N322SW

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED FRAME SECTION PER SWA EA.

Part: TORQUE TUBE — CORRODED (T/E FLAP) · airframe 64,552 hrs · 60,093 cycles

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

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD CRACKED AT BS 1016 DOME CAP 4 O'CLOCK POSITION. REPAIRED DOME CAP PER ACO AND SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD CRACKED AT BS 1016 DOME CAP 2 O'CLOCK POSITION. REPAIRED DOME CAP PER ACO AND SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,552 hrs · 60,093 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED 20Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT ASSY LOOSE AT ROW 16 DEF. SECURED LIGHT ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 16R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,552 hrs · 60,093 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,552 hrs · 60,093 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED 20Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT ASSY LOOSE AT ROW 1 ABC. SECURED LIGHT ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,552 hrs · 60,093 cycles

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

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 360, STR 13R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 9R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,552 hrs · 60,093 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 9R. REPAIRED FRAME SECTION PER SWA EA.

Part: GIMBAL JOINT — CORRODED (T/E FLAP) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED 20Y CHECK, FOUND LEFT WING INBOARD FLAP INBOARD GIMBAL ASSY CORRODED. REMOVED AND REPLACED GIMBAL ASSY PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CRACKED BETWEEN BS 540 AND BS 559, STR 10L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 26R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,552 hrs · 60,093 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947.5, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 330, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,552 hrs · 60,093 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 294 S13L) · airframe 64,552 hrs · 60,093 cycles

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

Part: STRINGER CLIP — CRACKED (BS 500C S26L) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 26L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 947 S18L) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 947, STR 18L. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500B S26L) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 26L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 297) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 297, RBL 55, WL 208. REPAIRED FRAME PER SRM.

Part: STRINGER — CORRODED (BS 1009 S26R) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 26R CORRODED AT BS 1009. REPAIRED STRINGER PER SRM.

Part: FLOOR SUPPORT — CRACKED (BS 661) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED BRDG CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 661, LBL 25. REPAIRED BEAM PER SWA EA.

Part: SHEAR TIE — CRACKED (BS 440 S14R) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 440, STR 14R. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 794 S27R) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT AFT CARGO DOOR CUTOUT, BS 794, STR 27R. REPAIRED FRAME SECTION PER SRM.

Part: SHEAR TIE — CRACKED (BS 500D S28L-28R) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 500D, STR 28L TO STR 28R. REPAIRED SHEAR TIE PER SRM.

Part: FLOOR SUPPORT — CRACKED (BS 668) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED BRDG CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 668, LBL 25. REPAIRED BEAM PER SWA EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 64,552 hrs · 60,093 cycles

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

Part: BELTFRAME — CORRODED (BS 867 S26R) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED 20Y CHECK, FOUND BELTFRAME CORRODED AT BS 867, STR 26R. REPAIRED FRAME SECTION PER SRM.

Part: FLOORBEAM — CRACKED (BS 662-668) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CRACKED AT BS 662 TO BS 668, RBL 25. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, RBL 20 TO RBL 45. REMOVED AND REPLACED FLOORBEAM SECTION PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 328) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CHORD CORRODED AT BS 328, LBL 34 TO RBL 56. REMOVED AND REPLACED FLOORBEAM CHORD PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 64,552 hrs · 60,093 cycles

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

Part: SHEAR TIE — CORRODED (BS 986) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 986.5, RBL 44. REMOVED AND REPLACED SHEAR TIE PER SRM AND BOEING DRAWING.

Part: BULKHEAD — CRACKED (BS 178) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED 20Y CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, RBL 10, WL 194. REPAIRED WEB SECTION PER SRM.

Part: FRAME — CRACKED (BS 500D S20R) · airframe 64,552 hrs · 60,093 cycles

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

Part: FRAME — CORRODED (BS 849 S25R) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 849, STR 25R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRINGER — CRACKED (BS 967) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER 27L CRACKED AT BS 967. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: SKIN — CRACKED (BS 758) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 758, STR 18L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (BS 767) · airframe 64,552 hrs · 60,093 cycles

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

Part: SKIN — CRACKED (BS 527) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT GROUND A/C SERVICE DOOR CUTOUT BS 527, LBL 5.5. REPAIRED SKIN PER SWA EA.

