N347SW

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,830 hrs · 66,498 cycles

FUSELAGE SKIN CRACK EMITTING FROM UNDER STR 4R LAP MOD AT STA 908. REPAIRED DAMAGE PER EA 1-353-21296.

Part: BATTERY — DISCHARGED (CABIN) · airframe 75,600 hrs · 66,327 cycles

EMERGENCY LIGHTS INOP AT OUTSIDE AFT SERVICE DOOR AND OVERHEAD LIGHT AT AFT ENTRY DOOR. REMOVED AND REPLACED BATTERY AT M1134 EMERGENCY LIGHT CHARGING MODULE OPS CHECK GOOD PER MM.

Part: LENS — LOOSE (CABIN) · airframe 75,590 hrs · 66,320 cycles

ROW 6 ABC STORAGE BIN EMERGENCY EXIT LENS UNSECURED. OK TO CONTINUE PER MEL 33-15-01 SP#1 TRACKING#77654. SECURED LENS OPS CHECK GOOD PER MM CL#77749.

Part: SPOILER — BROKEN (LT WING) · airframe 75,344 hrs · 66,136 cycles

LEFT WING GROUND SPOILER OUTBOARD ACTUATOR ATTACH POINT BROKEN. REMOVED AND REPLACED NR 4 GROUND SPOILER PER AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,242 hrs · 66,057 cycles

FUSELAGE SKIN CRACKED AT STA 513, BELOW STR 8L. REPAIRED SKIN PER EA.

Part: SKIN — DELAMINATED (NR 1 SPOILER) · airframe 74,962 hrs · 65,858 cycles

LEFT WING NR 1 GROUND SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED NR 1 SPOILER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,910 hrs · 65,816 cycles

SKIN CRACKED AT BS 440 + 4, STR 1. REPAIRED SKIN PER EA.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 73,120 hrs · 64,451 cycles

LEFT KEEL BEAM LOWER CHORD BS 673 TO 727 CORRODED. REPAIRED CHORD IAW EA.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 73,120 hrs · 64,451 cycles

RT KEEL BEAM LOWER CHORD STA 673 TO 727 CORRODED ON LOWER SURFACE. REPAIRED CHORD IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,118 hrs · 64,450 cycles

DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT BULB INOP. INSTALLED BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,118 hrs · 64,450 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT BULBS INOP. REMOVED AND REPLACED BULB PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,951 hrs · 65,125 cycles

DURING SCHEDULED SPV CHECK, FOUND LT INNER CHORD FRAME CRACKED AT BS 639, BETWEEN STR 14L TO STR 15L. REPAIRED FRAME PER EA.

Part: HOOK — OUT OF ADJUST (R1 DOOR) · airframe 71,653 hrs · 63,312 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,525 hrs · 63,216 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 376, STR 8L. REPAIRED SKIN PER ER AND ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,522 hrs · 63,215 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 376, STR 8L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 70,815 hrs · 62,668 cycles

R2 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: FRAME — CORRODED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CHORD CORRODED AT BS 277.8, BETWEEN RBL 16 TO LBL 16. REPAIRED FRAME PER EO.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 242 CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 360 TO BS 380, STR 17L. REMOVED AND REPLACED WEB PER SRM.

Part: TERMINAL — CONTAMINATED (COCKPIT) · airframe 70,600 hrs · 62,511 cycles

DIVERSION / DECLARED EMERGENCY. SMOKE AND FUMES FROM R1 WINDOW UPPER RIGHT ENTERED COCKPIT DURING CRUISE AT 36,000FT. REMOVED DEBRIS FROM TOP RIGHT WINDOW HEAT TERMINAL PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 990.3, STR 7L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 951, STR 11L. REPAIRED SKIN PER EO AND EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CORRODED AT BS 500, BETWEEN STR 28L TO STR 28R. REPAIRED FRAME PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 1006, STR 6L. REPAIRED SKIN PER EO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CORRODED AT BS 947.5, BETWEEN STR 25R TO STR 24R. REPAIRED FRAME PER EO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, BL 0. REPAIRED WEB PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CORRODED AT BS 807, STR 25L. REPAIRED FRAME PER EO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CORRODED AT BS 807, BETWEEN STR 25L TO STR 26L. REPAIRED FRAME PER EO.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING NR 5 SLAT DELAMINATED ON EXTERNAL SKIN LOWER SUFRACE O/B EDGE. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING T/E WEDGE AT I/B MID FLAP DELAMINATED. REMOVED AND REPLACED MID FLAP PER MM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING I/B FORE FLAP UPPER SKIN DELAMINATED. REPAIRED FORE FLAP PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 947.5, STR 26R. REPAIRED FRAME PER EO.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 706, BETWEEN RBL 45.5 TO RBL 64. REPAIRED BEAM PER EO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, BL 0. REPAIRED WEB PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 344, BETWEEN STR 22L TO STR 23L. REPAIRED FRAME PER EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 312 TO BS 323.7, STR 28R. REMOVED AND REPLACED STRINGER PER EO.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 540, STR 10R. REMOVED AND REPLACED SPLICE PER SRM.

