N348NB

Part: DOOR — LEAKING (ZONE 800) · airframe 60,037 hrs · 30,769 cycles

LEFT MID CABIN EMERGENCY DOOR HISSING IN FLIGHT. REMOVED AND INSTALLED LT EMERGENCY HATCH DOOR AND INSPECTED SEAL IAW AMM 52-21-11. (1334540).

Part: SHAFT — SHEARED (HYD PUMP) · airframe 59,930 hrs · 30,706 cycles

SHIP 3148 - DIV - TO PIT DUE TO LOSS OF THE GREEN SYSTEM HYDRAULIC PRESSURE. FOUND LT ENGINE HYDRAULIC PUMP SHAFT SHEARED. REPLACED LT ENGINE PUMP AND PTU. (LP 8013960, 8013958)

Part: STRUCTURE — DAMAGED (ZONE 900) · airframe 59,769 hrs · 30,609 cycles

FOUND FWD GALLEY LAMINATE COSMETICALLY DAMAGED. R & R FWD GALLEY HAND SANITIZER LAMINATE PER A319 AMM 25-31. (1272551).

Part: HOSE — LEAKING (OXYGEN MASK) · airframe 59,508 hrs · 30,472 cycles

OXYGEN LEAK ON FO'S MASK FOUND DURING TEAT. RESECURED HOSE PER A319 AMM 35-19. (7885844).

Part: STRUCTURE — DAMAGED (ZONE 200) · airframe 59,301 hrs · 30,347 cycles

FOUND FWD GALLEY LAMINATE COSMETICALLY DAMAGED. REPLACED LAMINATE IN FWD GALLEY PER A319 AMM 25-31. (1176012).

Part: WINDOW — DISTORTED (ZONE 200) · airframe 58,678 hrs · 29,996 cycles

SHIP 3148 THE WINDSCREEN IN THE AIR AT ALTITUDE DISTORTED HAS APPROXIMATELY 5 PIN HOLES IN IT ALSO IT IS IN THE FIELD OF VIEW OF FIRST OFFICER. CORRECTIVE ACTION: R/R R1 WINDSHIELD PER A319 AMM 56-11-11-000-001-A. (7194610)

Part: STRUCTURE — DAMAGED (ZONE 200) · airframe 57,979 hrs · 29,627 cycles

SHIP 3148 DISC: DTE, ER/A 620540-14AD REV A REQUIRES STAGE 3 DTA APPROVAL. A319 / 3148 / FUSELAGE / FRAMES/FORMERS / FR68 & STR22R / FRAME & SKIN / OVZ HOLE. C/A: ER/A 620540-14AD REV A REQUIRES STAGE 3 DTA APPROVAL ON OR BEFOR E 60,000 FC FROM SECTION I REPAIR EMBODIMENT. ASSOCIATED ER/A 00-620540 ADDED FOR AC 3148. (LP: 0852392)

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 57,979 hrs · 29,627 cycles

SHIP 3148 CRACK INDICATION WAS FOUND AT THE LOWER INB HOLE AT FR68RH, DOOR STOP FITTING 1 LEVEL. CORRECTIVE ACTION: COMPLIED WITH ER/A 620540-14AD. (0852386)

Part: UNKNOWN — ODOR (CABIN) · airframe 57,923 hrs · 29,596 cycles

SHIP 3148 DISC: ODER IN FRONT LAVE "DIRTY SOCK SMELL" DURING FLIGHT LASTED ABOUT 10 MIN - DISAPATED NO FURTHER EVENT. C/A: REFERENCE LOG PAGE 0840850 FOR CORRECTIVE ACTIONS. (LP: 6781799)

Part: RADOME — DELAMINATED (ZONE 100) · airframe 57,608 hrs · 29,433 cycles

SHIP 3148 FOUND NOSE RADOME INTERIOR DELAMINATED. CORRECTIVE ACTION: REPLACED RADOME PER A319 AMM 53-52. (6409219)

Part: SKIN — DAMAGED (ZONE 500) · airframe 56,899 hrs · 29,056 cycles

SHIP 3148 LH WING BOTTOM SKIN PANEL #3 WAS INADVERTENTLY DAMAGED. CORRECTIVE ACTION: COMPLIED WITH ER/A 568357-14. (0611151)

Part: SKIN — GROUND DAMAGE (ZONE 500) · airframe 56,899 hrs · 29,056 cycles

SHIP 3148 LH WING BOTTOM SKIN PANEL #3 WAS INADVERTENTLY DAMAGED. CORRECTIVE ACTION: COMPLIED WITH ER/A 568357-14. (0611142)

Part: OIL SYSTEM — LEAKING (APU) · airframe 56,819 hrs · 29,011 cycles

SHIP 3158 DITY SOCK SMELL FROM PACKS. CORRECTIVE ACTION: PERFORMED CK OUT PER A319 AMDS TASK CARD 0550-2002 SUSPECT APU INTERNAL LEAK. NO OIL LEAK IN ENGINES. PERFORMED DECONTAMINATION PER AMDS CARD 2100-2007. (4545471)

Part: CROSSBEAM — DAMAGED (ZONE 200) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 ELONGATE HOLES (5 EA) ON CROSSBEAM LOC. FR66 AT -Y1292 AFT GALLEY AREA. CORRECTIVE ACTION: REPAIRED PER ER/A 620041-14. (0584769)

Part: WINDOW POST — CRACKED (ZONE 200) · airframe 56,807 hrs · 29,004 cycles

SHIP 3148 RH FRONT WINDSHIELD - LOWER CENTER POST RADIOUS CRACK. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON FRONT WINDSHIELD AREA AS PER ER/A 581650-14AD. (0584728)

Part: HOUSING — CORRODED (ZONE 500 FLAP) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION ON O/B FLAP BEARING HOUSING LOC. AT FLAP TRACK 4 O/B FLAP L /H WING. CORRECTIVE ACTION: REPAIRED PER ER/A 620435-14. (0584599)

Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION UPPER SKIN LOWER SURFACE TRAILING EDGE OVERHANG AREA AT LEVE L RIB 15 ON RH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 619616-14. (0584629)

Part: SUPPORT — CORRODED (ZONE 500 FLAP) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION FOUND ON OUTB'D AND INB'D BORES OF PENDULUM SUPPORT ASSY AT FLAP TRACK 4 LEVEL OF OUTB'D FLAP, LH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 620435-14. (0582928)

Part: WINDOW POST — CRACKED (ZONE 200) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CRACK FOUND ON RH EINDSCHIELD CENTER POST LOWER ATTACHMENT AREA, PERFORM ER/A 619593-14AD. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS, MATCHES WITH ALL STEPS ON ER/A 619593-14. (0583471)

Part: ELEC CONNECTOR — CORRODED (ZONE 500) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION ON ELECTRICAL CONNECTOR INTERCONNEC TING STRUT ON LH WING. CORRECTIVE ACTION: REPLACED ELECTRICAL CONNECTOR FIN: 7543VC AT AREA FLAP INTERCONNECTING STRUT ON LH WING AS PER A320 FAM AMM 27-51-44- 000-001-A AND AMM 27-51-44-400-001-A. (0583192)

Part: ACCESS PANEL — CRACKED (ZONE 300) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CRACK ACCESS PANEL 342AB ON RH HORIZONTAL STABILIZER. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON ACCESS PANEL 342AB HORIZONTAL STABILIZER AS PER ER/A 620592-14 REV. (0581239)

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION CENTER FITTING LOCATED BETWEEN FRAME 16 TO FRAME 20 AND STRINGER 23 LEFT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED CENTER FITTING LOCATED BETWEEN FRAME 16 TO FRAME 20 AND STRINGER 23 LEFT FWD GALLEY AREA AS PER A319 SRM 51-72-11. (0581489)

Part: SUPPORT WEB — CRACKED (ZONE 100) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CRACK SUPPORT WEB BELLY FAIRING LOC. FR 52 LH AT LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON SUPPORT WEB BELLY FAIRING LOC. AT FR 52 LH AT LOWER FUSELAGE AS PER ER/A 620006-14. (0581436)

Part: SKIN — CRACKED (ZONE 800) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CRACK INDICATION FOUND ON AFT CARGO COMPARTMENT DOOR SKIN. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON AFT CARGO COMPARTMENT DOOR SKIN PIANO THE HINGE FITTING AT HOLE # 13, AS PER ER/A 619781-14AD.

