N149XA

Part: SKIN — GOUGED (L1 DOOR) · airframe 62,963 hrs · 39,449 cycles

WHILE WORKING L-1 DOOR, FOUND A GOUGE ON EXISTING REPAIR AT LOWER CORNER (AFT) OF DOOR, STA 350 STR 17L. L-1 DOOR LOWER CORNER AFT OF DOOR REPAIR IAW SWA-231113 REV 01. DAMAGE TOLERANCE ANALYSIS IS REQUEST NO LATER THAN ONE YEAR.

Part: FUEL TANK — CORRODED (LT WING) · airframe 62,963 hrs · 39,449 cycles

LH WING FUEL TANK INTERNAL CORROSION AT INBD RIVET ON STR 7 BETWEEN WBL 73.0 AND WBL 81.0. PERFORMED E.O.# SWA-231027. PERFORM STEP # 19 OF THIS EO EVERY C-CHECK.

Part: FUEL TANK — CORRODED (LT WING) · airframe 62,963 hrs · 39,449 cycles

LH WING CORROSION FUEL TANK INTERNAL 2 SPOTS BETWEEN STR 4-5 AND WBL 73.0 AND WBL 81.0. PERFORMED E.O. SWA-240201, PERFORM STEP # 18 OF THIS E.O. EVERY C-CHECK.

Part: FRAME — DAMAGED (BS 500C S20-21L) · airframe 62,963 hrs · 39,449 cycles

FWD CARGO COMPARTMENT STA 500C BETWEEN STR 20L TO STR 21L FRAME HAS DOUBLE HOLE. INSTALLED ANGLES ( 2 EA ) REPAIR ON FWD CARGO COMPARTMENT STR 20L TO 21L FRAME IAW B737-400 SRM 51-30-02, 51-30-01, AND 51-40-02.

Part: FLOORBEAM — CORRODED (BS 948 LBL4-R11) · airframe 62,963 hrs · 39,449 cycles

PASSENGER CABIN FLOOR BEAM UPPER SURFACE HAS CORROSION AT STA 947.5 AROUND LBL 4.5 TO RBL 11.0. ACCOMPLISHED PASSENGER CABIN FLOOR BEAM UPPER T-CHORD REPLACEMENT AT STA 947.5 LBL 4.5 TO RBL 11.0 IAW B737-400 SRM 51-40-02 AND E.O. SWA 231022.

Part: FUEL TANK — CORRODED (LT WING) · airframe 62,963 hrs · 39,449 cycles

LH WING, CORROSION FUEL TANK INTERNAL 2EA SPOTS BETWEEN STR 8-9 LH AND WBL 73-81. PERFORMED E.O # SWA-231026, PERFORM STEP # 18 OF THIS EO EVERY C-CHECK.

Part: FUEL TANK — CORRODED (RT WING) · airframe 62,963 hrs · 39,449 cycles

RH WING CORROSION FUEL TANK INTERNAL AT SUMP DRAIN BETWEEN STR 9-10 BETWEEN WBL 2.0 AND WBL 8.0. PERFORMED E.O.# SWA-231028, PERFORM STEP # 18 OF THIS E.O. EVERY C CHECK.

Part: DRAIN — CORRODED (SUMP) · airframe 62,963 hrs · 39,449 cycles

LH WING, CORROSION AT SUMP DRAIN INTERNAL BETWEEN STR 9-10 WBL 2.0-WBL 8.0. PERFORMED E.O. # SWA-231024. PERFORM STEP # 18 OF THIS EO EVERY C-CHECK.

Part: FLOORBEAM — CORRODED (BS 967 LBL27-31) · airframe 62,963 hrs · 39,449 cycles

PASSENGER CABIN FLOOR BEAM UPPER SURFACE HAS CORROSION AT STA 986.5, LBL 27 TO LBL 31. PASSENGER CABIN FLOOR BEAM UPPER SURFACE, REMOVED AND REPAIRED TO REMOVE CORROSION AT STA 986.5 LBL 27 TO LBL 31 IAW B737-400 SRM 53-60-51,SRM 51-40-02, SRM 51-20-01 AND E.O. SWA-231021.

Part: BATTERY PACK — DISCHARGED (ZONE 200) · airframe 61,861 hrs · 38,129 cycles

AISLE LIGHT EMERGENCY IS OUT. REMOVED AND REPLACED BATTERY PACK M1197 AT STA. 960L, IAW B737-400 AMM 33-51-51, OPS CHECK GOOD

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 60,476 hrs · 37,175 cycles

DURING SERVICE CHECK FOUND AFT CABIN CEILING EMERGENCY LIGHT INOP

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 60,476 hrs · 37,175 cycles

DURING SERVICE CHECK FOUND CABIN MIDDLE CEILING PANEL EMERGENCY LIGHTS BATTERY PACK INOP (M1576). REMOVED AND REPLACED CABIN MIDDLE CELING PANEL EMERGENCY LIGHT BATTERY PACK (M1576). PERFORMED OPS CHECK, NORMAL AS PER AMM 33-51-51 AND 33-51-02.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 60,476 hrs · 37,175 cycles

