N309US

Part: LINK — WORN (PAX DOOR) · airframe 93,620 hrs · 43,370 cycles

DETERIORATED PASSENGER CREW DOOR 831 YOKE LOWER LINK BTW SUPPORT ARM AND DOOR. REPLACED IAW AMM 52-11-21. OK FOR SERVICE.

Part: NONE — NONE · airframe 92,595 hrs · 42,763 cycles

SHIP 3209 PLASTIC EMERG PATHWAY LIGHT HOUSING BROKEN AT AISLE SEAT 18D. CORRECTIVE ACTION: REMOVED AND REPLACED EMERG LIGHT HOUSING AT SEAT 18D PER A320 AMM 33-51. OPS CHECKED GOOD. (8955949)

Part: NONE — NONE · airframe 91,711 hrs · 42,224 cycles

SHIP 3209 MAIN CABIN DOOR 1L HARD TO OPEN. CORRECTIVE ACTION: CLEANED AND LUBRICATED EXTERNAL CONTROL HANDLE PER A320 AMM 12-22-52, OPS NORMAL, OK FOR SVC. (82149344)

Part: NONE — NONE · airframe 91,710 hrs · 42,223 cycles

SHIP 3209 CRACK FOUND COMMON TO FASTENER AT UPPER FWD FRAME (FR4) OF THE L/H LATERAL SLIDING WINDOW FRAME. CORRECTIVE ACTION: COMPLIED WITH ERA 596981-14AD REV ORIGINAL. (8214926)

Part: NONE — NONE · airframe 91,710 hrs · 42,223 cycles

SHIP 3209 CRACK FOUND COMMON TO FASTENER AT UPPER FWD FRAME (FR4) OF THE L /H LATERAL (SLIDING) WINDOW FRAME. CORRECTIVE ACTION: COMPLIED WITH ERA 596981-14AD REV ORIGINAL. (2148559)

Part: NONE — NONE · airframe 91,708 hrs · 42,222 cycles

SHIP 3209 CRACK INDICATION - FR 4 HORIZONTAL UPPER STIFFENER, HAS CRACK INDICATION IN LOWER FORWARD RADIUS ABOVE AND OUTBOARD OF HORIZONTAL BOLT IN UPPER FORWARD CORNER. CORRECTIVE ACTION: COMPLIED WITH ERA 596540-14AD REV. ORIGINAL. (2098512)

Part: NONE — NONE · airframe 91,708 hrs · 42,222 cycles

SHIP 3209 RIGHT AFT CABIN DOOR SLIDE LACING COMING LOOSE. CORRECTIVE ACTION: REPLACED SLIDE. OK FOR SERVICE. (2097162)

Part: NONE — NONE · airframe 91,708 hrs · 42,222 cycles

SHIP 3209 L-1 DOOR DOES NOT OPEN FROM THE OUTSIDE. CORRECTIVE ACTION: ADJUSTED DOOR PER A320 AMM 52-11-11. OK FOR SERVICE. (2097750)

Part: NONE — NONE · airframe 91,708 hrs · 42,222 cycles

SHIP 3209 LACING COMING LOOSE ON DOOR SLIDE. CORRECTIVE ACTION: REPLACED DOOR SLIDE PER AMDS CARD 2561-4001-LA. OK FOR SERVICE. (2096991)

Part: NONE — NONE · airframe 91,708 hrs · 42,222 cycles

SHIP 3209 NEED TO INSTALL SHIM UNDER LOWER HORIZONTIAL LEGS OF FRAME. CORRECTIVE ACTION: COMPLIED WITH PRI 596617-14 REV. 1. AND REV 2. (2092247)

Part: NONE — NONE · airframe 91,708 hrs · 42,222 cycles

SHIP 3209 NEED TO INSTALL SHIM UNDER LOWER HORIZONTAL LEGS OF FRAME. CORRECTIVE ACTION: COMPLIED WITH PRI 596617-14 REV 1 AND 2. (2092233)

Part: NONE — NONE · airframe 91,708 hrs · 42,222 cycles

SHIP 3209 NEED TO INSTALL ANOTHER SHIM UNDER LOWER HORIZONTAL LEGS OF REPLACEMENT FRAME. CORRECTIVE ACTION: COMPLIED WITH 596617-14 REV 1 AND 2. (2092245)

Part: NONE — NONE · airframe 91,099 hrs · 41,845 cycles

SHIP 3209 BHEC INSPECTION OF LH FRAME 20 AT DOOR STOP FITTING #7 SHOWS CRACK INDICATIONS IN FRAME AND INTERCOSTAL LAYERS AT HOLE #1. CORRECTIVE ACTION: COMPLIED WITH ERA 594479-14AD REV 0. (1972734)

Part: NONE — NONE · airframe 91,099 hrs · 41,845 cycles

SHIP 3209 RH FRAME 20 AT DOOR STOP FITTING #1 SHOWS CRACK INDICATIONS IN INTERCOSTAL LAYER AT HOLES #1 AND #2. CORRECTIVE ACTION: COMPLIED WITH ERA 594479-14AD REV 0. (1972737)

Part: NONE — NONE · airframe 91,099 hrs · 41,845 cycles

SHIP 3209 RH FRAME 16 AT DOOR STOP FITTING #7 SHOWS CRACK INDICATIONS IN INTERCOSTAL LAYER AT HOLES #1 AND #3. CORRECTIVE ACTION: COMPLIED WITH ERA 594479-14AD REV 0. (1972736)

Part: NONE — NONE · airframe 91,099 hrs · 41,845 cycles

SHIP 3209 LH FRAME 16 AT DOOR STOP FITTING #7 SHOWS CRACK INDICATIONS IN INTERCOSTAL LAYER AT HOLES #1 AND #3. CORRECTIVE ACTION: COMPLIED WITH ERA 594479-14AD REV 0. (1972733)

Part: NONE — NONE · airframe 91,099 hrs · 41,845 cycles

SHIP 3209 FUSELAGE / FR 20 / L-1 DOOR OPENING / STOP FITTING #7 / CRACK INDICATION AT HOLE #1. CORRECTIVE ACTION: COMPLIED WITH REPETIVE INSPECTION PER ERA 594479-14AD. CONTINUE ON MON. OK FOR CONTINUED SERVICE. (1971568)

Part: PROTECTOR — DAMAGED (HORIZONTAL STAB) · airframe 90,550 hrs · 41,474 cycles

SHIP 3209 FOUND DAMAGE TO LEADING EDGE STEEL PROTECTIVE COVER ON RT HORIZONTAL STAB 6FT OUTBOARD OF FUSELAGE. CORRECTIVE ACTION: PERFORMED TEMPORARY SKIN REPAIR IAW A320 SRM 51-77-12. CONTINUE ON MONITOR. (7627366)

Part: FITTING — OUT OF ADJUST (L1 DOOR) · airframe 89,573 hrs · 41,027 cycles

SHIP 3209 LI DOOR REPORTED BY CREW TO BE HARD TO OPEN. CORRECTIVE ACTION: ADJUSTED FWD LOWER FITTING ON L1 DOOR FRAME PER A320 AMM 52-11. DOOR NOW EASY TO OPEN. OK FOR SERVICE. (7686654)

Part: OXYGEN BOX — NO TEST (SEAT 32 ABC) · airframe 88,995 hrs · 40,768 cycles

DURING TEST FOUND PSU OXY PANEL 32ABC WOULD NOT OPEN. CORRECTIVE ACTION: REPACKED PSU. OPERATIONS CHECK GOOD.

Part: OXYGEN BOX — NO TEST (SEAT 28 ABC) · airframe 88,995 hrs · 40,768 cycles

DURING TEST PSU OXY PANEL 28ABC WOULD NOT OPEN. CORRECTIVE ACTION: REPACKED PSU. OPERATIONS CHECK GOOD.

Part: OXYGEN BOX — NO TEST (SEAT 23 DEF) · airframe 88,995 hrs · 40,768 cycles

DURING TEST PSU OXY PANEL FOR SEAT 23 DEF WOULD NOT OPEN. CORRECTIVE ACTION: REPACKED PSU. OPERATIONS CHECK GOOD.

Part: PSU — NO TEST (SEAT 20 DEF) · airframe 88,974 hrs · 40,759 cycles

DURING TEST FOUND PSU AT SEAT 20DEF DID NOT OPEN. CORRECTIVE ACTION: REPACK PSU OPERATIONS CHECK GOOD.

