N343NB

Part: APU — CONTAMINATED (ZONE 100) · airframe 61,543 hrs · 32,338 cycles

VERY STRONG DIRTY SOCK/MUSTY ODOR AFTER APU TURNED ON AND PACKS TURNED ON. A/C WAS ON EXT AIR W/ APU OFF WHEN WE ARRIVED. ODOR STARTED AFTER APU TURNED ON. PERFORMED GVI OF APU INLET. FOUND PUDDLE OF DEICE FLUID UNDER BULKHEAD DRAIN AND APU INLET CLEANED. PERFROMED LEVEL A AND B DECONTAMINATION OF ECS. NO ODORS PRESENT. (8124434).

Part: SECU — FAULTED (ZONE) · airframe 61,350 hrs · 32,230 cycles

ATO - AT 10KNTS DUE TO A F/CTL GND SPLR 5 FAULT ECAM WARNING MESSAGE. R & R SEC 2 IAW AMM 27-94. OPS NORMAL. EFCS 1 & EFCS 2 TEST NO FAULTS. (LP 7338020)

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 60,763 hrs · 31,909 cycles

FWD CARGO FLOOR PANEL FOUND DAMAGED. COMPLIED WITH ER/A 587849-14TR. (7781763).

Part: O-RING — LEAKING (HYD SYSTEM) · airframe 60,646 hrs · 31,839 cycles

DURING CRUISE, GOT ECAM HYD B RSVR LOW LEVEL. HYD SYS PAGE SHOWS FLUID LEVEL BELOW THE LOW LEVEL LIMIT. R&R O-RING PER A319 AMM 29-12-42. OP-CHECK LEAK CHECK NORMAL. OK FOR SVC. (7781718)

Part: RETAINER — CRACKED (ZONE 900) · airframe 60,482 hrs · 31,743 cycles

CRACK ON BOTH GALLEY RETAINING BLOCKS ON COMPARTMENT OF 510M ON UPPER BLOCKS. REMOVED AND REPLACED RETAINING BLOCKS REF CMM PMC 68353751021-4050G-00001-01.

Part: RETAINER — CRACKED (ZONE 900) · airframe 60,482 hrs · 31,743 cycles

CRACK ON BOTH GALLEY RETAINING BLOCKS ON COMPARTMENT OF 511M ON UPPER BLOCKS BOTH MEASURING OVER 4 IN ALONG WITH BLOCK PANEL DELAMINATING. REMOVED AND REPLACED RETAINING BLOCKS REF CMM PMC 68353751021-4050G-00001-01. REPAIRED DELAMINATION REF A319 SRM 51-77-12.

Part: FAIRING — DELAMINATED (ZONE 100) · airframe 60,107 hrs · 31,522 cycles

SHIP 3143 FOUND WING TO BODY PANEL 192AB DELAMINATION ON WALKAROUND. CORRECTIVE ACTION: REMOVED AND REPLACED PANEL 192AB IAW A319 AMM 53-25-11. (7558541).

Part: NONE — NONE (NONE) · airframe 59,655 hrs · 31,279 cycles

SHIP 3143 DISC: THE LOG PAGE INCORPORATES STAGE 2 DTE THRESHOLD FOR ER/A 557100- 14, REV. E. C/A: COMPLY WITH ER/A 557100-14, REV. E THAT REQUIRES ADDITIONAL ENGINEERING APPROVAL TO OPERATE AIRCRAFT BEYOND 65,470 FLIGHT CYCLES OR 129,193 FLIGHT HOURS. ASSOCIATED ER/A 00-557100 ADDED FOR AC 3143. (LP: 0900942)

Part: ANTI-ICE VALVE — FAILED (LT WING) · airframe 58,984 hrs · 30,935 cycles

SHIP 3143 - DIV - TO JFK DUE THE LT WING ANTI-ICE VALVE FAILURE. CORRECTIVE ACTION: REPLACED LEAKING LT ENGINE BLEED OVERPRESSURE VALVE. (LP 6957080, 0746898)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 58,877 hrs · 30,878 cycles

SHIP 3143 CORROSION SEAT TRACK +Y1292 LOCATED BTW FR 64 TO FR 66 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED SEAT TRACK Y1292 AND FASTENERS LOC BTW FR64 TO FR66 AS PER A319 SRM 51-42-11 AND SRM 51-72-11.

Part: PIN — OBSTRUCTED (ZONE 800) · airframe 58,587 hrs · 30,724 cycles

SHIP 3143 FA REPORTED DOOR PIN AT DOOR 2L DOES NOT STAY IN PLACE. CORRECTIVE ACTION: REMOVED DEBRIS AS REQUIRED PER AMM 29-63. (0636971)

Part: WINDOW POST — CRACKED (ZONE 200) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CRACK INDICATION FOUND ON WINDSHIELD CENTER POST. CRACK DIRECTION 1 OC LOCK AND 5 OCLOCK. CORRECTIVE ACTION: COMPLIED WITH ER/A 619897-14AD. (0619008)

Part: HINGE FITTING — CRACKED (ZONE 100) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CRACK INDICATION FOUND ON MLG AFT FACE AFT LUG FWD HINGE FITTING LH S IDE. CRACK LENGTH:0.250 INCH APPROX. CORRECTIVE ACTION: COMPLIED WITH ER/A 619993-14AD. (0619061)

Part: ACCESS DOOR — CRACKED (ZONE 100) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CRACK ACCESS DOOR 172AR AROUND AFT HINGE AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 615217-14. (0619050)

Part: SKIN — CORRODED (ZONE 500) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION WAS FOUND ON THE LOWER SURFACE OF TOP SKIN PANEL 2, BETWEEN WX3494,5 - WX4010,2 AT THE TRAILING EDGE OVERHANG OF THE LEFT-HAND WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 619900-14. (0617492)

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION INTERNAL SKIN MACHINED AREA AT LEVEL STR 42L AND BTW FR60 TO FR61 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: COMPLIED WITH ER/A 557100-14AD. (0617562)

Part: BRACKET — CRACKED (ZONE 600) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CRACK OB FIXED LEADING EDGE BRACKET TELESCOPIC DUCT IB SIDE ON RH WIN G. CORRECTIVE ACTION: COMPLIED WITH ER/A 530598-14MA. (0617204)

Part: SKIN — CORRODED (ZONE 100) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION DAMAGE WAS FOUND ON FUSELAGE SKIN PANEL BETWEEN FR58-61 AND STGR42-43LH. CORRECTIVE ACTION: REPAIR PER ERA 557100-14AD. (0615883)

Part: DEFLECTOR — CRACKED (ZONE 800) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 THE DEFLECTOR OF THE DOOR 831 HAS BEEN FOUND AFFECTED WITH CRAK. CORRECTIVE ACTION: COMPLIED WITH ER/A 621462-14. (0614864)

Part: ACCESS PANEL — DAMAGED (FAIRING) · airframe 58,493 hrs · 30,670 cycles

SHIP 3142 HOLE ACCESS PANEL 192KB BELLY FAIRING ON EXISTING REPEIR LOWER FUSELAGE. CORRECTIVE ACTION: REPAIRED ACCESS PANEL 192KB BELLY FAIRING AT LOWER FUSELAGE AS PER ER/A 529512-14MA. (0614169)

Part: SPHERICAL BEARIN — CORRODED (FLAP TRACK) · corrosion level 2 · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION ON HOUSING SPHERICAL BEARING TRACK 3 O/B FLAP LH WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 620734-14. (0614370)

Part: SUPPORT ANGLE — CRACKED (ZONE 300) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CRACK SUPPORT ANGLE ELEVATOR HINGE ARM 5 ON RH HORIZONTAL STABILIZER. CORRECTIVE ACTION: REPLACED SUPPORT ANGLE (1EA) ON ELEVATOR HINGE ARM 5 HORIZONTAL STABILIZER AS PER A319 SRM 51-42-11 AND SRM 51-72-11. (0613962)

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION STRINGER 39L LOCATED BETWEEN FR30 TO FR34 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIR ON STRG 39L LOC BTW FR30 TO FR35 IN FWD CARGO COMPARTMENT AS PER A319 SRM 53-21-13-300-018 AND PERFORMED BLEND OUT ON AFFECTED AREA AS PER A319 SRM 51-74-00. (0610905)

Part: SUPPORT FITTING — EXCESS PLAY (ZONE 100) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 EXCESSIVE PLAY FITTING SUPPORT LOC FR20 LH SIDE IN AFT AVIONIC COMPARTMENT. CORRECTIVE ACTION: REPLACED FITTING ASSY LOC. ON FR20 LH SIDE ON AFT AVIONIC COMPARTMENT AS PER A319 SRM 51-42-11 AND SRM 51-72-11. (0610886)

