N301SW

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,913 hrs · 71,048 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 742C, STR 14R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,965 hrs · 70,331 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 21L. REPAIRED SKIN PER SWA EA.

Part: STRINGER — CORRODED (BS 480-492) · airframe 72,278 hrs · 69,852 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 28R CORRODED BETWEEN BS 480 AND BS 492. REPAIRED STRINGER PER SRM.

Part: STRINGER — CORRODED (BS 500 S27R) · airframe 72,278 hrs · 69,852 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 27R CORRODED AT BS 500. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,063 hrs · 69,619 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 865, STR 20L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,063 hrs · 69,619 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 900, STR 22R. REPAIRED SKIN PER SWA EA.

Part: SKIN — PUNCTURED (SPOILER) · airframe 72,714 hrs · 69,373 cycles

DURING SCHEDULED SERVICE CHECK, FOUND NR 4 GROUND SPOILER PUNCTURED AT UPPER SURFACE. REMOVED AND REPLACED SPOILER ASSY PER MM.

Part: SKIN — CRACKED (BS 714 S10R) · airframe 72,664 hrs · 69,330 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 714, STR 10R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 714 S10L) · airframe 72,664 hrs · 69,330 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 714, STR 10L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 506D S8L) · airframe 72,241 hrs · 68,997 cycles

FUSELAGE SKIN CRACKED AT BS 506D, STR 8L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,704 hrs · 68,582 cycles

FUSELAGE SKIN CRACKED AT BS 390, STR 18L. REPAIRED SKIN PER SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 70,751 hrs · 67,692 cycles

DURING SCHEDULED PM CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 4 DEF. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,160 hrs · 67,349 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 940, STR 22L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,871 hrs · 67,115 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 733, STR 14L. REPAIRED SKIN PER SWA EA AND SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,871 hrs · 67,115 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 678, STR 10L. REPAIRED SKIN PER SWA EA AND SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,871 hrs · 67,115 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 845, STR 15L. REPAIRED SKIN PER SWA EA AND SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,331 hrs · 66,702 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD CABIN LOWER EMERGENCY EXIT SIGNS INOP. R&R BATTERY PACK PER MM.

Part: SKIN — CRACKED (BS 328 S16-17L) · airframe 69,331 hrs · 66,701 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 328, BETWEEN STR 16L TO STR 17L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,331 hrs · 66,701 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 503D S12R) · airframe 69,331 hrs · 66,701 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503D, STR 12R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,331 hrs · 66,701 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT RT WING L/E SCANNING LIGHT CUTOUT, FWD UPPER CORNER. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 454) · airframe 69,331 hrs · 66,701 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 454, BL 0. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 505) · airframe 69,331 hrs · 66,701 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 505, STR 16L. REPAIRED SKIN PER SRM.

Part: STRINGER — CRACKED (BS 360) · airframe 69,331 hrs · 66,701 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 360, STR 15L. REPAIRED STRINGER PER SRM.

Part: WEB — CRACKED (BS 665) · airframe 69,331 hrs · 66,701 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BEADED WEB CRACKED AT BS 665, LBL 40. REPAIRED WEB PER SWA EA.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,331 hrs · 66,701 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. RECHARGED BATTERY PACK PER MM.

Part: DOUBLER — CORRODED (BS 513) · airframe 69,331 hrs · 66,701 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN INTERNAL DOUBLER CORRODED AT BS 513, RBL 26. REPAIRED SKIN PER SWA EA.

Part: FLOOR SUPPORT — CORRODED (BS 733D-794) · airframe 69,331 hrs · 66,701 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMP LONGITUDINAL FLOOR SUPPORT CORRODED BETWEEN BS 733D - BS 794, LBL 8. REPAIRED LONGITUDINAL FLOOR SUPPORT PER SWA EA.

Part: DOUBLER — CRACKED (BS 987) · airframe 69,331 hrs · 66,701 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN DOUBLER CRACKED AT L2 DOOR UPPER AFT CUT OUT, BS 987, STR 8L. REPAIRED SKIN DOUBLER PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 69,331 hrs · 66,701 cycles

DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM CORRODED AT BS 500D, STR 27L. REPAIRED KEEL BEAM PER SWA EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 69,159 hrs · 66,582 cycles

DURING SCHEDULED C3 CHECK, FOUND LH WING OUTBD T/E AFT FLAP DELAMINATED AT INBD END. R&R FLAP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,159 hrs · 66,582 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT GALLEY EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SKIN — CRACKED (BS 780) · airframe 65,332 hrs · 63,597 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 780, BETWEEN STR 17L TO STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 500B) · airframe 68,681 hrs · 66,215 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500B, STR 17L. REPAIRED SKIN PER SWA EA AND SRM.

Part: LIGHT — WORN (CABIN) · airframe 68,024 hrs · 65,706 cycles

DURING SCHEDULED A2 CHECK, FOUND EEPLS STRIP WORN BETWEEN ROW 5 TO ROW 7. REMOVED AND REPLACED STRIP PER MM.

Part: SKIN — CRACKED (BS 778) · airframe 67,587 hrs · 65,358 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 778, STR 20R. REPAIRED SKIN PER SWA EA & SRM.