Part: PSU — NO TEST (SEAT 30 DEF) · airframe 88,974 hrs · 40,759 cycles

FOUND SEAT 30 DEF PSU OXYGEN PANEL DID NOT OPEN DURING TEST. CORRECTIVE ACTION: REPACKED PSU, OPERATIONS CHECK GOOD.

Part: PSU — NO TEST (SEAT 25 DEF) · airframe 88,974 hrs · 40,759 cycles

DURING TEST PSU OXYGEN PANEL SEAT 25DEF DID NOT OPEN. CORRECTIVE ACTION: REPACK PSU, OPERATIONS CHECK GOOD.

Part: PSU — NO TEST (SEAT 23 DEF) · airframe 88,974 hrs · 40,759 cycles

DURING TEST FOUND PSU AT SEAT 23DEF DID NOT OPEN. CORRECTIVE ACTION: REPACK PSU OPERATIONS CHECK GOOD.

Part: PSU — NO TEST (SEAT 32 ABC) · airframe 88,974 hrs · 40,759 cycles

DURING TEST FOUND PSU DID NOT OPEN AT SEAT 32ABC. CORRECTIVE ACTION: REPACK PSU OPERATIONS CHECK GOOD.

Part: PSU — NO TEST (SEAT 14 DEF) · airframe 88,974 hrs · 40,759 cycles

DURING TEST FOUND PSU DID NOT OPEN AT SEAT 14DEF. CORRECTIVE ACTION: REPACK PSU OPERATIONS CHECK GOOD.

Part: PSU — NO TEST (SEAT 12 ABC) · airframe 88,974 hrs · 40,759 cycles

DURING TEST FOUND PSU DID NOT OPEN AT SEAT 12ABC. CORRECTIVE ACTION: REPACK PSU, OPERATIONS CHECK GOOD.

Part: PSU — NO TEST (SEAT 29 DEF) · airframe 88,974 hrs · 40,759 cycles

DURING TEST FOUND PSU DID NOT OPEN AT SEAT 29DEF. CORRECTIVE ACTION: REPACK PSU OPERATIONS CHECK GOOD.

Part: PSU — NO TEST (SEAT 24 DEF) · airframe 88,974 hrs · 40,759 cycles

DURING TEST FOUND PSU AT SEAT 24DEF DID NOT OPEN. CORRECTIVE ACTION: REPACK PSU OPERATIONS CHECK GOOD.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 87,589 hrs · 39,983 cycles

FLOOR NEAR 1R DOOR IS MUSHY, FA REPORTS IT FEELS LIKE A HOLE IN THE FLOOR, REPAIRED (TEMP) PER A320 SRM 53-12-00-300-005

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 87,382 hrs · 39,876 cycles

LEFT OVERWING EMERGENCY EXIT PULL HANDLE LIGHTS HAVE INOP BULBS BOTH EXITS, RELAMPED LEFT SIDE OW PULL HANDLE LIGHTS

Part: BULB — INOPERATIVE (LIGHT) · airframe 87,382 hrs · 39,876 cycles

RIGHT OVERWING EMERGENCY EXIT PULL HANDLE LIGHTS HAVE INOP BULBS FWD EXIT, RELAMPED RT OW FWD PULL HANDLE LIGHT

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 87,382 hrs · 39,876 cycles

DURING SERVICE CHECK - PERFORMING EMERGENCY LIGHT TEST - NO SYS OK LIGHT WITH MESSAGE BATTERY L, REPLACED BATTERY

Part: LIGHT — INOPERATIVE (SEAT 2CD) · airframe 86,842 hrs · 39,568 cycles

ONE WHITE EMERGENCY LIGHT AT SEAT 2CD INOP. REPLACED 2CD EMERGENCY PATH LIGHT PER A320 AMM 33-51.

Part: SKIN — DENTED (FRAMES 14-15) · airframe 86,331 hrs · 39,283 cycles

FUSELAGE SKIN DENTED BETWEEN FR14-15 STR 34-35RT AND BETWEEN FR15-16 STR 36-37RT, COMPLIED WITH PRI 547049-14 REVISION 1 AND ER/A 547049-14 REVISION H.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 84,135 hrs · 38,213 cycles

DURING APPROACH, WHEN THE LANDING GEAR WAS SELECTED DOWN, A FAILURE OCCURRED WITH SIMULTANEOUS ECAM WARNING LT L/G GEAR NOT DOWN LOCKED AND L/G DOORS NOT CLOSED. THE LANDING GEAR LEVER WAS CYCLED IAW QRH UNSUCCESSFULLY. ALTERNATE LANDING GEAR SELECTION WAS APPLIED AND THE FLIGHT LANDED UNEVENTFULLY. REPLACED THE GREEN ED PUMP, CASE DRAIN FILTER AND PERFORMED A LANDING GEAR EXTENSION/RETRACTION TEST.

Part: FRAME — CRACKED (NOT REPORTED) · airframe 90,114 hrs · 41,270 cycles

SHIP 3209 NEED TO COMPLY WITH ER/A 563929-14AD REV A (CRACK). CORRECTIVE ACTION: COMPLIED WITH ERA. JOB COMPLETE. (0698054)

Part: LANDING GEAR — MALFUNCTIONED · airframe 83,483 hrs · 37,884 cycles

AFTER TAKEOFF, MLG LEVER DIFFICULT TO MOVE TO THE UP POSITION. FOUR ATTEMPTS MADE BEFORE IT MOVED TO DESIRED POSITION. TROUBLESHOT, AND REPLACED THE LANDING GEAR.

Part: CONTROL UNIT — MALFUNCTIONED (MLG) · airframe 83,483 hrs · 37,884 cycles

AFTER TAKEOFF, UNABLE TO RAISE LANDING GEAR LEVER. LANDING GEAR EVENTUALLY WENT INTO DESIRED POSITION. TROUBLESHOT. REMOVED AND REPLACED LGICU NR 1 & 2 AND SERVICED NLG SHOCK ABSORBER.

Part: PIN — CORRODED (RT MLG) · airframe 83,470 hrs · 37,878 cycles

RIGHT GEAR AFT PINTLE PIN HAS PITTING WITH RUST IN RADIUS OF HEAD. REMOVED AND REPLACED PINTLE PIN.

Part: FRAME — CRACKED (FRM 36) · airframe 82,835 hrs · 37,591 cycles

CRACK INDICATION ON FRAME 36, RT SIDE, -Y1292+6.75. IN THE FWD CARGO, REPAIRED IAW PRI 563935-14, REV 0, 1, 2, 3, 4, 5 AND ERA 563935-14 AD, REV ORIGINAL.

Part: FRAME — CRACKED (FRM 36) · airframe 82,835 hrs · 37,591 cycles

CRACK INDICATION ON FRAME 36 LT SIDE, Y1292+6.75. PRESSURE DECK MENBRANE TO CENTER WING BOX IN FWD CARGO COMPARTMENT, PERMANENT REPAIR AT FRAME 36 L/H SIDE Y1292 + 6.75 PRESSURE DECK MENBRANE TO CENTER WING BOX IN FWD CARGO COMPARTMENT AS PER PRI#563935-14 REV. 0,1,2,3,4 AND 5 AND ERA 563935-14AD REV. ORIGINAL

Part: FRAME — CRACKED (FRM 36) · airframe 82,835 hrs · 37,591 cycles

CRACK INDICATION ON FRAME 36, RT SIDE, -Y1292+5.5'' IN FWD CARGO BAY, PERFORMED A PERMANENT REPAIR IAW PRI 563935-14, REV 0, 1, 2, 3, 4, & 5, AND ERA 563935-14AD, REV ORIGINAL.

Part: FRAME — CRACKED (FRM 36) · airframe 82,835 hrs · 37,591 cycles

CRACK INDICATION ON FRAME 36, RT SIDE, -Y1292 +7.5 IN FWD CARGO BAY. PERFORMED A PERMANENT REPAIR IAW PRI 563935-14, REV 0, 1, 2, 3, 4, & 5, AND ERA 563935-14AD, REV ORIGINAL.

