N387AM

Part: LENS — DAMAGED (CABIN) · airframe 91,955 hrs · 15,019 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY ESCAPE PATH LIGHT AT SEAT 24B HAS A DAMAGED LENS COVER. REMOVED AND REPLACED LENS COVER IAW AMM 33-50-00. OPERATIONAL CHECK GOOD.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 91,737 hrs · 14,982 cycles

EMERGENCY EXIT SIGN BY THE LEFT MAIN CABIN WINDOW HAS A DETACHED LENS. ATTACHED THE LENS. OPERATIONAL CHECKED GOOD.

Part: CYLINDER — LOW PRESSURE (LT OVRWG SLIDE) · airframe 91,632 hrs · 14,965 cycles

LEFT OVERWING ESCAPE SLIDE PRESSURE CYLINDER IS LOW. REMOVED AND REPLACED CYLINDER ASSEMBLY IAW AMM 25-65-02. OPERATIONAL CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: BATTERY — NO TEST (FLASHLIGHT) · airframe 91,589 hrs · 14,955 cycles

FLIGHT ATTENDANT FLASHLIGHT AT THE G5 GALLEY LEFT AISLE AFT JUMPSEAT FAILED TO TEST. REMOVED AND REPLACED THE BATTERY IAW ESO 11758. OPERATIONAL CHECKED GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 91,365 hrs · 14,902 cycles

AIRCRAFT WAS NOT GROUNDED. AFT LEFT FLIGHT ATTENDANT SEAT FLASHLIGHT ROW 17AB IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 91,102 hrs · 14,848 cycles

AIRCRAFT WAS NOT GROUNDED. AFT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT ADJACENT TO M1 LAVATORY WILL NOT TEST. REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERY AND ACCOMPLISHED OPERATIONAL CHECK IAW AMM 25-60-00. SYSTEM CHECK NORMAL.

Part: MECHANISM — DIRTY (R1 DOOR) · airframe 90,982 hrs · 14,813 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT REPORTS THE R1 DOOR IS DIFFICULT TO ARM. REMOVED DEBRIS AND LUBRICATED R1 DOOR SLIDE ARMING MECHANISM. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 90,540 hrs · 14,688 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT MID CABIN LEFT SIDE FAILED TEST. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-64-00. OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 89,835 hrs · 14,533 cycles

COCKPIT EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY IAW AMM 33-51-00. OPERATIONAL CHECK NORMAL.

Part: IDG — FAULTY (LT ENGINE) · airframe 87,592 hrs · 14,062 cycles

AIRCRAFT WAS GNDED. DURING TAKEOFF ROLL RECEIVED LT IDG WARNING. ABORTED TAKEOFF AT APPROX 75 KNOTS. R & R LT IDG IAW AMM 24-11-01. OPERATIONAL CHECKED GOOD. REPEAT OF EVENT ON 02 18 2016 FLIGHT 6. SEE AALA20160222003.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 87,585 hrs · 14,061 cycles

AIRCRAFT WAS NOT GNDED. DURING TAKEOFF ROLL RECEIVED LT IDG WARNING. ABORTED TAKEOFF AT APPROX 78 KNOTS. RECONNECTED IDG & ACCOMPLISHED FIM 24-20-00-815-801 WITH NO FAULTS FOUND. EVENT REPEATED ON 02 19 2016 FLIGHT 7. SEE AALA20160222004.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 86,958 hrs · 13,928 cycles

FLOORBEAM STIFFENER AT STATION 246 & RBL 15 IS CRACKED. FABRICATED & INSTALLED REPLACEMENT BRACKET IAW SRM 53-10-51-2R-3.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 86,958 hrs · 13,928 cycles

COOLING LINE ATTACH ANGLE IS CRACKED FWD SIDE OF FRAME 246 AT APPROX RBL 11. INSTALLED NEW SERVICEABLE COOLING LINE ATTACH ANGLE 141T5146-5 IAW DOCUMENT NR 141T5104 & IAW SRM 53-10-51-2R-3.

