N326SW

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,971 hrs · 70,420 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACK AT STA 500D+12, STR 8L. REPAIRED PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,968 hrs · 70,419 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACK AT STA 500D+12, STR 8L. REPAIRED PER EA.

Part: SKIN — DELAMINATED (SPOILER) · airframe 77,819 hrs · 70,313 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 6 SPOILER DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED SPOILER PER MM.

Part: ACTUATOR — CORRODED (SPOILER) · airframe 77,819 hrs · 70,313 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING I/B GROUND SPOILER ACTUATOR SURFACE CORRODED. REMOVED AND REPLACED ACTUATOR PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 77,505 hrs · 70,073 cycles

DURING SCHEDULED SPV CHECK, FOUND WEB CRACKED AT BS 639, LBL 45.5. REPAIRED WEB PER ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,505 hrs · 70,073 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500D, BETWEEN STR 19R TO STR 22R. REPAIRED FRAME PER SRM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 76,955 hrs · 69,659 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT GALLEY EMERGENCY EXIT SIGN LIGHT DIM. REMOVED AND REPLACED BATTERY CHARGER ASSY PER MM.

Part: LENS — LOOSE (CABIN) · airframe 76,946 hrs · 69,650 cycles

DURING SCHEDULED CV CHECK, FOUND LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LOOSE AT ROW 6. SECURED LENS PER MM.

Part: LENS — BROKEN (CABIN) · airframe 76,732 hrs · 69,473 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT PRESSURE BULKHEAD LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 76,010 hrs · 68,915 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS MISSING BETWEEN ROW 4 TO ROW 5. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,811 hrs · 68,756 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT UPPER FWD CORNER, BS 303. REPAIRED SKIN PER ER AND EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 75,811 hrs · 68,757 cycles

DURING SCHEDULED 24Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REMOVED AND REPLACED SLIDE PER MT.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,811 hrs · 68,756 cycles

DURING SCHEDULED 24Y CHECK, FOUND CRACK ON FRAME WEB STA 639, STR 7R. REPAIRED FRAME ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,811 hrs · 68,756 cycles

DURING SCHEDULED 24Y CHECK, FOUND CRACK ON FRAME WEB STA 420, STR 1. REPAIRED FRAME PER ER AND EA.

Part: SKIN — DEBONDED (FLAP) · airframe 75,811 hrs · 68,756 cycles

DURING SCHEDULED 24Y CHECK, FOUND LEFT I/B FORE FLAP UPPER SKIN DISBONDED 46 INCHES FROM I/B END AND 8 INCHES FROM T/E. REPAIRED PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 75,811 hrs · 68,756 cycles

DURING SCHEDULED 24Y CHECK, FOUND CRACK ON LONGITUDINAL FLOORBEAM STA 663, RBL 24.8. REPAIRED FLOORBEAM PER ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,811 hrs · 68,756 cycles

DURING SCHEDULED 24Y CHECK, FOUND CRACK ON FRAME STA 847, BELOW STR 1L. REPAIRED FRAME PER ER AND EA.

Part: STRAP — CORRODED (FUSELAGE) · airframe 75,811 hrs · 68,756 cycles

DURING SCHEDULED 24Y CHECK, FOUND BULKHEAD O/B CHORD STRAP CORRODED AT BS 727, BL 0. REPAIRED STRAP PER BAC DWG.

Part: SKIN — PUNCTURED (FOREFLAP) · airframe 75,811 hrs · 68,756 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING I/B FORE FLAP LOWER SKIN PUNCTURED. REPAIRED FORE FLAP PER SRM.

Part: SKIN — DEBONDED (FOREFLAP) · airframe 75,811 hrs · 68,756 cycles

DURING SCHEDULED 24Y CHECK, FOUND LEFT I/B FORE FLAP UPPER SKIN DISBONDED. REPAIRED FORE FLAP SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,811 hrs · 68,756 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,811 hrs · 68,756 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 13R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 75,811 hrs · 68,756 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO DOOR SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,811 hrs · 68,756 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 27R TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,811 hrs · 68,756 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,811 hrs · 68,756 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,811 hrs · 68,756 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,811 hrs · 68,756 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 16R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,811 hrs · 68,756 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 75,811 hrs · 68,756 cycles

DURING SCHEDULED 24Y CHECK, FOUND T-CHORD CRACKED AT BS 646, RBL 7. REMOVED AND REPLACED T-CHORD PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,811 hrs · 68,756 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 16R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,811 hrs · 68,756 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME WEB CRACKED AT BS 294.5 BETWEEN STR 2R -3R. INSTALLED NEW FRAME AND FASTENERS PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,811 hrs · 68,756 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 25R TO STR 26R. REPAIRED SHEAR TIE PER EA AND ER.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 75,811 hrs · 68,756 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 318 TO BS 323, STR 28R. REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,811 hrs · 68,756 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,811 hrs · 68,756 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,811 hrs · 68,756 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 75,811 hrs · 68,756 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 3 SLAT L/E LOWER SURFACE CRACKED. REPAIRED SLAT PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,811 hrs · 68,756 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 25R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — DELAMINATED (FUSELAGE) · airframe 75,811 hrs · 68,756 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP DELAMINATED AT BS 787, STR 25R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 75,811 hrs · 68,756 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM CORRODED AT BS 360, RBL 13. REPAIRED BEAM PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 75,713 hrs · 68,686 cycles

RT EMERGENCY EXIT BULLNOSE LIGHT LENS LOOSE AT ROW 16. SECURED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,251 hrs · 68,333 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: LENS — MISSING (CABIN) · airframe 75,107 hrs · 68,219 cycles

LT EEPLS LENS MISSING AT ROW 17. INSTALLED LENS PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 74,600 hrs · 67,822 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: LENS — MISSING (CABIN) · airframe 74,526 hrs · 67,760 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT EMERGENCY EXIT LIGHT LENS MISSING AT ROW 1. REMOVED AND REPLACED LENS PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 74,526 hrs · 67,760 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: LENS — MISSING (CABIN) · airframe 74,257 hrs · 67,532 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,743 hrs · 67,148 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 540 TO BS 672, STR 10R. REPAIRED SKIN PER ER.

