N313AA

Part: IDG — FAILED (RT GENERATOR)

JFK - FLT 679 - DURING TAKEOFF RECEIVED EICAS MESSAGES, RIGHT GEN OFF, RIGHT GEN DRIVE LT, AND RIGHT UTIL BUS RESET GEN DRIVE LIGHT ON STEADY. COMPLETED CHECKLISTS, RETURNED AND LANDED. REMOVED RIGHT IDG. INSTALLED NEW IDG OPS AND LEAK CHECK OK. (M)

Part: IDG — FAILED (RT ENGINE)

JFK - FLT 679 - EN ROUTE JFK-AUA - RIGHT ENGINE IDG FAILED. RETURNED JFK LANDING WITHOUT INCIDENT. REPLACED RIGHT ID GENERATOR. PERFORMED OPERATIONS CHECKED PER MM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS FLICKER AT ROWS 30 THROUGH 37 LEFT. REPLACED BATTERY PACK FOR ROWS 30 THROUGH 37. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DAMAGED (MID GALLEY)

BOS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT MID GALLEY DAMAGED. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — DAMAGED (CABIN)

JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE SEAT PATH LIGHT AT ROW 35 INOPERATIVE. REPAIRED WIRE AT SEAT 35A. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: GIRT BAR — BROKEN (PAX DOOR)

SFO - DURING OVERNIGHT MAINTENANCE, RIGHT SLIDE PACK RELEASE BAR BRACKETS BROKEN. REPLACED RIGHT SLIDE PACK. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEATS 28B AND 32B INOPERATIVE. RESECURED CONNECTOR TO EMERGENCY EXIT FLOOR PATH LIGHTS AT SEATS 28B AND 32B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLOORBEAM — CORRODED (BS 1480)

AFW - FLOORBEAM AT STATION 1480 HAS CORROSION REMOVAL ON UPPER SURFACE. BLENDED OUT CORROSION, ALODINE AND PRIMED ALL BLENDS AND REPAIR PARTS WITH 2 COATS BMS 10-11 PRIMED. FILLED BLENDS WITH BMS 5-95 SEALANT. INSTALLED 301 1/2H STAINLESS STEEL STRAP WET WITH BMS5-95 SEALANT. (M)

Part: CONNECTOR — FAILED (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT SEAT 37B INOPERATIVE. REPLACED EMERGENCY EXIT SEAT LIGHT CONNECTOR AT SEAT 37B. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)

Part: COFFEE MAKER — FAILED (GALLEY)

LHR - FLT 0046 - EN ROUTE ORD/LHR - BUSINESS CLASS NR 3 COFFEE MAKER EMITTED SMOKE. TURNED OFF COFFEE MAKER. LANDED LHR WITHOUT INCIDENT. REPLACED NR 3 COFFEE MAKER. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: FMC — FAILED (RIGHT)

LHR - FLT 0095 - IN-FLIGHT, RIGHT FMC FAILED. REPLACED RT FMC AND RT CDU. PERFORMED CROSS-LOAD PER SIC 2900. ALL OPS AND INDICATIONS NOW NORMAL. 31334F8FF/1520.09JAN.LHR. (X)

Part: LIGHT — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 29H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT HOUSING ASSEMBLY AT PAX SEAT 29H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PIN — NEEDED RESEATED (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 31H INOPERATIVE. RESEATED PIN AT CONNECTOR FOR EMERGENCY EXIT LIGHT AT PAX SEAT 31H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: IDG — FAILED (RT ENGINE)

RIGHT GEN DRIVE LIGHT ILLUMINATED. RIGHT GEN DRIVE DISCONNECTED IN FLIGHT. PLACARDED RIGHT ENG IDG INOP PER MEL. ACCOMPLISHED MPM 24-01 ENTERED IN MIC. REMOVED AND REPLACED RIGHT IDG LEAK AND OPS CHECK NORMAL. REMOVED PLACARD NR 04-164DC-B. CLEARED MIC. (M)

Part: APU — LOW OIL (APU COMPARTMENT)

