N76151

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 48,868 hrs · 7,182 cycles

DOOR 2R SLIDE PACK FELL DOWN WHEN DOOR WAS OPENED. FOUND SLIDE IN DISARM POSITION. DOOR 2R SLIDE PACK INSTALLED IAW AMM 25-66-01. INSTALLATION NEED RII INSPECTION. DEFERRED IAW MEL WITH DOOR 2R INOPERATIVE. MAINTENANCE PROCEDURE APPLIED. REMOVED, INSP, RE-INSTALLED R2 DOOR SLIDE PACK AS PER 25-6601-4 04-036, FOLLOWING CHECKS WERE DOWN, SLIDE CYCLINDER AMM25-66-02, GIRT BAR AMM25-66-05, ESCAPE SYSTEM 25-66-01-601, ALSO SAFETY PIN REMOVED AND STOWED BACK INTO POUCH ON SLIDE, ALL CHECK GOOD, REMOVED PLA.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 45,941 hrs · 6,798 cycles

CABIN BS 346-348 RIGHT O/B SEAT TRACK CORRODED. CABIN BS 343 TO BS 423 RT MOST O/B SEAT TRACK REPLACED AS PER SRM 51-10-02 AND FASTENER INSTALLED AS PER SRM 51-40-02 ATT MAINTENANCE WORK SHEET FORM 44.0008 ITEM 1 TO ITEM 12 ACCOMPLISHED.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 45,941 hrs · 6,798 cycles

MULT-33-3-0001 DOOR 1 LT EMERGENCY EXIT LIGHT FOUND INOP. DOOR 1 LT EMERGENCY EXIT SIGN LAMP REPLACED AND OPERATIONAL CHECK NORMAL AS PER AMM 33-51-09.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 45,941 hrs · 6,798 cycles

BULK CARGO COMPT STA 1439 BELOW FLOOR FLOORBEAM WEB FOUND DEFORM AND CRACK BETWEEN LBL 5 TO RBL 5. BULK CARGO COMPT STA 1439 BELOW FLOOR FLOORBEAM FRAME WEB REPAIRED AS PER ECRA5310-05346 REV- AND OPEN HOLE INSP, TRIMMED AREA NIL CRACK FOUND ATT MAINTENANCE WORK SHEET FORM 44.0008 ITEM 1 TO 16 ACCOMPLISHED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 45,941 hrs · 6,798 cycles

MULT-33-3-001, LHS DOOR 3 OUTSIDE EMERGENCY LIGHT INOP LEFT DOOR 3 OUTSIDE EMER LIGHT BULB REPLACED AND TEST NORMAL AS PER AMM 33-51-03.

Part: TRANSMITTER — FAILED (TE FLAP) · airframe 45,562 hrs · 6,753 cycles

T/E FLAP ASYM CAUTIONARY EICAS LIGHT ILLUMINATED AFTER TO AS FLAPS WERE RETRACTED FROM 5 INCHES TO 1 INCH FLAPS REMAINED STUCK AT 5 INCHES' ORH PROCEDURE ACCOMPLISHED OTHER BRAKES 6 OR BELOW REMOVED AND REPLACED NR 5 FLAP POSITION TRANSMITTER PER AMM 27-51-45 PERFORMED ADJUSTMENT TEST 4 & 5 TRANS. ADJUSTED BOTH TO TOLERANCES PER MM 27-51-45 OPS CHECKS GOOD ON GROUND NO ASYMMETRY OCCURRED DURING OPS CHECK RATABLE PARTS CHANGE WAS INDICATED - TAT # 0982104 S/N OFF 01283 TRANSMITTER, FL OFF 62-2751-9-0008 1283 ON 62-2751-9-0008 1144.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 44,892 hrs · 6,660 cycles

ON APPROACH T/E FLAP ASYM LIGHT ILLUMINATED WITH FLAPS AT 5 DEGR ESS COMPLETED QRH AND LANDED UNEVENTFULLY REF FIX 27-51-00LTE134 AND 27-52-45 PLE 216-220 PERFORM ALL TEST AND ALL VALUES ARE IN LIMITS. ALSO CHECK LEFT AND RIGHT XMISSION NO POPPER TABS FOUND OK TO CONT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,898 hrs · 6,388 cycles

SUPPORT TASK CABIN - AFTER E/E COMPT REMOVAL, RT STA 303 RBL 40-60 FLOORBEAM UPPER SURFACE FOUND CORROSION. CABIN FLOORBEAM UPPER TEE AT STA 303 LBL 40 - LBL 60 REPAIRED AS PER SRM 53-00-51 FIG 201 REPAIR 1 FORM 44.0008 ITEMS 1 TO 25 ACCOMPLISHED.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 36,616 hrs · 5,547 cycles

OVERHEAD EMERGENCY EXIT LIGHT IN COCKPIT INOPERATIVE. REPLACED OVERHEAD EMERGENCY EXIT LIGHT ASSEMBLY, OPERATIONAL CHECKS NORMAL.

Part: FLOORBEAM — CORRODED (BS 303) · airframe 33,443 hrs · 5,153 cycles

CABIN FLOOR SUPPORT FOUND CORRODED AT BS 303 BETWEEN LBL 21 - 54, AFTER FLOOR PNL REMOVED. CABIN STA 303 BETWEEN LBL 17"- 68" FLOORBEAM REPAIRED AS PER SRM 53-00-51 FIG 201 REPAIR 1 AND HFEC NO CRACK FOUND.

