N672SW

Part: VALVE — FAULTY (A/C BAY) · airframe 70,927 hrs · 60,479 cycles

CABIN ALTITUDE HORN SOUNDED. PLACED PACKS ON HIGH RAN EMERGENCY DESCENT CHECKLIST. R&R HIGH STAGE VALVE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,911 hrs · 60,465 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 518D, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,896 hrs · 60,454 cycles

FUSELAGE SKIN CRACKED AT BS 700, STR 10L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,896 hrs · 60,454 cycles

FUSELAGE SKIN CRACKED AT BS 583, STR 10L. REPAIRED SKIN PER SWA EA.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 70,208 hrs · 59,929 cycles

DURING SCHEDULED A1 CHECK, AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FITTING — CRACKED (LT WING) · airframe 70,208 hrs · 59,929 cycles

DURING SCHEDULED A1 CHECK, FOUND LT WALKING BEAM ACTUATOR FITTING CRACKED AT AFT SPAR. REMOVED AND REPLACED FITTING PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,208 hrs · 59,929 cycles

DURING SCHEDULED A1 CHECK, FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,208 hrs · 59,929 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 315, STR 24R. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,208 hrs · 59,929 cycles

DURING SCHEDULED A1 CHECK, MID CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,973 hrs · 59,746 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 1045, STR 24L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,444 hrs · 59,365 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 943, STR 24L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 69,444 hrs · 59,365 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 69,224 hrs · 59,207 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,492 hrs · 57,895 cycles

DURING SCHEDULED HOU CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 466, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,521 hrs · 57,914 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 466, STR 16R. REPAIRED SKIN PER SRM.

Part: SIGN — DISLODGED (EMERGENCY LIGHTS) · airframe 67,305 hrs · 57,745 cycles

LEFT OVERWING EMERGENCY EXIT SIGN FELL OFF. SECURED SIGN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,211 hrs · 57,669 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 516D, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 67,211 hrs · 57,669 cycles

DURING SCHEDULED MV2 CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 16R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,789 hrs · 57,339 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 735E AND BS 747, STR 18R. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,789 hrs · 57,339 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 24R. REPAIRED FRAME PER ACO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,716 hrs · 57,280 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,389 hrs · 57,031 cycles

FUSELAGE SKIN CRACKED AT BS 450, STR 16R. REPAIRED SKIN PER SRM.

Part: CABLE — MISROUTED (EVAC SLIDE) · airframe 65,971 hrs · 56,723 cycles

L2 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 65,777 hrs · 56,569 cycles

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

Part: SKIN — CRACKED (BS 736D S21L) · airframe 652,441 hrs · 56,156 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 736D, STR 21L. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 763 S19R) · airframe 652,441 hrs · 56,156 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 763, STR 19R. REPAIRED SKIN PER SWA EA & SRM.

Part: CHARGER — BROKEN (EMERGENCY LIGHT) · airframe 64,765 hrs · 55,788 cycles

DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT BATTERY CHARGER RECEPTICAL BROKEN AT OVERHEAD ROW 17. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: HOOK — BROKEN (R2 DOOR GIRT BAR) · airframe 64,445 hrs · 55,525 cycles

R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK BROKEN. REMOVED AND REPLACED EVAC SLIDE AFT GIRT BAR HOOK PER MM.

Part: SKIN — CRACKED (BS 727E S21R) · airframe 64,378 hrs · 55,472 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 21R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 845 S23L) · airframe 64,378 hrs · 55,472 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 845, STR 23L. REPAIRED SKIN PER SWA EA.

Part: ACTUATOR — SHEARED (NR 5 SPOILER) · airframe 63,759 hrs · 54,977 cycles

DURING SCHEDULED C4 CHECK, FOUND RT NR 5 GROUND SPOILER OUTBOARD ACTUATOR SHEARED. REMOVED AND REPLACED SPOILER ACTUATOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,759 hrs · 54,977 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 816, STR 23L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,759 hrs · 54,977 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 1012, STR 23R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 63,745 hrs · 54,964 cycles

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

Part: STRINGER — CRACKED (BS 598) · airframe 62,880 hrs · 54,276 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 598, STR 15L. REPAIRED STRINGER PER SRM.

Part: SKIN — CORRODED (BS 1000-1004) · airframe 62,880 hrs · 54,276 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN BEAR STRAP CORRODED BETWEEN BS 1000 TO BS 1004, STR 27R. REPAIRED SKIN PER SWA EA.

Part: STRINGER — CORRODED (BS 1006) · airframe 62,880 hrs · 54,276 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 1006, STR 26R. REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER — CORRODED (BS 500C) · airframe 62,880 hrs · 54,276 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 500C, STR 24R. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (BS 500D) · airframe 62,880 hrs · 54,276 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500D, LBL 5. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (BS 727E) · airframe 62,880 hrs · 54,276 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 727E, STR 14R. REPAIRED SHEAR TIE PER SWA EA.

