N514NK

Part: FLASHLIGHT — INOPERATIVE (ZONE 900) · airframe 58,700 hrs · 27,008 cycles

R2 EMERGENCY FLASHLIGHT INOP.-REPLACED EMERGENCY FLASHLIGHT IAW SPIRIT AIRLINES EMERGENCY EQUIPMENT.

Part: MEGAPHONE — DAMAGED (ZONE 900) · airframe 58,600 hrs · 26,949 cycles

FWD MEGAPHONE VOLUME KNOB MISSING-REMOVED AND REPLACED FWD MEGAPHONE IAW DRAWING A319 EMER EQUIP. OPS CHECK GOOD

Part: NONE — NONE · airframe 57,703 hrs · 26,478 cycles

PUNGENS DIRTY SOCK SMELL ON AIRCRAFT SAFETY CONCERN-ACCOMPLISHED TSM 05-50-00-810-836 PERFORMED DECONTAMINATION OF THE ENVIRONMENTAL CONTROL SYST IAW AMM 21-00-00 NO SIGHT OF CONTAMINATION ISOLATED BOTH PACKS ON APU NO SIGNS OF SMELL PERFORMED ENG 1 & 2 RUN IAW AMM 71-00-00 ISOLATED BOTH PACKS NO SIGHT OF SMELL WITH AEROTRACER WALT THRU CABIN R/R RECIRCULATION FILTERS IAW AMM 21-21-41 INSPECTED ENG APU AND PACK NO DEFECT NOTED. A/C OK FOR SERVICES

Part: NONE — NONE · airframe 57,695 hrs · 26,474 cycles

DIRTY SOCK SMELL IN AFT CABIN AFTER DECENDING THROUGH FL180-ACCOMPLISHED TSM 05-50-00-810-831 FOR CABIN ODOR. RAN BOTH PACK ON APU BLEED. ISOLATED PACKS, NO SIGN OF CONTAMINATION WITH AEROTRACER WALK THRU OF CABIN, RAN BOTH ENG BLEED, ISOLATED PACKS, NO SIGN OF CONTAMINATION, ENG APU + PACKS INSPECTED NO SIGN OF ODOR ORIGIN NOTED. PERFORMED DECONTAMINATION OF THE ENVIORMENTAL CONTROL SYS IAW AMM 21-00-00. NO SMELL NOTED AFTER DECONTAMINATION R+ R RECIRCULATION FILTERS IAW AMM 21-21-41. A/C OK FOR SVC

Part: NONE — NONE · airframe 57,697 hrs · 26,475 cycles

DIRTY SOCK ODOR IN AFT CABIN-PERFORMED TSM 05-50-00-810-831-A INSPECTION OF THE A/C WAS PERFORMED AND ENGINES WERE INSPECTED NO EVIDENCE OF LEAKS. ENGINE RUN-UP PERFORMED. WE IDENTIFIED THE SOURCE OF THE ODOR. PLEASE SEE ITEM 1 ON LOG PAGE 2975560-1

Part: NONE — NONE · airframe 55,894 hrs · 25,707 cycles

L2 DOOR ASSIST BOTTLE NEEDS SERVICE. -SERVICED L2 DOOR ASSIST BOTTLE I.A.W AMM 52-10-00.

Part: A/C PACK — ODOR (NR 2) · airframe 55,555 hrs · 25,571 cycles

BURNING OIL/ RUBBER SMELL ODOR IN AFT GALLEY.-T/S A/C IAW TSM 05-50-00-810-831-A. ISOLATED SMELL/ODER TO PACK 2. PERFORMED DECONTAMINATION OF ECS IAW AMM 21-00-00-615-802-A. NO MORE/SMELL AT THIS TIME. A/C RETURNED TO SERVICE.

