N276AY

Part: TOILET — LEAKING (LAVATORY) · airframe 78,925 hrs · 11,143 cycles

LAVATORY L61 & L62 HAVE A STRONG ODOR. CLEANED LAV L61. THE AIRCRAFT WAS GROUNDED. MAINTENACE REMOVED AND REPLACED LEAKING TOILET ASSY LAV L61 IAW AMM 38-31-41-0401.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 76,948 hrs · 10,882 cycles

OPS CHECK OF THE EMERGENCY LIGHTS FAILED TO TEST. REMOVED AND REPLACED THE BATTERY PACKS IAW AMM 33-51-38-400,33-51-38-0401. AIRCRAFT WAS GROUNDED.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 76,948 hrs · 10,882 cycles

OPS CHECK OF THE EMERGENCY LIGHTS FAILED TO TEST. REMOVED AND REPLACED THE ESPU IAW AMM 33-51-38-400, AND 33-51-38-0401. AIRCRAFT WAS GROUNDED.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 76,736 hrs · 10,849 cycles

EXIT LIGHT COVER NEAR THE L4 DOOR FELL OFF. REMOVED AND REPLACED THE LIGHT ASSEMBLY.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 76,721 hrs · 10,846 cycles

L4 DOOR EXIT LIGHT LENS DETACHED ON LANDING. INSTALLED THE LENS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,678 hrs · 10,836 cycles

THE AIRCRAFT IS IN BASE MAINTENANCE. CORROSION FOUND ON FLOOR STRUCTURE BEAM LOCATED AT FR69 BETWEEN STRINGER 48R AND STRINGER 50R BELOW FLOOR PANEL IN BULK CARGO COMPARTMENT. REPLACED FLOORBEAM PER SRM 51-42-11 AND DRAWING F53486063.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 76,678 hrs · 10,836 cycles

BROKEN EMERGENCY EXIT SIGN LENS IN THE AFT PASSENGER CABIN. REPLACED THE LENS.

Part: WINDOW — CRAZED (EMERGENCY EXIT) · airframe 76,678 hrs · 10,836 cycles

AIRCRAFT IN BASE MAINTENANCE. CRAZING IN EMERGENCY EXIT DOOR WINDOW PANES L3 IN PASSENGER CABIN. REPLACED WINDOW PANES ON EMERGENCY EXIT DOOR L3 IN PASSENGER CABIN PER AMM 56-31-11-400-801-A.

Part: WINDOW — CRAZED (EMERGENCY EXIT) · airframe 76,678 hrs · 10,836 cycles

AIRCRAFT IN BASE MAINTENANCE. CRAZING IN EMERGENCY EXIT DOOR WINDOW PANES R3 IN PASSENGER CABIN. REPLACED WINDOW PANES ON EMERGENCY EXIT DOOR R3 IN PASSENGER CABIN PER AMM 56-31-11-400-801-A.

Part: SUPPORT — CORRODED (FRAME 80) · corrosion level 2 · airframe 76,678 hrs · 10,836 cycles

CRACKED SUPPORT AT FRAME 80, Y1137.1. REPLACED THE SUPPORT IAW SRM 51-72-11, 51-42-11, AND DRAWING F53479750.

Part: SEAT TRACK — CORRODED (FRAMES 11-18) · corrosion level 2 · airframe 76,678 hrs · 10,836 cycles

CORRODED SEAT TRACK, FRAMES 11 AND 18, -Y953. REPLACED THE SEAT TRACK IAW SRM 51-42-11, DRAWINGS F53113532, AND F53911985.

Part: SEAT TRACK — CORRODED (FRAMES 11-18) · corrosion level 2 · airframe 76,678 hrs · 10,836 cycles

CORROSION FOUND ON THE SEAT TRACK BETWEEN FRAMES 11 AND 18, AT BL 0. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DRAWING F53114410.

Part: FLOOR SUPPORT — CORRODED (FRAMES 74-82) · corrosion level 2 · airframe 76,678 hrs · 10,836 cycles

CORRODED FLOOR SUPPORT BETWEEN FRAMES 74 TO 82, LBL Y794.3. REPLACED THE FLOOR SUPPORT IAW 51-72-11 AND DRAWING F53478012.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 76,678 hrs · 10,836 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACKED SPLICE LOCATED ON FLOOR BEAM AFT GALLEY AREA AT FR 73 PLUS 12 INCHES, RIGHT STRINGER 26, RBL -YA. REPLACED SPLICE PER SRM 51-72-11 AND DRAWING F53479335.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 76,678 hrs · 10,836 cycles

THE AIRCRAFT IS IN BASE MAINTENANCE. CRACKED PLATE (WEB SHEAR) LOCATED AT FRAME 75A TO FRAME 77 AT LEVEL -Y2462, STRINGER 26R AT RIGHT HAND AFT GALLEY AREA. REPLACED PLATE (WEB SHEAR) PER SRM 51-72-11 AND DRAWING F53479320.

Part: SHEAR WEB — CRACKED (FRAMES 75A-76) · airframe 76,678 hrs · 10,836 cycles

CRACKED SHEAR WEB AT FRAMES 75A TO 76, STRINGER 26L, AND Y2462. REPLACED THE SHEAR WEB IAW SRM 51-72-11, AND DRAWING F53479320.

Part: FLOOR SUPPORT — CORRODED (FRAMES 75-78) · corrosion level 2 · airframe 76,678 hrs · 10,836 cycles

CORRODED FLOOR SUPPORT BETWEEN FRAMES 75 TO 78, YE1. REPLACED THE FLOOR SUPPORT SRM 51-72-11, AND DRAWING 53478018.

Part: FLOOR SUPPORT — CORRODED (FRAMES 33-35) · corrosion level 2 · airframe 76,678 hrs · 10,836 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION FOUND ON FLOOR SUPPORT BETWEEN FRAMES 33 TO 35, Y2462. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DRAWING F53275795.

Part: SEAT TRACK — CORRODED (FRAMES 73-75) · corrosion level 2 · airframe 76,678 hrs · 10,836 cycles

CORRODED SEAT TRACK, FRAMES 73 TO 75, -Y450. REPLACED THE SEAT TRACK IAW SRM 51-72-11, 51-42-11, AND DRAWING F53478018.

Part: FLOORBEAM — CRACKED (FRAME 74) · airframe 76,678 hrs · 10,836 cycles

CRACKED FLOORBEAM AT FRAME 74, Y1959. REPAIRED CROSSBEAM IAW SRM 53-00-14-300-002, FIGURE 20102.

Part: SEAT TRACK — CORRODED (FRAMES 71-72) · corrosion level 2 · airframe 76,678 hrs · 10,836 cycles

CORRODED SEAT TRACK BETWEEN FRAMES 71 TO 72, +Y450. REPLACED THE SEAT TRACK IAW 51-72-11, AND DRAWING F53478018.

Part: FLOOR SUPPORT — CORRODED (FRAMES 75-80) · corrosion level 2 · airframe 76,678 hrs · 10,836 cycles

CORRODED FLOOR SUPPORT, FRAMES 75 TO 80, -Y50. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DRAWING F53478018.

Part: CROSSBEAM — CORRODED (FRAME 75) · corrosion level 2 · airframe 76,678 hrs · 10,836 cycles

CORROSION FOUND ON THE CROSSBEAM LOCATED AT FRAME 75, -Y450, IN THE AFT GALLEY AREA. PERFORMED A PERMANENT REPAIR ON THE CROSSBEAM IAW SRM 51-42-11, AND SRM 53-00-14-300-002.

Part: SEAT TRACK — CORRODED (FRAMES 73-74) · corrosion level 2 · airframe 76,678 hrs · 10,836 cycles

CORROSION FOUND ON THE SEAT TRACK BETWEEN FRAMES 73 & 74, -YB1. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DRAWING F53478018.

Part: FLOOR SUPPORT — CORRODED (FRAMES 30-37) · corrosion level 2 · airframe 76,678 hrs · 10,836 cycles

CORRODED FLOOR BEAM BETWEEN FRAMES 30 TO 37, -Y953. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DRAWING F53275849.

Part: SEAT TRACK — CORRODED (FRAMES 30-37) · corrosion level 2 · airframe 76,678 hrs · 10,836 cycles

THE AIRCRAFT IS IN BASE MAINTENANCE. CORROSION FOUND ON THE SEAT TRACK FRAMES 33 TO 35, -Y1959 IN THE PASSENGER CABIN. REPLACED SEAT TRACK IAW SRM 51-42-11, 51-72-11, AND DRAWING F53275849.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,678 hrs · 10,836 cycles

AIRCRAFT IN BASE MAINTENANCE. CORRODED SEAT TRACK BETWEEN FR 78 TO FR 74 AT LBL YC1. REPLACED SEAT TRACK PER A330 SRM 51-72-11 DRAWING F534782007.

Part: SEAT TRACK — CORRODED (FRAMES 73-74) · corrosion level 2 · airframe 76,678 hrs · 10,836 cycles

CORRODED SEAT TRACK, FRAMES 73 TO 74, -YB. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DRAWING F53478018.

Part: FLOOR SUPPORT — CORRODED (FRAMES 33-35) · corrosion level 2 · airframe 76,678 hrs · 10,836 cycles

CORRODED FLOOR SUPPORT, FRAMES 33 TO 35, -Y2462. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DRAWING F53275795.

Part: SEAT TRACK — CORRODED (FRAMES 72-73) · corrosion level 2 · airframe 76,678 hrs · 10,836 cycles

CORRODED SEAT TRACK, FRAMES 72 TO 73, +Y2462. REPLACED THE SEAT TRACK IAW 51-72-11, AND DRAWING F53478101.

Part: FLOOR SUPPORT — CORRODED (FRAMES 73) · corrosion level 2 · airframe 76,678 hrs · 10,836 cycles

CORROSION FOUND ON THE FLOOR SUPPORT BETWEEN FRAMES 73 AND 75, -Y648. REPLACED FLOOR SUPPORT IAW SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 75-78) · corrosion level 2 · airframe 76,678 hrs · 10,836 cycles

CORRODED FLOOR SUPPORT BETWEEN FRAMES 75 TO 78, -YE1. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DRAWING F53478018.

Part: FLOOR SUPPORT — CORRODED (FRAMES 75-80) · corrosion level 2 · airframe 76,678 hrs · 10,836 cycles

CORRODED FLOOR SUPPORT BETWEEN FRAMES 75 TO 80, Y450. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DRAWING F53478018.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,678 hrs · 10,836 cycles

DELAMINATED FLOOR PANEL 232BF, FRAME 15A TO 19, -Y450 TO -Y953. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, AND IRM 9701 REVISION G.

Part: SEAT TRACK — CORRODED (FRAME 33) · corrosion level 2 · airframe 76,678 hrs · 10,836 cycles

CORROSION FOUND ON THE SEAT TRACK AT FRAME 33, Y1959. REPLACED SEAT TRACK IAW SRM 51-72-11, AND DWG F53275849.

Part: FLOOR PANEL — DELAMINATED · airframe 76,678 hrs · 10,836 cycles

DELAMINATED FLOOR PANEL 231GF, FRAMES 20 TO 22, Y1456 TO Y953. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, PARAGRAPH 2.A, AND IRM 9701, REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,678 hrs · 10,836 cycles

DELAMINATED FLOOR PANEL 222JF, FRAMES 14 TO 16, -Y953 TO -Y1456. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, PARAGRAPH 2.A, FIGURE 20109, AND IRM 9701, REVISION G.

Part: SEAT TRACK — CORRODED (FRAMES 30-37) · corrosion level 2 · airframe 76,678 hrs · 10,836 cycles

CORROSION FOUND ON THE SEAT TRACK BETWEEN FRAMES 30 AND 37, -Y1456. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DWG F53275849.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,678 hrs · 10,836 cycles

DELAMINATED FLOOR PANEL 262PF, FRAMES 53.9 TO 55, -Y1959 TO -Y2462. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, PARAGRAPH 2.A, AND IRM 9701, REVISION G.

Part: SEAT TRACK — CORRODED (FRAMES 30-37) · corrosion level 2 · airframe 76,678 hrs · 10,836 cycles

CORROSION FOUND ON THE SEAT TRACK AT -Y450, BETWEEN FRAMES 30 TO 37. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DRAWING 53275849.

Part: SEAT TRACK — CORRODED (FRAMES 34-37) · corrosion level 2 · airframe 76,678 hrs · 10,836 cycles

CORRODED SEAT TRACK BETWEEN FRAMES 34 TO 37, LBL Y1552.5. REPLACED THE SEAT TRACK IAW SRM 51-72-11, 51-42-11, AND DRAWING F53275646.

