N661SW

Part: GASPER FAN — MALFUNCTIONED (AC BAY) · airframe 76,017 hrs · 57,538 cycles

AIR TURNBACK - AFTER DEPARTURE FLIGHT ATTENDANT SMELL FUMES IN CABIN, NO SMOKE. REMOVED AND REPLACED GASPER FAN EPR MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,539 hrs · 57,173 cycles

DURING SCHEDULED OTS CHECK, FOUND CRACK IN FUSELAGE SKIN, BS 280, STR 15R. REPAIRED PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 75,539 hrs · 57,173 cycles

DURING SCHEDULED OTS CHECK, FOUND CRACK RT WING NR 4 SLAT LWR T/E SKIN, O/B OF THE TAI DUCT. REPAIRED PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,790 hrs · 56,610 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER HINGE CUTOUT. REMOVED AND REPLACED L2 DOOR PER MM.

Part: HYDRAULIC LINE — LEAKING (LT MLG) · airframe 73,970 hrs · 55,996 cycles

AIR TURNBACK, HYDRAULIC A-SYSTEM LOSS. REMOVED AND REPLACED LT MLG ACTUATOR HYDRAULIC LINE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,544 hrs · 55,664 cycles

RIGHT EEPLS INOP AT ROW 4. REPAIRED EEPLS PER MM.

Part: FLAP — PUNCTURED (LT WING) · airframe 73,559 hrs · 55,678 cycles

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

Part: HYDRAULIC LINE — FAILED (LT MLG) · airframe 73,462 hrs · 55,595 cycles

DIVERSION/DECLARED EMERGENCY. A SYSTEM HYDRAULIC FAILURE ON TAKEOFF. REMOVED AND REPLACED LT MLG ACTUATOR LINE PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 73,187 hrs · 55,389 cycles

DURING SCHEDULED 26Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED BETWEEN BS 710 TO BS 715, LBL 24.5. REPAIRED WEB PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,187 hrs · 55,389 cycles

DURING SCHEDULED 26Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 14R. REPAIRED FRAME PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,187 hrs · 55,389 cycles

DURING SCHEDULED 26Y CHECK, FOUND FWD CARGO COMPT FRAME CRACKED AT BS 500C, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER ER.

Part: SKIN PANEL — DELAMINATED (SPOILER) · airframe 73,187 hrs · 55,389 cycles

DURING SCHEDULED 26Y CHECK, FOUND RT WING NR 9 SPOILER PANEL LOWER SURFACE DELAMINATED. REMOVED AND REPLACED NR 9 SPOILER PANEL PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,187 hrs · 55,389 cycles

DURING SCHEDULED 26Y CHECK, FOUND FWD CARGO COMPT FRAME CRACKED AT BS 500B, BETWEEN 20L TO STR 21L. REPAIRED FRAME PER ER.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 73,187 hrs · 55,389 cycles

DURING SCHEDULED 26Y CHECK, FOUND LT KEEL BEAM O/B FLANGE REPAIR ANGLE CORRODED AT APPROX BS 550. REPAIRED ANGLE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,187 hrs · 55,389 cycles

DURING SCHEDULED 26Y CHECK, FOUND FWD CARGO FRAME CRACKED AT BS 500C, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 73,187 hrs · 55,389 cycles

DURING SCHEDULED 26Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED BETWEEN BS 706 TO BS 717, BL 0. REPAIRED BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,187 hrs · 55,389 cycles

DURING SCHEDULED 26Y CHECK, FOUND FWD CARGO FRAME CRACKED AT BS 500D, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,187 hrs · 55,389 cycles

DURING SCHEDULE 26Y CHECK, FOUND FRAME CRACKED AT BS 500C, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,187 hrs · 55,389 cycles

DURING SCHEDULED 26Y CHECK, FOUND FRAME CRACKED AT BS 500D, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,440 hrs · 54,841 cycles

DURING SCHEDULED MV4 CHECK, FOUND AFT GALLEY EMERGENCY EXIT LIGHT BULBS INOP. RELAMPED PER MM.

Part: SKIN — CRACKED (BS 269.4 S16L) · airframe 71,625 hrs · 54,251 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 269.4, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (LT WING FOREFLAP) · airframe 71,625 hrs · 54,251 cycles

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

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 71,625 hrs · 54,251 cycles

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

Part: SKIN — DELAMINATED (FORE FLAP) · airframe 71,625 hrs · 54,251 cycles

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

Part: SLIDE — LOOSE (L1 DOOR) · airframe 71,625 hrs · 54,251 cycles

L1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 71,349 hrs · 54,034 cycles

R1 DOOR EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,324 hrs · 54,016 cycles

DURING SCHEDULED MV3 CHECK, FOUND BULLNOSE EMERGENCY LIGHT INOP AT 21 ABC. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 71,185 hrs · 53,899 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,185 hrs · 53,899 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 70,921 hrs · 53,712 cycles

DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING LOOSE. REMOVED AND REPLACED FITTING PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 70,891 hrs · 53,689 cycles

FWD EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: INDICATOR — FAULTY (COCKPIT) · airframe 70,811 hrs · 53,628 cycles

DECLARED EMERGENCY. SELECTED FLAPS 5 AND GOT RIGHT FLAPS 1, LEFT FLAPS BETWEEN 5 AND 10. ALSO L/E FLAP TRANSIT LIGHT ILLUMINATED. REMOVED AND REPLACED FLAP POSITION INDICATOR AND REPAIRED POSITION TRANSMITTER WIRING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,727 hrs · 53,558 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,727 hrs · 53,558 cycles

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

Part: MOTOR — FAULTY (TE FLAP) · airframe 70,394 hrs · 53,303 cycles

DECLARED EMERGENCY, T/E FLAPS WOULD NOT OPERATE. ABLE TO ACHIEVE VIA ALTERNATE METHOD. REMOVED AND REPLACED ALTERNATIVE FLAP DRIVE MOTOR AND HYD DRIVE MOTOR.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 70,337 hrs · 53,263 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 69,848 hrs · 52,898 cycles

DURING SCHEDULED MV2 CHECK, FOUND OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 15. SECURED LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 69,848 hrs · 52,898 cycles

OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS MISSING AT ROW 15. REMOVED AND REPLACED LENS PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,652 hrs · 52,767 cycles

DURING SCHEDULED MV1 CHECK, FOUND FWD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE. REPAIRED SKIN PER AAR EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 227, BETWEEN RBL 0 TO RBL 3. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 360, BETWEEN STR 28R TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SUPPORT FITTING — CORRODED (RT MLG) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT MLG UPLOCK ASSEMBLY FWD SUPPORT FITTING CORRODED. REPAIRED FITTING PER SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 286, STR 13R. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM TEE CAP CORRODED AT BS 986, BETWEEN LBL 2 TO RBL 16. REPAIRED BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 227, RBL 15. REPAIRED SKIN PER AAR EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 291, STR 16R. REPAIRED FRAME PER AAR EA.

Part: LIGHT — LOOSE (CABIN) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 17. SECURED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 518, STR 28L. REPAIRED SKIN PER SRM.

Part: SPAR — DELAMINATED (HORIZ STAB) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT HORIZONTAL STABILIZER REAR SPAR UPPER CHORD DELAMINATED AT BS 165. REMOVED AND REPLACED STABILIZER PER MM.

Part: LIGHT — CRACKED (CABIN) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND FWD LAV AFT WALL EMERGENCY EXIT LIGHT ASSY CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 663, STR 3R. REPAIRED FRAME PER SRM.

Part: WIRE — LOOSE (CABIN) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND R2 DOOR EXIT MARKER WIRE LOOSE. REPAIRED WIRE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND FWD CARGO SKIN CRACKED AT BS 518, STR 28L. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM CORRODED AT BS 987, RBL 48. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND R2 DOOR CREASE BEAM CORRODED AT BS 986, RBL 47, WL 208. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 27L. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND R2 DOOR CREASE BEAM CORRODED AT BS 986, RBL 49, WL 208. REPAIRED BEAM PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. RESEATED LAMP PER MM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 68,517 hrs · 61,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 480 + 10, STR 26L. REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,517 hrs · 61,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 27L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 68,517 hrs · 61,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 500B, STR 27L. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 22R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 3 SLAT O/B TRAILING EDGE WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,517 hrs · 51,951 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT DOOR CREASE BEAM CORRODED BETWEEN BS 312 TO BS 360. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 1006, STR 13L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND STUB FRAME CORRODED AT BS 793, STR 27R. REPAIRED STUB FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,517 hrs · 51,951 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 21R. REMOVED AND REPLACED CLIP PER SRM.

