N14383

Part: ANGLE — CORRODED (FUSELAGE) · airframe 18,521 hrs · 9,853 cycles

INSPECTION FOUND AFT FLOOR ATTACH ANGLE IN FORWARD CARGO AREA CORRODED AT STA 500D ABOVE S26L-S26R. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-02.

Part: PANEL — CORRODED (FUSELAGE) · airframe 18,521 hrs · 9,853 cycles

INSPECTION FOUND AFT CARGO PIT RT TRANSITION PANEL CORRODED AT STA 727 - 767 AND LT TRANSITION PANEL CORRODED AT STA 727 - 847. THE RT TRANSITION PANEL WAS REMOVED AND REPLACED IAW SRM 51-10-02. THE CORRODED SECTION OF LT TRANSITION PANEL WAS REMOVED AND REPLACED IAW SRM 53-60-53.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 18,521 hrs · 9,853 cycles

INSPECTION FOUND A .5 INCH CRACK IN ANGLE AT STA 380, L26L. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Part: ANGLE — GOUGED (FUSELAGE) · airframe 18,521 hrs · 9,853 cycles

INSPECTION FOUND RT SIDE VERTICAL STABILIZER TO FUSELAGE ANGLE GOUGED AT STA 1088 - 1156. THE LT ANGLE AT STA 1121 - 1138 WAS ALSO GOUGED. THE GOUGED SECTIONS WERE REMOVED AND REPLACED IAW ECRA 5380-01013.

Part: SKIN — DENTED (FUSELAGE) · airframe 18,521 hrs · 9,853 cycles

INSPECTION FOUND FUSELAGE SKIN DENTED AFT OF L-1 DOOR AT STA 380. THE DENTED AREA WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE 208.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 18,521 hrs · 9,853 cycles

INSPECTION FOUND A .5 INCH CRACK IN FLOOR SUPPORT AT STA 540, LBL 1. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 18,521 hrs · 9,853 cycles

INSPECTION FOUND A .5 INCH CRACK IN FLOOR SUPPORT AT STA 540, RBL 1. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Part: VALVE — WORN (SPOILER) · airframe 17,743 hrs · 9,461 cycles

THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM EWR. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND GROUND SPOILER INTERLOCK VALVE YOKE WORN. THE INTERLOCK VALVE WAS REMOVED AND REPLACED IAW MM 27-62-61, PAGE 403. IN ADDITION, THE LANDING GEAR SAFETY SENSORS WERE ADJUSTED AND TESTED IAW MM 32-09-01. THE GEAR WAS CYCLED SEVERAL TIMES AND OPERATIONAL CHECKS WERE GOOD.

Part: ROLLER — OBSTRUCTED (PAX DOOR) · airframe 16,292 hrs · 8,689 cycles

FORWARD ENTRY DOOR DIFFICULT TO CLOSE. INSPECTED DOOR AND FOUND LOWER ROLLER HITTING CAM PLATE. ADJUSTED UPPER GUIDE ARM PER MM 52-11-00.

Part: COFFEEMAKER — SHORTED (GALLEY)

SMOKE WAS REPORTED IN THE VICINITY OF THE AFT GALLEY COFFEEMAKER WHILE EN ROUTE TO IAH. THE FLIGHT ATTENDANT DISCHARGED THE HALON FIRE EXTINGUISHER ONTO THE AREA, THE GALLEY POWER WAS TURNED OFF, AND THE SMOKE CEASED. THE FLIGHT WAS CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AFT GALLEY COFFEEMAKER IN THE NR 1 POSITION AT FAULT. THE COFFEEMAKER WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD. NO OTHER DAMAGE WAS NOTED.

Part: ACM — LEAKING (RT PACK)

A SOUR/MUSTY ODOR WAS OBSERVED IN THE CABIN DURING DESCENT AT 6,000 FEET. THE ODOR STOPPED AFTER LANDING. MAINTENANCE FOUND THE RT ACM LEAKING. THE RT ACM WAS REMOVED AND REPLACED IAW MM 21-51-1,. OPERATIONAL CHECKS WERE GOOD WITH NO LEAKS NOTED.