N315US

Part: COMPRESSOR — SEIZED (WATER SYSTEM) · airframe 78,875 hrs · 35,611 cycles

HAD AN ACRID ELECTRICAL ODOR IN THE COCKPIT. REPLACED THE WATER SYSTEM AIR COMPRESSOR. FOUND SEIZED. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 78,389 hrs · 35,364 cycles

BROKEN EMERGENCY LIGHT WIRE, REPAIRED THE WIRE.

Part: SKIN — CORRODED (FRAMES 56-57) · airframe 75,496 hrs · 33,918 cycles

CORROSION ON SKIN UNDER STR 43L BETWEEN FRAME 56 & 57, PRI 541258-14AD, REV 0, 1, 2 AND ER/A 541258-14AD. BLENDED OUT CORROSION UNDER SKIN IAW 51-74-00, MININUM REMAINING THICKNESS .148.

Part: STRINGER — CORRODED (FRAMES 56-57) · airframe 75,496 hrs · 33,918 cycles

CORROSION ON STR 43L BETWEEN FRAMES 56-57. EXISTING SPLICE BETWEEN FRAMES 56-57 AND A SPLICE UNDER FRAME 54. FABRCATED STR 43L BETWEEN FRAMES 55 & 58 AND COUPLERS IAW SRM 53-00-13, FIG 201. TREATED PRIMED AND PAINTED STR IAW 51-75-12 INSTALLED STRINGER 43L IAW SRM 53-00-13.

Part: SKIN — CORRODED (FRAMES 56-57) · airframe 75,496 hrs · 33,918 cycles

CORROSION ON INSIDE SURFACE OF SKIN OTBD OF STR 42L BETWEEN FRAMES 56-57. PRI 541258-14AD, REV O,1,2. C/W PRI 541258-14AD, REV 2, STEP 9.

Part: STRINGER — CORRODED (FRAMES 56-57) · airframe 75,496 hrs · 33,918 cycles

CORROSION ON STR 42L BETWEEN 56-57. EXISTING REPAIR BETWEEN FRAMES 57-58 AND A SPLICE UNDER FRAME 53. FABRICATED STR 42L BETWEEN FRAMES 55 & 58 AND COUPLER IAW SRM 53-00-13, FIG 201. TREATED AND PRIMED AND PAINTED IAW SRM 51-75-12, INSTALLED STR 42L IAW SRM 53-00-13.

Part: STRINGER — CORRODED (41 RIGHT) · airframe 67,901 hrs · 30,183 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 41R LOCATED BETWEEN FR 28 TO FR 29 IN FORWARD CARGO COMPARTMENT; MEASURES APROX L=0.250" W=0.100" D= 0.002" PERFORMED PERMANENT REPAIR ON STRINGER 41R LOCATED BETWEEN FRAME 28 TO FRAME 29 IN FWD CARGO COMPARTMENT IAW ER/A NR 512765-14 REV ORIGINAL AND PRI 512765-14, REV 0.

Part: WEB — CORRODED (AFT CARGO BAY) · airframe 67,901 hrs · 30,183 cycles

DURING INSPECTION, FOUND CORROSION ON WEB IN AFT CARGO BAY S38L BETWEEN FR 56 AND FR 57 LOWER SURFACE. PERFORMED REPAIR ON WEB IAW ERA 513503-14, REV ORIGINAL PRI FROM REVISION N.0 TO REVISION N.2.

Part: SKIN — CORRODED (FUSELAGE) · airframe 67,901 hrs · 30,183 cycles

DURING INSPECTION, FOUND CORROSION ON SKIN, AFT CARGO BAY S38R+1.5 AND FR 64+20. PERFORMED PERMANENT REPAIR ON SKIN IAW ERA 513499-14, REV ORIGINAL AND PR I N. 513499-14 REV 0.

Part: STRINGER — CORRODED (43 LEFT) · airframe 67,901 hrs · 30,183 cycles

DURING INSPECTION, FOUND CORROSION STRINGER 43L, AFT CARGO BETWEEN FR 58 AND FR 59. PERFORMED PERMANENT REPAIR IAW SRM 53-00-13, PARA 4.A FIG 201, PAGES 202 TO 208.

Part: STRINGER — CORRODED (CARGO BAY) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 44 BETWEEN FR 31 TO FR 32 AND Y 0 FWD CARGO COMPARTMENT. PERFORMED REPAIR ON STRINGER 44 IAW ER/A NR 512769-14. REV ORIGINAL AND PRI 512769-14, REV.

Part: STRINGER — CORRODED (35 RIGHT) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 35R AFT CARGO COMP FR 64+20". REPLACED STRINGER 35R IAW SRM 51-72-11.

