N921FR

Part: PLATE — CORRODED (ZONE 100) · airframe 45,718 hrs · 22,495 cycles

LAVATORY WASTE VACUUM PORT SKIN CRACKING. CUTOUT DAMAGE, FABRICATED AND INSTALLED DOUBLER, FILLERS AND CONNECTION PLATE. RESTORED AREA IAW SRM 53-41-11-300-004 FIG 2, AMM 25-55-12-000-001-A, AND 25-55-12-420-050 B.

Part: SKIN — DEBONDED (RT ELEVATOR) · corrosion level 2 · airframe 39,712 hrs · 19,681 cycles

AIRCRAFT DUE C8 & S2 CHECK. DISCREPANCY, RT ELEVATOR THERMO GRAPHIC INSPECTION SHOWS INDICATIONS THAT ARE IRREGULAR IN SHAPE & BLACK IN COLOR. REPAIRED LT ELEVATOR WITH HOT BONDER IAW SRM 55-20-00, PB201, PAR 2 A & SRM 55-21-11, PB201, C1, PAR 5 D, FIG 204. ACFT DUE OUT OF CHECK 3/22/15.

Part: SKIN — DEBONDED (LT ELEVATOR) · corrosion level 2 · airframe 39,712 hrs · 19,681 cycles

AIRCRAFT DUE C8 & S2 CHECK. DISCREPANCY, LT ELEVATOR THERMO GRAPHIC INSPECTION SHOWS INDICATIONS THAT ARE IRREGULAR IN SHAPE & BLACK IN COLOR. REPAIRED LT ELEVATOR WITH HOT BONDER IAW SRM 55-20-00, PB201, PAR 2 A & SRM 55-21-11, PB201, PAR 5 E. SEE NDT REPORT FOR LOCATIONS. ACFT DUE OUT OF CHECK 3/22/15.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,712 hrs · 19,681 cycles

ACFT DUE C8 & S2 CHECK. DISCREPANCY, RT AFT LATERAL SHEAR PLATE HAS CORROSION. R & R SHEAR PLATE IAW SRM 51-42-11. ACFT DUE OUT OF C CHECK ON 3/22/2015.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,712 hrs · 19,681 cycles

ACFT DUE C8 & S2 CHECK. DISCREPANCY, LT AFT LATERAL SHEAR PLATE HAS CORROSION. R & R SHEAR PLATE IAW SRM 51-42-11. ACFT DUE OUT OF C CHECK ON 3/22/2015.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,712 hrs · 19,681 cycles

ACFT DUE C8 & S2 CHECK. DISCREPANCY, MAIN CABIN FLOOR & TRACK BEAM HAS CORROSION AT FRAME 19 - 20, Y1292, OUT OF LIMITS. R & R BEAM IAW SRM 51-42-11. ACFT DUE OUT OF C CHECK ON 3/22/2015.

Part: IDG — FAILED (NR 1 ENGINE) · airframe 37,015 hrs · 18,239 cycles

NUMBER 1 ENG GEN FAILED IN FLIGHT, UNABLE TO RESET. NR 2 ENG GEN FAILED IN FLIGHT, UNABLE TO RESET. REPLACED NR 1 ENG IDG IAW AMM 24-21-51 PB 401. OPERATIONS & LEAK CHECKED GOOD. R & R NR 2 ENG IDG IAW AMM 24-21-57 PB 401.

Part: BLOWER — SEIZED (ZONE 100) · airframe 36,527 hrs · 17,975 cycles

DISCREPANCY LP 828679 ITEM P 1. VENT BLOWER FAULT EN ROUTE. R & R FAN EXTRACT BLOWER, FIN 20HQ IAW AMM 21-26-51 PB 401. PERFORMED OPERATIONS CHECK OF AVIONICS EQUIPMENT VENTILATION IAW AMM 21-26-00-710-001A & OPERATIONS CHECK TEST OF AVIONICS SMOKE DETECTION IAW AMM 26-15-00-710-001A. OPERATIONS CHECKED GOOD, NO SMOKE DETECTED.

