N369AA

Part: BATTERY — DISCHARGED (CABIN) · airframe 103,165 hrs · 16,691 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. EMERGENCY EXIT LIGHTS FROM SEATS 25H TO 29H ARE INOPERATIVE. REMOVED AND REPLACED BATTERY ASSEMBLY M1210 PER AMM 33-60-98. OPERATIONAL CHECK GOOD.

Part: ANGLE — CRACKED (BS 1270-1286) · airframe 103,165 hrs · 16,691 cycles

CRACKED AFT CARGO ANGLE BETWEEN BS 1270 AND 1286, RBL 52. REMOVED AND REPLACED THE ANGLE IAW SRM 51-00-05.

Part: PIN — MISSING (CONNECTOR) · airframe 103,165 hrs · 16,691 cycles

SEAT MOUNTED EMERGENCY LIGHTS AT SEAT 21AB ARE INOPERATIVE. INSTALLED PIN TO EPL WIRE CONNECTOR IAW SWPM 20-10-11. OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 102,702 hrs · 16,583 cycles

AIRCRAFT WAS NOT GROUNDED. RIGHT HAND MID GALLEY FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REPLACED RIGHT HAND MID GALLEY FLASHLIGHT PER AMM 25-64-00. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 102,406 hrs · 16,508 cycles

EMERGENCY EXIT LIGHTS AT SEATS 25H THROUGH 29H ARE INOPERATIVE. SEATED THE CONNECTOR AT SEAT 30H IAW AMM 33-51-10. OPERATIONAL CHECKED GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 102,213 hrs · 16,467 cycles

SEAT MOUNTED EMERGENCY LIGHT AT SEAT 13B HAS A MISSING CLEAR LENS. INSTALLED THE LENS IAW AMM 33-51-10. OPERATIONAL CHECKED GOOD.

Part: SHUTOFF VALVE — FAULTY (FUEL SYS) · airframe 101,905 hrs · 16,417 cycles

DURING FLIGHT, THE CREW OBSERVED AN UNCOMMANDED FUEL TRANSFER FROM THE CENTER TANK TO THE LEFT MAIN FUEL TANK. REMOVED AND REPLACED OTBD FUELING SHUTOFF VALVE IAW AMM 28-21-02, FUELING SHUTOFF VALVE CONTROL UNIT IAW AMM 28-21-12, DEFUELING VALVE IAW AMM 28-26-01, DEFUELING VALVE ACTUATOR IAW AMM 28-26-11, AND FUELING MANIFOLD TUBE ASSEMBLY IAW AMM 28-21-10. LEAK AND OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: SHUTOFF VALVE — FAULTED (FUEL SYSTEM) · airframe 101,905 hrs · 16,417 cycles

AIRCRAFT WAS GROUNDED. DURING FLIGHT THE CREW OBSERVED UNCOMMANDED FUEL TRANSFER FROM THE CENTER TANK TO THE LEFT MAIN FUEL TANK. REMOVED AND REPLACED OUTBOARD FUELING SHUTOFF VALVE IAW AMM 28-21-02, FUELING SHUTOFF VALVE CONTROL UNIT IAW AMM 28-21-12, DEFUELING VALVE IAW AMM 28-26-01, DEFUELING VALVE ACTUATOR IAW AMM 28-26-11, AND FUELING MANIFOLD TUBE ASSEMBLY IAW AMM 28-21-10. LEAK AND OPERATIONAL CHECKED GOOD.

Part: TUBE — CRACKED (FUEL SYSTEM) · airframe 101,905 hrs · 16,417 cycles

DURING FLIGHT, THE CREW OBSERVED AN UNCOMMANDED FUEL TRANSFER FROM THE CENTER TANK TO THE LEFT MAIN FUEL TANK. REMOVED AND REPLACED OTBD FUELING SHUTOFF VALVE IAW AMM 28-21-02, FUELING SHUTOFF VALVE CONTROL UNIT IAW AMM 28-21-12, DEFUELING VALVE IAW AMM 28-26-01, DEFUELING VALVE ACTUATOR IAW AMM 28-26-11, AND FUELING MANIFOLD TUBE ASSEMBLY IAW AMM 28-21-10. LEAK AND OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: CONTROL UNIT — FAULTY (FUEL SYS) · airframe 101,905 hrs · 16,417 cycles

DURING FLIGHT, THE CREW OBSERVED UNCOMMANDED FUEL TRANSFER FROM THE CENTER TANK TO THE LEFT MAIN FUEL TANK. REMOVED AND REPLACED THE OTBD FUELING SHUTOFF VALVE IAW AMM 28-21-02, FUELING SHUTOFF VALVE CONTROL UNIT IAW AMM 28-21-12, DEFUELING VALVE IAW AMM 28-26-01, DEFUELING VALVE ACTUATOR IAW AMM 28-26-11, AND FUELING MANIFOLD TUBE ASSEMBLY IAW AMM 28-21-10. LEAK AND OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: ACTUATOR — FAULTY (FUEL SYSTEM) · airframe 101,905 hrs · 16,417 cycles

DURING FLIGHT, THE CREW OBSERVED AN UNCOMMANDED FUEL TRANSFER FROM THE CENTER TANK TO THE LEFT MAIN FUEL TANK. REMOVED AND REPLACED OTBD FUELING SHUTOFF VALVE IAW AMM 28-21-02, FUELING SHUTOFF VALVE CONTROL UNIT IAW AMM 28-21-12, DEFUELING VALVE IAW AMM 28-26-01, DEFUELING VALVE ACTUATOR IAW AMM 28-26-11, AND FUELING MANIFOLD TUBE ASSEMBLY IAW AMM 28-21-10. LEAK AND OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 101,824 hrs · 16,399 cycles

AIRCRAFT WAS NOT GROUNDED. HORIZONTAL ATTACHING FRAME HARDWARE PULLED THROUGH FLOORBOARD ON LEFT AISLE BETWEEN SEAT TRACKS 25 THROUGH 27BC. REMOVED AND REPLACED FLOORBOARD SUPPORT IAW AARD 51-00-05 AND AMM 53-01-01.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 101,336 hrs · 16,300 cycles

AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTS AT SEATS 25H TO 29H ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK M00732. OPERATIONAL CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 100,992 hrs · 16,210 cycles

AIRCRAFT WAS NOT GROUNDED. FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT. OPERATIONAL CHECK GOOD.