Part: GIRT BAR — CORRODED (L1 DOOR) · airframe 64,552 hrs · 60,093 cycles

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

Part: SHEAR TIE — CORRODED (BS 727D) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727D, RBL 8. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (BS 533) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 533, LBL 8. REPAIRED SKIN PER SWA EA.

Part: GIRT BAR — CORRODED (L1 DOOR) · airframe 64,552 hrs · 60,093 cycles

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

Part: STRINGER CLIP — CRACKED (BS 277 S16L) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (BS 277 S16L) · airframe 64,552 hrs · 60,093 cycles

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

Part: SKIN — CRACKED (BS 739E S19R) · airframe 64,552 hrs · 60,093 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 739E, STR 19R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 758) · airframe 64,352 hrs · 59,928 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 758, STR 18L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 385 S15R) · airframe 64,352 hrs · 59,928 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 385, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 782 S18L) · airframe 64,352 hrs · 59,928 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 782, STR 18L. REPAIRED SKIN PER SWA EA.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 63,389 hrs · 59,191 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT WILL NOT EXTINGUISH AT R2 DOOR. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: GUSSET — CRACKED (NLG W/W) · airframe 62,923 hrs · 58,823 cycles

DURING SCHEDULED A2 CHECK, FOUND NLG ACTUATOR ATTACH FITTING GUSSETT CRACKED IN THE RADIUS. REMOVED AND REPLACED NLG GUSSETT FITTING PER MM.

Part: SKIN — CRACKED (BS 450) · airframe 62,133 hrs · 58,221 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 450, STR 26L. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 269) · airframe 62,099 hrs · 58,193 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 269, STR 16L. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 797) · airframe 62,099 hrs · 58,193 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 797, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 739E) · airframe 62,099 hrs · 58,193 cycles

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

Part: TAB — DELAMINATED (RT WING AILERON) · airframe 62,091 hrs · 58,181 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT WING AILERON TAB DELAMINATED. REMOVED AND REPLACED TAB PER MM.

Part: LENS — LOOSE (CABIN) · airframe 61,615 hrs · 57,791 cycles

DURING SCHEDULED C3 CHECK, FOUND EMERGENCY LIGHT LENS LOOSE AT ROW 6 ABC. SECURED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,615 hrs · 57,791 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 410, BL 0, NR 2 RADIO ALTIMETER ANTENNA CUTOUT. REPAIRED SKIN PER SWA EA.

Part: LENS — LOOSE (CABIN) · airframe 61,615 hrs · 57,791 cycles

DURING SCHEDULED C3 CHECK, FOUND EMERGENCY LIGHT LENS LOOSE AT ROW 1 DEF. SECURED LENS PER MM.

Part: BULB — FAULTY (NR 2 ENGINE) · airframe 61,262 hrs · 57,526 cycles

DIVERSION/DECLARED EMERGENCY. NR 2 ENGINE OIL TEMP EXCEEDED RED LINE. REMOVED AND REPLACED NR 2 ENGINE OIL TEMP BULB PER MM.

Part: SKIN — CRACKED (BS 444) · airframe 61,127 hrs · 57,428 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 444, STR 26L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 937) · airframe 60,672 hrs · 57,050 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 937, STR 23R. REPAIRED SKIN PER SWA EA AND SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,672 hrs · 57,050 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR UPPER HINGE CUTOUT, UPPER RADIUS. REPAIRED SKIN PER SWA EA AND SRM.

Part: SKIN — CRACKED (AFT CARGO) · airframe 60,672 hrs · 57,050 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT CARGO DOOR SKIN HANDLE CUTOUT CRACKED AT UPPER AFT CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,709 hrs · 56,280 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,709 hrs · 56,280 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 797, STR 17L. REPAIRED SKIN PER SRM.