Part: FLOORBEAM — DELAMINATED (ZONE 100) · airframe 76,678 hrs · 10,836 cycles

DELAMINATED FLOOR PANEL 221EF, FRAMES 14 TO 17 AT LBL Y953 TO RBL -Y953. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, FIGURE 20109, AND IRM 9701, REVISION G.

Part: SEAT TRACK — CORRODED (FRAMES 32-34) · corrosion level 2 · airframe 76,678 hrs · 10,836 cycles

CORRODED SEAT TRACK BETWEEN FRAMES 32 TO 34, -Y1552.5. REPLACED SEAT TRACK IAW SRM 51-72-11, AND DRAWING F53275677.

Part: SEAT TRACK — CORRODED (FRAME 17) · corrosion level 2 · airframe 76,678 hrs · 10,836 cycles

CORROSION FOUND ON THE SEAT TRACK AT FRAME 17, -Y450 IN THE FORWARD GALLEY AREA. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DRAWING F53111246.

Part: FLOOR PANEL — DELAMINATED (FRAMES 78-80) · airframe 76,678 hrs · 10,836 cycles

DELAMINATED FLOOR PANEL 272QF, FRAMES 78 TO 80 , -Y450 TO -Y1447.8. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, PARAGRAPH 2.A, FIGURE 20109, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — CORRODED (FRAME 3-36) · airframe 76,678 hrs · 10,836 cycles

CORROSION FOUND ON THE FLOOR PANEL BETWEEN FRAMES 3 AND 36, AND STRINGER 26R. REPLACED THE FLOOR PANEL IAW SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FRAMES 12A-18) · corrosion level 2 · airframe 76,678 hrs · 10,836 cycles

CORRODED SEAT TRACK BETWEEN FRAMES 12A TO 18, +Y450. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DRAWING F53111248.

Part: FLOOR PANEL — DELAMINATED (AFT GALLEY) · airframe 76,678 hrs · 10,836 cycles

DELAMINATION FOUND ON FLOOR PANEL 271FF IN THE AFT GALLEY AREA. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-2009, PARA 2-A, FIGURE 20109, AND IRM, REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,678 hrs · 10,836 cycles

DELAMINATED FLOOR PANEL 271PF, FRAMES 78 TO 80, Y450 TO -Y450. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-00, PARAGRAPH 2.A, AND IRM 9701, REVISION G.

Part: SKIN — CONTAMINATED (RUDDER) · airframe 76,678 hrs · 10,836 cycles

TRAPPED WATER INDICATED ON THE RUDDER SHELL ASSEMBLY, LOCATED BETWEEN RS 463 AND 576 AND HINGE BEARING 4 AND 5. REPAIRED THE RUDDER SKIN IAW EA 276924.

Part: SKIN — CONTAMINATED (RUDDER) · airframe 76,678 hrs · 10,836 cycles

TRAPPED WATER INDICATION ON RUDDER LEFT HAND SHELL HONEYCOMB CORE CELLS BETWEEN RUDDER RS 274 AND 327 AND BETWEEN BR 1 AND 2. REPAIRED RUDDER PER EA 276924.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,678 hrs · 10,836 cycles

THE AIRCRAFT IS IN BASE MAINTENANCE. DELAMINATION FOUND ON FLOOR PANEL 241AF (TOP LAYER) IN PASSENGER CABIN. REPAIRED FLOOR PANEL PER EA N 277008.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,678 hrs · 10,836 cycles

DELAMINATED FLOOR PANEL 241GF, FRAMES 33 TO 37, Y450 TO Y953. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-004, FIGURE 20109, AND IRM 9701, REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,678 hrs · 10,836 cycles

DELAMINATION FOUND ON THE FLOOR PANEL 241HF TOP LAYER, IN PASSENGER CABIN. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300, PARA 2A, FIGURE 20109, AND IRM 9701, REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,678 hrs · 10,836 cycles

DELAMINATED FLOOR PANEL 242CF IN THE PASSENGER CABIN. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-00 PAR.2.A AND IRM 9701.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,678 hrs · 10,836 cycles

DELAMINATED FLOOR PANEL 271QF, FRAMES 78 TO 80, Y1447.8 TO Y450. REPLACED FLOOR PANEL IAW SRM 53-02-00-300-009, PARAGRAPH 2.A, FIGURE 20109, AND IRM 9701.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,678 hrs · 10,836 cycles

DELAMINATED FLOOR PANEL 242GF, BETWEEN FRAMES 33 TO 37, Y-450 TO Y-953. REPLACED FLOOR PANEL IAW SRM 53-02-00-300-009, AND IRM 9701, REVISION G.

Part: FLOOR PANEL — DELAMINATED (AFT GALLEY) · airframe 76,678 hrs · 10,836 cycles

DELAMINATION FOUND ON FLOOR PANEL 271GF IN THE AFT GALLEY. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-000, PARA 2A, FIGURE 20109, AND IRM 9701, REVISION G.

Part: FLOOR PANEL — DELAMINATED (GALLEY) · airframe 76,678 hrs · 10,836 cycles

DELAMINATION FOUND ON THE FLOOR PANEL 271KF IN THE AFT GALLEY AREA. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, PARA 2A, FIGURE 20109.

Part: SEAT TRACK — CORRODED (FRAME 37) · corrosion level 2 · airframe 76,678 hrs · 10,836 cycles

CORRODED SEAT TRACK AT FRAME 37, +Y450. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DRAWING F53275849.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,678 hrs · 10,836 cycles

DELAMINATED FLOOR PANEL 272GF, FRAMES 73 TO 76, -Y381 TO -Y794.3. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, PARAGRAPH 2.A, FIGURE 20109, AND IRM 9701, REVISION G.

Part: FLOOR PANEL — DELAMINATED (FRAMES 73-75) · airframe 76,678 hrs · 10,836 cycles

DELAMINATED FLOOR PANEL 272KF, FRAMES 73 TO 75, -Y1137.1 TO -Y1447.8. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, PARAGRAPH 2.A AND IRM 9701, REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,678 hrs · 10,836 cycles

DELAMINATED FLOOR PANEL 241FF, FRAMES 33 TO 37, Y450 TO -Y450. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 76,678 hrs · 10,836 cycles

DELAMINATION FOUND ON THE FLOOR PANEL 242HF IN THE PASSENGER CABIN. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, PARA 2A, FIGURE 20109, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,678 hrs · 10,836 cycles

DELAMINATED FLOOR PANEL 271MF, FRAMES 75 TO 78 AT Y450 TO -Y950. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-00, PARAGRAPH 2.A, AND IRM 9701.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 76,678 hrs · 10,836 cycles

DELAMINATED FLOOR PANEL 242DF IN THE PASSENBER CABIN. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, PARA 2-A, AND IRM 9701.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,678 hrs · 10,836 cycles

THE AIRCRAFT IS IN BASE MAINTENANCE. DELAMINATION FOUND ON FLOOR PANEL 221LF AT FORWARD GALLEY AREA. REPLACED FLOOR PANEL PER SRM 53-12-00-300-006 FIGURE 20106 AND IRM 9701 REVISION G.

Part: SIGN — DETACHED (EMERGENCY LIGHT) · airframe 76,666 hrs · 10,832 cycles

R3 EXIT SIGN DETACHED DURING LANDING. SECURED THE EXIT SIGN.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 76,461 hrs · 10,796 cycles

SEAT 28B EMERGENCY LIGHT INOPERATIVE. SECURED THE ELECTRICAL CONNECTOR.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 75,907 hrs · 10,718 cycles

EMERGENCY FLASHLIGHT BATTERY BY THE L2 FOOR INOPERATIVE. REPLACED THE BATTERY.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 75,907 hrs · 10,718 cycles

EMERGENCY FLASHLIGHT BY THE L1 HAS A BATTERY DEAD. REPLACED THE BATTERY.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 75,529 hrs · 10,671 cycles

DELAMINATION FOUND ON THE LOWER SKIN LEFT OTBD FLAP TE BETWEEN RIBS 4 AND 5, AT FLAP TRACK NR 3. REPAIRED THE SKIN IAW EA 273948. AIRCRAFT WAS GROUNDED

Part: BOTTLE — LOW PRESSURE (L4 DOOR ASSIST) · airframe 75,529 hrs · 10,671 cycles

L4 DOOR ASSIST BOTTLE HAD LOW PRESSURE. SERVICED THE DOOR ASSIST BOTTLE. AIRCRAFT WAS GROUNDED.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,529 hrs · 10,671 cycles

EMERGENCY LIGHTS VIA MCDU CLASS 1 BATTERY, EPSU 14WL INOPERATIVE. REPLACED THE EPSU BATTERY. AIRCRAFT WAS GROUNDED.

Part: DECODER — MALFUNCTIONED (L2 DOOR) · airframe 75,287 hrs · 10,642 cycles

L2 DOOR MESSAGE FOR LOW PRESSURE. REPLACED DECODER.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 74,815 hrs · 10,583 cycles

EMERGENCY FLASHLIGHT BATTERY DEAD AT 4L JUMP SEAT. REPLACED THE FLASHLIGHT BATTERY

Part: OVEN — FAILED (AFT GALLEY) · airframe 74,626 hrs · 10,560 cycles

AFT GALLEY OVEN 6-11 MAKING NOISE AND HAS ODOR. REPLACED AFT GALLEY OVEN.

Part: CONNECTOR — NOT SEATED (EMERGENCY LIGHTS) · airframe 73,989 hrs · 10,483 cycles

DURING EMERGENCY POWER SUPPLY UNIT OPERATIONAL CHECK, FOUND A FAULT ON EXIT SIGN AT THE L3 DOOR POWER SUPPLY (15WL). RESEATED THE CONNECTOR AT THE L3 DOOR SLIDE IAW AMM 33-51-38. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 73,998 hrs · 10,484 cycles

DURING EMERGENCY POWER SUPPLY (16WL) OPERATIONAL CHECK, FOUND FAULT ON THE BATTERY AT 3R. REPLACED BATTERY IAW AMM 33-51-38.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 73,981 hrs · 10,482 cycles

EMERGENCY EXIT LIGHT BY THE L3 DOOR HAS A LOOSE LENS. REMOVED AND REPLACED LENS IAW AMM 33-50-00. OPS CHECKED GOOD.

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 73,410 hrs · 10,411 cycles

EXIT SIGN AT THE L3 DOOR DETACHED. ATTACHED THE EXIT SIGN COVER.

Part: BOTTLE — LOW PRESSURE (L4 DOOR) · airframe 73,139 hrs · 10,374 cycles

AIRCRAFT WAS NOT GROUNDED. L4 DOOR ASSIST PRESSURE LOW. SERVICED L4 ASSIST BOTTLE.

Part: LENS — MISSING (CABIN) · airframe 72,865 hrs · 10,335 cycles

AIRCRAFT WAS GROUNDED. LEFT AFT LAVATORY SMALL EXIT LIGHT PANEL FALLEN OFF. RESTORED EMERGENCY LIGHT COVER IN AFT LT LAVATORY.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 72,786 hrs · 10,316 cycles

BROKEN LOCK ON CABLE ASSEMBLY 618WL5. REPLACED CONNECTOR AND REINSTALLED CABLE ASSEMBLY IAW DRAWING F92393044.

Part: CABLE — DAMAGED (EMERGENCY LIGHT) · airframe 72,786 hrs · 10,316 cycles

DAMAGED CABLE ASSEMBLY 740WL4. REPLACED THE CABLE ASSEMBLY IAW DRAWING F92393044.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 72,786 hrs · 10,316 cycles

EMERGENCY LIGHT CABLE ASSEMBLY 704WL21, INSTALLED CLOSE TO SEAT 15AB, HAS A MISSING PROTECTIVE COVER. REPLACED THE COVER IAW AMM 33-51-12.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 72,786 hrs · 10,316 cycles

BROKEN BACKSHELL ON CABLE ASSEMBLY 740WL9 CONNECTOR. REPLACED CABLE ASSEMBLY IAW DRAWING F923044.