Part: FITTING — CORRODED (ZONE 500 TE) · corrosion level 2 · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION TRAILING EDGE FITTING LOCATED BTW RIB 7 TO RIB 8 ON LH WING. CORRECTIVE ACTION: REPLACED FITTING ON TRAILING EDGE LOCATED BTW RIB 7 TO RIB 8 ON LH WING AND FASTENERS AS PER A319 SRM 51-42-11 AND SRM 51-72-11. (0607442)

Part: ACCESS PANEL — CRACKED (ZONE 400) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CRACK ACCESS PANEL 423DL ON RH PYLON. CORRECTIVE ACTION: REPAIRED ACCESS PANEL 423DL RH PYLON AS PER ER/A # 540187-14MA. (0607492)

Part: BONDING PLATE — CORRODED (FLAP TRK FAIRING) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION STATIC DISCHARGER PLATE-BONDING FLAP TRACK FAIRING 533CB ON LH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON FLAP TRACK FAIRING 533CB AS PER ER/A 620280-14. (0601042)

Part: ACCESS PANEL — CORRODED (ZONE 600) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION ACCESS PANEL 631CB BONDING STRAP ON RH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON FLAP TRACK FAIRING 631CB AS PER ER/A 620280-14. (0601048)

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION SHEAR TIE LOCATED FR28 AND BETWEEN STR38L TO STR39L IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE LOCATED FR28 AND BETWEEN STR38L TO STR39L IN FWD CARGO COMPARTMENT AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (0600953)

Part: BONDING PLATE — CORRODED (FLAP TRK FAIRING) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION STATIC DISCHARGER PLATE-BONDING FLAP TRACK FAIRING 532CB ON LH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON FLAP TRACK FAIRING 532CB AS PER ER/A 620280-14. (0601037)

Part: BONDING STRAP — CORRODED (FLAP TRK FAIRING) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION FLAP TRACK FAIRING 633CB BONDING STRAP ON RH WING CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON FLAP TRACK FAIRING 633CB AS PER ER/A 620280-14 REV. (0601045)

Part: PLATE — CORRODED (NR 2 FLAP TRACK) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION FOUND AT INB & OUTB PLATES TRACK #2, BEARING AT RIB 9 LEVEL. CORRECTIVE ACTION: REPAIR PER ERA 621041-14. (0600186)

Part: BONDING STRAP — CORRODED (ZONE 500) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION ACCESS PANEL 531CB BONDING STRAP ON LH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON FLAP TRACK FAIRING 531CB AS PER ER/A 620280-14. (0601050)

Part: ACCESS PANEL — DAMAGED (ZONE 300) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 ELONGATED HOLE ACCESS PANEL 335AB ON LH HORIZONTAL STABILIZER. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON ACCESS PANEL 335AB AT LH HORIZONTAL STABILIZER AS PER ER/A 620628-14. (0601055)

Part: CROSSBEAM — BENT (ZONE 100) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 BENT CROSS BEAM INTERNAL STRUCTURE LOCATED FR30 AND STR38L TO STR38R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED CROSSBEAM AND FASTENERS LOCATED FR30 AND STR38L TO STR38R IN FWD CARGO COMPARTMENT AS PER A319 SRM 51-42-11 AND SRM 51-72-11. (0601057)

Part: SKIN — CORRODED (ZONE 500) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION WAS FOUND IN TOP SKIN PANEL 2, TRAILING EDGE OVERHANG AREA, LH WING. CORRECTIVE ACTION: REPAIR PER ERA 619900-14. (0598728)

Part: RIB — CORRODED (FLAP TRK FAIRING) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION FOUND AT OUTBD FLAP TRACK #3 INNER & OUTER RIB 5 AT ECCENTRIC BEARING. CORRECTIVE ACTION: REPAIR PER ERA 620734-14. (0598319)

Part: BUSHING — CORRODED (ZONE 600) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION FIXED BUSHING I/B SIDE CENTER HINGE REAR SPAR ON SPOILER 3 RH WING REFER TO AMDS CARD 5770-1010-RT-DE FOR RII. CORRECTIVE ACTION: REPLACED FIXED BUSHING (1 EA) ON ATTACH FITTING I/B SIDE REAR SPAR OF SPOILER 3 RH WING. AS PER A319 SRM 51-72-12-911-002. (0595657)

Part: BEARING — EXCESS PLAY (ZONE 500) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 EXCESSIVE PLAY ON BEARING AILERON HINGE ARM 4 LH WING (1 EA). CORRECTIVE ACTION: REPLACED BEARING (1 E/A) AND SLEEVE (1 E/A) ON HINGE ARM #4 AILERON ON LH WING, AS PER CMM 57-51-54. (0595636)

Part: BEARING — EXCESS PLAY (ZONE 500) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 EXCESSIVE PLAY ON BEARINGS AILERON HINGE ARM #1 LH WING (1 EA). CORRECTIVE ACTION: REMOVED AND REPLACED BEARING (1 E/A) AND SLEEVE (1 E/A) ON HINGE ARM 1 AILERON ON LH AS PER CMM 57-51-54. (0595612)

Part: PROFILE — GOUGED (ZONE 100) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 GOUGE PROFILE LOCATED BTW FR 47/51 TO FR 55A STR 35R AFT CARGO COMPARTMENT (3 EA). CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS SECTION PER ERA 559065-14MA. (0593811)

Part: PROFILE — GOUGED (ZONE 100) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 GOUGE PROFILE LOCATED FR24A AND FROM - Y254 TO -Y12.92 FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS PER ERA 559065-14MA. (0593821)

Part: PROFILE — GOUGED (ZONE 100) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 GOUGE PROFILE LOCATED FR56 BTW STR41R TO STR38L IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS PER ERA 559065-14MA. (0593806)

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION SHEAR TIE LOCATED FR28 AND BETWEEN STR44 TO STR43R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE LOC. FR28 AND BTW STR44 TO STR43R IN FWD CARGO COMPARTMENT AS PER A319 SRM 51-42-11 AND SRM 51-72-11. (0590402)

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION STRINGER 41R LOCATED BTW FR63 TO FR64 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED STRINGER 41R BTW FR61 TO FR64 IN AFT CARGO COMPARTMENT AS PER A319 SRM 51-72-11 AND SRM 51-42-11. (0590478)

Part: PROFILE — CORRODED (ZONE 100) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION PROFILE LOCATED BETWEEN FR 63 TO FR 65 AND STR 38R AFT CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS SECTION I AS PER ER/A 559065-14MA. (0588589)

Part: PROFILE — CORRODED (ZONE 100) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION PROFILE LOCATED BETWEEN FR58 AND STR38L TO STR38R AFT CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS SECTION I AS PER ERA 559065-14MA. (0588632)

Part: PROFILE — CORRODED (ZONE 100) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION PROFILE LOCATED BETWEEN FR 47/51 TO FR 52 AND STR 38R AFT CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS SECTION I AS PER ERA 559065-14MA. (0588615)

Part: PROFILE — CORRODED (ZONE 100) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION PROFILE LOCATED AT LEVEL FR34 AND FROM STR35L TO STR38L FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS SECTION I AS PER ERA 559065-14MA. (0588635)

Part: PROFILE — CORRODED (ZONE 100) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION PROFILE LOCATED BTW FR 59 TO FR 63 STR 38R AFT CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS SECTION I AS PER ERA 559065-14MA. (0588650)

Part: PROFILE — CORRODED (ZONE 100) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION PROFILE LOCATED BETWEEN FR47/51 AND STR38L TO STR38R AFT CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS SECTION I AS PER ERA 559065-14MA. (0588626)

Part: PROFILE — SCRATCHED (ZONE 100) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION PROFILE LOCATED BETWEEN FR65 AND STR38L TO STR38R AFT CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS PER ER/A 559065-14MA. (0577644)

Part: ACCESS PANEL — CRACKED (ZONE 300) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CRACK ACCESS PANEL 322BL ON VERTICAL STABILIZER. CORRECTIVE ACTION: REPAIR INSTRUCTIONS ON ACCESS PANEL 322BL AT VERTICAL STABILIZER AS PER ER/A 620143-14. (0577592)

Part: PROFILE — SCRATCHED (ZONE 100) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION PROFILE LOCATED BETWEEN FR56 TO FR58 AND STR38L AFT CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS SECTION I AS PER ER/A 559065-14MA. (0577626)

Part: PROFILE — SCRATCHED (ZONE 100) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 SCRATCH PROFILE LOCATED FR24A AND +Y765 TO +Y12.92 FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS SECTION I AS PER ER/A 559065-14MA. (0577598)

