N59SW

Part: LIGHT — INOPERATIVE (SERVICE DOOR)

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

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED A1 CHECK, FOUND AFT CABIN LOWER EMERGENCY FLASHLIGHT INOP. REPLACED BATTERY PER BOEING M/M.

Part: SKIN — CRACKED (BS 932-947)

THREE EACH FASTENER HOLES CRACKED IN FUSELAGE SKIN AT STA 908 TO STA 927, STR 14R. EIGHT EACH FASTENER HOLES CRACKED IN FUSELAGE SKIN AT STA 932 TO STA 947, STR 14R. BEAR STRAP IS CRACKED AT THE AFT ENTRY DOOR LOWER HINGE CUT-OUT. REPAIRED PER: DALFORT AEROSPACE, L.P. XEA X2-53-215, REV 1 DATED 7-31-98 AND SB 737-53-1074, REV 3.

Part: SKIN — CRACKED (BS 908-927)

THREE EACH FASTENER HOLES CRACKED IN FUSELAGE SKIN AT STA 908 TO STA 927, STR 14R. EIGHT EACH FASTENER HOLES CRACKED IN FUSELAGE SKIN AT STA 932 TO STA 947, STR 14R. BEAR STRAP IS CRACKED AT THE AFT ENTRY DOOR LOWER HINGE CUT-OUT. REPAIRED PER: DALFORT AEROSPACE, L.P. XEA X2-53-215, REV 1 DATED 7-31-98 AND SB 737-53-1074, REV 3.

Part: SKIN — CRACKED (BS 908-928/940)

SEVEN EACH FASTENER HOLES CRACKED IN THE FUSELAGE SKIN, STA 908 TO STA 928, STR 14L. TWO EACH FASTENER HOLES CRACKED IN THE FUSELAGE SKIN, STA 940, STR 14L. FUSELAGE SKIN IS CRACKED AT THE AFT ENTRY DOOR LOWER HINGE CUT-OUT (THE BEAR STRAP IS NOT CRACKED). REPAIRED PER DALFORD AEROSPACE XEA X2-53-216 DATED 7-22-98 AND BOEING 737 SRM 53-30-3, FIGURE 42.

Part: SKIN — CRACKED (BS 1006)

EIGHT EACH FASTENER HOLES CRACKED IN THE FUSELAGE SKIN AT STA 1006, STR 14L. REPAIRED PER DALFORD AEROSPACE, L.P. XEA X2-53-214, REV 1 DATED 7-29-98 AND 737 SRM 53-30-3 FIGURE 42.

Part: BATTERY — DISCHARGE (CABIN)

DURING WALK AROUND CHECK, FOUND FWD F/A POSITION INBD EMERGENCY FLASH LIGHT SEAL BROKEN TO DMAL. REMOVED AND REPLACED FWD INBD F/A LIGHT BATTERY PER BOEING MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING WALKAROUND CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXIT LIGHT REMAINS ILLUMINATED WITH SWITCH ON. REPLACED LIGHT ASSEMBLY PER BOEING M/M.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED C2 CHECK, FOUND EMERGENCY EXIT LIGHT ABOVE L1 DOOR INOP. REPLACED LIGHT ASSEMBLY PER BOEING M/M.

Part: SKIN — CRACKED (BS 908-920)

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED FROM BS 908 TO 920, RIGHT. REPAIRED PER BOEING SRM.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED TERMINAL CHECK, FOUND EMERGENCY EXIT LIGHTS INOP BEHIND AFT SERVICE DOOR. REPLACED BATTERY PACK PER BOEING M/M.

Part: SLIDE — EXPIRED DATE (SERVICE DOOR)

DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE ESCAPE SLIDE DATE NEAR EXPIRATION. REPLACED SLIDE PER BOEING M/M.