Part: LENS — LOOSE (CABIN) · airframe 73,736 hrs · 67,144 cycles

DURING SCHEDULED CV CHECK, FOUND LT OVERHEAD BIN EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 6. SECURED LENS PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 73,684 hrs · 67,104 cycles

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

Part: LENS — MISSING (CABIN) · airframe 73,149 hrs · 66,689 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS MISSING AT ROW 5. INSTALLED LENS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 73,138 hrs · 66,682 cycles

EEPLS LOOSE BETWEEN ROW 6 TO ROW 7. SECURED EEPLS PER MM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 73,020 hrs · 66,595 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 28R. REMOVED AND REPLACED SPLICE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,020 hrs · 66,595 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 382, STR 20R. REMOVED AND REPLACED STRINGER PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 73,020 hrs · 66,595 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CORRODED AT BS 361, BETWEEN STR 26L TO STR 27L. REPAIRED SKIN PER ER.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 73,020 hrs · 66,595 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 908, STR 24L. REPAIRED SPLICE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,020 hrs · 66,595 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 420, BETWEEN STR 19L TO STR 20L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,020 hrs · 66,595 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED BETWEEN BS 408 TO 414, STR 20R. REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 73,020 hrs · 66,595 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 21R. REMOVED AND REPLACED SPLICE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,014 hrs · 66,590 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 727C, STR 14R. REPAIRED FRAME PER ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 17R TO STR 18R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED BS 360, BETWEEN STR 15R TO STR 16R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: LENS — CRACKED (CABIN) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND LT EMERGENCY EXIT LIGHT CRACKED AT BS 370. REMOVED AND REPLACED LENS PER SOPM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER FITTING CORRODED AT BS 540, STR 23R. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER FITTING CORRODED AT BS 540, STR 26L. REMOVED AND REPLACED FITTING PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED BS 440, STR 25R. REMOVED AND REPLACED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED BS 360, BETWEEN STR 16R TO STR 17R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED BS 767, BETWEEN STR 16R TO STR 17R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 14L TO STR 15L. REMOVED AND REPLACED SHEAR TIE PER ACO.

Part: FITTING — CORRODED (GIRT BAR) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED BS 360, BETWEEN STR 27R TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,012 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 360, BETWEEN STR 20R TO STR 21R. REMOVED AND REPLACED FRAME PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,012 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, BETWEEN STR 13L TO STR 14L. REPAIRED SHEAR TIE PER ER.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 73,012 hrs · 66,588 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,012 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 25R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,012 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 480, BETWEEN STR 13L TO STR 14L. REPAIRED SHEAR TIE PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,012 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 22L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,012 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 480, BETWEEN STR 13R TO STR 14R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: WIRE — BROKEN (CABIN) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND EMERGENCY EXIT TWO GROUND WIRES BROKEN AT BS 360, BETWEEN STR 14L TO STR 15L. CONNECTED WIRE PER WDM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER END FITTING CORRODED AT BS 540, STR 25L. REPAIRED FITTING PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 420, BETWEEN STR 13R TO STR 14R. REPAIRED SHEAR TIE PER ER.

Part: FRAME — CORRODED (FUSELAGE) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CORRODED AT BS 360, BETWEEN STR 27R TO STR 28R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,013 hrs · 66,588 cycles

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

Part: SILL — CORRODED (FUSELAGE) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR SILL WEB CORRODED AT BS 822. REMOVED AND REPLACED SILL WEB PER SRM.

Part: SKIN — DELAMINATED (ELEVATOR) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND LT ELEVATOR UPPER SURFACE DELAMINATED. REPAIRED ELEVATOR PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 73,013 hrs · 66,588 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND LT OVERHEAD BULLNOSE LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 500A, BETWEEN STR 16R TO STR 17R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 767, BETWEEN STR 14R TO STR 15R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 500A, BETWEEN STR 15R TO STR 16R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 910, STR 22L. REMOVED AND REPLACED SPLICE PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 21L. REMOVED AND REPLACED SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 16R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 947, BETWEEN STR 24L TO STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 21L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 16R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 380 S20L) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 20L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 616 S1) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 1. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 597 S8L) · airframe 73,013 hrs · 66,588 cycles

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

Part: STRINGER CLIP — CRACKED (BS 907 S21L) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 21L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,013 hrs · 66,588 cycles

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

Part: STRINGER CLIP — CRACKED (BS 807 S10L) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,013 hrs · 66,588 cycles

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

Part: STRINGER CLIP — CRACKED (BS 500B S26L) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 26L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727B S1) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 1. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 767 S8R) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 578 S8L) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727B S2L) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 440 S2L) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 847 S9R) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CRACKED (BS 480 S15-16R) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 480, BETWEEN STR 15R TO STR 16R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727C S7R) · airframe 73,013 hrs · 66,588 cycles

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

Part: STRINGER CLIP — CRACKED (BS 727D S4R) · airframe 73,013 hrs · 66,588 cycles

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

Part: STRINGER CLIP — CRACKED (BS 847 S4R) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 4R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (BS 727C S6R) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (BS 827 S4R) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 4R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (BS 727B S5R) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 5R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (BS 727C S3R) · airframe 73,013 hrs · 66,588 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 3R. REMOVED AND REPLACED CLIP PER SI.

Part: WINDOW — CRACKED (EVAC SLIDE) · airframe 72,676 hrs · 66,350 cycles

DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE VIEWING WINDOW CRACKED. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 72,255 hrs · 66,041 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,152 hrs · 65,966 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 510D, STR 15L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,152 hrs · 65,966 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 501D, STR 15L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,152 hrs · 65,966 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 506D, STR 15L. REPAIRED SKIN PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 72,151 hrs · 65,966 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 668.75, LBL 24.5. REPAIRED CHORD PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 72,151 hrs · 65,966 cycles

DURING SCHEDULED 22Y CHECK, FOUND CENTER BOX WING FLOORBEAM UPPER CHORD CRACKED AT BS 665.0, LBL 24.5. REPAIRED CHORD PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,151 hrs · 65,966 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 72,151 hrs · 65,966 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 673.75, LBL 24.5. REPAIRED CHORD PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,152 hrs · 65,966 cycles

DURING SCHEDULED MV CHECK, FOUND FRAME CRACKED AT BS 507D, STR 17L. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,152 hrs · 65,966 cycles

DURING SCHEDULED MV CHECK, FOUND SKIN CRACKED AT BS 933, STR 22L. REPAIRED SKIN PER SWA EA.

