N316AA

Part: IDG — FAILED (LT ENGINE)

LEFT GEN DRIVE LEFT CAME ON 30 MINUTES INTO FLIGHT WITH ASSOCIATED ICAS MESSAGE DISCONNECTED LEFT IDG IAW QRH PROCEDURES APU STARTED AND RAN FOR REMAINDER OF FLIGHT. REMOVED AND REPLACED LEFT IDG PER MM, OPS CHECK AND LEAK CHECK GOOD PER MM. (M)

Part: TRANSMITTER — FAULTY (HYD SYSTEM)

SJC - FLT 268 - EN ROUTE SJC-BOS, IMMEDIATELY AFTER TAKEOFF RIGHT HYDRAULIC SYSTEM INDICATED ZERO. AIRCRAFT RETURNED TO SJC.; LANDED WITHOUT INCIDENT. REPLACED RIGHT HYDRAULIC TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: IDG — FAILED (RIGHT)

RIGHT GENERATOR OFF LIGHT ANNUNCIATION QRH PROCEDURE CAME BACK ON LINE FOR SHORT TIME. BITE ON BPCU SHOWED UNDER VOLTAGE TRIP AND REPLACED GCU, ON RIGHT GENERATOR SYSTEM. REMOVED AND REPLACED RIGHT GCU. RAN ENGINE AND FOUND VOLTAGE WANDERING. PLACED THE RIGHT IDG AS INOPERATIVE REF MEL MAN 24-01 PER MEL AUTH 6 560DC-A. ENT INTO MIC ACCOMPLISHED MPM PROCEEDING NR 24-01 AND CHECKS OK. REPLACED RIGHT IDG ASSY LEAK CEHCK OPS CHECK NORMAL CLEARED MEL 06-560DC-A CLEARED MIC REMOVED PLACARD. (M)

Part: LIGHT — MISSING (MID GALLEY)

ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT MID GALLEY MISSING. REPLACED WALL MOUNTED EMERGENCY EXIT LIGHT ASSEMBLY AT MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: DUCT — LEAKING (LT WING)

ORD - FLT 682 - EN ROUTE SFO-ORD, ON FINAL APPROACH DETECTED A LOUD BANG AND LEFT SIDE PACK TURNED OFF. LEFT SIDE DUCT LIGHT ILLUMINATED. LANDED ORD WITHOUT FURTHER INCIDENT. REPLACED PNEUMATIC DUCTS AT WING AREA. ACCOMPLISHED LEAK CHECKS IAW THE MM. NO LEAKS NOTED. SYTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: VIDEO UNIT — FAILED (CABIN)

BOS - FLT 194 - DURING FLIGHT, DVD PLAYER SMOKING. REMOVED FROM AIRCRAFT. (M)

Part: SKIN — CORRODED (CENTER WING)

AFW - DURING CORROSION REMOVED FROM CENTER WING UPPER SKIN AT STATION 956 RBL 78 AND LBL 77. REMOVED CORROSION COMPLETELY PER 767 SRM 57-10-01 FIG 101. INSPECTED BLENDED AREA TO ENSURE A CRACK FREE CONDITION. ROTO-PEENED THE BLENDED AREA, ALODINE, APPLY 2 COATS OF PRIMER AND RESTORE FUEL VAPOR BARRIER. REINSTALL ALL FASTENERS THAT WERE REMOVED PER 767 SRM. (M)

Part: FRAME — CORRODED (BS 1087)

AFW - AFT CARGO FRAME J CAP AT STATION 1087 RBL 20 HAD CORROSION BLENDED BEYOND SRM LIMITS. REPAIR IAW MRB 767-1719. (M)

Part: LIGHT — INOPERATIVE (EMERG EXIT)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT FIXTURE RIGHT SIDE OF BUSINESS CLASS GALLEY MISSING. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY FOR RIGHT SIDE OF BUSINESS CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 30B FOUND INOPERATIVE. REPAIRED WIRE AT SEAT 30B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: WIRE — BROKEN (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT PAX SEAT 17B INOPERATIVE. REPAIRED BROKEN EMERGENCY EXIT LIGHT WIRE AT PAX SEAT 17B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 26H FOUND INOPERATIVE. REPLACED EMERGENCY EXIT LAMP ASSEMBLY AT PASSENGER SEAT 26H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: SKIN — CORRODED (CTR WING)