Part: SPLICE — FAULTY (LE SLAT) · airframe 100,784 hrs · 16,163 cycles

AIRCRAFT WAS GROUNDED. DURING FCF AFTER 9 MINS IN CRUISE AT FL380 THE LEADING EDGE SLAT ASYMMETRY ANNUNCIATED ON EICAS. REPEATED SEVERAL TIMES THEN REMAINED ANNUNCIATED. EMERGENCY DECLARED. RETURNED TO TUL. MAINTENANCE FOUND SPLICE SM8 ON WIRE W430-008-18 FOR SLAT SENSOR S283 BAD. REMOVED AND REPLACED SPLICE SM8 IAW WDM 27-88-12 AND CHAPTER 20 20-30-12.

Part: GIRT BAR — OBSTRUCTED (R4 DOOR) · airframe 100,265 hrs · 16,033 cycles

R4 DOOR WILL NOT ARM. REMOVED DEBRIS FROM GIRT BAR TRACK IAW FIM 25-66-00. OPS CHECKED GOOD.

Part: ATTACH ANGLE — CRACKED (BS 246) · airframe 99,516 hrs · 15,875 cycles

PULLEY BRACKET ATTACH ANGLE AT BS 246 AND RBL 5 FOUND CRACKED. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 53-10-51-2R-3.

Part: ATTACH ANGLE — CRACKED (BS 246) · airframe 99,516 hrs · 15,875 cycles

PULLEY BRACKET ATTACH ANGLE AT BS 246, RBL 18 FOUND CRACKED. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 53-10-51-2R-3.

Part: ATTACH ANGLE — CRACKED (BS 246) · airframe 99,516 hrs · 15,875 cycles

PULLEY BRACKET ATTACH ANGLE AT BS 246 AND RBL 2 IS CRACKED. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 53-10-51-2R-3.

Part: BATTERY — DISCHARGED (CABIN) · airframe 99,265 hrs · 15,829 cycles

AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED EMERGENCY LIGHTS BETWEEN ROWS 33HJ AND 41HJ ARE INOPERATIVE. R & R EMERGENCY BATTERY AND CHARGER ASSEMBLIES IAW AMM 33-60-98. SYSTEM CHECKS NORMAL. ALSO AALA20160627008.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 99,265 hrs · 15,829 cycles

AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED EMERGENCY LIGHTS BETWEEN ROWS 33HJ AND 41HJ ARE INOPERATIVE. R & R EMERGENCY BATTERY AND CHARGER ASSEMBLIES IAW AMM 33-60-98. SYSTEM CHECKS NORMAL. ALSO AALA20160628002.

Part: BOLT — BROKEN (LE SLAT) · airframe 98,393 hrs · 15,639 cycles

AIRCRAFT WAS GNDED. DURING POST ARRIVAL MX WALK AROUND, THE NR 2 SLAT WAS OBSERVED TO BE NOT FAIRED WITH THE WING. UPON FURTHER INVESTIGATION THE NR 2 SLAT OTBD ACTUATOR ARM ROD END BOLT WAS FOUND BROKEN. R & R ROD END BOLT, ROD END & BRACKET ASSEMBLY IAW AMM 27-81-02.

Part: CHARGER — FAILED (MASTER BATTERY) · airframe 97,000 hrs · 15,347 cycles

MAIN BATTERY CHARGER STATUS MSG DISPLAYED. FLIGHT DECLARED AN EMER & DIVERTED WITHOUT FURTHER INCIDENT. ACFT WAS REMOVED FROM SERVICE. R & R BATTERY CHARGER IAW MM 24-31-02.

Part: LENS — MISSING (CABIN) · airframe 95,794 hrs · 15,143 cycles

SEAT 6B IS MISSING TWO EMER LIGHT LENS. REPLACED TWO EACH LENSES ON SEAT 6B. SYS CHECKED NORMAL. SEE ALSO AALA20150608008.

Part: LENS — MISSING (CABIN) · airframe 95,794 hrs · 15,143 cycles

SEAT 6B IS MISSING TWO EMER LIGHT LENSES. REPLACED TWO EACH LENSES ON SEAT 6B. SYS CHECKED NORMAL. SEE ALSO AALA20150608009.

Part: SKIN — DAMAGED (BS 963) · airframe 95,433 hrs · 15,089 cycles

FASTENER HOLE IN SKIN & STRAP AT BS 963.5, RBL 99, WL 180 ELONGATED. REPAIRED HOLE IAW EA 250399.

Part: FAILSAFE — MISREPAIRED · airframe 95,433 hrs · 15,089 cycles

DURING THE BULKHEAD FITTING FAILSAFE STRAP INSPECTION, REPAIR IAW ECO C3039CA, 12 FASTENER HOLES ON THE WING TE ACCESS PANEL WERE FOUND TO BE THE WRONG SIZE, 1/4 INCH INSTEAD OF 3/16 INCH. INSTALLED 12 EACH LARGER FASTENERS IAW EA 250902 & SRM 51-40-0W.

Part: SKIN — CORRODED (BS 961) · corrosion level 2 · airframe 95,433 hrs · 15,089 cycles

FUSELAGE SKIN CORROSION & FRETTING AT BS 961 BETWEEN STRINGER 22R & 23R. REPAIRED IAW EA 250455.

Part: TEE FITTING — CORRODED (BS 977) · corrosion level 2 · airframe 95,433 hrs · 15,089 cycles

RIGHT TEE FITTING FOUND CORRODED AFTER REMOVAL. R & R TEE FITTING IAW ECO C3039CA FIGURE 5 SHEET 3,4 & 5.

