N912FR

Part: BATTERY — DISCHARGED (CABIN) · airframe 41,890 hrs · 20,531 cycles

AFT EPSU BATTERY FAILED A CHECK TASK CARD FFT-335100-03-1, CAPACITY CHECK. R & R BATTERY ASSEMBLY IAW AMM 33-51-39-000-005A & AMM 33-51-39-400-005-A.

Part: SKIN — SATURATED (RT ELEVATOR) · airframe 39,535 hrs · 19,283 cycles

AIRCRAFT OUT OF SERVICE DUE TO C8 52 CHECK. RT ELEVATOR SN CC2574 THERMO GRAPHIC INSPECTION REVEALED INDICATIONS ON UPPER PANEL IRREGULAR IN SHAPE & BLACK IN COLOR. REPAIRED RT ELEVATOR UPPER PANEL AT 13 EACH AREAS OF LIQUID INGRESS IAW A319 SRM 55-20-00, PB201, PAR 2 A 1 A C, 2 A 2 A J, 2B 1, 2 B 2 A 1-10, A319 SRM 55-21-11, PB201, FIG 204 & 205, PAR2 F 1-6, 2 G & CMM 55-21-15-210-010-601, PARA 1-5, 6 A 7-8, 9 B. APPLIED PRIMER & TOP COAT. WEIGHED ELEVATOR, FOUND TO BE LESS THAN MAX LIMIT.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 39,535 hrs · 19,283 cycles

AIRCRAFT OUT OF SERVICE DUE TO C8 S2 CHECK. MAIN CABIN RT SIDE SHEAR PLATE FR 69 TO FR 70 IS CRACKED. REMOVED RT SHEAR PLATE FROM FR 69 - FR 70, REPLACED WITH NEW SHEAR PLATE IAW AIRBUS A319 SRM 51-42-11 PG 6 & 7.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,535 hrs · 19,283 cycles

AIRCRAFT OUT OF SERVICE DUE TO C8 S2 CHECK. MAIN CABIN FLOOR BEAM Y 1292 HAS CORROSION AT FR 16. R & R MAIN CABIN FLOOR BEAM LAW A319 SRM 51-72-11 PARA 5 & 6.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,535 hrs · 19,283 cycles

AIRCRAFT OUT OF SERVICE DUE TO C8 S2 CHECK. MAIN CABIN AFT FLOOR SUPPORT BEAM AFT OF SEAT TRACK BEAM Y 1732 HAS CORROSION AT FR 68. REMOVED CORROSION ON AFT CABIN FLOOR SUPPORT BEAM IAW SRM 51-74-00 & FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14 PB 101 FIG 102, SH 1. R & R FLOOR SUPPORT BEAM IAW SRM 51-42-11 FIG 5 & 7.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,535 hrs · 19,283 cycles

AIRCRAFT OUT OF SERVICE FOR C8 S2 CHECK. AFT CABIN FLOOR SUPPORT BEAM INBD OF SEAT TRACK BEAM Y 765 6 INCHES FWD OF FR 66 HAS CORROSION. R & R FLOOR BEAM AT AFT CABIN INBD OF SEAT TRACK Y 765 6 INCHES FWD OF FR 66 IAW A319 SRM 51-42-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,535 hrs · 19,283 cycles

AIRCRAFT OUT OF SERVICE DUE TO C8 S2 CHECK. AFT CABIN LT LATERAL SHEAR PLATE CRACKED AT FRAME 69. R & R LT LATERAL SHEAR PLATE WITH NEW PART IAW SRM 51-42-11, PAR 6, 7 & 13.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,535 hrs · 19,283 cycles

AIRCRAFT OUT OF SERVICE FOR C8 S2 CHECK. MAIN CABIN FLOOR BEAM Y 254 HAS CORROSION AT FR 18. REMOVED CORROSION AT MAIN CABIN FLOOR BEAM Y 254, FR L8 IAW SRM 51-74-00, 6 B ORIGINAL THICKNESS .079 INCHES, REMOVED .022 INCHES FOUND TO BE WITHIN LIMITS IAW SRM 53-11-15, PBL01, FIG 104, SH L. REAPPLIED PROTECTIVE COATING.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,535 hrs · 19,283 cycles

AIRCRAFT OUT OF SERVICE DUE TO C8 S2 CHECK. FLOOR SUPPORT BEAM AFT OF SEAT TRACK Y 1292 HAS CORROSION AT FR 68. REMOVED FLOOR SUPPORT BEAM Y 1292 AT FR 68. REPLACED WITH NEW FLOOR SUPPORT BEAM PN D5347218920400 IAW A319 SRM 51-42-11 PG 7.

