N327SW

Part: SKIN — LOOSE (SPOILER) · airframe 76,766 hrs · 69,223 cycles

RT WING NR 9 GROUND SPOILER SKIN LOOSE. REMOVED AND REPLACED SPOILER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,595 hrs · 69,078 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 791, STR 6R. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 76,595 hrs · 69,078 cycles

DURING SCHEDULED CV CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FUSE — BLOWN (CABIN) · airframe 76,301 hrs · 68,847 cycles

DURING SCHEDULED MV1 CHECK FOUND, FWD EEPLS INOP. REMOVED AND REPLACED FUSE PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 75,791 hrs · 68,441 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND AFT EEPLS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND FWD LAV AFT WALL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER SOPM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,414 hrs · 68,146 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 305, STR 7R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,414 hrs · 68,146 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 240, STR 17L. REPAIRED SKIN PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 420, STR 26R. REPAIRED FRAME PER ER AND EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 809, STR 26R. REPAIRED STRINGER PER ER.

Part: LIGHT — BROKEN (CABIN) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT SIDEWALL OVERWING EMERGENCY EXIT DOOR LIGHT BROKEN. REMOVED AND REPLACED LIGHT PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CRACKED AT BS 1006, STR 12L. REMOVED AND REPLACED STRINGER PER SRM.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND BUTT SPLICE CORROED AT BS 727, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SPLICE PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND L2 DOOR STUB FRAME CRACKED AT BS 955, WL 254. REMOVED AND REPLACED FRAME PER SRM AND BAC DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME SHEAR TIE CRACKED AT BS 947, STR 4L TO STR 5L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 664, RBL 24.8. REPAIRED BEAM PER ER AND EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 10 TO RBL 10. REPAIRED BEAM PER ER AND SWA EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 26L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND NR 4 L/E SLAT DELAMINATED AT T/E. REPAIRED SLAT PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND NR 5 L/E SLAT SKIN CRACKED AT T/E. REPAIRED SKIN PER SRM.

Part: SLAT — DELAMINATED (RT WING) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING NR 6 SLAT UPPER T/E INBOARD END DELAMINATED. REPAIRED SLAT PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 947, STR 4L. REPAIRED SKIN PER ER.

Part: BEAM — CRACKED (FUSELAGE) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL BEAM CRACKED AT BS 727B-3, RBL 45.5. REPAIRED BEAM PER EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 846, RBL 2.5. REMOVED AND REPLACED SUPPORT PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED BETWEEN BS 700 TO BS 712, BBL 0.07. REPAIRED WEB PER SI.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOOR SUPPORT ANGLE CORRODED AT BS 773, LBL 12. REPAIRED ANGLE PER BAC DWG AND SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CORRODED AT BS 905.5, BL 0. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 827, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOOR SUPPORT ANGLE CORRODED AT BS 773, RBL 7.5 REPAIRED ANGLE PER BAC DWG AND EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOOR SUPPORT ANGLE CORRODED AT BS 825, LBL 7.5. REPAIRED ANGLE PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 26L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 20L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 26L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,414 hrs · 68,145 cycles

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 860, RBL 7.5. REMOVED AND REPLACED SUPPORT PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 813, RBL 7.5. REMOVED AND REPLACED SUPPORT PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 26L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 732D, LBL 2.5. REPAIRED SUPPORT PER EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 860, LBL 12. REMOVED AND REPLACED SUPPORT PER EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 860, RBL 2.5. REMOVED AND REPLACED SUPPORT PER EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 732D, LBL 7.5. REPAIRED SUPPORT PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 28L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 75,414 hrs · 68,145 cycles

DURING SCHEDULED 24Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR RETAINTER BRACKET LOOSE. REMOVED AND REPLACED BRACKET PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,041 hrs · 67,032 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 266.5, STR 9L. REPAIRED SKIN PER SRM.

Part: COVER — LOOSE (CABIN) · airframe 73,309 hrs · 66,491 cycles

DURING SCHEDULED CV CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER PER MM.

Part: COVER — LOOSE (CABIN) · airframe 73,309 hrs · 66,491 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,618 hrs · 65,981 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 500D, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,618 hrs · 65,981 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 500D, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 72,236 hrs · 65,687 cycles

EEPLS LOOSE AT ROW 8. REPAIRED EEPLS PER MM.

