N505NK

Part: MEGAPHONE — INOPERATIVE (ZONE 900) · airframe 60,127 hrs · 27,827 cycles

AFT FA EMERG MEGAPHONE INOP-R/R AFT FA EMERG MEGAPHONE IAW AMM 25-65-00

Part: NONE — NONE · airframe 57,066 hrs · 26,336 cycles

REF TC 256551-01-1,FOUND SCREWS STRIPPED ON MEGAPHONE IN FWD GALLEY.-R/R MEGAPHONE IAW DRAWING # A320-EMER EQUIP.MEGAPHONE OK FOR SVC.

Part: MEGAPHONE — INOPERATIVE (AFT CABIN) · airframe 54,440 hrs · 25,241 cycles

AFT MEGAPHONE INOP-R/R MEGAPHONE IAW AMM 25-65-00 OPC GOOD AT THIS TIME A/C OK FOR SERVICES.

Part: SKIN — CORRODED (LT WING) · airframe 54,296 hrs · 25,180 cycles

CORROSION ON LH WING UPPER WING SKIN PNL RIB 11 STR.11 REF HAECO S/O 122094 NRI 20131. RAF-01 OPENED-REPAIRED PREWORKED AREA IAW A319 SRM 51-44-11, R57258616. THIS REPAIR IA CAT B REQ. REINSP PER RDAF AT 30,000 FC, 41,900 FH INTERVALS OF 25,000FC 34,900FH AT UPPER SKIN SURFACE AT 65,800FC, 98,500FH INTERVALS TBD AT BUTTSTRAP ATTACH LOCATION RIBS 11-12 PE

Part: SKIN — CORRODED (LT WING) · airframe 54,296 hrs · 25,180 cycles

CORROSION ON LH WING UPPER WING SKIN PNL RIB 11 STR.11 REF HAECO S/O 122094 NRI 20131. RAF-01 OPENED-REPAIRED PREWORKED AREA IAW A319 SRM 51-44-11, R57258616. THIS REPAIR IA CAT B REQ. REINSP PER RDAF AT 30,000 FC, 41,900 FH INTERVALS OF 25,000FC 34,900FH AT UPPER SKIN SURFACE AT 65,800FC, 98,500FH INTERVALS TBD AT BUTTSTRAP ATTACH LOCATION RIBS 11-12 PE

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 54,289 hrs · 25,178 cycles

EPSU 13WL LEFT FAULTED DURING EMERGENCY LIGHT TEST.-REMOVED & REPLACED EPSU 13WL BATTERY IAW A319 AMM 33-51-38. OPS CHECKS GOOD IAW A319 AMM 33-51-00-710-001.

Part: A/C PACK — ODOR (AC BAY) · airframe 51,608 hrs · 23,940 cycles

FUME EVENT ON LANDING PACK 1 SUSPECTED-PERFORMED TSM 05-50-00-810-831-A. FOUND THE MOST PROBABLE CAUSE TO BE ENG 1. PERFORMED TSM 71-00-00-810-801-A. MINOR ODOR NOTED FROM ENG 1 PACK 1. NO SMELL NOTED ON ANY OTHER SOURCE. SEE LOGPAGE 2524013-1 FOR CORRECTIVE ACTION.

Part: KNOB — MISSING (MEGAPHONE) · airframe 51,473 hrs · 23,879 cycles

DURING WEEKLY CHECK FOUND MEGAPHONE VOLUME KNOB MISSING. R&R MEGAPHONE IAW EMERGENCY EQUIPMENT LAYOUT.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 50,560 hrs · 23,447 cycles

AFTER TAKEOFF, DOOR L1 PRESSURIZATION LIGHT WAS FLASHING INDICATING DOOR WAS NOT PRESSURIZING. FAP ALSO SHOWED L1 DOOR WAS NOT ARMED, DESPITE LEVER BEING IN ARMED POSITION. ( CABIN PRESSURE LIGHT (ON DOORS) )-REFER. LOG PAGE 2486499-1 FOR CORRECTIVE ACTION . THIS CLEARS DMI # 2486496-1. MOC NOTIFIED LOG UPDATED AND PLACARD REMOVED

Part: PROXIMITY SWITCH — OUT OF ADJUST (CARGO DOOR) · airframe 49,972 hrs · 23,222 cycles

"AFT CARGO DOOR INDICATES OPEN WHEN CLOSED. DURING TAKEOFF ROLL ( ECAM DOOR PAGE INDICATIONS CARGO DOOR )-ACCOMPLISHED ADJUSTMENT OF AFT CARGO DOOR PROXIMITY SWITCH PER AMM 52-71-00. OP CHECK NORMAL. THIS CLOSES DMI # 235552401, MOC NOTIFIED PLACARD REMOVED."