Part: SLAT — DELAMINATED (RT WING) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING L/E NR 4 SLAT O/B DELAMINATED. REPAIRED SLAT PER SRM.

Part: SLAT — CRACKED (LT WING) · airframe 68,517 hrs · 51,951 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM TEE CAP CORRODED AT BS 1006, LBL 9, WL 208. REPAIRED BEAM PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 28L. REMOVED AND REPLACED SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,517 hrs · 51,951 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 16R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 1006, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE L1 DOOR FRAME CRACKED BETWEEN 5TH TO 7TH STOP FITTINGS. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,517 hrs · 51,951 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SLAT — DELAMINATED (RT WING) · airframe 68,517 hrs · 61,951 cycles

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

Part: SKIN — DELAMINATED (NR 6 SPOILER) · airframe 67,494 hrs · 51,189 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING NR 6 SPOILER UPPER SURFACE DELAMINATED AT INBOARD END. REMOVED AND REPLACED SPOILER PER MM.

Part: LIGHT — DISCONNECTED (EMERGENCY EXIT) · airframe 65,864 hrs · 50,007 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 1 DEF. FOUND LIGHT ASSY DISCONNECTED. RECONNECTED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,787 hrs · 49,948 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 951, STR 26L. REPAIRED SKIN PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 65,787 hrs · 49,948 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 24R CORRODED AT BS 363. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,787 hrs · 49,948 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 902, STR 23R. REPAIRED SKIN PER ER.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 65,787 hrs · 49,948 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR CUTOUT AFT FRAME CRACKED AT NR 5 DOOR STOP. REPAIRED FRAME PER ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,787 hrs · 49,948 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,787 hrs · 49,948 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 413, LBL 2. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 65,787 hrs · 49,948 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 947, STR 25R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER — CRACKED (BS 515 S20R) · airframe 65,787 hrs · 49,948 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 20R CRACKED AT BS 515. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (BS 400 S8L) · airframe 65,787 hrs · 49,948 cycles

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

Part: STRINGER — CORRODED (BS 360 S22R) · airframe 65,787 hrs · 49,948 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 22R CORRODED AT BS 360. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (BS 727 S13L) · airframe 65,787 hrs · 49,948 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT BS 727, STR 13L. REPAIRED CHORD PER BFG ER.

Part: STRINGER — CORRODED (BS 420 S26R) · airframe 65,787 hrs · 49,948 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER CORRODED AT BS 420, STR 26R. REPAIRED STRINGER PER SRM.

Part: STRINGER — CORRODED (BS 360 S23R) · airframe 65,787 hrs · 49,948 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 23R CORRODED AT BS 360. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (BS 767 S8L) · airframe 65,787 hrs · 49,948 cycles

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

Part: FRAME — CRACKED (BS 767 S8L) · airframe 65,787 hrs · 49,948 cycles

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

Part: FRAME — CRACKED (BS 727 S12L) · airframe 65,787 hrs · 49,948 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727, STR 12L. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CRACKED (BS 480 S17R) · airframe 65,787 hrs · 49,948 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 480, STR 17R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (BS 947 S24L) · airframe 65,787 hrs · 49,948 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 947, STR 24L. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (BS 752 S23L) · airframe 65,787 hrs · 49,948 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 752, STR 23L. REPAIRED SKIN PER ACO.

Part: SKIN — CRACKED (BS 752 S23R) · airframe 65,787 hrs · 49,948 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 752, STR 23R. REPAIRED SKIN PER ACO.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,787 hrs · 49,948 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, RBL 7. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,787 hrs · 49,948 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,787 hrs · 49,948 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,787 hrs · 49,948 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,787 hrs · 49,948 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,787 hrs · 49,948 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,787 hrs · 49,948 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (BS 500C S8L) · airframe 65,787 hrs · 49,948 cycles

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

Part: FRAME — CRACKED (BS 827 S8R) · airframe 65,787 hrs · 49,948 cycles

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

Part: FRAME — CRACKED (BS 847 S8R) · airframe 65,787 hrs · 49,948 cycles

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

Part: STRINGER CLIP — CRACKED (BS 460 S1) · airframe 65,787 hrs · 49,948 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (BS 908 S4R) · airframe 65,787 hrs · 49,948 cycles

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

Part: STRINGER CLIP — CRACKED (BS 400 S8L) · airframe 65,787 hrs · 49,948 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500B S1) · airframe 65,787 hrs · 49,948 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 440 S8R) · airframe 65,787 hrs · 49,948 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 727B S9R) · airframe 65,787 hrs · 49,948 cycles

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

Part: STRINGER CLIP — CRACKED (BS 727C S7L) · airframe 65,787 hrs · 49,948 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 (BS 727D S7L) · airframe 65,787 hrs · 49,948 cycles

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

Part: STRINGER CLIP — CRACKED (BS 727A S6L) · airframe 65,787 hrs · 49,948 cycles

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

Part: STRINGER CLIP — CRACKED (BS 727D S5L) · airframe 65,787 hrs · 49,948 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 (BS 727B S7L) · airframe 65,787 hrs · 49,948 cycles

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

Part: FRAME — CRACKED (BS 727A S8L) · airframe 65,787 hrs · 49,948 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 727D S5R) · airframe 65,787 hrs · 49,948 cycles

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

Part: STRINGER CLIP — CRACKED (BS 727A S9R) · airframe 65,787 hrs · 49,948 cycles

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

Part: STRINGER CLIP — CRACKED (BS 277 S15R) · airframe 65,787 hrs · 49,948 cycles

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

Part: STRINGER CLIP — CRACKED (BS 616 S3L) · airframe 65,787 hrs · 49,948 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727A S7R) · airframe 65,787 hrs · 49,948 cycles

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

Part: STRINGER CLIP — CRACKED (BS 685 S2R) · airframe 65,787 hrs · 49,948 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 847 S8L) · airframe 65,787 hrs · 49,948 cycles

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

Part: STRINGER CLIP — CRACKED (BS 727D S6R) · airframe 65,787 hrs · 49,948 cycles

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

Part: STRINGER CLIP — CRACKED (BS 685 S3L) · airframe 65,787 hrs · 49,948 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 867 S8L) · airframe 65,787 hrs · 49,948 cycles

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

Part: STRINGER CLIP — CRACKED (BS 727C S6R) · airframe 65,787 hrs · 49,948 cycles

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

Part: FRAME — CRACKED (BS 887 S8L) · airframe 65,787 hrs · 49,948 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 685 S4R) · airframe 65,787 hrs · 49,948 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727C S7R) · airframe 65,787 hrs · 49,948 cycles

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

Part: FRAME — CRACKED (BS 480 S8L/R) · airframe 65,787 hrs · 49,948 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 500D S4R) · airframe 65,787 hrs · 49,948 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 500C S8R) · airframe 65,787 hrs · 49,948 cycles

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

Part: STRINGER CLIP — CRACKED (BS 597 S9R) · airframe 65,787 hrs · 49,948 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 616 S2R) · airframe 65,787 hrs · 49,948 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 400 S8R) · airframe 65,787 hrs · 49,948 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,787 hrs · 49,948 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,787 hrs · 49,948 cycles

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

Part: SKIN — CRACKED (BS 787 S18R) · airframe 65,491 hrs · 49,719 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787 STR 18R. REPAIRED SKIN PER SWA EA.

