N319NB

Part: SKIN — GROUND DAMAGE (ZONE 100) · airframe 67,015 hrs · 34,536 cycles

A GROUND VEHICLE HOSE CONTACTED THE AIRCRAFT ON THE FUSELAGE BETWEEN FR2 AND FR4, ABOVE Y330 RH. COMPLIED WITH ER/A 628044-14. (1213814).

Part: SKIN — GROUND DAMAGE (ZONE 100) · airframe 67,015 hrs · 34,536 cycles

A GROUND VEHICLE HOSE CONTACTED THE AIRCRAFT ON THE FUSELAGE BETWEEN FR2 AND FR4, ABOVE Y330 RT. CORRECTIVE ACTION: COMPLIED WITH ER/A 628044-14. (1213648).

Part: SKIN — SCRATCHED (ZONE 100) · airframe 67,005 hrs · 34,532 cycles

SCRATCH ON EXTERNAL SKIN LOCATED BTW FR 57 TO FR 58 AND STR 26L TO ST R 27L AT LOWER FUSELAGE. COMPLIED WITH ER/A 629166-14AD. (1212626).

Part: SKIN — SCRATCHED (ZONE 100) · airframe 67,005 hrs · 34,532 cycles

FOUND SCRATCHES AAFFECTING THE FUSELAGE SKIN PANEL BETWEEN FR 57 AND STR 26L-27L. COMPLIED WITH ER/A 629166-14AD. (1212433).

Part: COVER — DAMAGED (ZONE 800) · airframe 67,005 hrs · 34,532 cycles

SLIDE COVER NEEDS TO BE REPLACED. REMOVE AND RE-INSTALL SLIDE COVER AND INSTALL AND REMOVE SAFETY LOCK P IN ON RESERVOIR ASSY OF ESCAPE SLIDE OF PASSENGER CREW DOOR 831, 832, 841 AND 842. (1212191).

Part: PLATE — CRACKED · airframe 66,961 hrs · 34,510 cycles

SHIP 3119 FOUND PLATE CRACKED. CORRECTIVE ACTION: INSTALLED NEW SLAT TRACK CLOSING PLATE ON RIGHT INBOARD SLAT PER A319 AMM 27-84. ALL CHECKS OK. (7415292)

Part: SKIN — DAMAGED · airframe 66,697 hrs · 34,362 cycles

SHIP 3119 FWD FUSELAGE DAMAGE FR 1-4. CORRECTIVE ACTION: COMPLIED WITH ER/A 628044-14. (1108228).

Part: SKIN — DENTED (ZONE 200) · airframe 66,760 hrs · 34,398 cycles

SHIP 3119 FOUND DENT ON THE CROWN SKIN AFT OF FR 53 BETWEEN STR 3L-4L. CORRECTIVE ACTION: COMPLIED WITH ER/A 626580-14. (1107420).

Part: SKIN — GROUND DAMAGE (ZONE 100) · airframe 66,760 hrs · 34,398 cycles

SHIP 3119 GROUND VEHICLE HOSE CONTACTED THE AIRCRAFT ON THE FUSELAGE BETWEEN FR 2-4 AND ABOVE Y=330 RH. CORRECTIVE ACTION: COMPLIED WITH ER/A 628044-14. (1107429).

Part: RADOME — DAMAGED (ZONE 100) · airframe 66,686 hrs · 34,356 cycles

SHIP 3119 DAMAGE TO NOSE RADOME RIGHT SIDE. CORRECTIVE ACTION: R/R RADOME PER A320 AMM 53-15-11. (1102409)

Part: PANEL — DELAMINATED (ZONE 300) · airframe 66,686 hrs · 34,356 cycles

SHIP 3119 LEFT HORIZONTAL STAB UPPER PANEL 334BT DELAMINATED/SEPERATED. CORRECTIVE ACTION: R/R'D PANEL 334BT ON LEFT HORIZONTAL STAB IAW A319 AMM 55-10. (7455080).

Part: CONTROLLER — FAULTED (CARGO HEAT) · airframe 66,561 hrs · 34,276 cycles

SHIP 3119 - ATO - DUE TO AFT CARGO HEAT MESSAGE AT THROTTLE UP. DEFERRED AFT CARGO HEAT PER MEL AND CONTINUE. REPLACED AFT CARGO HEAT CONTROLLER 10HV.

Part: FAIRING — DAMAGED (ZONE 600) · airframe 66,501 hrs · 34,246 cycles

SHIP 3119 RIGHT WING SLAT TRACK FAIRING RACKED AND PEELED BACK. CORRECTIVE ACTION: INSTALLED NEW SLAT CLOSING PLATE PER A319 AMM 27-84. (7441368)

Part: PIN — BROKEN (ZONE 800) · airframe 65,820 hrs · 33,877 cycles

SHIP 3119 DISC: L1 DOOR BOARDER DOOR PIN LEAGH FOR PIN IS BROKEN. C/A: FWD TO NEF 52-13-03 NO "M" PROCEDURE. DOOR 1L DISARM PIN LANYARD ALREADY ON NEF DEFERRAL, SEE LP 088291. (LP: 7209952)

Part: FRAME — CRACKED (FRM 35 S30L) · airframe 63,153 hrs · 32,546 cycles

SHIP 3119 CRACK 2.0" LONG FOUND RUNNING THROUGH FASTENER HOLES #2, #6, AND #7, LHS FR35 BH AT LEVEL OF STR 30. CORRECTIVE ACTION: REPAIRED PER ER/A 612601-14. (0344522)

Part: FRAME — CRACKED (FRM 35 S30L) · airframe 63,153 hrs · 32,546 cycles

SHIP 3119 CRACK 2.0" LONG FOUND RUNNING THROUGH FASTENER HOLES #2,#6, AND #7, LHS FR35 BH AT LEVEL OF STR 30. CORRECTIVE ACTION: REPAIRED PER ER/A 612601-14. (0344509)

Part: FRAME — CRACKED (FRM 35 S30L) · airframe 63,153 hrs · 32,546 cycles

SHIP 3119 CRACK 2.0" LONG FOUND RUNNING THROUGH FASTENER HOLES #2, #6, AND #7, LHS FR35 BH AT LEVEL OF STR 30. CORRECTIVE ACTION: REPAIRED PER ER/A 612601-14. (0344527)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 63,129 hrs · 32,529 cycles

SHIP 3119 ON TAKE OFF PLACE PLANE PULLED TO THE RIGHT ON LANDING PLANE PULLS TO THE RIGHT. CORRECTIVE ACTION: PERFORMED STEERING CHECK AT GATE NO DEFECTS NOTED. TAXI A/C WITH NO STEERING FAULTS NOTED. PER A319 AMM 32-51-00. A/C OF FOR SERVICE. (5876236)

Part: INSERT — MISALIGNED (L1 GUST LOCK) · airframe 63,108 hrs · 32,517 cycles

SHIP 3119 GUST LOCK ON DOOR 1L NOT OPERATING CORRECTLY VERY DIFFICULT TO UNLOCK IN IAH AND UPON ARRIVAL AT GATE IN LAX IT WILL NOT LOCK. CORRECTIVE ACTION: PERFORMED A GVI OF 1L DOOR GUST LOCK FOUND TEFLON INSERT MISALINGED, REALINGED TEFLON INSERT IN REF TO A319 AMM 52-10, OPS CHECK NORMAL OK FOR SVC. (5876216)

Part: HOUSING — CORRODED (NR 2 FLAP TRACK) · airframe 63,108 hrs · 32,517 cycles

SHIP 3119 CORROSION FOUND IN TRACK 2 BEARING HOUSING AT RIB 9 LEVEL ON RH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 612951-14. (0334300)

Part: GIRT BAR — OBSTRUCTED (L2 DOOR SLIDE) · airframe 62,807 hrs · 32,355 cycles

SHIP 3119 2L DOOR/ SLIDE WILL NOT ARM. CORRECTIVE ACTION: REMOVED FOD FROM GIRT BAR LOCKING MECHANISM PER A319 AMM 52-12. OK FOR SVC. (5352444)

Part: SENSOR — FAULTED (THRUST LEVER) · airframe 62,527 hrs · 32,202 cycles

SHIP 3119 - ATO - AT 40KTS DUE TO A MOMENTARY #2 THRUST LEVER ANGLE SENSOR FAULT. CORRECTIVE ACTION: DEFERRED TLA SENSOR PER MEL 76-11-01. LATER REPLACED #2 THRUST CONTROL MODULE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,144 hrs · 31,966 cycles

SHIP 3119 EPLS ROW'S 14-17 INOP. CORRECTIVE ACTION: REMOVED & REPLACED POWER (EPSU) FIN 12WL AS PER A320F AMM 33-51-38. OPS CHECK GOOD. A/C OK FOR SERVICE. (4334732)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,100 hrs · 31,939 cycles

SHIP 3119 DAMAGED SEAT TRACK Y1292 LOC. BTW FR64 TO FR66 AFT GALLEY AREA SEAT TRACK. CORRECTIVE ACTION: REPLACED PER ER/A 612734-14. (0080000)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CRACK HAS BEEN NOTICED IN UPPER AREA OF FR20 LHS, EXISTING REPAIR ON HOLE 5. CORRECTIVE ACTION: REPAIRED PER ER/A 563224-14AD. (0078904)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 WEAR FORWARD FITTING MAIN DOOR AT MAIN LANDING GEAR L/H SIDE. CORRECTIVE ACTION: REPLACED FORWARD FITTING MAIN DOOR AT MAIN LANDING GEAR L/H SIDE AS PER AIRBUS CMM 52-81-18. (0079084)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CRACK INDICATION WAS FOUND ON FR16LH AT HOLE IDENTIFIED AS HOLE #6. CORRECTIVE ACTION: REPAIRED PER ER/A 563227-14AD. (0078062)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CRACK INDICATION WAS FOUND ON FR16RH AT HOLE IDENTIFIED AS HOLE #6. CORRECTIVE ACTION: REPAIRED PER ER/A 563226-14AD. (0078980)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION INTERNAL STRUCTURE WEB AND NUT PLATE LOC.AT STR 38L BTW FR 5 8 AND FR 59 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED INTERNAL STRUCTURE WEB AND NUT PLATE LOC.AT STR 38L BTW FR 58 AND FR 59 IN AFT CARGO COMPARTMENT AS PER A319 SRM51-42- 11 & A319 SRM 51-72-11. (0078888)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHME NT AREA CONTINUITY FITTING LH SIDE. CORRECTIVE ACTION: REPAIRED PER ER/A 612406-14AD. (0079068)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CRACK HAS BEEN NOTICED IN UPPER AREA OF FR20 LHS, EXISTING REPAIR ON HOLE 6. CORRECTIVE ACION: REPAIRED PER ER/A 563224-14AD. (0078632)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHME NT INTERNAL AREA, FROM UPPER TENSION BOLT, LH SIDE. CORRECTIVE ACTION: REPAIRED PER ER/A 612406-14AD. (0079046)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHME NT INTERNAL AREA FROM UPPER TENSION BOLT, RH SIDE. CORRECTIVE ACTION: REPAIRED PER ER/A 612406-14AD. (0079050)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CRACK ON AIR INTAKE COWL AFT BULKHEAD LOC. AT 4 OCLOCK ON ENGINE 1. CORRECTIVE ACTION: REPAIRED PER ER/A 613867-14. (0076470)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION AIR INTAKE COWL ON ENG 2. CORRECTIVE ACTION: REPLACED AIR INTAKE COWL ON ENG 2 AS PER A320 FAM AMM 71-11-00- 000-040-A. (0076358)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CRACK INDICATION ON FRAME 20 LH SIDE CROSSBEAM SPLICING AREA. CORRECTIVE ACTION: REPAIRED PER ERA 612506-14AD. (0077678)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION FLAP TRACK 3 BUSHING (2 EA) LOCATED ON FITTING ON LH WING. CORRECTIVE ACTION: REPLACED END STOP FITTING FLAP TRACK 3 ON LH WING AS PER A320 FAM AMM 27-54-46-000-001-A AND AMM 27-54-46-400-001-A. (0077178)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CRACK INDICATION ON FRAME 16 RH SIDE CROSSBEAM SPLICING AREA. CORRECTIVE ACTION: REPAIRED PER ER/A 612478-14AD. (0077687)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CRACK FRAME 35 STR 30 LH FWD FACE PRESSURE BULKHEAD IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER ER/A 612601-14AD. (0077732)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,100 hrs · 31,939 cycles

