N324SW

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,939 hrs · 65,241 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BETWEEN BS 375 TO BS 378, STR 15L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,811 hrs · 65,161 cycles

DURING SCHEDULED 22Y CHECK, FOUND R1 DOOR FUSELAGE SKIN CRACKED AT BS 290. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,813 hrs · 65,162 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,811 hrs · 65,161 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT BS 430, RADIO ALTIMETER CUTOUT OPENING. REPAIRED SKIN PER PAE ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,811 hrs · 65,161 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT BS 291. REPAIRED SKIN PER PAE ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,811 hrs · 65,161 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT BS 410, RADIO ALTIMETER CUTOUT OPENING. REPAIRED SKIN PER PAE ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,811 hrs · 65,161 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 20R. REPAIRED FRAME PER PAE ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,811 hrs · 65,161 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 179, RBL 5.7, WL 184. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,811 hrs · 65,161 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 305, WL 258. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,811 hrs · 65,161 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 305, WL 262. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,811 hrs · 65,161 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 305, WL 261. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,811 hrs · 65,161 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 303, WL 261. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,811 hrs · 65,161 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 303, WL 258. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,811 hrs · 65,161 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 304, WL 259. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 70,811 hrs · 65,161 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CRACKED AT BS 420, RBL 5. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,811 hrs · 65,161 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 302, WL 261. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,813 hrs · 65,162 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 680, STR 10R. REPAIRED SKIN PER SWA EA.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 70,811 hrs · 65,161 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT MAIN WHEEL WELL LOWER CHORD SKIN CRACKED AT BS 679. REMOVED AND REPLACED SKIN PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 70,811 hrs · 65,161 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING O/B FORE FLAP DELAMINATED. REPAIRED FLAP PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 70,811 hrs · 65,161 cycles

DURING SCHEDULED 22Y CHECK, FOUND BULKHEAD WEB CRACKED AT BS 1016, BETWEEN STR 5L TO STR 6L. REPAIRED WEB PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 70,811 hrs · 65,161 cycles

DURING SCHEDULED 22Y CHECK, FOUND BULKHEAD WEB CRACKED AT BS 1016, STR 5L. REPAIRED WEB PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 70,811 hrs · 65,161 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REPAIRED FLAP PER SRM.

Part: SLIDE — OUT OF ADJUST (EMERGENCY EXIT) · airframe 70,732 hrs · 65,107 cycles

DURING SCHEDULED SPV CHECK, FOUND L2 EMERGENCY EXIT SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,732 hrs · 65,107 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 731 TO BS 791 AT STR 14L. REPAIRED SKIN PER PAE ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 70,732 hrs · 65,107 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 727D, STR 14L TO STR 15L. REMOVED AND REPLACED TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 70,732 hrs · 65,107 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 727C, STR 14L TO STR 15L. REMOVED AND REPLACED TIE PER SRM.

Part: DRIVE UNIT — FAULTY (T/E FLAP) · airframe 70,447 hrs · 64,908 cycles

AIR TURNBACK, FLAPS STUCK AT 5 DEGREE ON CLIMBOUT OF OAK. REMOVED AND REPLACED HYDRAULIC FLAP DRIVE UNIT PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 68,759 hrs · 63,652 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 847, STR 27L. REPAIRED FRAME PER FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,759 hrs · 63,652 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 28R. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,757 hrs · 63,651 cycles

DURING SCHEDULED SPV CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,757 hrs · 63,651 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,757 hrs · 63,651 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,757 hrs · 63,651 cycles

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

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 68,757 hrs · 63,651 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,610 hrs · 63,542 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 943, STR 25R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,710 hrs · 62,855 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 372, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,710 hrs · 62,855 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 906, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 921 S24R) · airframe 67,312 hrs · 62,540 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 921, STR 24R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 739 S18L) · airframe 67,312 hrs · 62,540 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 739, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 740 S19R) · airframe 67,330 hrs · 62,554 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740, STR 19R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 740 S19R) · airframe 67,312 hrs · 62,540 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740, STR 19R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 804-813) · airframe 67,312 hrs · 62,540 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 804 AND BS 813, STR 19L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 500C S15R) · airframe 37,275 hrs · 62,503 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 15R. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,214 hrs · 62,457 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,214 hrs · 62,457 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,696 hrs · 60,500 cycles

