N923FR

Part: BATTERY — DISCHARGED (CABIN) · airframe 36,598 hrs · 18,121 cycles

EPSU BATTERY EMER L FAULT ON EPSU TEST. R & R EPSU BATTERY IAW AMM 33-51-38-OOO-002-A & 33-51-38-400-002-A. OPERATIONS CHECKED GOOD.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,639 hrs · 17,608 cycles

AIRCRAFT OUT OF SERVICE DUE TO C7 S2 CHECK. AFT MAIN CABIN LT LATERAL SHEAR PLATE CORROSION. R & R SHEAR PLATE LT IAW AIRBUS SRM 51-42-11, PAR 6, EO A0-53EO-31434.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,639 hrs · 17,608 cycles

AIRCRAFT OUT OF SERVICE DUE TO C7 S2 CHECK. AFT MAIN CABIN RT LATERAL SHEAR CORROSION. R & R SHEAR PLATE RT IAW A319 SRM 41-42-11, PAR 6, EO A0-53EO-31434.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 32,368 hrs · 15,849 cycles

ONE EMERGENCY BATTERY PACK TESTED BAD. R & R BATTERY PACK. OPS CHECKED GOOD IAW AMM 33-S1-38-400-002A.

Part: SWITCH — FAILED (ZONE 200) · airframe 31,857 hrs · 15,582 cycles

02 MASK DROPPED. REPLACED PASSENGER OXYGEN ALTITUDE SWITCH IAW AMM 35-23-15 PB 401.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 30,241 hrs · 14,715 cycles

DURING THE HEAVY SERVICE CHECK, DISCOVERED SEAT ROW 7ABC'S EMERGENCY LIGHT ON SEAT IS INOPERATIVE. EMERGENCY LIGHT ASSY R & R IAW AMM 33-51-19 PB 401 AND UNIT OPERATED NORMAL. ACFT RETURNED TO SERVICE.

Part: SEAL — OUT OF POSITION (CARGO DOOR) · airframe 20,958 hrs · 10,209 cycles

CREW MADE AN AIR TURN BACK TO DEN DUE TO CABIN EXCEEDING 10,000' PRESSURE THROUGH FL230. MAINTENANCE REMOVED AND REPLACED THE AFT CARGO DOOR SEAL AND INSTALLED NEW SEAL IAW AMM 52-32-18 PB 401 AND PERFORMED PRESSURIZATION LEAK CHECK IAW AMM 05-53-00 PB 401.

Part: PROFILE — CORRODED (ZONE 100) · airframe 20,798 hrs · 10,124 cycles

DURING C4 C-CHECK, INSP NOTED THE FWD CARGO COMPARTMENT FLOOR PANEL SUPPORT PROFILE AT FRAME 28 HAS CORROSION AROUND NUTPLATES. MX REMOVED AND REPLACED PROFILE IAW SRM 51-42-11.

Part: PROFILE — CORRODED (ZONE 100) · airframe 20,798 hrs · 10,124 cycles

DURING C4 C-CHECK, INSP NOTED THE AFT CARGO COMPARTMENT PROFILE AT FRAME 58 HAS CORROSION AROUND NUTPLATES. MX REMOVED AND REPLACED THE PROFILE IAW SRM 51-41-11.

Part: PROFILE — CORRODED (ZONE 100) · airframe 20,798 hrs · 10,124 cycles

DURING C4 C-CHECK, INSP NOTED THE AFT CARGO COMPARTMENT PROFILE AT FRAME 58 -UPPER SURFACE- HAS CORROSION AROUND NUTPLATES. MX REMOVED AND REPLACED THE PROFILE IAW SRM 53-42-11.

