N319SW

Part: TORQUE TUBE — WORN (T/E FLAP) · airframe 67,061 hrs · 62,198 cycles

FLAPS SETTING FROM 25 TO 30, FLAPS LOCKED OUT. REMOVED AND REPLACED RT FLAP TORQUE TUBE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,933 hrs · 62,088 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, RBL 3. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (BS 801 S18L) · airframe 66,901 hrs · 62,062 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 801, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,800 hrs · 61,221 cycles

DURING MV2 CK, FOUND FUSELAGE SKIN CRACKED AT BS 415, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,800 hrs · 61,221 cycles

DURING MV2 CK, FOUND FUSELAGE SKIN CRACKED AT BS 425, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,800 hrs · 61,221 cycles

FUSELAGE SKIN CRACKED AT BS 475, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,800 hrs · 61,221 cycles

DURING MV2 CK, FOUND FUSELAGE SKIN CRACKED AT BS 485, STR 16R. REPAIRED SKIN PER SRM.

Part: LENS — MISSING (CABIN) · airframe 65,622 hrs · 61,074 cycles

BULL NOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 17 DEF. INSTALLED LIGHT LENS PER MM.

Part: TIRE — RUPTURED (RT MLG) · airframe 65,603 hrs · 61,059 cycles

DIVERSION / DECLARED EMERGENCY. NR 3 MAIN TIRE RUPTURED ON TAKEOFF. REMOVED AND REPLACED NR 3 WHEEL AND TIRE ASSY, RIGHT WING INBOARD GROUND SPOILER, FORE FLAP AND MID FLAP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,276 hrs · 60,823 cycles

DURING SCHEDULED HC1 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 19 DEF. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,319 hrs · 60,093 cycles

DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 430, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,319 hrs · 60,093 cycles

DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 376, STR 15R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,319 hrs · 60,093 cycles

DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 480, STR 19L. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 64,319 hrs · 60,093 cycles

DURING SCHEDULED MV4 CHECK, FOUND SHEAR TIE CRACKED AT BS 380, STR 14R. REPAIRED SHEAR TIE PER SWA EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,944 hrs · 29,785 cycles

DURING SCHEDULED MV3 CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FITTING — CORRODED (RT WING MLG) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT MLG HANGER SHAFT AFT FITTING CORRODED. REMOVED AND REPLACED MLG SHAFT AFT FITTING PER MM.

Part: RIB — CRACKED (BS 151) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT HORIZONTAL STAB RIB CRACKED AT STA 151.75. REMOVED AND REPLACED HORIZONTAL STAB RIB PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 63,493 hrs · 59,418 cycles

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

Part: FRAME — CRACKED (BS 296 S7R) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND STUB FRAME CRACKED AT FWD SIDE UPPER CORNER BS 296, STR 7R. REMOVED AND REPLACED STUB FRAME SECTION PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 63,493 hrs · 59,418 cycles

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

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT ELEVATOR SKIN DELAMINATED AT UPPER SURFACE STA 84. REPAIRED ELEVATOR SKIN PER SRM.

Part: FITTING — CORRODED (RT WING MLG) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT MLG HANGER SHAFT AFT FITTING CORRODED. REMOVED AND REPLACED MLG SHAFT AFT FITTING PER MM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT FWD CARGO DOOR CUTOUT FWD LOWER CORNER. REPAIRED SKIN SECTION PER ER.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING INBOARD FORE FLAP DELAMINATED INBOARD T/E. REPAIRED FORE FLAP SKIN PER SRM.

Part: FITTING — CORRODED (RT WING MLG) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT MLG STABILIZER BEAM AFT FITTING CORRODED. REMOVED AND REPLACED AFT FITTING PER MM.

Part: BULKHEAD — CRACKED (BS 1016 S7R) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD DOME CAP CRACKED AT BS 1016, STR 7R. REPAIRED DOME CAP PER SRM.

Part: FLOORBEAM — CORRODED (BS 270) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 270, LBL 11 TO RBL 11. REMOVED AND REPLACED FLOORBEAM CHORD PER SRM.

