N801FR

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 25,982 hrs · 3,390 cycles

BATTERY PACK 12W FAILED CAPACITY CHECK IAW TASK CARD A332204-02. REPLACED ESPU 12WL IAW AMM 33-51-38, PB 401.

Part: ENCODER — FAULTY (CABIN) · airframe 24,902 hrs · 12,996 cycles

REFERENCE HEAVY MAINTENANCE NON ROUTINE N0526. EMERGENCY LIGHT OPERATIONAL TEST FAILED WITH A CLASS 1 MESSAGE EPSU (11WL) AND (12WL). FOUND HIGH AND LOW CODING SWITCHES ON TERMINATION/CONNECTION BOX 3000RH8-DEU B TO BE CODED ONE NOTCH OFF. SET CODING POTENTIOMETERS TP PROPER POSITION IAW A318 AMM 23-73-47-400-001. OPERATIONAL CHECK GOOD IAW A318 AMM 33-51-00-710-001.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,902 hrs · 12,996 cycles

REFERENCE HEAVY MAINTENANCE NON ROUTINE N0499. DURING TEST FORWARD EMERGENCY LIGHT 61WL WOULD NOT ILLUMINATE. TROUBLESHOT SYSTEM IAW A318 TSM 25-62-00-810-813. FOUND TWO BULBS BURNT OUT. REPLACED BULBS IAW A318 AMM 33-51-15 PAGE BLOCK 401. OPERATIONAL TEST GOOD IAW A318 AMM 33-51-00-710-001.

Part: FLAP — DAMAGED (RT WING) · airframe 24,902 hrs · 12,996 cycles

REFERENCE HEAVY MAINTENANCE NON ROUTINE N0001. TEMPORARY REPAIR TO LIGHTNING STRIKE DAMAGE ON RIGHT WING OUTBOARD FLAP TRAILING EDGE 4.25 INCHES FROM OUTBOARD EDGE AND 3.5 INCHES FROM TRAILING EDGE. DAMAGE MEASURED 1.75 X 0.50 INCH. INSTALLED PERMANENT REPAIR IAW A318 SRM 57-53-00 PAGES 256 AND 257, 51-75-12 PARAGRAPH 4, AND 51-21-11 PAGE 5.

Part: COMPUTER — INOPERATIVE (ELEVATOR AILERON) · airframe 20,562 hrs · 10,649 cycles

PILOT REPORTED AFTER TAKEOFF THE AIRCRAFT DID NOT AUTO TRIM, CONSTANT FORWARD PRESSURE WAS REQUIRED TO MAINTAIN DESIRED PITCH. SAME RESULT ON BOTH STICKS. AIRCRAFT TRIMMED NOSE UP IF NO STICK INPUT RUNAWAY NOSE UP. MAINTENANCE REMOVED AND REPLACED THE NR 2 ELEVATOR AILERON COMPUTER AND PERFORMED OPERATIONAL CHECK, REFERENCE AMM 27-93-34 PB 401. MAINTENANCE ALSO PERFORMED AN OPERATIONAL TEST OF THE TRIMMABLE HORIZONTAL STABILIZER ACTUATOR ELECTRICAL CONTROL, REFERENCE AMM 27-96-00-710-002 AND RETAINED LAND CAT III B, REFERENCE AMM 22-97-00-710-001.

Part: FITTING — OUT OF ADJUST (GIRT BAR) · airframe 19,082 hrs · 9,852 cycles

DURING C4 C-CHECK, INSPECTION NOTED THE R2 DOOR ARMED HANDLE WAS SPONGY WHEN IN THE ARMED POSITION. MAINTENANCE ADJUSTED THE R2 GIRT BAR FITTING AND PERFORMED OPERATION CHECK IN ACCORDANCE WITH A318 AMM 52-13-00-820-001.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 19,082 hrs · 9,852 cycles

DURING C4 C-CHECK, INSPECTION NOTED THAT THE EMERGENCY LIGHT TEST THROUGH THE CENTRALIZED FAULT DISPLAY UNIT FAILED OPERATIONAL CHECK. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT BATTERY IN ACCORDANCE WITH AMM 33-51-38-000-001.