Part: ACTUATOR — INTERMITTENT (MLG) · airframe 35,229 hrs · 17,015 cycles

ACFT LEFT C-CHECK AFTER COMPLETE SET LANDING GEAR TIME, DEPARTED. NLG DID NOT LOCK UP, GEAR DOORS DID NOT CLOSE. ACFT WAS PREPPED FOR GEAR DOWN FERRY FLIGHT. FERRY FLIGHT DID NOT OCCUR. DISCREPANCY WAS WORKED AT AIRPORT, ADJUSTMENTS MADE, REF NR 43936. OCF UNSATISFACTORY, NLG WOULD NOT RETRACT AT 170 KTS OR 130KTS, NLG DID RETRACT AT TAKEOFF. DISCREPANCY WAS WORKED ON, NLG ACTUATOR REPLACED, REF NR 43937. OCF SATISFACTORY.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 30,246 hrs · 14,515 cycles

C-CHECK: NON ROUTINE 2994; LATERAL SHEAR PLATE, FRAME 69 - 70 RIGHT, HAS OUT OF LIMITS CORROSION AT FASTENER HOLES. REMOVED AND REPLACED SHEAR PLATE IAW AO-53EO-31434.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 30,246 hrs · 14,515 cycles

C-CHECK: NON ROUTINE # 29844; LATERAL SHEAR PLATE, FRAME 69 - 70 LEFT, HAS OUT OF LIMITS CORROSION AT FASTENER HOLES. REMOVED AND REPLACED SHEAR PLATE IAW AO-53EO-31434.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 30,246 hrs · 14,515 cycles

C-CHECK: NON ROUTINE 29941; FRAME 69 -Y765 HAS OUT OF LIMITS CORRORION AT FASTER HOLES, PER SRM 53-00-14 FIG 102. REMOVED AND REPLACE BEAM IAW A319 SRM 51-42-1.

Part: THERMOSTAT — INOPERATIVE (BLEED AIR SYS) · airframe 27,075 hrs · 12,986 cycles

CAPTAIN REPORTED BLEED 2 FAULT AND LOSS OF CABIN PRESSURISATION. MAXIMUM CABIN ALTITUDE 10,500. FLIGHT NR 963 DIVERTED FOR AN UNSCHEDULED LANDING. MX TROUBLESHOOT NR 2 ENGINE BLEED AIR SYS IAW AMM 36-11-00-720-005 AND R & R THE NR 2 ENGINE FAN AIR VALVE THERMOSTAT IAW AMM 36-11-43 PB 401. LEAK AND OPS CHECKS GOOD IAW AMM 36-11-00-710-003.

Part: EPSU — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 26,085 hrs · 12,541 cycles

THE FLIGHT CREW NOTED THAT THE EMERGENCY EXIT LIGHTS AND ESCAPE PATH LIGHTS IN CABIN ARE CONTINUOUSLY ON WITH THE EMERGENCY EXIT LIGHT SWITCH IN THE ARM POSITION. MX PERFORMED AN OPS TEST OF THE EMERGENCY LIGHTING SYS AND THE OPS CHECK WAS GOOD IAW AMM 33-51-00-710-008.

Part: WINDOW — CRACKED (ZONE 200) · airframe 23,570 hrs · 11,239 cycles

AT FL 390, PILOT REPORTED THE RIGHT SLIDING WINDOW CRACKED IN BOTH PANES. MAINTENANCE REMOVED AND REPLACED THE RIGHT SLIDING WINDOW AND PERFORMED LEAK CHECK IAW AMM 56-12-11 PB 401.

