N39367

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 95,293 hrs · 15,172 cycles

RIGHT EXTERIOR EMER LIGHT FWD OF AFT CARGO DOOR WOULD NOT ILLUMINATE. REPLACED POWER SUPPLY & BATTERY. SYS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 95,293 hrs · 15,172 cycles

RIGHT AFT DOOR EMER SLIDE ILLUMINATION LIGHT WOULD NOT TEST. R & R BATTERY & CHARGER. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 94,899 hrs · 15,101 cycles

LEFT NR 1 DOOR EXIT IDENTIFIER SIGN DOOR HANDLE ILLUMINATION LIGHTS INOPERATIVE. REPLACED LAMP FOR LT NR 1 DOOR EXIT IDENTIFIER SIGN DOOR HANDLE ILLUMINATION LIGHTS. OPERATIONS CHECKED NORMAL.

Part: LIGHT — MISSING (EXIT SIGN) · airframe 94,899 hrs · 15,101 cycles

EMERGENCY EXIT SIGN AT RT NR 4 DOOR MISSING HANDLE ILLUMINATION LIGHT ASSEMBLY. REPLACED DOOR HANDLE ILLUMINATION LIGHT ASSEMBLY ON EMER EXIT SIGN AT RT NR 4 DOOR. OPERATIONS CHECKED NORMAL.

Part: COVER — MISSING (CABIN) · airframe 94,065 hrs · 14,983 cycles

SEAT MOUNTED EMER LIGHT 23H MISSING COVER. REPLACED LIGHT ASSEMBLY FOR SEAT MOUNTED EMER LIGHT AT 23H. OPERATIONS CHECKED NORMAL.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 92,625 hrs · 14,739 cycles

CORROSION FOUND ON STRINGER IN AFT CARGO. ACCOMPLISHED SPLICE REPAIR IAW SRM 53-00-03-2R 2.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 92,132 hrs · 14,653 cycles

LT NR 1 DOOR EXIT EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LT NR 1 DOOR EXIT EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 92,132 hrs · 14,653 cycles

LT NR 2 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LAMP FOR LT NR 2 DOOR EMERGENCY EXIT LIGHT. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 91,689 hrs · 14,577 cycles

FLIGHT DECK EMERGENCY EXIT LIGHT ABOVE COCKPIT DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR FLIGHT DECK EMERGENCY EXIT LIGHT ABOVE COCKPIT DOOR. OPERATIONS CHECKED NORMAL.

Part: FMC — INOPERATIVE (LEFT) · airframe 89,293 hrs · 14,193 cycles

BOS - INFLIGHT MIA-CDG CREW REPORTED LEFT FLIGHT MANAGEMENT COMPUTER INOPERATIVE. EMERGENCY DECLARED FLIGHT DIVERTED BOS LANDED WITHOUT INCIDENT. REPLACED LEFT FLIGHT MANAGEMENT COMPUTER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SHUTOFF VALVE — LEAKING (HYDRAULIC SYS) · airframe 89,293 hrs · 14,193 cycles

SAN - CREW REPORTED CENTER HYDRAULIC FLUID DECREASING IN FLIGHT. EMERGENCY DECLARED FLIGHT LANDED SAN WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FLAP/SLAT SHUTOFF VALVE AND AIR DRIVEN HYDRAULIC PUMP THAT WERE LEAKING. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 87,408 hrs · 13,891 cycles

LEFT SIDE EMERGENCY LIGHT AFT OF THE FLAP FAIRING FUSELAGE INOPERATIVE. REPLACED BATTERY PACK FOR LEFT SIDE EMERGENCY LIGHT AFT OF FLAP FAIRING. OPS CHECKED NORMAL.

