N680AA

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 71,663 hrs · 60,812 cycles

DURING SCHEDULED OTS CHECK, FOUND SHEAR TIE CORRODED AT BS 747, STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 71,663 hrs · 60,812 cycles

DURING SCHEDULED OTS CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 71,663 hrs · 60,812 cycles

DURING SCHEDULED OTS CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 71,663 hrs · 60,812 cycles

DURING SCHEDULED OTS CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 71,663 hrs · 60,812 cycles

DURING SCHEDULED OTS CHECK, FOUND FRAME CORRODED AT BS 767, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 71,663 hrs · 60,812 cycles

DURING SCHEDULED OTS CHECK, FOUND FRAME CORRODED AT BS 747, STR 27L. REPAIRED FRAME PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,231 hrs · 60,491 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,128 hrs · 60,402 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER FWD CORNER CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,634 hrs · 60,036 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 460, BETWEEN STR 16R TO STR 17R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,634 hrs · 60,036 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 495, STR 16R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 69,393 hrs · 59,119 cycles

DURING SCHEDULED 22Y CHECK, FOUND R2 DOOR EMERGENCY EVACUATION SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,393 hrs · 59,119 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE BEAR SKIN CRACKED AT BS 305, STR 10L, WL 258. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,393 hrs · 59,119 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,393 hrs · 59,119 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 304, STR 10L, WL 258. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,393 hrs · 59,119 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT, BS 305, WL 262. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,393 hrs · 59,119 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,393 hrs · 59,119 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME WEB CRACKED AT BS 303, STR 16L. REPAIRED FRAME PER ACO.

Part: LENS — CRACKED (CABIN) · airframe 69,393 hrs · 59,119 cycles

DURING SCHEDULED 22Y CHECK, FOUND L2 DOOR EMERGENCY EXIT SIGN CRACKED. R&R LENS ASSY PER MM.

Part: LENS — CRACKED (CABIN) · airframe 69,393 hrs · 59,119 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 69,393 hrs · 59,119 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 663, BBL .07, UPPER CHORD TOP FLANGE. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 69,393 hrs · 59,119 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM T CAP CRACKED AT BS 665, BL 0. REPAIRED BEAM PER AAR EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 69,393 hrs · 59,119 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM T CAP CRACKED AT BS 666, BL 0. REPAIRED BEAM PER AAR EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 69,393 hrs · 59,119 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM T CAP CRACKED AT BS 669, BL 0. REPAIRED BEAM PER AAR EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 69,393 hrs · 59,119 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 685, BBL 0. REPAIRED BEAM PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,393 hrs · 59,119 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 26L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 69,393 hrs · 59,119 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 69,393 hrs · 59,119 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CRACKED AT BS 400, STR 8R. REMOVED AND REPLACED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,393 hrs · 59,119 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 360, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,393 hrs · 59,119 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,393 hrs · 59,119 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 887, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,393 hrs · 59,119 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,393 hrs · 59,119 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 69,393 hrs · 59,119 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 685, RBL .07. REPAIRED BEAM PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,393 hrs · 59,119 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,393 hrs · 59,119 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 847, STR 8R. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,393 hrs · 59,119 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED BS 980, STR 21L. REPAIRED SKIN PER SRM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 69,393 hrs · 59,119 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME SUPPORT WEB CRACKED AT BS 348, STR 15L. REMOVED AND REPLACED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,393 hrs · 59,119 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED BETWEEN BS 265 TO BS 275, STR 15R. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,393 hrs · 59,119 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 727C, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,393 hrs · 59,119 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,393 hrs · 59,119 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,393 hrs · 59,119 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,393 hrs · 59,119 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,393 hrs · 59,119 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,393 hrs · 59,119 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 270, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,393 hrs · 59,119 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,393 hrs · 59,119 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 270, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,393 hrs · 59,119 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,581 hrs · 58,550 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (BS 947 S24-25R) · airframe 68,240 hrs · 58,282 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, BETWEEN STR 24R AND STR 25R. REPAIRE SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,996 hrs · 58,105 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503D, STR 16R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,996 hrs · 58,105 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, BL 0. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,996 hrs · 58,105 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, BL 0. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,996 hrs · 58,105 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503D, STR 16R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,996 hrs · 58,105 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, BL 0. REPAIRED SKIN PER EA.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 67,594 hrs · 57,822 cycles