Part: LENS — MISSING (CABIN) · airframe 71,239 hrs · 64,937 cycles

FWD EMERGENCY EXIT LIGHT LENS COVER MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,077 hrs · 64,803 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 360, STR 8L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 71,077 hrs · 64,803 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 71,077 hrs · 64,803 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD RETAINING BRACKET LOOSE. SECURED BRACKET PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 70,924 hrs · 64,692 cycles

DURING SCHEDULED MV1 CHECK, FOUND AFT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY ASSY PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 69,472 hrs · 63,660 cycles

L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. REINSTALLED SLIDE ASSY PER MT.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,978 hrs · 64,032 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,978 hrs · 64,032 cycles

DURING SCHEDULED 22Y CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 69,978 hrs · 64,032 cycles

DURING SCHEDULED 22Y CHECK, FOUND BULKHEAD HORIZONTAL FLANGE CRACKED AT BS 663, RBL 6. REPAIRED BULKHEAD PER DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 69,978 hrs · 64,032 cycles

DURING SCHEDULED 22Y CHECK, FOUND BULKHEAD HORIZONTAL FLANGE CRACKED AT BS 663, LBL 6. REPAIRED BULKHEAD PER DWG.

Part: SLAT — CRACKED (RT WING) · airframe 69,978 hrs · 64,032 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING 6 SLAT CRACKED O/B OF ACTUATOR. REMOVED AND REPLACED SLAT PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 69,978 hrs · 64,032 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING NR 1 SLAT SKIN CRACKED AT O/B CORNER. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,978 hrs · 64,032 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 1006, LBL 2. REPAIRED BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,591 hrs · 63,752 cycles

DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 312, STR 19R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 68,973 hrs · 63,291 cycles

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

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 68,973 hrs · 63,291 cycles

R1 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. REPOSITIONED SLIDE ASSY PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,822 hrs · 63,181 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT AFT CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,822 hrs · 63,181 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LENS — LOOSE (CABIN) · airframe 68,437 hrs · 62,880 cycles

FWD CABIN EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 68,155 hrs · 62,680 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,155 hrs · 62,680 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 578, STR 13R. REPAIRED FRAME PER ER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,155 hrs · 62,680 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,155 hrs · 62,680 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 430 AND BS 450, STR 28R AND STR 28L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,155 hrs · 62,680 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 540, STR 17R. REPAIRED SKIN PER ER.

Part: HINGE FITTING — CRACKED (KRUEGER FLAP) · airframe 68,155 hrs · 62,680 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING NR 4 KRUEGER FLAP INBOARD HINGE FITTING CRACKED. REMOVED AND REPLACED FITTING PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,155 hrs · 62,680 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,155 hrs · 62,680 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 14R. REPAIRED FRAME PER ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 68,155 hrs · 62,680 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 28L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 68,155 hrs · 62,680 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 22R. REPAIRED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,155 hrs · 62,680 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 887 TO BS 907, RBL 65. REMOVED AND REPLACED WEB PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,155 hrs · 62,680 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 927, STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,155 hrs · 62,680 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 328, STR 21R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 747 S24L) · airframe 68,155 hrs · 62,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 24L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 68,155 hrs · 62,680 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 344, STR 18R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,155 hrs · 62,680 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 19R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,155 hrs · 62,680 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 485, STR 26R. REPAIRED SKIN PER ACO.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 68,155 hrs · 62,680 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CRACKED AT STR 17R. REPAIRED FRAME PER BOEING DRAWING.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 68,155 hrs · 62,680 cycles

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

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 68,155 hrs · 62,680 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,155 hrs · 62,680 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 20R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,155 hrs · 62,680 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,155 hrs · 62,680 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 420, STR 13R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,155 hrs · 62,680 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 21L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,155 hrs · 62,680 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 20L. REPAIRED FRAME PER ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 68,155 hrs · 62,680 cycles

