N922FR

Part: POWER SUPPLY — FAILED (CABIN) · airframe 50,244 hrs · 24,682 cycles

POWER SUPPLY UNIT FOR EMERGENCY LIGHTS 10WL FAILED EPSU TEST. REMOVED AND REPLACED POWER SUPPLY UNIT 10WL PER AMM 33-51-38 PB401. OPS CHECK GOOD.

Part: UPLOCK — INOPERATIVE (MLG DOOR) · airframe 50,021 hrs · 24,582 cycles

AFTER TAKE OFF, ECAM FOR LANDING GEAR SHOCK ABSORBER FAULT. MLG DOORS NOT CLOSED. REMOVED AND REPLACED NOSE GEAR DOOR UPLOCK ASSY IAW AMM 32-31-14 PB 401. LEAK CHECKED GOOD.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 49,898 hrs · 24,528 cycles

YELLOW HYD SYSTEM FAILURE, NO FLUID LOSS OF ACCUMULATOR PRESSURE. PUMP RAN 20 SECONDS, PTU RAN 30 SECONDS, FOUND HYD LINE LEAKING. REMOVED AND REPLACED HYDRAULIC LINE IAW AMM 20-23-11-911-001, AND 20-23-11-917-001. PERFORMED NR 2 ENGINE IDLE AND LEAK CHECKED GOOD. ACFT OK FOR SERVICE.

Part: SEAT TRACK — CORRODED (FRAME 66) · corrosion level 2 · airframe 48,376 hrs · 23,781 cycles

MAIN CABIN WET AREA AT FRAME 66, SEAT TRACK -Y765 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-11, 51-72-11-911-002, 53-00-14-283-002, 51-74-00, AND 51-44-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,376 hrs · 23,781 cycles

LT LOWER SIDE AT Y765 AND FR66 HAS CORROSION ALONG ATTACHMENT HOLE. REMOVED AND REPLACED FLOORBEAM Y765 AT FR 66 IAW SRM 51-72-11-911-001, SRM 53-00-14-283-002, SRM 51-21-11 AND SRM 53-41-14-283-004.

Part: SKIN — DENTED (FRAME 12) · airframe 48,376 hrs · 23,781 cycles

SKIN DENTED ONE INCH FORWARD OF FRAME 12, SIX INCH FORWARD OF OXYGEN DISCHARGE PORT. INSTALLED A REPAIR DOUBLER IAW SRM 53-00-11-300-029, FIGURE 001.

Part: DOOR SILL — CORRODED (R2 DOOR) · corrosion level 2 · airframe 48,376 hrs · 23,781 cycles

RIGHT R2 DOOR SILL WAS FOUND CORRODED AROUND THREE NUT PLATES. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-72-11-911-001, AND 53-41-14-300-001.

Part: FLOORBEAM — CORRODED (FRAME 66) · corrosion level 2 · airframe 48,376 hrs · 23,781 cycles

FLOORBEAM, Y512.5 CORRODED TOP SURFACE AT FRAME 66. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-72-11-911-001, AND 53-41-14-283-004.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 43,876 hrs · 23,781 cycles

RIGHT FLOOR SUPPORT -Y765 CORRODED ON THE TOP SURFACE BETWEEN FRAMES 66 - 68. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11-911-001, SRM 51-73-11, SRM 53-00-14-283-002, AND SRM 53-41-14-283-004.

Part: FLOORBEAM — CORRODED (FRAME 66) · corrosion level 2 · airframe 48,376 hrs · 23,781 cycles

FLOORBEAM, -Y464 CORRODED TOP SIDE AT FRAME 66. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-00, 51-72-11-911-001, 53-41-14-283-004, AND 51-42-11.

Part: SKIN — DENTED (FRAMES 23-24) · airframe 48,376 hrs · 23,781 cycles

SKIN DENTED, FOUND DURING WALK AROUND AT FRAMES 23 AND 24, STRINGERS 23 - 24L. INSTALLED A REPAIR DOUBLER IAW SRM 53-00-11-300-029.