Part: FRAME — CORRODED (BS 360) · airframe 62,880 hrs · 54,276 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 360, BL 0. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 616) · airframe 62,880 hrs · 54,276 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, STR 17L. REPAIRED FRAME PER SRM.

Part: GIRT BAR — CORRODED (L1 DOOR SLIDE) · airframe 62,880 hrs · 54,276 cycles

DURING SCHEDULED 1/2D CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT FLOOR FITTING CORRODED. REMOVED AND REPLACED FLOOR FITTING PER SRM.

Part: STRINGER — CORRODED (BS 365) · airframe 62,880 hrs · 54,276 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 365, STR 28L. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (BS 639) · airframe 62,880 hrs · 54,276 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 17L. REPAIRED FRAME PER SWA EA.

Part: STRINGER — CORRODED (BS 354) · airframe 62,880 hrs · 54,276 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 354, STR 16L. REPAIRED STRINGER PER SRM.

Part: STRINGER — CORRODED (BS 312) · airframe 62,880 hrs · 54,276 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 312, STR 26L. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (BS 727) · airframe 62,880 hrs · 54,276 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727, STR 14L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 500D) · airframe 62,880 hrs · 54,276 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 500D, STR 18R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 62,880 hrs · 54,276 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 579, STR 13L. REPAIRED SHEAR TIE PER SWA EA.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 62,880 hrs · 54,276 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 500D, STR 19R. REPAIRED BELTFRAME PER SWA EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 62,880 hrs · 54,276 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 597, STR 13L. REPAIRED SHEAR TIE PER SWA EA.

Part: SKIN — CRACKED (BS 732E-741E) · airframe 62,880 hrs · 54,276 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 732E TO BS 741E, STR 22L TO STR 24L. REPAIRED SKIN PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 927) · airframe 62,880 hrs · 54,276 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 927, BL 0. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER — CORRODED (BS 365) · airframe 62,880 hrs · 54,276 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 365, STR 27L. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (BS 751) · airframe 62,880 hrs · 54,276 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 751, STR 19R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,880 hrs · 54,276 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 737) · airframe 62,880 hrs · 54,276 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 19L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,880 hrs · 54,276 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT CARGO DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 753-764) · airframe 62,880 hrs · 54,276 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 753 TO BS 764, STR 19L TO STR 20L. REPAIRED SKIN PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 663) · airframe 62,880 hrs · 54,276 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (BS 764-765) · airframe 62,880 hrs · 54,276 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 764 TO BS 765, STR 19L. REPAIRED SKIN PER SWA EA AND SRM.

Part: BRACKET — CORRODED (GIRT BAR) · airframe 62,880 hrs · 54,276 cycles

DURING SCHEDULED 1/2D CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FLOOR BRACKET CORRODED. REMOVED AND REPLACED FWD BRACKET PER SRM.

Part: SKIN — CRACKED (NR 2 SLAT) · airframe 62,880 hrs · 54,276 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LEFT WING NR 2 L/E SLAT LOWER T/E SKIN CRACKED AT OUTBOARD END. REPAIRED SLAT PER SRM.

Part: SKIN — CRACKED (BS 372) · airframe 62,820 hrs · 54,219 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 372, STR 8L. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 793) · airframe 62,820 hrs · 54,219 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 793, STR 19L. REPAIRED SKIN PER SRM.

Part: OUTFLOW VALVE — FAULTY (AFT CARGO) · airframe 62,592 hrs · 54,046 cycles

AIR TURNBACK, CABIN ALTITUDE HORN SOUNDED. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER AND MAIN OUTFLOW VALVE PER MM. RESECURED AFT CARGO DOOR SEAL PER MM.

Part: FAN — FAULTY (A/C BAY) · airframe 62,412 hrs · 53,915 cycles

SMOKE ODOR IN CABIN. REMOVED AND REPLACED GASPER FAN PER MM.

Part: LINE — LOOSE (A/C BAY) · airframe 62,260 hrs · 53,797 cycles

FUMES SMELL IN FWD GALLEY. FOUND HYDRAULIC FLUID LEAK AT LINE FWD OF RT AIR CYCLE MACHINE. TIGHTENED HYDRAULIC LINE PER MM.