Part: FLAP — PUNCTURED (LT WING) · airframe 72,005 hrs · 65,853 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING I/B AFT FLAP PUNCTURED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 71,673 hrs · 65,612 cycles

R2 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. DID NOT DEPLOY. RE-INSTALLED SLIDE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,565 hrs · 65,536 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 291, WL 233, RT SIDE. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,565 hrs · 65,536 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER MOD DOUBLER CUTOUT BETWEEN BS 308 TO BS 339, BETWEEN STR 6L TO STR 9L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,565 hrs · 65,536 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT AT BS 290, BETWEEN WL 233 TO WL 260. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,565 hrs · 65,536 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT, BS 305, WL 258. REPAIRED SKIN PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,565 hrs · 65,536 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT T-CAP BS 665, RBL 24. REPAIRED BEAM PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,565 hrs · 65,536 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT AT BS 305, WL 238. REPAIRED SKIN PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,565 hrs · 65,536 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 663, RBL 24. REPAIRED CHORD PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,565 hrs · 65,536 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT, BETWEEN BS 292 TO BS 293, BETWEEN WL 261 TO WL 262. REPAIRED SKIN PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,565 hrs · 65,536 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 664, RBL 25. REPAIRED CHORD PER EA.

Part: COVER — CRACKED (CABIN) · airframe 71,565 hrs · 65,536 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT EEPLS COVER CRACKED AT ROW 1. REMOVED AND REPLACED COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,565 hrs · 65,536 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, BETWEEN BS 303 TO BS 305, BETWEEN WL 234 TO WL 236. REPAIRED SKIN PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,565 hrs · 65,536 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED BETWEEN BS 706 TO BS 737, BBL 0. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,565 hrs · 65,536 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT T-CAP BS 665, LBL 24. REPAIRED BEAM PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,584 hrs · 65,547 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT OVERWING EMERGENCY EXIT SIGN BULB INOP. RELAMPED PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,602 hrs · 65,558 cycles

DURING SCHEDULED HC2 CHECK, FOUND NOSE WHEEL WELL LT SIDE DOUBLER CRACKED AT BS 259. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,584 hrs · 65,547 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT OVERWING EMERGENCY EXIT SIGN BULB INOP. RELAMPED PER MM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 71,584 hrs · 65,547 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT NOSE WHEEL WELL DOUBLER CRACKED AT BS 259. REPAIRED DOUBLER PER SWA EA.

Part: FLOORBEAM — CRACKED (BS 667) · airframe 71,565 hrs · 65,536 cycles

DURING SCHEDULED 22Y CHECK, FOUND CENTER BOX WING FLOORBEAM UPPER CHORD CRACKED AT STA 667, LBL 25.5. REPAIRED CHORD PER EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 71,565 hrs · 65,536 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT ENTRY DOOR CUTOUT, CRACKED ON FWD FRAME. R&R FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,565 hrs · 65,536 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 760, STR 19R. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,565 hrs · 65,536 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED BS 500C, STR 13R. REPAIRED FRAME PER SWA EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 71,656 hrs · 65,536 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING O/B MID FLAP DELAMINATED. R&R MID FLAP PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 71,656 hrs · 65,536 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED LOWER O/B END. R&R AFT FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,565 hrs · 65,536 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 375, STR 26R. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 71,565 hrs · 65,536 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING OTBD MID FLAP DELAMINATED. REPAIRED FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,565 hrs · 65,536 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 2R. REMOVED AND REPLACED CLIP PER SRM.

Part: ATTACH FITTING — BROKEN (SPOILER ACTUATOR) · airframe 71,333 hrs · 65,364 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING NR 4 SPOILER I/B ACTUATOR ATTACH FITTING BROKEN. REMOVED AND REPLACED FITTING PER MM

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,969 hrs · 65,116 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 10. REMOVED AND REPLACED LAMP PER MM.

Part: LENS — LOOSE (CABIN) · airframe 70,810 hrs · 65,001 cycles

LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,461 hrs · 64,766 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 15L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,195 hrs · 64,583 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR SKIN CUTOUT CRACKED AT UPPER AFT CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,195 hrs · 64,583 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,195 hrs · 64,583 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT CARGO DOOR CUTOUT UPPER AFT CORNER. REPAIRED SKIN PER SRM.

Part: MOUNT BRACKET — CRACKED (R2 DOOR) · airframe 70,147 hrs · 64,549 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR SLIDE AFT MOUNTING BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER MM.

Part: COVER — MISSING (CABIN) · airframe 70,054 hrs · 64,481 cycles

FOUND LT EMERGENCY EXIT BULLNOSE LIGHT COVER MISSING AT ROW 17. REPLACED COVER PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 69,345 hrs · 63,951 cycles

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

Part: CHARGER — INOPERATIVE (CABIN) · airframe 68,632 hrs · 63,442 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,362 hrs · 63,253 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 950, STR 21L. REPAIRED SKIN PER SWA EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 68,362 hrs · 63,253 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,362 hrs · 63,253 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, STR 23R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 68,362 hrs · 63,253 cycles

DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,362 hrs · 63,253 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 772, STR 14R. REPAIRED SKIN PER SRM.

Part: ROD END — LOOSE (LT AILERON) · airframe 68,362 hrs · 63,253 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING AILERON TAB INBOARD HINGE LOOSE. REMOVED AND REPLACED BUSHING AND ROD END PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,362 hrs · 63,253 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, STR 24L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,333 hrs · 63,230 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 21R. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,010 hrs · 63,007 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 66,628 hrs · 61,948 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (BS 500D S16L) · airframe 66,628 hrs · 61,948 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 787 S19L) · airframe 66,628 hrs · 61,948 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 19L. REPAIRED SKIN PER SWA EA.

Part: CIRCUIT BREAKER — FAULTY (FLIGHT DECK) · airframe 66,616 hrs · 61,933 cycles

NR 1 GENERATOR TRIPPED OFF-LINE RESET, THEN TRIPPED AGAIN. BOTH PILOTS SMELLED ELECTRICAL BURNING ODOR IN COCKPIT. REMOVED AND REPLACED BUSS TIE BREAKER PER MM.