DURING SCHEDULED MV1 CHECK, FOUND NLG W/W FWD LEFT PRESSURE WEB CRACKED AT BS 246, WL 170. REPAIRED WEB PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,594 hrs · 57,822 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 760, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,443 hrs · 57,709 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 940 AND BS 980, STR 21L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,146 hrs · 57,476 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 438, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,146 hrs · 57,476 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 505D, STR 16L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,681 hrs · 57,412 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 420, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,217 hrs · 56,779 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 511D, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SLAT — CRACKED (RT WING) · airframe 65,446 hrs · 56,187 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING NR 5 L/E SLAT CRACKED AT INBOARD LOWER END. REPAIRED SLAT PER SRM.

Part: SLAT — CRACKED (RT WING) · airframe 65,446 hrs · 56,187 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING NR 6 L/E SLAT CRACKED AT INBOARD LOWER END. REPAIRED SLAT PER SRM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 65,420 hrs · 56,168 cycles

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

Part: ACTUATOR — WEAK (RT MLG) · airframe 64,921 hrs · 55,745 cycles

RT MLG UNSAFE LIGHT IND CYCLED GEAR HANDLE AND LIGHT IND WENT AWAY. REMOVED AND REPLACED RT MLG UPLOCK ACTUATOR PER MM.

Part: SENSOR — OUT OF ADJUST (RT MLG) · airframe 64,719 hrs · 55,579 cycles

AIRTURN BACK / DECLARED EMERGECNY, ON CLIMBOUT THE RIGHT MLG LIGHT STAYED ON WITH LANDING GEAR HANDLE PLACED TO UP AND OFF. ADJUSTED RIGHT MLG UPLOCK SENSOR PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 64,506 hrs · 55,417 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 64,506 hrs · 55,417 cycles

DURING SCHEDULED HC1 CHECK, FOUND NLG WHEEL WELL WEB CRACKED AT RIGHT BS 259, WL 174. REPAIRED WEB PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 64,506 hrs · 55,417 cycles

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

Part: SENSOR — FAULTY (RT MLG) · airframe 64,356 hrs · 55,291 cycles

AFTER GEAR RETRACTION WITH GEAR HANDLE IN OFF POSITION, RIGHT MLG RED LIGHT ILLUMINATED. CYCLED GEAR LIGHT EXTINGUISHED. REMOVED AND REPLACED RIGHT MLG UPLOCK SENSOR PER MM.

Part: SLIDE — DISLODGED (L2 DOOR) · airframe 62,865 hrs · 54,148 cycles

L2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,836 hrs · 54,124 cycles

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

Part: FLAP — DEBONDED (RT WING) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DISBONDED AT INBOARD END. REPAIRED FLAP PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD CARGO DOOR FWD FRAME CRACKED AT NR 5 DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO DOOR FWD FRAME CRACKED AT NR 5 DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 15R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT VERTICAL STAB FITTING PRIMARY LUG FACE CORRODED. REPAIRED STAB FITTING PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 967, STR 7L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SPOILER — CORRODED (LT WING) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING NR 3 SPOILER CRACKED AT INBOARD AFT T/E. REPAIRED SPOILER PER SRM.

Part: FITTING — CORRODED (LT WING) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT MLG BEAM CORRODED AT STAB BEAM FITTING. REMOVED AND REPLACED FITTING PER MM.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 62,836 hrs · 54,124 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 19 TO RBL 36. REPAIRED FLOORBEAM PER ER.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT HORIZ STAB L/E RIB CRACKED AT STA 120.30. REMOVED AND REPLACED RIB PER SRM.

Part: STRINGER — CORRODED (BS 500-500A S28L) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER 28L CORRODED AT BS 500 TO BS 500A. REPAIRED STRINGER PER SRM.