Part: GLOWSTRIP — WORN (CABIN) · airframe 65,491 hrs · 49,719 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIPS WORN BETWEEN ROW 1 DEF AND ROW 5 DEF. REMOVED AND REPLACED STRIPS PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 65,491 hrs · 49,719 cycles

DURING SCHEDULED C4 CHECK, FOUND RIGHT WING INBOARD MID FLAP DELAMINATED. REMOVED AND REPLACED MID FLAP PER MM.

Part: LIGHT — LOOSE (EMERGENCY EXIT) · airframe 65,497 hrs · 45,719 cycles

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

Part: SKIN — CRACKED (BS 780 S18L) · airframe 65,087 hrs · 49,406 cycles

DURING SCHEDULE SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 780, STR 18L. REPAIRED SKIN PER SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,567 hrs · 49,002 cycles

DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: WIRE — BROKEN (NR 5 SLAT) · airframe 64,537 hrs · 48,979 cycles

AIR TURNBACK, ON FLAP RETRACTION RIGHT WING NR 5 L/E SLAT WOULD NOT RETRACT. CYCLED FLAPS PER QRH, NO HELP. FOUND BROKEN WIRE AT NR 5 L/E SLAT ACTUATOR, REPAIRED WIRE PER MM.

Part: TAB — WORN (AILERON) · airframe 63,717 hrs · 48,326 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING AILERON TAB ATTACH POINTS WORN. REMOVED AND REPLACED AILERON TAB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,717 hrs · 48,326 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 794, STR 19L. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,052 hrs · 47,820 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,052 hrs · 47,820 cycles

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

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,674 hrs · 47,516 cycles

DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 62,674 hrs · 47,516 cycles

DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LOWER LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 62,313 hrs · 47,235 cycles

FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: STRINGER — CRACKED (BS 520 S10L) · airframe 62,177 hrs · 47,125 cycles

DURING SCHEDULED SERVICE CHECK, FOUND STRINGER 10L CRACKED AT BS 520. REPAIRED STRINGER PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,113 hrs · 47,075 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 375, STR 15L. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,669 hrs · 46,722 cycles

DURING SCHEDULED C4 CHECK, FOUND LT AFT CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY AND BATTERY PACK PER MM.

Part: FRAME — CRACKED (BS 500B) · airframe 61,223 hrs · 46,370 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 21R. REPAIRED FRAME SECTION PER SWA EA.

Part: KEELBEAM — CORRODED (BS 520) · airframe 61,223 hrs · 46,370 cycles

DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM CORRODED AT BS 520, RBL 6.50. REPAIRED KEEL BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,223 hrs · 46,370 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME WEB CRACKED AT LOWER DOOR DOOR STOP. REPAIRED FRAME WEB PER SWA EA.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,223 hrs · 46,370 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD CABIN EMERGENCY EXIT FLOOR LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SHEAR TIE — CRACKED (BS 986) · airframe 61,223 hrs · 46,370 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE CRACKED AT BS 986, LBL 7. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: KEELBEAM — CORRODED (BS 554) · airframe 61,223 hrs · 46,370 cycles

DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM CORRODED AT BS 554, LBL 6.5. REPAIRED KEEL BEAM PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,223 hrs · 46,370 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 505, STR 4R. REPAIRED SKIN PER SWA EA.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 61,223 hrs · 46,370 cycles

DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM CORRODED AT BS 520, LBL 6. REPAIRED KEEL BEAM PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 61,223 hrs · 46,370 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME AT FWD CARGO DOOR CUTOUT FWD WEB CRACKED AT RADIUS BELOW LOWER STOP FITTING. REPAIRED WEB PER SWA EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 61,223 hrs · 46,370 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME AT FWD CARGO DOOR CUTOUT AFT WEB CRACKED AT RADIUS ABOVE LOWER STOP FITTING. REPAIRED FRAME WEB PER SWA EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 61,223 hrs · 46,370 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 25L CORRODED AT BS 767 TO BS 827. REPAIRED STRINGER SECTION PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 61,223 hrs · 46,370 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 25L CORRODED AT BS 799. REPAIRED STRINGER SECTION PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,223 hrs · 46,370 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 514, STR 10L. REPAIRED SKIN PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,223 hrs · 46,370 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,223 hrs · 46,370 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 772, RBL 3. REPAIRED FLOORBEAM PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,223 hrs · 46,370 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 504, STR 10L. REPAIRED SKIN PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,223 hrs · 46,370 cycles

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

Part: TEE FITTING — CRACKED (AFT CARGO DOOR) · airframe 61,223 hrs · 46,370 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO DOOR INTERNAL TEE CHORD CRACKED AT FWD END NEAR NR 4 STOP FITTING. REMOVED AND REPLACED TEE CHORD PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 61,223 hrs · 46,370 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, RBL 4.5. REPAIRED BULKHEAD WEB PER SRM.

Part: WINDOW POST — CRACKED (COCKPIT) · airframe 61,223 hrs · 16,370 cycles

DURING SCHEDULED 1/4D CHECK, FOUND COCKPIT L1 WINDOW UPPER OUTBOARD POST CRACKED. REPAIRED WINDOW POST PER SRM.

Part: PRESSURE PANEL — CRACKED (BS 663) · airframe 61,223 hrs · 46,370 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 663, RBL 36 TO RBL 42. REPAIRED WEB PER SRM.

Part: SHEAR TIE — CORRODED (BS 520) · airframe 61,223 hrs · 46,370 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE CORRODED AT DOME NUT BS 520, RBL 6. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (BS 504D) · airframe 60,710 hrs · 45,953 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS BS 504D, AND BS 515D STR 10L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 504C) · airframe 60,710 hrs · 45,953 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 504C STR 10R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 768) · airframe 60,662 hrs · 45,916 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 768, STR 19R. REPAIRED SKIN PER SRM.

Part: BOLT — BROKEN (LT WING TE FLAPS) · airframe 60,518 hrs · 45,816 cycles

DURING WALKAROUND INSP, FOUND LEFT INBOARD T/E FLAP OUTBOARD ROLLER BEARING BOLT BROKEN. REMOVED AND REPLACED BOLT PER MM.

Part: SKIN — CORRODED (BS 734) · airframe 59,807 hrs · 45,242 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 734, STR 27R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 518D) · airframe 59,807 hrs · 45,242 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 518D, BETWEEN STR 11R AND STR 13R. REPAIRED SKIN PER SWA EA.

Part: LIGHT — CRACKED (CABIN) · airframe 59,711 hrs · 45,170 cycles

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

Part: SKIN — CORRODED (FUSELAGE) · airframe 58,541 hrs · 44,247 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 500A, STR 26R. REPAIRED SKIN PER SWA EA.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 58,359 hrs · 44,101 cycles

OVERHEAD BIN EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 15 DEF. SECURED LENS PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 57,219 hrs · 43,214 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND 2 EA FUSELAGE WEB CRACKS AT BS 178 BULKHEAD, BETWEEN LBL 13.5 TO RBL 9 & BETWEEN WL 218 TO WL 234. REPAIRED FUSELAGE WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,174 hrs · 43,177 cycles

DURING SCHEDULED C3 CHECK, FOUND SKIN CRACK AT BS 737, BELOW STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,128 hrs · 43,145 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 737, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM.

Part: GLOWSTRIP — DELAMINATED (CABIN) · airframe 57,106 hrs · 43,125 cycles

DURING SCHEDULED A1 CHECK, FOUND 2 EACH SECTIONS OF EMERGENCY EXIT PHOTOLUMINESCENT STRIPS IN FWD CABIN, DELAMINATED. REMOVED AND REPLACED PHOTOLUMINESCENT STRIPS PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 55,018 hrs · 41,491 cycles

BULL NOSE EMERGENCY EXIT LENS AT ROW 6 ABC, MISSING. INSTALLED LIGHT LENS PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,410 hrs · 41,004 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L1 AND R1 DOOR LOWER EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 54,351 hrs · 40,955 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR SKIN FWD SIDE AT CABLE ATTACH BOLT, CRACKED. REMOVED AND REPLACED AFT CARGO DOOR PER MM.