Part: PROFILE — SCRATCHED (ZONE 100) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 SCRATCH ON PROFILE LOCATED FR24A AND FROM STR35L TO STR38R FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS PER EA/A 559065-14MA. (0577604)

Part: ACCESS PANEL — CRACKED (ZONE 300) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CRACK ACCESS PANEL 322AL ON VERTICAL STABILIZER. CORRECTIVE ACTION: REPAIRED PER ER/A 620158-14. (0577576)

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION STRINGER 42R BTW FR60 TO FR61 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED STRINGER 42R BTW FR60 TO FR64 IN AFT CARGO COMPARTMENT AS PER A319 SRM 51-72-11 AND A319 SRM 51-42-11. (0572369)

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION SHEAR TIE LOCATED FR28 AND BETWEEN STR40L TO STR41L IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE LOCATED FR28 AND BETWEEN STR40L TO STR41L IN FWD CARGO COMPARTMENT AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (0563668)

Part: SHEAR TIE — CORRODED (ZONE 200) · corrosion level 2 · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION SHEAR TIE LOCATED FR30 AND STR41R TO STR42R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE LOCATED FR30 AND STR41R TO STR42R IN FWD CARGO COMPARTMENT AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (0563807)

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION SHEAR TIE LOCATED FR28 AND BETWEEN STR42R TO STR43R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE LOCATED FR28 AND BETWEEN STR42R TO STR43R IN FWD CARGO COMPARTMENT AS PER A319 SRM 51-42-11 AND A319 SRM 51- 72-11. (0563805)

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CRACK INDICATION WAS FOUND AT LH FRONT WINDSHIELD FRAMING (CENTER POST, LOWER RADIUS). CORRECTIVE ACTION: REPAIRED PER ERA 619897-14AD. (0563108)

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION SHEAR TIE LOCATED FR28 AND BETWEEN STR42L TO STR41L IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE LOCATED FR28 AND BETWEEN STR42L TO STR41L IN FWD CARGO COMPARTMENT AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (0563662)

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION SHEAR TIE LOCATED FR28 AND BETWEEN STR42R TO STR41R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE LOCATED FR30 AND STR41R TO STR42R IN FWD CARGO COMPARTMENT AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (0563800)

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 NOSE FUSELAGE WINDSHIELD FRAMING CENTER POST LH CRACK DAMAGE. CORRECTIVE ACTION: REPAIRED PER ERA 619897-14AD. (0563161)

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION SHEAR TIE LOCATED FR28 AND BETWEEN STR39L TO STR40L IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE LOCATED FR28 AND BETWEEN STR39L TO STR40L IN FWD CARGO COMPARTMENT AS PER A319 SRM 51-42-11 AND SRM 51-72-11. (0563650)

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION SHEAR TIE LOCATED FR30 AND FROM STR40R TO STR41R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE LOCATED FR30 AND FROM STR4OR TO STR41R IN FWD CARGO COMPARTMENT AS PER A319 SRM 51-42-11 AND SRM 51-72-11. (0551469)

Part: BEARING — EXCESS PLAY (ZONE 500) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 EXCESSIVE PLAY ON BEARINGS AILERON HINGE ARM #2 LH WING (1 EA). CORRECTIVE ACTION: REPLACED BEARING (1 E/A) AND SLEEVE (1 E/A) ON AILERON HINGE ARM #2 ON LH WING AS PER AIRBUS CMM 57-51-54. (0551478)

Part: HINGE PIN — CORRODED (SPOILERS) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION CENTER HINGE PIN ON SPOILER #2, #3 AND #4 ON LH WING (6E/A). CORRECTIVE ACTION: REPLACED CENTER HINGE PIN ON SPOILER #2, #3 AND #4 ON LH WING (6E/A). (0547808)

Part: BEARING — EXCESS PLAY (AILERON ARM) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 EXCESSIVE PLAY ON BEARINGS AILERON HINGE ARM #5 LH WING (3 EA). CORRECTIVE ACTION: REPLACED BEARINGS (3 E/A) AND SLEEVES (3 E/A) ON HINGE ARM #5 AILERON ON LH WING, AS PER CMM 57-51-54. (0547807)

Part: ATTACH FITTING — CORRODED (ZONE 600) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION ON BUSHING ATTACH FITTING O/B SIDE REAR SPAR OF SPOILER 4 RH WING. CORRECTIVE ACTION: REPLACED BUSHING (1 EA) TO HINGE LATERAL O/B SIDE LUG REAR SPAR OF SPOILER 4 RH WING, AS PER A319 SRM 51-72-12-911-002. (0546311)

Part: SKIN — CORRODED (ZONE 600) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION TRAILING EDGE UPPER SKIN LOWER SURFACE AT LEVEL RIB 19 ON RH WING. CORRECTIVE ACTION: PERFORMED BLEND OUT ON AFFECTED AREA (4E/A POINTS) LOC. ON UPPER SKIN LOWER SURFACE AT TRAILING EDGE OVERHANG AREA BTW RIB 17 TORIB 20 ON RH WING AS PER A319 SRM 51-74-00. (0546224)

Part: BEARING — CORRODED (RT FLAP TRACK) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION ON HOUSING SPHERICAL BEARING TRACK 3 O/B FLAP RH WING. CORRECTIVE ACTION: INSTALLATION OF THE SERVICEABLE FLAP ASSY ACCOMPLISHED ON AMDS CARD # 2750 -6020-RT. (0541070)

Part: BUSHING — EXCESS PLAY (ZONE 800) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 EXCESSIVE PLAY PASSENGER CREW DOOR 841 BONDING BUSH ON UPPER AND LOWER CONNECTION LINK NEXT TO SUPPORT ARM (8 EA). CORRECTIVE ACTION: REPLACED BONDING BUSH ON UPPER AND LOWER CONNECTION LINK AND SUPPORT ARM OF PASSENGER CREW DOOR 841 AS PER A320 FAM AMM 52-11 -21-000-001-A, AMM 52-11-21-400-001-A AND AMM 52-10-00-915-001-A. (0539177)

Part: BUSHING — CORRODED (ZONE 600) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION ON BUSHING ATTACH FITTING I/B SIDE REAR SPAR OF SPOILER 3 RH WING. CORRECTIVE ACTION: REPLACED BUSHING (1 EA) ON ATTACH FITTING I/B SIDE REAR SPAR OF SPOILER 3 RH WING AS PER A319 SRM 51-72-12-911-002. (0535586)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION FLOOR SUPPORT -Y1292 LOCATED FROM FR12 TO FR24 FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR SUPPORT -Y1292 LOCATED FR12 TO FR24 FWD GALLEY AREA. AS PER A319 SRM 51-42-11 AND SRM 51-72-11.

Part: BUSHING — CORRODED (ZONE 500) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION ON FIXED BUSH LOCATED ON BRACKET OF THE AILERON HINGE ARM #3 UPPER POSITION AT REAR SPAR LH WING (2 EA). CORRECTIVE ACTION: REPLACED BUSHINGS (2 E/A) ON AILERON HINGE ARM 3 UPPER POSITION REAR SPAR LH WING AND PERFORMED VISUAL INSPECTION ON BORES NO DAMAGES FOUND AS PER A319 SRM 51-72-12-911-002. (0535614)

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION WEB FRAME 20 AT LEVEL STR 23RH SIDE AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED WEB FRAME 20 TO FRAME 24 AT LEVEL STR 23RH SIDE AT FWD GALLEY AREA AS PER A319 SRM 51-72-11 AND SRM 51-42-11. (0535450)

Part: BUSHING — CORRODED (ZONE 600) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION ON BUSHING ATTACH FITTING O/B SIDE REAR SPAR OF SPOILER 2 RH. CORRECTIVE ACTION: REPLACED BUSHING (1 EA) ON ATTACH FITTING O/B SIDE REAR SPAR OF SPOILER 2 RH WING AS PER A319 SRM 51-72-12-911-002. (0535475)

Part: BUSHING — CORRODED (ZONE 600) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION ON BUSHING ATTACH FITTING I/B SIDE REAR SPAR OF SPOILER 5 RH WING. CORRECTIVE ACTION: REPLACED BUSHING (1 EA) ON ATTACH FITTING I/B SIDE REAR SPAR OF SPOILER 5 RH WING. AS PER A319 SRM 51-72-12-911-002. (0535478)

Part: BUSHING — CORRODED (ZONE 600) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION FIXED BUSHING O/B SIDE CENTER HINGE REAR SPAR ON SPOILER 5 RH WING. CORRECTIVE ACTION: REPLACED FIXED BUSHING (1 EA) OF O/B SIDE ON CENTER HINGE REAR SPAR ON SPOILER 5 RH WING AS PER A319 SRM 51-72-12-911-002. (0535595)