Part: FRAME — CRACKED (FRM 36) · airframe 82,835 hrs · 37,591 cycles

CRACK INDICATION ON FRAME 36, LT SIDE Y1292+5.5 PRESSURE DECK MEMBRANE TO CENTER WING BOX IN FWD CARGO COMPARTMENT, PERFORMED A PERMANENT REPAIR IAW PRI 563935-14, REV 0, 1, 2, 3, 4, & 5 AND ERA 563935-14AD REV ORIGINAL.

Part: FRAME — CORRODED (FRM 16) · corrosion level 2 · airframe 82,835 hrs · 37,591 cycles

CORROSION ON FRAME 16, AFT FACE AT STRINGER 23R, PERFORMED SECTION TEMPORARY REPAIR IAW ER/A 563934-14, REV ORIGINAL, AND PRI 563934-14, REV 0,1,2, AND 3

Part: STRINGER — CORRODED (FRAME 67) · corrosion level 2 · airframe 82,835 hrs · 37,591 cycles

STRINGER 25R CORRODED, FRAME 67, REPLACED THE STRINGER IAW SRM 51-72-11, AND DRAWING D534800200.

Part: SKIN — SCRATCHED (FRAME 26) · airframe 82,835 hrs · 37,591 cycles

SKIN SCRATCH ON LOWER FUSELAGE, FRAME 26+7, STRINGER 41 TO 42R. REPAIRED THE SKIN IAW ER/A 565259-14AD, REV ORIGINAL, AND PRI 3 565259-14 REV.0.

Part: FRAME — BENT (EMERGENCY EXIT) · airframe 82,835 hrs · 37,591 cycles

BENT FRAME AT THE EMERGENCY EXIT DOOR INTERNAL STRUCTURE ON THE UPPER FUSELAGE. REPLACED THE FRAME IAW SRM 51-72-11, AND DRAWING D5227-9036

Part: SUPPORT — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 82,835 hrs · 37,591 cycles

CORROSION LOWER SUPPORT, FRAMES 66 TO 68 LT SIDE, REPLACED SUPPORT IAW SRM 51-72-11 AND DWG D53480020.

Part: FLOOR SUPPORT — CORRODED (FRAMES 68-69) · corrosion level 2 · airframe 82,835 hrs · 37,591 cycles

CORRODED FLOOR SUPPORT, -Y1162.5 BETWEEN FRAMES 68 TO 69. REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, AND DWG D53472000.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · corrosion level 2 · airframe 82,835 hrs · 37,591 cycles

CORRODED FLOOR SUPPORT, -Y1292, BETWEEN FRAMES 64 TO 66 IN THE AFT GALLEY AREA, REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, AND DRAWING D53472230.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 82,835 hrs · 37,591 cycles

CORRODED FLOOR SUPPORT, -Y1225, BETWEEN FRAMES 66 TO 68 IN THE AFT GALLEY AREA, REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DWG 5347200.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-70) · corrosion level 2 · airframe 82,835 hrs · 37,591 cycles

CORRODED FLOOR SUPPORT, +Y512, BETWEEN FRAMES 64 TO 70, REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, DWG D53472094, AND DWG D53472000.

Part: SUPPORT — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 82,835 hrs · 37,591 cycles

CORRODED LOWER SUPPORT FRAMES 66 TO 68, RT SIDE. REPLACED THE SUPPORT IAW SRM 51-72-11, SRM 51-42-11, AND DWG D53480020.

Part: SEAT TRACK — CORRODED (FRAMES 47-64) · corrosion level 2 · airframe 82,835 hrs · 37,591 cycles

SEAT TRACK CORRODED, Y765, BETWEEN FRAMES 47 TO 64. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DRAWING D53472000.

Part: SEAT TRACK — CORRODED (FRAMES 47-64) · corrosion level 2 · airframe 82,835 hrs · 37,591 cycles

SEAT TRACK, -Y765, BETWEEN FRAMES 47 TO 64 CORRODED. REPLACED THE SEAT TRACK IAW SRM 51-72-11, 51-42-11, AND DRAWING D53472000.

Part: SEAT TRACK — CORRODED (FRAME 41) · corrosion level 2 · airframe 82,835 hrs · 37,591 cycles

SEAT TRACK CORRODED, Y765, FRAME 41, REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DRAWING D53371110.

Part: SEAT TRACK — CORRODED (FRAMES 47-64) · corrosion level 2 · airframe 82,835 hrs · 37,591 cycles

SEAT TRACK CORRODED, -Y1292, BETWEEN FRAMES 47 TO 64, REPLACED THE SEAT TRACK IAW SRM 51-72-11, 51-42-11, AND DRAWING D53472000.

Part: FLOOR SUPPORT — CORRODED (FRAME 16) · corrosion level 2 · airframe 82,835 hrs · 37,591 cycles

CORRODED FLOOR SUPPORT -Y254, FRAME 16+17 INCHES, REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, 51-72-11, AND DRAWING D531128190.

Part: FLOOR SUPPORT — CORRODED (FRAME 16) · corrosion level 2 · airframe 82,835 hrs · 37,591 cycles

CORRODED FLOOR SUPPORT +Y765, FRAME 16, REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, 51-72-11 AND DRAWING D53110876.

Part: FLOOR SUPPORT — CORRODED (FRAME 20) · corrosion level 2 · airframe 82,835 hrs · 37,591 cycles

CORRODED FLOOR SUPPORT -Y765, FRAME 20, INSTALLED A NEW FLOOR SUPPORT IAW 51-42-11. 51-72-11, DRAWINGS D53112812, AND D53110920

Part: SEAT TRACK — CORRODED (FRAME 47-64) · corrosion level 2 · airframe 82,835 hrs · 37,591 cycles

CORRODED SEAT TRACK Y1292, FRAME 47 TO 64, REPLACED THE SEAT TRACK.

Part: FLOOR SUPPORT — CORRODED (FRAME 20) · corrosion level 2 · airframe 82,835 hrs · 37,591 cycles

CORRODED FLOOR SUPPORT -Y1292, FRAME 20, INSTALLED A NEW FLOOR SUPPORT IAW SRM 51-42-11, 51-72-11, DRAWINGS D53110900, AND D533112812

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-70) · corrosion level 2 · airframe 82,835 hrs · 37,591 cycles

CORRODED FLOOR SUPPORT +Y765, FRAMES 66 TO 70, REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, AND DWG #D53472000

Part: SEAT TRACK — CORRODED (FRAME 36) · corrosion level 2 · airframe 82,835 hrs · 37,591 cycles

CORRODED SEAT TRACK Y-765, FRAME 36, INSTALLED A NEW SEAT TRACK IAW SRM 51-42-11, 51-72-11, DRAWINGS D53370500, AND D57130146,

Part: SEAT TRACK — CORRODED (FRAME 41) · corrosion level 2 · airframe 82,835 hrs · 37,591 cycles

CORRODED SEAT TRACK Y-765, FRAME 41, INSTALLED A NEW SEAT TRACK IAW SRM 51-42-11, 51-72-11, DRAWINGS 53370500, AND D53371000.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 82,835 hrs · 37,591 cycles

CORRODED FLOOR SUPPORT +Y1292, FRAME 16. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DRAWING D53112812

Part: LIGHT — BROKEN (CABIN) · airframe 80,865 hrs · 36,551 cycles

FLOOR PROX EMERGENCY ESCAPE PATH MARKING SYSTEM AT 25D IS BROKEN, REPLACED PROXIMITY LIGHT AT 25D.

Part: SKIN — DENTED (FRAME 69) · airframe 77,466 hrs · 34,921 cycles

DENT ON EXTERNAL SKIN AT LOWER FUSELAGE ON FRAME 69 BETWEEN STR 28 RT TO STR 29 RT. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOCATION ON FRAME 69, STR 27 RT TO STR 32 RT IAW ERA 544182-14AD REV A AND PRI 524182-14.

Part: SKIN — CORRODED (FRAMES 69-70) · airframe 77,466 hrs · 34,921 cycles

CORROSION ON EXTERNAL SKIN AT LOWER FUSELAGE FROM FRAME 69 TO FRAME 70 BETWEEN STR 29R TO STR 30R. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN AT LOWER FUSELAGE FROM FRAME 69 TO FRAME 70 BETWEEN STR 29R, STR 30R IAW SRM 53-41-11 PARA 5.D FIG 205 PAGES 256/262.