Part: CABIN PRESSURE — FLUCTUATES · airframe 19,179 hrs · 9,088 cycles

THE FLIGHT CREW REPORTED, DURING CLIMB-OUT, PRESSURIZATION FLUCTUATED 200 FEET PER MINUTE BETWEEN FLIGHT LEVEL 350 UP TO AND LEVELING AT FLIGHT LEVEL 380. AT THE SAME TIME, THE R2 DOOR PRESSURE LIGHT FLASHED AND THE SLIDE "DISARM" ILLUMINATED, ON THE LOWER ECAM SYSTEM DISPLAY, SHOWING THE DOOR PAGE. AFTER LEVEL OFF, PRESSURIZATION STABILIZED AND THE SLIDE DISARM INDICATOR RESET TO "ARMED." MAINTENANCE PERFORMED A VISUAL AND OPERATIONAL CHECK OF THE R2 DOOR IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 52-10-13 PB 501. MAINTENANCE THOROUGHLY CLEANED AND INSPECTED THE GIRT BAR FITTINGS, IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 52-13-22 PB 501. AN OPERATIONAL CHECK OF THE R2 DOOR WAS DONE AND THE DOOR CHECKED GOOD.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,980 hrs · 9,004 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED FLOOR PANEL 262FF CORRODED ON LOWER SURFACE. REMOVED AND REPLACED FLOOR PANEL 262FF IAW EO A0-53T-11996.

Part: FASTENER — CORRODED (FAIRING) · corrosion level 2 · airframe 18,980 hrs · 9,004 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED RT WING-TO-BODY FAIRING 192DT HAD CORRODED FASTENERS AT LOWER SEAL. REMOVED AND REPLACED RT WING UPPER WING-TOO-BODY FAIRING PANEL NR 192DT LOWER SEAL MOUNTING SCREWS IAW 51-42-11.

Part: FASTENER — CORRODED (FAIRING) · corrosion level 2 · airframe 18,980 hrs · 9,004 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED CORRODED FASTENERS THAT SECURE LIGHT TO RT WING-TO-BODY FAIRING 192DT. REMOVED AND REPLACED RT UPPER WING LIGHT COVER MOUNTING SCREWS ON PANEL NR 192DT.

Part: PLATE — CORRODED (GIRT BAR LATCH) · corrosion level 2 · airframe 18,980 hrs · 9,004 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED R2 DOOR AFT GIRT BAR LATCH FILLER CORRODED. REMOVED AND REPLACED R2 DOOR AFT GIRT BAR LATCH FILLER PANEL IAW AMM 53-42-12-PB401.

Part: PLATE — CORRODED (GIRT BAR LATCH) · corrosion level 2 · airframe 18,980 hrs · 9,004 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED L2 DOOR AFT GIRT BAR LATCH FILLER CORRODED. REMOVED AND REPLACED L2 DOOR AFT GIRT BAR LATCH FILLER IAW AMM 53-42-12-PB401.

Part: PLATE — DAMAGED (FUSELAGE) · airframe 18,980 hrs · 9,004 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT AFT BULKHEAD CROSSOVER BEAM HAD FASTENERS PULLING THROUGH THE CENTER PLATE. REMOVED AND REPLACED AFT CARGO COMPARTMENT AFT BULKHEAD CROSSOVER BEAM CENTER PLATE IAW SRM 51-42-11.

Part: PLATE — CORRODED (GIRT BAR LATCH) · corrosion level 2 · airframe 18,980 hrs · 9,004 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED L2 DOOR FWD GIRT BAR LATCH FLOOR FILLER HAD A SMALL SPOT OF CORROSION. REMOVED AND REPLACED L2 DOOR FWD GIRT BAR LATCH FILLER PANEL IAW AMM 53-42-12-PB401.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,980 hrs · 9,004 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED DUMMY RAIL AT Y503.2, FR 12 TO FR 16, CORRODED ON TOP. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14. REMOVED AND REPLACED DUMMY RAIL IAW SRM 51-42-11 AND 51-44-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,980 hrs · 9,004 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED FLOORBEAM AT FR16, STA Y254, CORRODED ON THE TOP CAP. DETERMINED CORROSION TO BE OUT OF LIMITS IAW SRM 53-11-14. REMOVED AND REPLACED FLOORBEAM FROM FR12 THRU FR24, STA 254, IAW SRM 52-42-11 AND 51-72-11.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,980 hrs · 9,004 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED FLOOR PANEL 221FF (L1 DOOR) CORRODED ON BOTTOM SIDE. REMOVED AND REPLACED FLOOR PANEL 221FF IAW AMM 53-12-12-PB401.