Part: SKIN — CORRODED (ZONE 500) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION WAS FOUND IN TOP SKIN PANEL 2, TRAILING EDGE OVERHANG AREA, LH WING. CORRECTIVE ACTION: REPAIRED PER SECTION II OF 619615-14. (0581147)

Part: SKIN — CORRODED (ZONE 600) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION WAS FOUND ON TOP SKIN PANEL 2, TRAILING EDGE OVERHANG AREA, ON THE RH WING. CORRECTIVE ACTION: REPAIRED PER SECTION II OF ER/A 619616-14.

Part: SKIN — CORRODED (ZONE 500) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION WAS FOUND IN TOP SKIN PANEL 2, TRAILING EDGE OVERHANG LH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 619615-14. (0581168)

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 MACHINE SEAT TRACK Y1292 LOCATED FR64 TO FR66 AT AFT GALLEY AREA DAMAGED. CORRECTIVE ACTION: COMPLIED WITH ER/A # 619814-14 REV. (0581615)

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 DAMAGED SEAT TRACK -Y1292 LOC. FR64 TO FR66 AT AFT GALLEY AREA DAMAGED. CORRECTIVE ACTION: COMPLIED WITH ER/A # 620097-14. (0581640)

Part: HOUSING — CORRODED (FRAP BEARING) · airframe 56,807 hrs · 29,004 cycles

SHIP 3148 CORROSION ON I/B FLAP BEARING HOUSING LOC. AT FLAP TRACK 3 O/B FLAP R /H WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 620418-14. (0581553)

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 SEAT TRACK -Y765 LOC. FROM FR64 TO FR66 AFT GALLEY AREA DAMAGED. CORRECTIVE ACTION: REPAIRED PER ER/A 619939-14. (0581629)

Part: WEB — CORRODED (ZONE 100) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION ON WEB LOCATED BETWEEN FRAME 69 TO FRAME 70 AND STRINGER 23 RIGHT AT AFT GALLEY AREA. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON WEB LOCATED BTW FRAME 69 TO FRAME 70 AND STRINGER 23 RIGHT AT AFT GALLEY AREA AS PER ER/A 620567-14 REV. (0579922)

Part: REINFORCEMENT — CORRODED (ZONE 500) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION LOWER SURFACE ON PYLON REINFORCING PLATE LOC. AT RIB8 AT LEVEL STR 5 ON LH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON BOTTOM SKIN PYLON REINFORCING PLATE AT RIB 8 AND STR 5, LH SIDE AS PER ER/A 620045-14AD REV. (0579898)

Part: FRAME — CORRODED (ZONE 100) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION FRAME 20 AT LEVEL STRINGER 23 RIGHT FWD GALLEY AREA. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON FRAME 20 AS PER ER/A 620187-14. (0579927)

Part: FRAME — CRACKED (ZONE 100) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CRACK INDICATION FOUND AT HOLE 4 HOLE. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON FR 68 ON STR 22R AT HOLE 4 LOWER INBOARD POSITION LOCATED AT DOOR STOP FITTING 1 AS PER ER/A 620540-14AD. (0579914)

Part: PLATE — CORRODED (LT PYLON) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION WAS FOUND IN PYLON REINFORCING PLATE IN BOTTOM SKIN AT RIB AND STR 5 ON LH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 620045-14. (0578017)

Part: CROSSBEAM — DAMAGED (ZONE 200) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 ELONGATED HOLES WERE FOUND COMMON TO THE UPPER FLANGE OF CROSS BEAM AT FR66 AND -Y765 AND -Y1292. CORRECTIVE ACTION: REPAIRED PER ER/A 620041-14. (0577843)

Part: BONDING PLATE — DEBONDED (LT FLAP TRACK) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 DEBONDED BONDING PLATE FLAP TRACK FAIRING 2 (531CB) ON LH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON FLAP TRACK FAIRING 531CB AS PER ER/A 620004-14. (0575552)

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION SHEAR TIE LOCATED FR29 BETWEEN STR41R TO STR42R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE AND FASTENERS LOC. FR29 BETWEEN STR41R TO STR42R IN FWD CARGO COMPARTMENT AS PER A319 SRM 51-72-11 AND A319 SRM 51-42-11. (0575520)

Part: BONDING PLATE — CORRODED (RT FLAP TRACK) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION BONDING PLATE FLAP TRACK FAIRING 632CB ON RH WING. CORRECTIVE ACTION: ER/A 620004-14. (0575544)

Part: BONDING PLATE — CORRODED (FLAP TRACK) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION BONDING PLATE FLAP TRACK FAIRING 3 (532CB) ON LH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON FLAP TRACK FAIRING 532CB AS PER ER/A 620004-14. (0575537)

Part: WEB — MECHANIC ERROR (ZONE 100) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 MIS DRILL ON VERTICAL WEB LOCATED BTW FR 57 TO FR 58 AT LEVEL STR 41R AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED VERTICAL WEB LOCATED BTW FR 57 TO FR 58 AT LEVEL STR 41R AFT CARGO COMPARTMENT AS PER A319 SRM 51-72-11 AND INSTALLED FASTENERS AS PER A319 SRM. (0573857)

Part: BEARING — EXCESS PLAY (RUDDER HING ARM) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 EXCESSIVE PLAY ON RUDDER HINGE ARM NUMBER 6 BEARING. CORRECTIVE ACTION: REPLACED RUDDER HINGE ARM NUMBER 6 BEARING AS PER A320 FAM AMM 55-46-11-000-001-A AND AS PER A320 FAM AMM 55-46-11-400-001-A. (0573812)

Part: SKIN — CRACKED (CARGO DOOR) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CRACK INDICATION FOUND IN HOLE 13 OF THE AFT CARGO DOOR SKIN AT PIANO HINGE FITTING. CORRECTIVE ACTION: REPAIRED PER ER/A 619781-14. (0574138)

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION WEB FRAME 20 AT S-23LH FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED WEB LOCATED FR20 TO FR24 BTW STRG 23 LH AS PER A319 SRM 51-42-11-801 AND A319 SRM 51-72-11-911-001. (0573875)

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CRACK INDICATION FOUND AT LWR INB'D HOLE AT FR68 RH, AT DOORSTOP FTG #1 LEVEL. CORRECTIVE ACTION: REPAIRED PER ER/A 620540-14. (0572526)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION SEAT TRACK -Y765 LOCATED FROM FR 64 TO FR66 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED SEAT TRACK -Y765 LOCATED FROM FR 64 TO FR66 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (0572195)

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION FLOOR BEAM +Y765 FROM FRAME 66 TO FRAME 70 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM Y765 LOC. FRAME 66 TO FRAME 70 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11-801 AND SRM 51-72-11-911-001. (0568559)

Part: FLAP TRACK — CORRODED (ZONE 600) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 RH WING INB'D FLAP TRACK #2 / ATTCHT BEARING AT RIB 9 CORROSION. CORRECTIVE ACTION: REPAIRED PER ER/A 620272-14. (0568620)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION SEAT TRACK +Y1292 AT FR66 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED SEAT TRACK Y1292 FROM FR64 TO FR66 AT AFT GALLEY AREA AS PER A319 SRM 51-72-11-911-001. (0569053)