Part: STRINGER CLIP — CRACKED (BS 277 S15R) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: ANGLE — CORRODED (BS 312-348) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD ENTRY DOOR ZEE ANGLE CORRODED AT BS 312 TO BS 348, LBL 62. REMOVED AND REPLACED ZEE ANGLE PER SRM.

Part: BULKHEAD — CRACKED (BS 1016) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD DOME CAP CRACKED AT BS 1016, FIRST FASTENER AT 7 O'CLOCK POSITION. REPAIRED DOME CAP PER SRM.

Part: FLOORBEAM — CORRODED (BS 1016) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 1016, LBL 4. REMOVED AND REPLACED FLOORBEAM CHORD PER SRM.

Part: BEAR STRAP — CRACKED (BS 440 S19R) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT BS 440, STR 19R. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (BS 1016 S4L) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD DOME CAP CRACKED AT BS 1016, STR 4L. REPAIRED DOME CAP PER ER.

Part: FRAME — CRACKED (BS 480) · airframe 63,493 hrs · 59,418 cycles

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

Part: FLOOR SUPPORT — CRACKED (BS 727B) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOOR SUPPORT CRACKED AT BS 727B, RBL 45. REPAIRED FLOORBEAM PER ER.

Part: SPAR — CORRODED (HORIZONTAL STAB) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT AND RT HORZ STAB SPARS LUG FACES CORRODED. REPAIRED HORZ STAB PER SRM.

Part: FRAME — CRACKED (BS 827) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 827, LBL4, WL 154. REPAIRED FRAME SECTION PER SRM.

Part: FLOOR SUPPORT — CRACKED (BS 663-671) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOOR SUPPORT CRACKED AT BS 663 TO BS 671, LBL 25. REPAIRED FLOORBEAM PER ER.

Part: STRINGER SPLICE — CRACKED (BS 358 S15L) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 358, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SKIN — CORRODED (BS 986) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 986.5, BL 0. REPAIRED SKIN PER ER.

Part: BEAM — CRACKED (VERTICAL STAB) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND VERTICAL STAB LT TRAILING EDGE BEAM CRACKED. REMOVED AND REPLACED VERTICAL STAB BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 26L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 727D S25L) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D. STR 25L. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FRAME — CRACKED (BS 440) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (BS 887) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8R. REPAIRED FRAME SECTION PER SRM.

Part: SHEAR TIE — CRACKED (BS 520) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 22L. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 807) · airframe 63,493 hrs · 59,418 cycles

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

Part: FRAME — CRACKED (BS 380) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (BS 827) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (BS 907) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME SECTION PER SRM.

Part: SKIN — CORRODED (BS 942 S26L) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 942.5, STR 26L. REPAIRED SKIN SECTION PER SWA EA.

Part: SKIN — CRACKED (BS 958 S17L) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 958, STR 17L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,493 hrs · 59,418 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,493 hrs · 59,418 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,493 hrs · 59,418 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,493 hrs · 59,418 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 9L. REPAIRED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,493 hrs · 59,418 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 24L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,493 hrs · 59,418 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,493 hrs · 59,418 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,493 hrs · 59,418 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,493 hrs · 59,418 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,493 hrs · 59,418 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,493 hrs · 59,418 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 23L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,493 hrs · 59,418 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,493 hrs · 59,418 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 63,493 hrs · 59,418 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,493 hrs · 59,418 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 19L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 1138, STR 13L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: TORQUE TUBE — CORRODED (RT FOREFLAP) · airframe 63,493 hrs · 59,418 cycles

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

Part: TORQUE TUBE — CORRODED (RT FOREFLAP) · airframe 63,493 hrs · 59,418 cycles

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

Part: SKIN — CRACKED (BS 517D) · airframe 62,077 hrs · 58,361 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 517D, STR 13L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 907) · airframe 62,077 hrs · 58,361 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 907, STR 4L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 737) · airframe 62,073 hrs · 58,359 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 737, STR 18R. REPAIRED SKIN PER SWA EA & SRM.