Part: FLAP TRACK — CORRODED (LT WING) · airframe 62,836 hrs · 54,124 cycles

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

Part: FLAP TRACK — CORRODED (LT WING) · airframe 62,836 hrs · 54,124 cycles

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

Part: FLAP TRACK — CORRODED (LT WING) · airframe 62,836 hrs · 54,124 cycles

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

Part: FLAP TRACK — CORRODED (LT WING) · airframe 62,836 hrs · 54,124 cycles

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

Part: STRINGER CLIP — CRACKED (BS 639 S4R) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 767 S9R-9L) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 9R AND STR 9L. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (BS 807 S9R) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 9R. REPAIRED FRAME SECTION PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 639 S3R) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 639 S2R) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLAP TRACK — CORRODED (LT WING) · airframe 62,836 hrs · 54,124 cycles

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

Part: STRINGER CLIP — CRACKED (BS 639 S2L) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLAP TRACK — CORRODED (RT WING) · airframe 62,836 hrs · 54,124 cycles

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

Part: STRINGER CLIP — CRACKED (BS 706 S2L) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 520 S9R) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 9R. REPAIRED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (BS 727E S9R) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 9R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (BS 827 S9L) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 9L. REPAIRED FRAME SECTION PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 639 S4L) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 787 S9R) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 9R. REPAIRED FRAME SECTION PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 706 S5R) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLAP TRACK — CORRODED (LT WING) · airframe 62,836 hrs · 54,124 cycles

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

Part: FLAP TRACK — CORRODED (RT WING) · airframe 62,836 hrs · 54,124 cycles

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

Part: STRINGER CLIP — CRACKED (BS 616 S2L) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLAP TRACK — CORRODED (RT WING) · airframe 62,836 hrs · 54,124 cycles

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

Part: FRAME — CRACKED (BS 867 S9L) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 9L. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (BS 887 S9L) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 9L. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (BS 727D S9R) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 9R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (BS 747 S9L) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 9L. REPAIRED FRAME SECTION PER SWA EA.

Part: TORQUE TUBE — CORRODED (RT WING TE FLAP) · airframe 62,836 hrs · 54,124 cycles

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

Part: TORQUE TUBE — CORRODED (RT WING TE FLAP) · airframe 62,836 hrs · 54,124 cycles

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

Part: SKIN — DELAMINATED (WING FORE FLAP) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND RIGHT WING INBOARD FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 615 S5R) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 615, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM.

Part: STRINGER CLIP — CRACKED (BS 639 S4R) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — DEBONDED (NR 2 SLAT) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING NR 2 L/E SLAT WEDGE OUTBOARD END DISBONDED. REPAIRED SLAT PER SRM.

Part: FRAME — CRACKED (BS 827 S9R) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 9R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (BS 847 S9L) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 9L. REPAIRED FRAME SECTION PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 907 S4L) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 807 S9R) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 787 S9L) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 9L. REPAIRED FRAME SECTION PER SWA EA.

Part: HOOK — LOOSE (L1 DOOR GIRT BAR) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. REMOVED AND REPLACED FWD GIRT BAR HOOK PER MM.

Part: FRAME — CRACKED (BS 480 S9R-9L) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 9R AND STR 9L. REPAIRED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (BS 380 S9R) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 9R. REPAIRED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (BS 747 S9R) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 9R. REPAIRED FRAME SECTION PER SRM.

Part: FRAME — CORRODED (BS 927) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 927, LBL 20. REPAIRED FRAME SECTION PER SRM.

Part: STRINGER — CORRODED (BS 382 S27L) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER 27L CORRODED AT BS 382. REPAIRED STRINGER SECTION PER SRM.

Part: SHEAR TIE — CORRODED (BS 500 S27L) · airframe 62,836 hrs · 54,124 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 62,432 hrs · 53,807 cycles

FOUND EMERGENCY EXIT LIGHT LENS LOOSE AT R1 DOOR. SECURED LIGHT LENS PER MM.

Part: WEB — CRACKED (BS 251) · airframe 62,352 hrs · 53,744 cycles

DURING SCHEDULED C3 CHECK, FOUND NLG W/W CEILING PANEL CUTOUT WEB CRACKED AT BS 251, LBL 7.75 TO RBL 7.75. REPAIRED WEB PER SWA EA.