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION ON FITTING LOC. FLOOR BEAM Y1162.5 FR69. CORRECTIVE ACTION: REPLACED FITTING LOC. FLOOR BEAM Y1162.5 FR69 AFT GALLEY AREA AS PER A319 SRM 51-42-11. (0569055)

Part: FRAME — GOUGED (ZONE 200) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 GOUGE ON SECTION FRAME 70 AT FORWARD FACE OF THE REAR PRESSURE BULKHEA D LEFT SIDE ON AFT GALLEY AREA. CORRECTIVE ACTION: REPAIRED PER ER/A 619976-14. (0568568)

Part: BUSHING — CORRODED (RT FLAP TRACK) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION ON BUSHING (2 E/A) ON FLAP DRIVE ARM TRACK 4 ON O/B FLAP R/ H WING. CORRECTIVE ACTION: REPAIRED PER ER/A 620350-14. (0569072)

Part: FRAME — GOUGED (ZONE 200) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 GOUGE ON SECTION FRAME 70 AT FORWARD FACE OF THE REAR PRESSURE BULKHEAD LEFT SIDE ON AFT GALLEY AREA. CORRECTIVE ACTION: REPAIRED PER ER/A 619976-14. (0569050)

Part: CONNECTOR — CORRODED (ZONE 600) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION ON CONNECTORS 75 42VC AND 7540VC OF INTERCONNECTING STRUT INBOARD FLAP ON RH WING. CORRECTIVE ACTION: REPLACED CONNECTORS 7542VC AND 7540VC OF INTERCONNECTING STRUT INBOARD FLAP ON RH WING AS PER A320 FAM ESPM-20-44-11. (0569139)

Part: FLOOR PANEL — CORRODED (ZONE 200) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION ON INSERTS FLOOR PANEL IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR PANEL IN PASSENGER CABIN WITH NEW REPLACEMENT MATERIAL AS PER A319 SRM 53-02-00-300-011. (0567220)

Part: FLOOR PANEL — CORRODED (ZONE 200) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION ON INSERTS FLOOR PANEL IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR PANEL IN PASSENGER CABIN WITH NEW REPLACEMENT MATERIAL AS PER A319 SRM 53-02-00-300-011. (0567174)

Part: FLOOR PANEL — CORRODED (ZONE 200) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION ON INSERTS FLOOR PANEL IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR PANEL IN PASSENGER CABIN WITH NEW REPLACEMENT MATERIAL AS PER A319 SRM 53-02-00-300-011. (0567232)

Part: DECK PLATE — CORRODED (ZONE 100) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION ON LOWER WORK DECK COMPARTMENT 110 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPAIRED PER ER/A 619768-14. (0566989)

Part: FLOOR PANEL — CORRODED (ZONE 200) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION ON INSERTS FLOOR PANEL IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR PANEL IN PASSENGER CABIN WITH NEW REPLACEMENT MATERIAL AS PER A319 SRM 53-02-00-300-011. (0567224)

Part: SKIN — CORRODED (ZONE 600) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION UPPER SKIN LOWER SURFACE TRAILING EDGE OVERHANG AREA AT LEVEL RIB 12 R/H WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS LOC. ON UPPER SKIN LOWER SURFACE TRAILING EDGE OVERHANG AREA AT LEVEL RIB 12 R/H WINGAS PER A319 SRM 57-21-11-283-026. (0567006)

Part: SHEAR PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION SHEAR PLATE LOCATED BETWEEN FRAME 69 TO FRAME 70 AND STRINGER 23 RIGHT AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED SHEAR PLATE LOCATED BETWEEN FRAME 69 TO FRAME 70 AND STRINGER 23 RIGHT AT AFT GALLEY AREA AS PER A319 SRM 51-42-11 AND A319 SRM 51- 72-11. (0566913)

Part: FLOOR PANEL — CORRODED (ZONE 200) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION ON INSERTS FLOOR PANEL IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR PANEL IN PASSENGER CABIN WITH NEW REPLACEMENT MATERIAL AS PER A319 SRM 53-02-00-300-011. (0567214)

Part: PLATE — CORRODED · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION FOUND ON IB AND OB AL PLATES (FACES AND BORES) AT TRACK #3 IN THE INNER AND OUTER RIB 5 ECCENTRIC BEARING. CORRECTIVE ACTION: REPAIRED PER ER/A 620418-14. (0564838)

Part: LUG — CORRODED (ZONE 300) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION FOUND IN LWR LUG BORE AT BR3 OF THE RUDDER. CORRECTIVE ACTION: REPAIRED PER ER/A 620196-14. (0565566)

Part: HINGE FITTING — CORRODED (ZONE 100) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION ON RH MLG DOOR HINGE FITTING KEEL BEAM AT AFT LUG. CORRECTIVE ACTION: REPLACED PER ER/A 620217-14AD. (0562073)

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 DELAMINATED TOP LAYER FLOOR PANEL 261DF IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED PER ER/A 619952-14. (0562104)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION SEAT TRACK -Y1292 FROM FRAME 64 TO FRAME 66 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED SEAT TRACK -Y1292 AND FASTENERS FROM FRAME 64 TO FRAME 66 AT AFT GALLEY AREA AS PER A319 SRM 51-72-11 AND A319 SRM 51-42-11. (0559899)

Part: WINDOW FRAME — DAMAGED (ZONE 200) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 DAMAGE TO FRONT WINDSHIELD FRAME. CORRECTIVE ACTION: REPAIRED PER ER/A 581650-14AD. (0559666)

Part: WINDOW FRAME — DAMAGED (ZONE 200) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 DAMAGE TO FRONT WINDSHIELD FRAME. CORRECTIVE ACTION: REPLACED PER ER/A 619593-14. (0556965)

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION WEB LOCATED BETWEEN FR27 TO FR28 AND STR38L IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED WEB AND LOC. BTW FR27 TO FR28 STRG 38L AS PER A319 SRM 51-42-11-801 AND SRM 51-72-11-001A. (0550978)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION SEAT TRACK +Y765 LOCATED FROM FRAME 64 TO FRAME 66 AT AFT GA LLEY AREA. CORRECTIVE ACTION: REPLACED SEAT TRACK Y765 AND FASTENERS LOC.FR64 TO FR66 AT AFT GALLEY AREA LH SIDE AS PER A319 SRM 51-72-11 AND A319 SRM 51-42-11. (0551005)

Part: SKIN — BROKEN (ZONE 500) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 BROKEN AILERON AERODYNAMIC COMPOSITE UPPER AND LOWER SURFACE ON LH WING. CORRECTIVE ACTION: REPAIRED LH AILERON AERODYNAMIC COMPOUND UPPER AND LOWER SURFACE ON LH WING AS PER A319 SRM 57-61-21-300-011. (0549342)

Part: STRUT — CORRODED (ZONE 500) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION INTERCONNECTING STRUT OB FLAP ON LH WING (1 EA). CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT ON LH WING AS PER A320 FAM AMM 27 -51-44-000-001-A. (0549813)

Part: STRUT — CORRODED (ZONE 600) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION INTERCONNECTING STRUT IB FLAP ON RH WING (1 EA). CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT ON RH WING AS PER A320 FAM AMM 27 -51-44-000-001-A. (0549819)

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION SHEAR TIE LOCATED FR27 AND FROM STR41R TO STR42R IN FWD CAR GO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE AND FASTENERS LOC FR 27 AND FROM STRG 41R TO STRG 42R ON FWD CARGO COMPARTMENT AS PER A319 SRM 51-72-11. (0545982)