Part: ACTUATOR — FAULTED (SLAT SYSTEM) · airframe 86,169 hrs · 13,800 cycles

EMERGENCY DECLARED, LANDING UNEVENTFUL, ACFT NOT OVERWEIGHT. DURING APPROACH LE SLAT DISAGREE LIGHT ILLUMINATED AS FLAPS EXTENDED TO 25. MX FOUND RT WING INBD ROTARY ACTUATOR NOT LOCKED, IS MOVING 3 TO 4 INCHES WITH FLAP IN EXTENDED POSITION 30. R & R RT WING INBD FLAP OTBD ROTARY ACTUATOR IAW AMM 27-51-11.

Part: MEC — FAULTY (LT ENGINE) · airframe 85,885 hrs · 13,751 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS NOT OVERWEIGHT. RETURNED DUE TO LT ENG COMPRESSOR STALL AT 10,000 FEET. NO ENG SHUTDOWN REPORTED. REPLACED THE MAIN ENG CONTROL IAW 73-94-02.

Part: PUMP — FAULTY (LT ENGINE) · airframe 85,885 hrs · 13,751 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS NOT OVERWEIGHT. RETURNED DUE TO LT ENG COMPRESSOR STALL AT 10,000 FEET. NO ENG SHUTDOWN REPORTED. REPLACED LT ENG FUEL PUMP IAW 73-94-04.

Part: SENSOR — FAULTY (LT ENGINE) · airframe 85,885 hrs · 13,751 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS NOT OVERWEIGHT. RETURNED DUE TO LT ENG COMPRESSOR STALL AT 10,000 FEET. NO ENG SHUTDOWN REPORTED. REPLACED CIT SENSOR IAW 73-21-02.

Part: SENSOR — FAILED (LT ENGINE) · airframe 84,428 hrs · 13,505 cycles

LT ENG COMPRESSOR STALLED AT 10,000 FT. AIR INTERRUPTION, EMERGENCY DECLARED. LANDING UNEVENTFUL. NO ENG SHUTDOWN REPORTED. REPLACED ELECTRIC FAN INLET TEMP SENSOR IAW 73-21-02.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 83,922 hrs · 13,405 cycles

CEILING MOUNTED EMER LIGHT AT 13G INOPERATIVE. R & R LAMP AT SEAT 13G IAW AMM 33-51-04. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 83,922 hrs · 13,405 cycles

RIGHT FWD SLIDE FUSELAGE EMER LIGHT INOPERATIVE. R & R LAMP IAW AMM 33-51-06. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 83,922 hrs · 13,405 cycles

R2 DOOR LOWER EXIT SIGN INOPERATIVE. R & R LAMPS AT R2 LOWER EXIT SIGN IAW AMM 33-51-01. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 83,922 hrs · 13,405 cycles

LEFT FWD SLIDE FUSELAGE EMER LIGHT INOPERATIVE. R & R LAMP IAW AMM 33-51-06. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 83,922 hrs · 13,405 cycles

L1 DOOR EXIT SIGN DOOR HANDLE LIGHTS INOPERATIVE. R & R LAMP IAW AMM 33-51-01. SYS CHECKED NORMAL.

Part: CHARGER — DEFECTIVE (CABIN) · airframe 83,922 hrs · 13,405 cycles

L2 & R2 DOOR EXIT & EXIT THRESHOLD LIGHTS INOPERATIVE. R & R BATTERY & CHARGER ASSEMBLY M1210 IAW AMM 33-51-07. SYS CHECKED NORMAL.

Part: SIGN — DAMAGED (CABIN) · airframe 83,922 hrs · 13,405 cycles

L2 DOOR UPPER EXIT SIGN DAMAGED. R & R L2 DOOR UPPER EXIT SIGN IAW AMM 33-51-01. SYS CHECKED NORMAL.

Part: SOCKET — INOPERATIVE (CABIN) · airframe 83,648 hrs · 13,353 cycles

SEAT 25B EMER LIGHT IS INOPERATIVE. R & R SOCKET LIGHT ASSEMBLY AT 25B. SYS CHECKED NORMAL.