Part: STRINGER — CORRODED (FRAMES 33-34) · airframe 77,466 hrs · 34,921 cycles

CORROSION ON STRINGER 44 BETWEEN FRAMES 33 TO 34 IN FWD CARGO COMPARTMENT. REPLACED THE STRINGER IAW SRM 51-72-11 AND DWG D53231544, D53370500.

Part: BUSHING — CORRODED (LT MLG) · airframe 77,462 hrs · 34,920 cycles

CORROSION FWD BUSHING OF PINTLE PIN AT RIB 5 ON RETRACTION ACTUATOR ON LT MLG REPLACED BUSHING, 1 EA OF FWD POSITION ON RETRACTION ACTUATOR ON LT MLG IAW CMM 32-11-33.

Part: BATTERY PACK — FAILED (RT DOOR SLIDE) · airframe 75,758 hrs · 34,112 cycles

RT SLIDE BATTERY PACK FAILES TEST. REPLACED RT EPSU AND BTTERY PACK AND FUNCTIONAL CHECK WAS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 74,216 hrs · 33,371 cycles

DURING EPCU TEST, FOUND BATTERY AFT LT MESSAGE. REPLACED AFT LT BATTERY PACK AND FUNCTIONAL CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 72,244 hrs · 32,436 cycles

DURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHT SIGN MID CABIN AND EXIT SIGN OVER WING INOPERATIVE. MAINTENANCE REPLACED EPSU 11WL AND BATTERY. FUNCTONAL CHECK WAS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,244 hrs · 32,436 cycles

DURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHTS ON SEATS INOPERATIVE. MAINTENANCE REPLACED BATTERY AND FUNCTIONAL CHECKED NORMAL.

Part: STRAP — CRACKED (RT WING) · airframe 72,099 hrs · 32,357 cycles

DURING INSPECTION, FOUND CRACK ON BUTT STRAP LOCATED IN T/E BETWEEN RIB 10 TO RIB 11 RT WING. REPLACED BUTT STRAP, LOCATED ON T/E BETWEEN RIB 10 TO RIB 11 RT WING IAW SRM 51-72-11 AND DWG D57541686.

Part: SKIN — DENTED (FRAME 79) · airframe 72,099 hrs · 32,357 cycles

DURING INSPECTION, FOUND DENT ON EXTERNAL SKIN LOCATED FR 79 AND BETWEEN STR 1-STR 2R UPPER FUSELAGE TAIL CONE AREA. PERFORMED PERMANENT REPAIR, FR 79 AND BETWEEN STR 1-STR 2R ON UPPER FUSELAGE TAIL CONE AREA IAW SRM 53-51-11, PAR 5B, FIG 203, SHEET 2.

Part: SKIN — SCRATCHED (FRAME 57) · airframe 72,110 hrs · 32,362 cycles

DURING INSPECTION, FOUND SCRATCH ON EXTERNAL SKIN BETWEEN FRAMES 57A AND 4" ABOVE OF BEAM, 3 INCHES AFT CARGO DOOR. REPAIRED IAW SRM 52-32-00, PARA 4E, FIG 205, PAGES 229-234.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 71,228 hrs · 31,946 cycles

DURING NON ROUTINE CHECK, FOUND 11C SEAT MOUNTED EMERENCY LIGHT INOPERATIVE. MAINTENACE REPAIRED WIRING AND OPS CHECKED GOOD.

Part: BATTERY PACK — FAULTED (EMERGENCY LIGHTS) · airframe 71,006 hrs · 31,834 cycles

DURING NON ROUTINE CHECK, FOUND EMERGENCY SYSTEM TEST SHOW BATTERY FAULTED. INSTALLED NEW BATTERY AND FUNCTIONAL CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,162 hrs · 30,439 cycles

DURING NON ROUTINE CHECK, FOUND EMERGENCY PATH LIGHT AT ROWS 13, 14, 15, 18, 19, 20, 23, 24, 25 INOPERATIVE. REPLACED AFT LT EPSU AND FUNCTIONAL CHECK WAS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,772 hrs · 30,233 cycles

DURING NON-ROUTINE CHECK, FOUND EMERGENCY LIGHTS AT SEATS 13-26 INOPERATIVE. REPLACED AFT CABIN EMERGENCY LIGHT EPSU AND CHECK WAS NORMAL.

Part: EPSU — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,676 hrs · 30,194 cycles

DURING NON-ROUTINE CHECK, FOUND AFT LT EPSU INOPERATIVE. MX REPLACED AFT LT EPSU AND BATTERY PACK. FUNCTIONAL CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,579 hrs · 30,146 cycles

DURING NON ROUTINE, SEVERAL EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MX REPLACED AFT L ESPU AND FUNCTIONAL CHECK WAS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,556 hrs · 30,133 cycles

DURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED EPSU AND FUNCTIONAL CHECKED NORMAL.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 6,296 hrs · 2,844 cycles

DURING INSPECTION, FOUND LT WING INBD FLAP HAS COMPOSITE DAMAGE ON UPPER SKIN APPROX 5FT FROM INBD END. REPAIRED LT WING INBD FLAP IAW SRM 57-52-00 PARAGRAPH 8F FIG 206.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 6,296 hrs · 2,844 cycles

DURING NON ROUTINE CHECK, FOUND THE LOWER EMERGENCY EXIT SIGNS AT FWD AND AFT RIGHT OVERWING INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY AND FUNCTIONAL CHECK WAS NORMAL. A/C RETURNED TO SERVICE.

Part: RING — GOUGED (THRUST REVERSER) · airframe 6,296 hrs · 2,844 cycles

DURING INSPECTION, FOUND LT ENGINE OTBD THRUST REVERSER 9 O'CLOCK TO 12 O'CLOCK JAY RING GOUGED AND HAS FRETTING DAMAGE. REPLACED LT ENGINE OTBD THRUST REVERSER JAY RING IAW CMM 78-32-35. ADJUSTED LT ENGINE RING IAW AMM 78-36-42-820-001.

Part: STRINGER — CORRODED (CARGO BAY) · airframe 6,296 hrs · 2,844 cycles

DURING INSPECTION, FOUND FWD CARGO COMPARTMENT BETWEEN FR 30 AND FR 31, STR 41L STRINGER DOUBLER HAS CORROSION. REPLACED STRINGER DOUBLER IAW SRM 51-42-11.

Part: STRINGER — CORRODED (CARGO BAY) · airframe 6,296 hrs · 2,844 cycles

DURING INSPECTIONS, FOUND FWD CARGO BAY BETWEEN FRAMES 30 AND 31, STR 42R, STRINGER DOUBLER HAS CORROSION. REMOVED SHEER TIE FOR ACCESS IAW SRM 51-42-11. REMOVED SPLICE FABRICATED NEW SPLICE ON STAM TRAVELER INSTALLED SPLICE AND SHEAR TIE FABRICATED IAW SRM 53-21-13.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,655 hrs · 29,705 cycles

DURING INSPECTIONS, FOUND FWD CARGO COMPARTMENT FR32 BETWEEN STR 42R AND STR 43R, FRAME CLIP HAS CORROSION. REMOVED CLIP IAW SRM 51-42-11. FABRICATED NEW CLIP IAW SRM 53-21-12 AND INSTALLED IAW SRM 51-42-11.

Part: ANGLE — CORRODED (CARGO BAY) · airframe 66,627 hrs · 29,693 cycles

DURING INSPECTIONS, FOUND FWD CARGO COMPARTMENT FR30, BETWEEN STR 41R AND STR 42R FRAME ANGLE HAS CORROSION. REMOVED ANGLE IAW SRM 51-42-11. FABRICATED ANGLE AND INSTALLED IAW SRM 51-42-11.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,655 hrs · 29,705 cycles

DURING INSPECTIONS, FOUND FWD CARGO COMPARTMENT FR 32 BETWEEN STR 41R AND STR 42R, FRAME CLIP HAS CORROSION. REMOVED CLIP IAW SRM 51-42-11. FABRICATED NEW CLIP IAW SRM 53-21-12 AND INSTALLED CLIP IAW SRM 51-42-11.

Part: ANGLE — CORRODED (CARGO BAY) · airframe 66,627 hrs · 29,693 cycles

DURING INSPECTIONS, FOUND FWD CARGO COMPARTMENT FR33 BETWEEN STR 42L AND STR 43L, FRAME ANGLE HAS CORROSION. REMOVED ANGLE IAW SRM 51-42-11. FABRICATED NEW ANGL IAW SRM 53-21-12 AND INSTALLED IAW SRM 51-42-11.