Part: PROCESSING UNIT — INOPERATIVE (FUEL SYSTEM) · airframe 86,491 hrs · 13,746 cycles

SJU - INFLIGHT MIA-CNF CREW REPORTED FUEL SYSTEM BECAME ERRATIC AND UNRELIABLE AND THE FUEL TOTALIZER WAS BLANK ON BOTH FLIGHT MANAGEMENT COMPUTERS. EMERGENCY DECLARED FLIGHT DIVERTED SJU LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FUEL QUANTITY INDICATING SYSTEM PROCESSOR UNIT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — DEBONDED (NR 5 SLAT) · airframe 85,970 hrs · 13,655 cycles

ULTRASONIC INSPECTION SHOWS A DISBOND ON NUMBER 5 SLAT INBOARD END, LOWER SURFACE. ACCOMPLISHED BONDED REPAIR PER SRM 51-7-10-2R.

Part: CAP — CORRODED (ZONE 100) · corrosion level 2 · airframe 85,970 hrs · 13,655 cycles

STATION 520 SHORT J-CAP HAS SMALL SPOT OF CORROSION AT MOUNTING NUT PLATE FOR POWER DRIVE UNIT 5R BOTTOM SIDE AT DOOR CUTOUT. REPLACED J-CAP PER SRM 51-10-02.

Part: CAP — CORRODED (ZONE 100) · corrosion level 2 · airframe 85,970 hrs · 13,655 cycles

BS 512 SHORT JAY CAP HAS CORROSION AT MOUNTING NUT PLATE FOR POWER DRIVE UNIT 5R BOTTOM SIDE AT DOOR CUTOUT. INSTALLED NEW J-CAP PER SRM 51-10-02.

Part: WEDGE — DEBONDED (NR 12 SLAT) · airframe 85,970 hrs · 13,655 cycles

RIGHT WING NUMBER 12 LEADING EDGE SLAT TRAILING EDGE WEDGE GOUGED AND DISBONDED. ACCOMPLISHED METAL BOND REPAIR PER SRM 51-70-10.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 85,289 hrs · 13,546 cycles

LEFT NUMBER 4 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 4 DOOR EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: FAN — FAULTY (E&E BAY) · airframe 84,427 hrs · 13,396 cycles

MCO - INFLIGHT LHR-MIA. CREW REPORTED ELECTRICAL SMELL INTERMITTANTLY IN COCKPIT DURING FLIGHT. TURNING OFF RECIRCULATION FANS DID NOT HELP. EMERGENCY DECLARED FLIGHT DIVERTED MCO LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND EQUIPMENT COOLING FAN AT FAULT. PLACARD FORWARD EQUIPMENT COOLING FAN INOPERATIVE PER MEL. REPLACED FORWARD EQUIPMENT COOLING FAN AT MIA ON 11/01/2011. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 80,887 hrs · 12,825 cycles

LAVATORY M1 SMOKE DETECTOR HAD FALSE ALARM. REPLACED LAVATORY M1 SMOKE DETECTOR.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 80,072 hrs · 12,679 cycles

EMERGENCY EXIT LIGHT AT LEFT AFT EXTERIOR IS INOPERATIVE. REPLACED M738 BATTERY PACK. OPS CHECK GOOD.

Part: FAN BLADE — BENT (LT ENGINE) · airframe 79,389 hrs · 12,561 cycles

POS - CREW REPORTED BIRD STRIKE TO LEFT ENGINE ON TAKEOFF. VIBRATION ON LEFT ENGINE WENT TO MAXIMUM. EMERGENCY DECLARED RETURNED POS LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED DAMAGED FAN BLADES NUMBER 32 AND 33. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PAWL — BROKEN (R1 DOOR) · airframe 79,315 hrs · 12,547 cycles

AFTER DOORS CLOSED CAPTAIN CALLED MAINTENANCE DUE TO FLIGHT ATTENDANT UNABLE TO ARM THE RIGHT NUMBER 1 DOOR SLIDE. INSPECTED 1R DOOR ARM MECHANISM AND FOUND THE PAWL BROKE. REPLACED PAWL. OPS CHECK NORMAL.