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION SHEAR TIE LOCATED FR28 AND FROM STR42R TO STR43R IN FWD CARG O COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEER TIE LOCATED AT FR28 AND FROM STR42R TO STR43R IN FWD CARGO COMPARTMENT AND MEASURES OF CORROSION. (0545933)

Part: SUPPORT BRACKET — CORRODED (ZONE 400) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION ON SUPPORT BRACKET AFT ATTACH FITTING ON AFT FIXED FAIRING LH PYLON. CORRECTIVE ACTION: REPLACED SUPPORT BRACKET AFT ATTACH FITTING ON AFT FIXED FAIRING LH PYLON PER AMDS CARD 5450-6010-LT

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION SHEAR TIE LOCATED FR29 BETWEEN STR40R TO STR41R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE AND FASTENERS LOCATED FR29 BETWEEN STR40R TO STR41R IN FWD CARGO COMPARTMENT AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (0545979)

Part: HINGE FITTING — CORRODED (RUDDER) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION ON HINGE FITTING 4 LOWER LUG UPPER FACE ON RUDDER. CORRECTIVE ACTION: REPLACED HINGE FITTING #4 LOC ON RUDDER AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (0545939)

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION SHEAR TIE LOCATED FR34 AND FROM STR41R TO STR42R IN FWD CAR GO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE AND FASTENERS LOCATED FR34 AND FROM STR41R TO STR42R IN FWD CARGO COMPARTMENT AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (0545867)

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION SHEAR TIE LOCATED FR30 AND FROM STR41L TO STR42L IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE AND FASTENERS LOCATED FR30 AND FROM STR41L TO STR42L IN FWD CARGO COMPARTMENT AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (0544914)

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION LOWER SILL AT FR68 AND S-23L AFT GALLEY AREA. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON LOWER SILL AT FR68 AND S-23L AFT GALLEY AREA AS PER A319 SRM 53-41-14-300-001. (0541332)

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION SHEAR TIE LOCATED FR28 AND FROM STR41R TO STR42R IN FWD CAR GO COMPARTMENT. CORRECTIVE ACTION: EPLACED SHEAR TIE LOCATED FR28 AND FROM STR41R TO STR42R IN FWD CARGO COMPARTMENT AS PER A319 SRM 51-42-11-801 AND A319 SRM51- 72-11. (0541397)

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION WEB FRAME 16 AT LEVEL STRINGER 23 LEFT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED WEB LOC. FRAME 16 AT LEVEL STRINGER 23 LEFT FWD GALLEY AREA SIDE, AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (0541035)

Part: FITTING — CORRODED (ZONE 400) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION ON SPIGOT RECEPTACLE FITTING UPPER SPAR ON LH PYLON. CORRECTIVE ACTION: REPLACED NEW SPIGOT RECEPTACLE FITTING UPPER SPAR ON LH PYLON AS PER A319 SRM 51-42-11 AND AS PER A319 SRM 54-51-12-300-001. (0540982)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION FLOOR BEAM +Y1292 FROM FRAME 12 TO FRAME 24 FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED SEAT TRACK Y1292, SPLICE (1 E/A), COVER (1EA) AND FASTENERS LOC. BTW FR12 TO FR24 AT FWD GALLEY AREA AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (0541039)

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION ON WEB FROM FRAME 12 TO FRAME 16 AT LEVEL STRINGER 23 RIGHT FLOOR STRUCTURE AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED WEB FROM FRAME 12 TO FRAME 16 AT LEVEL STRINGER 23 RIGHT FLOOR STRUCTURE AT FWD GALLEY AREA. (0541017)

Part: BLANKING PLATE — BROKEN (ZONE 200) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 BROKEN BLANKING PLATE GIRT BAR FITTINGS FWD POSITION DOOR 832 AT AFT G ALLEY AREA (1 EA). CORRECTIVE ACTION: REPLACED BLANKING PLATE GIRT BAR FITTINGS FWD POSITION DOOR 832 AT AFT GALLEY AREA (1 EA) AS PER A319 FAM AMM 52-13-31-000-007-A AND A319 FAM AMM 52-13-31-400-007-A. (0533504)

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION CENTER FITTING FROM FRAME 16 TO FRAME 20 AT LEVEL STRINGER 23 RIGHT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED CENTER FITTING LOC. FRAME 16 TO FRAME 20 AT LEVEL STRINGER 23 RIGHT FWD GALLEY AREA AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (0530486)

Part: SKIN — DENTED (ZONE 500 FLAP) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 DENT IB FLAP LOCATED AT 24IN FROM I/B EDGE LOWER SURFACE TRAILING EDGE ON LH WING. CORRECTIVE ACTION: REPAIRED IB FLAP ON LH WING AS PER A319 SRM 57-52-00-300-093. (0530529)

Part: PROFILE — CORRODED (ZONE 200) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION ON HORIZONTAL PROFILE LOC. BTW FR 12 TO FR13 AND FROM -Y254 TO -Y1732 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED HORIZONTAL PROFILE LOC. BTW FR 12 TO FR13 AND FROM - Y254 TO -Y1732 AT FWD GALLEY AREA. AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (0530538)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION FLOOR BEAM +Y1162.5 BTW FR68 TO FR69 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM Y1162.5 BTW FR68 TO FR69 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (0530493)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION ON FLOOR BEAM -Y464.8 LOCATED FROM FRAME 67 TO FRAME 70 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM LOCATED -Y464.8 AND BTW FR 67 TO FR 70 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (0530541)

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION SHEAR TIE LOCATED FR30 AND FROM STR40R TO STR41R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE LOCATED FR30 AND STR40R TO STR41R IN FWD CARGO COMPARTMENT AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (0530570)

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION SHEAR TIE LOCATED FR30 AND FROM STR41R TO STR42R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE LOC. FR30 AND FROM STR41R TO STR42R IN FWD CARGO COMPARTMENT AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (0530573)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION FLOOR BEAM +Y1292-1162 FROM FR66 TO FR68 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM Y1292-1162 FROM FR66 YO FR68 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (0530498)

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION ON CHANNEL STRUCTURE LOCATED FROM FRAME 12 TO FRAME 16 AT LEVEL OF STRINGER 23 RIGHT AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED CHANNEL STRUCTURE LOCATED FROM FRAME 12 TO FRAME 16 AT LEVEL OF STRINGER 23 RIGHT AT FWD GALLEY AREA AS PER A319 SRM 51 -72-11 AND SRM 51-42-11. (0530549)

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION SHEAR TIE LOCATED FR34 AND FROM STR41L TO STR42L IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE LOCATED FR34 AND FROM STR41L TO STR42L IN FWD CARGO COMPARTMENT AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (0530535)

Part: PRESSURE BLKHD — GOUGED (ZONE 100) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 REAR FUSELAGE AFT PRESSURE BULKHEAD FR70 UPPER SECTION INB'D FLANGE GOUGE. CORRECTIVE ACTION: REPAIRED PER ER/A 619976-14. (0526975)

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION SHEAR TIE LOCATED FR29 BETWEEN STR39R TO STR40R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE LOC. FR29 BETWEEN STR39R TO STR40R IN FWD CARGO COMPARTMENT AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (0517861)

Part: SHEAR TIE — GOUGED (ZONE 100) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 GOUGE SHEAR TIE AFT FRAME 29 LOCATED BETWEEM STR41L TO STR42L IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE LOC.AFT FRAME 29 LOCATED BETWEEN STR41L TO STR42L IN FWD CARGO COMPARTMENT AS PER A319 SRM 51-42-11, A319 SRM 51-72-11. (0517867)

