N362AA

Part: FUEL CONTROL — FAILED (LT ENGINE) · airframe 109,700 hrs · 17,818 cycles

DURING APPROACH LT ENG SPEED REDUCED TO IDLE. EMERGENCY DECLARED, LANDING UNEVENTFUL. TROUBLESHOT FAULT TO FUEL CONTROL UNIT. R & R LT ENGINE FUEL CONTROL IAW WC 73-94-02. PERFORMED OPERATIONAL & LEAK CHECKS IAW WC 71-95-20. SYS CHECKED NORMAL. REPEATED DURING TAXI AFTER MX.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 108,724 hrs · 17,636 cycles

CORROSION WAS FOUND IN THE FORM OF BULGING FASTENERS COMMON TO THE FUSELAGE SKIN AT APPROX STATION 1197+128 & STRINGER 37 LT. REPAIRED DAMAGE IAW EA 53-038771 & SRM 53-00-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 108,689 hrs · 17,625 cycles

EMERGENCY LIGHT LENS AT LT MID GALLEY INOPERATIVE. RELAMPED IAW AMM 33-51-012. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 108,689 hrs · 17,625 cycles

SEAT 11H OVERHEAD EMER LIGHT INOPERATIVE. RELAMPED SEAT 11H OVERHEAD EMER LIGHT IAW MM 33-51-05. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 107,592 hrs · 17,448 cycles

SEAT MOUNTED ESCAPE PATH EMER EXIT LIGHT AT 35B INOPERATIVE. REPLACED LIGHT ASSEMBLY OF SEAT MOUNTED ESCAPE PATH LIGHT AT 35B. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 107,592 hrs · 17,448 cycles

CEILING MOUNTED ESCAPE PATH EMER EXIT LIGHT ABOVE SEAT 22B INOPERATIVE. REPLACED LAMP FOR CEILING MOUNTED EMER EXIT LIGHT ABOVE SEAT 22B. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 106,779 hrs · 17,321 cycles

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

Part: LENS — MISSING (CABIN) · airframe 106,779 hrs · 17,321 cycles

EMERGENCY LIGHT AT SEAT 31B MISSING LENS. REPLACED LENS FOR EMER LIGHT AT SEAT 31B. OPERATIONS CHECKED NORMAL.

Part: ATTACH FITTING — CRACKED (LT PYLON) · airframe 106,779 hrs · 17,321 cycles

LEFT PYLON NAC 285 OTBD FRAME, UPPER ATTACH CLIP IS CRACKED. REPLACED CLIP IAW SRM 51-00-05 REPAIR 1.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 105,394 hrs · 17,102 cycles

LT HAND EXTERNAL EMERGENCY LIGHT AFT OF WING INOPERATIVE. REPLACED LAMP FOR LT HAND EXTERNAL EMERGENCY LIGHT AFT OF WING, OPERATIONS CHECKED NORMAL.

Part: INDICATOR — LEAKING (HYDRAULIC SYS) · airframe 102,558 hrs · 16,658 cycles

CREW REPORTED LT HYD SYS PRESSURE EICAS MESSAGE FOLLOWED BY LT HYD QTY MESSAGE. EMERGENCY DECLARED, FLIGHT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED LEAKING DIFFERENTIAL PRESSURE INDICATOR ON INBD SIDE OF LT HYD FILTER MODULE. SYS GROUND CHECK NORMAL OPERATION. (CLOSED)

Part: CIRCUIT BREAKER — DAMAGED (COCKPIT) · airframe 101,310 hrs · 16,456 cycles

SFO - INFLIGHT DFW-HNL. CREW REPORTED DURING FLIGHT BATTERY BUSS DISTRIBUTION CIRCUIT BREAKER LOCATED ON THE P-6-1 PANEL POPPED. FLIGHT DIVERTED SFO LANDED WITHOUT INCIDENT. FOUND BREAKER C-829 OUT AND SHOWED SIGNS OF DAMAGE. REPLACED CIRCUIT BREAKER C829. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: ACTUATOR — INOPERATIVE (AC PACK) · airframe 101,078 hrs · 16,415 cycles