Part: FLASHLIGHT — ABNORMAL (COCKPIT) · airframe 48,627 hrs · 22,665 cycles

FO SIDE FOOTREST FLASHLIGHT MISSING. INSTALLED NEW FLASHLIGHT AT F/O SIDE IAW EMERGENCY EQUIPMENT LAYOUT DRAWING A319-132 EEQ.

Part: UNKNOWN — SMOKE (CABIN) · airframe 47,709 hrs · 22,257 cycles

WHILE CLIMBING THROUGH FL320, A LOUD NOISE AND VIBRATION COULD BE HEARD AND FELT IN THE COCKPIT. THE CABIN BEGAN TO FILL WITH FOG, SMOKE AND ODOR. SMOKE ODOR WAS STRONGER IN THE AFT CABIN.

Part: UNKNOWN — ODOR (CABIN) · airframe 55,853 hrs · 22,016 cycles

FLT ATTENDANT REPORTED A MUSTY ODOR STARTING AT TAKEOFF TO TOP OF CLIMB. REPORTED AT APPROXIMATELY FL200. TURN OFF THE NR 2 PACK WHICH SEEMED TO HELP TO DISSIPATE THE ODOR.

Part: KNOB — MISSING (MEGAPHONE) · airframe 46,798 hrs · 21,872 cycles

FORWARD F/A MEGAPHONE VOLUME KNOB MISSING. REPLACED THE MEGAPHONE IAW DRAWING N319-131EQ.

Part: UNKNOWN — ODOR (CABIN & COCKPIT) · airframe 46,695 hrs · 21,830 cycles

FUME EVENT ON FINAL APPROACH. STRONG ODOR IN BOTH THE COCKPIT AND CABIN. COMPLETED AN ENGINE RUN AND PACK ISOLATION IAW TSM 05-50-500-00-810-831A. NO ODOR NOTED. AIRCRAFT OKAY FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 46,697 hrs · 21,831 cycles

NR 2 PACK 2 FUME EVENT. ACCOMPLISHED T.I 2100-1706, NO DISCREPANCIES NOTED, NR 2 PACK, NO FUMES NOTED.

Part: SEAL — LEAKING (DEOILER) · airframe 46,307 hrs · 21,682 cycles

STRONG DIRTY SOCK ODOR DURING FINAL APPROACH. FOUND THE DEOILER SEAL LEAKING ON THE NR 1 ENGINE. R & R THE DEOILER SEAL IAW AM 72-60-31. CLEANED THE ENVIROMENTAL CONTROL SYSTEM WITH BOTH ENGINES IAW AMM 21-00-00. NO ODOR NOTED.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 46,026 hrs · 21,550 cycles

ODOR DETECTED IN THE COCKPIT AND CABIN DURING FINAL DESCENT. RAN THE NR 1 AND 2 PACKS ON APU AND ENGINE POWER OPERATED AT FULL HOT FOR 30 MINUTES AND FULL COLD FOR 30 MINUTES. NO ODORS NOTED IN THE COCKPIT OR CABIN IAW AMM 21-63-00.

Part: TURBINE BLADES — DAMAGED (NR 2 ENGINE) · airframe 41,565 hrs · 19,745 cycles

LOST THE NR 2 ENGINE AT 4500 FT, NO FIRE, SLIGHT N2 REMAINED THROUGHOUT APP TO 4L. EMERGENCY CREW REPORTED NO FIRE BUT METAL FRAGMENTS BELOW ENGINE ON RUNWAY, VISUAL INSPECTION OF THE EXHAUST SECTION REVEALED MANY DAMAGED OR MISSING TURBINE BLADES. VISUAL INSPECTION OF THE INTAKE AND FAN BLADES REVEALED NO DEFECTS OR EVIDENCE OF FOD INGESTION.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 43,388 hrs · 20,408 cycles

FIRST OFFICER`S OXYGEN MASK HARNESS LEAKING WHEN INFLATED. R & R THE OXYGEN MASK IAW AMM 35-12-41. OPS & LEAK CHECKED GOOD.