RIGHT OVERWING EMERGENY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: STRINGER — CRACKED (BS 639 S16L) · airframe 64,281 hrs · 60,168 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER 16L CRACKED AT BS 639. REPAIRED STRINGER SECTION PER SRM.

Part: SKIN — CORRODED (BS 908-934 S26L) · airframe 64,281 hrs · 60,168 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 908 TO BS 934, STR 26L. REPAIRED SKIN PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 728 S23L) · airframe 64,281 hrs · 60,168 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 728, STR 23L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (BS 845) · airframe 64,281 hrs · 60,168 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 845, RBL 18. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 950-965) · airframe 64,281 hrs · 60,168 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 950 TO BS 965, STR 25L. REPAIRED SKIN PER BOEING DRAWING AND SRM.

Part: SKIN — CRACKED (BS 940 S20L) · airframe 64,281 hrs · 60,128 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 940, STR 20L. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CRACKED (BS 927 S22L) · airframe 64,281 hrs · 60,168 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 927, STR 22L. REMOVED AND REPLACED SHEAR TIE PER SWA EA.

Part: SKIN — CRACKED (BS 951 S25L) · airframe 64,281 hrs · 60,168 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 951, STR 25L. REPAIRED SKIN PER BOEING DRAWING AND SRM.

Part: KEELBEAM — CORRODED (BS 717-735) · airframe 64,281 hrs · 60,168 cycles

DURING SCHEDULED 20Y CHECK, FOUND KEEL BEAM CORRODED AT LT BS 717 TO BS 735. REMOVED AND REPLACED KEEL BEAM SECTION PER SRM.

Part: FRAME — CRACKED (BS 294 S2R) · airframe 64,281 hrs · 60,168 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 294.5, STR 2R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRUCTURE — CORRODED (AFT CARGO BAY) · airframe 64,281 hrs · 60,168 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE STRUCTURE CORRODED AT BS 727, LBL 4 TO LBL 6. REMOVED AND REPLACED STRUCTURE SECTION PER SRM.

Part: FRAME — CRACKED (BS 616) · airframe 64,281 hrs · 60,168 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, LBL 65, WL 201. REPAIRED FRAME SECTION PER TYPICAL REPAIR MANUAL.

Part: FRAME — CRACKED (BS 294 S17R) · airframe 64,281 hrs · 60,168 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 294.5, STR 17R. REPAIRED FRAME SECTION PER SRM.

Part: TAB — DELAMINATED (LT ELEVATOR) · airframe 64,281 hrs · 60,168 cycles

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

Part: BULKHEAD — CRACKED (BS 1016) · airframe 64,281 hrs · 60,168 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD DOME CAP CRACKED AT BS 1016, BL 0. REPAIRED BULKHEAD DOME CAP PER SRM.

Part: SHEAR TIE — CRACKED (BS 277 S10R) · airframe 64,281 hrs · 60,168 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CRACKED (BS 295 S10L) · airframe 64,281 hrs · 60,168 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER 10L CRACKED AT BS 295. REPAIRED STRINGER PER SRM.

Part: KEELBEAM — CORRODED (BS 733) · airframe 64,281 hrs · 60,168 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT KEELBEAM CORRODED AT BS 733. REPAIRED KEEL BEAM PER SRM.

Part: SHEAR TIE — CRACKED (BS 277 S12R) · airframe 64,281 hrs · 60,168 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 277, STR 12R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: VERTICAL BEAM — CRACKED (BS 180) · airframe 64,281 hrs · 60,168 cycles

DURING SCHEDULED 20Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 180, LBL 5.7, WL 177. REPAIRED WEB PER SRM.