ORD INFLIGHT RDU-LHR. CREW REPORTED RIGHT PACK FAILED DURING CRUISE. FLIGHT DIVERTED ORD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT PACK EXHAUST ACTUATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: IDG — OVERHEATED (LT ENGINE) · airframe 100,344 hrs · 16,296 cycles

JFK - CREW REPORTED LEFT ENGINE GENERATOR FAILED. EMERGENCY DECLARED FLIGHT RETURNED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. TROUBLESHOOTING REVEALED INTEGRATED DRIVE GENERATOR OVERHEATED. REPLACED IDG. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 97,893 hrs · 15,914 cycles

RIGHT AFT FUSELAGE EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP. OPS CHECKED NORMAL.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 97,893 hrs · 15,914 cycles

LEFT AFT FUSELAGE EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP. OPS CHECKED NORMAL.

Part: ROLLER TRAY — DAMAGED (ZONE 100) · airframe 97,440 hrs · 15,844 cycles

ROLLER TRAY 1269 DAMAGED. REPLACED ROLLER TRAY 1269.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 97,440 hrs · 15,844 cycles

INTERCOSTAL FROM BS 742 TO 764 RBL 40 CRACKED. REPLACED INTERCOSTAL PER SRM 51-40-02.

Part: ROLLER TRAY — DAMAGED (ZONE 100) · airframe 97,440 hrs · 15,844 cycles

ROLLER TRAY 1266 DAMAGED. REPLACED ROLLER TRAY 1266.

Part: ROLLER TRACK — CRACKED (ZONE 100) · airframe 97,440 hrs · 15,844 cycles

A-2 ROLLER TRACK HAS A EDGE CRACK ON INBOARD FLANGE AT FORWARD END. REPLACED A-2 ROLLER TRACK PER SRM 51-40-02.

Part: FRAME — CRACKED (ZONE 400) · airframe 97,440 hrs · 15,844 cycles

RIGHT PYLON FRAME ON INBOARD SIDE AT STATION 285 FOUND CRACKED. REPLACED FRAME PER SRM 51-40-02.

Part: WEB — CRACKED (LT NACELLE) · airframe 97,440 hrs · 15,844 cycles

LEFT PYLON FORWARD UPPER WEB CRACKED. INSTALLED DOUBLER PER AARD 54-52-01-1.

Part: CONNECTOR — LOOSE (ENGINE IND) · airframe 97,436 hrs · 15,840 cycles

CREW REPORTED LEFT HAND ENGINE EXHAUST GAS TEMPERATURE EICAS DISPLAY AND STANDBY INDICATOR WENT BLANK AND THEN STARTED TO FLUCTUATE. EMERGENCY DECLARED FLIGHT DIVERTED AND LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. RECONNECTED LOOSE CONNECTOR BACKSHELL D4208P. SYSTEM GROUND CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 97,313 hrs · 15,819 cycles

EMERGENCY LIGHT AT SEAT 3H INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 3H. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 97,313 hrs · 15,819 cycles

EMERGENCY LIGHT AT RIGHT NUMBER 1 DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER 1 DOOR. OPS CHECK NORMAL.

Part: FUEL FILTER — INOPERATIVE (LT ENGINE) · airframe 93,176 hrs · 15,158 cycles

HNL - INFLIGHT OGG-LAX. CREW REPORTED LEFT ENGINE FUEL FILTER EICAS MESSAGE ILLUMINATED. FLIGHT DIVERTED HNL LANDED WITHOUT INCIDENT. REPLACED LEFT ENGINE FUEL FILTER. SYSTEM GROUND CHECK NOMAL OPERATION.

Part: WEDGE — DEBONDED (LE SLAT) · airframe 92,972 hrs · 15,125 cycles

NR 10 SLAT T/E WEDGE IS DISBONDED ON THE AFT I/B CORNER. CUT OUT IS 7 X 3 INCHES, DATA CONCERNING THIS REPAIR HAS BEEN ENTERED INTO THE MAJOR REPAIR TRACKING REPORT, DO NOT RE-ENTER THIS REPAIR.