Part: BLANKING PLATE — CORRODED (GIRT BAR) · corrosion level 2 · airframe 18,980 hrs · 9,004 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED F1 DOOR AFT GIRT BAR STOP LEVER FITTING BLANKING PLATE CORRODED ON BOTTOM SIDE. REMOVED AND REPLACED R1 DOOR AFT GIRT BAR STOP LEVER FITTING BLANKING PLATE IAW AMM 53-12-12-PB401.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,980 hrs · 9,004 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM AT Y1292 AND FR16, AT ATTACH POINT. REMOVED AND REPLACED FLOORBEAM AT Y1292 IAW SRM 51-42-11.

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 18,980 hrs · 9,004 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED FLOOR PANEL 222FF (R1 DOOR) CORRODED ON BOTTOM SIDE. REMOVED AND REPLACED FLOOR PANEL 222FF IAW AMM 53-12-12-PB401.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,980 hrs · 9,004 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED FLOORBEAM AT Y1292, FR66, CORRODED AT NUTPLATE HOLES. REMOVED AND REPLACED FLOORBEAM AT Y1292, FR66, IAW SRM 51-42-11.

Part: ATTACH BOLT — CORRODED (LAVATORY) · corrosion level 2 · airframe 18,980 hrs · 9,004 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED LWR ATTACHMENT BOLT ON INBD AFT CORNER OF LAV "A" SEVERELY CORRODED. REMOVED AND REPLACED BOLT IAW AMM 25-41-41-PB401.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,980 hrs · 9,004 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED FLOORBEAM AT Y765, FR68, CORRODED. DETERMINED CORROSION TO BE OUT OF LIMITS IAW 53-00-14. REMOVED AND REPLACED FLOOR BEAM AT Y768 IAW SRM 51-42-11.

Part: SUPPORT BEAM — BENT (FUSELAGE) · airframe 18,980 hrs · 9,004 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED AFT CARGO FWD BULKHEAD PANEL SUPPORT BEAM AT APPROX STR 42L, FR47 TO FR51, BENT. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SUPPORT BEAM IAW SRM 51-42-11, SRM 51-44-11, 51-75-12 AND DRAWING D53974679.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,980 hrs · 9,004 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED FLOORBEAM AT Y1292, FR68, CORRODED. DETERMINED CORROSION TO BE OUT OF LIMITS IAW SRM 53-00-14, PAR 4 B. REMOVED AND REPLACED FLOORBEAM Y1292 AT FR 68-69 IAW SRM 51-42-11 AND 51-44-11.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,980 hrs · 9,004 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED L2 DOOR SILL CORRODED AT VARIOUS LOCATIONS BETWEEN FR 66 AND FR 68. REMOVED AND REPLACED L2 DOOR SILL PLATE IAW SRM 51-42-11, 51-44-11, DRAWING D53480505 AND EA A9-53R-12330.

Part: LOCK FASTENER — CORRODED (GIRT BAR) · corrosion level 2 · airframe 18,980 hrs · 9,004 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED L2 DOOR SILL AFT GIRT BAR FITTING CORRODED AT LOCK FASTENER. REMOVED AND REPLACED FASTENER IAW SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,980 hrs · 9,004 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED FLOORBEAM AT BS -Y1292 HAD CORROSION AT NUT PLATE HOLES BETWEEN FR 68 AND FR 69. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-00-14, FIG. 102. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,980 hrs · 9,004 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED SHEAR PLATE AT BS -Y1292 BETWEEN FR 69 AND FR 70 CORRODED. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14-101. REMOVED AND INSTALLED REPLACEMENT SHEAR PLATE IAW SRM 51-42-11, SRM 51-44-11 AND EA A9-53R-12329.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,980 hrs · 9,004 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED SHEAR PLATE AT Y1292, BETWEEN FR69 AND FR70, CORRODED. REMOVED AND REPLACED SHEAR PLATE AND FLOORBEAM IAW SRM 51-42-11 AND EA A9-53R-12329.