Part: UPLOCK ACTUATOR — FAULTY (LT MLG) · airframe 66,110 hrs · 61,530 cycles

CLIMBING OUT OF GEG LEFT MLG RED LIGHT STAYED ILLUMINATED. CYCLED GEAR, LIGHT WENT OUT. REMOVED AND REPLACED LEFT MLG UPLOCK ACTUATOR PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 65,982 hrs · 61,424 cycles

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

Part: LENS — DISLODGED (EMERGENCY LIGHTS) · airframe 65,513 hrs · 61,053 cycles

BULLNOSE EMERGENCY EXIT LIGHT LENS FELL OFF AT ROW 3 DEF. INSTALLED LIGHT LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,143 hrs · 60,749 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 444, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 444 S16R) · airframe 65,134 hrs · 60,739 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 444, STR 16R. REPAIRED SKIN PER SRM.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727C, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 9L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 3L. REPAIRED FRAME PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 312, STR 6L. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CRACKED AT BS 947, LBL 55. REPAIRED FLOORBEAM PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 344, STR 7L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 3R. REPAIRED FRAME PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 413, LBL 3. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 1. REPAIRED FRAME PER ER.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED AT STA 127. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 2L. REPAIRED FRAME PER ER.

Part: SKIN — CRACKED (BS 502D S12R) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 502D, STR 12R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (BS 572 S10L) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 572, STR 10L. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (BS 787 S13L) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 13L. REPAIRED FRAME PER SRM.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT AND LT HORIZONTAL STAB FITTING CLEVIS LUG FACES CORRODED. REPAIRED STAB FITTING PER SRM.

Part: SHEAR TIE — CORRODED (BS 460) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 460, BL 0 TO RBL 3. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — DELAMINATED (RUDDER) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND RUDDER T/E LOWER AFT SURFACE DELAMINATED. REPAIRED RUDDER PER SRM.

Part: FRAME — CRACKED (BS 867 S8R) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 360 S9L) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 707 S11R) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 707, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (BS 583 S10R) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 583, STR 10R. REPAIRED SKIN PER SWA EA.

Part: FLAP TRACK — CORRODED (RT WING) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND LEFT INBOARD MID FLAP OUTBOARD FORE FLAP TRACK CORRODED. REMOVED AND REPLACED FLAP TRACK PER MM.

Part: FLAP TRACK — CORRODED (RT WING) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND LEFT INBOARD MID FLAP INBOARD FORE FLAP TRACK CORRODED. REMOVED AND REPLACED FLAP TRACK PER MM.

Part: STRINGER CLIP — CRACKED (BS 827 S9L) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: TORQUE TUBE — CORRODED (RT WING TE FLAP) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND RIGHT WING INBOARD MID FLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: FLAP TRACK — CORRODED (RT WING) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND RIGHT WING OUTBOARD MID FLAP INBOARD FORE FLAP TRACK CORRODED. REMOVED AND REPLACED FORE FLAP TRACK PER MM.

Part: STRINGER CLIP — CRACKED (BS 727A S8L) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: BULKHEAD — CRACKED (BS 1016 S3R) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 3R. REPAIRED WEB PER SRM.

Part: WEDGE — DEBONDED (RT WING TE FLAP) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND RIGHT WING INBOARD MID FLAP T/E WEDGE LOWER SKIN DISBONDED AT OUTBOARD END. REMOVED AND REPLACED T/E WEDGE PER MM.

Part: TORQUE TUBE — CORRODED (RT WING TE FLAP) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND RIGHT WING INBOARD MID FLAP OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND RIGHT HORIZONTAL STAB RIB LOWER CHORD CRACKED AT STA 120. REMOVED AND REPLACED RIB CHORD PER SRM.

Part: SHEAR TIE — CORRODED (BS 500 S26L) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 807 S7L) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLOORBEAM — CORRODED (BS 294) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 294.5, LBL 53. REPAIRED FLOORBEAM PER SRM.

Part: SKIN — CRACKED (NR 6 SLAT) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED SPV CHECK, FOUND RIGHT WING NR 6 L/E SLAT SKIN CRACKED AT INBOARD END. REPAIRED SLAT PER SRM.

Part: SKIN — CRACKED (NR 4 SLAT) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED SPV CHECK, FOUND RIGHT WING NR 4 L/E SLAT SKIN CRACKED AT OUTBOARD END. REPAIRED SLAT PER SRM.

Part: STRINGER CLIP — CORRODED (BS 767 S26R) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CORRODED AT BS 767, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED SPV CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP SKIN CRACKED AT INBOARD CARRIAGE ARM CUTOUT. REPAIRED FLAP PER SRM.

Part: SKIN — PUNCTURED (T/E FLAP) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING INBOARD FORE FLAP PUNCTURED AT LOWER SURFACE. REPAIRED FORE FLAP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 1016 UPPER SURFACE. REPAIRED FLOORBEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 912, STR 21L. REPAIRED SKIN PER SRM.

Part: FLAP — DEBONDED (LT WING) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND LEFT WING INBOARD AFT T/E FLAP DISBONDED AT AFT EDGE. REPAIRED FLAP PER SRM & BAC DRAWING.

Part: STRINGER — CORRODED (BS 987 S27L) · airframe 64,970 hrs · 60,619 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER 27L CORRODED AT BS 987. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (AFT CARGO DOOR) · airframe 64,778 hrs · 60,462 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT CARGO DOOR SKIN CRACKED AT OUTER DOOR HANDLE CUTOUT. REPAIRED CARGO DOOR PER SWA EA.

Part: SKIN — CRACKED (BS 560 S10L) · airframe 64,660 hrs · 60,374 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 560, STR 10L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 731D S18R) · airframe 64,660 hrs · 60,374 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 731D, STR 18R. REPAIRED SKIN PER SWA EA.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 63,934 hrs · 59,804 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SKIN — CRACKED (BS 731C S14R) · airframe 63,764 hrs · 59,664 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 731C, STR 14R. REPAIRED SKIN PER SWA EA.

Part: FLAP — CRACKED (LT WING) · airframe 63,659 hrs · 69,574 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT WING OUTBOARD FORE FLAP CRACKED AT OUTBOARD END. REMOVED AND REPLACED FORE FLAP PER MM.

Part: BOLT — LOOSE (RT WING TE FLAP) · airframe 63,434 hrs · 59,386 cycles

PUT FLAPS DOWN AT 210 AND GOT UNUSUAL RUMBLE. AS AIRCRAFT SLOWED TO 180 RUMBLE STOPPED. RUMBLE CAME BACK IN 30 DEGREE BANK AND THEN QUIT. SECURED NR 6 T/E FLAP DRIVE UNIT BOLT PER MM.