Part: STRINGER — CORRODED (42 RIGHT) · airframe 6,296 hrs · 2,844 cycles

DURING INSPECTIONS, FOUND FWD CARGO BAY BETWEEN FRAMES 33 AND 34, STRINGER 42R DOUBLER HAS CORROSION. REMOVED CORROSION, FABRICATED NEW ANGLE AND INSTALLED ANGLE IAW SRM 53-00- 13 FIG 202.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 6,296 hrs · 2,844 cycles

DURING INSPECTION, FOUND FWD CABIN FLOOR PANEL 222FF CORRODED 4.5" X 3.0". RECEIVED NEW FLOOR PANEL PN ES367 147800600, TO BE INSTALLED ON W/C 2500-6601.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 6,296 hrs · 2,844 cycles

DURING INSPECTION, FOUND FWD CABIN FLOOR PANEL 221FF CORRODED 5.0" X 5.0". RECEIVED NEW FLOOR PANEL PN ES367147800600, TO BE INSTALLED ON W/C 2500-6601.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 6,296 hrs · 2,844 cycles

DURING INSPECTION, FOUND FWD CABIN FLOOR PANEL 221FF CORRODED 5.0" X 5.0". RECEIVED NEW FLOOR PANEL PN ES367147800600, TO BE INSTALLED ON W/C 2500-6601.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 6,296 hrs · 2,844 cycles

DURING INSPECTIONS, FOUND FWD CARGO COMPT BET FR29 AND FR30, STRG 41R STRINGER DOUBLER HAS CORROSION. REMOVED CORROSION IAW A320 SRM 51-74-00, NO ALLOWABLE LIMITS. FABRICATED REPAIR AND INSTALLED PER SRM 53-21-13 FIG 203 SHEET 2.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 67,520 hrs · 30,118 cycles

DURING INSPECTIONS, FWD CARGO COMPARTMENT BETWEEN FR 28 AND FR 29 STRINGER 41R HAS CORROSION. REMOVED FASTENERS FROM FR 28 TO FR 29 STGR 41R IAW SRM 51-42- 11. REMOVED CORROSION IAW SRM 51-74-00. INSTALLED REPAIR PARTS IAW SRM 53-21-13 FIG 202.

Part: WEB — CORRODED (FUSELAGE) · airframe 6,296 hrs · 2,844 cycles

FORWARD UTILITY AREA LT SIDE AT FR 16 UPPER SURFACE WEB HAS SURFACE CORROSION. REMOVED AND REPLACED WEB IAW A320 SRM 51-42-11. NO ESTABLISHED LIMITS. ORIG MAT=0.070" DAMAGE DIM. L=1.70" W=1.40" D=0.008".

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 6,296 hrs · 2,844 cycles

DURING INSPECTON, FOUND COCKPIT, FWD OF FR11, LT SIDE AREA, 37 INCHES FROM O/B, FLOOR SUPPORT WEB HAS CRACK AT LOWER AFT CORNER. MEASURED LENGTH OF CRACK IS 0.450 INCH THE ALLOWED IS 0.310 INCH FOUND TO BE OUT OF LIMITS IAW A320 SRM 53-11-14 FIG 205, REMOVED FLOOR SUPPORT WEB IAW A320 SRM 51-42-11. FABRICATED NEW FLOOR SUPPORT WEB ON STAM TRAVELER AND INSTALLED NEW FLOOR SUPPORT WEB IAW A320 SRM 51-42-11.

Part: SKIN — DENTED (FUSELAGE) · airframe 6,296 hrs · 2,844 cycles

DURING INSPECTIONS, FOUND FWD LWR FUSELAGE SKIN DENTED APPROX 7 O'CLOCK POSITION AT FR 2 REQUIRES RE-EVALUATION. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-11 DIAGRAM 103 PARAGRAPH 4C. ACCOMPLISHED REPAIR AS PER ER/A NR 501388-14 REV. REV ORIGINAL SECTION 1 PERMANENT REPAIR.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 6,296 hrs · 2,844 cycles

MID CABIN AT FR36 Y765 -Y1292 FLOOR SUPPORT UPPER FLANGE HAS SCRIBE MARK. REMOVED AND REPLACED FLOOR SUPPORT AT FR36 Y765 -Y1292 IAW A320 SRM 51-42-11. RETAIN FOR RECORDS.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 6,296 hrs · 2,844 cycles

FORWARD CABIN FLOOR SUPPORT FROM FR18 TO FR20 RT -Y254 UPPER SURFACE CORRODED. NO ALLOWABLE DAMAGE ON SRM, REMOVED FLOOR SUPPORT AND SPLICES IAW A320 SRM 51-42-11. RECEIVED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT IAW A320 SRM 51-42-11. ORIG MAT 0.125" DAMAGE DIM. L=2" X W=2" X D=0.080".

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 6,296 hrs · 2,844 cycles

DURING CHECK, FOUND AFT UTILITY AREA FLOORBEAM FROM FR68-69-Y1292 UPPER AND LOWER SURFACE HOLES CORRODED & SEVERAL BROKEN RIVETS. INSTALLED NEW FLOORBEAM IAW A320 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 6,296 hrs · 2,844 cycles

DURING CHECK, FOUND AFT UTILITY AREA FLOORBEAM UPPER SURFACE FROM FR 64T0 FR 66 RT -Y1292 HARD POINT HOLES CORRODED. INSTALLED NEW FLOORBEAM IAW A320 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 6,296 hrs · 2,844 cycles

DURING CHECK, FOUND AFT UTILITY AREA FLOORBEAM UPPER LOWER SURFACE HOLES FROM FR66 TO FR68 -Y1292 CORRODED. REMOVED FLOOR SUPPORT BEAM IAW A320 SRM 51-42-11 AND INSTALLED NEW FLOORBEAM IAW A320 SRM 51-42-11.

Part: FLOOR SUPPORT — BROKEN (FUSELAGE) · airframe 6,296 hrs · 2,844 cycles

DURING CHECK, FOUND FWD CABIN BETWEEN FR30 TO FR31 -Y254 FLOOR SUPPORT BROKEN UPPER FLANGE MISSING PIECES BY 2.800" X.900". LOCATED AND DRILLED REPAIR PARTS IAW A320 SRM 53-00-14 FIG 204. TREATED AND PRIMED REPAIR. INSTALLED REPAIR PARTS IAW A320 SRM 53-00-14.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 6,296 hrs · 2,844 cycles

FORWARD UTILITY AREA FLOOR SUPPORT FROM FR18 TO FR21 UPPER FLANGE AND SEAT TRACK CORRODED -Y765. REMOVED CORROSION BY BLENDING IAW A320 SRM 51-74-00 CHECKED LIMITS W=.21" L=1.5" D=.035". FOUND TO BE OUT OF LIMITS IAW A320 SRM 53-00-15 FIG 101. REMOVED AND REPLACED SEAT TRACK. RETAIN FOR RECORDS.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 6,296 hrs · 2,844 cycles

FORWARD UTILITY AREA FLOOR SUPPORT FROM FR18 TOFR21 UPPER FLANGE AND SEAT TRACK CORRODED -Y765. SSI 531189. REMOVED CORROSION BY BLENDING IAW A320 SRM 51-74-00. CHECKED LIMITS W=.21" L=1.5" D=.035". FOUND TO BE OUT OF LIMITS IAW A320 SRM 53-00-15 FIG 101. REMOVED AND REPLACED SEAT TRACK IAW A320 SRM 51-42-11. RETAIN FOR RECORDS.

