N321SW

Part: SKIN — CRACKED (BS 932 S23L) · airframe 67,683 hrs · 62,599 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 932, STR 23L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,551 hrs · 62,507 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 366, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,551 hrs · 62,507 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515A, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,653 hrs · 61,802 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 14L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 970 S21L) · airframe 65,985 hrs · 61,281 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 970, STR 21L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,703 hrs · 61,060 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 793, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,703 hrs · 61,060 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515, STR 21R. REPAIRED SKIN PER SRM.

Part: ACTUATOR — FAULTY (RT MLG) · airframe 65,517 hrs · 60,926 cycles

DIVERSION - RIGHT MLG UNSAFE LIGHT ILLUMINATED AFTER TAKEOFF. CYCLED GEAR, NO HELP. RIGHT MLG DID NOT RETRACT. REMOVED AND REPLACED RIGHT MLG LOCK ACTUATOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,410 hrs · 60,849 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 748, STR 18L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,410 hrs · 60,849 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 738E, STR 18L. REPAIRED SKIN PER SWA EA.

Part: ACTUATOR — MALFUNCTIONED (RT MLG) · airframe 64,938 hrs · 60,477 cycles

DURING CLIMB LANDING GEAR LEVER SELECTED TO UP POSITION, RIGHT MLG UNSAFE LIGHT ILLUMINATED. CYCLED GEAR HANDLE, LIGHTS EXTINGUISHED. REMOVED AND REPLACED RIGHT MLG UPLOCK ACTUATOR PER MM.

Part: ACTUATOR — FAULTY (RT MLG) · airframe 64,305 hrs · 59,980 cycles

ON TAKEOFF FROM SMF, WHEN MOVING THE LANDING GEAR HANDLE TO OFF POSITION, THE RT MLG EXTENDED. RT MLG RETRACTED NORMALLY WHEN GEAR LEVER PLACED UP. REMOVED AND REPLACED RT MLG UPLOCK ACTUATOR PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 64,234 hrs · 59,916 cycles

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

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 64,234 hrs · 59,916 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 2 DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 64,234 hrs · 59,916 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD CABIN EMERGENCY FLASHLIGHT BROKEN. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: FITTING — CRACKED (LT WING MLG BEAM) · airframe 64,234 hrs · 59,916 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING MLG BEAM INBOARD FITTING CRACKED. REPAIRED MLG FITTING PER ER.

Part: SKIN — CRACKED (ELEVATOR TAB) · airframe 64,234 hrs · 59,916 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT ELEVATOR TAB LOWER SURFACE CRACKED AT HINGE CUTOUT. REMOVED AND REPLACED ELEVATOR TAB PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 64,324 hrs · 59,916 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CHORD CORRODED AT BS 986.5, RBL 15 TO LBL 46. REPAIRED FLOORBEAM WEB PER ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 64,324 hrs · 59,916 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM WEB CORRODED AT BS 328, LBL 47. REPAIRED FLOORBEAM WEB PER ER.

Part: SKIN — DEBONDED (LT WING FOREFLAP) · airframe 64,234 hrs · 59,916 cycles

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

Part: WEDGE — DEBONDED (MID FLAP) · airframe 64,234 hrs · 59,916 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING IB MID FLAP T/E WEDGE UPPER AND LOWER AREAS DISBONDED. REMOVED AND REPLACED LT WING MID FLAP IAW MM.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 64,324 hrs · 59,916 cycles

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

Part: FRAME — CRACKED (BS 440 S9R) · airframe 64,234 hrs · 59,916 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 9R. REPAIRED FRAME SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (BS 294 S11L) · airframe 64,234 hrs · 59,916 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 480 S9L) · airframe 64,234 hrs · 59,916 cycles

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

Part: TORQUE TUBE — CORRODED (LT WING FLAP) · airframe 64,234 hrs · 59,916 cycles

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

Part: FRAME — CRACKED (BS 907 S9L) · airframe 64,234 hrs · 59,919 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 9L. REPAIRED FRAME SECTION PER SRM.

Part: TORQUE TUBE — CORRODED (RT WING FLAP) · airframe 64,234 hrs · 59,916 cycles

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

Part: FRAME — CRACKED (BS 907) · airframe 64,234 hrs · 59,919 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, RBL 2. REPAIRED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (BS 867 S9R) · airframe 64,234 hrs · 59,919 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 9R. REPAIRED FRAME SECTION PER SRM.