Part: HOOK — WORN (ZONE 800) · airframe 19,082 hrs · 9,852 cycles

DURING C4 C-CHECK, INSPECTION NOTED THAT DURING INSTALLATION OF THE ESCAPE SLIDE THE L2 DOOR HANDLE WAS ABLE TO MOVE INTO THE CLOSED POSITION BEFORE THE DOOR WAS CLOSED. MAINTENANCE REMOVED AND REPLACED THE DOOR HOOK IN ACCORDANCE WITH AMM 52-13-21-420-052.

Part: HINGE FITTING — GOUGED (NR 3 SPOILER) · airframe 19,082 hrs · 9,852 cycles

DURING C4 C-CHECK, INSPECTION NOTED THE RIGHT NR 3 SPOILER ANTI-ROTATION WEB FLAT WAS GOUGED. MAINTENANCE REPAIRED THE DAMAGE IN ACCORDANCE WITH ENGINEERING AUTHORIZATION A8-57R-30776.

Part: HINGE FITTING — GOUGED (NR 4 SPOILER) · airframe 19,082 hrs · 9,852 cycles

DURING C4 C-CHECK, INSPECTION NOTED THE RIGHT NR 4 SPOILER ANTI-ROTATION WEB FLAT WAS GOUGED. MAINTENANCE REPAIRED THE DAMAGE IN ACCORDANCE WITH ENGINEERING AUTHORIZATION A8-57R-30776.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 15,885 hrs · 8,185 cycles

FLIGHT CREW REPORTED EPSU "13WL" AFT LEFT MESSAGE. REPLACED EPSU BATTERY AT 13WL LOCATION IAW AMM 33-51-38-400-002. OPS CHECK GOOD.

Part: OXYGEN MASK — NO TEST (CABIN) · airframe 13,570 hrs · 6,977 cycles

WHILE PERFORMING MASK DROP TEST, ROWS 15 AND AFT ON BOTH SIDES, 7, 8, AND 9 RT SIDE, R2 DOOR AND C LAV DID NOT DROP COMPLETELY. RESET MASKS AND PERFORMED TEST AGAIN IAW AMM 35-23-00-710-001. OPS CHECKED GOOD.

Part: WEB — CORRODED (FUSELAGE) · airframe 13,570 hrs · 6,977 cycles

DURING C-3 CHECK, INSPECTION REPORTED RT SIDE CABIN FLOOR WEB 69 AND 70 HAD VERY LIGHT CORROSION AT NUT PLATES, MOSTLY ON LWR SIDE. REPLACED SHEAR PLATE IAW SRM 51-42-11.

Part: SHEAR PLATE — CORRODED (CABIN FLOOR) · corrosion level 2 · airframe 13,570 hrs · 6,977 cycles

DURING C-3 CHECK, INSPECTION REPORTED LT SIDE OF CABIN FLOOR WEB 69 AND 70 HAD VERY LIGHT CORROSION AT NUT PLATES, MOSTLY ON LWR SIDE. REPLACED SHEAR PLATE IAW SRM 51-42-11.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,570 hrs · 6,977 cycles

DURING C-3 CHECK, INSPECTION REPORTED FLOOR PANEL 262FF AT R-2 DOOR CORRODED ON BOTTOM OF PANEL. REPLACED FLOORBOARD 262FF IAW AMM 53-42-12-400-001.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 13,570 hrs · 6,977 cycles

DURING C-3 CHECK, INSPECTION REPORTED FWD SPLICE OF R2 DOOR SILL HAD TWO DOUBLE DRILLED HOLES, ONE COMPLETELY THROUGH THE FWD FLOORBEAM. REPLACED DAMAGED FLOORBEAM IAW SRM 51-42-11.

Part: RIB — SCRATCHED (VERTICAL STAB) · airframe 13,570 hrs · 6,977 cycles

DURING C-3 CHECK, INSPECTION REPORTED LE OF VERTICAL STAB FIN HAD DEEP SCRATCH MARKS (TOOL MARKS) BETWEEN PANELS NR 322BL AND 322CL ON ATTACHMENT BRACKET WHERE PANEL 322BL ATTACHES. REPLACED RIB FOR VERT STAB LE BETWEEN PANELS 322BL AND 322CL IAW SRM 51-42-11 AND AMM 20-21-11.