Part: SEAL — TORN (CARGO DOOR) · airframe 53,541 hrs · 40,314 cycles

DECLARED EMERGENCY, AIRCRAFT EXPERIENCED A MILD DEPRESSURIZATION AT 31,000 FEET NOTICED BY ALT. WARNING HORN GOING OFF. CABIN PRESSURE REACHED 10,00 FEET WENT TO STANDBY AND THEN MANUAL TO CONTROL CABIN. DESCENDED TO 14,000 WHERE STANDBY WORKED. REMOVED AND REPLACED AFT CARGO DOOR SEAL PER MM.

Part: GUSSET — CRACKED (R1 DOOR) · airframe 52,780 hrs · 39,717 cycles

DURING SCHEDULED 1/2D CHECK, FOUND R1 DOOR AFT LOWER GUSSET CRACKED. REPAIRED GUSSET PER BAC DRAWING.

Part: LIGHT — LOOSE (CABIN) · airframe 52,780 hrs · 39,717 cycles

DURING SCHEDULED 1/2D CHECK, FOUND EMERGENCY BULLNOSE LIGHT LOOSE AT ROW 13 ABC. SECURED LIGHT ASSY PER MM.

Part: FLOORBEAM — CORRODED (CABIN FLOOR) · airframe 52,780 hrs · 39,717 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 1016 FLOORBEAM CORRODED AT RBL 22. REPAIRED BEAM PER SWA EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 52,780 hrs · 39,717 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED ABOVE STR 7L. REPAIRED WEB PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 52,780 hrs · 39,717 cycles

DURING SCHEDULED 1/2D CHECK, FOUND KEEL BEAM SECTION CORRODED FROM BS 727 TO BS 727+9 RT SIDE. REPAIRED KEEL BEAM PER SRM.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 52,780 hrs · 39,717 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED OUTER BELTFRAME CHORD BS 639 STR 17. REPLACED CHORD PER EA.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 52,780 hrs · 39,717 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED FWD LEG OF BELTFRAME BS 727D RBL 4. REPAIRED PER SRM.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 52,780 hrs · 39,717 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED BELTFRAME WEB BS 639 STR 17 WL 208. REPAIRED WEB PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,780 hrs · 39,717 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 312, LBL 12 TO RBL 12. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 52,780 hrs · 39,717 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 26R CORRODED BETWEEN BS 747 AND BS 760. REPAIRED STRINGER PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,780 hrs · 39,717 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 344, LBL 12 TO RBL 12. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,780 hrs · 39,717 cycles

DURING SCHEDULED 1/2D CHECK, FOUND INNER CHORD CRACKED AT BS 616, WL 208, LBL 62.5. REPAIRED CHORD PER SWA T1-153-18.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,780 hrs · 39,717 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR FWD LOWER CUTOUT. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — SEVERED (FUSELAGE) · airframe 52,780 hrs · 39,717 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER T-CHORD SEVERED AT BS 660, BL-0, WL 207. REPAIRED PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,780 hrs · 39,717 cycles

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

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 52,780 hrs · 39,717 cycles

DURING SCHEDULED 1/2D CHECK, FOUND 0.5 INCH CRACK IN PRESSURE WEB AT BS 665, LBL 32.5. REPAIRED PER SRM.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 52,780 hrs · 39,717 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED R1 DOOR FRAME AT DOOR STOP BRACKET THIRD FROM TOP. REPAIRED PER SRM

Part: BRACKET — CORRODED (GIRT BAR) · airframe 52,780 hrs · 39,717 cycles

DURING SCHEDULED 1/2D CHECK, FOUND L1 DOOR EVACUATION SLIDE GIRT BAR FLOOR ATTACH BRACKETS CORRODED. REMOVED AND REPLACED BRACKETS PER SRM.

Part: FRAME — CRACKED (R1 DOOR) · airframe 52,780 hrs · 39,717 cycles

DURING SCHEDULED 1/2D CHECK, FOUND R1 DOOR AFT FRAME CRACKED AT NR 3 STOP FITTING. REPAIRED FRAME PER SRM.

Part: CIRCUIT CARD — FAULTY (E/E BAY) · airframe 51,508 hrs · 38,695 cycles

NLG RED UNSAFE LIGHT ILLUMINATED WITH GEAR UP. CYCLED GEAR, SYSTEM NORMAL THROUGH DURATION OF FLIGHT. REMOVED AND REPLACED M983 CIRCUIT CARD PER MM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 51,278 hrs · 38,512 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL STIFFENER WEB CRACKED AT BS 180, WL 177 & LBL 5.7. REPAIRED VERTICAL BEAM WEB PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,278 hrs · 38,512 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, LBL 5.7, WL 183 & WL 213. REPAIRED BULKHEAD WEB PER SRM.

Part: PIN — CORRODED (RT MLG) · airframe 51,001 hrs · 38,306 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT MLG TRUNNION PIN CORRODED. REMOVED AND REPLACED RT MLG TRUNNION PIN PER MM.

Part: CABLE — DAMAGED (AFT ENTRY DOOR) · airframe 50,597 hrs · 37,988 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE DAMAGED. REMOVED AND REPLACED SLIDE CABLE PER MM.

Part: BRACKET — CRACKED (NLG W/W) · airframe 49,841 hrs · 37,388 cycles

DURING SCHEDULED SERVICE CHECK, FOUND NLG UPPER ACTUATOR SUPPORT BRACKET CRACKED. REMOVED AND REPLACED NLG UPPER ACTUATOR SUPPORT BRACKET PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,831 hrs · 36,589 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 950, STR 24L. REPAIRED SKIN PER SRM.

Part: SLAT — CRACKED (LT WING) · airframe 48,804 hrs · 36,572 cycles

DURING SCHEDULED C2 CHECK, FOUND NR 1 L/E SLAT CRACKED AT INBD MAIN TRACK CUTOUT ON T/E ROW OF RIVETS. REPAIRED SLAT PER SRM.

Part: SEAL — LEAKING (CARGO DOOR) · airframe 48,627 hrs · 36,420 cycles

DURING CRUISE, CABIN ALTITUDE WARNING HORN SOUNDED. DESCENDED TO 11,000 FT, MASKS DID DEPLOY AND WERE USED. REMOVED AND REPLACED AFT CARGO DOOR PRESS SEAL. RESEALED AFT ENTRY DOOR SCUFF PLATE, RETORQUED AND RESEALED NR 1 COCKPIT WINDOW, CLEANED AFT SVC DOOR UPPER HINGE SEAL. OPS CHECKED GOOD PER MM.

Part: SLIDE — OUT OF ADJUST (FWD SVC DOOR) · airframe 47,927 hrs · 35,834 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: TAB — WORN (LT ELEVATOR) · airframe 47,237 hrs · 35,265 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT ELEVATOR TAB HAS EXCESSIVE PLAY AT HINGE POINTS. REMOVED AND REPLACED LT ELEVATOR TAB PER MM.

Part: TAB — WORN (RT ELEVATOR) · airframe 47,237 hrs · 35,265 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT ELEVATOR TAB HAS EXCESSIVE PLAY AT HINGE POINTS. REMOVED AND REPLACED RT ELEVATOR TAB PER MM.

Part: CABLE — FRAYED (AFT SVC DOOR) · airframe 46,107 hrs · 34,349 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. R&R SLIDE CABLE PER MM.

Part: SLIDE — LOOSE (FWD ENTRY DOOR) · airframe 45,816 hrs · 34,130 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM.

Part: BUSHING — WORN (RH ELEVATOR) · airframe 45,175 hrs · 33,570 cycles

DURING SCHEDULED C2 CHECK, RH ELEVATOR TAB FAILED FREE PLAY CHECK. R&R INBD ELEVATOR TAB HINGE BUSHING PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,733 hrs · 35,327 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED, BS 727D, AFT OF RH WING BODY FAIRING EMERGENCY EXIT LIGHT. REPAIRED SKIN PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 44,463 hrs · 32,985 cycles

DURING SCHEDULED 1/4 D-CHECK, FOUND KEEL BEAM STRUCTURE CORRODED FROM BS 500D TO BS 523, STR 28R. REPAIRED KEEL BEAM PER BFG ER.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 44,463 hrs · 32,985 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EMERGENCY EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,463 hrs · 32,985 cycles

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

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 44,463 hrs · 38,985 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 234, LBL 7.0. REPAIRED WEB PER SRM.