Part: FLOORBEAM — CORRODED (BS 1016) · airframe 64,281 hrs · 60,168 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 1016, LBL 9 TO LBL 36. REPAIRED FLOORBEAM PER SRM.

Part: SHEAR TIE — CORRODED (BS 520 S27R) · airframe 64,281 hrs · 60,168 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 520, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: VERTICAL BEAM — CRACKED (BS 180) · airframe 64,281 hrs · 60,168 cycles

DURING SCHEDULED 20Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 180, RBL 5.7, WL 177. REPAIRED WEB PER SRM.

Part: SHEAR TIE — CRACKED (BS 277 S14R) · airframe 64,281 hrs · 60,168 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 277, STR 14R. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 500B S20R) · airframe 64,281 hrs · 60,168 cycles

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

Part: SKIN — CRACKED (BS 732B S14R) · airframe 64,281 hrs · 60,168 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 732B, STR 14R. REPAIRED SKIN PER SRM.

Part: KEELBEAM — CORRODED (BS 518C-520) · airframe 64,281 hrs · 60,168 cycles

DURING SCHEDULED 20Y CHECK, FOUND KEEL BEAM CORRODED AT RT BS 518C AND LT BS 520. REPAIRED KEEL BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (BS 294 S13L) · airframe 64,281 hrs · 60,168 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 13L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 440 S4R) · airframe 64,281 hrs · 60,168 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 277 S15R) · airframe 64,281 hrs · 60,168 cycles

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

Part: STRINGER CLIP — CRACKED (BS 727 S22R) · airframe 64,281 hrs · 60,168 cycles

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

Part: STRINGER CLIP — CRACKED (BS 787 S24R) · airframe 64,281 hrs · 60,168 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 24R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 400 S4L) · airframe 64,281 hrs · 60,168 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 663 S10L) · airframe 64,281 hrs · 60,168 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 663 S10R) · airframe 64,281 hrs · 60,168 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 277 S10R) · airframe 64,281 hrs · 60,168 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 440 S4L) · airframe 64,281 hrs · 60,168 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 277 S11R) · airframe 64,281 hrs · 60,168 cycles

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

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 64,281 hrs · 60,168 cycles

DURING SCHEDULED 20Y CHECK, FOUND VERTICAL BEAM STIFFENER CRACKED AT BS 178. RBL 17.1. REPAIRED STIFFENER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,281 hrs · 60,168 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 251, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 688) · airframe 63,668 hrs · 59,678 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 688, STR 10R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 702) · airframe 63,668 hrs · 59,678 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 702, STR 10R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 733E) · airframe 63,668 hrs · 59,678 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 733E, STR 19L. REPAIRED SKIN PER SWA EA.

Part: CASTING — BROKEN (NR 5 SPOILER) · airframe 63,466 hrs · 59,521 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT WING NR 5 GROUND SPOILER OUTBOARD ACTUATOR CASTING BROKEN. REPAIRED SPOILER CASTING PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 63,261 hrs · 59,359 cycles

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

Part: SKIN — CRACKED (BS 910 S21L) · airframe 62,709 hrs · 58,944 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 910, STR 21L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 933-951) · airframe 62,709 hrs · 58,944 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 933 TO BS 951, STR 21L TO STR 22L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 750 S18R) · airframe 62,709 hrs · 58,944 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 18R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 732E-734E) · airframe 62,709 hrs · 58,944 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 732E TO BS 734E, STR 19R TO STR 20R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 562) · airframe 62,709 hrs · 58,944 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 562, STR 10R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 761) · airframe 62,041 hrs · 58,408 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 761, STR 19R. REPAIRED SKIN PER SWA EA & SRM.

Part: BULB — INOPERATIVE (CABIN) · airframe 61,743 hrs · 58,165 cycles

DURING SCHEDULED A1 CHECK, FOUND RT MID CABIN EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SKIN — CRACKED (BS 814-815) · airframe 61,451 hrs · 57,920 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 814 TO BS 815.125, STR 18L. REPAIRED SKIN PER SWA EA AND SRM.