Part: SKIN — CRACKED (BS 941) · airframe 62,223 hrs · 53,771 cycles

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

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 61,812 hrs · 53,432 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 61,782 hrs · 53,407 cycles

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

Part: SKIN — CRACKED (BS 787) · airframe 61,782 hrs · 53,407 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 21R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 727E) · airframe 61,782 hrs · 53,407 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 24L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 767) · airframe 61,782 hrs · 53,407 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 21R. REPAIRED SKIN PER SRM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 61,552 hrs · 53,228 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT SIDEWALL LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SLIDE — OUT OF ADJUST (L1 & R1 DOOR) · airframe 60,846 hrs · 52,661 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,887 hrs · 51,896 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 23R. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,887 hrs · 51,896 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747 + 2, STR 24R. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,887 hrs · 51,896 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 19L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,887 hrs · 51,896 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 777, STR 24L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,887 hrs · 51,896 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740, STR 23L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,887 hrs · 51,896 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 980, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,887 hrs · 51,896 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515, STR 16L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,531 hrs · 51,636 cycles

DURING SCHEDULED A1 CHECK, FOUND 3 EACH FUSELAGE SKIN CRACKS AT BS 727E, STRINGER 23L AND STRINGER 19R, BS 867, STRINGER 24R. REPAIRED SKIN PER EA.

Part: SKIN — DELAMINATED (RT WING FOREFLAP) · airframe 58,951 hrs · 51,172 cycles

DURING SCHEDULED C3 CHECK, FOUND RT WING INBOARD T/E FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,840 hrs · 51,094 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 727 + 10, BELOW STRINGER 22L, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,840 hrs · 51,094 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 940, STRINGER 21L, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,840 hrs · 51,094 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 751, BELOW STRINGER 19R, CRACKED. REPAIRED SKIN PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,045 hrs · 49,662 cycles

DURING SPV, FOUND FRAME AND FRAME WEB AT BS 639, STRINGER 17R, CRACKED. REPAIRED FRAME AND FRAME WEB PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,045 hrs · 49,662 cycles

DURING SPV, FOUND STRINGER CLIPS AT BS 500C AND BS 500D, STRINGER 9L, CRACKED. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 57,045 hrs · 49,662 cycles

DURING SPV, FOUND SHEAR TIE AT BS 500C, STRINGER 16R, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 57,045 hrs · 49,662 cycles

DURING SPV, FOUND BULLNOSE EMERGENCY EXIT LIGHT AT ROW 10 DEF, LOOSE. SECURED BULLNOSE LIGHT PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,045 hrs · 49,662 cycles

DURING SPV, FOUND STRINGER 20L AT BS 727D + 4, CRACKED. REPAIRED STRINGER SECTION PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 57,045 hrs · 49,662 cycles

DURING SPV, FOUND SHEAR TIES AT BS 360, BELOW AND ABOVE STRINGER 14L, CRACKED. REMOVED AND REPLACED SHEAR TIES PER SRM.

Part: BUTTSTRAP — CRACKED (FUSELAGE) · airframe 57,045 hrs · 49,662 cycles

DURING SPV, FOUND BUTT STRAP AT BS 360, STRINGER 14L, CRACKED. REPAIRED STRAP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 57,045 hrs · 49,662 cycles

DURING SPV, FOUND SHEAR TIE AT BS 360, STRINGER 14R, CRACKED. REPAIRED SHEAR TIE PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 57,045 hrs · 49,662 cycles

DURING SPV, FOUND STRINGER SPLICES AT BS 908, STRINGER 4R AND STRINGER 4L, CRACKED. REMOVED AND REPLACED STRINGER SPLICES PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,045 hrs · 49,662 cycles

DURING SPV, FOUND STRINGER 4R AT BS 639, CRACKED. REPAIRED STRINGER PER SRM.

Part: SENSOR — FAULTY (NLG) · airframe 56,968 hrs · 49,603 cycles

NOSE GEAR UNSAFE LIGHT ILLUMINATED, CYCLED GEAR NO HELP, VISUALLY CHECK NOSE GEAR DOWN AND LOCKED. ON FINAL GOT THREE GREEN LIGHTS FOR A SHORT PERIOD THEN RED NOSE GEAR LIGHT ILLUMINATED. REMOVED AND REPLACED LOGIC CARDS AND PROX SENSOR, PER MM.

Part: CIRCUIT CARD — FAULTY (MLG) · airframe 56,961 hrs · 49,598 cycles

DECLARED EMERGENCY, UNSAFE NOSE GEAR INDICATION, CYCLED GEAR SEVERAL TIMES, WITH SAME RESULT. OBTAINED SAFE INDICATION AFTER LANDING. REMOVED AND REPLACED LOGIC CARD, ADJUSTED SENSOR AND PERFORMED INTEGRITY CHECK OF WIRING PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,946 hrs · 49,585 cycles

FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 727 + 5, BS 767 + 6, STRINGER 20L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 56,126 hrs · 48,930 cycles

DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 54,965 hrs · 47,972 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 663, LBL 30. REPAIRED WEB PER SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 54,965 hrs · 47,972 cycles

DURING SCHEDULED 1/4D CHECK, FOUND NLG W/W CEILING CRACKED AT OUTBD SIDE OF RT TIRE BRAKE ASSY. REPAIRED CEILING WEB PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,951 hrs · 47,958 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CUTOUT CRACK AT AFT ENTRY DOOR UPPER AFT CORNER. REPAIRED SKIN PER SRM AND SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,951 hrs · 47,958 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 4 EA FUSELAGE SKIN CRACKS, BS 500C+14 STR 10L, BS 500+13, STR 10R, BS 384, STR 10L, AND BS 500D+10, STR 12R. REPAIRED SKIN PER SRM.

