N091SW

Part: WEDGE — DELAMINATED (L/E SLAT) · airframe 66,238 hrs · 72,109 cycles

NR 1 SLAT T/E WEDGE DELAMINATED. REMOVED AND REPLACED NR 1 SLAT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,238 hrs · 72,109 cycles

FOUND CRACK IN FUSELAGE SKIN AT BS 780 STRINGER 18L AND BS 763, STRINGER 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,238 hrs · 72,109 cycles

DURING SCHEDULED PM CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT STR 18L, BETWEEN BS 763 AND BS 780. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,550 hrs · 71,244 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED 2 LONG AT BS 894, STRINGER 25R. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,291 hrs · 70,272 cycles

DURING SCHEDULED C2 CHECK, FOUND SEVERAL BULBS INOP IN BOTH AFT ENTRY AND MID CABIN OVERHEAD EMERGENCY EXIT LIGHTS. RELAMPED EXIT LIGHTS PER MM.

Part: BATTERY PACK — DISCHARGED (COCKPIT) · airframe 65,232 hrs · 70,839 cycles

DURING SCHEDULED PM CHECK, FOUND FLIGHT DECK EXIT DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,185 hrs · 70,778 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 960, STR 21L. REPAIRED SKIN PER SRM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,896 hrs · 40,405 cycles

DURING SCHEDULED C2 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT IN FWD CABIN INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BEAM — CRACKED (BULKHEAD) · airframe 64,889 hrs · 70,395 cycles

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

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,886 hrs · 70,391 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT EMERGENCY EXIT LIGHT BATTERY INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 64,886 hrs · 70,391 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, WL 230 AND RBL 17.1. REMOVED AND REPLACED VERTICAL BEAM WEB PER SRM.

Part: SKIN — CORRODED (KEEL BEAM) · airframe 64,886 hrs · 70,391 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CORRODED AT LT KEEL BEAM, BS 727 PLUS 10. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,886 hrs · 70,391 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT GROUND AIR CONDITIONING CONNECTION CUTOUT, RT FWD FASTENER HOLE. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,886 hrs · 70,391 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 64,886 hrs · 70,391 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BOTH LT AND RT NLG W/W WEBS CRACKED (2 EA) AT BS 246.0,WL 168.5. REPAIRED WEBS PER SWA EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 64,886 hrs · 70,391 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT SVC DOOR FRAME LOWER HINGE CUTOUT CRACKED. REPAIRED FRAME PER SRM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 64,221 hrs · 69,567 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,673 hrs · 70,462 cycles

L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: DUCT — RUPTURED (A/C BAY) · airframe 63,605 hrs · 68,802 cycles

( AIR TURNBACK )………………………FWD CARGO FIRE DETECTION ACTIVATED WITH SMOKE IN CABIN, DISCHARGED BOTTLE. MX FERRY TO DALLAS. FOUND RH PNEUMATIC DUCT RUPURED IN A/C MIX BAY. R&R PNEUMATIC DUCT PER MM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 63,440 hrs · 68,602 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,375 hrs · 68,519 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT BULB INOP. RELAMPED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,168 hrs · 68,263 cycles

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 14R. REPAIRED SKIN PER SRM.

Part: ENGINE — STALLED (RT WING) · airframe 63,050 hrs · 68,128 cycles

DURING APPROACH NR 2 ENGINE COMPRESSOR STALLED TWO TIMES IN SHORT SUCCESSION. REMOVED AND REPLACED NR 2 ENGINE PER MM.

Part: RHEOSTAT — OVERTEMP (CABIN) · airframe 63,034 hrs · 68,110 cycles

SPARKS AND SMOKE AT FWD GALLEY WORK LIGHT SW. REMOVED AND REPLACED WORK LIGHT REHOSTAT AND REPAIRED WIRES PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,980 hrs · 68,043 cycles

DURING SCHEDULED SPECIAL VISIT FOUND FUSELAGE SKIN CRACKED AT AFT LOWER CORNER OF AIRSTAIR CUTOUT, BS 348 AND STR 20L. REPAIRED SKIN PER SWA EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 64,526 hrs · 70,223 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 234 AND LBL 10. REPAIRED WEB PER SRM.