Part: BATTERY — LOW (CABIN) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT OVERHEAD EMERGENCY EXIT LIGHT BATTERY CHARGER LOW AT BS 616. REMOVED AND REPLACED BATTERY PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 18R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CRACKED AT BS 597, STR 10R. REMOVED AND REPLACED STRINGER PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO CHANNEL CORRODED AT BS 860, RBL 8.10. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO CHANNEL CORRODED AT BS 732D, LBL 8.10. REPAIRED CHANNEL PER EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, RT WING NR 6 SLAT SKIN CRACKED AT OUTBOARD EDGE. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING NR 5 SLAT SKIN I/B EDGE DELAMINATED. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 26R. REMOVED AND REPLACED CLIP PER BAC DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 860, RBL 3.0. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 846, LBL 3.0. REPAIRED CHANNEL PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 277, STR 16L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND CRACK ON DOOR CUTOUT STRUCTURE STA 294.5, STR 7R. REPAIRED FRAME PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 730E, LBL 12.50. REPAIRED CHANNEL PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 26L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND UPPER CHORD OF FLOORBEAM AT STA 727B, LBL 24.8 CENTER CABIN FLOOR STRUCTURE CRACKED. REPAIRED BEAM PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 754, LBL 8.10. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 730E, RBL 8.10. REPAIRED CHANNEL PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947.5, STR 27L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING T/E NR 3 SLAT LOWER SKIN DELAMINATED. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 9L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 9L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 20R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 20L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 312, BETWEEN BL 0 TO RBL 24.5. REPAIRED BEAM PER SRM.

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND CROSS BEAM CRACKED AT BS 294.5, LBL 53.5. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 28R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22YCHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 25R. REMOVED AND REPLACED CLIP PER SRM.

Part: LENS — BROKEN (CABIN) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND FWD LAV EMERGENCY EXIT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND WEB CRACKED BETWEEN BS 277 TO BS 294.5, STR 9R. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: FLAP — DELAMINATED (LT WING) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND DELAMINATION LT WING OUTBOARD AFT FLAP INBOARD END. REPAIRED FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 26L. REMOVED AND REPLACED CLIP PER SRM & BAC DRAWING.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 27L. REMOVED AND REPLACED CLIP PER SRM & BAC DRAWING.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND FWD EMERGENCY FLASHLIGHT BASE ASSY BROKEN. REMOVED AND REPLACED BASE ASSY PER MM.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND FWD EMERGENCY FLASHLIGHT STRAP BROKEN. REMOVED AND REPLACED STRAP PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 21L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 1016, RBL 36. REPAIRED BEAM PER EA.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT AFT FLASHLIGHT STRAP BROKEN. REMOVED AND REPLACED STRAP PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 25L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 26L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,588 hrs · 62,503 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SKIN — CRACKED (L1 DOOR) · airframe 69,835 hrs · 61,938 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND L1 DOOR CRACKED ON INNER SKIN. REMOVED AND REPLACED L1 DOOR PER MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 69,619 hrs · 61,772 cycles

DURING SCHEDULED OTS CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING LOOSE. SECURED FITTING PER MM.

Part: CONNECTOR — BROKEN (CABIN) · airframe 68,192 hrs · 60,664 cycles

DURING SCHEDULED SPV CHECK, FOUND LT OVERHEAD EMERGENCY EXIT LIGHT WIRE CONNECTOR BROKEN AT BS 727D, STR 9L. REMOVED AND REPLACED CONNECTOR PER SMPM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,192 hrs · 60,665 cycles

DURING SCHEDULED SPV CHECK, FOUND RT EGRESS LIGHT AFT OF WING INOP. RELAMPED LIGHT PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 68,192 hrs · 60,665 cycles

DURING SCHEDULED SPV CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM AND MT.

Part: CONNECTOR — BROKEN (CABIN) · airframe 68,192 hrs · 60,664 cycles

DURING SCHEDULED SPV CHECK, FOUND LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT WIRE BROKEN AT ROW 10. REMOVED AND REPLACED CONNECTOR PER SWPM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,192 hrs · 60,664 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 18L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,192 hrs · 60,664 cycles

DURING SCHEDULED SPV1 CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 24L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 68,192 hrs · 60,664 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CORRODED AT BS 967, STR 25L. REMOVED AND REPLACED SKIN DOUBLER PER DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,192 hrs · 60,664 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,192 hrs · 60,664 cycles

DURING SCHEDULED SPV CHECK, FOUND STUB FRAME CRACKED AT BS 792.5, BETWEEN STR 19L TO STR 20L. REMOVED AND REPLACED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,192 hrs · 60,664 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,192 hrs · 60,664 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 3L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,192 hrs · 60,664 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 1L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,192 hrs · 60,664 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,192 hrs · 60,664 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,192 hrs · 60,664 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,192 hrs · 60,664 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,192 hrs · 60,664 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,192 hrs · 60,664 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,192 hrs · 60,664 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,192 hrs · 60,664 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,192 hrs · 60,664 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,192 hrs · 60,664 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,192 hrs · 60,664 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,192 hrs · 60,664 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,192 hrs · 60,664 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 4R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,192 hrs · 60,664 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 4R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,192 hrs · 60,664 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,718 hrs · 60,304 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 747, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,718 hrs · 60,304 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 757, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,718 hrs · 60,304 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 977, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,718 hrs · 60,304 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 757, STR 19L. REPAIRED SKIN PER SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 67,310 hrs · 60,008 cycles

DURING SCHEDULED OTS CHECK, FOUND PRESSURE DECK WEB CRACKED AT BS 664, LBL 26.97. REPAIRED WEB PER EA.