Part: FITTING — CORRODED (RT PYLON) · airframe 95,430 hrs · 15,087 cycles

CORROSION ON RT WING LOWER SURFACE PYLON PITCH FITTING FWD INBD HOLE. REPAIRED PITCH FITTING IAW EA 57-039231 DATED APRIL 1 2015.

Part: FITTING — CORRODED (LT PYLON) · airframe 95,430 hrs · 15,087 cycles

CORROSION ON LT WING LOWER SURFACE PYLON PITCH FITTING FWD INBD HOLE. REPAIRED PITCH FITTING IAW EA B767-57-039231 DATED APRIL 1 2015.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 95,430 hrs · 15,087 cycles

RED EMER LIGHT MOUNTED ON DIVIDER BETWEEN SEAT 17B & 20B WAS INOPERATIVE. RELAMPED RED EMER LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 95,430 hrs · 15,087 cycles

IN SEAT EMER LIGHTING ON SEATS 32AB - 41AB WENT DIM DURING EMER LIGHT DURATION TEST. REPLACED EMER LIGHT BATTERY PACK.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 95,430 hrs · 15,087 cycles

SEAT MOUNTED EMER PATH LIGHTS INOPERATIVE BETWEEN SEATS 25B & 31B. R & R EMER PATH LIGHTING CHARGER & BATTERY FOR THAT ZONE. SYS CHECKED NORMAL.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,430 hrs · 15,087 cycles

SKIN & STRINGER CORROSION FROM FS 654+121 TO 654+134 BETWEEN STRINGERS 34 LT & 36 LT. REPAIRED SKIN IAW SRM 53-00-01 & EA 53-039120 DATED 3 24 2015.

Part: STRINGER — CORRODED (BS 654) · corrosion level 2 · airframe 95,430 hrs · 15,087 cycles

SKIN & STRINGER & DRAIN MAST SKIN CORROSION. FUSELAGE SKIN REPAIR WITH STRINGER & DRAIN MAST CUT OUT. REPAIRED STRINGER 36 LEFT PER SRM 53-00-01 AND EA B767-53-039120.

Part: LIGHT — DIM (CABIN) · airframe 95,430 hrs · 15,087 cycles

SEAT MOUNTED EMER ESCAPE PATH LIGHTS ON SEAT 41B ARE DIM. REPLACED SEAT MOUNTED EMER ESCAPE PATH LIGHT BULB ON SEAT 41B. OPERATIONAL CHECKED IAW AMM 33-60-98. SYS CHECKED NORMAL.

Part: LIGHT — DIM (CABIN) · airframe 95,430 hrs · 15,087 cycles

SEAT MOUNTED EMER ESCAPE PATH LIGHTS ON SEATS 20H & 21H ARE DIM. REPLACED SEAT MOUNTED EMER ESCAPE PATH LIGHTS BULBS ON SEATS 20H & 21H. OPERATIONAL CHECK IAW AMM 33-60-98. SYS CHECKED NORMAL.

Part: LIGHT — DIM (CABIN) · airframe 95,430 hrs · 15,087 cycles

SEAT MOUNTED EMER ESCAPE PATH LIGHTS ON SEATS 30H & 31H ARE DIM. REPLACED SEAT MOUNTED EMER ESCAPE PATH LIGHT BULBS ON SEATS 30H & 31H. OPERATIONAL CHECK IAW AMM 33-60-98. SYS CHECKED NORMAL.

Part: LIGHT — DIM (CABIN) · airframe 95,430 hrs · 15,087 cycles

SEAT MOUNTED EMER ESCAPE PATH LIGHTS DIM ON SEAT 12B. RELAMPED SEAT MOUNTED EMER ESCAPE PATH LIGHTS ON SEAT 12B IAW AMM 33-51-10. SYS CHECKED NORMAL.

Part: LIGHT — DIM (CABIN) · airframe 95,430 hrs · 15,087 cycles

SEAT MOUNTED EMER ESCAPE PATH LIGHTS ON SEATS 36H & 37H ARE DIM. REPLACED SEAT MOUNTED EMER ESCAPE PATH LIGHT BULBS ON SEATS 36H & 37H. OPERATIONAL CHECK IAW AMM 33-60-98. SYS CHECKED NORMAL.

Part: LIGHT — DIM (CABIN) · airframe 95,430 hrs · 15,087 cycles

SEAT MOUNTED ESCAPE PATH LIGHT DIM AT SEATS 36B, 37B, 38B & 39B. REPLACED LIGHT BULBS. SYS CHECKED NORMAL.

Part: CONNECTOR — BROKEN (CABIN) · airframe 95,430 hrs · 15,087 cycles

EMERGENCY LIGHT CONNECTOR ON SEAT 40B IS BROKEN. REPLACED EMER LIGHT CONNECTOR ON SEAT 40B. OPERATIONAL CHECK IAW AMM 33-60-98. SYS CHECKED NORMAL.

Part: LIGHT — DIM (CABIN) · airframe 95,430 hrs · 15,087 cycles

SEAT MOUNTED EMER ESCAPE PATH LIGHTS ON SEAT 34H ARE DIM. REPLACED SEAT MOUNTED EMER ESCAPE PATH LIGHT BULB ON SEAT 34H. OPERATIONAL CHECK IAW AMM 33-60-98. SYS CHECKED NORMAL.

