N920FR

Part: DUCT — FAILED (BLEED AIR SYS) · airframe 41,441 hrs · 20,417 cycles

DISCREPANCY, ENG 2 FIRE, AIR TURN BACK 1839 Z. ENG 2 FIRE INDICATION ON TAKEOFF AFTER THRUST REDUCTION ON ENG 2 IAW ECAM. FIRE INDICATION CHANGED TO AMBER, ENG 2 SHUTDOWN. ENG 2 SHUTDOWN COMPLETED. FOUND HIGH PRESS BLEED DUCT BROKEN CAUSING ENG 2 FIRE INDICATION. R & R DUCT IAW AMM 36-11-49-000-046-A & AMM 36-11-49-400-046-A. RAN ENG WITHIN 24 HOURS IAW AMM 65-51-34-200-001A. REF LOG PAGE 901197, 901198, 901199 & 901200 FOR ALL ADDITIONAL DAMAGE & REPAIR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,513 hrs · 19,457 cycles

SEAT 2ABC EMER EXIT PATH LIGHT BULB INOPERATIVE & LENS IS BROKEN. R & R BULB & LENS. OPERATIONAL CHECKED OK IAW AMM 33-51-19 PB401.

Part: CONTROL UNIT — UNBONDED (RT ELEVATOR) · airframe 39,035 hrs · 19,186 cycles

RIGHT ELEVATOR THERMOGRAPHY INDICATIONS OF IRREGULAR SHAPE & BLACK IN COLOR. REPAIRED RT ELEVATOR IAW SRM 55-21-11 PB 201. WORK ACCOMPLISHED ON NR 41243 WORK ORDER 1150.

Part: CONTROL UNIT — UNBONDED (LT ELEVATOR) · airframe 39,035 hrs · 19,186 cycles

LEFT ELEVATOR THERMOGRAPHY INDICATIONS OF IRREGULAR SHAPE & BLACK IN COLOR. REPAIRED LT ELEVATOR IAW SRM 55-21-11 PB 201. WORK ACCOMPLISHED ON NR 41242 WORK ORDER 1150.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,035 hrs · 19,186 cycles

LEFT AFT PAX DOOR L2 CUT OUT UNDERNEATH THE SCUFF PLATE HAS EXFOLIATION CORROSION AT 2 LOCATIONS. REMOVED SILL PLATE FROM L2 DOOR LOWER CUT OUT IAW SRM 51-42-11 PAR 6. LOCATED & DRILLED NEW SILL PLATE PN D5348004800003 PO P6020837 IAW SRM 51-44-11. INSTALLED SILL PLATE IAW SRM 51-42-11 PAR 6.

Part: BATTERY PACK — FAILED (CABIN) · airframe 36,748 hrs · 17,970 cycles

AIRCRAFT OUT OF SERVICE FOR HEAVY SERVICE CHECK. EMERGENCY LIGHT BATTERY 11WL FAILED HEAVY SERVICE CHECK TEST. R & R BATTERY ASSEMBLY & OPERATIONS CHECKED GOOD IAW AMM 33-51-39-000-05A & AMM 33-51-39-400-05A.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,931 hrs · 6,978 cycles

EPSU, NO COMM FWD LT ON PUCH TO TEST PANEL. REPLACED EPSU 10WL FWD LT IAW AMM 33-51-38 PB401. OPS TEST NORMAL IAW AMM 33-51-00-710-001 AND AMM 23-73-00-740-005.

Part: EPSU — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,931 hrs · 6,978 cycles

SEAT ROW LIGHTS FROM ROW 14 TO 25 WOULD NOT ILLUMINATE WHEN TESTED. TROUBLESHOT EPSU, NO COMM. REPLACED EPSU 13WL IAW AMM 33-51-38, PB401. OPS TEST NORMAL AFT IAW AMM 33-51-00-710-001 AND AMM 23-73-00-740-005.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 31,237 hrs · 15,059 cycles

EPSU BATTERY FAILED TEST DURING HEAVY SERVICE CHECK. 10WL FWD LT. R & R BATTERY FOR EPSU 10WL, OPS CHECKED OK IAW AMM 33-51-38-000-002A & AMM 33-51-38-400-0002A.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 31,237 hrs · 15,059 cycles

EPSU BATTERY FAILED TEST DURING HEAVY SERVICE CHECK, 13WL AFT LT. R & R BATTERY ASSY FOR EPSU 13WL, OPS CHECKED OK IAW AMM 33-51-38-000-002A & AMM 33-51-38-400-002A.