Part: CONTROL PANEL — FAULTY (CABIN PRESSURE) · airframe 67,310 hrs · 60,008 cycles

DURING FERRY FLIGHT TO DALLAS, PILOT REPORTED THAT DURING CABIN PRESSURE STARTED TO CLIMB. SWITCHED TO MANUAL DC AND ATTEMPTED TO CLOSE OUTFLOW VALVE. VALVE WENT TO FULL CLOSE UNCOMMANDED BUMPED SWITCH TO OPEN AND VALVE DROVE FULL OPEN. ALL O2 MASKS DROPPED. REMOVED AND REPLACED PRESS CONTROL PANEL PER MM.

Part: SLIDE — OUT OF POSITION (RT DOOR) · airframe 66,670 hrs · 59,505 cycles

RT DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,444 hrs · 59,341 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 16L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 65,658 hrs · 58,783 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 SLAT SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 65,658 hrs · 58,783 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 3 SLAT SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 65,658 hrs · 58,783 cycles

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

Part: SKIN — CRACKED (LT WING) · airframe 65,658 hrs · 58,783 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 1 SLAT SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 65,418 hrs · 58,622 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD CARGO COMPARTMENT Z-ANGLE CRACKED AT BS 482, STR 26R. REMOVED AND REPLACED Z-ANGLE PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 65,418 hrs · 58,622 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD CARGO COMPARTMENT Z-ANGLE CRACKED AT BS 472, STR 25R. REMOVED AND REPLACED Z-ANGLE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,418 hrs · 58,622 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT, BS 304, WL 257. REPAIRED SKIN PER AAR EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 65,418 hrs · 58,622 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 380, AT STR 16R. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,418 hrs · 58,622 cycles

DURING SCHEDULED 20Y CHECK, FOUND RADIO ALTIMETER FUSELAGE SKIN CUTOUT CRACKED AT BS 450. REPAIRED SKIN PER AAR EA.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 65,418 hrs · 58,622 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT KEEL BEAM CORRODED AT BS 500D, BETWEEN LBL 8 TO LBL 10. REMOVED AND REPLACED BEAM PER SRM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 65,418 hrs · 58,622 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE BEAR STRAP SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, BS 305, BETWEEN WL 236 TO WL 239. REPAIRED SKIN PER SRM.

Part: RIB — CRACKED (HORIZ STAB) · airframe 65,418 hrs · 58,622 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT HORIZONTAL STABILIZER L/E 5TH RIB I/B CRACKED. REMOVED AND REPLACED RIB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,418 hrs · 58,622 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, BETWEEN BS 303 TO BS 305, WL 236 TO WL 240. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,418 hrs · 58,622 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, BS 303, WL 236. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,418 hrs · 58,622 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT, BS 294, BETWEEN WL 229 TO WL 233. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 65,418 hrs · 58,622 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 28L. REPAIRED SHEAR TIE PER SRM.

Part: COVER — CRACKED (CABIN) · airframe 65,418 hrs · 58,622 cycles

DURING SCHEDULED 20Y CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT COVER CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,418 hrs · 58,622 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 22R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 65,418 hrs · 58,622 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 732, RBL 3. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,418 hrs · 58,622 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 656+16, LBL 25.5. REPAIRED BEAM PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,418 hrs · 58,622 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 23R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: RIB — CRACKED (MIDFLAP) · airframe 65,418 hrs · 58,622 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING T/E OUTBOARD MID FLAP SUPPORT RIB CRACKED. REMOVED AND REPLACED RIB PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 65,418 hrs · 58,622 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 520, RBL 10 TO RBL 20. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,418 hrs · 58,622 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 16L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,418 hrs · 58,622 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, BETWEEN STR 24L TO STR 25L. REPAIRED SKIN PER SRM.

Part: RIB — CRACKED (HORIZ STAB) · airframe 65,418 hrs · 58,622 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT HORIZONTAL STABILIZER I/B LEADING EDGE RIB CRACKED. REMOVED AND REPLACED RIB PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,418 hrs · 58,622 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, BETWEEN LBL 1 TO LBL 4. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,418 hrs · 58,622 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 967, BETWEEN STR 27R TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,418 hrs · 58,622 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 867, BETWEEN STR 27R TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,418 hrs · 58,622 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 19L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,418 hrs · 58,622 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 25R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,418 hrs · 58,622 cycles

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

Part: WINDOW — ARCED (COCKPIT) · airframe 65,071 hrs · 58,381 cycles

EN ROUTE MDW-SDF L2 SLIDING WINDOW ARCED. REMOVED AND REPLACED L2 WINDOW PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,122 hrs · 57,670 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT STA 410, STR 1. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,122 hrs · 57,670 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SERVICE DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,931 hrs · 57,520 cycles

DURING SCHEDULED SPV CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,038 hrs · 56,873 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 771, STR 18L. REPAIRED SKIN PER SRM.

Part: LENS — CRACKED (CABIN) · airframe 62,446 hrs · 56,455 cycles

R2 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: SKIN — CRACKED (BS 779-792 S18L) · airframe 60,945 hrs · 55,301 cycles

DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 779 AND BS 792, STR 18L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 60,507 hrs · 54,975 cycles

DURING SCHEDULED MV2 CHECK, FOUND RIGHT FWD FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,507 hrs · 54,975 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 505C, STR 15L. REPAIRED SKIN PER SWA EA.