Part: BUSHING — CORRODED (ZONE 500) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION ON FIXED BUSH LOCATED ON BRACKET OF THE AILERON HINGE ARM #3 LOWER POSITION AT REAR SPAR LH WING (2 EA). CORRECTIVE ACTION: REPLACED BUSHINGS (2 EA) ON AILERON HINGE ARM 3, LOWER POSITION, REAR SPAR, LH WING. AS PER A319 SRM 51-72-12-911-002. (0535620)

Part: SKIN — CORRODED (ZONE 500) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION UPPER SURFACE EXTERNAL SKIN LOCATED BTW RIB 11 TO RIB 12 AT LEVEL STR 11 ON LH WING. CORRECTIVE ACTION: PERFORMED BLEND OUT LOC. UPPER SURFACE EXTERNAL SKIN LOCATED ON RIB 11 PLUS 13 IN AT LEVEL STR 11 ON LH WING AS PER A319 SRM 51-74-00. (0533926)

Part: SUPPORT WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION STRINGER 23L SUPPORT WEB BTW FR69 TO FR70 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED SUPPORT WEB LOC. ON STRINGER 23L BTW FR69 TO FR70 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (0528166)

Part: BOTTLE — NO TEST (ZONE 800) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 DONT PASS OPERATIONAL TEST PASSENGER CREW DOOR 842 EMERGENCY DOOR DAMPER. CORRECTIVE ACTION: REPLACED PER A319 AMM 52-13-14-000-001-B. (0527091)

Part: ROLLER — EXCESS PLAY (LT TE FLAP) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 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. (0526876)

Part: ROLLER — EXCESS PLAY (RT TE FLAP) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 EXCESSIVE PLAY CRUISE ROLLER I/B FLAP ON RH WING. CORRECTIVE ACTION: REPLACED CRUISE ROLLER I/B FLAP ON RH WING AS PER AIRBUS CMM 57-52-21. (0526868)

Part: ROLLER — EXCESS PLAY (LT TE FLAP) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 EXCESSIVE PLAY CRUISE ROLLER OB FLAP ON LH WING. CORRECTIVE ACTION: REPLACED CRUISE ROLLER OB FLAP ON L/H WING AS PER AIRBUS CMM 57- 53-21. (0526845)

Part: ROLLER — EXCESS PLAY (RT TE FLAP) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 EXCESSIVE PLAY CRUISE ROLLER OB FLAP ON RH WING. CORRECTIVE ACTION: REPLACED CRUISE ROLLER OB FLAP ON R/H WING AS PER AIRBUS CMM-57- 53-21. (0526861)

Part: SKIN — CORRODED (ZONE 500) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION UPPER SURFACE EXTERNAL SKIN LOCATED BTW RIB 3 TO RIB 4 AT LE VEL STR 11 ON LH WING. CORRECTIVE ACTION: PERFORMED BLEND OUT LOC. UPPER SURFACE EXTERNAL SKIN LOCATED ON RIB 3 PLUS 7 IN. AT LEVEL STR 11 AS PER A319 SRM 51-74-00. (0525036)

Part: SKIN — CORRODED (ZONE 500) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION UPPER SURFACE EXTERNAL SKIN LOCATED BTW RIB 4 TO RIB 5 FRONT SPAR (2 POINTS). CORRECTIVE ACTION: PERFORMED BLEND OUT LOC. ON UPPER SURFACE EXTERNAL SKIN BTW RIB 4 TO RIB 5 FROM SPART LH WING (2 POINTS) AS PER A319 SRM51-74-00. (0525058)

Part: SKIN — CORRODED (ZONE 500) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION UPPER SURFACE EXTERNAL SKIN LOCATED BTW RIB 8 TO RIB 9 REAR SPAR ON LH WING. CORRECTIVE ACTION: PERFORMED BLEND OUT ON AFFECTED AREA (5 POINTS) LOC. ON UPPER SURFACE EXTERNAL SKIN LOCATED BTW RIB 8 TO RIB 9 REARSPAR ON LH WING. AS PER A319 SRM 51-74-00. (0525061)

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION FLOOR BEAM -Y254 LOCATED FROM FR12 TO FR24 FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED SEAT TRACK - Y254, LOC. BTW FR12 TO FR24 AT FWD GALLEY AREA AS PER A319 SRM 51-42-11 AND SRM 51-72-11. (0515855)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION FLOOR BEAM -Y765 BTW FR66 TO FR68 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y765 LOCATED BTW FR66 TO FR70 AT AFT GALLEY AREA. AS PER A319 SRM 51-42-11 AND SRM 51-72-11. (0516644)

Part: STRUT — CORRODED (ZONE 600) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION INTERCONNECTING STRUT ON RH WING. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT ON RH WING, THE INSTALLATION IS TO BE ACCOMPLISHED WITH AMDS CARD 2750-6020-RT AND AMDS2750-6010. (0513439)

Part: STRUT — CORRODED (ZONE 500) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION INTERCONNECTING STRUT ON LH WING. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT ON LH WING PER AMDS CARD 2750-6010-LT AND AMDS CARD2750 -6020-LT. (0513445)

Part: ACTUATOR — CORRODED (FLAP) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION ON FLAP ROTARY ACTUATOR 2 LOCATED AT INTERNAL SPLINE OF THE TORQUE SHAFT LH WING. CORRECTIVE ACTION: REPLACED PER AMDS CARD 2754-4001-LT. (0514683)

Part: BUSHING — EXCESS PLAY (ZONE 800) · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 EXCESSIVE PLAY ON PASSENGER CREW DOOR 831 ON BONDED BUSHES OF UPPER A ND LOWER CONNECTION LINK NEXT TO SUPORT ARM AND UPPER AND LOWER CONNEC TION SUPPORT ARM AT FWD GALLEY AREA (8 EA). CORRECTIVE ACTION: REPLACED ON PASSENGER CREW DOOR 831 BONDED BUSHES OF UPPER AND LOWER CONNECTION LINK NEXT TO SUPORT ARM AND UPPER AND LOWER CONNECTION SUPPORT ARM AT FWD GALLEY AREA (8 EA) AS PER A320 FAM AMM 52-11-21-000-001-A, AND AS PER A320 FAM AMM 52-11-21-400- 001-A. (0512527)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 58,493 hrs · 30,670 cycles

SHIP 3143 CORROSION SEAT TRACK -Y765 LOCATED FROM FR12 TO FR24 FWD GALLEY AREA. REPLACED SEAT TRACK -Y765 LOCATED FROM FR12 TO FR24 FWD GALLEY AREA AS PER A319 SRM 51-42-11 AND SRM 51-72-11. (0513290)

Part: UNKNOWN — ODOR (CABIN) · airframe 57,985 hrs · 30,400 cycles

SHIP 3143 DURING DEPLANING TWO PAX REPORTED SMELL OF SMOKE DURING TAKEOFF. CORRECTIVE ACTION: C/W WORK CARD 0550-2002. (5351006)

Part: GUST LOCK — FAULTED (L2 DOOR) · airframe 57,924 hrs · 30,359 cycles

SHIP 3143 DOOR 2L GUST LOCK IS NOT LOCKING WHILE OPEN. CORRECTIVE ACTION: LUBED GUST LOCK HOOK ASSY CKS NML PER A320 52-12. (5876458)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,686 hrs · 29,727 cycles

SHIP 3143 -DIV- TO PHX DUE TO ANTI ICE ENG2 VALVE CLSD ECAM MESSAGE. CORRECTIVE ACTION: T/S. NO FAULTS. FOUND HARD LINE SNAPPED OFF AT THE B-NUT. REPLACED HARD SENSE LINE FOR ANTI-ICE VALVE. (4278924)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,138 hrs · 29,456 cycles

SHIP 3143 DOOR 2L LIGHT INDICATION INOPERATIVE. CORRECTIVE ACTION: REMOVED DIBRIS FROM DOOR 2L SLIDE GIRT BAR AND OPERATED SYSTEM PER A319 AMM 52- 70. (4909287)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,101 hrs · 29,437 cycles

SHIP 3143 LT WING FEED THROUGH PLATE HAS 1EA DAMAGED HOLE. CORRECTIVE ACTION: COMPLIED WITH ER/A 611961-14. (2966265)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,104 hrs · 29,438 cycles

SHIP 3143 G5 GALLEY STABBING COVER PLATE CORRODED. CORRECTIVE ACTION: REPAIRED PER ER/A 611882-14. (2966276)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,693 hrs · 29,219 cycles

