N60SW

Part: SKIN — CRACKED (BS 767)

DURING WALK ARROUND INSP, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 767, STRINGER 14R. REPAIRED SKIN PER SRM.

Part: ACTUATOR — FAILED (NR 4 LE SLAT)

AIR TURNBACK, NR 4 LE SLAT WOULD NOT RETRACT. REMOVED AND REPLACED NR 4 SLAT ACTUATOR PER MM.

Part: CHORD — CRACKED (CARGO DOOR)

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO DOOR T-CHORD CRACKED AT FWD LOWER CORNER. REMOVED AND REPLACED DOOR ASSY PER MM AND SWA RA NR 1-352-0325.

Part: STRINGER — CRACKED (BS 900)

DURING SCHEDULED 1/4D CHECK, FOUND CRACKED STRINGER 24R, BS 900. REPAIRED PER SRM.

Part: LIGHT — INOP (FLIGHT DECK)

FLIGHT DECK EMERGENCY EXIT LIGHT WILL NOT EXTINGUISH. OK TO CONTINUE PER MEL 33-15. REPLACED LIGHT ASSEMBLY PER BOEING M/M.

Part: LIGHT — INOP (COCKPIT)

FLIGHT DECK EMERGENCY EXIT LIGHT WILL NOT EXTINGUISH. OK TO CONTINUE PER MEL 33-15. REMOVED AND REPLACED LIGHT ASSY, OPS CK OK PER M/M.

Part: COMPRESSOR — DAMAGED (NR 1 ENGINE)

RETURNED TO MDW DUE TO BIRD STRIKE TO NR 1 ENG. INSPECTED AND FOUND 2 SHINGLED FAN BLADES. REMOVED AND REPLACED C1 FAN ASSY AND PERFORMED ENG RUN, OPS CKS GOOD.

Part: SKIN — CRACKED (BS 908-951)

FOUR FASTENER HOLES CRACKED IN THE FUSELAGE SKIN, STA 908 - STA 951, S10R. THREE FASTENER HOLES CRACKED IN THE FUSELAGE SKIN, STA 908 - STA 951, S10L. REPAIRED PER DALFORT AEROSPACE XEA X2-53-219, REV 2 DATED 8-25-98 AND BOEING SRM 53-30-3, FIG 42. APPROVAL DATA: FAA FORM 8110-3 DATED 8-24-98.

Part: SKIN — CRACKED (BS 908-951)

SKIN CRACKED AT AFT ENTRANCE DOOR, LOWER HINGE CUTOUT, AT STR 14L BETWEEN STA 908 - STA 951. SKIN CRACKED AT AFT SERVICE DOOR, LOWER HINGE CUTOUT, AT STR 14R BETWEEN STA 908 - STA 951. REPAIRED PER DALFORT AEROSPACE XEA X2-53-218 DATED 8-6-98 AND SB 737-53-1074, REV 3. APPROVAL DATA: FAA FORM 8110-3 DATED 8-18-98.

Part: SKIN — DENTED (BS 970)

DURING SCHEDULED B CHECK, FOUND FUSELAGE SKIN DENTED BELOW AFT ENTRY DOOR AT BS 970, S21L. REPAIRED PER BOEING SRM.

Part: QUICK DISCONNECT — LEAKING (NR 2 BRAKE)

RETURNED TO PHX DUE TO EXPERIENCING A-SYSTEM HYDRAULIC PRESSURE LOSS RIGHT AFTER GEAR RETRACTION. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED AND FOUND NR 2 BRAKE ASSEMBLY QUICK DISCONNECT BLANKING PLUG SHEARED AND LEAKING. REMOVED AND REPLACED BRAKE ASSEMBLY, CHECKED FILTERS AND SERVICED HYDRAULIC SYSTEM PER BOEING M/M.

Part: LAMP — FAILED (CABIN)

DURING TERMINAL CHECK, FOUND LT AFT ENTRY EMERGENCY EXIT LIGHT INOP. RELAMPED PER BOEING M/M.

Part: SKIN — CRACKED (BS 885)

DURING SCHEDULED TERMINAL CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 885, AT S24R. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (CARGO DOORWAY)

DURING SCHEDULED C2 CHECK, FOUND AFT LOWER CARGO FWD DOORWAY FRAME CRACKED AT O/B END OF DOUBLER. REPLACED PER BOEING SRM.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN)

CABIN PRESSURIZATION FAILED 35,000 FT CABIN OUTFLOW VALVE CLOSED. DESCENDED TO 24,000 TO REDUCE CABIN ALTITUDE. CABIN ALTITUDE STABILIZED AT 5500. AIRCRAFT MADE AN UNEVENTFUL LANDING AT DAL. REPLACED PACK VALVE AND OP CHECKED PER BOEING M/M.

