N324NB

Part: OXYGEN MASK — UNWANTED DEPLOY (ZONE 200) · airframe 63,054 hrs · 32,844 cycles

SEAT 10E O2 MASK DEPLOYED NOTED WHILE DEPLANING. CORRECTIVE ACTION: ESTOWED MASK PER A319 AMM 35-21, OK FOR SERVICE. (7936350)

Part: WIRE — DAMAGED (ZONE 200) · airframe 62,751 hrs · 32,678 cycles

LEFT AFT PASS/CREW DOOR EMERGENCY OVHD EXIT SIGN AND PATH LIGHTING INOP. REPAIRED WIRING PER A330 AMM 33-51. OK FOR SERVICE. (7961126)

Part: MICROPHONE — INOPERATIVE (OXYGEN MASK) · airframe 62,735 hrs · 32,668 cycles

CAPT SIDE O2 MASK MIC INOPERATIVE. R & R CAPT SIDE O2 MASK STORAGE BOX PER A 319 AMM 35-12. (7961120).

Part: OXYGEN MASK — DISLODGED (ZONE 200) · airframe 62,631 hrs · 32,601 cycles

L1 DOOR OXYGEN MASK DROPPED ON LANDING. STOWED THE L1 O2 MASK IAW AMM 35-21-41. (7786072).

Part: FITTING — DAMAGED (ZONE 300) · airframe 62,534 hrs · 32,543 cycles

RUDDER HINGE LINE BEARING BR4 A/C SIDE, LOWER FITTING HAS A GOUGE ON BOTTOM SIDE. COMPLIED WITH ER/A 629674-14. (1257741).

Part: FITTING — DAMAGED (ZONE 300) · airframe 62,534 hrs · 32,543 cycles

RUDDER HINGE LINE BEARING BR4 A/C SIDE TOP SIDE FITTING HAS DRILL START ON O/B SIDE OF #7 HOLE. COMPLIED WITH ER/A 629674-14. (1257738)

Part: PLATE — CRACKED (RUDDER HINGE) · airframe 62,534 hrs · 32,543 cycles

SHIP 3124 RUDDER HINGE #3 BOTTOM PLATE HAS A CRACK INDICATION IN HOLE #7. CORRECTIVE ACTION: COMPLIED WITH ER/A 629756-14. (1257519).

Part: FRAME — CRACKED · airframe 62,525 hrs · 32,538 cycles

CRACK INDICATION WAS FOUND AT FASTENER HOLE NR 6. COMPLIED QITH ER/A 614228-14AD. (1255318).

Part: HINGE ARM — CORRODED (ZONE 300) · airframe 62,525 hrs · 32,538 cycles

VERTICAL STABILIZER RUDDER HINGE ARM BR3 CRACKED HOLE. REPAIRED PER ER/A 629756-14. (1255486)

Part: BUSHING — EXCESS PLAY (ZONE 500 SPOILER) · airframe 62,525 hrs · 32,538 cycles

LEFT WING NR 2 SPOILER CENTER HINGE FITTING TO WING HAS EXCESSIVE PLAY. REPLACED BUSHINGS PER A319 CMM 57-72-21. (1253102)

Part: ROLLER — BINDING (ZONE 600 FLAP) · airframe 62,525 hrs · 32,538 cycles

RIGHT WING OTBD FLAP INBD GUIDE ROLLER BINDING WHEN ROLLING WITH PRESSURE ON IT. REPLACED OTBD FLAP CRUISE ROLLER IAW CMM 57-53-21 AND ADJUSTED CRUISE ROLLER IAW AMM SUBTASK 27-54- 62-820-052-C. (1252270)

Part: ROLLER — BINDING (ZONE 500 FLAP) · airframe 62,525 hrs · 32,538 cycles

LEFT WING OTBD FLAP INBD GUIDE ROLLER BINDING WHEN PRESSURE APPLIED AND TRYING TO ROLL. REPLACED OTBD FLAP CRUISE ROLLER IAW CMM 57-53-21 AND ADJUSTED CRUISE ROLLER IAW AMM SUBTASK 27-54- 62-820-052-C. (1250793)

Part: RETAINER — CORRODED (ZONE 900) · airframe 62,525 hrs · 32,538 cycles

SHIP 3124 G5 GALLEY HAS DELAMINATION REPORTED IN TROLLEY RETAINER BLOCK COMPARTMENT 510, 511, AND 512 ON EMPOWER NR 327, 328, AND 329. CORRECTIVE ACTION: REPLACED PER ERA 629680-14. (1249884)

Part: PIN — NOT SEATED (ZONE 800) · airframe 62,525 hrs · 32,538 cycles

DURING INSTALLATION AND RE-ARMING PROCEDURE OF THE L/H OVERWING EMERGENCY EXIT HATCH, LATCH PIN WILL NOT SEAT AND LOCK IN ARMED POSITION. CORRECTIVE ACTION: RE-ARMED ESCAPE SLIDE RELEASE MECHANISM REF A319 AMM 52-21-11-400-001-A. (1247239).

Part: STRUT — OUT OF TOLERANCE (ZONE 500 FLAP) · airframe 62,525 hrs · 32,538 cycles

LT WING FLAP INTERCONNECT STRUT FAILS RADIAL PLAY CHECK. REPLACED AND ADJUSTED INTERCONNECT STRUT REF A319 AMM 27-51-44. (1239803)

Part: STRUT — OUT OF TOLERANCE (ZONE 600 FLAP) · airframe 62,525 hrs · 32,538 cycles

RIGHT FLAP INTERCONNECT STRUT FAILED RADIAL PLAY DIMENSION CHECK. REPLACED AND ADJUSTED INTERCONNECT STRUT REF A319 AMM 27-51-44. (1239789)

Part: RETAINER — CORRODED (ZONE 900) · airframe 62,525 hrs · 32,538 cycles

SHIP 3124 BUFFET AND GALLEY G5 GALLEY CORROSION. CORRECTIVE ACTION: REPLACEMENT OF ALL TROLLEY RETAINER BLOCKS ( COMPARTMENTS 510, 511, AND 512) OF G5 GALLEY PER ER/A 629680-14. (1232453)

Part: SKIN — DENTED (ZONE 200) · airframe 62,525 hrs · 32,538 cycles

AFT FUSELAGE TOP SURFACE JUST RIGHT OF RUDDER CENTER HAS A DENT. ASSESSED DENT PER A319 SRM 53-51-11-283-024. (1230717).

Part: SWITCH — STICKING (ZONE 800) · airframe 61,902 hrs · 32,192 cycles

SHIP 3124 GROUND PERSONAL REPORTED AFT CARGO DOOR SWITCH STICKING IN THE OPEN POSITION. REMOVED AND REPLACED AFT CARGO MANUAL SELECTOR VALVE IAW A319 AMM 52-36.

Part: WIRE — DAMAGED (ZONE 100) · airframe 60,099 hrs · 31,277 cycles

SHIP 3124 FORWARD CARGO DOOR INDICATION INOP. CORRECTIVE ACTION: REPAIRED WIRE 5235-5035 AS REQ'D REF A319 AWM 52-35 & ESPM 20-53. OK FOR SERVICE. (5447792)

Part: RADOME — NO DISCREPANCY (ZONE 100) · airframe 59,986 hrs · 31,226 cycles

SHIP 3124 BIRD STRIKE ON LANDING 250 KTS. BIRD RIGHT SIDE OF RADOME. CORRECTIVE ACTION: R/R RADOME IAW A319 AMM 53-15 C/W POWER ASSURANCE CHECK IAW A319 AMM 71-00-00-00-710-008-A. ALL CHECKS GOOD A/C OK FOR SVC. (5447770)

Part: APU — ODOR (ZONE 100) · airframe 59,729 hrs · 31,088 cycles

SHIP 3124 FA AFT SMELLED STRONG MUSTY DIRTY SOCK ODOR. CORRECTIVE ACTION: APU CHANGED PER W/C 4900-9002, FCS DECONTAMINATION ON W/C 2100-2003 AND COMPARTMENT WASH ON W/C 4916-2001. (4011142)

Part: UNKNOWN — ODOR (CABIN) · airframe 59,723 hrs · 31,084 cycles

SHIP 3124 CREW SMELLED "DIRTY SOCK" ODOR THROUGHOUT CABIN STRONG ODOR. CORRECTIVE ACTION: COMPLETED WC 2100-2003. WC 0550-2002 C/W. W/C 4900-2001. (4011136)

Part: COOLING FAN — ODOR (ZONE 100) · airframe 59,716 hrs · 31,080 cycles

SHIP 3124 PILOTS SMELLED "DIRTY SOCK" ODOR. CORRECTIVE ACTION: REMOVED AND REPLACED COOLING FAN PER A 319 AMM 49-52. (4011126)

Part: BEARING — CORRODED (LT FLAP TRACK) · airframe 59,135 hrs · 30,755 cycles

SHIP 3124 CORROSION LH WING INB FLAP TRACK 2 BEARING AT RIB 9 LEVEL / INB & OUTB PLATES. CORRECTIVE ACTION: REPAIRED PER ER/A 614887-14. (0441615)

Part: CROSSBEAM — CRACKED (ZONE 200) · airframe 59,126 hrs · 30,748 cycles

SHIP 3124 CROSSBEAM JUNCTION AREA AT FR20 LH CRACKED HOLES 25 AND 26. CORRECTIVE ACTIONS: REPAIRED PER ER/A 614242-14AD. (0440204)

