N13066

Part: SKIN — DELAMINATED (NR 2 ENG COWL) · airframe 92,204 hrs · 14,622 cycles

INSPECTION FOUND INTERNAL SURFACE OF NR 2 ENGINE LT TRANSLATING COWL DELAMINATED. THE LT TRANSLATING COWL WAS REMOVED AND REPLACED IAW MM 78-32-17.

Part: BRACKET — CRACKED (TE FLAP) · airframe 92,204 hrs · 14,622 cycles

INSPECTION FOUND A .5 INCH CRACK IN LT WING O/B FLAP INTERNAL AFT ANGULAR BRACKET. THE BRACKET WAS REPLACED IAW SRM 51-31-01.

Part: STRUCTURE — CRACKED (LT MLG DOOR) · airframe 92,204 hrs · 14,622 cycles

INSPECTION FOUND A 1 INCH CRACK AT CORNER OF LT MLG DOOR. THE DOOR CORNER WAS REPAIRED IAW SRM 51-31-01.

Part: SKIN — CORRODED (RT AILERON)

INSPECTION FOUND RT WING OUTBOARD AILERON LOWER SKIN INTERNALLY CORRODED. THE AILERON SKIN WAS REPLACED IAW SRM 51-31-01 AND 51-33-01.

Part: SKIN — CRACKED (WS 402)

INSPECTION FOUND A 1 INCH CRACK IN RT WING LEADING EDGE OUTBOARD LOWER SKIN AT STA XORS 402. A REPAIR WAS PERFORMED IAW SRM 57-10-00, PAGE 216.

Part: SPAR — CRACKED (WS 317)

INSPECTION FOUND A 0.8 INCH CRACK IN RT WING DROOPED LEADING EDGE ON LATERAL SPAR AT STA XORS 317. A REPAIR WAS PERFORMED IAW ECRA 5720-01738.

Part: SPAR — CRACKED (WS 317)

INSPECTION FOUND A 1.5 INCH CRACK IN RT WING DROOPED LEADING EDGE ON INTERNAL SPAR AT STA XORS 317. A REPAIR WAS PERFORMED IAW ECRA 5720-01738.

Part: PANEL — CRACKED (RT WING)

INSPECTION FOUND A FOUR INCH CRACK IN RT WING PANEL NR 617CT. REPAIRED IAW SRM 57-10-00, PAGE 25.

Part: SKIN — DELAMINATED (LT WING)

INSPECTION FOUND LT WING LOWER SKIN PANEL OF LANDING GEAR VANE DELAMINATED ON THE UPPER AND LOWER SURFACE. THE UPPER AND LOWER SKIN WAS REPAIRED IAW SRM 51-71-00, PARAGRAPH 18B.

Part: SKIN — CRACKED (LT ELEVATOR)

INSPECTION FOUND A .75 INCH CRACK IN LT OUTBOARD ELEVATOR TRAILING EDGE. THE TRACK SECTION TRAILING EDGE WAS REPLACED IAW SRM 55-30-00.

Part: ANGLE — CRACKED (RT TE FLAP)

INSPECTION FOUND A 1 INCH CRACK IN RT WING INBOARD FLAP OUTBOARD AFT FITTING ANGLE. THE ANGLE WAS REPLACED IAW SRM 51-30-00.

Part: FLOORBEAM — CORRODED (BS 449.250)

INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 449.250 ON RT SIDE. THE FLOORBEAM WAS REPLACED IAW SRM 51-30-00.

Part: FLOORBEAM — CORRODED (BS 1887-2007)

INSPECTION FOUND CABIN FLOORBEAM CORRODED BETWEEN STA 1887 AND 2007 ON LT SIDE. THE FLOORBEAM WAS REPLACED IAW SRM 51-31-01.

Part: FLOORBEAM — CORRODED (BS 450.162)

INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 450.162 IN CENTER AND ON RT SIDE. THE FLOORBEAM SECTIONS WERE REPLACED IAW SRM 51-30-00.

Part: FLOORBEAM — CORRODED (BS 450.162 & 515)

INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 450.162 AND 515, LT SIDE. A NEW FLOORBEAM WAS INSTALLED IAW SRM 51-30-00.

Part: FLOORBEAM — CORRODED (BS 427-450)

INSPECTION FOUND CABIN FLOORBEAM CORRODED BETWEEN STA 427.668 AND 450.162 ON LT SIDE. THE BEAM WAS REPLACED IAW SRM 51-30-00.

Part: SKIN — CRACKED (LT WING LE)

INSPECTION FOUND A 1 INCH CRACK IN LT WING LEADING EDGE INTERNAL SKIN AT OUTBOARD LOWER CORNER. A REPAIR WAS PERFORMED IAW SRM 57-00-01.

Part: FLOOR — CORRODED (BS 1099)

INSPECTION FOUND FORWARD CARGO RT SUPPORT FLOOR PANEL CORRODED AT STA 1099. A REPAIR ANGLE WAS INSTALLED IAW SRM 51-30-00.

Part: BEAM — CRACKED (WS 299)

INSPECTION FOUND A 1 INCH CRACK IN RT WING TRAILING EDGE PANEL FITTING BEAM AT STA XORS 299. A REPAIR WAS PERFORMED IAW SRM 57-00-01.

Part: SEAT TRACK — CORRODED (BS 824)

INSPECTION FOUND SEAT TRACKS CORRODED AT STA 824, LT AND RT SIDES. THE SEAT TRACKS WERE REPLACED IAW MM 53-20-00.

Part: FLOORBEAM — CORRODED (BS 1902-2007)

INSPECTION FOUND CABIN FLOORBEAM CORRODED BETWEEN STA 1902 AND 2007, RT SIDE. THE FLOORBEAM WAS REPLACED IAW SRM 51-31-01.