Part: DUCT CLAMP — SEPARATED (AC BAY) · airframe 35,547 hrs · 17,470 cycles

AIRCRAFT WAS OPERATING FLIGHT 245 IAH-DEN, DEC 7, 2013. PACK 2 WAS ALREADY INOPERATIVE ON MEL, MDDR 1101834. PACK 1 FAILED IN FLIGHT, CABIN ALTITUDE CLIMBED TO THE POINT 02 MASKS DEPLOYED, AIRCRAFT DIVERTED TO DFW. AIRCRAFT WAS FERRIED TO GYR WITH BOTH PACKS INOPERATIVE & UNPRESSURIZED. PACK 1 DUCT CLAMP SEPARATED. REPLACED DUCT CLAMP & SEALS IAW AMM 21-52-23-400-001-A. R & R NR 1 PACK CONTROLLER FOR PACK 1 FAULT IAW AMM 21-61-34 PB401, OPERATIONS & LEAK TESTED GOOD.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 33,783 hrs · 16,525 cycles

ACFT OUT OF SERVICE DUE TO C7 CHECK. EMERGENCY LIGHT LOCATED AT PASSENGER SEAT ROW NR 2 LT IS INOPERATIVE. R & R LIGHT ASSY IAW AMM 33-51-19-020-051D, STEP 4.A, 1-2 AND AMM 33-51-19-420-051D STEP 4.B, 1-2. OPS CHECKED GOOD.

Part: PIN — BINDING (EMERGENCY EXIT) · airframe 33,783 hrs · 16,525 cycles

AIRCRAFT OUT OF SERVICE DUE TO C7 CHECK. UNABLE TO DISARM LT EMERGENCY EXIT DOOR FROM INSIDE ACFT. REMOVED DOOR IN ARMED POSITION IAW AMM 52-21-00-710-003-A, STEP 4.A (2)1. INSPECTED LATCH PIN RELEASE LEVER AREA FOR DAMAGE, NO DAMAGE WAS NOTED. INSTALLED DOOR IAW AMM 52-21-11-400-001-A, STEP 4.A. PERFORMED OPS TEST OF THE UNLOCKING AND THE OPENING FROM THE CABIN IN THE ARMED MODE IAW AMM 52-21-00-710-003-A. OPS TESTED GOOD.

Part: BALLAST — FAILED (CABIN LIGHTS) · airframe 31,333 hrs · 15,234 cycles

ODOR COMING FROM AFT CABIN. R & R BALLAST ASSY COVE LIGHT AT ROW 24 DEF. OPS CHECK GOOD, NO TROUBLE NOTED REF AMM 33-21-11, PAGE BLOCK 401.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 30,702 hrs · 14,907 cycles

UNIT HARD FAULTED ON SELF TEST. ACFT WAS PLACED IN OUT OF SERVICE STATUS. R & R POWER SUPPLY UNIT. SYS CHECKED GOOD. ACFT RETURNED TO SERVICE IAW AMM 33-51-38, P 401.

Part: SKIN — DENTED (ZONE 200) · airframe 29,659 hrs · 14,406 cycles

C-CHECK: NON ROUTINE NR 37572; RT FUSELAGE SKIN AT FRAME 54, STRINGER 22 RT HAS A DENT. REPAIRED DENT IAW SRM 53-00-11 PB201 PARA 4A, FIG 205 AND NTM 51-10-08-250-802.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 28,454 hrs · 13,804 cycles

DURING MX, PERFORMED OPS CHECK OF THE EMERGENCY LIGHTING, RECEIVED A FAILURE MESSAGE OF EPSU BATTERY PERFORMED TSM 33-51-00-810-801 AND FOUND WEAK BATTERY. R & R BATTERY IAW AMM 33-51-00-710-006, AMM 33-51-38-000-002 AND AMM 33-51-38-400-002. OPS CHECKED GOOD.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 25,335 hrs · 12,276 cycles

C-CHECK: NON ROUTINE N0573: AFT CARGO FLOOR PANEL 162EF HAS TOP SKIN DISBONDED FWD INBD CORNER. FABRICATED AND REPLACEMENT PANEL 162 EF IAW MCG IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 25,335 hrs · 12,276 cycles

C-CHECK: NON ROUTINE N0687: AFT CARGO TRASITION FLOOR PANEL 151 AE UPPER SURFACE DELAMINATED 4 AREAS. FABRICATED PANEL 151 AE IAW MCG IRM 9701 REV G.

