N524NK

Part: MEGAPHONE — NO TEST (AFT GALLEY) · airframe 60,698 hrs · 27,920 cycles

MEGAPHONE IN AFT NOT TESTING-R&R AFT GALLEY MEGAPHONE AS PER A319 SPIRIT EMERGENCY EQUIPMENT DRAWING. OK FOR SVC.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,353 hrs · 27,755 cycles

CABIN ODOR ON DESCENT -10000' APU BLEED OFF GOT WORSE AT100' AND LANDING-PERFORMED TSM 05-50-00-810-831-A. FOUND CAUSE OF ODOR TO BE PACK 2.

Part: CHECK VALVE — LEAKING (HYD PTU) · airframe 59,363 hrs · 27,274 cycles

IN CRUISE HYD Y RSVR LO LVL PTU AND ENG 2 PUMP TURNED OFF PER ECAM YELLOW RSVR QTY IN AMBER RANGE-FOUND PTU CHECK VALVE PLUG CAUSE OF LEAK. R/R PTU CHECK VALVE PLUG O-RING IAW AMM 20-29-00, 20-21-12, AND CMM 29-10-23. LEAK CHECK GOOD. PERF OPS TEST OF PTU IAW AMM 29-23-00. TEST GOOD. A/C OK FOR SVC

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,951 hrs · 27,090 cycles

L1 DOOR ASSIST BOTTLE REQ SERVICING-SERVICED L1 DOOR DAMPER IAW AMM 52-10-00. NO LEAKS NOTED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,237 hrs · 26,783 cycles

L1 DOOR ASSIST BOTTLE REQ'S SERVICING-SERVICED L1 DOOR ASSIST BOTTLE IAW AMM 52-10-00-614-001. LEAK CHECK GOOD

Part: PCU — FAULT MESSAGE (6001CM) · airframe 57,786 hrs · 26,564 cycles

FLT/CTR ECAM SLAT FAULT CAME ON. SLATS JAMMED AT ZERO.-PERFORMED TSM 27-81-00-810-810A FOR SLAT SYSTEM JAM. FOUND SLAT PCU AT FAULT. R&R SLAT PCU IAW AMM 27-84-51. OPS CHECK GOOD. A/C OK FOR CONTINUED SERVICE. NO LEAKS NOTED

Part: NONE — NONE · airframe 56,401 hrs · 25,877 cycles

CA EMERGENCY FLASHLIGHT IS NOT CHARGING ( FLASHLIGHT AND HOLDERS (FLIGHT DECK OR CABIN) )-R&R CA FLASHLIGHT IAW A3199 SPIRIT AIRLINES EMERGENCY EQUIPMENT DARWINGS. THIS CLEARS DMI 2850821-1 MOC NOTIFIED PLACRAD REMOVED LOG UPDATED

Part: NONE — NONE · airframe 53,650 hrs · 24,640 cycles

F/CTL SPOILER FAULT AND SPOILER 5 RIGHT SIDE PARTIALLY DEPLOYED IN FLIGHT-INSP FOUND RH SPOILER 5 IMPROPERLY DEACTIVATED PER MEL 27-64-01-7. CANNON PLUG NOT DISCONNECTED & SPOILER KEY STILL INSTALLED AND IN THE "MX" POSITION. RECOMPLIED WITH MEL PROCEDURE PER AMM 27-64-00-040-001-A. OPS CK GOOD. RH/LH SPOILER 5 DO NOT DEPLOY. SPOILER LOCKED

Part: TRANSCEIVER — FAILED (WX RADAR SYS) · airframe 53,149 hrs · 24,430 cycles

WX RADAR HAD NO POWER INFLIGHT. ATTEMPTED SEVERAL RESETS W/ NO SUCCESS-FOUND CFDS MSG: WXR1(1SQ1) TROUBLE SHOT IAW TSM 34-1-00-810-802-A, REMOVED AND REPLACED WEATHER RADAR TRANSCEIVER IAW AMM 34-41-33. BITE TEST GOOD AT THIS TIME. A/C OK FOR SERVICE

Part: BUSHING — CORRODED (LT MLG) · airframe 53,015 hrs · 24,367 cycles

LEFT MLG RETRACTION JACK ACTUATOR BUSHING HAS CORROSION.-LMLG RETRACTION JACK FITTING ASSY REMOVED AND REPLACED ON HAECO SERVICE ORDER 122106 NON ROUTINE 24013. SDR CREATED

Part: BUSHING — CORRODED (RT MLG) · airframe 53,015 hrs · 24,367 cycles

RIGHT MLG RETRACTION JACK ACTUATOR BUSHING HAS CORROSION.-RTMLG RETRACTION JACK FITTING ASSY REMOVED AND REPLACED ON HAECO SERVICE ORDER 122106 NON ROUTINE 24014. SDR CREATED

Part: A/C PACK — ODOR (NR 2) · airframe 52,526 hrs · 24,153 cycles

FUME EVENT STRONG DIRTY SOCKS SMELL ON APPROACH TO LANDING. EVENT LASTED ABOUT 3 MINUTES-PERFORMED TSM 05-50-00-810-831 FOR CAUSE OF ODOR.RAN APU,PACKS, ENGINES. FOUND PACK 2 CAUSING ODOR.