SHIP 3119 CORROSION ON ELECTRICAL CONNECTOR OF MANUAL DRIVE CWW EXTEND OF APU IN LET FLAPPER. CORRECTIVE ACTION: REPLACED APU AIR INTAKE FLAP ACTUATOR PER A320 FAM AMM 49-16-51-000-003-A AND A320 FAM AMM 49-16-51-400-003-A. (0076551)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CRACK INDICATION WAS FOUND ON FR16RH AT HOLE IDENTIFIED AS HOLE #6. CORRECTIVE ACTION: REPAIRED PER ER/A 31-563226. (0075057)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CRACK INDICATION WAS FOUND ON FR16LH AT HOLE IDENTIFIED AS HOLE #6. CORRECTIVE ACTION: REPAIRED PER ERA 563227-14AD. (0075894)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 DENT INTERNAL STRUCTURE DOOR AT LOWER FORWARD CORNER IN AFT CARGO COMP ARTMENT. CORRECTIVE ACTION: REPAIRED PER ER/A 613185-14. (0076074)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 FR35 PRESSURE BH ATTACHMENTS A CRACK 2.0" LONG WAS FOUND RUNNING THROUGH FASTENER HOLES #2, #6, AND #7 IN LHS FR35 BH AT LEVEL OF STR30. CORRECTIVE ACTION: COMPLIED WITH ERA 612601-31. (0073402)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 GOUGE WEB UPPER SPAR LOC. BTW RIB8 AND RI9 OUTBOARD SIDE LH PYLON. CORRECTIVE ACTION: COMPLIED WITH ERA 612671-14 REV. ORIGINAL. (0072104)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CRACK INDICATIONS FOUND IN LH FRONT WINDSHIELD FRAME AT THE CENTER LWR NODE AREA IN UPPER TENSION BOLT ATTACH HOLE D1. CORRECTIVE ACTION: COMPLIED WITH ERA 612406-31. (0071632)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 MACHINE SEAT TRACK Y765 LOC. BTW FR64 TO FR66 AT AFT GALLEY AREA. CORRECTIVE ACTION: COMPLIED WITH ERA 612886-14 REV. ORIGINAL. (0070611)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CRACK INDICATIONS FOUND IN LH FRONT WINDSHIELD FRAME AT THE CENTER LWR NODE AREA IN UPPER TENSION BOLT ATTACH HOLE D1. CORRECTIVE ACTION: COMPLIED WITH ERA 612406-31. (0071606)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CRACK INDICATIONS FOUND IN LH FRONT WINDSHIELD FRAME AT THE CENTER LWR NODE AREA IN UPPER TENSION BOLT ATTACH HOLE D1. CORRECTIVE ACTION: COMPLIED WITH ERA 612406-31. (0071624)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION FRAME 20 TO FR 21 INTERNAL SKIN LEVEL STR 42L IN AFT AVIONIC COMPARTMENT. CORRECTIVE ACTION: COMPLIED WITH ER/A 612896-14 REV. ORIGINAL. (0069897)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 ELONGATED HOLE ACCESS PANEL 424CR ON RH PYLON. CORRECTIVE ACTION: COMPLIED WITH ERA 613110-14 REV. ORIGINAL. (0069915)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CRACK ON BONDING PLATE HINGE ARM 2 ELEVATOR ON RH HORIZONTAL STABILIZER. CORRECTIVE ACTION: REPLACED BONDING PLATE HINGE ARM 2 ON ELEVATOR HORIZONTAL STABILIZER RH AS PER A319 SRM 51-42-11, 51-72-11. (0067993)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION AFFECTING THE RIB 9A ASSY, INNER FACE AND BORE, AND OUTER FACE AND BORE OF MILLING PART RIB 9B AT FLAP TRACK #2 LVL OF LH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 613215-14. (0068197)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 GOUGE ACCESS PANEL 194AB BELLY FAIRING AT LOWER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER ER/A 612784-14. (0066503)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 GOUGE ACCESS PANEL 193AB BELLY FAIRING AT LOWER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER ER/A 612784-14. (0066494)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CRACK ACCESS PANEL 322AL LH AND RH SIDE VERTICAL STABILIZER. CORRECTIVE ACTION: REPAIRED PER ER/A 612713-14. (0066512)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 BROKEN BONDING PLATE HINGE ARM 2 ON LH ELEVATOR. CORRECTIVE ACTION: REPLACED BONDING PLATE HINGE ARM 2 ON LH ELEVATOR AS PER A319 SRM 51-42-11 AND A320 FAM AMM 55-16-42-000-001-A. (0066697)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION IN TRACK 2 BEARING HOUSING AT RIB 9 LEVEL ON RH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 612951-14. (0064852)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 FR20 LHS CROSS BEAM SPLICE AREA, CRACK IN HOLE #26. CORRECTIVE ACTION: REPAIRED PER ER/A 612506-14AD. (0064621)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CRACK INDICATION ON FRAME 4 HORIZONTAL UPPER STIFFENER ON LATERAL WINDOW FRAME RH. CORRECTIVE ACTION: REPAIRED PER ER/A 563229-14AD. (0063879)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CRACK INDICATION FOUND ON FRAME 4 HORIZONTAL UPPER STIFFENER, LATERAL WINDOW FRAME 4 LH SIDE. CORRECTIVE ACTION: REPAIRED PER ER/A 563228-14AD. (0063751)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CRACK IN UPPER AREA OF FR20 LHS (ABOVE DOOR STOP 7) AT HOLE NO 6. CORRECTIVE ACTION: REPAIRED PER ER/A 563224-14. (0063000)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 OVERSIZED HOLE 1 AT DOORSTOP FITTING 5 LOCATED FR68 LH. CORRECTIVE ACTION: REPAIRED PER ER/A 612628-14AD. (0063598)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 OVERSIZED HOLE 2 AND HOLE 3 AT DOOR STOP FITTING 7 LOCATED FR68. CORRECTIVE ACTION: REPAIRED PER ER/A 612793-14. (0062417)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 OVERSIZED HOLE 1, HOLE 2 AT DOORSTOP FITTING 6 LOCATED FR68 LH. CORRECTIVE ACTION: REPAIRED PER ER/A 612628-14AD. (0063607)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 OVERSIZED HOLE 3 AT DOORSTOP FITTING 4 LOCATED FR68 RH DIAMETER. CORRECTIVE ACTION: REPAIRED PER ER/A 612793-1. (0062392)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 OVERSIZED HOLE 2, AND HOLE 3 AT DOOR STOP FITTING 6 LOCATED FR 68 RH. CORRECTIVE ACTION: REPAIRED PER ER/A 612793-14. (0062406)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 OVERSIZED HOLE 3 AT DOORSTOP FITTING 4 LOCATED FR68 LH. CORRECTIVE ACTION: REPAIRED PER ER/A 612628-14AD. (0063610)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 OVERSIZED HOLE 3 AT DOORSTOP FITTING. CORRECTIVE ACTION: REPAIRED PER ER/A 612793-14. (0062396)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 OVERSIZED HOLE 1 AT DOOR STOP FITTING 7 LOCATED FR68 LH. CORRECTIVE ACTION: REPAIRED PER ER/A 612628-14AD. (0063576)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 BROKEN BONDING PLATE HINGE ARM 2 ON RH ELEVATOR. CORRECTIVE ACTION: REPLACED BONDING PLATE HINGE ARM 2 ON RH ELEVATOR AS PER A319 SRM 51-42-11 AND SRM 51-72-11. (0063093)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION ON STRINGER 39R FR 63 TO FR 64 ON AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED STRINGER 39R FR 63 TO FR 64 ON AFT CARGO COMPARTMENT AND REINSTALLED TWO SPLICES (COUPLING) AS PER A319 SRM 51-42-11. (0063568)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 OVERSIZED HOLE 2 AND HOLE 4 AT DOORSTOP FITTING 1 LOCATED FR68 LH. CORRECTIVE ACTION: REPAIRED PER ER/A 612628-14AD. (0063614)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 OVERSIZED HOLE 1 AT DOORSTOP FITTING 3 LOCATED FR68 LH. CORRECTIVE ACTION: REPAIRED PER ER/A 612628-14AD. (0063604)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 OVERSIZED HOLE 2 AT DOORSTOP FITTING 5 LOCATED FR68 RH. CORRECTIVE ACTION: REPAIRED PER ER/A 612793-14. (0062403)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 OVERSIZED HOLE 2 AT DOORSTOP FITTING 2 LOCATED FR68 LH. CORRECTIVE ACTION: REPAIRED PER ER/A 612628-14AD. (0063602)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION ON FIXED BUSHINGS MOVABLE FAIRING ON LH PYLON (4 EA). CORRECTIVE ACTION: REPAIRED INBOARD LUG OF INBOARD SIDE AND REPLACED BUSHINGS (3 EA) OF MOVABLE FAIRING ON LH PYLON AS PER A319 SRM 51-72-12-911-002, A319 SRM 51-21 -11-801 AND A319 SRM 54-55-12-300-003. (0061882)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION ON CARRIAGE BOLTS ON FLAP TRACK 3 (1 EA) AND TRACK 4. CORRECTIVE ACTION: REPLACED CARRIAGE BOLTS ON FLAP TRACK 3 (1 EA), TRACK 4 (1 EA), AND BOLT DRIVE ARM TRACK 3 O/B FLAP ON RH WING IAW AMDS CARD # 2750-6020-RT. (0061847)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION FIXED BUSH ON RUDDER LOWER ACTUATOR FITTING (2EA). CORRECTIVE ACTION: REPLACED BUSHINGS (2 EA) ON ACTUATOR ATTACH FITTING RUDDER BUSHINGS. (0061883)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION STRINGER 41R LOC. BTW FR 61 AND FR 62 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED STRINGER 41 RH, BTW FR 61R TO FR 64R AND STR 4O R TO STR42 R AT AFT CARGO COMPARTMENT AS PER A 319 SRM 51-42-11 AND SRM51-72-11. (0061859)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION FIXED BUSH ON RUDDER UPPER ACTUATOR (2EA). CORRECTIVE ACTION: REPLACED BUSHINGS (2 EA) ON ACTUATOR ATTACH FITTING RUDDER BUSHINGS (UPPER POSITION) ON VERTICAL STABILIZER AS PER A319 SRM 51-72-12-911-002. (0061891)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 EXCESSIVE PLAY CRUISE ROLLER IB FLAP ON LH WING. CORRECTIVE ACTION: REPLACED CRUISE ROLLER IB FLAP ON LH WING AS PER AIRBUS CMM 57- 52-21. (0061870)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 EXCESSIVE PLAY TRACK 2 IB FLAP BEARING ON LH WING (1 EA). CORRECTIVE ACTION: REPLACED BEARING TRACK 2 I/B FLAP ON LH WING (1 EA) AS PER A320 FAM AMM 57-52-21-000-001-A 4.A(3) AND AS PER A320 FAM AMM57-52-21-400-001 -A. 4.