Part: TEE CHORD — CRACKED (FUSELAGE) · airframe 64,526 hrs · 70,223 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND T-CHORD CRACKED AT BS 178, WL 182 AND RBL 5.7. REPAIRED T-CHORD PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 62,980 hrs · 68,043 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 234 AND LBL 12.5. REPAIRED WEB PER SRM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 62,887 hrs · 67,928 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,785 hrs · 67,804 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 885, STR 24R. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 62,785 hrs · 67,804 cycles

DURING SCHEDULED C3 CHECK, FOUND BS 1016 PRESS BULKHEAD CRACKED (2 EA) AT APPROX 3 O'CLOCK POSITION. REPAIRED BULKHEAD PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,785 hrs · 67,804 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 17L. REPAIRED FRAME PER SRM.

Part: COFFEEMAKER — MALFUNCTIONED (GALLEY) · airframe 62,538 hrs · 67,505 cycles

SMOKE COMING FROM AFT GALLEY COFFEEMAKER. REMOVED AND REPLACED COFFEEMAKER PER MM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 62,242 hrs · 67,132 cycles

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

Part: SPAR — CRACKED (T/E FLAP) · airframe 62,114 hrs · 66,968 cycles

DURING SCHEDULED C2 CHECK, FOUND LT OUTBOARD MID FLAP AFT SPAR UPPER FLANGE CRACKED. REMOVED AND REPLACED LT OUTBOARD MID FLAP PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 62,098 hrs · 66,946 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 61,872 hrs · 66,663 cycles

DURING SCHEDULED RON, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 61,810 hrs · 66,584 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 61,749 hrs · 66,507 cycles

DURING SCHEDULED A1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: WIRE — DISCONNECTED (COCKPIT) · airframe 61,356 hrs · 66,011 cycles

FIRE WARNING BELL CUTOUT LIGHT FLICKERED IN FLIGHT. FOUND WIRE DISCONNECTED AT NR 1 FIRE WARNING BELL CUTOUT SWITCH, RECONNECTED WIRE. OPS CK OK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,511 hrs · 65,000 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 2.5 INCHES LONG AT BS 791, STR 19L. REPAIRED SKIN PER SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 60,285 hrs · 64,722 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD FUSELAGE EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 60,126 hrs · 64,540 cycles

DURING SCHEDULED RON, FOUND FWD SVC DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BRACKET — LOOSE (CABIN) · airframe 60,064 hrs · 64,471 cycles

DURING SCHEDULED C3 CHECK, FOUND R2 DOOR AFT FLOOR GIRT BAR BRACKET LOOSE. TIGHTENED AFT GIRT BAR BRACKET PER MM.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 60,064 hrs · 64,471 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED 1/4 INCH LONG ON FIRST OFFICER'S CD WINDOW POST AT LOWER END. REPAIRED SKIN PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 59,321 hrs · 63,630 cycles

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND FUSELAGE STRINGERS CRACKED AT BS 360, STR 15R & BS 540, STR 15L. REPAIRED STRINGERS PER SRM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 59,321 hrs · 63,630 cycles

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

Part: COVER — LOOSE (CABIN) · airframe 59,629 hrs · 63,570 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK COVER LOOSE AT AFT END. SECURED EEPLS COVER PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 59,139 hrs · 63,420 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,106 hrs · 63,383 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 25L. REPAIRED SKIN PER SRM

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,890 hrs · 63,129 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 380, BELOW STR 14R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,756 hrs · 62,985 cycles

DURING WALKAROUND INSPECTION, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 727C+10, STR 19R. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (COCKPIT) · airframe 58,423 hrs · 62,623 cycles

DURING SCHEDULED C1 CHECK, FOUND COCKPIT EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF ADJ (ENTRY DOOR) · airframe 58,423 hrs · 62,623 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE ASSY OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D CHECK, FOUND AFT ENTRY EMERGENCY EXIT LIGHT INOP. R&R LIGHT ASSY PER MM.

Part: FITTING — CRACKED (LT WING) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D CHECK, FOUND LT WING REAR SPAR UPPER CHORD CRACKED AT MLG BEAM FITTING. REPAIRED MLG FITTING PER EO 00-1248.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D CHECK, FOUND BEADED PRESS WEB CRACKED AT BS 665, RBL 39 TO RBL 40, WL 202. REPAIRED BEADED WEB PER ER 00-1239.