Part: DOME — MISSING (NR 1 ENGINE)

AFTER TAKEOFF AT 1500 FT, HEARD A VERY LOUD BANG, ENGINE PARAMETERS WERE NORMAL. RETURNED TO MDW AND MADE AN UNEVENTFUL LANDING. DURING INSPECTION, FOUND NR 1 ENGINE NOSE DOME MISSING. REPLACED FRONT ACCESSORY DRIVE SUPPORT AND NOSE DOME PER BOEING M/M.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED A1 CHECK, FOUND EMERGENCY EXIT AT AFT ENTRY DOOR INOPERATIVE. REPLACED BATTERY PACK PER BOEING M/M.

Part: WIRE — BROKEN (CABIN)

DURING SCHEDULED A1 CHECK, FOUND BOTH AFT EMERGENCY EXTERIOR LIGHTS REMAINING ILLUMINATED WITH SWITCH IN ARM POSITION. REPAIRED BROKEN WIRE AT BATTERY PACK PER BOEING M/M.

Part: WIRE — BROKEN (AFT GALLEY)

AT GATE, FOUND BOTH AFT EMERGENCY EXIT LIGHTS REMAINING ILLUMINATED AT ALL TIMES. REMOVED AFT GALLEY AND REPAIRED BROKEN WIRE. OPS CHECKED OK PER BOEING M/M.

Part: FRAME — CRACKED (BS 807)

DURING SCHEDULED SV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, WL 236, LBL 68. REPAIRED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 767)

DURING SCHEDULED SV CHECK, FOUND STRINGER CRACKED AT BS 767, S10R. REPAIRED PER BOEING SRM.

Part: STRINGER — CORRODED (BS 360-420)

DURING SCHEDULED SV CHECK, FOUND STRINGER CORRODED AROUND FASTENER HOLES FROM BS 360 TO BS 420, WL 305. REPAIRED PER BOEING SRM.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED T-CHECK, FOUND AFT ENTRY DOOR AND AFT SERVICE DOOR EXTERIOR EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PER BOEING M/M.

Part: CHORD — CRACKED (BS 338/339)

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM INBOARD CHORD CRACKED AT BS 638 AND BS 639, LBL 63, WL 208. INSTALLED REPAIR PER BOEING SRM.

Part: FRAME — CRACKED (AFT GALLEY DOOR)

DURING SCHEDULED D-CHECK, FOUND FOWARD GALLEY DOOR AFT FRAME CRACKED ON FRAME LOWER STOP PIN FITTING AND AT NR 4 STOP FITTING. INSTALLED REPAIR PER BOEING SRM.

Part: ANGLE — CRACKED (BS 948.5)

DURING SCHEDULED D-CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 947.5, AT S22R. REPLACED PER BOEING SRM.

Part: STRAP — CORRODED (BS 436-455)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE TIE STRAP CORRODED AT NUTPLATE HOLES, BS 436-455, RBL 27. INSTALLED REPAIR PER BOEING SRM.

Part: SKIN — DAMAGED (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 402.5 BETWEEN S24 AND 25R AND AT BS 357 AND BS 358, BETWEEN S24 AND 25R. INSTALLED DOUBLER REPAIRS PER BOEING SRM.

Part: SHEAR TIE — CRACKED (BS 460)

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 460 BETWEEN S19 AND 20L. REPLACED PER BOEING SRM.

Part: SKIN — DENTED (BS 379-384)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 379-384, BETWEN S22 AND 23R. INSTALLED DOUBLER REPAIR PER BOEING SRM.

Part: WEB — CRACKED (BS 1138)

DURING SCHEDULED D-CHECK, FOUND CRACKED WEB AT BS 1138, S5L. INSTALLED REPAIR PER BOEING SRM.

Part: CLIPS — CRACKED (BS 380)

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 380, S21L AND S22L. REPLACED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 495)

DURING SCHEDULED D-CHECK, FOUND STRINGER 22R CRACKED AT BS 495. REPLACED PER BOEING SRM.