Part: O-RING — DAMAGED (HYDRAULIC SYS) · airframe 78,708 hrs · 12,434 cycles

ORD - INFLIGHT SFO-JFK. CREW REPORTED CENTER HYDRAULIC FLUID LOSS IN FLIGHT. FLIGHT DIVERTED ORD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND O-RING PROTRUDING FROM FITTING ON HYDRAULIC PRESSURE MODULE. REPLACED O-RING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MODULE — FAULTY (HYDRAULIC SYS) · airframe 78,342 hrs · 12,361 cycles

MIA - CREW REPORTED LOST CENTER HYDRAULIC PRESSURE SYSTEM WITH GEAR EXTENSION. FLIGHT LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FLAP/SLAT SHUT-OFF VALVE MODULE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,950 hrs · 11,715 cycles

AFW - AFT CARGO DOOR CUTOUT LOWER MAIN SILL INNER CHORD HAS CORROSION. REPAIRED UNDER MRB 767-3412 AND SRM 51-27-09-7.

Part: SUPPORT FITTING — WORN (NLG) · airframe 74,950 hrs · 11,715 cycles

AFW - BOTH ACTUATOR SUPPORT FITTINGS LOCATED IN THE NOSE LANDING GEAR FORWARD BULKHEAD WERE FOUND WITH LOOSE ACTUATOR LINK ARM BUSHINGS. THE SUPPORT FITTINGS BUSHED HOLES WERE FOUND OVERSIZED TO 1.0018 INCH FROM 1.0000 INCH TO 1.0007 INCH FROM FACTORY. REPAIRED IN ACCORDANCE WITH MRB 767-3411 AND SRM 51-20-09.

Part: LIGHT — LOOSE (ZONE 200)

JFK - FIRST CLASS AISLE LIGHT FIXTURE AT LEFT SIDE LOOSE. SECURED LIGHT FIXTURE AT FIRST CLASS AISLE LEFT SIDE.

Part: LIGHT — INOPERATIVE (CABIN)

LAX- MOUNTED EVACUATION FORWARD POSITION AT SEAT 5A AND 5B INOPERATIVE. REPLACED LIGHT ASSEMBLY AT SEAT 5A AND 5B.

Part: FLASHLIGHT — INOPERATIVE (CABIN)

DFW EMERGENCY FLASHLIGHT AT RT MID CABIN INOPERATIVE. REPLACED FLASHLIGHT AT RT MID CABIN. SYSTEM GROUND CHECKED NORMAL OPS.

Part: BRAKE — OVERHEATED (NR 5) · 72,596 cycles

PAP INFLIGHT T871/20AUG. REPORTED HIGH ENERGY STOP AFTER LANDING. NR 5 WHEEL BRAKE REPORTED INTERMITTENT FLAME ON TAXI. FIRE EXTINGUISHED. REPLACED NR 5 BRAKE ASSEMBLY AND NR 5 TIRE. SYSTEM GROUND CHECKED NORMAL OPS.

Part: CHILLER — INOPERATIVE (GALLEY) · airframe 72,314 hrs

DEN INFLIGHT T073/22JUL ORD TO HNL. CREW REPORT SMOKE AND FUMES IN CABIN AT LT NR FOUR LAVATORY. CREW WAS ABLE TO CLEAR SMOKE. LANDED DEN WITHOUT INCIDENT. FOUND RT HAND AFT CHILLER CIRCUIT BREAKER POPPED AND HOT. REPLACED RT HAND AFT CHILLER. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)

Part: WIRE — SHORTED (CABIN) · airframe 72,089 hrs

SFO - EMERGENCY LIGHT AT LT OVERWING INOPERATIVE. REPAIRED SHORT CIRCUIT AT LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT LT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,089 hrs

SFO - EMERGENCY EXIT SIGN LIGHT AT LEFT NR TWO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT SIGN LIGHT AT LEFT NR TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,089 hrs

SFO - EMERGENCY LIGHT AT LT AFT CABIN INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,089 hrs

SFO - EMERGENCY EXIT SIGN LIGHT AT RT NR ONE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT SIGN LIGHT AT RT NR ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: FUSE — INOPERATIVE (CABIN) · airframe 72,089 hrs