Part: CABLE — DAMAGED (EMERGENCY LIGHT) · airframe 72,786 hrs · 10,316 cycles

DAMAGED CABLE ASSEMBLY 740WL3. REPLACED THE CABLE ASSEMBLY IAW DRAWING F92393044.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 72,786 hrs · 10,316 cycles

CABLE ASSEMBLY 740WL10 HAS A BROKEN CONNECTOR LOCK. REPLACED THE CABLE ASSEMBLY IAW DRAWING F92393044.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 72,786 hrs · 10,316 cycles

EMERGENCY LIGHT CABLE ASSEMBLY 740WL10 HAS A MISSING PROTECTIVE COVER. INSTALLED A NEW COVER IAW DRAWING F92393044.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 72,786 hrs · 10,316 cycles

EMERGENCY LIGHT CABLE ASSEMBLY 618WL12 HAS A MISSING PROTECTIVE COVER. INSTALLED A NEW COVER FOR CABLE ASSEMBLY IAW DRAWING F92393044.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 72,786 hrs · 10,316 cycles

EMERGENCY LIGHT CABLE ASSEMBLY 740WL9 HAS MISSING PROTECTIVE COVER. INSTALLED A NEW PROTECTIVE COVER FOR CABLE ASSEMBLY IAW DWG F92393044.

Part: GIRT BAR — OBSTRUCTED (L1 DOOR SLIDE) · airframe 72,662 hrs · 10,293 cycles

L1 DOOR WON'T DISARM, SLIDE LEVER MOVES BUT DOOR INDICATES STILL ARMED. MAINTENANCE CLEANED GIRT BAR IAW TSM 52-71-00-810-801A AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: GIRT BAR — OBSTRUCTED (R1 DOOR) · airframe 72,327 hrs · 10,240 cycles

R1 DOOR ARM LIGHT INOPERATIVE. CLEARED DEBRIS FROM GIRT BAR AND VERIFIED SENSOR GAP PER / AMM 52-11-00.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 71,946 hrs · 10,175 cycles

SEAT 1A EMERGENCY LIGHT INOPERATIVE. REPINNED EMERGENCY LIGHT WIRE HARNESS CONNECTOR PER ESPM 20-33-11.

Part: TRACK — OBSTRUCTED (R2 DOOR) · airframe 71,923 hrs · 10,172 cycles

AIRCRAFT WAS NOT GROUNDED. 2R DOOR WILL NOT ARM. MAINTENANCE REMOVED DEBRIS FROM 2R DOOR SLIDE TRACK AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 71,760 hrs · 10,146 cycles

L1 FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT ASSEMBLY AND ACCOMPLISHED A SATISFACTORY OPS CHECK.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 71,353 hrs · 10,094 cycles

FLIGHT CREW REPORTED A LOSS OF CREW OXYGEN AND MADED AN EMERGENCY DESCENT TO 10,000 FEET. THE FLIGHT DIVERTED WHERE THE AIRCRAFT LANDED SAFELY AND WAS REMOVED FROM SERVICE. AIRCRAFT WAS GROUNDED. MAINTENANCE ISOLATED THE LEAK TO THE CAPTAINS OXYGEN MASK ASSEMBLY AND REPLACED IT PER AMM 35-123-41-401.

Part: LIGHT — BROKEN (CABIN) · airframe 71,112 hrs · 10,065 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT ON SEAT 16AB BROKEN. REPLACED EMERGENCY LIGHT AND ACCOMPLISHED A SATISFACTORY OPS CHECK IAW AMM 33-51-11.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 70,439 hrs · 9,983 cycles

EMERGENCY LIGHT LENS COVER MISSING AT LAVATORY L73. REPLACED THE EMERGENCY LIGHT LENS COVER AT LAV L73.

Part: LENS — MISSING (CABIN) · airframe 70,345 hrs · 9,970 cycles

ACFT WAS NOT GROUNDED. LAVATORY L61 BULKHEAD EMERGENCY LIGHT LENS MISSING. INSTALLED LIGHT LENS ON THE LAVATORY L61 BULKHEAD EMERGENCY LIGHT.

Part: LENS — MISSING (CABIN) · airframe 70,345 hrs · 9,970 cycles

ACFT WAS NOT GROUNDED: EMERGENCY LIGHT LENS MISSING MID GALLEY LT SIDE. INSTALLED LIGHT LENS.

Part: APU — MALFUNCTIONED (ZONE 100) · airframe 70,138 hrs · 9,944 cycles

AIRCRAFT WAS GROUNDED: THE APU EXPERIENCED AN AUTO SHUTDOWN, RESULTING IN SMOKE IN THE CABIN. THE AFT 2 SLIDES WERE DEPLOYED ALONG WITH AN OVERWING EXIT SLIDE AND THE ACFT WAS EVACUATED. MAINTENANCE REPLACED THE APU PER TASK CARD 33L31549001 AND ACCOMPLISHED A SATISFACTORY LEAK AND OPERATIONAL CHECK WITH NO ODORS NOTED.

Part: COVER — UNSECURE (EXIT SIGN) · airframe 69,702 hrs · 9,890 cycles

AIRCRAFT WAS NOT GNDED. EXIT SIGN COVER OVER R3 DOOR CAME OFF. SECURED EXIT SIGN. OK FOR SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 69,436 hrs · 9,858 cycles

AIRCRAFT WAS NOT GNDED. AFT GALLEY RT JUMP SEAT EMER FLASHLIGHT NOT FLASHING OR CHARGING. REPLACED RT JUMP AT FLASHLIGHT & BATTERY ASSEMBLY IN AFT GALLEY. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK. SEE AALA 201605099004 FOR ADDITIONAL PART INFORMATION.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 69,436 hrs · 9,858 cycles

AIRCRAFT WAS NOT GNDED. AFT GALLEY RT JUMP SEAT EMER FLASHLIGHT NOT LASHING OR CHARGING. REPLACED RT JUMP SEAT FLASHLIGHT & BATTERY ASSEMBLY IN AFT GALLEY. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK. SEE AALA 201605089001 FOR ADDITIONAL PART INFORMATION.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 69,384 hrs · 9,848 cycles

AIRCRAFT WAS NOT GNDED. DURING THE ACCOMPLISHMENT OF THE A-9 CHECK, THE DOOR ASSIST BOTTLE AT 2L WAS BELOW THE REQUIRED PSI OF 1783. SERVICED THE DOOR ASSIST BOTTLE AT 2L IAW TASK CARD 33C80052002.

Part: BOTTLE — LOW PRESSURE (R3 DOOR) · airframe 69,384 hrs · 9,848 cycles

AIRCRAFT WAS NOT GNDED. DURING THE ACCOMPLISHMENT OF THE A-9 CHECK, THE DOOR ASSIST BOTTLE AT 3R WAS BELOW THE REQUIRED PSI OF 1783. SERVICED THE DOOR ASSIST BOTTLE AT 3R IAW TASK CARD 33C80052002.

Part: SIGN — UNSECURE (CABIN) · airframe 69,099 hrs · 9,805 cycles

AIRCRAFT WAS NOT GNDED. 3R EXIT SIGN NEEDS TO BE SECURED. ATTACHED 3R EXIT SIGN.

Part: COVER — MISSING (CABIN) · airframe 69,029 hrs · 9,793 cycles

AIRCRAFT WAS NOT GNDED. EMER LIGHT COVER MISSING AT SEAT 25H. INSTALLED EMER LIGHT COVER AT SEAT 25H. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: COVER — MISSING (CABIN) · airframe 69,029 hrs · 9,793 cycles

AIRCRAFT WAS NOT GNDED. EMER LIGHT COVER MISSING AT AFT RT CABIN JUMP SEAT. INSTALLED EMER LIGHT COVER AT AFT RT CABIN JUMP SEAT. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LENS — MISSING (CABIN) · airframe 68,615 hrs · 9,694 cycles

AIRCRAFT WAS NOT GNDED. EMER LIGHT AT 2L DOOR ON LAVATORY MISSING. REPLACED LENS COVER. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: SLIDE RAFT — DEFECTIVE (L1 DOOR) · airframe 68,490 hrs · 9,661 cycles

WHILE INSTALLING A NEW SERVICEABLE SLIDE ON THE L1 DOOR, IT WAS NOTED THAT THE FLAP FOR GUIDE RELEASE BAR PACKED INCORRECTLY, CAUSING TENSION ON GIRT BAR & PREVENTING THE ABILITY TO DISARM THE DOOR. REMOVED THE DEFECTIVE SLIDE, RETURNED IT TO SUPPLY TO BE SENT OUT FOR REPAIR & ANOTHER SERVICEABLE SLIDE WAS INSTALLED IN ITS PLACE.

Part: GIRT BAR — OBSTRUCTED (R2 DOOR) · airframe 68,215 hrs · 9,596 cycles

AIRCRAFT WAS NOT GNDED. CABIN DOOR 2R SLIDE WILL NOT ARM. MECHANISM LEVER WILL NOT SLIDE TO FULL ARMED POSITION. REMOVED DEBRIS FROM GIRT BAR AREA. REMOVED BROKEN SEAL RETAINER. OPERATIONAL CHECK NOW NORMAL IAW AMM 52-71-00-0501.

Part: SIGN — MISINSTALLED (CABIN) · airframe 66,181 hrs · 9,299 cycles

CENTER AISLE EXIT SIGN 3L UPSIDE DOWN. REPLACED EXIT SIGN AT 3L.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 65,204 hrs · 9,162 cycles

SEAT MOUNTED ESCAPE PATH LIGHT AT 5H INOPERATIVE. CONNECTED THE CONNECTOR AT SEAT 5H. EMERGENCY LIGHT AT SEAT 5H OPS CHECKED GOOD.

Part: FITTING — DEFECTIVE (L1 DOOR) · airframe 64,348 hrs · 9,011 cycles

C2 CHECK, 3 DH CTRL UNIT SLIDE F HEAT G AFT INDICATOR LIGHT INOPERATIVE. REPLACED AFT SLIDE FITTING 7 DH AT THE L1 DOOR AREA IAW AMM 52-12-00.

Part: FITTING — DEFECTIVE (R2 DOOR) · airframe 64,348 hrs · 9,011 cycles

C2 CHECK, 10 DH CTL UNIT SLIDE F HEAT G AFT INDICATOR LIGHT INOPERATIVE. REPLACED AFT SLIDE FITTING 14 DH AT THE R2 DOOR AREA IAW AMM 30-46-11.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,719 hrs · 9,093 cycles

CORROSION ON AFT BELLY FAIRING SUPPORT AT FRAME 53.4 CTR LOWER WEB BETWEEN STRINGER 51L & 51R. R & R AFT BELLY FAIRING SUPPORT AT FRAME 53.4 CTR LOWER WEB BETWEEN STRINGER 51L & 51R IAW SRM 51-42-11.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 64,719 hrs · 9,093 cycles

BULK CARGO FLOOR PANEL RT AFT BETWEEN FRAME 69 & 73 AT -Y965 IS DELAMINATED & MISSING SEVERAL INSERTS. REPLACED BULK CARGO FLOOR PANEL IAW SRM 53-02-00.

Part: PIN — CORRODED (RT MLG) · airframe 64,719 hrs · 9,093 cycles

RIGHT MLG RETRACT ACTUATOR UPPER ATTACH PIN CORRODED. REPLACED RT MLG RETRACT ACTUATOR UPPER ATTACH PIN IAW AMM 32-11-11.

Part: AXLE — CORRODED (LT MLG) · airframe 64,719 hrs · 9,093 cycles

LEFT MLG AFT AXLE HAS PITTING CORROSION. REPLACED LT MLG AFT AXLE IAW SB A33 34-32-300.

Part: PIN — CORRODED (RT MLG) · airframe 64,719 hrs · 9,093 cycles

RIGHT MLG RETRACTION LINK REAR SPAR ATTACH PIN CORRODED. REPLACED RT MLG RETRACTION LINK REAR SPAR ATTACH PIN.

Part: PIN — CORRODED (LT MLG) · airframe 64,719 hrs · 9,093 cycles

LEFT MLG RETRACTION LINK REAR SPAR ATTACH PIN CORRODED. REPLACED PIN IAW AMM 32-11-11.

Part: SIGN — DETACHED (CABIN) · airframe 63,656 hrs · 8,892 cycles

3R EXIT SIGN FELL OFF. ATTACHED EXIT SIGN. OPERATIONAL CHECKED GOOD.

Part: OVEN — ODOR (GALLEY) · airframe 63,556 hrs · 8,879 cycles

FORWARD GALLEY OVEN 1 - 7 HAS RUBBER ODOR WHEN OPERATING. R & R OVEN.

Part: LENS — MISSING (CABIN) · airframe 61,425 hrs · 8,607 cycles

EXIT LIGHT PLASTIC LENS MISSING ROW 25 ACFT RT. REPLACED ROW 25 BULLHEAD EMERGENCY LIGHT LENS, OPERATIONS CHECKED NORMAL.