Part: NONE — NONE · airframe 55,491 hrs · 25,544 cycles

DURING INITIAL CLIMB - VERY LARGE SINGLE BIRD STRIKE TO AN UNKNOWN AREA OF THE AIRCRAFT. RETURNED SAP FOR INSPECTION CORRETION - JL - LEFT WINGLET.-PERFORMED INSP OF AIR FRAME AFTER BIRD STRIKE NO DAMAGE FOUND TO FUSELAGE, PYLON AND NACELLS, NO EVIDENCE OF BIRD INGESION IN ENGINE IAW AMM 05-51-14-200-803-A A/C OK TO CONT SERVICE.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 54,610 hrs · 25,165 cycles

AFT FACING FA JUMPSEAT FLASHLIGHT INOP-REMOVED AND REPLACED AFT FACING FA JUMPSEAT FLASHLIGHT IAW SPIRIT AIRLINES EMERGENCY EQUIPMEMT DRAWING NK319-132-EQ

Part: BOTTLE — LOW PRESSURE (L1 DOOR ASSIST) · airframe 52,945 hrs · 24,446 cycles

L1 DOOR ASSIST BOTTLE REQ. SVC.-SERVICE DOOR IAW AMM 52-10-00

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 52,047 hrs · 24,068 cycles

L1 DOOR ASSIST BOTTLE REQUIRES SVC. SVC L1 DOOR ASSIST BOTTLE IAW AMM 52-10-00-614-001-A TO REQUIRED LIMITS.

Part: OUTFLOW VALVE — WARNING MESSAGE (CABIN PRESSURE) · airframe 50,363 hrs · 23,322 cycles

VENT SKIN VALVE FAULT AFTER ROTATION. PERFORM AVEC TEST PER AMM 21-+26-00. TESTED OK, ACFT OK FOR SERVICE. MSG CLEARED.

Part: A/C PACK — ODOR (AC BAY) · airframe 50,036 hrs · 23,187 cycles

ODOR FROM PACK 1 ON DESCENT-PER TSM 05-50-00-810-831-A CONFIRMED PACK 1 SOURCE OF ODOR SEE L/P 2535157-02 FOR CORRECTIVE ACTION.

Part: CONTROL ROD — DAMAGED (NLG DOOR) · airframe 49,157 hrs · 22,844 cycles

IN FLIGHT L/G DOORS NOT CLOSED ECAM MESSAGE-REPLACED NLG DOOR CONTROL RODS PER AMM 32-31-41.PERFORMED OPS TEST PER 32-22-00 OPS CHECK NORMAL FAULT CLEARED.

Part: SCREW — STRIPPED (MEGAPHONE) · airframe 48,126 hrs · 22,392 cycles

R&R MEGAPHONE BATTERYS. SCREW STRIP ON FWD MEGAPHONE COULD NOT REMOVE BATT. R&R FWD MEGAPHONE IAW EMERGENCY EQUIPMENT DRAWING LAYOUT EQ REV 6.

Part: CLAMP — LOOSE (NR 1 A/C PACK) · airframe 46,979 hrs · 21,873 cycles

ODOR DURING DESCENT, PERFORMED A VISUAL INSPECTION OF THE NR 1 ENGINE, NO LEAKKS NOTED. ENG. OIL CONSUMPTIION OK. PERFORMED GVI OF THE A/C PACKS, FOUND PIPE ASSY FROM NR 1 ACM HEAT EXCHANGER AND ACM CLAMP LOOSE, SECURED THE PIPE ASSY IAW AMM 21-52-33 , LEAK CHECKED OK. PERFORMED A NR 1 ENG. IDLE RUN CHECK NO ODOR , PERFORMED DECONTAMINATION OF THE EC SYSTEM IAW AMM 21-00-00, NO ODOR.

Part: UNKNOWN — ODOR (CABIN) · airframe 46,977 hrs · 21,872 cycles

DURING DESCENT, HAD AN ODOR IN THE CABIN. PERFORMED TSM 05-50-00-810-831-A. PERFORMED A WALKAROUND, NO DISCREPANCIES NOTED. COMPLETED APU, NR 1 & 2 PACKS OPS CHECKED. PERFORMED ENGINE RUNS, FOUND OK.

Part: SKIN — DEBONDED (NR 2 FAN COWL) · airframe 45,356 hrs · 21,202 cycles

NR 2 ENGINE INBD FAN COWL OUTER SKIN & INNER SKIN DAMAGE SHOWS DEBONDING. COMPLIED WITH EO 5414-1719.

Part: WINDOW FRAME — CRACKED (RT WINDSHIELD) · airframe 45,356 hrs · 21,202 cycles

RIGHT WINDSHIELD FRAME D53111061211 AT FRAMES 3 - 4 CRACKED, COMPLIED WITH THE WINDHSIELD SIDE POST LOWER ATTACHMENT LOWER STIFFENER.