SFO - EMERGENCY LIGHT AT AFT LEFT OVERWING INOPERATIVE. REPLACED FUSE ON BATTERY PACK FOR EMERGENCY LIGHT AT AFT LEFT HAND OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: LENS — MISSING (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT BASE OF RIGHT AFT LAVATORY MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT BASE OF RIGHT AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHTS)

SFO - EMERGENCY LIGHT AT LAVATORY A5 HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT LAVATORY A5. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT 32H INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 32H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: TUBE — LEAKING (ZONE 500)

DURING FLIGHT, LEFT ENGINE N2 INDICATION AND STANDBY INDICATION SHOWING 0.0. ALL OTHER ENGINE INDICATIONS NORMAL. AFTER LANDING FOUND EVIDENCE OF FUEL LEAK FROM LEFT ENGINE. FOUND LEAK FROM FUEL PIPE LOW PRESSURE FILTER TO OIL COOLER, PIPE FRACTURED. REPLACED TUBE FOR LEAKING LEFT ENGINE FUEL PIPE. REPLACED DEDICATED GENERATOR FOR LEFT ENGINE N2. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT OVERHEAD ADJACENT ROW 6B INOPERATIVE. RELAMPED EMERGENCY LIGHT AT OVERHEAD ADJACENT HOW 6B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: HOUSING — DEFECTIVE (CABIN)

DFW - EMERGENCY LIGHT AT SEAT 28H INOPERATIVE. REPLACED HOUSING ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 28H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY LIGHT AT SEAT 38B INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 38B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — BROKEN (CABIN)

DFW - EMERGENCY LIGHT AT SEAT 21B INOPERATIVE. REPLACED BROKEN CONNECTOR AT SEAT 21B FOR INOPERATIVE EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (CABIN)

DFW - EMERGENCY LIGHT AT SEAT 20B INOPERATIVE. FOUND LOOSE CONNECTOR AT SEAT 20B. RECONNECTED CONNECTOR FOR INOPERATIVE EMERGENCY LIGHT AT SEAT 20B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: HOUSING — DEFECTIVE (CABIN)

DFW - EMERGENCY LIGHT AT SEAT 31B INOPERATIVE. RELAMPED NO HELP. ONE LAMP WORKS NORMAL. REPLACED EMERGENCY LIGHT HOUSING ASSEMBLY AT SEAT 28H FOR INOPERATIVE EMERGENCY LIGHT AT SEAT 31B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT 2B INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 2B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT 21G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT 21G. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT 4G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 4G. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT 30B INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 30B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SKIN — DAMAGED (FUSELAGE)

AFW - UPPER FUSELAGE SKIN AT STATION 1417, 1439, 1461, AND 1480 HAS TEAR STRAP CUT. AREA IS SIX INCHES BY 2 INCHES AND IS CUT OUT. FABRICATED REPAIR SPLICE FROM 6 AL 4V TITANIUM .040 INCH THICK. SIZED TO PICK UP THREE ROWS OF FASTENERS ON EACH SIDE OF CUTOUT. FABRICATED A FILLER PIECE FROM 2024 T3 .071 INCH THICK. FINISHED ALL BARE METAL WITH ALODINE AND TWO COATS OF PRIMER. INSTALLED SPLICE PLATE AND PICKED UP A MINIMUM OF THREE ROWS OF 3.3/16 INCH FLUSH SHEAR HEAD, ALUMINUM COATED HI LOKS ON EACH SIDE OF SPLICE.

Part: BATTERY PACK — INOPERATIVE (EMERGNECY LIGHT)

SFO - EMERGENCY LIGHTS ON LEFT SIDE OF FIRST CLASS AND IN LAVATORY INOPERATIVE. REPLACED BATTERY PACK M735 AND SEAT 2A AFT LIGHT ASSEMBLY FOR EMERGENCY LIGHTS ON LEFT SIDE OF FIRST CLASS AND IN LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHTS AT SEATS 2AB THROUGH 6AB INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEATS 2AB THROUGH 6AB. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHTS AT BOTTOM OF FIRST CLASS MOVIE SCREEN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT BOTTOM OF FIRST CLASS MOVIE SCREEN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW EMERGENCY LIGHT AT BOTTOM FORWARD LAVATORY FS3 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT BOTTOM FORWARD LAVATORY FS3. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: STRINGER — CORRODED (FUSELAGE)

AFW - FUSELAGE STRINGER SECTION 46 AT S34L HAD CORROSION AT APPROXIMATELY STATION 1213 TO 1219. CORROSION AREA 3 FEET BY 5 INCHES. ACCOMPLISHED FUSELAGE FITTING AND STRINGER SPLICE REPAIR PER SRM 53 30 03 2.