Part: FLAP — VIBRATES (LT WING) · airframe 63,258 hrs · 59,253 cycles

DURING FLAPS EXTENSION TO POSITION 5, A STEADY VIBRATION FELT IN BOTH CONTROL COLUMNS. REMOVED AND REPLACED LT WING INBOARD FORE FLAP PER MM.

Part: TOGGLE — WORN (LT WING TE FLAP) · airframe 63,217 hrs · 59,220 cycles

VIBRATION REPORTED WITH FLAPS AT 5 AND 180 KNOT AIRSPEED. REMOVED AND REPLACED LT WING AFT FLAP TOGGLES PER MM.

Part: SKIN — DELAMINATED (LT WING SLAT) · airframe 62,936 hrs · 58,997 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING NR 2 L/E SLAT T/E WEDGE DELAMINATED ON LOWER SURFACE AT ACTUATOR AREA. REMOVED AND REPLACED NR 2 SLAT PER MM.

Part: WEDGE — DELAMINATED (LT WING TE FLAP) · airframe 62,928 hrs · 58,990 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING MID FLAP WEDGE PANEL DELAMINATED AT OUTBOARD T/E. REMOVED AND REPLACED MID FLAP WEDGE PANEL PER MM.

Part: SKIN — DELAMINATED (LT WING SLAT) · airframe 62,928 hrs · 58,990 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING NR 1 L/E SLAT DELAMINATED OUTBOARD T/E. REMOVED AND REPLACED LT WING NR 1 SLAT PER MM.

Part: SKIN — DELAMINATED (LT WING SLAT) · airframe 62,928 hrs · 58,990 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING NR 3 L/E SLAT T/E WEDGE DELMINATED UPPER AND LOWER SURFACES. REMOVED AND REPLACED LT WING NR 3 SLAT PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 62,928 hrs · 58,990 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING OUTBOARD AFT FLAP DELAMINATED AT INBOARD SIDE. REMOVED AND REPLACED LT OUTBOARD FLAP PER MM.

Part: SKIN — CRACKED (BS 308) · airframe 62,928 hrs · 58,990 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 308, STR 18R. REPAIRED SKIN PER SWA EA.

Part: MOTOR — FAILED (T/E FLAP) · airframe 62,669 hrs · 58,778 cycles

DURING SCHEDULED MV1 CHECK, T/E FLAPS WOULD NOT RETRACT AFTER LEVER SELECTED 40 DEGREES. REMOVED AND REPLACED FLAP DRIVE MOTOR PER MM.

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 61,433 hrs · 57,801 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER WDM & MM.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 61,176 hrs · 57,598 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: FRAME — CRACKED (AFT CARGO) · airframe 61,084 hrs · 57,524 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT AFT CARGO DOOR CUTOUT, FWD FRAME NR 5 STOP FITTING. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SKIN — CRACKED (BS 931) · airframe 60,969 hrs · 57,432 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 931, STR 22R. REPAIRED SKIN PER SRM.

Part: SLIDE — DISLODGED (R2 DOOR) · airframe 60,229 hrs · 56,815 cycles

R2 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 60,157 hrs · 56,754 cycles

DURING SCHEDULED RON CHECK, AFT GALLEY EMERGENCY EXIT LIGHTS BATTERY PACK FAILED TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (BS 727D) · airframe 60,056 hrs · 56,673 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,056 hrs · 56,673 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER BEAR STRAP CUTOUT. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,056 hrs · 56,673 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 767 TO BS 797, STR 18L TO STR 19L. REPAIRED SKIN PER SRM.

Part: BULB — FAULTY (NR 1 ENG INDICAT) · airframe 59,998 hrs · 56,629 cycles

INFLIGHT SHUTDOWN/DECLARED EMERGENCY. NR 1 ENGINE OIL TEMPERATURE INDICATED ABOVE RED LINE. REMOVED AND REPLACED NR 1 ENGINE OIL TEMP BULB PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 59,632 hrs · 56,323 cycles

FWD CABIN EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: SIGN — BROKEN (EMERGENCY EXIT) · airframe 59,531 hrs · 56,244 cycles

FWD ENTRY EMERGENCY EXIT SIGN BROKEN. REPAIRED SIGN PER MM.

Part: SMOKE DETECTOR — FAULTY (AFT CARGO) · airframe 59,098 hrs · 55,886 cycles

AIR TURNBACK/DECLARED EMERGENCY. CLIMBING THRU 11,000 FT AFT CARGO FIRE WARNING LIGHT CAME ON. DISCHARGED FIRE BOTTLE & LANDED. NO FIRE INDICATIONS NOTED. REMOVED AND REPLACED 3 EA SMOKE DETECTORS IN AFT CARGO BAY & FIRE WARNING CONTROL UNIT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,946 hrs · 55,751 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT EXTERNAL A/C RECEPTICLE CUTOUT, BS 520. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,946 hrs · 55,751 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 485, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,946 hrs · 55,751 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 913, STR 25L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,205 hrs · 55,168 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 787, STRINGER 19L, CRACKED. REPAIRED SKIN PER SRM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 58,009 hrs · 55,014 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EXIT SIGN LENS MISSING. REMOVED AND REPLACED LENS PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 57,232 hrs · 54,437 cycles

DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 57,218 hrs · 54,421 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM.

Part: BEAM — CRACKED (BULKHEAD) · airframe 56,638 hrs · 53,938 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM AT BS 178, RBL 17.1, WL 226, CRACKED. REMOVED AND REPLACED VERTICAL BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,629 hrs · 53,933 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 884, LBL 9, BS 888 RBL 9, CRACKED. REPAIRED SKIN PER EA.

Part: FLOORBEAM — CORRODED (BS 772) · airframe 56,629 hrs · 53,933 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 772, BETWEEN RBL 8 TO LBL 8 CORRODED. REPAIRED FLOORBEAM PER EA.

Part: HINGE — CRACKED (PAX DOOR) · airframe 56,629 hrs · 53,933 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR UPPER HINGE INTERIOR H-DOUBLER CRACKED. REPAIRED FWD ENTRY DOOR HINGE PER EA.

Part: FITTING — CRACKED (RT & LT WING) · airframe 56,629 hrs · 53,933 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT AND RT CENTER SECTION FITTINGS ABOVE CENTER TANK RT AND LT BS 616, CRACKED. REPAIRED FITTINGS PER T1-153-018.