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

Part: LENS — CRACKED (EXTERIOR) · airframe 68,155 hrs · 62,680 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,155 hrs · 62,680 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 20R. REPAIRED FRAME PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,515 hrs · 62,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 11R CRACKED AT BS 540. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,155 hrs · 62,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,155 hrs · 62,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,155 hrs · 62,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,155 hrs · 62,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 68,155 hrs · 62,680 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 908, STR 15L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,155 hrs · 62,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,155 hrs · 62,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,155 hrs · 62,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,155 hrs · 62,680 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,155 hrs · 62,680 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,155 hrs · 62,680 cycles

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

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 68,066 hrs · 62,617 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,746 hrs · 62,382 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 464 TO BS 470, STR 16R. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,343 hrs · 61,325 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 20R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,343 hrs · 61,325 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 373, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,343 hrs · 61,325 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 952, STR 22R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,343 hrs · 61,325 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 28R. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,343 hrs · 61,325 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE FUSELAGE FRAME CRACKED AT BS 344, STR 24L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,249 hrs · 61,252 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 328, STR 18R. REPAIRED SKIN PER SWA EA.

Part: BLADE — WARPED (NR 2 ENGINE) · airframe 66,098 hrs · 61,143 cycles

NR 2 ENG FAN BLADES NR 6 & NR 7 WARPED. REMOVED AND REPLACED BOTH NR 2 ENG FAN BLADES PER MM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 64,839 hrs · 60,162 cycles

DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM CHORD CRACKED AT BS 639, LBL 70. REMOVED AND REPLACED CREASE BEAM CHORD PER ER.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND RIGHT CREASE BEAM CRACKED AT BS 639, RBL 70. REPAIRED CREASE BEAM PER ER.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 6L. REPAIRED BULKHEAD WEB PER ER.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 6R. REPAIRED BULKHEAD WEB PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 414, LBL 2. REPAIRED SKIN PER ER.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 13L. REPAIRED BULKHEAD WEB PER ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 11 TO LBL 13. REPAIRED FLOORBEAM PER ER.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 660, BL 0. REPAIRED FLOORBEAM PER ER.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 64,808 hrs · 60,141 cycles

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

Part: CABLE — FRAYED (EVAC SLIDE) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED EVAC SLIDE CABLE PER MM.

Part: HOOK — LOOSE (L2 DOOR) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CRACKED AT BS 947, LBL 53. REMOVED AND REPLACED FLOORBEAM PER ER.

Part: STRINGER SPLICE — CRACKED (BS 360 S15L) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: GIRT BAR — CORRODED (L1 DOOR) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED GIRT BAR FITTING PER SRM.

Part: TORQUE TUBE — FAILED (RT ELEVATOR) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, RT ELEVATOR BUSS LINKAGE FAILED TEST. REMOVED AND REPLACED ELEVATOR OUTPUT TORQUE TUBE PER MM.

Part: FRAME — CRACKED (BS 639 S8R) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 8R. REPAIRED FRAME PER SRM.

Part: GIRT BAR — CORRODED (L1 DOOR) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED GIRT BAR FITTING PER SRM.

Part: FRAME — CRACKED (BS 303 S16L) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303, STR 16L. REPAIRED FRAME PER ER AND SB.

Part: FRAME — CRACKED (BS 663 S3L) · airframe 64,808 hrs · 60,141 cycles

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

Part: FLOORBEAM — CORRODED (BS 344) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 344, RBL 9 TO LBL 50. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER — CORRODED (BS 420-513A) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER 27L CORRODED AT BS 420 TO BS 513A. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 64,808 hrs · 60,141 cycles

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

Part: FRAME — CORRODED (BS 847 S25R) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 847, STR 25R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FLOORBEAM — CORRODED (BS 1016) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 1016, RBL 30 TO RBL 35. REPAIRED FLOORBEAM PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 277 S10R) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 294 S13L) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 400 S8L) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SHEAR TIE — CORRODED (BS 847 S27R) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 847, STR 27R. REMOVED AND REPLACED SHEAR TIE PER ACO.

Part: FRAME — CRACKED (BS 807 S8L) · airframe 64,808 hrs · 60,141 cycles

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

Part: FRAME — CRACKED (BS 500A S8L) · airframe 64,808 hrs · 60,141 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 520 S8R) · airframe 64,808 hrs · 60,141 cycles

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

Part: SKIN — DELAMINATED (NR 4 SLAT) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND RIGHT WING NR 4 L/E SLAT DELAMINATED AT OUTBOARD END. REPAIRED L/E SLAT PER SRM.