Part: STRINGER — CORRODED (41 RIGHT) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 41R BETWEEN FR 32 TO FR 33 FORWARD CARGO BAY. PERFORMED PERMANENT REPAIR ON STRINGER 41R IAW ER/A NR 512764-14, REV ORIGINAL AND PRI 512764-14 REV NR 0 AND REV NR 1.

Part: TRUNNION — WORN (LT FLAP DRIVE) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND SEVERE WEAR ON LOWER SURFACE OF LT INBD FLAP DRIVE TRUNNION, MEASURE THE OUTSIDE DIAMETER OF THE TRUNNION SHAFT IS:2.864". REPLACED LT INBD FLAP DRIVE TRUNNION IAW ER/A 512773-14AD REV ORIGINAL AND PRI NR 512773-14AD FROM REV NR 0 AND REV.

Part: STRINGER — CORRODED (35 RIGHT) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 35R, AFT CARGO BAY FR 64+15". REPLACED STRINGER 35R, IAW SRM 51-72-11.

Part: STRINGER — CORRODED (43 LEFT) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 43L, AFT CARGO BAY BETWEEN FR 64 AND STR 65. PERFORMED PERMANENT REPAIR ON STRINGER 43L IAW SRM A320 53-00-13, FIG 201 (SHEET 2) PAGES 211 TO 212.

Part: STRINGER — CORRODED (FWD CARGO BAY) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 44 LOCATED BTW FR 24 TO FR 24A IN FORWARD CARGO COMPARTMENT. PERFORMED REPAIR ON STRINGER 44 IAW ER/A 512766-14 REV.

Part: SKIN — CORRODED (FUSELAGE) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND SEVERE CORROSION ON INTERNAL SURFACE SKIN LOCATED BETWEEN FR 33 TO FR 34 AND STRINGERS 39R TO 41L IN FWD CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR ON INTERNAL SURFACE SKIN IAW ER/A 512771-14, REV ORIGINAL AND PRI 512771-14, REV O;

Part: STRINGER — CORRODED (FWD CARGO) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 41R LOCATED BETWEEN FR 31 TO FR 32 IN FORWARD CARGO COMPARTMENT. PEFORMED REPAIR ON STRINGER 41R IAW ER/A NR 512772-14, REV ORIGINAL AND PRI 512772-14 REV O;

Part: STRINGER — CORRODED (43 RIGHT) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 43R LOCATED BTW FR 32 TO FR 33 IN FORWARD CARGO COMPARTMENT; MEASURES APROX. POINT 1 L=0.100" W=0.098" D=0.001"; POINT 2 L=0.105" W=0.097" D=0.001", POINT 3 L=0.095 W=0.088" D=0.001"; REPAIRED STRINGER 43R LOCATED BETWEEN FR 32 TO FR 33 IN FORWARD CARGO COMPARTMENT IAW SRM 53-00-13, FIG 201 PARA 4A STEP 6, SHEET 2 AND DWG D53231626 IDENTIFIED PERMANENT.

Part: WEB — CORRODED (CARGO BAY) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON WEB LOCATED BETWEEN FR 51 TO FR 52 STR 38R IN AFT CARGO COMPARTMENT (AFTER REMOVED PROFILE LOC BETWEEN FR 48 AND FR 52A STR 38R AFT CC PERFORMED VISUAL INSPECTION) REPLACED WEB LOCATED BETWEEN FR 51 TO FR 52 STR 38R IN AFT CARGO COMPARTMENT IAW SRM 51-72-11.

Part: STRINGER — CORRODED (40 RIGHT) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 40R LOCATED AT LEVEL FR 34 IN FWD CARGO COMPARTMENT SSI 532180; MEASURES APROX. L=0.175" W=0.120"D=0.001" PERFORMED PERMANENT REPAIR ON STRINGER 40R LOCATED AT LEVEL FR34 IN FORWARD CARGO COMPARTMENT IAW SRM A320 53-00-13, FIG 201, PARA 4A. THIS JOB MUST BE INSPECTED AT INSPECTION START POINT FROM ACFT FIRST FLIGHT 60,000 FC/FH NOT RELEVANT, SMP FROM ACFT FIRST FLIGHT 60,000 FC/FH NOT RELEVANT IAW SRI A320 53-00-13-2-001-00, TABLE 201, PARA 3.A TABLE 203.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 30 AND BETWEEN STR 43L TO STR 43R IN FORWARD CARGO COMPARTMENT. MEASURES APROX. L=3.00" W=0.350" D=0.002". REPLACED CLEAT AT FR 30 BETWEEN STR 43L TO STR 43R IN FORWARD CARGO COMPARTMENT IAW SRM 51-72-11.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 33 AND BETWEEN STR 42L TO STR 43L IN FORWARD CARGO COMPARTMENT. MEASURES APROX. L=0.800" W=0.300" D=0.002". REPLACED CLEAT AT FR 33 AND BETWEEN STR 42L TO STR 43L IN FWD CARGO COMPARTMENT IAW SRM 51-72-11.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 34 AND BETWEEN STR 42R TO STR 43R IN FWD CARGO COMPARTMENT. MEASURES APROX. L=2.00" W=0.300" D=0.003" REPLACED CLEAT AT FR 34 AND BETWEEN STR 42R TO STR 43R IN FORWARD CARGO COMPARTMENT IAW SRM A320 51-72-11 AND DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 67,879 hrs · 30,169 cycles

