N7375A

Part: ROD END — OUT OF ADJUST (SLIDING WINDOW) · airframe 95,912 hrs · 15,377 cycles

AIRCRAFT IN BASE MAINTENANCE. CAPTAIN'S SLIDING WINDOW LOCK LEVER VERY DIFFICULT TO UNLOCK AND LOCK. MAINTENANCE PERFORMED ADJUSTMENT ON ROD END ON CAPTAIN'S SLIDING LOCK LEVER PER AMM 56-11-02-805-122 AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK PER 56-11-02-715-145.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,913 hrs · 15,377 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT BILGE AREA SKIN SURFACE BETWEEN STRINGER 37R AND 38R AT STATION 1085, RBL 13. REPAIRED SKIN PER EA 269288A.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 95,912 hrs · 15,377 cycles

AIRCRAFT IN BASE MAINTENANCE. FLIGHT DECK DOOR EMERGENCY LIGHT DID NOT CYCLE PROPERLY DURING TEST. REPLACED EMERGENCY LIGHT PER AMM 33-51-01-022-029.

Part: SUPPORT — CRACKED (BS 345-368) · airframe 95,913 hrs · 15,377 cycles

GALLEY SUPPORT BRACKET BETWEEN BS 345 AND 368 HAD BARE METAL AND GOUGED. BLENDED AREA AND FOUND IT CRACKED. ACCOMPLISHED A REPAIR IAW EA 269627.

Part: FLOORBEAM — CORRODED (BS 1480) · corrosion level 2 · airframe 95,913 hrs · 15,377 cycles

CORROSION ON AFT MAIN CABIN FLOORBEAM AT BS 1480, BETWEEN RBL 50 AND 70. REPAIRED IAW SRM 53-00-51-2R-1.

Part: SEAT TRACK — CORRODED (BS 345-400) · corrosion level 2 · airframe 95,913 hrs · 15,377 cycles

CORROSION ON THE CABIN SEAT TRACK BETWEEN BS 345 AND 400, LBL 85. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-00-52-1A, SRM 53-10-52, AND SRM 51-40-02.

Part: STRINGER — CORRODED (BS 654) · corrosion level 2 · airframe 95,913 hrs · 15,377 cycles

CORROSION WAS FOUND ON THE FORWARD CARGO BAY INSIDE CHANNEL AT THE NUTPLATE ATTACHMENT ON STRINGER 25R, BS 654+110, & 654+121. REPAIRED STRINGER IAW SRM 53-00-03-2R-2.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 95,748 hrs · 15,338 cycles

AIRCRAFT WAS NOT GNDED. EMER LIGHT AT SEAT 21H INOPERATIVE. R & R IN SEAT EMER LIGHT ASSEMBLY IAW AMM 33-51-10. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 94,885 hrs · 15,170 cycles

R1 DOOR EXTERIOR SLIDE LIGHT & THE 3 EXTERIOR OVERWING ESCAPE LIGHTS ON THE RT SIDE ARE INOPERATIVE. R & R THE R1 DOOR EXTERIOR SLIDE LIGHT BATTERY & CHARGER ASSEMBLY & THE 3 EXTERIOR OVERWING ESCAPE LIGHTS IAW AMM 33-51-07. SYS CHECKED NORMAL. SEE ALSO AALA20150909020, AALA20150911004 & AALA20150911005.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 94,885 hrs · 15,170 cycles

R1 DOOR EXTERIOR SLIDE LIGHT & THE 3 EXTERIOR OVERWING ESCAPE LIGHTS ON THE RT SIDE ARE INOPERATIVE. R & R THE R1 DOOR EXTERIOR SLIDE LIGHT BATTERY & CHARGER ASSEMBLY & THE 3 EXTERIOR OVERWING ESCAPE LIGHTS IAW AMM 33-51-07. SYS CHECKED NORMAL. SEE ALSO AALA20150909020, AALA20150911004 & AALA20150911006.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 94,885 hrs · 15,170 cycles

R1 DOOR EXTERIOR SLIDE LIGHT & THE 3 EXTERIOR OVERWING ESCAPE LIGHTS ON THE RT SIDE ARE INOPERATIVE. R & R THE R1 DOOR EXTERIOR SLIDE LIGHT BATTERY & CHARGER ASSEMBLY & THE 3 EXTERIOR OVERWING ESCAPE LIGHTS IAW AMM 33-51-07. SYS CHECKED NORMAL. SEE ALSO AALA20150909020, AALA20150911005 & AALA20150911006.