Part: SKIN — CRACKED (RT WING) · airframe 64,234 hrs · 59,916 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING INBOARD MID FLAP L/E SKIN CRACKED AT EXHAUST GATE PUSH ROD CUTOUT. REPAIRED MID FLAP SKIN PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 64,234 hrs · 59,916 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 360, RBL 47 TO RBL 55. REPAIRED FLOORBEAM CHORD PER SRM.

Part: TORQUE TUBE — CORRODED (LT WING) · airframe 64,234 hrs · 59,916 cycles

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

Part: SKIN — CRACKED (BS 753 S18L) · airframe 64,234 hrs · 59,916 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 753, STR 18L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (BS 480 S9R) · airframe 64,234 hrs · 59,916 cycles

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

Part: CABLE — FRAYED (L2 DOOR SLIDE) · airframe 64,234 hrs · 59,916 cycles

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

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 64,234 hrs · 59,916 cycles

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

Part: STRINGER CLIP — CRACKED (BS 277 S11R) · airframe 64,234 hrs · 59,916 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 867 S4L) · airframe 64,324 hrs · 59,916 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727E S5R) · airframe 64,324 hrs · 59,916 cycles

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

Part: STRINGER CLIP — CRACKED (BS 616 S2R) · airframe 64,324 hrs · 59,916 cycles

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

Part: STRINGER CLIP — CRACKED (BS 616 S1) · airframe 64,324 hrs · 59,916 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: BULKHEAD — CRACKED (BS 294 S9L) · airframe 64,234 hrs · 59,916 cycles

DURING SCHEDULED 20Y CHECK, FOUND BULKHEAD CRACKED AT BS 294.5, STR 9L. REMOVED AND REPLACED WEB SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727E S4R) · airframe 64,324 hrs · 59,916 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 360 S8R) · airframe 64,324 hrs · 59,916 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727E S4L) · airframe 64,324 hrs · 59,916 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,234 hrs · 59,916 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,115 hrs · 59,834 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 803 TO BS 813, STR 13R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,115 hrs · 59,835 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 804 TO BS 827, STR 14R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 732 S14R) · airframe 63,818 hrs · 59,583 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 732, STR 14R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 506 S21R) · airframe 63,775 hrs · 59,553 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 506, STR 21R. REPAIRED SKIN PER SWA EA AND SRM.

Part: SKIN — CRACKED (BS 465 S16R) · airframe 63,775 hrs · 59,553 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 465, STR 16R. REPAIRED SKIN PER SWA EA AND SRM.

Part: SKIN — CRACKED (BS 747) · airframe 63,324 hrs · 59,231 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 18R. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 920) · airframe 63,324 hrs · 59,231 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 920, STR 26R. REPAIRED SKIN PER SRM.

Part: WEB — CRACKED (BS 259) · airframe 63,324 hrs · 59,231 cycles

DURING SCHEDULED C1 CHECK, FOUND NLG W/W LEFT SIDE WEB CRACKED AT BS 259, WL 174. REPAIRED WEB PER SWA EA.

Part: SKIN — CRACKED (BS 315) · airframe 63,324 hrs · 59,231 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 318, STR 18R. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 404) · airframe 63,324 hrs · 59,231 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 404, STR 16R. REPAIRED SKIN PER SWA EA.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,141 hrs · 59,078 cycles

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

Part: SKIN — CRACKED (BS 767) · airframe 62,369 hrs · 58,496 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 791) · airframe 62,369 hrs · 58,496 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 791, STR 14R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 807) · airframe 62,369 hrs · 58,496 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 807, STR 19L. REPAIRED SKIN PER SWA EA AND SRM.