Part: SKIN — DAMAGED (ZONE 100) · airframe 25,335 hrs · 12,279 cycles

C-CHECK: NON ROUTINE N0012; FRAME 17, STR 30L LIGHTNING STRIKE, TEMPORARY REPAIR IAW SRM 53-11-11 FIG 207. REPAIR IAW SRM 53-11-11.

Part: FLOOR PANEL — PUNCTURED (ZONE 100) · airframe 25,335 hrs · 12,276 cycles

C-CHECK: NON ROUTINE N0622; AFT PIT SLOPE PANEL 151GE (LOWER) PUNCTURED. FABRICATED REPLACEMENT PANEL 151 GE IAW MCG IRM 9701, REV G.

Part: FLOOR PANEL — DENTED (ZONE 100) · airframe 25,335 hrs · 12,276 cycles

C-CHECK: NON ROUTINE N0549; AFT PIT TRANSITION PANEL 161CF HAS APPROX 35 DENTS ALONG ENTIRE PANEL LENGHT. FABRICATED REPLACEMENT PANEL 161CF IAW MCG IRM 9701, REV G.

Part: HMU — MALFUNCTIONED (NR 2 ENGINE) · airframe 21,199 hrs · 10,286 cycles

PILOT REPORTED ON DESCENT, THE NR 2 ENG SHUTDOWN. MX REMOVED AND REPLACED THE NR 2 ENG HYDRO MECHANICAL UNIT AND PERFORMED OPS AND LEAK CHECK IAW AMM 73-21-10-000-002 AND 73-21-10-400-002. THE OPS CHECK FLIGHT WAS SUCCESSFUL, REF LOG PAGE 464330.

Part: SENSOR — MALFUNCTIONED (NR 2 ENGINE) · airframe 20,992 hrs · 10,171 cycles

DURING DESCENT, PILOT REPORTED NR 2 ENG N1, N2, EGT AND FUEL FLOW WERE FLUCTUATING DRASTICALLY, HIGH POWER TO LOW PWR WITH NO APPARENT YAW OF THE PLANE. PILOT STATES THAT IT SEEMED LIKE THE NR 2 ENG WAS OPERATING NORMALLY, BUT IGNITION DID TURN ON AUTOMATICALLY WHEN SITUATION OCCURRED AND THEY NOTICED AUTO THRUST OF THE NR 2 ENG LAGGED SLIGHTLY BEHIND THE NR 1 ENG. MX PERFORMED TROUBLESHOOTING AND INSP IAW TSM 70-00-00-810-866 AND TSM 73-20-00-810-920. MX REMOVED AND REPLACED THE NR 2 ENGINE T-12 SENSOR IAW AMM 73-21-40 PB401. ACFT WAS DETERMINED OK FOR CONTINUED SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 20,049 hrs · 9,685 cycles

PILOT REPORTED THAT THE AFT EXIT SIGN LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT, REFERENCE AMM 33-51-17 PB 401 AND AMM 33-51-39 PB 401.

Part: SKIN — DAMAGED (ZONE 100) · airframe 19,905 hrs · 9,613 cycles

PILOT REPORTED LIGHTNING STRIKE ON ACFT LEFT FRONT. MAINTENANCE DETERMINED DAMAGE TO BE LOCATED AT FRAME 34 + 8 INCH AND STRINGER 20L. MAINTENANCE PERFORMED MAJOR REPAIR BY REMOVING DAMAGED AREA AND INSTALLING SKIN PATCH IAW SRM 53-21-11 FIGURE 213.

Part: PROXIMITY SENSOR — OUT OF ADJUST (EMERGENCY EXIT) · airframe 19,614 hrs · 9,458 cycles

DURING CLIMB-OUT, "EMERGENCY EXIT" AMBER INDICATION APPEARED. MAINTENANCE ADJUSTED THE LT EMERGENCY EXIT PROXIMITY SWITCH IAW AMM 57-71-00-820-009 AND PERFORMED OPERATIONAL CHECK OF THE WARNING SYSTEM IAW AMM 52-73-00-710-002.