Part: SPAR — CRACKED (HORIZONTAL STAB) · airframe 62,073 hrs · 58,359 cycles

DURING SCHEDULED C4 CHECK, FOUND RT HORIZONTAL STAB AFT SPAR CRACKED 5 INCHES FROM ROOT. REPAIRED HORIZONTAL STAB PER SRM.

Part: SKIN — CRACKED (BS 500) · airframe 62,073 hrs · 58,359 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500, STR 15L. REPAIRED SKIN PER SRM.

Part: CONTROL VALVE — FAILED (L/E SLAT) · airframe 61,618 hrs · 58,012 cycles

AIR TURNBACK, L/E DEVICES DID NOT RETRACT AND L/E FLAPS TRANSIT LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED AUTO SLAT CONTROL VALVE PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,546 hrs · 57,958 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 2. RELAMPED LIGHT PER MM.

Part: SKIN — CRACKED (BS 927) · airframe 61,151 hrs · 57,607 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 23L. REPAIRED SKIN PER SWA EA.

Part: LATCH — MISSING (R2 DOOR SLIDE) · airframe 59,773 hrs · 56,528 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR LATCH SPRING MISSING. REMOVED AND REPLACED LATCH ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,277 hrs · 56,137 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACK AT STA 931, STR 24R. REPAIRED SKIN PER EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,295 hrs · 55,360 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD LT CUTOUT OF EXTERNAL A/C ACCESS HOOK UP. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,295 hrs · 55,360 cycles

DURING SCHEDULED C4 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS BETWEEN BS 927 & BS 935, STR 24R TO STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,295 hrs · 55,360 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 410, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,295 hrs · 55,360 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500, STR 19L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 57,793 hrs · 54,951 cycles

L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 57,782 hrs · 54,942 cycles

L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,763 hrs · 54,923 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,292 hrs · 54,537 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,292 hrs · 54,537 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT FWD ENTRY DOOR LOWER HINGE CUTOUT, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,292 hrs · 54,537 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT FWD SERVICE DOOR LOWER HINGE CUTOUT, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,441 hrs · 53,852 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 500D + 6, STRINGER 16L, CRACKED. REPAIRED SKIN PER EA.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 56,052 hrs · 53,536 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT KEEL BEAM WEB CORRODED AT BS 727 + 11, STRINGER 27R, BS 727 + 14, STRINGER 27R. REPAIRED WEB SECTION PER ER.

Part: FRAME — CRACKED (R1 DOOR) · airframe 56,052 hrs · 53,536 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR ASSEMBLY FRAME CRACKED AT NR 3 AFT STOP MOUNT. REMOVED AND REPLACED R1 DOOR PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,052 hrs · 53,536 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO DOOR FRAME CUTOUT CRACKED AT FORWARD SIDE OF CUTOUT, BY CENTERING PAD. REPAIRED FUSELAGE FRAME PER EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 56,052 hrs · 53,536 cycles

DURING SCHEDULED 1/4D CHECK, FOUND L1 DOOR CUTOUT FRAME CRACKED AT THE NR 6 AND NR 7 STOPS. REPAIRED FRAME PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 56,053 hrs · 53,536 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, LBL 5.7. REPAIRED WEB PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 60,081 hrs · 58,817 cycles

DURING SCHEDULED 1/4D CHECK, FOUND L1 DOOR FRAME CUTOUT CRACKED AT FORWARD WEB. REMOVED AND REPLACED WEB PER SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 56,052 hrs · 53,536 cycles

DURING SCHEDULED 1/4D CHECK, FOUND WING CENTER SECTION BEADED WEB CRACKED AT RBL 38. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,052 hrs · 53,536 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CRACKS IN FUSELAGE SKIN AT BS 727E + 3, STRINGER 18R, AND BS 924, STRINGER 23R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,232 hrs · 52,877 cycles

DURING SCHEDULED PM CHECK, FOUND 4 IN LONG FUSELAGE SKIN CRACK AT BS 727E, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,533 hrs · 52,303 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500B + 4, STR 14L. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,928 hrs · 54,270 cycles