SHIP 3143 - DIV - TO DFW DUE TO O2 MASKS DROPPED IN ROW 19ABC AND ROW 3CD. CORRECTIVE ACTION: REPACKED O2 MASK PSU IN ROW 19ABC AND ROW 3CD. OK FOR SERVICE. (4035360)

Part: MASK — DEPLOYED · airframe 53,199 hrs · 27,890 cycles

SHIP 3143 - FWD LAV O2 MASK DEPLOYED DURING CLIMB OUT. CORRECTIVE ACTION: STOWED O2 MASK I/A/W A320 AMM 35-21. (8715466)

Part: CONTROL UNIT — INOPERATIVE (F) · airframe 53,159 hrs · 27,870 cycles

SHIP 3143 - DIV - TO MIA DUE TO FLIGHT CREW REPORT OF AIRFRAME VIBRATION FELT IN AFT FUSELAGE. VIBRATIONS LESSENED AT LOWER SPEEDS AND STOPPED AT 250KTS. CORRECTIVE ACTION: FOUND AFT DRAIN MAST HEATER C/B POPPED AND HEAVY ICE BUILDUP ON MAST. PLACED SYSTEM ON MEL AND CONTINUED FLIGHT. REMOVED AND REPLACED DRAIN MAST CONTROL UNIT IAW A319 AMM 30-71. (8715448)

Part: NONE — NONE · airframe 52,729 hrs · 27,629 cycles

SHIP 3143 - RIGHT MAIN LANDING GEAR ANCHOR FITTING BORE AND FACES CORRODED. CORRECTIVE ACTION: REPAIRED RH MLG RETRACT ACTUATOR ANCHORAGE FITTING PER A319 SRM 57-26-13.(2229100)

Part: HEAT EXCHANGER — DEFECTIVE (001) · airframe 52,580 hrs · 27,547 cycles

SHIP 3143 -CREW REPORTED DIRTY SOCK SMELL IN CABIN. CORRECTIVE ACTION: CLEANED APU PER WORKCARD 4916-2001. C/W PACK BURNOUT PER 4916-2001. COMPLIED WITH WORK AND 0550-2002. (8851900)

Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT 11AB) · airframe 50,719 hrs · 26,529 cycles

SHIP 3143 - ON TAKEOFF OXYGEN MASK AT 11 A/B DROPPED DOWN. CORRECTIVE ACTION: REPACKED PASS O2 MASK 11 A/B PER A319 AMM 35-21. OK FOR SVC. (7351178)

Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT 14 ABC) · airframe 50,719 hrs · 26,529 cycles

SHIP 3143 - ON TAKE OFF OXYGEN MASK AT 14A,B,C FELL DOWN. CORRECTIVE ACTION: REINSTALLED OXYGEN MASKS AT SEAT ROW 14ABC, REF A319 AMM 35-21. (7351174)

Part: O-RING — BLOWN (HYD SYSYTEM) · airframe 50,023 hrs · 26,205 cycles

SHIP 3143 - HYD - HYD G RSVR LO LVL ECAM MSG DURING CRUISE AT FL380, PERFORMED ECAM/QRH PROCEDURE RESULTING IN GRAVITY EXTENSION OF LANDING GEAR. CORRECTIVE ACTION: FOUND GREEN EDP HYD PRESSURE SWITCH HOUSING LOOSE AND "O" RING BLOWN OUT. REPLACED PACKING PER A319 AMM 29-11.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,790 hrs · 24,392 cycles

CRACK INDICATION ON FRAME 68 LT SIDE AFT FACE WEB JOINT RADIUS AT STR 8 (L=0.270 INCH) AT AFT GALLEY AREA (1 EA). REPAIR ON FRAME 68 LT AFT FACE WEB AT STR 8 AT AFT GALLEY AREA AS PER SRM 53-41-12-300-012 AND ER/A 581051- 14AD REV ORIGINAL. REPAIR APROVAL IS LIMITED TO 60,500FC FROM FIRST FLIGHT AS PER ER/A 581051-14AD.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 46,790 hrs · 24,392 cycles

CRACK INDICATION ON FRAME 16 LT SIDE AT OPEN FASTENER HOLES UPPER INBOARD AND LOWER INBOARD AT DOOR STOP 7 (CRACK DIRECTIONS ARE: UPPER: 3 O'CLOCK, LOWER: 2 AND 3 OCLOCK) AT FWD GALLEY AREA (1 EA). REPLACED FITTING INTERCOSTAL ON FRAME 16 LT SIDE AND LOWER INBOARD AT DOOR STOP 7 AT FWD GALLEY AREA AS PER SRM 51-42-11, SRM 51-72-11 AND DWG #D53112300.

Part: ANGLE — CRACKED (RT MLG WW) · airframe 46,790 hrs · 24,392 cycles

CRACK STRUCTURE SUPPORT AFT TI-ANGLE LOCATED AT FR 42 R/SIDE IN MAIN WHEEL WELL (1 EA) (AD 19-08-07), REQUIRED PRIOR TO FURTHER FLIGHT ). REPLACED STRUCTURE SUPPORT AFT TI-ANGLE LOCATED AT FR42 RT SIDE IN MAIN WHEEL WELL (1E/A) AS PER CARD #5353-01006-03.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 46,790 hrs · 24,392 cycles

CRACK INDICATION ON FRAME 16 RT SIDE AT OPEN FASTENER HOLES UPPER INBOARD AND LOWER INBOARD AT DOOR STOP 7 (CRACK DIRECTIONS ARE: UPPER: 9 O CLOCK, LOWER: 9 AND 11 OCLOCK) AT FWD GALLEY AREA (2 EA). REPLACED FITTING (INTERCOSTAL) ON FRAME 16 RT SIDE AND LOWER INBOARD AT DOOR STOP 7 AT FWD GALLEY AREA AS PER SRM 51- 42-11, SRM 51-72-11 AND DWG #D53112300.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,790 hrs · 24,392 cycles

CORROSION LEVEL: 2. CORROSION FLOORBEAM +Y254 LOCATED BTW FR 12 TO FR 24 AT FWD GALLEY AREA (1 EA). REPLACED FLOORBEAM +Y254 LOCATED BTW FR12 TO FR24 AT FWD GALLEY AREA (1E/A) AS PER SRM 51-72-11, SRM A319 51-42-11 AND DWG #D53-110920 ISSUE "D", D53110984 ISSUE "B", D53112816 ISSUE "G" MEASURE OF CORROSION IS 0.010".

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,790 hrs · 24,392 cycles

CORROSION LEVEL: 2. CORROSION FLOORBEAM +Y1292 AT LEVEL FR 16 FWD GALLEY AREA (1 EA ) (SSI 531189). REPLACED FLOORBEAM +Y1292 BTW FR12 AND FR24 FWD GALLEY AREA AS PER SRM 51-72-11 AND DWG D53112812.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,790 hrs · 24,392 cycles

CORROSION LEVEL: 2. CORROSION RAIL DUMMY -Y81 AT LEVEL FR 16 FWD GALLEY AREA (SSI 531189). REPLACED RAIL DUMMY -Y81 BTW FR 12 TO FR 16 FWD GALLEY AREA AS PER SRM 51-72-11 AND DWG D53112830 REPLACED DUE TO CORROSION EXCEED THE PERMITED ON SRM REMAINING THICKNESS IS: 0".

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,790 hrs · 24,392 cycles

CORROSION LEVEL: 2. CORROSION RAIL DUMMY Y503.2 AT LEVEL FR 16 FWD GALLEY AREA (1 EA) (SS I531189). REPLACED RAIL DUMMY Y503.2 AT LEVEL FR 16 FWD GALLEY AREA ASPER 51-72-11 SRM AND DRAWING D53112825.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,790 hrs · 24,392 cycles

CORROSION LEVEL: 2. CORROSION FRAME 71 AT SUPPORT ANGLE LOCATED FWD CUT OUT INTERNAL AREA OF ACCESS DOOR 312AR AT LOWER FUSELAGE. REPLACED SUPPORT ANGLE LOC FR 71 FWD CUT OUT INTERNAL AREA OF ACCESS DOOR 312AR IN LOWER FUSELAGE ASPER SRM 51-72-11 AND DWG 53571510.

Part: SKIN — CORRODED (FRAMES 69-70) · airframe 41,872 hrs · 21,822 cycles

CORROSION ON THE SKIN BETWEEN FRAMES 69 TO 70, STRINGERS 31 - 32R. REPAIRED IAW SRM 53-41-11-300-004.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 40,122 hrs · 21,054 cycles

AFT ATG HAS OVER SIZE HOLES WITH NO EDGE DISTANCE, COMPLIED WITH ERA 557100-14 REV O,1

Part: LIGHT — INOPERATIVE (EXIT HANDLE) · airframe 39,623 hrs · 20,786 cycles

RIGHT OVERWING EMERGENCY EXIT HANDLE LED LIGHT INOPERATIVE, REPLACED LIGHT

Part: STRINGER — CORRODED (FRAME 62) · airframe 31,420 hrs · 16,295 cycles

AFT CARGO BILGE, STRINGER 41R CORRODED UNDER AT FRAME 62. REMOVED CORROSION IAW SRM 51-74-00. R & R STRINGER SECTION IAW DWG D53476433, D53476324 & SRM 51-42-11.