Part: PIN — INOPERATIVE (EMERGENCY LIGHT)

ORD - EMERGENCY ESCAPE PATH LIGHT AT SEAT 40B INOPERATIVE. PLACARD PER MEL 33-16D AUTHORIZATION 4-197-C. FOUND PUSHED PIN ON EMERGENCY ESCAPE PATH LIGHT SYSTEM. REPAIRED PIN FOR EMERGENCY ESCAPE PATH LIGHTING SYSTEM AT SEAT 40B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — BROKEN (CABIN)

EMERGENCY FLOOR SEAT LIGHTS AT SEAT 34H INOPERATIVE. REPAIRED BROKEN WIRES FOR EMERGENCY FLOOR SEAT LIGHTS AT SEAT 34H. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED--

Part: PRESSURE SWITCH — FAULTY (HYD SYSTEM)

HNL T162/01 EN ROUTE HNL-LAX CENTRAL HYDRAULIC PRIME MESSAGE AND PRESSURE LIGHT ON NUMBER 2 CENTER ELECTRIC HYDRAULIC PUMP ILLUMINATED. RETURNED HNL. REPLACED PRESSURE SWITCH FOR CENTER HYDRAULIC SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, FOUND SEAT 3AB EMERGENCY LIGHT WIRE HARNESS INOPERATIVE. REPLACED SEAT 3AB LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SOCKET — DEFECTIVE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 35B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SOCKET AT SEAT 35B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CHARGER — FAILED (E/E BAY)

AIRCRAFT MAIN BATTERY CHARGER FAILED DURING FLIGHT. REMOVED AND REPLACED MAIN BATTERY AND MAIN BATTERY CHARGER. ACCOMPLISHED ALL REQUIRED CHECKS IAW MM. ALL CHECKS NORMAL.

Part: FITTING — CORRODED (WING)

AFW - FLAP ATTACH HOLES WERE REAMED TO REMOVE CORROSION. FABRICATE FREEZE FIT PLUGS IN ORDER TO ACHIEVE A MIN 0.001 INCH INTERFERENCE FIT. (M)

Part: STRUCTURE — CORRODED (TEL FLAPS)

AFW - FLAP ATTACH HOLES WERE REAMED TO REMOVE CORROSION. FABRICATE FREEZE FIT PLUGS FROM 7075-T6 IN ORDER TO ACHIEVE A MIN .001 INCH INTERFERENCE FIT PER RF. ALODINE PLUGS AND INSTALL WET WITH BM55-95 SEALANT. (M)

Part: BEAM — CORRODED (RT WING)

AFW - RIGHT INBOARD FLAP SUPPORT BEAM (9-10 BEAM ASSY) HAD THE MOST OUTBOARD FLAP ATTACH HOLE REAMED TO .503 TO REMOVED CORROSION. OVERSIZE HOLE TO REMOVE CORROSION AND VISUALLY INSPECT THE BORE TO ENSURE CORROSION REMOVAL. FABRICATED REPAIR BUSHING. INSTALLED BUSHING NET, REAMED THE BUSHING BORE. INSTALLED REPAIR WASHER AGAINST THE SUPPORT BEAM IN PLACE OF THE ORIGINAL WASHER. (M)

Part: STRUCTURE — CORRODED (TE FLAPS)

