N382AN

Part: LENS — DETACHED (EXIT SIGN) · airframe 93,301 hrs · 15,181 cycles

AIRCRAFT NOT GROUNDED. EMERGENCY EXIT SIGN LENS COVER OVER L1 DOOR DETACHED. REINSTALLED LENS COVER IAW AMM 33-51-01. OPERATIONAL CHECK GOOD.

Part: LENS — UNSECURE (EMERGENCY LIGHT) · airframe 93,276 hrs · 15,174 cycles

L1 DOOR EMERGENCY EXIT SIGN LENS FELL OFF. SECURED EXIT SIGN LENS IAW 33-51-01. OPERATIONAL CHECK GOOD.

Part: LENS — DETACHED (EXIT SIGN) · airframe 93,233 hrs · 15,160 cycles

AIRCRAFT NOT GROUNDED. L1 DOOR EMERGENCY EXIT SIGN LENS DETACHED. INSTALLED LENS IAW AMM 33-51-09. OPERATIONAL CHECK GOOD.

Part: LIGHT — DAMAGED (SEAT 25B) · airframe 92,625 hrs · 15,033 cycles

EMERGENCY LIGHT AT SEAT 25B DAMAGED. REMOVED AND REPLACED THE LIGHT ASSEMBLY IAW AMM 33-51-10. OPS CHECKED NORMAL.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 91,940 hrs · 14,895 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT NOT OVERWEIGHT. DURING APPROACH WHEN FLAPS 25 SELECTED RECEIVED AN EICAS L/E SLAT DISAGREE MESSAGE. MAINTENANCE ACCOMPLISHED SFCU BITE, OPS AND FUNCTIONAL CHECK OF FLAPS AND SLATS IAW AMM 27-51-00 WITH NO FAULTS FOUND.

Part: ACTUATOR — LEAKING (NR 1 SPOILER) · airframe 90,793 hrs · 14,616 cycles

RIGHT HYD QTY EICAS MSG, QUANTITY LIGHT ON, QUANTITY DECREASED TO .38 RF. SECURED LT ENG & LT ELEC PUMPS TO SAVE FLUID FOR LANDING. FLIGHT DECLARED AN EMER & LANDED WITHOUT FURTHER INCIDENT. R & R NR 1 SPOILER PCA IAW MM 27-61-02. OPERATIONALLY CHECKED GOOD, LEAK CHECKED GOOD. THE ACFT WAS GNDED.

Part: SENSOR — FAULTY (LE FLAP) · airframe 89,947 hrs · 14,438 cycles

HAD LE FLAP ASYMMETRY AFTER TAKEOFF. PERFORMED CHECKLIST & RETURNED. DECLARED EMER & OVERWEIGHT LANDING WITHOUT INCIDENT. ACFT TAKEN OUT OF SERVICE. REPLACED NR 10 OTBD SLAT SENSOR S296 IAW AMM 27-88-01. ADJUSTED GAP & TESTED OK IAW AMM 27-88-01.

Part: CABLE — DAMAGED (ZONE 800) · airframe 89,947 hrs · 14,438 cycles

LEFT HATCH OVERWING, DOOR STEP UNABLE TO DEPLOY DUE TO DAMAGED SUPPORT CABLES. R & R SUPPORT CABLES & RESEALED IAW SRM 51-40-02 & MM 51-31-01.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 89,437 hrs · 14,349 cycles

L1 DOOR EMER EXIT LIGHT INOPERATIVE. R & R POWER SUPPLY M1208 IAW AMM 33-51-07. SYS CHECKED NORMAL.

Part: PSEU — FAILED (ZONE 100) · airframe 89,327 hrs · 14,332 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB, CREW REPORTED LE SLAT ASYMMETRY MSG & LE LIGHT ON WHEN FLAPS RETRACTED FROM 1DG TO UP. R & R PSEU IAW AMM 32-09-04. SYS CHECKED NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 88,967 hrs · 14,259 cycles

SEATS 32AB TO 39AB EMER LIGHTS INOPERATIVE. FOUND LOOSE CONNECTOR ON SEAT 40B FOR THE ESCAPE PATH EMER LIGHT. SECURED CONNECTOR & PERFORMED OPERATIONAL CHECK IAW AMM 33-51-10. SYS CHECKED NORMAL.