Part: SKIN — CRACKED (BS 404) · airframe 62,369 hrs · 58,496 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 404, STR 26R. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 62,369 hrs · 58,496 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING OTBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SKIN — DELAMINATED (NR 6 SLAT) · airframe 62,369 hrs · 58,496 cycles

DURING SCHEDULED C4 CHECK, FOUND NR 6 L/E SLAT T/E WEDGE DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: SKIN — CRACKED (BS 500D) · airframe 62,369 hrs · 58,496 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 520) · airframe 61,865 hrs · 58,092 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 12R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 473-474) · airframe 61,865 hrs · 58,092 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 473 TO BS 474, STR 16R. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 739) · airframe 61,865 hrs · 58,092 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 739, STR 19R. REPAIRED SKIN PER SWA EA & SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 61,708 hrs · 57,977 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,404 hrs · 57,720 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 727C TO BS 727D, STR 14L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 61,404 hrs · 57,720 cycles

DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,212 hrs · 57,565 cycles

DURING WALKAROUND INSP, FOUND FUSELAGE SKIN CRACKED AT BS 727C + 8, STR 14R. REPAIRED SKIN PER SWA EA & SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 60,427 hrs · 56,925 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,427 hrs · 56,925 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,309 hrs · 56,827 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747 + 6, STR 14R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,299 hrs · 56,815 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500B + 11, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,211 hrs · 56,747 cycles

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

Part: CHARGER — INOPERATIVE (CABIN) · airframe 60,135 hrs · 56,692 cycles

DURING SCHEDULED RON CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 59,905 hrs · 56,520 cycles

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

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 59,894 hrs · 56,510 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF HOUSING. SLIDE DID NOT DEPLOY. REINSTALLED SLIDE PER MM.

Part: FLASHLIGHT — CRACKED (AFT CABIN) · airframe 59,732 hrs · 56,365 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 1 EA EMERGENCY FLASHLIGHT CRACKED AT AFT CABIN. REMOVED AND REPLACED EMERGENCY FLASHLIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 59,732 hrs · 56,365 cycles

DURING SCHEDULED RON CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. REINSTALLED L1 DOOR EVAC SLIDE PER MM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 59,732 hrs · 56,365 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 2 EA CABIN EMERGENCY FLASHLIGHTS INOP AT FWD AND AFT CABIN. REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERIES PER MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 58,562 hrs · 55,425 cycles

DURING SCHEDULED C4 CHECK, FOUND LEFT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED LEFT AFT T/E FLAP PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,562 hrs · 55,425 cycles

DURING SCHEDULED C4 CHECK, FOUND RT AFT EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,399 hrs · 55,284 cycles

DURING WALK AROUND INSPECTION FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 505, BS 515, STRINGER 16R. REPAIRED SKIN SECTIONS PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,179 hrs · 55,104 cycles

DURING SCHEDULED THRU CHECK, FOUND FUSELAGE SKIN AT BS 277, STRINGER 16L, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,682 hrs · 54,691 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 907, STRINGER 22R, CRACKED. REPAIRED SKIN PER SRM.

Part: GIRT BAR — LOOSE (R1 DOOR SLIDE) · airframe 57,674 hrs · 54,685 cycles

DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EVAC SLIDE GIRT BAR HOOKS LOOSE. REMOVED AND REPLACED R1 DOOR EVAC SLIDE GIRT BAR HOOK RIVETS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,674 hrs · 54,685 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 907, STRINGER 22R, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,674 hrs · 54,684 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT AFT ENTRY DOOR LWR HINGE CUTOUT, CRACKED. REPAIRED SKIN PER EA.

Part: HOOK — LOOSE (L1 DOOR) · airframe 57,368 hrs · 54,433 cycles

L1 DOOR EVAC SLIDE GIRT BAR HOOKS LOOSE. SECURED L1 DOOR EVAC SLIDE GIRT BAR HOOKS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,765 hrs · 53,969 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN AT BS 440, STRINGER 13L, CRACKED. REPAIRED SKIN PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 56,036 hrs · 53,392 cycles

DURING SCHEDULED 1/4D CHECK, FOUND L1 DOOR CUT OUT LOWER FORWARD STOP FITTING WEB DOUBLER CRACKED. REMOVED AND REPLACED PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,035 hrs · 53,390 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE CRACKED AT BS 380 BETWEEN STRINGERS 27L AND 27R. REPAIRED SHEAR TIES PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,035 hrs · 53,390 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM CORRODED AT BS 727 + 6, RBL 3 TO RBL 14. REPAIRED FLOORBEAM PER EA.