Part: PLATE — CORRODED (L2 DOOR) · airframe 31,420 hrs · 16,295 cycles

L2 DOOR AFT PLATE ASSY CORRODED. NO ALLOWABLE LIMIT ON SRM. L2 DOOR PLATE ASSY REPLACED IAW SRM 51-72-00.

Part: SKIN — CHAFED (LT WING SLAT) · airframe 31,420 hrs · 16,295 cycles

LEFT WING NR 3 SLAT LOWER SURFACE INBD UPPER T/E HAS CHAFED. REMOVED DAMAGE AREA, 1.900" X 0.600" IAW SRM 57-44-21, FIG 202. HFEC IAW NTM 51-10-08 NO CRACK INDICATION NOTED. FABRICATED & INSTALLED EXTERNAL PLATE FROM MATERIAL 2024-T3 0.071C BATCH 2500590, & SKIN INSERT FROM MATERIAL 2024-T3 0.090C BATCH 2540972 IAW SRM 51-42-11 & SRM 57-44-21, FIG 202. INSTALLED ID TAG IAW PS 900-5-1 NR O4. PERMANENT REPAIR.

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 31,420 hrs · 16,295 cycles

AFT CARGO BAY SLOPE PANEL 152WG HAS DAMAGED INSERT HOLE & DISBONDED. SLOPE PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 31,420 hrs · 16,295 cycles

AFT CARGO BAY FLOOR PANEL 151CE HAS DEEP SCRATCHES & MULTIPLE DENTS. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 31,420 hrs · 16,295 cycles

AFT CARGO BAY SLOPE PANEL 151DE HAS MULTIPLE DENTS & CRACKS. FABRICATED SLOPE PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 31,420 hrs · 16,295 cycles

AFT CARGO BAY SLOPE PANEL 151UG HAS SEVEN EXISTING REPAIRS & MULTIPLE DENTS. FABRICATED SLOPE PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (FWD CARGO BAY) · airframe 31,420 hrs · 16,295 cycles

FWD CARGO BAY SLOPE PANEL 132DG HAS MULTIPLE DENTS, DISBONDED & CRACKED. FABRICATED SLOPE PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 31,420 hrs · 16,295 cycles

AFT CARGO BAY FLOOR PANEL 161PF EDGE DISBONDED AND TOP SKIN LIFTED OFF. FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 31,420 hrs · 16,295 cycles

AFT CARGO BAY SLOPE PANEL 151AE HAS MULTIPLE DENTS & DISBONDED. FABRICATED SLOPE PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 31,420 hrs · 16,295 cycles

AFT CARGO BAY SLOPE PANEL 162BF HAS MULTIPLE DENTS & DISBONDED. SLOPE PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 31,420 hrs · 16,295 cycles

AFT CARGO BAY SLOPE PANEL 151FE HAS MULTIPLE DENTS & PUNCTURED. FABRICATED SLOPE PANEL IAW SRM 53-02-00, FIG. 209 & DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 31,420 hrs · 16,295 cycles

AFT CARGO BAY SLOPE PANEL 161BF HAS EXISTING REPAIR & MULTIPLE DENTS. FABRICATED SLOPE PANEL IAW SRM 53-02-00, FIG. 209 & DWG NW3D25-40532.

Part: FLOOR PANEL — DAMAGED (FWD CARGO BAY) · airframe 31,420 hrs · 16,295 cycles

FWD CARGO BAY SLOPE PANEL 131BF HAS NINE PREVIOUS REPAIRS, MULTIPLE DENTS, DISBONDED & CRACKED, SLOPE PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 31,420 hrs · 16,295 cycles

AFT CARGO BAY SLOPE PANEL 152TG HAS MULTIPLE DENTS, DISBONDED & CRACKED HONEYCOMB, FABRICATED SLOPE PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 31,420 hrs · 16,295 cycles

AFT CARGO BAY FLOOR PANEL 151ZG HAS MULTIPLE DENTS & PUNCTURES. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG NW3D25-40532.

Part: FLOOR PANEL — DAMAGED (FWD CARGO BAY) · airframe 31,420 hrs · 16,295 cycles

FWD CARGO BAY FLOOR PANEL 131CG HAS MULTIPLE DENTS & PUNCTURED. FLOOR PANEL. FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (FWD CARGO BAY) · airframe 31,420 hrs · 16,295 cycles

FWD CARGO BAY SLOPE PANEL 131EG HAS FIVE PREVIOUS REPAIRS & MULTIPLE DENTS. FABRICATED SLOPE PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 31,420 hrs · 16,295 cycles

AFT CARGO BAY FLOOR PANEL 161NF HAS DAMAGED INSERTS AND MULTIPLE DENTS. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 31,420 hrs · 16,295 cycles

AFT CARGO BAY SLOPE PANEL 151GE HAS EXISTING REPAIR, MULTIPLE DENTS & DISBONDED. FABRICATED SLOPE PANEL IAW SRM 53-02-00, FIG 209, DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 31,420 hrs · 16,295 cycles

AFT CARGO BAY SLOPE PANEL 151TG DISBONDED. FABRICATED SLOPE PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 31,420 hrs · 16,295 cycles

AFT CARGO BAY FLOOR PANEL 161DF FWD EDGE DISBONDED, FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 31,420 hrs · 16,295 cycles

AFT CARGO BAY SLOPE PANEL 151HE HAS EXISTING REPAIR, MULTIPLE DENTS & PUNCTURED. FABRICATED SLOPE PANEL IAW SRM 53-02-00, FIG. 209 & DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (FWD CARGO BAY) · airframe 31,420 hrs · 16,295 cycles

FWD CARGO BAY SLOPE PANEL 132EG HAS MULTIPLE DENTS, DISBONDED & CRACKED. FABRICATED SLOPE PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 31,420 hrs · 16,295 cycles

AFT CARGO BAY SLOPE PANEL 151BE HAS THREE EXISTING REPAIRS & MULTIPLE DENTS. SLOPE PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (FWD CARGO BAY) · airframe 31,420 hrs · 16,295 cycles

FWD CARGO BAY SLOPE PANEL 131DG HAS THREE PREVIOUS REPAIRS, MULTIPLE DENTS, DISBONDED & CRACKED. FABRICATED SLOPE PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 31,420 hrs · 16,295 cycles

AFT CARGO BAY FLOOR PANEL 151PE HAS MULTIPLE DENTS, DISBONDED & CRACKED HONEYCOMB. AFT CARGO FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (FWD CARGO BAY) · airframe 31,420 hrs · 16,295 cycles

FWD CARGO BAY SLOPE PANEL 131CF HAS THREE PREVIOUS REPAIRS, MULTIPLE DENTS & DISBONDED. FABRICATED SLOPE PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 31,420 hrs · 16,295 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 151VG HAS MULTIPLE DENTS. FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40532.

Part: FLOOR PANEL — DELAMINATED (AFT CABIN) · airframe 31,420 hrs · 16,295 cycles

AFT CABIN FLOOR PANEL 261DF, DELAMINATED. FOUND OUT OF LIMITS IAW SRM 53-12-00. DIAGRAM 102. REPLACED FLOOR PANEL IAW SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FRAME 66) · airframe 31,420 hrs · 16,295 cycles

AFT UTILITY AREA FLOOR SUPPORT -Y1292 FRAME 66 CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. R & R FLOOR SUPPORT IAW TRM 53-21-01.

Part: FLOOR SUPPORT — CORRODED (FRAMES 68-69) · airframe 31,420 hrs · 16,295 cycles

AFT UTILITY AREA FLOOR SUPPORT -Y1292 FRAMES 68-69 CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS. R & R FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · airframe 31,420 hrs · 16,295 cycles

AFT UTILITY AREA FLOOR SUPPORT -Y1292 FRAMES 66-68 CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS. R & R FLOOR SUPPORT IAW TRM 53-21-01.

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 31,420 hrs · 16,295 cycles

MAIN CABIN FLOORBOARD 221PF DAMAGED. FOUND OUT OF LIMITS IAW SRM 53-12-00, DIAGRAM 103. FLOORBOARD FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · airframe 31,420 hrs · 16,295 cycles

AFT UTILITY AREA FLOOR SUPPORT Y1292 FRAMES 66-68 CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14, FIG. 102. R & R FLOOR SUPPORT IAW SRM 51-42-11 & TRM 53-21-01.