Part: SENSOR — FAULTY (NLG) · airframe 59,465 hrs · 56,089 cycles

AIR TURNBACK. NLG WOULD NOT INDICATE RETRACT. RECYCLED GEAR & STILL HAD RED & GREEN LIGHTS INDICATING. REMOVED AND REPLACED S845 SENSOR PER MM.

Part: LENS — LOOSE (CABIN) · airframe 59,367 hrs · 56,007 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,216 hrs · 55,889 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 760, STR 24R. REPAIRED SKIN PER SRM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 59,026 hrs · 55,743 cycles

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

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 58,727 hrs · 55,546 cycles

DURING SCHEDULED C4 CHECK, FOUND RT AND LT LOWER HORIZONTAL STAB SKIN AT AFT SPAR, STATION 148, CRACKED. REPAIRED SKIN PER SRM.

Part: TIRE — FAILED (LT MLG) · airframe 57,863 hrs · 54,883 cycles

ON TAKEOFF FROM (JAN) HEARD LOUD NOISE SIMILAR TO A DOOR OR WINDOW OPEN, EVERYTHING ELSE NORMAL, DOOR HANDLE IN PROPER POSITION. FOUND THE NR 1 MAIN TIRE BURST ON TAKEOFF, DAMAGED 5 EACH NR 1 ENGINE FAN BLADES, 1 EACH ACOUSTIC PANEL, INNER AND MID MLG DOORS, LMLG SUPPORT SHELF PANEL, DENT ON FUSELAGE AND INBOARD MID FLAP. REMOVED AND REPLACED NR 1 MAIN TIRE AND WHEEL PER MM.

Part: WHEEL — CRACKED (MLG)

WHEEL/ TIRE ASSY WENT FLAT. SHOP FINDINGS THROWN TREAD AND 4 BROKEN WHEEL TIE BOLTS. (K)

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,781 hrs · 54,825 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520+2, STR 12L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,718 hrs · 54,772 cycles

DURING SCHEDULED C3 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 945, STRINGER 21R AND STRINGER 21L. REPAIRED SKIN SECTIONS PER EA.

Part: CABLE — FRAYED (L2 DOOR SLIDE) · airframe 57,718 hrs · 54,772 cycles

DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED L2 DOOR EVAC SLIDE CABLE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,743 hrs · 54,004 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT AFT ENTRY DOOR UPPER HINGE CUTOUT CRACKED. REPAIRED SKIN PER EA.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 56,661 hrs · 53,938 cycles

L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,234 hrs · 53,588 cycles

DURING SPV, FOUND SHEAR TIE AT BS 520, RBL 7, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 56,234 hrs · 53,588 cycles

DURING SPV, FOUND KEELBEAM CHORD AT BS 727 +2.5, AT RBL 7, CORRODED. REMOVED AND REPLACED KEELBEAM CHORD PER EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 56,228 hrs · 53,586 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT KEEL BEAM VERTICAL WEB AT BS 727 + 7 TO BS 727 + 8, CORRODED. REPAIRED WEB PER EA.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 59,228 hrs · 53,586 cycles

DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM CHORD AFT CARGO COMPARTMENT, AT BS 727 TO BS 730, LBL 12, CORRODED. REPAIRED KEEL BEAM PER EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 56,228 hrs · 53,586 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FRAME AT L1 DOOR CUTOUT, LOWER STOP FITTING CRACKED. REPAIRED FRAME PER EA.

Part: TIE — CORRODED (FUSELAGE) · airframe 56,228 hrs · 53,586 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIES AT BS 967 AND BS 989, STRINGER 27L, CORRODED. REMOVED AND REPLACED SHEAR TIES PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 56,228 hrs · 53,586 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 986 TO BS 1006, STRINGER 27L, CORRODED. REPAIRED SKIN PER SRM.

Part: LIGHT — LOOSE (OVERWING EXIT) · airframe 56,228 hrs · 53,586 cycles

DURING SCHEDULED 1/4D CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT LOOSE. SECURED EMERGENCY EXIT LIGHT PER MM.