Part: PANEL — OUT OF POSITION (AC BAY) · airframe 61,250 hrs · 8,582 cycles

APPROX 2 HOURS AFTER TAKEOFF, LOUD VIBRATING NOISE REPORTED ROW 13 ACFT RT. NOISE APPEARED COMING FROM OVERHEAD POSITION & FELT OVERHEAD & IN FLOOR BELOW. NOISE IS HIGH PITCHED & CONSTANT, GETTING LOUDER AT 4:50 INTO FLIGHT. FOUND INSPECTION PANEL ON PACK 2 PLENUM CHAMBER TO BE MISSING FROM ITS PROPER INSTALLATION. REINSTALLED WITH NEW HARDWARE.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 60,502 hrs · 8,479 cycles

C01 CHECK, CRACK ON FWD CARGO FLOOR PANEL 131PF BETWEEN FRAME 26.3 TO FRAME 28 & BETWEEN Y920 TO Y1420. REPLACED FWD CARGO FLOOR PANEL 131PF IAW SRM 53-00-00-400-802-A.

Part: PIN — CORRODED (RT MLG) · airframe 60,502 hrs · 8,479 cycles

C1 CHECK, CORROSION ON RT MLG BOGIE BEAM PIVOT PIN AT FRAME 51. REPLACED RT MLG BOGIE BEAM PIVOT PIN IAW EO 3211U006.

Part: BOTTLE — LOW PRESSURE (R4 DOOR) · airframe 60,377 hrs · 8,461 cycles

PHL DOOR 4R DOOR ASSIST PRESS IN YELLOW. ACCOMPLISHED SERVICE 4R DOOR.

Part: PUMP — SHEARED (NR 1 ENGINE) · airframe 60,066 hrs · 8,410 cycles

FLIGHT 718, PHL-FLO, THE FLIGHT LOST THE GREEN HYD SYS AFTER TAKEOFF & RETURNED TO THE FIELD. EMERGENCY EQUIPMENT RESPONDED AS A PRECAUTION, SINCE STEERING IS AFFECTED BY THE LOSS OF GREEN SYS HYD. THE ACFT HAD TO BE TOWED TO THE GATE. R & R THE NR 2 GREEN EDP DUE TO INTERNAL FAILURE & NR 1 GREEN EDP DUE TO NO OUTPUT & SHEARED SHAFT. SYS FLUSH, APPLICABLE FILTER CHANGES & SYS BLEEDING ALL PERFORMED.

Part: PUMP — FAILED (RT ENGINE) · airframe 60,066 hrs · 8,410 cycles

FLIGHT 718, PHL-FLO, THE FLIGHT LOST THE GREEN HYD SYS AFTER TAKEOFF & RETURNED TO THE FIELD. EMERGENCY EQUIPMENT RESPONDED AS A PRECAUTION, SINCE STEERING IS AFFECTED BY THE LOSS OF GREEN SYS HYD. THE ACFT HAD TO BE TOWED TO THE GATE. R & R THE NR 2 GREEN EDP DUE TO INTERNAL FAILURE & NR 1 GREEN EDP DUE TO NO OUTPUT & SHEARED SHAFT. SYS FLUSH, APPLICABLE FILTER CHANGES & SYS BLEEDING ALL PERFORMED.

Part: UNKNOWN — MALFUNCTIONED (CABIN) · airframe 59,893 hrs · 8,387 cycles

EXIT LIGHTS VICINITY DOORS 1L, 2L, 2R & 3R COME ON INFLIGHT INTERMITTENTLY WITHOUT COMMAND. COULD NOT VERIFY VIA PFR OR SYSTEM MAINTENANCE BITE. REPLACED CIDS 1 ASSEMBLY AS PRECAUTION & SYSTEM OPERATIONAL CHECK ACCOMPLISHED SATISFACTORY.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 59,656 hrs · 8,353 cycles

1L DOOR AFT FACING INBD FLIGHT ATTENDANT JUMP SEAT FLASHLIGHT NOT FLASHING. REPLACED BATTERY IN 1L DOOR JUMP SEAT TESTED OK.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 59,121 hrs · 8,280 cycles

ESPU BATTERY PACKS AT 11WL & 15WL FAILED CAPACITENCE CHECK. MAINTENANCE R & R ESPU BATTERY PACKS AT 11WL & 15WL.

Part: CONTROL PANEL — ODOR (ZONE 200) · airframe 58,604 hrs · 8,214 cycles

F/A REPORTED ODOR COMING FROM IFE SYSTEM, ELECTRICAL ODOR, WHEN TURNED OFF ODOR GOES AWAY. SYS LEFT OFF REMAINDER OF FLIGHT. MX REPLACED FWD IFE CREW TERMINAL. RAN IFE SYS 4HRS NO ODOR. OP'S CHECKED OK.

Part: SIGN — BROKEN (EMERGENCY LIGHT) · airframe 58,165 hrs · 8,154 cycles

EMERGENCY EXIT OVERHEAD SIGN AT L3 DOOR BROKEN. MX R & R EMERGENCY EXIT OVERHEAD AISLE SIGN AT L3 DOOR. OPS CHECKED GOOD.

Part: BOTTLE — LOW PRESSURE (L3 DOOR) · airframe 57,810 hrs · 8,110 cycles

L- 3 DOOR DOOR PRESSURE LOW. MX SERVICED L3 DOOR ASSIST BOTTLE AS REQUIRED.

Part: COVER — DETACHED (CABIN) · airframe 57,651 hrs · 8,090 cycles

AT 25C COVER FOR EMERGENCY PATH LIGHTING CAME OFF. MX REFITTED COVER AT 25C.

Part: BOTTLE — LOW PRESSURE (L3 DOOR) · airframe 57,004 hrs · 8,007 cycles

CLT - L3 DOOR ASSIST BOTTLE PRESSURE LOW. SERVICED ASSIST BOTTLE.

Part: COVER — MISSING (CABIN) · airframe 57,004 hrs · 8,007 cycles

CLT - 3-18 EXIT LIGHT COVER MISSING. INSTALLED MISSING EMERGENCY EXIT LIGHT COVER.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 56,275 hrs · 7,908 cycles

A15 VISIT - L1 & L3 DOOR ASSIST PRESSURES IN YELLOW BAND REQUIRE SERVICE. SERVICES L1 & L3 DOOR DAMPER & EMERGENCY OPERATION CYLINDERS IAW A330 AMM 52-10-00-600-802A & 52-22-00-600-801A.

Part: SKIN — SATURATED (RT ELEVATOR) · airframe 56,273 hrs · 7,907 cycles

A15 VISIT - WATER INGRESS AT 6 AREAS ON RIGHT ELEVATOR UPPER SURFACE (PREVIOUSLY REPAIRED) & 1 NEW AT 41ST, 29TH, 25TH, 4TH, 23RD & 26TH FASTENER HOLE FROM THE OUTBOARD END. ALSO APPROX 3.875, 3.5, 3.5, 4.5, 7.5, 4 & 6.5 INCHES RESPECTIVELY FROM TRAILING EDGE. REPAIRED RIGHT ELEVATOR IAW A330 AMM 27-34-41 & 55-16-48.

Part: SKIN — SATURATED (LT ELEVATOR) · airframe 56,273 hrs · 7,907 cycles

A15 VISIT - WATER INGRESS AT 6 AREAS ON LEFT ELEVATOR UPPER SURFACE (PREVIOUSLY REPAIRED) & 1 NEW AT 11TH,12TH,16TH, 20TH, 21ST, 29TH, 35TH & 42ND FASTENER HOLE FROM THE OUTBOARD END. ALSO APPROX .125, 3.625, 4.0, 4.875, 3.375, 3.625 & 4 INCHES RESPECTIVELY FROM TRAILING EDGE. REPAIRED LEFT ELEVATOR IAW A330 AMM 27-34-41 & 55-16-48.

Part: BOTTLE — LOW PRESSURE (R4 DOOR) · airframe 56,196 hrs · 7,895 cycles

THE 4R DOOR AND SLIDE LOW PRESSURE. MAINTENANCE SERVICED R4 DOOR ASSIST BOTTLE AND REPLACED THE CIDS DIRECTOR 1.

Part: COVER — MISSING (CABIN) · airframe 55,633 hrs · 7,813 cycles

EXIT LIGHT COVER AT SEAT 25C IS MISSING. MAINTENANCE RELOCATED AND FITTED THE EXIT LIGHT COVER.

Part: DAMPER — LOW PRESSURE (L3 DOOR) · airframe 55,451 hrs · 7,789 cycles

DOOR 3L LOW PRESSURE INDICATION ON FAP. MAINTENANCE SERVICED 3L DOOR DAMPER TO CORRECT PRESSURE.

Part: OVEN — OVERHEATED (GALLEY) · airframe 55,307 hrs · 7,771 cycles

SINGLE OVEN 7-12 AIRCRAFT LEFT AFT GALLEY OVER HEATED ON MEDIUM IN 15 MINUTES, VERY SMOKEY, VERY HOT. MAINTENANCE REPLACED OVEN, OPERATIONAL CHECK IS GOOD.

Part: CYLINDER — LOW PRESSURE (L3 DOOR) · airframe 53,480 hrs · 7,519 cycles

LOW PRESSURE ON L-3 DOOR CIDS CAUTION. MAINTENANCE SERVICED PRESSURE ON L-3 DOOR, OK FOR SERVICE.

Part: FILTER — DIRTY (CABIN) · airframe 53,307 hrs · 7,495 cycles

FLIGHT ATTENDANT REPORTED INTENSE ODOR IN AFT GALLEY AFTER TAKEOFF ON WET RUNWAY. FLAPS 2 SMELL DESCRIBED AS PETROLEUM OR CHEMICAL LIKE OCCURING INTERMITTENTLY ON FOUR OCCASIONS. THE FLIGHT DIVERTED TO PHL AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FORWARD AND AFT HEPA FILTERS.

Part: DAMPER — LOW PRESSURE (L3 DOOR) · airframe 52,745 hrs · 7,419 cycles

DOOR 3L DOOR DAMPER HAS LOW PRESSURE. MAINTENANCE ADJUSTED DOOR 3L DAMPER.

Part: GIRT BAR — FAULTY (L1 DOOR) · airframe 51,721 hrs · 7,287 cycles

TSI - L1 DOOR IS STILL DIFFICULT TO DISARM. MAINTENANCE CHECKED ADJUSTMENT OF ECAPE SLIDE RELEASE MECHANISM AND FOUND THAT THE DOOR WOULD NOT DISARM WITH THE GIRT BAR LOADED INBOARD. ADJUSTED THE SLIDE SKIRT VELCRO ACCORDINGLY. REMOVED AND REPLACED THE REAR GIRT BAR SLIDER AS A PRECAUTIONARY. MAINTENANCE REMOVED AND REPLACED THE GIRT BAR. REMOVED L1 DOOR ESCAPE SLIDE AND RE-INSTALLED SLIDE AFTER GIRT REPLACEMENT.

Part: LEVER — FROZEN (L1 DOOR) · airframe 51,705 hrs · 7,285 cycles

DOOR 1L WILL NOT DISARM - LEVER APPEARS TO BE FROZEN. MAINTENANCE EXERCISED & FREED OFF DOOR 1L ARM/DISARM SLIDE LEVER . ARM/DISARM OPERATION IS NOW SATISFACTORY PER AMM TASK 52-10-00-710-805-A.

Part: GIRT BAR — BENT (L1 DOOR) · airframe 51,705 hrs · 7,285 cycles

TSI SEVEN PREVIOUS SQUAWKS L1 DOOR WILL NOT DISARM PER LOG PAGE 6479702 THE L1 DOOR SLIDE GIRT BAR WAS REPLACED AT BFM HEAVY MAINTENANCE BECAUSE IT WAS BENT. MAINTENANCE CORRECTLY POSITIONED LAY OF ESCAPE SLIDE GIRT BAR FLAP. CORRECTLY INSTALLED QUICK RELEASE BAR INTO ITS BRACKET PER AMM 25-62-41OPS CK NORMAL. OK FOR SERVICE.

Part: RELEASE MECH — LACK OF LUBE (L1 DOOR) · airframe 51,688 hrs · 7,283 cycles

SLIDE 1L WILL NOT DISARM. MAINTENANCE LUBRICATED SLIDE QUICK RELEASE BAR RELEASE LEVER . ARM/DISARM OF SLIDE CARRIED OUT SEVERAL TIMES, NOW OK.