Part: CROSSBEAM — CRACKED (ZONE 200) · airframe 59,126 hrs · 30,748 cycles

SHIP 3124 CROSSBEAM JUNCTION AREA AT FR20 LH CRACKED HOLES 25 AND 26. CORRECTIVE ACTION: REPAIRED PER ER/A 614242-14AD. (0440185)

Part: UNKNOWN — ODOR (CABIN) · airframe 58,345 hrs · 30,330 cycles

SHIP 3124 SWEET SMELL FROM BLEED SYS UPON STARING APU ON GND. CORRECTIVE ACTION: INSPECTED ENGINES AND APU PER WORK CARD 0550-2002 FOR LEAKS AND SIGNS OF FLUID CONTAMINATION NO LEAKS NOTED. REPLACED RECIRC FILTERS PER A319 AMM 21-21 OP GOOD. (0274021)

Part: UNKNOWN — ODOR (CABIN) · airframe 58,345 hrs · 30,330 cycles

SHIP 3124 STRONG SMELL OF BURNING RADIATOR FLUID (SWEET TYPE) WHEN SWITCHING ON APU BLEED LASTED ABOUT 30 SECONDS. CORRECTIVE ACTION: INSPECTED ENGINES AND APU PER WORK CARD 0550-2002 FOR LEAKS AND SIGNS OF FLUID CONTAMINATION NO LEAKS NOTED. REPLACED RECIRC FILTERS PER A319 AMM 21-21 OP GOOD. (5744849)

Part: UNKNOWN — ODOR (CABIN) · airframe 58,353 hrs · 30,335 cycles

SHIP 3124 SMOKE AND FUMES EVENT POSSIBLY DUE TO INGESTION OF FLUIDS BY APU. CORRECTIVE ACTION: INSPECTED ENGINES AND APU PER WORK CARD 0550-2002, R&R AVIONICS RECIRC FILTER PER AMM 21-26. (0274659)

Part: ROD — EXCESS PLAY (RUDDER) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 EXCESSIVE PLAY SPRING ROD RUDDER MECHANISM ON VERTICAL STABILIZER. CORRECTIVE ACTION: REPLACED SPRING ROD RUDDER MECHANISM ON VERTICAL STABILIZER AS PER A320 FAM AMM 27-21-48-000-001-A AND AMM 27-21-48-400-001- A. (0201017)

Part: PENDULUM — CORRODED (TE FLAP) · corrosion level 2 · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION ON O/B FLAP O/B PENDULUM LH WING REFER TO AMDS CARD 2750-6020-LT. CORRECTIVE ACTION: REPAIRED PER ER/A 614884-14. (0200838)

Part: FRAME — CRACKED (FRM 16) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CRACK INDICATION FOUND ON FR16 RH SIDE DOUBLE JOGGLE AREA LOCATED IN HOLE 6. CORRECTIVE ACTION: REPAIRED PER ER/A 614228-14AD. (0201028)

Part: HINGE FITTING — CORRODED (LT MLG DOOR) · corrosion level 2 · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION WAS FOUND ON THE FORWARD FACE OF THE LH MLG DOOR HINGE FITTING FORWARD LUG. CORRECTIVE ACTION: REPAIRED PER ER/A # 544078-14AD. (0201169)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 MATERIAL BURRED (OVALIZATION) ON LOWER LATERAL FITTING RH SIDE ON RACK 80VU (AD RELATED 2515-01014-02B). CORRECTIVE ACTION: REPAIRED PER ER/A 614456-14AD. (0200845)

Part: BEARING — CORRODED (RT NR 3 FLAP) · corrosion level 2 · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION ON HOUSING OF FLAP BEARING LOC. TRACK 3 OF O/B FLAP R /H WING. CORRECTIVE ACTION: REPAIRED PER ER/A # 614897-14. (0201984)

Part: HINGE FITTING — CORRODED (LT MLG DOOR) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION WAS FOUND ON THE FORWARD FACE OF THE LH MLG DOOR HINGE FITTING FORWARD LUG. CORRECTIVE ACTION: REPAIRED PER ER/A # 544078-14AD. (0201162)

Part: PENDULUM — CORRODED (TE FLAP) · corrosion level 2 · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION ON O/B FLAP O/B PENDULUM RH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 614888-14. (0200891)

Part: PENDULUM — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION ON I/B FLAP PENDULUM LH WING. CORRECTIVE ACTION: PERFORMED SANDING PROCESS TO REMOVED CORROSION AS PER A319 SRM 51-74-00-801 AND SRM 51-73- 00-801. (0201567)

Part: PENDULUM — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION ON I/B FLAP PENDULUM LH WING. CORRECTIVE ACTION: REPAIRED PER ER/A # 614887-14. (0201538)

Part: CROSSBEAM — CRACKED (FRM 20) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CRACK INDICATION ON FRAME 20 LH SIDE CROSSBEAM SPLICING AREA HOLE H25. CORRECTIVE ACTION: REPAIRED PER ER/A 614242-14AD. (0200384)

Part: BEARING — EXCESS PLAY (LT WING TE FLAP) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 EXCESSIVE PLAY ON I/B FLAP O/B DRIVE ARM BEARING L/H WING. CORRECTIVE ACTION: REPLACED BRACKET BEARING ASSY ON I/B FLAP O/B DRIVE ARM BEARING L/H WING AS PER AIRBUS CMM 57-52-21-040-005-B01. (0200026)

Part: FLAP TRACK — CORRODED (RT TE FLAP) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION FOUND ON THE RH WING OUTB'D FLAP INB'D AND OUTB'D AT TRACK #3, IN THE INNER AND OUTER RIB 5 ECCENTRIC BEARING AREA. CORRECTIVE ACTION: REPAIRED PER ER/A 614897-14. (0198762)

Part: BUSHING — MIGRATED (RT MLG ACTUATOR) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 MIGRATED FITTING BUSHINGS FWD RH ACTUATOR (FWD AND AFT LUG) IN MAIN WHEEL WELL. CORRECTIVE ACTION: REPLACED PER ER/A 614254-14AD. (0197551)

Part: BUSHING — MIGRATED (LT MLG WW) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 MIGRATED FITTING BUSHINGS FWD LH ACTUATOR (FWD AND AFT LUG) IN MAIN WHEEL WELL. CORRECTIVE ACTION: REPLACED PER ER/A 614605-14A. (0195957)

Part: LUG — CORRODED · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION FOUND ON OUTB'D INB'D LUG BORES OF THE PENDULUM SUPPORT ASSY. CORRECTIVE ACTION: REPAIRED PER ER/A 614884-14. (0195827)

Part: FRAME — CRACKED (FRM 20) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CRACK INDICATION FOUND ON OPEN HOLE 6 FR20RH DOUBLE JOGGLE. CORRECTIVE ACTION: REPAIRED PER ER/A 614198-14AD. (0195890)

Part: HINGE FITTING — CORRODED (LT MLG DOOR) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION WAS FOUND ON THE FORWARD FACE OF THE LH MLG DOOR HINGE FITTING FORWARD LUG. CORRECTIVE ACTION: REPAIRED PER ER/A 31-544078. (0196084)

Part: FAIRING — CRACKED (FRM 52) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CRACK WEB BELLY FAIRING AT LEVEL FR52 LH SIDE AT LOWER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER ER/A 615016 -14. (0196222)

Part: BUSHING — MIGRATED (RT MLG WW) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 DAMAGE ON DOOR RH FWD FITTING BUSHINGS (FWD LUG) AT MAIN WHEEL WELL. CORRECTIVE ACTION: REPAIRED PER ER/A 614558-14AD. (0195946)

Part: SEAT TRACK — CORRODED (FRMS 64-66) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 DAMAGED SEAT TRACK -Y1292 LOC. BTW FR64 TO FR66 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED PER ER/A 614478-14. (0196218)

Part: FITTING — UNKNOWN (RT MLG DOOR) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 RH MLG DOOR KEEL BEAM/ACTUATOR FITTING FWD AND AFT LUG REPLACEMENT. CORRECTIVE ACTION: REPLACED PER ER/A 31-614254. (0194236)

Part: BEARING — CORRODED (LT FLAP TRACK) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 LH WING/INB FLAP/TRACK 2 BEARING AT RIB 9 LEVEL/INB & OUTB'D PLATES/ CORROSION. CORRECTIVE ACTION: REPAIRED PER ER/A 31-614887. (0193526)

Part: FLOORBEAM — CORRODED (FRM 20) · corrosion level 2 · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION FLOOR BEAM -Y1292 LOCATED LEVEL FR 20 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y1292 LOCATED BTW FR12 TO FR24 AT FWD GALLEY AREA AS PER A319 SRM 51-72-11. (0193282).

Part: FLAP TRACK — CORRODED (RT NR 4) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 RH WING/OUTBOARD FLAP ASSY/AT FLAP TRACK #4 LEVEL/PENDULUM SUPPORT/ CORROSION. CORRECTIVE ACTION: REPAIRED PER ER/A 614888-14. (0193041).

Part: PLATE — CORRODED (FRM 70) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION ON PERIMETRAL PLATE AT FR 70 (1EA). CORRECTIVE ACTION: REPAIRED PER ER/A 614586-14. (0190490).

Part: DOOR FRAME — CRACKED (FRM 16) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 FR16RH AT DOOR STOP NO 7 LEVEL, DBL JGL AREA / FASTENER HOLE #6 CRACK. CORRECTIVE ACTION: REPAIRED PER ER/A 614228-14. (0191951).