Part: STIFFENER — CRACKED (BULKHEAD) · airframe 56,228 hrs · 53,586 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT PRESSURE BULKHEAD AT BS 1016, RT RADIAL STIFFENER CRACKED. REPAIRED STIFFENER PER BAC DRAWING.

Part: HOOK — LOOSE (GIRT BAR) · airframe 56,228 hrs · 53,586 cycles

DURING SCHEDULED 1/4D CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR HOOKS LOOSE. SECURED L1 DOOR EVAC SLIDE GIRT BAR HOOKS PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 56,119 hrs · 53,496 cycles

DURING SCHEDULED RON, L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED AND SECURED L1 DOOR EVAC SLIDE PER MM.

Part: SKIN — CRACKED (ELEVATOR TAB) · airframe 55,883 hrs · 53,307 cycles

DURING SCHEDULED C1 CHECK, FOUND BOTH LT AND RT ELEVATOR TABS SKIN CRACKED AT NR 2 HINGE CUTOUTS. REMOVED AND REPLACED BOTH ELEVATOR TABS PER MM.

Part: FAN — FAULTY (E/E BAY) · airframe 55,475 hrs · 52,985 cycles

RECIRCULATING FAN CAUSING ODOR IN COCKPIT. REMOVED AND REPLACED RECIRCULATING FAN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,927 hrs · 52,573 cycles

DURING SCHEDULED C4 CHECK, FOUND 3 INCH LONG FUSELAGE SKIN CRACK AT BS 967, BELOW STR 20L. REPAIRED SKIN PER SRM.

Part: SLIDE — DEPLOYED (SERVICE DOOR) · airframe 54,058 hrs · 51,866 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,006 hrs · 51,831 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) BS 737 AT STR 18L AND BS 930 AT STR 25R. REPAIRED SKIN PER SRM.

Part: LENS — MISSING (CABIN) · airframe 54,006 hrs · 51,831 cycles

DURING SCHEDULED C3 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING IN AFT CABIN. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,035 hrs · 51,031 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) AT BS 930 AT STR 24L, BS 520 AT STR 15R & BS 930 AT STR 21L. REPAIRED SKIN PER SRM.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 52,954 hrs · 50,963 cycles

LT OVERWING EMERGENCY EXIT LIGHT LENS CRACKED AND LIGHT LOOSE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT LENS AND SECURED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,784 hrs · 50,822 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 967, STR 21L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 51,800 hrs · 50,029 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,756 hrs · 49,995 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CRACKED AT BS 777, STR 11L. REPAIRED STRINGER PER SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 51,756 hrs · 49,995 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FWD LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 51,756 hrs · 49,995 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,756 hrs · 49,995 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAMES CRACKED (2 EA) AT STR 14L, BS 767 AND BS 787. REPAIRED FRAMES PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 51,756 hrs · 49,995 cycles

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

Part: SPLICE — CRACKED (FUSELAGE) · airframe 51,756 hrs · 49,995 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED, BS 360, STRINGER 14L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 51,756 hrs · 49,995 cycles

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

Part: SPLICE — CRACKED (FUSELAGE) · airframe 51,756 hrs · 49,995 cycles

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

Part: CLIP — CRACKED (FUSELAGE) · airframe 51,756 hrs · 49,995 cycles

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

Part: SPLICE — CRACKED (FUSELAGE) · airframe 51,756 hrs · 49,995 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND 2 EA STRINGER SPLICES CRACKED, BS 908, STRINGER 4L, AND STRINGER 4R. REMOVED AND REPLACED BOTH STRINGER SPLICES PER SRM.

Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 51,717 hrs · 49,964 cycles

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

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 50,740 hrs · 49,148 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,635 hrs · 49,060 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) ABOVE STR 10L AT BS 455 AND BS 500 PLUS 4. REPAIRED SKIN PER SWA RA.

Part: SLIDE — OUT OF ADJUST (FWD CABIN DOORS) · airframe 50,218 hrs · 48,716 cycles

DURING SCHEDULED C3 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED SLIDES PER MM.