DURING INSP, FOUND CORROSION ON CLEAT AT FR 32 AND BETWEEN STR 41R TO STR 42R IN FWD CARGO COMPARTMENT SSI 532180; MEASURES APROX L=3.5" W=0.300" D=0.003" REPLACED CLEAT AT FR 32 AND BTW STR 41R TO STR 42R IN FORWARD CARGO COMPARTMENT IAW SRM 51-72-11.

Part: COVER — CORRODED (FUSELAGE) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON COVER SHEET, AFT CARGO COMP. DOOR (L=1.900"; W=0.155" AND DEPT=0.001") REPLACED COVER SHEET, AFT CARGO COMPT. DOOR IAW SRM 51-72-11 AND DWG D53475500.

Part: STRINGER — WORN (42 LEFT) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND WEAR ON STRINGER 42L, AFT COMP BETWEEN FR 57 AND FR 58. PERFORMED PERMANENT REPAIR ON STRINGER 42L BETWEEN FR 57 TO FR58 AFT CARGO COMP. SRM 53-00-13, PARA 4A, FIGURE 201 (SHEET 3) PAGE 213/214.

Part: ATTACH FITTING — CORRODED (CARGO BAY) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT LOCATED AT FR 29 AND BETWEEN STR 41R TO STR 42R IN FWD CARGO COMPARTMENT; MEASURES APROX L=1.700" W=0.300" D=0.002". REPLACED CLEAT LOCATED AT FR 29 AND BETWEEN STR 41R TO STR 42R IN FWD CARGO COMPARTMENT IAW SRM 51-72-11.

Part: STRINGER SPLICE — CORRODED (38 RIGHT) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER SPLICE, AFT CARGO BAY STR 38R, FR 51 (L=0.026", W=0.017" AND D=0.003") WC 5320-5010. REPLACED STRINGER SPLICE LOC STR 38R AT LEVEL OF FR 51 AFT CARGO COMP IAW SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND AFT CABIN UTILITY ARE FLOOR SUPPORT BETWEEN FR 64-66,Y765 UPPER SURFACE FLANGE HAS CORROSION. BLENDED AREA L=1.8",W=1.8"D=.034", MAX ALLOWABLE D=.027" AND FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15 AND SRM 51-74-00. REPLACED FLOOR SUPPORT IAW SRM 51-42-11, SRM 51-44-11 AND TRM 53-21-01, RESTORED FINISH IAW SRM 51-75-12.

Part: ATTACH FITTING — CORRODED (CARGO BAY) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 33 AND BETWEEN STR 41R TO STR 42R IN FORWARD CARGO COMPARTMENT; MEASURES APROX L=2.00", W=0.310", D=0.002". REPLACED CLEAT AT FR 33 AND BETWEEN STR 41R TO STR 42R IN FWD CARGO COMPARTMENT IAW SRM 51-72-11.

Part: ATTACH FITTING — CORRODED (CARGO BAY) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 33 AND BETWEEN STR 40R TO STR 41R IN FWD CARGO COMPARTMENT; MEASURES APROX. L=0.750",W=0.250", D=0.002". REPLACE CLEAT AT FR 33 AND BETWEEN, STR 40R TO STR 41R IN FWD CARGO COMPARTMENT IAW SRM 51-72-11.

Part: ATTACH FITTING — CORRODED (CARGO BAY) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 32 AND BETWEEN STR 38R TO STR 39R IN FORWARD CARGO COMPARTMENT L=0.800", W=0.250", D=0.002" MEASURES APPROX SSI 532180. REPLACED CLEAT AT FR 32 AND BETWEEN STR 38R TO STR 39R IN FWD CARGO COMPARTMENT IAW SRM 51-72-11.