Part: GIRT BAR — OUT OF ADJUST (EVAC SLIDE) · airframe 51,688 hrs · 7,283 cycles

1L DOOR SLIDE WILL NOT DISARM AT GATE ARRIVAL. MAINTENANCE REMOVED GIRT BAR FROM DOOR LATCHES COVER AND RECENTERED ON SLIDE HOLDING MECHANISM. ALL WORK PERFORMED PER A330 AMM 52-11-22-820-801 -A, OPERATION CHECK OK VARIOUS TIMES, OK FOR SERVICE.

Part: ANGLE — LEAKING (LT WING) · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - BASED ON REPORTS OF FUEL LEAKS ON OTHER A330-232 A/C'S, RIB 1/FR 42 OUTER ANGLES. REPLACED OUTER ANGLE AT LEFT RIB 1, FR42 IAW EA 103576A.

Part: TERMINAL — BROKEN (CABIN) · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - AFT G5 GALLEY EMERGENCY ESCAPE PATH LIGHT INOP. REPAIRED AFT G5 GALLEY EMERGENCY ESCAPE PATH LIGHT & PERFORMED OPS CHECK IAW A330 AMM 33-51-00-710-803-A.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FR14 TO FR16, Z-831. REPLACED FLOOR SUPPORT BETWEEN FR14 TO FR16, Z-831 IAW A330 SRM 51-42-11.

Part: ANGLE — LEAKING (RT WING) · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - BASED ON REPORTS OF FUEL LEAKS ON OTHER A330-232 A/C'S, RIB 1/FR 42 OUTER ANGLES REPLACED. REPLACED OUTER ANGLE AT RIGHT RIB 1, FR42 IAW EA 103576A.

Part: GIRT BAR — BENT (L1 DOOR) · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - L1 DOOR SLIDE ASSEMBLY GIRT BAR IS BENT. REPLACED GIRT BAR ON L1 DOOR SLIDE ASSEMBLY IAW A330 AMM 25-62-41-400-801-A.

Part: SKIN — BROKEN (LE SLAT) · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - BROKEN EDGE ON RIGHT WING NR 1 SLAT AT UPPER SURFACE APPROX 2.88 INCHES FROM OUTBOARD END OF SLAT. REPAIRED RIGHT WING NR 1 SLAT IAW EA 134608.

Part: FLOOR PANEL — BROKEN (CARGO BAY) · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - AFT CARGO FLOOR PANEL 152DK BROKEN BETWEEN FR53.6 TO FR54, -Y833. REPLACED AFT CARGO FLOOR PANEL 152DK IAW A330 SRM 53-02-00 FIG 211.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - CORROSION ON FLOOR PANEL 221GF (21DS) BETWEEN FR14 TO FR17, Y1959. REPAIRED FLOOR PANEL 221GF (21DS) IAW TYPICAL REPAIR TR330-5302-11-0330.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - CORROSION ON FLOOR PANEL 222GF (20DS) BETWEEN FR14 TO FR17, -Y1959. REPAIRED FLOOR PANEL 222GF (20DS) IAW TYPICAL REPAIR TR330-5302-11-0330.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR40.3 TO FR41, -Y2462. REPLACED SEAT TRACK BETWEEN FR40.3 TO FR41, -Y2462 IAW A330 SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT AT FR15A, Y953. REPLACED FLOOR SUPPORT AT FR15A, Y953 IAW A330 SRM 51-42-11.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR PANEL 28DS BETWEEN FR33 TO FR35, -Y1708. REPAIRED FLOOR PANEL 28DS IAW TYPICAL REPAIR TR330-5302-11-0330.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR PANEL 27DS BETWEEN FR33 TO FR35, Y2218. REPLACED FLOOR PANEL 27DS IAW TRM 330-5302-11-0330.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR PANEL 29DS BETWEEN FR34 TO FR36, -Y1705. REPLACED FLOOR PANEL 29DS IAW TRM 330-5302-11-0330.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON DOOR SILL PANEL 242LF BETWEEN FR33 TO FR35A, S26L. REPLACED DOOR SILL PANEL 242LF IAW A330 SRM 51-42-11.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR PANEL 26DS BETWEEN FR33 TO FR35, -Y1705. REPLACED FLOOR PANEL 26DS IAW TRM 330-5302-11-0330.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON DOOR SILL PANEL 241LF BETWEEN FR33 TO FR35A, S26L. REPLACED DOOR SILL PANEL 241LF IAW A330 SRM 51-42-11.

Part: FLOOR PANEL — BROKEN (ZONE 100) · airframe 51,630 hrs · 7,271 cycles

S2 CHECK, BROKEN FLOOR PANEL 241RF BETWEEN FR35 TO FR37 & BETWEEN Y1456 TO Y1959. REPLACED FLOOR PANEL IAW SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 51,630 hrs · 7,271 cycles

S2 CHECK, DELAMINATION ON FLOOR PANEL 231CF BETWEEN FR17 TO FR19 & BETWEEN Y953 TO Y2462. REPLACED FLOOR PANEL IAW SRM 53-02-00.

Part: FLOOR PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK, LEVEL 2 GALVANIC CORROSION ON FLOOR PANEL 22DS BETWEEN FR14 TO FR 17 & BETWEEN -Y1456 TO -Y1959. REPAIRED FLOOR PANEL IAW TR330-5302-11-0330.

Part: RIB — WORN (NR 1 NACELLE) · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - NR 1 PYLON AT RIB 18A INBOARD PYLON TO WING ATTACHMENT FITTING SLEEVE HAS WORN PROTECTIVE COATING & SCRATCHES. REPLACED NR 1 PYLON AT RIB 18A INBOARD PYLON TO WING ATTACHMENT FITTING SLEEVE IAW AMM 54-51-17.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT AT FR17 BETWEEN -Y953 TO -Y1456. REPLACED FLOOR SUPPORT AT FR17 BETWEEN -Y953 TO -Y1456 IAW A330 SRM 51-44-11 & 51-42-11.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR17 BETWEEN -Y1456 TO -Y1959. REPLACED FLOORBEAM AT FR17 BETWEEN -Y1456 TO -Y1959 IAW SRM 51-44-11 & 51-42-11.

Part: PIN — WORN (NR 2 PYLON) · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - WORN 2 EA SLEEVE PINS ON NR 2 OUTBOARD PYLON AT RIB 12. REPLACED 2 EA SLEEVE PINS ON NR 2 OUTBOARD PYLON AT RIB 12 AT INBOARD & OUTBOARD WING TO PYLON FITTINGS IAW A330 MM 54-51-17.

Part: RIB — WORN (NR 1 NACELLE) · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - NR 1 PYLON AT RIB 18A TOP PYLON TO WING ATTACHMENT FITTING SLEEVE HAS WORN PROTECTIVE COATING & SCRATCHES. REPLACED NR 1 PYLON AT RIB 18A TOP PYLON TO WING ATTACHMENT FITTING SLEEVE IAW A330 AMM 54-51-17.

Part: SKIN — SATURATED (RT ELEVATOR) · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - MOISTURE INGRESSION ON RIGHT ELEVATOR BETWEEN ELEVATOR RIB 10 TO RIB 11 APPROX 3.875 INCHES FORWARD OF TRAILING EDGE. REPAIRED RIGHT ELEVATOR BETWEEN ELEVATOR RIB 10 TO RIB 11 IAW EO 5511U056.

Part: SKIN — SATURATED (RT ELEVATOR) · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - MOISTURE INGRESSION ON RIGHT ELEVATOR BETWEEN ELEVATOR RIB 7 TO RIB 8 APPROX 3.5 INCHES FORWARD OF TRAILING EDGE. REPAIRED RIGHT ELEVATOR BETWEEN ELEVATOR ELEVATOR RIB 7 TO RIB 8 IAW EO 5511U056.

Part: SEAT TRACK — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON SEAT TRACK BETWEEN FR58 TO FR62, -Y2462. REPLACED SEAT TRACK IAW SRM 53-00-15 FIG 101 & 51-42-11.

Part: SKIN — SATURATED (LT ELEVATOR) · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - MOISTURE INGRESSION ON LEFT ELEVATOR AT ELEVATOR RIB 4 APPROX 4 INCHES FORWARD OF TRAILING EDGE. REPAIRED LEFT ELEVATOR AT ELEVATOR RIB 4 IAW EO # 5511U056.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK, LEVEL 2 FILIFORM CORROSION ON SEAT TRACK AT FR13A, -Y953. REPLACED SEAT TRACK IAW SRM 53-11-15 FIG 101 & 51-42-11.

Part: SKIN — SATURATED (LT ELEVATOR) · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - MOISTURE INGRESSION ON LEFT ELEVATOR BETWEEN ELEVATOR RIB 7 TO RIB 8 APPROX 4.875 INCHES FORWARD OF TRAILING EDGE. REPAIRED LEFT ELEVATOR BETWEEN ELEVATOR RIB 7 TO RIB 8 IAW EO 5511U056.

Part: SKIN — SATURATED (RT ELEVATOR) · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - MOISTURE INGRESSION ON RIGHT ELEVATOR BETWEEN ELEVATOR RIB 2 TO RIB 3 APPROX 4 INCHES FORWARD OF TRAILING EDGE. REPAIRED RIGHT ELEVATOR BETWEEN ELEVATOR ELEVATOR RIB 2 TO RIB 3 IAW EO 5511U056.

Part: SKIN — SATURATED (RT ELEVATOR) · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - MOISTURE INGRESSION ON RIGHT ELEVATOR AT ELEVATOR RIB 7 APPROX 3.5 INCHES FORWARD OF TRAILING EDGE. REPAIRED RIGHT ELEVATOR AT ELEVATOR RIB 7 IAW EO 5511U056.

Part: SKIN — SATURATED (LT ELEVATOR) · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - MOISTURE INGRESSION ON LEFT ELEVATOR AT ELEVATOR RIB 9 APPROX 4.125 INCHES" FORWARD OF TRAILING EDGE. REPAIRED LEFT ELEVATOR AT ELEVATOR RIB 4 IAW EO # 5511U056.

Part: SKIN — SATURATED (RT ELEVATOR) · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - MOISTURE INGRESSION ON RIGHT ELEVATOR BETWEEN ELEVATOR RIB 6 TO RIB 7 APPROX 4.5 INCHES FORWARD OF TRAILING EDGE. REPAIRED RIGHT ELEVATOR BETWEEN ELEVATOR ELEVATOR RIB 6 TO RIB 7 IAW EO 5511U056.

Part: SKIN — SATURATED (LT ELEVATOR) · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - MOISTURE INGRESSION ON LEFT ELEVATOR BETWEEN ELEVATOR RIB 6 TO RIB 7 APPROX 3.625 INCHES FORWARD OF TRAILING EDGE. REPAIRED LEFT ELEVATOR BETWEEN ELEVATOR RIB 6 TO RIB 7 IAW EO 5511U056.

Part: SKIN — SATURATED (LT ELEVATOR) · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - MOISTURE INGRESSION ON LEFT ELEVATOR BETWEEN ELEVATOR RIB 8 TO RIB 9 APPROX 4 INCHES FORWARD OF TRAILING EDGE. REPAIRED LEFT ELEVATOR BETWEEN ELEVATOR RIB 8 TO RIB 9 IAW EO 5511U056.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR33 TO FR37, Y953. REPLACED SEAT TRACK BETWEEN FR33 TO FR37, Y953 IAW A330 SRM 51-00-15 FIG 101, 51-42-11 & 51-75-12.

Part: SKIN — SATURATED (LT ELEVATOR) · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - MOISTURE INGRESSION ON LEFT ELEVATOR BETWEEN ELEVATOR RIB 7 TO RIB 8 APPROX 3.375 INCHES FORWARD OF TRAILING EDGE. REPAIRED LEFT ELEVATOR BETWEEN ELEVATOR RIB 7 TO RIB 8 IAW EO 5511U056.

Part: SKIN — SATURATED (LT ELEVATOR) · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - MOISTURE INGRESSION ON LEFT ELEVATOR BETWEEN ELEVATOR RIB 8 TO RIB 9 APPROX 3.625 INCHES FORWARD OF TRAILING EDGE. REPAIRED LEFT ELEVATOR BETWEEN ELEVATOR RIB 8 TO RIB 9 IAW EO 5511U056.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK, LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT AT FR13A, -Y450. REPLACED FLOOR SUPPORT IAW SRM 51-42-11.