AFW - FOUND RIGHT INBOARD FLAP SUPPORT BEAM (9-10 BEAM ASSY) HAD THE MOST OUTBOARD FLAP ATTACH HOLE REAMED TO .503 TO REMOVE CORROSION. OVERSIZE HOLE TO REMOVE CORROSION AND VISUALLY INSPECT THE BORE TO ENSURE COMPLETE CORROSION REMOVAL. FABRICATED AND REPAIR BUSHING TRIM AL-N1-BR WITH DIMENSION TO ACHIEVE A .001 INCH INTERFERENCE FIT. ALODINE THE REWORKED HOLE. INSTALLED BUSHING WET WITH BMS5-95 SEALANT. REAM THE BUSHING BORE TO THE ORIGINAL HOLE DIAMETER. VISUALLY INSPECT THE BUSHING BORE FOR DAMAGE. FABRICATE A REPAIR WASHER FROM .125 INCH THICK CRES WITH AN OUTER DIA OF .75 INCH. REFINISH REPAIR WASHER PER AARD 51-20-01-1. INSTALL REPAIR WASHER AGAINST THE SUPPORT BEAM IN PLACE OF THE ORIGINAL WASH

Part: WIRE — DAMAGED (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 26H AND 32H INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT SEAT 26H AND 32H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 35B INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 35B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BRAKE ASSY — DEFECTIVE (LT MLG)

DFW - FLT 367 - DURING TAKEOFF, AIRCRAFT BEGAN TRACKING TO LEFT. AIRCRAFT RETURNED DFW GATE WITHOUT INCIDENT. REPLACED NR 1 BRAKE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — INOPERATIVE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 23B INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 22H INOPERATIVE. RE-SECURED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FSEU — DEFECTIVE (E/E BAY)

SLC - FLT 59 - IN CRUISE GOT FOLLOWING WARNING. FLAP LIMIT OVERSPEED, T/E DISAGREE AND T/E AMBER LIGHT, AIRCRAFT SHOOK. AUTO PILOT DISCONNECTED. EMERGENCY DECLARED. LANDED SLC WITH NR 3 AND NR 4 WHEELS FUSE PLUGS BLOWN. TOUCH DOWN SMOOTH AT 175 KNOTS AUTO BRAKING DISCONNECTED AT TOUCHDOWN. REPLACED NR 3 AND NR 4 WHEELS AND FLAP/SLAT ELECTRONIC UNIT (FSEU). SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVER-NIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS AT SEAT 36H INOPERATIVE. RECONNECTED LOOSE CONNECTOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: CONNECTOR — LOOSE (CABIN)

DFW - EMERGENCY EXIT ESCAPE PATH LIGHT AT SEAT 27B INOPERATIVE. REPLACED CONNECTOR AT SEAT 27B. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: CONNECTOR — DEFECTIVE (ROW 35B)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHTS AT 35B INOPERATIVE. REPLACED EMERGENCY EXIT SEAT LIGHT CONNECTOR AT SEAT 35B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: SOCKET — DEFECTIVE (ROW 29B)

SFO - DURING OVERNIGHT, MAINTENANCE EMERGENCY EXIT SEAT LIGHTS AT 29B INOPERATIVE. REPLACED EMERGENCY EXIT SEAT LIGHT SOCKET AT SEAT 29B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: CONNECTOR — BROKEN (ROW 35B)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT 35B INOPERATIVE. REPLACED EMERGENCY EXIT SEAT LIGHT CONNECTOR AT SEAT 35B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: CONNECTOR — BROKEN (CABIN)

ORD - DURING OVERNIGHT CHECK, RIGHT HAND EMERGENCY EXIT LIGHT FOUND INOPERATIVE. REPLACED CONNECTOR TO RIGHT HAND EMERGENCY EXIT DOOR LIGHT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: FLOOR BEAM — CORRODED (BS 864-926)

AFW - FLOOR BEAM HAS CORROSION BEYOND SRM LIMITS AFTER BLEND-OUT. INSTALLED REPAIR ANGLES 0.060 INCH 7075 T6 PER ENGINEERING MRB 767-1532. TST: 27,657 HOURS. CYCLES: 4,334. (X)

Part: JAMB — CORRODED (BS 612-620)