Part: SILL — CORRODED (FUSELAGE) · airframe 6,296 hrs · 2,844 cycles

DURING CHECK, FOUND RT AFT PASSENGER DOOR SILL BEAM UPPER SURFACE FROM FR66 TO FR68 & GIRT BAR ATTACH HOLES CORRODED. BLENDED AREA IAW A320 SRM51-74-00 DIM.L=2.0"W=0.400" D=0.072" FOUND TO BE OUT OF LIMITS IAW A320 SRM 53-41-14- FIG 101. REPLACED DOOR SILL IAW A320 SRM 51-42-11 & SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 6,296 hrs · 2,844 cycles

DURING CHECK, FOUND FWD UTILITY AREA FLOOR SUPPORT FROM FR18TO FR21 UPPER FLANGE & SEAT TRACK CORRODED. REMOVED CORROSION BY BLENDING IAW A320 SRM 51-74-00 CHECKED LIMITS W=.21" L=1.5" D=.035" FOUND TO BE OUT OF LIMITS PER SRM 53-00-15 FIG 101. REPLACED SEAT TRACK P/N D53112 78220201 BATCH NO.0002212833 IAW A320 SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 6,296 hrs · 2,844 cycles

DURING CHECK, FOUND FWD CABIN FLOOR SUPPORT FROM FR18 TO FR21 RT -Y1292 UPPER SURFACE AND SEAT TRACK CORRODED. INSTALLED NEW FLOOR SUPPORT SUPPORT BEAM P/N D5311278220201 IAW A320 SRM 51-42-11.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 6,296 hrs · 2,844 cycles

DURING INSPECTION, FWD PIT FLOOR PANEL 131EF IS DELAMINATED,12" X 12" AREA. FABRICATED FLOOR PANEL 131EF ON STAM TRAVELER #T12/927772 PER DWG 3D25-37705. PANEL TO BE INSTALLED ON W/C 2500-5018.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 6,296 hrs · 2,844 cycles

DURING INSPECTION, FOUND FWD PIT FLOOR PANEL 131HF DELAMINATED AND IS MISSING UPPER SKIN AROUND TIE DOWN FITTINGS. FABRICATED FLOOR PANEL 131HF ON STAM TRAVELER T12/927777 PER DWG 3D25-37705. DAMAGE DIA L=6" X W=6". PANEL TO BE INSTALLED ON W/C 2500-5018.

Part: BLANKING PLATE — CORRODED (R2 DOOR) · airframe 6,296 hrs · 2,844 cycles

R2 DOOR FWD AND AFT BLANKING PLATES CORRODED. RETAIN FOR RECORDS. REPLACED BLANKING PLATES FORWARD AND AFT AT R2 DOOR IAW A320 SRM 51-72-00. INSTALLED ON W/C 2500-6602.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 6,296 hrs · 2,844 cycles

DURING INSPECTION, FOUND AFT PIT FLOOR PANEL 151AF IS DELAMINATED, 14" X 12" AREA. FABRICATED FLOOR PANEL 151AF ON STAM TRAVELER #T12/927895 PER DWG 3D25-37705. PANEL TO BE INSTALLED ON W/C 2500-5019.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 6,296 hrs · 2,844 cycles

DURING INSPECTION, FWD PIT FLOOR PANEL 131AF IS DELAMINATED AND MISSING UPPER SKIN AROUND TIE DOWN. FABRICATED FLOOR PANEL 131AF ON STAM TRAVELER #T12/927774 PER DWG 3D25-37705. DAMAGE DIA. L=6" X W=6" PANEL TO BE INSTALLED ON W/C 2500-5018, STAM CRS#MZARO13L RC3085329.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 6,296 hrs · 2,844 cycles

DURING CHECK, FOUND FWD CABIN FLOOR PANEL 221AB IS DELAMINATED, 8" X 3" AREA. FABRICATED FLOOR PANEL 221AB ON STAM TRAVELER #T12/928077 PER DWG 3D25-37498. DAMAGE DIM L=8" X W=3", PANEL TO BE INSTALLED ON W/C 2500-6617.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 6,296 hrs · 2,844 cycles

FORWARD UTILITY AREA FLOOR SUPPORT FROM FR12 TO FR16 RT -Y81 HARD POINT HOLES AND UPPER FLANGE CORRODED. REMOVED CORROSION IAW A320 SRM 51-74-00. DAMAGED DIM. L=1.25" W=.042" D=.051". CHECKED LIMITS IAW A320 SRM 53-11-14 FIG 106 FOUND TO BE OUT OF LIMITS. REMOVED JOINT COVER AND DUMMY RAIL IAW A320 SRM 51-42-11. INSTALLED JOINT COVER AND DUMMY RAIL IAW A320 SRM 51-42-11. RETAIN FOR RECORD.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 6,296 hrs · 2,844 cycles

FORWARD CABIN FLOOR PANEL 232DF HAS CORROSION AROUND INSERT. FABRICATED FLOOR PANEL 232DF IAW DWG 3D25-37498. DAMAGE DIM L=3.5" W=2.5". RETAIN FOR RECORD.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 6,296 hrs · 2,844 cycles

FORWARD CABIN FLOOR PANEL 232FF HAS AN ELONGATED HOLE. FABRICATED FLOOR PANEL 231FF IAW DWG 3D25-37498. DAMAGE DIM L=2.4" W=2.4". RETAIN FOR RECORD.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 6,296 hrs · 2,844 cycles

DURING CHECK, FOUND AFT CABIN FLOOR PANEL 262FF HAS CORROSION AND EDGE DAMAGE. RECEIVED NEW FLOOR PANEL P/N D5367180500300 BATCH#0002216005. PANEL TO BE INSTALLED ON W/C 2500-6602.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 6,296 hrs · 2,844 cycles

UTILITY AREA FLOORBEAM AT FR 66 TO FR 68 LT Y1292 UPPER SURFACE SEVERAL HOLES CORRODED. REMOVED FLOORBEAM +Y1292 FR66 TO 68 IAW A320 SRM 51-42-11. RECEIVED NEW FLOORBEAM INSTALLED NEW FLOORBEAM IAW A320 SRM 51-42-11. BLENDED OUT CORROSION IAW A320 SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW A320 SRM 53-31-15 FIG 101. RETAIN FOR RECORD.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 6,296 hrs · 2,844 cycles

AFT CABIN FLOOR PANEL 261PF HAS A CRACK AND DELAMINATION AROUND A FASTENER HOLE. FABRICATED FLOOR PANEL 261PF IAW DWG 3D25-37498. DAMAGE DIM L=2.7" W=2.7". RETAIN FOR RECORD.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 6,296 hrs · 2,844 cycles

DURING CHECK, FOUND AFT CABIN FLOOR PANEL 261FF HAS CORROSION AT LOWER AND UPPER SURFACE. RECEIVED NEW FLOOR PANEL P/N D5367180500200 BATCH#0002216084. PANEL TO BE INSTALLED ON W/C 2500-6602.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 6,296 hrs · 2,844 cycles

AFT CABIN FLOOR PANEL 261DF HAS MULTIPLE PUNCTURES AND DELAMINATED. FABRICATED FLOOR PANEL 261DF IAW DWG 3D25-37498. DAMAGE DIM L=1.5" W=1.5". RETAIN FOR RECORD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 6,296 hrs · 2,844 cycles

AFT UTILITY AREA FLOORBEAM AT FR68 TO FR69 LT Y1292 UPPER SURFACE HOLES CORRODED. REMOVED NEW FLOORBEAM. INSTALLED NEW FLOORBEAM IAW A320 SRM 51-42-11. BLENDED OUT CORROSION IAW A320 SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW A320 SRM 53-31-15 FIG 101.

Part: PANEL — MISSING (FUSELAGE) · airframe 6,296 hrs · 2,844 cycles

DURING CHECK, FOUND AFT PIT SLOPE PANEL 152QF IS MISSING UPPER SKIN AROUND TIE DOWN FITTINGS. AFT PIT SLOPE PANEL 152QF FABRICATED NEW ON STAM TRAVELER T12/927901 IAW DWG 3D25-37705. DAMAGE DIM. L=10" W=10".

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 6,296 hrs · 2,844 cycles

AFT PIT FLOOR PANEL 151GF IS DELAMINATED, 20" X 20" AREA. FABRICATED FLOOR PANEL 151GF IAW DWG 3D25-37705. DAMAGE DIM L=20" W=20". RETAIN FOR RECORDS.

Part: PANEL — MISSING (FWD CARGO) · airframe 6,296 hrs · 2,844 cycles

DURING CHECK, FOUND FWD PIT SLOPE PANEL 132JF IS MISSING UPPER SKIN AROUND TIE DOWN FITTINGS. FABRICATED NEW ON STAM TRAVELER T12/927775 IAW DWG 3D25-37705. DAMAGE DIM: L=9.5 W=8.5 AND INSTALLED.