Part: FRAME — CRACKED (LT PYLON) · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - CRACK IN LEFT PYLON INBOARD SUPPORT FRAME BETWEEN RIB 10 & RIB 11. REPAIRED LEFT PYLON INBOARD SUPPORT FRAME BETWEEN RIB 10 & RIB 11 IAW A330 SRM 54-52-12 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR31 TO FR37, Y1456. REPLACED SEAT TRACK BETWEEN FR31 TO FR37, Y1456 IAW A330 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK, LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR44 TO FR45, Y450. REPLACED SEAT TRACK IAW SRM 53-31-15 FIG 101 & 51-42-11.

Part: SEAT TRACK — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR31 TO FR37, -Y450. REPLACED SEAT TRACK BETWEEN FR31 TO FR37, -Y450 IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK, LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BETWEEN FR53.4 TO FR53.6, -Y1959. REPLACED SEAT TRACK IAW SRM 53-00-15 FIG 101, 51-42-11 & 51-75-12.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT AT FR13A BETWEEN Y232 TO Y450. REPLACED FLOOR SUPPORT AT FR13A BETWEEN Y232 TO Y450 IAW A330 SRM 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - DELAMINATED ON FLOOR PANEL 222JF BETWEEN FR14 TO FR17 & BETWEEN Y953 TO Y1456. REPLACED FLOOR PANEL 222JF IAW A330 SRM 53-02-00 FIG 211.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 241GF BETWEEN FR33 TO FR37, BETWEEN Y450 TO Y953. REPLACED FLOOR PANEL 241GF IAW A330 SRM 53-02-00 FIGURE 211.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 271AG BETWEEN FR71 TO FR73, BETWEEN Y1456 TO Y2462. REPLACED FLOOR PANEL 271AG IAW A330 SRM 53-02-00 FIGURE 211.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 251WG BETWEEN FR53.2 TO FR53.4, BETWEEN Y1456 TO Y1959. REPLACED FLOOR PANEL 251WG IAW A330 SRM 53-02-00 FIGURE 211.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 51,630 hrs · 7,271 cycles

S2 CHECK- DELAMINATION ON FLOOR PANEL 271PF BETWEEN FR78 TO FR80, BETWEEN -Y450 TO Y450. REPLACED FLOOR PANEL 271PF IAW A330 SRM 53-02-00 FIGURE 211.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 272BF BETWEEN FR71 TO FR73, BETWEEN -Y450 TO -Y953. REPLACED FLOOR PANEL 272BF IAW A330 SRM 53-02-00 FIGURE 211.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK, LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR31.5 TO FR37, -Y1456. REPLACED SEAT TRACK IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FR12A TO FR17.5, -Y450. REPLACED FLOOR SUPPORT BETWEEN FR12A TO FR17.5, -Y450 IAW A330 SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FR12 TO FR17.5, Y450. REPLACED FLOOR SUPPORT BETWEEN FR12 TO FR17.5, Y450 IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR37 TO FR37.4, Y953. REPLACED SEAT TRACK BETWEEN FR37 TO FR37.4, Y953 IAW A330 SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT AT FR13A, -Y1456. REPLACED FLOOR SUPPORT AT FR13A, -Y1456 IAW A330 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK, LEVEL 2 FILIFORM CORROSION ON SEAT TRACK BETWEEN FR53.5 TO FR53.6, -Y2462. REPLACED SEAT TRACK BETWEEN IAW SRM 51-42-11 & 51-44-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FR75 TO FR76, -Y1447.8. REPLACED FLOOR SUPPORT BETWEEN FR75 TO FR76, -Y1447.8 IAW A330 SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT AT FR13A, Y=0. REPLACED FLOOR SUPPORT AT FR13A, Y=0 IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK, LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR31 TO FR37, Y450. REPLACED SEAT TRACK IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR53.4 TO FR53.5, -Y1959. REPLACED SEAT TRACK BETWEEN FR53.4 TO FR53.5, -Y1959 IAW A330 SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FR71 TO FR72, Y2462. REPLACED FLOOR SUPPORT BETWEEN FR71 TO FR72, Y2462 IAW A330 SRM 53-41-11, 51-74-00, 51-42-11 & 51-75-12.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - CRACK ON SUPPORT ANGLES AT FR53.2, Y1959. REPLACED SUPPORT ANGLES AT FR53.2, Y1959 IAW A330 SRM 51-42-11, 51-44-11 & 51-21-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR39.2 TO FR40, Y450. REPLACED SEAT TRACK BETWEEN FR39.2 TO FR40, Y450 IAW A330 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR39.2 TO FR40, -Y2462. REPLACED SEAT TRACK BETWEEN FR39.2 TO FR40, -Y2462 IAW A330 SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FR10 TO FR13A, -Y721.6. REPLACED FLOOR SUPPORT BETWEEN FR10 TO FR13A, -Y721.6 IAW A330 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR71 TO FR75, -Y450. REPLACED SEAT TRACK BETWEEN FR71 TO FR75, -Y450 IAW A330 SRM 51-42-11.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - CRACK ON SUPPORT BRACKET AT FR53.2, -Y1959. REPLACED SUPPORT BRACKET AT FR53.2, -Y1959 IAW A330 SRM 51-42-11.

Part: SUPPORT — CORRODED (FAIRING) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER FUSELAGE FAIRING SUPPORT AT FR40 BETWEEN -Y450 & Y450. REPLACED LOWER FUSELAGE FAIRING SUPPORT AT FR40 BETWEEN -Y450 & Y450 IAW A330 SRM 51-74-00, 53-35-14 PB 122 FIG 104 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR58 TO FR59, Y1959. REPLACED SEAT TRACK BETWEEN FR58 TO FR59, Y1959 IAW A330 SRM 51-74-00, 51-44-11 & 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FR74 TO FR75, -Y794.3. REPLACED FLOOR SUPPORT BETWEEN FR74 TO FR75, -Y794.3 IAW A330 SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT AT FR76, Y1447.8. REPLACED FLOOR SUPPORT AT FR76, Y1447.8 IAW A330 SRM 51-42-11.

Part: PLATE — CRACKED (FUSELAGE) · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - CRACK ON SUPPORT PLATE AT FR57, Y=0. REPLACED SUPPORT PLATE AT FR57, Y=0 IAW A330 SRM 51-42-11 PAR 5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR53.2 TO FR54, Y450. REPLACED SEAT TRACK BETWEEN FR53.2 TO FR54, Y450 IAW A330 SRM 51-42-11, 53-31-15 FIG 101 SHT 8 SEC M-M.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR73 TO FR74, YC1. REPLACED SEAT TRACK BETWEEN FR73 TO FR74, YC1 IAW A330 SRM 51-74-00, 53-00-15 FIG 101 & 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON FLOOR SUPPORT BEAM BETWEEN FR73 TO FR75, -Y703. REPLACED FLOOR SUPPORT BEAM BETWEEN FR73 TO FR75, -Y703 IAW A330 SRM 53-41-14 FIG 103 & 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON FLOOR SUPPORT BEAM BETWEEN FR71/72 TO FR74, Y794.3. REPLACED FLOOR SUPPORT BETWEEN FR71/72 TO FR74, Y794.3 IAW A330 SRM 53-41-14 FIG 103 & 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON BEAM ASST / FLOOR SUPPORT BETWEEN FR75 TO FR76, -Y1447.8. REPLACED BEAM ASST / FLOOR SUPPORT BETWEEN FR75 TO FR76, -Y1447.8 IAW A330 SRM 53-41-14 FIG 101 & 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BEAM BETWEEN FR71 TO FR74, -Y794.3. REPLACED FLOOR SUPPORT BEAM BETWEEN FR71 TO FR74, -Y794.3 IAW A330 SRM 53-00-15 FIG 101 & 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FR34 TO FR35, Y=0. REPLACED FLOOR SUPPORT BETWEEN FR34 TO FR35, Y=0 IAW A330 SRM 53-21-14 FIG 102 & 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FR33 TO FR34, Y=0. REPLACED FLOOR SUPPORT BETWEEN FR33 TO FR34, Y=0 IAW A330 SRM 53-21-14 FIG 201 & 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT AT FR13A, Y232. REPLACED FLOOR SUPPORT AT FR13A, Y232 IAW A330 SRM 53-11-14 FIGURE 101 AND SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT AT FR73, Y0. REPLACED FLOOR SUPPORT AT FR73, Y0 IAW A330 SRM 51-74-00, 53-41-14, 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BEAM BETWEEN FR61 TO FR71, Y794.3. REPLACED FLOOR SUPPORT BEAM BETWEEN FR61 TO FR71, Y794.3 IAW A330 SRM 51-42-11, 51-44-11, 51-75-12.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON AUXILIARY BEAM BETWEEN FR73 TO FR74, BETWEEN -Y1959 TO -Y2462. REPLACED AUXILIARY BEAM BETWEEN FR73 TO FR74, BETWEEN -Y1959 TO -Y2462 IAW A330 SRM 53-41-14 FIGURE 103, AND, 51-42-11, 51-74-00.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,630 hrs · 7,271 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON AUXILIARY BEAM BETWEEN FR73 TO FR74, BETWEEN Y1959 TO Y2462. REPLACED AUXILIARY BEAM BETWEEN FR73 TO FR74, BETWEEN Y1959 TO Y2462 IAW A330 SRM 53-41-14 FIGURE 103, AND 51-44-11, 51-42-11.

Part: SLIDE — MALFUNCTIONED (R3 DOOR)

PHL - SLIDE OPS CHECK DUE ON DOOR R-3. MAINTENANCE ACCOMPLISHED R3 SLIDE DEPLOY WITH UNSATISFACTORY RESULTS. REMOVED AND REPLACED R-3 SLIDE PER J/C 33L20025001.

Part: COVER — MISSING (CABIN) · airframe 51,378 hrs · 7,237 cycles

CLT - LEFT EMERGENCY LIGHT MISSING COVER SIDEWALL. MAINTENANCE INSTALLED NEW COVER, OPS CHECK IS GOOD.

Part: SLIDE — FAILED (L1 DOOR) · airframe 51,153 hrs · 7,209 cycles

PHL - L1 DOOR SLIDE EMERGENCY LIGHTS FAILED TO ILLUMINATE DURING SLIDE DEPLOY TEST. REPLACED SLIDE ASSY.

Part: BATTERY — DISCHARGED (CABIN) · airframe 51,132 hrs · 7,205 cycles

LGW - EMERGENCY LIGHT AT CREW STATION AFT ENTRY DOOR LEFT, U/S. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERY.

Part: LENS — BROKEN (EXIT SIGN) · airframe 50,697 hrs · 7,150 cycles

PHL - EXIT SIGN 3L BROKEN. MAINTENANCE REMOVED AND REPLACED SIGN LENS.

Part: BOTTLE — LOW PRESSURE (L3 DOOR) · airframe 50,383 hrs · 7,111 cycles

PHL - AFTER CLOSING CABIN DOORS, BEFORE PUSHBACK, CIDS CAUTION "CHECK DOOR PRESSURE 3L". MAINTENANCE SERVICED 3L DOOR CIDS CAUTION WENT AWAY, OPS NORMAL, AMM 52-20-00.

Part: OVEN — FAULTY (GALLEY) · airframe 50,049 hrs · 7,067 cycles

FLIGHT 735, MAN - PHL - OVEN IN AFT GALLEY LEFT SIDE LOOKING AFT CREATED SO MUCH IT CAUSED PAPER ON CART BELOW TO DISCOLOR (WHITE TO YELLOW) AND ACTUALLY CATCH FIRE. PULL OVEN BREAKER AS A PRECAUTIONARY AND RELEASED ON MEL. PHL MAINTENANCE REMOVED AND REPLACED THE NR 1 OVEN PER AMM 25-35-19, OPERATIONAL TEST IS GOOD, REMOVED MEL.

Part: OVEN — MALFUNCTIONED (GALLEY) · airframe 50,019 hrs · 7,063 cycles

FLIGHT 719, FCO-PHL - FWD GALLEY OVEN NR 2 INOP. FLT ATTEND REPORTED ELECTRICAL ODOR 15 MINS AFTER TURNED ON. DISCONTINUED OFF. C/B PULLED PER CAPTAIN. MAINTENANCE RESET FWD GALLEY OVEN NR 2 , RAN FOR 30 MINUTES, NO CIRCUIT BREAKER TRIP OR ODOR. NO 30 DAY HISTORY, CHECKS OK.