Part: PROFILE — CORRODED (ZONE 100) · airframe 20,798 hrs · 10,124 cycles

DURING C4 C-CHECK, INSP NOTED CORROSION ON FLOOR PANEL PROFILE LOCATED AT FRAME 61 AND STRINGER 38L. MX REMOVED PROFILE, FABRICATED NEW PROFILE AND INSTALLED IAW SRM 53-41-14 ABD 51-42-11.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 20,798 hrs · 10,124 cycles

DURING DEN C4 C-CHECK, INSP NOTED THE FWD PIT BULKHEAD FLOOR PANEL SUPPORT PLATE HAS CORROSION AROUND NUT PLATES. MX REMOVED AND REPLACED THE WEB ASSY IAW SRM 51-42-11, 51-70-00 AND 51-75-12.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 20,798 hrs · 10,124 cycles

DURING C4 C-CHECK, INSP NOTED THE FWD CARGO COMPARTMENT FLOOR PANEL SUPPORT PLATE THAT RUNS FROM FRAME 28 TO FRAME 34, JUST BELOW PANEL 131DG, HAS CORROSION AROUND NUT PLATES. MX REMOVED AND REPLACED THE FLOOR PANEL SUPPORT PLATE IAW SRM 51-42-11 AND 51-72-11.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 20,798 hrs · 10,124 cycles

DURING C4 C-CHECK, INSP NOTED THE FWD CARGO COMPARTMENT FLOOR PANEL SUPPORT PLATE THAT RUNS FROM FRAME 28 TO FRAME 34, JUST BELOW PANEL 132DG, HAS CORROSION AROUND NUT PLATES. MX REMOVED AND REPLACED THE FLOOR PANEL SUPPORT PLATE IAW SRM 51-44-11 AND 51-42-11.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 20,798 hrs · 10,124 cycles

DURING C4 C-CHECK, INSP NOTED THAT THE EMERGENCY PWR SUPPLY UNIT AT POSITION 10WL FAILED THE BATTERY CAPACITY CHECK. MX REMOVED AND REPLACED THE EMERGENCY PWR SUPPLY BATTERY AND PERFORMED OPS TEST IAW AMM 33-51-38 PB 401.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 20,798 hrs · 10,124 cycles

DURING DEN C4 C-CHECK, INSP NOTED THE FWD CARGO FLOOR PANEL SUPPORT PLATE THAT RUNS FROM FRAME 24A TO FRAME 28 JUST BELOW PANEL 131BF HAS CORROSION AROUND NUT PLATES. MX REMOVED AND REPLACED FLOOR PANEL SUPPORT PLATE IAW A319 SRM 51-42-11 AND 51-44-11.

Part: FLOOR PANEL — CORRODED (ZONE 100) · airframe 20,798 hrs · 10,124 cycles

DURING DEN C4 C-CHECK, INSP NOTED THE FWD CARGO COMPARTMENT FLOOR PANEL FWD OF FRAME 34 AT THE AFT BULKHEAD HAS CORROSION AROUND NUT PLATES. MX REMOVED AND REPLACED THE FLOOR PANEL SUPPORT PLATE IAW A319 SRM 51-42-11 AND 51-44-11.

Part: ENCODER — MALFUNCTIONED (ZONE 200) · airframe 19,593 hrs · 9,493 cycles

PILOT REPORTED THE AFT HALF OF THE ESCAPE LIGHT SYSTEM WAS ON CONTINUOUSLY WITH THE "NO SMOKING" SWITCH POSITION ON "IN" OR "AUTO". MAINTENANCE REMOVED AND REPLACED THE DECODER/ENCODER UNIT AT POSITION 300RH5 AND PERFORMED OPERATIONAL TEST, REFERENCE AMM 23-73-47 PB 401. MAINTENANCE PERFORMED EMERGENCY LIGHT TEST, REFERENCE AMM 33-51-11-710-050.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 19,157 hrs · 9,275 cycles