(A). (0061855)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION FIXED BUSH ON RUDDER MIDDLE ACTUATOR (2EA). CORRECTIVE ACTION: REPLACED BUSHINGS (2 EA) ON ACTUATOR ATTACH FITTING RUDDER BUSHINGS ON VERTICAL STABILIZER AS PER A319 SRM51-72-12-911-002. (0061886)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 DENT WITH GOUGE WAS FOUND AFFECTING AFT CARGO DOOR INNER SKIN. CORRECTIVE ACTION: REPAIRED PER ER/A 613185-14. (0059084)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CRACK WEB FR8-11 - Y765 IN COCKPIT. CORRECTIVE ACTION: REPLACED WEB LOC. FR8 TO FR 11 - Y765 IN COCKPIT AS PER A319 SRM 51-42-11. (0059172)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 FR68 LHS DOORSTOP FITTING #7, HOLES FOUND WITH STARTING HOLE DIAMETER GREATER THAN MAX STARTING HOLE DIAMETER REQUIRED. CORRECTIVE ACTION: REPAIRED PER ER/A 612628-14AD. (0058820)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CRACK INDICATION ON FRAME 68 RH, DOORSTOP FITTING 1 HOLE 4, LOWER INBOARD HOLE AT AFT GALLEY AREA (1 EA). CORRECTIVE ACTION: REPAIRED FRAME 68 RH, DOORSTOP FITTING 1 HOLE 4, LOWER INBOARD HOLE AT AFT GALLEY AREA AS PER A319 SRM 53-41-12- 300-011. (0059233)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 FR68 RHS DOORSTOP FITTINGS #6 & #7, STARTING HOLE DIAMETERS GREATER THAN MAX STARTING HOLE DIAMETER REQUIRED. CORRECTIVE ACTION: REPAIRED PER ER/A 612793-14AD. (0059012)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CRACK WEB FR8-11 + Y765 IN COCKPIT. CORRECTIVE ACTION: REPLACED WEB Y765 LOCATED BTW FR 8 TO FR 11 UPPER SURFACE AS PER A319 SRM 51-42-11 AND 51-72-11. (0058105)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION FOUND ON CENTER WING BOX, TOP PANEL, AFT SIDE BETWEEN FR41 - FR42, AND BETWEEIN Y1292 - Y1732. CORRECTIVE ACTION: REPAIRED PER ER/A 612632-14. (0055658)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 EXCESSIVE PLAY TRACK 3 OB FLAP BEARING ON LH WING (1 EA). CORRECTIVE ACTION: REPLACED BEARING TRACK 3 O/B FLAP ON LH WING AS PER A320 FAM AMM 57-53-21-000-001-A AND AS PER A320 FAM AMM 57-53-21-400-001- A. (0050915)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CRACK WAS FOUND IN UPPER ATTACHMENT STIFFENER OF THE LH SLIDING WINDOW FR4. CORRECTIVE ACTION: REPAIRED PER ER/A 563228-14. (0050929)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CRACK WAS FOUND IN THE PREVIOUSLY REPAIRED, UPPER ATTACHMENT STIFFENER OF THE RH SLIDING WINDOW FR4. CORRECTIVE ACTION: REPAIRED PER ER/A 563229-14. (0051048)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 EXCESSIVE PLAY BEARING ATTACHMENT BRACKET AFT FIXED FAIRING ON RH PYLON (1EA). CORRECTIVE ACTION: REPLACED BEARING (1E/A) AND SLEEVE (1/A) ATTACHMENT BRACKET AFT FIXED FAIRING ON RH PYLON AS PER A319 AMM 54-52. (0050886)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 EXCESSIVE PLAY FWD BEARING AFT FIXED FAIRING ON RH PYLON (1 EA). CORRECTIVE ACTION: REPLACED HINGE FITTING FWD POSITION ON AFT FIXED FAIRING ON RH PYLON AS PER SRM 51-42-11-801, A319 SRM 51-44-11-801, A319 SRM 51-72-11-911-001, A319 SRM 51-21-11-801 AND A319 SRM51-49-00-801. (0050900)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 EXCESSIVE PLAY FWD BEARING AFT FIXED FAIRING ON LH PYLON (1 EA). CORRECTIVE ACTION: REPLACED HINGE FITTING FWD POSITION ON AFT FIXED FAIRING ON LH PYLON AS PER. (0050892)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION RAIL DUMMY -Y81 LOCATED BTW FR 12 TO FR 16 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED RAIL DUMMY -Y81 LOCATED BTW FR 12 TO FR 16 AT FWD GALLEY AREA AS PER A319 SRM 51-42-11 AND SRM 51-72-11. (0049638)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 EXCESSIVE PLAY CARRIAGE FLAP TRACK 3 BEARING O/B FLAP ON RH WING (1 EA). CORRECTIVE ACTION: REPLACED NEW BEARING O/B FLAP TRACK 3 ON RH WING (1 EA) AS PER A320 FAM AMM 57-53-21-000-001-A AND AMM 57-53-21-400-001-A. (0049641)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 EXCESIVE PLAY ON BARING (1 E/A) OF DRIVE ARM TRACK #4 ON O/B FLAP R/H WING. CORRECTIVE ACTION: REPLACED BEARING (1 E/A) OF DRIVE ARM TRACK 4 ON O/B FLAP R/H WING. AS PER AIRBUS CMM 57-53-21. (0048530)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 EXCESSIVE PLAY BUSHINGS FLAP TRACK 4 DRIVE ARM O/B FLAP ON RH WING. CORRECTIVE ACTION: REPLACED BUSHINGS (2E/A) FLAP TRACK 4 DRIVE ARM O/B FLAP ON RH WING AS PER A319 SRM 51-72-12-911-002. (0048579)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 EXCESSIVE PLAY FLAP TRACK 1 BEARING DRIVE LEVER ON RH WING. CORRECTIVE ACTION: REPLACED BEARING (1E/A) OF FLAP TRACK 1 DRIVE LEVER ON RH WING AS PER A319 AMM 57-42. (0048516)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 EXCESSIVE PLAY FLAP TRACK 2 DRIVE LEVER ON LH WING (1 EA). CORRECTIVE ACTION: REPLACED BEARING OF FLAP TRACK 2 DRIVE LEVER BEARING ON LH WING AS PER A319 AMM 57-51. (0048558)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 EXCESSIVE PLAY BEARING DRIVE ARM TRACK 4 O/B FLAP ON RH WING. CORRECTIVE ACTION: REPLACED BEARING (1EA) FROM DRIVE ARM TRACK 4 O/B FLAP ON RH WING AS PER AIRBUS CMM 57-53-21. (0048492)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 EXCESSIVE PLAY FLAP TRACK 2 DRIVE ARM BEARING I/B FLAP ON L/H WING. CORRECTIVE ACTION: REPLACED BEARING (1EA) FROM FLAP TRACK 2 DRIVE ARM I/B FLAP AT LH WING, AS PER A319 AMM 57-51. (0048540)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION FIXED BUSH ON VERTICAL STABILIZER UPPER RUDDER ACTUATOR. CORRECTIVE ACTION: REPLACED BUSHINGS (2 EA) ON VERTICAL STABILIZER UPPER RUDDER ACTUATOR. AS PER A319 SRM 51-72-12-911-002. (0048573)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION FLOOR BEAM LOCATED BTW FR 12 TO FR 24 AND -Y765 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM LOCATED BTW FR 12 TO FR 24 AND -Y765 AT FWD GALLEY AS PER SRM A319 51-42-11. (0046910)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 EXCESSIVE PLAY FLAP TRACK 2 DRIVE ARM IB FLAP ON RH WING (1 EA). CORRECTIVE ACTION: REPLACED BEARING (1 E/A) FROM FLAP TRACK #2 DRIVE ARM IB FLAP ON R/H WING AS PER AIRBUS CMM 57-52-21. (0046837)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CRACK BONDING PLATE ON FLAP TRACK FAIRING 633CB ON RH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 612690-14. (0046985)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 EXCESSIVE PLAY FLAP TRACK 2 BEARING IB FLAP ON RH WING (1 EA). CORRECTIVE ACTION: REPLACED BEARING I/B FLAP TRACK 2 ON RH WING AS PER A320 FAM AMM 57-52-21-000-001-A AND AS PER A320 FAM AMM 57-52-21-400-001-A. (0046937)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 EXCESSIVE PLAY ON BEARING FLAP TRACK 2 DRIVE ARM IB FLAP ON LH WING (1 EA). CORRECTIVE ACTION: REPLACED BEARING (1EA) FROM FLAP TRACK 2 DRIVE ARM IB FLAP AT LH WING AS PER AIRBUS CMM 57-52-21. (0046840)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION ON AILERON HINGE PINS LH WING (4 E/A). CORRECTIVE ACTION: REPLACED AILERON HINGE PINS LH WING (4 E/A) IAW AMDS CARD 5760-1010S-LT. (0046841)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION ON CARRIAGE BOLTS TRACK 4(1EA) AND TRACK 3(1EA) O/B FLAP ON LH WING. CORRECTIVE ACTION: REPLACED BOLTS TRACK 4(1EA) AND TRACK 3(1EA) O/B FLAP ON LH WING. (0046668)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 EXCESSIVE PLAY BEARING FLAP DRIVE TRUNNION IB FLAP ON RH WING (1 EA). CORRECTIVE ACTION: REPLACED BEARING (1E/A) ON DRIVE ARM TRACK #1 I/B FLAP. AS PER AIRBUS CMM57-52-21, PMS 01-05-26. (0046673)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CRACK BONDING PLATE FLAP TRACK FAIRING 3 (532CB) ON LH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 612690-14. (0047005)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 BROKEN BONDING PLATE FLAP TRACK FAIRING 632CB ON RH WING. CORRCTIVE ACTION: REPAIRED PER ER/A 612690-14. (0046993)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 EXCESSIVE PLAY BEARING FLAP DRIVE ARM IB FLAP TRUNNION ON LH WING (1 EA). CORRECTIVE ACTION: REPLACED BEARING (1EA) FROM FLAP DRIVE ARM IB FLAP TRUNNION ON LH WING. AS PER AIRBUS CMM 57 -52-21. (0046670)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION LOWER SILL LOCATED BETWEEN FR66 AND STR23R AFT GALLEY AREA. CORRECTIVE ATION: REPLACED LOWER SILL LOC. BETWEEN FR 66 TO FR 68 AND STR 23R AFT GALLEY AREA AS PER A319 SRM 51-42-11. (0046925)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION FLOOR BEAM +Y1292 LOCATED BTW FR 64 TO FR 66 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM Y1292 LOC. BTW FR64 TO FR66 AT AFT GALLEY AS PER A319 SRM 51-42-11. (0046911)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 EXCESSIVE PLAY BEARING (1 EA) FLAP TRACK 3 DRIVE ARM OB FLAP ON LH WING (2 EA). CORRECTIVE ACTION: REPLACED BEARING (1 EA) ON TRACK 3 DRIVE ARM O/B FLAP ON LH WING AS PER AIRBUS CMM 57-53-21. (0046895)

