N092SW

Part: SLIDE — DISCHARGED (L2 DOOR) · airframe 66,196 hrs · 72,248 cycles

DURING SCHEDULED A1 CHECK, FOUND L2 DOOR EVACUATION SLIDE PRESS IND LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: START VALVE — FAULTY (NR 1 ENGINE) · airframe 66,077 hrs · 72,103 cycles

INFLIGHT ENG SHUTDOWN, NR 1 ENG START VALVE LIGHT ILLUMINATED AND WOULD NOT EXTINGUISH. REMOVED AND REPLACED NR 1 ENG START VALVE PER MM.

Part: GEARBOX — LEAKING (NR 2 ENGINE) · airframe 65,989 hrs · 71,988 cycles

LOSS OF ALL OIL QTY INDICATION AT NR 2 ENGINE. REMOVED AND REPLACED ACCY GEAR BOX PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,469 hrs · 71,306 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) STR 25L, BS 775 AND BS 895. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,389 hrs · 71,206 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 960, STR 21R. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,192 hrs · 70,939 cycles

DURING SCHEDULED C3 CHECK, FOUND T-CHORD CRACKED AT TOP NOSE WHEEL WELL FWD CENTER BEAM AT BS 230. REMOVED AND REPLACED T-CHORD AND WEB PER SRM.

Part: LATCH — BROKEN (COCKPIT) · airframe 64,921 hrs · 70,597 cycles

F/O'S EMERGENCY ESCAPE ROPE DOOR LATCH BROKEN. REPAIRED LATCH ASSY PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 64,783 hrs · 70,411 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 234 AT RBL 10.5. REPAIRED BULKHEAD WEB PER SRM.

Part: SKIN — CRACKED (FWD SVC DOOR) · airframe 64,783 hrs · 70,411 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR OUTER SKIN CRACKED. REMOVED AND REPLACED FWD SVC DOOR PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 64,783 hrs · 70,411 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 179.5, WL 177 AT LBL 5.7. REPAIRED VERTICAL BEAM WEB PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 64,783 hrs · 70,411 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED (2 EA) AT LBL 17.1, BS 179 AT WL 227 AND BS 183 AT WL 231. REPAIRED VERTICAL BEAM WEB PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 64,783 hrs · 70,411 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, WL 234, LBL 8.5 AND LBL 9.5. REPAIRED BULKHEAD WEB PER SRM.

Part: FIRE LOOP — MALFUNCTIONED (NR 1 ENGINE) · airframe 64,530 hrs · 70,091 cycles

IN FLIGHT SHUTDOWN, DECLARED EMERGENCY. NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. NO SIGN OF ENGINE PROBLEMS INDICATED ON ENGINE INSTRUMENTS. BOTH FIRE BOTTLES EXTINGUISHED. REMOVED AND REPLACED NR 1 ENGINE LOWER FIRE LOOP & FIRE DETECTION UNIT PER MM.

Part: GAUGE — OUT OF POSITION (ESCAPE SLIDE) · airframe 64,489 hrs · 70,039 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,929 hrs · 69,343 cycles

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 757, STR 18L. REPAIRED SKIN PER SRM.

Part: SLIDE — UNSERVICEABLE (R1 DOOR) · airframe 63,836 hrs · 69,228 cycles

FWD SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATION LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,733 hrs · 67,180 cycles

DURING SCHEDULED A2 CHECK, FOUND AFT SVC DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT ASSY PER MM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 63,047 hrs · 68,244 cycles

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

Part: CAP — MISSING (CABIN) · airframe 63,047 hrs · 68,244 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS END CAP MISSING AT AFT CABIN. INSTALLED END CAP PER MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 63,047 hrs · 68,244 cycles

DURING SCHEDULED C4 CHECK, FOUND NR 1 L/E SLAT DELAMINATED AT INBD T/E. REMOVED AND REPLACED NR 1 L/E SLAT PER MM.

Part: SLIDE — LOOSE (SERVICE DOOR) · airframe 62,715 hrs · 67,820 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 62,667 hrs · 67,762 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,427 hrs · 67,451 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: CAP — MISSING (CABIN) · airframe 62,393 hrs · 67,408 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS END CAP MISSING IN AFT CABIN. INSTALLED END CAP PER MM.