Part: RELAY — FAILED (EMERGENCY EXIT) · airframe 82,173 hrs · 13,140 cycles

EMERGENCY EXITS FAILED SQUIB TEST. REPLACED LT & RT K1 RELAY.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 82,031 hrs · 13,115 cycles

AFT LT SIDE EMER LIGHT JUST AFT OF WING EXIT LIGHT INOPERATIVE. REPLACED LAMP FOR AFT LT SIDE EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 82,031 hrs · 13,115 cycles

AFT RT SIDE EMER LIGHT JUST AFT OF WING EXIT LIGHT INOPERATIVE. REPLACED LAMP FOR AFT RT SIDE EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: HOUSING — DEFECTIVE (EXIT SIGN) · airframe 81,558 hrs · 13,038 cycles

LEFT NR 1 DOOR EMERGENCY EXIT SIGN LOWER LIGHTS INOPERATIVE. REPLACED HOUSING ASSEMBLY FOR LT NR 1 DOOR EMERGENCY EXIT SIGN LOWER LIGHTS, OPERATIONS CHECKED NORMAL.

Part: COFFEEMAKER — MALFUNCTIONED (GALLEY) · airframe 80,865 hrs · 12,919 cycles

CDG CREW REPORTED SMOKE IN FWD GALLEY EMANATING FROM OVERHEAD VENT FWD OF CEILING LIGHT. UTILITY SWITCHES SELECTED OFF. FLIGHT LANDED CDG WITHOUT INCIDENT. FOUND COFFEE MAKER 2 BURNED OUT WITH A SPREAD OF WHITE POWDER. REPLACED NR 2 COFFEE MAKER. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 80,270 hrs · 12,814 cycles

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

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 78,802 hrs · 12,585 cycles

EMERGENCY FLASHLIGHT AT F/A JUMPSEAT RT SIDE AFT GALLEY INOPERATIVE. REPLACED EMERGENCY FLASHLIGHT AT F/A JUMPSEAT RT SIDE AFT GALLEY. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 78,802 hrs · 12,585 cycles

EXTERIOR EMERGENCY LIGHT AT BULK CARGO DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT BULK CARGO DOOR. OPS CHECK NORMAL.

Part: HEAT EXCHANGER — INOPERATIVE (AC BAY) · airframe 74,069 hrs · 11,820 cycles

DFW - CREW REPORTED CABIN GRADUALLY FILLED WITH OIL FUMES AND SMOKE. AFT LAVATORY SMOKE DETECTORS ALSO BEGAN TO CHIME. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. AIRCRAFT FERRIED TO AFW FOR REPAIRS. REPLACED PRIMARY AND SECONDARY HEAT EXCHANGERS AND AIR CYCLE MACHINE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONTROL PANEL — INOPERATIVE (BLEED AIR SYS) · airframe 73,944 hrs · 11,799 cycles

CREW REPORTED LEFT ENGINE BLEED AIR "OFF" LIGHT ILLUMINATED FOLLOWED BY "LEFT PACK OFF". NO DUCT PRESSURE FROM LEFT ENGINE BLEED SYSTEM. EMERGENCY DECLARED FLIGHT DIVERTED & LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED ENGINE FIRE CONTROL PANEL AND BLEED AIR SUPPLY PANEL. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SHUTOFF VALVE — INOPERATIVE (BLEED AIR SYS) · airframe 73,936 hrs · 11,795 cycles

LHR - INFLIGHT JFK-ZRH. CREW REPORTED LEFT ENGINE BLEED LIGHT ILLUMINATED ON EICAS PANEL IN FLIGHT. FLIGHT DIVERTED LHR LANDED WITHOUT INCIDENT. REPLACED AIR SUPPLY CONTROL VALVE AND PRESSURE REGULATING SHUT-OFF VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SENSOR — FAULTY (LE SLAT) · airframe 72,478 hrs · 11,563 cycles

LAX - CREW REPORTED LEADING EDGE SLAT ASSYMETRY EICAS MESSAGE WHEN FLAPS RETRACTED. EMERGENCY DECLARED FLIGHT RETURNED LAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED SENSOR S278. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 3 · airframe 72,464 hrs · 11,560 cycles