DURING SCHEDULED RON, FOUND BOTH AFT CABIN DOORS OVERHEAD EMERGENCY EXIT LIGHTS BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,864 hrs · 51,773 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED (2 EA) BS 520 AT STR 16L AND BS 727E AT STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,854 hrs · 51,763 cycles

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED (2 EA) BS 727E PLUS 12 AT STR 19R AND BS 520 AT STR 16L. REPAIRED SKIN PER SRM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 53,618 hrs · 51,574 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,539 hrs · 51,512 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727C, BETWEEN STR 18R AND STR 19R. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 52,878 hrs · 50,983 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 500D, BELOW STR 10R. R&R SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,878 hrs · 50,983 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED ( 3 EA ) AT BS 500D, STR 13R & BS 520, STR'S 12R & 12L. REPAIRED SKIN PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 52,878 hrs · 50,983 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,878 hrs · 50,983 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT BS 663.75, STR 2L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,878 hrs · 50,983 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT BS 520, BETWEEN STR 12R & STR 13R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,878 hrs · 50,983 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND PAX WINDOW CUTOUT CRACKED AT RH WINDOW # 9. REPAIRED SKIN PER SWA ERO.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 52,875 hrs · 50,981 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIP CRACKED AT BS 616, STR 5R. REMOVED AND REPLACED STR TIE CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,875 hrs · 50,981 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND 2 EA 3.5 IN LONG CRACKS AT FUSELAGE SKIN, BS 941 AND BS 972, BELOW STRINGER 21L. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 52,875 hrs · 50,981 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 360, BETWEEN STRINGERS 13L TO 14L. REMOVED AND REPLACED SHEAR TIE SECTION PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 52,875 hrs · 50,981 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER 4R CRACKED BETWEEN BS 663 AND BS 727. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,875 hrs · 50,981 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 360, STRINGER 14L. REPAIRED SKIN PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 52,875 hrs · 50,981 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4L. REPAIRED STRINGER SPLICE PER SRM.

Part: CABLE — MISROUTED (SERVICE DOOR) · airframe 52,629 hrs · 50,784 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,863 hrs · 50,164 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,863 hrs · 50,164 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 4R, BS 597 AND BS 706. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,832 hrs · 49,287 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 25R. REPAIRED SKIN PER SRM.

Part: COVER — MISSING (AFT SVC DOOR) · airframe 50,670 hrs · 49,150 cycles

DURING SCHEDULED PM CHECK, FOUND AFT SVC DOOR EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED LIGHT COVER PER MM.

Part: LIGHT — ERRATIC (COCKPIT) · airframe 50,550 hrs · 49,043 cycles

AIR TURNBACK, DURING CLIMB ENG ANNUNCIATOR WARNING LIGHT ILLUMINATED, ALL ENGINE PARAMETERS CHECK NORMAL. REMOVED AND REPLACED F/O'S SIX PACK LIGHTS PER MM.

Part: TAB — CRACKED (LT ELEVATOR) · airframe 50,326 hrs · 48,857 cycles

DURING SCHEDULED A1 CHECK, FOUND LT ELEVATOR TAB INBD CONTROL ROD ATTACH POINT CRACKED. REMOVED AND REPLACED LT ELEVATOR TAB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,932 hrs · 48,537 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSLAGE SKIN CRACKED AT AFT SVC DOOR ON LOWER HINGE CUT OUT. REPAIRED SKIN PER SRM.

Part: SLIDE — LOOSE (FWD SVC DOOR) · airframe 49,691 hrs · 48,351 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE NOT SECURED IN CONTAINER. SECURED SLIDE PER MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 49,185 hrs · 47,957 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,425 hrs · 47,332 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACK ( 2 EA ) AT BS 932, STR 24L & BS 930, STR 23R. REPAIRED SKIN PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 48,050 hrs · 47,019 cycles

DURING SCHEDULED 1/2D CHECK, FOUND VERTICAL BEAM WEBS CRACKED ( 2 EA ) AT BS 180, WL 224, RBL 17.1 & BS 185, WL 227, LBL 17.1. R&R WEBS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,050 hrs · 47,019 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD CARGO DOOR CUTOUT FRAME CRACKED AT BS 440, STR 23R. REPAIRED FRAME PER SWA T1-653-044.