JFK - FLT 0105 - TAKEOFF + 1 HR RIGHT GEN CONT OFF LIGHT ILLUMINATED. TROUBLESHOT SYSTEM. REPLACED RIGHT IDG. ALL SYS CKS NORMAL. TAKEOFF + 4 HRS APU SHUT DOWN WITH FAULT LT OAT -53C FUEL -19C. SERVICED APU OIL TO FULL RAN APU FOR 5 HOURS. NO LEAKS FOUND. APU OK FOR SERVICE. (X)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 29AB INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR ON BACK OF LIGHT ASSEMBLY AT PAX SEAT 29AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

SFO - DURING OVERNIGHT CHECK, MID-GALLEY EMERGENCY EXIT EGRESS LIGHTS INOPERATIVE. REPAIRED BROKEN WIRES AT MID-GALLEY FOR EMERGENCY EXIT EGRESS LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SPLICE — CORRODED (BS 434)

AFW - STRINGER CORRODED. DAMAGE REQUIRED REMOVAL OF .90 INCH OF STRINGER AT AFT END OF SPLICE. REMOVED CORROSION. FABRICATED AND INSTALLED NEW REPAIR SPLICE. APPROVED BY ENINEERING PER MRB 767-1113. TST: 42,562.49 HRS. CYCLES, 10,821. (X)

Part: FLOOR BEAM — GOUGED (BS 845)

AFW - FLOOR BEAM WEB GOUGED. DAMAGE BLENDED AND FOUND BEYOND SRM LIMITS. FABRICATED AND INSTALLED .071 INCH THICK 7075-T6 DOUBLER. APPROVED BY ENGINEERING PER MRB 767-1126. TST: 42,562.49 HRS. CYCLES, 10,821. (X)

Part: BULKHEAD — CORRODED (BS 957)

AFW - FOUND AND BLENDED OUT CORROSION ON THE UPPER SURFACE OF THE MAIN CABIN PRESSURE DECK. BLEND-OUTS EXCEEDED SRM MAXIMUM LIMITS. REMOVED CORROSION, ROTO-PEENED. ALODINED, PRIMED, AND PAINTED. APPROVED BY ENGINEERING WITH NOTED CONDITION PER MRB 767-1115. TST: 42,562.49 HRS. CYCLES, 10,821. (X)

Part: CHORD — CORRODED (BS 1087)

AFW - FOUND AND BLENDED OUT CORROSION ON THE UPPER SURFACE OF THE INNER CHORD IN AFT CARGO. PRIMED AND FILLED BLENDED AREA. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1131. TST: 42,562.49 HRS. CYCLES, 10,821. (X)

Part: FLOOR BEAM — CORRODED (BS 1480)

AFW - FLOOR BEAM CORRODED. AFTER BLENDING, FOUND DAMAGE BEYOND SRM LIMITS. ALODINED BLENDED AREA. FABRICATED AND INSTALLED REPAIR STOP USING .050 INCH 301 1/2 HARD STAINLESS STEEL. APPLIED TWO COATS OF PRIMER. APPROVED BY ENGINEERING PER MRB 767-1124. TST: 42,562.49 HRS. CYCLES, 10,821. (X)

Part: SKIN — GOUGED (FUSELAGE)

AFW - FUSELAGE SKIN GOUGED FORWARD OF LOWER FORWARD CORNER OF FORWARD CARGO DOOR CUT-OUT. BLENDED GOUGE, PARENT MATERIAL .202 INCH THICK. LOW POINT OF BLEND .143 INCH THICK. APPROVED FOR CONTINUED SERVICE IN NOTED CONDITION BY ENGINEERING PER MRB 767-1110. TST: 42,562.49 HRS. CYCLES, 10,821. (X)

Part: CHORD — CORRODED (FUSELAGE)

AFW - OVERSIZED EXISITNG HOLE ON CHORD TO ELIMINATE INNER GRANULAR CORROSION. INSTALLED FREEZE PLUG IN HOLE AFTER DRILLING. DRILLED NEW HOLE THROUGH FREEZE PLUG. CHORD TO BE REPLACED AT NEXT MBV. APPROVED BY ENGINEERING PER MRB 767-1132. TST: 42,562.49 HRS. CYCLES, 10,821. (X)