Part: FITTING — CORRODED (LT WING) · airframe 58,884 hrs · 53,658 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT MLG SUPPORT BEAM FWD STABILIZER FITTING CORRODED. REMOVED AND REPLACED STABILIZER FITTING PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 58,884 hrs · 53,658 cycles

DURING SCHEDULED 18Y CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 947, LBL 53. REMOVED AND REPLACED UPPER CHORD PER ER.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 58,884 hrs · 53,658 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,884 hrs · 53,658 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 3R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 787 S8L) · airframe 58,884 hrs · 53,658 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787. STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: CREASE BEAM — CORRODED (BS 400-420 S17R) · airframe 58,884 hrs · 53,658 cycles

DURING SCHEDULED 18Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 400 TO BS 420 STR 17R. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: CONNECTOR — CORRODED (EMERGENCY LIGHT) · airframe 58,884 hrs · 53,658 cycles

DURING SCHEDULED 18Y CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT ASSY CONNECTOR CORRODED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FITTING — CORRODED (LT MLG SUPPORT) · airframe 58,884 hrs · 53,658 cycles

DURING SCHEDULED 18Y CHECK, FOUND LEFT MLG SUPPORT BEAM AFT STAB FITTING CORRODED. REMOVED AND REPLACED AFT STAB FITTING PER MM.

Part: STRINGER CLIP — CRACKED (BS 388 S2L) · airframe 58,884 hrs · 53,658 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 2L. REMOVED AND REPLACED RT STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,884 hrs · 53,658 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 1050, STR 25L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,884 hrs · 53,658 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 390, BL 0, RADIO ALTIMETER ANTENNA CUTOUT. REPAIRED SKIN PER ER.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 58,884 hrs · 53,658 cycles

DURING SCHEDULED 18Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 45 TO LBL 27. REPAIRED FLOORBEAM PER SRM.

Part: PLATE — CORRODED (R1 DOOR SLIDE) · airframe 58,884 hrs · 53,658 cycles

DURING SCHEDULED 18Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FLOOR ATTACH PLATE CORRODED. REMOVED AND REPLACED ATTACH PLATE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,884 hrs · 53,658 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,884 hrs · 53,658 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,884 hrs · 53,658 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME SECTION PER SWA EA.

Part: SKIN — DELAMINATED (L/E SLAT) · airframe 58,884 hrs · 53,658 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT WING NR 3 L/E SLAT UPPER SURFACE DELAMINATED. REPAIRED SLAT PER SRM.

Part: FRAME — CRACKED (BS 380 S8R) · airframe 58,884 hrs · 53,658 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 559 S11R) · airframe 58,884 hrs · 53,658 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 520 S8R) · airframe 58,884 hrs · 53,658 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 500A S8L) · airframe 58,884 hrs · 53,658 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 400 S9R) · airframe 58,884 hrs · 53,658 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 578 S11R) · airframe 58,884 hrs · 53,658 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: CARRIAGE — CORRODED (RT WING TE FLAP) · airframe 58,884 hrs · 53,658 cycles

DURING SCHEDULED 18Y CHECK, FOUND RIGHT WING INBOARD MID FLAP OUTBOARD CARRIAGE CORRODED. REMOVED AND REPLACED FLAP CARRIAGE PER MM.

Part: STRINGER CLIP — CRACKED (BS 616 S5L) · airframe 58,884 hrs · 53,658 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: TORQUE TUBE — CORRODED (RT WING TE FLAP) · airframe 58,884 hrs · 53,658 cycles

DURING SCHEDULED 18Y CHECK, FOUND RIGHT WING INBOARD MID FLAP OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: SKIN — CRACKED (BS 500D S13L) · airframe 58,526 hrs · 53,374 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 13L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 500D S16L) · airframe 58,526 hrs · 53,374 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (FORE FLAP) · airframe 58,526 hrs · 53,374 cycles

DURING SCHEDULED C4 CHECK, FOUND LEFT WING INBOARD FORE FLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED FORE FLAP PER MM.

Part: GIRT BAR — BROKEN (L1 DOOR) · airframe 57,960 hrs · 52,935 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING BROKEN. REMOVED AND REPLACED AFT GIRT BAR FITTING PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,595 hrs · 52,623 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SERVICE DOOR CUTOUT, BS 328, STR 17R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,595 hrs · 52,623 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 25L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,595 hrs · 52,623 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 730E, STR 19R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,595 hrs · 52,623 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 739E, STR 19R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 749) · airframe 57,024 hrs · 52,180 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 749, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 741) · airframe 57,024 hrs · 52,180 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 741, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 744) · airframe 57,024 hrs · 52,180 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 744, STR 19L. REPAIRED SKIN PER SRM.

Part: CABLE — MISROUTED (L2 DOOR SLIDE) · airframe 56,657 hrs · 51,899 cycles

DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED SLIDE CABLE PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,657 hrs · 51,899 cycles

DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: PANEL — CRACKED (NLG WW) · airframe 56,425 hrs · 51,725 cycles

DURING SCHEDULED SERVICE CHECK, FOUND NLG W/W CEILING PANEL CRACKED AFT OF LT BRAKE MOUNT, BS 251.62, LBL 7.75. MX FERRY TO DAL FOR REPAIRS. REPAIRED PANEL PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,395 hrs · 51,701 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SRM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 56,250 hrs · 51,602 cycles

BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 8 DEF. INSTALLED LENS PER MM.