Part: SUPPORT — CORRODED (SPOILER) · airframe 92,961 hrs · 15,123 cycles

NUMBER 2 SPOILER SUPPORT TORQUE TUBE BUSHING HOLE, MOST INBOARD HAD CORROSION INSIDE BORE. ACCOMPLISHED REPAIR PER EA 013354.

Part: STRAP — CRACKED (FUSELAGE) · airframe 92,972 hrs · 15,125 cycles

THE FLOORBEAM STABILIZATION STRAP AT STATION 347 RIGHT BUTTLINE 39 CRACKED ON THE FORWARD EDGE OF THE FLOORBEAM. WHEN THE FORWARD GALLEY IS INSTALLED, IT IS NOT POSSIBLE TO REMOVE AND INSTALL THE BLIND OR SOLID FASTENERS WHEN ACCOMPLISHING THE SRM REPAIR. ENGINEERING ISSUED THIS EA TO INSTALL A REPAIR STRAP FABRICATED FROM 7075-T6 AND ATTACHED TO THE ORIGINAL SECTIONS OF THE STABILIZATION STRAP WITH 3M EC-3333 STRUCTURAL ADHESIVE. ACCOMPLISHED REPAIR PER SRM 53-00-51-2R.

Part: BUSHING — MIGRATED (SPOILER) · airframe 92,972 hrs · 15,125 cycles

MAINTENANCE FOUND A MIGRATED BUSHING COMMON TO THE LEFT WING NUMBER SPOILER CENTER INBOARD HINGE. ACCOMPLISHED REPAIR PER EA 013354.

Part: SILL — CORRODED (CARGO DOOR) · airframe 92,961 hrs · 15,123 cycles

SURFACE CORROSION WAS FOUND ON THE FORWARD CARGO DOOR LOWER SILL OUTER CHORD VERTICAL FLANGE INBOARD SURFACE BETWEEN STATIONS 568 TO 570. ACCOMPLISHED REPAIR PER EA 013166.

Part: FMC — INOPERATIVE (LEFT) · airframe 91,284 hrs · 14,851 cycles

LAX - INFLIGHT ORD-HNL. CREW REPORTED LEFT FLIGHT MANAGEMENT COMPUTER FAILED INFLIGHT. FLIGHT DIVERTED LAX LANDED WITHOUT INCIDENT. REPLACED THE LEFT FLIGHT MANAGEMENT COMPUTER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS)

DFW - AFT LEFT DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT AFT LEFT DOOR.

Part: FAN — INOPERATIVE (CARGO BAY) · airframe 87,036 hrs · 14,137 cycles

YQX - INFLIGHT LHR-BOS. CARGO DETECTED AIR STATUS MESSAGE APPEARED DURING FLIGHT. EMERGENCY DECLARED, LANDED YQX WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER 1 AND 2 FORWARD CARGO DETECTION FANS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BPCU — FAILED (ZONE 100) · airframe 86,078 hrs

JFK - INFLIGHT, CREW REPORTED LEFT BUSS CIRCUIT BREAKER POPPED FOLLOWED BY THE WEATHER RADAR, LEFT FLIGHT DIRECTOR, ACARS, UPPER EICAS AND AUTO THROTTLE GOING OUT. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. REPLACED THE BUSS POWER CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PROCESSING UNIT — MALFUNCTIONED (FUEL SYSTEM) · airframe 83,855 hrs

LHR INFLIGHT T049/13MAY CDG TO DFW - CREW REPORTED RIGHT QUANTITY AND TOTAL QUANTITY BLANKED OUT WITH FUEL IMBALANCE INDICATION. LANDED LHR WITHOUT INCIDENT. REPLACED FUEL QUANTITY PROCESSOR UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

MIA - EMERGENCY LIGHTS AT SEAT ROWS 32H TO 41H AND CEILING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 32H TO 41H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SKIN — CORRODED (BS 448 S34L) · corrosion level 2