Part: CABLE — MISROUTED (R2 DOOR SLIDE) · airframe 61,188 hrs · 57,713 cycles

DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE ASSY MISROUTED. REROUTED CABLE ASSY PER MM.

Part: SKIN — CRACKED (BS 259) · airframe 61,188 hrs · 57,713 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 259, BETWEEN STR 22L TO STR 25L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 727B) · airframe 60,811 hrs · 57,401 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727B, STR 14L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 727D) · airframe 60,811 hrs · 57,401 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 19R. REPAIRED SKIN PER SRM.

Part: LIGHT — BROKEN (ROW 1ABC) · airframe 60,471 hrs · 57,117 cycles

FWD CABIN LEFT OVERHEAD BIN BULLNOSE LIGHT BROKEN AT ROW 1 ABC. REMOVED AND REPLACED LIGHT PER MM.

Part: FRAME — CRACKED (AFT CARGO DOOR) · airframe 60,289 hrs · 56,969 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT CARGO DOOR LOWER STOP FITTING CUTOUT CRACKED. REMOVED AND REPLACED AFT CARGO DOOR PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 60,289 hrs · 56,969 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD GALLEY EMERGENCY LIGHTS INOP. RELAMPED LIGHTS PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 60,150 hrs · 56,863 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,751 hrs · 56,548 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D + 12, STR 15L. REPAIRED SKIN PER SWA EA.

Part: WIRE HARNESS — FAULTY (APU BAY) · airframe 59,751 hrs · 56,548 cycles

DIVERSION, APU FIRE WARNING LIGHT ILLUMINATED IN FLT. APU FIRE BOTTLE DISCHARGED. APU FIRE WARNING LIGHT STILL ILLUMINATED MULTIPLE TIMES AFTER BOTTLE DISCHARGED. FOUND APU AFT TAILPIPE HARNESS CONNECTORS GROUNDING OUT THRU CERAMIC. REMOVED AND REPLACED APU AFT TAILPIPE HARNESS PER MM.

Part: FIRE DETECTOR — FAULTY (APU BAY) · airframe 59,728 hrs · 56,532 cycles

APU FIRE WARNING LIGHT ILLUMINATED. DISCHARGED APU FIRE BOTTLE. REMOVED AND REPLACED APU AFT TAILPIPE FIRE DETECTOR PER MM.

Part: CIRCUIT BREAKER — BROKEN (COCKPIT) · airframe 59,586 hrs · 56,414 cycles

EMERGENCY LIGHT C/B BROKEN. REMOVED AND REPLACED C/B PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 59,349 hrs · 56,220 cycles

DURING SCHEDULED C4 CHECK, FOUND 2 EA FUSELAGE CRACKS AT AFT PRESSURE BULKHEAD, BS 1016, STR 4L & BETWEEN STR 6R TO STR 7R. REPAIRED AFT PRESSURE BULKHEAD PER SWA EA.

Part: WEDGE — DELAMINATED (RT WING SLAT) · airframe 59,349 hrs · 56,220 cycles

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

Part: WEDGE — DELAMINATED (RT WING FLAP) · airframe 59,349 hrs · 56,220 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING INBOARDD MIDFLAP OUTBOARD T/E WEDGE DELAMINATED. REMOVED AND REPLACED WEDGE PER MM.

Part: SKIN — CRACKED (FUSLAGE) · airframe 59,349 hrs · 56,220 cycles

DURING SCHEDULED C4 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT BS 908 & BS 920, STR 23L. REPAIRED SKIN PER SRM.