Part: BATTERY — ERRATIC (CABIN) · airframe 49,619 hrs · 48,236 cycles

DURING SCHEDULED RON, FOUND BOTH FWD CABIN DOOR EMERGENCY EXIT LIGHTS REMAIN ILLUMINATED AFTER SW IS TURNED OFF. REMOVED AND REPLACED LIGHT BATTERY PER MM.

Part: TAB — WORN (RT ELEVATOR) · airframe 49,322 hrs · 47,996 cycles

DURING SCHEDULED C2 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB PER MM.

Part: SLIDE — OUT OF ADJUST (FWD ENTRY DOOR) · airframe 49,322 hrs · 47,996 cycles

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

Part: SLIDE — DEPLOYED (R1 DOOR) · airframe 48,749 hrs · 47,529 cycles

FWD SERVICE DOOR EVACUATION SLIDE INADVERTATLYDEPLOYED. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: SENSOR — INTERMITTENT (MLG) · airframe 48,429 hrs · 47,248 cycles

AFTER TAKEOFF, GEAR RETRACTION, FWD PANEL GEAR WARNING LIGHTS ILLUMINATED. RESET GEAR WARNING LIGHTS C/B, RECYCLED LANDING GEAR HANDLE, AND LIGHTS EXTINGUISHED. REMAINING OF THE FLIGHT WAS NORMAL. OPERATED LANDING GEAR SYS. NO DEFECTS NOTED. OPS CK GOOD PER MM.

Part: COVER — MISSING (CABIN) · airframe 48,414 hrs · 47,234 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR LOWER EMERGENCY EXIT LIGHT MISSING COVER. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,414 hrs · 47,234 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR AT UPPER HINGE CUT OUT. REPAIRED SKIN PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 48,414 hrs · 47,234 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 234 & LBL 12. REPAIRED WEB PER SRM.

Part: LENS — CRACKED (CABIN) · airframe 48,414 hrs · 47,234 cycles

DURING SCHEDULED 1/2D CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT LENS CRACKED AT ROW # 3. R&R LIGHT LENS PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 48,414 hrs · 47,234 cycles

DURING SCHEDULED 1/2D CHECK, FOUND WEB CRACKED AT BS 344, STR 12R. REPAIRED WEB PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 48,414 hrs · 47,234 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 27L CORRODED AT BS 420 TO BS 500A. REPAIRED STR PER SRM.

Part: WEB — CRACKED (LH W/W) · airframe 48,414 hrs · 47,234 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 663, LBL 32. REPAIRED WEB PER SWA RA.

Part: STRINGER — CRACKED (FWD CABIN) · airframe 48,414 hrs · 47,234 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER WEBS CRACKED ( 2 EA ) AT BS 294.5, STR'S 7L & 8L. R&R WEBS PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 48,414 hrs · 47,234 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 294.5, LBL 12 TO RBL 12. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 48,414 hrs · 47,234 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAMS CRACKED (3 EA) AT BS 787, 747 & 727D, RBL 14. REPAIRED FLOORBEAM PER SRM.

Part: DOOR FRAME — CRACKED (FWD ENTRY DOOR) · airframe 48,414 hrs · 47,234 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR FRAME CRACKED AT # 5 STOP PIN. REPAIRED DOOR FRAME PER SRM.

Part: SHEAR TIE — CORRODED (AFT CARGO) · airframe 48,414 hrs · 47,234 cycles

DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CORRODED AT BS 787, STR 27L. R&R SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,414 hrs · 47,234 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIPS CRACKED (2 EA) AT BS 663 & BS 706, STR 10L. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: INDICATOR — FAULTY (COCKPIT) · airframe 48,354 hrs · 47,184 cycles

AIR TURNBACK, CAPT'S HORIZONTAL SITUATION IND HDG FLAG IN VIEW AND SMOKE SMELL IN COCKPIT. REMOVED AND REPLACED CAPT'S HORIZONTAL SITUATION IND PER MM.