Part: DOUBLER — DEBONDED (FUSELAGE) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D CHECK, FOUND SKIN DOUBLER DISBONDED AT BS 383 BETWEEN STR 27L & STR 27R. R&R DOUBLER PER SRM.

Part: SKIN — CRACKED (L/E SLAT) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D CHECK, FOUND NR 2 L/E SLAT LOWER SKIN CRACKED BETWEEN ROD END FITTINGS. REPAIRED SLAT PER DWG 65C30133, ER 00-1246 & SRM.

Part: WIRE — LOOSE (CABIN) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT WIRING PULLED LOOSE FROM CONNECTOR. REPAIRED WIRING PER WDM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D CHECK, FOUND STR CORRODED AT BS 550 TO 553, STR 16R. REPAIRED STR PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D CHECK, FOUND STRINGERS CORRODED AT BS 1016 - 1006, STR 25R & BS 986, STR 26R. REPAIRED STRINGERS PER SRM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER FITTINGS CORRODED AT BS 727 STR 21L, STR 22L & STR 24L. REPAIRED FITTINGS PER SRM.

Part: SKIN — CRACKED (L/E SLAT) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D CHECK, FOUND NR 6 L/E SLAT LOWER CHORD CRACKED AT ACTUATOR ROD END CUTOUT. R&R SLAT LOWER CHORD PER SRM.

Part: SKIN — CRACKED (L/E SLAT) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D CHECK, FOUND NR 3 L/E SLAT FIXED INNER SKINS (4 EA.) CRACKED AT UPPER ATTACH HOLES. REPAIRED SLAT PER ER 00-1279 & SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D CHECK, FOUND STR CRACKED AT BS 887, STR 21R. REPAIRED STR PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT WL 196, RBL 21.5. REPAIRED BULKHEAD PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,006 hrs · 62,170 cycles

DURING RON CHECK, FOUND 3 EXTERNAL FUSELAGE SKIN CRACK ON RT SIDE, 3' FWD OF OUTFLOW VALVE. REPAIRED SKIN PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER FITTING CORRODED AT BS 727, STR 27L. R&R FITTING PER MM.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D-CHECK, FOUND 27 INCH LONG SKIN CREASE IN RT HORIZ STAB, GOING THROUGH A PREVIOUS REPAIR; EXTENDING DIAGONALLY FROM 2 AFT OF L/E SPAR AT L/E STA 198.23 TO 5.5 FWD OF REAR SPAR AT APPROX ELEV STA 168.67. REPAIRED SKIN PER DWG 65C36195 & SRM.

Part: FRAME — CORRODED (CABIN FLOOR) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D-CHECK, FOUND INBOARD CHORD CORRODED AT BS 480 - 520, RBL 64, WL 208. REMOVED AND REPLACED INBOARD CHORD PER SRM.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAMS CORRODED AT BS 947, RBL 53 TO LBL 53 & BS 1006, RBL 10. REPAIRED FLOORBEAMS PER SRM & T1-253-024.

Part: STRINGER — CORRODED (CARGO BAY) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGERS CORRODED AT BS 757 STR 24R, BS 767 - BS 777 STR 26R & BS 771 STR 21R. REPAIRED STRINGERS PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D-CHECK, FOUND 4 CRACKS AT BS 178 BULKHEAD WEB, AFT ROW OF Y CHORD, FWD SIDE OF BULKHEAD, STR 6L. REPAIRED BULKHEAD PER SRM.

Part: LENS — CRACKED (EXTERIOR LIGHT) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D-CHECK, FOUND EXTERNAL LOWER RT EMERGENCY EXIT LIGHT LENS CRACKED. REPLACED LENS PER MM.