Part: FRAME — CRACKED (CARGO DOORWAY)

DURING SCHEDULED RON CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CRACKED UNDER EXISTING REPAIR. REPAIRED PER BOEING SRM AND DRAWING 65C35243.

Part: BULB — FAILED (CABIN)

DURING SCHEDULED C2 CHECK, FOUND EMERGENCY LIGHT ABOVE FWD SERVICE DOOR FLICKERS ON AND OFF. REPLACED LIGHT BULBS AND CLEANED CONNECTORS PER BOEING M/M.

Part: SKIN — CRACKED (APU COMPT)

DURING SCHEDULED B-CHECK, FOUND FUSELAGE SKIN CRACKED .125 INCH AT APU COWL LATCH, AFT CUTOUT. REPAIRED CRACK PER TI-A53-019.

Part: RT UNIT — INOPERATIVE (E/E COMPT)

DURING CLIMBOUT, WEATHER RADAR BECAME INOPERATIVE. AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING. REPLACED R/T UNIT AND ANTENNA PER BOEING M/M.

Part: SLIDE — LOW PRESS (AFT SERV DOOR)

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

Part: CHORD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 SIDE CHORD CRACKED ON LEFT SIDE AT WL 200. REPAIRED PER TRAMCO EWO 96-0527.

Part: STRINGER — CORRODED (BS 907)

DURING SCHEDULED D-CHECK, FOUND STRINGERS 21R AND 22R CORRODED AT BS 907. REPAIRED PER BOEING SRM.

Part: BEAM — CRACKED (BS 639)

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM AT BS 639, LBL 65, WL 208 CRACKED. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 1148)

DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AT BS 1148 S5R. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND DOUBLER CRACKED AT BS 1088 TO 1138 S5L. ALSO, AT BS 1088 TO 1156, S12L. REPAIRED PER BOEING SRM.

Part: DOOR — DAMAGE (AFT ENTRY)

DURING SCHEDULED D-CHECK, FOUND AFT ENTRY DOOR DAMAGE AROUND LOWER HINGE FITTING ARM. INSTALLED REPAIR DOUBLER PER BOEING SRM.

Part: SKIN — CORRODED (BS 727)

DURING SCHEDULED D-CHECK, FOUND CORROSION BULGING BETWEEN DOUBLERS AND SKIN AT BS 727, WL 148, LBL 4. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 862, RBL 16, WL 160, AT BS 502, RBL 52, WL 169, AT BS 819, RBL 11, WL 155 AND AT BS 421, RBL 47, WL 165. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 520)

DURING SCHEDULED D-CHECK, FOUND CRACK INDICATIONS AT SKIN LAP JOINT BS 520, S10L. INSTALLED REPAIR DOUBLER PER BOEING SRM.

Part: CLIP — CRACKED (BS 1138)

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 1138, S16L. INSTALLED REPAIR DOUBLER PER BOEING SRM.

Part: AIR DISTR — SMOKE (AFT GALLEY)

SMOKEY ODOR NOTED IN AFT GALLEY AREA, BUT NO VISIBLE SMOKE. INSPECTED AFT GALLEY COFFEEMAKERS AND C/B PANEL, NO DISCREPANCIES NOTED.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SV CHECK, FOUND OVERWING EXIT EXTERIOR EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PER BOEING M/M.

Part: SKIN — CRACKED (BS 790)

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 1.5 INCHES AT BS 790, AT S24L, BOTTOM SIDE OF S24L. REPAIRED PER BOEING SRM.

Part: WEB — DAMAGE (BS 344)

DURING SCHEDULED SERVICE CHECK, FOUND WEB AND FAILSAFE CHORD DAMAGE AT BS 344 AND S21R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — DAMAGE (BS 320)

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN DAMAGE AT BS 320 AND S20R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: BELTFRAME — CRACKED (BS 328)

DURING SCHEDULED SERVICE CHECK, FOUND BELTFRAME CRACKED 17 BELOW FLOORBEAM AT BS 328, RIGHT SIDE BETWEEN S20 AND 21R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: FRAME — CRACK (BS 663.75)

DURING SCHEDULED MAINT CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663.75, STRINGER 3R. REPAIRED PER SWA RA 1-253-1260.