Part: FRAME — DENTED (BS 480)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME DENTED AT BS 480, S22L. INSTALLED DOUBLER PER BOEING SRM.

Part: FRAMES — DAMAGED (BS 440/492)

DURING SCHEDULED D-CHECK, FOUND FORWARD CARGO FRAMES CRACKED IN UPPER FLANGE AT BS 492, RBL 36, WL 167, AT BS 440, RBL 35 AND AT RBL 39. INSTALLED DOUBLER REPAIRS PER BOEING SRM.

Part: FRAME — DAMAGED (BS 420)

DURING SCHEDULED D-CHECK, FOUND FRAME DENTED AND GOUGED AT BS 420, LBL 62. REPLACED FRAME PER BOEING SRM.

Part: FRAMES — DAMAGED (BS 500)

DURING SCHEDULED D-CHECK, FOUND FRAMES CRACKED AT BS 500B, LBL 34-50, WL 160-169, AND AT BS 500, LBL 35-38, WL 161-168. INSTALLED DOUBLER REPAIRS PER BOEING SRM.

Part: STRINGER — DAMAGED (BS 787)

DURING SCHEDULED D-CHECK, FOUND STRINGER DAMAGE AT BS 787, S16R. REPAIRED PER BOEING SRM.

Part: STRAP — CORRODED (BS 1138)

DURING SCHEDULED D-CHECK, FOUND FUSE RT HORIZONTAL STRAPS CRACKED AT BS 1138, S12L AND 12R. REPLACED PER BOEING SRM.

Part: STRAP — CORRODED (BS 1138)

DURING SCHEDULED D-CHECK, FOUND FUSE LT HORZIZONTAL STRAP CRACKED AT BS 1138, S5. REPLACED PER BOEING SRM.

Part: STRINGER — CORRODED (BS 907)

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CORROSION AT BS 907, RBL 5.5, WL 165. REPLACED CORRODED SECTION PER BOEING SRM.

Part: SKIN — DENTED (BS 1016)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 1016, BETWEEN 18 AND 19R. INSTALLED REPAIR DOUBLER PER BOEING SRM.

Part: SKIN — DENTED (BS 318)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 318, BETWEEN S2L AND S3L. REPAIRED PER BOEING SRM.

Part: STRAP — CORRODED (BS 328)

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM STRAP CORRODED AT BS 328 RBL 5 WL 208. INSTALLED NEW STRAP PER BOEING SRM.

Part: FLOOR BEAM — CORRODED (BS 294)

DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORRODED AT BS 294 RBL 15, 27, 39, 44.5 AND 46.5. REPAIRED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 967)

DURING SCHEDULED D-CHECK, FOUND MOP SILL FLOOR STIFFENER ANGLE BS 967 TO 987.5 RBL 46, WL 207. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 303.9)

DURING SCHEDULED D-CHECK, FOUND FRAME WEB CRACKED AT BS 303.9, JUST BELOW S16L. REPLACED WEB PER BOEING SRM.

Part: SPLICE — CRACKED (BS 359)

DURING SCHEDULED D-CHECK, FOUND STRINGER END SPLICE CRACKED AT BS 359, S14L, UPPER AND LOWER FASTENER HOLES. REPLACED PER BOEING SRM.

Part: FLOOR BEAM — CORRODED (BS 987.5)

DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORRODED AT BS 987,5, LBL 40, WL 208 AT RBL 40, WL 208. REPAIRED PER BOEING SRM.

Part: CHORD — DAMAGE (BS 616)

DURING SCHEDULED D-CHECK, FOUND FRAME WEB DAMAGED AT BS 616 RBL 170, WL 221. INSTALLED DOUBLER REPAIR PER BOEING SRM.

Part: CHORD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND CRACK IN SIDE CHORD FROM WL 194 TO 195, BS 178, LEFT. REPLACED CHORD PER BOEING SRM.