Part: DUMMY RAIL — CORRODED (ZONE 200) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION RAIL DUMMY Y503.2 AT LEVEL FRAME 16 FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED RAIL DUMMY Y503.2 RAIL AT LEVEL FRAME 16 FWD GALLEY AREA AS PER A319 SRM 51-42-11. (0515885)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION FLOOR BEAM -Y1292-1162 BETWEEN FRAME 66 TO FRAME 68 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM Y1292-1162 BETWEEN FRAME 66 TO FRAME 68 AT AFT GALLEY AREA AS PER A319 SRM 51-72-11 AND A319 SRM 51-42-11. (0516021)

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION ON WEB LOCATED BETWEEN FRAME 69 TO FRAME 70 AND STRINGER 23 LEFT AT AFT PASSENGER CABIN. CORRECTIVE ACTION: REPLACED WEB LOC. BTW FR69 TO FR70 AND STRINGER 23 LEFT AT AFT PASSENGER CABIN AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (0508883)

Part: SHEAR TIE — DAMAGED (ZONE 100) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 TOOL MARK SHEAR TIE AT LEVEL OF FR60 AND BTW STR 42L TO STR 43L IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE AND FASTENERS AS PER A319 SRM 51-42-11-801, SRM 51-72-11-911-001. (0508913)

Part: FITTING — CORRODED (ZONE 400) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION ON SPIGOT RECEPTACLE FITTING UPPER SPAR ON RH PYLON. CORRECTIVE ACTION: REPLACED SPIGOT RECEPTACLE FITTING UPPER SPAR ON RH PYLON AS PER A319 SRM 54-51-12-300-001. (0508887)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION SEAT TRACK -Y1292 AT LEVEL F20 FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED SEAT TRACK -Y1292 LOC. ON FR12 TO FR24 AT FWD GALLEY AREA. (0500308)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION SEAT TRACK -Y765 AT LEVEL FRAME 20 FWD GALLEY AREA. CORRECTIVE ACTION: REPAIRED PER A319 SRM 51-44-11 AND AS PER A319 SRM 51-42-11. (0500313)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION FLOOR BEAM -Y765 LOCATED FROM FR66 TO FR70 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y765 LOCATED FROM FR66 TO FR70 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (0493760)

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION WEB FRAME 20 AT LEVEL OF STRINGER 23 RIGHT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED WEB LOCATED ON FRAME 20 TO FRAME 24 AT LEVEL OF STRINGER 23 RH SIDE FWD GALLEY AREA AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (0488227)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION FLOOR SUPPOR -Y1162.5 BETWEEN FRAME 68 TO FRAME 69 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR SUPPORT -Y1162.5 BETWEEN FRAME 68 TO FRAME 69 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (0484636)

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION SHEAR TIE LOCATED FR34 AND FROM STR44 TO STR43L IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE LOCATED FR34 AND FROM STR44 TO STR43L IN FWD CARGO COMPARTMENT AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (0484640)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION SEAT TRACK +Y765 AT LEVEL FRAME 20 FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED SEAT TRACK Y765 LOCATED BTW FR12 TO FR24 AT FWD GALLEY AREA AS PER A319 SRM 51-72-11 AND A319 SRM 51-42-11. (0480653)

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 CORROSION SEAT TRACK +Y765 AT LEVEL FRAME 20 FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED SEAT TRACK Y765 LOCATED BTW FR12 TO FR24 AT FWD GALLEY AREA AS PER A319 SRM 51-72-11 AND A319 SRM 51-42-11. (0480650)

Part: CRADLE — BROKEN (ZONE 200) · airframe 56,806 hrs · 29,003 cycles

SHIP 3148 BROKEN BASE FLASHLIGHT IN AFT WINDSCREEN RH IN PASSENGER CABIN (1EA). CORRECTIVE ACTION: INSTALLED BASE FLASHLIGHT PER AMDS CARDS 2560-2425. (0462098)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,721 hrs · 28,963 cycles

SHIP 3148 ENROUTE APU GENERATOR DID AN AUTOSHUT DOWNAT FL330. GENERATOR AIRBORN RESTART SUCCESFULL. CORRECTIVE ACTION: REPLACED APU LOW PRESSURE OIL SWITCH AND REPLACED RIGHT ENGINE IDG. OK FOR SERVICE. (4507048)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,475 hrs · 28,833 cycles

SHIP 3148 DURING CRUZ FL 370, ECAM IND. "SMOKE LAV SMOKE" APPEARED (APPROX 5 SEC) AND WAS AUTO REMOVED. CORRECTIVE ACTION: T/S PER TSM 26-17-00-810-804-A. NO DISCREPANCIES NOTED. (4935440)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,155 hrs · 28,663 cycles

AIRCRAFT 3148, DURING SVC CHECK FOUND EEPL INOP AT SEATS 26D/27D. CORRECTIVE ACTION: FOUND WIRE 3351-9050 BROKEN AT CONNECTOR 9159VC. REPINNED WIRE PER A319 ESPM 20-44-11. PERFORMED OPS CHECK OF EEPLS PER A319 AMM 33-51. CHECKS GOOD. OK FOR SVC.

Part: NONE — NONE · corrosion level 2 · airframe 54,299 hrs · 27,632 cycles

SHIP 3148 - LEFT MLG ACTUATOR ANCHORAGE FITTING BORE AND UPPER AND LOWER FACE HAS CORROSION. CORRECTIVE ACTION: REPAI RED FITTING REF ERA 601628-14 REV. ORIGINAL.(2378629)

Part: NONE — NONE · airframe 54,299 hrs · 27,632 cycles

SHIP 3148 - RMLG, FWD PINTLE PIN SPHERICAL BEARING, RETAINING THREAT SHOW LIGHT CORROSION. CORRECTIVE ACTION: CLEANED AND INSPECTED PER A319 CMM 32-11-07. (2369748)

Part: NONE — NONE · airframe 54,299 hrs · 27,632 cycles

SHIP 3148 - RMLG AFT SUPPORT FWD LUG, AFT BUSHING SHOWS LIGHT CORROSION. CORRECTIVE ACTION: CLEANED AND INSPECTED PER A319 CMM 32-11-07 NO WAS CORROSION FOUND. (2369870)

Part: COMPUTER — FAULTY (X) · airframe 53,365 hrs · 27,089 cycles

SHIP 3148 - DIV - TO JFK DUE TO NOSEWHEEL STEERING FAULT AFTER GEAR EXTENSION FOR LANDING AT LGA. SYSTEM FAULTS STEERING MODULE 6GC. CORRECTIVE ACTION: REPLACED STEERING CONTROL MODULE & BSCU. (8742140)

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 51,589 hrs · 26,156 cycles

SHIP 3148 - AISLE EMERGENCY LIGHTS AT SEAT ROWS 26-27 INOP. CORRECTIVE ACTION: FOUND WIRE BROKEN AT CONNECTOR 9159VC RE PINNED WIRE IN 9159VC REF A319 WDM 33-51-08 AND ESPM 20-33. (7368863)

Part: CONTROL SWITCH — FAULTED (EMERGENCY LIGHTS) · airframe 50,266 hrs · 25,603 cycles

EMERGENCY LIGHT ARE ON WHEN EMERGENCY LIGHTS SWITCH IS ARMED. CORRECTVE ACTION: REMOVED AND REPLACED EMERGENCY LIGHT CONTROL SWITCH FIN 4WL, IAW A319 AMM 33-51. OPERATIONS CHECK GOOD.