Part: FITTING — CORRODED (CABIN) · airframe 67,879 hrs · 30,169 cycles

CORROSION ON CORNER FITTING LOCATED FR 68 RT SIDE AFT CABIN FLOOR STRUCTURE. L=4" W=1.25" D=0.003" APPROX. REPLACED CORNER FITTING LOCATED FR 68 RT SIDE AFT CABIN FLOOR STRUCTURE IAW SRM 51-72-11.

Part: ATTACH FITTING — CORRODED (CARGO BAY) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 33 AND BETWEEN STR 43R TO STR 43L IN FORWARD CARGO COMPARTMENT SSI 532180; MEASURES APROX L=3.5" W=0.375" D=0.002". REPLACED CLEAT AT FR 33 AND BTW STR 43R TO STR 43L IN FORWARD CARGO COMPARTMENT IAW SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON LOWER SILL LOCATED BTW FR 66 AND FR 68 RT SIDE AFT CABIN FLOOR STRUCTURE L=2" W=1.5" D=0.003" APPROX. SSI 534147. REPLACED LOWER SILL AND FASTENERS LOCATED BETWEEN FR 66 AND FR 68 RT SIDE AFT CABIN FLOOR STRUCTURE IAW SRM 51-72-11.

Part: ATTACH FITTING — CORRODED (CARGO BAY) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 31 AND BETWEEN STR 41R TO STR 42R IN FWD CARGO COMPARTMENT SSI 532180; MEASURES APROX. L=1.300" W=0.350" D=0.003". REPLACED CEAT AND FASTENERS LOCATED FR 31 AND BETWEEN STR 41R TO STR 42R IN FORWARD CARGO COMPARTMENT IAW SRM 51-72-11.

Part: ATTACH FITTING — CORRODED (CARGO BAY) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 32 AND BETWEEN STR 43L TO STR 43R IN FWD CARGO COMPARTMENT; MEASURES APROX. L=3.00" W=0.375" D=0.003". REPLACED CLEAT AT FR 32 AND BETWEEN STR 43L TO STR 43R IN FORWARD CARGO COMPARTMENT IAW SRM 51-72-11.

Part: ATTACH FITTING — CORRODED (CARGO BAY) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 32 AND BETWEEN STR 42L TO STR 43L IN FORWARD CARGO COMPARTMENT; MEASURES APROX. L=1.00" W=0.310" D=0.002". REPLACED CLEAT AT FR 32 AND BETWEEN STR 42L TO STR 43L IN FORWARD CARGO COMPARTMENT IAW SRM 51-72-11.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 31 AND BETWEEN STR 42R TO STR 43R IN FORWARD CARGO COMPARTMENT. MEASURES APROX. L=0.900"W=0.340" D=0.001". REPLACED CLEAT AT FR 31 AND BTW STR 42R TO STR 43R IN FWD CARGO COMPARTMENT IAW SRM 51-72-11.

Part: STRINGER — CORRODED (25 RIGHT) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 25R, BULK CARGO COMP BETWEEN FR 64 AND FR 65. REPLACED STRINGER 25R LOCATED BULK CARGO COMPARTMENT BETWEEN FR 64 TO FR 67 IAW SRM 51-72-11.

Part: ATTACH FITTING — CORRODED (CARGO BAY) · airframe 67,879 hrs · 30,169 cycles

DURING INSPETION, FOUND CORROSION ON CLEAT AT FR 32 AND BETWEEN STR 42R TO STR 43R IN FORWARD CARGO COMPARTMENT; MEASURES APROX. L=3.00" W=0.375" D=0.003". REPLACED CLEAT AT FR 32 AND BTW STR 42R TO STR 43R IN FWD CARGO COMPARTMENT IAW SRM 51-72-11.

Part: ATTACH FITTING — CORRODED (CARGO BAY) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 32 AND BETWEEN STR 40R TO STR 41R IN FWD CARGO COMPARTMENT; MEASURES APPROX. L=0.800" W=0.300" D=0.002". REPLACED CLEAT AT FR 32 AND BETWEEN STR 40R TO STR 41R IN FWD CARGO COMPARTMENT IAW SRM A320 51-72-11.

Part: ATTACH FITTING — CORRODED (CARGO BAY) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 31 AND BETWEEN STR 43R TO STR 44 IN FORWARD CARGO COMPARTMENT; MEASURES APROX. L=0.750" W=0.210" D=0.002". REPLACED CLEAT AT FR 31 AND BETWEEN STR 43R TO STR 44 IN FORWARD CARGO COMPARTMENT IAW SRM 51-72-11.