AFW - FUSELAGE SKIN AT STATION 448 AND STRINGER 34 LEFT HAD MINOR CORROSION ON INNER SURFACE. MATERIAL REMAINING IS BEYOND SRM LIMITS. BLEND IS 0.6 INCH BY 0.3 INCH AND 0.011 INCH DEEP. CONFIRMED SURROUNDING STRUCTURE WITHIN A 22 INCH RADIUS FROM CENTER OF BLEND OUT IS CORROSION AND DAMAGE FREE. PERFORMED A 10X VISUAL INSPECTION OF THE BLENDOUT TO ENSURE COMPLETE CORROSION REMOVAL. PERFORMED SURFACE HIGH FREQUENCY EDDY CURRENT INSPECTION OF THE BLEND OUT TO ENSURE CRACK OR DAMAGE FREE. APPLIED ALODINE TO ALL BARE SURFACES THEN APPLIED TWO COATS OF BMS 10-11 TYPE 1 PRIMER AND ALLOWED DRY TIMES BETWEEN COATS.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS)

MIA - EMERGENCY LIGHT AT SEAT 3B OVERHEAD INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 3B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LAX - CROSS AISLE EMERGENCY FLOOD LIGHT INOPERATIVE. REPLACED BATTERY PACK M1210 FOR INOPERATIVE CROSS AISLE EMERGENCY FLOOD LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LAX - EMERGENCY EXIT FLOOD LIGHT AT AFT RIGHT AND LEFT EXIT INOPERATIVE. REPLACED BATTERY PACK M1210 FOR EMERGENCY EXIT FLOOD LIGHTS AT AFT RIGHT AND LEFT EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LAX - EMERGENCY SEAT MOUNTED LIGHTS ON RIGHT SEAT ROWS 25 TO 31 INOPERATIVE. REPLACED BATTERY PACK M1209 FOR EMERGENCY SEAT MOUNTED LIGHTS ON RIGHT SEAT ROWS 25 TO 31. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ATTACH FITTING — CRACKED (SPOILER HINGE)

AFW - NUMBER TWO SPOILER OUTBOARD HINGE ATTACH FITTING HAS SMALL CRACK ON LOWER OUTBOARD LEG. AREA OF CRACK IS 0.5 INCH BY 0.2 INCH WITH AT DEPTH OF 0.2 INCH. CRACK LENGTH IS 0.5 INCH. BLEND/ROUTE OUT CRACK. PERFORMED HIGH FREQUENCY EDDY CURRENT TO VERIFY AREA IS CRACK FREE. FABRICATED REPAIR FITTING FROM 7075T6A. REFINISHED ALL BARE ALUMINUM SURFACES WITH ALODINE AND TWO COATS BMS1011 PRIMER. INSTALLED REPAIR WET WITH BMS595 USING 3/16 INCH HI-LOKS. REPLACE HINGE FITTING AT NEXT MAIN BASE VISIT NOT TO EXCEED 24 MONTHS. REFERENCE TFI 362575AD5. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LAX - LEFT AFT EXTERIOR EMERGENCY LIGHTS INOPERTIVE. REPLACED BATTERY PACK FOR LEFT AFT EXTERIOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY ESCAPE FLASH LIGHT INOPERATIVE AT AFT FLIGHT ATTENDANT SEAT. REPLACED BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SOCKET — INOPERATIVE (EMERGENCY LIGHT)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 12B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SOCKET AT SEAT 12B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FAILSAFE — CORRODED (FUSELAGE)

AFW - FOUND LOWER MAIN SILL FAIL SAFE CHORD HAS CORROSION REMOVAL ON UPPER SURFACE AS SHOWN ON SKETCH. REMOVED ALL CORROSION PER 767 SRM. REPLACED BOLT BACB30NN, COUNTERSINK WITH BACB30N, PROTRUDING HEAD. INSTALL BOLTS WET USING BMS 5-95 SEALANT. ROTO-PEEN BLENDED SURFACE. ALODINE AND PRIME BLENDED AREA. (M)

Part: WIRE — INOPERATIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 9 H INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT SEAT 9 H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DAMAGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 9H INOPERATIVE. REPLACED EMERGENCY LIGHT CONNECTOR AT SEAT 9H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SHUTOFF VALVE — DEFECTIVE (NR 1 ENGINE)