Part: SILL — CORRODED (FUSELAGE) · airframe 19,614 hrs · 9,458 cycles

REFERENCE NON-ROUTINE C059497. DURING C4/S1 C-CHECK, INSPECTION NOTED AFT (SMALLER SECTION) OF AFT PIT DOOR SILL 152YG HAS CORROSION. MAINTENANCE REPLACED THE PLATE ASSEMBLY WITH NEW AND INSTALLED ON ROUTINE WORK CARD CP753-25.

Part: FASTENER — SHEARED (FUSELAGE) · airframe 19,614 hrs · 9,458 cycles

REFERENCE NON-ROUTINE C059730. DURING C4/S1 C-CHECK, INSPECTION NOTED THE FORWARD GALLEY FLOORBEAM FITTING Y765 AT FRAME 12 HAS SHEARED HI-LOK AND LOOSE HI-LOK. MAINTENANCE REPLACED THE FITTING IAW SRM 51-42-11 PARAGRAPH 7.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 19,614 hrs · 9,458 cycles

REFERENCE NON-ROUTINE C059718. DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION ON THE CENTERLINE FRAME BETWEEN FRAME 57 AND FRAME 58 AT FASTENER HOLE AND DIRECTLY BELOW. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11 PARAGRAPH 5 AND 6.

Part: SLIDE — DISCONNECTED (L1 DOOR) · airframe 19,614 hrs · 9,458 cycles

REFERENCE NON-ROUTINE C059791. DURING C4/S1 C-CHECK, INSPECTION NOTED THE L1 DOOR ESCAPE SLIDE PACK RELEASE MECHANISM ON BACK HAS TWO RELEASE CABLES DISCONNECTED. MAINTENANCE REMOVED L1 SLIDE PACK ASSEMBLY AND INSTALLED NEW SERVICEABLE IAW AMM 25-62-44-400-006.

Part: SHEAR PLATE — CORRODED (ZONE 200) · airframe 19,614 hrs · 9,458 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED THE RIGHT SHEAR PLATE AT FRAME 70 WAS CORRODED. MAINTENANCE REMOVED AND REPLACED THE RIGHT SHEAR PLATE IAW SRM 51-42-11 PG7 AND 51-72-11.

Part: SHEAR PLATE — CORRODED (ZONE 200) · airframe 19,614 hrs · 9,458 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED THE LEFT SHEAR PLATE WAS CORRODED AT FRAME 70. MAINTENANCE REMOVED AND REPLACED THE LEFT SHEAR PLATE AT FRAME 70 IAW SRM 51-42-11 PG7 AND 51-72-11.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 19,614 hrs · 9,458 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED THE FORWARD GALLEY FLOORBEAM Y-1292 AT FRAME 20 WAS CORRODED ON THE UPPER SURFACE. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-40-00 PARAGRAPH 2B, SRM 51-40-00 PARAGRAPH 3B AND SRM 51-72-11.

Part: SILL — CORRODED (FUSELAGE) · airframe 19,614 hrs · 9,458 cycles

REFERENCE NON-ROUTINE C059845. DURING C4/S1 C-CHECK, INSPECTION NOTED THE AFT CARGO DOOR SILL WEB HAS SPOTS OF CORROSION FROM FRAME 56 TO THE FORWARD CUTOUT OF C-2 DOOR. MAINTENANCE REPAIRED CORROSION IAW ENGINEERING AUTHORIZATION A9-53R-31000 STEPS 1 THRU 5.