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 88,093 hrs · 14,121 cycles

DURING CLIMB CREW REPORTED OF A VIOLENT SHAKE & LOUD BANG. DURING RETURN APPROACH CREW REPORTED UNUSUAL FLIGHT CHARACTERISTICS WHEN FLAPS SELECTED TO 30. NORMAL FLIGHT CHARACTERISTICS REGAINED WHEN FLAPS SELECTED TO 25. RETURNED TO DEPARTURE, EMERGENCY DECLARED. R & R RT ENGINE. POWER PLANT ENGINEERING REPORTS NO FAILURES FOUND.

Part: LEVER — OUT OF RIG (ZONE 800) · airframe 87,540 hrs · 14,020 cycles

FORWARD RT EMER EXIT DOOR AUTO ARMING SWITCHES LEVER ASSEMBLY OUT OF RIG. CROSSBAR MOVED SWITCHES UP INTO FIRING POSITION WHEN DISABLE HANDLE WAS MOVED UP TO ARM POSITION, CAUSING SLIDE TO DEPLOY. SLIDE DEPLOYED SUCCESSFULLY. ADJUSTED SHORT EYEBOLT ON STRAIGHT PIN BRACKET ASSEMBLY. CHECKED DISABLE HANDLE TO ENSURE ARMING SWITCHES STAYED DOWN & EMER EXIT DOOR TO ENSURE STRIKER PIN PUSHED AUTO ARM & AUTO FIRE SWITCHES UP. SYS CHECKED NORMAL.

Part: LENS — MISSING (CABIN) · airframe 87,334 hrs · 13,989 cycles

EGRESS SEAT 22H LENS MISSING. REPLACED LENS IAW AMM 33-51-10. OK FOR CONTINUED SERVICE.

Part: LENS — MISSING (CABIN) · airframe 87,334 hrs · 13,989 cycles

EGRESS SEAT 30B LENS MISSING. REPLACED LENS IAW AMM 33-51-10. OK FOR CONTINUED SERVICE.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 86,607 hrs · 13,859 cycles

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

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 85,398 hrs · 13,666 cycles

BOTH EMER PATH SIGNS FWD OF 20CEG ARE INOPERATIVE. R & R LIGHT ASSEMBLY. OPERATIONS CHECKED NORMAL.

Part: LENS — MISSING (CABIN) · airframe 85,398 hrs · 13,666 cycles

OVERHEAD EMER LIGHT AT SEAT 26G MISSING LENS. REPLACED LENS FOR OVERHEAD EMER LIGHT AT SEAT 26G. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 85,398 hrs · 13,666 cycles

EMERGENCY LIGHT AT SEAT 22H INOPERATIVE. REPLACED LAMP & RESEATED CONNECTOR TO LUMINESCENCE FOR EMER LIGHT AT SEAT 22H. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 85,398 hrs · 13,666 cycles

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

Part: CHARGER — INOPERATIVE (CABIN) · airframe 84,936 hrs · 13,598 cycles

RIGHT FUSELAGE EXTERNAL EMERGENCY LIGHT L644 FWD AFT CARGO DOOR INOPERATIVE. REPLACED CHARGER. OPERATIONS CHECKED NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 84,936 hrs · 13,598 cycles

RIGHT FUSELAGE EXTERNAL EMER LIGHT FWD AFT CARGO DOOR INOPERATIVE. REPLACED CHARGER M733 FOR RT FUSELAGE EXTERNAL EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 84,936 hrs · 13,598 cycles

LEFT BULKHEAD LOWER CROSS AISLE LIGHT FWD OF SEAT 20C INOPERATIVE. REPLACED LAMP FOR LT BULKHEAD LOWER CROSS AISLE LIGHT FWD OF SEAT 20C. OPERATIONS CHECKED NORMAL.

Part: LENS — MISSING (CABIN) · airframe 84,936 hrs · 13,598 cycles

SEAT MOUNTED EMER LIGHT AT 35H MISSING LENS. REPLACED LENS FOR SEAT MOUNTED EMER LIGHT AT 35H. OPERATIONS CHECKED NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 84,936 hrs · 13,598 cycles

RIGHT EMER LIGHT L392 AFT DOOR EXTERNAL LIGHT IS INOPERATIVE. REPLACED CHARGER M733. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 84,936 hrs · 13,598 cycles

SEAT MOUNTED EMER LIGHT AT SEAT 36B INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR SEAT MOUNTED EMER LIGHT AT SEAT 36B. OPERATIONS CHECKED NORMAL.