Part: FRAME — CRACKED (BS 867 S8R) · airframe 64,808 hrs · 60,141 cycles

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

Part: FRAME — CRACKED (BS 847 S8R) · airframe 64,808 hrs · 60,141 cycles

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

Part: FRAME — CRACKED (BS 480 S8L) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 500C S8R) · airframe 64,808 hrs · 60,141 cycles

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

Part: SHEAR TIE — CORRODED (BS 827 S25L) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 827, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 766 S11R) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 766, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLOORBEAM — CORRODED (BS 967) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 967, RBL 5. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727D S5R) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 43. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (BS 947) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947, LBL 5 AND LBL 11. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (BS 927) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 927, LBL 5 AND LBL 11. REPAIRED FLOORBEAM PER SRM.

Part: SHEAR TIE — CRACKED (BS 460) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 460, STR 13R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 663 S10L) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (BS 400 S14R) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 400, STR 14R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727A S5L) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 766 S11L) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 766, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 907 S8R) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 294) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 294, RBL 27, WL 208. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CRACKED (BS 947 S3L) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 947.5, STR 3L. REPAIRED FRAME SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727D S5R) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 807 S11R) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727A S6L) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 827 S11R) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: TORQUE TUBE — CORRODED (LT TE FLAP) · airframe 64,808 hrs · 60,141 cycles

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

Part: STRINGER CLIP — CRACKED (BS 727D S6L) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (BS 277 S11L) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 277, STR 11L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: WEDGE — DEBONDED (T/E FLAP) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND LEFT WING INBOARD MID FLAP T/E WEDGE LOWER T/E OUTBOARD END DISBONDED. REPAIRED MID FLAP PER SRM.

Part: SKIN — DELAMINATED (FORE FLAP) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING INBOARD FORE FLAP UPPER SKIN DELAMINATED AT OUTBOARD END. REPAIRED FORE FLAP PER SRM.

Part: TORQUE TUBE — CORRODED (T/E FLAP) · airframe 64,808 hrs · 60,141 cycles

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

Part: TORQUE TUBE — CORRODED (T/E FLAP) · airframe 64,808 hrs · 60,141 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 64,808 hrs · 60,141 cycles

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

Part: TORQUE TUBE — CORRODED (T/E FLAP) · airframe 64,808 hrs · 60,141 cycles

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

Part: TORQUE TUBE — CORRODED (T/E FLAP) · airframe 64,808 hrs · 60,141 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 64,808 hrs · 60,141 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 480, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 21R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT R1 DOOR AFT CUTOUT NR 4 DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 21R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,808 hrs · 60,141 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 21R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (BS 386 S15R) · airframe 64,338 hrs · 59,778 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 386, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 366 S16R) · airframe 64,338 hrs · 59,778 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 366, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 396 S15R) · airframe 64,338 hrs · 59,778 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 396, STR 15R. REPAIRED SKIN PER SWA EA.

Part: MOTOR — SEIZED (T/E FLAP) · airframe 63,661 hrs · 59,231 cycles

ON FINAL APPROACH, T/E FLAPS WOULD NOT EXTEND. COULD NOT EXTEND FLAPS ELECTRICALLY DUE TO OPEN CB. REMOVED AND REPLACED FLAP DRIVE MOTOR PER MM.