Part: SKIN — WORN (FUSELAGE) · airframe 58,713 hrs · 55,735 cycles

DURING SPV, FOUND FUSELAGE SKIN BETWEEN BS 860 AND BS 880, RBL 3, WORN. REPAIRED SKIN PER ER AND SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,713 hrs · 55,735 cycles

DURING SPV, FOUND FUSELAGE SKIN AT BS 500D + 4, STRINGER 12R, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 58,448 hrs · 55,540 cycles

DURING SCHEDULED C3 CHECK, FOUND RT WING NR 6 L/E SLAT SKIN CRACKED. REPAIRED SLAT SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,440 hrs · 55,534 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN AT BS 727D, STRINGER 15R, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 57,531 hrs · 54,784 cycles

DURING SCHEDULED C3 CHECK, FOUND RT WING AFT INBOARD T/E FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 57,176 hrs · 54,494 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,648 hrs · 54,075 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 937, STRINGER 22R AND STINGER 24R, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,640 hrs · 54,069 cycles

DURING SCHEDULED C1 CHECK, FOUND R1 DOOR UPPER HINGE CUTOUT LOWER FRAME, CRACKED. REPAIRED SKIN PER EA.

Part: LENS — LOOSE (CABIN) · airframe 56,403 hrs · 53,871 cycles

DURING SCHEDULED 1/4D CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT LENS LOOSE AT ROW 9 DEF. SECURED LENS PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,403 hrs · 53,871 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 907, BL 0, CORRODED. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,403 hrs · 53,871 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 772.5, RBL 2.5 TO LBL 2.5, CORRODED. REPAIRED FLOORBEAM PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,403 hrs · 53,871 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 927, STRINGER 26R, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 56,403 hrs · 53,871 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR FWD FRAME CUTOUT AT AFT STOP FITTINGS CRACKED. REPAIRED DOOR CUTOUT FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,403 hrs · 53,871 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 805, STRINGER 18L, CRACKED. REPAIRED SKIN PER SRM.

Part: CABLE — MISROUTED (L2/R2 DOORS) · airframe 55,613 hrs · 53,246 cycles

DURING SCHEDULED C4 CHECK, FOUND BOTH L2 AND R2 DOOR EVAC SLIDES CABLES MISROUTED. REROUTED BOTH DOOR EVAC SLIDE CABLES PER MM.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 54,502 hrs · 52,350 cycles

LOST 'A' SYSTEM HYD, NR 1 ENG HYD LOW PRESS LIGHT ILLUMINATED. REMOVED AND REPLACED LT ELEVATOR PCU HYD PRESS LINE AND 'A' SYSTEM CASE DRAIN FILTER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,487 hrs · 51,499 cycles

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED (3 EA) BS 743 AT STR 19L, BS 767 AT STR 20R AND BS 947 AT STR 22R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,878 hrs · 51,016 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, BETWEEN STRINGERS 15L AND 16L, AND BS 500D, STRINGER 13R. REPAIRED SKIN PER SRM.

Part: SLAT — CRACKED (LT WING) · airframe 51,527 hrs · 49,911 cycles

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND NR 1 L/E SLAT CRACKED AT LOWER SKIN. REPAIRED NR 1 L/E SLAT PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,527 hrs · 49,911 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 1L. REPAIRED FRAME PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,527 hrs · 49,911 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND OVERHEAD BIN BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW NR 2. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 51,527 hrs · 49,911 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND EMERGENCY EXIT LIGHT BATTERY PACK POWER CHARGER INOP. REMOVED AND REPLACED POWER CHARGER PER MM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 51,527 hrs · 49,911 cycles

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

Part: SPLICE — CRACKED (FUSELAGE) · airframe 51,527 hrs · 49,911 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,527 hrs · 49,911 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CRACKED AT BS 460, STR 10L. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,527 hrs · 49,911 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 16L. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 51,527 hrs · 49,911 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,527 hrs · 49,911 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIP CRACKED AT BS 380, STR 14L. REMOVED AND REPLACED STRINGER TIE CLIP PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,527 hrs · 49,911 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIPS CRACKED (3 EA) AT BS 639 AT STR 5R, BS 639 AT STR 1R AND BS 616 AT STR 1R. REMOVED AND REPLACED TIE CLIPS PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,527 hrs · 49,911 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIPS CRACKED (3 EA) AT STR 4L, BS 727B, 727C AND 727D. REMOVED AND REPLACED STR TIE CLIPS PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 51,527 hrs · 49,911 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,904 hrs · 49,409 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 20L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 50,904 hrs · 49,409 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,031 hrs · 48,674 cycles