Part: FLOORBOARD — CORRODED (CABIN) · corrosion level 2 · airframe 13,570 hrs · 6,977 cycles

DURING C-3 CHECK, INSPECTION REPORTED FLOORBOARD 222FF (R1 ENTRY) CORRODED. REPLACED FLOORBOARD 222FF IAW AMM 53-12-12-400-001.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,570 hrs · 6,977 cycles

DURING C-3 CHECK, INSPECTION REPORTED CORROSION IN NUTPLATE HOLE UNDER THE FWD GIRT FITTING ON THE L2 DOOR SILL. REPLACED L2 DOOR SILL IAW SRM 51-42-11, FIG 6 AND 7.

Part: SPLICE — CORRODED (L2 DOOR SILL) · corrosion level 2 · airframe 13,570 hrs · 6,977 cycles

DURING C-3 CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON OTBD UPPER ANGLE AFT ATTACHMENT HOLE UPON REMOVAL OF L2 DOOR SILL SPLICE ANGLES FWD OF FR66. REPLACED L2 DOOR SILL SPLICE ANGLES IAW SRM 51-42-11, FIG 6 AND 7.

Part: LATCH — MISSING (L2 GIRT BAR) · airframe 13,570 hrs · 6,977 cycles

DURING C-3 CHECK, INSPECTION REPORTED AFT OTBD NUTPLATE FOR THE AFT FILLER PLATE AROUND THE L2 DOOR GIRT BAR LATCH MISSING. REPLACED L2 DOOR SILL IAW SRM 51-42-11, FIG 6 AND 7.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,570 hrs · 6,977 cycles

DURING C-3 CHECK, INSPECTION REPORTED L2 DOOR SILL PLATE HAD CORROSION FWD OF FR66. REPLACED L2 DOOR SILL IAW 51-42-11, FIG 6 AND 7.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,570 hrs · 6,977 cycles

DURING C-3 CHECK, INSPECTION REPORTED L2 DOOR SILL THRESHOLD HAD CORROSION AROUND SEVERAL NUTPLATE HOLES. REPLACED L2 DOOR SILL IAW SRM 51-42-11, FIG 6 AND 7.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,570 hrs · 6,977 cycles

DURING C-3 CHECK, INSPECTION REPORTED CORROSION IN NUTPLATE HOLES ON THE L2 DOOR SILL PLATE AT FR66. REPLACED L2 DOOR SILL IAW SRM 51-42-11, FIG 6 AND 7.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,570 hrs · 6,977 cycles

DURING C-3 CHECK, INSPECTION REPORTED CORROSION AROUND NUT PLATE HOLE ON FLOORBEAM Y1292 FWD OF FR68. REPLACED FLOORBEAM AT Y1292 FWD OF FR68 IAW SRM 51-42-11, FIG 6 AND 7.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,570 hrs · 6,977 cycles

DURING C-3 CHECK, INSPECTION REPORTED CORROSION AROUND NUT PLATE HOLE ON FLOORBEAM Y1292 AFT OF FR68. REPLACED FLOORBEAM AT Y1292 AFT OF FR68 IAW 51-42-11, FIG 6 AND 7.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,570 hrs · 6,977 cycles

DURING C-3 CHECK, INSPECTION REPORTED R2 DOOR SILL PLATE CORRODED FWD OF FR66. REPLACED R2 DOOR SILL IAW SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,570 hrs · 6,977 cycles

DURING C-3 CHECK, INSPECTION REPORTED CORROSION AROUND NUT PLATE ON FLOORBEAM Y1292, AFT OF FR66. REPLACED FLOORBEAM AT Y1292 AFT OF FR66 IAW SRM 51-42-11, FIG 6 AND 7.