Part: SKIN — DELAMINATED (FORE FLAP) · airframe 61,553 hrs · 53,129 cycles

DURING SCHEDULED A1 CHECK, FOUND RT WING T/E FORE FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — CRACKED (BS 914 S25L) · airframe 61,362 hrs · 52,990 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 914, STR 25L. REPAIRED SKIN PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 60,712 hrs · 52,475 cycles

DURING SCHEDULED A2 CHECK, FOUND LT OVERWING EXIT LIGHT HOUSING BROKEN. REMOVED AND REPLACED LIGHT ASSY PER SWA EA.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 60,638 hrs · 52,421 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND RT WING OUTBD T/E AFT FLAP DELAMINATED AT INBD END. REPAIRED AFT FLAP PER SRM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 60,638 hrs · 52,421 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT AFT CARGO DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 59,456 hrs · 51,470 cycles

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

Part: BEARING — WORN (RT WING TE FLAP) · airframe 58,872 hrs · 51,006 cycles

VIBRATION FELT DURING FLAPS OPERATION. FOUND 5 EACH RIGHT INBOARD T/E FOREFLAP TRACK BEARINGS WORN & ONE BEARING BROKEN. REMOVED AND REPLACED BEARINGS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,856 hrs · 50,995 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500B, STR 19L. REPAIRED SKIN PER SRM.

Part: PRIORITY VALVE — FAULTY (RT MLG) · airframe 58,822 hrs · 50,965 cycles

RT MLG EXTENDED UNCOMMANDED WITH RED RIGHT GEAR LIGHT ILLUMINATING FOR 5 MINUTES BEFORE GREEN RIGHT GEAR LIGHT ILLUMINATED. RETRACTED GEAR NORMALLY. MX FERRY TO PHX FOR REPAIRS. REMOVED AND REPLACED MLG PRIORITY MODULAR VALVE, MLG TRANSFER VALVE AND CONNECTOR PER MM.

Part: UPLOCK SENSOR — FAULTY (RT MLG) · airframe 58,770 hrs · 50,925 cycles

RIGHT MLG TRANSIT LIGHT ILLUMINATED, CYCLED GEAR HANDLE & LIGHT EXTINGUISHED. REMOVED AND REPLACED RIGHT MLG UPLOCK SENSOR & UPLOCK CARD PER MM.

Part: ACTUATOR — FAULTY (RT MLG WW) · airframe 58,597 hrs · 50,788 cycles

RIGHT MLG EXTENDED AFTER SUCCESSFUL RETRACTION. GEAR HANDLE RECYCLED & RIGHT GEAR REMAINED IN RETRACT POSITION. REMOVED AND REPLACED RIGHT MLG UPLOCK ACTUATOR PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 57,881 hrs · 50,252 cycles

DURING SCHEDULED RON, FOUND FWD OUTBOARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,800 hrs · 50,194 cycles

DURING WALKAROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 450, STR 15R. REPAIRED SKIN PER SRM.

Part: LENS — BROKEN (CABIN) · airframe 57,118 hrs · 49,613 cycles

DURING SPV, FOUND R1 DOOR EMERGENCY EXIT LIGHT LENS, BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SKIN — DEBONDED (FUSELAGE) · airframe 57,118 hrs · 49,613 cycles

DURING SPV, FOUND FUSELAGE SKIN BETWEEN BS 887 AND BS 897, BETWEEN STRINGERS 5L AND 9L, DISBONDED. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 57,118 hrs · 49,613 cycles

DURING SPV, FOUND 2 EACH CRACKS ON SHEAR TIES AT BS 360, ABOVE AND BELOW STRINGER 14L. REMOVED AND REPLACED SHEAR TIES PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 57,118 hrs · 49,613 cycles

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

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 57,118 hrs · 49,613 cycles

DURING SPV, FOUND STRINGER SPLICE AT BS 360, STRINGER 4L, CRACKED. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,118 hrs · 49,613 cycles

DURING SPV FOUND BELT FRAME AT BS 908, STRINGER 4R, CRACKED. REPAIRED BELT FRAME PER SRM.

Part: SPLICE — CRACKED (STRINGER) · airframe 57,118 hrs · 49,613 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 57,118 hrs · 49,613 cycles

DURING SPV, FOUND 4 EACH SHEAR TIES BETWEEN BS 727C AND BS 767, STRINGER 4L, CRACKED. REMOVED AND REPLACED SHEAR TIES PER SRM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 56,574 hrs · 49,232 cycles

DURING SCHEDULED C1 CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LT WING FLAP PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,574 hrs · 49,232 cycles

DURING SCHEDULED C1 CHECK, FOUND CABIN EMERGENCY EXIT LIGHTS INOP WITH FWD AND AFT SWITCHES. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,574 hrs · 49,232 cycles

DURING SCHEDULED C1 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 270, STRINGER 16L AND BS 945, STRINGER 24L. REPAIRED SKIN SECTIONS PER EA.

