N39365

Part: TERMINAL — DISCONNECTED (EMERGENCY LIGHT) · airframe 111,673 hrs · 18,137 cycles

LEFT OVERWING EMERGENCY EXIT IDENTIFIER AT ROW 21A WOULD NOT TEST. FOUND IDENTIFIER, L00978, DISCONNECTED AT TERMINAL D11734. SECURED IAW WDM 33-51-14 & PERFORMED OPERATIONAL CHECK IAW AMM 33-51-09. SYS CHECKED NORMAL.

Part: SLIDE — UNLACED (R2 DOOR) · airframe 111,643 hrs · 18,130 cycles

MCM 0917 R2 DOOR SLIDE UNLACING. REPLACED DOOR SLIDE R2. THE ACFT WAS NOT GNDED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 110,703 hrs · 17,970 cycles

EXTERIOR EMER EXIT LIGHT AT R1 DOOR INOPERATIVE. RELAMPED R1 DOOR EMER LIGHT IAW AMM 33-51-03. OPERATIONS CHECKED GOOD.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 109,996 hrs · 17,851 cycles

AFT CARGO COMPARTMENT INTERCOSTAL BETWEEN FS 1285 & 1307 AT RBL 20 IS CRACKED IN BEND RADIUS. R & R INTERCOSTAL IAW AARD 53-60-53-1.

Part: CONTROL VALVE — FAULTY (AC BAY) · airframe 109,438 hrs · 17,757 cycles

AIR INTERRUPT, RETURNED & EMER DECLARED. LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB FLIGHT ATTENDANTS REPORTED VISUAL SMOKE IN CABIN & FLIGHT CREW OBSERVED, R ENG BLEED OFF, EICAS MSG DISPLAYED INTERMITTENTLY. ACCOMPLISHED WC 05-96-70 & PACK BURN IAW AMM 21-00-21. SYS CHECKS NO ODOR. R & R RT PACK FLOW CONTROL VLV. PERFORMED OPERATIONAL CHECK IAW AMM 21-51-01. SYS CHECKED NORMAL.

Part: DENSITOMETER — FAULTY (FUEL SYSTEM) · airframe 109,110 hrs · 17,707 cycles

AIR INTERRUPT, EMER DECLARED & LANDING UNEVENTFUL. ACFT WAS OVERWEIGHT. LT MAIN TANK FUEL QTY INDICATOR & TOTALIZER INDICATED 2700 POUNDS LOW. FLIGHT CREW ELECTED TO DIVERT, PROBLEM CORRECTED ITSELF PRIOR TO LANDING. FQIS PROCESSOR RECORDED D1, LT MAIN TANK DENSITOMETER, FAULT. R & R LT MAIN TANK DENSITOMETER IAW 28-41-03-004 & 28-41-00-404. SYS CHECKED NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 108,427 hrs · 17,595 cycles

RIGHT WING SLIDE GND ILLUMINATION LIGHT L391 INOPERATIVE. R & R BATTERY CHARGER AT M733 IAW WDM 33-51-21. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 108,134 hrs · 17,547 cycles

LEFT NR 4 DOOR EXIT IDENTIFIER INOPERATIVE. REPLACED LAMP FOR LT NR 4 DOOR EXIT IDENTIFIER. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 108,134 hrs · 17,547 cycles

RIGHT NR 1 DOOR EMER EXIT IDENTIFIER SIGN HAS INOPERATIVE. REPLACED LAMP FOR RT NR 1 EMER EXIT IDENTIFIER SIGN. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 108,134 hrs · 17,547 cycles

LEFT NR 4 DOOR EMER EXIT IDENTIFIER SIGN INOPERATIVE. REPLACED LAMP FOR LT NR 4 DOOR EMER EXIT IDENTIFIER SIGN. OPERATIONS CHECKED NORMAL.