Part: SKIN — CRACKED (BS 939 S21L) · airframe 63,570 hrs · 59,157 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 939.5, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 505D-515D) · airframe 63,570 hrs · 59,157 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 505D TO BS 512D, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 944 S23L) · airframe 63,570 hrs · 59,157 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 944, STR 23L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (BS 847) · airframe 62,454 hrs · 58,262 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME WEB CRACKED AT BS 847, AFT CARGO DOOR CUTOUT NR 1 DOOR STOP FITTING. REPAIRED FRAME WEB PER ER.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 62,454 hrs · 58,262 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 494, FWD CARGO DOOR CUTOUT #1 STOP PAD. REPAIRED FRAME SECTION PER ER AND SB.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 62,454 hrs · 58,262 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME WEB CRACKED AT BS 794, AFT CARGO DOOR CUTOUT #5 STOP PAD. REPAIRED FRAME WEB PER ER AND SB.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 62,454 hrs · 58,262 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 440, FWD CARGO DOOR CUTOUT #5 STOP PAD. REPAIRED FRAME SECTION PER ER AND SB.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 62,454 hrs · 58,262 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT BS 442, STR 19R. REPAIRED FUSELAGE SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,454 hrs · 58,262 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 441, STR 22R. REPAIRED FUSELAGE SKIN PER SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,454 hrs · 58,262 cycles

DURING SCHEDULED SPV CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 12 DEF. RELAMPED LIGHT PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,454 hrs · 58,262 cycles

DURING SCHEDULED SPV CHECK, FOUND SEVERAL EMERGENCY EXIT LIGHTS INOP IN FWD CABIN. RELAMPED LIGHTS PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,454 hrs · 58,262 cycles

DURING SCHEDULED SPV CHECK, FOUND EMERGENCY EXIT SLIDE LIGHT INOP AT L2 DOOR. RELAMPED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,454 hrs · 58,262 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 953, STR 24R. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 62,069 hrs · 57,984 cycles

DURING SCHEDULED C3 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 58,177 hrs · 54,833 cycles

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

Part: SKIN — CRACKED (BS 520) · airframe 61,128 hrs · 57,233 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 480) · airframe 61,128 hrs · 57,233 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 480, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 370) · airframe 60,577 hrs · 56,803 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 370, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,386 hrs · 56,652 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 801 TO BS 805, STR 17L. MX FERRY TO PHX FOR REPAIRS. REPAIRED SKIN PER SWA EA & SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 60,163 hrs · 56,466 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,297 hrs · 55,754 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 11L TO STR 12L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,297 hrs · 55,754 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 817, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,297 hrs · 55,754 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 58,921 hrs · 55,434 cycles

RIGHT WING INBOARD T/E FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.

Part: SLIDE — OUT OF ADJUST (L2 & R2 DOORS) · airframe 58,301 hrs · 54,933 cycles

DURING SCHEDULED C3 CHECK, FOUND L2 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED BOTH L2 AND R2 DOOR EVAC SLIDES PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,860 hrs · 54,599 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN AT BS 400 + 4, STRINGER 16R, CRACKED. REPAIRED SKIN SECTION PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,860 hrs · 54,599 cycles

DURING SCHEDULED A1 CHECK, FOUND STRINGER 23R AT BS 499, CRACKED. REPAIRED STRINGER PER SRM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,984 hrs · 53,891 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT AFT WING EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT BATTERY PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 56,554 hrs · 53,523 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT KEELBEAM AT BS 500C, RBL 12, CORRODED. REMOVED AND REPLACED KEEL BEAM CHORD SECTION PER EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 56,554 hrs · 53,523 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD VERTICAL BEAM WEB AT BS 178, RBL 17, CRACKED. REPAIRED WEB PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 56,554 hrs · 53,523 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 663, LBL 33, CRACKED. REPAIRED PRESSURE WEB PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 56,224 hrs · 53,522 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 727, STRINGER 27L, CORRODED. REPAIRED SKIN PER EA.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 56,554 hrs · 53,522 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SEVERAL PHOTOLUMINESCENT STRIPS THROUGHOUT CABIN, DAMAGED. REMOVED AND REPLACED PHOTOLUMINESCENT STRIPS PER MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 56,554 hrs · 53,522 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 727 + 15, STRINGER 27L, CORRODED. REPAIRED SKIN PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,554 hrs · 53,522 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 500C + 16, RBL 13.8, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 56,554 hrs · 53,522 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO DOOR FWD FRAME CUTOUT, CRACKED. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,554 hrs · 53,522 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 773, RBL 3 TO LBL 17, CORRODED. REPAIRED FLOORBEAM PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,458 hrs · 53,470 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 960, STRINGER 21L, CRACKED. REPAIRED SKIN PER EA.