CORROSION WAS FOUND AROUND NUT PLATE CLIP ON FUSELAGE MAIN DECK FLOORBEAM AT STATION 347 RIGHT BUTLTINE 26.5. INSTALLED REPAIR STRAP PER EA B767-53-018731.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 3 · airframe 72,464 hrs · 11,560 cycles

HEAVY CORROSION ON THE FUSELAGE SKIN INNER SURFACE BETWEEN STATIONS 1082 TO 1087 STRINGERS 38 LEFT AND 38 RIGHT BETWEEN KEEL BEAM CHORDS. REMOVED DAMAGE IAW B767 SRM 53-00-01, PERFORMED DVI WITHIN 22 INCHES OF THE REPAIR TO ENSURE DAMAGE FREE CONDITION. PERFORMED SURFACE HFEC ON ALL REWORKED AREAS. ACCOMPLISHED REPAIR PER EA 018724.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 3 · airframe 72,464 hrs · 11,560 cycles

SEVERAL AREAS OF CORROSION WERE FOUND ON THE FORWARD CARGO DOOR LOWER SILL OUTER CHORD AND FAIL SAFE STRAP. REMOVED ALL CORROSION PER SRM 51-10, ACCOMPLISHED SURFACE HFEC AND OPEN HOLE HFEC INSPECTION. INSTALLED DRAWING TYPE FASTENERS BACK INTO THE FASTENER HOLES WET WITH BMS 5-95 PER EA 018620.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 3 · airframe 72,464 hrs · 11,560 cycles

SEVERE CORROSION FOUND ON FUSELAGE SKIN INNER SURFACE AT STATION 1087 AND BUTTLINE 0. ACCOMPLISHED DOUBLER REPAIR PER EA B767-53-018755.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,182 hrs · 11,513 cycles

LEFT AFT EXTERIOR EMERGENCY SLIDE LIGHT INOPERATIVE. REPLACED BATTERY PACK M738. OPS CHECK NORMAL.

Part: COOLING FAN — SHORTED (E&E BAY) · airframe 65,723 hrs · 10,438 cycles

INFLIGHT CREW REPORTED BURNING SMELL IN COCKPIT. FORWARD EQUIPMENT EXHAUST FAN CIRCUIT BREAKER POPPED. DIVERTED AUA AND LANDED WITHOUT INCIDENT. THE FORWARD EQUIPMENT COOLING FAN WAS PLACARD AND REPLACED IN BOS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,410 hrs

MIA - EMERGENCY LIGHT AT SEAT 11B INOPERATIVE. REPLACED LAMP CPN5576218 FOR EMERGENCY LIGHT AT SEAT 11B.

Part: FSEU — TRIPPED (LE SLAT) · airframe 63,043 hrs · 10,019 cycles

SSA INFLIGHT - CREW REPORTED LEADING EDGE SLAT ASYMMETRY INDICATION. LANDED SSA WITHOUT INCIDENT. RESET FLAP SLAT ELECTRONIC UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,723 hrs

DFW - EMERGENCY FLOOD LIGHT AT RIGHT NR ONE ENTRY DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RT NR ONE ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: LENS — MISSING (EMERGENCY LIGHTS)

MIA - EMERGENCY LIGHT AT SEAT 21A MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 21A. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PLUG — CRACKED (SPOILER ACTUATOR) · airframe 59,693 hrs

LAX INFLIGHT T88/02MAR - AFTER TAKEOFF, LEFT HYDRAULIC QUANTITY DECREASED TO .15. RETURNED TO LAX AND LANDED WITHOUT INCIDENT. FOUND NUMBER SIX SPOILER ACTUATOR FILTER PLUG CRACKED AND LEAKING. REPLACED NUMBER SIX SPOILER ACTUATOR FILTER PLUG AND O-RING. REPLACED ALL FOUR LEFT BRAKES DUE TO HYDRAULIC CONTAMINATION. SERVICED LEFT HYDRAULIC SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS)