Part: LENS — MISSING (CABIN) · airframe 84,501 hrs · 13,529 cycles

EMERGENCY LIGHT AT SEAT 22H MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 22H, OPERATIONS CHECKED NORMAL.

Part: LENS — MISSING (CABIN) · airframe 84,501 hrs · 13,529 cycles

EMERGENCY LIGHT AT SEAT 22H MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 22H, OPERATIONS CHECKED NORMAL.

Part: LIGHT — DAMAGED (CABIN) · airframe 83,579 hrs · 13,374 cycles

EMERGENCY PATH LIGHTS ABOVE FLOOR LEVEL ON MID GALLEY RT WALL ARE DAMAGED. REPLACED LUMINATOR BASE & REINSTALLED LENS, OPERATIONS CHECKED NORMAL.

Part: LIGHT — DAMAGED (CABIN) · airframe 83,579 hrs · 13,374 cycles

EMERGENCY PATH LIGHTS ABOVE FLOOR LEVEL ON MID GALLEY LT WALL ARE DAMAGED. REPLACED LUMINATOR BASE & INSTALLED LENS, OPERATIONS CHECKED NORMAL.

Part: WIRE — DAMAGED (CABIN) · airframe 83,579 hrs · 13,374 cycles

SEAT 17J SEAT MOUNTED EMERGENCY EXIT PATH LIGHTS INOPERATIVE. REPAIRED WIRING UNDER SEAT, OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 83,165 hrs · 13,303 cycles

EMERGENCY CEILING LIGHT AT ROW 26HJ INOPERATIVE. REPLACED LAMP FOR EMERGENCY CEILING LIGHT AT ROW 26HJ. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 82,676 hrs · 13,226 cycles

SEAT 26H EMERGENCY PATH LIGHT FAILED. REPLACED LAMP FOR SEAT 26H EMERGENCY PATH LIGHT. OPERATIONS CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 82,607 hrs · 13,215 cycles

LT EMERGENCY OVERWING EXIT SLIDE LIGHTS INOPERATIVE. REPLACED POWER SUPPLY M961. OPERATIONS CHECKED NORMAL.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 82,607 hrs · 13,215 cycles

RT EMERGENCY OVERWING EXIT SLIDE LIGHTS INOPERATIVE. R & R POWER SUPPLY M962. OPERATIONS CHECKED NORMAL.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 82,607 hrs · 13,215 cycles

EMERGENCY LIGHTS FROM ROWS 20 THRU 24 LT INOPERATIVE. REPLACED POWER SUPPLY M737. OPERATIONS CHECKED NORMAL.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 82,607 hrs · 13,215 cycles

SEATS 20 & 21 RT EMERGENCY LIGHTS INOPERATIVE. REPLACED M1209 POWER SUPPLY. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 82,462 hrs · 13,196 cycles

RT FUSELAGE EMERGENCY LIGHT ABOVE AFT WING FAIRING INOPERATIVE. REPLACED LAMP FOR RT FUSELAGE EMERGENCY LIGHT ASSEMBLY ABOVE AFT WING FAIRING. OPERATIONS CHECKED NORMAL.

Part: LENS — MISSING (CABIN) · airframe 82,462 hrs · 13,196 cycles

ROW 20H MISSING RED ESCAPE PATH LENS. INSTALLED NEW RED ESCAPE PATH LENS FOR ROW 20H. OPERATIONS CHECKED NORMAL.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 82,045 hrs · 13,124 cycles

EMERGENCY EXIT LIGHT DIM. REPLACED LIGHT ASSEMBLY FOR EMERGENCY EXIT LIGHT. OPERATIONS CHECKED NORMAL.

Part: DUCT — LEAKING (RT PYLON) · airframe 79,399 hrs · 12,697 cycles

JFK INFLIGHT RDU-LHR. FLIGHT CREW REPORTED RIGHT STRUT DUCT LEAK MESSAGE ON EICAS AFTER TAKEOFF. EMERGENCY DECLARED FLIGHT DIVERTED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED DUCT AND WHEEL WELL FIRE CARD M691. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 79,285 hrs · 12,683 cycles

LEFT NUMBER 1 EMERGENCY EXIT SIGN HANDLE ILLUMINATION LIGHTS INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 1 EMERGENCY EXIT SIGN HANDLE ILLUMINATION LIGHT. OPS CHECK NORMAL.