DURING SCHEDULED C2 CHECK, FOUND 1.5 INCH SKIN CRACK AT AFT SVC DOOR CUTOUT BS 957, NEAR STR 14L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (FWD SVC DOOR) · airframe 49,177 hrs · 47,963 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,177 hrs · 47,963 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED ON AFT ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA RA.

Part: LENS — OUT OF ADJ (CABIN) · airframe 48,281 hrs · 47,240 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BULLNOSE MOUNTED EMERGENCY LIGHT LENS AT 7C OUT OF ADJUST. ADJUSTED LENS PER MM.

Part: POST — CRACKED (FUSELAGE) · airframe 48,281 hrs · 47,240 cycles

DURING SCHEDULED 1/2D CHECK, FOUND F/O'S UPPER WINDOW POST CRACKED. REPAIRED F/O'S WINDOW POST PER SRM.

Part: WEB — CRACKED (RH MLG W/W.) · airframe 48,281 hrs · 47,240 cycles

DURING SCHEDULED 1/2D CHECK, FOUND WEB IN RH MLG W/W CEILING CRACKED AT BS 675, RBL 35. REPAIRED WEB PER SWA TI.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 48,281 hrs · 47,240 cycles

DURING SCHEDULED 1/2D CHECK, FOUND 2 CRACKS AT FWD SERVICE DOOR LOWER HINGE CUTOUT BEAR STRAP. REPAIRED STRAP ASSY PER SWA RA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,281 hrs · 47,240 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR CUTOUT SKIN CRACKED AT BS 300, WL 210. REPAIRED SKIN PER SWA RA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 48,281 hrs · 47,240 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT SERVICE DOOR LOWER FWD CUT OUT BEAR STRAP CRACKED. REPAIRED STRAP ASSY PER SWA RA.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 48,018 hrs · 46,998 cycles

DURING SCHEDULED RON, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: FITTING — CORRODED (LH WING) · airframe 47,332 hrs · 46,404 cycles

DURING SCHEDULED SERVICE CHECK, FOUND MLG WALKING BEAM SUPPORT FITTING CORRODED AT LH FWD. R&R FITTING PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 46,519 hrs · 45,708 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBD FORE FLAP DISBONDED. R&R FORE FLAP PER MM.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 46,281 hrs · 45,534 cycles

CLIMBING THROUGH FL350, AURAL WARNING INTERMITTENTLY SOUNDED AND CABIN PRESSURE BEGAN PASSING 10,000 FT. DESCENDED TO 10,000 FT AND DIVERTED TO TPA. MX FERRY TO DAL FOR REPAIRS. REPAIRED THE FOLLOWING DISCREPANCIES; NOSE RADOME HINGE CUTOUTS RESEALED, FWD ENTRY DOOR FWD & AFT LOWER CORNER SEALS REPAIRED, FWD CARGO DOOR SEAL REPAIRED, AFT CARGO DOOR SCUFF PLATES RESEALED, AFT ENTRY DOOR LOWER AFT CORNER & UPPER HINGE ARM RESEALED, LT OVERWING EMERGENCY EXIT READJUSTED, REMOVED AND REPLACED PRESSURE CONTROLLER (P/N 761268-8, S/N HG846) PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,755 hrs · 45,080 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 2 EXTERNAL FUSELAGE SKIN CRACK AT BS 500D, WL 246 LT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,539 hrs · 44,905 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE EXT SKIN CRACKED, BS 827, STR 18L. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (LH WING) · airframe 45,539 hrs · 44,905 cycles