Part: SHEAR PLATE — LOOSE (ZONE 200) · airframe 19,614 hrs · 9,458 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED THAT THE LEFT SILL PLATE BETWEEN FRAME 68 AND FRAME 69 HAS SHEARED RIVETS. MAINTENANCE REMOVED AND REPLACED SHEARED RIVETS (P/N DAN6-5-4) IAW ENGINEERING AUTHORIZATION A9-53T-30392, STEP 2.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 19,614 hrs · 9,458 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED THE FLOORBEAM Y1292 AT FRAME 66 HAS CORROSION AT NUT CLIP HOLE. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11, 51-44-11, 51-40-00, 51-72-11 AND ENGINEERING AUTHORIZATION A9-53T-30392 STEPS 1 AND 2.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 19,614 hrs · 9,458 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED FLOORBEAM AT Y1162 AT FRAME 68 HAS CORROSION AT NUT CLIP HOLE. MAINTENANCE REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11 PG 7, SRM 51-42-11 AND ENGINEERING AUTHORIZATION A9-53T-30392 STEPS 1 AND 2.

Part: FLOOR PANEL — CORRODED (ZONE 200) · airframe 19,614 hrs · 9,458 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED THE AFT GALLEY FLOOR PANEL, 261PF, HAS INSERTS PULLED OUT BY CORROSION. MAINTENANCE INSTALLED A NEW FLOOR PANEL IAW AMM 53-42-12-400-001.

Part: PROFILE — CORRODED (ZONE 100) · airframe 19,614 hrs · 9,458 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION ON THE CENTERLINE FRAME BETWEEN FRAME 59 AND FRAME 58 AT FASTENER HOLE. MAINTENANCE REMOVED, FABRICATED AND INSTALLED FLOOR SUPPORT IAW AIRBUS DWG D53476573 AND SRM 51-42-11.

Part: CHANNEL — CORRODED (ZONE 100) · airframe 19,614 hrs · 9,458 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION ON THE U CHANNEL AT FRAME 59, STRINGER 38R TO 40R. MAINTENANCE REMOVED AND REPLACED THE U CHANNEL IAW SRM 51-42-11 AND 51-72-11.

Part: FITTING — SHEARED (ZONE 100) · airframe 19,614 hrs · 9,458 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED THE FORWARD GALLEY FLOORBEAM Y1292 AT THE FITTING THAT ATTACHES TO CROSS BEAM AT FRAME 12 HAS A SHEARED LOCK FASTENER AND A LOOSE LOCK FASTENER BELOW THE SHEARED ONE. MAINTENANCE INSTALLED A NEW FITTING AND FASTENERS IAW ENGINEERING AUTHORIZATION A9-53R-31018.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 19,614 hrs · 9,458 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION AT THE NUT CLIP HOLE ON FLOORBEAM -Y1162. MAINTENANCE REMOVED AND REPLACED FLOORBEAM IN REFERENCE TO SRM 51-42-11 AND 53-41-14 FIGURE 11.

Part: FRAME — CORRODED (ZONE 100) · airframe 19,614 hrs · 9,458 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION IN SEVERAL FASTENER HOLES AT FLOOR PANEL MATING SURFACE IN AFT PIT AT FRAME 59 BETWEEN STRINGER 38L AND 38R. MAINTENANCE REPAIRED FASTENER HOLES IAW ENGINEERING AUTHORIZATION A9-53R-31013, STEPS 1-5.

Part: SILL — CORRODED (FUSELAGE) · airframe 19,614 hrs · 9,458 cycles

DURING C4 C-CHECK, INSPECTION NOTED THE L2 DOOR SILL, AFT, INBOARD NUT PLATE HOLE HAS CORROSION AT FRAME 68. MAINTENANCE PERFORMED REPAIR IAW A319 SRM 53-41-14 FIGURE 201.

Part: SILL — CORRODED (ZONE 200) · airframe 19,614 hrs · 9,458 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION ON THE L2 DOOR SILL AT FRAME 66. MAINTENANCE REMOVED CORROSION DAMAGE AND PERFORMED REPAIR IAW ENGINEERING AUTHORIZATION A9-53R-30999.