Part: SKIN — CRACKED (AFT SVC DOOR) · airframe 47,515 hrs · 46,532 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SVC DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 46,850 hrs · 45,949 cycles

DURING SCHEDULED SERVICE CHECK, FOUND MLG WHEEL WELL BULKHEAD VERTICAL STIFFENER CRACKED, BS 663, RBL 6.5. REPAIRED PER SWA RA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,617 hrs · 45,743 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SVC DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA T1-353-041.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,617 hrs · 45,743 cycles

DURING SCHEDULED C3 CHECK, FOUND 2.5 LONG FUSELAGE SKIN CRACK AT BS 510, STR 12 R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,575 hrs · 44,864 cycles

DURING SCHEDULED C2 CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 940, BELOW STR 24L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,143 hrs · 44,502 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD VERTICAL CHORDS CRACKED AT LBL 5.7 WL 179, LBL 5.7 WL 184 & LBL 17.1 WL 229.5. REPAIRED CHORDS PER ER 00-1275 & ER 00-1274.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 45,143 hrs · 44,502 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD CRACKED AT VERTICAL BEAM HOLE, LBL 17.1, WL 183. REPAIRED BULKHEAD PER ER 00-1274.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 45,143 hrs · 44,502 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD CRACKED AT WL 213.5 - 214, RBL 6.7. REPAIRED BULKHEAD PER SRM.

Part: LIGHT — DAMAGED (CABIN) · airframe 44,616 hrs · 44,048 cycles

LT OVERWING EXIT LIGHT DAMAGED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,353 hrs · 43,836 cycles

DURING SCHEDULED RON, FOUND EEPLS INOP AT ROW 3. REPAIRED EEPLS WIRING PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,334 hrs · 43,817 cycles

DURING SCHEDULED RON, FOUND EEPLS INOP AT ROW 3. REPAIRED EEPLS WIRES PER MM.

Part: SLIDE — DEPLOYED (PAX DOOR) · airframe 44,224 hrs · 43,725 cycles

FWD ENTRY DOOR EVACUATION SLIDE DEPLOYED INADVERTENTLY. REINSTALLED SLIDE ASSY PER MM.

Part: SLIDE — DISCHARGED (PAX DOOR) · airframe 44,008 hrs · 43,541 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE PRESSURE INDICATION LOW. R&R SLIDE ASSY PER MM.

Part: HANDLE — OUT OF POSITION (ESCAPE SLIDE) · airframe 46,093 hrs · 42,765 cycles

AFT SERVICE DOOR EVACUATION SLIDE RELEASE HANDLE OUT OF POSITION. REPOSITIONED SLIDE ASSY PER MM.

Part: SKIN — DELAMINATED (TE FLAP)

DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: TIRE — SEPARATED (LH MLG)

AIR TURNBACK, AFTER TAKEOFF, DURING GEAR RETRACTION NR 2 MLG TIRE SEPARATED, DAMAGING ALL THREE INBD T/E FLAPS, INBD GROUND SPOILER AND GEAR UPLOCK ACTUATOR HYD LINE. REMOVED AND REPLACED NR 1 AND NR 2 MLG TIRE/WHEEL ASSY'S, ALL THREE INBD FLAPS, INBD GROUND SPOILER AND HYD LINE PER MM.

Part: SKIN — DELAMINATED (RT TE FLAP)

DURING SCHEDULED C1 CHECK, FOUND RT INBD T/E FLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED FORE FLAP ASSY PER MM.

Part: SKIN — CRACKED (BS 929-932)

DURING OVERNIGHT CHECK, FOUND FUSELAGE SKIN CRACKED, BS 929-932, JUST BELOW STRINGER 23R. REPAIRED SKIN PER SRM.

Part: PMC — INOPERATIVE (NR 1 ENGINE)

AFTER TAKEOFF, NR 1 ENG N2, EGT AND FUEL FLOW INDICATIONS INOP DUE TO PMC. ALSO PMC INOP. REMOVED AND REPLACED NR 1 ENG PMC PER MM.

Part: CHORD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND LT SIDE CHORD CRACKED AT BS 178, LBL 26, WL 207. REPAIRED PER SRM.