Part: ATTACH FITTING — CORRODED (CARGO BAY) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 30 AND BETWEEN STR 41R TO STR 42R IN FORWARD CARGO COMPARTMENT; MEASURES APROX. L=1.500" W=0.300" D=0.002". REPLACED CLEAT ON FWD CARGO COMP FR 30 BETWEEN STR 41R AND STR 42R IAW SRM 51-72-11.

Part: ATTACH FITTING — CORRODED (CARGO BAY) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 33 AND BETWEEN STR 42R TO STR 43R IN FORWARD CARGO COMPARTMENT SSI 532180; MEASURES APROX. L=0.750" W=0.210 " D=0.002". REPLACED CLEAT AND FASTENERS LOCATED FR 33 AND BETWEEN STR 42R TO STR 43R IN FORWARD CARGO COMPARTMENT IAW SRM 51-72-11.

Part: ATTACH FITTING — CORRODED (CARGO BAY) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 31 AND BETWEEN STR 39R TO STR 40R IN FWD CARGO COMPARTMENT SSI 532180; MEASURES APROX. L=0.210" W=0.105" D=0.002" REPLACED CLEAT AT FR 31 AND BETWEEN STR 39R TO STR 40R IN FWD CARGO COMPARTMENT IAW SRM A320 51-72-11.

Part: ATTACH FITTING — CORRODED (CARGO BAY) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 34 AND BETWEEN STR 41R TO STR 42R IN FWD CARGO COMPARTMENT SSI 532180; MEASURES APROX L=2.100" W=0.300" D=0.002". REPLACED CLEAT AND FASTENERS LOCATED FR 34 AND BETWEEN STR 41R TO STR 42R IN FORWARD CARGO COMPARTMENT IAW SRM 51-72-11.

Part: ATTACH FITTING — CORRODED (CARGO BAY) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 31 AND BETWEEN STR 42L TO STR 43L IN FORWARD CARGO COMPARTMENT; MEASURES APROX. L=1.500" =0.800" D=0.002". REPLACED CLEAT AND FASTENERS LOCATED FR 31 AND BETWEEN STR 42L TO STR 43L IN FWD CARGO COMPARTMENT IAW SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON FLOORBEAM. REPLACED FLOORBEAM AND FASTENERS IAW SRM A320 51-72-11.

Part: CLEAT — CORRODED · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT. REPLACED CLEAT IAW SRM 51-72-11.

Part: FLOORBEAM — CORRODED (BS 1225) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON FLOORBEAM BS 1225. REPLACED FLOORBEAM IAW SRM 51-72-11.

Part: FLOORBEAM — CORRODED (BS 1162) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON FLOORBEAM BS 1162. REPLACED FLOORBEAM IAW SRM 51-72-11.

Part: CLEAT — CORRODED (FUSELAGE) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 30 AND BETWEEN STR 42L TO STR 43L. REPLACED CLEAT IAW SRM A320 51-72-11.

Part: FLOORBEAM — CORRODED (BS 1292) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON FLOORBEAM BS 1292. REPLACED FLOORBEAM AND FASTENERS, IAW SRM 51-72-11.

Part: CLEAT — CORRODED · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT LOCATED AT FR 28 AND BETWEEN STR 41L TO STR 42L IN FWD CARGO COMPARTMENT. REPLACED CLEAT IAW 51-72-11.

Part: CLEAT — CORRODED (FUSELAGE) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 30 AND BETWEEN STR 42R TO STR 43R. REPLACED CLEAT IAW SRM 51-72-11.

Part: CLEAT — CORRODED (FUSELAGE) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT FR 29 AND BETWEEN 42R TO STR 43R IN FORWARD CARGO COMPARTMENT. MEASURE APROX. L=3.500" W=0.350" D=0.002". REPLACED CLEAT AND FASTENERS IAW SRM 51-72-11 AND DWG D53231626.

Part: CLEAT — CORRODED (FUSELAGE) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 29 AND BETWEEN STR 43R TO STR 44 IN FWD CARGO COMPARTMENT. MEASURE APROX L=2.100" W=0.350" D=0.002". REPLACED CLEAT AND FASTENER AT FR 29 AND BETWEEN STR 43R TO STR 44 FWD CARGO COMPARTMENT IAW SRM 51-72-11.

Part: CLEAT — CORRODED (FUSELAGE) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT FR 28 AND BETWEEN STR 43R TO STR 44 IN FWD CARGO COMPARTMENT. MEASURE APROX L=1.750" W=0.600" D=0.003". REPLACED CLEAT IAW SRM 51-72-11 .