Part: OXYGEN MASK — DEFECTIVE (COCKPIT)

CA O2 MASK OXYGEN HOSE LOOSE. DISCONNECTED TWO TIMES DURING FLIGHT. R&R CA O2 FULL FACE QUICK DONNING MASK IAW AMM 35-12-41. OPS CHECK NORMAL. A/C OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 42,175 hrs · 19,888 cycles

POSSIBLE FUME EVENT. SHUT DOWN PACK NR 2, SHUT DOWN PACK NR 1 COCKPIT AND CABIN SMELLED ODOR STRONGLY. PERFORMED TSM 05-20-00-810-831-A. ISOLATED PACK NR 2 . PACK NR 2 FOUND DEFECTIVE. NO LEAKS FOUND ON ENGINES OR APU.

Part: UNKNOWN — ODOR (CABIN)

DURING APPROACH, FA NOTICED A PAINT ODOR IN THE FWD CABIN AND A MUSTY SOCKS ODOR WAS REPORTED IN THE AFT CABIN. PERFORMED PACK BURN WITH APU ON NR 1 AND 2 PACKS IAW AMM 21-00-00-615-002 AND 21-00-00-615-004. NO ODOR NOTED

Part: UNKNOWN — ODOR (COCKPIT) · airframe 40,924 hrs · 19,322 cycles

ON DESCENT HAD MUSTY FUMES ODOR IN COCKPIT. PERFORMED OB16-13 PROCEDURE PACK 1 OFF AND ODOR DISSIPATED.

Part: OXYGEN MASK — BROKEN (COCKPIT) · airframe 38,295 hrs · 18,112 cycles

F/O OXYGEN MASK STRAP BROKEN. CONFIRMED DAMAGED. R & R F/O OXYGEN MASK IAW AMM 35-12-41. OPS CHECK AND LEAK CHECK GOOD.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 32,885 hrs · 15,622 cycles

FOUND CORROSION ON LT WING TOP SKIN. REMOVE CORROSION IAW 51-74-00. FOUND TO BE IN LIMITS IAW 57-21-11.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 32,885 hrs · 15,622 cycles

FOUND LT WING TOP SKIN CORRODED AT RIBS 15-16. REMOVED CORROSION IAW 51-74-00. FOUND TO BE WITHIN LIMITS IAW SRM 57-21-11.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 32,885 hrs · 15,622 cycles

FOUND RT WING TOP SKIN CORRODED RIBS 15-16. BLENDED CORROSION IAW SRM 57-74-00, FOUND TO BE WITHIN LIMITS IAW SRM 51-21-11.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 32,885 hrs · 15,622 cycles

FOUND LT WING TOP SKIN CORRODED AT RIBS 18-19. REMOVED CORROSION9 IAW 51-74-00. FOUND TO BE WITHIN LIMITS IAW SRM 57-21-11.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 32,885 hrs · 15,622 cycles

FOUND CORROSION LT WING TOP SKIN PANEL BETWEEN RIBS 10-11, S7L. REPAIRED IAW EO 5721-1425, REV 00.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 32,855 hrs · 15,622 cycles

FOUND CORROSION RT WING TOP SKIN AT RIBS 11-12. BLENDED & REPAIRED RT WING SKIN IAW SRM 57-74-00. REPAIR INSTRUCTION R572-58998.

Part: OXYGEN MASK — UNWANTED DEPLOY (ROW 10ABC) · airframe 32,589 hrs · 15,481 cycles

OXYGEN MASKS DEPLOYED AT ROW 10 A-B-C. STOWED MASKS, ROW 10 ABC IAW AMM 35-21-43-550-801-A. PERFORMED MANUAL MASK RELEASE TEST IAW AMM 35-23-00-710-001-A, DROP TESTED GOOD.