Part: CHORD — CRACKED (CARGO DOOR)

DURING SCHEDULED 1/4D CHECK, FOUND FWD CARGO DOOR LOWER T-CHORD CRACKED ON AFT END. REMOVED AND REPLACED DOOR ASSY PER MM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND LT SIDE BS 178 BULKHEAD CRACKED LBL 26, WL 207. REPAIRED BULKHEAD PER SRM.

Part: KEEL BEAM — CRACKED (BS 706)

DURING SCHEDULED 1/4D CHECK, FOUND LOWER KEEL BEAM CRACKED AT BS 706. REPAIRED KEEL BEAM PER SRM.

Part: FIRE DETECTOR — MALFUNCTIONED (CARGO COMPT)

AIR TURNBACK, DURING CLIMB, BELL INDICATION OF FIRE IN AFT CARGO COMPT. DISCHARGED BOTH BOTTLES. LIGHT EXTINGUISHED AT GATE RETURN. INSPECTED AFT CARGO BIN, NO EVIDENCE OF FIRE OR EXCESSIVE HEAT. DEACTIVATED FIRE DETECTION SYSTEM PER SI 575, OK FOR CONTINUE.

Part: FLOORBEAM — CRACKED (BS 663)

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND CRACKED CENTER FLOORBEAM AT BS 663, BL O. REPAIRED BEAM PER SWA RA 1-357-0679, AND ACO 658-57.

Part: INTERCOSTAL — BROKEN (CARGO COMPT)

DURING SCHEDULED C1 CHECK, FOUND AFT CARGO COMPT INTERCOSTAL BROKEN. REMOVED AND REPLACED PER BOEING SRM.

Part: GEAR BOX — FAILED (NR 2 ENGINE)

NR 2 ENGINE FAILED CLIIMBING THROUGH 31,000, AIRCRAFT RETURN TO DAL MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND ACCY GEARBOX FAILURE WITH DAMAGE TO RT T/B COWLING AND R/T INBD LANDING LIGHT LENS COVER. REMOVED AND REPLACED NR 2 ENGINE AND R/T I/B LANDING LIGHT LENS PER BOEING MM.

Part: SKIN — CRACKED (PAX DOORWAY)

DURING SCHEDULED A1 CHECK, FOUND ENTRY DOOR HINGE ARM CUTOUT CRACKED .187 LONG AT UPPER CORNER. REPAIRED PER SWA RA 1-A57-1745

Part: FRAME — CRACKED (BS 827/480)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 827, AT STRINGER 9, AND AT BS 480, S9L. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 496)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 496, 1 INCH ABOVE S16R. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 480, BS 887 S9L AND 9R, BS 907, S9L. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 294/328)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 294 RBL 145, WL 208 AND AT BS 328 RBL 21.5 AND 35. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — DENTED (BS 519)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM DENTED AT BS 519, LBL 8, WL 156. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 455)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 455, 1 INCH BELOW S16L. REPAIRED PER BOEING SRM.

Part: BULKHEAD ANGLE — CORRODED (BS 947)

DURING SCHEDULED D-CHECK, FOUND FLOOR TO BULKHEAD SUPPORT ANGLE CORRODED AT BS 947, LBL 21 TO RBL 21, WL 179. REPAIRED PER BOEING SRM.

Part: CHORD — CRACKED (BS 1138)

DURING SCHEDULED D-CHECK, FOUND LOWER CHORD ON STRINGER 5L, AT BS 1138 + 7 CRACKED. REPLACED PER BOEING SRM.

Part: SKIN — DENTED (BS 380)

DURING SCHEDULED D-CHECK, FOUND SKIN DENTED AT BS 380, BETWEEN STRINGERS 23 AND 24. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 540)

DURING SCHEDULED D-CHECK, FOUND DRAG ANGLE CRACKED IN RADIUS AT BS 540, RIGHT 2 INCHES ABOVE S22. REPLACED PER BOEING SRM.

Part: SKIN — DAMAGED (BS 787)

DURING SCHEDULED D-CHECK, FOUND SKIN DAMAGED AT BS 787 + 8, BETWEEN STRINGERS 18 AND 19L. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 384)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 384, AT S17L. REPAIRED PER BOEING SRM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND PRESSURE WEB CRACKED AT BULKHEAD BS 178, LBL 4.7, WL 198. REPAIRED PER TRAMCO EWO 96-0691.