Part: BEAM — CRACKED (CENTER WING) · airframe 54,951 hrs · 47,958 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,951 hrs · 47,958 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) ABOVE STR 10L, BS 727B PLUS 14 AND BS 727D PLUS 12. REPAIRED SKIN PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 54,951 hrs · 47,958 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CRACKED AT BS 947, STRINGER 26R. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,951 hrs · 47,958 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) BS 759 AT STR 23L AT BS 773 AT STR 25L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,951 hrs · 47,958 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727 PLUS 3, BELOW STR 22L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,951 hrs · 47,958 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) BS 882 AT STR 25R AND BS 885 AT STR 23R. REPAIRED SKIN PER SRM.

Part: RETAINER — CRACKED (CABIN) · airframe 54,747 hrs · 47,798 cycles

FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS HOLDER CRACKED. REMOVED AND REPLACED LENS HOLDER PER MM.

Part: CABLE — MISROUTED (ESCAPE SLIDE) · airframe 54,212 hrs · 47,360 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,138 hrs · 46,450 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (3 EA) AT STR 4R, BS 629, BS 689 AND BS 690. REPAIRED SKIN PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,138 hrs · 46,450 cycles

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

Part: SLAT — CRACKED (LT WING) · airframe 52,424 hrs · 45,873 cycles

DURING SCHEDULED C4 CHECK, FOUND NR 2 L/E SLAT CRACKED AT AFT ROW OF FASTENERS. REPAIRED NR 2 L/E SLAT PER SRM.

Part: SKIN — DELAMINATED (ELEVATOR) · airframe 52,424 hrs · 45,873 cycles

DURING SCHEDULED C4 CHECK, FOUND RT ELEVATOR DELAMINATED ON LOWER SURFACE. REMOVED AND REPLACED ELEVATOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,413 hrs · 45,865 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 7237E, STR 24R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 52,173 hrs · 45,655 cycles

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

Part: BATTERY — DISCHARGED (CABIN) · airframe 51,936 hrs · 45,462 cycles

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

Part: COFFEEMAKER — OVERHEATED (GALLEY) · airframe 51,103 hrs · 44,784 cycles

STRONG ELECTRICAL ODOR NOTED AT FWD PART OF CABIN DISSIPATED WITH GALLEY PWR OFF. REMOVED AND REPLACED FWD GALLEY COFFEEMAKER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,693 hrs · 44,435 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) AT STR 10R, BS'S 500A, 500C AND 500D. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,421 hrs · 44,226 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) AT BS 727D AT STR 19R, BS 749 AT STR 18R, BS 745 AT STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,421 hrs · 44,226 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 905, STR 23R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,982 hrs · 43,087 cycles

DURING WALK AROUND INSPECTION FOUND FUSELAGE SKIN CRACKED 2.2 INCH LONG AT BS 308, STR 18R. REPAIRED SKIN PER SRM.

Part: HYDRAULIC LINE — DAMAGED (LT MLG) · airframe 48,967 hrs · 43,072 cycles

(AIR TURNBACK) A-SYSTEM HYDRAULIC FAILURE AFTER TAKEOFF AND GEAR RETRACTION. FOUND HOLE IN LT MLG RETRACT LINE. REMOVED AND REPLACED LINE, OPS AND LEAK CHECK GOOD PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,857 hrs · 42,982 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 957 TO BS 961, STR 21L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 48,826 hrs · 42,957 cycles

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

Part: LIGHT — INOPERATIVE (SERVICE DOOR) · airframe 48,826 hrs · 42,957 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR VERTICAL EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM.

Part: LENS — MISSING (CABIN) · airframe 48,826 hrs · 42,957 cycles

DURING SCHEDULED C4 CHECK, FOUND LH OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,755 hrs · 42,899 cycles

DURING WALK AROUND INSPECTION FOUND FUSELAGE SKIN CRACKED 1.0 INCH LONG AT BS 727D + 6, BETWEEN STR 19L & 20L. REPAIRED SKIN PER SRM & SWA RA 1-353-2678.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 47,182 hrs · 41,528 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,990 hrs · 41,376 cycles

DURING SCHEDULED C2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 18 ABC. RELAMPED LIGHT ASSY PER MM.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 46,753 hrs · 41,170 cycles

DURING SCHEDULED D-CHECK, FOUND INTERNAL FUSELAGE SKIN DOUBLER CORRODED AT BS 967, LBL 3 TO LBL 7. REPAIRED SKIN PER BFG ER.