Part: CONTACT — DIRTY (EXTERIOR LIGHT) · airframe 108,134 hrs · 17,547 cycles

RIGHT EXTERIOR EMER LIGHT AFT OF WING INOPERATIVE. CLEANED CONTACTS. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 106,943 hrs · 17,343 cycles

RIGHT NR 1 DOOR EXTERIOR EMER LIGHT INOPERATIVE. REPLACED LAMP FOR RT NR 1 DOOR EXTERIOR EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 106,411 hrs · 17,270 cycles

LEFT NR 4 UPPER AFT EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LAMP FOR LT NR 4 UPPER AFT EMERGENCY EXIT LIGHT. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 106,411 hrs · 17,270 cycles

RIGHT NR 1 DOORWAY EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RT NR 1 DOORWAY EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 106,411 hrs · 17,270 cycles

EMERGENCY LIGHT AT SEAT 40H INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 40H. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 106,411 hrs · 17,270 cycles

RIGHT NR 4 LOWER AFT EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LAMP FOR RT NR 4 LOWER AFT EMERGENCY EXIT LIGHT. OPERATIONS CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 105,988 hrs · 17,190 cycles

RIGHT AFT FUSELAGE GND SCAN EMERGENCY LIGHT INOPERATIVE. REPLACED M00733 POWER SUPPLY. OPERATIONS CHECKED NORMAL.

Part: RIB — CRACKED (NR 2 SPOILER) · airframe 105,050 hrs · 17,029 cycles

NR 2 SPOILER RIB SUPPORT WAS FOUND CRACKED. REPLACED NR 2 SPOILER RIB IAW EA B767-57-033149 & SRM 57-70-02.

Part: LATCH — UNSERVICEABLE (CABIN) · airframe 105,050 hrs · 17,029 cycles

RT HAND OFF WING ESCAPE SLIDE LATCH TORQUE EXCEEDS LIMITS DURING ACCOMPLISHMENT OF PATTERN CARD 1934. R & R THE TWO AFT LATCHES. COMPLETED INSTALLATION OF ALL FOUR LATCHES IAW AMM 25-65-09-404-007.

Part: SLIDE — DAMAGED (CABIN) · airframe 105,050 hrs · 17,029 cycles

LT HAND OVERWING SLIDE DAMAGED FROM INTERFERENCE RUBBING IN COMPARTMENT. INSTALLED REPLACEMENT SLIDE. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 105,050 hrs · 17,029 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 104,638 hrs · 16,970 cycles

RT SIDE AFT FUSELAGE EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RT SIDE AFT FUSELAGE EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.

Part: LENS — CRACKED (CABIN) · airframe 103,830 hrs · 16,844 cycles

LT FORWARD OVERWING ESCAPE HATCH EMERGENCY LIGHT MARKER LENS CRACKED. REPLACED LENS FOR LT FORWARD OVERWING ESCAPE HATCH LIGHT. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 103,830 hrs · 16,844 cycles

LT FS AFT SLIDE WING GROUND ILLUMINATION EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LT OVERWING SLIDE AFT FLOODLIGHT. OPERATIONS CHECKED NORMAL.

Part: LENS — CRACKED (CABIN) · airframe 103,830 hrs · 16,844 cycles

EMERGENCY LIGHT EXIT MARKER LENS CRACKED AT LT NR 2 DOOR UPPER FORWARD CORNER. REPLACED LT NR 2 EMERGENCY EXIT MARKET LENS. OPERATIONS CHECKED NORMAL.

Part: FITTING — WORN (LT WING) · airframe 99,308 hrs · 16,136 cycles

LEFT WING INBOARD SIDE FAILSAFE WING FITTING HAS WEAR. INSTALLED DOUBLER PER EA B767-57-016371.

Part: ROLLER TRAY — CRACKED (CARGO BAY) · airframe 99,308 hrs · 16,136 cycles

ROLLER TRAY 3D IN FORWARD CARGO CRACKED. REPLACED ROLLER TRAY.

Part: ROLLER TRAY — CRACKED (CARGO BAY) · airframe 99,308 hrs · 16,136 cycles

ROLLER TRAY 3B IN FORWARD CARGO CRACKED. REPLACED ROLLER TRAY.

Part: WEB — CRACKED (LT PLYON) · airframe 99,308 hrs · 16,136 cycles

LEFT PYLON UPPER WEB CRACKED AT INTEGRATED DRIVE GENERATOR FEEDER CABLE THRU HOLE. INSTALLED DOUBLER REPAIR PER AARD 54-52-01-1.

Part: ROLLER TRAY — CRACKED (CARGO BAY) · airframe 99,308 hrs · 16,136 cycles

ROLLER TRAY C2 IN AFT CARGO IS CRACKED. REPLACED ROLLER TRAY.

Part: WEDGE — DEBONDED (LE SLAT) · airframe 99,308 hrs · 16,136 cycles

NUMBER 11 SLAT TRAILING EDGE WEDGE HAS DISBOND. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-10.