Part: DOOR — STIFF (L1) · airframe 67,410 hrs · 65,228 cycles

L1 DOOR HARD TO OPEN OR CLOSE. ADJUSTED DOOR PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 67,177 hrs · 65,025 cycles

DURING SCHEDULED C1 CHECK, FOUND 2 EMERGENCY BULLNOSE LIGHT LENSES LOOSE AT ROW 8 DEF AND ROW 16 ABC. SECURED BOTH LIGHT LENSES PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,177 hrs · 65,025 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727C, STR 14R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,177 hrs · 65,025 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 934, STR 25L. REPAIRED SKIN PER SWA EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 67,177 hrs · 65,025 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE WEB CRACKED AT AFT PRESSURE BULKHEAD, BS 1016, STR 6R. REPAIRED AFT PRESSURE BULKHEAD WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,177 hrs · 65,025 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 687, STR 10L. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (AFT CABIN) · airframe 67,160 hrs · 65,003 cycles

DURING SCHEDULED SERVICE CHECK, FOUND SEVERAL LIGHT BULBS INOP AT EMERGENCY EXIT LIGHT NEAR AFT F/A STA. RELAMPED LIGHT AASY PER MM.

Part: STIFFENER — CRACKED (MLG W/W) · airframe 66,192 hrs · 64,268 cycles

DURING SCHEDULED C4 CHECK, FOUND 2 EA VERTICAL STIFFENERS CRACKED AT BS 663, LBL 4 & RBL 4. REPAIRED STIFFENERS PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,192 hrs · 64,268 cycles

DURING SCHEDULED C4 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS BETWEEN BS 312 & BS 317, BETWEEN STR 18R & STR 19R. REPAIRED SKIN PER SWA EA & SRM.

Part: SPOILER — DELAMINATED (RT WING) · airframe 66,192 hrs · 64,268 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING NR 8 SPOILER DELAMINATED. REMOVED AND REPLACED NR 8 SPOILER PER MM.

Part: SPOILER — DELAMINATED (RT WING) · airframe 66,192 hrs · 64,268 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING NR 6 SPOILER DELAMINATED. REMOVED AND REPLACED NR 6 SPOILER PER MM.

Part: SKIN — CRACKED (L/E SLAT) · airframe 66,192 hrs · 64,268 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING NR 4 L/E SLAT INBOARD & OUTBOARD AUX TRACK CUTOUTS CRACKED. REPAIRED SLAT PER SWA EA & SRM.

Part: SPOILER — DELAMINATED (RT WING) · airframe 66,192 hrs · 64,268 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING NR 9 SPOILER DELAMINATED. REMOVED AND REPLACED NR 9 SPOILER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,121 hrs · 64,203 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 269, STR 16R. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,121 hrs · 64,203 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 939, BETWEEN STR 21R TO STR 22R. REPAIRED SKIN PER SWA EA.

Part: VALVE — LEAKING (NR 2 ENGINE) · airframe 65,443 hrs · 63,672 cycles

AIR TURNBACK, DURING CLIMB NR 2 ENGINE DRIVEN HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED, WITH LOSS OF SYSTEM-B HYDRAULIC FLUID. REMOVED AND REPLACED NR 2 T/R SHUTTLE VALVE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,436 hrs · 62,877 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 500C, STRINGER 14L, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,417 hrs · 62,863 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 914, STRINGER 23R, CRACKED. REPAIRED SKIN PER EA AND SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 64,414 hrs · 62,860 cycles

DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,211 hrs · 62,693 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 935, STR 21L, CRACKED. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 63,577 hrs · 62,169 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT LENS AT ROW 20 ABC, LOOSE. SECURED LIGHT LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,467 hrs · 62,088 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT RIGHT EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,467 hrs · 62,088 cycles

DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT AT ROW 19 DEF, INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM.

Part: UPLOCK SENSOR — FAULTY (RT MLG) · airframe 63,261 hrs · 61,920 cycles

LEFT MLG RED LIGHT FLICKERED AND THEN REMAINED STEADY AFTER GEAR RETRACTION. CYCLED GEAR, NO HELP. LIGHT WENT OUT AFTER 30 MINUTES. RIGHT MLG UPLOCK SENSOR RESISTANCE OUT OF RANGE. REMOVED AND REPLACED RIGHT MLG UPLOCK SENSOR.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 63,133 hrs · 61,815 cycles

DURING SCHEDULED A2 CHECK, FOUND FWD BULLNOSE EMERGENCY LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,087 hrs · 61,776 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 932, STRINGER 21R, BS 941, STRINGER 22R, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,587 hrs · 61,342 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 957, STR 22L. REPAIRED SKIN PER SRM.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 62,043 hrs · 60,912 cycles

FWD UPPER EMERGENCY FLASHLIGHT RED LED DOES NOT BLINK. REMOVED AND REPLACED UPPER FLASHLIGHT AND BATTERY PACK ASSEMBLY.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 61,604 hrs · 60,560 cycles

DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM.