DURING SCHEDULED C1 CHECK, FOUND LH AFT OUTBD T/E FLAP DELAMINATED AT LOWER SURFACE. R&R FLAP PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 45,057 hrs · 44,497 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,933 hrs · 44,388 cycles

A 3 INCH SKIN CRACK FOUND 55 FWD OF AFT CARGO DOOR, 5 BELOW WHITE STRIPE. REPAIRED SKIN PER SRM.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 44,306 hrs · 43,840 cycles

ABORTED TAKEOFF, WARNING HORN SOUNDED DURING TAKEOFF ROLL, ALL SETTINGS WERE NORMAL. OPERATED TAKEOFF WARNING SYS SEVERAL TIMES, COULD NOT DUPLICATE.

Part: WARN HORN — ACTIVATED (COCKPIT) · airframe 44,144 hrs · 43,688 cycles

ABORTED TAKEOFF, WARNING HORN SOUNDED. TAKEOFF WARNING TEST, OPS CK GOOD PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 43,725 hrs · 43,315 cycles

FWD SERVICE DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: LIGHT — INOPERATIVE (ROW 7) · airframe 43,676 hrs · 43,273 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 7 LT SIDE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 43,676 hrs · 43,273 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND LT MLG W/W PRESS WEB CRACKED JUST O/B OF AILERON QUADRANT. REPAIRED WEB PER MM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 43,676 hrs · 43,273 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 CREASE BEAM CRACKED IN TWO PLACES, RBL 28 AND LBL 28, WL 207. REPAIRED BEAM PER SRM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 43,095 hrs · 42,755 cycles

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

Part: SKIN — CRACKED (BS 792)

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 792, STRINGER 19L AND STRINGER 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 500C)

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 500C, STRINGER 10R. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (TE FLAP)

DURING SCHEDULED SERVICE CHECK, FOUND LT AND RT OUTBOARD T/E FLAPS DELAMINATED AT INBOARD ENDS. REMOVED AND REPLACED T/E FLAPS PER MM.

Part: FLOORBEAM — CRACKED (BS 660)

DURING SCHEDULED 1/4D CHECK, FOUND BEAM UPPER CHORD CRACKED AT BS 660, BL 0. REPAIRED BEAM PER BAC DRAWING.

Part: BULHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, LBL 12, WL 234. REPAIRED BULKHEAD PER SRM.

Part: SKIN — CRACKED (PAX DOORWAY)

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT LOWER HINGE CUT OUT OF FWD ENTRY DOOR. REPAIRED SKIN PER SRM.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SC CHECK, FOUND CABIN EMERGENCY LIGHTS AFT OF WING INOP. REMOVED AND REPLACED BATTERY PACK PER BOEING M/M.

Part: BULB — MISSING (SERVICE DOOR)

DURING SCHEDULED C1 CHECK, FOUND CABIN FWD SERVICE DOOR LOWER EMERGENCY EXIT LIGHT BAR MISSING ONE LIGHT. RELAMPED FWD SERVICE DOOR LWR EMERGENCY EXIT LIGHT BAR PER MM.

Part: PUMP — LOW PRESS (NR 1)

AIR TURNBACK DUE TO NR 1 (B) ELECTRIC HYD PUMP LOW PRESURE LIGHT ILLUMINATED. AIRCRAFT MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED B PUMP, OPS CHECK GOOD PER BOEING MM (LPG 267342).

Part: LIGHTS — INOPERATIVE (CABIN)

DURING SCHEDULED RON CHECK, FOUND FWD EMERGENCY TRACK LIGHTS INOP. REMOVED AND REPLACED POWER SUPPLY PER BOEING MM.

Part: SLIDE — FELL OUT (FWD SERV DOOR)

DURING WALKAROUND INSPECTION, FWD SERVICE DOOR ESCAPE SLIDE FELL FROM ITS HOLDER. REPLACED SLIDE ASSEMBLY PER BOEING M/M.

Part: LAMP — FAILED (CABIN)

DURING SCHEDULED BC1 CHECK, FOUND EMERGENCY EXIT SYSTEM CEILING LIGHTS INOP. RELAMPED PER BOEING M/M.