Part: SLIDE — OUT OF ADJUST (R1 &R2 DOORS) · airframe 56,574 hrs · 49,232 cycles

DURING SCHEDULED C1 CHECK, FOUND R1 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED R1 AND R2 DOOR EVAC SLIDES PER MM.

Part: BULKHEAD — CRACKED (AFT FUSELAGE) · airframe 55,717 hrs · 48,524 cycles

DURING SCHEDULED C4 CHECK, FOUND BS 1016 AFT PRESS BULKHEAD WEB CRACKED AT STR 6L. REPAIRED WEB PER SWA EA.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 55,709 hrs · 48,518 cycles

DURING SCHEDULED C4 CHECK, FOUND LEFT AND RIGHT HORIZONTAL STAB LOWER SKIN AT REAR SPAR STATION 107, CRACKED. REPAIRED HORIZONTAL STAB SKIN PER SRM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 58,149 hrs · 43,674 cycles

DURING SCHEDULED C4 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS AT ROW 6 ABC, LOOSE. SECURED EMERGENCY EXIT LIGHT LENS PER MM.

Part: BOLT — WORN (ELEVATOR) · airframe 55,709 hrs · 48,518 cycles

DURING SCHEDULED C4 CHECK, RIGHT ELEVATOR TAB FAILED FREEPLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB CONTROL ROD END BOLTS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,183 hrs · 48,082 cycles

DURING SCHEDULED 1/4D CHECK, FOUND L1 DOOR CUTOUT AFT LOWER CORNER, CRACKED. REPAIRED SKIN PER EA.

Part: CABLE — MISROUTED (L2 DOOR) · airframe 55,183 hrs · 48,082 cycles

DURING SCHEDULED 1/4D CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE CABLE PER MM.

Part: HOOK — LOOSE (R1 DOOR) · airframe 55,183 hrs · 48,082 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR EVAC SLIDE GIRT BAR HOOKS LOOSE. SECURED R1 DOOR EVAC SLIDE GIRT BAR HOOKS PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 54,404 hrs · 47,464 cycles

R1 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: STIFFENER — CRACKED (BULKHEAD) · airframe 54,002 hrs · 47,140 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT PRESS BULKHEAD ZEE STIFFENERS CRACKED AT 12 AND 7 O'CLOCK POSITIONS. REPAIRED STIFFENERS PER SRM.

Part: CAP — CRACKED (BULKHEAD) · airframe 54,002 hrs · 47,140 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT PRESS BULKHEAD AT BS 1016, CRACKED AT CENTER CAP. REPAIRED PER EA.

Part: WEDGE — DELAMINATED (LT WING SLAT) · airframe 54,002 hrs · 47,140 cycles

DURING SCHEDULED C2 CHECK, FOUND NR 3 SLAT T/E WEDGE INBOARD END DELAMINATED. REMOVED AND REPLACED NR 3 SLAT PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 53,994 hrs · 47,133 cycles

DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,888 hrs · 46,257 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 2.5 LONG AT BS 933, STRINGER 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,489 hrs · 45,926 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (12 EA) AT STR 4R, BS'S 380, 410, 420, 430, 460, 500, 500B, 500C, 500C + 10, 500D, 520 AND 530. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,489 hrs · 45,926 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (5 EA) AT STR 4L, BS'S 409, 488, 470, 692 AND BS 697. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,489 hrs · 45,926 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) BS 895 AT STR 14R AND BS 866 AT STR 10R. REPAIRED SKIN PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 52,489 hrs · 45,926 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND KEEL BEAM CORRODED AT BS 727 + 3, STR 27R. REPAIRED KEEL BEAM PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,489 hrs · 45,926 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CLIP CRACKED AT BS 887, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 51,106 hrs · 44,847 cycles

DURING DESCENT,THRUST LEVERS RETARDED, HEARD LOUD BANGING NOISE FROM NR 1 ENGINE. REMOVED AND REPLACED NR 1 ENGINE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,209 hrs · 44,162 cycles