Part: LIGHT — DIM (CABIN) · airframe 95,430 hrs · 15,087 cycles

SEAT MOUNTED EMER ESCAPE PATH LIGHTS ON SEAT 27H ARE DIM. REPLACED SEAT MOUNTED EMER ESCAPE PATH LIGHT BULB ON SEAT 27H. OPERATIONAL CHECK IAW AMM 33-60-98. SYS CHECKED NORMAL.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,430 hrs · 15,087 cycles

CABIN FLOORBEAM CHORD AT FS 325 IS CORRODED BETWEEN RBL 78 & LBL 31 IAW SRM 51-10-02, SRM 53-00-51 REPAIR 1 FIGURE 201 & EA 53-039001 DATED 03 16 2015.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 95,430 hrs · 15,087 cycles

STRINGER 37 LT IS CRACKED AT FS 534. REPAIRED STRINGER IAW SRM 53-00-03 DETAIL III & EA 53-039010 DATED 3 17 15.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 95,430 hrs · 15,087 cycles

STRINGER 30 LT DAMAGED BETWEEN FS 500 & 522. REPAIRED STRINGER IAW 53-00-03-2R & EA 53-038862.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,430 hrs · 15,087 cycles

FORWARD CARGO COMPARTMENT STIFFENER AFT OF DRAIN AT FS 654.135, BETWEEN LONGERONS 34 LT & 35 LT IS CORRODED. R & R STIFFENER IAW SRM 51-00-05.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,430 hrs · 15,087 cycles

FORWARD CARGO COMPARTMENT STIFFENER AFT OF DRAIN AT FS 654.129, BETWEEN LONGERONS 34 LT & 35 LT IS CORRODED. R & R STIFFENER IAW SRM 51-00-05.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,430 hrs · 15,087 cycles

FORWARD CARGO THRESHOLD SUPPORT HAS CORROSION AT FS 534 IN 2 PLACES. R & R SUPPORT BETWEEN FS 478 & 610 IAW AARD 51-00-05.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 95,430 hrs · 15,087 cycles

AFT CARGO INTERCOSTAL CRACKED AT UPPER FLOORBOARD SUPPORT. R & R INTERCOSTAL IAW AARD 51-00-05.

Part: TEE FITTING — BROKEN (FUSELAGE) · airframe 95,430 hrs · 15,087 cycles

INTERCOSTAL IN FWD CARGO HAS ATTACH LUG BROKEN. REMOVED & INSTALLED TEE ON INTERCOSTAL IAW DWG 452T2001 SHEET 31 & AARD 51-00-05.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 95,430 hrs · 15,087 cycles

AFT CARGO FLOORBEAM AFT FLANGE HAS CORROSION. INSTALLED REPAIR ANGLE IAW SRM 53-00-07.

Part: INTERCOSTAL — DENTED (FUSELAGE) · airframe 95,430 hrs · 15,087 cycles

DENT IN BOTTOM OF INTERCOSTAL IN AFT CARGO COMPARTMENT CEILING AT APPROX FS 1197+40 & RBL 43. R & R INTERCOSTAL IAW AARD51-00-05.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 95,430 hrs · 15,087 cycles

CRACKED CHORD AT NR 8 CARGO PDU AFT INBD ATTACHMENT LOCATION AT FS 583 BETWEEN RBL 30 & 43. R & R CHORD IAW AARD 51-00-05-1 & DWG 143T8201 SHEETS 1 & 3.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 95,430 hrs · 15,087 cycles

CRACK AT AFT CARGO DOOR OPENING CEILING IN THE CORNER OF INTERCOSTAL. R & R INTERCOSTAL ASSEMBLY IAW SRM 51-00-05.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 95,430 hrs · 15,087 cycles

CRACK FOUND IN AFT CARGO DOOR OPENING CEILING IN CORNER OF INTERCOSTAL. R & R INTERCOSTAL IAW SRM 51-00-05.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,430 hrs · 15,087 cycles

CORROSION ON FLOOR STRUCTURE INTERCOSTAL UPPER CHORD. REPLACED INTERCOSTAL IAW AARD 51-00-05-1 & DWG 141T2200.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 95,430 hrs · 15,087 cycles

FORWARD CARGO CEILING AREA FLOOR SUPPORT INTERCOSTAL WEB CRACKED. R & R WEB IAW AARD 51-00-05.

Part: CONNECTOR — MISWIRED (CABIN) · airframe 95,430 hrs · 15,087 cycles

SEAT MOUNTED ESCAPE PATH LIGHTS ON SEAT 4H ARE INOPERATIVE. FOUND TWO WIRES CROSSED ON CONNECTOR, FIXED ISSUE & THE LIGHTS OPERATIONS CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,430 hrs · 15,087 cycles

CORROSION ON TOP & BOTTOM OF FLOORBOARD SUPPORT AT FS 478 & LBL 36. R & R FLOORBOARD SUPPORT WITH NEW SUPPORT IAW SRM 51-10-02.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 95,274 hrs · 15,063 cycles

ROW 32AB - 41AB EMER PATH IN SEAT LIGHTS INOPERATIVE. R & R CHARGER ASSEMBLY CHA5031 IAW AMM 33-51-05. SYS CHECKED NORMAL.

Part: CHARGER — DEFECTIVE (CABIN) · airframe 95,274 hrs · 15,063 cycles

BATTERY CHARGER AT SEAT 39AB REQUIRES REPLACEMENT. R & R CHARGER ASSEMBLY IAW AMM 33-51-05. SYS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 95,274 hrs · 15,063 cycles

OVERHEAD AISLE EMER LIGHTS FROM 32AB - 41AB ARE INOPERATIVE. R & R BATTERY AT M738 IAW AM 33-51-05. SYS CHECKED NORMAL.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 95,200 hrs · 15,052 cycles

AIR INTERRUPT, DURING CLIMB ISFD FLAG CAME ON WITH NO AIRSPEED & ERRONEOUS ALTITUDE INDICATIONS. R & R ISFD SQD & PERFORMED OPERATIONAL CHECK IAW AMM 34-24-03, 34-11-00 & GPM 18.01. SYS CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 95,048 hrs · 15,018 cycles

R4 DOOR EMER LIGHT SIGN INOPERATIVE. R & R POWER SUPPLY M1210 IAW AMM 33-51-07. OPERATIONS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 94,604 hrs · 14,935 cycles

SEAT MOUNTED EMER LIGHTS INOPERATIVE FROM SEAT 32AB TO 41AB. REPLACED BATTERY PACK IAW MM 33-51-00. SYS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 94,245 hrs · 14,880 cycles

EMERGENCY LIGHTS AFT OF 31AB TO 42AB INOPERATIVE. REPLACED BATTERY PACK. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 93,850 hrs · 14,818 cycles

CABIN 4L EMER SIGN FLOOD LIGHT INOPERATIVE. REPLACED LAMP FOR CABIN 4L EMER SIGN FLOOD LIGHT. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 93,850 hrs · 14,818 cycles

SEAT 17AB PROXIMITY EMER LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT 17AB PROXIMITY EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: LIGHT — DAMAGED (CABIN) · airframe 93,850 hrs · 14,818 cycles

SEAT 21AB PROXIMITY EMER LIGHT ASSEMBLY DAMAGED. R & R SEAT 21AB EMER LIGHT ASSEMBLY. OPERATIONS CHECKED NORMAL.