Part: LENS — MISSING (CABIN) · airframe 61,604 hrs · 60,560 cycles

DURING SCHEDULED C3 CHECK, FOUND EMERGENCY BULLNOSE LIGHT LENS MISSING AT ROW 6 ABC. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,604 hrs · 60,560 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 269, ABOVE STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,062 hrs · 60,120 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 764, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,062 hrs · 60,120 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR FWD LOWER CUTOUT. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CORRODED (CABIN FLOOR) · airframe 61,062 hrs · 60,120 cycles

DURING SCHEDULED D CHECK, FOUND AFT CABIN FLOORBEAMS CORRODED AT BS 986, AND BS 1016. REPAIRED FLOORBEAMS PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,062 hrs · 60,120 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, RBL 67, WL 206. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FLOORBEAM — CRACKED (AFT CARGO COMP) · airframe 61,062 hrs · 60,120 cycles

DURING SCHEDULED D CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, WL 208 AND LBL 46. REPAIRED FLOORBEAM PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,062 hrs · 60,120 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, BETWEEN STR 22R AND STR 23R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,062 hrs · 60,120 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED (3 EA) BS 277 AT STR 15R, BS 807 AT STR 26R AND BS 727B AT STR 18L. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,062 hrs · 60,120 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED (2 EA) BS 277, BETWEEN STR 14R AND STR 16R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 61,062 hrs · 60,120 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CORRODED AT BS 984, STR 25R. REPAIRED STRINGER PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 61,062 hrs · 60,120 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 827, STR 20L. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,062 hrs · 60,120 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 20L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: FITTING — CORRODED (TAIL) · airframe 61,062 hrs · 60,120 cycles

DURING SCHEDULED D CHECK, FOUND HORIZ STAB CENTER SECTION AFT SPAR LT/RT AFT LUGS CORRODED. REPAIRED AFT LUGS PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 61,062 hrs · 60,120 cycles

DURING SCHEDULED D CHECK, FOUND BULKHEAD TO KEEL BEAM STIFFENERS CRACKED (2 EA) BS 727, WL 151 BOTH LBL 6 AND RBL 6. REMOVED AND REPLACED STIFFENERS PER SRM.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 61,062 hrs · 60,120 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,062 hrs · 60,120 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,062 hrs · 60,120 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 13L. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,062 hrs · 60,120 cycles

DURING SCHEDULED D CHECK, FOUND BS 947, FUSELAGE FRAME CORRODED AT WL 210, RBL 45. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,062 hrs · 60,120 cycles

DURING SCHEDULED D CHECK, FOUND BS 480, FUSELAGE SHEAR TIE CORRODED AT STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,062 hrs · 60,120 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303.9, STR 16L. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,062 hrs · 60,120 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED, BS 907, LBL 3 TO RBL 3. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,062 hrs · 60,120 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED, BS 767, STR 13R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,062 hrs · 60,120 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, BETWEEN STR 14L AND STR 15L. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,062 hrs · 60,120 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 907, WL 162 AND RBL 3. REPAIRED FRAME PER SRM.

Part: SKIN — DELAMINATED (L/E SLAT) · airframe 61,062 hrs · 60,120 cycles

DURING SCHEDULED D CHECK, FOUND NR 4 L/E SLAT DELAMINATED ON UPPER SURFACE OUTBD END. REPAIRED NR 4 L/E SLAT PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,062 hrs · 60,120 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 9L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,062 hrs · 60,120 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED (4 EA) BS 500C AT STR 10R, BS 500C AT STR 5L, BS 500D AT STR 8L AND BS 727B AT STR 7R. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,062 hrs · 60,120 cycles

DURING SCHEDULED D CHECK, FOUND BOTH LEFTH AND RIGHT STUB FRAMES CRACKED AT BS 188, WL 207. REMOVED AND REPLACED STUB FRAMES PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,062 hrs · 60,120 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED (4 EA) BS 747 AT STR 22L, BS 747 AT STR 24L, BS 727E AT STR 24L AND BS 907 AT STR 23L. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 60,736 hrs · 59,834 cycles

DURING SCHEDULED C2 CHECK, FOUND RT OUTBD AFT T/E FLAP DELAMINATED AT INBD END LOWER SURFACE. REMOVED AND REPLACED RT OUTBD AFT T/E FLAP PER MM.

Part: MOTOR — FAILED (FLAP DRIVE) · airframe 59,913 hrs · 59,189 cycles

AFTER PUSHBACK T/E FLAPS WOULD NOT FULLY EXTEND, CABIN CREW REPORTED NOISE RT OVERWING. REMOVED AND REPLACED FLAP DRIVE MOTOR AND FLAP DRIVE UNIT PER MM.

Part: DRIVE GEAR — WORN (LT MLG WW) · airframe 59,871 hrs · 59,152 cycles

DURING APPROACH T/E FLAPS INDICATED SPLIT, WOULD NOT DEPLOY OR RETRACT. REMOVED AND REPLACED SHAFT DRIVE ASSY FOR LT WING T/E FLAPS PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 59,843 hrs · 59,129 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BS 1016 BULKHEAD CRACKED (5 EA) AT THE 12, 1 AND 3 O`CLOCK POSITIONS RADIATING FROM RIVETS AT THE PERIPHERY OF THE PRESS PLUG. REPAIRED BULKHEAD PER SWA EA AND SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 59,843 hrs · 59,129 cycles

DURING SCHEDULED C1 CHECK, FOUND BS 1016 BULKHEAD CRACKED AT LOWEST FASTENER ON STR 5R. REPAIRED BULKHEAD PER SRM.