Part: DOOR FRAME — CRACKED (FRM 16) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 FR16RH AT DOOR STOP NO 7 LEVEL, DBL JGL AREA / FASTENER HOLE #6 CRACK. CORRECTIVE ACTION: REPAIR PER ER/A 614198-14. (0191626).

Part: ELECTRICAL BOX — CRACKED (RT NACELLE) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CRACK ELECTRIC JUNCTION BOXES FWD POSITION OB SIDE ON RH PYLON. CORRECTIVE ACTION: REPAIRED PER E.R/A # 563665-14MA. (0189822)

Part: PLATE — CRACKED (NR 5 SLAT TRACK) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CRACK CLOSING PLATE SLAT TRACK 5 AND SLAT TRACK 11 ON RH WING. CORRECTIVE ACTION: REPLACED CLOSING PLATE SLAT TRACK 5 AND SLAT TRACK 11 ON RH WING AS PER A320 FAM AMM 27-84-69-000-001-A AND AMM 27-84-69-400-001-A. (0189809)

Part: PROFILE — CRACKED (EMERGENCY EXIT) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CRACK AFT LOAD TRANSMITTING PROFIL LOC INTERNAL AREA EMERGENCY EXIT DO OR 844 PASSENGER CABIN. CORRECTIVE ACTION: REPAIRED PER ER/A 614593-14AD. (0188603)

Part: NUT — CORRODED (FLAP TRACK BOLT) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION ON NUT OF FLAP CARRIAGE BOLT OF TRACK #4 O/B FLAP (1 E/A) L/H WING. CORRECTIVE ACTION: REPLACED NUT OF FLAP CARRIAGE BOLT OF TRACK #4 (1 E/A) L/H WING INSTALLATION IS TO BE ACCOMPLISHED AS PER AMDS CARD 2750-6020-LT. (0188571)

Part: CROSSBEAM — CRACKED (FRM 20) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CRACKS FOUND IN HOLE #25 AND HOLE #26 OF FR 20 LHS CROSSBEAM SPLICING. CORRECTIVE ACTION: REPAIRED PER ER/A 614242-14. (0186903)

Part: BUSHING — CORRODED (RT MLG) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION ON BUSHING OF LOWER TORQUE LINK AND NUT ON TORQUE LINK MLG RH. CORRECTIVE ACTION: REPLACED TORQUE LINK PIN (3) SLEEVE (16) AND R/H MLG NUT (18) ON R/H MLG AS PER A320 FAM AMM 32-11-29-000-001-A. (0186731)

Part: DOOR — CRACKED (EMERGENCY EXIT) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CRACKS WERE FOUND IN EMERGENCY EXIT DOOR 834 (LHS) & 844 (RHS). CORRECTIVE ACTION: REPAIRED PER ER/A 614593-14AD. (0185890)

Part: BUSHING — CORRODED (LT WING TE FLAP) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION ON BUSHING OF O/B FLAP DRIVE ARM O/B POSITION AFT SIDE 2E/A ON LH WING. CORRECTIVE ACTION: REPLACED BUSHINGS (2EA) ON O/B FLAP DRIVE ARM O/B SIDE AFT POSITION LH WING AS PER AIRBUS CMM 57-53-21, A319 SRM 51-21-00-801 AND A319 SRM 51-74-00-801. (0185494)

Part: BUSHING — CORRODED (LT WING TE FLAP) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION ON BUSHING OF O/B FLAP DRIVE ARM I/B POSITION AFT SIDE 2E/A ON LH WING. CORRECTIVE ACTION: REPLACED BUSHINGS (2E/A) OF O/B FLAP DRIVE ARM I/B POSITION AFT SIDE L/H PER AIRBUS CMM 57-53-21. (0185487)

Part: BLOCK — DAMAGED (GALLEY TROLLEY) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 WORKDECK ASSY WAS FOUND WITH SEVERAL DENTS AND CORROSION DAMAGE WAS FOUND IN THE TROLLEY RETAINER BLOCKS ON LOWER SKIN OF G1 FWD GALLEY. CORRECTIVE ACTION: REPAIRED PER ER/A 614688-14. (0185502)

Part: BUSHING — CORRODED (RT MLG) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION ON BUSHING OF LOWER TORQUE LINK, AND CORROSION ON APEX PIN AND NUT ON TORQUE LINK MLG RH. CORRECTIVE ACTION: REPLACED TORQUE LINK PIN (3) SLEEVE (16) AND NUT (18) ON R/H MLG AS PER A320 FAM AMM 32-11-29-000-001-A. (0184396)

Part: BEARING — EXCESS PLAY (LT WING TE FLAP) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 EXCESSIVE PLAY ON O/B FLAP BEARING O/B SIDE LH WING. CORRECTIVE ACTION: REPLACED BEARING TRACK #4 ON O/B FLAP L/H WING (1 E/A) AS PER A320 FAM AMM 57-53-21-000-001-A AND AMM 57-53-21-400-001-A. (0180541)

Part: BEARING — EXCESS PLAY (LT WING TE FLAP) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 EXCESSIVE PLAY ON O/B FLAP BEARING I/B SIDE LH WING. CORRECTIVE ACTION: REPLACED FLAP BEARING LOC. AT TRACK #3 ON O/B FLAP L/H WING AS PER A320 FAM AMM 57-53-21-000-001-A AND AMM 57-53-21-400-001-A. (0180521)

Part: NUT — CORRODED (LT FLAP TRACK) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION ON NUT OF FLAP CARRIAGE BOLT OF TRACK 3 (1 E/A) L/H WING. CORRECTIVE ACTION: REPLACED NUT OF FLAP CARRIAGE BOLT OF TRACK #3 (1 E/A) L/H WING PER AMDS CARD 2750-6020-LT. (0180548)

Part: BEARING — EXCESS PLAY (NR 3 FLAP TRACK) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 EXCESSIVE PLAY ON FLAP BEARING LOC. AT TRACK 3 ON O/B FLAP R/H WING (1 E/A). CORRECTIVE ACTION: REPLACED FLAP BEARING LOC. AT TRACK #3 ON O/B FLAP R/H WING (1 E /A) FOR REMOVE AS PER A320 FAM AMM 57-53-21-000-001-A. (0179408).

Part: FRAME — CRACKED (FRM 4) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CRACK INDICATION FOUND IN OPEN HOLE LOCATED AT FR 4 LATERAL SIDE POST INTERNAL LH SIDE. CORRECTIVE ACTION: REPAIRED PER ER/A 614131-14AD. (0177825)

Part: FLAP TRACK — CORRODED (NR 2) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION ON FLAP BEARING TRACK 2 ON I/B FLAP L/H WING (1 E/A). CORRECTIVE ACTION: REPLACED FLAP BEARING TRACK #2 ON I/B FLAP L/H WING (1 E/A) PER A320 FAM AMM 57-52-21-000-001-A AND A320 FAM AMM 57-52-21-400-001-A. (0177748)

Part: ROD END — EXCESS PLAY (LT WING TE FLAP) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 EXCESSIVE PLAY FLAP INTERCONNECTING STRUT ROD END BEARING ON LH WING (1 EA). CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT ON L/H WING AS PER A320 FAM AMM 27-51-44-000-001-A AND A320 FAM AMM 27-51-44-400-001-A. (0175848)

Part: ACCESS PANEL — CRACKED (HORIZONTAL STAB) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CRACK ACCESS PANEL 332AB ON LH HORIZONTAL STABILIZER. CORRECTIVE ACTION: REPAIRED PER ER/A 614672-14. (0173765)

Part: WINDOW FRAME — CRACKED (SLIDING WINDOW) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CRACK WAS FOUND IN HOLE #3 AT THE LH LATERAL SLIDING WINDOW FRAME UPPER ATTACHMENT. CORRECTIVE ACTION: REPAIRED PER ER/A 614131-14. (0173458)

Part: TRACK — CORRODED (RT WING FLAP) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION ON FLAP BEARING TRACK 4 ON O/B FLAP R/H WING (1 E/A). CORRECTIVE ACTION: REMOVED AND INSTALLED NEW FLAP BEARING TRACK #4 ON O/B FLAP RH WING (1E/A) AS PER A320 FAM AMM 57-53-21-000-001-A AND AS PER A320 FAM AMM 57-53-21-400-001-A. (0169633)

Part: SUPPORT BRACKET — CRACKED (HORIZONTAL STAB) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CRACK TRAILING EDGE SUPPORT BRACKET LOCATED AT HINGE ARM #1 ON LH HORIZONTAL STABILIZER. CORRECTIVE ACTION: REPLACED SUPPORT BRACKET LOCATED TRAILING EDGE AT HINGE ARM 1 ON LH HORIZONTAL STABILIZER AS PER A319 SRM 51-42-11 & SRM 51-72-11. (0168673)

Part: WEB — GOUGED (LT NACELLE) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 GOUGE WEB LOC. BTW RIB08 TO RIB09 UPPER SPAR AT BLEED DUCT AREA ON LH PYLON. CORRECTIVE ACTION: REPAIRED PER ER/A 614973-14. (0168701)

Part: LEVER — EXCESS PLAY (ROTARY DRIVE ARM) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 EXCESSIVE PLAY ON BEARING OF ROTARY DRIVE ARM LEVER TRACK #3 ON R/H WING. CORRECTIVE ACTION: REPLACED BEARING (1 EA) ON ROTARY DRIVE ARM LEVER TRACK #3 ON RH WING AS PER AMDS CARD 2750-6020-RT. (0167017)