Part: RIVET — SHEARED (FUSELAGE) · airframe 18,980 hrs · 9,004 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED SHEARED RIVETS ON WEB AT STA. -Y1292 BETWEEN FR68 AND FR69. REMOVED AND REPLACED RIVETS IAW A319 SRM 51-44-11, 51-46-11 AND EA A9-53R-12329.

Part: MOUNT BOLT — CORRODED (LAVATORY) · corrosion level 2 · airframe 18,980 hrs · 9,004 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED LAV E LOWER FLOOR MOUNT BOLTS CORRODED. REMOVED AND REPLACED CORRODED FLOOR MOUNT BOLTS IN LAV E IAW AMM 25-43-42-PB401.

Part: BOLT — CORRODED (LAVATORY) · corrosion level 2 · airframe 18,980 hrs · 9,004 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED LAV "D" MOUNT BOLTS CORRODED. REMOVED AND REPLACED CORRODED MOUNT BOLTS IAW AMM 25-43-41-PB401.

Part: BATTERY PACK — FAILED (CABIN) · airframe 18,980 hrs · 9,004 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED RT OVERWING EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. REMOVED AND INSTALLED SERVICEABLE BATTERY PACK IN RT OVERWING EPSU IAW AMM 33-51-38-400-002. PERFORMED BITE TEST OF RT OVERWING EMERGENCY LIGHT EPSU/BATTERY PACK IAW 33-51-38-400-002 AND CHECKED GOOD.

Part: RELEASE CABLE — INOPERATIVE (EVAC SLIDE) · airframe 18,980 hrs · 9,004 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED LT OVERWING EMERGENCY EXIT SLIDE RELEASE CABLE WOULD NOT RETRACT. REMOVED AND REPLACED LT OVERWING EXIT SLIDE RELEASE CABLE IAW AMM 25-62-43-000-001. COMPLETED ADJUSTMENT AND OPERATIONAL CHECK OF SLIDE RELEASE CABLE IAW AMM 25-62-43-400-001. OPS CHECK GOOD.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 18,980 hrs · 9,004 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED AFT EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. REMOVED AND INSTALLED SERVICEABLE AFT EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-38-000-002. PERFORMED BITE TEST OF AFT EMERGENCY LIGHT EPSU/BATTERY PACK IAW AMM 33-51-38-400-002 AND CHECKED GOOD.

Part: BATTERY PACK — FAILED (CABIN) · airframe 18,980 hrs · 9,004 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED FWD EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. REMOVED AND INSTALLED SERVICEABLE BATTERY IN FWD EPSU (10WL) IAW AMM 33-51-38-400-002. PERFORMED A BITE TEST OF THE FWD EMERGENCY LIGHT EPSU/BATTERY PACK IAW AMM 33-51-38-400-002. OPS CHECK GOOD.

Part: RELEASE CABLE — INOPERATIVE (EVAC SLIDE) · airframe 18,980 hrs · 9,004 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED RT OVERWING EXIT SLIDE RELEASE CABLE WOULD NOT RETRACT. REMOVED AND REPLACED RT OVERWING SLIDE RELEASE CABLE IAW AMM 25-62-43-PB401.

Part: BATTERY PACK — FAILED (CABIN) · airframe 18,980 hrs · 9,004 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED LT OVERWING EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. REMOVED AND INSTALLED SERVICEABLE BATTERY IN LT OVERWING EPSU IAW AMM 33-51-38-420-052. PERFORMED BITE TEST IAW AMM 33-51-38-400-002 AND TESTED GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 13,041 hrs · 6,023 cycles

DURING C-3 CHECK, INSPECTION REPORTED CABIN EMERGENCY LIGHT SYSTEM TEST SHOWED EPSU INT LOADED AFT LEFT FAULT. FOR TROUBLESHOOTING PURPOSES, DISCONNECTED CONNECTOR TO AFT LEFT EPSU (13WL). RECONNECTED CONNECTOR AND PERFORMED OPS CHECK PER AMM 33-51-38-000-001, AMM 33-51-38-400-001. OPS CHECK GOOD PER AMM 33-51-00-710-001.