AFW - WING BOX UPPER SKIN FOUND CORRODED AT AFT DRAIN LOCATION. REMOVED FASTENERS IN CORRODED AREA. REMOVED CORROSION, EDDY CHECKED FOR CRACKS. SPOT FACED FLAP PEENED AREA AND ALODINED. REINSTALLED FASTENER, APPLIED FUEL BARRIER PER AA SPEC P5-54. APPLIED CORROSION INHIBITING COMPOUND PER SRM. APPROVED BY ENGINEERING PER MRB 767-1072. (M)

Part: FLOOR BEAM — CORRODED (BS 870)

FOUND THREE SPOTS OF CORROSION ON FLOOR BEAM TOP CHORD. HOLES WERE DRILLED TO REMOVE THE DEEP CORROSION PER SRM. TWO HOLES ARE 0.090 INCH TOO CLOSE PER SRM. FLOOR BEAM APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1071. (M)

Part: DOOR SILL — CORRODED (BS 1272)

AFW - FOUND AND BLENDED OUT CORROSION ON THE AFT CARGO DOOR OPENING LOWER MAIN SILL UPPER CHORD. FOUND BEYOND SRM LIMITS AFTER BLENDING. INSURED THAT NO FASTENER OR FASTENER HOLE WAS PRESENT. INSURED THAT NO FURTHER CORROSION OR CRACKING WAS PRESENT. REFINISHED AREA PER SRM. APPROVED FOR CONTINUED SERVICE BY ENGINEERING PER MRB 767-1075. (M)

Part: SKIN — DELAMINATED (RT ELEV)

AFW - ULTRASOUND INSPECTION INDICATES .5 INCH DIAMETER INTERPLY DELAMINATION APPROX 50 PERCENT OF ORIGINAL THICKNESS ON THE SKIN APPROX 1 INCH FROM THE LEADING EDGE OF THE RT ELEVATOR. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1068. (M)

Part: SKIN — DELAMINATED (RT ELEV)

AFW - ULTRA SOUND INSPECTION INDICATES INTERNAL DELAMINATION 1.7 INCH LONG AND .75 INCH WIDE ON RT ELEVATOR LEADING EDGE LOWER SKIN. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1069. FOLLOW UP INSPECTION AT NEXT MBV. (M)

Part: SKIN — GOUGED (BS 740)

AFW - FOUND AND BLENDED SMALL GOUGE IN THE EXTERNAL SURFACE OF THE FUSELAGE SKIN. AFTER BLENDING FOUND THE BLENDOUT EXCEEDS SRM MAX ALLOWABLE LIMITS. INSURED NO FASTENER OR FASTENER HOLE DAMAGE WAS PRESENT. INSURED NO CORROSION OR CRACKING WAS PRESENT. REFINISHED BLENDOUT PER SRM. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1074. (M)

Part: FLOOR BEAM — CORRODED (BS 287)

AFW - FLOOR BEAM HAS CORROSION ON UPPER SURFACE. ALODINED BLENDED AREA, FILLED BLENDOUT. FABRICATED AND INSTALLED REPAIR STRAP WING .050 INCH 301.5 HARD STAINLESS STEEL. APPLIED PRIMER, APPROVED BY ENGINEERING AND ACCOMPLISHED PER MRB 767-1073. (M)

Part: SKIN — DELAMINATED (LT ELEV)

AFW - ULTRASOUND INSPECTION INDICATES .5 INCH INTERPLY DELAMINATION IN SKIN APPROX 1 INCH FROM THE L/E OF THE LEFT ELEVATOR. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1070. REINSPECTION AT NEXT MBV. (M)

Part: EEL BASE — BROKEN (MID GALLEY)

SFO - DURING OVERNIGHT CHECK, EMERGENCY LIGHT IN MID GALLEY BROKEN/INOPERATIVE. REPLACED EMERGENCY LIGHT BASE AND LENS AT MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL LAMP — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT CHECK, SEAT MOUNTED EMERGENCY FLOOR LIGHTS AT PAX SEATS 3B, 4H, 22B AND 33B INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY FLOOR LIGHT LAMP ASSEMBLIES AT PAX SEATS 3B, 4H, 22B AND 33B. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)