Part: FLOORBEAM — CORRODED (AFT CARGO BAY) · airframe 56,035 hrs · 53,390 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 859, RBL 8 TO LBL 3. REPAIRED BEAM PER EA.

Part: SKIN — CRACKED (L2 DOOR) · airframe 56,035 hrs · 53,390 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SKIN CRACKED AT L2 DOOR TOP HINGE. REPAIRED DOOR SKIN PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,035 hrs · 53,390 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE CORRODED AT AFT CARGO DOOR FRAME BS 794, RBL 9. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,035 hrs · 53,390 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SKIN CRACK AT BS 761, STRINGER 19R. REPAIRED SKIN CRACK PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 56,035 hrs · 53,390 cycles

DURING SCHEDULED 1/4D CHECK, FOUND L2 DOOR FRAME UPPER AND LOWER HINGE CUTOUT CRACKED. REPAIRED L2 DOOR CUTOUT PER EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 54,365 hrs · 52,026 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CRACKED AT BS 372, STR 15L. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,365 hrs · 52,026 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIP CRACKED AT BS 360, STR 11R. REMOVED AND REPLACED TIE CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 54,365 hrs · 52,028 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 14L AND STR 15L. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,245 hrs · 51,113 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 21L, BS 941 AND BS 986. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,245 hrs · 51,113 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 396, STR 12R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,149 hrs · 51,035 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT GROUND AIR CONDITIONING CONNECT POINT. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,345 hrs · 50,392 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND AFT CABIN OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS M1197 AND M1137 PEP MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,341 hrs · 50,391 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 4R, BS 727E AND BS 727D + 10. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,341 hrs · 50,391 cycles

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

Part: SIGN — LOOSE (CABIN) · airframe 51,939 hrs · 50,067 cycles

OVERHEAD EMERGENCY EXIT SIGN LOOSE AT ROW NR 3. SECURED SIGN PER MM.

Part: LENS — MISSING (CABIN) · airframe 51,869 hrs · 50,015 cycles

OVERHEAD BIN EMERGENCY EXIT BULLNOSE LIGHT LENS MISSING AT ROW NR 3 ABC. INSTALLED LENS PER MM.

Part: HINGE FITTING — WORN (ELEVATOR TAB) · airframe 51,762 hrs · 49,928 cycles

AIRFRAME VIBRATION FELT ABOVE 280 KNOTS. REMOVED AND REPLACED LEFT INBD ELEVATOR TAB HINGE FITTING PER MM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 51,283 hrs · 49,522 cycles

DURING SCHEDULED C4 CHECK, FOUND RT HORIZ STAB LOWER SKIN CRACKED AT THE AFT SPAR. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,819 hrs · 49,132 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500C + 4, STR 15R. REPAIRED SKIN PER SRM.

Part: PRINTED CKT BOARD — FAULTY (E/E BAY) · airframe 50,567 hrs · 48,924 cycles

SELECTED GEAR TO UP POSITION, POSITION LIGHTS WENT OUT, SELECTED GEAR TO OFF POSITION, MLG LT AND RT LIGHTS WERE BOTH RED AND GREEN. TRIED AGAIN WITH SAME RESULTS, ON THIRD TRY ALL INDICATIONS NORMAL. REMOVED AND REPLACED LANDING GEAR PRINTED CIRCUIT CARD PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,397 hrs · 48,778 cycles

DURING SCHEDULED BC3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 951, STR 21L. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 50,397 hrs · 48,778 cycles

DURING SCHEDULED C3 CHECK, FOUND OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW NR 11 ABC. SECURED LENS PER MM.

Part: UPLOCK SENSOR — FAILED (LT MLG) · airframe 49,579 hrs · 48,118 cycles

AIR TURNBACK, AFTER GEAR RETRACTION, LT RED MLG LIGHT ILLUMINATED. REMOVED AND REPLACED LT MLG UPLOCK SENSOR PER MM.

Part: LENS — MISSING (CABIN) · airframe 48,757 hrs · 47,439 cycles

DURING SCHEDULED C1 CHECK, FOUND OVERHEAD BIN BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 3B. INSTALLED LENS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 48,131 hrs · 46,881 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT LOOSE AT ROW 23 DEF. SECURED EXIT LIGHT PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 48,131 hrs · 46,881 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOOR BEAM UPPER T CHORD CRACKED AT BS 344, LBL 9. REPAIRED FLOOR BEAM TEE PER SRM.