Part: SLAT — CRACKED (LH WING) · airframe 48,050 hrs · 47,019 cycles

DURING SCHEDULED 1/2D CHECK, FOUND # 1 L/E SLAT CRACKED AT MID AUX TRACK CUTOUT. R&R SLAT PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,050 hrs · 47,019 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD CARGO DOOR CUTOUT FRAME CRACKED AT BS 492, STR 23R. REPAIRED FRAME PER SWA T1-653-044.

Part: BEAM — CRACKED (CABIN FLOOR) · airframe 48,050 hrs · 47,019 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOOR BEAM CRACKED AT BS 947, LBL 56. REPAIRED FLOOR BEAM PER SRM.

Part: BEAM — CORRODED (AFT CARGO) · airframe 48,050 hrs · 47,019 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOOR BEAMS CORRODED AT BS 727E & BS 772, LBL 12. REPAIRED FLOOR BEAM PER SWA RA.

Part: WEB — CRACKED (FUSELAGE) · airframe 48,050 hrs · 47,019 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD BULKHEAD WEB CRACKED AT BS 1016, STR 2R. REPAIRED WEB PER SRM.

Part: SLAT — CRACKED (RH WING) · airframe 48,050 hrs · 47,019 cycles

DURING SCHEDULED 1/2D CHECK, FOUND # 6 SLAT LOWER SKIN CRACKED INBD OF ACTUATOR. REPAIRED SLAT PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 48,050 hrs · 47,019 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FLOORBEAM AT BS 987, LBL 17 TO LBL 44.5. REPAIRED FLOORBEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 48,050 hrs · 47,019 cycles

DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIES CORRODED AT BS 827 BETWEEN STR 27R & STR 27L. REPAIRED SHEAR TIES PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,050 hrs · 47,019 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 500C & BS 500D, STR 25R. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 48,050 hrs · 47,019 cycles

DURING SCHEDULED 1/2D CHECK, FOUND VERTICAL BEAM WEB CRACKED .50 LONG AT BS 185, RBL 17.1 & WL 227. R&R VERTICAL BEAM WEB PER SRM.

Part: WEB — CRACKED (MAIN WHEEL WELL) · airframe 48,050 hrs · 47,019 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BEADED WEB CRACKED AT BS 663, LBL 32. REPAIRED WEB PER SWA T1-353-046.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 48,050 hrs · 47,019 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIPS CORRODED AT STR 26R, BS 727E, BS 767 & BS 787. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: LENS — MISSING (CABIN) · airframe 47,542 hrs · 46,601 cycles

OVER HEAD BIN BULL NOSE EMERGENCY EXIT LENS MISSING AT ROW 20 DEF. REPLACED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,206 hrs · 46,329 cycles

DURING SCHEDULED BC4 CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT INOP. REPAIRED EGRESS LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,740 hrs · 45,919 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,599 hrs · 45,792 cycles

DURING WALK AROUND INSPECTION, FOUND 3 EXTERNAL FUSELAGE SKIN CRACK AT BS 760, BELOW STR 19R. REPAIRED SKIN PER SRM.

Part: COVER — CRACKED (CABIN FLOOR) · airframe 46,199 hrs · 45,453 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK COVERS CRACKED AT ROW 1 & AT AFT GALLEY. REMOVED AND REPLACED TRACK COVERS PER MM.

Part: SCREW — MISSING (ESCAPE SLIDE) · airframe 46,174 hrs · 45,428 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE ASSY MISSING SCREW. INSTALLED SCREW INBOARD SIDE PER MM.

Part: SLAT — CRACKED (LT WING SLAT) · airframe 45,253 hrs · 44,666 cycles

DURING SCHEDULED C2 CHECK, FOUND NR 1 SLAT LOWER SKIN CRACKED 6 AFT OF ANTI-ICE DUCT. REPAIRED SLAT PER T1-657-012.