Part: PROXIMITY SWITCH — DEFECTIVE (R1 DOOR) · airframe 48,832 hrs · 24,839 cycles

(AIRCRAFT 3148, L/P 7131542) R1 DOOR WHITE SLIDE ARMED LIGHT DOES NOT ILLUMINATE WHEN DOOR CLOSED AND LOCKED AND SLIDE ARMED. CORRECTIVE ACTION: REMOVED AND REPLACED R1 DOOR SLIDE ARMING PROX SWITCH 4WN2 PER A319/320 AMM 52-73. NO SLIDE REMOVAL NECESSARY.

Part: LIGHT — UNKNOWN (CABIN) · airframe 48,734 hrs · 24,792 cycles

(AIRCRAFT 3148, L/P 1535694) EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:EME / EMERGENCY CABIN LIGHTING /ALL LIGHTS COME ON GROUND/ / INTERIOR. CORRECTIVE ACTION: FRC 335201 EMERGENCY CABIN LIGHTS COME ON GROUND. PERF POWER TRANSFER AND OPN OF CABIN EMERGENCY LIGHTING PER A320 33-51. OPN NORM.

Part: PROXIMITY SWITCH — MALFUNCTIONED (R1 DOOR) · airframe 48,410 hrs · 24,657 cycles

AT DEPARTURE 1R DOOR SLIDE ARMED LIGHT AT DOOR HANDLE ILLUMINATED WITH DOOR ARMED. R/R R1 DOOR PROXIMITY SWITCH PER A319 AMM 52-71.

Part: WARNING MESSAGE — FALSE INDICATION (E/E BAY DOOR) · airframe 47,940 hrs · 24,435 cycles

SHIP 3148 - ATO - AT APPROXIMATELY 60KTS DUE TO AFT AVIONICS DOOR OPEN INDICATION. / CORRECTIVE ACTION: DEFERRED DOOR INDICATION PER MEL 52-70-01N. ON RON, PERFORMED INSPECTION OF AVIONICS DOOR PER AMM. NTF.

Part: SKIN — GOUGED (NR 3 SLAT) · airframe 47,409 hrs · 24,184 cycles

GOUGE SLAT 3 TRAILING EDGE LOWER AREA RH WING. PERFORMED PERMANENT REPAIR ON SLAT 3 TRAILING LOWER AREA RH WING AS PER SRM A319 57-44-21-300-011.

Part: SKIN — DENTED (RT) · airframe 47,409 hrs · 24,184 cycles

DENT RH SIDE STATIC PORT DURING PREFLIGHT F/O FOUND DENT ON RIGHT SIDE OF NOSE (F/O SIDE) REFER TO (LOG PAGE 4600672). PERFORMED REPAIR ON FUSELAGE SKIN ON RIGHT SIDE OF (F/O SIDE) IAW SRM A319 53-11-11-300-041.

Part: WINDOW FRAME — CRACKED (RIGHT) · airframe 47,409 hrs · 24,184 cycles

CRACK INDICATION ON INTERNAL AREA LOWER ATTACHMENT OF THE WINDSHIELD CENTER POST RH SIDE IN COCKPIT (1 EA) L= (0.375 IN. APPROX.). PERFORMED REPAIR ON INTERNAL AREA LOWER ATTACHMENT OF THE WINDSHIELD CENTER POST RH SIDE IN COCKPIT AS PER ER/A 581650-14AD. REPAIR APPROVAL IS LIMITED TO 6,600 CYCLES AFTER SECTION I OF ER/A 581650-14AD. DELTA ENGINEERING MUST CONTACT AIRBUS BEFORE DUE DATE OF SECTION II REQUESTING INSTRUCTIONS FOR PART REPLACEMENT INFORMATION FOR THE WINDSHIELD FRAME PN D53111077203. (REF. RDAS 80685751/003/2019 ISSUE: A).

Part: HINGE — WORN (VERTICAL STAB) · airframe 47,409 hrs · 24,184 cycles

WEAR ON BEARING HINGE ARM ON THE VERTICAL STABILIZER. REPLACED THE NR 3 HINGE IAW SRM 51-72- 11, SRM 51-42-00, AND DWG 55371052, ISSUE U.

Part: DAMPER — NO TEST (PAX DOOR) · airframe 47,409 hrs · 24,184 cycles

PASSENGER DOOR DAMPER AT FWD GALLEY AREA WOULD NOT PASS TEST . REMOVED AND REPLACED PASSENGER DOOR DAMPER IAW AMM 52-11-14-400-001-B.

Part: DAMPER — NO TEST (PAX DOOR) · airframe 47,409 hrs · 24,184 cycles

PASSENGER DOOR AT THE AFT GALLEY DID NOT PASS A TEST. REPLACED THE DAMPER IAW AMM 52-13-14-400-001-B.

Part: FLOOR SUPPORT — CORRODED (FRAMES 67-69) · corrosion level 2 · airframe 47,409 hrs · 24,184 cycles

CORROSION FLOOR SUPPORT BETWEEN FRAMES 67+16 INCHES TO 69+4 INCHES, Y+1292. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, SRM 51-42-00, AND DWG 53472780.

Part: FLOOR SUPPORT — CORRODED (FRAMES 67-69) · corrosion level 2 · airframe 47,409 hrs · 24,184 cycles

CORROSION FLOOR SUPPORT BETWEEN FRAMES 67+16 INCHES TO 69+4 INCHES, Y-1292. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11-911-001, AND DWG D53472780.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · corrosion level 2 · airframe 47,409 hrs · 24,184 cycles

CORRODED FLOOR SUPPORT BETWEEN FRAMES 64 TO 66, +Y1292. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, SRM 51-42-00, AND DWG D53472780.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-24) · corrosion level 2 · airframe 47,409 hrs · 24,184 cycles

CORROSION FLOOR SUPPORT, BETWEEN FRAMES 12 TO 24, Y+ 254. REPLACED THE FLOOR SUPPORT IAW SRM 51-42-00, SRM 51-72-11, AND DRAWING D53110984.

Part: FRAME ANGLE — CORRODED (FRM 59) · corrosion level 2 · airframe 47,409 hrs · 24,184 cycles

CORROSION ON FRAME 59 ANGLE AFT FACE LOCATED BETWEEN STRINGERS 42L TO 43L IN THE AFT CARGO COMPARTMENT. REPLACED THE FRAME ANGEL IAW SRM A319 51-72-11 51-42-11 AND DRAWING D53476342.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 46,132 hrs · 23,579 cycles

RT EPSU FAIL MESSAGE FOR EMERGENCY LIGHT TEST. FOUND RT OVER WING EXIT BATTERY NOT TESTING. R AND R BATTERY PER AMM 33-50 OPS TEST NORMAL SYSTEM TEST OK.

Part: REPAIR — UNKNOWN · airframe 47,415 hrs · 24,186 cycles

ERA 568357-14 HAS BEEN ISSUED FOR PUNCTURE AND DENT THAT WAS REP AIRED PER EA 31-203749 REV F. DURING AIRBUS' RDAS REVIEW FOR THE A319 WV INCREASE PROJECT THE APPROVAL REQUIRED REVISION. ERA 568357-14 SECTION IV IMPOSES A LIFE LIMIT ON THE BOTTOM SKIN REPAIR. THE REPAIR LIFE HAS BEEN LIMITED TO 27,600 FLIGHT CYCLE S OR 55,200 FLIGHT HOURS FROM FIRST FLIGHT OR 20 MONTHS FROM 30- APR-2018 (30-DEC-2019) (WHICHEVER OCCURS FIRST). ASSOCIATED ER/A 31-568357. REPLACED BUTT STRAP LOC TRAILING EDGE SECTION 1V OF ERA 568357- 14 REV ORIGINAL LOC BOTTON SKIN PANEL 3 BTW RIB 9 TO RIB 10 ON LH WING. MONITOR,ERA 568357-14 HAS BEEN ISSUED FOR PUNCTURE.