LT ENGINE HIGH PRESSURE SHUTOFF VALVE ILLUMINATED DURING CRUISE. AIRCRAFT RETURNED TO LAX ACCOMPLISHED OVERWEIGHT LANDED WITHOUT INCIDENT. ACCOMPLISHED OVERWEIGHT INSPECTION AND REPLACED NR 1 ENGINE HIGH PRESSURE CONTROL VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — DAMAGED (CABIN)

LAX - DURING OVERNIGHT, MAINTENANCE EMERGENCY EXIT LIGHT AT SEAT 39H INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT SEAT 39H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SOCKET — DAMAGED (CARGO DOOR)

SFO - DURING OVERNIGHT MAINTENANCE, RIGHT SIDE EMERGENCY EXIT LIGHT AT AFT CARGO DOOR INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT CONTACT AT AFT CARGO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONTACTOR — DIRTY (RT OVERWING)

LAX - DURING OVERNIGHT MAINTENANCE, RIGHT SIDE OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED RIGHT SIDE OVERWING EMERGENCY EXIT BULB CONTACT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

SFO - FOUND DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AFT RIGHT SIDE INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT WIRE RIGHT SIDE AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: VIDEO UNIT — DEFECTIVE (CABIN)

LHR - FLT 136 - EN ROUTE LAX-LHR, DURING CRUISE, FIRST CLASS OVERHEAD PROJECTOR BEGAN MAKING A LOUD POPPING SOUND AFTER WORKING FINE FOR 20 MINUTES. FLASHES OF LIGHT WERE SEEN IN HOUSING. FLIGHT ATTENDANTS REPORTED AN ODOR. POWER SUPPLY WAS REMOVED. LANDED LHR WITHOUT INCIDENT. FIRST CLASS PROJECTOR REPLACED BY RCI. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — MISINSTALLED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT PATH LIGHTS ON LEFT SIDE COACH INOPERATIVE. REWIRED EMERGENCY EXIT SEAT PATH LIGHTS ON LEFT COACH. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: WIRE — SHORTED (ROWS 25 AND 30)

SFO - DURING OVERNIGHT MAINTENANCE, LEFT SIDE COACH EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED WIRES TO EMERGENCY EXIT LIGHTS AT 25 AND 30. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: FAN — FAILED (E/E BAY)

LHR - FLT 104 - DURING CRUISE, FLIGHT ATTENDANT NOTED A ELECTRICAL BURNING SMELL IN THE FORWARD CABIN AND AN UNUSUAL NOISE FROM SEAT ROW 2HJ. AIRCRAFT LANDED LHR WITHOUT INCIDENT. MAINTENANCE FOUND THE EQUIPMENT COOLING FAN OVERHEATING. REPLACED EQUIPMENT COOLING FAN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT 30HJ INOPERATIVE. RECONNECTED SEAT 30HJ CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: GCU — MALFUNCTIONED (RT SYSTEM)

RTY - FLT 2101 - AT 330, 1 HR IN-FLIGHT, RT GEN CONTACTOR R-BUS. R-BUS TIE ISO AND UTILITY BUS LIGHTS ILLUMINATED. CYCLED RT GEN AND RESTORED BUS, BUT ISO LIGHT AND UTILITY BUS LIGHTS REMAINED ON. HELP FROM TECH SUPPORT, ISOLATED THE PROB TO THE GALLEY. PULLED GALLEY FWD/MID CB AND RESET UTILITY BUSES. WORKED FINE FOR 30 MINUTES. NEXT, THE RT UTILITY BUS WAS LEFT OFF AND THE RT GEN CONT AND BUS TIE SWITCHES. WORKED 5 MINTUES. BITE OF BPCU/SHOWED DP TRIP AND RT MAIN BUS OVERLAP ZONE. ACCOMPLISHED T/S CHECKS PER MM REF 24-20-00-1. ALL CKS NORMAL. INSP IDG HARNESS FROM IDG TO ENG FIRE WALL. NO DEFECTS FOUND. REPLACED RT GCU, RT IDG, RT BUS TIE BREAKER (C904) AND THE BPCU. ALL CKS NORMAL. (X)