MULTIPLE EMERGENCY ESCAPE PATH LIGHTS WERE ILLUMINATED WITH THE EMERGENCY EXIT LIGHT SWITCH IN THE ARM POSITION. MAINTENANCE INSPECTED OVERHEAD AFT GALLEY BETWEEN THE L2 AND R2 DOORS AND FOUND INSULATION BLANKETS WET (CONDENSATION) CAUSING EMERGENCY LIGHTS TO COME ON INTERMITTENTLY. MAINTENANCE DRIED AND REPAIRED BLANKETS IAW AMM 25-80-00 PB 801 AND PERFORMED OPERATIONAL CHECK IAW AMM 33-51-00 PB 501. EMERGENCY POWER LIGHTING IN AFT CABIN STAYS ON WHEN THE EMERGENCY EXIT LIGHT SWITCH IS IN THE ARMED POSITION. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT AT 13WL AND PERFORMED OPERATIONAL TEST PER AMM 33-57-38 PB 401.

Part: CONNECTOR — FAULTY (CABIN) · airframe 18,647 hrs · 9,021 cycles

REFERENCE LOG PAGE 422843. MX NOTED THAT THE AFT SECTION EMERGENCY ESCAPE PATH LIGHTING WOULD NOT EXTINGUISH. MX PERFORMED TROUBLESHOOTING, REMOVED AND REPLACED CONNECTOR 7245VC AND PERFORMED OPS CHECK IAW A319 ELECTRICAL STANDARDS PRACTICES MANUAL AND AMM 33-51-00-710-001.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 18,555 hrs · 8,979 cycles

PILOT REPORTED THAT THE EMERGENCY PATH LIGHTING WOULD NOT TURN OFF. MAINTENANCE REMOVED AND REPLACED CONNECTOR 7245VC IAW A319 ELECTRICAL STANDARDS PRACTICES MANUAL 20-44-29. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT AT FIN 13WL IAW A319 AMM 33-51-38-000-001 AND 33-51-38-400-001.

Part: CONNECTOR — FAILED (CABIN) · airframe 18,555 hrs · 8,979 cycles

PILOT REPORTED THAT THE EMERGENCY PATH LIGHTING WOULD NOT TURN OFF. MAINTENANCE REMOVED AND REPLACED CONNECTOR 7245VC IAW A319 ELECTRICAL STANDARDS PRACTICES MANUAL 20-44-29. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT AT FIN 13WL IAW A319 AMM 33-51-38-000-001 AND 33-51-38-400-001.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 18,541 hrs · 8,973 cycles

PILOT REPORTED THAT WITH THE CABIN EMERGENCY EGRESS LIGHT SYSTEM SET TO THE "OFF" POSITION, THE SEAT MOUNTED AISLE PATH LIGHTS AT SEAT ROW 15 AND AFT ON LEFT SIDE OF AIRCRAFT REMAINED ILLUMINATED. MAINTENANCE PERFORMED COMPUTER RESET OF CABIN INTERCOMMUNICATION DATA SYSTEM NR 1 AND 2, REFERENCE TROUBLESHOOTING MANUAL 24-00-00-810-818. FAULT CLEARED. AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 18,418 hrs · 8,911 cycles

PILOT REPORTED THE EMERGENCY LIGHTS WERE ON IN ROWS 14 AND AFT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT AT POSITION 10WL IN ACCORDANCE WITH AMM 33-51-38PB401 AND PERFORMED AN OPERATIONAL TEST.

Part: POWER SUPPLY — FAILED (ZONE 200) · airframe 18,419 hrs · 8,912 cycles

PILOT REPORTED THE EMERGENCY LIGHTS WERE ON IN ROWS 14 AND AFT. MAINTENANCE REMOVED MOISTURE FROM THE AFT LEFT HAND EXIT SIGN CONNECTOR 7245VC AND REPLACED THE EMERGENCY POWER SUPPLY UNIT IN POSITION 13WL IN ACCORDANCE WITH A319 AMM 33-51-38 PB401 AND PERFORMED OPERATIONAL TEST.