Part: DOOR — OPEN (OXYGEN MASK) · airframe 32,437 hrs · 15,418 cycles

OXYGEN DOOR DROPPED DUE TO TURBULANCE. ROW 7. PERFORMED MANUAL MASK RELEASE OPS CHECK IAW AMM 35-23-00. OPS CHECKED GOOD. NO DEFECT NOTED.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 31,855 hrs · 15,188 cycles

F/A EMERGENCY LIGHT ON AND EXIT LIGHT AND EXIT LIGHT ON DURING FLIGHT. OPS TEST OF EMERGENCY LIGHT IAW AMM. TEST OK, NO FAULTS NOTED AT THIS TIME. ACFT OK FOR SERVICES.

Part: OXYGEN MASK — DAMAGED (COCKPIT) · airframe 31,805 hrs · 15,167 cycles

CAPTAIN`S OXYGEN MASK PLASTIC STRAP THAT HOLDS, SECURES MASK BROKEN. R & R CAPTAIN'S OXYGEN MASK IAW AMM. OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 31,794 hrs · 15,163 cycles

FWD INBD F/A EMERGENCY FLASHLIGHT BROKEN. R & R EMERGENCY FLASHLIGHT IAW FWD INBD F/A SEAT IAW CMM.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 31,404 hrs · 15,010 cycles

F/A REPORTS PROBLEM WITH EMERGENCY EXIT LIGHTS ON IN FLIGHT. PERFORM POWER UP TEST IAW AMM. OPS CHECKED GOOD. ALL INDICATIONS NORMAL.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 31,396 hrs · 15,006 cycles

F/A REPORTED EMERGENCY EXIT LIGHTS ILLUMINATED IN FLIGHT. RESET EMERGENCY EXIT LIGHT SWITCH BUT LIGHTS STAY ON. PERFORMED INTERFACE AND POWER UP TEST IAW AMM 23-73-00-740-001-A, INDICATIONS NORMAL.

Part: OXYGEN MASK — FAULTY (COCKPIT) · airframe 31,021 hrs · 14,854 cycles

FIRST OBSERVER`S OXYGEN MASK WILL NOT PUSH TO TEST. R & R THE OXYGEN MASK STOWAGE BOX IAW AMM, OPS CHECKED GOOD.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 30,892 hrs · 14,804 cycles

F/A REPORTED EMERGENCY LIGHTS IN CABIN WOULD ILLUMINATE INTERMITTENTLY DURING FLIGHT. PERFORMED OPS TEST OF THE EMERGENCY LIGHTS IAW AMM, NO FAULTS NOTED, OK FOR SERVICE.

Part: OXYGEN MASK — NO TEST (COCKPIT) · airframe 30,792 hrs · 14,765 cycles

FIRST OBSERVER`S OXYGEN MASK WILL NOT PUSH TO TEST.

Part: OXYGEN MASK — NO TEST (COCKPIT) · airframe 30,783 hrs · 14,760 cycles

OXYGEN MASK FOR SECOND OBSERVER WILL NOT TEST WHEN PUSH TO TEST PRESSED.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 30,783 hrs · 14,760 cycles

EMERGENCY LIGHTS CAME ON WHEN NR 2 ENGINE WAS SHUTDOWN AND STAYED ON. NO POWER INTERUPTION NOTED. PERFORMED OPS TEST IAW AMM. TEST PASS, NO FAULTS RECORDED.

Part: SWITCH — MISSING (MEGAPHONE) · airframe 30,719 hrs · 14,734 cycles

VOLUME SWITCH MISSING ON FOWARD MEGAPHONE. INST KNOB AS REQ IAW CMM. NO OTHER DEFECTS.

Part: LIFE VEST — DAMAGED (CABIN) · airframe 28,381 hrs · 14,102 cycles

LIFE VEST IS DAMAGED . R & R VEST.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 28,683 hrs · 13,785 cycles

FWD CABIN MEGAPHONE MISSING VOLUME KNOB. R & R FWD MEGAPHONE IAW ACFT MM. OPS CHECKED GOOD.

Part: BATTERY PACK — FAULTED (EMERGENCY LIGHTS) · airframe 28,418 hrs · 13,659 cycles

EXTERNAL POWER DROPPED OFF AND NOTICED EMERGENCY LIGHTS INOPERATIVE, FORWARD PORTION OF ACFT. ACCOMPLISHED OPS TEST OF EPSU IAW ACFT MM. FAULT BAT/EPSU 10WL FWD LT R & R BATTERY PACK. TEST OK.