Part: PROFILE — DAMAGED (FRAME 47-51) · airframe 45,356 hrs · 21,202 cycles

AFT CARGO CEILING PROFILE DAMAGED. REPAIRED IAW 80395404/003, CLASSIFIED AS MINOR.

Part: DOOR SILL — CORRODED (RIGHT) · airframe 45,356 hrs · 21,202 cycles

FWD RT DOOR SILL CORRODED. REPAIRED THE DOOR SILL IAW 803942001, AND EO 5311-1790.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 45,356 hrs · 21,202 cycles

LEFT WINDSHIELD FRAME CRACKED. REPAIRED IAW EO 5311-1786, REV 00.

Part: TORSION BOX — CRACKED (FRAME 43) · airframe 45,356 hrs · 21,202 cycles

TORSION BOX AT FRAME 43, STR 15R CRACKED. REPAIRED IAW 80932748, AND EO 5331-1792.

Part: SKIN — GOUGED (FRAMES 34-35) · airframe 45,356 hrs · 21,202 cycles

SKIN FRAMES 34 - 35, STRINGER 43L & R GOUGED. REMOVED THE GOUGES IAW 80392172 AND EO 5311-1791.

Part: UNKNOWN — ODOR · airframe 44,951 hrs · 21,043 cycles

STRONG DIRTY SOCK SMELL ON DESCENT AROUND 6,000 FEET TURNED OFF PACK 1 SMELL EVENTUALLY WENT AWAY.

Part: MEGAPHONE — MALFUNCTIONED (CABIN) · airframe 43,179 hrs · 20,240 cycles

MEGAPHONE ALARM SOUND UNLESS HELD IN THE OFF POSITION. REMOVED AND REPLACED THE FLIGHT ATTNDANT MEGAPHONE FWD, IAW DWG NK319-132-EQ, OPS CHECKED GOOD.

Part: OXYGEN MASK — UNSECURE (CABIN) · airframe 41,485 hrs · 19,525 cycles

OXYGEN MASK OVER ROW 11 FELT OUT OF OVERHEAD. OPS CHECK MANUAL MASK RELEASED IAW AMM 35-23-00.

Part: DOOR — DEFECTIVE (CABIN O2) · airframe 41,457 hrs · 19,511 cycles

F/A AFT GALLEY O2 MASK DROPPED FROM CEILING. R&R AFT GALLEY F/A O2 MASK CONTAINER DOOR IAW B/E CMM 35-21-74. OPS TEST OK IAW AMM 35-23-00. NO FURTHER DEFECTS NOTED.

Part: APU — ODOR · airframe 40,442 hrs · 19,064 cycles

FUMES REPORTED BY AFT F/A'S. PERFORMED IDENTIFICATION OF THE CAUSE OF CABIN ODOR IAW TSM 05-50-00-810-8311-A. APU SUSPECTED TO BE AT FAULT. PERFORMED ECS CLEANING IAW AMM 21-00-00-615-004-A. NO MORE ODOR IN AIRCRAFT.

Part: PANEL — LOOSE (ROW 15) · airframe 38,633 hrs · 18,235 cycles

OXYGEN MASK FELL OVER ROW 15. FOUND ALL OXYGEN MASKS SECURE. FILLER PANEL WAS FOUND HANGING, SECURED FILLER PANEL IAW AMM 25-25-11.

Part: TOILET — BLOCKED (LAVATORY) · airframe 38,188 hrs · 18,053 cycles

F/A REPORTS RAW SEWAGE/LIQUID SEEPING FROM FWD LAV AREA AND UNDER BULKHEAD WHERE F/A JUMPSEATS LOCATED. MAINTENANCE CONTROL AND DISPATCH REQUIRE AIR RETURN TO DEPARTURE. REMOVED TOILET SHROUD AND CLEANED FWD LAVATORY IAW AMM 12-21-12 AND REINSTALLED TOILET IAW AMM 25-45-22

Part: PANEL — LOOSE (PSU) · airframe 35,541 hrs · 16,865 cycles

OXYGEN MASK COMPARTMENT LOOSE ABOVE 1 B/C. SECURED PAX PSU PANEL AT 1 B/C IAW AMM 35-21-43. NO FURTHER DEFECTS NOTED.

Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT 26 DEF) · airframe 34,969 hrs · 16,595 cycles

OXYGEN MASK, SEATS 26 DEF SELF DEPLOYED AFTER TAKEOFF. SECURED O2 MASK ASSY, CONTAINER IAW AMM 35-210. NO OTHER DEFECTS NOTED.

Part: OXYGEN MASK — UNSECURE (SEAT 16 DEF) · airframe 34,502 hrs · 16,396 cycles

16 DEF, O2 MASKS DEPLOYED. RE-STOWED MASKS AND PERFORMED TEST OF MANUAL MASK RELEASE IAW AMM 35-23-00.

Part: OXYGEN MASK — UNSECURE (CABIN) · airframe 34,490 hrs · 16,391 cycles

ROW 26DEF OXY MASK COMPARTMENT OPEN ON TAKEOFF. SECURED O2 PASS MASK CONTAINER IAW AMM 33-21-11.

Part: MEGAPHONE — INOPERATIVE (FWD GALLEY) · airframe 34,004 hrs · 16,168 cycles

FWD MEGAPHONE INOPERATIVE. R & R FWD MEGAPHONE IAW EMERGENCY EQUIPMENT LAYOUT DWG NK319-132-EQ, OPS CHECKED GOOD.

Part: SETSCREW — BROKEN (MEGAPHONE) · airframe 33,799 hrs · 16,079 cycles

FWD MEGAPHONE SET SCREW ATTACHMENT BROKEN. R & R FWD MEGAPHONE IAW AMM 25-65-51. ALL CHECKED NORMAL

Part: SLIDE — UNWANTED DEPLOY (R1 DOOR) · airframe 29,594 hrs · 14,198 cycles

R1 DOOR ESCAPE SLIDE DEPLOYED. R & R R1 DOOR ESCAPE SLIDE IAW AMM REMOVAL AND AMM INSTALL. OPS CHECKED IAW AMM, OPS CHECKED GOOD. DOOR PUT BACK TO SERVICEABLE CONDITION IAW AMM.

Part: COVER — UNSECURE (EMERGENCY EXIT) · airframe 29,310 hrs · 14,080 cycles

DOOR RT EMERGENCY EXIT ECAM. FOUND EMERGENCY COVER FELL LOOSE, OFF ON DOOR. SECURED COVER AND DOOR LIGHT WENT AWAY FOR OVERWING EXIT. INSPECTED RT EMERGENCY OVERWING EXIT COVER FLAP IAW AMM AND FOUND IT PROPERLY INSTALLED.

Part: COVER — MISINSTALLED (EMERGENCY EXIT) · airframe 28,928 hrs · 13,903 cycles

DURING DESCENT FROM APPROX 12,000 - 6000 FT, DOOR RT EMERGENCY EXIT ECAM. F/A CHECKED DOOR & REPORTED DOOR LIGHT ON & DOOR NOT SEALED PROPERLY. APPLIED TSM 52-21-00-810-807-A. FOUND R EXIT DOOR COVER FLAP NOT CORRECTLY INSTALLED WITH ASSOCIATED FAULT IND ON ECAM AND SLIDE ARMED LIGHT ILLUMINATED. MAINTENANCE CORRECTLY REINSTALLED COVER FLAP IAW TSM AND FAULTS DISAPPEARED. DOOR CONSIDERED SERVICABLE.

Part: BOTTLE — LOW PRESSURE (L2 DOOR SLIDE) · airframe 28,873 hrs · 13,877 cycles

LT AFT L2 SLIDE RESERVOIR PRESSURE GAUGE SHOWS AT BORDER LINE. R & R IAW AMM 25-62-44-000-012-A & 25-62-44-400-007-A. OPS CHECKED GOOD.

Part: SPAR — CORRODED (RT WING) · airframe 28,697 hrs · 13,792 cycles

CORROSION ON RIGHT WING AFT SPAR OVERHANG PANEL SUPPORT JUST OTBD OF NR 3 SPOILER INBD DOGBONE. BOTH SIDES OF SUPPORT, WORK ACCOMPLISHED AND CLEARED ON NON-ROUTINE NR 7230N00361 AND EO 5753-1312 AND STEP 08, TD J1-52-25452-20.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 28,697 hrs · 13,792 cycles

BOTTOM FWD LAVATORY ATTACHMENT CHANNEL AT L1 DOOR HAS CORROSION IN CENTER ATTACHMENT HOLE. WORK ACCOMPLISHED AND CLEARED ON NON-ROUTINE 7230N00205.