Part: CYLINDER — DEFECTIVE (R1 DOOR) · airframe 19,614 hrs · 9,458 cycles

DURING C4 C-CHECK, INSPECTION NOTED THE R1 DOOR FAILED THE DAMPING TEST. MAINTENANCE REMOVED AND REPLACED THE CYLINDER AT DOOR R1 IAW AMM 52-11-14-000-001 AND AMM 52-11-14-400-001.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 19,614 hrs · 9,458 cycles

REFERENCE NON-ROUTINE C059560. DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION ON FLOOR PANEL 222FF. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL IAW AMM 53-12-12 PB 401.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 19,614 hrs · 9,458 cycles

REFERENCE NON-ROUTINE C059559. DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION ON FLOOR PANEL 221FF. MAINTENANCE REPLACED FLOOR PANEL IAW AMM 53-12-12 PB 401.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 19,614 hrs · 9,458 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED THE "TEST EMERGENCY LIGHT BATTERIES" TEST FAILED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNITS AT POSITIONS 10WL, 11WL, 12WL AND 13WL AND PERFORMED OPERATIONAL TEST IAW AMM 33-51-38-000-002 AND 33-51-38-400-002.

Part: CABLE — LACK OF LUBE (EMERGENCY EXIT) · airframe 19,614 hrs · 9,458 cycles

INSPECTION NOTED THAT THE LEFT OVERWING EMERGENCY EXIT FAILED THE OPERATIONAL TEST OF THE UNLOCKING AND OPENING FROM THE CABIN IN THE ARMED MODE. MAINTENANCE LUBRICATED THE LEFT OVERWING EXIT SLIDE CABLE IAW ENGINEERING AUTHORIZATION AO-52T-30102 AND PERFORMED OPERATIONAL CHECK IAW AMM 52-21-00-720-001.

Part: WIRE — BROKEN (RUDDER PEDAL) · airframe 18,322 hrs · 8,831 cycles

MAINTENANCE FOUND WIRES 2792-1918 AND 2792-7407 BROKEN IN CONDUIT AT RUDDER PEDAL FORCE TRANSDUCER UNIT. CAUSE OF BREAKAGE WAS DETERMINED TO BE WIRE ROUTING. MAINTENANCE REPAIRED WIRES IN ACCORDANCE WITH THE ELECTRICAL STANDARDS PRACTICES MANUAL 20-53-22, 20-53-21, 20-48-11, 20-48-21 AND PERFORMED ELECTRONIC FLIGHT CONTROL MESSAGE GROUND SCAN IN ACCORDANCE WITH AMM 27-96-00-740-001. NO FAULTS RECORDED. MAINTENANCE AND INSPECTION FELT THAT THIS SHOULD BE REPORTED TO ALERT AIRBUS AND/OR THE FAA OF THIS ISSUE OCCURRING ON OTHER AIRCRAFT WITH ASSOCIATED FLIGHT CONTROL MESSAGES.

Part: SKIN — PUNCTURED (LT LE FLAP) · airframe 16,888 hrs · 8,084 cycles

DURING WALK AROUND MAINTENANCE NOTED A BIRD STRIKE ON THE LEFT OUTBOARD LEADING EDGE FLAP APPROXIMATELY SIX FEET FROM OUTBOARD END OF FLAP. ENGINE PARAMETERS WERE REPORTED NORMAL BY THE PILOT. MAINTENANCE REPAIRED THE LEFT OUTBOARD FLAP LEADING EDGE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 57-53-00 FIGURE 202. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: EPSU — INOPERATIVE (EMERGENCY LIGHTS) · airframe 15,630 hrs · 7,490 cycles

DURING REMAIN OVER NIGHT MAINTENANCE, THE EMERGENCY EXIT LIGHT EPSU, FOR THE OVERWING EXITS FOR THE LEFT SIDE OF THE CABIN, FIN NR 11LN, FAILED ITS FUNCTIONAL TEST. MAINTENANCE REMOVED AND REPLACED THE EPSU IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 33-51-38 P 401. FOLLOWING COMPLETION OF THE INSTALLATION AND ITS INSPECTION, THE UNIT OPERATIONALLY CHECKED OKAY.

Part: GIRT BAR — OUT OF POSITION (L1 DOOR SLIDE) · airframe 14,345 hrs · 6,890 cycles

FLIGHT CREW REPORTED L1 DOOR SLIDE WOULD NOT ARM. REMOVED L1 DOOR GIRT BAR AND REPOSITIONED MOORING LINE. REINSTALLED L1 DOOR GIRT BAR. PERFORMED OPS CHECK IAW 25-62-44-000-002. CHECKED GOOD.