Part: STIFFENER — CRACKED (MLG WW) · airframe 42,224 hrs · 44,637 cycles

MX FERRY TO DAL, MLG WHEEL WELL VERTICAL STIFFENER CRACKED. REMOVED AND REPLACED STIFFENER PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 45,133 hrs · 44,562 cycles

DURING SCHEDULED SPECIAL VISIT AT DALFORT, FOUND 19 CRACKS AT BS 178 BULKHEAD, LBL 26 - RBL 15. REPAIRED BULKHEAD PER SRM & XEA X2-53-283.

Part: FRAME — CRACKED (BULKHEAD) · airframe 45,133 hrs · 44,562 cycles

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

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 45,133 hrs · 44,562 cycles

DURING SCHEDULED SPECIAL VISIT AT DALFORT, FOUND BS 178 BULKHEAD WEB CRACKED AT WL 188.5, LBL 75 & RBL 75, WL 205, RBL 26. REPAIRED BULKHEAD WEB PER SRM.

Part: FRAME — CRACKED (BULKHEAD) · airframe 45,133 hrs · 44,562 cycles

DURING SCHEDULED SPECIAL VISIT AT DALFORT, FOUND BS 178 BULKHEAD VERTICAL CHORD CRACKED AT LBL 5.7, WL 184.5. REPAIRED CHORD PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,133 hrs · 44,562 cycles

DURING SCHEDULED SPECIAL VISIT AT DALFORT, FOUND BS 178 RT SIDE CHORD CRACKED AT WL 207. REPAIRED RT SIDE CHORD PER ACO7342-53.

Part: SPOILER MIXER — BINDING (MLG WW)

AILERON STIFF AND FEELS BINDING WHEN MAKING LEFT ROLL. REMOVED AND REPLACED SPOILER MIXER, RATIO CHANGER AND AILERON BUS DRUM BEARING PER MM. OPS CHECK GOOD.

Part: SENSOR — MALFUNCTIONED (RT MLG)

AIR TURNBACK, LANDING GEAR WOULD NOT RETRACT DURING TAKEOFF. HANDLE WOULD NOT MOVE ABOVE OFF POSITON. ADJUSTED MAIN GEAR SAFETY SENSOR AND PERFORMED GEAR SWING CHECK PER MM.

Part: LIGHT — LOOSE (CABIN)

DURING SCHEDULED C1 CHECK, FOUND EMERGENCY ESCAPE FLOOR TRACK LIGHT LOOSE NEXT TO AFT GALLEY. RESECURED TRACK LIGHT PER MM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND 4 CRACKS AT BS 178 BULKHEAD BETWEEN LBL12.5-RBL 9.5. REPAIRED BULKHEAD PER SRM.

Part: BULKHEAD — CRACKED (BS 1016)

DURING SCHEDULED SC CHECK, FOUND BS 1016 BULKHEAD CRACKED NEAR S6L. REPAIRED PER SWA RA 1-353-2005.

Part: LAMP — FAILED (ROW 22)

DURING SCHEDULED SC CHECK, FOUND ROW 22 BULLNOSE EMERG LIGHT INOP. RELAMPED PER BOEING M/M.

Part: INTERCOSTAL — CRACKED (CARGO DOORWAY)

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

Part: FIRE WARNING — MALFUNCTIONED (APU)

ON DESCENT, AFTER STARTING APU, CREW RECIEVED FIRE WARNING. CREW COMPLIED WITH CHECKLIST AND EXPENDED BOTH FIRE BOTTLES. INSPECTED AND FOUND NO EVIDENCE OF FIRE OR OVERHEAT CONDTION. REMOVED AND REPLACED APU TAILPIPE MUFFLER, AND FIRE EXTINGUISHER BOTTLES PER BOEING M/M.

Part: SKIN — CRACKED (GALLEY DOORWAY)

DURING SCHEDULED A CHECK, FOUND FWD GALLEY DOOR SKIN CUTOUT CRACKED 3.2. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 516-520)

DURING SCHEDULED A CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 516 TO 520, AT S12L. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 942)

DURING SCHEDULED A CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 942, AT S24L. REPAIRED PER BOEING SRM.