Part: SKIN — CRACKED (L/E SLAT) · airframe 59,840 hrs · 59,128 cycles

DURING SCHEDULED C1 CHECK, FOUND NR 6 L/E SLAT LOWER SKIN CRACKED AT AFT FASTENERS 17 INCHES FROM OTBD END. REPAIRED SLAT PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,840 hrs · 59,128 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510, ABOVE STR 16L. REPAIRED SKIN PER SRM.

Part: BUSHING — WORN (LT ELEVATOR) · airframe 59,187 hrs · 58,592 cycles

DURING SCHEDULED C4 CHECK, SWA SI 11139-55, FOUND LT ELEVATOR TAB INBD ATTACH POINT WORN. REMOVED AND REPLACED HARDWARE AND BUSHING AT INBD HINGE ATTACH POINT PER MM.

Part: SKIN — CRACKED (FWD SVC DOOR) · airframe 58,964 hrs · 58,426 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR SKIN CRACKED AT BOTH UPPER AND LOWER HINGE ATTACH POINTS. REMOVED AND REPLACED FWD SVC DOOR PER MM.

Part: BUSHING — WORN (LT ELEVATOR) · airframe 58,959 hrs · 58,420 cycles

DURING SCHEDULED C4 CHECK, SWA SI 11139-55,FOUND LT ELEVATOR TRIM TAB WORN AT INBD HINGE POINT. REMOVED AND REPLACED BUSHING AT INBD HINGE POINT PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 58,049 hrs · 57,690 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 13L AND STR 14L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: RUDDER — DELAMINATED (VERTICAL STAB) · airframe 58,049 hrs · 57,690 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND RUDDER DELAMINATED AT FIN WL 96. REMOVED AND REPLACED RUDDER PER MM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 58,049 hrs · 57,690 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME DOUBLER CRACKED AT BS 727, STR 10R. REPAIRED FRAME DOUBLER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,041 hrs · 57,683 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIPS CRACKED (8 EA) AT BS 605 AT STR 2R, BS 706 AT STR 4R, BS 685 AT STR 4R, BS 360 AT STR 9R, BS 500 AT STR 4L, BS 663 AT STR 4L, BS 616 AT STR 5L AND BS 597 AT STR 9L. REMOVED AND REPLACED STR TIE CLIPS PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 58,041 hrs · 57,683 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIES CRACKED (2 EA) AT BS 360, STR 14L AND STR 14R. REMOVED AND REPLACED SHEAR TIES PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 58,041 hrs · 57,683 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STR SPLICES CRACKED (3 EA) AT STR 4L, BS 360, BS 727 AND BS 908. REMOVED AND REPLACED STR SPLICES PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,031 hrs · 57,674 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT UPPER CORNER OF R-1 COCKPIT WINDOW. REPAIRED SKIN PER SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 58,031 hrs · 57,674 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BEADED PRESSURE WEB CRACKED AT BS 665, RBL 41. REPAIRED PRESS WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,031 hrs · 57,674 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 727E PLUS 6, ABOVE STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,031 hrs · 57,674 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) ABOVE STR 10L, BS 520 PLUS 5 AND BS 500C PLUS 13. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,031 hrs · 57,674 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 510, ABOVE STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,980 hrs · 57,634 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) 2 ABOVE LAP AT STR 10L, BS'S 500 AND 500B PLUS 5. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,805 hrs · 57,483 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 760, STR 18R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,805 hrs · 57,843 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACK AT BS 760, STR 18R. REPAIRED SKIN PER SRM.

Part: BUSHING — WORN (BOTH ELEVATORS) · airframe 57,349 hrs · 57,110 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, ELEVATOR TABS FAILED FREE PLAY INSPECTION. REMOVED AND REPLACED BOTH LT AND RT TAB CONTROL ROD BUSHINGS PER MM.

Part: SLIDE — OUT OF ADJUST (FWD ENTRY DOOR) · airframe 57,113 hrs · 56,938 cycles

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

Part: BATTERY — DISCHARGED (CABIN) · airframe 56,336 hrs · 56,301 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EXIT LIGHTS DIMMED. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,229 hrs · 56,220 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED 2 INCHES LONG AT BS 460, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,229 hrs · 56,220 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED 2 INCHES LONG AT BS 360, STR 15L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,229 hrs · 56,220 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 770, STR 14R AND BS 740, STR 17R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,229 hrs · 56,220 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED 2 INCHES LONG AT BS 500, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,998 hrs · 56,041 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKEDAT BS 270, 16 INCHES ABOVE FLOOR LINE. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 55,707 hrs · 55,800 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,963 hrs · 55,207 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED ( 2 EA ) BOTH 3 INCHES LONG AT BS 500 & BS 500B, STR 10R. REPAIRED SKIN PER SWA RA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,963 hrs · 55,207 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 19R. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,450 hrs · 54,773 cycles