Part: LEVER — EXCESS PLAY (ROTARY DRIVE ARM) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 EXCESSIVE PLAY ON BEARING OF ROTARY DRIVE ARM LEVER TRACK 2 ON R/H WING. CORRECTIVE ACTION: REPLACED BEARING (1 EA) ON ROTARY DRIVE ARM LEVER TRACK #2 ON RH WING PER AMDS CARD 2750-6020-RT. (0167049)

Part: LEVER — EXCESS PLAY (ROTARY DRIVE ARM) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 EXCESSIVE PLAY ON BEARING OF ROTARY DRIVE ARM LEVER TRACK 3 ON L/H WING. CORRECTIVE ACTION: REPLACED BEARING (1 EA) ON ROTARY DRIVE ARM LEVER TRACK #3 ON LH WING AS PER AMDS CARD 2750-6020-LT. (0167042)

Part: LEVER — EXCESS PLAY (ROTARY DRIVE ARM) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 EXCESSIVE PLAY ON BEARING OF ROTARY DRIVE ARM LEVER TRACK 4 ON R/H WING. CORRECTIVE ACTION: REPLACED BEARING (1 EA) ON ROTARY DRIVE ARM LEVER TRACK #4 ON RH WING AS PER AMDS CARD 2750-6020-RT. (0167030)

Part: LEVER — EXCESS PLAY (ROTARY DRIVE ARM) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 EXCESSIVE PLAY ON BEARING OF ROTARY DRIVE ARM LEVER TRACK 1 ON L/H WING. CORRECTIVE ACTION: REPLACED BEARING (1 EA) ON ROTARY DRIVE ARM LEVER TRACK #1 ON LH WING AS PER AMDS CARD 2750-6020-LT. (0167026)

Part: LEVER — EXCESS PLAY (ROTARY DRIVE ARM) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 EXCESSIVE PLAY ON BEARING OF ROTARY DRIVE ARM LEVER TRACK 2 ON L/H WING. CORRECTIVE ACTION: REPLACED BEARING (1 EA) ON ROTARY DRIVE ARM LEVER TRACK #2 ON LH WING AS PER AMDS CARD 2750-6020-LT. (0167036)

Part: HINGE PIN — CORRODED (RT AILERON) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION AILERON HINGE PINS ON RH WING (5 EA). CORRECTIVE ACTION: REPLACED HINGE PINS (5 EA) OF AILERON ON RH WING PER AMDS CARD 5760-1010S-RT. (0165547)

Part: BOLT — CORRODED (RT WING FLAP) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION ON ECCENTRIC BOLT (1 E/A) AND PLAIN BUSHING (1 E/A) LOC. ON DRIVE ARM TRACK 3 O/B FLAP R/H WING. CORRECTIVE ACTION: REPLACED ECCENTRIC BOLT (1 E/A) AND PLAIN BUSHING (1 E/A) LOC. ON DRIVE ARM TRACK #3 O/B FLAP R/H WING AS PER AIRBUS CMM 57-53-21-400-805-C01. (0162177)

Part: BOLT — CORRODED (FLAP TRACK) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION ON NUT FLAP CARRIAGE BOLT OF TRACK 2 AND MISSING PIN INDICA TOR OF FLAP TRACK 1 ON R/H WING. CORRECTIVE ACTION: REPLACED NUT OF FLAP CARRIAGE BOLT OF TRACK #2 AND INSTALLED NEW PIN INDICATOR OF TRACK #1 ON RH WING PER AMDS CARD 2750-6010-RT. (0162184)

Part: TRACK — CORRODED (TE FLAPS) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION ON ECCENTRIC BOLT (1 E/A) AND PLAIN BUSHING (1 E/A) LOC. ON DRIVE ARM TRACK 4 O/B FLAP R/H WING. CORRECTIVE ACTION: REPLACED EXCENTRICAL BOLT AND PALIN BUSHING OF DRIVE ARM TRACK #4 OUTBOARD FLAP RH WING AS PER AIRBUS CMM 57-53-21. (0161140)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 DENT LEADING EDGE LOCATED AT OUTBD SIDE THE CAVINITY AREA OF SLAT TRAC K 5 ON LH WING. CORRECTIVE ACTION: PERFORMED REPAIR ON LEADING EDGE LOCATED AT OUTBD SIDE THE CAVINITY AREA OF SLAT TRACK 5 ON LH WING AS PER A319 SRM57-41-11 -300-037. (0154650)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION INTERNAL STRUCTURE ON COUPLING STR31 LH SIDE FR67 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED COUPLING STR31 LH SIDE FR67 IN AFT CARGO COMPARTMENT AS PER A319 SRM 51-42-11 AND SRM 51-72-11. (0154344)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 EXCESSIVE PLAY OB LINK FLAP TRACK 2 AND FLAP TRACK 3 ON RH WING. CORRECTIVE ACTION: INSTALLED NEW WASHER OB LINK FLAP TRACK 2 AND FLAP TRACK 3 ON RH WING AS PER A320 FAM AMM 57-55-11-000-001-A. (0150056)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 NICK SPIGOT FITTING RECEPTACLE BORE ON LH PYLON. CORRECTIVE ACTION: REPLACED FITTING SPIGOT ON L/H PYLON AS PER A319 SRM 54-51-12- 300-001. (0148491)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION SPIGOT FITTING RECEPTACLE ON RH PYLON. CORRECTIVE ACTION: REPLACED FITTING SPIGOT ON R/H PYLON AS PER A319 SRM 54-51-12-300-001. (0147566)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 EXCESSIVE PLAY ON BEARING OF INTERCONNECTING STRUT BRACKET ON I/ B FLAP L/H WING (1 E/A). CORRECTIVE ACTION: REPLACED BEARING (1E/A) ON INTERCONNECTING STRUT BRACKET ON I/B FLAP L/H WING AS PER A319 AMM 57-51. (0146896)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 EXCESSIVE PLAY ON BEARING OF INTERCONNECTING STRUT BRACKET ON I/ B FLAP R/H WING (1 E/A). CORRECTIVE ACTION: REPLACED BEARING (1E/A) ON INTERCONNECTING STRUT BRACKET ON I/B FLAP RH WING AS PER A319 AMM 57-51. (0146902)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION ON PLAIN BUSH AILERON HINGE #5 ON L/H AILERON (2 E/A). CORRECTIVE ACTION: REPLACED BUSHINGS (2 E/A) ON HINGE #5 OF L/H AILERON AS PER AIRBUS CMM 57-61-21. (0141640)