Part: FLOOR SUPPORT — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION FLOOR BEAM -Y464.5 LOCATED BETWEEN FR67 TO FR70 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y464.5 LOC. FR67 TO FR70 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (0046913)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 EXCESSIVE PLAY FLAP TRACK 2 BEARING IB FLAP ON RH WING (1 EA). CORRECTIVE ACTION: REPLACED BEARING I/B FLAP TRACK 2 ON RH WING AS PER A320 FAM AMM 57-52-21-000-001-A AND AS PER A320 FAM AMM 57-52-21-400-001-A. (0046845)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 OUT OF ADJUSTMENT PASSENGER CREW DOOR 832 TENSION OF INNER CONTROL HANDLE. CORRECTIVE ACTION: PERFORMED ADJUSTMENT PASSENGER CREW DOOR 832 AS PER A320 FAM AMM 52-13-21-400-001-A. (0046866)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 EXCESSIVE PLAY CRUISE ROLLER OB FLAP ON RH WING. CORRECTIVE ACTION: REPLACED CRUISE ROLLER ON OB FLAP LH WING AS PER AIRBUS CMM 57- 53-21. (0046960)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION FLOOR BEAM -Y1292 LOCATED BETWEEN FR12 TO FR24 FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y1292 LOCATED BTW FR 12 TO FR 24 AT FWD GALLEY AREA AS PER A319 SRM 51-42-11 AND SRM 51-72-11. (0045431)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION LOWER SILL LOCATED BETWEEN FR68 AND STR23L AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED LOWER SILL LOC. BETWEEN FR 66 TO FR 68 AND STR 23L AFT GALLEY AREA AS PER A319 SRM 51-42-11. (0045408)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION WEB LOCATED BETWEEN FR20 TO FR21 AND STR23R FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED WEB LOCATED BETWEEN FR20 TO FR21 AND STR23R FWD GALLEY AREA AS PER A319 SRM 51-42-11. (0045390)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION THRESHOLD SHEET AND COVER SHEET LOWER SILL AREA IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED COVER SHEET LOCATED BTW FR 24 TO FR 28 AT FWD CARGO COMPARTMENT AS PER A319 SRM 51-42-11 AND SRM 51-72-11. (0045426)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 EXCESSIVE PLAY CRUISE ROLLER OB FLAP ON LH WING. CORRECTIVE ACTION: REPLACED CRUISE ROLLER ON OB FLAP LH WING AS PER AIRBUS CMM 57- 53-21. (0043522)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CRACK PLATE LOCATED BTW FR 68 TO FR 69 LEVEL STR 23R AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED PLATE BTW FOR 68 TO 69 LEVEL STR 23 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11. (0043898)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION FIXED BUSH ON VERTICAL STABILIZER MIDDLE RUDDER ACTUATOR (2EA). CORRECTIVE ACTION: REPLACED BUSHINGS (2 EA) VERTICAL STABILIZER MIDDLE RUDDER ACTUATOR. AS PER A319 SRM 51-72-12 -911-002. (0042090)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 EXCESSIVE PLAY BEARING ON AILERON HINGE 2 RH WING. CORRECTIVE ACTION: REPLACED BEARING (1 EA) AND NEW SLEEVE (1 EA) ON AILERON HINGE #2 ON RH AS PER AIRBUS CMM 57-51-54. (0042008)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 EXCESSIVE PLAY BEARING ON AILERON HINGE 1 LH WING. CORRECTIVE ACTION: REPLACED BEARING (1 EA) AND NEW SLEEVE (1 EA) ON AILERON HINGE #1 L/H AS PER AIRBUS CMM 57-51-54. (0042004)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 EXCESSIVE PLAY BEARING ON AILERON HINGE 5 LH WING. CORRECTIVE ACTION: REPLACED BEARING (1 EA) AND NEW SLEEVE (1 EA) ON AILERON HINGE #5 ON LH AS PER AIRBUS CMM 57-51-54. (0041896)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 EXCESSIVE PLAY BEARING ON AILERON HINGE 2 LH WING. CORRECTIVE ACTION: REPLACED BEARING (1 EA) AND NEW SLEEVE (1 EA) ON AILERON HINGE #2 ON LH AS PER AIRBUS CMM 57-51-54. (0041973)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 EXCESSIVE PLAY FLAP TRACK 4 BEARING O/B FLAP ON RH WING (1 EA). CORRECTIVE ACTION: REPLACED FLAP TRACK 4 BEARING O/B FLAP ON RH WING (1 EA) AS PER A320 FAM AMM 57-53-21-000-001-A AND AMM 57-53-21-400-001-A. (0042029)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 EXCESSIVE PLAY BEARING ON AILERON HINGE 1 RH WING. CORRECTIVE ACTION: REPLACED BEARING (1 EA) AND NEW SLEEVE (1 EA) ON AILERON HINGE #1 ON RH AS PER AIRBUS CMM 57-51-54. (0041969)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 EXCESSIVE PLAY BEARING ON AILERON HINGE 5 RH WING. CORRECTIVE ACTION: REPLACED BEARING (1 EA) AND NEW SLEEVE (1 EA) ON AILERON HINGE #5 ON RH AS PER AIRBUS CMM 57-51-54. (0042021)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 EXCESSIVE PLAY BEARING AFT FIXED FAIRING ON RH PYLON (2 EA). CORRECTIVE ACTION: REPLACED BEARINGS (2 EA) ON AFT FIXED FAIRING ON RH PYLON, AS PER A319 AMM 54-52. (0042084)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 EXCESSIVE PLAY BEARING ON AILERON HINGE 3 RH WING. CORRECTIVE ACTION: REPLACED BEARING (1 EA) AND NEW SLEEVE (1 EA) ON AILERON HINGE #3 ON RH AS PER AIRBUS CMM 57-51-54. (0041953)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 EXCESSIVE PLAY BEARING AFT FIXED FAIRING ON LH PYLON (2 EA). CORRECTIVE ACTION: REPLACED BEARINGS (2 EA) ON AFT FIXED FAIRING ON LH PYLON AS PER A319 AMM 54-52. (0042104)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 EXCESSIVE PLAY BEARING ON AILERON HINGE 4 LH WING. CORRECTIVE ACTION: REPLACED BEARING (1 EA) AND NEW SLEEVE (1 EA) ON AILERON HINGE #4 ON LH AS PER AIRBUS CMM 57-51-54. (0041915)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 EXCESSIVE PLAY BEARING ON AILERON HINGE 4 RH WING. CORRECTIVE ACTION: REPLACED BEARING (1 EA) AND NEW SLEEVE (1 EA) ON AILERON HINGE #4 ON RH AS PER AIRBUS CMM 57-51-54. (0042073)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 EXCESSIVE PLAY BEARING ON AILERON HINGE 3 LH WING. CORRECTIVE ACTION: REPLACED BEARING (1 EA) AND NEW SLEEVE (1 EA) ON AILERON HINGE #3 ON LH AS PER AIRBUS CMM 57-51-54. (0041963)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 EXCESSIVE PLAY ON BEARING THAT ATTACH THRUST REVERSER COWL DOOR TO FWD O/B SIDE ON RH PYLON. CORRECTIVE ACTION: REPLACED BEARING (1E/A) THAT ATTACH THRUST REVERSER COWL DOOR TO FWD O/B SIDE ON RH PYLON AS PER A319 AMM 78-31. (0041903)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION FLOOR BEAM +Y765 LOCATED BTW FR 64 TO FR 66 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM Y765 LOCATED BTW FR 64 TO FR 66 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (0039003)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 EXCESSIVE PLAY BEARING ON LINK MOVABLE FAIRING ON LH PYLON (2 EA). CORRECTIVE ACTION: REPLACED BEARINGS (2 E/A) OF LINK MOVABLE FAIRING ON LH PYLON AS PER A319 AMM 54-52. (0037312)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 EXCESSIVE PLAY BEARING ON LINK MOVABLE FAIRING ON RH PYLON. CORRECTIVE ACTION: REPLACED BEARINGS (2 E/A) OF LINK MOVABLE FAIRING ON RH PYLON AS PER A319 AMM 54-52. (0037315)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION RUDDER HINGE 6 BEARING. CORRECTIVE ACTION: REPLACED RUDDER HINGE #6 NEW BEARING ON VERTICAL STABILIZER (1 EA) AS PER A320 FAM AMM 55-46-11-000-001-A AND AMM 55-46-11-400-001-A. (0030956)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CRACK EMERGENCY EXIT DOOR 844 LOAD TRANSMITTING PROFILE INTERNAL AREA FWD POSITION PASSENGER CABIN. CORRECTIVE ACTION: REPLACED SEGMENT EMERGENCY EXIT DOOR 844 INTERNAL AREA FWD POSITION PASSENGER CABIN AS PER A319 SRM 51-72-11 AND SRM 51-42-11. (0030119)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION FIXED BUSH ON VERTICAL STABILIZER LOWER RUDDER ACTUATOR. CORRECTIVE ACTION: REPLACED BUSHINGS (2 EA) ON VERTICAL STABILIZER LOWER RUDDER ACTUATOR AS PER A319 SRM 51-72-12-911-002. (0030108)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION ON INBOARD ELEVATOR SERVO CONTROL ACTUATOR RH HORIZONTAL STA BILIZER. CORRECTIVE ACTION: REPLACED I/B ELEVATOR SERVO-CONTROL ACTUATOR ON RH HORIZONTAL STABILIZER AS PER A320 FAM AMM 27-34-51-400-001-A. (0027312)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 DETERIORATED PASSENGER CREW DOOR 842 BONDED BUSHES UPPER AND LOWER CONNECTION LINK BTW SUPPORT ARM AND DOOR. CORRECTIVE ACTION: REPLACED PASSENGER CREW DOOR 842 BONDED BUSHES UPPER AND LOWER CONNECTION LINK BTW SUPPORT ARM AND DOOR AT AFT GALLEY AREA AS PER A320 FAM AMM 52-10-00-915-001-A. (0022128)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION FIXED BUSH ON RUDDER HINGE 5 (2EA). CORRECTIVE ACTION: REPLACED BUSHINGS (2 EA) ON HINGE FITTING 5 OF RUDDER AS PER A319 SRM51-72-12-911-002. (0019016)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION FIXED BUSH ON HINGE 3 (2 EA) AILERON RH. CORRECTIVE ACTION: REPLACED BUSHING (2E/A) ON HINGE FITTING 3 OF AILERON R/H ASPER AIRBUS CMM 57-61-21. (0019024)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION FIXED BUSH ON FITTING OUTBOARD SERVO CONTROL ACTUATOR AILERON LH (2 EA). CORRECTIVE ACTION: REPLACED BUSHING (2E/A) ON O/B ACTUATOR FITTING OF AILERON L/H ASPER AIRBUS CMM 57-61-21. (0019163)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION FIXED BUSH ON HINGE 4 (2 EA) AILERON LH. CORRECTIVE ACTION: REPLACED BUSHING (2E/A) ON HINGE FITTING 4 OF AILERON L/H ASPER AIRBUS CMM 57-61-21. (0019190)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION FIXED BUSH ON HINGE 5 (2 EA) AILERON LH. CORRECTIVE ACTION: REPLACED BUSHING (2E/A) ON HINGE FITTING 5 OF AILERON L/H ASPER AIRBUS CMM 57-61-21. (0019196)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION FIXED BUSH ON FITTING INBOARD SERVO CONTROL ACTUATOR AILERON LH (2 EA). CORRECTIVE ACTION: REPLACED BUSHING (2E/A) ON I/B ACTUATOR FITTING OF AILERON L/H ASPER AIRBUS CMM 57-61-21. (0019153)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION FIXED BUSH ON RUDDER HINGE 7 (2EA). CORRECTIVE ACTION: REPLACED BUSHINGS (2 EA) ON HINGE FITTING 7 OF RUDDER AS PER A319 SRM51-72-12-911-002. (0019012)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION FIXED BUSH ON HINGE 1 (2 EA) AILERON LH. CORRECTIVE ACTION: REPLACED BUSHING (2E/A) ON HINGE FITTING 1 OF AILERON L/H ASPER AIRBUS CMM 57-61-21. (0019149)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION FIXED BUSHING ON HINGE 5 (2 EA) AILERON RH. CORRECTIVE ACTION: REPLACED BUSHING (2E/A) ON HINGE FITTING 5 OF AILERON R/H ASPER AIRBUS CMM 57-61-21. (0019020)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION FIXED BUSH ON RUDDER HINGE 4 (2EA). CORRECTIVE ACTION: REPLACED BUSHINGS (2 EA) ON HINGE FITTING 4 OF RUDDER AS PER A319 SRM51-72-12-911-002. (0019006)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION FIXED BUSH ON RUDDER HINGE FITTING 1 (2EA). CORRECTIVE ACTION: REPLACED BUSHINGS (2 EA) ON HINGE FITTING 1 OF RUDDER AS PER A319 SRM 51-72-12-911-002. (0019000)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION FIXED BUSH ON RUDDER HINGE 2 (2EA). CORRECTIVE ACTION: REPLACED BUSHINGS (2 EA) ON HINGE FITTING 2 OF RUDDER AS PER A319 SRM51-72-12-911-002. (0018994)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION FIXED BUSH ON FITTING OUTBOARD SERVO CONTROL ACTUATOR AILERON RH (2 EA). CORRECTIVE ACTION: REPLACED BUSHING (2E/A) ON O/B ACTUATOR FITTING OF AILERON R/H ASPER AIRBUS CMM 57-61-21. (0019138)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION FIXED BUSH ON RUDDER HINGE 3 (2EA). CORRECTIVE ACTION: REPLACED BUSHINGS (2 EA) ON HINGE FITTING 3 OF RUDDER AS PER A319 SRM 51-72-12-911-002. (0019008)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION FIXED BUSH ON HINGE 4 (2 EA) AILERON RH. CORRECTIVE ACTION: REPLACED BUSHING (2E/A) ON HINGE FITTING 4 OF AILERON R/H ASPER AIRBUS CMM 57-61-21. (0019136)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION FLOOR SUPPORT-Y765 LOCATED BTW FR 66 TO FR 70 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR SUPPORT LOCATED -Y745 FR 66 TO FR 70 AFT GALLEY AREA AS PER A319 SRM 51-42-11 AND SRM 51-72-11. (0018901)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION FIXED BUSH ON HINGE 2 (2 EA) AILERON RH. CORRECTIVE ACTION: REPLACED BUSHING (2E/A) ON HINGE FITTING 2 OF AILERON R/H ASPER AIRBUS CMM 57-61-21. (0019210)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION FIXED BUSH ON HINGE 2 (2 EA) AILERON LH. CORRECTIVE ACTION: REPLACED BUSHING (2E/A) ON HINGE FITTING 2 OF AILERON L/H ASPER AIRBUS CMM 57-61-21. (0019170)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION FIXED BUSH ON HINGE 1 (2 EA) AILERON RH. CORRECTIVE ACTION: REPLACED BUSHING (2E/A) ON HINGE FITTING 1 OF AILERON R/H ASPER AIRBUS CMM 57-61-21. (0019200)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION FIXED BUSH ON HINGE 3 (2 EA) AILERON LH. CORRECTIVE ACTION: REPLACED BUSHING (2E/A) ON HINGE FITTING 3 OF AILERON L/H ASPER AIRBUS CMM 57-61-21. (0019187)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION FIXED BUSH ON FITTING INBOARD SERVO CONTROL ACTUATOR AILERON RH (2 EA). CORRECTIVE ACTION: REPLACED BUSHING (2E/A) ON I/B ACTUATOR FITTING OF AILERON R/H ASPER AIRBUS CMM 57-61-21. (0019208)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION SPIGOT RECEPTACLE LOC. ON UPPER SPAR LH PYLON. CORRECTIVE ACTION: REPLACED FITTING SPIGOT ON L/H PYLON AS PER A319 SRM 54-51-12- 300-001. (0011063)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION FLOOR BEAM -Y1292 LOCATED BTW FR 66 TO FR 68 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y1292 LOCATED BTW FR 66 TO FR 68 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11 AND SRM 51-72-11. (0011084)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION SPIGOT BALL JOINT BEARING ON LH PYLON. CORRECTIVE ACTION: INSTALLED NEW SPIGOT BALL JOINT ON LH PYLON AS PER A320 FAM AMM 54-51-41-400-001-A. (0011067)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION FLOOR BEAM -Y1162.5 LOCATED BTW FR 68 TO FR 69 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y1162.5 LOCATED BTW FR 68 TO FR 69 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11 AND SRM 51-72-11. (0011074)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION SPIGOT BALL JOINT BEARING ON RH PYLON. CORRECTIVE ACTION: INSTALLED NEW SPIGOT BALL JOINT BEARING ON RH PYLON AS PER A320 FAM AMM 54-51-41-000-001-A. (0011094)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION FLOOR BEAM +Y765 LOCATED BETWEEN FR66 TO FR70 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM Y765 BTW FR66 TO FR70 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11 AND SRM 51-72-11. (0009207)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CRACK FRAME 1 STIFFENER FWD FACE OF BULKHEAD LOCATED BTW Y675 TO -Y675 ON UPPER FUSELAGE. CORRECTIVE ACTION: REPLACED STIFFENER LOC. FWD FACE OF BULKHEAD LOCATED BTW Y675 TO -Y675 ON UPPER FUSELAGE AS PER A319 SRM 51-72-11. (0008098)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 62,096 hrs · 31,937 cycles