Part: CHORD — CORRODED (BS 1351)

AFW - FOUND AND BLENDED OUT CORROSION ON THE UPPER SURFACE OF THE 146T1213-11 INNER CHORD. THE BLEND-OUT EXCEEDS SRM MAXIMUM LIMITS. REFINISHED BLENDED AREA PER SRM. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1123. TST: 42,562 HRS. CYCLES, 10,821. (X)

Part: FLOOR BEAM — CORRODED (BS 859)

AFW - FOUND AND REMOVED CORROSION ON FLOOR BEAM. AFTER BLENDING, FOUND BEYOND SRM LIMITS. EDDY CHECKED BLEND-OUTS. ROTO-PEENED AND REFINISHED BLENDED AREAS. APPROVED BY ENGINEERING PER MRB 767-1118. TST: 42,562.49 HRS. CYCLES, 10,821. (X)

Part: FLOOR BEAM — CORRODED (BS 850-870)

AFW - FLOOR BEAM CORRODED AND BLENDED ON THE UPPER OUTER SURFACE. FOUND THE BLEND-OUT EXCEEDED SRM LIMITS. REMOVED FLOOR BEAM SECTION FROM STA 849 TO STA 878. SPLICED IN NEW SECTION. APPROVED BY ENGINEERING PER MRB 767-1119. TST: 42,562.49 HRS. CYCLES, 10,821. (X)

Part: STRINGER — CORRODED (BS 434)

AFW - STRINGER CORRODED. DAMAGE REQUIRED THE REMOVAL OF 2.5 INCHES OF STRINGER AT AFT END OF SPLICE. REMOVED CORROSION. FABRICATED AND INSTALLED NEW REPAIR SPLICE. APPROVED BY ENGINEERING PER MRB 767-1112. TST: 42,562.49 HRS. CYCLES, 10,821. (X)

Part: SKIN — CORRODED (WING CTR SECTION)

AFW - CORROSION REMOVED FROM CENTER WING UPPER SKIN AT AFT DRAINS LOCATIONS. APPROVED AND REPAIRED PER INSTRUCTIONS OF MRB 767-1117. TST: 42,562.49 HRS. CYCLES, 10,821. (X)

Part: CHORD — CORRODED (BS 539.5)

AFW - FOUND AND BLENDED CORROSION IN TWO LOCATIONS ON INNER SURFACE OF FAIL-SAFE CHORD. REMOVED CORROSION. ROTO-PEENED TREATED AND PAINTED. APPROVED BY ENGINEERING PER MRB 767-1111. TST: 42,562.49 HRS. CYCLES, 10,821. (X)

Part: STRINGER — CORRODED (BS 434)

AFW - STRINGER CORRODED. DAMAGE REQUIRED REMOVAL OF .70 INCH OF STRINGER FORWARD OF SPLICE. REMOVED ALL CORROSION. FABRICATED AND INSTALLED REPAIR SPLICE. REPAIR APPROVED BY ENGINEERING PER MRB 767-1109. TST: 42,562.49 HRS. CYCLES, 10,821. (X)

Part: REAR SPAR — CORRODED (WING CTR SECTION)

AFW - FOUND AND REMOVED CORROSION ON WING BOX REAR SPAR ASSY UPPER CHORD. CORROSION ALSO REMOVED FROM UPPER SKIN AT SAME LOCATION AND LOWER CHORD TO FLOOR BEAM (T-EXTRUSION) WAS CUT TO REMOVE CORROSION. APPROVED AND REPAIRED PER INSTRUCTIONS OF MRB 767-1116. TST: 42,562.49 HRS. CYCLES, 10,821. (X)

Part: EEL WIRE — BROKEN (CABIN)

MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT FIRST CLASS GALLEY INOPERATIVE. REPLACED BROKEN/SHORTED EMERGENCY FLOOR LIGHT WIRES AT FWD FLIGHT ATTENDANT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION.