N354AA

Part: ENGINE — FAILED (LEFT) · airframe 115,384 hrs · 19,018 cycles

DURING DEPARTURE, PASSING ABOUT 2000 MSL, THE LEFT ENGINE EGT AND N1 EXCEEDANCE (BOTH IN RED) AND ANTI-ICE STATUS MESSAGE WAS ON WITH SIGNIFICANT AIRFRAME VIBRATION. THE LEFT ENGINE WAS SHUTDOWN. THE FLIGHT DECLARED AN EMERGENCY AND RETURNED TO RDU. SINGLE ENGINE TIME WAS 18 MINUTES. REMOVED AND REPLACED LEFT ENGINE IAW MCM 71-93-01. OPERATIONS AND LEAK CHECK GOOD. THE AIRCRAFT WAS GROUNDED.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 112,638 hrs · 18,451 cycles

CAPTAINS WINDSHIELD CRACKED EN-ROUTE. EMERGENCY DECLARED, FLIGHT DIVERTED & LANDED WITHOUT FURTHER INCIDENT. ACFT WAS REMOVED FROM SERVICE. R & R THE L1 WINDOW IAW 56-11-01.

Part: CONTROLLER — FAULTY (WINDOW HEAT) · airframe 112,638 hrs · 18,451 cycles

CAPTAIN`S WINDSHIELD CRACKED EN-ROUTE. EMER DECLARED, FLIGHT DIVERTED & LANDED WITHOUT FURTHER INCIDENT. R & R THE LT WINDOW HEAT CONTROL UNIT IAW 30-41-01. ALL TEST ED OK. OK FOR SERVICE. THE A CFT WAS GNDED.. SEE ALSO AALA20150923007.

Part: WIRE — BROKEN (CABIN) · airframe 111,478 hrs · 18,269 cycles

EMERGENCY LIGHTS INOPERATIVE ON SEAT 20B. FOUND BROKEN WIRE UNDERNEATH SEAT 20B AT CONNECTOR. REPINED CONNECTOR IAW MM 20-64-17. PERFORMED OPERATIONAL CHECK IAW MM 33-51-00. SYS CHECKED NORMAL.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 111,337 hrs · 18,246 cycles

SKIN SHEAR TIE BULGING AT FRAME STATION 785. REPAIRED AREA IAW EA 250499.

Part: PANEL — DEBONDED (VERTICAL STAB) · airframe 111,337 hrs · 18,246 cycles

VERTICAL STABILIZER PANEL 321E DISBONDED. REPAIRED PANEL IAW EA 250876 & EA 250812.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 111,337 hrs · 18,246 cycles

CHORD STRAP AT FS 1725.5 IS CORRODED BETWEEN STRINGERS 4R & 5R UNDER THE APU AIR INTAKE PORT FWD LIP. REPAIRED CHORD STRAP IAW EA 250618.

Part: SHROUD — BROKEN (CABIN) · airframe 110,686 hrs · 18,115 cycles

SEAT 26H EMER LIGHT SHROUD IS BROKEN. R & R SHROUD. SYS CHECKED NORMAL.

Part: SHROUD — BROKEN (CABIN) · airframe 110,686 hrs · 18,115 cycles

SEAT 42H EMER LIGHT SHROUD IS BROKEN. R & R SHROUD. SYS CHECKED NORMAL.

Part: SHIM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 109,194 hrs · 17,879 cycles

STRINGER 37 LT SPLICE SHIM AT STATION 1307 CORRODED. REPLACED SHIM IAW EA B767-53-036509.