Part: FITTING — CORRODED (LT WING) · airframe 46,753 hrs · 41,170 cycles

DURING SCHEDULED D-CHECK, FOUND LT WING STABILIZER BEAM FITTING CORRODED ON REAR SPAR CHORD. REMOVED AND REPLACED BEAM FITTING PER MM.

Part: RIB — CRACKED (LT&RT WING) · airframe 46,753 hrs · 41,170 cycles

DURING SCHEDULED D-CHECK, FOUND LT AND RT WING RIB LOWER CHORDS CRACKED AT WBL 135.5, BETWEEN STR 2 AND 3. REPAIRED LOWER CHORDS PER BFG ER''S.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,753 hrs · 41,170 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CORRODED AT BS 967, LBL 3. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,753 hrs · 41,170 cycles

DURING SCHEDULED D-CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 727E+5, BELOW STR 26R. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 46,753 hrs · 41,170 cycles

DURING SCHEDULED D-CHECK, FOUND BS 727 BULKHEAD WEB CRACKED AT WL 148, LBL 6.5 & RBL 6.5. REPAIRED BULKHEAD WEB PER BFG ER.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 46,753 hrs · 41,170 cycles

DURING SCHEDULED D-CHECK, FOUND STR SPLICE CHANNEL CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED STR SPLICE CHANNEL PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,753 hrs · 41,170 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 294.5, BETWEEN STR 1R & 2R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,753 hrs · 41,170 cycles

DURING SCHEDULED D-CHECK, FOUND STR CLIPS CRACKED AT STR 6R, BS 500D & BS 520. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: FITTING — CORRODED (LT WING) · airframe 46,753 hrs · 41,170 cycles

DURING SCHEDULED D-CHECK, FOUND LT MLG STABILIZER BEAM FITTING CORRODED AT SUPPORT BEAM. REMOVED AND REPLACED FITTING PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 46,753 hrs · 41,170 cycles

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD WEB CRACKS AT RBL 17.1, WL 163 & LBL 17.1, WL 229. REPAIRED BULKHEAD WEB PER BFG ER.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 46,753 hrs · 41,170 cycles

DURING SCHEDULED D-CHECK, FOUND STR 6R CRACKED AT BS 520. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,753 hrs · 41,170 cycles

DURING SCHEDULED D-CHECK, FOUND FWD SVC DOOR CUTOUT FWD LOWER FRAME CRACKED AT INBD LOWER CORNER. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 46,753 hrs · 41,170 cycles

DURING SCHEDULED D-CHECK, FOUND BS 727 CHORD CORRODED AT BL 0, WL 148. REPAIRED CHORD PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,753 hrs · 41,170 cycles

DURING SCHEDULED D-CHECK, FOUND FWD SVC DOOR CUTOUT FWD UPPER FRAME CRACKED AT UPPER INBD RADIUS, BS 296.5, WL 274. REPAIRED UPPER FRAME PER SRM.

Part: FRAME — CRACKED (CABIN) · airframe 46,753 hrs · 41,170 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 500D, 2 ABOVE STR 13R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 46,753 hrs · 41,170 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 13L & 14L.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,753 hrs · 41,170 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED, BS 500B, STR 9L, BS 500D, STR 5L, BS 520, STRS 5R, 6L & 8L, BS 1121, STR 21L. REMOVED AND REPLACED CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,753 hrs · 41,170 cycles

DURING SCHEDULED D-CHECK, FOUND 12 STRINGER CLIPS CRACKED, BS 559-BS 727A, STRINGERS 10L, 5R, 8L, 5L, 4L, 1, 2L, 6R, 7R, 3L & 6L. REMOVED AND REPLACED CLIPS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,753 hrs · 41,170 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 21R. REPAIRED FRAME PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 46,753 hrs · 41,170 cycles

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED, LBL 4.7, WL 212-213. REPAIRED BULKHEAD PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 46,753 hrs · 41,170 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 520, BETWEEN STR 15L & 16L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,753 hrs · 41,170 cycles

DURING SCHEDULED D-CHECK, FOUND STR CLIPS CRACKED AT BS 380, STR 8L, BS 520, STR 16L, BS 500D, STR 3L, 6L, 7L, 8L, 5R, & 8R, BS 500C, STR 7R, BS 360, STR 5L, BS 360, STR 2L, BS 344, STR 11R, BS 639, STR 8L, BS 597, STR 8R, & BS 663.75, STR 10R. REMOVED AND REPLACED STR CLIPS PER SRM & TRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 46,753 hrs · 41,170 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 1040, BETWEEN STR 2L & 3L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 46,753 hrs · 41,170 cycles

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD WEB CRACKS AT LBL 12 TO LBL 13, WL 218 & RBL 6.7, WL 200 TO WL 201. REPAIRED BULKHEAD WEB PER SRM.