Part: HINGE PIN — MIGRATED (STRUCTURE) · airframe 13,041 hrs · 6,023 cycles

DURING C-3 CHECK, TECH SERVICES REPORTED HINGE PIN ON 103VU ELECTRICAL BOX HAD MIGRATED OUT. SHORTENED HINGE PIN ON 103VU ELECTRICAL BOX AND CRIMPED ENDS OF HINGE TO PREVENT FUTURE MIGRATION OF PIN PER EO A0-25EO-20207. THE MANDATORY INSPECTION (AD 2006-03-10) FOR THIS AIRCRAFT WAS ACCOMPLISHED ON 3/12/05 PER EO #A0-25EO-20207. NO MIGRATION WAS FOUND AT THAT TIME.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 13,041 hrs · 6,023 cycles

DURING C-3 CHECK, INSPECTION REPORTED STR 1L DAMAGED FWD SIDE OF FS 54. BURNISHED DAMAGED AREA PER ASRM 51-73-00. PERFORMED HFEC ON WORKED AREA AND FOUND NO DEFECTS PER NDTM PART 6, 51-10-08, PAGE 601. TREATED AND PRIMED PER AMM 51-23-00 AND EA A9-53R-11386, STEPS 1, 2, AND 3.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 13,041 hrs · 6,023 cycles

DURING C-3 CHECK, INSPECTION REPORTED FRAME 55 AT STR 2L DAMAGED INBD SIDE AFT EDGE. BURNISHED DAMAGED AREA PER ASRM 51-73-00. PERFORMED HFEC ON WORKED AREA AND FOUND NO DEFECTS PER NDTM PART 6, 51-10-08, PAGE 601. TREATED AND PRIMED AREA PER AMM 51-23-00 AND EA A9-53R-11386, STEPS 1,2 AND 3.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 13,041 hrs · 6,023 cycles

DURING C-3 CHECK, INSPECTION REPORTED STR 3R DAMAGED FWD SIDE OF FS 54. BURNISHED DAMAGED AREA PER ASRM 51-73-00. PERFORMED HFEC ON WORKED AREA AND FOUND NO DEFECTS PER NDTM PART 6, 51-10-08, PAGE 601. TREATED AND PRIMED AREA PER AMM 51-23-00 AND EA A9-53R-11386, STEPS 1, 2 AND 3.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 13,041 hrs · 6,023 cycles

DURING C-3 CHECK, INSPECTION REPORTED FRAME 55 AT STR 2R DAMAGED INBD SIDE AFT EDGE. BURNISHED DAMAGED AREA PER SRM 51-73-00. PERFORMED HFEC ON WORKED AREA AND FOUND NO DEFECTS PER NDTM PART 6, 51-10-08, PAGE 601. TREATED AND PRIMED AREA PER AMM 51-23-00 AND EA A9-53R-11386, STEPS 1, 2 AND 3.

Part: STRINGER — DAMAGED · airframe 13,041 hrs · 6,023 cycles

DURING C-3 CHECK, INSPECTION REPORTED STR 1R DAMAGED FWD SIDE OF FS 54. BURNISHED DAMAGED AREA PER ASRM 51-73-00. PERFORMED HFEC ON WORKED AREA AND FOUND NO DEFECTS PER NDTM PART 6, 51-10-08, PAGE 601. TREATED AND PRIMED PER AMM 51-23-00 AND EA A9-53R-11386, STEPS 1, 2 AND 3.