Part: LIGHT — INOPERATIVE (L4 DOOR) · airframe 108,812 hrs · 17,820 cycles

LEFT NR 4 DOOR EMER LIGHT INOPERATIVE. REPLACED LAMP FOR LT NR 4 DOOR EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: LIGHT — LOOSE (CABIN) · airframe 108,812 hrs · 17,820 cycles

SEAT MOUNTED EMER LIGHT AT 33B INOPERATIVE. SECURED LUMINATOR FOR SEAT MOUNTED EMER LIGHT AT 33B. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 108,305 hrs · 17,732 cycles

RIGHT NR 4 DOOR, UPPER AFT EMER EXIT SIGN INOPERATIVE. REPLACED LAMP FOR RT NR 4 DOOR UPPER AFT EMER EXIT SIGN. OPERATIONS CHECKED NORMAL.

Part: GARLOCK SEAL — LEAKING (RT ENGINE) · airframe 107,941 hrs · 17,668 cycles

LIM CREW REPORTED RT ENG OIL QTY LOSS. RT ENG SHUTDOWN WHEN OIL PRESS WENT TO AMBER, SINGLE ENG TIME WAS APPROXIMATELY 32 MINUTES. EMERGENCY DECLARED FLIGHT RETURNED LIM LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED STARTER GARLOCK SEAL THAT WAS LEAKING. SYS GND CHECKED NORMAL, OPERATION CLOSED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 107,013 hrs · 17,525 cycles

RT HAND OVERWING SLIDE ESCAPE PATH AFT EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RT HAND OVERWING SLIDE ESCAPE PATH AFT EMERGENCY LIGHT, OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 107,013 hrs · 17,525 cycles

RT NR 2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RT NR 2 DOOR EXTERIOR EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 106,714 hrs · 17,465 cycles

EMERGENCY LIGHT AT SEAT 33B INOPERATIVE. REPLACED LAMP FOR SEAT 33B EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.

Part: LENS — MISSING (CABIN) · airframe 106,714 hrs · 17,465 cycles

SEAT MOUNTED EMERGENCY LIGHT AT 33B MISSING LENS. REPLACED LENS FOR SEAT MOUNTED EMERGENCY LIGHT AT 33B. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 106,714 hrs · 17,465 cycles

RT NR 4 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RT NR 4 DOOR EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.

Part: LENS — MISSING (CABIN) · airframe 106,714 hrs · 17,465 cycles

LENS MISSING AT SEAT MOUNTED EMERGENCY LIGHT AT 12B. REPLACED LENS FOR SEAT MOUNTED EMERGENCY LIGHT AT 12B. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 106,714 hrs · 17,465 cycles

OVERHEAD RT AISLE EMERGENCY LIGHT AT ROW 33 INOPERATIVE. REPLACED LAMP FOR OVERHEAD RT AISLE EMERGENCY LIGHT AT ROW 33. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 106,714 hrs · 17,465 cycles

EMERGENCY LIGHT AT SEAT 12B INOPERATIVE. REPLACED LAMP FOR SEAT 12B EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 106,120 hrs · 17,354 cycles

CORROSION WAS FOUND ON THE FUSELAGE SKIN AT STATION 1582 BETWEEN STRINGERS 38 LT & 38 RT. REMOVED CORROSION & ACCOMPLISHED REPAIR IAW SR 3-2523976473, SRM 53-00-01 & EA B767-53-032552.

Part: SUPPORT — CRACKED (NR 2 SPOILER) · airframe 106,120 hrs · 17,354 cycles

NR 2 SPOILER ACTUATOR OTBD SUPPORT IS CRACKED. INSTALLED NEW SUPPORT IAW AARD 57-51-02-1.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 106,120 hrs · 17,354 cycles

TEMPORARY REPAIR INSTALLED AT STATION 1329 FROM STRINGERS 37 TO 39 LT. INSTALLED NEW REPAIR DOUBLER IAW EA 767-53-032517.

Part: SKIN — GOUGED (FUSELAGE) · airframe 106,120 hrs · 17,354 cycles

GOUGES IN FUSELAGE SKIN AT STATION 1572. INSTALLED DOUBLER REPAIR IAW SRM 53-00-01-2R-14.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 105,449 hrs · 17,247 cycles

FOUND RIVET HEADS PROTRUDING AT STATION 1324 & STRINGER 37 LT. REMOVED CORROSION & INSTALLED EXTERNAL DOUBLER REPAIR IAW SRM 53-00-01-2R-1.