Part: UNION — LEAKING (RT MLG WW) · airframe 79,245 hrs · 12,677 cycles

MIA - CREW REPORTED CENTER HYDRAULIC SYSTEM QUANTITY LOSS. EMERGENCY DECLARED FLIGHT LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND LEAK IN RIGHT WHEEL WELL FITTING ON LANDING GEAR SELECTOR VALVE. REPLACED UNION. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — DENTED (FUSELAGE) · airframe 76,904 hrs · 12,305 cycles

DENT TO FUSELAGE SKIN AT STATION 450 BETWEEN STRINGERS 30 AND 31 RIGHT. INSTALLED FLUSH DOUBLER PER SRM 53-00-01-2R-6.

Part: ACTUATOR — INOPERATIVE (RUDDER) · airframe 76,886 hrs · 12,300 cycles

LHR - CREW REPORTED RUDDER RATIO ANNUNCIATOR AND EICAS MESSAGE DISPLAYED DURING CRUSE FLIGHT. EMERGENCY DECLARED FLIGHT LANDED LHR WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RUDDER RATIO CHANGER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 76,366 hrs · 12,213 cycles

EMERGENCY LIGHT ABOVE SEAT 13H INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT ABOVE SEAT 13H. OPS CHECKED NORMAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 75,813 hrs · 12,122 cycles

STATION 271 BETWEEN STRINGERS 21 AND 22 RIGHT DAMAGED. ACCOMPLISHED DOUBLER REPAIR PER SRM 53-00-01-2R6.

Part: CONNECTOR — OUT OF POSITION (CABIN) · airframe 74,754 hrs · 11,953 cycles

SEAT ROW 33AB EMERGENCY EXIT LIGHT INOPERATIVE. FOUND CONNECTOR MISPLACED. REFITTED CONNECTOR FOR EMERGENCY LIGHT AT SEAT ROW 33AB. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,187 hrs · 11,723 cycles

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

Part: HOSE — LOOSE (AC BAY) · airframe 72,553 hrs · 11,616 cycles

DFW - CREW REPORTED LEFT HAND PACK FAILED IN FLIGHT. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND HOSE BETWEEN PACK PRECOOLER AND LOW LIMIT VALVE LOOSE. RE SECURED HOSE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 71,649 hrs · 11,463 cycles

FOUND CRACK ON FORWARD CHORD ON RIGHT SIDE AND CURRENTLY ACCOMPLISHING THE PERMANENT REPAIR PER SB FIGURE 7 ON THE RIGHT SIDE ONLY. REMOVE GOUGES SMOOTH PER 767-300 SRM CHAPTER 51 STANDARD PRACTICES AS SHOWN IN FIGURE 1 AND 2. REF: EA B767-53-014036 FOR COMPLETE DETAILED REPAIR INSTRUCTIONS.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,649 hrs · 11,463 cycles

CORROSION TO FUSELAGE SKIN INNER SURFACE BETWEEN STATIONS 1087 TO 1092 AND STRINGER 39 LEFT TO 39 RIGHT. CORROSION WAS BLENDED AWAY. ACCOMPLISHED REPAIR PER EA B767-53-013986.

Part: STRAP — CRACKED (FUSELAGE) · airframe 71,649 hrs · 11,463 cycles

FLOORBEAM STABILIZATION STRAP AT STATION 347 RIGHT BUTTLINE 39 WAS FOUND CRACKED ON FORWARD EDGE OF THE FLOOR BEAM. ACCOMPLISHED GENERAL VISUAL INSPECTION OF THE AREA FOR OTHER DAMAGE. REMOVED STRAP, FABRICATED, TREATED, AND SEALED REPAIR STRAP PER EA B767-53-014114.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 71,649 hrs · 11,463 cycles

FOUND TYPICAL DENT DAMAGE TO STATIONS 478 TO 500, FUSELAGE FRAME INNER CHORD BETWEEN STRINGER 30 LEFT AND 31 LEFT DUE TO IMPACT DAMAGE FROM CARGO PALLETS. COLD WORKED AS BEST POSSIBLE, HIGH FREQUENCY EDDY CURRENT SURFACE SCAN BOTH SIDES OF REWORKED FLANGE. FABRICATED, TREATED AND SEALED PER EA B767-53-013924.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 71,545 hrs · 11,440 cycles

LEFT AFT ENTRY DOOR EXT EMERGENCY LIGHT INOPERATIVE. REPAIRED LIGHT ASSEMBLY. OPS CHECKS GOOD.