Part: DOOR SILL — CORRODED (FRAMES 65-66) · corrosion level 2 · airframe 48,376 hrs · 23,781 cycles

THE L2 DOOR SILL CORRODED AROUND THREE NUTPLATES. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-21-11, SRM 51-23-11, SRM 51-22-11, SRM 51-42-11, 51-41-11, AND 51-41-14, SRM 51-44-00 AND SRM 53-41-14-300-001.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 48,376 hrs · 23,781 cycles

LEFT FLOOR SUPPORT -Y1292 CORRODED BETWEEN FRAMES 66 - 68. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, SRM 51-42-11, 53-41-14-283-004, 51-44-11, AND 53-00-14-283-001.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · corrosion level 2 · airframe 48,376 hrs · 23,781 cycles

FLOOR SUPPORT Y1292 CORRODED FROM FRAMES 66 - 64. FOUND OUT OF LIMITS IAW SRM 53-41-14-283-004. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND 51-42-11.

Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG) · airframe 44,705 hrs · 22,045 cycles

REFERENCE LOG PAGE 991830. AFTER TAKEOFF THE FLIGHT CREW RECEIVED A WARNING INDICATION THE LG FAILED TO RETRACT. PERFORMED AN AIR TURN BACK & THE ACFT RETURNED TO THE FIELD. PERFORMED AN INSPECTION OF THE NLG PROXIMITY SENSORS 24GA & 25GA & FOUND THE PROXIMITY SENSORS OUT OF CLEARANCE LIMITS. ADJUSTED THE CLEARANCE GAPS OF THE 24GA & 25GA PROXIMITY SENSORS IAW AMM 32-31-73-200-002A & 32-31-73-820-006A. PERFORMED A GEAR EXTENSION & RETRACTION TEST IAW AMM 32-30-00. OPERATIONAL CHECKED NORMAL.

Part: ENGINE — LEAKING (ZONE 600) · airframe 44,464 hrs · 21,927 cycles

AFTER TAKEOFF THE FLIGHT CREW RECEIVED A CARGO & LAVATORY SMOKE MSG. THE ACFT RETURNED TO THE FIELD & MX DISCOVERED OIL WETTING IN THE NR 2 ENG COMPRESSOR. MX REMOVED ENG SN 575632 & INSTALLED SERVICEABLE ENG 575640 IAW MPD TASK CARDS MP 71042-01, MP 71042-02 & REFERENCE DETAILS ON NON-ROUTINE 113264, 113272, 113273, 113274, 113275, 113277, 113278, 113279, 113280 & 113281.

Part: WEB — CRACKED (FUSELAGE) · corrosion level 2 · airframe 41,514 hrs · 20,554 cycles

AIRCRAFT DUE C8 CHECK, DISCREPANCY. MAIN CABIN RT TRAY WEB IS CRACKED 4'' AFT OF FRAME 68 RT. R & R CRACKED TRAY WEB IAW SRM 51-42-11 PAR 6 7 13. ACFT DUE OUT OF C CHECK 06 23 2015.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · corrosion level 2 · airframe 41,514 hrs · 20,554 cycles

AIRCRAFT DUE C8 CHECK, DISCREPANCY. MAIN CABIN LT SHEAR PLATE IS CRACKED AFT OF FRAME 69. R & R CRACKED SHEAR PLATE IAW SRM 51-42-11 PAR 6 13 & EO A0-53EO-31434. ACFT DUE OUT OF C CHECK 6 23 2015.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · corrosion level 2 · airframe 41,514 hrs · 20,554 cycles

AIRCRAFT DUE C8 CHECK, DISCREPANCY. MAIN CABIN LT SHEAR PLATE IS CRACKED AFT OF FRAME 69. R & R CRACKED SHEAR PLATE IAW SRM 51-42-11 PAR 6 1 & EO A0-53EO-31434. ACFT DUE OUT OF C CHECK 6 23 2015.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 39,188 hrs · 19,397 cycles

EMERGENCY EXIT LIGHTS SEAT ROWS 16, 17, 20, 21, 24 & 25 INOPERATIVE. R & R AFT EPSU 13WL. OPERATIONS TESTED GOOD IAW AMM 33-51-58 PB 401.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,707 hrs · 16,959 cycles

ACFT OUT OF SERVICE FOR C7-S2 CHECK. MAIN CABIN FLOORBEAM HAS CORROSION ONE FWD OF FR68 Y765. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 53-00-14, PB10L, 4.B, FIG L02. R & R FLOORBEAM IAW SRM 51-42-11, PAR5, A-C.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,707 hrs · 16,959 cycles

AIRCRAFT OUT OF SERVICE FOR C7-S2 CHECK. AFT CABIN FLOORBEAM JUST IN FRONT OF R2 DOOR HAD MINOR CORROSION AT FR 68, -Y1292. REMOVED CORROSION. CHECKED LIMITS. FOUND OUT OF LIMITS REF SRM 53-00-14 PB10L. 4.B. FIGL02. R & R FLOORBEAM REF SRM 51-42-11. PAR 5, A-C.