Part: ACM — OVERTEMP (RT A/C BAY) · airframe 62,141 hrs · 67,094 cycles

AIR TURN BACK, DURING TAKEOFF CABIN BEGAN FILLING WITH SMOKE. REMOVED AND REPLACED RT AIR CYCLE MACHINE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,936 hrs · 66,828 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 892, STR 25R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (AFT DOOR) · airframe 61,872 hrs · 66,750 cycles

DURING SCHEDULED RON, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE PRESS IND'S OUT OF VIEW. REPOSITIONED SLIDES PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 61,658 hrs · 66,483 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,605 hrs · 66,417 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (ENTRY DOOR) · airframe 61,202 hrs · 65,932 cycles

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

Part: SPOILER — DELAMINATED (RT WING) · airframe 61,188 hrs · 65,914 cycles

DURING WALK AROUND INSPECTION, FOUND NR 7 FLIGHT SPOILER DELAMINATED ON T/E. REMOVED AND REPLACED NR 7 FLIGHT SPOILER PER MM.

Part: SLIDE — OUT OF POSITION (CABIN DOOR) · airframe 60,994 hrs · 65,684 cycles

DURING SCHEDULED C1 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDES PRESS IND OUT OF VIEW. REPOSITIONED SLIDES PER MM.

Part: DETECTOR — ERRATIC (# 2 ENGINE) · airframe 60,509 hrs · 65,111 cycles

( ENGINE SHUTDOWN, DECLARED EMERGENCY )……………………….DURING FLIGHT # 2 ENGINE FIRE WARNING LIGHT ILLUMINATED & BELL SOUNDED. R&R # 2 ENG LOWER FIRE OVERHEAT DETECTOR PER MM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 60,293 hrs · 64,860 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,821 hrs · 64,305 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 1 1/2 LONG AT BS 847, STR 24L. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,712 hrs · 64,172 cycles

DURING SCHEDULED A1 CHECK, FOUND EMERGENCY EXIT DOOR LIGHTS INOP, BOTH AFT EXTERIOR LIGHTS. REMOVED AND REPLACED LIGHT BATTERY PACK PER MM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 59,574 hrs · 64,017 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 59,574 hrs · 64,017 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGERS 15L & 15R CRACKED BETWEEN BS 520 & BS 540. REPAIRED STR PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 59,574 hrs · 64,017 cycles

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

Part: CAP — MISSING (CABIN) · airframe 59,551 hrs · 63,991 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS END CAP MISSING AT AFT GALLEY. INSTALLED END CAP PER MM.

Part: SENSOR — MALFUNCTIONED (STALL WARNING) · airframe 59,118 hrs · 63,494 cycles

ABORTED TAKEOFF, STALL WARNING CONTROL COLUMN SHAKER ACTIVATED. R&R AOA VANE PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 58,887 hrs · 63,234 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EXTERNAL EMERGENCY EXIT LIGHT INOP AT LT AFT LOWER FUSELAGE. RELAMPED LIGHT ASSY PER MM.

Part: BEARING — OUT OF POSITION (RT SPOILER) · airframe 58,849 hrs · 63,188 cycles

DURING SCHEDULED C2 CHECK, FOUND NR 5 SPOILER OUTBD BEARING MIGRATED OUT OF CASTING. REMOVED AND REPLACED NR 5 SPOILER PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 58,849 hrs · 63,188 cycles

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

Part: DOOR FRAME — CRACKED (SERVICE DOOR) · airframe 58,849 hrs · 63,188 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR FRAME CRACKED AT LOWER AFT CORNER. REPAIRED DOOR FRAME PER SRM.

Part: CAP — MISSING (CABIN) · airframe 58,849 hrs · 63,188 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS END CAP MISSING AT AFT CABIN. INSTALLED END CAP PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 58,661 hrs · 62,963 cycles

OVERHEAD EMERGENCY EXIT LIGHT LOOSE AT OVERWING EXIT. SECURED LIGHT ASSY PER MM.