Part: CONNECTOR — LOOSE (RT PYLON) · airframe 70,140 hrs · 11,174 cycles

MAD - CREW REPORTED RIGHT ENGINE FIRE LOOP 2 ILLUMINATED DURING TAKEOFF. OVERHEAT LOOP 1 ON MEL. EMERGENCY DECLARED FLIGHT RETURNED MAD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. RE-SECURED LOOSE CONNECTOR D4145P ON PYLON. PRECAUTIONARY CHANGE OF HARNESS (FBD1543503) AND HARNESS (FBD1542503) DUE HISTORY OF DETECTOR CHANGES. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,581 hrs · 11,074 cycles

EMERGENCY EXIT LIGHTS LEFT SIDE FROM AFT OF 17B TO 24B OUT. REPLACED BATTERY PACK AT 23B FOR EMERGENCY EXIT LIGHTS. OPS CHECKED NORMAL.

Part: CONNECTOR — LOOSE (ANIT-ICE VALVE) · airframe 69,395 hrs · 11,045 cycles

FRA - CREW REPORTED LEFT ENGINE ANTI-ICE EICAS MESSAGE (ENGINE *VALVE* LIGHT) AFTER TAKEOFF. EMERGENCY DECLARED RETURNED FRA LANDED WITHOUT INCIDENT. FOUND CONNECTOR ON ENGINE ANTI-ICE VALVE LOOSE, CLEANED CONNECTOR, RETORQUED, RAN OPERATIONAL TEST OF ENGINE ANTI-ICE VALVE AND OPERATION NORMAL. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: ACTUATOR — LEAKING (SPOILER) · airframe 66,827 hrs · 10,593 cycles

LAX INFLIGHT DFW-OGG. CREW REPORTED CENTER HYDRAULIC FLUID LOSS INDICATION. LANDED LAX WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEAKING NUMBER NINE SPOILER ACTUATOR. SYSTEM GROUND CHECK NORMAL OPERATION. (CLOSED)

Part: LIGHT — INOPERATIVE (SEAT 6H) · 64,470 cycles

JFK EMERGENCY LIGHT AT SEAT 6H INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 6H. SYSTEM GROUND CHECKED NORMAL OPS.

Part: LIGHT — DAMAGED (LAVATORY) · airframe 63,913 hrs

MIA EMERGENCY LIGHT MID NR 1 LAVATORY DAMAGED. REPLACED BASE FOR EMERGENCY LIGHT AT MID NR 1 LAVATORY. SYS GROUND CHECKED NORMAL OPS. (CLOSED)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)

MIA - EMERGENCY EXIT LIGHT AT RIGHT SIDE AFT CABIN INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT LIGHT AT RIGHT SIDE AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: VALVE — INOPERATIVE (HYD SYSTEM)

AUA INFLIGHT T929/16SEP MIA TO GRU - CENTER HYDRAULIC SYSTEM QUANTITY DECREASING. DIVERTED TO AUA AND LANDED WITHOUT INCIDENT. REPLACED VALVE FOR CENTER HYDRAULIC SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

SFO - EMERGENCY EXIT LIGHT AT RIGHT HAND FORWARD SERVICE DOOR INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT AT RIGHT FORWARD SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

SFO - EMERGENCY EXIT LIGHT AT LEFT FORWARD SERVICE DOOR INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT AT LEFT FORWARD SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — BROKEN (CABIN)

DFW - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 21B HAS BROKEN SHROUD. REPLACED SHROUD FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 21B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (CABIN)

DFW - EMERGENCY LIGHT AT SEAT 2B HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 2B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FLASHLIGHT — INOPERATIVE (GALLEY)

SFO - EMERGENCY FLASHLIGHT IN AFT GALLEY INOPERATIVE. REPLACED EMERGENCY FLASHLIGHT IN AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — LOOSE (EMERGENCY LIGHT)

FCO - EMERGENCY LIGHT AT MID GALLEY LEFT SIDE FLOOR LEVEL HAS LOOSE LENS. SECURED LENS FROM EMERGENCY LIGHT AT MID GALLEY LEFT SIDE FLOOR LEVEL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS)