Part: ANGLE — CRACKED (TE FLAP) · airframe 103,227 hrs · 16,894 cycles

UPPER AFT SPAR CHORD ANGLE CRACKED AT INBOARD END. INSTALLED TYPICAL EXTRUDE (SPAR) SECTION REPAIR ON RIGHT INBOARD TRAILING EDGE FLAP PER SRM 51-70-12-0G PAGES 1 THRU 20.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 103,072 hrs · 16,872 cycles

SEAT 33AB EMERGENCY SEAT LIGHT INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY PATH LIGHT ASSEMBLY AT SEAT 33AB. OPS CHECK NORMAL.

Part: WIRE — DAMAGED (CABIN) · airframe 103,072 hrs · 16,872 cycles

SEAT 2HJ EMERGENCY SEAT LIGHT INOPERATIVE. FOUND DAMAGED WIRE IN SHORT LEAD BENEATH SEAT 2HJ. REPIARED WIRE. OPS CHECK NORMAL.

Part: FAN — OVERHEATED (E&E BAY) · airframe 102,626 hrs · 16,797 cycles

MIA - CREW REPORTED AFTER TAKEOFF, EQUIPMENT COOLING OVERHEAT LIGHT ILLUMINATED AND HAD LOUD POP/BANG. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FORWARD EQUIPMENT NUMBER ONE FAN. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 102,067 hrs · 16,703 cycles

SEAT 33B EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT 33B EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 100,890 hrs · 16,518 cycles

AFT LEFT LAVATORY MOUNTED FLOOD EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR AFT LEFT LAVATORY FLOOR EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: ROLLER TRAY — CRACKED (ZONE 100) · airframe 100,297 hrs · 16,424 cycles

A2 ROLLER TRAY CRACKED. INSTALLED SERVICEABLE ROLLER TRAY.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 100,297 hrs · 16,424 cycles

SHEAR TIE AT STATION 1540 STRINGER 39 TO 38 RIGHT. REPLACED WITH SERVICEABLE SHEAR TIE PER SRM 51-40-02.

Part: ROLLER TRAY — CRACKED (ZONE 100) · airframe 100,297 hrs · 16,424 cycles

A4 ROLLER TRAY CRACKED. INSTALLED SERVICEABLE ROLLER TRAY.

Part: ROLLER TRAY — CRACKED (ZONE 100) · airframe 100,297 hrs · 16,424 cycles

B2 ROLLER TRAY CRACKED. INSTALLED SERVICEABLE ROLLER TRAY.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 100,297 hrs · 16,424 cycles

SHEAR TIE AT STATION 1540 BETWEEN STRINGERS 39 LEFT AND RIGHT CORRODED. REPLACED SHEAR TIE PER 51-40-02.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 100,297 hrs · 16,424 cycles

LIGHTING STRIKE AT STATION 239 STRINGER 24. REMOVED DAMAGE PER SRM 53-00-01 AND INSTALLED WET RIVET PER SRM 53-00-01-2R.

Part: SPOILER — DAMAGED (LT WING) · airframe 100,297 hrs · 16,424 cycles

HAIL DAMAGE ON NUMBER 2 SPOILER. ACCOMPLISHED BONDED REPAIR PER SRM 57-70-01.

Part: SPOILER — DAMAGED (WING) · airframe 100,297 hrs · 16,424 cycles

HAIL DAMAGE ON NUMBER 9 SPOILER. ACCOMPLISHED BONDED REPAIR PER SRM 57-70-04.

Part: SPOILER — DAMAGED (RT WING) · airframe 100,297 hrs · 16,424 cycles

HAIL DAMAGE ON NUMBER 10 SPOILER. ACCOMPLISHED BONDED REPAIR PER SRM 57-70-04.