Part: FRAME — CRACKED (FRM 20 S10-11R) · airframe 52,391 hrs · 24,090 cycles

CRACK FOUND AT FRAME 20 UPPER AT STR 10-11 RH. RAF-01 2720608-02 OPENED. REF TC 531155-02-2-R.-REPAIRED R1 DOOR FR2 DOUBLE JOGGLE AREA HOLES A , C + 8 AND ASSOCIATED HOLES IAW R531-13041, REV E AND RDAF 80911838/004/2021. CAT A REPAIR

Part: OIL SYSTEM — LOW · airframe 52,128 hrs · 23,978 cycles

ENROUTE WE HAD AN ADVISORY ON ECAM WARNING US OF LOW OIL LEVEL IT DROPPED TO 2.5 QTS ( OIL QUANTITY INDICATIONS )--

Part: ECS — CONTAMINATED (AC BAY) · airframe 51,783 hrs · 23,834 cycles

MUSTY SOCK / OIL FUME SMELL IN COCKPIT PACK 1 ISOLATED ODER REMOVED -TROUBLE SHOT IAW TSM 05-50-00 INSPECTED APU NO OIL LEAKS OR DEFECTS NOTED. PERFORMED DECONTAMINATION OF THE ECS IAW 21-00-00 REMOVED AND REPLACED PACK 1 RECIRCULATION FILTER IAW AMM 21-21-41 OPS CHECK GOOD NO FURTHER ODOR PRESENT

Part: FILTER — ODOR (AC BAY) · airframe 49,800 hrs · 22,991 cycles

"ON DESCENT THROUGH APPROX FL 200 NOTICED SMELL OF DIRTY SOX/SOUR MILK. PERFORMED FUME PRECEDURE, PACK 1 OFF, FUME DISAPPATED. PERFORMED PACK BURN IAW AMM 21-00-00. FILTERS REMAINS IN PACK # 1. BOTH RECIRCULATION FILTERS R&R IAW AMM 21-21-41. REF LOG OGES # 2547231-1, 2547233-2, 2547234-1 FOR REMOVAL AND REPLACEMENT OF # 1 PACK. OPS AND LEAK CHECK GOOD"

Part: SEAL — DAMAGED (ENGINE) · airframe 49,797 hrs · 22,990 cycles

1 AIR CONDITIONING SMELL DIRTY SOCKS PASSING FLIGHT LEVEL 290-PERFORM TSM 05-50-00-810-831-A AND IDENTIFY THE APU LEAKING OIL AND FOUND ENGINE # 1 AND ENGINE # 2 LEAKING OIL FROM DE-OILER SEAL. PERFORM ACTION ON LOG PAGE 2547222-1. PERFORM ACTION ON LOG PAGE 2547222-1. PERFORM FUEL BURN OUT IAW AMM 21-00-00. AIRCRAFT OK.

Part: UNKNOWN — ODOR (CABIN) · airframe 49,483 hrs · 22,847 cycles

FAS CONCERNED ABOUT POSSIBLE FUME EVENT IN AFT CABIN-PERFORMED OPS CHECK OF BOTH PACKS, NO ODOR REPRODUCED, NO ID OF CABIN ODODRS IAW TSM 05-50-00-810-831-A. A/C OK FOR SERVICE.

Part: ECS — CONTAMINATED (AC BAY) · airframe 47,774 hrs · 22,112 cycles

FUME EVENT THROUGH 8000'-REF LOG PGS 2480796-1; -2 FOR CORRECTIVE ACTIONS. ACCOMPLISHED ECS DECONTAMINATION IAW AMM 21-00-00 PB201 R&R RECIRCULATING FILTER IAW AMM 22-21-14 PB401. NO FURTHER FUMES NOTED AT THIS TIME. NR 1 & NR 2 ENG DEOILERS NO LEAKS NOTED.

Part: UNKNOWN — ODOR (CABIN) · airframe 45,265 hrs · 21,068 cycles

IN CRUISE AT FL350 FA REPORTS STRONG SMELL OF RUBBER/TIRE/HOT ELECTRICAL PACK 2 SELECT OFF SMELL DISIPATED. TROUBLESHOT IAW TSM 05-50-00-810-831-A. NO DEFECTS NOTED AT THIS TIME. REACTIVATED AND OPS CHECKED PACK NR 2 IAW AMM 21-51-00. OPS CHECK GOOD.

Part: STRUCTURE — GOUGED (NR 1 PYLON) · airframe 44,059 hrs · 20,548 cycles

GOUGE FOUND ON THE NR 1 PYLON RIBS 7 - 8. PERFORMED A DOUBLER REPAIR IAW TD 80432583, 005, 2018 A.