Part: RIB — CRACKED (RT HORIZ STAB)

DURING SCHEDULED D-CHECK, FOUND RT HORZ STAB L/E RIBS NR 1, 3, 4, 5, 6 AND 7 CRACKED. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 814)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE DENTED AT BS 814, LBL 7, WL 146, AT S28L. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 PRESSURE WEB CRACKED 2 PLACES AT WL 201, LBL 4.7, AND AT WL 198, LBL 4.7. REPAIRED PER TRAMCO EWO 96-0621.

Part: FRAME — CRACKED (GALLEY DOOR)

DURING SCHEDULED D-CHECK, FWD GALLEY DOOR AFT SIDE FRAME CRACKED AT NR 4 STOP FITTING CUTOUT. REPLACED PER BOEING SRM.

Part: SUPPORT — CRACKED (BS 540)

DURING SCHEDULED D-CHECK, FOUND CRACKED FLOOR SUPPORT AT BS 540, RBL 2, WL 208. REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 296)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 296, RBL 54, WL 209. REPAIRED PER BOEING SRM.

Part: CLIP — BROKEN (BS 616/663/639)

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS BROKEN AT BS 616, S1, 2L, 4L, AT BS 663, S10R, S10L, AND AT BS 639, S1, 2R, AND S2L. REPLACED PER BOEING SR.

Part: FLOORBEAM — CORRODED (BS 727-947.5)

DURING SCHEDULED D-CHECK, FOUND AFT CARGO BAY FLOOR BEAM CORRODED FROM 727-947.5, RBL 13.8, WL 155.5. REPLACED DAMAGED SECTION PER BOEING SRM.

Part: SKIN — DENTED (BS 390-398)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE DENTED BETWEEN BS 390 AND 398, BETWEEN S24 AND 25R. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 PRESSURE WEB CRACKED 2 PLACES AT WL 201, RBL 4.7, AND AT WL 198, RBL 4.7. REPAIRED PER TRAMCO EWO 96-0621.

Part: SKIN — DENTED (BS 1000)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 1000, UNDER S14L. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 415)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE DENTED AT BS 415, BETWEEN S24 AND 26R. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 986.5)

DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORRODED AT BS 986.5, RBL 26, RBL 4-5, AND AT LBL 3-5, WL 208. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 616)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, RBL 64, WL 202. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 PRESSURE WEB CRACKED AT WL 219, RBL 10.7. REPAIRED PER TRAMCO EWO 96-0621.

Part: FRAME — DAMAGED (BS 500)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (SERV DOORWAY)

DURING SCHEDULED D-CHECK, FWD SERVICE DOOR FRAME CUT-OUT WEB CRACKED. REPLACED DAMAGED SECTION PER BOEING SRM.

Part: CHORD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 SIDE CHORD CRACKED 1 INCH LT SIDE AT APPROXIMATELY WL 195. CUT OUT DAMAGED SECTION AND REPLACED PER BOEING SRM.

Part: SKIN — GOUGED (BS 360)

DURING SCHEDULED TC CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 360, BETWEEN S5L AND S6L. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 887/500)

DURING SCHEDULED TC CHECK, FOUND FUSELAGE SKIN DENTED AT BS 887 BETWEEN S16 AND 17L, BS 500 S22 TO 23L. REPAIRED PER BOEING SRM.

Part: SKIN — LIGHTNING STRIKE (L1 DOOR CUTOUT)

DURING SCHEDULED TC CHECK, FOUND FUSELAGE SKIN DAMAGED FROM LIGHTNING STRIKE AT BS LOWER CORNER L1 DOOR CUTOUT. REPAIRED PER BOEING SRM.

Part: SKIN — LIGHTNING STRIKE (BS 480)

DURING SCHEDULED BC2 CHECK, FOUND FUSELAGE SKIN DAMAGED FROM LIGHTNING STRIKE AT BS 480 BELOW S18L. REPAIRED PER BOEING SRM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK AND CHARGER HOUSING PER BOEING M/M.

Part: STRAP — CRACKED (E/E COMP)

DURING SCHEDULED B/C1 CHECK, FOUND FLOOR BEAM SUPPORT STRAP CRACKED AT RBL 31 IN E AND E COMPARTMENT. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.