Part: BOTTLE — LOW PRESSURE (L3 DOOR) · airframe 49,757 hrs · 7,031 cycles

FRA FLT 0704 CIDS PANEL "CHECK 3L DOOR PRESSURE". MAINTENANCE SERVICED 3L DOOR BOTTLE.

Part: COVER — OUT OF POSITION (COCKPIT) · airframe 49,596 hrs · 7,011 cycles

FRA - 2L OVERHEAD EXIT SIGN COVER FELL OFF, IT IS IN THE COCKPIT. MAINTENANCE SECURED OVERHEAD EXIT SIGN AT 2L. OK FOR SERVICE.

Part: BUTTON — OUT OF ADJUST (L2 DOOR) · airframe 49,468 hrs · 6,995 cycles

FRA - 2L DOOR PACK PUSH BUTTON FROZEN IN DOWN POSITION. MAINTENANCE ADJUSTED 2L DOOR OPEN LATCH BUTTON. OKAY FOR SERVICE.

Part: BOTTLE — LOW PRESSURE (L3 DOOR) · airframe 49,358 hrs · 6,980 cycles

LGW - DOOR 3 LEFT, DOOR ASSIST BOTTLE PRESSURE GAUGE IN YELLOW BAND. MAINTENANCE SERVICED DOOR 3 L ASSIST BOTTLE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 49,252 hrs · 6,966 cycles

MAN - EMERGENCY FLASHLIGHT AT DOOR 2L LOW BATTERY. MAINTENANCE REPLACED EMERGENCY FLASHLIGHT BATTERY.

Part: EPSU — INOPERATIVE (CABIN) · airframe 49,251 hrs · 6,966 cycles

PHL - R2 FAILS EPSU QUICKIE TEST (14WL) INTERIOR/EXTERIOR LIGHTS FAULT ON EPSU INDICATOR OVERLOAD OR SHORT CIRCUIT OF CONNECTED LOADS OR PROX SWITCHES. (LIGHTS FEEDING OFF THIS 14WL ARE DIMMER). MAINTENANCE REPLACED RIGHT MID GALLEY EMERG LIGHT ASSY EPSU SYS TEST OK.

Part: SIGN — OUT OF POSITION (CABIN) · airframe 49,144 hrs · 6,952 cycles

FRA - EXIT SIGN 3L CEILING FELL DOWN MAINTENANCE RE-INSTALLED EXIT SIGN.

Part: SIGN — UNSECURE (CABIN) · airframe 48,923 hrs · 6,923 cycles

EXIT SIGN AT 4L DOOR FELL DOWN FROM CEILING. RE-INSTALLED EXIT SIGN CHECK 4L DOOR.

Part: O-RING — CRUSHED (NR 1 ENGINE)

BOS FLT 721 FCO TO CLT. THE NUMBER ONE ENGINE BEGAN TO HAVE LOSS OF OIL. THE CREW VERIFIED THAT IT WAS NOT AN INDICATION PROBLEM. THE FLIGHT DIVERTED INTO BOS WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE NUMBER ONE ENGINE OIL FILTER HOUSING RUNNING OIL LEAK DUE TO A CRUSHED O-RING. REMOVED AND REPLACED THE NUMBER ONE ENGINE OIL FILTER AND O-RING, AND REPLENISHED OIL AS REQUIRED. LEAK CHECKED GOOD.

Part: EPSU — FAILED (CABIN)

PHL - EPSU 14 WL UNIT FAULT. REMOVED AND REPLACED EPSU.

Part: FITTING — OUT OF ADJUST (GIRT BAR)

PHL - THE R1 DOOR SLIDE WILL NOT DISARM. THE LEVER ONLY MOVES HALF WAY. MAINTENANCE ADJUSTED THE R1 DOOR AFT GIRT BAR FITTING.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,066 hrs · 6,811 cycles

CWF - C2 - CORROSION ON SEAT TRACK AT FR16A, -Y1959. REPLACED SEAT TRACK AT FR16A, -Y1959 IAW A330 SRM 53-11-14.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,066 hrs · 6,811 cycles

CWF - C2 - CORROSION ON SEAT TRACK AT FR58, -Y450. REPAIRED SEAT TRACK AT FR58, -Y450 IAW A330 SRM 53-00-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,066 hrs · 6,811 cycles

CWF - C2 - CORROSION ON SEAT TRACK BETWEEN FR14 TO FR18, -Y953. REPLACED SEAT TRACK BETWEEN FR14 TO FR18, -Y953 IAW A330 SRM 53-11-14.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,066 hrs · 6,811 cycles

CWF - C2 - CORROSION ON SEAT TRACK AT FR18, Y450. REPAIRED SEAT TRACK AT FR18, Y450 IAW A330 SRM 53-00-15.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 48,066 hrs · 6,811 cycles

CWF - C2 - CRACKED FLOOR STRUCTURE VERTICAL ANGLE AT FR7, -Z100, -Y790. REPLACED FLOOR STRUCTURE VERTICAL ANGLE AT FR7, -Z100, -Y790 IAW EA 140304.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,066 hrs · 6,811 cycles

CWF - C2 - CORROSION ON SEAT TRACK AT FR53.9 + 15 INCHES, -Y1959. REPAIRED SEAT TRACK AT FR53.9 + 15 INCHES, -Y1959 IAW A330 SRM 53-31-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,066 hrs · 6,811 cycles

CWF - C2 - CORROSION ON SEAT TRACK AT FR48 + 17 INCHES, Y450. REPAIRED SEAT TRACK AT FR48 + 17 INCHES, Y450 IAW A330 SRM 51-72-11 AIRBUS DRAWING F53311325.

Part: FASTENER — LOOSE (CENTER WING) · airframe 48,066 hrs · 6,811 cycles

CWF - TRACES OF FUEL HAVE BEEN FOUND IN THE CENTER WING DRY BAY OF A330-300 AIRCRAFT AT RIB 1. AS A RESULT OF THIS AN INSPECTION WAS PERFORMED ON THIS AIRCRAFT & FASTENERS WERE FOUND LOOSE & LEAKING AT FR42 LEFT & RIGHT SIDE AT RIB 1. BOLTS WERE REPLACED & AREA WAS SEALED IAW EA 102839B & 102875A.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 48,066 hrs · 6,811 cycles

CWF - C2 - CRACKED FLOOR STRUCTURE VERTICAL ANGLE AT FR7, -Z100, Y790. REPLACED FLOOR STRUCTURE VERTICAL ANGLE AT FR7, -Z100, Y790 IAW EA 140304.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,066 hrs · 6,811 cycles

CWF - C2 - CORROSION ON SEAT TRACK BETWEEN FR72 TO FR74 + 7 INCHES, Y450. REPAIRED SEAT TRACK BETWEEN FR72 TO FR74 + 7 INCHES, Y450 IAW A330 SRM 53-00-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,066 hrs · 6,811 cycles

CWF - C2 - CORROSION ON SEAT TRACK BETWEEN FR62 TO FR67, -Y1959. REPAIRED SEAT TRACK BETWEEN FR62 TO FR67, -Y1959 IAW A330 SRM 53-00-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,066 hrs · 6,811 cycles

CWF - C2 - CORROSION ON SEAT TRACK BETWEEN FR15 TO FR19 + 17 INCHES, Y450. REPAIRED SEAT TRACK BETWEEN FR15 TO FR19 + 17 INCHES, Y450 IAW A330 SRM 53-11-15.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 48,066 hrs · 6,811 cycles

CWF - C2 - CRACKED FLOOR SUPPORT ATTACH BRACKET AT FR80, -Y1447. REPLACED FLOOR SUPPORT ATTACH BRACKET AT FR80, -Y1447 IAW A330 SRM 51-72-11.

Part: BEAM — CORRODED (FUSELAGE) · airframe 48,066 hrs · 6,811 cycles

CWF - C2 - CORROSION ON LONGERON BEAM BETWEEN FR74 TO FR77, Y1447. REPLACED LONGERON BEAM BETWEEN FR74 TO FR77, Y1447 IAW A330 SRM 51-72-11.

Part: BEAM — CORRODED (FUSELAGE) · airframe 48,066 hrs · 6,811 cycles

CWF - C2 - CORROSION ON LONGERON BEAM BETWEEN FR75 TO FR80, -Y450. REPLACED LONGERON BEAM BETWEEN FR75 TO FR80, -Y450 IAW A330 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,066 hrs · 6,811 cycles

CWF - C2 - CORROSION ON SEAT TRACK BETWEEN FR18 TO FR19 + 4 INCHES, -Y450. REPAIRED SEAT TRACK BETWEEN FR18 TO FR19 + 4 INCHES, -Y450 IAW A330 SRM 53-11-15.

Part: BEAM — CORRODED (FUSELAGE) · airframe 48,066 hrs · 6,811 cycles

CWF - C2 - CORROSION ON LONGERON BEAM AT FR76 + 12 INCHES, Y380. REPLACED LONGERON BEAM AT FR76 + 12 INCHES, Y380 IAW A330 SRM 51-42-11.

Part: BEAM — CORRODED (FUSELAGE) · airframe 48,066 hrs · 6,811 cycles

CWF - C2 - CORROSION ON LONGERON BEAM BETWEEN FR75 TO FR80, Y450. REPLACED LONGERON BEAM BETWEEN FR75 TO FR80, Y450 IAW A330 SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 48,066 hrs · 6,811 cycles

CWF - C2 - CORROSION ON FLOOR SUPPORT PROFILE AT FR80 + 6 INCHES, Y380. REPLACED FLOOR SUPPORT PROFILE AT FR80 + 6 INCHES, Y380 IAW A330 SRM 51-72-11.

Part: BEAM — CORRODED (FUSELAGE) · airframe 48,066 hrs · 6,811 cycles

CWF - C2 - CORROSION ON LONGERON BEAM BETWEEN FR72 TO FR76, Y=0. REPLACED LONGERON BEAM BETWEEN FR72 TO FR76, Y=0 IAW A330 SRM 51-42-11.

Part: BEAM — CORRODED (FUSELAGE) · airframe 48,066 hrs · 6,811 cycles

CWF - C2 - CORROSION ON LONGERON BEAM BETWEEN FR74 TO FR80, Y1137. REPLACED LONGERON BEAM BETWEEN FR74 TO FR80, Y1137 IAW A330 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,066 hrs · 6,811 cycles

CWF - C2 - CORROSION ON SEAT TRACK BETWEEN FR65 TO FR68, Y450. REPAIRED SEAT TRACK BETWEEN FR65 TO FR68, Y450 IAW A330 SRM 53-00-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,066 hrs · 6,811 cycles

CWF - C2 - CORROSION ON SEAT TRACK BETWEEN FR40 TO FR47, Y450. REPLACED SEAT TRACK BETWEEN FR40 TO FR47, Y450 IAW A330 SRM 51-42-11.

Part: BEAM — CORRODED (FUSELAGE) · airframe 48,066 hrs · 6,811 cycles

CWF - C2 - CORROSION ON LONGERON BEAM BETWEEN FR75 TO FR76, -Y380. REPLACED LONGERON BEAM BETWEEN FR75 TO FR76, -Y380 IAW A330 SRM 51-42-11.

Part: BEAM — CORRODED (FUSELAGE) · airframe 48,066 hrs · 6,811 cycles

CWF - C2 - CORROSION ON LONGERON BEAM BETWEEN FR74 TO FR74 + 5 INCHES, -Y1137.1. REPLACED LONGERON BEAM BETWEEN FR74 TO FR74 + 5 INCHES, -Y1137.1 IAW A330 SRM 51-72-11.

Part: BEAM — CORRODED (FUSELAGE) · airframe 48,066 hrs · 6,811 cycles

CWF - C2 - CORROSION ON AUXILLARY BEAM AT FR75 + 17 INCHES & BETWEEN -Y1959 TO -Y2462. REPLACED AUXILLARY BEAM AT FR75 + 17 INCHES & BETWEEN -Y1959 TO -Y2462 IAW A330 SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 48,066 hrs · 6,811 cycles

CWF - C2 - CORROSION ON FLOOR SUPPORT Z-PROFILE AT FR78, -Y1726. REPLACED FLOOR SUPPORT Z-PROFILE AT FR78, -Y1726 IAW A330 SRM 51-72-11.

Part: FITTING — CRACKED (FUSELAGE) · airframe 48,066 hrs · 6,811 cycles

CWF - C2 - CRACKED FLOOR SUPPORT ATTACH BRACKET FITTING AT FR80, Y1500. REPLACED FLOOR SUPPORT ATTACH BRACKET FITTING AT FR80, Y1500 IAW A330 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,066 hrs · 6,811 cycles

CWF - C2 - CORROSION ON SEAT TRACK AT FR58 + 6 INCHES, Y450. REPLACED SEAT TRACK AT FR58 + 6 INCHES, Y450 IAW A330 SRM 53-42-11.