Part: BRACKET — LOOSE (SIGN) · airframe 55,823 hrs · 51,300 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD GALLEY EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED ATTACH BRACKET PER MM.

Part: SKIN — CRACKED (BS 791) · airframe 55,008 hrs · 50,649 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 791, STR 17L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (BS 847) · airframe 55,008 hrs · 50,649 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT AFT CARGO DOOR CUT OUT BS 847, NR 5 STOP FITTING. REPAIRED FRAME BFG ER.

Part: SKIN — WORN (BS 882-887) · airframe 55,008 hrs · 50,649 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN WORN AT BS 882 TO BS 887, STR 1R TO STR 2R. REPAIRED SKIN PER BFG ER.

Part: FRAME — CRACKED (BS 495) · airframe 55,008 hrs · 50,649 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUT OUT BS 495, NR 1 STOP FITTING. REPAIRED FRAME BFG ER.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 55,004 hrs · 50,648 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND AFT CARGO DOOR AFT FRAME CRACKED AT NR 5 STOP FITTING CUTOUT. REPAIRED FRAME PER BFG ER.

Part: SKIN — CRACKED (BS 328) · airframe 54,850 hrs · 50,514 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 328, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 930) · airframe 54,845 hrs · 50,508 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 24L. REPAIRED SKIN PER SWA EA.

Part: CONTROL PANEL — FAULTY (GASPER FAN) · airframe 54,147 hrs · 49,920 cycles

SMOKE/ELECTRICAL ODOR BEHIND GASPER FAN SWITCH & A/C PANEL. REMOVED AND REPLACED P5-10 PANEL PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 53,884 hrs · 49,722 cycles

DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 53,884 hrs · 49,722 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: PCU — LEAKING (LT ELEVATOR) · airframe 52,163 hrs · 48,326 cycles

AIR TURNBACK, DECLARED EMERGENCY. A HYDRAULIC SYSTEM FAILURE AND FLUID LOSS IN FLIGHT. REMOVED AND REPLACED LT ELEVATOR PCU PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 51,946 hrs · 48,164 cycles

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

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 51,321 hrs · 47,672 cycles

DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT LENS, MISSING. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SKIN — DELAMINATED (RT WING SLAT) · airframe 50,274 hrs · 46,837 cycles

DURING SCHEDULED 1/2D CHECK, FOUND NR 4 L/E SLAT DELAMINATED. REPAIRED NR 4 L/E SLAT PER MM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 50,265 hrs · 46,827 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT MLG WHEEL WELL CEILING BEADED PRESSURE WEB AT BS 671, RBL 41, CRACKED. REPAIRED RT MLG PRESSURE WEB PER SRM.

Part: STIFFENER — CORRODED (BULKHEAD) · airframe 50,265 hrs · 46,827 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BULKHEAD STIFFENER AT BS 1016, BL 0, CORRODED. REMOVED AND REPLACED BULKHEAD STIFFENER PER ACO.

Part: GLOWSTRIP — WORN (CABIN) · airframe 50,265 hrs · 46,827 cycles

DURING SCHEDULED 1/2D CHECK, FOUND PHOTOLUMINESCENT STRIP BETWEEN BS 336 AND BS 948, WORN. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER ACO.

Part: FITTING — CORRODED (L2/R1 DOORS) · airframe 50,265 hrs · 46,827 cycles

DURING SCHEDULED 1/2D CHECK, FOUND L2 AND R1 DOOR EVAC SLIDES FWD AND AFT GIRT BAR FITTINGS CORRODED. REMOVED AND REPLACED EVAC SLIDE GIRT BAR FITTINGS PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 50,254 hrs · 46,820 cycles

DURING SCHEDULED 1/2D CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT LENS AT ROW 10 ABC, MISSING. REPLACED LIGHT LENS PER MM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,253 hrs · 46,818 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT MLG VERTICAL ANGLE AT BS 695, STRINGER 18R, CRACKED. REMOVED AND REPLACED MLG ANGLE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 50,253 hrs · 46,818 cycles

DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE AT BS 965, STRINGER 6R, CRACKED. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,253 hrs · 46,818 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR FRAME CUTOUT AT LOWER STOP FITTING, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SKIN — DELAMINATED (LT WING SLAT) · airframe 50,253 hrs · 46,818 cycles

DURING SCHEDULED 1/2D CHECK, FOUND NR 2 L/E SLAT, OUTBOARD END DELAMINATED. REPAIRED NR 2 SLAT PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,253 hrs · 46,818 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 847, STRINGER 14R, CRACKED. REPAIRED SKIN PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,253 hrs · 46,818 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 1121, STRINGER 2L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 50,253 hrs · 46,818 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT HORIZONTAL STAB L/E RIB AT STAB STA 243, CRACKED. REMOVED AND REPLACED HORIZONTAL STAB RIB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,253 hrs · 46,818 cycles

DURING SCHEDULED 1/2D CHECK, FOUND L1 DOOR CUTOUT, LOWER HINGE, CRACKED. REPAIRED L1 DOOR CUTOUT PER SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 50,253 hrs · 46,818 cycles