Part: AILERON — DAMAGED (RT WING) · airframe 100,297 hrs · 16,424 cycles

HAIL DAMAGE TO RIGHT AILERON. ACCOMPISHED BONDED REPAIR PER SRM 57-60-02-2R.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 100,297 hrs · 16,424 cycles

PUNCTURE IN UPPER SURFACE OF RIGHT ELEVATOR. ACCOMPLISHED HOTBOND REPAIR PER SRM 51-70-04.

Part: AILERON — DAMAGED (LT WING) · airframe 100,297 hrs · 16,424 cycles

HAIL DAMAGE TO LEFT AILERON. ACCOMPLISHED BONDED REPAIR PER SRM 57-60-02R.

Part: SKIN PANEL — DAMAGED (RT ELEVATOR) · airframe 100,297 hrs · 16,424 cycles

HAIL DAMAGE TO RIGHT OUTBOARD ELEVATOR UPPER SKIN PANEL. ACCOMPLISHED HOTBOND REPAIR PER SRM 51-70-04.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 100,276 hrs · 16,419 cycles

SEAT MOUNT EMERGENCY LIGHT FROM SEATS 32B TO 41B INOPERATIVE. REPLACED BATTERY PACK AND SECURED CONNECTOR AT SEAT 39. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 99,462 hrs · 16,284 cycles

LEFT FUSELAGE EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT FUSELAGE EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 99,067 hrs · 16,224 cycles

RIGHT NUMBER 2 DOOR EXTERNAL FUSELAGE EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 2 EXTERNAL FUSELAGE EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 97,737 hrs · 16,011 cycles

LEFT NUMBER 1 DOOR EMERGENCY EXIT SIGN FLOOD LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 1 DOOR EMERGENCY EXIT SIGN FLOOD LIGHT. OPS CHECK NORMAL.

Part: SHUTOFF VALVE — INOPERATIVE (BLEED AIR SYS) · airframe 96,482 hrs · 15,816 cycles

BOS - INFLIGHT MIA-CDG. CREW REPORTED LEFT ENGINE HIGH PRESSURE SHUT-OFF VALVE MESSAGE AND BLEED LIGHT ILLUMINATED IN FLIGHT. EMERGENCY DECLARED FLIGHT DIVERTED BOS LANDED WITHOUT INCIDENT. REPLACED LEFT HIGH SHUT-OFF VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 96,083 hrs · 15,747 cycles

SMOKE ALARM IN A6 LAVATORY IS GOING OFF WITH NO SMOKE PRESENT. RESET A6 SMOKE DETECTOR SMOKE DETECTOR. OPS CHECK NORMAL.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 95,863 hrs · 15,711 cycles

AFT LAVATORY SMOKE DETECTER WENT OFF. RESET UNIT AND DETECTOR WAS SILENCED ACCOMPLISHED AFT RIGHT LAVATORY SMOKE DETECTOR TEST PER AMM 26-13-00-5. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 95,166 hrs · 15,584 cycles

CEILING EMERGENCY EXIT LIGHT AT 28H INOPERATIVE. REPLACED LAMP FOR CEILING EMERGENCY EXIT LIGHT AT 28H. OPS CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 95,166 hrs · 15,584 cycles

SEAT 12B EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT 12B EMERGENCY EXIT LIGHT. OPS CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 95,166 hrs · 15,584 cycles

CEILING EMERGENCY EXIT LIGHT AT 25H INOPERATIVE. REPLACED LAMP FOR CEILING EMERGENCY EXIT LIGHT AT 25H. OPS CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 95,166 hrs · 15,584 cycles

CEILING EMERGENCY EXIT LIGHT AT 12H INOPERATIVE. REPLACED LAMP FOR CEILING EMERGENCY EXIT LIGHT AT 12H. OPS CHECKS NORMAL.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 92,714 hrs · 15,143 cycles

RIGHT NUMBER FOUR DOOR EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED BATTERY.