Part: SLAT — CRACKED (LH WING) · airframe 48,131 hrs · 46,881 cycles

DURING SCHEDULED 1/2D CHECK, FOUND # 4 L/E SLAT LOWER SKIN CRACKED OTBD OF ACTUATOR ATTACH. REPAIRED SKIN PER SRM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 48,131 hrs · 46,881 cycles

DURING SCHEDULED 1/2D CHECK, FOUND VERTICAL BEAM WEB CRACKED .125 IN AT BS 180, LBL 5.7 & WL 180. REPAIRED WEB PER SWA RA.

Part: TAB — WORN (RH ELEVATOR) · airframe 48,131 hrs · 46,881 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RH ELEVATOR TAB INBD HINGE WORN. R&R TAB PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,131 hrs · 46,881 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,569 hrs · 46,411 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 937, ABOVE STR 25L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,569 hrs · 46,411 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D+10, BELOW STR 11L. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (LT FORE FLAP) · airframe 46,917 hrs · 45,843 cycles

DURING SCHEDULED PM CHECK, FOUND LT WING L/E OUTBD FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,917 hrs · 45,843 cycles

DURING SCHEDULED C3 CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 771, STR 18R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,753 hrs · 45,704 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 927, BELOW STR 23R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,670 hrs · 45,644 cycles

DURING WALK-AROUND INSPECTION, FOUND 4 EXTERNAL FUSELAGE SKIN CRACK AT BS 516.5, STR 10R & .75 INCH CRACK AT BS 500B STR 10R. REPAIRED SKIN PER RA.

Part: BEAM — CORRODED (RT MLG) · airframe 45,892 hrs · 45,006 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT MLG STABILIZER BEAM AFT LUG FACE CORRODED. REMOVED AND REPLACED STABILIZER BEAM PER MM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 45,843 hrs · 44,961 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND CREASE BEAM CRACKED, BS 178, WL 207. REPAIRED CREASE BEAM PER ER 00-1236.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,843 hrs · 44,961 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD LT SIDE CHORD CRACKED ABOVE AND BELOW WL 207. REMOVED AND REPLACED CHORD PER SWA ACO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 45,843 hrs · 44,961 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD CRACKS AT WL 188 TO 234, LBL 9.0 TO RBL 5.7. REPAIRED BULKHEAD PER SWA ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,843 hrs · 44,961 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD RT SIDE CHORD CRACKED ABOVE AND BELOW WL 208. REMOVED AND REPLACED SIDE CHORD PER SWA ACO.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 45,758 hrs · 44,892 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD SECTION EEPLS INOP. REMOVED AND REPLACED EEPLS BATTERY PACK AND CHARGER ASSY PER MM.

Part: BATTERY PACK — INOPERATIVE (ROWS 1 - 7) · airframe 45,607 hrs · 44,820 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP FROM ROWS 1 - 7 AND EXIT DOORS R1 AND L1. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 45,567 hrs · 44,745 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT FORWARD SECTION. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 44,257 hrs · 43,600 cycles

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

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 44,158 hrs · 43,525 cycles

FWD ENTRY DOOR FELL OUT OF CONTAINER 3 TIMES, AT ONT FLT NR 1710, AT SMF FLT NR 1710 AND AT OAK FLT NR 1702. REINSTALLED SLIDE ASSY IN ALL THREE LOCATIONS PER MM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 44,059 hrs · 43,441 cycles

FWD ENTRY DOOR EVACUATION SLIDE INDICATOR VIEWING GLASS BROKEN, LATER AT MDW THE SLIDE ASSY FELL OUT OF CONTAINER WHEN DOOR WAS CLOSING. R & R VIEWING GLASS AND REINSTALLED SLIDE ASSY PER MM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 43,877 hrs · 43,282 cycles

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

Part: GCU — FAILED (NR 2)

NR 2 GENERATOR DROPPED OFF THE LINE. APU SWITCHED AND POWER RESUMED NORMAL. APPROX 4 MINUTES LATER NR 2 GENERATOR BUS POWER DROPPED OFF THE LINE AND IT WOULD NO LONGER POWER. FLIGHT ATTENDANT REPORTED A LOUD GRINDING NOISE AND WHAT THEY DESCRIBED AS A ENGINE BACKFIRING. APU GEN BUS VOLTS AND FREQUECY WERE NORMAL, APU AMP GAGE WAS FLUCTUATING. SHUT DOWN APU AND DIVERTED TO BHM. REMOVED AND REPLACED NR 2 ENGINE GENERATOR CONTROL UNIT, OPS CKD GOOD PER MM.