Part: HINGE FITTING — CRACKED (RT PYLON) · airframe 93,397 hrs · 14,747 cycles

RIGHT PYLON STRUT TORQUE BOX OTBD CORE COWL BACKUP HINGE FITTING CRACKED AT STATION 285 & WL 154. ACCOMPLISHED SPLICE REPAIR IAW EA B767-54-035940.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 92,408 hrs · 14,597 cycles

LEFT NR 2 DOOR EMERGENCY LIGHT INOPERATIVE. REPAIRED GND & REPLACED BATTERY CHARGER FOR LT NR 2 DOOR EMERGENCY LIGHT, OPERATIONS CHECKED NORMAL.

Part: CHARGER — FAILED (CABIN) · airframe 91,174 hrs · 14,399 cycles

TWO EMERGENCY EXIT SIGNS INOPERATIVE. R & R CHARGING UNIT, OPERATIONS CHECKED NORMAL.

Part: FUSE — INOPERATIVE (CABIN) · airframe 91,152 hrs · 14,396 cycles

LT & RT NR 1 DOORS EMERGENCY EXIT SIGN UPPER & LOWER LIGHTS ARE INOPERATIVE. REPLACED EMERGENCY EXIT SIGN BATTERY SUPPLY FUSE. OPERATIONS CHECKED NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 90,676 hrs · 14,321 cycles

EMERGENCY EXIT SIGN BY LT & RT NR 4 DOORS INOPERATIVE. REPLACED CHARGER FOR EMERGENCY EXIT SIGN FOR LT & RT NR 4 DOORS. OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 90,216 hrs · 14,257 cycles

RT SIDE EXTERNAL FS MOUNTED NR 5 AREA ILLUMINATION EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK M733. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 90,216 hrs · 14,257 cycles

MID GALLEY AISLE LOWER MARKER INOPERATIVE. REPLACED LAMP FOR MID GALLEY AISLE LOWER MARKER. OPERATIONS CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 90,216 hrs · 14,257 cycles

RT SIDE EXTERNALLY MOUNTED NR 5 EMERGENCY LIGHT INOPERATIVE. REPLACED RT SIDE EXTERNALLY MOUNTED NR 5 EMERGENCY POWER SUPPLY. OPERATIONS CHECKED NORMAL.

Part: SKIN — DENTED (FUSELAGE) · airframe 89,768 hrs · 14,191 cycles

DENT FOUND AT BS 1197 BETWEEN STRINGERS 35 & 38 RT. INSTALLED DOUBLER IAW SRM 53-00-01-2R-12.

Part: WEB — CORRODED (FUSELAGE) · airframe 89,768 hrs · 14,191 cycles

CORROSION ON UNDERSIDE OF WEB AT POWER DRIVE UNIT 8R AFT INBD MOUNT HOLE, STATION 587 & RBL 31. ACCOMPLISHED CORROSION R&R IAW EA 767-53-031512.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 89,768 hrs · 14,191 cycles

TWO PULLEY BRACKET SUPPORT ANGLES WERE FOUND CRACKED AT BL 0 & STATION 246 FWD SIDE. REPLACED TWO EACH PULLEY BRACKET SUPPORT ATTACH ANGLES AT STATION 246 & BL 0 IAW AARD 51-00-05 & DRAWING 114T5104.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 89,548 hrs · 14,162 cycles

RIGHT HAND FUSELAGE EXTERIOR FORWARD SLIDE/WING/GROUND ILLUMINATION LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT HAND FUSELAGE EXTERIOR FORWARD SLIDE/WING/GROUND ILLUMINATION LIGHT. OPS CHECKED NORMAL

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 87,977 hrs · 13,900 cycles

EMERGENCY LIGHTS ROWS 32 TO 4 RIGHT SIDE INOPERATIVE. REPLACED BATTERY PACK M734. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 87,977 hrs · 13,900 cycles

RIGHT SIDE EXTERIOR EMERGENCY LIGHT ABOVE AFT GEAR FAIRING INOPERATIVE. REPLACED LAMP FOR RIGHT EXTERIOR EMERGENCY LIGHT ABOVE AFT GEAR FAIRING. OPS CHECK NORMAL.

Part: LIGHT — BROKEN (CABIN) · airframe 87,977 hrs · 13,900 cycles

CEILING EMERGENCY LIGHT ABOVE SEAT 32C FOUND HANGING. REPLACED CEILING EMERGENCY LIGHT ASSEMBLY ABOVE SEAT 32C. OPS CHECK NORMAL.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 87,012 hrs · 13,752 cycles

JFK - INFLIGHT DFW-MAD. CREW REPORTED THE FIRST OFFICERS O2 MASK WOULD NOT TEST AND DEVELOPED A LEAK IN THE O2 LINE. EMERGENCY DECLARED FLIGHT DIVERTED JFK LANDED WITHOUT INCIDENT. REPLACED FIRST OFFICERS O2 MASK. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FUEL CAP — LEAKING (LT WING) · airframe 84,909 hrs · 13,426 cycles

FRA - CREW REPORTED POSSIBLE FUEL LEAK APPEARED TO BE COMING FROM THE FUEL CAP ON THE LEFT WING. NO NOTICEABLE DIFFERENCE IN THE FUEL QUANTITY BETWEEN THE LEFT AND RIGHT TANKS. FLIGHT LANDED FRA WITHOUT INCIDENT. REPLACED LEFT WING OVERWING REFUEL CAP ASSEMBLY. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 84,733 hrs · 13,392 cycles

RIGHT NUMBER 2 LOWER PORTION OF EMERGENCY SIGN LIGHTS INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 2 LOWER PORTION OF EMERGENCY SIGN LIGHT. OPS CHECKS GOOD.