DURING SCHEDULED C2 CHECK, FOUND BOTH UPPER AND LOWER HINGE CUTOUTS CRACKED ON AFT ENTRY DOOR. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,209 hrs · 44,162 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT EXTERNAL AIR CONDITIONING DOOR CUTOUT AT FWD LT SIDE. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (FWD ENTRY DOOR) · airframe 50,292 hrs · 44,156 cycles

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

Part: BATTERY — ERRATIC (CABIN) · airframe 48,797 hrs · 42,976 cycles

AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT ILLUMINATED CONTINOUSLY. REMOVED AND REPLACED EXIT LIGHT BATTERY PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 48,734 hrs · 42,927 cycles

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

Part: POST — CRACKED (FUSELAGE) · airframe 47,092 hrs · 41,587 cycles

DURING SCHEDULED 1/2D CHECK, FOUND F/O'S UPPER WINDOW POST CRACKED. REPAIRED POST PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 47,092 hrs · 41,587 cycles

DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CRACKED AT BS 380, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: LENS — LOOSE (FUSELAGE) · airframe 47,092 hrs · 41,587 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT OVERWING EMERGENCY LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,092 hrs · 41,787 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FRAME CRACKED AT 2 EA PLACES, BS 616, LBL 65 AND RBL 65, WL 200. REPAIRED FRAME PER TI-153-018.

Part: FRAME — CRACKED (FWD ENTRY DOOR) · airframe 47,092 hrs · 41,587 cycles

during scheduled 1/2d check, found forward entry door frame cracked (3 ea) at aft stop pin cutout Nr 5, 6, 7. repaired door frame per srm.

Part: BEAM — CRACKED (CABIN FLOOR) · airframe 47,092 hrs · 41,787 cycles

DURING SCHEDULED 1/2D CHECK, FOUND 3 EA FLOORBEAMUPPER CHORDS CORRODED, BS 312, LBL 11 TO RBL 19, BS 328, LBL 11, AND BS 294, LBL 11 TO RBL 22. REMOVED AND REPLACED UPPER CHORD SECTIONS PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 47,092 hrs · 41,587 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BELTFRAME SHEAR TIE CORRODED, BS 842, BETWEEN STRINGER 28L AND 28R. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,092 hrs · 41,587 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED, BS 986.5, LBL 16.5. REPAIRED BEAM PER SRM.

Part: BEAM — CORRODED (CABIN FLOOR) · airframe 47,092 hrs · 41,587 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED, BS 986, LBL 29 TO RBL 51.5. REMOVED AND REPLACED FLOORBEAM UPPER CHORD PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 47,092 hrs · 41,587 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED, BS 727A, STRINGER 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: BRACKET — BROKEN (FWD SVC DOOR.) · airframe 46,861 hrs · 41,399 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE BAR BRACKET BROKEN. REMOVED AND REPLACED BRACKET PER MM.

Part: RETAINER — LOOSE (ENTRY DOOR) · airframe 46,778 hrs · 41,326 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE COVER GIRT BAR HOLDER LOOSE. SECURED HOLDER PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 46,249 hrs · 40,886 cycles

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

Part: FITTING — CRACKED (MLG WW) · airframe 45,922 hrs · 40,596 cycles

DURING SCHEDULED C1 CHECK, FOUND MLG WALKING BEAM FWD ATTACH HANGER FITTING CRACKED AT WBL 135.5. REMOVED AND REPLACED ATTACH FITTING BY ALM, SWA W/W 10418.

Part: ACTUATOR — FAILED (L/E FLAP) · airframe 45,898 hrs · 40,573 cycles

AIR TURNBACK, RT WING L/E FLAP TRANSIT AND NR 3 L/E DEVICE LIGHTS ILLUMINATED. REMOVED AND REPLACED NR 3 L/E FLAP ACTUATOR PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 45,893 hrs · 40,567 cycles

EEPLS LOOSE AT ROW 5. INSTALLED EEPLS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,001 hrs · 39,810 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA RA.

Part: RETAINER — LOOSE (SERVICE DOOR) · airframe 45,001 hrs · 39,810 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINER LOOSE. SECURED RETAINER PER MM.