Part: BEAM — CRACKED (LT WING)

DURING SERVICE CHECK, WALKAROUND INSPECTION FOUND THE LEFT WING LOWER TRAILING EDGE BEAM CRACKED. REMOVED AND REPLACED BEAM PER SRM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND CRACK THRU EDDY CURRENT INSPECTION AT BULKHEAD FWD WEB BS 178, RBL 10, WL 234. REPAIRED PER SRM.

Part: FLOORBEAM — CORRODED (BS 500)

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON FLOORBEAM, BS 500C AROUND TIE DOWNS. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CRACKED (BS 661)

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CRACKED AT BL 0, BS 661. REPAIRED BEAM PER SB 737-57-1210.

Part: FLOORBEAM — CORRODED (BS 794)

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON FLOORBEAM, BS 794, RBL 5. REPAIRED PER SWA RA NR1-353-2028.

Part: SKIN — CRACKED (NR 6 LE SLAT)

DURING SCHEDULED 1/4D CHECK, FOUND NR 6 SLAT LOWER SKIN CRACKED BETWEEN ACTUATOR STOPS, CRACK LENGTH 1.5 INCH. REPAIRED SLAT PER SWA RA NR 1-357-0646.

Part: FLOORBEAM — CORRODED (BS 727)

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON FLOORBEAM, BS 727D LBL 68 AND RBL 68. REPAIRED BEAM PER SWA RA NR 1-353-2028.

Part: FRAME — CRACKED (CARGO DOOR)

DURING SCHEDULED 1/4D CHECK, FOUND FWD CARGO DOOR FRAME CRACKED AT LOWER AFT CORNER. REPLACED DOOR PER MM.

Part: WEB — CRACKED (BS 664)

DURING SCHEDULED 1/4D CHECK, FOUND CRACK IN BEADED PRESSURE WEB AT STA 664, LBL 32. REPAIRED PER SWA RA NR 1-353-2033.

Part: SKIN — CRACKED (BS 310)

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED 2 INCHES AT BS 310, AT S18R. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 310)

DURING SCHEDULED A1 CHECK, FOUND 2 INCH SKIN CRACK AT BS 310 STRINGER 18R AND 2 INCH CRACK 2 INCHES BELOW TOP CRACK. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (AFT CARGO)

DURING SCHEDULED C2 CHECK, FOUND AFT CARGO DOOR UPLOCK INTERCOSTAL CRACKED. REMOVED AND REPLACED PER BOEING SRM.

Part: BULB — FAILED (CABIN)

DURING SCHEDULED C1 CHECK, FOUND L1 DOOR VERTICAL EMERGENCY EXIT LIGHT HAS SOME BULBS INOP. REMOVED AND REPLACED LIGHT BULBS PER BOEING MM.

Part: RACK — CRACKED (E/E COMP)

DURING SCHEDULED C1 CHECK, FOUND CRACKED E1 RACK RT FWD STANCHION. REPAIRED PER BOEING SRM.

Part: WINDOW — CRACKED (LT EMER EXIT)

DURING SCHEDULED C1 CHECK, FOUND LT EMERGENCY EXIT HATCH INNER PANE CRACKED. REMOVED AND REPLACED LIGHT INNER PANE PER BOEING MM.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT AC GROUND CONNECTION DOOR. REPAIRED PER BOEING SRM.

Part: STRAP — CRACKED (BS 344)

DURING C1 CHECK, FOUND FLOORBEAM STRAP CRACKED AT BS 344, WL 210. REPAIRED PER BOEING SRM.

Part: DOUBLER — CRACKED (FUSELAGE)

DURING SCHEDULED BC2 CHECK, FOUND EXTERNAL DOUBLER CRACKED AT UPPER LT PITOT PROBE AREA, BS 219 TO 235, S15L TO 16L. REPLACED DOUBLER PER BOEING SRM.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED A1 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M.