Part: BATTERY — FAILED (ZONE 200) · airframe 29,778 hrs · 14,319 cycles

RT EMERGENCY EXIT LIGHTING POWER SUPPLY 12 WL BATTERY FAILED TEST. R & R BATTERY, OPS CHECKED OK IAW AMM 33-51-38-000-001 AND 33-51-38-400-001.

Part: SAFETY VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 21,883 hrs · 10,477 cycles

DEN - PILOT REPORTED CABIN PRESSURE SAFETY VALVE OPEN ABOVE 37,000 FEET IN CRUISE. MANUAL PRESSURE MODE OPERATED NORMALLY PER (ECAM) ELECTRONIC CENTRALIZED AIRCRAFT MONITORING. EXCESSIVE CABIN DELTA P CAUSED ECAM. DESCENDED TO 36,000 FT AND ENGAGED AUTO PRESSURE MODE. BOTH AUTO PRESSURE SYSTEMS FAILED TO MAINTAIN NORMAL DELTA P AND CABIN ALTITUDE. MAINTENANCE REMOVED AND REPLACED THE NR 1 SAFETY VALVE AND PERFORMED OPERATIONAL CHECK, REFERENCE AMM 21-31-52 PB 401 AND AMM 21-31-00-710-006. MAINTENANCE ALSO PERFORMED OPERATIONAL TEST OF THE PRESSURE CONTROL AND MONITORING, REFERENCE AMM 21-31-00-710-002.

Part: SAFETY VALVE — MALFUNCTIONED (ZONE 200) · airframe 21,883 hrs · 10,477 cycles

DEN - PILOT REPORTED CABIN PRESSURE SAFETY VALVE OPEN ABOVE 37,000 FEET IN CRUISE. MANUAL PRESSURE MODE OPERATED NORMALLY PER (ECAM) ELECTRONIC CENTRALIZED AIRCRAFT MONITORING. EXCESSIVE CABIN DELTA P CAUSED ECAM. DESCENDED TO 36,000 FT AND ENGAGED AUTO PRESSURE MODE. BOTH AUTO PRESSURE SYSTEMS FAILED TO MAINTAIN NORMAL DELTA P AND CABIN ALTITUDE. MAINTENANCE REMOVED AND REPLACED THE NR 2 SAFETY VALVE AND PERFORMED OPERATIONAL CHECK, REFERENCE AMM 21-31-52 PB 401 AND AMM 21-31-00-710-006. MAINTENANCE ALSO PERFORMED OPERATIONAL TEST OF THE PRESSURE CONTROL AND MONITORING, REFERENCE AMM 21-31-00-710-002.

Part: LIGHT — BROKEN (CABIN) · airframe 20,842 hrs · 9,948 cycles

LINE MAINTENANCE NOTED THAT DURING INTERIOR CHECK, THE SEAT MOUNTED EMERGENCY LIGHTS ON ROWS 7, 13 AND 17 WERE FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE SEAT MOUNTED EMERGENCY LIGHTS AND PERFORMED OPERATIONAL CHECK, REFERENCE AMM 33-51-19 PB 401.

Part: BEARING — CORRODED (MLG) · corrosion level 2 · airframe 19,591 hrs · 9,320 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION ON LEFT MAIN LANDING GEAR LOWER BEARING. MAINTENANCE REMOVED AND REPLACED LOWER BEARING ASSEMBLY IN ACCORDANCE WITH ENGINEERING AUTHORIZATION A9-32R-30744 AND A9-32R-30742.