Part: WEDGE — DEBONDED (LE SLAT) · airframe 99,308 hrs · 16,136 cycles

NUMBER 12 SLAT TRAILING EDGE WEDGE HAS DISBOND. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-10-2R-4.

Part: SKIN — DELAMINATED (ELEVATOR) · airframe 99,308 hrs · 16,136 cycles

DELAMINATION ON TOP SIDE OF ELEVATOR. ACCOMPLISHED HOTBOND REPAIR PER SRM 55-20-01.

Part: FILLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,308 hrs · 16,136 cycles

LAVATORY PAN FILLER FAIRING CORRODED. REPLACED FILLER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 97,500 hrs · 15,841 cycles

EMERGENCY LIGHT ON SEAT 22HJ INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22HJ. OPS CHECK NORMAL.

Part: SIGN — INOPERATIVE (CABIN) · airframe 97,500 hrs · 15,841 cycles

EMERGENCY SIGN AT LEFT NUMBER 1 DOOR INOPERATIVE. REPLACED EMERGENCY SIGN ASSEMBLY AT LEFT NUMBER DOOR 1. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 97,500 hrs · 15,841 cycles

EMERGENCY LIGHT AT SEAT 22B INOPERATIVE. REPLACED LAMP FOR SEAT 22B EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 97,500 hrs · 15,841 cycles

EMERGENCY LIGHT AT SEAT 18AB INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT 18AB. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 97,083 hrs · 15,779 cycles

EMERGENCY LIGHT AFT OF RIGHT NUMBER 4 DOOR ENTRY WAY INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AFT OF RIGHT NUMBER 4 DOOR ENTRY WAY. OPS CHECK NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 97,083 hrs · 15,779 cycles

EMERGENCY LIGHTS IN 1ST CLASS FROM 2AB TO 10AB INOPERATIVE. RESEATED BATTERY PACK FOR EMERGENCY LIGHTS IN FIRST CLASS FROM 1AB TO 10AB. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 97,083 hrs · 15,779 cycles

AFT RIGHT NUMBER 4 DOOR EMERGENCY LIGHTS ON EXIT SIGN INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 4 DOOR EMERGENCY EXIT SIGN. OPS CHECK NORMAL.

Part: LENS — MISSING (CABIN) · airframe 97,083 hrs · 15,779 cycles

RED EMERGENCY LIGHT LENS MISSING AT FORWARD OVERWING DOOR. REPLACED RED EMERGENCY LIGHT LENS AT FORWARD OVERWING DOOR. OPS CHECK NORMAL.

Part: MODULE — FAULTY (RUDDER) · airframe 96,262 hrs · 15,662 cycles

MIA - CREW REPORTED DURING TAKEOFF EXCESSIVE RIGHT RUDDER TRIM AND EICAS MESSAGE LEFT FUEL LOW PRESSURE LIGHT ILLUMINATED. FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT AND RIGHT RUDDER RATIO MODULES. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FMC — INOPERATIVE (LEFT) · airframe 95,401 hrs · 15,532 cycles

JFK - INFLIGHT DFW-MAD. CREW REPORTED DURING FLIGHT EQUIPMENT COOLING OVERHEAT MESSAGE FOLLOWED BY LEFT HAND FLIGHT MANAGEMENT COMPUTER UNABLE TO RESPOND. EMERGENCY DECLARED FLIGHT DIVERTED JFK LANDED WITHOUT INCIDENT. REPLACED LEFT FMC. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: MODULE — FAULTED (RUDDER) · airframe 95,146 hrs · 15,492 cycles

JFK - CREW REPORTED EICAS MESSAGE FOR RUDDER RATIO WITH LIGHT AND AILERON LOCKOUT MESSAGE WITH LIGHT. EMERGENCY DECLARED FLIGHT RETURNED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED BOTH SAMS M525 AND M524. ALSO REPLACED LEFT AIR DATA COMPUTER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,873 hrs · 15,280 cycles

FOUND CORROSION TO THE FUSELAGE SKIN INNER SURFACE BETWEEN STATIONS 1087 TO 1093 AND STRINGERS 39 LEFT TO 39 RIGHT. THE CORROSION WAS BLENDED AWAY AND EXTERNAL DOUBLERS WERE INSTALLED PER EA 767-53-014915.