Part: FRAME — CORRODED (APU TAILCONE) · corrosion level 2 · airframe 42,671 hrs · 21,976 cycles

APU TAILCONE FRAME 86 HAS CORROSION AROUND LOWER GUIDE PIN, REPLACED THE FRAME SECTION IAW DWG D5358541820200, AND SRM 53-51-12-300-001.

Part: SKIN — GOUGED (FRAME 70) · airframe 36,940 hrs · 19,308 cycles

RT AFT FUSELAGE SKIN APPROXIMATELY 4" FWD OF FRAME 70 BETWEEN STR 14 - 15R, DENT WITH SHARP GOUGE, DOUBLER REPAIR IAW SRM 53-00-11, FIG 229.

Part: FLOOR PANEL — CORRODED (AFT CABIN) · airframe 36,940 hrs · 19,308 cycles

AFT CABIN FLOOR PANEL 262FF HAS CORROSION. REPLACED THE FLOOR PANEL IAW SRM 51-72-11.

Part: LIGHT — INOPERATIVE · airframe 34,279 hrs · 17,776 cycles

EMERGENCY LIGHT AT 4C INOPERATIVE, PLUGGED LIGHT IN.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,368 hrs · 16,784 cycles

LEFT OVER WING EMERGENCY EXIT LIGHT BATTERY FAULT ILLUMINATED. REPLACED EPSU BATTERY PACK IAW AMM 33-51-38, PG 401.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 31,759 hrs · 16,442 cycles

SEAT 14C EMERGENCY SEAT MOUNTED LIGHT DAMAGED. REPLACED BROKEN LENS 4. OPS CHECKED OK IAW AMM 33-51. OK FOR SERVICE.

Part: SKIN — DENTED (FRAMES 21-23) · airframe 31,481 hrs · 16,277 cycles

DURING M1 CHECK, A DENT WAS FOUND ON SKIN BETWEEN FRAMES 21-23 AND STRINGER 25L. FOUND OUT OF LIMITS IAW SRM 53-11-11 PB 4.C DIAGRAM 10. REPAIRED IAW ERA 521960-14 SECTION I.

Part: SKIN — DENTED (FRAMES 21-23) · airframe 31,398 hrs · 16,232 cycles

DURING M1 CHECK, A DENT WAS LOCATED BETWEEN FRAMES 21 - 23 AND S25L. DENT FOUND BEYOND LIMITS IAW SRM 53-11-11, PB 4.C DIAGRAM 10. REPAIRED IAW ERA 521960-14 SECTION I.

Part: STRUCTURE — CORRODED (CENTER WING BOX) · airframe 38,992 hrs · 20,301 cycles

CORROSION ON UPPER SURFACE OF CENTER WING BOX LOC AT LEVEL FR 42 AND BTW -Y1732 TO -Y 1292 PAX CABIN MEASURE L=1.500" W=1" D=0.002" APPROX. REPAIR ON UPPER SURFACE OF CENTER WING BOX LOCATED AT LEVEL FR41 TO FR42 BTW Y-1292 TO Y-1732 AND RIB 1 PAX CABIN PER ERA 521963-14.

Part: ACCESS PANEL — CORRODED (WING) · airframe 31,397 hrs · 16,231 cycles

CORROSION ON FUEL TANK ACCESS PANEL 540FB. REPLACED ACCESS PANEL 540FB ON LT WING IAW AMM 57-27-11-400-001-A.

Part: SILL — CORRODED (FRAMES 16-20) · airframe 31,397 hrs · 16,231 cycles

CORROSION ON LOWER SILL LOCATED FWD PAX CABIN ENTRY DOOR LT BETWEEN FRAME 16-20 WITH MEASUREMENT L=0.080", W=0.050", D=0.005" APPROXIMATELY, SSI 531189. PERFORMED REPAIR ON LOWER SILL LOCATED FWD PAX CABIN ENTRY DOOR BETWEEN FRAME 16 LT AND FR 20 LT IAW SRM 53-11-14, FIG 108 AND MUST BE INSPECTED AT 60000FC/FH NOT RELEVANT IAW SRI 53-11-14-1-001-00, PARA 3.A, TABLE 102 THE DEEPEST POINT IS FRAME 20 AFT INBD L=1.149", W=1.097", MRT=0.148".

Part: SILL — CORRODED (FRAMES 16-20) · airframe 31,397 hrs · 16,231 cycles

CORROSION ON LOWER SILL LOCATED FWD PAX CABIN ENTRY DOOR BETWEEN FR 16 AND FR 20 RT WITH MEASUREMENT L=0.080", W=0.060", D=0.006", APPROX. PERFORMED REPAIR ON LOWER SILL LOCATED FWD PAX CABIN ENTRY DOOR BETWEEN FRAME 16-20 RT SIDE IAW SRM 53-11-14, FIG 108 SHEET'S AND MUST BE REINSPECTED AT 60000FC/FH NOT RELEVANT, FROM ACFT FIRSTFLIGHT IAW SRI 53-11-14-1-001-00, PARA 3A, TABLE 102, THE DEEPEST. POINT IS : FRAME 16 AFT OTBD L=1.690", W=1.222, MRT 0.148".

Part: SKIN — CORRODED (FRAMES 30-34) · airframe 31,397 hrs · 16,231 cycles

CORROSION ON EXTERNAL SKIN LOCATED ON AREA OF DRAIN MAST FRAME 30-34, STR 42L-43L. REWORKED AREA IAW SRM 51-74-00 ON EXTERNAL FUSELAGE SKIN LOCATED FR30, FR34, STR 42L TO 43L LT SIDE EVALUATED AND FOUND WITHIN LIMITS ASPER SRM 53-21-11, PARA 4E FIG 115 AND DIAGRAM 105, MEASURE AFTER REWORKED AREA ARE:L=2114, W=1.661. MINIMUN REAMING THICKNESS ON REWORK AREA=0.090" INITIAL THICKNESS IN NON-REWORKED AREA IS 0.094" MEASURED IAW NTM 51-10-04 PB4 EQUIPMENT, PN 45MG, SN 130061901 DUE DATE DEC.27.2014 HFEL INSPECTION ON REWORKED AREA ON EXTERNAL SKIN IAW NTM 51-10-08 PB6, NO CRACK INDICATION.

Part: CHANNEL — CORRODED (LT WING) · airframe 31,397 hrs · 16,231 cycles

CORROSION ON RETAINER NUT PLATES AT FRONT AREA OF DOOR BETWEEN RIBS 5 - 6 IN LT WING DRY BAY. REPLACED CHANNEL IAW SRM A319 51-42-11 AND DWG D57252700.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 31,397 hrs · 16,231 cycles

DELAMINATION ON LT INBD FLAP UPPER AND LOWER SKIN. REPAIRED IAW SRM 57-52-00, PARA 8.0, ITEMS 2 AND 3 .

Part: FLOOR SUPPORT — CORRODED (FRAMES 68-69) · airframe 31,397 hrs · 16,231 cycles

CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 68 - 69 + Y1162. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472780.

Part: FLOOR SUPPORT — CORRODED (FRAME 20) · airframe 31,397 hrs · 16,231 cycles

CORROSION ON FLOOR SUPPORT AT FRAME 20, Y-1292. REPLACED FLOOR SUPPORT BETWEEN FRAMES 12 - 24 IAW SRM 51-72-11 AND DWG D53112812.

Part: FITTING — CORRODED (FRAME 66) · airframe 31,397 hrs · 16,231 cycles

CORROSION ON AFT CORNER FITTING LOCATED FRAME 66. REPLACED AFT CORNER FITTING IAW SRM 51-72-11 AND DWG D53480009.