Part: BEAM — CORRODED (FUSELAGE) · airframe 48,066 hrs · 6,811 cycles

CWF - C2 - CORROSION ON LONGERON BEAM AT FR78 + 1 INCHES, Y=0. REPLACED LONGERON BEAM AT FR78 + 1 INCHES, Y=0 IAW A330 SRM 51-72-11.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 48,066 hrs · 6,811 cycles

CWF - C2 - CRACKED FLOOR SUPPORT PROFILE AT FR79 + 11 INCHES, S26L, Y1548. REPLACED FLOOR SUPPORT PROFILE AT FR79 + 11 INCHES, S26L, Y1548 IAW A330 SRM 51-72-11.

Part: DIAPHRAGM — DAMAGED (ASSIST BOTTLE) · airframe 48,066 hrs · 6,811 cycles

CWF - C2 - DOOR R4 ASSIST BOTTLE PRESSURE READS ZERO UPON INSPECTION. REPLACED DIAPHRAGM IAW A330 AMM 52-10-00-860-8030 & SERVICED IAW A330 AMM 52-10-00-600-802.

Part: BOTTLE — LOW PRESSURE (R4 DOOR)

MAN - THE R4 DOOR HAD A PRESSURE MESSAGE ON THE FAP. THE DOOR ASSIST BOTTLE PRESSURE GAUGE READ AT THE YELLOW BAND ARROW. MAINTENANCE RE-CHARGED THE R4 DOOR ASSIST BOTTLE PRESSURE TO THE CORRECT PRESSURE.

Part: ACTUATOR — LOW PRESSURE (L3 DOOR)

LHR - CHECK DOOR PRESSURE L3 WARNING LIGHT (WAS ILLUMINATED). THE L3 DOOR ASSIST ACTUATOR WAS SERVICED.

Part: BOTTLE — LOW PRESSURE (L3 DOOR)

PHL - FLT 700 EN-ROUTE PHL TO FRA. AFTER PUSH BACK FROM THE GATE, CREW REPORTS "L3 DOOR ASSIST BOTTLE LOW PRESSURE" MESSAGE ON CIDS PANEL. THE FLIGHT RETURNED TO THE GATE. MAINTENANCE "SERVICED L3 DOOR ASSIST BOTTLE".

Part: BOTTLE — LOW PRESSURE (R4 DOOR)

MAN - DOOR R4 DOOR ASSIST PRESSURE SHOWING LOW ON SERVICING REPORT AND GAUGE. THE DOOR ASSIST BOTTLE PRESSURE WAS ADJUSTED.

Part: BOTTLE — LOW PRESSURE (R4 DOOR)

PHL - THE DOOR R4 BOTTLE/DOOR ASSIST PRESSURE IS LOW. SERVICED R4 DOOR ASSIST/BOTTLE.

Part: DAMPER — LOW PRESSURE (L3 DOOR)

FCO - SERVICING REPORT SHOWS "L3 DOOR BOTTLE LOW PRESSURE". DOOR L3 CYLINDER DOOR DAMPER SERVICED.

Part: DAMPER — LOW PRESSURE (L3 DOOR)

MAD - DOOR L3 DAMPER REQUIRES SERVICING DUE TO LOW PRESSURE. DOOR L3 DAMPER WAS SERVICED.

Part: CYLINDER — LOW PRESSURE (L3 DOOR ASSIST)

PHL - L3 DOOR LOW PRESSURE PER SERVICE REPORT. SERVICED L3 DOOR CYLINDER.

Part: CYLINDER — LOW PRESSURE (L3 DOOR)

CDG - ON SERVICING REPORT - DOOR 3L OPENING ASSIST LO PRESSURE (ALSO DISPLAYED ON FAP). PX INDICATOR FOUND IN YELLOW ZONE OF GAUGE. DOOR OPENING ASSIST CYLINDER SERVICED.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT)

MAD - FOUND FIRST OFFICER'S FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FIRST OFFICER'S FLASHLIGHT.

Part: EPSU — INOPERATIVE (EMERGENCY LIGHTS)

THE EXIT SIGNS ABOVE R2 DOOR WERE INOPERATIVE. MX REPLACED EPSU FIN 14 WL. OPERATIONALLY CHECKS, OK. (K)

Part: DAMPER — LOW PRESSURE (R4 DOOR)

PHL - FLIGHT ATTENDANT PANEL SHOWS SLIDE LOW PRESS (4R). ACTUAL SLIDE GAUGE READ IN GREEN. COCKPIT INDICATION SHOWS ARMED AND NORMAL. SERVICED R4 DOOR ASSIST DAMPER.

Part: BOTTLE — LOW PRESSURE (L3 DOOR)

MAN - THE DOOR L3 DOOR ASSIST BOTTLE PRESSURE WAS LOW. BOTTLE PRESSURE ADJUSTED.

Part: CYLINDER — LOW PRESSURE (R4 DOOR)

CLT - THE R4 DOOR ASSIST WAS LOW. SERVICED THE R4 DOOR ASSIST.

Part: BOTTLE — LOW PRESSURE (L3 DOOR)

MAN - THE DOOR L3 DOOR ASSIST BOTTLE HAD LOW PRESSURE. DOOR ASSIST BOTTLE PRESSURE RECHARGED.

Part: BOTTLE — LOW PRESSURE (R4 DOOR)

PHL - THE 4R DOOR BOTTLE HAD LOW PRESSURE. MAINTENANCE SERVICED 4R DOOR BOTTLE.

Part: FLASHLIGHT — INOPERATIVE (CABIN)

MAD - THE FLASHLIGHT AT THE L2 DOOR WAS INOPERATIVE. THE FLASHLIGHT WAS REPLACED.

Part: BOTTLE — LOW PRESSURE (R2 DOOR)

PHL - THE BOTTLE PRESSURE FOR SLIDE ON R2 DOOR IS IN YELLOW RANGE. SERVICED THE R2 DOOR BOTTLE.

Part: BOTTLE — LOW PRESSURE (R2 DOOR)

PHL - THE R2 ENTRY DOOR ASSIST BOTTLE HAD LOW PRESSURE. THE BOTTLE WAS SERVICED TO FULL AND LEAK CHECKED OK.

Part: DIAPHRAGM — LEAKING (R2 DOOR)

CLT - FLT 731 FRA TO CLT. CHECK DOOR PRESSURE ON DOOR R2 ON APPROACH IN CIDS PANEL. REMOVED AND REPLACED DIAPHRAM IN PERCUSSION MECHANISM. SERVICED DOOR BOTTLE.

Part: MOUNT — CORRODED (NR 1 ENGINE) · airframe 38,471 hrs · 5,544 cycles

PHL - ENGINE CHANGE - MAJOR REPAIR - NR 1 ENGINE FWD MOUNT MATING SURFACE SHOWING EVIDENCE OF CAD PLATING MISSING AND CORROSION. REPAIRED NR 1 ENGINE FWD MOUNT IAW US AIRWAYS EA 112487.

Part: MOUNT — CORRODED (NR 1 ENGINE) · airframe 38,471 hrs · 5,544 cycles

PHL - ENGINE CHANGE - MAJOR REPAIR - NR 1 ENGINE AFT MOUNT AFT MOUNT SHOWING SIGNS OF SURFACE CORROSION. REPAIRED NR 1 ENGINE AFT MOUNT IAW US AIRWAYS EA 112487.

Part: BOTTLE — LOW PRESSURE (L3 DOOR)

MAN - CHECK DOOR PRESSURE ON DOOR L3. MAINTENANCE TOPPED OFF DOOR L3 BOTTLE PRESSURE.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 37,482 hrs · 5,402 cycles

BFM - C2 - EEL - NR 6056406 - EMERGENCY EXIT LIGHTING WIRE HARNESS AT SEAT 16HG DAMAGED. REPLACED EMERGENCY EXIT LIGHTING WIRE HARNESS AT SEAT 16HG IAW A320 AMM 33-51-12.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,482 hrs · 5,402 cycles

BFM - C2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR70 TO FR71, -Y2462. REPAIRED SEAT TRACK BETWEEN FR70 TO FR71, -Y2462 IAW A330 SRM 51-42-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,482 hrs · 5,402 cycles

BFM - C2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR58 TO FR68, -Y450. REPAIRED SEAT TRACK BETWEEN FR58 TO FR68, -Y450 IAW A330 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,482 hrs · 5,402 cycles

BFM - C2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR53.9 TO FR55, -Y450. REPAIRED SEAT TRACK BETWEEN FR53.9 TO FR55, -Y450 IAW A330 SRM 53-31-15.

Part: EPSU — FAULTED (CABIN)

PHL - THERE WAS AN EPSU FAULT FOR THE R3 DOOR. MAINTENANCE REPLACED THE R3 DOOR EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK.

Part: ADIRU — INOPERATIVE (NR 1)

LGW FLT 705 FRA TO CLT - THE FLIGHT RECEIVED ECAM MESSAGES "ADR 1 FAULT" AND "IR 1 FAULT" PRIOR TO ENTERING THE ETOPS SEGMENT OF FLIGHT. THE FLIGHT COULD NOT CONTINUE ETOPS, PER PROCEDURES, WITHOUT IR 1. THE FLIGHT DIVERTED TO LGW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE IN LGW SWAPPED THE NR 1 AND NR 2 ADIRUS, AND DEFERRED THE NR 2 ADIRU ON MEL. MAINTENANCE IN CLT REPLACED THE NR 2 ADIRU. OPERATIONALLY CHECKS OK. (S)

Part: ATTACH FITTING — INOPERATIVE (L3 DOOR)

CWF - MAINTENANCE FOUND THE FORWARD HEATER, FIN 15DH, FOR THE L3 DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE 15DH FORWARD HEATER GIRT BAR ATTACH FITTING PER MM 30-46-00. OPERATIONAL CHECK GOOD.

Part: ATTACH FITTING — DEFECTIVE (EVAC SLIDE)

CWF - FOUND AFT HEATER, FIN 4DH, INOPERATIVE. MAINTENANCE REPLACED 4DH AFT HEATED SLIDE ATTACHMENT FITTINGS. OPERATIONALLY CHECKS OK.

Part: ATTACH FITTING — INOPERATIVE (EVAC SLIDE)

CWF - THE FORWARD, MAIN ENTRY DOOR EMERGENCY ESCAPE SLIDE ATTACH FITTING ICE PROTECTION WAS FOUND INOPERATIVE. MAINTENANCE REPLACED HEATED ATTACH FITTING. OPS CHECKED OK.

Part: TIRE — LEAKING (MLG) · airframe 31,098 hrs · 4,540 cycles

FLIGHT 718, PHL-FCO: DURING FLIGHT, CREW NOTICED THE LEFT NOSE TIRE PRESSURE SLOWLY DROPPING. FLIGHT DIVERTED TO BOS. MAINTENANCE REPLACED BOTH NOSE TIRES.

Part: DUCT — OBSTRUCTED (CABIN AIR) · airframe 30,833 hrs · 4,501 cycles

FLIGHT 705, FRA-CLT: CREW REPORTED A STRONG ELECTRICAL BURNING ODOR IN THE AFT GALLEY AREA. FLIGHT DIVERTED TO SNN. MAINTENANCE REMOVED AN AFT GALLEY CEILING PANEL AND FOUND A CLOTH LODGED IN A VENTILATION DUCT. REMOVED THE CLOTH, RE-ASSEMBLED THE DUCT AND CEILING PANEL, AND RAN AFT GALLEY SYSTEMS AND AIR DISTRIBUTION SYSTEMS. NO SMOKE OR ODORS NOTED. A/C WAS RELEASED FOR SERVICE WITH NO FURTHER DIFFICULTIES.

Part: POWER SUPPLY — FAULTED (EMERGENCY LIGHTS) · airframe 30,780 hrs · 4,494 cycles

MAINTENANCE FOUND THE STANDBY POWER SUPPLY UNIT FAULTED. REPLACED POWER SUPPLY UNIT. NO FURTHER FAULTS.

Part: BATTERY — DISCHARGED (CABIN) · airframe 27,710 hrs · 4,045 cycles

DURING EMERGENCY LIGHTS TEST, MAINTENANCE FOUND A FAULT INDICATED ON EPSU AT POSITION 4L. REPLACED EPSU BATTERY, NO FURTHER FAULTS.