SHIP 3119 CORROSION SPIGOT RECEPTACLE LOC ON UPPER SPAR RH PYLON. CORRECTIVE ACTION: REPLACED FITTING SPIGOT ON R/H PYLON AS PER A319 SRM 54-51-12- 300-002. (0003387)

Part: THERMOSTAT — INOPERATIVE (002) · airframe 58,318 hrs · 29,886 cycles

SHIP 3119 - DIV - TO ORF DUE TO NO 2 ENGINE BLEED LEAK MESSAGE. UNABLE TO CONTINUE WITH BLEED ISOLATED DUE TO POSSIBLE ICING CONDITIONS. CORRECTIVE ACTION: REPLACED FAN AIR VALVE THERMOSTAT AND PRV CONTROL SOLENOID DUE TO SUSPECTED SEAL LEAKAGE. REPLACED PYLON DETECTION LOOP 1HF2. AIRCRAFT RTS.(8727702)

Part: STRUT — CORRODED (L) · airframe 57,006 hrs · 29,110 cycles

SHIP 3119 - L/H FLAP I/B SIDE INTERCONNECTING STRUT HOUSING CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED L/H FLAP INTERCONNECTING STRUT. IAW A319 AMM 27-51-44. (1984487)

Part: STRUT — CORRODED (R) · airframe 57,006 hrs · 29,110 cycles

SHIP 3119 - R/H FLAP I/B SIDE ON INTERCONNECTING STRUT HOUSING CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED R/H FLAP INTERCONNECTING STRUT. IAW A319 AMM 27-51-44. (1984477)

Part: FILTER — ODOR (RECIRCULATION) · airframe 56,899 hrs · 29,046 cycles

SHIP 3119 - NOTICEABLE CHEMICAL/DIRTY SOCK ODOR PREVALENT IN THE FRONT OF THE CABIN. CORRECTIVE ACTION: APU CHANGED ON LOG 1951245. REPLACED AVIONICS AIR FILTER PER A319 AMM 21-26.REPLACED BOTH CABIN RE CIRCULATION AIR FILTERS WITH NEW PER A319 AMM 21-21. (7896904)

Part: CONTROL UNIT — INOPERATIVE (NLG STEERING) · airframe 56,778 hrs · 28,972 cycles

SHIP 3119 - ENROUTE DURING CRUISE ECAM WHEEL N/W STRG FAULT CAUTION. AFTER LANDING AC HAD NO STEERING AND WAS TOWED TO THE GATE. CORRECTIVE ACTION: REMOVED AND REPLACED NOSE WHEEL STEERING SERVO CONTROL. OPS CHECKED NORMAL PER A319 AMM 32-51.(7795227)

Part: STRINGER — DAMAGED (FRMS 23-24 S26) · airframe 55,830 hrs · 28,475 cycles

SHIP 3119 - STRINGER DAMAGED FR23-FR24 S26 . CORRECTIVE ACTION: INSTALLED NEW STRINGER SECTION REF A319 SRM 51-42-11 AND A319 SRM 53-11-11-300-041. (1772146)

Part: SKIN — DAMAGED · airframe 55,830 hrs · 28,475 cycles

SHIP 3119 - AIRCRAFT DAMAGE ON RT SIDE OF A/C. CORRECTIVE ACTION : INSTALLED REPAIR DOUBLER REF A319 SRM 53-11-11-300-041.(1772144)

Part: BATTERY — INOPERATIVE (EPSU) · airframe 55,621 hrs · 28,369 cycles

(LOG 7387409) EPSU UNIT EMER L FAULT AFTER EPSU TEST. REMOVED AND REPLACED EPSU AND BATTERY AT 11WL PER A319 AMM 33-51. OPS CKS GOOD.

Part: BATTERY — INOPERATIVE (EPSU) · airframe 55,621 hrs · 28,369 cycles

(LOG 7387408) EPSU BATTERY EMER R FAULT AFTER EPSU TEST. REMOVED AND REPLACED BATT AT 12WL. TEST OK PER A319 AMM 33-51.

Part: POWER SUPPLY — FAULTED (EMERGENCY LIGHTS) · airframe 55,274 hrs · 28,205 cycles

EMERGENCY LIGHTS ON SEATS 14,15,16,17 INOPERABLE. CORRECTIVE ACTION: TEST OF POWER SUPPLY AT RT OVERWING EXIT FAULTS UNIT. INSPECTED WIRES UNDER SEATS DIDN'T FIND ANY DICREPANCIES. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT, PER A319 AMM 33-51-38. OPERATIONS CHECK GOOD.

Part: COOLING FAN — ODOR · airframe 55,258 hrs · 28,198 cycles

STRONG ODOR (DIRTY SOCK SMELL) DURING DESCENT IN COCKPIT AND CABIN. CORRECTIVE ACTION: REMOVED AND REPLACED APU COOLING FAN, PER A319 AMM 49-52.

Part: LIGHT — MALFUNCTIONED (EMERGENCY EXIT) · airframe 55,224 hrs · 28,173 cycles

DOOR LT EMERGENCY EXIT MESSAGE CAME ON AFTER LANDING. WE CONFIRMED THE WINDOW WAS SECURE. CORRECTIVE ACTION: INSPECTED LT DOOR EMERGENCY EXIT, REF A319/320 AMM 52-22. NO TROUBLE FOUND, MESSAGE EXTINGUISHED. CIDS1&2 NO FAULT.

Part: HYDRAULIC SYSTEM — OVERSERVICED (GREEN SYS) · airframe 55,146 hrs · 28,124 cycles

DIRTY SOCK SMELL AT IDLE POWER ON DOWNWARD/BASE INTO ATL. CONFIRMED W/FA DISSIPATED ONCE ENGINES SPOOLED BACK UP. DID NOT SMELL AT HIGHER ALTITUDES ON DESCENT. CORRECTIVE ACTION: OPERATED BOTH ENGINES. PACKS AND APU, DETECTED SLIGHT ODOR WHILE RUNNING NR 1 ENGINE AND PACK 1 INSPECTED ENGINE HP DUCTING NO OIL/RESIDUE PRESENT. INSPECTED NR 1 ACM DUCTING NO OIL/ RESIDUE PRESENT. FOUND GREEN SYSTEM HYD RESERVOIR OVERSERVICED. DRAINED APPROXIMATELY 1.5 QTS FROM RESERVOIR. OPENED CRANKPAD & BORESCOPE PLUGS S1 & S2. C/W BSI, PER A319-20-21 M/M 71-00. NO RESTRICTIVE ITEMS FOUND. INSTALLED BORESCOPE PLUGS S1 & S2 & CRANKPAD COVER, PER A319 AMM 72-31. C/W W/C 7900-2001 FOR LT ENGINE, PER DECISION TABLE ON W/C 0550-2002. NO CONTAMINATION FOUND. NO ECS DECONTAMINATION NECESSARY. INSPECT APU AREA. NO DEFECTS NOTED.

Part: FUEL SYS — OUT OF BALANCE · airframe 53,162 hrs · 27,066 cycles

SHIP 3119 - DIV - TO FSD DUE TO FUEL IMBALANCE. COULD NOT GET FUEL FROM THE RIGHT TANK. CORRECTIVE ACTION: ALL REQUIRED TESTS FOR FUEL IMBALANCE WERE CONDUCTED WITH NO FAULTS FOUND. AIRCRAFT RELEASED FOR SERVICE.

Part: PRESSURE PANEL — CRACKED (FRAMES 35-36) · airframe 52,873 hrs · 26,929 cycles

ERA 582759-14AD SECTION I ISSUED FOR CRACK INDICATIONS FOUND DURING WORKCARD 5311-01171-04 INSPECTION OF FR35-36 PRESSURE PANEL. FOLLOW ON ACTION REQUIRED. MONITOR,ERA 582759-14AD SECTION I ISSUED FOR CRACK STATUS: OPEN DEFRL AUTHORITY AMM: TRM/SRM: AA: ER TOPP: REFERENCE 00-582759 PAGE DEF CHECK TASK CITEXT: AMI: INSP#: SERIAL#: PROC/AMI/AMDS#: DEF TASK STEPS: INSP TIME STANDARD HOURS CYCLES DAYS CHECK BY DATE INITIAL REPETITIVE 62500 HOURS 31200 CYCLES. LOG ENTRY REMAINS OPEN.