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION ON BOLTS OF THE SERVO CONTROL I/B AND O/B IN THE ELEVATOR SIDE LH (2 E/A). CORRECTIVE ACTION: REPLACED BOLTS OF THE SERVO CONTROL I/B AND O/B IN THE ELEVATOR SIDE (2E/A) AS PER A320 FAM AMM 27-34-51-400-001-A. (0141571)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION ON PLAIN BUSH AILERON HINGE #2 ON L/H AILERON (2 E/A). CORRECTIVE ACTION: REPLACED BUSHINGS (2 E/A) ON HINGE #2 OF L/H AILERON AS PER AIRBUS CMM 57-61-21. (0141630)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION ON PLAIN BUSH AILERON HINGE #4 ON L/H AILERON (2 E/A). CORRECTIVE ACTION: REPLACED BUSHINGS (2 E/A) ON HINGE #4 OF L/H AILERON AS PER AIRBUS CMM 57-61-21. (0141638)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION ON PLAIN BUSH AT I/B AILERON ACTUATOR BRACKET I/B LUG ON L/H AILERON (1 E/A). CORRECTIVE ACTION: REPLACED BUSHING (1 EA) ON I/B AILERON ACTUATOR BRACKET I/B LUG ON LH AILERON AS PER AIRBUS CMM 57-61-21. (0141626)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION ON PLAIN BUSH AT AILERON HINGE 1 I/B LUG ON L/H AILERON. CORRECTIVE ACTION: REPLACED BUSHINGS (2 E/A) ON HINGE #1 OF L/H AILERON AS PER AIRBUS CMM 57-61-21. (0139854)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION HARDWARE RUDDER HINGE 1 BUSHINGS 2E/A, NUT ASSY 1E/A AND WASHER 1E/A. CORRECTIVE ACTION: REPLACED HARDWARE ON RUDDER HINGE #1 BUSHINGS (2E/A), NUT ASSY (1E/A) AND WASHER (1E/A) IAW AMDS CARD 5530-4001. (0137034)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION HARDWARE RUDDER HINGE 5 BUSHINGS 2E/A, BOLT 1E/A, DEVICE-ANT IROTATION 1E/A AND WASHER 1E/A. CORRECTIVE ACTION: REPLACED HARDWARE RUDDER HINGE #5 BUSHINGS (2E/A), BOLT (1E/A ), DEVICE-ANTIROTATION (1E/A) AND WASHER (1E/A) IAW AMDS CARD 5530-4001. (0137049)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION HARDWARE RUDDER HINGE 2 BUSHINGS 2E/A AND WASHER 1E/A. CORRECTIVE ACTION: REPLACED HARDWARE ON RUDDER HINGE #2 BUSHINGS (2E/A) AND WASHER (1E/A) IAW AMDS CARD 5530-4001. (0137037)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION HARDWARE RUDDER HINGE 7 BUSHINGS 2E/A. CORRECTIVE ACTION: REPLACED HARDWARE ON RUDDER HINGE #7 BUSHINGS (2E/A) IAW AMDS CARD 5530-4001. (0137056)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION HARDWARE RUDDER HINGE 3 BUSHINGS 2 E/A, NUT ASSY 1E/A AND WASHER 1E/A. CORRECTIVE ACTION: REPLACED HARDWARE ON RUDDER HINGE #3 BUSHINGS (2 E/A), NUT ASSY (1E/A) AND WASHER (1E/A) IAW AMDS CARD 5530-4001. (0137042)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION HARDWARE RUDDER HINGE 4 BUSHINGS 2E/A, NUT ASSY 1E/A AND WASHER 1E/A. CORRECTIVE ACTION: REPLACED HARDWARE ON RUDDER HINGE #4 BUSHINGS (2E/A), BOLT (1E/A) AND WASHER (1E/A) IAW AMDS CARD 5530-4001. (0137030)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION FLOOR BEAM -Y1292 LOCATED BTW FR 64 TO FR 66 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y1292 LOCATED BTW FR 64 TO FR 66 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11 AND SRM 51-72-11. (0129805)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION WEB FLOOR STRUCTURE BTW FR69 TO FR70 RH SIDE IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED WEB LOC BTW FR69 TO FR70 AT LEVEL STR 23RH AS PER A319 SRM 51-72-11 AND SRM 51-42-11-801. (0130085)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION SEAT TRACK -Y1292 BTW FR41 TO FR46. CORRECTIVE ACTION: REPLACED SEAT TRACK -Y1292 BTW FR41 TO FR46 AS PER A319 SRM 51-72-11. (0129810)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION BEAM SEAT TRACK Y1292 LOC.FR 20 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM Y1292 LOCATED BTW FR 12 TO FR 24 AT FWD GALLEY AREA AS PER A319 SRM 51-72-11 AND SRM 51-42-11. (0129794)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION WEB FLOOR STRUCTURE BTW FR69 TO FR70 RH SIDE IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED WEB LOC BTW FR69 TO FR70 AT LEVEL STR 23RH AS PER A319 SRM 51-72-11 AND SRM 51-42-11-801. (0130100)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 CORROSION WEB FLOOR STRUCTURE BTW FR69 TO FR70 AT LEVEL STR23 LH SIDE IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED WEB LOC. BTW FR69 TO FR70 AT LEVEL STR 23LH IN PASSENGER CABIN AS PER A319 SRM 51-42-11-801 AND SRM 51-72-11-801. (0130082)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 DETERIORATED PASSENGER CREW DOOR 841 ROLLER UPPER AND LOWER AT FWD AND AFT POSITION OF THE DOOR AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED PASSENGER CREW DOOR 841 ROLLER UPPER AND LOWER AT FWD AND AFT POSITION OF THE DOOR AT FWD GALLEY AREA AS PER A320 FAM AMM 52-11 -31-000-002-A AND AMM 52-11-31-400-002-A. (0107007)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 OUT OF ADJUSTMENT PASSENGER CREW DOOR 842 LOAD NECESSARY WHEN YOU OPE N THE DOOR FROM INNER CONTROL HANDLE AT AFT GALLEY AREA. CORRECTIVE ACTION: ADJUSTED PASSENGER CREW DOOR 842 AS PER A320 FAM AMM 52-13-21-400-001-A. (0106992)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 DETERIORATED PASSENGER CREW DOOR 842 LOWER ROLLER AT FWD AND AFT POSIT ION OF THE DOOR AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED PASSENGER CREW DOOR 842 LOWER ROLLER AT FWD AND AFT POSITION OF THE DOOR AT AFT GALLEY AREA AS PER A320 FAM AMM 52-13-31-000-002-A STEP 4H AND AS PER A320 FAM AMM 52-13-31-400-002-A. (0106976)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 OUT OF ADJUSTMENT PASSENGER CREW DOOR 841 DIMENSION A BTW THE FINGER AND STRIKE LEVER OF DOOR DAMPER AT FWD GALLEY AREA. CORRECTIVE ACTION: PERFORMED ADJUSTMENT PASSENGER CREW DOOR 841 DIMENSION A (J2) BTW THE FINGER AND STRIKE LEVER OF DOOR DAMPER AS PER A320 FAM AMM 52-11-14-820-002-A. (0106987)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 OUT OF ADJUSTMENT PASSENGER CREW DOOR 832 INNER CONTROL HANDLE LOAD WHEN YOU OPEN THE DOOR FROM INSIDE AT AFT GALLEY AREA. CORRECTIVE ACTION: ADJUSTED PASSENGER CREW DOOR 832 AS PER A320 FAM AMM 52-13-21-400-001-A. (0107017)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 DETERIORATED PASSENGER CREW DOOR 832 ROLLER UPPER AND LOWER AT FWD AND AFT POSITION OF THE DOOR AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED PASSENGER CREW DOOR 832 ROLLER UPPER AND LOWER AT FWD AND AFT POSITION OF THE DOOR AT AFT GALLEY AREA AS PER A320 FAMAMM 53-13-31-000-002-A. (0106983)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,980 hrs · 30,117 cycles

SHIP 3124 DETERIORATED PASSENGER CREW DOOR 831 ROLLER UPPER AND LOWER, ON FWD AND AFT POSITION AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED PASSENGER CREW DOOR 831 ROLLER UPPER AND LOWER, ON FWD AND AFT POSITION AT FWD GALLEY AREA AS PER A320 FAM AMM 52-11-31-000-002-A AND AMM 52-11-31-400-002-A. (0106998)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,904 hrs · 30,076 cycles

SHIP 3124 CAPT FIXED WINDOW DELAM AROUND EDGE. CORRECTIVE ACTION: REPLACED PER A319 AMM 56-12. (0045926)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,200 hrs · 29,706 cycles

SHIP 3124 R1 DOOR OVERHEAD EMERGENCY LIGHT INOP. CORRECTIVE ACTION: R/R R1 DOOR OVERHEAD EMERGENCY LIGHT LENS PER CMM 33-52-01. (4827750)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,015 hrs · 29,597 cycles

SHIP 3124 RH INBD ELEVATOR ACTUATOR LEAKING. CORRECTIVE ACTION: REMOVED AND REPLACED RH INBOARD ELEVATOR SERVO PER AMM 27-34-51. (2887203)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,899 hrs · 29,536 cycles

SHIP 3124 FORWARD GALLEY FA O2 MASK HAS FALLEN FROM ITS COMPARTMENT. CORRECTIVE ACTION: RESECURED GALLEY F/A O2 MASK COMPARTMENT IAW A319 AMM 35-21. (4934014)

Part: SLIDE — PARTIAL DEPLOY (L1 DOOR) · airframe 55,414 hrs · 28,736 cycles

MAIN CABIN DOOR L1 SLIDE PARTIALLY OUT. REMOVED AND REPLACED L1 SLIDE IAW WORK CARD 2561-4003-LF.

Part: OXYGEN MASK — NO TEST (ROW 23 ABC) · airframe 55,119 hrs · 28,588 cycles

DURING WKCD 2527-01014-02 O2 MSK MAN DROP TEST FOUND MASK AT 23 ABC DID NOT DROP. CORRECTIVE ACTION: CLEARED LANYARD FROM DOOR - AFTER CONCURRENT DROP TEST DOOR DROPPED NML. (9503088)

Part: UNKNOWN — ODOR (CABIN) · airframe 52,710 hrs · 27,283 cycles

F/A REPORT ODOR IN AFT CABIN. COMPLIED WITH NO GO ODI PROCEDURES ATA 2172 AND WORK CARD 0550- 2002. ODOR TYPE 9 MISC. NO ISSUES NOTED. NEW CABIN INTERIOR PROBABLE CAUSE. MCC NOTIFIED. (LP# 7071718)

Part: NONE — NONE · airframe 52,710 hrs · 27,283 cycles

CRACK INDICATION ON FRAME 16 LH SIDE, DOOR STOP NO7, HOLE NO3 ( LOWER INB OARD), AT FWD GALLEY AREA. (LOWER INBOARD) AT FWD GALLEY AREA ASPER PRI 595882-14AD REV.0,1AND ERA 595882-14AD REV. ORIGINAL,FOR TIME CONTROL ITEM SEC II SEE LOG PAGE 2058723 , AND ALL STEPS ARE DOCUMENTED ON NONROUTINE CARD 16/220 RII INSPECTION COMPLETE 0396628 AE131QC JOB COMPLETE ASSOCIATED ER/A 00-595882 ADDED FOR AC 3124 LOG-PAGE UPDATED @ 20DEC21 1856 UTC ALTD BY BORUCH 00311927 ATG 21DEC21 ENTR 00311927 W REQUESTING REPAIR DISPOSITION, REPAIR MUST BE ACCOMPLISHED PRIOR TO FURTHER FLI GHT. REFER TO EM 5311-01229, AD 2019-20-10, SB A320-53-1330 REV O. (LP# 2059078)

Part: NONE — NONE · airframe 52,710 hrs · 27,283 cycles

CRACK INDICATION ON FRAME 16 DOOR STOP ?7, HOLE ?1 (UPPER INBOARD) AT FWD GALLEY AREA. PERFORMED REPAIR SECTION I ON FRAME 16 RH DOOR STOP #7, HOLE #1 (UPPER INBOARD) AT FWD GALLEY AREA ASPER PRI 595885-14AD REV .1AND ERA 595885-14AD REV. ORIGINAL. RII INSPECTION COMPLETE 0396628 AE131QC JOB COMPLETE.REFER TO EM 5311-01229, AD 2019-20-10, SB A320-53-1330 REV O. (LP# 2059067)