DURING SCHEDULED A1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,307 hrs · 54,636 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKINS CRACKED AT BS 500B, STR 10R & BS 360, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,307 hrs · 54,636 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 940, STR 23R. REPAIRED STR PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,105 hrs · 54,481 cycles

DURING SCHEDULED RON CHECK, ON WALK AROUND INSPECTION FOUND FUSELAGE SKIN CRACKED AT BS 500+5, STR 10R. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,934 hrs · 54,337 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,404 hrs · 53,901 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACK AT BS 343, ABOVE STR 17L. REPAIRED SKIN PER BFG ER.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 53,404 hrs · 53,901 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT KEEL BEAM CORRODED ON OUTBD FLANGE, BS 708 TO BS 727. REPAIRED KEEL BEAM OUTBD FLANGE PER BFG ER.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,404 hrs · 53,901 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 1006, BETWEEN STR 20L & 21L. REPAIRED FRAME PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 53,404 hrs · 53,901 cycles

DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM CORRODED AT BS 500D, LT SIDE. REPAIRED KEEL BEAM PER BFG ER.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 53,404 hrs · 53,901 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAM WEBS CRACKED AT LBL 17.1, WL 230 & RBL 17.1, WL 182. REMOVED AND REPLACED BEAM WEB PER BFG ER.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 53,404 hrs · 53,901 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 2 BS 178 BULKHEAD WEB CRACKS AT RBL 5.0 TO RBL 6.0, WL 212 TO WL 213. REPAIRED BULKHEAD PER SRM.

Part: LENS — BROKEN (CABIN) · airframe 53,404 hrs · 53,901 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT ENTRY DOOR EMERGENCY LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: SPLICE PLATE — CRACKED (BULKHEAD) · airframe 53,404 hrs · 53,901 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD SKIN SPLICE PLATE CRACKED AT LBL 4, WL 242. REPAIRED SKIN SPLICE PER BFG ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,404 hrs · 53,901 cycles

DURING SCHEDULED 1/4D CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT AFT SVC DOOR CUTOUT, BS 960, RBL 70, WL 210. REPAIRED SKIN PER SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 53,404 hrs · 53,901 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FITTING CRACKED AT BS 727, LBL 19, WL 201. REMOVED AND REPLACED FITTING PER SRM.

Part: FRAME — CRACKED (SVC DOOR) · airframe 53,404 hrs · 53,901 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR AFT FRAME CRACKED AT NR 3 & 4 STOP FITTINGS. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,404 hrs · 53,901 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD AFT SIDE VERTICAL CHORD CRACKED AT LBL 5.7, WL 184 TO WL 188. REMOVED AND REPLACED VERTICAL CHORD PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,349 hrs · 53,859 cycles

DURING SCHEDULED C2 CHECK, FOUND 2.36 EXTERNAL FUSELAGE SKIN CRACK AT AFT SVC DOOR LOWER FWD CUTOUT. REPAIRED SKIN PER SRM.

Part: SPOILER — DELAMINATED (LT WING) · airframe 53,349 hrs · 53,859 cycles

DURING SCHEDULED C2 CHECK, FOUND NR 3 SPOILER UPPER SKIN DELAMINATED ABOVE THE ACTUATOR RECESS. REMOVED AND REPLACED SPOILER PER MM.

Part: RADAR — INOPERATIVE (E/E BAY) · airframe 53,045 hrs · 53,615 cycles

DIVERSION, CREW REPORTED WEATHER RADAR INOP. DUE TO DESTINATION WEATHER, DIVERTED TO LAS. REMOVED AND REPLACED WEATHER RADAR R/T UNIT PER MM. OPS CHECK GOOD.

Part: SLIDE — OUT OF POSITION (FWD ENTRY) · airframe 53,023 hrs · 53,598 cycles

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

Part: SLIDE — OUT OF POSITION (FWD PAX DOOR) · airframe 52,957 hrs · 53,544 cycles

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

Part: SLIDE — OUT OF POSITION (FWD PAX DOOR) · airframe 52,957 hrs · 53,544 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,919 hrs · 53,507 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 500D, STR 15R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,919 hrs · 53,507 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK BETWEEN BS 727E & BS 747, STR 17R & STR 18R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 52,599 hrs · 53,236 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE CAUGHT ON SIDE OF AIRCRAFT WHILE DOOR WAS BEING CLOSED & SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: COVER — CRACKED (CABIN) · airframe 52,440 hrs · 53,105 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS COVER CRACKED AT ROWS 23 - 24. REMOVED AND REPLACED COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,440 hrs · 53,105 cycles

DURING SCHEDULED C1 CHECK, FOUND 2 INCH LONG EXTERNAL FUSELAGE SKIN CRACK AT BS 470, ABOVE STR 10. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,268 hrs · 51,235 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, 4 EA, BETWEEN BS 495 - BS 515, STRINGER 10R. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EXTERNAL EMERGENCY LIGHT INOP. RELAMPED PER MM.

Part: SKIN — CRACKED (BS 380)

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 380, STRINGER 10R. REPAIRED SKIN PER SRM.