Part: POWER SUPPLY — SHORTED (ENTERTAIN SYS) · airframe 91,423 hrs · 14,886 cycles

CREW REPORTED SMOKING VIDEO MONITOR AT SEAT 17AB SHORTLY AFTER TAKEOFF. RETURNED TO LAX AND LANDED WITHOUT INCIDENT. FOUND A SHORTED POWER SUPPLY UNIT AT THE MONITOR. REPLACED POWER SUPPLY AND VIDEO MONITOR AT ROW 17AB. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW EMERGENCY LIGHTS AT LEFT SIDE OF FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT LEFT SIDE OF FIRST CLASS.

Part: LIGHT — INOPERATIVE (CABIN)

DFW AFT EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED LAMPS IN AFT EXIT EMERGENCY LIGHT.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 89,078 hrs

SFO - EMERGENCY LIGHTS FROM ROWS 32 TO 41 INOPERATIVE. REPLACED BATTERY PACK FOR ROWS 32 TO 41.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS)

DFW - INTERIOR EMERGENCY LIGHTS AT SEATS 32AB THRU 41AB INOPERATIVE. REPLACED BATTERY PACK FOR SEATS 32AB THRU 41AB.

Part: STRAP — BROKEN (FLASHLIGHT)

MIA - EMERGENCY FLASHLIGHT STRAP BROKEN AT FLIGHT ATTENDANT SEAT MID GALLEY LEFT FORWARD POSITION INOPERATIVE. REPLACED STRAP FOR EMERGENCY FLASHLIGHT AT FLIGHT ATTENDANT SEAT MID GALLEY LEFT FORWARD POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

MIA - EMERGENCY LIGHT AT SEAT 41B INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 41B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — MISROUTED (MLG)

SNN INFLIGHT - TWO AIRCRAFT TIRES ON LEFT MAIN LANDING GEAR BLEW DURING MODERATE ANTI-SKID BRAKING AFTER LANDING. REPLACED ALL FOUR LEFT MAIN LANDING GEAR TIRES AND WHEEL ASSEMBLIES. REPLACED NUMBER SIX BRAKE PACK ASSEMBLY. FOUND INCORRECT WIRING ROUTING BETWEEN J1 AND J3 JUNCTION BOXES. CORRECTED WIRING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT RT FORWARD OVERWING INOPERATIVE. RELAMPED RT FORWARD OVERWING EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — SHORTED (EMERGENCY LIGHT)

AFW - EMERGENCY EXIT LIGHT AFT OF AFT CABIN ENTRY DOORS INOPERATIVE. RELAMPED RIGHT SIDE EXIT LIGHT AND CHANGED FUSE IN BATTERY CHARGER. REPAIRED SHORTED WIRE RIGHT SIDE EXIT LIGHT FOR INOPERATIVE EMERGENCY EXIT LIGHT AFT OF AFT CABIN ENTRY DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SWIVEL — CORRODED (LT & RT STRUT)

LT & RT STRUT SWIVEL ASSY HAD CORROSION & PITTING IN BORE & AROUND BUSHING HAT. BORE & BUSHING HAT HAVE BEEN MACHINED TO ACCOMPLISH CORROSION REMOVAL. ALL DAMAGE REMOVED BY BORING LUGS, SPOT FACING LUG FACES, & RE-CHAMBERING BORE EDGES TO DIMENSIONS GIVEN. BETWEEN 2 FITTINGS MAXIMUM SPOT FACE DEPTH IS 0.130 INCH, MAXIMUM OVERSIZED BORE DIAMETER IS 3.35522. ALODINED & PRIMED ALL REWORKED SURFACES USING 2 COATS OF BMS1011 TYPE 1. MANUFACTURED 2 OVERSIZED BUSHINGS, ADJUSTING BUSHING HAT THICKNESS TO COMPENSATE FOR AMOUNT OF MATERIAL REMOVED FROM RESPECTIVE SPOT FACE LOCATIONS. INSPECT ALL MANUFACTURED BUSHINGS INSURING THERE WERE NO DISCREPANCIES. CAD PLATED BUSHINGS, FILLET SEALED AROUND BUSHING FLANGES.