Part: STRUCTURE — CORRODED (CABIN FLOOR) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON BEAM -Y765 LOCATED FR 65+21" AFT CABIN FLOOR STRUCTURE L=0.5" W=0.025" D=0.001" APROX SSI 534147. REPLACED BEAM -Y765 LOCATED FR 65+21" AFT CABIN FLOOR STRUCTURE IAW SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON FLOORBEAM -Y1732 LOCATED FR.65+19.5" RT SIDE AFT CABIN FLOOR STRUCTURE L=1" W=0.5" D=0.002" APROX. REPLACED FLOORBEAM -Y1732 LOCATED FR 65 TO FR 66 RT SIDE CABIN FLOOR STRUCTURE IAW SRM 51-72-11.

Part: FITTING — CORRODED (DOOR SILL) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON CENTER FITTING, FWD CABIN LT ENTRY DOOR LOWER SILL, REPLACED CENTER FITTING, FWD CABIN LT ENTRY DOOR LOWER SILL IAW SRM A320 51-72-11, DWG D53112198.

Part: FLOOR SUPPORT — CORRODED · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT FR 66 AND FR 68. REPLACED FLOOR SUPPORT IAW SRM 51-72-11.

Part: CLEAT — CORRODED (FUSELAGE) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 32 AND BETWEEN STR 41L TO STR 42L IN FWD CARGO COMPARTMENT; MEASURES APROX. L=0.800" W=0.300" D=0.002" REPLACED CLEAT AT FR 32 AND BETWEEN STR 41L TO STR 42L IN FORWARD CARGO COMPARTMENT IAW SRM A320 51-72-11.

Part: CLEAT — CORRODED (FUSELAGE) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 30 AND BETWEEN STR 41L TO STR 42L IN FWD CARGO COMPARTMENT. REPLACED CLEAT AT FR 30 AND BETWEEN STR 41L TO STR 42L IN FORWARD CARGO COMPARTMENT IAW SRM 51-72-11.

Part: FITTING — CORRODED (FUSELAGE) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON CENTER FITTING FWD PAX CABIN BETWEEN FR 16+5" TO FR 19+5" AND AT LEVEL OF STR 23R. L=0.230", W=0.113", D=0.002". REPLACED CENTER FITTING IAW SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK Y1292 LOCATED BETWEEN FR 41 TO FR 47 AND IS BEYOND ALLOWABLE DAMAGE LIMITS IAW ROUTINE CARD 2500-2031. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG D53371000.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK -Y1292 LOCATED BETWEEN FR 36 TO FR 41 AND IS BEYOND ALLOWABLE DAMAGE LIMITS IAW ROUTINE CARD 2500-2031. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG D53372500.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 67,879 hrs · 30,169 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK Y1292 LOCATED BETWEEN FR 36 TO FR 41 AND IS BEYOND ALLOWABLE DAMAGE LIMITS IAW ROUTINE CARD 2500-2031. REPLACED SEAT TRACK IAW SRM 51-72-11, AND DWG D57130146.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,546 hrs · 30,016 cycles

DURING NON-ROUTINE CHECK, FOUND BATTERY FAULT FOR EPSU 13WL CHECK. MX REPLACED EPSU 13WL BATTERY PACK WITH SERVICEABLE UNIT AND FUNCTIONAL CHECK WAS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,798 hrs · 29,665 cycles

DURING NON ROUTINE CHECK, FOUND RIGHT EPSU BATTERY FAIL ON EMERGENCY LIGHT TEST FOR SERVICE CHECK. MX REPLACED BATTERY PACK AND FUNCTIONAL CHECK WAS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,595 hrs · 29,565 cycles

DURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED LIGHT ASSEMBLY AND TESTED NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,469 hrs · 29,502 cycles

DURING NON ROUTINE CHECK, FOUND FWD EPSU BATTERY FAULTED. MAINTINANCE REPLACED EPSU BATTERY AND FUNCTIONAL CHECK WAS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,914 hrs · 29,208 cycles

LEFT EMERGENCY BATTERY FAILED CHECK REMOVED AND REPLACED BATTERY IAW A319/320 MM 33-51. CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING A NON ROUTINE CHECK, MAINTENANCE FOUND AFT LEFT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY AND FUNCTIONAL TEST WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — DAMAGED (CABIN) · airframe 63,322 hrs · 27,957 cycles

DURING EMERGENCY LIGHT TEST, MAINTENANCE FOUND ROW 8C PATH LIGHT WAS INOPERATIVE. MAINTENANCE REPAIRED A WIRE AT THE CONNECTOR AND LIGHT NOW TESTS OK.