Part: PROFILE — CORRODED (ZONE 100) · corrosion level 2 · airframe 19,591 hrs · 9,320 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION IN THE FORWARD CARGO COMPARTMENT ON PROFILE LOCATED AT STRINGER 38 RIGHT, BETWEEN FRAME 28 AND FRAME 31. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH A319 SRM 51-72-11 AND 51-42-11.

Part: PROFILE — CRACKED (ZONE 100) · airframe 19,591 hrs · 9,320 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED CRACKED PROFILE AT FRAME 55A, UPPER SIDE OF AFT CARGO COMPARTMENT. MAINTENANCE REMOVED AND REPLACED CRACKED PROFILE FROM FRAME 55A TO FRAME 52 IN ACCORDANCE WITH A319 SRM 51-72-11 PAGES 1 AND 2.

Part: PROFILE — CORRODED (ZONE 100) · corrosion level 2 · airframe 19,591 hrs · 9,320 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION IN THE FORWARD CARGO COMPARTMENT ON PROFILE LOCATED AT STRINGER 38 LEFT, BETWEEN FRAME 28 AND FRAME 31. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH A319 SRM 51-72-11 PAGE 1 AND 2.

Part: PROFILE — CORRODED (ZONE 100) · corrosion level 2 · airframe 19,591 hrs · 9,320 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION IN THE AFT CARGO COMPARTMENT ON PROFILE LOCATED AT BUTT LINE 0, BETWEEN FRAME 56 AND FRAME 57. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH A319 SRM 51-72-11 PAGE 1 AND 2.

Part: PROFILE — CORRODED (ZONE 100) · corrosion level 2 · airframe 19,591 hrs · 9,320 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION IN THE AFT CARGO COMPARTMENT ON PROFILE LOCATED AT FRAME 58 BETWEEN STRINGER 38 LEFT AND 38 RIGHT. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH A319 SRM 51-72-11 PAGE 1 AND 2.

Part: PROFILE — CORRODED (ZONE 100) · corrosion level 2 · airframe 19,591 hrs · 9,320 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION IN THE FORWARD CARGO COMPARTMENT ON PROFILE LOCATED AT STRINGER 38 LEFT BETWEEN FRAME 24A AND FRAME 28. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH A319 SRM 51-72-11 PAGE 1 AND 2.

Part: PROFILE — CORRODED (ZONE 100) · corrosion level 2 · airframe 19,591 hrs · 9,320 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION IN THE AFT CARGO COMPARTMENT ON PROFILE LOCATED AT FRAME 59 BETWEEN STRINGER 38 LEFT AND 38 RIGHT. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH A319 SRM 51-72-11 PAGE 1 AND 2.

Part: PROFILE — CORRODED (ZONE 100) · corrosion level 2 · airframe 19,591 hrs · 9,320 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION IN THE FORWARD CARGO COMPARTMENT ON PROFILE AT FRAME 28 BETWEEN STRINGER 38 LEFT AND 38 RIGHT. MAINTENANCE REPLACED PROFILE IN ACCORDANCE WITH A319 SRM 51-72-11 PAGE 1 AND 2.

Part: PROFILE — CORRODED (ZONE 100) · corrosion level 2 · airframe 19,591 hrs · 9,320 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION IN THE AFT CARGO COMPARTMENT ON PROFILE LOCATED AT STRINGER 38 (RIGHT) BETWEEN FRAME 52 AND FRAME 55A. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH A319 SRM 51-72-11 PAGE 1 AND 2.

Part: PROFILE — CORRODED (ZONE 100) · corrosion level 2 · airframe 19,591 hrs · 9,320 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION IN THE AFT CARGO COMPARTMENT LOCATED AT FRAME 53 BETWEEN STRINGER 38 LEFT AND 38 RIGHT. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH A319 SRM 51-72-11 PAGE 1 AND 2.