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

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT SEAT 5B INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT 5B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EXTERIOR EMERGENCY LIGHT AT LEFT WING AFT OF TRAILING EDGE INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LEFT WING AFT OF TRAINING EDGE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHTS AT SEAT ROWS 32AB TO 41AB INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 32AB TO 41AB. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

MIA - SEAT MOUNTED EMERGENCY LIGHTS FROM SEAT 32H TO 41H INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS FROM SEAT 32H TO 41H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

MIA - OVERHEAD EMERGENCY LIGHTS AT SEATS 37H AND 39H INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT SEATS 37H TO 39H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — LOOSE (EMERGENCY LIGHTS)

MIA - EMERGENCY EXIT LIGHT COVER IN COCKPIT FELL OFF LIGHT ASSEMBLY. SECURED LENS FOR EMERGENCY EXIT LIGHT ASSEMBLY IN COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHT)

MIA - EMERGENCY EXIT SIGN LIGHT AT RIGHT OVERWING DOOR MISSING LENS. REPLACED LENS FOR EMERGENCY EXIT SIGN LIGHT AT RIGHT OVERWING DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT OVERHEAD SEAT ROW 23B MISSING LENS. REPLACED OVERHEAD EMERGENCY LIGHT LENS AT SEAT ROW 23B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRAP — DAMAGED (FUSELAGE)

AFW - BLENDING ON FORWARD LARGE CARGO DOOR LOWER SILL FAIL/SAFE STRAP BEYOND LIMITS AT STATION 550. AREA OF DISCREPANCY IS 2.5 INCHES BY 1.5 INCHES WITH AT DEPTH OF .38 INCH. REPAIRED PER MRB 767 2938.

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT RIGHT HAND GALLEY INOPERATIVE. RELAMPED EMERGENCY LIGHT AT RIGHT HAND GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SOCKET — INOPERATIVE (CABIN)

MIA - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 23H INOPERATIVE. FOUND BROKEN WIRE AT SOCKET OF EMERGENCY LIGHT CONNECTOR UNDER SEAT 23J. INSTALLED NEW SOCKET FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 23H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — BURNED (EMERGENCY LIGHTS)

AFW - CEILING FORWARD OVERHEAD AND MID CABIN LIGHTING PANELS HAD BURNED WIRE, BURNED TERMINALS, AND BURNED TRANSFORMER AT T180. REPLACED TRANSFORMER AND TERMINAL LUGS FOR CEILING FORWARD OVERHEAD AND MID CABIN LIGHTING PANELS AT T180. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LAX - TWO LEFT HAND OVERHEAD AISLE EMERGENCY LIGHTS AFT OF EXIT SIGN AT OVERWING EXITS INOPERATIVE. REPLACED BATTERY PACK FOR TWO LEFT HAND OVERHEAD AISLE EMERGENCY LIGHTS AFT OF EXIT SIGN AT OVEWING EXITS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: GASKET — LEAKING (FUEL FLOW METER)

GRU - INFLIGHT T0907 ON DESCENT THROUGH 22000 FEET RT ENGINE FLAMED OUT. ACCOMPLISHED AN INFLIGHT START WITHIN 2 MINUTES. DESCENDING THROUGH 6000 FT, RT ENGINE HAD UNCOMMANDED SHUTDOWN. ACCOMPLISHED SINGLE ENGINE LANDING. LANDED WITHOUT INCIDENT. FOUND FUEL LEAK FROM FLOWMETER FUEL TUBE SEAL GASKET. REPLACED THE SEAL GASKET AND FOUR BOLTS FOR RIGHT HAND ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SEAL — DAMAGED (NR 1 SPOILER)

LAX - INFLIGHT T192/20 AFTER TAKEOFF CENTER HYDRAULIC SYSTEM QUANTITY WENT TO ZERO WITH R/F SHOWING CENTER SYSTEM PRESSURE LIGHT ILLUMINATED. RETURNED TO LAX AND LANDED WITHOUT INCIDENT. REPLACED NUMBER 1 SPOILER FILTER SEAL. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