Part: SPINDLE — FAILED (RT WING TE FLAP) · airframe 56,620 hrs · 53,925 cycles

INBOUND CREW REPORTED A HEAVY THUMP WHEN FLAPS 30 SELECTED. UPON INSPECTION, MX REPORTED RT OUTBOARD FLAP SPINDLE FAILURE. REMOVED AND REPLACED RT OUTBOARD FLAP SPINDLES PER MM.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 56,267 hrs · 53,626 cycles

DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT AT ROW 11 DEF, INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 56,267 hrs · 53,626 cycles

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

Part: LENS — MISSING (CABIN) · airframe 56,159 hrs · 53,541 cycles

DURING SCHEDULED RON, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 56,133 hrs · 53,523 cycles

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

Part: SPOILER — DELAMINATED (LT WING) · airframe 56,124 hrs · 53,545 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT WING NR 4 SPOILER DELAMINATED. REMOVED AND REPLACED NR 4 SPOILER PER MM.

Part: FIRE LOOP — FAULTY (APU BAY) · airframe 56,007 hrs · 53,433 cycles

AIR TURNBACK, DURING CLIMBOUT, APU FIRE INDICATION, C/W QRH AND RETURNED TO IND. REMOVED AND REPLACED APU FWD FIRE LOOP PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 55,945 hrs · 53,382 cycles

DURING SCHEDULED SERVICE CHECK, FOUND KEELBEAM AT BS 727 - 19, STRINGER 27R, AND BS 727 + 9, STRINGER 27L, CORRODED. REPAIRED KEEL BEAM PER EA.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 55,797 hrs · 53,260 cycles

FWD OUTBOARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED OUTBOARD FLASHLIGHT BATTERY PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 55,105 hrs · 52,688 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR CUTOUT FWD LOWER CORNER CRACKED. REPAIRED PER EA.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 54,465 hrs · 52,163 cycles

DURING SCHEDULED C3 CHECK, FOUND RH OUTBD T/E AFT FLAP DELAMINATED AT INBD END. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: BULKHEAD — CRACKED (AFT FUSELAGE) · airframe 54,465 hrs · 52,163 cycles

DURING SCHEDULED C3 CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT STR 6L. REPAIRED WEB PER SRM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 53,284 hrs · 51,208 cycles

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

Part: LENS — MISSING (MID CABIN) · airframe 52,644 hrs · 50,679 cycles

DURING SCHEDULED C1 CHECK, FOUND BOTH LT/RT OVERWING EMERGENCY EXIT LIGHT LENSES MISSING. INSTALLED LENSES PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 52,090 hrs · 50,232 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT BROKEN ADJACENT TO AFT ENTRY DOOR. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 51,671 hrs · 49,908 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND WINDOW FRAMES CRACKED (2 EA) AT LT WINDOW NR 7 AND RT WINDOW NR 11. REMOVED AND REPLACED WINDOW FRAMES PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,405 hrs · 49,695 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT BS 663.75, STR 2R AND RBL 10. REPAIRED FRAME PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 51,405 hrs · 49,695 cycles

DURING SCHEDULED SPECIAL VISIT FOUND STRINGER SPLICES CRACKED (2 EA) AT BS 360 AT STR 4R AND BS 908 AT STR 4L. REMOVED AND REPLACED STRINGER SPLICES PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,405 hrs · 49,695 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIP CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 51,405 hrs · 49,695 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIES CRACKED (2 EA) AT BS 400 BETWEEN STR 15L AND 16L AND BS 787, ABOVE STR 14R. REPAIRED SHEAR TIES PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,405 hrs · 49,695 cycles

DURING SCHEDULED, FOUND STRINGER TIE CLIPS CRACKED (9 EA) BS 380 AT STR 15L, BS 500D AT STR 1L, BS 500D AT STR 4R, BS 520 AT STR'S 2R, 3R AND 4R, BS 767 AT STR 2L, BS 747 AT STR 4R AND BS 787 AT STR 4R. REMOVED AND REPLACED STRINGER TIE CLIPS PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,405 hrs · 49,695 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CRACKED AT BS 401, STR 15L. REPAIRED STRINGER PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,405 hrs · 49,695 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIPS CRACKED (2 EA) AT BS 874 AT STR 4L AND BS 500A AT STR 10L. REMOVED AND REPLACED STRINGER TIE CLIPS PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 49,919 hrs · 48,481 cycles

DURING SCHEDULED C2 CHECK, FOUND OVERHEAD BIN EMERGENCY EXIT BULL NOSE LIGHT LENS LOOSE AT ROW 23 DEF. REMOVED AND REPLACED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,919 hrs · 48,481 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 910, STR 23L. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 49,837 hrs · 48,416 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 847, BETWEEN STR'S 27L AND 27R. REPAIRED SHEAR TIE PER SRM.

Part: HYDRAULIC LINE — LEAKING (B SYSTEM) · airframe 49,595 hrs · 48,223 cycles

AIR TURNBACK, DURING CLIMB LOST B-SYSTEM HYDRAULIC FLUID. REMOVED AND REPLACED HYDRAULIC LINE, FROM B-SYSTEM PRESS MODULE TO THE ACOUSTIC FILTER ASSY PER MM.

Part: FRAME — CRACKED (FWD CARGO DOOR) · airframe 48,893 hrs · 47,624 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD CARGO COMPT DOOR FWD FRAME CRACKED. REPAIRED FRAME PER SB 737-52A1100.

Part: SKIN — CRACKED (AFT SVC DOOR) · airframe 48,893 hrs · 47,624 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT SVC DOOR OUTER SKIN CRACKED AT FWD EDGE ABOVE BOTTOM HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,893 hrs · 47,624 cycles

DURING SCHEDULED 1/2D CHECK, FOUND E/E BAY FRAME CRACKED AT BS 328, STR 20R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,893 hrs · 47,624 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD CARGO COMPT DOOR CUTOUT AT BS 480 + 15', STR 22R. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FWD SVC DOOR) · airframe 48,893 hrs · 47,624 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR AFT FRAME CRACKED ADJACENT TO STR 12R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (E/E BAY DOOR) · airframe 48,893 hrs · 47,624 cycles

DURING SCHEDULED 1/2D CHECK, FOUND E/E BAY DOOR FRAME CRACKED. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,892 hrs · 47,623 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 21R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,892 hrs · 47,623 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED 2 INCHES AT BS 500C, ABOVE STR 10L. REPAIRED SKIN PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 48,892 hrs · 47,623 cycles

DURING SCHEDULED 1/2D CHECK, FOUND OVERHEAD BIN BULLNOSE EMERGENCY EXIT LIGHTS LOOSE AT ROWS 5 DEF AND 23 DEF. SECURED LIGHTS PER MM.