Part: SHEAR PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,707 hrs · 16,959 cycles

AIRCRAFT OUT OF SERVICE FOR C7-S2 CHECK. LEFT LATERAL SHEAR PLATE CORRODED AT FR 70, STR 23L. R & R SHEAR PLATE, REF SRM 52-42-11, PAR6 AND EO A0-53EO-31434.

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,707 hrs · 16,959 cycles

ACFT OUT OF SERVICE FOR C7-S2 CHECK. MAIN CABIN, FRAME SUPPORT HAS CORROSION EIGHT INCHES AFT OF FR 69, S23L. REMOVED CORROSION, 100 PERCENT MATERIAL LOSS, FOUND OUT OF LIMITS. R & R FRAME SUPPORT, REF SRM 51-42-11, PAR 6. B.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,707 hrs · 16,959 cycles

ACFT OUT OF SERVICE FOR C7-S2 CHECK. MAIN CABIN FLOORBEAM HAS CORROSION ONE INCH FWD OF FR 68, Y1292. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 53-00-14 PB101, 4.B, FIG102. R & R FLOORBEAM IAW SRM 51-42-11, PAR5 A-C.

Part: SHEAR PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,707 hrs · 16,959 cycles

AIRCRAFT OUT OF SERVICE FOR C7-S2 CHECK. RT LATERAL SHEAR PLATE CORRODED AT FR 70, STR 23R. R & R SHEAR PLATE, REF SRM 52-42-11, PAR 6 AND EO A0-53EO-31434.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,707 hrs · 16,959 cycles

ACFT OUT OF SERVICE DUE TO C7 S2 CHECK. SEAT TRACK CORRODED THREE INCHES AFT OF FRAME 31, Y765. REMOVED CORROSION IAW SRM 53-00-15, PBL01, PARA 4.A, FIG 102, SHEET 1, SRM 51-75-12, PARA 3.C.(1)-(7). FOUND TO BE WITHIN LIMITS.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,707 hrs · 16,959 cycles

ACFT OUT OF SERVICE DUE TO C7 S2 CHECK, SEAT TRACK CORRODED IN SEVERAL AREAS FRAME 28 TO FRAME 35 -Y765. REMOVED CORROSION IAW SRM 53-00-15, PBL01, PARA 4.A, FIG 102 SHEET 1, SRM 51-75-12, PARA 3.C.(1)-(7). FOUND TO BE WITHIN LIMITS.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,707 hrs · 16,959 cycles

AIRCRAFT OUT OF SERVICE DUE TO C7S2 CHECK. SEAT TRACK CORRODED TWELVE INCHES AFT OF FRAME 24 -Y1292. REMOVED CORROSION IAW SRM 53-00-15, PBL01, PARA 4.A, FIG 102 SHEET 1, SRM 51-75-12, PARA 3.C.(1)-(7). FOUND TO BE WITHIN LIMITS.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,707 hrs · 16,959 cycles

ACFT OUT OF SERVICE DUE TO C7S2 CHECK, SEAT TRACK CORRODED FROM FRAME 26 TO 27 -Y765. REMOVED CORROSION IAW SRM 53-00-15, PB101, PARAGRAPH 4.A., FIG 102 SHEET 1, SRM 51-75-12, PARAGRAPH 3.C.(1)-(7). FOUND TO BE WITHIN LIMITS.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,707 hrs · 16,959 cycles

AIRCRAFT OUT OF SERVICE DUE TO C7 S2 CHECK. CABIN SEAT TRACK CORRODED FIVE INCHES AFT OF FRAME 28, Y765. REMOVED CORROSION IAW SRM 53-00-15, PB101, PARA 4.A, FIG 102 SHEET 1, SRM 51-75-12, PARA 3.C.(1)-(7). FOUND TO BE WITHIN LIMITS.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,707 hrs · 16,959 cycles

ACFT OUT OF SERVICE DUE TO C7 S2 CHECK. SEAT TRACK CORRODED FOUR INCHES AFT OF FRAME 61 ON -Y765. REMOVED CORROSION IAW SRM 53-41-15, PB 101, PARAGRAPH 4 A, FIGURE 101, SRM 51-75-12, PARAGRAPH 3.C.(1)-(7). FOUND TO BE WITHIN LIMITS.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 34,707 hrs · 16,959 cycles

ACFT OUT OF SERVICE DUE TO C7 S2 CHECK. LT ELEVATOR THERMOGRAPHIC INSPECTION REVEALED INDICATIONS ON UPPER PANEL IRREGULAR IN SHAPE AND BLACK IN COLOR. REPAIRED IAW SRM 55-20-00, PB201, PARAGRAPH 2.A.(1-2), 2.B(1), 2.B(2)(A)1-10 AND SRM 55-21-11PB201, C1 PARA 5.E(2)(B)(1), 5.E(2)(B)(2), 5.E. (2)(C) FIG 205, SHEET 1 AND 2, 5.E.(2)(F)1-6, 5.E.(G).