MIA - EMERGENCY LIGHTS UNARMED ANNUNCIATOR LIGHT HAS ONE BULB INOPERATIVE. RELAMPED EMERGENCY LIGHT UNARMED ANNUNCIATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: COVER — MISSING (CABIN)

DFW - EMERGENCY LIGHT AT SEAT 3B MISSING LENS COVER. REPLACED EMERGENCY LIGHT LENS COVER FOR SEAT 3B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SOCKET — DAMAGED (EXTERIOR)

DFW - EMERGENCY LIGHT ON OUTSIDE OF LEFT NUMBER 4 DOOR INOPERATIVE. REPAIRED LIGHT SOCKET FOR EMERGENCY LIGHT ON OUTSIDE OF LEFT NUMBER 4 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHTS AT RIGHT HAND SEAT ROW 20 AND 21 INOPERATIVE. REPLACED BATTERY FOR EMERGENCY LIGHTS AT RIGHT HAND SEAT 20 AND 21. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FLOORBEAM — CORRODED (FUSELAGE)

AFW - UPPER SURFACE OF FLOORBEAM AT STATION 325 HAD CORROSION BLENDED BEYOND LIMITS. BLENDS AT RIGHT BUTTLINES 17, 22, 22.5, 26.5, 31, 37.5, 40, 41.5, AND 47. CRITICAL BLENDS AT RIGHT BUTTLINE 17 IS 0.8 INCH IN DIAMETER WITH .048 REMAINING FROM A PARENT THICKNESS OF .085. FABRICATED REPAIR STRAP OUT OF 301 AND ONE HALF H STAINLESS STEEL 0.050 INCH THICK. ALODINE ALL BARE ALUMINUM SURFACES. FINISH BLENDS AND REPAIR PARTS WITH TWO COATS BMS10 11 PRIMER. FILLED BLENDS WITH BMS595 SEALANT. INSTALLED REPAIR STRAP WET WITH BMS595 SEALANT. INSTALLED FASTENERS WITH 46D SPACING.

Part: FLOORBEAM — CORRODED (FUSELAGE)

AFW - UPPER SURFACE OF FLOORBEAM AT STATION 325 HAD CORROSION BLENDED BEYOND SRM LIMITS. BLENDS AT RBL 17, 22, 22.5, 26.5, 31, 35.5, 37.5, 40, 41.5, AND 47. THE CRITICAL BLEND IS AT RBL 17. IT IS 0.8 INCH DIAMETER WITH .048 INCH REMAINING FROM A THICKNESS OF .085 INCH. FABRICATED REPAIR STRAP OUT OF 301 1/2H STAINLESS STEEL 0.050 INCH THICK. ALODINE ALL BARE ALUMINUM SURFACES. FINISH BLENDS AND REPAIR PARTS WITH 2 COATS BMS10 11 PRIMER. FILL BLENDS WITH BMS 5 95 SEALANT. INSTALL REPAIR STRAP WET WITH BMS5 95 SEALANT. FASTENERS TO BE INSTALLED WITH 4 6D SPACING.

Part: FITTING — OVERSIZED (RT PYLON)

AFW - RIGHT HAND PYLON LINK LOWER BEARINGS ON BOTH SIDES LOOSE IN THE LOWER FITTINGS. VISUALLY CHECKED BORE HOLES FOR CRACKS. INSTALLED BEARINGS WET WITH BMS5 26 SEALANT IPC/DRAWING NUMBER 311T2287 14 AND 13.

Part: CONNECTOR — DISCONNECTED (CABIN)

SFO - EMERGENCY PATH LIGHT AT 31B INOPERATIVE. FOUND CONNECTOR AT 31B SIDEWALL DISCONNECTED. RECONNECTED EMERGENCY LIGHT CONNECTOR AT 31B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — LOOSE (SEAT 40D)

SFO - EMERGENCY SEAT MOUNTED AISLE LIGHTING AT SEAT 40D LOOSE. REPLACED NUT PLATE AND LIGHT ASSEMBLY FOR EMERGENCY SEAT MOUNTED AISLE LIGHTING AT SEAT 40D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FAN — INOPERATIVE (AFT CARGO)