Part: FRAME — DENTED (FUSELAGE) · airframe 93,873 hrs · 15,280 cycles

DENT DAMAGE TO THE STATION 500 FUSELAGE FRAME INNER CHORD BETWEEN STRINGERS 30 TO 31 LEFT. DAMAGE REPAIRED ON EA B767-53-014931.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,873 hrs · 15,280 cycles

SEAT TRACK 146T5217-4 REPLACEMENT DUE TO CORROSION FROM STATIONS 1210 TO 1427. REPLACED SEAT TRACK.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,853 hrs · 15,275 cycles

STATION 347 FLOOR BEAM AT RIGHT BUTTLINE 30 UPPER CHORD CORRODED. REPAIRED DISCREPANCY PER EA 767-53-014761.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 92,637 hrs · 15,053 cycles

EMERGENCY LIGHT WILL NOT ILLUMINATE AT EXTERIOR RIGHT NUMBER 4 DOOR. REPLACED LAMP FOR EXTERIOR RIGHT NUMBER 4 EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: PROCESSOR — FAULTY (FUEL SYSTEM) · airframe 91,533 hrs · 14,846 cycles

JFK - INFLIGHT LHR-DFW. CREW REPORTED AIRCRAFT LOST ALL FUEL QUANTITY INDICATORS. FUEL QUANTITY PANEL WAS ALL BLANKS EXCEPT FUEL TEMP. EMERGENCY DECLARED DIVERTED JFK LANDED WITHOUT INCIDENT. REPLACED FUEL QUANTITY INDICATING SYSTEM PROCESSOR AND FLIGHT DECK INDICATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: DECODER — INOPERATIVE (CABIN) · airframe 91,317 hrs · 14,809 cycles

BOS - FLIGHT ATTENDANTS OBSERVED AN ELECTRICAL ODOR IN CABIN AT ROW 25. PILOTS PULLED THE ENTERTAINMENT SYSTEM CIRCUIT BREAKER ON OVERHEAD PANEL AND SMELL DISSIPATED. FLIGHT LANDED BOS WITHOUT INCIDENT. FOUND CIRCUIT BREAKER FOR AFT COLUMN TIME DECODER POPPED. RESET CIRCUIT BREAKER. FOUND CALL LIGHTS FROM SEATS 29CEG TO LAST ROW IN COACH INOPERATIVE. REPLACED OVERHEAD DECODER AT 29CEG. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: WIRE HARNESS — DEFECTIVE (CABIN) · airframe 91,183 hrs · 14,783 cycles

MIA - FLIGHT ATTENDANTS REPORTED SMOKE IN THE CABIN. CREW DESCENDED TO 8000 FT SMOKE DISAPPEARED AND REOCCURED SEVERAL TIMES DURING CABIN FIRE CHECK LIST AND SMOKE REMOVAL CHECK LIST. EMERGENCY DECLARED LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED POWERPORT HARNESS AT ROWS 20 AND 24.

Part: HYDRAULIC LINE — LEAKING (ZONE 200) · airframe 90,795 hrs · 14,706 cycles

GIG - CREW REPORTED LEFT HYDRAULIC QUANTITY DROPPED TO .04 (LOST ALL FLUID) AFTER TAKEOFF. EMERGENCY DECLARED RETURNED GIG LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND POWER CONTROL ACTUATOR HOSE FROM RUDDER RATIO CHANGER ACTUATOR WITH HEAVY LEAKING. REPLACED POWER ACTUATOR HOSE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: O-RING — DAMAGED (HYDRAULIC SYS) · airframe 90,092 hrs · 14,580 cycles

ORD - CAPTAIN REPORTED LOST RIGHT HYDRAULIC SYSTEM QUANTITY AND PRESSURE. EMERGENCY DECLARED, RETURNED ORD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND THE RIGHT HYDRAULIC SYSTEM LATERAL CENTRAL CONTROL ACTUATOR LEAKING AT CAP. REMOVED AND REPLACED O-RING. REMOVED AND REPLACED RIGHT ENGINE CASE DRAIN FILTER AND RIGHT ENGINE DRIVEN HYDRAULIC PUMP. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PRESSURE SWITCH — INOPERATIVE (LT ENGINE) · airframe 88,583 hrs · 14,311 cycles

EZE - CREW REPORTED RUDDER RATIO LIGHT ILLUMINATED WITH STRONG CROSS WINDS. RETURNED EZE WITHOUT INCIDENT. REPLACED PRESSURE SWITCH ON LEFT ENGINE DRIVEN PUMP CASE DRAIN FILTER MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: HYDRAULIC LINE — LEAKING (LT ENGINE) · airframe 88,301 hrs · 14,262 cycles