Part: BRACKET — CORRODED (ENTRY DOOR) · airframe 46,753 hrs · 41,170 cycles

DURING SCHEDULED D-CHECK, FOUND BOTH FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR BRACKETS CORRODED. REMOVED AND REPLACED BRACKETS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,753 hrs · 41,170 cycles

DURING SCHEDULED D-CHECK, FOUND STR CLIPS CRACKED AT BS 616, STR 3R, BS 639, STR 4R & BS 706, STR 2L. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (CABIN) · airframe 46,753 hrs · 41,170 cycles

DURING SCHEDULED D-CHECK, FOUND STR CLIPS CRACKED AT STR 8R, BS 578 & 637, STR 7R, BS 557, STR 8L, BS 616, STR 4R, BS 616, & STR 6L BS 597 & 616. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 46,092 hrs · 40,618 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,994 hrs · 40,542 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 2 EXTERNAL FUSELAGE SKIN CRACKS AT BS 727D, STR 4L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,977 hrs · 40,523 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EXIT SIGN HAS THREE BULBS INOP. REMOVED AND REPLACED BULBS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,977 hrs · 40,523 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR LOWER EMERGENCY LIGHT HAS SEVERAL BULBS INOP. REPLACED BULBS PER MM.

Part: LENS — MISSING (CABIN) · airframe 45,977 hrs · 40,523 cycles

DURING SCHEDULED C1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: COVER — BROKEN (CABIN FLOOR) · airframe 45,977 hrs · 40,523 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS COVER BROKEN NEAR MID CABIN LOUNGE.

Part: RETAINER — LOOSE (ESCAPE SLIDE) · airframe 45,977 hrs · 40,523 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR STOWAGE RETAINER HOOKS LOOSE. SECURED HOOKS PER MM.

Part: BOTTLE — DISCHARGED (SLIDE) · airframe 45,631 hrs · 40,219 cycles

DURING SCHEDULED A2 CHECK, FOUND FWD ENTRY EMERGENCY EVAC SLIDE PRESSURE IND BELOW LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 45,084 hrs · 39,129 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,999 hrs · 39,655 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 727D+18, STRINGER 22R. REPAIRED SKIN PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 44,684 hrs · 39,390 cycles

EEPLS TRACK LOOSE AT ROW 8. SECURED TRACK ASSY PER MM.

Part: CABLE — MISROUTED (GIRT BAR) · airframe 44,494 hrs · 39,213 cycles

AFT ENTRY DOOR EVACUATION SLIDE GIRT BAR RELEASE CABLE OUT OF POSITION. REROUTED CABLE PER MM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 44,184 hrs · 38,946 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE GIRT ASSY OUT OF POSITION. REPOSITIONED SLIDE ASSY PER MM.

Part: SLIDE — DISLODGED (AFT ENTRY) · airframe 44,036 hrs · 38,830 cycles

AFT ENTRY DOOR EVACUATION SLIDE FALLING OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (BS 727D)

DURING SCHEDULED SERVICE, FOUND EXTERNAL FUSELAGE SKIN CRACKED, BS 727B, STRINGER 23R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 747)

DURING WALK-AROUND CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACKED, BS 747, STRINGER 20L. ALSO, FOUND ANOTHER CRACK AT BS 727B, STRINGER 23R. REPAIRED SKIN PER SRM.

Part: LENS — MISSING (ROW 23)

DURING SCHEDULED C2 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING AT ROW 23. INSTALLED LENS PER MM.

Part: INDICATOR — MALFUNCTIONED (COCKPIT)

AIR TURNBACK, T/E FLAP POSITION INDICATION OF FLAPS NOT RETRACTING BETWEEN 2 AND 5 DEGREES. RESET T/E FLAP POSITION INDICATOR C/B, RESEATED T/E FLAP POSITION TRANSMITTER CONNECTOR. OPERATED T/E FLAPS, OPS CK GOOD. LATER DURING RON AT BWI REMOVED AND REPLACED T/E FLAP POSITION INDICATOR FOR MX CONVENIENCE.

Part: CHARGER — INOP (CABIN)

DURING SCHEDULED SC CHECK, FOUND LT AND RT OVERWING EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER PER BOEING MM.