Part: CABLE — MISROUTED (EVAC SLIDE) · airframe 44,326 hrs · 32,854 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT CABLE ASSY MISROUTED. REPOSITIONED CABLE ASSY PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 44,326 hrs · 32,854 cycles

DURING SCHEDULED C1 CHECK, FOUND 1.25 CRACK AT LT HORIZ STAB LOWER SKIN, FWD OF REAR SPAR ACCESS PANEL NR 9107L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,326 hrs · 32,854 cycles

DURING SCHEDULED C1 CHECK, FOUND 3 EA. BULBS INOP IN AFT ENTRY DOOR EMERGENCY EXIT LIGHT. RELAMPED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (L/E SLAT) · airframe 44,326 hrs · 32,854 cycles

DURING SCHEDULED C1 CHECK, FOUND NR3 L/E SLAT LOWER SKIN CRACKED AT INBD AUX TRACK. REPAIRED SLAT SKIN PER SRM.

Part: WEDGE — DELAMINATED (T/E FLAP) · airframe 44,326 hrs · 32,854 cycles

DURING SCHEDULED C1 CHECK, FOUND LT WING INBD MID FLAP T/E WEDGE PANEL DISBONDED. R&R T/E WEDGE PER MM.

Part: COVER — LOOSE (CABIN) · airframe 3,547 hrs · 32,245 cycles

EEPLS TRACK COVER LOOSE AT ROW 18 TO ROW 20. SECURED TRACK COVER PER MM.

Part: COVER — LOOSE (CABIN) · airframe 43,547 hrs · 32,245 cycles

EEPLS TRACK COVER LOOSE BETWEEN ROW 18 & 20. SECURED TRACK COVER PER MM.

Part: FITTING — CORRODED (RT WING) · airframe 43,406 hrs · 32,144 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT MLG ACTUATOR BEAM SUPPORT FWD FITTING, AT AFT SPAR, CORRODED. REMOVED AND REPLACED FITTING PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 43,294 hrs · 32,065 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING T/E AFT FLAP DELAMINATED AT INBOARD AFT CORNER. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 43,294 hrs · 32,065 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING T/E AFT FLAP DELAMINATED AT INBOARD AFT CORNER. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SKIN — DELAMINATED (LT WING LE FLAP) · airframe 43,294 hrs · 32,065 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING L/E OUTBOARD FORE FLAP DELAMINATED AT INBOARD T/E. REMOVED AND REPLACED FORE FLAP PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 42,314 hrs · 31,255 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND TWO CRACKS AT BS 178 INNER WEB, BETWEEN RBL 1 AND LBL 1, WL 181.5. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (BULKHEAD) · airframe 42,314 hrs · 31,255 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 RT AND LT O/B CHORD ANGLES CRACKED. REMOVED AND REPLACED CHORD ANGLES PER ACO 7342-53.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 42,314 hrs · 31,255 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEBS CRACKED AT WL 195, RBL 23, RBL 1, TO LBL 1, WL 181.5 & WL 207, LBL 23. REMOVED AND REPLACED WEB PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,004 hrs · 30,146 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY THRESHOLD EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,004 hrs · 30,146 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: LENS — MISSING (CABIN)

DURING SCHEDULED C1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LENS ASSY PER MM.

Part: SLIDE — LOOSE (PAX DOOR)

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE GIRT OUT OF ADJUSTMENT. REINSTALLED SLIDE ASSY PER MM.

Part: BALLAST — INOPERATIVE (CABIN)

SMOKE AND ELECTRICAL SMELL AT ROW 2 ABC.. FOUND SIDEWALL LIGHT BALLAST INOP, DEFERRED PER MEL AND LATER ON AT PHX. REMOVED AND REPLACED SIDEWALL LIGHT BALLAST PER MM.

Part: BOLT — SHEARED (LT MLG)

LT MLG TORQUE LINK BOLT SHEARED IMMEDIATELY AFTER LANDING. SHIMMY DAMPER DEPARTED FROM GEAR, WALKING BEAM OUTBD ATTACH FITTING CRACKED, OUTER CYL TRUNION ATTACH LUGS CHAFED. MX FERRY TO DAL. REPLACED LT MLG TORQUE LINK BOLT. REPLACED SHIMMY DAMPER. REMOVED AND REPLACED WALKING BEAM OUTBOARD ATTACH FITTING, C/W 12K NR 1 PYLON INSPECTION. REPAIRED OUTER CYL TRUNION ATTACH LUGS PER SWA RA NR 1-332-0023, REV 1.

Part: LINE — RUPTURED (NR 2 ENGINE)

LOSS OF B-SYSTEM HYD PRESS DURING FLIGHT. LOW PRESS LIGHT ILLUMINATED AND HYD QTY IND DECREASED TO 1/8 FULL. DISCOVERED RUPTURED NR 2 ENG T/R LOCKING ACTUATOR PRESS LINE. REMOVED AND REPLACED FLEX LINE PER MM. LEAK AND OPS CHECKED GOOD.

Part: SKIN — CORRODED (SERVICE DOORWAY)

DURING SCHEDULED C3 CHECK, FOUND AFT SERVICE DOOR LOWER HINGE CUT OUT FUSELAGE SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR LOWER HINGE FUSELAGE SKIN CUT OUT CRACKED. REPAIRED SKIN PER SRM.

Part: AIR DIST — ODOR (COCKPIT)

DURING CRUISE AND DESCENT, A STRONG ODOR IN COCKPIT (HOT RUBBER). PERFORMED INSPECTION OF FWD AND AFT E/E COMPARTMENT AND COCKPIT AREA. NO DEFECTS NOTED.

Part: WIRE — FRAYED (BS 907)

DURING SCHEDULED TRANSITION CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT AT BS 907 TO HAVE FRAYED WIRES ON BACK OF LIGHT. REPAIRED FRAYED WIRES ON OVERHEAD EMERGENCY EXIT LIGHT PER BOEING MM.

Part: SKIN — GOUGED (LT WING)

DURING SCHEDULED TRANS CHECK, FOUND LT WING T/E LOWER WING SKIN JUST BELOW BEAM TO SPAR FITTING IS GOUGED AROUND FASTENERS. REPAIRED LOWER WING SKIN BELOW BEAM TO SPAR FITTING PER TRAMCO ER 98-0940.

Part: INTERCOSTAL — CRACKED (BS 269)

DURING SCHEDULED TRANSITION CHECK, FOUND CRACKED INTERCOSTAL AT BS 269, RBL 2, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: FAIRING — CRACKED (RT WING)

DURING SCHEDULED TRANSITION CHECK, WHILE WORKING DELAMINATION ON BODY FAIRING JUST FWD OF THE RT WHEEL WELL, FOUND RT WING ROOT FAIRING JUST FWD OF RT MLG WHEEL WELL HAS SEVERAL CRACKS BETWEEN FASTENER HOLES ON T/E. REPAIRED CRACKS BETWEEN FASTENER HOLES ON RT WING ROOT FAIRING JUST FWD OF RT MLG WHEEL WELL ON T/E PER BOEING SRM.

Part: SHEAR TIE — CORRODED (BS 330)

DURING SCHEDULED TRANSITION CHECK, FOUND SHEAR TIE CORRODED BETWEEN STRINGERS 27 AND 28L, BS 330. REPLACED SECTION PER BOEING SRM.

Part: SKIN — DAMAGED (BS 303)

DURING SCHEDULED TRAN CHECK, FOUND DAMAGED TO INTERIOR SKIN AT BS 303 WL 305 LBL 11. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — GOUGED (LT WING)

DURING SCHEDULED TRAN CHECK, FOUND LT WING LEADING EDGE IS GOUGED IN SEVERAL AREAS ABOVE NR 1 K-FLAP BETWEEN 15 AND 32 I/B OF NR 1 PYLON. REPAIRED DAMAGED LEADING EDGE SKIN PER ER 98-0785.