AFW - EMERGENCY EXIT LIGHT ON RIGHT SIDE OF BUSINESS CLASS SEATS AND OVERHEAD INOPERATIVE. REPLACED BATTERY AND BATTERY CHARGER FOR EMERGENCY EXIT LIGHTS ON RIGHT SIDE OF BUSINESS CLASS SEATS AND OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (L1 DOOR)

SFO - DURING OVERNIGHT MAINTENANCE, EXTERIOR EMERGENCY L1 DOOR LIGHT INOPERATIVE. REPLACED EXTERIOR EMERGENCY LIGHT SOCKET AT L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT AT 26H INOPERATIVE. SECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 26H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DISCONNECTED (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 34H INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT SEAT 23H IS INTERMITTENT. RE-SECURED CONNECTOR AT FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FMC — FAILED (E/E BAY)

DFW - FLT 48 - LT FMC FAIL MESSAGE APPEARED ON CLIMB-OUT. PULLED AND RESET FMC CB-E9 AS PER ABNORMAL PROCEDURE. NO EFFECT SELECTED ALT AND FMC AND GOT DISPLAY BACK. REPLACED LT FMC COMPUTER. OPS CHECK OK AS PER MM 34-61-01-4. (M)

Part: WIRE — SHORTED (CABIN)

LAX - DURING OVERNIGHT NAINTENANCE, EMERGNECY EXIT ESCAPE PATH LIGHTS FROM SEAT 2AB TO 9AB INOPERATIVE. REPAIRED WIRE AT SEAT 3AB. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: FLOORBEAM — CORRODED (BS 791)

AFW - FLOORBEAM AT LBL 33, STATION 791 HAD CORROSION BLENDED BEYOND SRM LIMITS. REMOVE CORROSION PER REF /D/. VERIFY CRACK FREE ROTOPEEN, APPLY ALODINE AND TWO COATS PRIMER TO BLENDED AREA. FILL BLENDED AREA WITH BMS5-95. RETURN TO SERVICE WITH NOTED CONDITION. (M)

Part: FLOORBEAM — CORRODED (BS)

FLOORBEAM AT STATION 347 HAS CORROSION REMOVAL ON UPPER SURFACE BEYOND SRM LIMITS. REMOVED CORROSION PER REF D, VERIFY CRACK FREE. APPLY ALODINE AND TWO COATS PRIMER TO BLENDED AREA. FILL BLEND WITH BK155-95. RETURN TO SERVICE WITH NOTED CONDITION. (M)

Part: FLOORBEAM — CORRODED (BS 798)

AFW - FLOORBEAM AT RBL 11, STATION 798 HAD CORROSION BLENDED ON TOP SURFACE BEYOND SRM LIMITS. REMOVE CORROSION PER REF /D/ AND ENSURE CORROSION HAS BEEN COMPLETELY REMOVED. ROTO PEEN, APPLY ALODINE AND 2 COATS PRIMER TO BLEND AREA. FILL BLENDED AREA WITH BMS5-95. RETURN TO SERVICE WITH NOTED CONDITION. (M)

Part: FLOORBEAM — CORRODED (BS 1480)

AFW - FLOORBEAM AT STATION 1480 HAD CORROSION BLENDED BEYOND SRM LIMITS. REMOVED CORROSION PER REF /D/. VERIFY CRACK FREE. APPLY ALODINE AND TWO COATS PRIMER TO BLENDED AREAS. FILL BLENDED AREAS WITH BMS5-95. RETURN TO SERVICE WITH NOTED CONDITION. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

FLOORBEAM AT STATION 764 HAD TWO AREAS OF CORROSION BLENDED BEYOND SRM LIMITS. REMOVED CORROSION PER REF D. VERIFY BLENDED AREA IS CRACK FREE. APPLIED ALODINE, TWO COATS OF PRIMER TO BLENDED AREA. FILL BLENDS WITH BMS5-95. RBL 33 FABRICATE REPAIR STRAP OUT OF 301.5H STAINLESS STEEL, .050 INCH THICK. ALODINE ALL BARE ALUMINUM SURFACES. FINISH BLENDS AND REPAIR PARTS WITH 2 COATS BMS10-11 PRIMER CPN 4026120. FILL BLENDS WITH BMS 5-92. CPN 5796546. INSTALL REPAIR STRAP WET WITH BMS5-95 SEALANT, PROSEAL 870. FASTENER LOCATIONS AND SHAPE OF REPAIRS STRAP MAY VERY. (M)