Part: SKIN — DAMAGE (BS 847)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DAMAGE AT BS 847, RBL 12, S26 TO 25R. INSTALLED REPAIR DOUBLER PER BOEING SRM.

Part: STRINGERS — CRACKED (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND STRINGERS CRACKED AT S16 AT WING ICE LIGHT CUTOUT. REPAIRED PER BOEING SRM.

Part: FRAME — DENTED (BS 727)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME DENTED AT BS 727A PLUS 16 TO 19 AT S20L. INSTALLED DOUBLER REPAIR PER BOEING SRM.

Part: SILL — CORRODED (BS 967-992.5)

DURING SCHEDULED D-CHECK, FOUND AFT SERVICE DOOR MOP SILL FLOOR CORRODED AT BS 967 TO 992.5, RBL 49 TO 47, WL 208 AND 209. REPAIRED PER BOEING SRM.

Part: FLOOR BEAM — CORRODED (BS 312)

DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORRODED AT BS 312, LBL 7 AND AT BL 0, WL 208. REPAIRED PER BOEING SRM.

Part: FLOOR BEAM — CORRODED (BS 203)

DURING SCHEDULED D-CHECK, FOUND COCKPIT FLOOR BEAM CORROSION AT BS 203 WL 208 RBL 12 TO 18. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 178, WL 234, RBL 10 AROUND FASTENER HEAD. INSTALLED DOUBLER REPAIR PER BOEING SRM.

Part: ANGLE — CRACKED (BS 947.5)

DURING SCHEDULED D-CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 947.5, RBL 22, WL 178. REPAIRED PER BOEING SRM.

Part: BRACKET — CRACKED (BS 947)

DURING SCHEDULED D-CHECK, FOUND SUPPORT BRACKET CRACKED AT BS 947, BETWEEN S24 AND 25L. REPLACED PER BOEING SRM.

Part: WEB — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND 8 CRACKS AT BS 178 PRESSURE WEB BETWEEN WL 190 AND 201, LBL 4.7. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 500)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STRINGER 23 TO 25R. REPAIRED PER BOEING SRM.

Part: CLIPS — CRACKED (BS 747)

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 747, S18R AND AT S20R. REPLACED BOTH PER BOEING SRM.

Part: WEB — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 PRESSURE WEB CRACKED AT WL 219, RBL 11. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 711)

DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AND CHAFED AT BS 711, BL 0, WL 150. REPLACED WEB AT BS 711, BL 0, WL 150 PER BOEING SRM.

Part: SKIN — CRACKED (BS 740)

DURING SCHEDULED SERVICE CHECK, FOUND LEFT FUSELAGE SKIN CRACKED AT BS 740, S17L. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 381/766)

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN LAP CRACK INDICATIONS AT THE FOLLOWING LOCATIONS: BS 766, S10L, AT BS 776, S10L, AND AT BS 381, S14R, AT LOWER ROW OF FASTENERS. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED SERVICE CHECK, FOUND SEVERAL CRACK INDICATIONS UNDER BULKHEAD STRAP, RBL 5.5, WL 188 TO 202.5. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: EEL BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND CABIN FLOOR TRACK LIGHTING INOP. REPLACED AFT BATTERY PACK AND REWIRED TRACK LIGHTING PER BOEING M/M.

Part: SKIN — CRACKED (NLG WW)

DURING SCHEDULED A CHECK, FOUND A 1.8 CRACK AT NOSE WHEEL WELL VERTICAL WEB RIGHT SIDE BELOW FWD ACCESS PANEL CUTOUT. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: WEB — CRACKED (NLG WW)

DURING SCHEDULED A-CHECK, FOUND NOSE GEAR RETACT ACTUATOR SUPPORT VERT WEB CRACKED AT RADIUS. REPLACED WEB PER BOEING STRUCTURAL REPAIR MANUAL.

Part: EEL BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED A2 CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M.