Part: FLOORBEAM — CORRODED (BS 1841-1887)

INSPECTION FOUND CENTRAL FLOORBEAM (NR 2) CORRODED BETWEEN STA 1841 AND 1887. THE FLOORBEAM WAS REPLACED IAW SRM 51-31-01.

Part: FLOORBEAM — CORRODED (BS 1821-1887)

INSPECTION FOUND CABIN FLOORBEAM CORRODED ON LT AND RT SIDES AT STA 1821-1887. THE FLOORBEAM SECTIONS WERE REPLACED IAW SRM 51-30-00.

Part: FLOORBEAM — CORRODED (BS 1905-2007)

INSPECTION FOUND CABIN FLOORBEAM CORRODED AT RT SIDE BETWEEN STA 1905 AND 2007. THE FLOORBEAM WAS REPLACED IAW SRM 51-31-01.

Part: FLOORBEAM — CORRODED (BS 859-879)

INSPECTION FOUND FLOORBEAM CORRODED BETWEEN STA 859 AND 879, RT SIDE. THE BEAM WAS REPLACED IAW SRM 51-30-00.

Part: ACTUATOR — FAILED (LT MLG)

THE LT MLG WOULD NOT RETRACT AFTER TAKEOFF. CYCLING THE GEAR DID NOT HELP. FUEL WAS DUMPED AND THE GEAR WAS VISUALLY CONFIRMED DOWN BY TOWER. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE SWUNG THE LANDING GEAR SEVERAL TIMES, BUT COULD NOT DUPLICATE THE PROBLEM. THE LT GEAR RETRACT CYLINDER AND LT GEAR DOWNLOCK BUNGEE CYLINDER WERE REMOVED AND REPLACED IAW MM 32-33-01 AS A PRECAUTIONARY MEASURE. THE LANDING GEAR WAS SWUNG FOUR MORE TIMES AND OPERATION CHECKED GOOD.

Part: SKIN — CORRODED (LT TE FLAP)

INSPECTION FOUND LT WING INBOARD FLAP SKIN TORN AND CORRODED AT OUTBOARD EDGE CLOSURE RIB. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-21-01, 51-31-01, AND ECRA 5752-01023.

Part: FITTING — CRACKED (R-3 DOOR)

INSPECTION FOUND A 2 INCH CRACK IN R-3 DOOR LOWER FITTING. THE LOWER FITTING WAS REMOVED, A NEW BEAM AND FASTENERS WERE INSTALLED IAW SRM 51-31-01.

Part: STIFFENER — CRACKED (LT MLG WW)

INSPECTION FOUND A 2 INCH CRACK ON LT MLG WHEEL WELL AFT WEB VERTICAL STIFFENER. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WAS FABRICATED AND INSTALLED IAW SRM 53-53-01, 51-21-01, AND 51-31-01.

Part: HYD HOSE — PUNCTURED (NR 2 HYD SYST)

THE NR 2 HYDRAULIC SYSTEM QUANTITY WAS LOST WHILE EN ROUTE FROM IAH TO LGW. THE AIRCRAFT LANDED AT LGW WITHOUT INCIDENT. MAINTENANCE FOUND HYDRAULIC LINE FROM 2-3 REVERSIBLE MOTOR PUMP PUNCTURED AND THE FORWARD SHUTOFF VALVE OF 2-3 REVERSIBLE MOTOR PUMP WAS INOPERATIVE. THE SHUTOFF VALVE WAS REMOVED AND REPLACED. THE HYDRAULIC LINE WAS REPLACED USING FLEX HOSE AND A DIP WAS ISSUED TO REPLACE THE HOSE WITHIN 500 FLIGHTS OR 1200 FLIGHT HOURS. IN ADDITION, BOTH THE LT AND RT HYDRAULIC PUMPS WERE REMOVED AND REPLACED.

Part: BATT CHARGER — INOPERATIVE (CABIN)

THE CREW REPORTED EMERGENCY LIGHT TEST IN COCKPIT DID NOT GIVE GREEN LIGHT. MAINTENANCE FOUND MID CABIN OVERWING BATTERY CHARGER SUPPLY AT FAULT. THE BATTERY CHARGER WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD.

Part: INTERCOSTAL — CORRODED (BS 470)

KUL - INSPECTION FOUND INTERCOSTAL CORRODED ON LEFT SIDE OF AVIONICS COMPARTMENT AT STATION 470, STRINGER 48L. THE INTERCOSTAL WAS REPLACED IAW SRM 53-11-01, FIGURE 5. (M)

Part: INTERCOSTAL — CORRODED (BS 464)

KUL - INSPECTION FOUND INTERCOSTAL CORRODED AT LOWER FUSELAGE FORWARD SECTION STATION 464R. THE INTERCOSTAL WAS REPLACED IAW SRM 53-11-01, FIGURE 5. (M)

Part: SUPPORT — CORRODED (GALLEY 'G')

KUL - INSPECTION FOUND A GALLEY 'G' SUPPORT CORRODED. THE SUPPORT WAS REPLACED IAW SRM 53-70-00, FIGURE 13. (M)

Part: SUPPORT — CORRODED (GALLEY 7)

KUL - INSPECTION FOUND GALLEY 7 INBOARD SUPPORT CORRODED. THE SUPPORT WAS REPAIRED IAW SRM 53-70-00, FIGURE 13. (M)

Part: SUPPORT — CORRODED (BS 1871)

KUL - INSPECTION FOUND LAV 'E' OUTBOARD SUPPORT CORRODED AT STATION 1871. THE SUPPORT WAS REPAIRED IAW SRM 53-70-00, FIGURE 13. (M)