Part: TORQUE BOX — CRACKED (NACELLE) · airframe 84,143 hrs · 13,296 cycles

UPPER TORQUE BOX WEB CRACK. REPAIRED PER AARD 54-52-01-1.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 84,143 hrs · 13,296 cycles

RIGHT WING OUTBOARD FLAP UPPER SURFACE HAS DELAMINATION. ACCOMPLISHED BONDED REPAIR PER SRM 57-53-01.

Part: INDICATOR — TRIPPED (TE FLAP) · airframe 83,803 hrs · 13,242 cycles

LAX - CREW REPORTED WITH FLAPS AT 15 DEGRESS ALL NORMAL BUT WITH FLAPS SELECTED TO 20 DEGREES THE TRAILING EDGE FLAP DISAGREE ILLUMINATED. EMERGENCY DECLARED FLIGHT LANDED LAX WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND RIGHT WING INBOARD ROTARY ACTUATOR OVERLOAD INDICATOR TRIPPED. THE OVERLOAD TRIP INDICATOR WAS RESET AND THE FLAPS WERE RAN THROUGH ALL SETTINGS WITH NO FAULT INDICATIONS NOTED. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 82,826 hrs · 13,084 cycles

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

Part: LENS — MISSING (CABIN) · airframe 82,096 hrs · 12,977 cycles

ROW 17A CEILING EMERGENCY LIGHT MISSING LENS. REPLACED LENS FOR ROW 17A EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LENS — MISSING (CABIN) · airframe 82,096 hrs · 12,977 cycles

LEFT NUMBER 2 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LENS FOR LEFT NUMBER 2 DOOR EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 82,096 hrs · 12,977 cycles

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

Part: LENS — MISSING (CABIN) · airframe 82,096 hrs · 12,977 cycles

ROW 17H CEILING EMERGENCY LIGHT MISSING LENS. REPLACED LENS FOR ROW 17H CEILING EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 82,096 hrs · 12,977 cycles

LEFT NUMBER 2 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 2 DOOR EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: IDG — FAULTY (LEFT) · airframe 80,954 hrs · 12,804 cycles

JFK - INFLIGHT ORD-DUB. CREW REPORTED THE LEFT GENERATOR FAULTED ALONG WITH THE LEFT AFT AND RIGHT FORWARD FUEL PUMPS. FLIGHT DIVERTED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED BITE CHECK OF BPCU WHICH HAD A "LEFT OPEN PHASE TRIP" MSG. FOUND T2 FEEDER CABLE AT LEFT INTEGRATED DRIVE GENERATOR BURNT. REPLACED LEFT INTEGRATED DRIVE GENERATOR AND GENERATOR CONTROL UNIT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SMOKE DETECTOR — DIRTY (LAVATORY) · airframe 80,352 hrs · 12,697 cycles

DURING FLIGHT SMOKE DETECTORS AT LAVS F1 AND M2 SOUNDED ONCE FOR 5 MINUTES. DURING TAXI IN LAV F1 SOUNDED AGAIN, NO EVIDENCE OF SMOKE. SMOKE DETECTORS CLEANED AND RE-INSTALLED. OPS CHECK NORMAL.

Part: INDICATOR — TRIPPED (TE FLAP) · airframe 80,302 hrs · 12,691 cycles

DFW - CREW REPORTED ON DESCENT FLAP DISAGREE AT 15 DEGREES. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. RESET ROTARY TRIP INDICATORS AT POSITIONS TWO AND FIVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SWITCH — LOOSE (LT NACELLE) · airframe 79,638 hrs · 12,567 cycles

DUB INFLIGHT JFK-BRU - CREW REPORTED LEFT STRUT OVERHEAT INDICATION. FLIGHT DIVERTED DUB LANDED WITHOUT INCIDENT. FOUND TS236 SWITCH LOOSE. REPLACED TS236 AND TS237 SWITCH. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 77,448 hrs · 12,194 cycles

FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT LEFT MID CABIN INOPERATIVE. REPLACED BATTERY. OPS CHECKED NORMAL.

Part: RELIEF VALVE — FAULTY (HYDRAULIC SYS) · airframe 76,355 hrs · 12,012 cycles

ORD - CREW REPORTED HYDRAULIC SYSTEM MAINTENANCE MESSAGE AND THEN THE CENTER 2 HYDRAULIC OVERHEAT LIGHT ILLUMINATED. EMERGENCY DECLARED RETURNED ORD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED AIR DRIVEN PUMP FILTER MODULE PRESSURE RELIEF VALVE.

Part: OVEN — MALFUNCTIONED (GALLEY) · airframe 76,291 hrs · 12,003 cycles

GALLEY 7 OVEN NUMBER 5 HAS ELECTRICAL ODOR WHEN IN USE. PULLED CIRCUIT BREAKER. REPLACED NUMBER 5 OVEN IN AFT GALLEY. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: COVER — LOOSE (EXIT SIGN) · airframe 75,579 hrs · 11,879 cycles

EMERGENCY EXIT SIGN AT SEAT ROW 4L JUMPSEAT FALLS OFF. SECURED EXIT SIGN COVER.

Part: SENSOR — INOPERATIVE (PACK COMP TEMP) · airframe 73,826 hrs · 11,592 cycles

LEFT PACK INOPERATIVE AND PACK OFF LIGHTS WITH L PACK OFF AND L PACK TEMPERATURE EICAS MESSAGE. AIR INTERRUPT TO ORD FOR REPAIRS. FOUND LEFT PACK COMPRESSOR OUTLET TEMPERATURE SENSOR INOPERATIVE. REPLACED LEFT HAND PACK TEMPERATURE SENSOR. OPS GOOD. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — BROKEN (ZONE 200) · airframe 29,626 hrs

JFK - EMERGENCY LIGHT EXIT SIGN AT 21A LOCATION INOPERATIVE. REPLACED LIGHT ASSEMBLY AT 21A EXIT SIGN.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 72,014 hrs · 11,295 cycles

AFW - AFT CARGO SILL UPPER CHORD HAD CORROSION. BLENDED TO 0.170 INCH REMAINING FROM 0.196 PARENT WITH A DEPTH OF APPROXIMATELY .375 INCH DIAMETER. REPAIRED IN ACCORDANCE WITH SRM 53 00 15 1A FIG 101 AND MRB 767 3367.