Part: COMPUTER — MALFUNCTIONED (NR 2 ELAC) · airframe 10,174 hrs · 4,637 cycles

AIR RETURN. AFTER DEPARTURE AT 8500 FT, ACFT PFD DISPLAYED ALTN LAW, AMBER XXS AND ECAM VERIFIED LANDING WT 130,400 PER POST FLIGHT REPORT. NR 2 ELAC REPLACED. OPS CHECKED GOOD PER AMM 27-93-34-401 AND 27-93-00-710-001. GROUND SCAN DETECTED NO FAULTS PER AMM 27-96-00-740-001. PERFORMED AFS TEST PER WORK CARD MP 22900-1. TESTED GOOD. COMPLIED WITH WORK CARD TC 22200-1, CAT 3B LAND VERIFY. CAT 3B RETAINED.

Part: ACTUATOR — FAULTY (TE FLAP) · airframe 8,967 hrs · 4,055 cycles

ON APPROACH, CREW REPORTED FLAP SYSTEM JAM WHEN FLAPS 2 SELECTED, SLATS EXTENDED TO E CONFIG 3. DECLARED AN EMERGENCY. CHECKED FLAP SYSTEM. FOUND LT WING NR 1 TRANSMISSION TORQUE LIMITER TRIPPED. RESET TORQUE LIMITER. PERFORMED TEST FLIGHT, MADE 3 APPROACHES & SYSTEM TESTED NORMALLY. REMOVED & REINSTALLED PANELS 575DB, 575EB, 575BB AND 573AB. PERFORMED FRICTION CHECK OF NR 4 LT FLAP TRANSMISSION, NR 3 FLAP ACTUATOR, NR 2 FLAP ACTUATOR AND INLINE OFFSET GEARBOX AND CHECKED GOOD. FOUND NR 1 LT AND RT FLAP ACTUATOR CAVITIES FULL OF WATER. REPLACED NR 1 LT AND RT FLAP ACTUATORS PER AMM 27-54-49-PB401 AND CHECKED NORMAL. PERFORMED OPS CHECK OF FLAPS PER AMM 27-54-45-000-003 AND 27-511-49-740-068.

Part: PCU — FAILED (TE FLAPS) · airframe 8,944 hrs · 4,042 cycles

UPON APPROACH SELECTED FLAPS 2, ECAM: FLT CTL FLAPS STUCK AT 0 DEG. RAN CHECK LISTS. FLIGHT CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. SLATS EXTENDED VAPP 155. PERFORMED TROUBLESHOOTING PER TSM 27-51-00-810-810. REPLACED FLAP PCU PER AMM 27-54-51PB401. FLAP SYSTEM OPERATION NORMAL.

Part: PROXIMITY SWITCH — INOPERATIVE (R1 DOOR) · airframe 4,207 hrs · 1,913 cycles

FLIGHT CREW REPORTED R1 DOOR OPEN INDICATION IN FLIGHT. COMPLETED ECAM PROCEDURES. DIVERTED TO IND AND LANDED WITHOUT INCIDENT. PERFORMED OPERATIONAL CHECK OF R1 DOOR PER MM 52-71-00-801. NO DEFECTS NOTED. PLACARD AS PRECAUTIONARY MEASURE PER MM 52-70-01B. PERFORMED OVERWEIGHT LANDING INSPECTION PER WORK CARD MP055104. NO DEFECTS NOTED. VISUALLY CHECKED DOOR WAS CLOSED AND LOCKED AT DEPARTURE. UPON ARRIVAL IN DEN, REPLACED F1 DOOR SLIDE ARMED HANDLE PROXIMITY SWITCH 4WN2 AND R1 DOOR PROXIMITY SWITCH 13WV2 PER MM 52-71-11. OPS CHECKED NORMAL AND PLACARD WAS REMOVED.

Part: INDICATOR — MALFUNCTIONED (COCKPIT) · airframe 1,071 hrs · 471 cycles

ABORTED TAKEOFF. FLIGHT CREW REPORTED AIRSPEED INDICATIONS UNRELIABLE AT 90 KTS. PERFORMED TSM 22-66-00-810-872, LOSS OF SPEED LIMITS INDICATION ON BOTH PFD'S. NO FAULTS ON PFR. RAN CFD'S CHECK OF NR 1, 2 AND 3 ADR'S. NO FAULTS NOTED. INSPECTED FOR HOT BRAKES PER TASK 05-51-16-200-001. ALLOWED BRAKES TIME TO COOL.