Part: STIFFENER — CRACKED (NR 1 PYLON) · airframe 23,051 hrs · 3,657 cycles

INSPECTION FOUND A 1.5 INCH CRACK IN NR 1 PYLON O/B FRAME CHORD ATTACH SUPPORT -T- (STIFFENER) DURING FRAME CHORD REMOVAL AT NAC STA 285.45 TO NAC STA 295. THE STIFFENER WAS REPLACED IAW ECRA 5420-01444.

Part: CLIP — CRACKED (NR 1 PYLON) · airframe 23,051 hrs · 3,657 cycles

INSPECTION FOUND A 1.5 INCH CRACK IN NR 1 PYLON LT NACELLE STRUT FRAME CLIP AT NAC STA 285.45. THE FRAME CLIP WAS REPLACED IAW ECRA 5420-01444.

Part: FRAME — CRACKED (NR 2 PYLON) · airframe 23,051 hrs · 3,657 cycles

INSPECTION FOUND A 2 INCH CRACK IN NR 2 PYLON NACELLE STRUT FRAME CHORD AT NAC STA 285.45, I/B AREA. THE FRAME CHORD WAS REPLACED IAW ECRA 5420-01444.

Part: STIFFENER — CRACKED (BS 285.45-295) · airframe 23,051 hrs · 3,657 cycles

INSPECTION FOUND A 2 INCH CRACK IN NR 2 PYLON I/B FRAME CHORD ATTACH SUPPORT -T- (SUPPORT STIFFENER) DURING FRAME CHORD REMOVAL AT NAC STA 285.45 TO NAC STA 295. THE SUPPORT STIFFENER WAS REPLACED IAW ECRA 5420-01444.

Part: FRAME — CRACKED (NR 1 PYLON) · airframe 23,051 hrs · 3,657 cycles

INSPECTION FOUND A .5 INCH CRACK IN NR 1 PYLON O/B FRAME CHORD DURING ATTACH CLIP REMOVAL AT UPPER CLIP ADJACENT AREA, NAC STA 285.45. THE FRAME CHORD WAS REPLACED IAW ECRA 5420-01444.

Part: STIFFENER — CRACKED (STA 285.45 - 295) · airframe 23,051 hrs · 3,657 cycles

INSPECTION FOUND A 4.5 INCH CRACK IN NR 1 PYLON I/B FRAME CHORD ATTACH SUPPORT -T- (STIFFENER) AT NAC STA 285.45 TO NAC STA 295. THE SUPPORT STIFFENER WAS REPLACED IAW ECRA 5420-01444.

Part: FLOORBEAM — CORRODED (BS 325) · airframe 22,699 hrs · 3,603 cycles

INSPECTION FOUND CABIN FLOORBEAM CORRODED AT BS 325, LBL 55. THE CORRODED SECTION OF FLOORBEAM WAS REPLACED IAW SRM 53-00-51 FIGURE 201, REPAIR 2.

Part: FLOORBEAM — CORRODED (BS 303) · airframe 22,699 hrs · 3,603 cycles

INSPECTION FOUND THE FLOORBEAM CORRODED AT BS 303, LBL 27 TO LBL 31. THE CORRODED SECTION OF FLOORBEAM WAS REPLACED IAW SRM 53-00-51, FIGURE 201, REPAIR 2.

Part: COFFEEMAKER — INOPERATIVE (GALLEY) · airframe 22,273 hrs · 3,450 cycles

THE FORWARD ESPRESSO COFFEEMAKER BEGAN TO SMOKE AND GAVE OFF A BURNED ELECTRICAL ODOR WHILE EN ROUTE FROM EWR TO FCO. THE CIRCUIT BREAKER WAS PULLED AND THE SMOKE CEASED. THE FLIGHT WAS CONTINUED TO FCO WHERE IT LANDED WITHOUT FURTHER INCIDENT. THE ESPRESSO COFFEEMAKER 209 IN THE FIRST CLASS GALLEY WAS REMOVED AND REPLACED. THE AREA WAS INSPECTED FOR BURNED WIRING AND NONE WAS FOUND. OPERATIONAL CHECKS WERE GOOD.

Part: ENTERTAIN SYS — MALFUNCTIONED (CABIN) · airframe 17,595 hrs · 2,864 cycles

STRONG FUMES WITH A BURNING WIRE-LIKE ODOR WERE NOTED IN THE FIRST CLASS CABIN (FORWARD IN AREA OF ENTERTAINMENT SECTION) AFTER APPROXIMATELY 3 HOURS OF FLIGHT WHILE EN ROUTE TO EWR. THE ENTERTAINMENT SYSTEMS WERE SECURED AND THE ODOR CLEARED. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE NOTED THAT THE NR 1 EADB (ENHANCED AREA DISTRIBUTION BOX) SMELLED BURNT. THE NR 1 EADB WAS REMOVED AND REPLACED. THE IFE FILTER WAS CHECKED AND IT WAS NOT CLOGGED. OPERATIONAL CHECKS WERE GOOD. THE IFE SYSTEM WAS RUN FOR 30 MINUTES AND OPERATION CHECKED GOOD.

Part: ACTUATOR — INOPERATIVE (SLIDE) · airframe 10,116 hrs · 1,688 cycles

THE FORWARD AND AFT DOOR ACTUATORS FOR THE RT SIDE OFF-WING SLIDE DOOR WERE FOUND EXPENDED. THE DOOR ACTUATORS WERE REMOVED AND REPLACED IAW MM 25-65-10.