Part: BEAM — CORRODED (FRAME 68) · airframe 44,059 hrs · 20,548 cycles

DOOR SILL BEAM CORRODED FRAME 68, STRINGER 23L. EO 5341-1817 HAS BEEN ACCOMPLISHED.

Part: SEAL — LEAKING (DEOILER) · airframe 44,004 hrs · 20,524 cycles

DURING DESCENT THROUGH 10,000 FT. A DIRTY SOCKS ODOR BEGAN. FLIGHT ATTENDANT CALLED AND STATED THE SAME INDEPENDENT OF OUR DETECTION. AIRCRAFT CONFIG WAS PACK 1 ON, PACK 2 OFF, BLEED 1 ON, BLEED 2 ON, IAW TSM 05-50-00-810-831-A. FOUND DEOILER ON BOTH ENGINES HAD RESIDUAL OIL AROUND SEALS. R & R DEOILER SEALS ON THE ENGINES IAW AMM 72-60-31.. PERFORMED DECONTAMINATION OF ECS. NO FUMES DETECTED.

Part: SENSOR — LEAKING (APU OIL PRESSURE) · airframe 44,001 hrs · 20,523 cycles

DURING DESCENT, THE FA REPORTED A CHEMICAL, ROTTEN EGG ODOR IN THE MID CABIN AND AFT GALLEY AT AROUND 11000 FT. TURNED OFF THE NR 2 PACK, CROSS BLEED CONFIG, IAW TSM 05-50-00-710-080-A. ISOLATED THE ODOR TO THE NR 2 PACK. PERFORMED AN INSPECTION OF THE APU COMPARTMENT IAW AMM 49-00-00, FOUND OIL LEAKING FROM OIL PRESSURE SENSOR & OIL AROUND APU INLET. REMOVED & REPLACED OIL PRESSURE SENSOR IAW AMM 49-94-14, OPS & LEAK CHECKED GOOD, PERFORMED DECONTAMINATION OF THE ESC, NO DEFECTS NOTED IAW AMM 21-00-00.

Part: A/C PACK — CONTAMINATED (NR 2) · airframe 43,993 hrs · 20,520 cycles

DURING AN FA SAFETY CHECK, THE FA REPORTED A DIRTY SOCK ODOR. IAW TSM 05-50-810-831-A, PERFORMED A DECONTAMINATION OF THE ECS. ISOLATED EACH BLEED SOURCE INDIVIDUALLY. FOUND APU AND PACK NR 2 CONTAMINTED.

Part: ECS — CONTAMINATED (AC BAY) · airframe 43,824 hrs · 20,449 cycles

DURING DESCENT THE FA'S CALLED UP AND SAID ODOR OF DIRTY SOCKS WAS VERY STRONG. PILOTS DONNED MASK. ODOR DISSIPATED W/ PACK 2 OFF. PERFORM DECONTAMINATION OF ENVIRONMENTAL CONTROL SYSTEM IAW AMM 21-00-00. WENT THROUGH CABIN, NO SMELL NOTED. THIS CLEARS DMI 230768701. PLACARD REMOVED, MOC NOTIFIED.

Part: ECS — CONTAMINATED (AC BAY) · airframe 43,820 hrs · 20,446 cycles

DIRTY SOCK SMELL UPON ENTERING AIRCRAFT TURNED OFF NR 2 PACK AND SMELL WENT AWAY. PERFORMED DECONTAMINATION OF ENVIRONMENTAL CONTROL SYSTEM IAW AMM 21-00-00. WENT THROUGH CABIN, NO SMELL NOTED.

Part: SWITCH — LEAKING (APU) · airframe 43,343 hrs · 20,245 cycles

FUME EVENT DURING APPROACH. ODOR CLEARED WITH PACKS OFF AND RAM AIR OPEN. DURING PREP FOR ECS DECONTAMINATION, FOUND THE APU LOP SWITCH LEAKING AND OIL COATING THE INTAKE PLENUM. CLEANED OIL CONTAMINATION, AND R & R LOW OIL PRESSURE SWITCH IAW AMM 49-94-14. LEAK CHECKED GOOD.

Part: LINE — LOOSE (APU OIL TRANSFER) · airframe 42,683 hrs · 19,954 cycles

ODOR OF SWEATY FEET/SOCKS IN COCKPIT ON DESCENT. FOUND APU OIL TRANSFER TUBES LOOSE. RESECURED OIL TUBES AS REQ IAW AMM 49-21-00. LEAK CHECK GOOD. C/W DECONTAMINANT OF ECS AS REQ IAW AMM 21-00-00-615-002 & 21-00-615-004. NO SMELL DETECTED. REMOVED & REPLACED REARC FILTERS AS PRECAUTION IAW AMM 21-21-41.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 41,313 hrs · 19,361 cycles

LEFT INBD TE FLAP HAS A HOLE ,25MM X 25MM ON UPPER & LOWER SKINS & CORE. REPAIR IAW EO 5752-1728 AND SRM 57-52-00-300-016.