Part: STRINGER — CORRODED (BS 347)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED STRINGER 25L, AT BS 347, LBL 34. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (LT LE FLAP)

DURING SCHEDULED TRAN CHECK, FOUND LT WING ANGLE CRACKED ON FIXED LEADING EDGE O/B END OF K-FLAP AT AIRLOAD RIB. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — DAMAGED (LT HORIZ STAB)

DURING SCHEDULED TRAN CHECK, FOUND LT HORIZONTAL STAB L/E SKIN IS DAMAGED AT UPPER SURFACE FASTENER L/E BS 98.66. REMOVED DAMAGE FROM HORIZONTAL STAB. REPAIRED L/E SKIN PER ER 98-0863.

Part: STRINGER — CORRODED (BS 268-290)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED STRINGER 26 RT FROM BS 268 TO 290. REMOVED AND REPLACED PER BOEING SRM.

Part: SHEAR TIE — CORRODED (BS 344)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED SHEAR TIE AT BS 344, RBL 17 TO 18, WL 153. REMOVED AND REPLACED PER BOEING SRM.

Part: STRINGER — CORRODED (BS 360)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED STRINGER TIE AT BS 360, STR 25L. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — DAMAGED (BS 360)

DURING SCHEDULED TRAN CHECK, FOUND DAMAGED SKIN AT BS 259.5 TO 360, BL 0 TO STR 24R. REMOVED AND REPLACED PER BOEING SRM.

Part: SUPPORT — CRACKED (BS 540)

DURING SCHEDULED TRAN CHECK, FOUND CRACKED SUPPORT STRUCTURE AT BS 540, RBL 70.5, JUST ABOVE FWD O/B CORNER OF RT A/C BAY DOOR. REMOVED AND REPLACED PER BOEING SRM.

Part: STRINGER — CORRODED (BS 363)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED STRINGER 27R AT BS 363. REMOVED AND REPLACED PER BOEING SRM.

Part: SHEAR TIE — DAMAGED (BS 267)

DURING SCHEDULED TRAN CHECK, FOUND SHEAR TIE WITH EIGHT BALLED HOLE ABOVE STR 24 AT BS 267. REMOVED AND REPLACED PER BOEING SRM.

Part: STRINGER — CORRODED (BS 363-421)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED STRINGER 26 RT AT BS 363 TO 421. REMOVED AND REPLACED PER BOEING SRM.

Part: SHEAR TIE — CORRODED (BS 277)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED SHEAR TIE AT BS 277, STR 27 LT, WL 165. REMOVED AND REPLACED PER BOEING SRM.

Part: SHEAR TIE — CORRODED (BS 285)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED SHEAR TIE AT BS 285, RBL 18 TO 20, WL 152. REMOVED AND REPLACED WEB PER BOEING SRM.

Part: FRAME — MIS DRILLED (BS 827)

DURING SCHEDULED TRAN CHECK, FOUND WHILE WORKING (FUSE 164), EIGHT BALLED HOLE ON FRAME AT BS 827, LBL 23 UNDER FLOOR TO SIDE WALL SUPPORT IN ACB. REPAIRED PER ENGINEERING NR 98-0815 AND BOEING SRM.

Part: STRINGER — CORRODED (BS 348-356)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED STRINGER 26 RT AT BS 348 TO 356, CONTINUES ON TO SPLICE AT BS 357 TO 360. REMOVED AND REPLACED PER BOEING SRM.

Part: SHEAR TIE — CORRODED (BS 966)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED SHEAR TIE AT BS 966 BETWEEN STRINGER 23 AND 24R. REMOVED AND REPLACED PER BOEING SRM.

Part: STRINGER — CORRODED (BS 265-296)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED STRINGER 25RT AT BS 265 TO 296. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — DAMAGED (BS 867)

DURING SCHEDULED TRAN CHECK, FOUND MECHANICAL DAMAGED FRAME AT BS 867, STR 26R. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — DAMAGED (FUSELAGE)

DURING SCHEDULED TRAN CHECK, FOUND PANEL NR 3678 HAS NUMEROUS ELONGATED FASTENERS HOLES. REMOVED AND REPLACED DAMAGED SKIN AND ELONGATED FASTENER HOLES PER TRAMCO ER 98-0855.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED TRAN CHECK, FOUND CRACKED 178 BULKHEAD, RBL 4, WL 211.75-212 TO 25. CUT OUT CRACKED AREA AND REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 350-356)

DURING SCHEDULED TRAN CHECK, FOUND LOWER HORIZONTAL WEB CRACKED AT APPROX NAC BS 350 TO 356. REMOVED AND REPLACED INTERCOSTAL PER BOEING SRM.

Part: FRAME — CRACKED (BS 380)

DURING SCHEDULED TRAN CHECK, FOUND CRACKED FRAME AT BS 380 RBL 20 WL 152. REMOVED AND REPLACED PER BOEING SRM.

Part: CHORD — CORRODED (BS 297-305)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED T-CHORD, RBL 16, AT BS 297 TO 305, WL 150. REMOVED AND REPLACED PER BOEING SRM.

Part: STRINGER — CORRODED (BS 359)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED STRINGER SPLICE 27 LT AT BS 359. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — DAMAGED (BS 259.5)

DURING SCHEDULED TRAN CHECK, FOUND REPLACED FUSELAGE SIDE SKIN AT BS 259.5 TO 360, BL 0, STR 24L. REPAIRED PER BOEING SRM.

Part: CHORD — CRACKED (BS 344)

DURING SCHEDULED TRAN CHECK, FOUND WHILE WORKING (FUSE 354), CRACKED FAIL-SAFE CHORD AT STRINGER 25 LT, BS 344, WL 158. REMOVED AND REPLACED PER BOEING SRM.

Part: STRINGER — DAMAGED (BS 285.62)

DURING SCHEDULED TRAN CHECK, FOUND STRINGER CLIP AT BS 285.62, STR 26L HAS MECHANICAL DAMAGE. REMOVED AND REPLACED PER BOEING SRM.

Part: STRINGER — CORRODED (BS 324-331)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED STRINGER 25 RT AT BS 324 TO 331. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — DAMAGED (FUSELAGE)

DURING SCHEDULED TRAN CHECK, FOUND PANEL NR 3578 HAS NUMEROUS ELONGATED FASTENERS HOLES. REMOVED AND REPLACED DAMAGED SKIN AND ELONGATED FASTENER HOLES PER TRAMCO ER 98-0855.

Part: STRINGER — CRACKED (BS 324-331)

DURING SCHEDULED TRAN CHECK, FOUND FUSELAGE 367 CRACKED STRINGER 25 LT AT BS 324 TO 331. TRAMCO RESPONSIBILITY. REMOVED AND REPLACED PER BOEING SRM.

Part: SUPPORT — MISDRILLED (BS 727-740)

DURING SCHEDULED TRAN CHECK, FOUND MISDRILLED NUT PLATE HOLE CAUSING A EIGHT BALL HOLE EFFECT AT BS 727 +13, RBL 6, WL 155 ON CARGO TRACK. REMOVED AND REPLACED A REPLACEMENT SECTION OF FLOOR SUPPORT CHANNEL PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 400-420)

DURING SCHEDULED TRAN CHECK, FOUND CRACKED INTERCOSTAL AT BS 400 TO 420, RBL 20, WL 152. REMOVED AND REPLACED PER BOEING SRM.

Part: SILL — CORRODED (BS 440-492)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED FWD CARGO DOOR SILL WEB SUPPORTING STRUCTURE AT BS 440 TO 492.4, RBL 24, WL 155. REMOVED AND REPLACED PER BOEING SRM.

Part: STRINGER — DAMAGED (BS 987-1017)

DURING SCHEDULED TRAN CHECK, FOUND STRINGER 23RT AT BS 987 TO 1017 HAS ELONGATED HOLES. REMOVED AND REPLACED STRINGER PER BOEING SRM.