Part: FRAME — CRACKED (BULKHEAD) · airframe 72,014 hrs · 11,295 cycles

AFW - DURING BULKHEAD OUTER CHORD INSPECTION CRACK INDICATION WAS NOTICED AT ONE HOLE LOCATION COMMON TO SKIN FORWARD LOWER TENSION FITTING, SPLICE FITTING, AND FORWARD OUTER CHORD. CRACK INDICATION WAS REMOVED BY ONE SIXTY FOURTH INCH HOLE OVERSIZING AND CONFIRMED NO CRACK INDICATION USING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION. REPAIRED IAW MRB 3316.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 72,014 hrs · 11,295 cycles

AFW - CORROSION FOUND ON PASSENGER FLOOR STRUCTURE FLOORBEAM UPPER CAP ON THE HORIZONTAL FLANGE AT STATION 347 BETWEEN RIGHT BUTTLINE 21 AND RIGHT BUTTLINE 79. CORROSION WAS BLENDED ON THE UPPER SURFACE WITH THE REMAINING THICKNESS AT 0.053 INCH. A SECTION OF ONE OF THE HORIZONTAL FLANGES WAS TRIMMED AND REPAIRED PER SRM 53-00-51-2R. REPAIRED IN ACCORDANCE WITH MRB 767-3366.

Part: SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 72,014 hrs · 11,295 cycles

AFW - FORWARD CARGO DOOR CUT OUT LOWER MAIN SILL OUTER CHORD HAD CORROSION. HIGH FREQUENCY EDDY CURRENT AT BLEND OUT SHOWS NO CRACKS. ROTARY SCAN OF FASTENER HOLES IN BLEND OUT SHOWS NO CRACKS. DAMAGED IS LIMITED TO THE VERTICAL LEG INBOARD AT STATION 569.65 WITH A MINIMUM REMAINING THICKNESS OF 0.130 INCH FROM PARENT OF 0.150 INCH. REPAIRED IN ACCORDANCE WITH SRM 53 00 15 1A FIGURE 101 AND MRB 767 3364.

Part: FLOORBEAM — CORRODED (BS 325) · corrosion level 2 · airframe 72,014 hrs · 11,295 cycles

AFW - FLOORBEAM AT STATION 325 HAD CORROSION ON THE HORIZONTAL FLANGE. AREA OF DISCREPANCY WAS 0.250 INCH DIAMETER WITH A MAXIMUM DEPTH OF 0.04900. REPAIRED IN ACCORDANCE WITH SRM 53 41 00 AND MRB 767 3365.

Part: LIGHT — INOPERATIVE (CABIN)

DFW EMERGENCY LIGHT AT MID CABIN LOWER LT SIDEWALL INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT MID CABIN LOWER LT SIDEWALL. SYSTEM GROUND CHECKED NORMAL OPS.

Part: PSEU — INOPERATIVE (MLG) · airframe 70,164 hrs · 70,164 cycles

DFW INFLIGHT T963/01JUL. AFTER TAKEOFF CREW REPORTED EICAS PROBE HEAT AND LANDING GEAR INDICATIONS. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED PROXIMITY SENSOR ELECTRONICS UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (S)

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

JFK - EMERGENCY LIGHT AT OVERHEAD SEAT ROW 21C. RELAMPED EMERGENCY LIGHT AT OVERHEAD SEAT ROW 21C. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

JFK - EMERGENCY EXIT SIGN LIGHTS AT LEFT AND RIGHT NUMBER FOUR DOORS INOPERATIVE. REPLACED BATTERY PACK AT LEFT NUMBER FOUR DOOR FOR EMERGENCY EXIT SIGN LIGHTS AT LEFT AND RIGHT NUMBER FOUR DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — MISSING (CABIN)

MIA - EMERGENCY LIGHT ASSEMBLY AT SEAT 12H MISSING. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 12H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHT AT SEAT 29H INOPERATIVE. RECONNECTED WIRE AT CONNECTOR FOR EMERGENCY LIGHT AT SEAT 29H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHT AT SEAT 25A INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 25A. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 10H HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT OVERHEAD SEAT 10H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY LIGHT AT RIGHT OVERWING INTERIOR MID POSITION INOPERATIVE. RELAMPED EMERGENCY LIGHT AT RIGHT OVERWING INTERIOR MID POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT 30H INOPERATIVE. RESEATED LIGHT FIXTURE CONNECTOR FOR EMERGENCY LIGHT AT SEAT 30H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FLOORBEAM — CORRODED (FUSELAGE)

FOUND FLOORBEAM AT STATION 764 HAD CORROSION REMOVED ON UPPER SURFACE, AT RBL 33 REPAI AS FOLLOWS, FABRICATE REPAIR STRAP OUT OF 301.5 HARD STAINLESS STEEL .050 INCH THICK. ALODINE BARE OF ALUMINUM SURFACES FINISH BLEND AND REPAIR PARTS WITH 2 COATS OF BMS10-11 PRIMER, FILL BLENDS WITH BMS5-92, INSTALL REPAIR STRAP WITH BMS 5-95. AT RBL 43, RBL 8 AND RBL 44 REPAIR AS FOLLOWS, ALODINE AND PRIME ALL BARE ALUMINUM SURFACES FINISH BLENDED AREA WITH 2 COATS OF BMS 10-11 PRIMER FILL BLENDS WITH BMS-5-95. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

AFW - FOUND CORROSION ON BEAM RBL 11.06 STATION 798 OUT OF SRM LIMITS. REMOVED CORROSION PER SRM. DYE PENETRANT CHECKED AREA AFTER BLENDING FOR CRACKS, ROTO-PEENED AREA, APPLIED ALODINE AND TWO COATS OF PRIMER. FILLED BLENDED AREA WITH BMS 5-95. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