Part: CONTROL PANEL — INOPERATIVE (COCKPIT)

LAX EMERGENCY LIGHT UNARMED LIGHT DOES NOT ILLUMINATE WITH LIGHT DECK EMERGENCY LIGHT SWITCH IN OFF POSITION. REPLACED PILOTS EMERGENCY LIGHT CONTROL PANEL FOR INOPERATIVE EMERGENCY LIGHT UNARMED LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: VALVE — INOPERATIVE (FUEL SYSTEM)

ORD - INFLIGHT DURING CLIMB RECEIVED FUEL INBALANCE EICAS MESSAGE. FUEL WAS 2500 POUNDS HEAVIER IN RIGHT HAND MAIN TANK. FUEL WAS THEN BALANCED. ON LANDING RIGHT HAND MAIN TANK SHOWED 1500 POUNDS LESS THAN LEFT HAND MAIN TANK. REPLACED RIGHT HAND MAIN TANK DISCHARGE CHECK VALVE, MOTIVE FLOW VALVE, AND SCREEN VALVE. ALSO REPLACED RIGHT HAND AFT BOOST PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SWITCH — INOPERATIVE (EMERGENCY LIGHT)

UNARM LIGHT DOES NOT ILLUMINATE WHEN EMERGENCY LIGHTS ARE IN THE OFF POSITION. CLEANED EMERGENCY LIGHT SWITCH CONTACTS PER FOR EMERGENCY SWITCH UNARM LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — BROKEN (SEAT 2G)

MIA EMERGENCY LIGHT DIRECTIONAL ARROW IN FRONT OF SEAT 2G IS BROKEN. REPLACED DIRECTION ARROW EMERGENCY LIGHT IN FRONT OF SEAT 2G. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (4L DOOR)

MIA EMERGENCY EXIT INDICATOR LENS AT LOWER AFT DOOR 4L IS DAMAGED. REPLACED EMERGENCY EXIT INDICATOR AT LOWER AFT 4L DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: RELIEF VALVE — INOPERATIVE (NR 1 ENGINE)

LAX INFLIGHT T/217/19 OIL QUANTITY DECREASED IN FLIGHT TO 11 QUARTS. RECOVERED UPON LANDING. REPLACED NUMBER 1 ENGINE PRESSURIZATION AND PRESSURE RELIEF VALVES ON NR 1 ENGINE OIL TANK. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ALTIMETER — INOPERATIVE (COCKPIT)

DFW - FLT 946 - CAPTAINS ALT INOPERATIVE. REPLACED CAPTAINS ALT IND, ACCOMPLISHED REQUIRED INSTALLATION TEST . GROUND CHECKS GOOD. (M)

Part: WIRE — BROKEN (BLEED AIR SYS)

BOS - FLT 146 - EN ROUTE BOS-CDG, RIGHT ENGINE BLEED LIGHT CAME ON ONE HOUR AFTER TAKEOFF. WIRE AT AFT TERMINAL ON AIR SUPPLY MODULE BROKEN. RETURNED BACK TO BOS. LANDED WITHOUT INCIDENT. REPLACED WIRE, INSTALLED NEW TERMINAL. BITE ON AIR SUPPLY MODULE SHOWS NO FAULTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SOCKET — INOPERATIVE (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT INOPERATIVE SEAT 24J. RECONNECTED SOCKET TO EMERGENCY LIGHT SEAT 24J. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT MARKERS AT SEVERAL SEATS INOPERATIVE. SECURED EMERGENCY EXIT SEAT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)

Part: CONNECTOR — LOOSE (ROW 3B)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT ROW 3B INOPERATIVE. RESEATED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED, NORMAL OPERATION.