Part: SEAL — LEAKING (L2 DOOR) · airframe 28,015 hrs · 13,464 cycles

L2 DOOR SEAL LEAKING. PERFORMED DETAILED INSPECTION OF DOOR SEAL. FOUND DEBRIS AND SLIDE STRAP UNDER SEAL. FOUND DE-ICE FLUID UNDER LOWER PORTION OF DOOR SEAL. CLEARED DEBRIS, STOWED STRAP, CLEANED DE-ICE FLUID. NO DAMAGE FOUND WITH SEAL. NO FURTHER DEFECT IAW ACFT MM.

Part: ACTUATOR — INOPERATIVE (OXYGEN MASK) · airframe 27,629 hrs · 13,288 cycles

NR 21 RT O2 DOOR DID NOT DEPLOY. NR 21 RT O2 DOOR AND ACTUATOR WAS R & R.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 25,944 hrs · 12,432 cycles

EXIT SIGNS REMAINED ON AFTER TAKEOFF. ACCOMPLISHED INTERFACE POWER UP TEST. SYSTEM CHECKED GOOD, NO FAULTS IAW AMM 23-73-00-740-005-B.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,728 hrs · 12,327 cycles

CFDS FAULT CODE "BAT/EPSU (11WG) EMERGENCY LIGHT. TROUBLESHOT IAW TSM 33-51-00-810-855-A. R & R BATTERY IAW AMM 33-51-38-000-002-A & 33-51-38-400-002-A. OPS TEST OK IAW AMM 33-51-00-710-003 & 33-51-00-710-001.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,728 hrs · 12,327 cycles

CFDS FAULT MESSAGE EPSU 12WL EMERGENCY R . TROUBLESHOOT IAW TSM 33-51-00-810-835A. R & R EPSU IAW AMM 33-51-38-000-001 & 33-51-38-400-001 AND R & R EPSU BATTERY IAW AMM 33-51-38-000-002-A & 33-51-38-400-001-A. OPS TEST PK IAW AMM.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHTS) · airframe 25,574 hrs · 12,244 cycles

EPSU TEST FAILED (10WL) FWD L. REMOVED BATTERY & POWER SUPPLY UNIT CONNECTOR, CLEANED CONTACTS & REINSTALLED AMM-33-51-38-000-002-A, 33-51-38-400-002-A, 33-51-38-000-001-A, 33-51-38-400-001-A. OPS TEST OK AMM.

Part: EPSU — FAILED (EMERGENCY LIGHT) · airframe 25,574 hrs · 12,244 cycles

EPSU TEST FAILED (12WL). REMOVED BATTERY & POWER SUPPLY UNIT CONNECTOR, CLEANED CONTACTS & REINSTALLED AMM 33-51-38-000-002-A, 33-51-38-400-002-A, 33-51-38-000-001-A, 33-51-38-400-001-A. OPS TESTED OK AMM.

Part: EPSU — FAILED (EMERGENCY LIGHTS) · airframe 25,574 hrs · 12,244 cycles

EPSU TEST FAILED (11WL) EMERGENCY LIGHT. REMOVED BATTERY & POWER SUPPLY UNIT CONNECTOR, CLEANED CONTACTS & REINSTALLED AMM 31-51-38-000-002-1, 33-51-38-400-002-A, 33-51-38-000-001-A, 33-51-38-400-001-A. OPS CHECKED IAW AMM 33-51-00-710-001-A.

Part: PANEL — WORN (THRUST REVERSER) · airframe 21,245 hrs · 10,241 cycles

ENGINE NR1, INBD/RT THRUST REVERSE C-DUCT, PAN-DOWN PANEL WITH WEAR. MAJOR REPAIR.

Part: FITTING — CRACKED (NR 1 PYLON) · airframe 21,245 hrs · 10,241 cycles

ENGINE NR 1, PYLON AFT FIXED FAIRING, PYLON STA 837 FWD LOWER SECTION INTERNAL FITTING CRACKED. NOTE: THE FITTING CRACK REQUIRES A MAJOR REPAIR IAW SRM GUIDELINES.