Part: ANGLE — CORRODED (BS 500)

DURING SCHEDULED D-CHECK, FOUND FWD CARGO BAY, FLOOR TO BULKHEAD SUPPORT ANGLE CORRODED AT BS 500D, LBL 24, RBL 24. WL 156. REPAIRED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 498)

DURING SCHEDULED D-CHECK, FOUND STRINGER CRACKED AT BS 498, S23R. REPLACED DAMAGED SECTION PER BOEING SRM.

Part: T-ANGLE — DAMAGED (BS 727)

DURING SCHEDULED D-CHECK, FOUND T-ANGLES DAMAGED AT BS 727, AT S20L AND S20R. REPLACED PER BOEING SRM.

Part: SKIN — DENTED (BS 380+19)

DURING SCHEDULED D-CHECK, FOUND SKIN DENTED AT BS 380 + 19, BETWEEN STRINGERS 24 AND 25R. REPAIRED PER BOEING SRM.

Part: SHEAR TIE — DAMAGED (BS 1138)

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 1138 AT STRINGER 5R DAMAGED. REPLACED PER BOEING SRM.

Part: SKIN — DENTED (BS 887)

DURING SCHEDULED D-CHECK, FOUND PROTRUDING DENT AT BS 887 + 2, BETWEEN STRINGERS 18 AND 19L. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 1020)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 1020, AT S14L. REPAIRED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 998/1003)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CRACKED AT BS 947 LBL 54 WL 208 AND AT RBL 4.5 AND 5.3, WL 207 AND 208. REPLACED PER BOEING SRM.

Part: SKIN — DENTED (BS 319)

DURING SCHEDULED D-CHECK, FOUND SKIN DENTED AT BS 319, BETWEEN STRINGERS 20 AND 21. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 289)

DURING SCHEDULED D-CHECK, FOUND SKIN DENTED AT BS 289, BETWEEN STRINGERS 21 AND 22. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 330)

DURING SCHEDULED D-CHECK, FOUND SKIN DENTED AT BS 330, BETWEEN STRINGERS 25 AND 26. REPAIRED PER BOEING SRM.

Part: SHEAR TIE — DAMAGED (BS 1138)

DURING SCHEDULED D-CHECK, FOUND LOWER CHORD ON STRINGER 5T AT 1139 + 5 CRACKED. REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (BS 328)

DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOORWAY LOWER AFT SKIN CUTOUT CRACKED AT BS 328, RBL 65, WL 210. REPAIRED PER BOEING SRM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND PRESSURE WEB CRACKED AT BULKHEAD BS 178, RBL 4.7, WL 201. REPAIRED PER TRAMCO EWO 96-0691.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND WEB AT BULKHEAD BS 178, BL 0, WL 187, CRACKED 1 INCH LONG. REPAIRED PER TRAMCO EWO 96-0690.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND PRESSURE WEB CRACKED AT BULKHEAD BS 178, LBL 6.7, WL 212.5. REPAIRED PER TRAMCO EWO 96-0691.

Part: SUPPORT — CORRODED (BS 998/1003)

DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 1003 AND 998. REPLACED PER BOEING SRM.

Part: CLIP — CRACKED (BS 277/520/663.5)

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, S15R, AT BS 663.5, S10R AND AT BS 520, S4R. REPLACED PER BOEING SRM.

Part: CLIP — CRACKED (BS 500 S19L)

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, S19L. REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (L1 DOOR CUTOUT)

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY LOWER HINGE CUTOUT CRACKED ON LOWER CORNER. REPAIRED PER SWA RA 1-352-255.

Part: EEL BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED MAINT CHECK, FOUND AFT SECTION OF CABIN EMERGENCY EXIT LIGHTING INOP. REPLACED BATTERY PACK PER BOEING MM.

Part: EEL BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS LEFT AND RIGHT SIDES INOP. REPLACED BATTERY PACK AND BASE PER BOEING M/M.