N303AA

Part: LIGHT — DEFECTIVE (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ILLUMINATED. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: STRINGER — CORRODED (FUSELAGE)

AFW - FOUND STRINGER 34L WAS BADLY CORRODED JUST FORWAD OF PRODUCTION SPLICE AT STATION 1307. REQUEST ENG APPROVED TO SPLICE NEW SECTION OF STRINGER PER ATTACHED DRAWING. REPAIR SPLICE WILL BE CLASSED THAN 20 INCH TO PRODUCTION SPLICE. (M)

Part: DUCT — FAILED (APU)

PSP - FLT 0160 - EN ROUTE SAN/JFK, AIRCRAFT EXPERIENCED LOW RUMBLE FOLLOWED BY CENTER DUCT LEAK LIGHT. CLOSED ISOLATION VALVE AND APU BLEED. CABIN CONTINUED TO CLIMB AT MAXIMUM RATE. ACCOMPLISHED EMERGENCY DESCENT TO 10,000 FEET. INSULATION BLEW THROUGH AFT CABIN FROM RIGHT SIDE NEAR ROW 27. CREW AND PASSENGER OXYGEN MASKS DEPLOYED. EMERGENCY DECLARED, DIVERTED TO PSP AND LANDED WITHOUT FURTHER INCIDENT. REPLACED APU AIR SUPPLY DUCT ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. APU AIR SUPPLY DUCT WELD BROKE. (X)

Part: OVEN — DIRTY (CABIN)

SFO - FLT 177 - EN ROUTE JFK-SFO, NR 2 OVEN IN FIRST CLASS GALLEY PRODUCED SMOKE AND A BURNING ODOR. CLEANED NUMBER 2 FIRST CLASS GALLEY OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: STRINGER — CORRODED (BS 1400)

AFW - STRINGER 35L AT APPROX STATION 1400 WAS CORRODED AT PRODUCTION SPLICE. CUT AND REMOVE CORRODED SECTION. ALODINE AND PRIME ALL BARE ALUMINUM. INSTALL NEW SPLICE AND REPAIR PER SKETCHES. (M)

Part: KEEL BEAM — CORRODED (FUSELAGE)

AFW - LEFT KEEL BEAM HAS CORROSION REMOVAL. REMOVED ALL CORROSION AND REFINISH THE SURFACE PER SRM. INSTALL SHIMS/WASHERS BETWEEN THE FLANGE AND THE RETAINER TO PREVENT FASTENER PULL UP AND SEAL THE AREA WITH BMS5-95. (M)

Part: SIGN — BROKEN (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT SIGN ON LAVATORY M-5 WALL BROKEN. REPLACED EMERGENCY EXIT SIGN ON LAVATORY M-5 WALL. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: STRAP — CORRODED (BS 539)

AFW - FOUND AND BLENDED OUT CORROSION ON THE UPPER SURFACE OF THE M3T1590-2 FAIL/SAFE STRAP. REFINISHED BLENDED AREA. APPROVED FOR CONTINUE SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1434. (M)

Part: FRAME — CORRODED (BS 1329)

AFW - FOUND CORROSION ON THE WEB AT THE FUSELAGE FRAME. THE CORROSION WAS TRIMMED OUT. INSTALLED .040 INCH THICK DOUBLER PER INSTRUCTIONS OF MRB 767-1441. (M)

Part: CHORD — CORRODED (BS 1270)

AFW - FOUND CORROSION ON AFT CARGO DOOR FAIL/SAFE CHORD, TOP SIDE (FWD). REMOVED ALL CORROSION FROM DOOR FRAME IAW SRM 51-20-06-0 AND TREATED, PRIMED AREA. (M)

Part: FRAME — CORRODED (BS 1329)

AFW - WEB OF FUSELAGE FRAME HAS CORROSION. SPLICE PLATE TO BE INSTALLED ON THE FORWARD SIDE OF WEB. (M)

Part: ACTUATOR — DEFECTIVE (TE FLAPS)

JFK - FLT 20 - DURING APPROACH TO JFK UPON FLAP EXTENSION, TRAILING EDGE FLAP DISAGREE CAME ON WITH FLAPS AT 1 DEGREE. FLAP HANDLE AT 5 DEGREES AND ALTERNATE FLAP EXTENSION TO 20 DEGREES NORMAL. AFTER FLAP EXTENSION, A LEADING EDGE SLAT ASYMMETRICAL AND ACCESS DOORS EICAS MESSAGE CAME ON AND WENT OUT SEVERAL TIMES. AT 138 KNOTS IN LANDING CONFIGURATION, STICK SHAKER ACTIVATED. AIRCRAFT LANDED JFK WITHOUT INCIDENT. REPLACED OUTBOARD TRAILING EDGE NR 1 FLAP ROTARY ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: TRACK — WORN (NR 11 SLAT)

AFW - FOUND NR 11 SLAT TRACKS WORN BEYOND MM LIMITS. INBOARD TRACK WORN TO .011 INCH. OUTBOARD TRACK WORN TO .013 INCH. BLENDED WORN AREAS. EDDY CURRENT CHECKED. NO CRACKS FOUND. ROTO-PEENED, PRIMED, AND COATED WITH AEROSHELL 7. APPROVED BY ENGINEERING PER MRB 767-1146. TRACKS WILL BE REPLACED AT NEXT MBV. TST: 43,462.33 HRS. CYCLES, 13,660. (X)

Part: TRACK — WORN (NR 1/12 SLAT)

AFW - NR 1 AND NR 12 SLAT TRACKS FOUND WORN BEYOND MM LIMITS. NR 1 WORN TO .011 INCH AND NR 12 WORN TO .014 INCH. BLENDED WORN AREAS. EDDY CURRENT CHECKED. NO CRACKS FOUND. ROTO-PEENED, PRIMED, AND LUBED. APPROVED BY ENGINEERING PER MRB 767-1147. TRACKS WILL BE REPLACED NEXT MBV. TST: 43,462.33 HRS. CYCLES, 13,660. (X)

Part: SKIN — CORRODED (RT PYLON)

AFW - FOUND AND BLENDED DAMAGE ON THE RT PYLON INBOARD SIDE SKIN. FOUND THE BLEND EXCEEDED SRM LIMITS. REFINISHED BLENDED AREA PER SRM. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1141. TST: 43,462.33 HRS. CYCLES, 13,660. (X)

Part: SELECTOR VALVE — DEFECTIVE (LT MLG)

MIA - FLT 1165 - DURING APPROACH WHEN EXTENDING THE LANDING GEAR, THE GEAR DID NOT EXTEND. DID GO-AROUND AND CYCLED GEAR WITH SAME RESULT. ACCOMPLISHED ALTERNATE GEAR EXTENSION, DID FLYBY TO CONFIRM GEAR EXTENSION, AND LANDED MIA WITHOUT INCIDENT. REPLACED MAIN GEAR SELECTOR VALVE, ACCOMPLISHED GEAR SWING, AND REPLACED RT MLG FORWARD DRAG BRAKE. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)