Part: PANEL — WORN (THRUST REVERSER) · airframe 21,245 hrs · 10,241 cycles

ENGINE NR 2, OTBD/RT THRUST REVERSER C-DUCT, PAN-DOWN PANEL WITH WEAR. MAJOR REPAIR.

Part: PANEL — WORN (THRUST REVERSER) · airframe 21,245 hrs · 10,241 cycles

ENGINE NR 1, OTBD/LT THRUST REVERSER C-DUCT, PAN-DOWN PANEL WITH WEAR. MAJOR REPAIR.

Part: STRAP — WORN (ZONE 600) · airframe 21,245 hrs · 10,241 cycles

RT WING, STA 4862 T/E FIXED UPPER PANEL STRAP WITH WEAR. MAJOR REPAIR.

Part: PANEL — WORN (THRUST REVERSER) · airframe 21,245 hrs · 10,241 cycles

ENGINE NR 2, INBD/LT THRUST REVERSE C-DUCT, PAN-DOWN PANEL WITH WEAR. MAJOR REPAIR.

Part: STRAP — WORN (ZONE 500) · airframe 21,245 hrs · 10,241 cycles

LT WING, STA 4862 T/E FIXED UPPER PANEL STRAP WITH WEAR. MAJOR REPAIR.

Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 21,245 hrs · 10,241 cycles

LOWER FUSELAGE, LT LATERAL AVIONIC COMPARTMENT AT STA 808 WASTE DUCT SUPPORT BRACKET CRACKED. MAJOR REPAIR.

Part: FITTING — BROKEN (ZONE 300) · airframe 21,245 hrs · 10,241 cycles

HORIZONTAL STABILIZER, LT ELEVATOR INBD ACTUATOR FITTING WITH LOCK BROKEN. MAJOR REPAIR.

Part: SKIN — CRACKED (NR 1 NACELLE) · airframe 21,245 hrs · 10,241 cycles

ENGINE NR 1, PYLON PRECOOLER PANEL (413DL) SKIN VENT GRILL WITH CRACKS. MAJOR REPAIR.

Part: SKIN — CRACKED (NR 2 NACELLE) · airframe 21,245 hrs · 10,241 cycles

ENGINE NR 2 PYLON PRECOOLER PANEL (423DL) SKIN VENT GRILL WITH CRACKS. MAJOR REPAIR.

Part: FITTING — CORRODED (ZONE 600) · airframe 21,245 hrs · 10,241 cycles

RT WING, INNER REAR SPAR BETWEEN RIB 2 AND RIB 3, MLG RETRACTION JACK ANCHORAGE FITTING'S BORE AND SPOTFACE WITH CORROSION. MAJOR REPAIR.

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 21,245 hrs · 10,241 cycles

LT WING, BETWEEN RIB 12 AND RIB 13 STRINGER 8 TOP SKIN WITH CORROSION. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,245 hrs · 10,241 cycles

PAX CABIN, UPPER REAR FUSELAGE BETWEEN C68 (STA 2884) AND C69 (STA 2936) -Y1732 FLOOR SUPPORT WITH CORROSION. MAJOR REPAIR.

Part: SKIN — CORRODED (NACELLE) · corrosion level 2 · airframe 21,245 hrs · 10,241 cycles

ENGINE NR 1, PYLON AFT FIXED FAIRING, OTBD AND INBD LATERAL SKIN PANEL WITH CORROSION. MAJOR REPAIR.

Part: FITTING — CORRODED (ZONE 500) · airframe 21,245 hrs · 10,241 cycles

LT WING, INNER REAR SPAR BETWEEN RIB 2 AND RIB 3, MLG RETRACTION JACK ANCHORAGE FITTING'S BORE AND SPOTFACE WITH CORROSION. MAJOR REPAIR.

Part: SKIN — CORRODED (NR 2 NACELLE) · corrosion level 2 · airframe 21,245 hrs · 10,241 cycles

ENGINE NR 2, PYLON AFT FIXED FAIRING, OTBD AND INBD LATERAL SKIN PANEL WITH CORROSION. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,245 hrs · 10,241 cycles

PAX CABIN, UPPER REAR FUSELAGE BETWEEN C68 (STA 2884) AND C69 (STA 2936) Y 1292 FLOOR SUPPORT LONGITUDINAL BEAM WITH CORROSION. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,245 hrs · 10,241 cycles

PAX CABIN, UPPER REAR FUSELAGE BETWEEN C67 (STA 2835)AND C68 (STA 2884) -Y 65 FLOOR SUPPORT LONGITUDINAL BEAM WITH CORROSION. MAJOR REPAIR.

Part: SKIN — DEBONDED (RUDDER) · airframe 21,245 hrs · 10,241 cycles

VERTICAL STABILIZER, RUDDER SIDE PANEL WITH WATER INGRESS AROUND HOISTING POINT NR 3. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,245 hrs · 10,241 cycles

PAX CABIN, UPPER REAR FUSELAGE STA 2786 -Y 765 RAIL SEAT WITH CORROSION. MAJOR REPAIR.

Part: WARNING SYSTEM — FALSE INDICATION (CARGO DOOR) · airframe 19,793 hrs · 9,475 cycles

AFTER T/O AT FLAP RETRACTION (END INHIBIT) MULTIPLE (15-20) CARGO DOOR OPEN ECAMS CAME ON & WENT OFF. VERIFIED AFT CARGO DOOR CLOSED AND LOCKED. AFT CARGO DOOR OPEN ECAM WARNING IS ERRONEOUS AND INTERMITTENT. TRANSFERRED TO DMI NR520295-1 IAW MEL 52-70-01H CAT "C" DUE 12-24-2010. MX PROCEDURES WERE COMPLIED WITH.

Part: RUDDER CONTROL — BINDING (ZONE 300) · airframe 18,941 hrs · 9,064 cycles

LOW SPEED ABORT 40KTS GATE RETURN DUE TO RUDDER BINDING,

Part: RADAR — INOPERATIVE (WX SYSTEM) · airframe 18,826 hrs · 9,007 cycles

GATE RETURN DUE TO A WEATHER RADAR OUTAGE. THE ACFT DID A LOW SPEED ABORT TAKEOFF, 75 KTS.

Part: SLIDE — DISCHARGED (L1 DOOR) · airframe 17,360 hrs · 8,294 cycles

L1 DOOR SLIDE IS IN THE RED. R & R L1 DOOR SLIDE

Part: SLIDE — DISCHARGED (L1 DOOR) · airframe 17,360 hrs · 8,294 cycles

L1 DOOR SLIDE IS IN THE RED. R & R L1 DOOR SLIDE

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,587 hrs · 7,457 cycles

FLOORBEAM AT FR59 HAS CORROSION. REMOVED AND REPLACED FLOORBEAM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,587 hrs · 7,457 cycles

AFT GALLEY FLOOR SUPPORT Y254 FR70 AT FR68 CORRODED. REPLACED FLOORBEAM.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,587 hrs · 7,457 cycles

TIE PLATES AT FR 68 HAVE CORROSION. REMOVED AND REPLACED TIE PLATES.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 9,283 hrs · 4,465 cycles

FOUND CORROSION AT FLOORBEAM Y765 FR66 TO FR70. REPLACED FLOORBEAM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 9,283 hrs · 4,465 cycles

FOUND FLOORBEAM CORROSION AT Y1292 BETWEEN FR66 AND FR68. REPLACED FLOORBEAM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 9,283 hrs · 4,465 cycles

AFT FUSELAGE FLOORBEAM AT Y254 BETWEEN FR68 AND FR70. REPLACED FLOORBEAM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 9,283 hrs · 4,465 cycles

FOUND CORROSION ON FLOORBEAM AT Y765 BETWEEN FR66 AND FR70. REPLACED FLOORBEAM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 9,283 hrs · 4,465 cycles

FOUND CORROSION ON AFT FUSELAGE FLOORBEAM Y765 BETWEEN FR64 AND FR66. REPLACED FLOORBEAM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 9,283 hrs · 4,465 cycles

AFT FUSELAGE FLOORBEAM CORRODED AT Y254 BETWEEN FR66 AND FR68. REPLACED FLOORBEAM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 9,283 hrs · 4,465 cycles

FOUND CORROSION ON FLOORBEAM AT Y1292 BETWEEN FR66 AND FR68. REPLACED FLOORBEAM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 6,825 hrs · 3,330 cycles

ON CHECK, EMERG LIGHTS FAIL 11WL POSITION. REMOVED AND REPLACED 11WL BATTERY PACK.