Part: SKIN — DENTED (FRAME 59) · airframe 41,313 hrs · 19,361 cycles

DENT FOUND AT FRAME 59 STRINGERS 5 - 6L, 74MM X 0.57MM. NO REPAIR.

Part: OXYGEN MASK — INOPERATIVE (COCKPIT) · airframe 40,977 hrs · 19,212 cycles

CAPTAIN`S OXYGEN MASK INOPERATIVE. R & R THE OXYGEN MASK, OPS CHECKED OK, NO LEAKS NOTED IAW 35-12-41.

Part: A/C PACK — ODOR (AC BAY) · airframe 39,816 hrs · 18,720 cycles

FUME EVENT THROUGH 16000 ON DESCENT. ENG 1 BLEED OFF, X-BLEED OPEN DUE TO HP VALVE DEFFERAL PER CREW CABIN ODOR REPORT SHEET, SMELL COMING FROM NR 2 ENG. PERFORMED ENG NR 2 PACK BURN OUT IAW AMM 21-00-00. NO ODOR SMELLED AT THIS TIME. OK FOR SVC.

Part: OXYGEN MASK — UNSECURE (CABIN) · airframe 39,272 hrs · 18,494 cycles

PAX O2 MASKS ROW 6 A,B,C FELL DOWN AGAIN. REPACK THE MASK PER AMM 35-21-43 PERFORMED DROP TEST PER AMM 35-23-00. OPS CHECKS OK.

Part: OXYGEN MASK — UNSECURE (CABIN) · airframe 39,272 hrs · 18,493 cycles

FWD LAV 02 MASKS DROPPED ENROUTE. PERFORMED OPERATIONAL CHECK OF O2 MASK DROPPING SYSTEM IAW AMM 35-23-00. OPS TEST GOOD. NO FURTHER DEFECTS NOTED.

Part: OXYGEN MASK — UNSECURE (CABIN) · airframe 39,261 hrs · 18,487 cycles

O2 MASKS IN ROW 6ABC DROPPED OUT. PERFORMED OPERATIONAL CHECK OF 02 MASK DROPPING SYSTEM IAW AMM 35-23-00. OPS CHECK GOOD. NO FURTHER DEFECTS FOUND.

Part: OXYGEN MASK — UNSECURE (CABIN) · airframe 39,238 hrs · 18,476 cycles

ROW 11 DEF O2 MASK MODULE OPENED ON LANDING. PERFORMED DROP CHECK IAW AMM 35-23-00. TEST OK.

Part: OXYGEN MASK — UNWANTED DEPLOY (ROW 26 ABC)

ROW 26 SEATS ABC OXYGEN MASKS DEPLOYED.

Part: OXYGEN MASK — BROKEN (COCKPIT)

F/O O2 MASK TAB BROKEN. REMOVED AND REPLACED FO'S O2 MASK IAW AMM 35-12-41. OPS AND LEAK CHECKS GOOD

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 37,391 hrs · 17,621 cycles

F/O FLASHLIGHT INOPERATIVE, R & R COCKPIT FLASHLIGHT IAW AMM 25-65-52-000-001-A/400-001-A.

Part: OXYGEN MASK — UNWANTED DEPLOY (ROW 5) · airframe 36,991 hrs · 17,442 cycles

ROW 5 ABC OXYGEN MASK DOOR OPEN. STOWED MASKS IAW AMM 35-21-43 AND PERFORMED TEST OF MANUAL MASK RELEASE IAW 35-23-00, TEST GOOD.

Part: FILTER — DIRTY (ZONE 200) · airframe 36,714 hrs · 17,314 cycles

DURING CLIMBOUT, COCKPIT CABIN ODOR, NOT VISABLE. ODOR, OILY TO COCKPIT, DIRTY SOCKS LAUNDRY TO CABIN. DISSAPATED IN CRUISE AND RETURNED, MORE SO IN DESCENT. O2 MASKS DONNED, ISOLATED TO PACK 2. PREFORMED STAGE 1 CLEANNING OF THE ECS PARA J REMOVED AND REPLACED RECIRC FILTERS IAW 21-00-00-860-077-B AND 21-21-41PB 401 NO OFFENSIVE ORDER AT THIS TIME

Part: OXYGEN MASK — UNWANTED DEPLOY (ROW 3 DEF) · airframe 34,289 hrs · 16,189 cycles

OXYGEN MASKS DEPLOYED ROW 3 DEF. PREFORMED OXYGEN MASK DROP TEST IAW AMM 35-21-41. OPS CHECKED GOOD.

Part: OXYGEN MASK — UNWANTED DEPLOY (ROW 5 ABC) · airframe 34,116 hrs · 16,104 cycles

UPON LANDING, O2 MASKS DROPPED IN ROW 5ABC. PERFORMED OPS CHECK OF MANUAL MASK. RELEASE ON SEAT/ROW 5A, 5B, 5C IAW AMM 35-23-00. OPS CK OK. NO DEFECTS NOTED.