Part: STRAP — CRACKED (BS 344)

DURING SCHEDULED TRAN CHECK, FOUND AT BS 344 FLOORBEAM TENSION STRAP CRACKED AT FASTENER LBL 46, WL 200. REMOVED AND REPLACED FLOORBEAM TENSION STRAP PER BOEING SRM.

Part: FRAME — CORRODED (BS 807)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED RADIUS OF SHEAR TIE AT BS 807, RBL 1 TO LBL 1, WL 152. REPAIRED FRAME SHEAR TIE PER BOEING SRM.

Part: SHEAR TIE — CRACKED (BS 827)

DURING SCHEDULED TRAN CHECK, FOUND CRACKED SHEAR TIE AT BS 827, 1 ABOVE STRINGER 23 LT. REMOVED AND REPLACED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 324-326)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 324 TO 326, WL 208, LBL 11. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — DAMAGED (BS 727)

DURING SCHEDULED TRAN CHECK, FOUND DAMAGED FRAME UNDER FLOOR TO SIDEWALL SUPPORT AT BS 727D, RBL 19, WL 158. REMOVED AND REPLACED PER BOEING SRM.

Part: STRINGER — DOUBLE DRILLED (BS 294-359)

DURING SCHEDULED TRAN CHECK, FOUND ELONGATED AND DOUBLE HOLES IN STRINGER 27 RT AT BS 294 TO 359. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — PILLOWED (BS 908-916)

DURING SCHEDULED TRAN CHECK, FOUND PILLOWING SKIN IN AREA OF A PREVIOUS REPAIR AT BS 908 TO 916, STR 24L-25L. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — DAMAGED (BS 344-360)

DURING SCHEDULED TRAN CHECK, FOUND DAMAGED FASTENER HOLES IN INTERCOSTAL AT BS 344 TO 360, STR 25LT. REMOVED AND REPLACED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 908-1006)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED LAV WEB SUPPORT AT BS 986 TO 1006, LBL 35, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — DELAMINATED (FUSELAGE)

DURING SCHEDULED TRAN CHECK, FOUND PANEL NR 3578 DELAMINATED AND CRACK AFT OF STAINLESS STEEL RUB PLATE ON HUMP OF PANEL. REMOVED DAMAGED SKIN AFT OF RUBPLATE AND REPAIRED PER BOEING SRM.

Part: SKIN — DAMAGED (BS 908-1016)

DURING SCHEDULED TRAN CHECK, REPLACE RIGHT HAND FUSELAGE SKIN AT BS 908 TO 1016 STR 20 LT TO STR 25 RT. REMOVED AND REPLACED PER BOEING SRM.

Part: CHORD — DAMAGED (BS 285)

DURING SCHEDULED TRAN CHECK, FOUND DAMAGED FAIL-SAFE CHORD HAS 2 GOUGES AT BS 285, RBL 16-17, WL 157. REMOVED AND REPLACED PER BOEING SRM.

Part: STRINGER — DAMAGED (BS 266)

DURING SCHEDULED TRAN CHECK, FOUND CRACKED STRINGER 26 LT AT A FASTENER HOLE BS 266. REMOVED AND REPLACED STRINGER DAMAGED PER BOEING SRM.

Part: FLOORBOARD — DAMAGED (BS 1040-1064)

DURING SCHEDULED TRAN CHECK, FOUND DAMAGED FLOORBOARD PLATAFORM IN TAIL COMPARTMENT LOCATED BETWEEN BS 1040 AND BS 1064. REMOVED AND REPLACED PER BOEING SRM.

Part: SHEAR TIE — DAMAGED (BS 767)

DURING SCHEDULED TRAN CHECK, FOUND DAMAGED SHEAR TIE AT BS 767 BETWEEN STR 21L AND 22L. REPAIRED PER BOEING SRM.

Part: ANGLE — DAMAGED (BS 795)

DURING SCHEDULED TRAN CHECK, FOUND L-ANGLE HAS ELONGATED HOLES AT BS 795, WL 155, RBL 20. REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 877)

DURING SCHEDULED TRAN CHECK, FOUND INTERCOSTAL CRACKED AT BS 877, STR 25 RT WL 155. REPLACED PER BOEING SRM.

Part: SHEAR TIE — DAMAGED (BS 727)

DURING SCHEDULED TRAN CHECK, FOUND DAMAGED SHEAR TIE AT BS 727D BETWEEN STR 21L AND 22L. REPAIRED PER BOEING SRM.

Part: STRINGER — CORRODED (BS 963)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED STR 22 RT, AT BS 963. REMOVED AND REPLACED PER BOEING SRM.

Part: STRINGER — DAMAGED (BS 794)

DURING SCHEDULED TRAN CHECK, FOUND STRINGER CLIP AND L ANGLE AT BS 794, WL 155, STR 26R HAS ELONGATED HOLES. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — DAMAGED (BS 847-867)

DURING SCHEDULED TRAN CHECK, FOUND DAMAGED HOLES IN INTERCOSTAL AT BS 847-867, RBL 24, WL 155. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — BENT (BS 795)

DURING SCHEDULED TRAN CHECK, FOUND WEB SUPPORT ANGLE BENTED AND SEVERAL TOOLING MARKS AT BS 795, WL 158, RBL 24. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — DAMAGED (BS 794)

DURING SCHEDULED TRAN CHECK, FOUND ELONGATED HOLES IN L-ANGLE AT BS 794, RBL 24, WL 155. REPAIRED PER BOEING SRM.

Part: STRAP — DAMAGED (BS 767-867)

DURING SCHEDULED TRAN CHECK, FOUND DAMAGED FASTENER HOLES ON STRAP AT BS 767-867, RBL 24. REMOVED AND REPLACED PER BOEING SRM.

Part: STRAP — DAMAGED (BS 840-867)

DURING SCHEDULED TRAN CHECK, FOUND DAMAGED FASTENER HOLES ON SHIM STRAP AT BS 840-867, RBL 24 . REMOVED AND REPLACED PER BOEING SRM.

Part: FITTING — CORRODED (FUSELAGE)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED FOUND ON RT MLG BEAM I/B ATTACH FITTING AROUND BUSHING FACES. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — DAMAGED (BS 787-794)

DURING SCHEDULED TRAN CHECK, FOUND DAMAGED FASTENER HOLE ON INTERCOSTAL AT BS 787-794.3, RBL 24, WL 155. REPAIRED PER BOEING SRM.

Part: DOUBLER — CORRODED (CARGO DOORWAY)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED FWD UPPER CORNER OF AFT CARGO DOOR CUTOUT BS 798, RBL 70, WL 195. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 967)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED FLOORBEAM AT BS 967, RBL 5-41.5, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 860)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED FASTENERS ON FLOORBEAM SUPPORT STRAP AT BS 860, WL 160, RBL 20 TO LBL 20. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CORRODED (BS 794)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED AFT CARGO DOOR CUTOUT FWD FRAME AT BS 794, RBL 42 TO 47, WL 167 TO 171 AROUND LATCH FITTING. REMOVED AND REPLACED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 950)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 950, RBL 26 TO 44, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 987)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED FLOORBEAM AT BS 987, RBL 1-40, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 727-773)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED CARGO FLOORBEAM AT FASTENER HOLES BS 727 TO 773, LBL 12, WL 10. REMOVED AND REPLACED PER BOEING SRM.

Part: SHEAR TIE — CORRODED (BS 767)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED ON SHEAR TIE UNDER FRAME TO KEEL BEAM CLIP AT BS 767, RBL 8, WL 150. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (BS 867-877)

DURING SCHEDULED TRAN CHECK, FOUND COMBINED TWO PREVIOUS SKIN REPAIRS INTO ONE REPAIR AT BS 867-877, STR 18R-20R. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 727-773)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED CARGO FLOORBEAM AT FASTENER HOLES BS 727 TO 773, RBL 8, WL 160. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — MISDRILLED (BS 7270)

DURING SCHEDULED TRAN CHECK, FOUND MISDRILLED HOLE ON FLOORBEAM AT BS 7270+5, LBL 17, WL 160. REPAIRED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 950)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 950, RBL 46 TO 52, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: SHEAR TIE — CORRODED (BS 727)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED ON SHEAR TIE BS 727E, LBL 3. REMOVED AND REPLACED PER BOEING SRM.