Part: WIRE — CHAFED (LAVATORY) · airframe 58,622 hrs · 62,919 cycles

DIVERSION - SMOKE/FUMES IN COCKPIT. COCKPIT CHECKLIST C/W AND SMOKE DISSIPATED. FOUND EVIDENCE THAT FWD LAV MIRROR LIGHT BALLAST OVERHEATED. COLLARED C/B AND PLACED ON MEL. BALLAST TO BE REPLACED IN DAL ON 03/03/01. REPLACED BALLAST IN DAL ON 03/03/01. DID NOT REMEDY PROBLEM. COLLARED C/B AND ACFT REMAINS ON MEL. ON 03/04/01 AT DAL, FOUND CHAFED WIRES AT CONNECTOR D466. REPAIRED WIRING AND REMOVED AND REPLACED BALLAST PER MM, OPS CHECK GOOD.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 58,115 hrs · 62,364 cycles

DURING SCHEDULED D-CHECK, FOUND HORIZONTAL STAB CENTER SECTION CORRODED AT ATTACH FITTING LUGS, LT UPPER AFT, LT LOWER AFT, LT LOWER FWD, RT UPPER AFT AND LOWER CLEVIS. REPAIRED FITTING AND LUGS PER ACO.

Part: HOUSING — CORRODED (HORIZONTAL STAB) · airframe 58,115 hrs · 62,364 cycles

DURING SCHEDULED D-CHECK, FOUND HORIZONTAL STAB CENTER SECTION CORRODED AT UPPER ATTACH LUG FOR HINGE HOUSING. REPAIRED HINGE HOUSING FITTING PER ERO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 58,115 hrs · 65,364 cycles

DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD WEB CRACKS AT RBL 17, WL 232 & WL 229. REPAIRED WEB PER ER 00-1333.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 58,115 hrs · 62,364 cycles

DURING SCHEDULED D CHECK, FOUND 2 EA. STR SPLICES CORRODED AT BS 907 & BS 910, STR 26L & STR 25R. R&R STR SPLICES PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,115 hrs · 62,364 cycles

DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD VERTICAL CHORD CRACKED AT RBL 5.7, WL 182 TO WL 184. REPAIRED BULKHEAD CHORD PER T1-253-022.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 58,115 hrs · 62,364 cycles

DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD VERTICAL CHORD CRACKED AT LBL 5.7, WL 182 TO WL 184.5 ON INBD RADIUS AND CHORD FLANGE. REPAIRED CHORD PER SWA T1-253-022.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 58,115 hrs · 62,364 cycles

DURING SCHEDULED D CHECK, FOUND STR SPLICE CRACKED AT BS 1016, STR 25R. R&R STR SPLICE PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 58,115 hrs · 62,364 cycles

DURING SCHEDULED D CHECK, FOUND 2 EA. BS 178 BULKHEAD HORIZ STIFFNERS CRACKED AT RBL 5.7 & LBL 5.7, WL 184. R&R STIFFNERS PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,112 hrs · 62,363 cycles

DURING SCHEDULED D CHECK, FOUND INTERNAL FUSELAGE SKIN CRACK AT BR 765, STR 4R. REPAIRED SKIN PER SRM.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 58,115 hrs · 62,364 cycles

DURING SCHEDULED D CHECK, FOUND STR SPLICE CORRODED AT BS 907, STR 26R. R&R STR SPLICE PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 58,115 hrs · 62,364 cycles

DURING SCHEDULED D CHECK, FOUND STR CRACKED AT BS 765, STR 4L. REPAIRED STR PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 58,112 hrs · 62,363 cycles

DURING SCHEDULED D CHECK, FOUND FLOOR BEAM CORRODED, BS 328, RBL 5 TO LBL 40. REPAIRED FLOOR BEAM PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 58,112 hrs · 62,363 cycles

DURING SCHEDULED D CHECK, FOUND BS 1016 BULKHEAD AFT SIDE CRACKED, RBL 3, WL 228. REPAIRED BULKHEAD PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,112 hrs · 62,363 cycles

DURING SCHEDULED D CHECK, FOUND STR CLIP CRACKED AT BS 520, STR 19L. R&R STR CLIP PER SRM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 58,112 hrs · 62,363 cycles

DURING SCHEDULED D CHECK, FOUND BS 360 SKIN CREASED AT APPROX STR 17R. REPAIRED SKIN PER ESR & SRM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 58,048 hrs · 62,297 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: COVER — CRACKED (CABIN FLOOR) · airframe 58,048 hrs · 62,297 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS TRACK COVER CRACKED AND LOOSE FROM FWD GALLEY TO ROW 4. REPLACED TRACK COVER PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 57,692 hrs · 61,902 cycles

DURING SCHEDULED A1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER SRM.