Part: OXYGEN MASK — UNWANTED DEPLOY (ROW 3) · airframe 33,259 hrs · 15,708 cycles

ROW 3, ACFT RT SIDE OXYGEN MASK DEPLOYED ON LANDING. ACFT LANDING WAS NOT FIRM NOR ABNORMAL. STOWED O2 MASKS AT 3R AND PERFORMED DROP TEST IAW AMM 35-23-00 NO FURTHER DEFECTS NOTED.

Part: PCU — INOPERATIVE (ZONE 100) · airframe 31,900 hrs · 15,110 cycles

DURING APPROACH 0 FLAP FULL SLAT FLGHT CONTROL FLAPS FAULT LANDING NORMAL DECLARED EMERGENCY. PERFORMED TROUBLESHOOTING IAW TSM 27-51-00-810-810-A FOUND YELLOW SYSTEM PCU MOTOR INOPERATIVE R & R PCU IAW AMM 27-54-51 PB 401. PERFORMED OPS AND LEAK CHECK IAW AMM 27-54-00-710-001-A, NO DEFECTS NOTED AT THIS TIME.

Part: GROUND WIRE — BROKEN (OXYGEN MASK) · airframe 31,530 hrs · 14,942 cycles

OXYGEN MASK GROUND WIRE BROKEN. R & R OBSERVERS OXYGEN MASK IAW CMM 35-13-60. OPS CHECKED GOOD.

Part: DOOR — FAULTED (EMERGENCY EXIT) · airframe 30,651 hrs · 14,535 cycles

LEFT EMERGENCY OVERWING EXIT ECAM CAME ON WHEN COVER COMING OUT OF POSITION TO LAMPS FAULTING OUT OF POSITION. VERIFIED INSTALLATION O/H LT EMERGENCY EXIT COVER FLAP IAW AMM 52-21-11 DOOR INDICATION NORMAL, OK FOR SERVICE.

Part: PROXIMITY SWITCH — INOPERATIVE (RT OVERWING) · airframe 30,282 hrs · 14,363 cycles

RT OVERWING SLIDE INDICATION ON DOOR, SOMETIMES SHOWS SLIDE NOT ARMED IN FLIGHT. R & R RT WINE EMERGENCY EXIT HATCH PROXIMITY SWITCH IAW AMM 52-71-13, OPS CHECKED NORMAL.

Part: OXYGEN MASK — UNWANTED DEPLOY (ROW 8) · airframe 29,708 hrs · 14,082 cycles

OXYGEN MASK ROW 8 DROPPED. STOWED OXYGEN MASK IAW AMM 35-21-41-400-001-A, DROP CHECKED GOOD IAW AMM 35-23-00-710-001-A.

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 29,563 hrs · 14,014 cycles

SEAT ROW 3 RT OXYGEN MASK DROPPED. REPACKED MASK AND ACCOMPLISHED DROP CHECK OF OXYGEN MASK IAW AMM 35-23-00-710-001. OPS CK GOOD.

Part: DOOR — OUT OF POSITION (ZONE 800) · airframe 28,995 hrs · 13,784 cycles

SLIDE ARMED INDICATION FLASHING ON & OFF OVERWING DOOR RIGHT. REMOVED AND REINSTALLED DOOR IAW AMM 52-21-11, PB 401, SLIDE ARM INDICATES STEADY. NO DISCREPANCY NOTED AT THIS TIME.

Part: SEAT TRACK — CORRODED (FRAMES 64-66) · airframe 28,950 hrs · 13,768 cycles

CORROSION FOUND ON TOP OF SEAT TRACK BETWEEN FRAMES 64-66. R & R SEAT TRACK IAW SRM 51-42-11 AND SRM 52-72-0.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 28,950 hrs · 13,768 cycles

CORROSION FOUND ON SEAT TRACK 6 IN FWD OF FRAME 66. R & R SEAT TRACK IAW SRM 51-42-11 AND SRM 52-72-0.

Part: DOOR SEAL — UNKNOWN (OVERWING EXIT) · airframe 28,370 hrs · 13,526 cycles

F/A REPORT OVERWING EXIT, ACFT LEFT VERY NOISEY AND FOGGED OVER DURING FLT. PERFORMED GENERAL VISUAL INSPECTION OF LEFT OVERWING EXIT DOOR AND PRESSURE ACFT IAW AMM. NO FAULTS NOTED. OK FOR SERVICE.

Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT ROW 6 DEF) · airframe 28,322 hrs · 13,506 cycles

SEAT ROW 6 DEF OXYGEN MASKS FELL. STOWED MASKS IN CONTAINER IAW AMM. OPS CHECKED GOOD IAW AMM.

Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT 10ABC) · airframe 28,293 hrs · 13,494 cycles

PAX OXYGEN MASK OVER 10 ABC DROPPED. PERFORMED OPS CHECK OF MANUAL MASK RELEASE IAW AMM. OPS CHECKED GOOD.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 28,293 hrs · 13,494 cycles

DURING CHECK OF EMERGENCY LIGHT BATTERY CAPACITY, FOUND EPSU FAULT AT FIN 12WL RT OVERWING ESCAPE. R & R EPSU AT LOCATION FIN 12WL IAW AMM. OPS CHECKED GOOD.

Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT ROW 23DEF) · airframe 28,167 hrs · 13,439 cycles

ROW 23DEF , OXYGEN MASK FELL. RESTOWED OXYGEN MASK IAW AMM.

Part: SEAL — DIRTY (EMERGENCY EXIT) · airframe 27,603 hrs · 13,215 cycles

AIR LEAKING SOUND COMING FROM LT OVERWING EMERGENCY EXIT. REMOVED LT OVERWING EXIT, FOUND DEBRIS, CLEANED IAW AMM AND INSTALLED OVERWING EXIT IAW AMM. NO DEFECTS NOTED.

Part: COVER — UNSECURE (EMERGENCY EXIT) · airframe 27,390 hrs · 13,118 cycles

ECAM "DOOR RT EMERGENCY EXIT" DURING CLIMBOUT, PRESSURIZATION NORMAL. FOUND RT PAX EMERGENCY EXIT DOOR COVER FLAP LOOSE. SECURED COVER FLAP REF AMM 52-21-00. OK FOR CONTINUED SERVICE.

Part: CABLE — MISROUTED (ESCAPE SLIDE) · airframe 27,336 hrs · 13,098 cycles

FWD RT ESCAPE SLIDE DEPLOYMENT CABLE MISROUTED AND FRAYED. R & R FWD RT ESCAPE SLIDE ASSY IAW 319 25-62-44. OK FOR SERVICE. WORK C/W ON NON ROUTINE.

Part: SHEAR PIN — MISINSTALLED (PAX DOOR) · airframe 27,336 hrs · 13,098 cycles

FWD RT DOOR SHEAR PIN INSTALLED WRONG ON PERCUSSION MECHANISM. R & R SHEAR PIN IAW 52-10-00-610-001A. OK FOR SERVICE.

Part: COVER — UNSECURE (ZONE 800) · airframe 27,134 hrs · 12,998 cycles

COVER OVER RT WING EMERGENCY EXIT WAS FALLING OFF DURING FLIGHT CAUSING A " RT EMER EXIT DOOR" ECAM. INSTALLED COVER FLAP RT OVERWING DOOR IAW AMM 52-21-11-410-059-D. ALL INDICATIONS, NORMAL.

Part: COVER — MISINSTALLED (EMERGENCY EXIT) · airframe 26,676 hrs · 12,792 cycles

EMERGENCY EXIT WINDOW, ON ACFT RT SIDE SLIDE INDICATOR INTERMITTENT DURING FLIGHT. INSTALLED RT EMERGENCY EXIT DOOR HANDLE COVER IAW AMM. INDICATION NORMAL AT THIS TIME.

Part: OXYGEN MASK — INOPERATIVE (COCKPIT) · airframe 26,522 hrs · 12,717 cycles

F/O O2 MASK INOPERATIVE. PERFORMED OPS TEST OF THE FULL FACE/QUICK DONNING O2 MASK IAW AMM. OPS CHECKED GOOD.

Part: LIFE VEST — MISSING (SEAT 26C) · airframe 26,055 hrs · 12,495 cycles

LIFE VEST AT SEAT 26C MISSING. INSTALLED LIFE VEST IAW DWGS.

Part: CONNECTOR — DIRTY (SLIDE) · airframe 24,896 hrs · 11,937 cycles

EMERGENCY EXIT SLIDE INDICATOR IS INTERMITTENT SHOWING WINDOW EXIT DISARM. CLEANED CONTACT AND PROXIMITY SWITCH ON ARMING FLAP AND CHECKED GAP. PERFORMED OPS CHECKED IAW MM. OPS OK.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 24,179 hrs · 11,611 cycles

EPSU 12WL FAILED CAPACITY TEST CLASS 1. R & R EPSU 12WL WITH A SERVICEABLE UNIT IAW MM.

Part: INDICATION SYS — MALFUNCTIONED (DOOR ARMING) · airframe 22,082 hrs · 10,578 cycles

R1 DOOR DOES NOT INDICATE "ARMED" ON F/A PANEL OR SYS PAGE WHEN DOOR IS ARMED. PERFORMED OPS TEST OF THE DOOR WARNING SYS IAW AMM 52-71-00-710-001-A, OPS TESTED NORMAL.

Part: LIGHT — DAMAGED (CABIN) · airframe 21,818 hrs · 10,444 cycles

DAMAGED EMERERGENCY ESCAPE LIGHT STRIP IN CABIN ON RT FWD. R & R EMERGENCY LIGHT IAW AMM 33-51-21-400-001-A.

Part: CYLINDER — DEACTIVATED (DOOR ASSIST) · airframe 21,729 hrs · 10,392 cycles

PAX DOOR ASSIST BOTTLE DEACTIVATED. REACTIVATED PAX CABIN DOOR OPENING ASSIST BOTTLE IAW AMM TASK 52-10-00-860-00-002-A, PAR 4.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,729 hrs · 10,392 cycles

PAX CABIN BETWEEN FR69 AND FR70 +X125 FLOOR CHANNEL WITH CORROSION. DAMAGED PART WAS REPLACED IAW THE SRM 51-72-11, UNDER THE NON ROUTINE ITEM.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,729 hrs · 10,392 cycles

PAX CABIN BETWEEN FR69 TO FR70 +Y160.5 MM FLOORBEAM WITH CORROSION. THE FLOORBEAM WAS REPLACED IAW SRM 51-72-11, PARA 1 THRU 6.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 21,729 hrs · 10,392 cycles

PAX CABIN BETWEEN FR69 AND FR70 -Y1250MM FLOOR SUPPORT WITH CRACK. DAMAGED PART WAS REPLACED IAW THE SRM 51-72-11, UNDER THE NON ROUTINE ITEM.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 21,729 hrs · 10,392 cycles

LOWER FUSELAGE AFT CARGO COMPARTMENT, FLOOR SUPPORT FITTING WITH CORROSION FROM FR58 TO FR59 AT STRINGER 38LH. DAMAGED PART WAS REPLACED IAW SRM 51-72-11, UNDER THE NON ROUTINE ITEM.

Part: ANCHOR FITTING — CORRODED (ZONE 600) · airframe 21,729 hrs · 10,392 cycles

RT WING, MLG RETRACTION ANCHOR ACTUATOR FITTING WITH CORROSION. DAMAGE PART WAS REPAIRED IAW AIRBUS REPAIR INSTRUCTIONS 70562772/011, DTD MAY 23, 2012 AND TD J1-S2 19995 2012 ISSUE A.

Part: ANCHOR FITTING — CORRODED (ZONE 500) · airframe 21,729 hrs · 10,392 cycles

LOWER FUSELAGE LT MLG RETRACTION ANCHORAGE ACTUATOR FITTING WITH CORROSION. DAMAGED PART WAS REPAIRED FOLLOWING REPAIR INSTRUCTIONS 70562772/011 DTD MAY 23, 2012 AND TD J1 S2 19995 2012 ISSUE A.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 21,155 hrs · 10,120 cycles

L1 DOOR ASSIST BOTTLE LOW. SERVICED L1 DOOR ASSIST BOTTLE IAW AMM 52-10-00-614-001.

Part: CYLINDER — LOW PRESSURE (R1 DOOR ASSIST) · airframe 18,986 hrs · 9,056 cycles

R1 DOOR ASSIST BOTTLE HAS LOW PRESSURE. SERVICED DOOR ASSIST BOTTLE TO PROPER RANGE IAW AMM 52-10-00-614-001.

Part: CYLINDER — LOW PRESSURE (L1 DOOR ASSIST) · airframe 18,858 hrs · 8,990 cycles

L1 DOOR ASSIST DAMPER PRESSURE LOW. SERVICED L1 DOOR ASSIST DAMPER TO PROPER PRESSURE IAW AMM 523-10-00-614-001.

Part: CYLINDER — LOW PRESSURE (R1 DOOR) · airframe 18,563 hrs · 8,831 cycles

R1 DOOR ASSIST CYLINDER ACTUATED DURING SLIDE CHANGE. REPLACED DIAPHRAGM AND SERVICED DOOR DAMPER CYLINDER RESERVOIR IAW AMM 52-10-00-610-001. NO FURTHER DEFECTS NOTED.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,754 hrs · 7,537 cycles

PAX CABIN, UPPER REAR FUSELAGE, AFT SERVICE AREA, FROM STA 2799 TO STA 2870 -Y116 FLOOR STRUCTURE BEAM CORRODED (BEAM PN: D5347218920400) NOTE: THE CORROSON REQUIRE MAJOR REPAIR.

Part: PANEL — CORRODED (NR 1 NACELLE) · corrosion level 2 · airframe 15,754 hrs · 7,537 cycles

ENGINE NR1, PYLON AFT FIXED FAIRING, OTBD/LT LATERAL SKIN PANEL WITH CORROSION (PANEL PN: D5453005220300) THE CORROSION REQUIRES A MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,754 hrs · 7,537 cycles

PAX CABIN, UPPER REAR FUSELAGE, AFT SERVICE AREA, FROM STA 2799 TO STA 2870 -Y129 FLOOR STRUCTURE BEAM CORRODED. CORROSION REQUIRES A MAJOR REPAIR.