Part: BLANKING PLATE — CORRODED (R2 DOOR) · corrosion level 2 · airframe 14,342 hrs · 6,889 cycles

DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON FWD BLANKING PLATE AT R2 DOOR. REPLACED R2 DOOR FWD GIRT BAR FITTING BLANKING PLATE IAW AMM 52-13-31-400-003.

Part: BLANKING PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,342 hrs · 6,889 cycles

DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON AFT BLANKING PLATE AT L2 DOOR. REPLACED L2 DOOR AFT GIRT BAR FITTING BLANKING PLATE IAW AMM 52-13-31-400-003.

Part: LUG — GOUGED (NR 4 SPOILER) · airframe 14,342 hrs · 6,889 cycles

DURING C-3 CHECK INSPECTION REPORTED THE RIGHT WING NR 4 SPOILER ANTI-ROTATION LUG GOUGED. FABRICATED AND INSTALLED REINFORCING PLATE FOR RIGHT NR 4 SPOILER CENTER HINGE FITTING PER EA A9-57R-12142, REV A.

Part: LUG — GOUGED (NR 4 SPOILER) · airframe 14,342 hrs · 6,889 cycles

DURING C-3 CHECK, INSPECTION REPORTED LEFT WING NR 4 SPOILER ANTI-ROTATION LUG GOUGED. FABRICATED AND INSTALLED REINFORCING PLATE FOR LEFT NR 4 SPOILER CENTER HINGE FITTING IAW EA A9-57R-12144.

Part: LUG — GOUGED (NR 3 SPOILER) · airframe 14,342 hrs · 6,889 cycles

DURING C-3 CHECK, INSPECTION REPORTED RIGHT WING NR 3 SPOILER ANTI-ROTATION LUG GOUGED. FABRICATED AND INSTALLED REINFORCING PLATE FOR RIGHT NR 3 SPOILER CENTER HINGE FITTING IAW EA A9-57R-12143, REV A.

Part: BLANKING PLATE — CORRODED (R2 DOOR) · corrosion level 2 · airframe 14,342 hrs · 6,889 cycles

DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON AFT BLANKING PLATE AT R2 DOOR. REPLACED R2 DOOR AFT GIRT BAR FITTING BLANKING PLATE IAW AMM 52-13-31-400-003.

Part: LUG — GOUGED (NR 3 SPOILER) · airframe 14,342 hrs · 6,889 cycles

DURING C-3 CHECK, INSPECTION REPORTED THE ANTI-ROTATION LUG ON THE LEFT NR 3 SPOILER ACTUATOR ATTACH POINT GOUGED. FABRICATED AND INSTALLED REINFORCING PLATE FOR LEFT NR 3 SPOILER CENTER HINGE FITTING IAW EA A9-57R-12137, REV A.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,342 hrs · 6,889 cycles

DURING C-3 CHECK, INSPECTION REPORTED FLOORBEAM INBD OF GIRT BAR FLOOR MOUNTS IN L2 DOOR ENTRY WAY CORRODED ON NUT PLATE HOLES (BOTTOM AND TOP). REPLACED FLOORBEAM AT Y1292 BETWEEN FR66 AND FR 68 IAW SRM 51-42-11 AND EA A0-53T-11472.

Part: FLOORBOARD — CORRODED (CABIN) · corrosion level 2 · airframe 14,342 hrs · 6,889 cycles

DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON SEVERAL AREAS OF FLOORBOARD PANEL 161FF. REPLACED FLOORBOARD PANEL 161FF IAW AMM 53-42-12, PB401.

Part: BUSHING — CORRODED (SEAT MOUNT) · corrosion level 2 · airframe 14,342 hrs · 6,889 cycles

DURING C-3 CHECK, INSPECTION REPORTED AFT LT FLT ATTENDANT SEAT (HOLD DOWN INSERTS) CORRODED IN MOUNTING HOLE AND EXTENDING INTO THE FLOORBEAM. REPLACED AFT LT FLT ATTENDANT SEAT FLOOR MOUNT BUSHINGS IAW AMM 25-22-42-400-001.