Part: SUPPORT — DAMAGED (LT WING) · airframe 28,697 hrs · 13,792 cycles

LEFT WING T/E OVERHANG PANEL SUPPORT JUST OTBD OF NR 3 INBD HINGE RIB 13 & 16 DAMAGED. REPAIRED IAW EA T4277, TD-J1-52-25441-2013 AND EO 5753-1313.

Part: SPAR — CORRODED (RT WING) · airframe 28,697 hrs · 13,792 cycles

CORROSION ON RT WING, AFT SPAR OVERHANG AT NR 3 SPOILER CENTER HINGE BRACKET INBD HING POINT. WORK ACCOMPLISHED AND CLEARED ON ROUTINE NR 7230N00361, EA T4276 AND TD J1-52-25452-20 AND EO 5753-1312.

Part: OXYGEN MASK — DISLODGED (CABIN) · airframe 28,497 hrs · 13,694 cycles

O2 MASKS FELL DOWN FROM 18B. RESTOWED O2 MASK IAW AMM 35-21-43-550-801-A PERFORMED OPS TEST OF MANUAL MASK RELEASE IAW AMM 35-23-00-710-001-A.

Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT 8 DEF) · airframe 28,467 hrs · 13,679 cycles

OXYGEN MASKS AT SEATS 8 EDF DEPLOYED ON LANDING. OP CHECKED GOOD IAW ACFT MM.

Part: LATCH — FAULTED (O2 MASK) · airframe 28,341 hrs · 13,619 cycles

PSU PANEL OPENED UP & O2 MASKS DROPPED OVER ROW 8 ACFT RIGHT. PERFORMED OPS CHECK OF MANUAL MASK RELEASE OF PASSAGER OXYGEN MASK RELEASE. TESTED OK IAW AMM 35-23-00-710-001-A.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 28,239 hrs · 13,577 cycles

LEFT WINDSHIELD HEAT SYS MALFUCTIONED, CRACKED WINDSHIELD, ARCING FLAME VISIBLE, FUMES PRESENT. R & R LT WINDSHIELD IAW AMM OPS CHECKED GOOD NO DEFECTS NOTED AT THIS TIME.

Part: INDICATOR — INOPERATIVE · airframe 28,002 hrs · 13,449 cycles

DURING CLIMBOUT, ISIS AIRSPEED INDICATION DISAPPEARS AND RED BOX WITH SPD DISPLAYED. FOUND CLOG ON PITOT 3. CLEANED PITOT PROBE IAW AMM 34-10-00 AND DRAIN AND FLUSH IAW AMM 34-22-25. INDICATOR REPLACED IAW AMM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 27,936 hrs · 13,416 cycles

LEFT OVERWING EXIT MARKER LENS BROKEN. R & R LT OVERWING EXIT MARKER LENS COVER IAW ACFT MM. OPS CHECKED GOOD.

Part: OXYGEN MASK — UNKNOWN (CABIN) · airframe 27,732 hrs · 13,319 cycles

SEAT 8E OXYGEN MASK HAS DROPPED. PERFORMED OPS CHECK OF MANUAL MASK RELEASE (DROP CHECK) IAW ACFT MM, NO DISCREPANCIES NOTED.

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 27,692 hrs · 13,299 cycles

O2 MASKS DROPPED ABOVE ROW 8. STOWED MASKS IAW AMM 35-21-43-550-801-A. PERFORMED OP TEST OF MANUAL MASK RELEASE IAW ACFT MM. OP CHECK OK.

Part: SEAL — LACK OF LUBE (L1 DOOR) · airframe 27,191 hrs · 13,058 cycles

LOUD VIBRATING NOISE COMING FROM L1 DOOR IN FLIGHT. LUBRICATED DOOR SEAL IAW ACFT MM AND CLEANED DEBRIS FROM GIRT BAR AND LUBRICATED GIRT BAR. REMOVED ICE AND MOISTURE FROM LOWER FWD BOTTOM OF DOOR SURFACE AND CLEANED. ACFT OK FOR SERVICE.