DURING SCHEDULED 1/2D CHECK, FOUND NR 3 VHF ANTENNA SUPPORT STRUCTURE AT BS 727D TO BS 727E, BL 0, CORRODED. REMOVED AND REPLACED ZEE SUPPORT SECTION PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 50,253 hrs · 46,818 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM AT R1 DOOR BELOW THE SILL, CORRODED. REMOVED AND REPLACED CREASE BEAM PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 50,253 hrs · 46,818 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT CREASE BEAM AT BS 957 TO BS 986, CORRODED. REMOVED AND REPLACED BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,253 hrs · 46,818 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 360, ABOVE AND BELOW STRINGER 21L, CRACKED. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,253 hrs · 46,818 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 908, STRINGER 10L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 50,253 hrs · 46,818 cycles

DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE AT BS 520, STRINGER 11R, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 50,253 hrs · 46,818 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO COMPARTMENT VERTICAL BEAM FITTING AT BS 727, LBL 18, CRACKED. REMOVED AND REPLACED FITTING PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 50,253 hrs · 46,818 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM AT BS 294.5, RBL 45, CORRODED. REPAIRED CREASE BEAM PER SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 50,253 hrs · 46,818 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT MLG WHEEL WELL CEILING BEADED PRESSURE WEB AT BS 663 TO BS 672, LBL 32, CRACKED. REPAIRED PRESSURE WEB PER SRM.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 50,523 hrs · 46,818 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 50,253 hrs · 46,818 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BULKHEAD AT BS 294.5, STRINGER 11L, FIFTH STOP, CRACKED. REPAIRED BULKHEAD PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,253 hrs · 46,818 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM AT BS 947, RBL 10, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 50,253 hrs · 46,818 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIPS CRACKED AT BS 727D, STRINGER 23L AND STRINGER 25R, BS 500B, STRINGER 26R AND STRINGER 25L, BS 767, STRINGER 23L AND STRINGER 22L, BS 847, STRINGER 20L. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,167 hrs · 46,755 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 1050, STRINGER 25L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,167 hrs · 46,755 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 948, STRINGER 24L. REPAIRED SKIN PER SRM.

Part: TORQUE TUBE — WORN (LT ELEVATOR) · airframe 47,377 hrs · 44,512 cycles

DURING SCHEDULED C4 CHECK, SWA SI 11038, LT ELEVATOR TAB FAILED FREE PLAY CHECK. FOUND,PLAY AT ELEVATOR TORQUE TUBE ASSY BETWEEN LT ELEVATOR INPUT ROD ARM AND OUTER TUBE. REMOVED AND REPLACED ELEVATOR TORQUE TUBE PER MM.

Part: COFFEEMAKER — OVERHEATED (AFT GALLEY) · airframe 46,505 hrs · 43,820 cycles

OVERHEAT FUME ODOR AT AFT COFFEE MAKER. FOUND, AFT COFFEE MAKER OVERHEATED AND TRIPPED C/B. REMOVED AND REPLACED COFFEE MAKER PER MM.

Part: SLIDE — OUT OF ADJUST (SVC DOORS) · airframe 46,442 hrs · 43,770 cycles

DURING SCHEDULED C3 CHECK, FOUND BOTH FWD AND AFT SVC DOOR EMERGENCY EVAC SLIDES OUT OF ADJUST. ADJUSTED BOTH SLIDES PER MM.

Part: LENS — MISSING (CABIN) · airframe 46,442 hrs · 43,770 cycles

DURING SCHEDULED C3 CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY LIGHT LENS MISSING AT ROW NR 11 ABC. INSTALLED LENS PER MM.

Part: SLIDE — OUT OF POSITION (AFT SVC DOOR) · airframe 44,934 hrs · 42,556 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: FRAME — CRACKED (FWD SVC DOOR) · airframe 44,615 hrs · 42,288 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR FRAME CRACKED IN RADIUS BELOW UPPER HINGE CUT OUT. REPAIRED FRAME PER SWA EA.

Part: BRACKET — CRACKED (NLG W/W) · airframe 43,373 hrs · 41,255 cycles

DURING SCHEDULED A2 CHECK, FOUND NOSE GEAR ACTUATOR ATTACH BRACKET GUSSET CRACKED. REMOVED AND REPLACED BRACKET PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 50,685 hrs · 24,517 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED (3 EA) AT BS 178, WL 188 AND LBL 1.0, WL 201 AND LBL 5.0, WL 199 AND LBL 5.0. REPAIRED WEB PER SRM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 41,873 hrs · 40,025 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,716 hrs · 39,875 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED ON CAPTIAN'S # 1 WINDOW POST UPPER AFT CORNER. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,712 hrs · 39,870 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR AFT LWR FRAME CRACKED AT STOP FITTING. REPAIRED PER BAC DWG 69-69854.

Part: LENS — LOOSE (CABIN) · airframe 41,712 hrs · 39,870 cycles

DURING SCHEDULED 1/4D CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 11 ABC. R&R LENS PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 41,712 hrs · 39,870 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LH OVERWING EMER EXIT SIGN LOOSE. SECURED EXIT SIGN PER MM.

Part: LENS — LOOSE (CABIN) · airframe 41,712 hrs · 39,870 cycles

DURING SCHEDULED 1/4D CHECK, FOUND OVHD BIN EMER EXIT LT LENS ROW 8 DEF LOOSE. SECURED LENS PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 41,712 hrs · 39,870 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL WEB CRACKED AT BS 178, LBL 5 & WL199. REPAIRED WEB PER SRM.