ORD - FLT 189 - EN ROUTE BOS-LAX - CARGO COMPARTMENT FIRE DETECTION SYSTEM INOPERATIVE. LANDED ORD WITHOUT INCIDENT. REPLACED AFT CARGO DET FAN 1. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE, OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT SEAT ROWS 22 THROUGH 34. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SHUTOFF VALVE — LOOSE (RT ENGINE)

RT ENGINE HPSOV EICAS MSG APPEARED IN FLIGHT, COMPLIED WITH QRH PROCEDURE. PLACARDED RT ENGINE HI STAGE HPSOV INOPERATIVE PER MEL. VALVE SECURED CLOSED PER MPM 36-02. ENT IN MIC SHEET AUTH 8 463DC. SECURED LOOSE SENSE LINES AT HP CONTROLLER CLEANED AND LUBED POSITION SWITCHES PERFORMED OPERATIONAL CHECK FOND NORMAL RESTORED TO NORMAL CONFIGURATION. (M)

Part: LIGHT — BROKEN (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE LIGHTING AT SEAT 23B BROKEN. REPLACED EMERGENCY ESCAPE LIGHTING ASSEMBLY AT SEAT 23B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, FOUND SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING ASSEMBLY AT SEAT 28H INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING ASSEMBLY AT SET 28H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, FOUND SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING ASSEMBLY AT SEAT 38H INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING ASSEMBLY AT SEAT 38H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

(POWER SUPPLY) DURING OVERNIGHT MAINTENANCE EXTERIOR R1 AND OVERWING EMERGENCY LIGHTING INOPERATIVE. REPLACED EMERGENCY LIGHTING POWER SUPPLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (CABIN)

AFW - FOUND EMERGENCY EXIT SIGNS AT R/2 AND L/2 DID NOT ILLUMINATE DURING SYSTEM TEST. REMOVED AND REPLACED BATTERY PACK. (M)

Part: PUMP — CONTAMINATED (FUEL SYSTEM)

ALL FUEL BOOST PUMPS ON, X-FEEDS CLOSED. FUEL FED FROM BOTH THE MAIN TANKS AND CENTER TANKS. TURNED OFF WD PUMPS, ON MAINS, CENTER TANK PROVIDED ALL FUEL REF ITEMS 62. A/C HAS BEEN INSPECTED AND FOUND TO BE IN SAFE CONDITION FOR FERRY FLIGHT FROM ORD TO AFW FOR FURTHER EVALUATION OF FUEL SYSTEM. THIS FERRY FLIGHT IS AUTHORIZED BY SPOTTING MESSAGE 6-974 DATED 6/15/02. REMOVED DEBRIS FROM CENTER TANK FUEL PUMP PICKUP SCREENS. ACCOMPLISHED ON AFW DROP IN BOW. OPS CHECK AND LEAK CHECKS OF CENTER TANK SYSTEM, CHECKS GOOD. (M)

Part: IDG — FAILED (RT ENGINE)

LHR - FLT 109 - RIGHT GEN DRIVE LIGHT ILLUMINATED 1.5 HOURS INTO FLIGHT ACCOMPLISHED GENERATOR DRIVE DISCONNECT PROCEDURE. REMOVED AND REPLACED RIGHT ENGINE IDG PER MM. ACCOMPLISHED REQUIRED CHECKS TEST GOOD, NO LEAKS NOTED. (M)

Part: CONNECTOR — LOOSE (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LIGHTING AT SEAT 34B INOPERATIVE. SECURED CONNECTOR AT WALL FOR SEAT 34B EMERGENCY ESCAPE PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LIGHTING AT SEAT 34B INOPERATIVE. SECURED CONNECTOR AT WALL FOR SEAT 34B EMERGENCY ESCAPE PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — DAMAGED (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT AT SEAT 34B INOPERATIVE. REPAIRED WIRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: RELAY — FAILED (TE FLAPS)

LAX - LEADING EDGE FLAP ASSY EICAS AND LEADING EDGE LIGHT REMAINED ON AFTER FLAPS SELECTED TO ZERO LE FLAP ASSY. CHECKLIST RUN, FLAPS SELECTED BY ALT MEANS. REMOVED AND REPLACED RELAY K2307, REQUIRES OPS CHECK. ALSO, INSPECTED AND VERIFIED WEAR LIMITS. FOUND WITHIN LIMITS. OPS CHECK NORMAL AS PER MM 27-81-24-6. ACCOMPLISHED OVERWEIGHT LANDING AS PER MM 05-51-35-2. (M)