Part: ENGINE — FLUCTUATES (NR 1) · airframe 26,293 hrs · 12,627 cycles

POWER FLUCTUATION DURING TAKEOFF. DURING CLIMB AT F 50 ACFT SUDDENLY YAWED ENGINE NR 1 EPR DROPPED TO ZERO ALONG WITH N1 THEN RECOVERED IT APPEARS THE ENGINE LOST POWER THIS OCCURRED THREE TO FOUR TIMES THROUGH FL 70 WHERE DESCISION TO TURN BACK WAS MADE, DURING DECENT AWD ON APPROACH ALL ENGINE PARAMETERS WERE NORMAL. R & R NR 1 ENGINE MAIN FUEL FILTER, R & R NR 1 ENG FMU, R & R NR 1 L/P HP FUEL PUMP. ACCOMPLISHED HIGH POWER ASSURANCE TEST/ENG RUN. NO FAULT NOTED. ALL CHECKED OUT OK. ACFT RETURNED TO SERVICE.

Part: FLOOR PANEL — CORRODED (ZONE 200) · airframe 22,546 hrs · 10,770 cycles

UPPER FUSELAGE PAX CABIN FLOOR PANEL WITH CORROSION AT STA 7087/FR16 AND +1800. THE DAMAGED FLOOR PANEL WAS REPLACED IAW SRM REQUIREMENTS WITH A NEW ONE.

Part: FLOOR PANEL — CORRODED (ZONE 200) · airframe 22,546 hrs · 10,770 cycles

UPPER FUSELAGE, PAX CABIN OVER FLOOR LEVEL, FROM STA7087/FR16 TO STA8077/FR20, BETWEEN -Y1219 AND -Y1600 FLOOR PANEL 222FF WITH CORROSION AT SEVERAL PLACES. DAMAGED FLOOR PANEL WAS REPLACED IAW SRM REQUIREMENTS UNDER THE NON ROUTINE ITEM.

Part: FLOOR PANEL — CORRODED (ZONE 200) · airframe 22,546 hrs · 10,770 cycles

UPPER FUSELAGE PAX CABIN OVER FLOOR LEVEL FROM STA7087 TO STA8077 FR20 FLOOR PANEL WITH CORROSION AT SEVERAL PLACES. DAMAGED FLOOR PANEL WAS REPLACED IAW SRM REQUIREMENTS, UNDER THE NON ROUTINE ITEM.

Part: FLOOR PANEL — CORRODED (ZONE 200) · airframe 22,546 hrs · 10,770 cycles

UPPER FUSELAGE PAX CABIN OVER FLOOR LEVEL, FROM STA 7087/FR16 TO STA 8077/FR20 BETWEEN -Y203 AND -Y1219, FLOOR PANEL 222EF WITH CORROSION AT SEVERAL PACES. DAMAGED FLOOR PANEL WAS REPLACED IAW SRM REQUIREMENTS, UNDER THE NON ROUTINE ITEM.

Part: SKIN — CORRODED (ZONE 400) · corrosion level 2 · airframe 22,546 hrs · 10,770 cycles

NR 1 ENGINE PYLON AFT LOWER SECTION, INBD AND OTBD SKINS FAIRING WITH CORROSION. THE DAMAGED SKIN WAS REPLACED IAW SRM 51-72-11, PARA 4 AND 6.

Part: ATTACH BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,546 hrs · 10,770 cycles

FUSELAGE LT MLG ACTUATOR ATTACHMENT BRACKET BEARING AREA WITH CORROSION. A TEMPORARY REPAIR WITH A LIFE OF 40000 FC MINIMUM WILL BE INSTALLED IAW REPAIR INSTRUCTIONS 70557467/006 DTD JAN 18, 2012, UNDER THE NON ROUTINE ITEM: JOB: A1A034, SUBJOB: 1, ITEM: 3.

Part: SKIN — CORRODED (ZONE 400) · corrosion level 2 · airframe 22,546 hrs · 10,770 cycles

NR 2 ENGINE PYLON AFT LOWER SECTION, INBD AND OTBD SKIN FAIRING WITH CORROSION. THE DAMAGED PARTS WERE REPLACED IAW SRM 51-72-11, PARA 4 AND 6.