Part: SENSOR — FAULTY (R2 DOOR SLIDE) · airframe 17,060 hrs · 8,196 cycles

FLIGHT CREW NOTED THE R2 DOOR INDICATION IS INOPERATIVE. WHILE CLOSED AND ARMED, THE ELECTRONIC CENTRALIZED AC MONITORING INDICATION IS AN AMBER BLOCK AND "SLIDE ARMED" INDICATION IS NOT ILLUMINATED. THIS DEFECT HAS BEEN DEFERRED (1063174) AND IS DUE ON 8/05/08. (A) THE FOLLOWING SUPPLEMENTAL INFORMATION IS BEING ADDED; MAINT REMOVED AND REPLACED THE DOOR HOOK SENSOR (DETECTOR) IAW AMM 52-71-11. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 7/31/08. (A)

Part: SKIN — DAMAGED (L1 DOOR) · airframe 13,563 hrs · 6,552 cycles

FOLLOWING CONTACT OF THE JET BRIDGE WITH THE L-1 DOOR, INSPECTION, DURING THE DAILY CHECK, REPORTED DAMAGE WAS FOUND TO THE LOWER, FORWARD CORNER OF THE DOOR SKIN. MAINTENANCE REPAIRED THE FORWARD LOWER CORNER OF THE L-1 DOOR IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-52R-30107 AND SRM 51-42-11. FOLLOWING COMPLETION OF THE REPAIR, THE DOOR WAS INSPECTED AND FOUND ACCEPTABLE.

Part: SKIN — DAMAGED (L1 DOOR) · airframe 13,563 hrs · 6,552 cycles

FOLLOWING CONTACT OF THE JET BRIDGE WITH THE L-1 DOOR, INSPECTION, DURING THE DAILY CHECK, REPORTED DAMAGE WAS FOUND TO THE LOWER, FORWARD CORNER OF THE DOOR SKIN. MAINTENANCE REPAIRED THE FORWARD LOWER CORNER OF THE L-1 DOOR IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-52R-30107 AND SRM 51-42-11. FOLLOWING COMPLETION OF THE REPAIR, THE DOOR WAS INSPECTED AND FOUND ACCEPTABLE.

Part: LINE — DAMAGED (BRAKE SYSTEM) · airframe 155,611 hrs · 7,493 cycles

DURING THE APPROACH, THE FLIGHT CREW REPORTED SEVERAL BIRD STRIKES (CANADIAN GEESE). ON LANDING, THE FLIGHT CREW REPORTED THE LOSS OF NORMAL BRAKING DURING THE ROLL OUT. MAINTENANCE INSPECTED THE LANDING GEAR AND FOUND BRAKE LINE 27 ON THE RIGHT MAIN LANDING GEAR TO BE DAMAGED. MAINTENANCE REPLACED BRAKE LINE 27 IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 32-11-12-400-001, STEPS 4B (2) (R) AND (W). FOLLOWING INSTALLATION OF THE BRAKE LINE, THE BRAKE AND STEERING SYSTEM WAS BITE TESTED IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 32-46-00-740-001 AND TESTED OKAY. THE AIRCRAFT WAS RETURNED TO SERVICE FOLLOWING OTHER MINOR REPAIRS.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 15,440 hrs · 7,415 cycles

DURING THE C3/S1 C CHECK, INSPECTION REPORTED THE AFT CARGO PIT FLOOR PANEL 161CF HAD TWO AREAS OF OUT OF LIMITS DAMAGE ON ITS TOP FACE. MAINTENANCE REPAIRED THE AFFECTED AREAS IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00, PRIMED AND PAINTED THE PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 25-00-00 801. UPON COMPLETION OF THE REPAIR AND PAINTING, THE PANEL WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — DAMAGED · airframe 15,440 hrs · 7,415 cycles

DURING C3/S1 C CHECK, INSPECTION REPORTED THE AFT CARGO PIT FLOOR PANEL 151BE HAD A PUNCTURE ON ITS UPPER SURFACE. MAINTENANCE REPAIRED THE DAMAGE IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00. FOLLOWING COMPLETION OF THE REPAIR, THE FLOOR PANEL WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — DAMAGED · airframe 15,440 hrs · 7,415 cycles