Part: NONE — NONE · airframe 52,710 hrs · 27,283 cycles

CRACK INDICATION ON FRAME 16 LH SIDE, DOOR STOP #7, HOLE #1 ( UPPER INB OARD), AT FWD GALLEY AREA. PERFORMED REPAIR SECTION I ON FRAME 16 LH DOOR STOP #7, HOLE #1 (UPPER INBOARD) AT FWD GALLEY AREA ASPER PRI 595882-14AD REV.0,1AND ERA 595882-14AD REV. ORIGINAL,FOR TIME CONTROL ITEM SEC II SEE LOG PAGE 2058723 RII INSPECTION COMPLETE 0396628 AE131QC JOB COMPLETE ASSOCIATED ER/A 00-595882 ADDED FOR AC 3124. (LP# 2059106)

Part: NONE — NONE · airframe 52,710 hrs · 27,283 cycles

CRACK INDICATION ON FRAME 16 RH SIDE, DOOR STOP ?7, HOLE ?3 ( LOWER INB OARD), AT FWD GALLEY AREA. PERFORMED REPAIR SECTION I ON FRAME 16 RH DOOR STOP #7, HOLE #3 (LOWER INBOARD) AT FWD GALLEY AREA ASPER PRI 595885-14AD REV .1AND ERA 595885-14AD REV. ORIGINAL, FOR REPLACED INTERCOSTAL FITTING REFER NON ROUTINE CARD 14/220 RII INSPECTION COMPLETE0396628 AE131QC. GHT. REFER TO EM 5311-01229, AD 2019-20-10, SB A320-53-1330 REV O. (LP# 2059108)

Part: NONE — NONE · airframe 52,705 hrs · 27,280 cycles

COLDWORK HOLE A AND HOLE B LOCATED AT FRAME 35 AND Y1292 (LH) IN ACCORDANCE WITH WORK CARD 5311-01171-03A PRIOR TO FURTHER FLIGHT IS REQUIRED. REFERENCES RELATED: AA 5311-01171, SB A320-53-1264, AD-2018-06-04. AT FORWARD CARGO COMPARTMENT. PERFORMED COLD EXPANSION ON HOLE A AND HOLE B LOCATED AT FRAME 35 AND Y1292(LH) IN ACCORDANCE WITH WORK CARD 5311-01171-03A, PRIOR TO FURTHER FLIGHT IS REQUIRED. REFERENCES RELATED: AA 5311-01171, SB A320-53-1264, AD-2018-06-04 AS PER SRM A319 51- 48-00 AND APPLIED PROTECTIVE TREATMENT AS PER SRM A319 51-75- 12 AT FORWARD CARGO COMPARTMENT RII INSPECTION COMPLETE 0294551 (AE166QC) JOB COMPLETE. (LP# 2055825)

Part: NONE — NONE · airframe 52,705 hrs · 27,280 cycles

SHIP 3124 - COLDWORK HOLE A AND HOLE B LOCATED AT FRAME 35 AND Y-1292(RH). CORRECTIVE ACTION: PERFORMED COLD EXPANSION ON HOLE A AND HOLE B LOCATED AT FRAME 35 AND Y-1292 (RH) IN ACCORDANCE WITH WORK CARD 5311.(2053603)

Part: PACKING — NOT REPORTED (BRAKE SYSTEM) · airframe 50,116 hrs · 26,016 cycles

A/C 3124 CLOSED LOG 5754449 FLT/CHK 2688 PILOT REPORT SDR: N POSITION: LT TASK HRS: 000001.0 TASK ELAPSE TIME HRS: 000002.0 01 ABORTED T/O AT 70KTS FOR HYD Y RES LOW LEVEL02 CORR ATA 3245 RII: N FOUND PACKING ON ALTERNATE BRAKE MANIFOLD CONTROL VALVE, REPLACED PER AMM 32-43, RAN BRAKES NO LEAKS NOTED. OK FOR SVC.

Part: PLUG — MISSING (LT MLG) · airframe 49,207 hrs · 25,591 cycles

LEFT GEAR UPPER BEARING BLANKING PLUG MISSING ON ARRIVAL. REMOVED SPEED TAPE ERA 575079 AS A TEMPORARY REPAIR AND REPLACED WITH LEFT GEAR UPPER BEARING BLANKING PLUG STK NR 00-3200-3-0198 PER ERA 575079 PERMANENT REPAIR.

Part: WEB — CORRODED (FRAMES 20-24) · corrosion level 2 · airframe 47,239 hrs · 24,700 cycles

CORRODED WEB, BETWEEN FRAMES 20 TO 24, STRINGER 23R IN THE FWD GALLEY, REPLACED THE WEB IAW SRM 51-72-11, AND DRAWING D53112783.

Part: SKIN — DENTED (BS 25-26) · airframe 47,239 hrs · 24,700 cycles

SKIN DENTED BETWEEN FRAMES 25 TO 26, STRINGERS 42L TO 43L. REPAIRED THE SKIN IAW SRM 53-00-11-300-011.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-24) · corrosion level 2 · airframe 47,239 hrs · 24,700 cycles

CORRODED FLOOR SUPPORT, - Y1292, BETWEEN FRAMES 12 TO 24. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DWG D53112812.

Part: FITTING — CORRODED (FRAMES 16-20) · corrosion level 2 · airframe 47,239 hrs · 24,700 cycles

CORRODED CENTER FITTING, BETWEEN FRAMES 16 TO 20, STRINGER 23L , REPLACED THE CENTER FITTING IAW SRM 51-72-11, AND DRAWING D53112109

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · corrosion level 2 · airframe 47,239 hrs · 24,700 cycles

CORRODED FLOOR SUPPORT, +Y1292, BETWEEN FRAMES 64 TO 66, REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, 51-42-11, AND DWG D53472015.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-24) · corrosion level 2 · airframe 47,239 hrs · 24,700 cycles

CORRODED FLOOR SUPPORT Y765, BETWEEN FRAMES 12 TO 24. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DRAWING D53112812.

Part: FLOOR SUPPORT — CORRODED (FRAMES 68-69) · corrosion level 2 · airframe 47,239 hrs · 24,700 cycles

CORRODED FLOOR SUPPORT, +Y1162, BETWEEEN FRAMES 68 TO 69, REPLACED THE FLOOR SUPPORT IAW SRM A319 51-72-11, AND DRAWING 53472780

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-67) · corrosion level 2 · airframe 47,239 hrs · 24,700 cycles

CORRODED FLOOR SUPPORT BETWEEN BETWEEN FRAMES 66+4 TO 67 +18, REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DRAWING D53472815

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-24) · corrosion level 2 · airframe 47,239 hrs · 24,700 cycles

CORRODED FLOOR SUPPORT, Y1292, BETWEEN FRAMES 12 TO 24 IN THE FWD GALLEY. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DWG D53112812.

Part: WEB — CORRODED (FUSELAGE) · airframe 47,239 hrs · 24,700 cycles

CORROSION WEB LOC BTW FR 20 TO FR 24 LEVEL STR 23L AT FWD GALLEY AREA, REPLACED WEB LOCATED BTW FR20 TO FR29. AT LEVEL STR 23L AT FWD GALLEY AREA AS PER SRM 51-72-11 AND DRAWING D53110920.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-24) · corrosion level 2 · airframe 47,239 hrs · 24,700 cycles

CORRODED FLOOR SUPPORT, -Y765 BETWEEN FRAMES 12 TO 24 IN THE FWD GALLEY. REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, AND DWD D53112812.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-16) · corrosion level 2 · airframe 47,239 hrs · 24,700 cycles

CORRODED FLOOR SUPPORT, -Y81, BETWEEN FRAMES 12 TO 16 IN THE FWD GALLEY, REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, SRM 51-72-11, AND DWG D53112829002.

Part: FITTING — CRACKED (RT MLG) · airframe 47,239 hrs · 24,700 cycles

CRACK INDICATION ON LOWER FITTING AROUND THE FASTENER OF CONNECTING PLATE ON FWD HINGE ON RT MAIN LANDING GEAR, REPLACED LOWER FWD FITTING AND FASTENER LOCATED AT FWD POSITION HINGE OF R/H MAIN LANDING GEAR DOOR AS PER SRM 51-72-11 AND DRAWING D53370720.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,239 hrs · 24,700 cycles

CORROSION FLOORBEAM BTW -Y1292 AND -Y1162 AT AFT GALLEY AREA BETWEEN FRAME 66+4 TO FRAME 67+18. REPLACED FLOORBEAM LOC BTW -Y1292 AND -Y1162 AT AFT GALLEY AREA FRAME 66+4" TO FRAME 67+18" AS PER SRM 51-72-11 AND DRAWING D53472815

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,239 hrs · 24,700 cycles

CORROSION FLOORBEAM -Y189 LOC BTW FR20 TO FR 24 AT FWD GALLEY AREA. REPLACED FLOORBEAM AND FASTENERS LOC Y189 BTW FR20 TO FR24 AT FWD GALLEY AREA AS PER SRM 51-72-11 AND DRAWING D531-11406.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,239 hrs · 24,700 cycles

CORROSION FLOORBEAM -Y1162 BTW FR 68 TO FR 69 AT AFT GALLEY AREA, REPLACED FLOORBEAM -Y1162 LOC BTW FR 68 TO FR 69 AT AFT GALLEY AREA AS PER SRM 51-72-11 AND DRAWING D53472780.