Part: ROD — FAILED (RT MLG BRAKE)

GRU FLT 0998 - AFTER TAKEOFF, GEAR DISAGREE AND GEAR DOOR MESSAGE APPEARED ON EICAS ALONG WITH UNSAFE GEAR AND GEAR DOOR LIGHTS ILLUMINATED. AIRCRAFT AIR INTERRUPTED AND RETURNED GRU AND LANDED OVERWEIGHT WITHOUT FURTHER INCIDENT. OVERWEIGHT LANDING INSPECTION ACCOMPLISHED WITH NO DAMAGE NOTED. HIGH ENERGY STOP INSPECTION ACCOMPLISHED WHICH REVEALED DAMAGE TO NR 8 MLG HYDRAULIC LINE, BRAKE AND WHEEL ASSEMBLIES DUE TO A FAILED BRAKE ROD RETAINING BOLT AND PIN. REPLACED MLG WHEEL/BRAKE ASSEMBLIES, BRAKE ROD/PIN, AND BRAKE HYDRAULIC LINE. SYSTEM GROUND AND LEAKED CHECKED NORMAL OPERATION. (X)

Part: FIRE LOOP — MALFUNCTIONED (RT ENGINE)

FRA - FLT 0070 - RIGHT ENGINE FIRE LOOP NR 1 EICAS MESSAGE APPEARED INTERMITTENTLY. PERFORMED ENGINE FIRE LOOP TEST. TESTS OK. (X)

Part: BATTERY — DISCHARGED (BATTERY COMPT)

JFK - MAIN BATTERY CHARGER, EICAS MSG IN CRUISE. REPLACED MAIN BATTERY CHARGER AND MAIN BATTERY. ACCOMPLISHED SYSTEM CHECK PER MM. SYSTEM OPS CHECKS NORMAL. (M)

Part: BATTERY CHARGER — FAILED (BATTERY COMPT)

JFK - MAIN BATTERY CHARGER, EICAS MSG IN CRUISE. REPLACED MAIN BATTERY CHARGER AND MAIN BATTERY. ACCOMPLISHED SYSTEM CHECK PER MM. SYSTEM OPS CHECKS NORMAL. (M)

Part: IDG — FAILED (LT ENGINE)

ORD - FLT 41 - LEFT GENERATOR DRIVE AND LEFT GENERATOR OFF. DISCONNECTED LEFT GENERATOR AFTER FLICKERING IN FLIGHT. DRIVE LIGHT WAS FLICKERING FOR 10 MINUTES BEFORE IT WAS MANUALLY DISCONENCTED. CHANGED LEFT IDG PER MM. OPS CHECK NORMAL, NO LEAKS. (M)

Part: IDG — FAILED (LT ENGINE)

IN CLIMB-OUT AT 280, LEFT GEN DRIVE LIGHT CAME ON. DRIVE WAS DISCONNECTED IAW OPS MANUAL. LEFT ENGINE IDG INOP AS PER MEL 24-1 AUTH 4-139DC-B, ENTERED IN MIC. REPLACED LT IDG, CHECKS OK ON RUN UP, LEAK CHECKS OK. REMOVED PLAC 4-139DC-B CLEARED MIC. (M)

Part: OXY GENERATOR — NOT ARMED (MID-LAVS)

SFO - DURING OVERNIGHT CHECK, WHILE GAINING ACCESS TO CEILING MOUNTED LAVATORY OXYGEN MODULES DURING FCD ACCOMPLISHMENT, OXYGEN GENERATORS AT M-1 AND M-2 MID CABIN LAVATORIES WERE FOUND WITH WARNING FLAGS AND SAFETY PINS INSTALLED. REMOVED WARNING FLAGS AND SAFETY PINS AT M-1 AND M-2 LAVATORIES. ACCOMPLISHED OXYGEN MODULE DOOR TEST WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)