N803FR

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 29,911 hrs · 15,648 cycles

AFT CABIN FRAME 68, Y-1292 FLOORBEAM HAS CORROSION. R & R FLOORBEAM IAW SRM 51-42-11, PARA 5.

Part: PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 29,911 hrs · 15,648 cycles

LATERAL SHEAR PLATE FRAME 69 TO FRAME 70, STRINGER 23 RT TO STRINGER 24 RT HAS CORROSION. R & R SHEAR PLATE IAW SRM 51 -42-11, PARA 6 B-18, D 1-5 AND EO AO-53EO-31 434.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 29,911 hrs · 1,548 cycles

AFT CABIN FRAME 66 TO FRAME 68, Y1292 FLOORBEAM HAS CORROSION IN 3 AREAS. R & R FLOORBEAM IAW SRM 51-42-11, PARA 5.

Part: TRAY — CRACKED (ZONE 200) · corrosion level 2 · airframe 29,911 hrs · 15,648 cycles

SHEAR PLATE TRAY AT FRAME 68 TO FRAME 69. STRINGER 23 RT TO STRINGER 24, RT IS CRACKED. R & R SHEAR PLATE TRAY IAW SRM 51 -42-11, PARAGRAPH 5, 6, 7 AND 13.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 29,911 hrs · 1,548 cycles

AFT CABIN FRAME 66 TO FRAME 68, Y1292 FLOOR SUPPORT HAS CORROSION IN 3 AREAS. R & R FLOOR SUPPORT IAW SRM 51-42-11, PARA 5.

Part: PLATE — CRACKED (ZONE 200) · corrosion level 2 · airframe 29,911 hrs · 15,648 cycles

C-CHECK, SHEAR PLATE TRAY AT FRAME 68 TO FRAME 69, S23-24L CRACKED. R & R SHEAR PLATE TRAY IAW SRM 51-42-11 PARAGRAPH 5, 6, 7 AND 13.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 29,911 hrs · 15,648 cycles

AFT CABIN FLOORBEAM FRAME 66 Y765 CORROSION. R & R FLOORBEAM IAW SRM 51-42-11, PARA 5.

Part: PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 29,911 hrs · 15,648 cycles

LATERAL SHEAR PLATE FRAME 69 TO FRAME 70, STRINGER 23 LT TO STRINGER 24 LT HAS CORROSION. R & R SHEAR PLATE IAW SRM 51-42-11 PARAGRAPH 6 B-1 B, 0 1-5 AND EO AO-53EO-31434.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 27,978 hrs · 1,461 cycles

ESPU LLWL (13WL) FAILED SYS TEST IAW A-CHECK CARD A332201-03. REPLACED BATTERY PACK ON ESPU LLWL(13WL) IAW AMM 33-51-38, PB 401.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 27,187 hrs · 14,158 cycles

ACFT LP 598021 I2M: EPSU TEST FAILED 11WL BATTERY. R & R EPSU BATTERY FOR 11WL IAW A318 AMM 33-51-38-000-002 AND 33-51-38-400-002. TEST OK.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 26,680 hrs · 13,904 cycles

F/O FRONT WINDSHIELD CRACKED, ANTI-ICE RT WINDSHIELD ECAM. R & R THE F/O FRONT WINDSHIELD IAW AMM 56-11-11-400-000-001.

Part: ENGINE — OVERTEMP · airframe 26,408 hrs · 13,767 cycles

AIR TURN BACK DUE TO BIRDSTRIKE ON NR 1 ENGINE. ENGINE SHUTDOWN, INVESTIGATION FOR ENGINE SHUTDOWN SHOWS THE EGT WAS EXCEEDED AT 1015 DEGREES CELCIUS FOR 21 SECONDS. PERFORMED AN AIRFRAME AND ENG NR 1 BIRDSTRIKE INSP. REF TASK CARDS MP05510-02 AND MP72400-01. PERFORMED TROUBLESHOOTING REF TSM 72-00-00-810-849 AND AMM 75-31-00-200-008. PERFORMED A FADEC MOTORING TEST REF AMM 73-29-00-710-040. NO FAULTS FOUND. INSPECTED VBV AND VSV SYS REF AMM 75-31-00-210-002 AND 75-32-00-210-002. NO DEFECTS NOTED. RESET EGT MAXIMUM POINTERS REF AMM77-00-00-710-042. PERFORMED BORESCOPE INSP OF THE HPT AND LPT STAGE 1, 2 AND 3 REF AMM 72-52-00-290-001 AND 72-54-00-290-005. NO DEFECTS NOTED. PERFORMED POWER ASSURANCE CHECK REF AMM 71-00-00710-008. COMPRESSOR STALLS AT 55 PERCENT TO 60 PERCENT N1, DURING DECELERATION.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 25,264 hrs · 13,214 cycles