Part: LENS — LOOSE (CABIN) · airframe 44,845 hrs · 39,671 cycles

EEPLS LENS LOOSE AT ROW 8. REMOVED AND REPLACED LENS PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 44,300 hrs · 39,227 cycles

AFT UPPER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT, BATTERY AND HOLDER PER MM.

Part: BRACKET — LOOSE (ESCAPE SLIDE) · airframe 44,018 hrs · 38,996 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY BRACKET RIVETS LOOSE. SECURED GIRT BRACKET PER MM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 43,430 hrs · 38,537 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 663 VERTICAL STIFFENERS CRACKED AT RBL 6.0 AND LBL 6.0. REMOVED AND REPLACED STIFFENERS PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,448 hrs · 37,704 cycles

EEPLS RED LIGHT INOP AT FWD END. REPAIRED WIRING PER MM.

Part: FEEL UNIT — INOPERATIVE (ELEVATOR) · airframe 42,037 hrs · 37,352 cycles

DIVERSION, ELEVATOR CONTROL DIFFICULT TO OPERATE. REMOVED AND REPLACED ELEVATOR FELL COMPUTER AND FEEL CENTERING UNIT PER MM.

Part: LIGHT — CRACKED (CABIN) · airframe 41,283 hrs · 36,728 cycles

DURING SCHEDULED BC4 CHECK, FOUND EEPLS LOOSE AND TRACK CRACKED AT ROW 23. SECURED LIGHT ASSY AND R&R TRACK COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,283 hrs · 36,728 cycles

DURING SCHEDULED BC4 CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 927, STRINGER 10 LT. REPAIRED SKIN PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 41,283 hrs · 36,728 cycles

DURING SCHEDULED BC4 CHECK, FOUND EMERGENCY EXIT LIGHTS LOOSE AT ROWS 3 ABC AND 11 ABC IN BULLNOSE OVERHEAD AREA. SECURED LIGHTS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 41,209 hrs · 36,664 cycles

EEPLS PULLED UP AT ROW 3. SECURED TRACK LIGHTS PER MM.

Part: LIGHT — INOPERATIVE (ROW 10)

EEPLS INOP AT ROW 10. REPAIRED WIRE PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED A2 CHECK, FOUND EEPLS INOP ANS MISSING LENS AT FWD END. RELAMPED AND INSTALLED LENS PER MM.

Part: SLIDE — DISCHARGED (SERVICE DOOR)

DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATOR LOW. REMOVED AND REPLACED SLIDE ASSY.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED 1/4D CHECK, FOUND EEPLS CENTER CABIN LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — DAMAGED (EMER EXIT)

DURING SCHEDULED 1/4D CHECK, FOUND RT EMERGENCY EXIT LIGHT ASSY DAMAGED AND UNSECURED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FLOORBEAM — CORRODED (BS 793)

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON FLOORBEAM, BS 793, RBL 3. REPAIRED BEAM PER SWA RA NR 1-A53-2021.

Part: WEB — CRACKED (BS 665)

DURING SCHEDULE 1/2D CHECK, FOUND CRACK IN PRESSURE WEB, BS 665, LBL 32. REPAIRED WEB PER SWA RA NR 1-353-2112.

Part: SKIN — CRACKED (NR 5 LE SLAT)

DURING SCHEDULED C1 CHECK, FOUND NR 5 LE SLAT HAS 7 CRACKS AT LOWER SKIN AFT RIVET ROW. REPAIRED SLAT PER SWA RA NR 1-357-0312.

Part: WIRE — DAMAGED (BS 540-700)

DURING SCHEDULED SPECIAL VISIT, FOUND EMERGENCY FLOOR TRACK ESCAPE LIGHTING BETWEEN BS 540 TO 700 WITH EXPOSED AND CRUSHED WIRING. REMOVED AND REPLACED WIRING PER MM.

Part: SLIDE — DETACHED (PAX DOOR)

FWD ENTRY DOOR EMERGENCY ESCAPE SLIDE FELL OUT OF SLIDE PACK WHEN DOOR WAS BEING CLOSED. RESECURED FORWARD LEFT EMERGENCY ESCAPE SLIDE PER M/M.

Part: LIGHT — MISSING (CABIN)

DURING PREFLIGHT, FOUND ONE EGRESS LIGHT MISSING AFT CABIN AREA. REPLACED PER BOEING M/M.