Part: PRESSURE PANEL — CRACKED (FRAMES 35-36) · airframe 52,873 hrs · 26,929 cycles

ERA 582759-14AD SECTION I ISSUED FOR CRACK INDICATIONS FOUND DURING WORKCARD 5311-01171-04 INSPECTION OF FR35-36 PRESSURE PANEL. FOLLOW ON ACTION REQUIRED. ACCOMPLISH SECTION II INSPECTION PRIOR TO THE EARLIER OF 57000 FLIGHT CYCLES OR 114000 FLIGHT HOURS FROM SECTION I ASSOCIATED AA 5311-01171 ADDED FOR AC 3119 ASSOCIATED ER/A 00-572759 ADDED FOR AC 3119. INSP TIME STANDARD HOURS CYCLES DAYS CHECK BY DATE INITIAL REPETITIVE TERMINATING 114000 57000. MON, 31 L/L, 1348623;VIS ;ERA572759;ERA 582759-14A. OPEN DEFFERAL

Part: DOOR — MISSING (HYD BAY) · airframe 52,830 hrs · 26,906 cycles

PDA PART DEPARTING AIRCRAFT. A/C 3119 CLOSED LOG 5949432 FLT/CHK 2942. CDL 52-00-21 ADD DATE: 23SEP19 STA: LAX. BLUE HYDRAULIC ACCESS DOOR MISSING ON ARRIVAL INTO LAX. INSTALLED BLUE HYD ACCESS DOOR PER A319 AMM 52-41. DOOR ASSY P/N D5347508401200, STK # 09-5200-3-1172.

Part: DOUBLER — DETACHED (NR 1 NACELLE) · airframe 50,769 hrs · 25,916 cycles

ON ARRIVAL FOUND NR 1 ENGINE PYLON THUMBNAIL FAIRING DETACHED. CORR BY FANTA 00608873 SEA 19FEB19 ATA 5433. INSTALLED THUMBNAIL PANEL PER A319 AMM 54-22 AND COMPLETED PHASE 1 INSPECTION PER A319 AMM 05-51. NO DAMAGE NOTED.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 49,804 hrs · 25,494 cycles

FOUND RT EMERGENCY LIGHT POWER SUPPLY UNIT INOP. REPLACED RT EMERGENCY LIGHT POWER SUPPLY UNIT.

Part: TRUNNION — DAMAGED (LT TE FLAP) · airframe 49,153 hrs · 25,181 cycles

FOUND THE LEFT INBD FLAP TRUNNION DAMAGED, REPLACED THE TRUNNION FITTING IAW AMDS 2750-6010-LT AND CMM 57-52-21.

Part: WIRE — SHORTED (EMERGENCY LIGHT) · airframe 47,858 hrs · 24,609 cycles

EMERGENCY LIGHTS INOPERATIVE AT ROWS 1 AND 2, ON THE SEATS, REPAIRED A SHORTED WIRE IAW SWPM 20-10.

Part: SKIN — CRACKED (SERVICE DOOR) · airframe 47,289 hrs · 24,370 cycles

CRACKED EXTERNAL SKIN LOCATED AFT LOWER CORNER FWD PASSENGER DOOR RT SIDE. REPAIRED THE SKIN IAW SRM 52-10-00-300-003.

Part: SKIN — CRACKED (PAX DOOR) · airframe 47,289 hrs · 24,370 cycles

CRACKED EXTERNAL SKIN OF THE AFT LOWER CORNER OF THE LT AFT PASSENGER DOOR, PERFORMED A REPAIR IAW SRM 52-10-00-300-003.

Part: SHEAR TIE — CORRODED (FRAME 55) · airframe 47,289 hrs · 24,370 cycles

CORROSION ON THE SHEAR TIE AT FR 55 BETWEEN STRINGERS 42L TO 43L IN THE AFT CARGO COMPARTMENT, REPLACED THE SHEAR TIE IAW SRM 51-72-11 AND DRAWING D53476342.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · airframe 47,288 hrs · 24,369 cycles

CORROSION FLOOR BEAM +Y1292 LOC FROM FR64 TO FR66 AT AFT GALLEY AREA. REPLACED FLOOR BEAM +Y1292 LOC. FROM FR64 TO FR66 AT AFT GALLEY AREA AS PER A319 SRM 51-72-11 AND DWG#D53472000

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-24) · airframe 47,288 hrs · 24,369 cycles

CORROSION FLOOR BEAM +Y1292 LOC. FROM FR12 TO FR24 AT FWD GALLEY AREA, REPLACED FLOOR BEAM +Y1292 LOC. FROM FR12 TO FR24 AT FWD GALLEY AREA AS PER SRM A319 51-72-11 AND DWG #D53112812

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-24) · airframe 47,288 hrs · 24,369 cycles

CORROSION FLOOR BEAM -Y765 LOC. FROM FR12 TO FR24 AT FWD GALLEY AREA, REPLACED FLOOR BEAM -Y765 LOC. FROM FR12 TO FR24 AT FWD GALLEY AREA AS PER A319 SRM 51-72-11 AND DWGS #D53112812

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-24) · airframe 47,288 hrs · 24,369 cycles

CORROSION FLOOR BEAM -Y1292 LOC. FROM FR12 TO FR24 AT FWD GALLEY AREA, REPLACED FLOOR BEAM -Y1292 LOC. FROM FR12 TO FR24 AT FWD GALLEY AREA AS PER A319 SRM 51-72-11 AND DWG# D53112812

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-24) · airframe 47,288 hrs · 24,369 cycles

CORROSION FLOOR BEAM +Y765 FROM FR12 TO FR24 AT FWD GALLEY AREA, REPLACED FLOOR BEAM +Y765 FROM FR22 TO FR24 AT FWD GALLEY AREA AS PER SRM A319 51-72-11

Part: DUMMY RAIL — CORRODED (FRAMES 12-16) · airframe 47,288 hrs · 24,369 cycles

CORROSION RAIL DUMMY Y503.2 LOC. FR12 TO FR16 AT FWD GALLEY AREA, REPLACED RAIL DUMMY Y503.2 LOC. FR12 TO FR16 AT FWD GALLEY AREA AS PER SRM 51-42-11 AND DRAWING D53112826

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 41,478 hrs · 21,721 cycles

EMERGENCY EXIT SIGNS ABOVE RT OVERWING DOOR AND CEILING WILL NOT ILLUMINATE. REPLACED EPSU W/O BATTERY AT RT OVERWING EXIT.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 41,412 hrs · 21,693 cycles

INOPERATIVE, 12WL, EPSU IN PASSENGER CABIN, REPLACED EPSU.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 41,407 hrs · 21,692 cycles

DELAMINATED FLOOR PANEL 261BG AT AFT GALLEY AREA.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 36,156 hrs · 18,707 cycles

ROW 4 + 6 EMERGENCY IN-SEAT LIGHTS ARE INOPERATIVE. REPLACED DAMAGED HARNESS IN ROWS 4 AND 6. OPS CHECKED GOOD IAW AMM 33-51.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,515 hrs · 18,395 cycles

DURING EMERGENCY LIGHT TEST. EPSU EMERGENCY RT FAULT. R & R THE EPSU BATTERY. OPS CHECKED GOOD. EMERGENCY LIGHT TEST PASSED. ALL MX COMPLETED IAW AMM 33-51-38. ACFT OK FOR SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,644 hrs · 17,838 cycles

EMERGENCY LIGHTS TEST FAIL EPSU UNIT AFT L MESSAGE. REPLACED CHARGER, CHECKED GOOD REF AMM 33-51 EPSU, WITH OUT BATTERY .

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,605 hrs · 17,812 cycles

EMERGENCY LIGHT AT SEAT C4 INOPERATIVE. REPAIRED SEAT HARNESS AT SEAT C4. OP'S CHECKED GOOD. OK FOR SERVICE.

Part: LANYARD — DAMAGED (L1 DOOR SLIDE) · airframe 34,589 hrs · 17,803 cycles

DOOR 1 LT SLIDE DISARM PIN LANYARD DAMAGED.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,101 hrs · 17,514 cycles

SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE AT ROW 15. R & R EMERGENCY LIGHT PIGTAIL HARNESS. OPS CHECKED GOOD. OK FOR SERVICE.

Part: WIRE HARNESS — BROKEN (EMERGENCY LIGHT) · airframe 33,787 hrs · 17,332 cycles

EMERGENCY EXIT LIGHT (RED) AT 9C INOPERATIVE. FOUND WIRE HARNESS UNDER SEAT BROKEN. REPAIRED BROKEN WIRE BY INSTALLING BUTT SPICE. PERFORMED OPS CHECK. CHECKS GOOD.

Part: WIRE — UNSECURE (EMERGENCY LIGHTS) · airframe 33,111 hrs · 16,962 cycles

SEAT 19A LOOSE CABLES/WIRES. STOWED AND SECURED SEAT 19A EMERGENCY LIGHT WIRING AS REQUIRED. ACFT OK FOR SERVICE.

Part: SILL — BENT (FUSELAGE) · airframe 5,029 hrs · 2,775 cycles

FOUND FORWARD CARGO COMPT DOOR SILL WEB AND INTERCOSTAL BENT BETWEEN FR26 - FR27 APPROX STR 41R. REMOVED WEB IAW A319 SRM 51-42-11. RECEIVED NEW WEB IAW A319 SRM 53-21-13. LOCATED AND DRILLED NEW WEB IAW A319 SRM 51-44-11. TREATED AND PRIMED NEW WEB IAW A319 SRM 51-21-11. PAINTED NEW WEB IAW A319 SRM 51-75-12. INSTALLED NEW WEB IAW A319 SRM 51-42-11. UPON REMOVAL OF INTERCOSTAL WEB. FOUND NO DAMAGE ON THE DOOR SILL UPPER WEB. NO ALLOWABLE DAMAGE LIMITS PER A319 SRM 53-21-14. RETAIN FOR RECORDS.

Part: EPSU — FAULTY (CABIN) · airframe 5,029 hrs · 2,775 cycles

AIRCRAFT 3119. OVERWING EMERGENCY EXIT SIGNS FLASH WHEN TURNED ON. REMOVED AND REPLACED EPSU PER AMM. OPERATIONAL CHECK WAS GOOD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 5,029 hrs · 2,775 cycles

AFT CARGO COMPT BETWEEN FR64 TO FR65 STGR 44 VERTICAL FLOOR SUPPORT CORRODED. SSI 534107. BLENDED FLOOR SUPPORT DAMAGE DIM L=1.5" X W=.8" X D=.015 OUT OF LIMITS. REMOVED AND REPLACED NEW PROFILE FORCE SUPPORT IAW A319 SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 5,029 hrs · 2,775 cycles

MAIN CABIN FR16 FLOOR SUPPORT WEB -Y1732 HAS CORROSION. REMOVED CORROSION IAW A319 SRM 51-74-00 MAT THICKNESS. .70" L=1.3" W=1.0" D=.033". NO ESTABLISHED LIMITS. REMOVED AND REPLACED FLOOR SUPPORT WEB -Y1732 IAW A319 SRM 51-42-11.

Part: CROSSBEAM — DAMAGED (FUSELAGE) · airframe 5,029 hrs · 2,775 cycles

MAIN DECK FWD UTILITY AREA AT Y1732 FRAME 23 CROSS BEAM UPPER FLANGE LWR SURFACE HAS START DRILLED DAMAGE SSI 531189. REMOVED DAMAGED CROSSBEAM IAW A319 SRM 53-00-14FIG 203. FABRICATED NEW PARTS (CROSSBEAM AND COUPLING), INSTALLED CROSSBEAM AND COUPLING IAW A319 SRM 53-00-14 FIG 203. RETAIN FOR RECORDS.