Part: BRACKET — LOOSE (PAX DOORWAY)

DURING SCHEDULED C1 CHECK, FOUND BOTH FWD ENTRY AND SERVICE DOOR EVACUATION SLIDE GIRT BAR ATTACH BRACKETS (FWD AND AFT) LOOSE. TIGHTENED BOTH BRACKETS PER MM.

Part: SKIN — DELAMINATED (RT TE FLAP)

DURING RON, FOUND RT WING OUTBOARD AFT FLAP DELAMINATED ON INBOARD END. REPAIRED FLAP PER SRM.

Part: SKIN — CRACKED (BS 930)

DURING RON, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 930, STRINGER 23R. REPAIRED SKIN PER SRM.

Part: ANGLE — CRACKED (RT AILERON)

DURING SCHEDULED C4 CHECK, FOUND RT WING AILERON 3RD RIB SUPPORT ANGLE CRACKED APPROX 1.5 INCH LONG. REPAIRED RIB SUPPORT ANGLE PER SWA RA NR 1-357-0729.

Part: SLIDE — DETACHED (PASSENGER DOOR)

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

Part: SENSOR — MALFUNCTIONED (NLG)

DURING LANDING, NLG UNSAFE LIGHT ILLUMINATED (ACFT DID BY-FLY TO VERIFY NLG DOWN). REMOVED AND REPLACED NLG SENSOR PER MM.

Part: SWITCH — DIRTY (NLG)

RED NOSE LANDING GEAR LIGHT ILLUMINATED AND STAYED ON AFTER GEAR RETRACTION. LANDING GEAR CYCLED TO OFF/DOWN/UP. LIGHT EXTINGUISHED AFTER SECOND RETRACTION. NOISE AND VIBRATION ACCOMPANIED RED LIGHT. INSPECTED NOSE GEAR, CLEANED NOSE GEAR POSITION SWITCHES.

Part: SKIN — CRACKED (BS 757)

DURING SCHEDULED CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 757, S14R. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER PER BOEING SRM 53-00-01 FIG 202.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED 1/2D-CHECK, FOUND CRACK INDICATION AT BS 178 BULKHEAD WEB AT WL 218 AND RBL 11 AT RADAR SUPPORT. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND EDDY CURRENT REVEALS CRACKED FWD SIDE OF BULKHEAD, LBL 5 WL 188.5. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 986.5)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM AFT FLANGE AT BS 986.5, LBL 9. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CRACKED (BS 663)

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED UPPER CHORD OF FLOORBEAM AT BS 663 BL 0. REPAIRED PER BOEING SRM.

Part: STRINGER — MISREPAIRED (BS 520)

DURING SCHEDULED 1/2D CHECK, FOUND BLIND RIVETS INSTALLED AT BS 520 STR 11-12 LEFT PREVIOUS PATCH REPAIR ON UPPER LOBE. REMOVED AND REPLACED PREVIOUS REPAIR PER BOEING SRM.

Part: SKIN — CRACKED (BS 213)

DURING SCHEDULED BC3 CHECK, FOUND L/E BS 213 KRUEGER FLAP CUTOUT CRACKED APPROX .625 IN LENGTH. REPAIRED PER SWA ACO 6820-57.

Part: FLOORBOARD — CORRODED (BS 767-847)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT BS 767-847 LBL 8 AROUND FLOORBOARDS HOLES. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 727)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AROUND NUT PLATE HOLE ON FLOORBEAM RBL 8, BS 727E + 2. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (RT WING)

DURING SCHEDULED 1/2D CHECK, FOUND ANGLE CRACKED AT AILERON MIDDLE HINGE WBL 494. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 767-847)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT BS 767-847, RBL 13 AROUND TIE DOWNS FLOORBOARDS HOLES ON FLOORBEAM. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 522)

DURING SCHEDULED 1/2D CHECK, FOUND 1.25 INCH CRACK, FUSELAGE SKIN AT BS 522 LBL 5. REPAIRED PER BOEING SRM.

Part: CHORD — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED RT SIDE CHORD AT BS 178 RBL 32 WL 207. REMOVED AND REPLACED PER BOEING SRM.

Part: SUPPORT — CRACKED (RT WING)

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED SUPPORT CHANNEL ON PANEL I/B OF NR 5 GROUND SPOILER. REPAIRED PER BOEING SRM.

Part: FLOORBOARD — CORRODED (BS 767-847)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT BS 767-847, LBL 3 AROUND FLOORBOARDS HOLES. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 847-947)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT BS 847-947 FLOORBEAM, RBL 13 AROUND TIE DOWNS AND FLOORBOARD HOLES. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 847-947)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT BS 847-947 RBL 7 LBL 12 AROUND FLOORBOARD HOLES. REPAIRED PER BOEING SRM.

Part: STRAP — CRACKED (BS 202 & 204)

DURING SCHEDULED 1/2D CHECK, FOUND 2 CRACKS UNDER VERTICAL STRAP LBL 5, WL 202 AND 204. ALSO AT RBL 5, WL 202 AND 204 AT FWD SIDE. REPAIRED PER SWA RA NR 1-353-1864.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED INDICATIONS AT BS 178 BULKHEAD WEB, LBL 5.7 AND WL 211. REPAIRED PER SWA RA NR 1-353-1864.