Part: LAMP — FAILED (ROW 18)

DURING SCHEDULED C3 CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOP AT ROW 18. RELAMPED PER BOEING M/M.

Part: LAMP — FAILED (ROW 18)

DURING SCHEDULED C3 CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOP AT ROW 18. RELAMPED PER BOEING M/M.

Part: DAMPER — LOOSE (LT MLG)

ON LANDING AT APPROX 80 KNOTS, AIRCRAFT MADE AN ABRUPT RIGHT TURN, DIFFICULT TO HOLD AIRCRAFT CENTERED, WITHOUT USING FULL LEFT RUDDER. CREW USED TILLER TO CORRECT. ENGINES, REVERSERS AND BRAKES APPEARED NORMAL. RETORQUED LT GEAR SHIMMY DAMPER PER BOEING M/M. HIGH SPEED TAXI CHECKED NORMAL.

Part: SKIN — GOUGED (BS 256/372)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 256, AT S20L, AND AT BS 372, BETWEEN S23 AND 24L. REPAIRED PER BOEING SRM.

Part: STIFFENER — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 LT VERTICAL STIFFENER CRACKED AT AFT SIDE OF BULKHEAD. REPAIRED PER BOEING SRM.

Part: THRESHOLD — CORRODED (BS 312-344)

DURING SCHEDULED D-CHECK, FOUND FORWARD ENTRY DOOR THRESHOLD CORRODED BETWEEN BS 312 AND 344, WL 208, OUTBOARD ANGLE AT LBL 69. REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 294)

DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORROSION AT BS 294, WL 208. REPLACED DAMAGED SECTION PER BOEING SRM.

Part: FRAME — GOUGED (BS 211)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME WEB GOUGED AT BS 211, RBL 39, WL 233. REPAIRED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 325)

DURING SCHEDULED D-CHECK, FOUND STRINGER CRACKED AT BS 325, S26R. REPLACED STRINGER SECTION PER BOEING SRM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 WEBS CRACKED AT LBL 4.7, WL 212 TO 213, AT 201.5 TO 200, AND AT RBL 1.5, WL 206. REPAIRED PER TRAMCO EWO 96-0869.

Part: SKIN — DAMAGE (BS 685/996)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DAMAGE AT BS 996, AT S13L AND 12L, AT BS 706, S11L, AND AT BS 685, S11L. REPAIRED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 987-1006)

DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CORROSION AT BS 987-1006, LBL 10 TO 19. REPAIRED PER BOEING SRM.

Part: SPLICE — CRACKED (BS 350)

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 350, AT S14L, AND STRINGER CLIP AT BS 294, S13L. REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED D-CHECK, FOUND FORWARD SERVICE DOOR CUTOUT CRACKED AT AFT LOWER CORNER SKIN. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 1016)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AROUND CLIP NUT HOLE, AT BS 1016, LBL 34. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CRACKED (BS 312-328)

DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM SUPPORT STRAP CRACKED AT BS 312-328, RBL 30. REPAIRED PER BOEING SRM.

Part: SPLICE — CRACKED (BS 359)

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 359, S2L. REPLACED STRINGER SPLICE SECTION PER BOEING SRM.

Part: SKIN — DENTED (FUSELAGE)

DURING SCHEDULED B/C1 CHECK, FOUND LEFT AFT FUSE SKIN DENTED AFT OF AFT ENTRY DOOR, JUST BELOW EMERGENCY EXIT LIGHT. REPAIRED PER BOEING SRM.

Part: CUTOUT — CRACKED (FWD GALLEY DOOR)

DURING SCHEDULED B/C1 CHECK, FOUND FORWARD GALLEY DOOR UPPER AND LOWER HINGE CUT-OUTS CRACKED .25 INCH. REPAIRED PER SWA RA 1-352-0251.

Part: SKIN — CRACKED (BS 1183)

DURING SCHEDULED B/C1 CHECK, FOUND FUSELAGE SKIN CRACKED 8 INCHES BELOW BS 1183. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (FWD FUSELAGE)

DURING SCHEDULED C-CHECK, FOUND FUSELAGE SKIN DOUBLER CRACKED JUST BEHIND RADOME AT 12 O'CLOCK POSITION. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.