Part: EPSU — INOPERATIVE (CABIN) · airframe 62,429 hrs · 27,541 cycles

DURING EMERGENCY LIGHT TEST PATH LIGHTS SEAT ROW 16, 17, 21, 22, AND 23 WERE INOP. REPLACED EPSU AND TESTS OK.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 61,958 hrs · 27,345 cycles

FWD CARGO FLOOR PANEL 131EF DELAMINATED. REMOVED PANEL IAW AMM 53-22-14. FABRICATED NEW PANEL ON TRAVELER T11/874676 PER DWG 3D25-37705. INSTALLED NEW PANEL AND SEALED IAW AMM 53-22-14. DAMAGE DIM: L=4" W=3 RETAIN FOR RECORDS.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 61,958 hrs · 27,345 cycles

FWD CARGO FLOOR PANEL 131AF DELAMINATED. REMOVED AND REPLACED FLOOR PANEL WITH NEW FABRICATED PANEL PER AMM 53-22-14.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 61,958 hrs · 27,345 cycles

AFT PIT FLOOR PANEL 151DF IS DELAMINATED 10X 3 INCH AREA. REMOVED AND REPLACED FLOOR PANEL WITH NEW FABRICATED PANEL PER MM 53-42=14 PB401.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 61,958 hrs · 27,345 cycles

AFT PIT FLOOR PANEL 151LF HAS SEVERAL PUNCTURES AND IS DELAMINATED, 6 X 4 INCH AREA. REMOVED FLOOR PANEL 151LF IAW AMM53-42-14-000-001. FABBED NEW PANEL IAW STAM TRAVELER T11/874678 BATCH 1886727 IAW DWG 3D25 -37705. INSTALLED PANEL IAW MM 53-42-14 PB401.

Part: EPSU — INOPERATIVE (CABIN) · airframe 59,875 hrs · 26,421 cycles

DURING A NON ROUTINE CHECK, EMERGENCY LIGHT FAILED TEST. REPLACED FWD AND AFT EPSU AND PERFORMED SUCCESSFUL TEST. A/C RETURNED TO SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 68,260 hrs · 30,355 cycles

ON WALK AROUND F/O FOUND TWO SMALL DENTS IN LT AFT FUSELAGE BELOW PAX WINDOWS. INSPECTED DENTS IAW SRM 53-41-11, PG 124. FOUND DENT TO BE WITHIN LIMITS. NO CRACKS FOUND IAW DIAGRAM 103. HFEC DENT AT FR 61 -FR 62 STR 21L-22L IAW NTM 51-10-08, PT 6, NO CRACK NOTED. FOUND SKIN GOUGED, BLENDED AREAS IAW SRM 51-73-00. HFEC IAW NTM 51-10-08, PT 6 NO CRACK NOTED. FOUND TO BE WITHIN LIMITS IAW SRM 53-41-11, DIA 101, TREATED AND PRIMED IAW SRM 51-21-11. PAINTED IAW SRM 51-75-12. OK TO CONTINUE MONITOR.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 58,726 hrs · 25,973 cycles

DURING NON ROUTINE CHECK, FOUND EMERGENCY FLOOR PATH LIGHT AT SEAT 11 INOPERATIVE. MX REPLACED SPLICE AND PERFORMED FUNCTIONAL TEST. TEST WAS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,251 hrs · 25,788 cycles

DURING A NON ROUTINE CHECK, FOUND EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY BATTERY PACK AND PERFORMED FUNCTIONAL CHECK GOOD. ACFT RETURNED TO SERVICE.

Part: O-RING — LEAKING (HYD SYSTEM) · airframe 54,363 hrs · 24,090 cycles

AT CRUISE (FL360) ECAM MESSAGE "YELLOW HYD SYSTEM LO", COMPLIED WITH COM PROCEDURES. ACFT LANDED UNEVENTFULLY. REPLACED O-RING ON YELLOW HP MANIFOLD, NO LEAKS NOTED. (S)

Part: ACM — SEIZED (A/C BAY) · airframe 36,706 hrs · 15,974 cycles

FLIGHT ATTENDANT REPORTED SMOKE IN AFT CABIN. CAPTAIN NOTICED LIGHT SMOKE IN THE COCKPIT. SMOKE CLEARED WITHIN A FEW MINUTES. AFTER LANDING, RECEIVED PACK 1 OVERHEAT WARNING. FOUND NR 1 AIR CYCLE MACHINE SEIZED. REPLACED THE NR 1 AIR CYCLE MACHINE. LEAK AND OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FITTING — CORRODED · corrosion level 2 · airframe 35,392 hrs · 15,391 cycles

During "M" check found corrosion in three holes of inner rear spar anchorage fitting. Repaired per EA 32-184839.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING EMERGENCY LIGHT TEST, RECEIVED EPSU INT LOAD AFT L MESSAGE. MAINTENANCE REPLACED BATTERY PACK AND POWER SUPPLY, OPERATIONAL CHECK OK.

