS 967)

DURING SCHEDULED 1/2 D-CHECK, FOUND BS 967 FLOORBEAM CORRODED. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CRACKED (BS 312)

DURING BC1 CHECK, FOUND FLOORBEAM LOWER STABILIZER CRACKED AT BS 312, LBL 11.1. REPAIRED PER BOEING SRM.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED RON CHECK, FOUND MID CABIN FLOOR TRACK LIGHTING INOP FROM ROW 19 TO 23. REPLACED BATTERY PACK PER BOEING M/M.