Part: ROD END — WORN (AILERON) · airframe 41,712 hrs · 39,870 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT AILERON HINGES NR 1, 3 & 4 WORN. REMOVED AND REPLACED AILERON HINGE BUSHINGS AND ROD END ASSY'S PER SWA ACO 7197-27.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 41,712 hrs · 39,870 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIPS CRACKED (4 EACH) AT BS 827, STR 23L, 24L, 26L & 27L. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 41,712 hrs · 39,870 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 27L. R&R STR CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,080 hrs · 39,321 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT E&E EQUIPTMENT COOLING DUCT CUT-OUT AFT EDGE. REPAIRED SKIN PER SRM.

Part: HEATER — INOPERATIVE (OUTFLOW VALVE) · airframe 40,190 hrs · 38,585 cycles

DURING DESCENT, CABIN PRESS ERRATIC IN AUTO & STANDBY MODES. FOUND OUTFLOW VALVE HEATER INOP CAUSING OUTFLOW VALVE TO FREEZE. REMOVED AND REPLACED AFT HEATER AND OUTFLOW VALVE PER MM. PERFORMED PACK CONFIDENCE CHECK PER SWA SAM 728 & CABIN PRESS CONTROLLER TEST PER SWA SAM 729. OPS CHECK GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,153 hrs · 38,556 cycles

DURING SCHEDULED C4 CHECK, FOUND 2 LONG EXTERNAL FUSELAGE SKIN CRACK AT BS 727D, STR 18R. REPAIRED SKIN PER SRM.

Part: CONTROLLER — FAILED (COCKPIT) · airframe 39,622 hrs · 38,102 cycles

AIR TURNBACK, UNABLE TO CONTROL CABIN PRESSURE. REMOVED AND REPLACED CABIN PRESS CONTROLLER. PERFOMED TEST AND LEAK TEST, OPS CHECK GOOD PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 39,616 hrs · 38,097 cycles

AFT LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: STIFFENER — CRACKED (MLG W/W) · airframe 39,399 hrs · 37,922 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND RT VERTICAL STIFFENER CRACKED, BS 663. REMOVED AND REPLACED STIFFENER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,181 hrs · 37,739 cycles

DURING SCHEDULED C3 CHECK, FOUND 1 EXTERNAL FUSELAGE SKIN CRACK AT AFT SVC DOOR, UPPER AFT CUT OUT, BS 986.5. REPAIRED SKIN PER SRM.

Part: CAP — MISSING (CABIN) · airframe 39,181 hrs · 37,739 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS LOOSE & MISSING END CAP AT FWD SECTION. SECURED EEPLS & REPLACED END CAP PER MM.

Part: DOOR — OPEN (CARGO BAY) · airframe 37,586 hrs · 36,352 cycles

AIR TURNBACK. ACFT WOULD NOT PRESSURIZED AFTER TAKE-OFF. FOUND AFT CARGO DOOR PARTIALLY OPENED. OPERATED DOOR. OPS CHECK GOOD.

Part: WARNING SYSTEM — ACTIVATED (LE SLAT) · airframe 36,654 hrs · 35,563 cycles

ABORTED TAKEOFF, NR 4 L/E SLAT LIGHT ILLUMINATED AND WARNING HORN SOUNDED 30 KNOTS INTO THE TAKEOFF. REMOVED AND REPLACED TERMINAL ENDS AT GD142DC AND GD3316DC PER MM. OPS CK GOOD.

Part: SWITCH — OUT OF ADJ (COCKPIT)

ABORTED TAKEOFF, TAKEOFF WARNING HORN SOUNDED, ALL SETTINGS APPEARED NORMAL. ADJUSTED SPEED BRAKE MICROSWITCH PER MM.

Part: LIGHT — LOOSE (ROW 7)

EEPLS TRACK LOOSE AT ROW 7. SECURED LIGHT ASSY PER MM.

Part: LIGHT — LOOSE (ROW 7)

EEPLS LOOSE AT ROW 7. SECURED LIGHTS PER MM.

Part: LIGHT — BROKEN (ROW 20)

DURING SCHEDULED D-CHECK, FOUND EMERGENCY ESCAPE FLOOR TRACK LIGHT BROKEN AT ROW 20. REMOVED AND REPLACED TRACK SECTION PER MM.

Part: SPAR — CRACKED (WS 225)

DURING SCHEDULED D CHECK, FOUND CRACK ON THE LT WING REAR SPAR UPPER CHORD AT FASTENER HOLE, STA 225. REPAIRED SPAR PER ER 99-5310.

Part: RIB — CRACKED (WS 135.5)

DURING SCHEDULED D CHECK, FOUND CRACK ON THE RT WING RIB LOWER CHORD AT RADIUS, BETWEEN STRINGERS 2 AND 3, STA 135.5. REPAIRED RIB PER ER 99-5318.

Part: FRAME — CRACKED (BS 787,872, 867)

DURING SCHEDULED D CHECK, FOUND 3 EA FRAMES CRACKED BETWEEN STRINGERS 8R-9R, BS 787, BS 827, AND BS 867. REPAIRED FRAMES PER ER 99-5337.

Part: FRAME — CRACKED (BS 400 & 440)

DURING SCHEDULED D CHECK, FOUND 2 EA FRAMES CRACKED BETWEEN STRINGERS 8L-9L, BS 400, AND BS 440. REPAIRED FRAMES PER ER 99-5337.