DURING C3/S1 C CHECK, INSPECTION REPORTED THE AFT CARGO PIT FLOOR PANEL 161BF HAD DENTS AND GOUGES OUT OF LIMITS. MAINTENANCE REPAIRED THE DENTS AND GOUGES IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00, TREATED, PRIMED AND PAINTED THE PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-21-11. UPON COMPLETION OF THE REPAIRS, THE PANEL WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,440 hrs · 7,415 cycles

REFERENCE NON ROUTINE 26658, DURING C3/S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE MAIN DECK FLOORBEAM AT LBL 47 AND FRAME 68. MAINTENANCE REMOVED AND REPLACED THE CORRODED FLOORBEAM IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11. UPON COMPLETION OF THE INSTALLATION, THE NEW FLOORBEAM WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 15,440 hrs · 7,415 cycles

DURING C3/S1 C CHECK, INSPECTION REPORTED THE FORWARD CARGO PIT FLOOR PANEL 132DG WAS DELAMINATED AND HAD OUT OF LIMIT DENTS. MAINTENANCE REPAIRED THE DELAMINATED AREA AND FILLED THE DENTS IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00, PRIMED AND PAINTED THE PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-21-11. UPON COMPLETION OF THE REPAIR, THE PANEL WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 15,440 hrs · 7,415 cycles

DURING C3/S1 C CHECK, INSPECTION REPORTED AFT CARGO PIT FLOOR PANEL 161FF HAD DENTS OUT OF LIMITS. MAINTENANCE REPAIRED THE DAMAGE IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-01-00, TREATED, PRIMED AND PAINTED THE PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-21-11. UPON COMPLETION OF THE REPAIRS, THE PANEL WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,440 hrs · 7,415 cycles

REFERENCE NON ROUTINE 26654, DURING C3/S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE MAIN DECK FLOORBEAM AT LBL 51 AND FRAME 66. MAINTENANCE REMOVED AND REPLACED THE CORRODED FLOORBEAM IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11. UPON COMPLETION OF THE INSTALLATION, THE NEW FLOORBEAM WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — DAMAGED (CARGO BAY]) · airframe 15,440 hrs · 7,415 cycles

DURING C3/S1 C CHECK, INSPECTION REPORTED UNACCEPTABLE DENTS AND GOUGES IN THE AFT CARGO COMPARTMENT FLOOR PANEL 162BF. MAINTENANCE REPAIRED THE FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00 AND PRIMED AND REPAINTED THE PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-21-11. UPON COMPLETION OF THE REPAIRS, THE FLOOR PANEL WAS INSPECTED AND FOUND ACCEPTABLE.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,440 hrs · 7,415 cycles

REFERENCE NON ROUTINE 26838, DURING C3/S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE FRAME PLATE AT FRAME 28, ON THE RIGHT SIDE, NEAR THE CARGO DOOR OPENING. MAINTENANCE REMOVED AND REPLACED THE CORRODED FRAME PLATE IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11. UPON COMPLETION OF THE INSTALLATION, THE NEW FRAME PLATE WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,440 hrs · 7,415 cycles

REFERENCE NON ROUTINE 26657, DURING C3/S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE MAIN DECK FLOORBEAM AT LBL 48 BETWEEN FRAMES 67 AND 68. MAINTENANCE REMOVED AND REPLACED THE CORRODED FLOORBEAM IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11. UPON COMPLETION OF THE INSTALLATION, THE NEW FLOORBEAM WAS INSPECTED AND FOUND ACCEPTABLE.

Part: ARM — DAMAGED (TE FLAP) · airframe 15,440 hrs · 7,415 cycles

DURING C3/S1 C CHECK, INSPECTION REPORTED THE LEFT WING, NUMBER 2 FLAP DRIVE LEVER EXTENSION ARM (STRUT) FITTING, ON THE FLAP, IS CHAFING INTO THE FITTING AT THE ATTACH POINT (BOTTOM AND TOP) ON THE FLAP. MAINTENANCE BLENDED AND CHAMFERED THE EDGE OF THE FITTING, TREATED, PRIMED AND PAINTED THE FITTING IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-57R-30041. UPON COMPLETION OF THE REPAIR, THE FITTING WAS INSPECTED AND FOUND ACCEPTABLE.