Part: SHEAR WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 22,546 hrs · 10,770 cycles

UPPER FUSELAGE PAX CABIN, AFT FLOORBEAM AREA, SHEAR WEB CORRODED AT STA 29921 FR70 AND +Y1800. THE DAMAGED SHEAR WEB WAS REPLACED IAW SRM REQUIREMENTS, UNDER THE NON ROUTINE ITEM.

Part: SUPPORT — CRACKED (ZONE 100) · airframe 22,546 hrs · 10,770 cycles

LOWER FUSELAGE, LT LATERAL AVIONICS COMPARTMENT, STA 7087/FR 16 ON LEVEL STRINGER 27, WASTE DRAIN DUCT SUPPORT WITH CRACK. THE DAMAGED SUPPORT WAS REPLACED IAW SRM REQUIREMENTS UNDER THE NON ROUTINE ITEM, WORK ORDER: A1A034.

Part: BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 22,546 hrs · 10,770 cycles

UPPER FUSELAGE PAX CABIN LT FWD DOOR SILL BEAM WITH CORROSION AT ESCAPE SLIDE GIRT BAR FITTINGS AREA. A REPAIR IS GOING TO BE PERFORMED IAW REPAIR GUIDELINES REF. 70557953/006 UNDER THE NON ROUTINE ITEM.

Part: CHANNEL — CRACKED (ZONE 400) · airframe 22,546 hrs · 10,770 cycles

NR 2 ENGINE PYLON UPPER SECTION AT RIB 8, RT SIDE CHANNEL CRACKED. REPAIRED IAW SRM 54-52-12, FIG 208.

Part: CHANNEL — CRACKED (ZONE 400) · airframe 22,546 hrs · 10,770 cycles

NR 1 ENGINE PYLON UPPER SECTION AT RIB NR 7 INBD SIDE CHANNEL CRACKED. REPAIRED IAW SRM 54-52-12, FIG 208.

Part: SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 22,546 hrs · 10,770 cycles

UPPER FUSELAGE PAX CABIN RT FWD DOOR SILL BEAM WITH CORROSION AT ESCAPE SLIDE GIRT BAR FITTINGS. A REPAIRED IAW REPAIR GUIDELINES REF. NR 70557953/006 UNDER THE NON ROUTINE ITEM.

Part: CHANNEL — CRACKED (ZONE 400) · airframe 22,546 hrs · 10,770 cycles

NR 2 ENGINE PYLON UPPER SECTION AT NR 7 RIB, INBD SIDE CHANNEL WITH CRACK. REPAIRED IAW SRM 54-52-12, FIG 208.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 22,006 hrs · 10,508 cycles

R2 DOOR SLIDE PRESSURE INDICATION IN THE RED. R & R R2 ESCAPE - SLIDE IAW 25-62-44, PB401.

Part: ATTACH FITTING — STUCK (GIRT BAR) · airframe 18,691 hrs · 8,910 cycles

L1 DOOR GIRT BAR HOLDING CLIP STUCK DOWN. PERFORMED OPS TEST PROCEDURE OF THE GIRT BAR ASSY IAW AMM TASK 25-62-44-710-060, OPS CHECKED GOOD.

Part: PANEL — CORRODED (L2 DOOR) · airframe 17,314 hrs · 8,296 cycles

L2 DOOR PANEL AT FLOOR CORRODED.

Part: SILL — CORRODED (ZONE 100) · airframe 17,314 hrs · 8,296 cycles

RT SILL PLATE HAS CORROSION.

Part: BEAM — CORRODED (ZONE 100) · airframe 17,314 hrs · 8,296 cycles

RT Z-BEAM AT FR67 AND FR68 HAS CORROSION.

Part: BEAM — CORRODED (ZONE 100) · airframe 17,314 hrs · 8,296 cycles

RT Z-BEAM FR 68 HAS CORROSION.

Part: SHEAR PLATE — CORRODED (ZONE 100) · airframe 17,314 hrs · 8,296 cycles

RT SHEAR PLATE HAS CORROSION.

Part: BEAM — SHEARED (FUSELAGE) · airframe 17,314 hrs · 8,296 cycles

RT Z-BEAM AT FR 69 HAS SHEARED FASTENERS.