Part: ACTUATOR — DEFECTIVE (NR 10 LE SLAT)

JFK - FLT T0354 - DURING CRUISE, LEADING EDGE SLAT DISAGREE LIGHT ILLUMINATED. CREW ACCOMPLISHED SLAT DISAGREE ALTERNATE PROCEDURES. FLIGHT AIR INTERRUPTED INTO LGA AND LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT WAS FERRIED TO JFK FOR REPAIRS. MAINTENANCE FOUND NR 10 LEADING EDGE SLAT ACTUATOR FAULTY. REPLACED NR 10 LEADING EDGE SLAT ACTUATOR. SYSTEM OPERATED NORMALLY WITH NO LEAKS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: CONNECTOR — FAILED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHTING AT SEATS 33H AND 39B INOPERATIVE. REPLACED EMERGENCY EXIT SEAT LIGHT CONNECTORS AT SIDEWALL. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: HARNESS — LOOSE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHTING AT SEAT 37H INOPERATIVE. RECONNECTED EMERGENCY EXIT SEAT LIGHT HARNESS AT SIDEWALL. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: CONNECTOR — BROKEN (CABIN)

SFO - DURING OVERNIGHT CHECK, SEAT 32H EMERGENCY EXIT PATH LIGHT INOPERATIVE. REPAIRED CONNECTOR PIN AT SEAT 32H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — BROKEN (CABIN)

SFO - DURING OVERNIGHT CHECK, SEAT 36H EMERGENCY EXIT LIGHT INOPERATIVE. RESET PUSH BACK PIN AT SEAT 36H CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT PAX SEAT 33H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 33H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT PAX SEAT 25B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 25B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT PAX SEAT 39B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 39B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SIGN — BROKEN (CABIN)

SFO - DURING OVERNIGHT CHECK, FIRST CLASS GALLEY EMERGENCY EXIT SIGN FOUND BROKEN. REPLACED FIRST CLASS GALLEY EMERGENCY EXIT SIGN BASE ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: SOCKET — BROKEN (CABIN)

SFO - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT LIGHTS AT SEATS 21AB INOPERATIVE. REPLACED SOCKET ON EMERGENCY EXIT LIGHTS AT SEATS 21AB. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: IDG — MALFUNCTIONED (RIGHT)

JFK - FLT 956 - RT GEN DRIVE LIGHT CAME ON WITH INTERMITTENT RT GEN DRIVE EICAS MSG RT GEN DRIVE DISCONNECTED PER PROCEDURE. REPLACED RT IDG, LEAK CHECK, THEN SERVICE OPS OK. APPROVED FOR SERVICE REMOVED PLACARD MEL AUTH 11-150DC-B CLEARED MIC SHEET 354240800/1239. (M)

Part: CONNECTOR — LOOSE (LT FUEL QTY IND)

DFW - FLT 1864 - LEFT FUEL QTY IND WENT BLANK IN FLT MESSAGE, FUEL QTY IND CAME ON. BITE CHECKED FUEL QTY PROC FOUND D1, D2, 63, 64 CHAN 1 AND 2 FAULTED. PLACARDED LEFT FUEL QTY INOP PER MEL AND PLACARDED TOTALIZER INOP PER MEL. NOTE ITEM NR 48 FOR TOT ALL OTHER FUEL QTY IND CHECK NORMAL. FOUND TERMINAL END ON UNIT 14 TAN7083 LOOSE. PERFORMED CAPACITANANCE CHECK ON UNIT 14 FOUND WITHIN LIMITS PER MM. PERFORMED BITE CHECK, NO FAULTS NOTE. SERVICED WITH FUEL. SYSTEM INDICATION OPERATIONS CHECK NORMAL. REMOVED PLACARD. (M)

Part: DENSITOMETER — FAILED (LT FUEL SYSTEM)