Part: LENS — LOOSE (CABIN) · airframe 56,064 hrs · 53,120 cycles

DURING SCHEDULED PM CHECK, FOUND EMERGENCY EXIT LIGHT LENS AT ROW 6 ABC, LOOSE. SECURED LIGHT LENS PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,936 hrs · 53,019 cycles

DURING SPV, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,790 hrs · 52,901 cycles

DURING SPV, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED L2 DOOR EMERGENCY EXIT LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,719 hrs · 52,843 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STRINGER 14R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,719 hrs · 52,843 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STRINGER 18L. REPAIRED SKIN PER SRM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 55,719 hrs · 52,843 cycles

DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP+) · airframe 54,776 hrs · 52,124 cycles

DURING SCHEDULED C3 CHECK, FOUND RT WING OUTBOARD AFT FLAP DISBONDED AT INBOARD END. REMOVED AND REPLACED FLAP PER MM.

Part: WEDGE — DELAMINATED (RT WING TE FLAP) · airframe 54,776 hrs · 52,124 cycles

DURING SCHEDULED C3 CHECK, FOUND RIGHT WING INBOARD MID FLAP T/E WEDGE DISBONDED. REMOVED AND REPLACED AFT WEDGE PANEL PER MM.

Part: LATCH — LOOSE (FWD ENTRY DOOR) · airframe 53,792 hrs · 51,338 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMRGENCY EVAC SLIDE GIRT ASSY LATCH LOOSE. SECURED LATCH PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 51,751 hrs · 49,754 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,505 hrs · 49,553 cycles

DURING SCHEDULED SERVICE CHECK, FOUND A 3.5 INCH LONG CRACK AT FUSELAGE SKIN, BS 328, BELOW STRINGER 18R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,093 hrs · 49,211 cycles

DURING SCHEDULED CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 980, BELOW STR 20L. REPAIRED SKIN PER SRM.

Part: CABLE — MISROUTED (AFT ENTRY DOOR) · airframe 51,093 hrs · 49,211 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY CABLE MISROUTED. REROUTED CABLE PER MM.

Part: SLIDE — OUT OF ADJUST (CABIN DOORS) · airframe 51,093 hrs · 49,211 cycles

DURING SCHEDULED C3 CHECK, FOUND BOTH FWD ENTRY AND AFT SVC CABIN DOOR EMERGENCY EVAC SLIDES GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDES PER MM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 50,934 hrs · 49,092 cycles

DURING SCHEDULED PM CHECK, FOUND LT VERTICAL CHORD CRACKED AT BS 663, RBL 6.5. REPAIRED CHORD PER SWA EA.

Part: CABLE — MISROUTED (AFT ENTRY DOOR) · airframe 49,211 hrs · 47,656 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 48,769 hrs · 47,271 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 48,468 hrs · 47,022 cycles

DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, ABOVE STR 10R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 48,468 hrs · 47,022 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4R. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,463 hrs · 47,018 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 663 FUSELAGE FRAME CRACKED AT STRINGERS 2L AND 2R. REPAIRED FRAME PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,463 hrs · 47,018 cycles

DURING SCHEDULED 1/2D CHECK, FOUND EEPLS INOP. REPAIRED EEPLS PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 48,468 hrs · 47,022 cycles

DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 14L. REMOVED AND RELACED SHEAR TIE PER SRM.

Part: LOCK — DAMAGED (GIRT FITTING) · airframe 48,463 hrs · 47,018 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BOTH AFT DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR BRACKET LOCKS, WITH DAMAGED HARDWARE ON FWD AND AFT LOCKS. REMOVED AND REPLACED HARDWARE PER MM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 48,468 hrs · 47,018 cycles

DURING SCHEDULED 1/2D CHECK, FOUND WEB CRACKED BELOW FLOOR AT BS 578, STR 17R. REPAIRED WEB PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 48,463 hrs · 47,018 cycles

DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CORRODED AT BS 960, STR 25R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,463 hrs · 47,018 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SVC DOOR UPPER CUTOUT. REPAIRED SKIN PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 48,463 hrs · 47,018 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIPS CRACKED (2 EACH) AT BS 1138, STR 14L AND 16L. REMOVED AND REPLACED STR TIE CLIPS PER SRM.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 48,373 hrs · 46,943 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR FWD FRAME CRACKED AT UPPER SECTION. REMOVED AND REPLACED DOOR PER MM..