Part: CLIP — CRACKED (BS 500/663)

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 500A, S16R AT BS 663, S10R, AND AT BS 663, S10L. REPLACED ALL PER BOEING SRM.

Part: SKIN — HOLE (BS 359.5)

DURING SCHEDULED D-CHECK, FOUND A SMALL HOLE IN FUSELAGE SKIN AT BS 359.5, WL 268, LBL 5.7. INSTALLED REPAIR DOUBLER PER BOEING SRM.

Part: FRAME — CRACKED (BS 827)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, S9L, AT ANGLE FASTENER HOLE. INSTALLED REPAIR PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND A CRACK INDICATION AT BULKHEAD BS 178, WL 195, LBL 30, SECTION OF SIDE CHORD. REPAIRED PER TRAMCO EWO 96-0461.

Part: DOOR FRAME — CRACKED (BS 294.5)

DURING SCHEDULED D-CHECK, FOUND SERVICE DOOR FWD DOOR FRAME CRACKED AT LOWER SECTION, BS 294.5, WL 208. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 372.5)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 372.5, WL 210, LBL 70. INSTALLED REPAIR DOUBLER PER BOEING SRM.

Part: ANGLE — CRACKED (BS 360)

DURING SCHEDULED D-CHECK, FOUND WEB TO FRAME ATTACH ANGLES CRACKED AT BS 360, S10 AND 11L. REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (BS 327)

DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOORWAY OUTER SKIN CRACKED AT BS 327 RBL 65 WL 210. REPAIRED PER BOEING SRM.

Part: CLIP — CRACKED (BS 1138)

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 1138. REPAIRED PER BOEING SRM.

Part: FLOORBEAM WEB — CORRODED (BS 1019/1030)

DURING SCHEDULED D-CHECK, FOUND WEB CORRODED AT BS 1019 RBL 5 AND AT BS 1030 RBL 10 WL 208. REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 986.5)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER FLANGE CORROSION AT BS 986.5 RBL 37 LBL 5 WL 208. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 394 5)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 394.5, LBL 10 TO 12, WL 208 AND RBL 37 TO 50. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 727)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACK AT BS 727 WL 190 RBL 60 COMMON TO S18A SHEAR WEB. REPAIRED PER SWA ACO 6580-53.

Part: STRINGER — CRACKED (BS 1139-1143)

DURING SCHEDULED D-CHECK, FOUND LOWER STRINGER 5 CHORD CRACKED AT BS 1139 TO 1143. REPAIRED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 1004)

DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT AND STRAP CORRODED AT BS 1012 TO 1016 AND BS 1004. REPLACED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND PRESSURE BULKHEAD BS 178 CRACKED AT RBL 4.7 WL 201 TO 201.5 AT RBL 6.7, WL 212 TO 212.5, AT LBL 4.7, WL 198 TO 199, LBL 6.7, WL 201.5 TO 202 AND AT LBL 4.7 WL 200 TO 201. REPAIRED PER BOEING SRM AND TRAMCO EWO 96-0468.

Part: SKIN — DENTED (BS 225)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 225 LBL 31 WL 212. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND CRACK INDICATION AT BS 178, WL 195, RBL 30. REPAIRED PER TRAMCO EWO 96-0461.

Part: SKIN — DENTED (BS 200)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 200, RBL 9, WL 168. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND A 2 INCH CRACK ON BS 178 BULKHEAD AT WL 189, LBL 7.5. REPAIRED PER BOEING SRM.

Part: BULKHEAD SKIN — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE BULKHEAD SKIN CRACK INDICATION AT BS 178, WL 195. REPLACED DAMAGED SECTION OF SIDE CHORD AND SPLICED IN NEW PER BOEING SRM.

Part: SKIN — GOUGED (BS 388)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 388, S21L. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 727D)

DURING SCHEDULED SERVICE CHECK, FOUND SKIN CRACKS AT LEFT FUSELAGE JUST FWD AND BELOW EMERGENCY OVERWING EXIT LIGHT UNDER T/E FLAPS AT BS 727D, AT S23LT AND RT. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.