Part: INDICATION — MALFUNCTION (CARGO DOOR)

DURING TAKEOFF, RECEIVED AFT CARGO DOOR OPEN INDICATION. TAKEOFF WAS ABORTED AT ABOUT 50 KNOTS, RETURNED TO GATE. DOOR WAS RECYCLED AND INDICATION CHECKED OK.

Part: INDICATION — MALFUNCTION (CARGO DOOR)

DURING TAKEOFF, AFT CARGO DOOR ECAM MESSAGE APPEARED AT ABOUT 30 KNOTS. TAKEOFF WAS ABORTED AT ABOUT 50 KNOTS. DOOR HANDLE WAS CYCLED AND INDICATION CHECKED OK.

Part: SILL — CORRODED (BS 32571)

DURING C-CHECK, FOUND CORROSION DAMAGE TO THE UMBRAIL SILL AT FRAME 68, Y+1292. REPAIRED PER EA 32-120561.

Part: O-RING — LEAKING (LT SPOILER ACT)

EN ROUTE, RECEIVED HYD G-RSVR LO LVL MESSAGE. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT AT ORIGINAL DESTINATION. MAINTENANCE REPLACED LEAKING O-RING SEAL ON THE NR 1 SPOILER ACTUATOR FILTER HOUSING, LEAK AND OPERATIONAL CHECK OK.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING MAINTENANCE, THE EMERGENCY LIGHTS TEST FAILED INT LOADS AFT L AND COMM AFT L. REPLACED POWER SUPPLY, OPERATIONAL CHECK OK.

Part: STRINGER — CORRODED (FS 14300-14834)

DURING IL CHECK, FOUND CORROSION ON STR 43L BETWEEN FRAMES 33 AND 34. REPAIRED STRINGER PER EA 32-104252.

Part: INDICATION — MALFUNCTIONED (LANDING GEAR)

DURING CLIMBOUT AFTER LANDING GEAR RETRACTION, RECEIVED 'L/G GEAR NOT UPLOCKED' AND 'L/G DOORS NOT CLOSED' MESSAGES. CYCLED LANDING GEAR HANDLE AND ALL INDICATIONS NORMAL. AIRCRAFT CONTINUED TO ORIGINAL DESTINATION AND LANDED WITHOUT INCIDENT. CORRECTIVE ACTION WILL BE ACCOMPLISHED DURING 'C' CHECK.

Part: CLAMP — LOOSE (LT WING)

DURING CLIMBOUT, RECEIVER 'AIR L WING LEAK' MESSAGE. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND DIVERTED TO MEM DUE TO ICING CONDITIONS AT ORIGINAL DESTINATION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REINSTALLED CLAMP ON EXTERNAL AIR DUCT. OPS AND LEAK CHECK OK.

Part: IDG — FAILED (NR 2 ENGINE)

DURING CLIMBOUT, RECEIVED NR 2 ENGINE IDG FAULT ACCOMPANIED WITH THE GENERATOR DROPPING OFF LINE. CREW DISCONNECTED NR 2 IDG PER COCKPIT OPERATING MANUAL PROCEDURE. DUE TO THE APU PREVIOUSLY ON MEL, RETURNED TO SEA AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 IDG, OPERATIONAL CHECK OK.

Part: WATER LINE — RUPTURED (AFT RIGHT LAV)

DURING CLIMBOUT FROM MIA, THE RIGHT AFT LAVATORY DEVELOPED AN UNCONTROLLABLE WATER LEAK. AIRCRAFT DIVERTED TO MCO AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE AFT RIGHT LAV WATER SUPPLY LINE. LEAK AND OPERATIONAL CHECK OK.

Part: FIRE LOOP — MALFUNCTIONED (NR 2 ENGINE)

DURING TAKEOFF WITH ENG NR 2 FIRE LOOP 'B' FAULT INDICATION ON MEL, RECEIVED NR 2 ENGINE FIRE WARNING. ENGINE WAS SHUT DOWN AND AIRCRAFT RETURNED TO DTW WHERE AN UNEVENTFUL LANDING TOOK PLACE. THE NR 2 PYLON LOOP 'B' AND CORE LOOP SUPPORT WERE REPLACED. THE SYSTEMS CHECKED OK AND THE AIRCRAFT WAS DEEMED READY FOR SERVICE.