Part: FLOORBEAM — CRACKED (CABIN) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 294.5, RBL 53. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CRACKED (TAIL) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D-CHECK, FOUND BS 1156 O/B CHORD CRACKED AT LBL 24, WL 260. REMOVED AND REPLACED CHORD DOUBLER PER DWG 69-77737.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 987, RBL 45 TO LBL 45. REPAIRED FLOORBEAM PER T1-253-024 AND T1-453-037.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED ON UPPER FLANGE AT BS 967, RBL 50 TO LBL 50. REPAIRED FLOORBEAM PER T1-453-037 AND T1-453-057.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D-CHECK, FOUND STR CRACKED AT BS 1010, STR 7L. REPAIRED STR PER SRM AND T1-A51-002.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D-CHECK, FOUND FRAMES CRACKED AT BS 887, STR 20R - 21R & BS 907, STR 21R. REPAIRED FRAMES PER SRM.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D-CHECK, FOUND BS 1016 BULKHEAD CORRODED AT RBL 3 TO RBL 6, WL 206. REPAIRED BULKHEAD PER SRM.

Part: FRAME — CRACKED (LT WING LE SLAT) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D-CHECK, FOUND NR 1 SLAT LOWER CHORD CRACKED BELOW I/B AUX CUTOUT. REMOVED AND REPLACED CHORD PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D-CHECK, FOUND BS 1016 BULKHEAD CRACKED AT BBL 0, WL 230. REPAIRED BULKHEAD PER SRM.

Part: FRAME — CRACKED (CABIN) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D-CHECK, FOUND BS 663 FRAME CRACKED UNDER STRINGER SPLICE, STR 2R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D-CHECK, FOUND FWD SVC DOOR LOWER STUB FRAME CRACKED AT BS 295, RBL 55, STR 15L. REPAIRED STUB FRAME PER SRM.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAMS CORRODED AT BS 344, RBL 12 - LBL 57 & BS 328, LBL 12 - RBL 56. REPAIRED FLOORBEAMS PER SRM.

Part: FRAME — CRACKED (E/E BAY) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 360 BETWEEN STR 19R & 20R. REPAIRED FRAME PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D-CHECK, FOUND EXTERNAL FUSELAGE SKIN CROWN WITH FRETTING CORROSION AT BS 927, LBL 2. REPAIRED SKIN PER SRM.

Part: STRINGER — CORRODED (CARGO BAY) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D-CHECK, FOUND STR 23L CORRODED AT BS 730. REPAIRED STR PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME CORRODED AT BS 827, STR 27R - 27L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (CABIN) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D-CHECK, FOUND STR CLIP CRACKED AT BS 847, STR 24L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: SPLICE — CRACKED (CABIN) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D-CHECK, FOUND STR SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D-CHECK, FOUND INTERNAL FUSELAGE SKIN CORRODED AT BS 986 BETWEEN STR 27L & 27R. REPAIRED SKIN PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D-CHECK, FOUND STR 26L CRACKED AT BS 870. REPAIRED STR PER SRM.

Part: FRAME — CORRODED (UPPER LOBE) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME CORRODED AT BS 951, WL 208, RBL 55. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D-CHECK, FOUND FRAMES CORRODED AT BS 867 & 887, STR 27R & STR 27L. REPAIRED FRAMES PER SRM.

Part: STRINGER — CORRODED (CARGO BAY) · airframe 58,003 hrs · 62,168 cycles

DURING SCHEDULED D-CHECK, FOUND STR CORRODED AT BS 1006 - 1016, STR 26R. REPAIRED STR PER SRM.

Part: SPLICE — CRACKED (CABIN) · airframe 58,006 hrs · 62,170 cycles

DURING SCHEDULED D-CHECK, FOUND STR SPLICE CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 58,003 hrs · 62,168 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 312, LBL 13 - RBL 14, WL 208. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER — CRACKED (CABIN) · airframe 580,013 hrs · 62,168 cycles

DURING SCHEDULED D-CHECK, FOUND STR 7L CRACKED AT BS 1010. REMOVED AND REPLACED STR PER SRM AND TR T1-A51-002.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 58,003 hrs · 62,168 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 360, RBL 14. REPAIRED FLOORBEAM UPPER CHORD PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,968 hrs · 62,134 cycles

ON WALKAROUND, FOUND 3 FUSELAGE SKIN CRACK ON RT SIDE, 3 FT FWD OF OUTFLOW VALVE. REPAIRED SKIN PER SRM.

Part: TAB — DELAMINATED (RT WING AILERON) · airframe 57,959 hrs · 62,124 cycles

RT AILERON TRIM TAB DELAMINATED. REMOVED AND REPLACED TRIM TAB PER MM.