Part: SLIDE — LOW PRESSURE (FWD SERV)

DURING SCHEDULED TERMINAL CHECK, FOUND R1 SLIDE PRESSURE LOW. REPLACED SLIDE ASSEMBLY PER BOEING M/M.

Part: SKIN — DAMAGED (FUSELAGE)

AIRCRAFT DAMAGEDBY LAV SERVICE CART AFT END BY OUTFLOW VALVE AND AFT LAV SERVICE PORT. REPAIRED PER TRAMCO EWO 97-0607.

Part: BALLAST — FAILED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND FWD SECTION OF CABIN EMERGENCY FLOOR TRACK LIGHTING. REPLACED BATTERY PACK BALLAST PER BOEING M/M.

Part: CHARGER — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND RT EXTERIOR OVERWING EXIT LIGHT INOP. REPLACED BATTERY CHARGER PER BOEING M/M.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT WL 183, RBL 19. REPAIRED ALL TRAMCO EWO 96-0854.

Part: FRAME — DAMAGE (BS 867)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME DAMAGE AT BS 867, S1. REPAIRED ALL PER BOEING SRM.

Part: SKIN — DAMAGE (BS 967)

DURING SCHEDULED D-CHECK, FOUND LIGHTNING STRIKE DAMAGE AT FUSELAGE SKIN AT BS 967, BELOW S21L, WL 174. REPAIRED ALL PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 328)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 328, RBL 12, 13, 27, 31, 34.5, 40.5, 54.5, WL 208 AND 207. REPAIRED PER BOEING SRM.

Part: CLIP — CRACKED (BS 500)

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, AT S19L, WL 193. REPLACED PER BOEING SRM.

Part: SKIN — DENTED (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 380 WL 206, BS 1080, BETWEEN S7 AND 8L, BS 211, 4 FROM NOSE DOOR CUTOUT LT SIDE, BS 388, S19L, AND BS 400 PLUS 3, BETWEEN S26 AND 27R. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 727)

DURING SCHEDULED D-CHECK, FOUND AFT CARGO FLOORBEAM CORRODED UNDER STRAP, BS 727D PLUS 5, LBL 3, 8 AND RBL 3. REPAIRED PER BOEING SRM.

Part: CLIP — CRACKED (BS 727)

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 727A AT S21R. REPLACED CLIP PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 770-859)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 770 TO 859, RBL 3, WL 161. REPLACED SECTION PER BOEING SRM.

Part: WEB — CRACKED (BS 294.5)

DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AT BS 294.5, S7L AND S11L. REPLACED WEBS PER BOEING SRM.

Part: T-CHORD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 VERTICAL CHORD LBL 5.5 FORWARD T-CHORD CRACKED AT WL 183.75. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 986.5)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 986.5, WL 208, LBL 17 TO RBL 46. REPLACED FLOORBEAM UPPER CHORD PER BOEING SRM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BULKHEAD BS 178 WEB CRACKS AT RBL 4.7, WL 201.7 TO 202.8. REPAIRED PER TRAMCO EWO 96-0778.

Part: STRINGER — CRACKED (BS 974/500/380)

DURING SCHEDULED D-CHECK, FOUND STRINGER 21L ON I/B FLANGE AT BS 974, AT BS 500D TO 520, S25L, AND AT BS 380, S22L CRACKED. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (CARGO DOOR)

AT GATE, FOUND A 4 INCH SKIN CRACK IN AFT CARGO DOOR SKIN. REPAIRED PER BOEING SRM.

Part: FLOOR BEAM STRAP — CRACKED (BS 312)

DURING SCHEDULED C1 CHECK, FOUND FLOOR BEAM SUPPORT STRAPS CRACKED AT BS 312, AT CENTERLINE, AT 31.75 INCHES TO RIGHT OF CENTERLINE, AND AT 11.25 INCHES TO THE LEFT OF CENTERLINE. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.