Part: LENS — LOOSE (CABIN) · airframe 47,547 hrs · 46,243 cycles

DURING SCHEDULED C3 CHECK, FOUND LH EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 47,547 hrs · 46,243 cycles

DURING SCHEDULED BC3 CHECK, FOUND RT AFT EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT PER MM.

Part: INDICATOR — OUT OF TOLERANCE (EVAC SLIDE) · airframe 45,662 hrs · 44,647 cycles

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

Part: UPLOCK SENSOR — OUT OF ADJ (LT MLG) · airframe 45,610 hrs · 44,607 cycles

AIR TURNBACK, DECLARED EMERGENCY. LEFT MLG RED LIGHT REMAINED ILLUMINATED UPON GEAR RETRACTION. CYCLED GEAR, LIGHT REMAINED ILLUMINATED. REPOSITIONED UPLOCK TARGET SENSOR & OPS CHECK GOOD PER MM.

Part: SLIDE — OUT OF ADJ (AFT PAX DOOR) · airframe 45,295 hrs · 44,352 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY PER MM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 44,720 hrs · 43,914 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 6 FUSELAGE SKIN CREASE AT BS 328, BETWEEN STR 22R & 23R. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 47,555 hrs · 43,787 cycles

DURING SCHEDULED SPECIAL VISIT CHECK AT DALFORT, FOUND BS 178 BULKHEAD CRACKS AT WL 207, RBL 17 - LBL 7.4. REPAIRED BULKHEAD PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,555 hrs · 43,787 cycles

DURING SCHEDULED SPECIAL VISIT AT DALFORT, FOUND BS 178 BULKHEAD CRACKED AT WL 207, LBL 24. REMOVED AND REPLACED LT SIDE CHORD PER ACO 7338-53.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,555 hrs · 43,787 cycles

DURING SCHEDULED SPECIAL VISIT AT DALFORT, FOUND BS 178 BULKHEAD SIDE CHORD CRACKED AT WL 207, LBL 24. REMOVED AND REPLACED SIDE CHORD PER ACO 7338-53.

Part: COVER — DAMAGED (ROW 9) · airframe 44,555 hrs · 43,787 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND EEPLS TRACK COVER DAMAGED AT ROW 9. REPLACED TRACK COVER PER MM.

Part: GIRT BAR — OUT OF ADJ (ESCAPE SLIDE) · airframe 43,770 hrs · 43,109 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE GIRT ASSY OUT OF ADJUSTMENT. ADJUSTED GIRT ASSY PER MM.

Part: SKIN — CRACKED (HORZONTAL STAB) · airframe 42,889 hrs · 42,351 cycles

DURING SCHEDULED C2 CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED, BS 125 ON AFT SPAR. REPAIRED SKIN PER SRM.

Part: BATTERY ASSY — INOP (CABIN)

DURING SCHEDULED RON, FOUND EEPLS FWD SECTION INOP. REMOVED AND REPLACED BATTERY ASSY PER MM.

Part: LENS — CRACKED (SRVC DOORWAY)

DURING SCHEDULED 1/4D CHECK, FOUND EMERGENCY EXIT LIGHT LENS CRACKED ABOVE AFT SERVICE DOOR. REMOVED AND REPLACED LENS PER MM.

Part: LENS — MISSING (ROW 7)

EMERGENCY LIGHT LENS MISSING FROM OVERHEAD BIN BULLNOSE AT ROW 7 ABC. INSTALLED LENS PER MM.

Part: SLIDE — LOW PRESSURE (PASSENGER DOOR)

FWD ENTRY DOOR ESCAPE SLIDE BOTTLE PRESSURE IS LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: SLIDE — OUT OF POSITION (PAX DOOR)

FWD ENTRY DOOR SLIDE WILL NOT STAY SECURE. REMOVED AMD REPLACED FWD ENTRY DOOR SLIDE PER M/M, GROUND OPS CK'S NORMAL.

Part: SLIDE — LOOSE (CABIN)

DURING PREFLIGHT, FOUND FWD ENTRY DOOR SLIDE WOULD NOT REMAIN SECURED. REPLACED PER BOEING M/M.