Part: FAN BLABE — DAMAGED (NR 2 ENGINE)

DURING CLIMB-OUT FROM SMF WE HIT A FLOCK OF LARGE BIRDS, ONE OR MORE IMPACTED NR 2 ENGINE. THE ENGINE RAN NORMAL AT IDLE POWER, BUT WE HAD AIRFRAME VIBRATION AND A BURN SMELL FROM THE RIGHT PACK. AIRCRAFT DIVERTED INTO OAK AND MADE AN UNEVENTFUL LANDING. PERFORMED BIRDSTRIKE INSPECTION PER 5-51-37. FOUND FAN BLADES NR 20 AND NR 21 WITH EXCESSIVE DISTORTION. REMOVED AND REPLACED AND REPOSITIONED BLADES AND REMOVED AND REPLACED ENG NOSE COWL PER MM. PERFORMED HIGH POWER RUN OK PER MM.

Part: SKIN — CRACKED (BS 348)

DURING SCHEDULED 1/4D CHECK, FOUND A CRACK INDICATION IN FUSELAGE SKIN EMANATING FROM FASTENER HOLE AT BS 348 BELOW FWD ENTRY DOOR. REPAIRED SWA RA 1-353-193 AND BOEING DRAWING 65C27257.

Part: SKIN — CRACKED (RT WING)

DURING SCHEDULED 1/4D CHECK, FOUND RT WING FIXED L/E CRACKED AT NR 6 SLAT I/B AUX TRACK CUTOUT. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 664)

DURING SCHEDULED 1/4D CHECK, FOUND CRACK IN BEADED PRESSURE WEB AT BS 664. REPAIRED PER SWA RA 1-353-1929.

Part: SKIN — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED 1/4D CHECK, FOUND 2 ADJACENT CRACKS IN FUSELAGE SKIN AT AFT LOWER CORNER OF FWD SERV DOOR CUTOUT. REPAIRED BOEING SRM.

Part: WIRE — BROKEN (CABIN)

DURING SCHEDULED 1/4D CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT OVERWING EXITS. REPAIRED BROKEN WIRE AND OP CHECKED PER BOEING M/M.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED 1/4 D CHECK, FOUND A FUSELAGE SKIN CRACK EMANATING FROM A RIVET HOLE AT FWD UPPER CORNER OF AIRSTAIRS CUTOUT. REPAIRED PER SWA RA 1-353-1940.

Part: FASTENER — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND 2 HFEC CRACKED INDICATIONS COMING FROM HI-LOK AT WL 234, LBL 11 (FWD SIDE). REPAIRED PER BOEING SRM.

Part: STRAP — CORRODED (BS 770)

DURING SCHEDULED 1/4D CHECK, FOUND CORRODED FLOORBEAM STRAP AT BS 770. REMOVED AND REPLACED STRAP PER BOEING SRM.

Part: FASTENER — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND HFEC CRACKED INDICATIONS COMING FROM HI-LOK AT WL 234, RBL 9 (FWD SIDE). REPAIRED PER BOEING SRM.

Part: STRAP — CORRODED (BS 860)

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION AROUND SCREW HOLES OF STRAP AT BS 860. REMOVED AND REPLACED STRAP PER BOEING SRM.

Part: ANGLE — CRACKED (BS 540)

DURING SCHEDULED 1/4D CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 540, STR 21. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 540)

DURING SCHEDULED 1/4D CHECK, FOUND BS 540, STR 21 SUPPORT ANGLE CRACKED. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — DAMAGED (BS 503)

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM KNICKED AT BS 503, RBL 9. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — MISDRILLED (BS 500)

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM ERRANT HOLE AT BS 500, LBL 13. REPAIRED PER BOEING SRM.

Part: WHEEL — DAMAGED (NR 1 & 2 MAIN)

AFTER LANDING FOUND EVIDENCE LEFT MAIN LANDING GEAR DEPARTED RUNWAY INTO DIRT. PERFORMED INSP PER 05-51-51-2, NO DAMAGE FOUND ON A/C. REMOVED AND REPLACED NR 1 MAIN AND NR 2 MAIN WHEEL ASSY AS PER CAUTION.

Part: SLIDE — DEPLOYED (PAX DOOR)

WHILE DEPLANING, AFT ENTRY DOOR SLIDE DEPLOYED. REPLACED PER BOEING M/M.

Part: SKIN — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED C1 CHECK, FOUND L2 DOOR UPPER HINGE CUTOUT CRACKED. REPAIRED PER SWA RA 1-353-1711.

Part: SKIN — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED C1 CHECK, FOUND L2 DOOR LOWER HINGE CUTOUT CRACKED. REPAIRED PER SWA RA 1-353-1710.

Part: SKIN — CRACKED (PAX DOORWAY)

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR LOWER HINGE CUTOUT CRACKED. REPAIRED PER SWA RA 1-352-0288.