Part: SKIN — TORN (L2 DOOR) · airframe 46,634 hrs · 24,422 cycles

FOUND A TEAR IN THE L2 DOOR SKIN LOWER AFT CORNER DAMAGE IS APPROX. 1.5 INCHES LONG AT LOWER AFT RADIUS. TEAR IS THROUGH OUTER SKIN AND UNDERLYING FRAME. REMOVED DAMAGED AREA, FABRICATED A DOUBLER AND REPAIR FILLER IAW SRM 52-10-00-300-003.

Part: NOT REPORTED — LEAKING (APU) · airframe 44,348 hrs · 23,356 cycles

PILOT REPORTED ODOR IN CABIN. FOUND APU TO HAVE INTERNAL OIL LEAK, APU REPLACED.

Part: SKIN — DENTED (LT WING SLAT) · airframe 41,615 hrs · 22,049 cycles

LT WING NR 3 SLAT FOUND WITH DENT ON L/E, REPAIR IAW SRM 57-40-00, FIG 205.

Part: LENS — UNSECURE (EMERGENCY LIGHT) · airframe 37,602 hrs · 19,669 cycles

EMERGENCY LIGHT DAMAGED. FOUND LENS COVER HANGING INTO ISLE. SECURED LENS, OPS GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 34,717 hrs · 18,081 cycles

FOUND 2B FORWARD EMERGENCY LIGHT INOPERATIVE, FOUND BROKE WIRE. REPAIRED BROKEN WIRE SEAT 2B, EMERGENCY LIGHT IAW A319-33-52. OPS CHECKED NORMAL.

Part: SKIN PANEL — DAMAGED (RT WING) · airframe 31,821 hrs · 16,315 cycles

RIGHT WING TOP SKIN PANEL NR 2, OVERWING REFUEL HOLE, BETWEEN RIBS 19 AND 20 REQUIRES FOLLOW-ON INSPECTION. REPAIR WAS ACCOMPLISHED ON N/R 640/6 DURING M CHECK AT BFM AUG 2012.

Part: PANEL — PUNCTURED (AFT CARGO) · airframe 31,818 hrs · 16,313 cycles

AFT CARGO SLOPING WALL PANEL 151AE IS PUNCTURED 1.0 INCH BY 1.0 AND GOUGED 32 INCH BY 0.33 INCH. INSTALLED NEW SLOPING PANEL IAW DWG 3D25-40532.

Part: SKIN — CHAFED (FUSELAGE) · airframe 31,821 hrs · 16,315 cycles

LEFT AFT PASSENGER DOOR CUT-OUT, FORWARD AND AFT UPPER CORNERS HAS CHAFED MARKS. BLENDED AFT AND FORWARD UPPER CORNERS IAW A319 SRM 51-73-00. FORWARD CORNER L=1.160 INCH W=.140 INCH D=.006 INCH, AFT CORNER L=1.900 INCH W=.298 INCH D=.026 INCH ORIGINAL MATERIAL .236 INCH. FOUND TO BE IN LIMITS IAW A319 SRM 53-41-11 FIG 105. TREATED AND PRIMED IAW A319 SRM 51-21-11. PAINTED IAW A319 SRM 51-75-12.

Part: PANEL — DAMAGED (AFT CARGO) · airframe 31,818 hrs · 16,313 cycles

AFT CARGO SLOPING WALL PANEL 161CF HAS MULTIPLE DAMAGE. RECEIVED NEW SLOPING PANEL IAW 3D25-40532. DAMAGE L=2.0 INCHES W=1.0 INCH D=0.025 INCH.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 31,818 hrs · 16,313 cycles

AFT CARGO FLOOR PANEL 161PF IS DAMAGED 3 INCHES BY 2.5 INCHES. INSTALLED NEW FLOOR PANEL IAW DWG 3D25-40532.

Part: FLOOR PANEL — PUNCTURED (AFT CARGO) · airframe 31,818 hrs · 16,313 cycles

AFT CARGO FLOOR PANEL 151ZG HAS MULTIPLE PUNCTURES AND BROKEN INSERTS. INSTALLED NEW FLOOR PANEL IAW DWG 3D25-40532.

Part: PANEL — DAMAGED (AFT CARGO) · airframe 31,818 hrs · 16,313 cycles

AFT CARGO SLOPING WALL PANEL 161CF HAS MULTIPLE DAMAGE. INSTALLED NEW SLOPING PANEL IAW 3D25-40532.

Part: PANEL — PUNCTURED (AFT CARGO) · airframe 31,818 hrs · 16,313 cycles

AFT CARGO SLOPING WALL PANEL 161BF IS PUNCTURED AND HAS MULTIPLE DENTS. SLOPE PANEL FABRICATED IAW DRAWING 3D25-40532. DAMAGE L=2.0 INCH BY W=1.0 INCH.

Part: PANEL — DELAMINATED · airframe 31,818 hrs · 16,313 cycles

FORWARD CORNER SLOPING WALL PANEL 131DG IS DELAMINATED ON CORNER 3.0 INCH BY 3.0 INCH. SLOPE PANEL 131DG FABRICATED IAW DWG 3D25-40532.

Part: PANEL — PUNCTURED (AFT CARGO) · airframe 31,818 hrs · 16,313 cycles

AFT CARGO SLOPING PANEL 162CF IS PUNCTURED 1.0 INCH BY 1.0 INCH. SLOPE PANEL FABRICATED IAW DWG 3D25-40532.

Part: PANEL — PUNCTURED (AFT CARGO) · airframe 31,818 hrs · 16,313 cycles

AFT CARGO SLOPING WALL PANEL 151BE IS PUNCTURED AND DENTED 1.2 INCH BY 1.0 INCH. SLOPE PANEL FABRICATED IAW DWG 3D25-40532.

Part: PANEL — PUNCTURED (FWD CARGO) · airframe 31,818 hrs · 16,313 cycles

FORWARD CARGO SLOPING WALL PANEL 131CF IS PUNCTURED (1.0 INCH BY 1.0 INCH). SLOPE PANEL FABRICATED IAW DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 31,818 hrs · 16,313 cycles

AFT CARGO FLOOR PANEL 151CE HAS MULTIPLE DENTS AND SCRATCHES. FLOOR PANEL FABRICATED IAW DWG 3D25-40532. DAMAGE L=12.0 INCH BY W= 12.0.

Part: PANEL — DELAMINATED (AFT CARGO) · airframe 31,818 hrs · 16,313 cycles

AFT CARGO SLOPING WALL PANEL 151TG IS DELAMINATED. SLOPE PANEL FABRICATED IAW DWG 3D25-40532. DAMAGE L=6.0 INCH BY W=4.0 INCH.

Part: PANEL — CRACKED (FWD CARGO) · airframe 31,818 hrs · 16,313 cycles

FORWARD CARGO SLOPING WALL PANEL 131BF CORNER IS CRACKED AND DELAMINATED. 2.5 INCH BY 2.5 INCH. SLOPE PANEL 131BF FABRICATED IAW DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED · airframe 31,818 hrs · 16,313 cycles

FLOOR PANEL 131AF INSERTS ARE DAMAGED AND MULTIPLE DENTS 3 INCH BY 2.5 INCH. FLOOR PANEL FABRICATED IAW DWG 3D25-40532.

Part: PANEL — PUNCTURED (AFT CARGO) · airframe 31,818 hrs · 16,313 cycles

AFT CARGO SLOPING WALL PANEL 151GE IS PUNCTURED 1.0 INCH BY 1.0 INCH. SLOPE PANEL FABRICATED IAW DWG 3D25-40532.

Part: PANEL — DELAMINATED (AFT CARGO) · airframe 31,818 hrs · 16,313 cycles

AFT CARGO SLOPING WALL PANEL 152XG IS DELAMINATED AND DENTED. SLOPE PANEL FABRICATED IAW DWG 3D25-40532. DAMAGED L=2.0 INCH BY 4.0 INCH.

Part: PANEL — DELAMINATED · airframe 31,818 hrs · 16,313 cycles

FORWARD SLOPING WALL PANEL 131EG IS DELAMINATED. SLOPE PANEL FABRICATED IAW DWG 3D25-40532. DELAMINATION L= 6.0 INCH BY W=6.0 INCH.

Part: FLOOR PANEL — DAMAGED · airframe 31,818 hrs · 16,313 cycles

AFT UTILITY FLOOR PANEL HAS CORROSION. INSTALLED NEW FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 31,818 hrs · 16,313 cycles

FORWARD CARGO FLOOR PANEL 131CG IS DAMAGED AND HAS SEVERAL BROKEN INSERTS 2.0 INCH BY 1.0 INCH. FABRICATED NEW FLOOR PANEL IAW DWG 3D25-40532.

Part: PANEL — DELAMINATED (AFT CARGO) · airframe 31,818 hrs · 16,313 cycles

AFT CARGO SLOPING WALL PANEL 152 UG IS DELAMINATED. FABRICATED NEW PANEL IAW DWG 3425-40532.

Part: FLOOR PANEL — DAMAGED (AFT CABIN) · airframe 31,818 hrs · 16,313 cycles

AFT CABIN FLOOR PANEL 261AB DAMAGED. FABRICATED NEW FLOOR PANEL IAW DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 31,818 hrs · 16,313 cycles

AFT CARGO FLOOR PANEL 151PE HAS EDGE DAMAGED (4.0 INCH BY 1.0 INCH). FABRICATED NEW FLOOR PANEL IAW DWG 3D25-40532.