Part: FRAME — CRACKED (BS 400, 440, 480)

DURING SCHEDULED D CHECK, FOUND 3 EA FRAMES CRACKED BETWEEN STRINGERS 8R-9R, BS 400, BS 440, AND BS 480. REPAIRED FRAMES PER ER 99-5337 AND SRM.

Part: FRAME — CRACKED (BS 787, 827, 867)

DURING SCHEDULED D CHECK, FOUND 3 EA FRAMES CRACKED BETWEEN STRINGERS 8L-9L, BS 787, BS 827, AND BS 867. REPAIRED FRAMES PER ER 99-5337.

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING SCHEDULED D CHECK, FOUND CORROSION AT FASTENER HOLE ON FLOORBEAM, BS 967, RBL 27. REPAIRED BEAM PER SRM.

Part: FRAME — CRACKED (BS 559)

DURING SCHEDULED D CHECK, FOUND BS 559, RT FRAME CRACKED AT RBL 65. REPAIRED FRAME PER SRM.

Part: STRINGER — CRACKED (BS 360)

DURING SCHEDULED D CHECK, FOUND CRACKED STRINGER AT BS 360, STR 14L. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (BS 360)

DURING SCHEDULED D CHECK, FOUND BS 360 FRAME CRACKED, BETWEEN STRINGERS 14R-15R. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (BS 328)

DURING SCHEDULED D CHECK, FOUND CORROSION ON UPPER CHORD OF FLOORBEAM, BS 328, RBL 57. REPAIRED BEAM PER SRM.

Part: CLIP — CRACKED (BS 277)

DURING SCHEDULED D CHECK, FOUND 3 EACH STRINGER CLIPS CRACKED AT BS 277, WL 254, 250, AND, 223 RT SIDE. REMOVED AND REPLACED CLIPS PER SRM.

Part: STRINGER — CRACKED (BS 907)

DURING SCHEDULED D CHECK, FOUND 2 EACH STRINGER SPLICES CRACKED AT BS 907, STRINGER 4L, AND STRINGER 4R. REPAIRED STRINGER PER SRM.

Part: FITTING — CORRODED (PAX DOORWAY)

DURING SCHEDULED D-CHECK, FOUND FORWARD ENTRY DOORWAY FWD GIRT BAR LATCH FITTING CORRODED. REMOVED AND REPLACED FITTING PER OHM.

Part: FLOORBEAM — CORRODED (BS 344)

DURING SCHEDULED D-CHECK, FOUND CORROSION ON BS 344 FLOORBEAM LBL 38, 31 AND 12 INSIDE CABIN. REPAIRED BEAM PER SRM.

Part: SKIN — CREASED (BS 299-333)

DURING SCHEDULED D-CHECK, FOUND A CREASE AT FUSELAGE SKIN, BS 299 TO 333, ABOVE STRINGER 23R. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D CHECK, FOUND 3 EA CRACKS AT BS 178 BULKHEAD, BETWEEN LBL 6.7 - RBL 6.7. REPAIRED BULKHEAD PER SRM.

Part: GRILLE — BROKEN (CARGO COMPT)

DURING SCHEDULED C2 CHECK, FOUND FWD CARGO AFT BULKHEAD BLOWOUT GRILLE BROKEN. REMOVED AND REPLACED PER BOEING MM.

Part: SKIN — GOUGE (BS 947)

DURING SCHEDULED C2 CHECK, FOUND GOUGE IN FUSELAGE SKIN AT BS 947L 1 FT BELOW DOOR CUTOUT AND AT BS 983L 2 FT. REPAIRED PER BOEING SRM.

Part: SKIN — GOUGE (BS 947)

DURING SCHEDULED C2 CHECK, FOUND GOUGE IN FUSELAGE SKIN AT BS 947L, 1 FT BELOW DOOR CUTOUT. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 727)

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, AT STR 24R \N\NREPAIRED PER BOEING SRM

Part: SLIDE — LOW PRESS (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND RIGHT AFT SERVICE DOOR SLIDE PRESSURE LOW. REPLACED SLIDE PER BOEING M/M.

Part: SKIN — GOUGED (BS 1031)

DURING SCHEDULED BC2 CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 1031 BELOW 20R. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (CARGO DOOR)

DURING SCHEDULED B/C1 CHECK, FOUND FWD CARGO DOOR FRAME CRACKED BELOW CEILING HOOK. REPAIRED PER SWA RA 1-A52-198.

Part: PANEL — CRACKED (NLG W/W)

DURING SCHEDULED MAINT CHECK, FOUND WHEEL WELL LOWER FIXED PANEL BELOW KEEL BEAM CRACKED 1 INCH ON RIGHT SIDE ACROSS FROM PREVIOUS REPAIR. REPAIRED PER BOEING SRM.

Part: OXYGEN MASKS — DEPLOYED (CABIN)

CABIN O2 MASKS DEPLOYED DURING CLIMBOUT. AIRCRAFT RETURNED TO LAS AND MADE AN UNEVENTFUL LANDING. REPACKED MASKS, REPLACED O2 GENERATORS, AND PRESSURIZATION CHECKED AIRCRAFT PER BOEING M/M.

Part: EEL SWITCH — INOP (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND AFT FLIGHT ATTENDANT PANEL EMERGENCY LIGHT SWITCH INOP. REPLACED SWITCH PER BOEING M/M.