Part: FLOOR SUPPORT — CORRODED (FRAME 66) · airframe 31,420 hrs · 16,295 cycles

AFT UTILITY AREA FLOOR SUPPORT Y1292 AT FRAME 66 CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14, FIG. 102. R & R FLOOR SUPPORT IAW SRM 51-42-11 & TRM 53-21-01.

Part: SILL — CORRODED (FRAMES 66-68) · airframe 31,420 hrs · 16,295 cycles

AFT UTILITY AREA BETWEEN FRAMES 66 - 68 RT DOOR SILL CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-41-13, FIG 1, SH 3. R & R SILL IAW SRM 51-42-11 AND DWG D53480019.

Part: FLOOR SUPPORT — CORRODED (FRAMES 68-69) · airframe 31,420 hrs · 16,295 cycles

AFT UTILITY AREA FLOOR SUPPORT Y1292 FRAMES 68-69 CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14, FIG. 102. R & R FLOOR SUPPORT IAW SRM 51-42-11 & TRM 53-21-01.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 31,420 hrs · 16,295 cycles

MAIN CABIN FLOORBOARD 231WG DELAMINATED. FOUND OUT OF LIMITS IAW SRM 53-12-00, DIAGRAM 102. FLOORBOARD FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 31,420 hrs · 16,295 cycles

MAIN CABIN FLOORBOARD 242HF DAMAGED. FOUND OUT OF LIMITS IAW SRM 53-12-00, DIAGRAM 102. FLOORBOARD FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.

Part: FLOOR PANEL — DELAMINATED (FWD CABIN) · airframe 31,420 hrs · 16,295 cycles

FORWARD CABIN FLOOR PANEL 222CF DELAMINATED. FOUND OUT OF LIMITS IAW SRM 53-12-00 DIAGRAM 102. FLOOR PANEL FABRICATED IAW SRM 53-02-00, PARA 84, FIG 209 AND DWG NW3ED25-40640.

Part: SKIN — SCRATCHED (NR 1 SLAT) · airframe 31,420 hrs · 16,295 cycles

RT WING NR 1 SLAT TOP SKIN BETWEEN NR 3 & NR 4 TRACKS SCRATCHED. REMOVED SCRATCH BY CLEANED IAW SRM 51-73-00, L=1", W=.200", D=0.001 & MAINTAINED SMOOTH CONTOUR FINISH IAW SRM 57-40-00, FIG 105 & FIG 106.

Part: SKIN — GOUGED (L1 DOOR) · airframe 31,420 hrs · 16,295 cycles

L1 DOOR UPPER AFT CORNER GOUGED. BLENDED AREA IAW SRM 51-73-00. FOUND WITHIN LIMITS IAW SRM 53-11-11, FIG 114.

Part: FITTING — CORRODED (DOOR FRAME) · airframe 31,420 hrs · 16,295 cycles

AFT UTILITY AREA RT AFT DOOR CUTOUT FITTING AT FRAME 68, LOWER CORNER CORRODED. REMOVED CORROSION IAW SRM 51-74-00. NO ESTABLISH LIMITS IN SRM. REPLACED CORNER FITTING.

Part: FLOOR SUPPORT — CORRODED (FRAMES 16-21) · airframe 31,420 hrs · 16,295 cycles

FORWARD UTILITY AREA FLOOR SUPPORT -Y254 FRAMES 16 - 21 UPPER FLANGE CORRODED. REMOVED CORROSION IAW SRM 51-74-00. R & R FLOOR SUPPORT IAW TRM 53-21-01.

Part: GIRT BAR — CORRODED (DOOR) · airframe 31,420 hrs · 16,295 cycles

AFT UTILITY AREA LT DOOR SILL AFT GIRT BAR FITTING CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW TRM 53-41-13, FIG 1, SHEET 3. R & R DOOR SILL IAW SRM 51-42-11 & DWG D53480019.

Part: FLOOR PANEL — DELAMINATED (CENTER CABIN) · airframe 31,420 hrs · 16,295 cycles

CENTER CABIN FLOOR PANEL 242FF DELAMINATED. FOUND OUT OF LIMITS IAW SRM 53-12-00, DIAGRAM 102. FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.

Part: FLOOR PANEL — DELAMINATED (AFT CABIN) · airframe 31,420 hrs · 16,295 cycles

AFT CABIN FLOOR PANEL 261PF DELAMINATED. FOUND OUT OF LIMITS IAW SRM 53-12-00, DIAGRAM 102. FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.

Part: FLOOR PANEL — DELAMINATED (FWD CABIN) · airframe 31,420 hrs · 16,295 cycles

FORWARD CABIN FLOOR PANEL 221EF DELAMINATED. FOUND OUT OF LIMITS IAW SRM 53-12-00, DIAGRAM 102. FLOOR PANEL FABRICATED IAW SRM 53-02-00 FIG 209 AND DWG 3D25-40640.

Part: FLOOR PANEL — DELAMINATED (FWD CABIN) · airframe 31,420 hrs · 16,295 cycles

FORWARD CABIN FLOOR PANEL 222EF DELAMINATED. FOUND OUT OF LIMITS IAW SRM 53-12-00, DIAGRAM 102. FLOOR PANEL FABRICATED IAW SRM 53-02-00 FIG 209 AND DWG 3D25-40640.

Part: PLATE — CORRODED (L2 DOOR) · airframe 31,420 hrs · 16,295 cycles

L2 DOOR FWD PLATE ASSY CORRODED. NO ALLOWABLE LIMITS IN SRM. REPLACED PLATE ASSY IAW SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (AFT CABIN) · airframe 31,420 hrs · 16,295 cycles

AFT CABIN FLOOR PANEL 261HG DELAMINATED. FOUND OUT OF LIMITS IAW SRM 53-12-00 DIAGRAM 102. FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG.209 AND DWG 3D25-40640.

Part: FLOOR PANEL — DELAMINATED (FWD CABIN) · airframe 31,420 hrs · 16,295 cycles

FORWARD CABIN FLOOR PANEL 221DF DELAMINATED. FOUND OUT OF LIMIT IAW SRM 53-12-00, DIAGRAM 102. FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.

Part: FLOOR PANEL — DELAMINATED (CENTER CABIN) · airframe 31,420 hrs · 16,295 cycles

CENTER CABIN FLOOR PANEL 241FF, DELAMINATED. FOUND OUT OF LIMITS IAW SRM 53-12-00, DIAGRAM 102. FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.

Part: FLOOR PANEL — DELAMINATED (AFT CABIN) · airframe 31,420 hrs · 16,295 cycles

AFT CABIN FLOOR PANEL 262HG DELAMINATED. FOUND OUT OF LIMITS IAW SRM 53-12-00, DIAGRAM 102. AFT CABIN FLOOR PANEL FABRICATED IAW SRM 53-02-00 FIG 209 AND DWG 3D25-40640.

Part: FLOOR PANEL — DELAMINATED (FWD CABIN) · airframe 31,420 hrs · 16,295 cycles

FORWARD CABIN FLOOR PANEL 231FF DELAMINATED. FOUND OUT OF LIMITS IAW SRM 53-12-00, DIAGRAM 102. FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.

Part: PLATE — CORRODED (R2 DOOR) · airframe 31,420 hrs · 16,295 cycles

R2 DOOR AFT PLATE ASSY CORRODED. NO ALLOWABLE LIMITS ON SRM. REPLACED PLATE ASSY IAW SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (CENTER CABIN) · airframe 31,420 hrs · 16,295 cycles

CENTER CABIN FLOOR PANEL 252GF DELAMINATED, FOUND OUT OF LIMITS IAW SRM 53-12-00 DIAGRAM 102. FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.

Part: FLOOR PANEL — DELAMINATED (FWD CABIN) · airframe 31,420 hrs · 16,295 cycles

FORWARD CABIN FLOOR PANEL 232EF DELAMINATED. FOUND OUT OF LIMITS IAW SRM 52-12-00, DIAGRAM 102. FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 31,420 hrs · 16,295 cycles

MAIN CABIN FLOORBOARD 241LF IS DAMAGED. FLOORBOARD FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.

Part: FLOOR PANEL — DELAMINATED (AFT CABIN) · airframe 31,420 hrs · 16,295 cycles

AFT CABIN FLOOR PANEL 261EF DELAMINATED, FOUND OUT OF LIMITS IAW SRM 53-12-00, DIAGRAM 102. FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.