DURING SERVICE CHECK FOUND CABIN AFT ENTRY CEILING PANEL EMERGENCY LIGHT BATTERY PACK INOP. REMOVED AND REPLACED CABIN AFT ENTRY CEILING PANEL EMERGENCY LIGHT (M1137), PERFORMED OPS CHECK, NORMAL AS PER AMMM 33-51-51 AND 33-51-02

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 60,476 hrs · 37,175 cycles

DURING SERVICE CHECK FWD CABIN FWD ENTRY CEILING PANEL EMERGENCY LIGHTS BATTERY PACK INOP (CONNECTOR M1149). REMOVED AND REPLACED FWD CABIN ENTRY CEILING PANEL EMERGENCY LIGHT BATTERY PACK (M1147) PERFORMED OPS CHECK NORMAL AS PER AMM 33-51-51 AND 33-51-02

Part: POWER SUPPLY — UNKNOWN (CABIN) · airframe 60,122 hrs · 36,854 cycles

L 1 DOOR EMERGENCY LIGHT(EXTERNAL) INOP.

Part: BUSHING — MISSING (LT MLG) · airframe 58,356 hrs · 35,543 cycles

DISCREPANCY: AT 2300Z AT FL240 A LOUD NOISE WAS HEARD FOLLOWED BY THE ILLUMINATION OF THE NOSE GEAR RED LIGHT AND A VIBRATION AFTER THE NOSE GEAR AND MAIN LANDING GEAR GREEN AND RED LIGHT CAME ON. DECLARED AN EMERGENCY WITH MIAMI AND REQUESTED EMERGENCY VEHICLES. LANDED SAFELY, FIRE TRUCK INSPECTED, THE A/C TAXIED TO GATE. CORRECTIVE ACTION: PERFORMED INSPECTIONS OF ALL THREE LANDING GEAR IAW AMM 05-51-47 AND 32-13-00. FOUND MISSING BUSHING AT LEFT HAND OUTER AFT ATTACH BOLT. INSTALLED MISSING BUSHING IAW AMM 32-13-21. PERFORMED LANDING GEAR SENSOR INSPECTION AND TEST IAW AMM 32-09-00 AND 32-08-02, ALL NORMAL. PERFORMED LANDING GEAR LEVER SWITCH INSPECTION AND CHECK IAW AMM 32-61-11, NO DISCREPANCY NOTED, OPERATIONAL CHECK GOOD. PERFORMED GEAR EXTENSION AND RETRACTION ADJUSTMENT/TEST AND FREE FALL IAW AMM 32-32-00, 32-34-00, 32-35-00 ALL OPERATIONAL CHECKS NORMAL.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,742 hrs · 35,047 cycles

LEFT FWD OVERWING EXIT EXTERNAL LIGHT INOPERATIVE. REMOVED AND REPLACED THE BATTERY CHARGER M1134 IAW AMM 33-51-51. OPS CHECKED GOOD

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,742 hrs · 35,047 cycles

LEFT ROW 13 INTERIOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERY CHARGER M1134 IAW AMM 33-51-51, OPS CHECKED GOOD

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,167 hrs · 34,771 cycles

DURING A POST FLIGHT INSPECTION, NOTICED THE RT MID CABIN EMERGENCY LIGHT WOULD NOT ILLUMINATE. REPLACED THE BATTERY PACK.

Part: WARNING LIGHT — ILLUMINATED (LT OVERWING) · airframe 57,060 hrs · 34,720 cycles

LEFT WING BODY OVERHEAT LIGHT ILLUMINATED IN FLIGHT & WOULD NOT EXTINGUISH.

Part: HANDSET — INOPERATIVE (INTERPHONE) · airframe 55,705 hrs · 33,801 cycles

F/A INTERCOM INOPERATIVE.

Part: STRAP — CRACKED (BS 312) · airframe 55,483 hrs · 33,640 cycles

E & E COMPARTMENT AT BS 312, RBL 32, WATERLINE 199. FLOORBEAM STABILIZER STRAP HAS A 0.50" CRACK. REMOVED ALL FASTNERS COMMON TO CRACK IAW SRM 51-40-02 AND SRM 53-10-51. STOPPED DRILLED A .250 HOLE AT THE END OF THE CRACK IAW SRM 53-10-51. FABRICATED REPAIR PLATE USING 2024-T3 0.040" IAW SRM 53-10-51. ALODINE, PRIME AND TOPCOAT IAW SRM 51-21-72 AND 51-21-23. INSTALLED REPAIR PLATE IAW SRM 53-10-51 AND 51-40-02. REPAIR DEMINSIONS 2.4" X 4.00".