Part: LIGHT — MISSING (CABIN) · airframe 57,263 hrs · 31,418 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS AFT SECTION LOOSE AND END CAP MISSING. SECURED LIGHT ASSY AND INSTALLED END CAP PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,578 hrs · 72,552 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED, BS 277, STRINGER 16L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,841 hrs · 60,942 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED IN TWO PLACES, BS 380 AND BS 390, STRINGER 10 LT. REPAIRED SKIN PER SRM.

Part: BRACKET — BROKEN (CABIN FLOOR) · airframe 56,298 hrs · 60,332 cycles

AFT SERVICE DOOR EVACUATION SLIDE GIRT BAR FLOOR ATTACH BRACKET BROKEN. REMOVED AND REPLACED BRACKET ASSY PER MM.

Part: COFFEEMAKER — MALFUNCTIONED (GALLEY)

BURNING SMELL DURING FLIGHT IN AFT GALLEY, TURNED COFFEEMAKERS OFF AND SMELL DISAPEARED. PULLED AND COLLARED AFT GALLEY LOWER COFFEEMAKER C/B AND CONTINUED PER MX NOTE. LATER AT MDW RESEATED LOWER COFFEEMAKER CONNECTOR. RESET C/B AND OPS CHECK GOOD PER MM.

Part: LIGHTS — INOP (EMER EXIT)

DURING SCHEDULED C1 CHECK, FOUND BOTH FWD DOOR EMERGENCY EXIT LIGHTS INOP. RELAMPED LIGHTS PER MM.

Part: SWITCH — OUT OF ADJUST (COCKPIT)

ABORTED TAKEOFF, TAKEOFF WARNING HORN SOUNDED. SPEED BRAKE LEVER WAS CYCLED, AND HORN SILENCED. ADJUSTED SPEED BRAKE TAKEOFF WARNING SWITCH S129 PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT AT CEILING INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BULKHEAD CHORD — CORRODED (BS 1016)

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION AT BS 1016 BULKHEAD LOWER CHORD BETWEEN STRINGERS 25R-26R. REPAIRED CHORD PER SWA RA NR 1-253-2087.

Part: CHORD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND LT SIDE CHORD 2 EA CRACKS, BS 178, LBL 26, WL 197 AND WL 207. REPAIRED CHORD PER SRM.

Part: FRAME — CORRODED (BS 1016)

DURING SCHEDULED 1/4D CHECK, FOUND INTERGRANULAR CORROSION AT BS 1016 BULKHEAD BELT FRAME, RBL 12. REPAIRED FRAME PER SWA RA NR 1-253-2087.

Part: CLIP — CRACKED (BS 1016)

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 1016, STRINGER 24R. REMOVED AND REPLACED CLIP PER SRM.

Part: BULKHEAD CHORD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND RT SIDE CHORD CRACKED AT BS 178, RBL 26, WL 207. REMOVED AND REPLACED CHORD PER SRM.

Part: STRINGER — CORRODED (BS 318)

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION AT STRINGER 26L AND SPLICE, BS 318. REPAIRED STRINGER AND SPLICE PER SRM.

Part: KEEL BEAM — CORRODED (BS 727)

DURING SCHEDULE 1/4D CHECK, FOUND CORROSION AT KEEL BEAM RT SIDE, JUST AFT OF BS 727 BULKHEAD. REPAIRED BEAM PER SRM.

Part: SKIN — CRACKED (BS 785)

DURING SCHEDULED 1/4D CHECK, FOUND APPROX A 1.25 INCH LONG CRACK AT FUSELAGE SKIN, BS 785 STRINGER 24L.

Part: CLIP — CRACKED (BS 344)

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STRINGER 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED 1/4D CHECK, FOUND GLIDE SLOPE ANT ATTACH PANEL CRACKED AT LOWER RT CORNER. STOPPED DRILLED CRACK AND REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 760)

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED BELOW STR 18R AT BS 760. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 885)

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