Part: FLOORBEAM — CORRODED (BS 767)

AFW - FLOORBEAM AT STATION 764 HAD CORROSION BLENDED UNDER SPLICE PLATE BEYOND LIMITS. REMOVE CORROSION PER REF /D/. ENSURE CORROSION HAS BEEN COMPLETELY REMOVED. APPLIED ALODINE AND TWO COATS OF PRIMER TO ALL BARE SURFACES. FILL BLENDED AREA WITH BMS5-95 SEALANT. RETURN TO SERVICE WITH NOTED CONDITION. (M)

Part: CONNECTOR — BROKEN (ROW 22H AND 31H)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATHWAY LIGHTS AT SEATS 22H AND 31H INOPERATIVE. REPLACED BROKEN CONNECTOR PINS TO EMERGENCY EXIT PATHWAY LIGHTS AT SEATS 22H AND 31H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (ROW 34H)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT PASSENGER SEAT 34H INOPERATIVE. MAINTENANCE FOUND A LOOSE CONNECTOR. RESECURED LOOSE CONNECTOR TO EMERGENCY EXIT LIGHTS AT PASSENGER SEAT 34H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SOCKET — DEFECTIVE (ROW 40 B)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT AT SEAT 40B INOPERATIVE. REPLCED EMERGENCY EXIT PATH LIGHT SOCKET AT SEAT 40B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — CHAFED (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHTS FROM SEAT ROW 32B TO 42B INOPERATIVE. REPAIRED WIRE AT LAMP SOCKET AT SEAT ROW 39B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 20H INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 20H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: IDG — FAILED (LT ENGINE)

MIA - FLT 0998 - TWO HOURS INTO FLIGHT, THE LEFT GENERATOR DRIVE LIGHT FLICKERED SEVERAL TIMES WITH A FLICKERING STATUS MESSAGE FOLLOWED IMMEDIATELY BY THE DRIVE LIGHT STEADY. LEFT GENERATOR DROPPED OFF-LINE. REF 24-1 AUTH 2-465DC-B DEF. LT ENG GEN AS INOP PER MEL SVCD. BOTH ENG IDG'S AND APU OIL - ENTERED IN MIC SHEET. T/S AND REPLACED LEFT ENG IDG. OPS CHECK GOOD UNDER FULL ELECTRICAL LOAD. NO LEAKS FOUND. CLEARED MIC SHEET AND REMOVED MEL PLACARD. (X)

Part: IDG — FAILED (LT ENGINE)

GRU - FLT 0007 - IDG DRIVE LIGHT ILLUMINATED, EICAS, LT GENERATOR DRIVE. DISCONNECTED LT IDG. DEFERRED LT IDG INOPERATIVE PER MEL. MPM 24-1 ACCOMPLISHED AND FOUND OIL LEVEL OK. MIC SHEET ENTERED. MEL 24-1 AUTH 1-97DC-B. INSTALLED AND SERVICED NEW LT IDG PER M LEAKS. CKS GOOD. OPS CKS NORMAL. REMOVED MEL DEV 1-97DC-B. CLEARED MIC SHEET. (X)

Part: FUSE — FAILED (POWER SUPPLY)

MAI - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR LIGHTS AT SEAT ROW 1J TO 9J INOPERATIVE. REPLACED FUSE IN EMERGENCY POWER SUPPLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT PASSENGER SEAT ROW 39H FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR AT PASSENGER SEAT ROW 39H. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)

Part: EEL — INTERMITTENT (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT PASSENGER SEAT ROW 16B FOUND INTERMITTENT. REPLACED EMERGENCY FLOOR LIGHTS AT PASSENGER SEAT ROW 16B. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)