C-CHECK: NON ROUTINE N0607; NUMEROUS EMERGENCY PATH LIGHTS INOP ON SEATS AND CEILING PANELS. PERFORMED OPS TEST OF EMERGENCY LIGHTS IAW AMM 33-51-00-710-059A. EMERGENCY POWER SUPPLY UNIT 10WL FAILED SYS TEST "BATT FAULT' LIGHT ILLUMINATED. R & R EPSU 10WL IAW A318 33-51-38-000-001 AND 33-51-38-740-050. TEST CHECK NORMAL.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 25,264 hrs · 13,214 cycles

C-CHECK: NON ROUTINE N0610; EMERGENCY LIGHT ABOVE L-1 DOOR, THE LENS IS CRACKED. R & R EMERGENCY LIGHT ASSY IAW AMM 33-51-11-020-050B AND AMM 33-51-11-420-050A.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 25,264 hrs · 13,214 cycles

C-CHECK: NON ROUTINE N0613; AFT CARGO FLOOR PANEL 161DF EDGE DELAMINATED AND EDGE FILLER DAMAGED 10 INCH. FABRICATED REPLACEDMENT FLOOR PANEL IAW MCG IRM 9701, REV G.

Part: FITTING — GOUGED (ZONE 100) · airframe 25,264 hrs · 13,214 cycles

C-CHECK: NON ROUTINE N0124; FWD CARGO LOWER FWD CORNER SEALING SECTION FITTING GOUGED .1250 IN X .2500 IN X .040 INCH. R & R FWD LOWER SEALING SECTION FITTING IAW SRM 51-72-11, PAGE 1.

Part: CONNECTOR — MISINSTALLED (EMERGENCY LIGHT) · airframe 25,264 hrs · 13,214 cycles

C-CHECK: NON ROUTINE N0033, EMERGENCY EXIT LIGHT AT ROW 13ABC INOP. FOUND CONNECTOR AT LIGHT ASSEMBLY TO BE INPROPERLY CONNECTED. RE-SEATED CONNECTOR IAW AIRBUS A318 AMM 33-51-19-400-003 SUBTASK 33-51-19-420-052 STEP A(1)(A)(B). OPS CHECK GOOD IAW AMM 33-51-00-710-001

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 25,264 hrs · 13,214 cycles

C-CHECK: NON ROUTINE N0616; L-1 ENTRY LOWER EXIT LIGHT, THE LENS IS ILLEGIBLE. R & R LENS ASSY ON L-1 DOOR LOWER EXIT LIGHT IAW AMM 33-51-13-400-001 PAGE 3 STEP A 3 AND AMM 33-51-13-020-050 STEP A(1)(A)(B).

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,058 hrs · 7,260 cycles

DURING C-3 CHECK, INSPECTION REPORTED L2 DOOR THRESHOLD CORRODED ON SURFACE OF PANEL 261FF. REPLACED FLOOR PANEL 261FF IAW AMM 53-42-12-400-002.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,058 hrs · 7,260 cycles

DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SUPPORT AT FR 66 TO FR 70 AT Y1292, FWD INBD FASTENER LOCATIONS. REPLACED FLOOR SUPPORT BETWEEN FR 66 AND FR 68 PER SRM 51-42-11. REPAIRED OTHER DAMAGE TO FLOOR SUPPORT IAW EA A8-53R-12042.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,058 hrs · 7,260 cycles

DURING C-3 CHECK, INSPECTION REPORTED L2 DOOR FWD AND AFT GIRT BAR FITTING BLANKING PLATES CORRODED. REPLACED L2 DOOR FWD AND AFT GIRT BAR FITTING BLANKING PLATES IAW AMM 52-11-31-991-011/012.