Part: SUPPORT FITTING — GOUGED (FUSELAGE) · airframe 5,029 hrs · 2,775 cycles

FWD CARGO DOOR SILL SUPPORT FITTING 2ND FROM FWD HAS GOUGE. BLENDED AREA IAW A319 SRM 51-73-00.L=.150" W=.120" D=.030". NO ESTABLISHED LIMITS PER A319 SRM 53-26-00. REMOVED, REPLACED AND INSTALLED NEW FITTING IAW A319 SRM 51-42-11. STRINGER 645112 BFM.

Part: SILL — CORRODED (FUSELAGE) · airframe 5,029 hrs · 2,775 cycles

RIGHT AFT DOOR THRESHOLD SILL FR 66 TO FR 68 UPPER SURFACE CORRODED. REMOVED CORROSION IAW A319 SRM 51-74-00, DIMENSION OF OVERSIZE HOLE AFT INBD W=.500 X L=.850. FWD INBD W=.550 X L=.800 FOUND OUT OF LIMITS IAW A319 TRM 53-41-13 FIG.1 SHT 3DETAIL II. REMOVED AND REPLACED A NEW DOOR SILL IAW A319 SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 5,029 hrs · 2,775 cycles

MAIN CABIN FR20 FLOOR SUPPORT WEB Y1732 HAS CORROSION. BLENDED AREA IAW A319 SRM 51-74-00 DIMENSION L=1" W=1" D=.015". FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-11-14. RECEIVED NEW REPLACEMENT PART. REMOVED WEB IAW A319 SRM 51-42-11. LOCATED AND DRILLED REPLACEMENT WEB IAW A319 SRM 51-44-11. TREATED AND PRIMED IAW A319 SRM 51-21-11 AND INSTALLED IAW A319 SRM 51-42-11.

Part: FITTING — CORRODED (FUSELAGE) · airframe 5,029 hrs · 2,775 cycles

LEFT AFT DOOR LOWER AFT CORNER FITTING CORRODED. SSI 534147. BLENDED CORRODED AREA IAW A319 SRM 51-74-00 L=1.20" W=0.750" D=0.040". NO LIMIT ESTABLISHED FOR THE AREA. REMOVED AND REPLACED AFT CORNER FITTING IAW A319 SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 5,029 hrs · 2,775 cycles

AFT CABIN UTILITY AREA CABIN FLOOR SUPPORT AT FR64 TO FR66 -Y1292 UPPER BEAM SURFACE CORRODED. REMOVED CORROSION IAW A319 SRM 51-74-00 L=3.0", W=1.0" D=0.035". FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-41-15. REMOVED AND REPLACED FLOOR SUPPORT IAW A319 SRM 51-42-11. STRINGER 645112 BFM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 5,029 hrs · 2,775 cycles

AFT CABIN UTILITY AREA CABIN FLOOR SUPPORT AT FR 66 Y765 UPPER AND LOWER SURFACE HOLES CORRODED. REMOVED CORROSION IAW SRM 51-74-00. L=2"W=1" D=.040". FOUND TO BE OUT OF LIMITS IAW SRM 53-41-15. REMOVED FLOOR SUPPORT Y765 FROM FR64 - FR66. REMOVED 4EA SPLICE PLATES FR66. REMOVED 3EA SPLICE PLATES FR64. TRANSFERRED 3EA BRACKETS FROM OLD FLOOR SUPPORT TO NEW FLOOR SUPPORT. LOCATED AND DRILLED NEW FLOOR SUPPORT. TOP COATED FASTENERS IAW SRM 51-42-11 AND 51-75-12. RETAIN FOR RECORDS.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 5,029 hrs · 2,775 cycles

CABIN FLOOR SUPPORT AT FR 66 Y1292 UPPER FLANGE SURFACE HOLE CORRODED. SSI 534147. REMOVED CORROSION IAW A319 SRM 51-74-00. CHECK DIMENSION L=1.700",W=1.100",D=.055" FOUND TO BE OUT OF LIMITS IAW A319 TRM 53-41-15. TR INSTRUMENT 17451. REMOVED FLOOR SUPPORT BEAM IAW A319 SRM 51-42-11 Y1292 FR 64 TO 66. RECEIVED NEW FLOOR SUPPORT BEAM. INSTALLED NEW FLOOR SUPPORT BEAM Y1292 FR64 TO 66 IAW A319 SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 5,029 hrs · 2,775 cycles

CABIN FLOOR SUPPORT AT FR 68 TO FR 69 Y1292 UPPER FLANGE SURFACE BEAM CORRODED. SSI 534147. REMOVED CORROSION IAW A319 SRM 51-74-00. CHECK DIMENSIONS L=1.300" W=1.300"D=.014". FOUND TO BE WITHIN LIMITS IAW A319 TRM 53-41-15. TREATED AND PRIMED AREA IAW A319 SRM 51-22-00 AND PAINTED IAW A319 SRM 51-75-12. REMOVED FOR ACCESS FLOOR SUPPORT BEAM Y1292 FR 68 TO FR 69 IAW A319 SRM 51-42-11. RE-INSTALLED FLOOR SUPPORT BEAM IAW A319 SRM 51-42-11 Y1292 FR 68 TO 69.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 5,029 hrs · 2,775 cycles

CABIN FLOOR SUPPORT AT FR 66 TO FR 68 Y1292 UPPER AND LOWER FLANGE CORRODED. SSI 534147. REMOVED CORROSION IAW A319 51-74-00. CHECK DIMENSIONS L=1.500" W=1.300"D=.043". FOUND TO BE OUT OF LIMITS IAW A319 TRM 53-41-15, TR INSTRUMENT 17451, Y1292 FR 66 TO 68. REMOVED FLOOR SUPPORT BEAM IAW A319 SRM 51-42-11. RECEIVED NEW FLOOR SUPPORT BEAM. INSTALLED NEW FLOOR SUPPORT BEAM IAW A319 SRM 51-42-11 Y1292 FR 66 TO 68.

Part: HINGE FITTING — CORRODED (FUSELAGE) · airframe 5,029 hrs · 2,775 cycles

R2 DOOR AFT CORNER FITTING FR 68 CORRODED. REMOVED AND REPLACED 1 EA AFT CORNER FITTING AT R2 DOOR FR68 IAW A319 SRM 51-42-11. DAMAGE DIM L=.350" W=.200" D=.030".

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 5,029 hrs · 2,775 cycles

AFT CABIN UTILITY AREA CABIN FLOOR SUPPORT AT FR68 TO FR 69 -Y1292 UPPER FLANGE BEAM CORRODED AND SEVERAL RIVETS BROKEN. SSI 534147. REMOVED CORROSION IAW A319 SRM 51-74-00 L=2.05",W=1.05 D=0.045-. FOUND TO BE OUT OF LIMITS IAW A319 SRM 5341-15. REMOVED AND REPLACED FLOOR SUPPORT IAW A319 SRM 51-42-11. RETAIN RECORDS. STRINGER 645112 BFM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 5,029 hrs · 2,775 cycles

AFT CABIN UTILITY AREA CABIN FLOOR SUPPORT AT FR66 TO FR68 -Y1292 UPPER AND LOWER HOLES SURFACE CORRODED. SSI 534147. REMOVED CORROSION IAW A319 SRM 51-74-00 L=1.05" W=1.0" D=0.040". FOUND TO BE OUT OF LIMITS IAW A319 TRM 53-41-15. REMOVED AND REPLACED FLOOR SUPPORT IAW A319 SRM 51-42-11. RETAIN FOR RECORDS. STRINGER 645112 BFM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 5,029 hrs · 2,775 cycles

AFT UTILITY AREA CABIN FLOOR SUPPORT AT FR66 TO FR70 Y765 UPPER FLANGED CORRODED. REMOVED CORROSION IAW A319 SRM 51-74-00 OUT OF LIMITS IAW A319 SRM 51-41-15. REMOVED FLOOR SUPPORT Y765 FR66-FR70 IAW A319 SRM 51-42-11. INSTALLED NEW FLOOR SUPPORT BEAM Y765 FR66 TO FR70 IAW A319 SRM 51-42-11. DAMAGE DIAMETER L=3"W=1" D=.050".

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 5,029 hrs · 2,775 cycles

MAIN CABIN BTW FR18 AND FR20 FLOOR SUPPORT -Y254 HAS CORROSION AS MARKED. REMOVED CORROSION IAW A319 SRM 51-74-00, NO ALLOWABLE LIMITS. INSTALLED NEW BEAM IAW A319 SRM 51-42-11. RETAIN FOR RECORDS.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 5,029 hrs · 2,775 cycles

MAIN CABIN BTW FR20 AND FR21 SEAT TRACK -Y765 HAS CORROSION. REMOVED CORROSION IAW A319 SRM 51-74-00. DIM. L=.50" W=.30" D=.14-0", ORIG THICK. .147". FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-11-14 FIG 102. REMOVED FLOOR SUPPORT BEAM IAW A319 SRM 51-42-11. RECEIVED NEW FLOOR SUPPORT BEAM. INSTALLED NEW FLOOR SUPPORT BEAM IAW A319 SRM 51-42-11. RETAIN FOR RECORDS.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 5,029 hrs · 2,775 cycles

FWD CARGO COMPARTMENT SLOPE PANEL 131DG HAS PUNCTURES. FABRICATED NEW SLOPE PANEL 131DG IAW DWG# 3D25-40532. DAMAGE DIA L=3.75" X W=4.0". RETAIN FOR RECORDS.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 5,029 hrs · 2,775 cycles

FWD CARGO COMPARTMENT SLOPE PANEL 132EG HAS PUNCTURES. FABRICATED NEW SLOPE PANEL 132EG IAW DWG# 3D25-40532. DAMAGE DIA. L=4.5" X W=3.5".

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 5,029 hrs · 2,775 cycles

FLOOR SUPPORT AT FR65 TO FR67 -Y583 SEVERAL HOLES POINT CORRODED. REMOVED CORROSION IAW SRM 51-74-00. NO LIMITS FOR ALLOWABLE DAMAGE. REMOVED AND REPLACED NEW FLOOR SUPPORT IAW A319 SRM 51-42-11. RETAIN FOR RECORDS.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 5,029 hrs · 2,775 cycles

FWD CARGO COMPARTMENT SLOPE PANEL 132DG HAS MULTIPLE PUNCTURES. FABRICATED NEW SLOPE PANEL 132DG IAW DWG# 3D25-40532. DAMAGE DIA. L=2.0" X W=2.0".

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 5,029 hrs · 2,775 cycles

FWD CARGO COMPARTMENT FLOOR PANEL 131CG HAS MULTIPLE PUNCTURES AND DELAMINATED. FABRICATED FLOOR PANEL. DAMAGE DIM. L=5.6" X W=5.6".

Part: FITTING — CORRODED (PAX DOOR) · airframe 5,029 hrs · 2,775 cycles

LT FORWARD PASSENGER DOOR ENTRANCE FWD CORNER FITTING UPPER FLANGE HOLES & NUT PLATES CORRODED. REMOVED OLD FITTING IAW A319 SRM 51-42-11. RECEIVED NEW FITTING LOCATED AND DRILLED NEW FITTING AND INSTALLED NEW NUT PLATES IAW A319 SRM 51-44-11 & 51-42-11. INSTALLED NEW FITTING IAW A319 SRM 51-42-11.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 5,029 hrs · 2,775 cycles

AFT CARGO SLOPE PANEL 152WG DELAMINATED. AFT CARGO SLOPE PANEL 152WG FABRICATED NEW IAW DWG 3D25-40532. DAMAGE DIA. L= 1.75" X W=1.0". RETAIN FOR RECORDS.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 5,029 hrs · 2,775 cycles

AFT CABIN UTILITY AREA CABIN FLOOR SUPPORT FR64TO FR70 -Y512. SEVERAL HOLES POINT CORRODED. REMOVED CORROSION IAW SRM 51-74-00. NO ESTABLISHED LIMITS FOR ALLOWABLE DAMAGE. REMOVED FLOOR SUPPORT -Y512 IAW A319 SRM 51-42-11. RECEIVED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT -Y512 IAW A319 SRM 51-42-11. PAINTED FASTENERS IAW A319 SRM 51-75-12. RETAIN FOR RECORDS.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 5,029 hrs · 2,775 cycles

FLOOR PANEL 242KF DELAMINATED. FLOOR PANEL 242KF FABRICATED NEW ON STAM TRAVELER T12/920944 P/N DA-D5367161600100 IAW DWG# 3D25-40640. DAMAGE DIM. L=3.5" X W=3.5".