Part: PROFILE — CORRODED (ZONE 100) · corrosion level 2 · airframe 19,591 hrs · 9,320 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION AND CRACKS IN THE AFT CARGO COMPARTMENT ON PROFILE LOCATED AT STRINGER 38 LEFT BETWEEN FRAME 52 AND FRAME 56. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH A319 SRM 51-72-11 PAGE 1 AND 2.

Part: PROFILE — CORRODED (ZONE 100) · corrosion level 2 · airframe 19,591 hrs · 9,320 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION IN THE AFT CARGO COMPARTMENT LOCATED ON PROFILE AT FRAME 61 BETWEEN STRINGER 38 LEFT AND 38 RIGHT. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH A319 SRM 51-72-11 PAGE 1 AND 2.

Part: PROFILE — CORRODED (ZONE 100) · corrosion level 2 · airframe 19,591 hrs · 9,320 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION IN AFT CARGO COMPARTMENT ON PROFILE LOCATED AT STRINGER 38 LEFT BETWEEN FRAME 56 AND FRAME 58. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH A319 SRM 51-72-11 PAGE 1 AND 2.

Part: PROFILE — CORRODED (ZONE 100) · corrosion level 2 · airframe 19,591 hrs · 9,320 cycles

DURING C4/S1 C-CHECK , INSPECTION NOTED CORROSION IN THE AFT CARGO COMPARTMENT ON PROFILE LOCATED AT FRAME 56 BETWEEN STRINGER 38 LEFT AND 41 RIGHT. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH A319 SRM 51-72-11 PAGE 1 AND 2.

Part: PROFILE — CORRODED (ZONE 100) · corrosion level 2 · airframe 19,591 hrs · 9,320 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION IN THE FORWARD CARGO COMPARTMENT ON PROFILE LOCATED AT FRAME 31 BETWEEN STRINGER 38 LEFT AND 38 RIGHT. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH A319 SRM 51-72-11 PAGE 1 AND 2.

Part: PROFILE — CORRODED (ZONE 100) · corrosion level 2 · airframe 19,591 hrs · 9,320 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION IN THE AFT CARGO COMPARTMENT ON PROFILE LOCATED AT STRINGER 38 LEFT BETWEEN FRAME 59 AND FRAME 63. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH A319 SRM 51-72-11 PAGE 1 AND 2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,591 hrs · 9,320 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION ON FLOORBEAM LOCATED AT Y1292 AND FRAME 68, PASSENGER CABIN. MAINTENANCE REMOVED AND REPLACED FLOORBEAM IN ACCORDANCE WITH A319 SRM 51-42-11 PAGES 1 AND 2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,591 hrs · 9,320 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION ON FLOORBEAM -Y1292 AT FRAME 68, PASSENGER CABIN. MAINTENANCE REMOVED AND REPLACED FLOORBEAM IN ACCORDANCE WITH A319 SRM 51-42-11 PAGE 1 AND 2.

Part: SKIN — DENTED (TE FLAP) · airframe 19,591 hrs · 9,320 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED DENT ON OUTBOARD FLAP TRAILING EDGE LOWER SURFACE BETWEEN RIB 16 AND RIB 17 ON THE RIGHT WING. MAINTENANCE PERFORMED REPAIR IN ACCORDANCE WITH A319 SRM 57-53-00, PARAGRAPH 8N.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,383 hrs · 6,771 cycles

DURING C-3 CHECK, INSPECTION REPORTED FLOOR PANEL 262FF CORRODED ON LOWER SIDE. REPLACED FLOOR PANEL IAW AMM 53-12-12-000-001.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,383 hrs · 6,771 cycles

DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM Y1292 BETWEEN BS FR66 AND FR68 AROUND ATTACH HOLES/NUT CLIPS, TOP AND BOTTOM. REPLACED FLOORBEAM IAW SRM 51-42-11.

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 14,383 hrs · 6,771 cycles

DURING C-3 CHECK, INSPECTION REPORTED FLOOR PANEL 261FF CORRODED ON LOWER SIDE. REPLACED FLOOR PANEL IAW AMM 53-12-12-000-001.