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,059 hrs · 16,090 cycles

ESCAPE PATH LIGHT INOPERATIVE AT SEAT ROW 15 ABC. REPLACED ESCAPE PATH LIGHT AT 15 ABC. OPS CHECKED GOOD, REF AMM 33-51-19, PAGE BLOCK 401.

Part: WARNING LIGHT — FALSE ACTIVATION (PAX DOOR) · airframe 31,442 hrs · 15,256 cycles

AFT LT CABIN DOOR SHOWS OPEN INDICATION WHEN DOOR IS IN CLOSED AND ARMED POSITION (PAX DOOR CLOSED ECAM IND). PERFORMED OPS CHECK OF L-2 DOOR CLOSED INDICATION AS GOOD WITH NO FAULTS NOTED. REF AMM 52-71-00-710-001 A STEP 4A (1) 52-71-00-710-050 G. REMOVED MEL 52-70-01 D.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 31,330 hrs · 15,196 cycles

EXIT LIGHT ABOVE R2 DOOR DOES NOT COME ON. INSPECTED AND TROUBLESHOT R2 DOOR EXIT LIGHT SYS AND FOUND CONNECTOR DISCONNECTED. SECURED CONNECTOR AND EXIT LIGHT. OPS CHECKED NORMAL REF AMM 33-51-00-710-001.

Part: TRANSITION PANEL — DELAMINATED (ZONE 100) · airframe 26,366 hrs · 12,686 cycles

C-CHECK: NON ROUTINE N0467; AFT CARGO COMPARTMENT LT TRANSITION PANEL NR 151DE HAS A 1.0" PUNTURE AND 3.0" SQUARE OF DELAMINATION. FABRICATED REPLEACEMENT PANEL IAW MCG IRM 9701, REV G.

Part: ACCESS PANEL — CRACKED (LT NACELLE) · airframe 26,366 hrs · 12,686 cycles

C-CHECK: NON ROUTINE N0565; LT PYLON ACCESS PANEL NR413DL CRACKED. IAW SRM 54-50-80 AND PMS 01-04-21, STOP DRILLED CRACK ENDS AND WELDED.

Part: SKIN — CRACKED (NR 2 PYLON) · airframe 26,366 hrs · 12,686 cycles

C-CHECK: NON ROUTINE N0178; NR2 ENGINE PYLON UPPER PANEL NR423DL HAS A 1 EACH CRACK ON THE INTERIOR SIDE AT THE CUT OUT ABOUT .25" IN LENGHT. IAW SRM 54-52-11, STOP DRILL CRACK ENDS AND WELDED IAW PMS 01-04-21.

Part: SKIN — CRACKED (RT NACELLE) · airframe 26,366 hrs · 12,686 cycles

C-CHECK: NON ROUTINE N0179; RT PYLON UPPER PANEL NR 423DL HAS A 4.0" CRACK AROUND LOUVERS AND ABOUT 1.0" IN LENGHT. IAW SRM 54-52-11 AND PMS 01-04-21, STOP DRILLED CRACK AND WELDED.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,800 hrs · 12,400 cycles

WHILE TROUBLESHOOTING EPSU REF. SWAPPED LT FWD EPSU INTO MID POSITION RESULTING IN ITS FAILURE. R & R LT FWD EPSU 10WL, OPS CHECKS NORMAL IAW AMM 33-51-38, PB 401.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,800 hrs · 12,400 cycles

LT MID CABIN EPSU FAULTED. R & R LT MID CABIN EPSU 11WL. OPS CHECKS NORMAL IAW AMM 33-51-38, PB 401.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,796 hrs · 12,398 cycles

EXIT LIGHT ACFT LT OVERWING EXIT OUT AND EXIT LIGHT OVERHEAD AISLE MID-CABIN OUT. FOUND EPSU 11WL INOPERATIVE, R & R WITH SERVICE UNIT. IAW AMM 33-51-38 PB 401. OPS CHECK NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,766 hrs · 12,386 cycles

LT SIDE AFT FACING EXIT ROW SIDE AND EXIT SIGN INOPERATIVE. R & R LT OVERWING EPSU. IAW AMM 33-51-38, PB 401.