Part: SERVICE DOOR — DAMAGED (FUSELAGE)

AFTER TAKEOFF, NOTED A RUMBLING SOUND FROM RIGHT SIDE OF AIRCRAFT. RETURNED TO HOU AND MADE AN UNEVENTFUL LANDING. FOUND FORWARD LAVATORY SERVICE DOOR OPEN, BENT AND WARPED. REPLACED WITH NEW DOOR PER BOEING M/M.

Part: ADC — MALFUNCTIONED (LT COCKPIT)

AFTER TAKEOFF, CAPT AIRSPEED INDICATOR ROLLED BACK CAUSING STALL AND WINDSHEAR WARNING. AIRSPEED THEN WENT TO MAX SCALE WITH STICK SHAKER ACTIVATION. AIRCRAFT RETUNED TO PHX AND MADE AN UNEVENTFUL LANDING. INSPECTED AND REPLACED CAPT ADC, PERFORMED PITOT STATIC LEAK CHECK AND DFCS BITE CHECK PER BOEING M/M.

Part: STIFFENER — CRACKED (BS 178)

DURING SCHEDULED SV CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 178, LBL 5.5, WL 184. REPAIRED PER BOEING SRM.

Part: BULKHEAD BRACKET — CRACKED (BS 727)

DURING SCHEDULED SV CHECK, FOUND AFT CARGO BULKHEAD SUPPORT BRACKET CRACKED AT BS 727 PLUS 4, BL 0, WL 160. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (GALLEY DOOR)

DURING SCHEDULED SV CHECK, FOUND FWD GALLEY DOOR UPPER HINGE CUTOUT OUTER SKIN CRACKED AT UPPER OUTER EDGE. REPAIRED PER SWA ACO 3189-52.

Part: SKIN — CREASE (BS 807)

DURING SCHEDULED SV CHECK, FOUND FUSELAGE SKIN CREASE AT BS 807, BL 0, WL 148. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 947-957)

DURING SCHEDULED SV CHECK, FOUND FUSELAGE SKIN DENTED FROM BS 947 TO 957, BETWEEN S18 AND 19L. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 570)

DURING SCHEDULED SV CHECK, FOUND CRACKED SKATE ANGLE AT BS 570, WL 171, LBL 43 TO 60. REPLACED PER BOEING SRM.

Part: FRAME — DENTED (BS 727)

DURING SCHEDULED SV CHECK, FOUND FUSELAGE FRAME DENTED AT BS 727E, S25R. REPAIRED PER BOEING SRM.

Part: DOOR FRAME — CRACKED (FWD SERV)

DURING SCHEDULED SV CHECK, FOUND FWD SERV DOOR, LWR FWD FRAME CRACKED AT BS 295, RBL 56, WL 209. REPLACED FRAME PER BOEING SRM.

Part: WEB — CRACKED (BS 178)

DURING SCHEDULED SV CHECK, FOUND WEB CRACKED AT BS 178, BL 0, WL 188.1. REPAIRED PER TRAMCO EWO 96-0228.

Part: FRAME — CRACKED (BS 492)

DURING SCHEDULED SV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 492, RBL 36, WL 162. REPAIRED PER TRAMCO EWO 96-0229.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED SV CHECK, FOUND BULKHEAD AT BS 178 PRESSURE WEB CRACKED 3 PLACES AT WL 201, WL 199 AND WL 198, RBL 4.7. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 639)

DURING SCHEDULED SV CHECK, FOUND WEB CRACKED AT BS 639, RBL 66, WL 221. REPLACED PER BOEING SRM.

Part: SKIN — CREASED (BS 460-480)

DURING SCHEDULED SV CHECK, FOUND FUSELAGE SKIN CREASED AT BS 460 TO BS 480, RBL 1 TO RBL 4, WL 149. REPAIRED PER BOEING SRM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED SV CHECK, FOUND BULKHEAD AT BS 178 PRESSURE WEB CRACKED 3 PLACES AT WL 213, LBL 4.7 AND LBL 6.7, WL 209.5. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 328)

DURING SCHEDULED SV CHECK, FOUND FUSELAGE OUTER SKIN CRACKED AT BS 328, WL 211, RBL 65. REPAIRED PER BOEING SRM.

Part: CLIP — CRACKED (BS 500)

DURING SCHEDULED SV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, S19L, WL 192. REPAIRED PER BOEING SRM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED SV CHECK, FOUND BULKHEAD AT BS 178 PRESSURE WEB CRACKED AT WL 213, RBL 6.7. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 380)

DURING SCHEDULED SV CHECK, FOUND INTERCOSTAL TO FRAME ANGLE CRACKED AT BS 380, LBL 24, WL 155. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 294.5-312)

DURING SCHEDULED SV CHECK, FOUND FUSELAGE SKIN DENTED AT BS 294.5 TO BS 312, BETWEEN S20 AMD 21R. REPAIRED PER BOEING SRM.