Part: PANEL — CORRODED (NR 1 NACELLE) · corrosion level 2 · airframe 15,754 hrs · 7,537 cycles

ENGINE NR 1, PYLON AFT FIXED FAIRING, INBD/RH LATERAL SKIN PANEL WITH CORROSION (PANEL PN: D5453005220300) NOTE: THE CORROSION REQUIRES A MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,754 hrs · 7,537 cycles

PAX CABIN, UPPER REAR FUSELAGE, AFT SERVICE AREA, FRO STA 2799 TO STA 2870 -Y116 FLOOR STRUCTURE BEAM CORRODED. CORROSION REQUIRES MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,754 hrs · 7,537 cycles

PAX CABIN, UPPER REAR FUSELAGE, AFT SERVICE AREA, FROM STA 2799 TO STA 2870 -Y129 FLOOR STRUCTURE BEAM CORRODED (BEAM PN D5347217220500) NOTE: THE CORROSION REQUIRES A MAJOR REPAIR).

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,754 hrs · 7,537 cycles

(EE4Y) PAX CABIN, UPPER REAR FUSELAGE, AFT SERVICE AREA FROM STA 2799 TO STA 2884, +76.5 FLOOR SUPPORT STRUCTURE BEAM CORRODED (BEAM PN: D5347219220000) NOTE: THE CORROSION REQUIRES A MAJOR REPAIR.

Part: BUMPER BLOCK — WORN (THRUST REVERSER) · airframe 15,754 hrs · 7,537 cycles

(EE4Y) ENGINE NR1, OTBD/LT THRUST REVERSE C-DUCT, PAN-DOWN ENGINE BUMPER WITH WEAR. THE WEAR REQUIRES A MAJOR REPAIR.

Part: BUMPER BLOCK — WORN (THRUST REVERSER) · airframe 15,754 hrs · 7,537 cycles

(EE4Y) ENG NR2, INBD/ LT THRUST REVERSE C-DUCT, PAN-DOWN ENGINE BUMPER WITH WEAR. THE WEAR REQUIRES A MAJOR REPAIR.

Part: PANEL — CORRODED (NR 2 NACELLE) · corrosion level 2 · airframe 15,754 hrs · 7,537 cycles

ENGINE NR 2, PYLON AFT FIXED FAIRING, INBD/LT LATERAL SKIN PANEL WITH CORROSION (PANEL PN: D5453005220200) THE CORROSION REQUIRES A MAJOR REPAIR.

Part: PANEL — CORRODED (NR 2 NACELLE) · corrosion level 2 · airframe 15,754 hrs · 7,537 cycles

ENGINE NR 2, PYLON AFT FIXED FAIRING, OTBD/RT LATERAL SKIN PANEL WITH CORROSION, (PANEL PN: D54530052220300) THE CORROSION REQUIRES A MAJOR REPAIR.

Part: BUMPER BLOCK — WORN (THRUST REVERSER) · airframe 15,754 hrs · 7,537 cycles

(EE4Y)ENGINE NR2, OTBD/RT THRUST REVERSE C-DUCT, PAN DOWN ENGINE BUMPER WITH WEAR. THE BUMPER WEAR REQUIRES A MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,754 hrs · 7,537 cycles

PAX CABIN, UPPER REAR FUSELAGE, AFT SERVICE AREA AT STA 2884 -Y76.5 FLOOR SUPPORT STRUCTURE BEAM CORRODED (BEAM PN: D5347219320000) THE CORROSION REQUIRES A MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,754 hrs · 7,537 cycles

PAX CABIN, UPPER REAR FUSELAGE, AFT SERVICE AREA, FROM STA 2936 TO STA 2992 +Y160.5 FLOOR STRUCTURE BEAM CORRODED (BEAM PN: D5347219620000) NOTE: THE CORROSION REQUIRES A MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,754 hrs · 7,537 cycles

PAX CABIN, UPPER REAR FUSELAGE, AFT SERVICE AREA, FROM STA 2936 TO STA 2992 +Y160.5 FLOOR STRUCTURE BEAM CORRODED (BEAM PN: D5347219620000) NOTE: THE CORROSION REQUIRES A MAJOR REPAIR.

Part: BUMPER BLOCK — WORN (THRUST REVERSER) · airframe 15,754 hrs · 7,537 cycles

(EE4Y) ENGINE NR1, INBD/RT THRUST REVERSE C-DUCT, PAN-DOWN ENGINE BUMPER WITH WEAR. THE WEAR REQUIRES A MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,754 hrs · 7,537 cycles

PAX CABIN, UPPER REAR FUSELAGE, AFT SERVICE AREA AT STA 2884 -Y76.5 FLOOR SUPPORT STRUCTURE BEAM CORRODED. CORROSION REQUIRES A MAJOR REPAIR.

Part: CONTROL PANEL — FAILED (WX RADAR SYS) · airframe 14,190 hrs · 6,794 cycles

WEATHER RADAR FAILED. R & R RADAR CONTROL PANEL.