Part: SILL — CORRODED (FRAMES 66-68) · airframe 31,397 hrs · 16,231 cycles

CORROSION ON LOWER SILL LOCATED RT PAX CREW DOOR BETWEEN FRAMES 66 - 68. REPLACED SILL IAW SRM 51-72-11, & DWG D53480009.

Part: FLOOR SUPPORT — CORRODED (FRAME 20) · airframe 31,397 hrs · 16,231 cycles

CORROSION ON FLOOR SUPPORT AT FRAME 20, Y-254. REPLACED FLOOR SUPPORT.

Part: SILL — CORRODED (FRAMES 66-68) · airframe 31,397 hrs · 16,231 cycles

CORROSION ON LOWER SILL LOCATED LT AFT PAX CREW DOOR BETWEEN FRAMES 66 TO 68. REPLACED LOWER SILL IAW SRM 51-72-11 AND DWG D53480009.

Part: FLOOR SUPPORT — CORRODED (FRAMES 68-69) · airframe 31,397 hrs · 16,231 cycles

CORROSION ON FLOOR SUPPORT -Y1162 BETWEEN FRAMES 68 - 69. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472780.

Part: SUPPORT — CORRODED (FRAMES 69-70) · airframe 31,397 hrs · 16,231 cycles

AFTER REMOVING SHEAR PLATE, FOUND CORROSION ON SUPPORT BETWEEN FRAMES 69- 70. REPLACED SUPPORT IAW 51-72-11 AND D53470100.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-67) · airframe 31,397 hrs · 16,231 cycles

CORROSION FOUND ON FLOOR SUPPORT -Y1225, FRAMES 66 - 67+15.5. REPLACED FLOOR SUPPORT IAW SRM A319 51-72-11 AND DWG D534 72780.

Part: FITTING — CORRODED (FRAME 68) · airframe 31,397 hrs · 16,231 cycles

CORROSION ON AFT CORNER FITTING LOCATED FR 68 AFT PAX CABIN LT SIDE. REPLACED AFT CORNER FITTING IAW SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · airframe 31,397 hrs · 16,231 cycles

CORROSION ON FLOOR SUPPORT -Y1292, BETWEEN FRAMES 64 - 66. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D534-72815.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-70) · airframe 31,397 hrs · 16,231 cycles

CORROSION ON FLOOR SUPPORT -Y765 BETWEEN FRAME 66 - 70. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472815.

Part: FLOOR SUPPORT — CORRODED (FLOOR SUPPORT) · airframe 31,397 hrs · 16,231 cycles

CORROSION FOUND ON FLOOR SUPPORT -Y765 BETWEEN FRAMES 64 - 66. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 & DWG D53472815.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · airframe 31,397 hrs · 16,231 cycles

CORROSION ON FLOOR SUPPORT +Y160, BETWEEN FRAMES 66-68. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472780.

Part: FITTING — CORRODED (FRAMES 16-20) · airframe 31,397 hrs · 16,231 cycles

CORROSION ON CENTER FITTING LOCATED FWD ENTRY PAX CABIN DOOR RT BETWEEN FRAMES 16-20. REPLACED CENTER FITTING IAW SRM 51-72-11 AND DWG D531-12198.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-67) · airframe 31,397 hrs · 16,231 cycles

CORROSION ON FLOOR SUPPORT Y1225 BETWEEN FRAMES 66 - 67+15.5. REPLACED FLOOR SUPPORT IAW SRM 51-72-11, & DWG D53472780.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · airframe 31,397 hrs · 16,231 cycles

CORROSION ON FLOOR SUPPORT Y1292 BETWEEN FRAMES 64 - 66. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472815.

Part: FLOOR SUPPORT — CORRODED (FRAME 20) · airframe 31,397 hrs · 16,231 cycles

CORROSION ON FLOOR SUPPORT AT FRAME 20 LEVEL Y-765. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112812 AND D53110984.

Part: FLOOR SUPPORT — CORRODED (FRAMES 16-20) · airframe 31,397 hrs · 16,231 cycles

CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 16-20, Y1292. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112812 AND D53110920.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-70) · airframe 31,397 hrs · 16,231 cycles

CORROSION ON FLOOR SUPPORT Y765 FRAMES 66 TO 70. REPLACED FLOOR SUPPORT IAW SRM A319 51-72-11 AND DWG D53472000.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-67) · airframe 31,397 hrs · 16,231 cycles

CORROSION ON FLOOR SUPPORT -Y465, BETWEEN FRAMES 64 - 67+10. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472816.

Part: FLOOR SUPPORT — CORRODED (FRAMES 18-23) · airframe 31,397 hrs · 16,231 cycles

CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 18 AND 23 Y254. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112816, D53110984 AND D55110920.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · airframe 31,397 hrs · 16,231 cycles

CORROSION ON FLOOR SUPPORT Y765, FRAMES 64 - 66. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.

Part: DUMMY RAIL — CORRODED (FRAMES 14-16) · airframe 31,397 hrs · 16,231 cycles

CORROSION ON DUMMY RAIL BETWEEN FRAMES 14-16. REPLACED DUMMY RAIL IAW SRM A319 51-72-11 AND DWG D53112825.

Part: SKIN — GOUGED (FRAME 28) · airframe 31,397 hrs · 16,231 cycles

GOUGE ON EXTERNAL FUSELAGE SKIN AT FRAME 28 PLUS 2 INCHES BETWEEN S43-44L LOWER FWD FUSELAGE. FOUND WITHIN LIMITS IAW SRM 53-21-11. HFEC INSPECTION DONE IAW NTM 51-10-08. NO CRACK INDICATIONS FOUND.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,415 hrs · 15,710 cycles

DURING NON ROUTINE CHECK, FOUND EPSU UNIT FAULT ON FWD LT EPSU. REPLACED EPSU UNIT AND BATTERY PACK AND FUNCTIONAL CHECK WAS NORMAL.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,013 hrs · 15,506 cycles

ESPU BATTERY FWD L MESSAGE FOUND WHILE PERFORMING STEP 7 OF THE SERVICE CHECK. R & R OVERWING EPSU BATTERY. INSTALLED SERVICEABLE BATTERY PACK IAW AMM 33-51-38, P6 401. OP TESTED OK FOR SERVICE.

Part: SKIN — DENTED (BS 59) · airframe 31,397 hrs · 16,231 cycles

DAMAGE TO FUSELAGE SKIN JUST AFT OF CARGO DOOR FS 59. FOUND TO BE WITHIN LIMITS IAW SRM 53-41-11. TREATED BUT DID NOT PAINT.

Part: TRUNNION — DAMAGED (TE FLAP) · airframe 5,224 hrs · 2,910 cycles

LEFT INBOARD FLAP TRUNNION DAMAGED. AREA WORN APPROXIMATE .250 DEEP. REMOVED LEFT INBOARD FLAP INBOARD TRUNNION IAW A319/320 CMM 57-52-21 (903393). REPLACED LEFT INBOARD FLAP TRUNNION IAW A319/320 CMM 57-52-21 AND PER PRI501285-14 REV 1. INSTALLED INBOARD FLAP TRUNNION OF FLAP AT AT TRACK 1. CHECKED FLAP RIGGING PER A319 AMM 27-54-61-400-001 (492156) QC 4056. RECEIVED ERA 501285-14AD REV ORIG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,075 hrs · 12,181 cycles

DURING A NON ROUTINE CHECK, FOUND THE EMERGENCY PATHLIGHT AT ROW 13 INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHT ASSEMBLY AND FUNCTIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 22,554 hrs · 11,349 cycles

DURING LINE CHECK, FOUND DENT IN FUSELAGE UNDER DOOR 1L. TEMPORARY REPAIR ACCOMPLISHED IAW SRM 53-00-11, FIG 219 TIME LIMITED TO 3000 FLIGHT CYCLES.