Part: FLOOR PANEL — DELAMINATED (CARGO ABY) · airframe 5,029 hrs · 2,775 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 151ZG DELAMINATED. FABRICATED FLOOR PANEL 151ZG ON STAM TRAVELER T12/921125 IAW DWG# 3D25-40532. DAMAGE DIM. L=4.5" X W=3.75".

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 5,029 hrs · 2,775 cycles

FWD CABIN FLOOR PANEL 231KF IS DELAMINATED, 18" X 3" AREA FWD CABIN FLOOR PANEL 231KF. FABRICATED NEW ON STAM TRAVELER T12/921249 P/N DA-5367160100000 IAW DWG 3D25-4D640.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 5,029 hrs · 2,775 cycles

MAIN CABIN BTW FR20 AND FR22 SEAT TRACK -Y1292 HAS CORROSION. SSI 531189. BLENDED CORRODED AREA IAW A319 SRM 51-74-00. DIM; L=1.2, W= .70" D=.030", FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-11-14. REMOVED FLOOR SUPPORT BEAM. LOCATED AND DRILLED NEW FLOOR SUPPORT BEAM IAW A319 SRM 51-44-11. INSTALLED NEW FLOOR SUPPORT BEAM IAW A319 SRM 51-42-11. RETAIN FOR RECORDS.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 5,029 hrs · 2,775 cycles

FLOOR PANEL 241KF DELAMINATED. FLOOR PANEL 241KF FABRICATED NEW ON STAM TRAVELER T12/920943 P/N DA-D5367161600000 IAW DWG 3D25-40640. DAMAGE DIM. L=2.75" X W=3.75.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 5,029 hrs · 2,775 cycles

MAIN CABIN BTW FR18 AND FR20 FLOOR SUPPORT Y254 HAS CORROSION. BLENDED CORRODED AREA IAW A319 SRM 51-74-00.L=2.0" W=1.5" D=0.050",ORIG THICKNESS =0.063 OUT OF LIMITS IAW A319 SRM 53-0014 FIG 102, REMOVED FLOOR SUPPORT BEAM IAW A319 SRM 51-42-11. INSTALLED NEW FLOOR SUPPORT BEAM IAW A319 SRM 51-42-11.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 5,029 hrs · 2,775 cycles

DURING NON ROUTINE CHECK, MAINTENANCE FOUND AFT CABIN UTILITY AREA LT SIDE AT FR 69-70 FRAME SUPPORT ATTACHMENT TO SHEAR PLATE CORRODED. REMOVED WEB SUPPORT FRAME FR69 TO 70 IAW A319 SRM 51-42-11. INSTALLED NEW WEB SUPPORT FRAME IAW A319 SRM 51-42-11.

Part: PANEL — CHAFED (TE FLAP) · airframe 5,029 hrs · 2,775 cycles

DURING NON ROUTINE CHECK, MAINTENANCE FOUND LEFT INBD FLAP SLIDING PANEL UPPER SURFACE HAS CHAFED MARK. BLENDED CHAFED MARK AREA IAW A319 SRM 51-73-00. FOUND TO BE IN LIMITS IAW ER/A 13 484369-14MA. REPAIR ACCOMPLISHED IAW ER/A 13 484369-14MA. IDENTIFIED REPAIR AS ENG.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 5,029 hrs · 2,775 cycles

AFT CABIN FLOOR PANEL 261FF IS CORRODED IN SEVERAL AREAS, 10"X2". RECEIVED NEW PANEL P/N D5367180500400 TO BE INSTALLED ON WORK CARD 2500-6602.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 5,029 hrs · 2,775 cycles

FWD CABIN ENTRY WAY FLOOR PANEL 222FF IS CORRODED, 6"X 3" AREA. RECEIVED NEW PANEL P/N E5367147800700 TO BE INSTALLED ON WORK CARD 2500-6617 (DAMAGE DIM. L=6" W=3" D=.025").

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 5,029 hrs · 2,775 cycles

AFT CABIN FLOOR PANEL 262FF IS CORRODED, 6"X 4" AREA. RECEIVED NEW PANEL P/N D5367180500500 TO INSTALLED ON WORK CARD 2500-6602 (DAMAGE DIM. L=6" W=4" D=.025").

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 5,029 hrs · 2,775 cycles

FWD CABIN ENTRY WAY FLOOR PANEL 221FF IS CORRODED, 6"X 2" AREA. RECEIVED NEW PANEL P/N E5367147801200 TO BE INSTALLED ON WORKCARD 2500-6617 (DAMAGE DIM. L=6" W=2" D=.025").

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 5,029 hrs · 2,775 cycles

MAIN CABIN FR 14 FLOOR SUPPORT WEB Y1732 HAS CORROSION. REMOVED AND REPLACED FLOOR SUPPORT WEB AT Y1732 IAW A319 SRM 51-42-11. LOCATED & DRILLED NEW FLOOR SUPPORT WEB IAW A319 SRM 51-44-11 (DAMAGE DIM. L=1" W=.4" D=.048" ORIG MAT.063").

Part: SILL — CORRODED (FUSELAGE) · airframe 5,029 hrs · 2,775 cycles

DURING NON ROUTINE CHECK, MAINTENANCE FOUND LEFT AFT DOOR THRESHOLD SILL ENTRANCE AT FORWARD FR 66 UPPER SURFACE CORRODED. REMOVED CORROSION IAW A319 SRM 51-74-00 L=1.6" W=.900" D=.052" ORIG MAT .150" FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-41-14 FIG 101. INSTALLED REPAIR PARTS IAW A319 SRM 51-42-11 AND SRM 53-41-14.

Part: BLANKING PLATE — CORRODED (R2 DOOR) · airframe 5,029 hrs · 2,775 cycles

R2 DOOR AFT BLANKING PLATE CORRODED (PNL RACK). R2 DOOR AFT BLANKING PLATE REPLACED IAW A319 SRM 51-72-00 P/N D5348015900700.

Part: PLATE — CORRODED (L2 DOOR) · airframe 5,029 hrs · 2,775 cycles

L2 DOOR FWD AND AFT BLANKING PLATES CORRODED (PNL RACK). REPLACED L2 DOOR FWD AND AFT BLANKING PLATES IAW A319 SRM 51-72-00 P/N 5348015800600 AND P/N D5398015900200.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 5,029 hrs · 2,775 cycles

MAIN CABIN BETWEEN FR15 AND FR16 FLOOR SUPPORT -Y1379.5 HAS CORROSION. BLENDED AREA HARD POINT L=1.00", W=1.50" D=.007" ORIG MAT.163" OUT OF LIMITS IAW A319 SRM 51-74-00. REMOVED FLOOR SUPPORT -Y1379.5 IAW A319 SRM 51-42-11. INSTALLED NEW FLOOR SUPPORT IAW A319 SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 5,029 hrs · 2,775 cycles

DURING NON ROUTINE CHECK, FOUND MAIN CABIN FR20 FLOOR SUPPORT WEB -Y1732 HAS CORROSION. REMOVED FLOOR SUPPORT. LOCATED,DRILLED AND INSTALLED NEW FLOOR SUPPORT PER SRM 53-00-14, 51-42-11 AND 51-44-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 5,029 hrs · 2,775 cycles

DURING NON ROUTINE CHECK, FOUND CABIN FLOOR SUPPORT AT FR 68 TO FR 70 Y254 WITH SEVERAL HOLES POINT. REMOVED CORROSION, DRILLED FLOOR SUPPORT AND INSTALLED CABIN FLOOR SUPPORT PER SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 5,029 hrs · 2,775 cycles

DURING NON ROUTINE CHECK, FOUND MAIN CABIN BETWEEN FR14 AND FR16 FLOOR SUPPORT Y503 HAS CORROSION. REMOVED CORROSION AND REPLACED Y503.2 FLOOR SUPPORT IAW A319 SRM 51-42-11.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 5,029 hrs · 2,775 cycles

DURING NON ROUTINE CHECK, FOUND LEFT AFT DOOR THRESHOLD SILL AT 68 UPPER SURFACE CORRODED. REMOVED CORROSION, FABRICATED 2EA FILLER MATERIAL 7075 T6 .063" BATCH# 2026472 AND INSTALLED REPAIR PARTS IAW A319 SRM 51-42-11 AND SRM 53-41-14 FIG 201.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 5,029 hrs · 2,775 cycles

MAIN CABIN FR21 FLOOR SUPPORT -Y189 HAS CORROSION AS MARK. REMOVED CORROSION IAW A319 SRM 51-74-00 DIMENSION L=.800" W=.300" D=.040" ORIG. MAT .075" FOUND TO OUT OF LIMITS IAW A319 SRM 53-11-14 FIG 104. REMOVED FLOOR SUPPORT BEAM IAW A319 SRM 51-42-11. RECEIVED NEW FLOOR SUPPORT (PRE-DRILLED). INSTALLED NEW FLOOR SUPPORT -Y189 IAW A319 SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 5,029 hrs · 2,775 cycles

DURING NON ROUTINE CHECK, FOUND CABIN FLOOR SUPPORT AT FR64 TO FR70 -Y465 SEVERAL HOLES POINT CORRODED. REMOVED CORROSION IAW A319 SRM 51-74-00 FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-00-14 FIG 02. ORIG MAT. .155" DAMAGE DIA. L=1.3" X W=.930" X D=.080". REPLACED FLOOR SUPPORT BEAM P/N D5347228400800 IAW A319 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 5,029 hrs · 2,775 cycles

DURING NON ROUTINE CHECK, MAINTENANCE FOUND MAIN CABIN BETWEEN FR12 AND FR13 SEAT TRACK Y1292 HAS CORROSION. REMOVED AND REPLACED A NEW SEAT TRACK P/N D5311281300051 AND RE-INSTALLED CLIPS, BRACKETS & PAN AT FR12-FR13 Y1292 PER SRM 51-42-11 FIG 102.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 5,029 hrs · 2,775 cycles

DURING NON ROUTINE CHECK, FOUND AFT CABIN UTILITY AREA CABIN FLOOR SUPPORT AT FR64 TO FR66-Y765 UPPER SURFACE BEAM CORRODED. FLOOR SUPPORT FOUND TO BE OUT OF LIMITS IAW A319 TRM 53-41-15. REPLACED FLOOR SUPPORT P/N D534219020300 IAW A319 SRM 51-42-11.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHT) · airframe 5,014 hrs · 2,769 cycles

SEAT EXIT PATH LIGHT AT 14 LEFT INOPERATIVE. COMPLETED HARNESS SPLICE REPAIR. OPERATIONAL CHECK IS GOOD (2012-00083) 887448 MSP.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 28,833 hrs · 14,453 cycles

DURING A NON ROUTINE CHECK, FOUND THE EMERGENCY PATH LIGHT AT ROW 11ABC INOPERATIVE. MX REPAIRED A LOOSE WIRE AND FUNCTIONAL CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.

Part: CYLINDER DAMPER — DISCHARGED (PAX DOOR) · airframe 19,454 hrs · 9,754 cycles

DURING LINE CHECK, FOUND RT AFT CABIN DOOR EMERGENCY OPERATION CYLINDER PRESSURE AT ZERO. MSP LINE MAINTENANCE REPLACED DOOR CYLINDER PER AMM 52-13-14.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHT) · airframe 12,676 hrs

LEFT OVERWING EMERGENCY LIGHT POWER SUPPLY FAILS TEST. CORRECTED BY REPLACING LEFT OVERWING EPSU, CHECKS OK.