Part: STANDOFF — BROKEN (BS 987)

DURING SCHEDULED TRAN CHECK, FOUND BROKEN STANDOFF ON LWR FLANGE AT BS 987 FLOORBEAM LBL 8, WL 200. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 986.5)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED AT BS 986.5 FLOORBEAM FASTENER HOLES LBL 5, 35.5 RBL 4.5, 31, 39, WL 208 AND 207. REMOVED AND REPLACED PER BOEING SRM.

Part: CREASE BEAM — CORRODED (BS 947-987)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED CREASE BEAM WEB AT BS 947-987 WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 727-773)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED FLOORBEAM AT FASTENER HOLES BS 727 TO 773, RBL 3, WL 160. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 1088)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED ANGLE ON INTERIOR OF RT TORQUE BOX AT BS 1088 JUST ABOVE CUTOUT FOR APU AIR INLET DUCT. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — CORRODED (HORIZ STAB)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED RT HORIZONTAL STAB O/B END WHERE STAB TIP MOUNTS TO STAB. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 344)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED BS 344 FLOORBEAM LBL 32 TO RBL 10, WL 208. REPAIRED PER BOEING SRM.

Part: STIFFENER — CORRODED (BS 328-344)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED STIFFENER AT BS 328-344, LBL 55-60, WL 208 AROUND FASTENER HOLES. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — CORRODED (BS 350-354)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED WEB AT BS 350- 354, WL 208 TO 223, LBL 63. REMOVED AND REPLACED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 993)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED AFT LT LAV FWD WALL SUPPORT AT BS 993, LBL 13.5- 40.5, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: RIB — DAMAGED (HORIZ STAB)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED RT HORIZONTAL STAB L/E HAS A DAMAGED RIB AT L/E BS 244.72. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — CORRODED (BS 1016)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED WEB BS 1016, LBL 41, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: DOUBLER — CORRODED (BS 306-615)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED TOP WEB DOUBLER FWD ENTRY DOOR SILL AT BS 306-315, WL 208, LBL 50-60. REMOVED AND REPLACED PER BOEING SRM.

Part: CHANNEL — CORRODED (BS 312-344)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED FWD ENTRY DOOR THRESHOLD SUPPORT CHANNEL AT BS 312 TO 344, LBL 60, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — CORRODED (BS 306-346)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED TOP AND BOTTOM OF WEB AROUND FASTENER HOLES AT BS 306-346, LBL 55-60, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: BEAM — CORRODED (BS 940-986)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED CREASE BEAM (AFT ENTRY DOOR AREA) AT BS 940-986, LBL 45-50 WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — CORRODED (BS 292)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED BOTTOM SIDE OF WEB AT BS 292, WL 207, RBL 52. REMOVED AND REPLACED PER SRM.

Part: STIFFENER — CORRODED (BS 1112-1124)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED HORIZONTAL STIFFENER BETWEEN BS 1112 AND BS 1124 LOWER SIDE OF APU AIR INLET CUTOUT ON TORQUE BOX RBL 13. REPAIRED PER SRM.

Part: BRACKET — CORRODED (BS 696)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED BOTTOM SIDE OF BRACKET AT BS 696, RBL 67, WL 208. REMOVED AND REPLACED PER SRM.

Part: FLOORBEAM — CORRODED (BS 312)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED FLOORBEAM AT BS 312, RBL 23, WL 208. REMOVED AND REPLACED PER SRM.

Part: SUPPORT — CORRODED (BS 304)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 304, LBL 29, WL 208. REMOVED AND REPLACED PER SRM.

Part: SUPPORT — CORRODED (BS 328)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 328, LBL 11, WL 208. REMOVED AND REPLACED PER SRM.

Part: STRINGER — CRACKED (BS 500)

DURING SCHEDULED TRAN CHECK, FOUND STRINGER 16 RT AND 16 LT CRACKED AT BS 500 + 4. REPAIRED PER SRM.

Part: STIFFENER — CORRODED (BS 1113)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED VERTICAL STIFFENER INTERIOR OF TORQUE BOX AT BS 1113 FWD SIDE OF APU AIR INLET CUTOUT RBL 12. REPAIRED PER SRM.

Part: FLOORBEAM — CORRODED (BS 328)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED FLOORBEAM AT BS 328, LBL 49, TO RBL 45, WL 208. REMOVED AND REPLACED PER SRM.

Part: SUPPORT — CORRODED (BS 302)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED INTERCOSTAL AT BS 302, RBL 15, WL 208. REMOVED AND REPLACED PER SRM.

Part: INTERCOSTAL — CORRODED (BS 329 - 332)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED INTERCOSTAL AT BS 329 TO 332, RBL 24, WL 208. REMOVED AND REPLACED PER SRM.

Part: WEB — CORRODED (BS 325)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED AFT SUPPORT WEB AT BS 325, WL 208 FWD GALLEY DOOR. REMOVED AND REPLACED PER SRM.

Part: ANGLE — CRACKED (BS 500-520)

DURING SCHEDULED TRAN CHECK, FOUND CRACKED ANGLE OF FLOOR SUPPORT FROM BS 500-520, BL 0, WL 208. REPAIRED PER BOEING SRM.

Part: BRACKET — CORRODED (BS 312)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED BRACKET AT BS 312, WL 208, LBL 54. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 967 - 987)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED INTERCOSTAL AT BS 967 TO 987, LBL 3, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 360)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED FLOORBEAM AT BS 360, WL 208, LBL 11. REPAIRED PER BOEING SRM.

Part: SKIN — CORRODED (BS 442)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED SKIN, LOWER FWD CORNER OF FWD CARGO DOOR CUTOUT, BS 442, RBL 32, WL 145. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 727-847)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED FLOORBEAM AT FASTENER HOLE BS 727 TO 847, LBL 3, WL 160. REPAIRED PER BOEING SRM.

Part: BRACKET — BROKEN (BS 727)

DURING SCHEDULED TRAN CHECK, FOUND (AFT CARGO BAY) SUPPORT BRACE BRACKETS BROKEN AT BS 727, LBL 1 AND RBL 2 (2) PLACES, WL 163. REMOVED AND REPLACED PER BOEING SRM.\N\N\N\N\N\N\N\N\N\N\N\N\N\N\NREPAIRED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 330-332)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED SUPPORT L-ANGLE FWD GALLEY DOOR SUB T-HOLD AT BS 330-332 BOTTOM SIDE. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — CORRODED (BS 293-298)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED WEB R1 DOOR AT BS 293-298, WL 208, RBL 55. REMOVED AND REPLACED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 951)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 951, LBL 12.5, WL 208 AND BS 951, LBL 23, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: SUPPORT — CORRODED (FUSELAGE)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 950, LBL 26 TO 44, WL 208; BS 947 TO 967, LBL 17, WL 208 AND BS 967 TO 987, LBL 17 WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED TRAN CHECK, FOUND CRACKED 178 BULKHEAD, RBL 6-7, WL 199. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED TRAN CHECK, FOUND CRACKED AT BS 178 BULKHEAD, LBL 4, WL 199-202. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — DAMAGED (BS 616)

DURING SCHEDULED TRAN CHECK, FOUND FRAME TO FLOORBEAM SUPPORT DAMAGED FASTENER AT BS 616, LBL 64.5, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — DAMAGED (BS 616)

DURING SCHEDULED TRAN CHECK, FOUND FRAME TO FLOORBEAM SUPPORT DAMAGED FASTENER AT BS 616, RBL 64.5, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — MISDRILLED (BS 1006)

DURING SCHEDULED TRAN CHECK, FOUND FRAME WITH EIGHT HOLES AT BS 1006 WL 300, RBL 5. REPAIRED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 308)

DURING SCHEDULED TRAN CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 308, RBL 11, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED TRAN CHECK, FOUND CRACKED BS 178 BULKHEAD, RBL 4, WL 199-202. REPAIRED PER BOEING SRM.