Part: GIRT BAR — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,058 hrs · 7,260 cycles

DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON L2 DOOR SEAL NUT PLATE HOLE AFT OF AFT GIRT BAR FITTING PLATE. REPAIRED PER EA A8-53R-12044.

Part: PLATE — CORRODED (GIRT BAR) · corrosion level 2 · airframe 14,058 hrs · 7,260 cycles

DURING C-3 CHECK, INSPECTION REPORTED L2 DOOR FWD AND AFT GIRT BAR FITTING BLANKING PLATES CORRODED. REPLACED BLANKING PLATES IAW A318 SRM 51-42-11 AND AMM 52-13-31-400-007.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,058 hrs · 7,260 cycles

DURING C-3 CHECK, INSPECTION REPORTED L1 DOOR THRESHOLD FLOOR PANEL 221FF CORRODED. REPLACED FLOOR PANEL 221FF IAW AIRBUS AMM 53-12-12-400-001.

Part: SKATE ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,058 hrs · 7,260 cycles

DURING C-3 CHECK, INSPECTION REPORTED MODERATE CORROSION IN NUT PLATE MOUNT HOLES OF SKATE ANGLE AFT OF R2 DOOR GIRT BAR CUTOUTS. REMOVED AND REPLACED SKATE ANGLE IAW A318 SRM 51-42-11, STEPS B AND D.

Part: TORQUE LINK — CORRODED (MLG) · corrosion level 2 · airframe 14,058 hrs · 7,260 cycles

DURING C-3 CHECK, INSPECTION REPORTED PITTING AND CORROSION ON NLG UPPER TORQUE LINK ATTACH POINT. REMOVED PITS AND CORROSION AND CADMIUM PLATED INNER BORE IAW EA A8-23R-12046.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,058 hrs · 7,260 cycles

DURING C-3 CHECK, INSPECTION REPORTED AFT GALLEY RT FLOORBEAM -Y1292, FR 68 TO FR69 CORRODED AT NUT PLATE FASTENER LOCATIONS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,058 hrs · 7,260 cycles

DURING C-3 CHECK, INSPECTION REPORTED FLOORBEAM INBD OF R2 DOOR GIRT BAR CUTOUTS HAD LIGHT TO MODERATE CORROSION AT ALL NUT PLATE ATTACH POINTS. REPLACED FLOORBEAM IAW A318 SRM 51-42-11, STEP 7B.

Part: PLATE — DAMAGED (FLOORBEAM) · airframe 14,058 hrs · 7,260 cycles

DURING C-3 CHECK, INSPECTION REPORTED HOLES ON JOINT PLATE COMMON TO FLOORBEAM AT -Y1292 BETWEEN FR68 AND FR69 DAMAGED. FABRICATED AND INSTALLED REPLACEMENT JOINT PLATE IAW A318 SRM 53-41-14, FIG 17, AND 51-42-11, STEP 7B.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,058 hrs · 7,260 cycles

DURING C-3 CHECK, INSPECTION REPORTED FLOORBEAM INBD OF L2 DOOR GIRT BAR CUTOUTS HAD LIGHT TO MODERATE CORROSION AT ALL NUT PLATE ATTACH POINTS. REPLACED FLOORBEAM IAW A318 SRM 51-42-11, PARA 5-7.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,058 hrs · 7,260 cycles

DURING C-3 CHECK, INSPECTION REPORTED AFT GALLEY RT FLOORBEAM -Y1292, FR 68 TO FR69 CORRODED AT NUT PLATE FASTENER LOCATIONS.

Part: SKATE ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,058 hrs · 7,260 cycles

DURING C-3 CHECK, INSPECTION REPORTED MODERATE CORROSION IN NUT PLATE MOUNT HOLES OF SKATE ANGLE AFT OF L2 DOOR GIRT BAR CUT OUTS. REMOVED AND REPLACED SKATE ANGLE IAW A318 SRM 51-42-11, PARA. 5, 6 AND 13.