Part: STRAP — OUT OF POSITION (SERVICE DOOR)

AFTER TAKEOFF, NOTED NOISE FROM FWD SERVICE DOOR AREA. AIRCRAFT RETURNED TO BWI AND LANDED WITHOUT INCIDENT. INSPECTED AND FOUND A SAFETY STRAP STUCK OUTSIDE OF DOOR. RESECURED FWD SERVICE DOOR SAFETY STRAP INSPECTED DOOR AND FRAME FOR DAMAGE. NO DAMAGE NOTED, OK TO CONTINUE.

Part: ENGINE — MALFUNCTIONED (NR 1)

UNSCHEDULED NR 1 ENGINE CHANGE DUE TO PERFORMANCE, RUNNING HOT. REPLACED ENGINE PER BOEING M/M.

Part: LIGHT — INOPERATIVE (FWD ENTRY)

DURING SCHEDULED TERMINAL CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHT INOP. RELAMPED PER BOEING M/M.

Part: SKIN — DENTED (BS 947.5/1006)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 947.5 +14, AND 18, BELOW S19L, WL 189, AND AT BS 1006, BETWEEN S21 AND 22L. REPAIRED PER BOEING SRM.

Part: SKIN — GOUGED (BS 345-348)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 345 AND 348, BETWEEN S17 AND 18R. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 294.5)

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 294.5, WL 269, RBL 49. REMOVED AND REPLACED FRAME STUB PER BOEING SRM.

Part: FLOORBEAM — CRACKED (BS 1138)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CHORD CRACKED AT BS 1138 PLUS 4, WL 294. REPAIRED PER BOEING SRM.

Part: SKIN — GOUGED (BS 500)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 500 PLUS 10, BETWEEN S23 AND 24L. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 340)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 340, BELOW S18R AT BS 807, FROM S25 TO 27, AND AT BS 349 TO 355, BETWEEN S1 AND 2R. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CRACKED (BS 947)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CRACKED AT BS 947, LBL 53, WL 208. REPAIRED PER BOEING SRM.

Part: SKIN — GOUGED (BS 403/450)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 403, AT S18 AND 19R AND AT BS 450, S26R. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT RBL 6.7, WL 209.75 TO 210.25 AND AT LBL4.7, WL 198.5 TO 200. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKS AT RBL 4.7, WL 198.5 TO 199.5 AND AT LBL 4.7, WL 212.25 TO 212.75. REPAIRED PER TRAMCO EWO 97-0089 AND BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND VERTICAL CHORD CRACKS AT BS 178 BULKHEAD AT WL 184.5, LT SIDE. REPAIRED PER BOEING SRM.

Part: SKIN — SCRATCHED (BS 400)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN SCRATCHED BEYOND SRM LIMITS AT BS 440 PLUS 8, BETWEEN S18 AND 19L. REPAIRED PER BOEING SRM.

Part: DOOR FRAME — CRACKED (BS 951)

DURING SCHEDULED D-CHECK, FOUND AFT GALLEY DOOR FRAME CRACKED BS 951, AT S21R. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND VERTICAL CRACKS AT BS 178 BULKHEAD AT WL 189, LBL .7 AND RBL .5. REPAIRED PER BOEING SRM.

Part: ENGINE — FAILED (NR 2)

CLIMBING THROUGH 18,000, CREW SHUTDOWN NUMBER 2 ENGINE DUE TO HIGH VIBRATION AND HIGH EGT. RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. REPLACED NUMBER 2 ENGINE PER BOEING M/M.

Part: SKIN — CRACKED (BS 947.5)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 947.5 PLUS 14 AND 18, BELOW S19L, WL 189, AND AT BS 1006, BETWEEN S21 AND 22L. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 328)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED FWD SERVICE DOOR CUTOUT AT LWR AFT CORNER, BS 328, RBL 66, WL 211. REPAIRED PER BOEING SRM.

Part: SKIN — GOUGED (BS 380-410)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 380-410, BETWEEN S22 AND 23R, AND AT BS 862-886, FROM LBL 5 TO RBL 5. REPAIRED PER BOEING SRM.