Part: FLOOR PANEL — DELAMINATED (CENTER CABIN) · airframe 31,420 hrs · 16,295 cycles

CENTER CABIN FLOOR PANEL 251LG DELAMINATED. FOUND OUT OF LIMITS IAW SRM 53-12-00, DIAGRAM 102. FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.

Part: FLOOR PANEL — DELAMINATED (CENTER CABIN) · airframe 31,420 hrs · 16,295 cycles

CENTER CABIN FLOOR PANEL 242GF DELAMINATED. FOUND OUT OF LIMITS IAW SRM 53-12-00, DIAGRAM 102. FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.

Part: FLOOR PANEL — DELAMINATED (AFT CABIN) · airframe 31,420 hrs · 16,295 cycles

AFT CABIN FLOOR PANEL 262EF DELAMINATED. FOUND OUT OF LIMITS IAW SRM 53-12-00, DIAGRAM 102. FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.

Part: FLOOR SUPPORT — CORRODED (FWD CABIN) · airframe 31,420 hrs · 16,295 cycles

FORWARD UTILITY AREA FLOOR SUPPORT Y765 FRAMES 14-21 UPPER SURFACE FLANGE CORRODED. REMOVED CORROSION IAW SRM 51-74-00, FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14 FIG 102. REMOVED DAMAGED FLOOR SUPPORT IAW SRM 51-42-11. INSTALLED NEW FLOOR SUPPORT IAW TRM 53-21-01.

Part: SKIN — CORRODED (DOOR CUTOUT) · airframe 31,420 hrs · 16,295 cycles

AFT UTILITY AREA LT AFT DOOR CUT-OUT AT FRAME 68 LOWER CORNER CORRODED. REMOVED CORROSION IAW SRM 51-74-00, FOUND TO BE NO LIMITS ESTABLISHED FOR SRM. LOCATED AND DRILLED NEW CORNER FITTING IAW SRM 51-44-00. INSTALLED NEW CORNER FITTING ACCOMPLISHED ON NON-ROUTINE 26/250.

Part: FITTING — CORRODED (FWD CABIN) · airframe 31,420 hrs · 16,295 cycles

AFT UTILITY AREA LT AFT DOOR CUT-OUT AT FRAME 68 LOWER CORNER CORRODED. REMOVED CORROSION IAW SRM 51-74-00, FOUND TO BE NO LIMITS ESTABLISHED FOR SRM. LOCATED AND DRILLED NEW CORNER FITTING IAW SRM 51-44-00. INSTALLED NEW CORNER FITTING ACCOMPLISHED ON NON-ROUTINE 25/250.

Part: SHEAR PLATE — CORRODED (AFT CABIN) · airframe 31,420 hrs · 16,295 cycles

AFT UTILITY AREA RT SHEAR PLATE CORRODED. REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-42-11 & DWG D53474180.

Part: SHEAR PLATE — CORRODED (AFT CABIN) · airframe 31,420 hrs · 16,295 cycles

AFT UTILITY AREA LT SHEAR PLATE CORRODED. REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-42-11 & DWG D53474180.

Part: WEB — CORRODED (FWD CABIN) · airframe 31,420 hrs · 16,295 cycles

FORWARD CABIN STRINGER 23R FRAMES 20-21 UPPER SURFACE WEB HAS CORRODED. BLENDED AREA IAW SRM 51-74-00. REMOVED & REPLACED WEB IAW SRM 51-42-11 & DWG D53118159.

Part: FLOOR PANEL — CORRODED (FWD CABIN) · airframe 31,420 hrs · 16,295 cycles

FORWARD UTILITY FLOOR PANEL 221FF CORRODED, NO ALLOWABLE LIMITS IN SRM. REPLACED FLOOR PANEL IAW SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FWD CABIN) · airframe 31,420 hrs · 16,295 cycles

FORWARD UTILITY AREA FLOOR SUPPORT Y1292 BETWEEN FRAMES 14 - 22 UPPER SURFACE FLANGE CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-15 FIG.101. REMOVED AND REPLACED FLOOR SUPPORT IAW TRM 53-21-01.

Part: FLOOR SUPPORT — CORRODED (AFT CABIN) · airframe 31,420 hrs · 16,295 cycles

AFT UTILITY AREA FLOOR SUPPORT Y765 AROUND THE HOLE AT FRAME 66 CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. REMOVED AND REPLACED FLOOR SUPPORT IAW TRM 53-21-01.

Part: FLOOR PANEL — CORRODED (AFT CABIN) · airframe 31,420 hrs · 16,295 cycles

AFT UTILITY FLOOR PANEL 262FF CORRODED, NO ALLOWABLE LIMIT ON SRM. REPLACED FLOOR PANEL IAW SRM 51-72-11.

Part: FLOOR PANEL — CORRODED (AFT CABIN) · airframe 31,420 hrs · 16,295 cycles

AFT UTILITY FLOOR PANEL 261FF CORRODED. REPLACED FLOOR PANEL IAW SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (AFT CABIN) · airframe 31,420 hrs · 16,295 cycles

AFT UTILITY AREA FLOOR SUPPORT Y254 AT FRAME 68 CORRODED. BLENDED AREA IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-14 FIG 102. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-42-11 AND TRM 53-21-01.

Part: SEAT TRACK — CORRODED (FWD CABIN) · airframe 31,420 hrs · 16,295 cycles

FORWARD UTILITY AREA SEAT TRACK -Y1292 BTW FRAMES 18 - 22 UPPER SURFACE FLANGE HAS SCRIBE LINE & CORROSION ON CROWN. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-15 FIG. 101. REMOVED AND REPLACED SEAT TRACK IAW TRM 53-21-01.

Part: FLOOR PANEL — CORRODED (FWD CABIN) · airframe 31,420 hrs · 16,295 cycles

FORWARD UTILITY FLOOR PANEL 222FF CORRODED, NO ALLOWABLE LIMITS IN SRM. REPLACED FLOOR PANEL IAW 51-72-11.

Part: FLOOR SUPPORT — CORRODED (AFT CABIN) · airframe 31,420 hrs · 16,295 cycles

AFT UTILITY AREA FLOOR SUPPORT Y765 AT FRAME 68 CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. REMOVED AND REPLACED FLOOR SUPPORT IAW TRM 53-21-01.

Part: FLOOR SUPPORT — CORRODED (FWD CABIN) · airframe 31,420 hrs · 16,295 cycles

FORWARD UTILITY AREA FLOOR SUPPORT Y254 BETWEEN FRAMES 16 - 20 UPPER SURFACE FLANGE CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14, FIG. 107. REMOVED & REPLACED FLOOR SUPPORT IAW TRM 53-21-01.

Part: FLOOR SUPPORT — CORRODED (FWD CABIN) · airframe 31,420 hrs · 16,295 cycles

FORWARD UTILITY AREA FLOOR SUPPORT Y503.2 BETWEEN FRAMES 12 - 16 UPPER SURFACE FLANGE CORRODED. REMOVED CORROSION IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-11-14 FIG 107. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-42-11 AND TRM 53-21-01.

Part: FLOOR SUPPORT — CORRODED (FWD CABIN) · airframe 31,420 hrs · 16,295 cycles

FORWARD CABIN FLOOR SUPPORT -Y189 FRAMES 20 - 24 UPPER FLANGE CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14 FIG.105. REMOVED & REPLACED FLOOR SUPPORT IAW SRM 51-42-11 & TRM 53-21-01.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 30,546 hrs · 15,836 cycles

RAMP CREW REPORTED .7500 " HOLE IN AFT BAG BIN FLOOR. HOLE IS 3.5 FT INSIDE OF AFT FRAME OF AFT BAG BIN DOOR. INSTALLED TEMP REPAIR IAW SRM 53-02-00.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,301 hrs · 15,146 cycles

EPSU BATTERY RT MESSAGE DURING EMERGENCY LIGHT TEST. REPLACED RT EPSU BATTERY IAW AMM 33-51-38. OPS CHECKED GOOD.

Part: EPSU — FAULTY (CABIN) · airframe 4,561 hrs · 2,463 cycles

DURING EMERGENCY LIGHT TEST, FORWARD LEFT EPSU FAULTED ON CIDS. REMOVED AND REPLACED FORWARD LEFT EPSU PER AMM. OPERATIONAL CHECK WAS NORMAL. AIRCRAFT OK FOR SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 19,309 hrs · 9,790 cycles

DURING GROUND OPERATIONS FORWARD FUSELAGE NOSE SKIN WAS DAMAGED BETWEEN FRAME 1-4 AND BETWEEN LAP SKIN S39L AND S41L-S41R. REPAIRED PER EA 31-215413 REV B OF EA 31-215413 REQUIRES A FATIGUE AND DAMAGE TOLERANCE APPROVAL FOR CONTINUED REVENUE FLIGHT BEYOND 10 OCT 09.