Part: FLOOR PANEL — PUNCTURED (AFT CARGO) · airframe 31,818 hrs · 16,313 cycles

AFT CARGO FLOOR PANEL 151VG HAS PUNCTURES, 4 INCHES BY 2 INCHES AND MULTIPLE BROKEN INSERTS. FABRICATED NEW PANEL IAW DWG 3D25-40532.

Part: FLOOR PANEL — TORN (MID CABIN) · airframe 31,818 hrs · 16,313 cycles

MID CABIN FLOOR PANEL 242MF TORN AROUND FASTENER HOLE ON BOTTOM (PANEL RACK). FABRICATED NEW FLOOR PANEL IAW DWG 3D25-40640.

Part: SILL — CORRODED (PAX DOORWAY) · airframe 31,818 hrs · 16,313 cycles

CORRODED AFT RT PAX DOOR SILL FORWARD END AT FR 66. REMOVED CORROSION IAW SRM 51-74-00. CHECKED LIMITS L=0.70 INCH W=0.400 INCH D=0.043 INCH ORIGINAL MATERIAL 0.150 INCH. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14 FIG 101. FABRICATED REPAIR AND FILLER IAW SRM 53-41-14 FIG 201. INSTALLED REPAIR IAW SRM 53-41-14 FIG 201.

Part: FLOOR SUPPORT — CORRODED (AFT CABIN) · airframe 31,818 hrs · 16,313 cycles

AFT CABIN FLOOR SUPPORT +Y765 SEVERAL FASTENER HOLES CORRODED BET FR 66 TO FR 68. REMOVED CORROSION IAW SRM 51-74-00 L=2.0 INCH W=2.0 INCH D=.075 INCH. ORIG MAT. 0.157. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15 FIG 1. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-42-11.

Part: SILL — CORRODED (FUSELAGE) · airframe 31,821 hrs · 16,315 cycles

CORRODED AFT RT PAX DOOR SILL FWD END AT FR 66. REMOVED CORROSION IAW A319 SRM 51-74-00. CHECKED LIMITS L=0.70 INCH W=0.400 INCH D=0.043 INCH ORIGINAL MATERIAL 0.150 INCH FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-41-14 FIG 101. FABRICATED REPAIR PARTS AND FILLER IAW A319 SRM 53-41-14 FIG 201. INSTALLED REPAIR PARTS IAW A319 SRM 53-41-14 FIG 201 REPAIR PRINCIPLE 6.

Part: WEB — CRACKED (FUSELAGE) · airframe 31,818 hrs · 16,313 cycles

CRACKED WEB TRAY ON AFT CABIN FUSELAGE BETWEEN FR 68-69. REMOVED AND REPLACED WEB TRAY IAW SRM 51-42-11. PAINTED AREA IAW SRM 51-75-12. CRACKED DIMENSION 6 INCHES.

Part: FLOOR SUPPORT — CORRODED (GALLEY AREA) · airframe 31,818 hrs · 16,313 cycles

CORRODED AFT GALLEY FLOOR SUPPORT -Y1292 FR 68/69. BLENDED AREA IAW SRM 51-74-00. ORIG MAT .157 DAMAGE DIM L=2.3 INCH W=1.2 INCH D=.052 INCH. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15 FIG 1. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (GALLEY AREA) · airframe 31,818 hrs · 16,313 cycles

CORRODED AFT GALLEY FLOOR SUPPORT -Y1292 BET FR 66 - FR 69 ON SEVERAL SPOTS. BLENDED AREAS IAW SRM 51-74-00. ORIG MAT .157 DAMAGE DIM. L=2.3 INCH W=1.2 INCH D=.052 INCH. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15 FIG 1. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-42-11.

Part: FLOOR PANEL — DAMAGED · airframe 31,818 hrs · 16,313 cycles

FORWARD UTILITY FLOOR PANEL 231AF CORRODED ON UPPER SURFACE. INSTALLED NEW FLOOR PANEL.

Part: SILL — CORRODED (FUSELAGE) · airframe 31,818 hrs · 16,313 cycles

CORRODED AFT LT PAX DOOR SILL FWD END AT FR 66. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14 FIG 101. FABRICATED REPAIR SPLICES IAW SRM 53-41-14. FABRICATED FILLER IAW SRM 53-41-14 FIG 201. DAMAGED CUTOUT L=1.30 W=0.700 IAW SRM 53-41-14 FIG 201. INSTALLED NEW REPAIR SPLICES AND FILLER IAW SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FWD CABIN) · airframe 31,818 hrs · 16,313 cycles

FORWARD CABIN FLOORBEAM AT FR20, RT SIDE -Y1292 UPPER FLANGE CORRODED. BLENDED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14 FIG 105. REMOVED AND REPLACED FLOORBEAM AT -Y1292 FR12-24 IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (AFT GALLEY) · airframe 31,818 hrs · 16,313 cycles

CORRODED AFT GALLEY FLOOR SUPPORT Y1292 BET 66-68. BLENDED CORROSION IAW SRM 51-74-00. BLENDED DEPTH WAS .040 MAX ALLOWABLE DEPTH IS .027 OUT OF LIMITS IAW TRM 53-41-15 PAGE (1). REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-42-11.

Part: SEAT TRACK — DAMAGED (AFT CABIN) · airframe 31,818 hrs · 16,313 cycles

SEVERAL SCRATCHES ON AFT CABIN SEAT TRACK Y1292 AFT OF FR64. BLENDED SCRATCHES IAW SRM 51-73-00, CHECK LIMITS DEPTH OF BLEND WAS .035 MAX DEPTH OF REMOVABLE MAT. IS .028 OUT OF LIMITS IAW SRM 53-41-15. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-42-11.

Part: SHEAR PLATE — CORRODED (AFT CABIN) · airframe 31,818 hrs · 16,313 cycles

AFT CABIN BETWEEN FR 69 AND 70, LT SHEAR PLATE SUPPORT HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00, L=2.70 INCH BY W=2.3 INCH BY D=.019 INCH. ORIGINAL MATERIAL 0.081 INCH. NO LIMITS FOUND IN SRM. REMOVED LT SHEAR PLATE SUPPORT IAW SRM 51-42-11. INSTALLED SHEAR PLATE SUPPORT. RESTORED PAINT INTERNALLY AND EXTERNALLY TO FASTENERS IAW SRM 51-75-12.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 31,818 hrs · 16,313 cycles

CORRODED AFT GALLEY FLOOR SUPPORT -Y765 BETWEEN FR 67-68 ON SEVERAL SPOTS. BLENDED AREAS IAW SRM 51-74-00, ORIG MAT .157 INCH DAMAGE DIM L=1.2 INCH W=1 INCH D=.032 INCH. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15 FIG 1. REMOVED AND REPLACED BEAM IAW SRM 51-42-11.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 31,818 hrs · 16,313 cycles

FORWARD UTILITY AREA FLOORBEAM LT SIDE BTW FR16 TO FR22 Y254 UPPER FLANGE BEAM HAS CORROSION. REMOVED CORROSION L=2.00 INCH W=1.50 INCH D=0.060 INCH. FOUND TO BE OUT OF LIMITS IAW SRM 51-74-00 LIMITS 53-11-14. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (AFT CABIN) · airframe 31,818 hrs · 16,313 cycles

AFT CABIN FLOOR SUPPORT -Y1732 FWD OF FR 66 HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. CHECKED LIMITS L=2.0 INCH W=0.700 INCH D=0.042 INCH. ORIGINAL MATERIAL 0.170 INCH. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14 FIG 102. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FWD CABIN) · airframe 31,818 hrs · 16,313 cycles

FORWARD CABIN FLOORBEAM AFT FR 20 -Y254 UPPER FLANGE HOLE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. CHECKED LIMITS L=1.50 INCH W=1.00 INCH D=0.024 INCH. OUT OF LIMITS IAW SRM 53-00-14. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11.

Part: STRUCTURE — GOUGED (PAX DOOR) · airframe 31,821 hrs · 16,315 cycles

RIGHT FORWARD PASSENGER DOOR LOWER AFT CORNER GOUGED. BLENDED GOUGED AREA IAW A319 SRM 52-10-00 FIG 104. CHECK LIMITS W=.40 INCH L=.010 INCH D=.003 INCH IN LIMITS IAW A319 SRM 52-10-00 FIG 104. RE-INSPECT PER SRI 52-10-00 IIR 52-10-00-1-002-00 TABLE 103 AFTER 60000 FLIGHT CYCLES.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,637 hrs · 16,201 cycles

FOUND FORWARD AND AFT LEFT EMERGENCY LIGHTS BATTERY PACKS FAULTING. REPLACED FORWARD AND AFT LEFT EMERGENCY LIGHT BATTERY PACKS PER AMM.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 4,554 hrs · 2,600 cycles

DURING NON ROUTINE CHECK, FOUND THE EPSU BATTERY FAULT FOR UNIT 12WL. MAINTENANCE REPLACED BATTERY PACK AND OPERATIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: SOLENOID — FAILED (OXYGEN CONTAINER) · airframe 27,368 hrs · 13,673 cycles

DURING A NON ROUTINE CHECK, THE OXYGEN CONTAINER FAILED A DROP TEST AT ROW 4 LT. MX REPLACED SOLENOID IN OXYGEN CONTAINER AND FUNCTIONAL TEST WAS NORMAL.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 26,901 hrs · 13,418 cycles

DURING L-CHECK, FOUND DAMAGE TO FWD CARGO COMPARTMENT PANEL 131CG. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG 209.