Part: PANEL — DAMAGED (CARGO BAY) · airframe 6,296 hrs · 2,844 cycles

FORWARD PIT SLOPE PANEL 132FF IS MISSING UPPER SKIN AROUND TIE DOWN FITTINGS. FABRICATED SLOPE PANEL 132FF IAW DWG 3D25-37705.DAMAGE DIM: L=2.4 W=2.4. RETAIN FOR RECORDS.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 6,296 hrs · 2,844 cycles

AFT PIT FLOOR PANEL 151DF IS DELAMINATED, 25" X25" AREA. FABRICATED FLOOR PANEL 151DF IAW DWG 3D25-37705. DAMAGE DIM L=10.5" W=11.5". RETAIN FOR RECORDS.

Part: PANEL — MISSING (FWD CARGO) · airframe 6,296 hrs · 2,844 cycles

DURING CHECK, FOUND FWD PIT SLOPE PANEL 131BF IS MISSING UPPER SKIN AROUND TIE DOWN FITTINGS. FABRICATED NEW SLOPE PANEL 131FF ON STAM TRAVELER T12/927773 IAW DWG 3D25-37705 DAMAGE DIM: L=4.1 W=4.1 AND INSTALLED.

Part: PANEL — DELAMINATED (CARGO BAY) · airframe 6,296 hrs · 2,844 cycles

AFT PIT SLOPE PANEL 151EF IS DELAMINATED AND MISSING UPPER SKIN AROUND TIE DOWN FITTINGS. FABRICATED SLOPE PANEL 151EF IAW DWG 3D25-37705. DAMAGE DIM. L=1.75" W=1.75". RETAIN FOR RECORDS.

Part: PANEL — DELAMINATED (CARGO BAY) · airframe 6,296 hrs · 2,844 cycles

DURING CHECK, FOUND AFT CARGO SLOPE WALL PANEL 152 RF DELAMINATED. FABRICATED NEW ON STAM TRAVELLER T12/928061 IAWDWG 3D25-37705.

Part: PANEL — DAMAGED (CVARGO BAY) · airframe 6,296 hrs · 2,844 cycles

AFT PIT SLOPE PANEL 152EF IS MISSING UPPER SKIN AROUND TIE DOWN FITTINGS. FABRICATED SLOPE PANEL 152EF IAW DWG 3D25-37705. DAMAGE DIM L=1.75" W=1.75". RETAIN FOR RECORDS.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 6,296 hrs · 2,844 cycles

DURING CHECK, FOUND FWD UTILITY AREA FLOOR SUPPORT AT FR21 -Y189 UPPER SURFACE FLANGE HAS CORROSION. REMOVED CORROSION IAW A320 SRM 51-74-00 CHECKED LIMITS L=1.5" W=1.0" D=.050". FOUND TO BE OUT OF LIMITS IAW A320 SRM 53-11-14 101. REMOVED & REPLACED -Y189 FLOOR SUPPORT BEAM IAW A320 SRM 51-42-11.

Part: PANEL — DAMAGED (FUSELAGE) · airframe 6,296 hrs · 2,844 cycles

DURING CHECK, FOUND AFT PIT SLOPE PANEL 161BF IS MISSING UPPER SKIN AROUND TIE DOWN FITTINGS. FABRICATED SLOPE PANEL ON STAM TRAVELER T12/927902 (161BF) IAW DWG 3D25-37705. DAMAGE DIM. L=8.0" W=8.5".

Part: PANEL — DAMAGED (CARGO BAY) · airframe 6,296 hrs · 2,844 cycles

FORWARD PIT SLOPE PANEL 131FF IS MISSING UPPER SKIN AROUND TIE DOWN FITTINGS. FABRICATED SLOPE PANEL 131FF IAW DWG 3D25-37705. DAMAGE DIM: L=2.5 W=3.5. RETAIN FOR RECORDS.

Part: PANEL — DAMAGED (CABIN) · airframe 6,296 hrs · 2,844 cycles

DURING CHECK, FOUND AFT PIT SLOPE PANEL 151NF HAS SEVERAL PUNCTURES AND MISSING UPPER SKIN AROUND TIE DOWN FITTINGS. FABRICATED SLOPE PANEL 151NF ON STAM TRAVELER T12/927899 IAWDWG 3D25-37705.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 6,296 hrs · 2,844 cycles

DURING CHECK, FOUND FORWARD CABIN FLOOR SUPPORT AT FR 20 Y503.2 UPPER FLANGES HOLES HAS CORROSION. REMOVED CORROSION IAW A320 SRM 51-74-00. FOUND TO BE OUT OF LIMIT IAW A320 SRM 53-11-14 FIG 103. INSTALLED REPAIR PER SRM 51-42-11.

Part: SILL — CORRODED (PAX DOORWAY) · airframe 67,520 hrs · 30,118 cycles

DURING INSPECTIONS, LT AFT PASSENGER DOOR SILL UPPER SURFACE AT AFT FR 68 IS CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FABRICATED ONE REPAIR ANGLE & INSTALLED IAW SRM 53-41-14 FIG 201 AND 51-42-11.

Part: FLOOR SUPPORT — CORRODED (UTILITY AREA) · airframe 67,520 hrs · 30,118 cycles

DURING INSPECTIONS, AFT UTILITY AREA FLOOR SUPPORT UPPER AND LOWER FLANGE AT FR 64 TO FR 67 -Y465 HARD POINT HOLES CORRODED. REMOVED CORROSION IAW SRM 51-74-00 & FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14 FIG 102. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-42-11.

Part: LIGHT — MISSING (CABIN) · airframe 64,063 hrs · 28,438 cycles

FLIGHT CREW REPORTED EMERGENCY PATH FLOOR LIGHT SEAT 5C MISSING AND WIRES ARE EXPOSED. INSTALLED COVER AND LIGHT HARNESS AND TESTS OK.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 63,707 hrs · 28,273 cycles

BATTERY EPSU (13WL) FAILED SYS CHECK, REPLACED BATTERY AND TESTS OK.

Part: WIRE — DAMAGED (CABIN) · airframe 63,264 hrs · 28,088 cycles

EMERGENCY LIGHT TEST FOUND ROW 3B PATH LIGHT INOP. REPAIRED WIRE AND TESTS OK.

Part: EPSU — FAULTY (CABIN) · airframe 63,062 hrs · 28,013 cycles

DURING EMERGENCY LIGHT TEST EPSU FAULTED, EPSU REPLACED AND TESTS OK.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,309 hrs · 26,823 cycles

DURING LINE CHECK FOUND CORROSION ON FLOOR SUPPORT WEB AT FR20 AND FLOOR LINE. REPAIRED IAW SRM 51-42-11, 53-22-12.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,140 hrs · 26,672 cycles

DURING L-CHECK FOUND CORROSION ON FRAME IN FORWARD CARGO AT FR29 BETWEEN S40R AND S43R. REPAIRED PER SRM 51-74-00, 53-21-12 FIG 3, 51-42-11, 51-21-11.

Part: POWER SUPPLY — SHORTED (CABIN) · airframe 58,989 hrs · 26,308 cycles

ROW 13-14-15, 18, 19 AND 20 SEAT EVAC LIGHTS INOP. FOUND BAD POWER SUPPLY INTERNALLY SHORTED. REPLACED POWER SUPPLY AND REPAIRED A BARE WIRE AT A CONNECTOR AND TESTED OK. REF LOG 6954560.

Part: CONTROL UNIT — FAULTY (CABIN) · airframe 58,987 hrs · 26,307 cycles

ESCAPE PATH LIGHT FOR SEATS 16, 17, 18, 21, 22 & 23 INOP". REMOVED AND REPLACED POWER CONTROL UNIT; OPERATIONAL CHECK OK.

Part: WIRE — BROKEN (CABIN) · airframe 58,826 hrs · 26,234 cycles

EMERGENCY EGRESS AISLE LIGHTING INOP ROWS 5-9. REPAIRED BROKEN WIRE, CHECKS OK.