SCL - FLT 945 - BITE TO FUEL PROCESSOR FOUND LEFT DENSITOMETER FAULTED. DEFERRED PER MEL 28-22 AUTH 10-470C-C, PLACARDED INOP AND ENTERED ON MIC SHEET. LEFT DENSITOMETER DEACTIVATED PER MPM 28-22. CLEANED DENSITOMETER CONNECTORS AND ACCOMPLISHED BITE CHECKS, SYSTEM OPERATION AND BITE CHECKS NORMAL. (M)

Part: BATTERY CHARGER — INOPERATIVE (BATTERY COMPT)

JFK - FLT 62 - MAIN BATTERY CHARGER STATUS LIGHT IN-FLIGHT. REPLACED BATTERY AND BATTERY CHARGER PER MM. UNITS ALL CHECKS GOOD. REF: OPERATOR CONTROL NR AALA971280.

Part: IDG — FAILED (RT ENGINE)

SNN - ONE HR INTO FLT, RT GEN LIGHT ILLUMINATED FOLLOWED BY RT BUS TIE AND RT BUS LIGHTS. RT AC BUSS WAS LOST. TRIED TO REINSTATE RT GCU AS PER CHECK LIST AND COULD NOT REGAIN POWER. PAX SAW AND SMELLED SOME SMOKE IN BUSINESS GALLEY AREA. SYSTEM WAS LEFT SHUT DOWN. APU WAS STARTED AND MADE EMERGENCY LANDING AT SNN. REMOVED AND REPLACED RT IDG PER MM. ALSO, REPAIRED T-3 FEEDER TERMINAL OPS CHECK AND LK CHECK NORMAL. REMOVED PLACARD AND CLEARED MIC SHEET. (M)

Part: IDG — FAILED (RT ENGINE)

RIGHT GEN DRIVE LIGHT REMAINS ILLUMINATED. TRIED TO RECYCLE RIGHT GEN CONT DRIVE LGHT AND GEN OFF. LIGHT REMAINS ON. GEN FIELD LIGHT DOES RESET. MEL 24-01 AUTH NR 04-155DC-6, AFTER PUSH BACK AND ENG START RT IDG FAILED AGAIN. DRIVE LT ON NO VOLTS. NO FREQ, BPCU SHOWS NO FAULT. DISC RT IDG AND DISPATCHED A/C AS PER MEL 24-01 AUTH 04-155DC-B FOR 120 MINS ETOPS ONLY, MPM PROC 24-01. FOUND IDG SHAFT SHEARED. REPLACD IDG EPR MM. OPS CHECK AND LEAK CHECK NORMAL. REMOVED MEL 4-155DC-B. REMOVED FROM MIC.

Part: FRAME — CORRODED (FUSELAGE)

AFW - FOUND AREA OF CORROSION BEYOND SRM LIMITS. BLENDED OUT DAMAGE PER ENGINEERING MRB 767-1231. (M)

Part: FRAME — CORRODED (BS 654)

AFW - FOUND AREA OF CORROSION BEYOND SRM LIMITS. BLEND OUT DAMAGE PER ENGINEERING MRB 767-1232. (M)

Part: STOP — CORRODED (BS 568-570)

AFW - ROLLOUT STOP ATTACH BOLT HOLES CORRODED BEYOND SRM LIMITS. INSTALLED 1 INCH DIAMETER FREEZE PLUGS PER ENGINEERING MRB 767-1233. (M)

Part: FRAME — CORRODED (FUSELAGE)

AFW - FOUND AREA OF CORROSION BEYOND SRM LIMITS. BLENDED OUT DAMAGE PER ENGINEERING MRB 767-1230. (M)

Part: EEL CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTS AT ROW 2-7B INOPERATIVE. CONNECTED LOOSE PINS IN CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)

Part: EEL CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT AT AFT FLIGHT ATTENDANT POSITION FOUND INTERMITTENT. RESECURED EMERGENCY FLOOR LIGHT CONNECTOR AT AFT FLIGHT ATTENDANT POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)