ORD - CREW RECEIVED STATUS MESSAGE OF LOW HYDRAULIC FLUID QUANTITY. EMERGENCY DECLARED, LANDED ORD WITHOUT INCIDENT. FOUND LEFT ENGINE HYDRAULIC LEAK. REPLACED LEFT ENGINE HYDRAULIC LINE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 88,280 hrs · 14,258 cycles

CORROSION WAS FOUND UNDER AND AROUND THE RIGHT WING UPPER SKIN ATTACH POINT COMMON TO OSS 644. THE ATTACH POINT WAS REMOVED AND ALL CORROSION WAS BLENDED AWAY PER 767-300 SRM 57-20-01-1A. THE BLENDED AREA MEASURES APPROX 5 INCHES BY 3.7 INCHES WITH A MINIMUM REMAINING THICKNESS OF 0.202. ACCOMPLISHED A HIGH FREQUENCY EDDY CURRENT INSPECTION. THE BLENDED AREA WAS ROTO-PEENED, ALODINED AND PRIMED. BOEING APPROVED THIS BLEND AS A CATAGORY A REPAIR.

Part: MODULE — LEAKING (HYDRAULIC SYS) · airframe 88,280 hrs · 14,257 cycles

DFW - AIRCRAFT RETURNED TO DFW DUE TO LOSS OF CENTER HYDRAULIC SYSTEM. AIRCRAFT REMOVED FROM SERVICE. REPLACED ENGINE DRIVEN PUMP MODULE IN LEFT WHEEL WELL. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PROCESSOR — FAILED (FUEL QTY) · airframe 85,717 hrs

BOS INFLIGHT JFK TO FCO - CREW REPORTED FUEL QUANTITY INDICATIONS WENT BLANK. LANDED BOS WITHOUT INCIDENT. REPLACED FUEL QUANTITY PROCESSOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (CABIN) · 84,832 cycles

ORD EMERGENCY LIGHT AT MID GALLEY LT HAND SIDE INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT MID GALLEY LT HAND SIDE. SYSTEM GROUND CHECKED NORMAL OPS.

Part: CONNECTOR — LOOSE (CABIN) · airframe 84,439 hrs

MIA - EMERGENCY LIGHTS AT MID GALLEY INOPERATIVE. SECURED CONNECTION FOR EMERGENCY LIGHTS AT MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

MIA - SEAT MOUNTED EMERGENCY LIGHTS FROM SEAT ROWS 2HJ TO 6HJ INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FROM SEAT ROWS 2HJ TO 6HJ. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS)

SFO - EMERGENCY FLASH LIGHT AT LEFT AFT FLIGHT ATTENDANT BULKHEAD JUMPSEAT INOPERATIVE. REPLACED BATTERY FOR EMERGENCY FLASH LIGHT AT LEFT AFT FLIGHT ATTENDANT BULKHEAD JUMPSEAT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT 13H INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 13H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHTS AT LEFT AND RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT LEFT AND RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT OVERHEAD ROW 39 RIGHT SIDE INOPERATIVE. RELAMPED OVERHEAD EMERGENCY LIGHT AT ROW 39 RIGHT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHTS AT SEAT 3H INOPERATIVE. REPLACED WALL TO SEAT HARNESS CONNECTOR FOR EMERGENCY LIGHTS AT SEAT 3H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT BETWEEN ROWS 10H AND 23H INOPERATIVE. SECURED CONNECTOR FOR BATTERY PACK FOR EMERGENCY LIGHTS BETWEEN ROWS 10H AND 23H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SUPPORT FITTING — CORRODED (WING)

AFW - LEFT AND RIGHT HAND WING TRUNNION BEARING SUPPORT FITTINGS HAD CORROSION UNDER HAT BUSHING LANDINGS. LEFT HAND WING FITTING LOWER AND UPPER HOLE. RIGHT HAND WING FITTING LOWER HOLE. PERFORMED HIGH FREQUENCY EDDY CURRENT INSPECTION FOR CRACKS. ROTO PEENED MACHINED AREA AND APPLIED ALODINE AND TWO COATS OF PRIMER. MACHINED NEW BUSHINGS WITH THICKER HAT TO ADJUST FOR MATERIAL REMOVED. CAD PLATE BUSHINGS AND INSTALL BUSHINGS WET WITH BMS595. FILLET SEAL AROUND BUSHING WITH BMS595. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

JFK - EMERGENCY LIGHT IN COCKPIT OVER DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT IN COCKPIT OVER DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY LIGHT IN COCKPIT INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY IN COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — DISCONNECTED (CABIN)

SFO - EMERGENCY LIGHTING AT SEATS 32H TO 41H INOPERATIVE. RECONNECTED SOCKET WIRES AT ROW 35 FOR EMERGENCY LIGHTING AT SEATS 32H TO 41H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

JFK - RIGHT AFT CABIN SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR RIGHT AFT CABIN SEAT MOUNTED EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

JFK - EMERGENCY LIGHT FROM SEAT ROW 32H TO 40H INOPERATIVE. REPLACED TWO EACH BATTERY PACKS FOR EMERGENCY LIGHTS FROM SEAT ROW 32H TO 40H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

JFK - EMERGENCY LIGHTS FROM ROW 31H BACK OF AIRCRAFT INOPERATIVE. REPLACED BATTERY PACK AND CHARGER ASSEMBLY M739 FOR EMERGENCY LIGHTS AT ROW 31H TO BACK OF AIRCRAFT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PIN — BENT (BATTERY PACK)

CDG - EMERGENCY EXIT LIGHTS AT SEAT 40HJ INOPERATIVE. FOUND BENT PIN ON BATTERY PACK M734. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHTS AT SEAT 40HJ. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — INOPERATIVE (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHTS AT ROWS 32 TO 40 INOPERATIVE. REPAIRED WIRING AT ROW 38H BATTERY PACK FOR EMERGENCY LIGHTS AT ROWS 32 TO 40. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — BROKEN (EMERGENCY LIGHT)

SFO - CEILING EMERGENCY EXIT LIGHT AT MID GALLEY RIGHT INOPERATIVE. REPAIRED BROKEN WIRES IN FORWARD CARGO PIT CEILING FOR CEILING EMERGENCY EXIT LIGHTS AT MID GALLEY RIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — DISCONNECTED (CABIN)

SFO - EMERGENCY ESCAPE PATH LIGHT IN FIRST CLASS GALLEY INOPERATIVE. FOUND WIRING FOR LIGHT WRAPPED AND STOWED BEHIND RIGHT SIDE FLOOR GRILL. ROUTED AND CONNECTED WIRING TO EMERGENCY LIGHT AT FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (EXTERIOR)

SFO - RIGHT HAND EMERGENCY LIGHT ABOVE AFT WING AND EXTENDING TO BODY FAIRINGS INOPERATIVE. CLEANED CONTACTS AND RELAMPED. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FITTING — LEAKING (LT HYD SYSTEM)

LOST LT HYDRAULIC SYSTEM QUANTITY. STOPPED LOSS AT .48 BY TURNING OFF LT PUMPS IAW PROCEDURE. RETURNED AND LANDED WITHOUT INCIDENT. REPLACED LEAKING CENTER RUDDER RATION SERVO FITTING AND SERVICED LT HYDRAULIC SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — CRACKED (NR 2 PYLON)

AFW - FOUND NR 2 ENGINE INBOARD SIDE PYLON TORQUE BOX AREA FOUND CRACK EXTENDING FROM ACCESS HOLE AFT. DAMAGED SKIN AREA REMOVED REPAIRED PER SRM REPAIR 54-52-01-2. (M)

Part: SLIDE — DEPLOYED (CABIN)

DURING TAXI TO THE GATE, FLIGHT ATTENDENT INADVERTENTLY DEPLOYED THE RIGHT NR 1 DOOR SLIDE. SLIDED DEPLOYMENT WAS SUCCESSFUL. REPLACED RIGHT NR 1 DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING OVERNIGHT MAINTENANCE FOUND SLIDE LIGHT AT L2 DOOR, INOPERATIVE. REPLACED BATTERY PACK FOR SLIDE LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTS AT 2-11H INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGHTS BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: IDG — MALFUNCTIONED (LT ENGINE)

HNL - INITIATED ABORT AT 110 KTS AT HNL, DUE OT LEFT GEN DRIVE LIGHT ILLUMINATED. PEAK A/S DURING ABORT WAS APPROX 120 KTS OUTSIDE AIR TEMP WAS 29 DEGREES CELSIUS. BITE CHECKED BPCU, SERVICED LEFT ENGINE IDG, ENG RUN AND OPS CHECK NORMAL. (M)