Part: EPSU — DISCHARGED (CABIN)

EEPL LIGHTING AT SEATS 13L, 14L, 15L, 16L, 18L, 19L, 20L, 24L, 25L, 26L INOPERATIVE. REPLACED (2) EPSU, AND DOOR 2R SLIDE. (K)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,022 hrs · 24,453 cycles

WHEN PERFORMING EMERGENCY LIGHT TEST, EPSU 11WL FAILED. REPLACED EPSU BATTERY PACK, CHECKS OK. (A)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,605 hrs · 21,850 cycles

FORWARD OVER DOOR EMERGENCY EXIT SIGN LIGHTS NOT WORKING. CORRECTED BY REMOVING AND REPLACING FORWARD BATTERY PACK. CHECKS OK.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 41,755 hrs · 18,229 cycles

AT CRUISE FL350, LOST CABIN PRESSURE. CABIN PRESSURE CLIMBED TO 11,000 FT DURING EMERGENCY DESCENT. DESCENDED TO 10,000 FT AT 10,000 FT CABIN RE-PRESSURIZED NORMALLY. PACKS FUNCTIONED NORMALLY AND OUTFLOW VALVE WAS CLOSED DURING EMERGENCY DESCENT. FLIGHT CONTINUED TO MSP WITH AN UNEVENTFUL LANDING. REPLACED PRESSURIZATION OUTFLOW VALVE (32-2130-9-0007, S/N OFF 3143) AND CABIN PRESSURE CONTROLLER (32-2130-9-0004, S/N OFF 54554). OPERATIONAL CHECK GOOD. AIRCRAFT EXPERIENCED A RAPID DEPRESSURIZATION ON THE FOLLOWING FLIGHT. FOUND FORWARD CARGO DOOR SEAL INFLATION HOLES FILLED WITH SEALANT. REPLACED SEAL.

Part: ENGINE — FAILED (NR 1) · airframe 39,082 hrs · 17,047 cycles

DURING CRUISE FLIGHT, ENGINE NR 1 FLAMED OUT. FLIGHT CREW DIVERTED AIRCRAFT AND PERFORMED AN UNEVENTFUL LANDING. MAINTENANCE FOUND THE ALTERNATOR/STATOR (PMA) DAMAGED AND METAL ON THE GEARBOX CHIP DETECTOR. ENGINE NR 1 REPLACED.

Part: STRUCTURE — DAMAGED (FUSELAGE)

DURING INSPECTION OF DOOR 1R SLIDE GIRT BAR TRIGGER SPRING PER EO 2561-01223, THE SLIDE DROPPED (UNPACKED) FROM THE DOOR PACKBOARD ASSEMBLY AND THE INFLATION BOTTLE HIT THE GROUND BRAKING AT THE NECK ALLOWING THE BOTTLE TO PROPEL ITSELF INTO THE FORWARD RIGHT UPPER AND LOWER WING TO FUSELAGE FAIRING AREA. FOUR FORMERS WERE DAMAGED ALONG WITH DENTS IN THE FUSELAGE SKIN AND A GOUGE WITH A 1.5 INCH CRACK. REPAIRED SKIN DAMAGE PER A320 SRM.

Part: OIL LINE — CRACKED (NR 1 ENGINE)

DURING CRUISE, AFT CARGO SMOKE INDICATION ILLUMINATED. CREW DISCHARGED CARGO FIRE EXTINGUISHER, DECLARED AN EMERGENCY, DIVERTED TO JAX, AND LANDED WITHOUT INCIDENT. NO INDICATION OF FIRE OR SMOKE IN AFT CARGO COMPARTMENT UPON INSPECTION BY FIRE FIGHTING CREW. MAINTENANCE TROUBLESHOOTING REVEALED NO DISCREPANCIES. THE NR 1 ENGINE WAS PREVIOUSLY REPLACED DUE TO A CRACKED OIL LINE INDUCING OIL INTO THE PNEUMATIC SYSTEM CONSEQUENTLY CREATING SMOKE IN THE CABIN.

Part: OIL SYST — LEAKING (NR 1 ENGINE)

SHORTLY AFTER TAKEOFF, FLIGHT CREW NOTICED A BURNING SMELL AND LIGHT SMOKE HAZE THROUGHOUT THE AIRCRAFT. AIRCRAFT RETURNED TO DEPARTURE AIRPORT. MAINTENANCE FOUND INTERNAL OIL LEAK IN NR 1 ENGINE. REPLACED THE NR 1 ENGINE.

Part: PACK — OVERHEAT (NR 1)

FOLLOWING TAKEOFF, GRAY SMOKE WITH AN OILY SMELL WAS OBSERVED IN THE COCKPIT AND CABIN. CREW PERFORMED THE AIR CONDITIONING SMOKE PROCEDURE PER COCKPIT OPERATING MANUAL AND DECLARED AN EMERGENCY, RETURNED TO DTW, AND LANDED WITHOUT INCIDENT. NR 1 PACK WAS PLACED ON DEFERRAL PER MEL 21-52-01A. SUBSEQUENT MAINTENANCE TROUBLESHOOTING REVEALED NO DISCREPANCIES. NR 1 PACK OPERATIONALLY CHECKED OK.

Part: CONNECTOR — LOOSE (CABIN)

DURING TEST OF EMERGENCY LIGHTS, FOUND LIGHTS INOPERATIVE AT SEAT ROWS 19 TO 21ABC. MAINTENANCE SECURED CANNON PLUG AT SIDEWALL BELOW SEAT 19ABC, OPERATIONAL CHECK OK.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO COMPT)

DURING CLIMB, RECEIVED MESSAGE SMOKE AFT CARGO SMOKE. CREW DISCHARGED AFT CARGO FIRE EXTINGUISHER. RETURNED TO BOS AND LANDED WITHOUT INCIDENT. NO INDICATION OF FIRE OR SMOKE UPON INSPECTION OF CARGO COMPARTMENT. MAINTENANCE TROUBLESHOOTING REVEALED NO DISCREPANCIES.

Part: WARNING — ACTIVATED (CARGO DOOR)

DURING TAKEOFF, CREW RECEIVED AFT CARGO DOOR OPEN ECAM MESSAGE. ABORTED TAKEOFF AT LOW SPEED. MAINTENANCE TROUBLESHOOTING REVEALED NO DISCREPANCIES.

Part: FLAPS — MISRIGGED (TE FLAPS)

DURING APPROACH, CREW SELCETED FLAPS 2 AND RECEIVED F/CTL FLAPS LOCKED MESSAGE. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE RIGGED FLAP SYSTEM, OPERATIONAL CHECK OK.

Part: BATTERY — DISCHARGED (CABIN)

DURING LINE MAINTENANCE, THE LEFT AFT EMERGENCY LIGHT FAILED TO TEST. REPLACED EPSU, OPERATIONAL CHECK OK.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN)

WHILE CLIMBING THROUGH 14,000 FEET, RECEIVED EXCESS CABIN ALTITUDE WARNING. NO ECAM WARNINGS WERE PRESENT PRIOR TO WARNING. OXYGEN MASKS DEPLOYED AND CREW FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES. WHILE SWITCHING TO MANUAL PRESSURIZATION, RECEIVED FIRST ABNORMAL CABIN PRESSURE READINGS ON ECAM CABIN PRESSURE PAGE. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE CABIN PRESSURE OUTFLOW VALVE 10HL, OPERATIONAL CHECK OK.

Part: SUPPORT — CORRODED (FS 31577-32571)

DURING IL CHECK, FOUND CORROSION ON THE FLOOR SUPPORTS AT Y=+- 1929 FRAME 66 TO 68. REPAIRED SUPPORTS PER EA 32-99197.

Part: LONGERON — CORRODED (FS 12700-13233)

DURING IL CHECK, FOUND CORROSION ON STR 41R BETWEEN FRAMES 30 TO 31. REPAIRED STRINGER (P/N D532-31542-200, D532-31543-200), PER EA 32-99208.

Part: LONGERON — CORRODED (FS 13767-15367)

DURING IL CHECK, FOUND CORROSION ON STR 43R BETWEEN FRAMES 32 TO 35. REPAIRED STRINGER (P/N D532-31511-200), PER EA 32-99209.

Part: LONGERON — CORRODED (FS 14300-14834)

DURING IL CHECK, FOUND CORROSION ON STR 42R BETWEEN FRAMES 33 TO 34. REPAIRED STRINGER (P/N D532-31523-200), PER EA 32-99207.

Part: SUPPORTS — CORRODED (FS 31577-32571)

DURING IL CHECK, FOUND CORROSION ON THE RIGHT AND LEFT OUTBOARD FLOOR SUPPORTS BS 1292. REPAIRED SUPPORTS (P/N 534-72172-203, -204) PER EA 32-99197.

Part: SILL — CORRODED (DOOR 4L)

DURING IL CHECK, FOUND CORROSION ON THE LEFT AFT DOOR SILL. REPAIRED SILL PER EA 32-99200.