FOUND CORROSION ON BEAM RBL 33 STATION 780-840 OUT OF SRM LIMITS. REMOVED CORROSION FROM AREA, DYE PENETRANT OF AREA FOR CRACKS. ROTO PEENED BLENDED AREA. APPLIED ALODINE AND 2 COATS OF PRIMER, FILLED BLENDED AREA WITH BMS 5-95 SEALANT. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 25H INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT CONNECTOR UNDER SEAT 25H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — BROKEN (CABIN)

DFW - DURING OVERNIGHT, MAINTENANCE EMERGENCY EXIT PATH MARKER FORWARD OF SEAT 24 E/F LENS CLIP BROKEN. REPLACED EMERGENCY PATH LIGHT ASSEMBLY FORWARD OF SEAT 24 E/F. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DAMAGED (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE LIGHT AT SEAT 30H INOPERATIVE. REPAIRED EMERGENCY ESCAPE LIGHTING PUSH BACK PINS AT SEAT 30H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — DAMAGED (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT AT SEAT 36H INOPERATIVE. REPAIRED EMERGENCY EXIT WIRE AT SEAT 36H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 3H INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: WIRE — FAILED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN RIGHT SIDE OF COACH CLASS INOPERATIVE. REPAIRED WIRING FOR EMERGENCY EXIT FLOOR PATH LIGHTS IN RIGHT SIDE OF COACH CLASS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: LIGHT — FAILED (COCKPIT)

LHR - FLT 100 - EN ROUTE JFK-LHR, FIRST OFFICERS GRIMES UTILITY LIGHT SHORTS OUT AND CAUSED SPARKS WHEN TOUCHED TO A METAL OBJECT. POPPED UTILITY P31 CIRCUIT BREAKER ON OVERHEAD PANEL. REPLACED FIRST OFFICERS GRIMES UTILITY LIGHT. GROUND CHECK NORMAL OPERATION. (M)

Part: WIRE — BROKEN (ROW 32B)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHTS AT 32B THROUGH 41B INOPERATIVE. REPAIRED EMERGENCY EXIT SEAT LIGHT WIRING AT 38B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — SHORTED (ROWS 25-31)

DFW - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT AT SEAT ROWS 25 THROUGH 31 INOPERATIVE. REPLACED SHORTED SEAT MOUNTED LIGHT SOCKET. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: CONNECTOR — BROKEN (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 31AB FOUND INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEAT 31AB. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: WIRE — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, FORWARD EMERGENCY EXIT LIGHT ON PAX SEAT 29H INOPERATIVE. RESECURED EMERGENCY EXIT LIGHT WIRE TO CONNECTOR PIN AT FORWARD LIGHT ON PAX SEAT 29H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CIRCUIT BREAKER — TRIPPED (APU)

ORD - FLT 83 - APU GENERATOR WILL NOT HOLD A LOAD. RESET NOT SUCCESSFUL. APU BUSS POWER CIRCUIT BREAKER RECYCLED. APU LOAD CHECK CARRIED OUT. (X)

Part: IDG — FAILED (RT ENGINE)

SFO - FLT 59 - RIGHT GENERATOR DRIVE AND GENERATOR CONTROL LIGHT ILLUMINATED ALONG WITH THE RIGHT BUS OFF LIGHT. RIGHT GENERATOR WAS DISCONNECTED. THE RIGHT BUS WAS NOT RESTROED. THE BUS TIE ISOLATION LIGHT WAS NOT ON AND BY RECYCLING THE BUS TIE SWITCH THE RIGHT AC BUS WAS RESTORED. REMOVED AND REPLACED RIGHT IDG. OPS CNA LEAK CHECK REQUIRED EMP 106357. OPERATED AND LEAKED CHECKED RT IDG. OPS CHECKS NORMAL. CHECKED A/C BUSS TIE OPERATION PER MM. NO FAULTS NOTED AIRCRAFT A/C. ELECTRICAL SYSTEM CHECKS OK. (M)

Part: FLAP WARNING — ACTIVATED (LE FLAPS)

MIA - FLT 111 - ON APPROACH TO MIA, WHILE EXTENDING FLAPS TO 20 DEGREES A LEADING EDGE SLAT ASYMMETRIC EICAS MESSAGE. DECLARED AN EMERGENCY AND LANDED AT MIA WITHOUT INCIDENT. PERFORMED BITE CHECK OF FFU WITH NO FAULTS NOTED. CYCLED FLAPS SEVERAL TIMES WITH NO FAULTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. COULD NOT DUPLICATE ON GROUND, AIRCRAFT RETURNED TO SERVICE. (M)

Part: WIRE — BROKEN (CABIN)

JFK - DURING OVERNIGHT CHECK, FOUND ARROWED EMERGENCY EXIT LIGHT AT LEFT FORWARD OVERWING DOOR INOPERATIVE. REPAIRED POWER WIRE AT TERMINAL ON LIGHT L-322. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT CHECK, FLOOR PROXIMITY AISLE LIGHTING SYSTEM BETWEEN PASSENGER SEATS 7H THROUGH 12H INOPERATIVE. REPLACED FLOOR PROXIMITY AISLE LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT PASSENGER SEATS 8B TO 12B FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT SIDEWALL CONNECTOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: CONNECTOR — LOOSE (ROWS 40-43AB)

SFO - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT LIGHTS AT SEAT ROWS 40 TO 43AB INOPERATIVE. RESEATED EMERGENCY EXIT FLOOR PATH TRACK CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL ASSY — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT CHECK, ONE SEGMENT OF EMERGENCY LIGHTS AT MID-GALLEY CROSS AISLE INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT MID-GALLEY CROSS AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL STRIP — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. REPLACED TWO EMERGENCY EXIT FLOOR PATH LIGHT STRIPS AND AN INVERTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)

Part: EEL ASSY — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS BETWEEN PAX SEAT ROWS 7B TO 12B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHTS BETWEEN PAX SEAT ROWS 7B AND 12B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)