Part: FLOORBEAM — CORRODED (BS 1016)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FLOORBEAM FWD FLANGE AT BS 1016 RBL 11. REPAIRED PER SWA RA NR 1-353-1864.

Part: STRINGER — CORRODED (BS 500)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION BELOW STR 28R AT BS 500C + 10. REPAIRED PER SWA RA NR 13531864.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND 4 INDICATIONS OF CRACKS FROM 3 FASTENER HEADS IN FWD SIDE OF BLKHD WL 234 LBL 9. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED AT BS 178 BULKHEAD, WL 207, LBL 11. REPAIRED PER SWA RA NR 1-353-1864.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED INDICATIONS AT BS 178 BULKEHAD WL 207 IN WEB BENEATH SUPPORT ANGLE AT RBL 1 WL 207 LBL 1 IN WEB BENEATH SUPPORT. REPAIRED PER SWA RA NR 13531864.

Part: WEB — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED WEB AT BS 178 WL 218 LBL 11. REPAIRED CUTOUT DAMAGED PER SWA RA NR 13531864.

Part: INTERCOSTAL — CORRODED (BS 967-986.5)

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

Part: ANGLE — CRACKED (BS 727)

DURING SCHEDULED 1/2D CHECK, FOUND WING TO BODY SUPPORT T-ANGLE FWD END CRACKED AT BS 727. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 927-947)

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED WEB UPPER ANGLE AT BS 927 TO 947 BL 0. REMOVED AND REPLACED PER BOEING SRM.

Part: SHEAR TIE — CRACKED (BS 1121)

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED SHEAR TIE AT BS 1121, LT INSIDE LIGHTENING HOLE APU CAVITY. REPAIRED PER BOEING SRM.

Part: WEB — CORRODED (BS 988)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED WEB FLOOR LEVEL AT BS 988, RBL 42. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — WORN (RT WING)

DURING SCHEDULED 1/2D CHECK, FOUND ANGLE HAS WASHER WORN THRU JUST I/B OF I/B FOREFLAP. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 986.5-1006)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED INTERCOSTAL AT BS 986.5 TO 1006 BL 0. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 767-847)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM AROUND FLOORBOARD HOLES AT BS 767 TO 847. REPAIRED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 948-990)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED RT Z-ANGLE AT BS 948 TO 990. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBOARD — CORRODED (BS 727-947)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED SURFACE AND FLOORBOARD HOLES LEFT TRANSITION ANGLE AT BS 727E-947. REPAIRED PER BOEING SRM.

Part: WEB — CORRODED (BS 1016)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED WEB AFT FROM 1016 FLOORBEAM RT SIDE. REPAIRED PER BOEING SRM.

Part: ANGLE — CORRODED (GALLEY)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED LT Z ANGLE AROUND CLIP NUT HOLES. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — WORN (BS 300)

DURING SCHEDULED 1/2D CHECK, FOUND WEB FWD OF DOOR FRAME AT BS 300 BELOW STR 13 WORN. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 727)

DURING SCHEDULED 1/2D CHECK, FOUND RT TRANSITIONAL ANGLE CRACKED AT BS 727C. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 950)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED INTERCOSTAL AT BS 950, RBL 31 TO RBL 47. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 1006 & 1016)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED INTERCOSTAL BETWEEN BS 1006 AND 1016 LBL 37. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 727)

DURING SCHEDULED 1/2D CHECK, FOUND CLIP CRACKED BELOW RT TRANSITION ANGLE AFT AT BS 727A BELTFRAME. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND WEB CRACKED AT BS 178, RBL 32, WL 207. REMOVED AND REPLACED PER BOEING SRM.

Part: CLIP — CRACKED (BS 500)

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 24L. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — BROKEN (CARGO COMPT)

DURING SCHEDULED 1/2D CHECK, FOUND O/B FLANGE OF RT CARGO TRACK AT TIE DOWN BROKEN OFF. REPAIRED FLOORBEAM PER BOEING SRM.

Part: BAFFLE — CRACKED (BS 500)

DURING SCHEDULED 1/2D CHECK, FOUND BAFFLE CRACKED BETWEEN BS 500A AND 500B RT SIDE UNDER INTERCOSTAL. REPAIRED PER BOEING SRM.

Part: BULKHEAD ANGLE — CORRODED (BS 947)

DURING SCHEDULED 1/2D CHECK, FOUND BS 947 RBL 22 LBL 22 AFT BULKHEAD CORNER ANGLE SURFACE CORRODED AROUND FLOORBEAM HOLE. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 460-480)

DURING SCHEDULED 1/2D CHECK, FOUND BENT AND CRACKED WEB BELOW LT TRANSITION ANGLE AT BS 460 TO 480. REPAIRED PER BOEING SRM.