Part: CONTACTOR — DAMAGED · airframe 13,170 hrs · 6,797 cycles

AIR RETURN AT 0130Z FOR MULTIPLE ECAMS ASSOCIATED W/AC ESS BUSS. DEPARTURE OUT OF KDEN, LEVELING AT 35,000 FT, RECEIVED ECAM ENG 1 IGN A AND ENG 2 IGN A, C/B TRIPPED L ELEC BAY, YAW DAMPER 1, RUD TRIM 1, AND TRV LIM 1. CAPTAINS PFD ND FWD DISPLAYS ALL WENT BLANK. AFTER SELECTING AC ESS FEED TO ALTN, RECOVERED ALL DISPLAY FUNCTIONS. STILL HAD REMAINING INOP SYSTEMS, INCLUDING NO FUEL INDICATIONS ON EWD. RETURNED TO KDEN AND LANDED AIRCRAFT WITHOUT INCIDENT. REPLACED CONTACTOR 9 BY U1 IAW AMM 24-2255, PB 401. OPS CHECKED GOOD. REPLACED CONTACTOR 3XC IAW AMM 24-25-55, PB 401. OPS CHECKED GOOD. REPLACED RELAY 13XC IAW AMM 20-46-50. OPS CHECKED GOOD. REPLACED C/B 4XC IAW AMM 20-46-10. OPS CHECKED GOOD.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 10,074 hrs · 5,205 cycles

DURING CRUISE, FLIGHT CREW REPORTED -Y- HYDRAULIC SYSTEM LEVEL LOW. AS A PRECAUTIONARY MEASURE, AN EMERGENCY WAS DECLARED UPON LANDING AT PDX. REPLACED NR 2 ENGINE YELLOW SYSTEM CASE DRAIN RETURN LINE FOR LEAKING. RAN NR 2 ENGINE. OPS AND LEAK CHECKED NORMAL. NO LEAKS NOTED. REF AMM 29-13-49-000-008 AND 29-13-49-400-008.

Part: CONTROLLER — UNSERVICEABLE (CABIN PRESSURE) · airframe 6,572 hrs · 3,262 cycles

FLT CREW REPORTED CABIN PRESSURIZATION FLUCTUATING FOLLOWED BY NR 2 CONTROLLER FAILURE. ECAM EXCESS CABIN ALT. AT APPROX 30,000 FT & CLIMBING. NOTICED CABIN ALT SHOWING IN EXCESS OF 29,000 FT, CABIN MODE NR 1 CONTROLLER LATER ASSUMED CONTROL & CABIN PRESSURE RETURNED TO BELOW 10,000 FT. CABIN O2 MASKS DID NOT AUTOMATICALLY DROP. MANUALLY DEPLOYED OXYGEN MASKS FROM FLT DECK. DECLARED AN EMERGENCY & PERFORMED AN OVERWEIGHT LANDING PER CHECKLIST. LANDING NORMAL. REPLACED PRESSURE CONTROLLER 11 HL PER LEAK LESS THAN 0.78 PSI/MIN. PERFORMED FUNCTIONAL CHECK OF AUTOMATIC MASK RELEASE PER AMM 35-23-00-720-003. OPS CHECK NORMAL.

Part: CONTROL UNIT — ODOR (COCKPIT) · airframe 2,518 hrs · 1,348 cycles

IN CRUISE CREW REPORTED SMOKE COMING FROM FLIGHT CONTROL UNIT. NO ECAMS NOTED, SMOKE/AVNCS SMOKE. QRH PROCEDURE APPLIED, EMERGENCY DECLARED. DIVERTED TO OKC & LANDED WITHOUT INCIDENT. PERFORMED INSPECTION OF FWD E&E BAY, MID & AFT E&E BAY, MID LT E&E BAY AND NO DAMAGE FOUND. FOUND FCU HAD SMELL OF BURNED WIRE INSULATION. REMOVED FCU, INSPECTED WIRING FWD TO LT & RT BEHIND LCD'S AND GLARESHIELD, NO DAMAGE FOUND. INSTALLED NEW FLIGHT CONTROL UNIT. PERFORMED LIGHT OPS TEST, TESTED GOOD. PERFORMED OPS TEST OF FLIGHT CONTROL UNIT AND TESTED GOOD. PERFORMED AFS TEST, TEST PASS. PERFORMED OPS LAND, TEST PASS. CLEANED AND STOWED CREW O2 MASKS.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 35 hrs · 16 cycles

FLIGHT CREW REPORTED SEAT BELT/NO SMOKING LIGHTS AND FWD GALLEY EXIT SIGNS INOPERATIVE. REPLACED EPSU IAW MM 33-51-13-04.