Part: PLATE — CORRODED · corrosion level 2 · airframe 14,383 hrs · 6,771 cycles

DURING C-3 CHECK, INSPECTION REPORTED BLANKING PLATE FOR GIRT BAR FITTING ON FWD SIDE OF L-2 DOOR CORRODED. REPLACED GIRT BAR BLANKING PLATE IAW AMM 52-12-400-003.

Part: SELECTOR VALVE — UNKNOWN (BRAKES) · airframe 13,538 hrs · 6,385 cycles

DURING DESCENT, FLIGHT CREW REPORTED BRAKES AUTO BRAKE FAULT. REPLACED BRAKE SELECTOR VALVE 23GG AS PRECAUTIONARY MEASURE DUE TO NO FAULTS PRESENT, REF AMM 32-42-11, PB401.

Part: WARNING LIGHT — ILLUMINATED (BRAKES) · airframe 3,134 hrs · 1,434 cycles

ABORTED TAKEOFF. FLIGHT CREW REPORTED BRAKE CONFIGURATION WARNING (TEMP). ABORTED TAKEOFF AT 65 KTS. NO FAULTS OR FAILURES ON POST FLIGHT REPORT. PERFORMED OPERATIONAL CHECK OF NORMAL BRAKE SYSTEM PER AMM 32-42-00-710-001. PERFORMED OPERATIONAL CHECK OF ALT BRAKE SYSTEM PER AMM 32-43-00-710-001. PERFORMED BRAKE INSPECTION OF FUSE PLUGS AND WHEELS. BRAKE TEMPERATURE MAX WAS LESS THAN 660 DEG CELSIUS AND WITHIN 150 DEG CELSIUS OF EACH OTHER. PERFORMED AFS TEST PER AMM 22-96-00-710-001. FMGC 1 AND 2 PASS; FAC 1 AND 2 PASS. PERFORMED REALIGNMENT. NO DAMAGE NOTED. NO FAULTS FOUND.

Part: SMOKE — DETECTED (COCKPIT) · airframe 2,206 hrs · 1,029 cycles

AIR TURN BACK. FLIGHT CREW REPORTED SMOKE IN CABIN SHORTLY AFTER TAKEOFF, JUST AFTER APU BLEED WAS TURNED OFF. AIRCRAFT LANDED WITHOUT INCIDENT. COMPLIED WITH MM 71-00-00-810-802. PERFORMED OPS CHECK AND COULD NOT DUPLICATE DISCREPANCY ON GROUND. PERFORMED TEST FLIGHT. PERFORMED NORMAL BLEED-OFF TAKEOFF AND REINSTATED BLEED CONFIGURATION IAW NORMAL TAKEOFF/CLIMB PROCEDURES. MONITORED CABIN AND COCKPIT FOR SMOKE, MIST INDICATIONS. CHECKED NORMAL, NO DISCREPANCIES FOUND.

Part: SMOKE — DETECTED (COCKPIT) · airframe 2,202 hrs · 1,026 cycles

AFTER LANDING, FLIGHT CREW REPORTED SMOKE FILLED COCKPIT AND CABIN. ECAM STATED AFT CARGO FIRE. FOLLOWED ECAM PROCEDURES AND FIRED AGENT BOTTLE. SMOKE STARTED TO DISSIPATE AFTER FIRING AGENT BOTTLE. REPLACED FIRE BOTTLE DUE TO DISCHARGE IAW AMM 26-23-41-400-005. REMOVED 4 SMOKE DETECTOR UNITS IN AFT CARGO COMPARTMENT IAW AMM 26-16-15-000-001. INSTALLED 4 SMOKE DETECTOR UNITS IN AFT CARGO COMPARTMENT IAW AMM 26-16-15-400-001. PERFORMED OPERATIONAL CHECK ON AFT CARGO SMOKE DETECTION SYSTEM IAW AMM 26-16-00-710-001 AND CHECKED OK.