AFW - FORWARD CARGO DOOR LOWER SILL HAS CORROSION BEYOND SRM LIMITS AFTER BLEND-OUT. CHORD IS SATISFACTORY FOR CONTINUED SERVICE WITH NOTED CONDITION PER ENGINEERING MRB 767-1537. TST: 27,657 HOURS. CYCLES: 4,334. (X)

Part: FRAME — CORRODED (BS 1197)

AFW - CHORD HAD CORROSION BEYOND SRM LIMITS AFTER BLEND-OUT. CHORD IS SATISFACTORY FOR CONTINUED SERVICE WITH NOTED CONDITION PER ENGINEERING MRB 767-1538. TST: 27,657 HOURS. CYCLES: 4,334. (X)

Part: FLOOR BEAM — CORRODED (BS 347)

AFW - FLOOR BEAM CORRODED BEYOND SRM LIMITS AFTER BLEND-OUT. INSTALLED 0.050 INCH REPAIR STRAP PER ENGINEERING MRB 767-1528. TST: 27,657.11 HOURS. CYCLES: 4,334. (X)

Part: FLOOR BEAM — CORRODED (BS 325)

AFW - FASTENER HOLE HAS CORROSION BEYOND SRM LIMITS AFTER BLEND-OUT. INSTALLED FREEZE PLUG PER ENGINEERING MRB 767-1530. TST: 27,657 HOURS. CYCLES, 4,334. (X)

Part: CHORD — CORRODED (PASSENGER DOOR)

AFW - CHORD HAS CORROSION BEYOND SRM LIMITS AFTER BLEND-OUT. CHORD IS ACCEPTABLE FOR CONTINUED SERVICE AFTER BLEND-OUT PER ENGINEERING MRB 767-1531. TST: 27,657 HOURS. CYCLES: 4,334. (X)

Part: FLOOR BEAM — CORRODED (BS 854-859)

AFW - CORROSION ON FLOOR BEAM IS BEYOND SRM LIMITS AFTER BLEND-OUT. INSTALLED SHIMS PER ENGINEERING MRB 767-1533. TST: 27,657.11 HOURS. CYCLES: 4,334. (X)

Part: FRAME — CORRODED (BS 1241)

AFW - J-CAP FRAME HAD CORROSION BEYOND SRM LIMITS AFTER BLEND-OUT. J-CAP FRAME IS ACCEPTABLE FOR CONTINUED SERVICE PER ENGINEERING MRB 767-1540. TST: 27,657 HOURS. CYCLES: 4,334. (X)

Part: FLOOR BEAM — CORRODED (BS 865-909)

AFW - FLOOR BEAM HAD CORROSION BEYOND SRM LIMITS AFTER BLEND-OUT. SHIM AS REQUIRED PER ENGINEERING MRD 767-1539. TST: 27,657 HOURS. CYCLES: 4,334. (X)

Part: SEAT TRACK — CORRODED (BS 764-768)

AFW - SEAT TRACK HAD CORROSION BEYOND SRM LIMITS AFTER BLEND-OUT. SEAT TRACK IS SATISFACTORY FOR CONTINUED SERVICE PER ENGINEERING MRB 767-1535. TST: 27,657 HOURS. CYCLES: 4,334. TST: 27,657 HOURS. CYCLES: 4,334. (X)

Part: IDG — FAILED (LT ENGINE)

ORY - FLT 42 - LEFT GENERATOR DRIVE LIGHT FLICKERING CONTINOUSLY THEN CAME ON STEADY WITH L GEN DRIVE EICAS MESSAGE LEFT GEN DRIVE WAS DISCONNECTED AS PER PROCEDURE. REPLACED LEFT IDG PER MM 24-11-01 PERF ENGINE RUN AND DISCONNECT TEST ALL CHECKS OK. (M)

Part: EEL WIRE — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT AT PASSENGER SEAT 7B FOUND INOPERATIVE. RESECURED LOOSE WIRE TO EMERGENCY FLOOR LIGHT AT PASSENGER SEAT 7B. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)