Part: CONDUIT — CHAFED (NR 1 SPOILER) · airframe 20,780 hrs · 9,913 cycles

DURING C4 C-CHECK, INSPECTION NOTED INSIDE OF PANEL 573DB THE WIRE BUNDLE FROM THE NR 1 SPOILER ACTUATOR WAS CHAFED BY AN ADJACENT HYDRAULIC LINE. NO DAMAGE FOUND TO HYDRAULIC LINE. INSPECTION FOUND MISSING INSULATION DOWN TO THE POLYAMIDE TAPE, WITH NO DAMAGE TO THE WIRES. MAINTENANCE REPAIRED 2794-4504 RED AND BLUE TWISTED WIRES FROM CONNECTOR 31CE1A PER ESPM 20-53-29 AND ESPM 20-53-21 SHEET 1, FIGURE 4, REPAIR TYPE 1B. MAINTENANCE ALSO PERFORMED REPAIR TYPE 1B ON TWISTED WIRE PAIRS 2794-4500, 2794-4505 AND 2794-4508, SAME REFERENCE AS ABOVE. REPAIR TYPE 1F WAS PERFORMED ON THE CONVOLUTED CONDUIT, REFERENCE ESPM 20-53-31, SHEET 1, FIGURE 3.

Part: FRAME — BROKEN (LT PYLON) · airframe 20,780 hrs · 9,913 cycles

DURING C4 C-CHECK, INSPECTION NOTED THAT THE LEFT PYLON HAS A BROKEN FRAME ON THE OUTBOARD SIDE NEAR AFT CORNER OF THE PRECOOLER. MAINTENANCE FABRICATED AND INSTALLED REPAIR EXTRUSION, REFERENCE SRM 51-42-11 AND 51-72-11.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,780 hrs · 9,913 cycles

DURING C4 C-CHECK, INSPECTION NOTED THE EMERGENCY EXIT LIGHT AT SEAT ROW NR 2 WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT, REFERENCE AMM 33-51-19-000-002 AND AMM 33-51-19-400-002. MAINTENANCE PERFORMED OPERATIONAL TEST, REFERENCE AMM 33-51-00-710-009, OPERATIONAL TEST NORMAL.

Part: SLIDE — UNWANTED DEPLOY (R1 DOOR) · airframe 16,229 hrs · 7,637 cycles

DURING THE TIME THE AIRCRAFT WAS ON THE GATE OVERNIGHT, A GATE AGENT INADVERTENTLY OPENED THE R1 DOOR AND DEPLOYED THE R1 DOOR EMERGENCY ESCAPE SLIDE. MAINTENANCE REMOVED AND REPLACED THE DEPLOYED SLIDE WITH A NEW UNIT IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 25-62-44-400-006. FOLLOWING COMPLETION OF THE INSTALLATION, THE UNIT RIG CHECKED GOOD. CORRECTED PART SN TO A12639 FROM A12679 AND ADDED TOTAL FLIGHT CYCLES.

Part: GIRT BAR — UNKNOWN (R2 DOOR SLIDE) · airframe 15,114 hrs · 7,132 cycles

ON FLIGHT FROM KDEN TO KSTL, FLIGHT CREW REPORTED SLIDE ARMING LEVER ON R2 DOOR POPPED OUT DURING FLIGHT. THE FWD F/A PANEL REGISTERED IT AS DISENGAGED, WHICH WAS CONFIRMED ON THE ECAM PAGE. AIRCRAFT WAS FERRIED ON THE RETURN TRIP TO KDEN. MAINTENANCE ADJUSTED THE R2 DOOR ESCAPE SLIDE AND GIRT BAR FITTINGS IAW AMM 52-13-00-820-057. PRESSURIZED AIRCRAFT IAW AMM 05-53-00-780-002-01. DOOR OPERATION AND INDICATION NORMAL. PERFORMED OPERATIONAL CHECK FLIGHT AND DISCREPANCY DID NOT DUPLICATE.

Part: GIRT BAR — MALFUNCTIONED (ESCAPE SLIDE) · airframe 15,114 hrs · 7,132 cycles

FLIGHT CREW REPORTED SLIDE ARMING LEVER ON R2 DOOR POPPED OUT DURING FLIGHT (1") AND CANNOT PUSH IT IN. REPACKED GIRT BAR ASSEMBLY AND PERFORMED ADJUSTMENT TEST OF THE RELEASE MECHANISM OF THE EMERGENCY ESCAPE SLIDE. PERFORMED OPS CHECK AND INDICATIONS NORMAL. REF A319-11 AMM 52-13-22-820-001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,112 hrs · 7,130 cycles

DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON SEAT TRACK AT FR66, Y1291. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-42-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,112 hrs · 7,130 cycles

DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON SHEAR PLATE BETWEEN FR 69 AND FR 70 AT -Y1162. REMOVED AND REPLACED SHEAR PLATE IAW DWG D5347418 AND D53471123.

Part: WEB — DAMAGED (FUSELAGE) · airframe 15,112 hrs · 7,130 cycles

DURING C-3 CHECK, INSPECTION REPORTED RIVETS SHEARED IN WEB JUST AFT OF L2 DOOR BETWEEN FR 68 AND FR 69. REMOVED AND REPLACED WEB AND FASTENERS IAW DRAWING D18D53480019 AND SRM 51-42-11.

Part: FAIRING — CRACKED (FUSELAGE) · airframe 15,112 hrs · 7,130 cycles

DURING C-3 CHECK, INSPECTION REPORTED APPROX A 2 1/2 INCH CRACK ALONG BOTTOM SECTION OF LT ENGINE INBD PYLON PANEL (ABOVE PANEL NR 473AR). REMOVED LATERAL FAIRING ASSY FROM LT ENG I/B SIDE IAW A319 MM 54-57-22-010-050. TRANSFERRED FASTENER HOLES AND NUT PLATES TO NEW FAIRING ASSY IAW SRM 51-72-11. INSTALLED REPLACEMENT LT ENG PYLON LATERAL FAIRING IAW AMM 54-51-21-400-001.

Part: RELEASE CABLE — OUT OF ADJUST (EMERGENCY EXIT) · airframe 15,112 hrs · 7,130 cycles

DURING C-3 CHECK, INSPECTION REPORTED RT EMERGENCY EXIT HATCH SLIDE RELEASE CABLE NEEDS ADJUSTMENT. ADJUSTED RT EMERGENCY EXIT HATCH SLIDE RELEASE. OPS TEST GOOD. RE-ATTACHED SLIDE RELEASE CABLE AND SAFTIED AS REQUIRED IAW 25-62-43-400-0001.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,112 hrs · 7,130 cycles

DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM AT Y1292 TO Y1162 JUST AFT OF FR 66 TO JUST FWD OF FR 68. REMOVED AND REPLACED FLOORBEAM IAW 51-42-11 AND DRAWING D53472780.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 15,112 hrs · 7,130 cycles

DURING C-3 CHECK, INSPECTION REPORTED EMERGENCY EXIT LIGHTS CONNECTOR 7260VC8 BROKEN. REMOVED AND REPLACED ELECTRICAL CONNECTOR 7260VC8 IN AFT CABIN EMERGENCY PATH FLOOR LIGHTING SYSTEM IAW AMM 33-51-08 P004, FIG 2. COMPLIED WITH OPERATIONAL TEST OF THE EMERGENCY LIGHTING IN THE CABIN BY THE EMERGENCY EXIT LT SWITCH. NO DEFECTS NOTED. PERFORMED THE OPERATIONAL TEST OF THE EMERGENCY LIGHTING IN THE CABIN BY THE "EMERGENCY EXIT LT" SWITCH IAW 33-51-00-710-008. NO DEFECTS NOTED.

Part: LUG — GOUGED (NR 3 SPOILER) · airframe 15,112 hrs · 7,130 cycles

DURING C-3 CHECK, INSPECTION REPORTED GOUGES IN RT WING NR 3 SPOILER ANTI-ROTATION LUG SURFACE. MACHINED ANTI-ROTATION FLAT, PERFORMED HFEC, AND BONDED REINFORCEMENT PLATE IAW EA NR A9-57R-12169.

Part: PLATE — GOUGED (LT WING) · airframe 15,112 hrs · 7,130 cycles

DURING C-3 CHECK, INSPECTION REPORTED GOUGES ON LT WING NR 3 SPOILER ANTI-ROTATION LUG SURFACES. MACHINED ANTI-ROTATION FLAT, PERFORMED HFEC, AND BONDED REINFORCING PLATE IAW EA NR A9-57R-12172.

Part: LUG — GOUGED (NR 4 SPOILER) · airframe 15,112 hrs · 7,130 cycles

DURING C-3 CHECK, INSPECTION REPORTED GOUGES ON RT WING NR 4 SPOILER ANTI-ROTATION LUG SURFACE. MACHINED ANTI-ROTATION FLAT, PERFORMED HFEC, AND BONDED REINFORCING PLATE IAW EA A9-57R-12170.

Part: LUG — GOUGED (NR 4 SPOILER) · airframe 15,112 hrs · 7,130 cycles

DURING C-3 CHECK, INSPECTION REPORTED GOUGES ON LT WING NR 4 SPOILER ANTI-ROTATION LUG SURFACE. MACHINED ANTI-ROTATION FLAT, PERFORMED HFEC, AND BONDED REINFORCING PLATE IAW EA A9-57R-12171.

Part: STRUCTURE — CORRODED (SILL) · corrosion level 2 · airframe 15,112 hrs · 7,130 cycles

DURING C-3 CHECK, INSPECTION REPORTED L2 DOOR SILL FWD GIRT BAR FITTING ATTACHMENT HOLE LOCATION AFT INBD CORRODED. REPAIRED DAMAGE IAW EA A9-53R-12160.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,112 hrs · 7,130 cycles

DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM -Y1292 ON UPPER SURFACE AT NUTPLATE HOLE, APPROX 8 INCHES AFT OF FR 67. REMOVED AND REPLACED FLOORBEAM IAW SRM'S 51-42-11, 51-72-11 AND 51-44-11.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,112 hrs · 7,130 cycles

DURING C-3 CHECK, INSPECTION REPORTED SHEAR PLATE SUPPORT AT -Y1292 BETWEEN FR69 TO FR70 CORRODED. REMOVED AND REPLACED SHEAR PLATE SUPPORT IAW AIRBUS DRAWINGS D53474180 AND D53471123, AND SRM 51-42-11, PARA 6B AND 7B.

Part: THRESHOLD — CORRODED (R1 DOORWAY) · airframe 15,112 hrs · 7,130 cycles

DURING C-3 CHECK, INSPECTION REPORTED R1 DOOR THRESHOLD STRIP CORRODED ON LOWER SURFACE. REMOVED AND REPLACED R1 THRESHOLD STRIP IAW AMM 53-12-991-003.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,112 hrs · 7,130 cycles

DURING C-3 CHECK, INSPECTION REPORTED LT FWD CARGO COMPARTMENT UNDER FLOOR TRANSITION PANEL SUPPORT HAD CORRODED FASTENER HOLE FROM FR 25 TO FR 30. REMOVED AND REPLACED SUPPORT PLATE IAW SRM 51-42-11, PAGE 7-9, SEC A-C.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,112 hrs · 7,130 cycles

DURING C-3 CHECK, INSPECTION REPORTED FWD CARGO COMPARTMENT FASTENER HOLES UNDER FLOOR SUPPORT FROM STR 38L TO STR 38R CORRODED. REMOVED AND REPLACED SUPPORT PLATE IAW SRMS 51-42-11 AND 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,112 hrs · 7,130 cycles

DURING C-3 CHECK, INSPECTION REPORTED CORRODED FASTENER HOLES UNDER FLOOR SUPPORT AT FR 28 IN FWD CARGO COMPARTMENT AND EXISTING REPAIR FROM STR 38L TO 38R. REMOVED AND REPLACED FLOOR SUPPORT PLATE AT FR 28 FROM STR 38L TO STR 38R IAW SRM 51-42-11, 51-44-11, 51-46-11, AND 51-72-11.

Part: COVER — CORRODED (L1 DOOR) · corrosion level 2 · airframe 15,112 hrs · 7,130 cycles

DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON LOWER SURFACE OF L1 DOOR THRESHOLD STRIP. REMOVED AND REPLACED THRESHOLD STRIP IAW AMM 53-12-12-400-001.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,112 hrs · 7,130 cycles

DURING C-3 CHECK, INSPECTION REPORTED CORRODED FASTENER HOLES UNDER FLOOR SUPPORT IN FWD CARGO COMPARTMENT FROM FR 24 TO FR 28. REMOVED CORROSION IAW SRM 51-74-00. PERFORMED HFEC ON BLENDOUTS OF CORROSION IAW NTM 51-10-08, PART 6. NO CRACKS NOTED. PERFORMED ULTRASOUND IAW NTM 51-10-04, PART 4. ONE LOCATION FWD OF FR C27 OUT OF LIMITS. AREA BLENDED WITH ADJACENT NUTPLATE REMOVED IAW EA #A9-53R-12159. PERFORMED ROTO PROBE INSPECTION OF FASTENER HOLE IAW NTM 51-10-01, PART 6. NO DEFECTS NOTED.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,112 hrs · 7,130 cycles

DURING C-3 CHECK, INSPECTION REPORTED RT FWD CARGO COMPARTMENT UNDER FLOOR TRANSITION PANEL SUPPORT HAD CORRODED FASTENER HOLE FROM FR 28 TO FR 31. REMOVED AND REPLACED SUPPORT PLATE IAW SRM 51-72-11.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,112 hrs · 7,130 cycles

DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON L2 DOOR SILL AT FR 66 NUT PLATE HOLE. REPAIRED L2 DOOR SILL IAW EA NR A9-53R-12173.

Part: SHEAR PLATE — DAMAGED (FUSELAGE) · airframe 15,112 hrs · 7,130 cycles

DURING C-3 CHECK, INSPECTION REPORTED SHEARED RIVETS IN SHEAR PLATE BETWEEN FR 69 AND FR 70 AT Y1162. FOUND SHEAR PLATE TO BE OUT OF LIMITS IAW SRM 53-00-14. REMOVED SHEAR PLATE IAW SRM 51-72-11. INSTALLED NEW SHEAR PLATE TO SUPPORT ASSY BETWEEN FR 69 AND FR 70 IAW SRM 51-42-11, PARA 6 AND 14.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,112 hrs · 7,130 cycles

DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM AT Y1162, FR 68. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11, PARA 7, AND AIRBUS DRAWING D53472780.

Part: EPSU — FAILED (EMERGENCY LIGHTS) · airframe 15,112 hrs · 7,130 cycles

DURING C-3 CHECK, INSPECTION REPORTED A/C FAILED EMERGENCY LIGHTS BATTERY CAPACITY TEST. REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY PACKS 10WL, 13WL, 11WL, AND 12WL IAW AMM 33-51-38-000-002 AND AMM 33-51-38-400-002. PERFORMED OPERATIONAL TEST OF EPSU'S IAW 33-51-38-400-002. TESTED GOOD.

Part: LIGHT — UNKNOWN (CABIN) · airframe 14,716 hrs · 6,934 cycles

FLIGHT CREW REPORTED C/B H05 TRIPPED IN FLIGHT, WHICH IS AN EMERGENCY LIGHT C/B. MAINTENANCE INSPECTED THE EMERGENCY LIGHT SYSTEM AND FOUND NO FAULTS. RESET C/B AND PERFORMED SYSTEM TEST. NO FAULTS FOUND.

Part: VALVE — FAILED (NR 1 ENGINE) · airframe 14,603 hrs · 6,879 cycles

DURING TAKEOFF FROM KMDW, FLIGHT CREW RECEIVED AN ECAM AIR BLEED 2 FAULT. RAN ECAM ACTION FOR FAULT. APPROX 1 HR INTO THE FLIGHT, THEY RECEIVED AN ECAM AIR BLEED 1 FAULT, THEN LOST BOTH PACKS. PERFORMED AN EMERGENCY DESCENT TO 10,000 FT AND DECLARED AN EMERGENCY. AIRCRAFT LANDED AT KDEN WITHOUT INCIDENT. NR 1 AND NR 2 ENGINE FAN AIR VALVES FAILED FUNCTIONAL TEST IAW AMM 36-11-54-720-001. REMOVED AND REPLACED NR 1 AND NR 2 ENGINE FAN AIR VALVES IAW AMM 36-11-54-000-001 AND 36-11-54-400-001. PERFORMED LEAK CHECK OF NR 1 AND NR 2 ENGINE FAN AIR VALVE CONNECTIONS IAW AMM 36-11-54-790-050, STEP B. (3) AND (4). PERFORMED OPERATIONAL TEST OF NR 1 AND NR 2 ENGINE FAN AIR VALVES IAW AMM 36-11-54-790-050 AND 36-1

Part: SCREW — MISSING (FLAP TRACK) · airframe 1,729 hrs · 823 cycles

FLIGHT CREW REPORTED FASTENER MISSING FROM FLAP TRACK ON RT WING IB OF ENGINE PYLON. PLACED ON MAC 0001276. DETERMINED THIS DID NOT AFFECT SAFETY OF FLIGHT. ON 2/10/04, REPLACED SCREW.