Part: WEB — CRACKED (LT MLG W/W) · airframe 48,892 hrs · 47,623 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BEADED PRESS WEB CRACKED IN CEILING AT BS 663, LBL 33. REPAIRED WEB PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 48,312 hrs · 47,147 cycles

DURING SCHEDULED C4 CHECK, FOUND LT INBD AFT T/E FLAP DELAMINATED ON LOWER SKIN. REMOVED AND REPLACED T/E FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,073 hrs · 43,470 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED .4 INCH AT BS 510, BETWEEN STR 27L AND 28L. REPAIRED SKIN PER SWA RA.

Part: SLAT — CRACKED (LT WING) · airframe 48,312 hrs · 47,147 cycles

DURING SCHEDULED C4 CHECK, FOUND NR 1 L/E SLAT CRACKED (3 EA), 45 INCHES FROM INBD END. REPAIRED NR 1 L/E SLAT PER SWA RA.

Part: SLAT — CRACKED (LT WING) · airframe 48,312 hrs · 47,147 cycles

DURING SCHEDULED C4 CHECK, FOUND NR 2 L/E SLAT CRACKED(3 EA), 38 INCHES FROM OTBD END. REPAIRED NR 2 L/E SLAT PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 48,312 hrs · 47,147 cycles

DURING SCHEDULED C4 CHECK, FOUND EMERGENCY EXIT BULL NOSE LIGHT LOOSE AT ROW NR 3 ABC. SECURED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,312 hrs · 47,147 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED 1.5 INCHES AT BS 500, STR 10L. REPAIRED SKIN PER SRM.

Part: SLIDE — DEPLOYED (FWD ENTRY DOOR) · airframe 48,304 hrs · 47,141 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: HYDRAULIC LINE — CRACKED (RT MLG WW) · airframe 48,186 hrs · 47,036 cycles

(AIR TURNBACK) A-SYSTEM HYDRAULIC FAILURE, PRESSURE TO ZERO, LOW PRESS LIGHT AND FEEL DIFFERENTIAL PRESSURE LIGHT ILLUMINATED. FOUND A-SYSTEM HYD PRESSURE SPOILER LINE CRACKED. REMOVED AND REPLACED LINE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,917 hrs · 46,819 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED ( 3 EA ) AT BS 944, STR 25R, BS 931, STR 25R & BS 937, STR 21L. REPIRED SKIN PER SRM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 47,044 hrs · 46,094 cycles

DURING SCHEDULED RON CHECK, FOUND EMERGENCY FLASHLIGHT AT FWD OTBD INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: TIRE — BLOWN (NLG) · airframe 47,019 hrs · 46,072 cycles

AIR TURNBACK. DURING TAKEOFF RT NOSE TIRE BLEW OUT DAMAGING THE FOLLOWING COMPONENTS. NLG EXTEND SENSOR CONDUIT, LWR TCAS ANTENNA, E&E ACCESS DOOR, ABRAIDABLE SHROUD NR 2 ENG, AFT ACOUSTIC PANEL NR 2 ENG AND FAN BLADES NR 2 ENG. REMOVED AND REPLACED BOTH NOSE TIRES AND WHEEL ASSY'S, SENSOR CONDUIT, TCAS ANTENNA, AND E&E DOOR. REPAIRED SHROUD. REMOVED AND REPLACED ACOUSTIC PANEL, NR 2 ENG FAN BLADES. ALL WORK DONE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,528 hrs · 45,638 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 745, STR 19L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJ (ENTRY DOOR) · airframe 46,528 hrs · 45,638 cycles

DURING SCHEDULE C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. RE-ADJUSTED EMERGENCY EVAC SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 46,528 hrs · 45,638 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDE PER MM.

Part: LENS — MISSING (CABIN) · airframe 46,528 hrs · 45,638 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS LENS MISSING AT ROW 11. REPLACED EEPLS LENS PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 45,695 hrs · 44,940 cycles

DURING CLOSING OF FWD ENTRY DOOR, EVACUATION SLIDE FELL OUT OF BRACKET. SECURED SLIDE ASSY AND COVER PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 45,544 hrs · 44,833 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS LOOSE AT FWD SECTION. SECURED EPPLS PER MM.

Part: SLAT — CRACKED (RT WING) · airframe 45,544 hrs · 44,833 cycles

DURING SCHEDULED C1 CHECK, FOUND 2 INCH CRACKAT NR 6 L/E SLAT EXTENDING FROM AFT ROW OF RIVETS, NEAR CENTER AUX TRACK, OTBD OF PREVIOUS REPAIR. REMOVED AND REPLACED SLAT ASSY PER MM.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 45,544 hrs · 44,833 cycles

DURING SCHEDULED C1 CHECK, FOUND 2 INCH CRACK ON KEEL BEAM, LOWER RT CHORD, BS 681. REPAIRED KEEL BEAM PER SRM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 45,159 hrs · 44,506 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE ASSY OUT OF POSITION. REPOSITIONED EVAC SLIDE ASSY.

Part: BATTERY PACK — INOPERATIVE (CABIN FLOOR) · airframe 44,709 hrs · 44,126 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY LIGHTING FLICKERING WHEN GROUND POWER SELECTED. REMOVED AND REPLACED FWD EMERGENCY LIGHT POWER PACK PER MM.

Part: SLIDE — DISLODGED (GALLEY DOOR) · airframe 44,662 hrs · 44,084 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. SECURED SLIDE ASSY PER MM.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 44,582 hrs · 44,016 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SERVICE DOOR GIRT BAR HOLD DOWN BRACKET LOOSE IN FLOOR. SECURED BRACKET PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,582 hrs · 44,016 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACK AT BS 510, STR 16R. REPAIRED SKIN PER SRM.