Part: FLOORBOARD — CORRODED (CABIN) · corrosion level 2 · airframe 14,342 hrs · 6,889 cycles

DURING C-3 CHECK, INSPECTION REPORTED SEVERAL AREAS OF CORROSION ON FLOORBOARD PANEL 163FF. REPLACED FLOORBOARD PANEL IAW AMM 53-42-12, PB401.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,342 hrs · 6,889 cycles

DURING C-3 CHECK, INSPECTION REPORTED RT OVERWING BATTERY FAILED CAPACITY CHECK. REPLACED 4 EMERGENCY POWER SUPPLY BATTERIES 10WL, 11WL, 12WL AND 13WL IAW AMM 33-51-38-000-002 AND 33-51-38-400-002. PERFORMED OPS CHECK OF EPSU'S 10WL, 11WL, 12WL AND 13WL IAW AMM 33-51-38-400-002, PARA 4 B. OPS CHECK NORMAL. S/N'S FOR REMOVED BATTERIES: 32470, 23972, 33431, 1951.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 4,490 hrs · 2,080 cycles

AIR TURNBACK, FLIGHT CREW REPORTED RT FWD WINDSHIELD SHATTERED IN FLIGHT AT APPROXIMATELY 20,500 FT MSL. REPLACED RT FWD WINDSHIELD AND PERFORMED TEST ON WINDOW HEAT PER AMM 56-11-11 PB401.

Part: WARNING LIGHT — ILLUMINATED (ELEVATOR) · airframe 3,145 hrs · 1,452 cycles

BLOCK TURN BACK. FLIGHT CREW REPORTED ELAC 2 ECAM MESSAGE. PERFORMED EFCS GROUND SCANS EFCS 1 AND 2. OPS CHECK NORMAL. NO FAULTS FOUND IAW MM 27-96-00-740-001 TSM. PERFORMED ELEVATOR AND AILERON TEST OF THE EFCS IAW MM 27-96-00 PB 001. NO FAULTS FOUND. PERFORMED ENGINE RUNS AND COULD NOT FIND ANY FAULTS. AIRCRAFT OPERATION IS NORMAL. NO FAULTS ON PFR'S.

Part: MODULE — MALFUNCTIONED · airframe 3,145 hrs · 1,452 cycles

AIR TURN BACK. FLIGHT CREW REPORTED ELAC2 PITCH FAULT AFTER TAKEOFF. SWAPPED ELAC2 ELECTRONIC MODULE OF THE PITCH FROM ACTUATOR WITH ELAC1/SEC1 ELECTRONIC MODULE IAW MM 27-44-57-000-002 AND MM 27-44-57-400-002. PERFORMED SYSTEM TEST OF THE THS ACTUATOR ELEC. CONTROL FOR BOTH ELAC2 AND ELAC1/SEC1 ELEC. MODULES IAW MM 27-41-00-730-001. OPS CHECK GOOD. ALSO PERFORMED TASK 27-96-00-710-002. OPS CHECK GOOD.

Part: SWITCH — MALFUNCTIONED (ELAC 2) · airframe 3,145 hrs · 1,452 cycles

BLOCK TURNBACK. FLIGHT CREW REPORTED ELAC 2 ECAM MESSAGE. RESET ELAC 2 SWITCHES AND FAULT CLEARED.

Part: TRANSDUCER — INOPERATIVE (FLT CONTROL) · airframe 2,662 hrs · 1,235 cycles

FLIGHT CREW REPORTED FLIGHT CONTROL ELAC 2 FAULT AFTER NR 2 ENGINE START. PERFORMED AFS TEST PER TASK 22-66-00-810-851. NO FAULTS FOUND. SWAPPED ELAC NR 1 AND NR 2. PERFORMED ELECTRONIC FLIGHT CONTROL SYSTEM TEST. LT AND RT ELEVATOR AND LT AND RT AILERON TESTED OKAY. REPLACED ELAC 2 POSITION TRANSDUCER ON THE ACTUATOR (9CE). OPS CHECK OK PER AMM 27-44-56 AND 27-96-00.