Part: FRAME — CORRODED (CARGO DOORWAY)

DURING SCHEDULED 1/2D CHECK, FOUND 2 STOP PADS CORRODED ON AFT FRAME DOOR CUTOUT. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 312)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED IN AND AROUND CLIP NUT HOLE AT BS 312, LBL 1 AFT LEG; BS 312 LBL 1 FWD LEG; BS 312, LBL 8, AFT LEG AND BS 312, LBL 8, FWD LEG. REPAIRED FLOORBEAM PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED INTERCOSTAL AT BS 986.5 TO 1006, LBL 13; BS 955, RBL 9-17; BS 947-967 RBL 8 AND BS 947 - 967, RBL 18. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 179)

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED WEB AT BS 179, LBL 32, WL 207. REPAIRED PER BOEING SRM.

Part: WEB — BENTED (BS 400-420)

DURING SCHEDULED 1/2D CHECK, FOUND BENT AT BS 400 TO 420 WEB BELOW RT TRANSITION ANGLE. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 757)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED AROUND NUT PLATE HOLE AT FLOORBEAM, BS 757 RBL 14. REPAIRED FLOORBEAM PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 312)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED IN AND AROUND FASTENER AT BS 312, LBL 12. REPAIRED FLOORBEAM PER BOEING SRM.

Part: STRINGER — CRACKED (BS 787)

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED STRINGER AT BS 787, 21R. REPAIRED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 400)

DURING SCHEDULED 1/2D CHECK, FOUND BS 400 STRINGER CLIP 23L CRACKED. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 308.5)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED INTERCOSTAL AT BS 308.5, RBL 10.5. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 328-344)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED INTERCOSTAL AT BS 328 TO 344 LBL 10. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

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

Part: ANGLE — CRACKED (GALLEY DOORWAY)

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED L ANGLE JUST BELOW STR 12R FWD OF FWD GALLEY DOOR. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (CARGO DOORWAY)

DURING SCHEDULED C4 CHECK, FOUND CRACKED AFT CARGO DOOR FRAME INSIDE DOOR FWD OF AFT I/B STOP. REMOVED AND REPLACED PER BOEING MM.

Part: FRAME — CORRODED (BS 986)

DURING SCHEDULED C4 CHECK, FOUND CORRODED BELL FRAME CLIP AT BS 986 STR 17R. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (CARGO DOORWAY)

DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR UPLOCK INTERCOSTAL CRACKED. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING WALKAROUND CHECK, FOUND CRACKED 3 FUSELAGE SKIN AT RT SIDE APPROX 18 FT AFT OF WING ILLUMINATION LIGHT. REMOVED AND REPLACED PER BOEING SRM.

Part: SLIDE — OUT OF DATE (FWD SERV DOOR)

DURING SCHEDULED A1 CHECK, FOUND FWD SERVICE DOOR SLIDE OUT OF DATE. REMOVED AND REPLACED SLIDE PER BOEING M/M.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN FLOOR TRACK LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M.

Part: SKIN — CRACKED (BS 767)

DURING SCHEDULED SERVICE CHECK, FOUND A 2 INCH FUSELAGE SKIN CRACK AT BS 767, WL 200. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 727/747)

DURING SCHEDULED TERM CHECK, FOUND A 3.5 INCH CRACK ON OUTER SKIN RT SIDE OF FUSELAGE, BETWEEN BS 747 AND BS 727R, AT S18R. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 780)

DURING SCHEDULED TERMINAL CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 780, AT S20R. REPAIRED PER BOEING SRM.

Part: SHEAR TIE — CORRODED (BS 807)

DURING SCHEDULED CHECK, FOUND AFT CARGO BELT FRAME AT BS 807 HAS CORRODED SHEAR TIE BETWEEN S27 AND 26R. REPLACED PER BOEING SRM.

Part: DOOR FRAME — CRACKED (FWD SERVICE DOOR)

DURING SCHEDULED 1/4 D-CHECK, FOUND FWD SERVICE DOOR FRAME CRACKED AT FWD UPPER LOCK CAM PLATE. REPLACED PER BOEING SRM.

Part: CONTROL UNIT — MALFUNCTION (ANTI-SKID SYST)

AFTER TAKEOFF, MAIN GEAR BRAKE ANTI-SKID INOP LIGHT FLICKERED MOMENTARILY, THEN REMAINED ILLUMINATED. AIRCRAFT RETURNED TO OAK AND MADE AN UNEVENTFUL LANDING. REPLACED ANTI-SKID CONTROL UNIT PER BOEING MM.

Part: SKIN — CRACKED (LT FUS)

DURING SCHEDULED A-CHECK, FOUND FUSELAGE SKIN CRACK BETWEEN PASSENGER WINDOWS 11 AND 12. THE CRACK MEASURED 3 INCHES IN LENGTH AND APPROX CENTERED IN THE SKIN PANEL BETWEEN WINDOWS JUST BELOW S12L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED A2 CHECK, FOUND 3 INCH FUSELAGE SKIN CRACK BELOW S12L AND FORWARD OF WINDOW NUMBER 12. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — CRACKED (BS 935)

DURING SCHEDULED A2 CHECK, FOUND 2.275 INCH FUSELAGE SKIN CRACK AT BS 935, BETWEEN S24 AND 25R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.