Part: CAP — MISSING (CABIN FLOOR) · airframe 44,582 hrs · 44,016 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS TRACK END CAP MISSING AT FWD END. INSTALLED END CAP PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,546 hrs · 43,984 cycles

DURING SCHEDULED D-CHECK, FOUND BS 178 LT AND RT SIDE CHORDS CRACKED AT WL 207. REMOVED AND REPLACED SIDE CHORDS PER ACO 7338-53 AND ACO 7342-53.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 44,546 hrs · 43,984 cycles

DURING SCHEDULED SPECIAL VISIT AT DALFORT, FOUND BS 178 BLKHD WEBS CRACKED AT WL 219 LBL 10, WL 218 LBL 11.5, WL 207 RBL 25 AND LBL 25. REPAIRED BULKHEAD PER ACO 7154-53 AND SRM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 44,434 hrs · 43,890 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,723 hrs · 43,297 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED BS 298 - BS 312, BETWEEN STRINGERS 17R - 18R. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,723 hrs · 43,297 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 42,624 hrs · 42,330 cycles

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

Part: SLIDE — DISLODGED (PAX DOOR)

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

Part: SKIN — CRACKED (BS 500C)

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 500C, STRINGER 15R. REPAIRED SKIN PER SRM AND SWA RA NR 1-353-2201.

Part: SLIDE — DETACHED (SERVICE DOOR)

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

Part: POWER SUPPLY — INOP (CABIN)

DURING SCHEDULED 1/4D CHECK, FOUND EEPLS LIGHTS DIMMED. REMOVED AND REPLACED AFT EEPLS POWER SUPPLY PER MM.

Part: SKIN — CORRODED (BS 727)

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION BULGE AT LOWER FUSELAGE EXTERNAL SKIN, BS 727. REPAIRED SKIN PER XEA X2-53-251, REVISION 1.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, RBL 5. REPAIRED BULKHEAD PER SRM.

Part: SEAL — LEAKING (PAX DOOR)

AIR TURNBACK DUE TO FWD ENTRY DOOR HAVING A VERY LOUD PRESSURIZATION LEAK. ADJUSTED LOWER HINGE COVER SEAL PER MM.

Part: FRAME — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED C2 CHECK, FOUND AFT SERVICE DOOR FRAME CRACKED AT LOWER HINGE CUTOUT, FWD LOWER RADIUS. REPAIRED PER SWA RA NR 1-353-2035.

Part: BATTERY — DISCHARGED (CABIN)

FWD I/B FLASHLIGHT TEST LIGHT NOT FLASHING. REPLACED BATTERY ASSY PER MM.

Part: SLIDE — DISENGAGED (PAX DOOR)

FORWARD ENTRY ESCAPE SLIDE FELL OUT WHILE TRYING TO CLOSE DOOR FOR DEPARTURE. RESTOWED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (R2 DOORWAY)

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED, .75 LENGTH AT UPPER HINGE CUTOUT AT R2 DOOR. REPAIRED PER SWA RA 1-353-1794.

Part: SKIN — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED B/C CHECK, FOUND AFT SERVICE DOOR UPPER HINGE CUTOUT AND STRAP CRACKED. REPAIRED PER BOEING SRM.

Part: SEAL — PRESS LEAK (SERVICE DOOR)

RETURNED TO DAL DUE TO FWD SERVICE DOOR PRESSURE LEAK SQUEALING. AIRCRAFT LANDED WITHOUT INCIDENT. REWORKED DOOR SEAL MATING SURFACE AND PRESSURE CHECKED PER BOEING M/M.

Part: LONGERON — GOUGED (NR 2 PYLON)

DURING SCHEDULED D-CHECK, FOUND NR 2 PYLON LONGERON AND DOUBLER GOUGED. REPAIRED PER BOEING SRM.

Part: SUPPORT BEAM — CORRODED (BS 967)

DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT BEAM CORRODED AT BS 967, LBL 18. REPAIRED PER BOEING SRM.

Part: CLIPS — CRACKED (BS 663.75)

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS AT S10 LT AND RT CRACKED AT BS 663.75. ALSO, S13L AT BS 1138. REPLACED PER BOEING SRM.

Part: FRAME — DAMAGED (BS 907)

DURING SCHEDULED D-CHECK, FOUND BS 907 FRAME DAMAGED AT LBL 2 AND RBL 2. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 365-370)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 365 TO 370, S4L. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 378)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 378, AT S22R, BELOW 02 BLOWOUT. REPAIRED PER BOEING SRM.

Part: WEB — CORRODED (BS 1016)

DURING SCHEDULED D-CHECK, FOUND UPPER SURFACE OF WEB CORRODED AT BS 1016. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT LBL .5 TO 1.75 AT RBL 4.7, LBL 6.7, LBL 2.0, RBL .5 AND AT RBL 11.5 TO 12.25. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 480)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT HAT SECTION ATTACH BRACKET AT STRINGER 9R. REPAIRED PER BOEING SRM.

Part: FRAME — DENTED (BS 827)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME DENTED AT BS 827, LBL 43, WL 171. REPAIRED PER BOEING SRM.

Part: DOOR FRAME — CRACKED (BS 494)

DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR FRAME CRACKED AT BS 494, RBL 36. REPAIRED PER EWO 97-0044.

Part: ANGLE — CORRODED (BS 992)

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM CHORD ANGLE CORRODED AT BS 992, LBL 77, WL 208. REPLACED DAMAGED SECTION PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 312)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CHORD CORRODED AT BS 312, AT LBL 39.26 AND RBL 7.5. REPAIRED PER BOEING SRM.

Part: AOA VANE — BROKEN (FUSE)

IN FLIGHT, EXPERIENCED STALL WARNING IN FLIGHT, WITH STICK SHAKER, CREW LOWERED FLAPS AND EXTENDED SLATS TO FULL DOWN. AIRCRAFT RETURNED TO MDW AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND AOA VANE BROKEN OFF. REPLACED AOA VANE AND OP CHECKED SYSTEM PER BOEING M/M.

Part: STRINGER — CRACKED (BS 727)

DURING SCHEDULED A-CHECK, FOUND STRINGER 18A AT BS 727 CRACKED ON LEFT AND RIGHT SIDES. REPAIRED PER SWA ACO 6580-53.

Part: SKIN — CRACKED (PAX DOOR)

DURING SCHEDULED B/C CHECK, FOUND FWD ENTRY DOOR UPPER HINGE CUTOUT CRACKED IN LOWER CORNER. REPAIRED PER SWA RA 1-352-206.

Part: SKIN — CRACKED (SERVICE DOOR)

DURING SCHEDULED B/C CHECK, FOUND FWD SERVICE DOOR UPPER HINGE CUTOUT CRACKED IN UPPER CORNER. REPAIRED PER SWA RA 1-252-207.