Part: CONNECTOR — DAMAGED (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 27H INOPERATIVE. REPLACED EMERGENCY EXIT CONNECTOR PIN AT SEAT 27H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT RIGHT OF FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT RIGHT OF FORWARD GALLEY. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: WIRE — BROKEN (ROW 21)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS AT ROW 21 INOPERATIVE. REPAIRED WIRE AT ROW 21. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: RETAINER — BROKEN (WING SLIDE)

SFO - FLT 1539 - LEFT SIDE OFF WING EMERGENCY SLIDE RETAINING BAR BROKEN. REPLACED EMERGENCY SLIDE. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: SOCKET — LOOSE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ON RIGHT SIDE OVERWING EXIT INOPERATIVE. RESECURED LAMP SOCKET WITHIN EMERGENCY EXIT LIGHT ASSEMBLY ON RIGHT SIDE OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLOORBEAM — CORRODED (BS 764)

AFW - FLOORBEAM AT STATION 764 HAS CORROSION REMOVAL ON UPPER SURFACE MATERIAL REMAINING IS BEYOND SRM LIMITS. BLENDED AREA. FABRICATED REPAIR STRAP OUT OF 301.5 HARD STAINLESS STEEL .050 INCH THICK. ALODINED ALL BARE ALUMINUM SURFACES AND FINISHED BLENDS WITH BMS-5-92. INSTALLED REPAIR STRAP WET WITH BMS 5-95 SEALANT. (M)

Part: LIGHT — BROKEN (R1 DOOR)

SFO - DURING OVERNIGHT MAINTENANCE CHECK, EMERGENCY EXIT FLOOD LIGHT IN R1 DOOR INOPERATIVE. REPLACED R1 DOOR EMERGENCY FLOOD LIGHT BASE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SEAT TRACK — CORRODED (BS 343)

AFW - FOUND AND BLENDED OUT CORROSION ON THE UPPER SURFACE OF THE UPPER FLANGE OF THE SEAT TRACK. CUT OUT SIX SETS OF LIPS OF THE TRACK. ALODINED AND PRIMED AFFECTED AREAS. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRR 767-1973. (M)

Part: FAN — DEFECTIVE (E/E COMPARTMENT)

SFO - FLT 962 - EN ROUTE DFW/SFO DURING CRUISE, SLIGHT ODOR OF SMOKE FOLLOWED BY FWD EQUIPMENT EXHAUST FAN MESSAGE AFTER WHICH ODOR DISSIPATED. AIRCRAFT PROCEEDED TO SFO, LANDING WITHOUT INCIDENT. PLACARDED FWD EQUIPMENT EXHAUST FAN INOPERATIVE. SUBSEQUENTLY, REPLACED FWD EQUIPMENT EXHAUST FAN AT JFK/20. SYSTEM GROUND CHECKED, NORMAL OPERATION, WITH NO SMOKE NOTED. (X)

Part: SKIN — WORN (LT TE FLAP)

AFW - FOUND LEFT WING INBOARD AFT FLAP LEADING EDGE SKIN WORN FROM CONTACT WITH SEAL RETAINER. FOUND WEAR TO BE BEYOND SRM ALLOWABLE LIMITS, BLENDED WEAR. ACCOMPLISHED EDDY CURRENT CHECK. NO CRACKS FOUND. FILLED AND RESTORED SURFACE FINISH. ADJUSTED SEAL TO PREVENT CHAFING. APPROVED BY ENGINEERING PER MRB 767-1225.

Part: FLOORBEAM — CORRODED (FS 902)

FOUND CORROSION ON UPPER FLANGE OF FLOORBEAM. BLEND FLAP PEEN AND REFINISHED, APPROVED FOR SERVICE PER MRB 767-916, DATED 5/5/95. (M)

Part: EEL CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS INOPERATIVE BETWEEN PAX SEAT ROWS 7HJ TO 21HJ. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR BY RT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)

Part: EEL ARROW — MISSING (RT OVERWING)

MIA - DURING OVERNIGHT CHECK, RT AISLE EMERGENCY LIGHT RED ARROW MISSING AT OVERWING EXIT. REPLACED RED ARROW AT RT AISLE OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (Z)