Part: BEARING — CORRODED (LT ELEVATOR) · airframe 17,314 hrs · 8,296 cycles

LT ELEVATOR NR 4 BEARING IS EMITTING RUST.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 17,314 hrs · 8,296 cycles

LT FLOORBEAM AT FR68 HAS CORROSION.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 17,314 hrs · 8,296 cycles

FLOORBEAM AT Y-765 BETWEEN FR67 AND FR68 HAS CORROSION.

Part: BEAM — SHEARED (ZONE 100) · airframe 17,314 hrs · 8,296 cycles

LT Z-BEAM AT FR 69 HAS SHEARED FASTENERS.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 17,314 hrs · 8,296 cycles

LT FLOORBEAM AT FR67 HAS CORROSION.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 17,314 hrs · 8,296 cycles

SEAT TRACK AT Y765 AT FR 66 HAS CORROSION.

Part: BEARING — CORRODED (ELEVATOR) · airframe 17,314 hrs · 8,296 cycles

RT ELEVATOR NR 4 HINGE BEARING IS EMITTING RUST AND SQUEAKS WHEN ELEVATOR IS MOVED.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 17,314 hrs · 8,296 cycles

SEAT TRACK AT Y1292 AT FR 66 HAS CORROSION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,314 hrs · 8,296 cycles

SEAT TRACK AT Y1292 AT FR66 HAS CORROSION.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 17,314 hrs · 8,296 cycles

FLOORBEAM AT Y300 BETWEEN FR68 AND FR69 SHOWS SIGNS OF CORROSION.

Part: SKIN — CORRODED (ZONE 100) · airframe 17,314 hrs · 8,296 cycles

RT AFT AVX COMP CORROSION AT SKIN AIR VALVE INLET DUCT,

Part: SEAL — LEAKING (NR 5 BEARING) · airframe 16,606 hrs · 7,968 cycles

JUST NORTH OF VOR, NOTICED AN UNUSUAL LOW OIL QTY IN THE NR2 ENG. WE ALSO HAD AN FAA MX INSP IN THE OBSERVERS SEAT. A 3 DAY SERVICE CHECK WAS DONE THE NIGHT BEFORE AND ALSO NOTICED NORMAL OIL QTY BEFORE LEAVING DEPARTURE. NOTICED THE OIL QTY AROUND 10 QRTS AROUND THE OMN VOR. WITHIN 10-15 MINUTES, THEN NOTICED 8.5 QRTS OF OIL IN THE NR2 ENG. CAME TO THE CONCLUSION OF A POSSIBLE OIL LEAK. CONTINUED TO MONITOR THE OIL QTY DROPPING LOWER. DECLARED AN EMERGENCY WITH ATC NOT KNOWING HOW MUCH TIME WE HAD BEFORE SHUTTING DOWN THE ENGINE. FLEW DIRECT TO DESTINATION AND LANDED WITH 3.5 QRTS OF OIL IN THE 2 ENGINE. MX MET US AT THE GATE AND CONFIRMED THERE WAS AN OIL LEAK.

Part: VALVE — FAILED (CABIN PRESSURE) · airframe 12,549 hrs · 6,062 cycles

NR 1 BLEED FAULT FOLLOWED BY LOSS OF CABIN PRESSURE. PERFORM ECAM EMERGENCY DECENT. ACFT WAS FERRIED.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 10,840 hrs · 5,234 cycles

FOUND CORROSION ON FLOORBEAM AT FR69 Y254. REMOVED AND REPLACED FLOORBEAM.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 10,840 hrs · 5,234 cycles

EVIDENCE OF CORROSION AT FR 68 AND Y765 BELOW AFT GALLEY. REMOVED AND REPLACED FLOORBEAM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 5,324 hrs · 2,644 cycles

FLOORBEAM AT Y765 AND FR 66 CORRODED. REPLACED FLOORBEAM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 5,324 hrs · 2,644 cycles

FLOORBEAM AT Y765 BETWEEN FR 67 AND FR 69 HAS CORROSION. REPLACED FLOORBEAM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 5,324 hrs · 2,644 cycles

FLOORBEAM AT R-2 DOOR ENTRANCE BETWEEN FR67 AND FR68 (-Y1292) CORRODED. REPLACED FLOORBEAM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 5,324 hrs · 2,644 cycles

FLOORBEAM AT -Y765 FR 66 CORRODED. REPLACED FLOORBEAM.