Part: DOOR LATCH — DEFECTIVE (LT WING SLIDE)

SFO - DURING OVERNIGHT MAINTENANCE, LEFT WING SLIDE DOOR WOULD NOT OPEN. REPLACED DOOR LATCH. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: CONNECTOR — DAMAGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE SEAT PATH LIGHT AT SEAT 34A INOPERATIVE. REPLACED EMERGENCY EXIT ESCAPE SEAT PATH LIGHT CONNECTOR AT SEAT 34A. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT PATH LIGHTS AT SEAT 36B INOPERATIVE. RECONNECTED EMERGENCY EXIT SEAT PATH LIGHT CONNECTOR. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: WIRE — BROKEN (SEAT 40)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT SEAT 40H HAD BROKEN WIRE AT CONNECTOR. REPAIRED EMERGENCY EXIT SEAT LIGHT CONNECTOR AT SEAT 40H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: WIRE — CHAFED (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHTS ON BUSINESS CLASS GALLEY WALL INOPERATIVE. REPAIRED WIRING TO EMERGENCY EXIT LIGHTS ON BUSINESS CLASS GALLEY WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT ASSY — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED RIGHT OVERWING EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: IDG — FAILED (RT ENGINE)

DFW - FLT 0049 - RIGHT GENERATOR DRIVE LIGHT ON AND EICAS RIGHT GENERATOR DRIVE DISCONNECTED RIGHT GENERATOR DRIVE. TROUBLESHOT, FOUND OIL PRESSURE FAULTED. REPLACED RIGHT ENGINE IDG. ACCOMPLISHED CARD 4944. RAN ENGINE, LEAK CHECK OK. APPROVED FOR SERVICE. 3652406CE/1506.10JAN.DFW. (X)

Part: LIGHT — DEFECTIVE (CABIN)

JFK - DURING MAINTENANCE, NR 2 GALLEY EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED NR 2 GALLEY EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: CONNECTOR — BROKEN (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT PASSENGER SEAT 21B FOUND INOPERATIVE. REPLACED BROKEN EMERGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEAT 21B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: CONNECTOR — BROKEN (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 17AB FOUND INOPERATIVE. REPLACED BROKEN EMERGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEAT 17AB. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: FLOOR BEAM — CORRODED (BS 786-848)

AFW - CORROSION ON THE UPPER SURFACE OF TWO MAIN CABIN FLOOR BEAMS. BLEND, SHIM, AND REFINISH PER MRB 767-1120. TST: 32,231.54 HRS. CYCLES, 5,446. (X)

Part: FLOOR BEAM — GOUGED (BS 941)

AFW - FLOOR BEAMS HAVE DEEP GOUGES. BLEND AND REFINISH PER MRB 767-1130. TST: 32,231.54 HRS. CYCLES, 5,446. (X)

Part: FLOOR BEAM — CORRODED (BS 871-928/786)

AFW - CORROSION ON THE UPPER SURFACE OF THE CABIN FLOOR BEAM. BLEND, SHIM, AND PAINT PER MRB 767-1122. TST: 32,231.54 HRS. CYCLES, 5,446. (X)

Part: CONNECTOR — LOOSE (CABIN)

MIA - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT LAST FOUR SEAT ROWS OF AFT CABIN RIGHT SIDE INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT SIDEWALL CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS, BETWEEN SEATS 26H-34H, SEATS 42H-2R DOOR, AND BELOW AFT GALLEY FLIGHT ATTENDANTS SEAT, INOPERATIVE. REATTACHED WIRE BETWEEN SEATS 26H-34H. REPAIRED WIRE ON FLOOR TRACK LIGHTING BETWEEN 42H AND 2R DOOR, AND WIRE AFT OF FLIGHT ATTENDANTS SEATS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, AFT EMERGENCY EXIT FLOOR PATH LIGHTS FOUND INOPERATIVE. SECURED LOOSE CONNECTION AT SEAT ROW 24HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)

Part: EEL CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT FLOOR PATH LIGHTS AT AFT GALLEY PARTITION A6 LAVATORY, AND FWD OF A6 LAVATORY INOPERATIVE. RECONNECTED CONNECTOR AT 41HJ. SYSTEM GROUND CHECKS NORMAL OPERATION. (W)