Part: INDICATOR — OUT OF POSITION (PAX DOOR SLIDE) · airframe 57,940 hrs · 62,102 cycles

AFT ENTRY EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 57,907 hrs · 62,063 cycles

AFT EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. ADJUSTED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,489 hrs · 61,595 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 840, ABOVE STRINGER 25L. REPAIRED SKIN PER SRM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 57,199 hrs · 61,293 cycles

AFT ENTRY DOOR EVACUATION SLIDE PRESSURE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: MODULE — ERRATIC (NLG WW) · airframe 57,141 hrs · 61,216 cycles

NLG DID NOT EXTEND ON FIRST ATTTEMPT, SECOND ATTEMPT NORMAL. R&R NLG MODULAR PACKAGE PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 57,049 hrs · 61,116 cycles

AFT ENTRY DOOR EVACUATION SLIDE PRESS INDICATOR IS OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 56,695 hrs · 60,716 cycles

AFT ENTRY DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 56,667 hrs · 60,690 cycles

AFT ENTRY DOOR EVACUATION SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: KEELBEAM — CORRODED (BS 546)

DURING SCHEDULED C2 CHECK, FOUND BS 546 KEEL BEAM CORRODED, RT SIDE. REPAIRED KEEL BEAM PER SRM AND RA NR 1-253-2239.

Part: SKIN — CRACKED (BS 914)

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

Part: CASTING — CRACKED (NLG W/W)

DURING SCHEDULED C4 CHECK, FOUND NLG ACTUATOR BEAM CASTING CRACKED. REMOVED AND REPLACED CASTING PER SRM.

Part: CHORD — CRACKED (NOSE W W)

DURING SCHEDULED C4 CHECK, FOUND NOSE WHEEL WELL VERTICAL SUPPORT CHORD ANGLE CRACKED, BS 260, LBL O TO 1.6, WL 208. REPAIRED CHORD PER SWA RA NR 1-253-2161.

Part: SKIN — CRACKED (NOSE W W)

DURING SCHEDULED C4 CHECK, FOUND NOSE WHEEL WELL LT CEILING SKIN CRACKED AT BOLT HOLE, AFT INBOARD CORNER REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 727)

DURING SCHEDULED C4 CHECK, FOUND 3 INCHES LONG CRACK ON FUSELAGE SKIN, BS 727B, STRINGER 17L. REPAIRED SKIN PER SRM.

Part: SLIDE GAUGE — OUT OF POSITION (PAX DOORWAY)

DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRES GAUGE OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: SLIDE — OUT OF POSITION (PAX DOOR)

AFT ENTRY EVACUATION SLIDE PRESS GAUGE OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: ENGINE — FAILED (NR 2)

INFLIGHT SHUT DOWN. NR 2 ENGINE, OIL LOSS. NO OIL PRESSURE AND QUANTITY INDICATION. REMOVED AND REPLACED NR 2 ENG PER MM.

Part: FITTING — DAMAGED (NLG)

EN ROUTE, ISOLATION VALVE (REVERSE) ILLUMINATED. FOLLOWED QRH. NO ACTION REQUIRED. UPON LANDING GEAR DOWN RESULTED IN THREE LARGE NOISES AS EACH GEAR REACHED LOCKED POSITION. FOUND NOSE GEAR SERVICE FITTING DAMAGED. REPLACED FITTING, SERVICED, RETRACTED GEAR PER MM. PERFORMED THRUST REVERSER SYS TEST PER MM. OPS CKD GOOD PER MM.

Part: SKIN — CRACKED (BS 801)

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 801, S23L. REPAIRED PER BOEING SWA RA 1-253-1895.

Part: ANGLE — CRACKED (FUSELAGE)

DURING SCHEDULED RON CHECK, FOUND 2 ANGLES CRACKED FWD OF NR 1 LT ELECT B PUMP STIFFENER RUNS FROM FWD END LT SIDE OF KEEL BEAM VENT TO BOTTOM OF AILERON PCU FITTING (CRACKED MIDDLE OF STRINGER). INSTALLED ANGLE AND FASTENER IN FUEL TANK BULKHEAD PER BOEING SRM.

Part: SKIN — CRACKED (BS 759)

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 759, STR 18L. REPAIRED PER BOEING SRM.