Part: BOLT — CORRODED (WINGLET ATTACH) · airframe 13,570 hrs · 6,977 cycles

DURING C-3 CHECK, INSPECTION REPORTED WINGLET ATTACH HARDWARE RUSTY. REPLACED WINGLET ATTACH HARDWARE (MILD SURFACE CORROSION ON BOLT HEADS) ON LT WING IAW AMM 57-31-22-400-001.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,570 hrs · 6,977 cycles

DURING C-3 CHECK, INSPECTION REPORTED CORROSION AROUND NUT PLATE HOLE ON FLOORBEAM -Y1292, AFT OF FR68. REPLACED FLOORBEAM AT FR68 STATION -Y1292 IAW SRM 51-42-11.

Part: BUSHING — CORRODED (NLG TORSION LINK) · airframe 13,570 hrs · 6,977 cycles

DURING C-3 CHECK, INSPECTION REPORTED NLG UPPER TORSION LINK FROM STRUT CORRODED INSIDE ATTACH LUG. REMOVED CORROSION UNDER BUSHINGS OF NLG UPPER TORSION LINK ATTACH POINT AND REPLACED BUSHINGS IAW EA NR A8-32R-11869.

Part: COMPUTER — FAILED (NR 2 ELAC) · airframe 10,284 hrs · 5,300 cycles

AIR TURNBACK. FLIGHT CREW REPORTED AILERON SERVO ECAM ON CLIMB. NORMAL LAW WAS LOST. RETURNED TO DEN AND PERFORMED AN OVERWEIGHT LANDING WITHOUT INCIDENT. REPLACED ELAC NR 2 PER TSM 27-93-00-810-855. OPS CHECKED GOOD PER AMM 27-93-34. PERFORMED AFS LAND TEST PER AMM 22-97-00-710-001 AND TESTED OKAY. CAT IIIB STATUS RETAINED. PERFORMED OVERWEIGHT LANDING TASK CARD MP05510-4, NO DEFECTS FOUND. PERFORMED DFDR DOWNLOAD PER AMM 31-33-00-710-009. AIRCRAFT RETURNED TO SERVICE.

Part: COMPUTER — FAILED (PROBE HEAT) · airframe 7,670 hrs · 3,854 cycles

FLIGHT CREW REPORTED A BURNING ELECTRICAL ODOR 20 MIN OUT FROM DEN FL390. APPROXIMATELY 20 SEC AFTER ODOR BEGAN, ECAM ANTI-ICE CAPT L & R STAT ILLUMINATED. REPLACED PROBE HEAT COMPUTER PER MM 30-31-34, PB 401. COMPLIED WITH MM 24-00-00-810-823 AND 30-31-20-710-001 AND CHECKED OKAY.

Part: COOLING FAN — FAILED (LIVE TV UNIT) · airframe 7,351 hrs · 3,666 cycles

FLIGHT CREW REPORTED LIVE TV SMOKE DETECTION WARNING HORN SOUNDED DURING FLIGHT. LIVE TV FAN C/B 2000VU POPPED AND WOULD NOT RESET. REPLACED AFT RACK COOLING FAN PER AMM 44-25-00, PAGE 471. OPS CHECK GOOD.

Part: SLEEVE — DAMAGED (NLG WHEEL) · airframe 3,317 hrs · 1,764 cycles

FLIGHT CREW REPORTED NOSE WHEEL VIBRATION ON GEAR RETRACTION. FOUND NOSE WHEEL LT BEARING AND SLEEVE DAMAGED. REMOVED SLEEVE AND INSPECTED AXLE FOR DAMAGE. NO DAMAGE NOTED. INSTALLED SERVICEABLE AXLE SLEEVE AT LT POSITION PER AMM 32-41-12-000-002 AND 32-41-12-400-002. REMOVED AND INSTALLED BOTH NOSE WHEEL ASSY'S FOR PRECAUTIONARY PER AMM 32-41-12-401 AND 32-41-12-401. TORQUE AND SPIN CHECK GOOD. NO DEFECTS NOTED.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 1,710 hrs · 885 cycles

AIR TURNBACK, FLIGHT CREW REPORTED FIRST OFFICER'S WINDSHIELD CRACKED. DECLARED AN EMERGENCY, AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED FIRST OFFICER'S WINDSHIELD PER 56-11-11-000-001 AND 56-11-11-400-001. PERFORMED TEST OF WINDOW HEAT AND DEFOGGING PER 30-42-00-710-001 AND CHECKED OKAY.