Part: ATTACH FITTING — DAMAGED · airframe 15,440 hrs · 7,415 cycles

DURING C3/S1 C CHECK, INSPECTION REPORTED THE RIGHT, OUTBOARD NUMBER 3 FLAP DRIVE LEVER EXTENSION ARM FITTING WAS FOUND GOUGED WHERE IT CONNECTS TO BOTTOM OF THE DRIVE ARM. MAINTENANCE BLENDED THE DAMAGED AREA IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-73-00. PERFORMED HFEC (EDDY CURRENT) INSPECTION AND FOUND NO DEFECTS. AREA WAS PRIMED AND PAINTED IN ACCORDANCE WITH EA A9-53R-30009. UPON COMPLETION OF THE REPAIRS, THE UNIT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: HINGE FITTING — DAMAGED · airframe 15,440 hrs · 7,415 cycles

DURING THE C3/S1 C CHECK, INSPECTION REPORTED THE RIGHT, FORWARD, MAIN LANDING GEAR DOOR, KEEL MOUNTED HINGE FITTING, AT THE AFT LUG, HAD A NICK IN ITS BOTTOM EDGE. MAINTENANCE BLENDED THE DAMAGE IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-73-00. PERFORMED HFEC (EDDY CURRENT) TESTING AND FOUND NO DEFECTS. THE PART WAS TREATED, PRIMED AND PAINTED IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-53R-30004. UPON COMPLETION OF THE REPAIR, THE PART WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — DAMAGED · airframe 15,440 hrs · 7,415 cycles

DURING THE C3/S1 C CHECK, INSPECTION REPORTED THE FORWARD CARGO PIT FLOOR PANEL 131QC HAD A PUNCTURE HOLE IN ITS UPPER SURFACE. MAINTENANCE REPAIRED THE PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00, PAGES 14 AND 15, STEPS A THROUGH M. UPON COMPLETION OF THE REPAIR, THE PANEL WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 15,440 hrs · 7,415 cycles

DURING C3/S1 C CHECK, INSPECTION REPORTED A PUNCTURE WAS FOUND IN THE FORWARD CARGO COMPARTMENT FLOOR PANEL, 131VG. MAINTENANCE REPAIRED THE FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00, PAGES 14 AND 15, STEPS A-M. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 11,778 hrs · 5,639 cycles

AIR TURN BACK, CAPTAIN'S WINDSHIELD CRACKED. REPLACED NR 1 WINDSHIELD IAW AMM 56-11-11.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 11,778 hrs · 5,638 cycles

FIRST OFFICERS WINDSHIELD CRACKED ALL THE WAY ACROSS. REPLACED NR 2 WINDSHIELD IAW MM 56-11-11 PB401.

Part: FAN BLADE — BENT (NR 1 ENGINE) · airframe 770 hrs · 352 cycles

ON WALKAROUND, FLIGHT CREW REPORTED NR 1 ENGINE BLADES BENT. REPLACED DAMAGED FAN BLADES AT POSITIONS 2, 3, 4, 6, 7, 8, 9, 10, 11, 12, 15, 16, 19, 20, 21, 22, 23, 24, 25, 26, 27, 28, 29, 30, 31, 34, AND 35. POSITIONS 14, 18, 32 AND 36 WERE NOT MOVED. POSITIONS 1, 5, 13 AND 17 WERE REMOVED SERVICEABLE. POSITIONS 10, 12, 19, 22, 27, 30, 31, 33 AND 35 WERE REMOVED UNSERVICEABLE. COMPLIED WITH WORK CARD MP72400-1 AND NO DEFECTS WERE NOTED PER AMM 72-21-00-300-028. IT IS SUSPECTED DAMAGE WAS RESULT OF ICE INGESTION.