Part: BATTERY — DISCHARGED (CABIN) · airframe 94,885 hrs · 15,170 cycles

R1 DOOR EXTERIOR SLIDE LIGHT & THE 3 EXTERIOR OVERWING ESCAPE LIGHTS ON THE RT SIDE ARE INOPERATIVE. R & R THE R1 DOOR EXTERIOR SLIDE LIGHT BATTERY & CHARGER ASSEMBLY & THE 3 EXTERIOR OVERWING ESCAPE LIGHTS IAW AMM 33-51-07. SYS CHECKED NORMAL. SEE ALSO AALA20150911004, AALA20150911005 & AALA20150911006.

Part: WIRE HARNESS — BROKEN (CABIN) · airframe 92,815 hrs · 14,810 cycles

SEAT MOUNTED ESCAPE PATH LIGHTING AT SEATS 32 - 40 LT SIDE FAILED FUNCTIONAL TEST. FOUND BROKEN WIRE AT SEAT 40AB, SEAT INTERFACE HARNESS. REPLACED HARNESS & TESTED IAW AMM 33-51-00. SYS CHECKED NORMAL.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 92,282 hrs · 14,707 cycles

EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING DESCENT AT FLAPS 0 - 1 SLAT DISAGREE LIGHT ILLUMINATED. ALL OTHER PARAMETERS NORMAL. ACCOMPLISHED FLAP SLAT ELEC UNIT BITE IAW FIM 27-51-00-815-808 WITH NO FAULTS FOUND. PERFORMED SLAT ALTERNATE POWER & DRIVE SYS TEST IAW AMM 27-81-00 WITH NO FAULTS FOUND. SYS CHECKED NORMAL.

Part: DOUBLER — UNKNOWN (FUSELAGE) · airframe 90,765 hrs · 14,441 cycles

DOUBLER AT STATION 1219 & STRINGER 37L INOPERATIVE. REMOVED DOUBLER & ACCOMPLISHED REPAIR IAW EA B767-53-035926.

Part: SKIN — GOUGED (NR 2 PYLON) · airframe 90,765 hrs · 14,441 cycles

GOUGE IN THE SKIN OF THE NR 2 PYLON AT STATION 293. ACCOMPLISHED REPAIR IAW EA B767-54-035869.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 90,291 hrs · 14,361 cycles

AISLE EMER LIGHT AT SEAT 26G INOPERATIVE. REPLACED LAMP FOR AISLE EMER LIGHT AT SEAT 26G. OPERATIONS CHECKED NORMAL.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 90,291 hrs · 14,361 cycles

EMERGENCY LIGHT AT SEAT 35A INOPERATIVE. RESEATED CONNECTOR FOR LIGHT ASSEMBLY AT SEAT 35A. OPERATIONS CHECKED NORMAL.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 89,897 hrs · 14,295 cycles

FIRST CLASS RT SIDE EMERGENCY FLOOR PATH LIGHTING INOPERATIVE. SECURED CONNECTOR AT POWER SUPPLY M00730, OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 89,897 hrs · 14,295 cycles

RIGHT OVERWING SLIDE FWD ESCAPE PATH LIGHT INOPERATIVE. REPLACED LAMP FOR RT OVERWING SLIDE FWD ESCAPE PATH LIGHT, OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 89,897 hrs · 14,295 cycles

EMERGENCY LIGHT AT SEAT 12H INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 12H, OPERATIONS CHECKED NORMAL.

Part: LENS — UNSECURE (CABIN) · airframe 89,897 hrs · 14,295 cycles

LEFT NR 4 DOOR EMERGENCY EXIT LIGHT LENS L334 HANGING DOWN. SECURED LENS FOR LT NR 4 DOOR EMERGENCY EXIT LIGHT, OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 89,897 hrs · 14,295 cycles

EMERGENCY LIGHT AT SEAT 13B INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 13B, OPERATIONS CHECKED NORMAL.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,897 hrs · 14,295 cycles

AFT LOWER FUSELAGE HAS CORROSION AT STATION 1219 & STRINGERS 36 LT. INSTALLED DOUBLER REPAIR IAW SRM 53-00-01-2R REPAIR 1.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 89,897 hrs · 14,295 cycles

LEFT OVERWING SLIDE FWD ESCAPE PATH LIGHT INOPERATIVE. REPLACED LAMP FOR LT OVERWING SLIDE FWD ESCAPE PATH LIGHT, OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 89,897 hrs · 14,295 cycles

LEFT AFT FUSELAGE GND SCAN EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LT AFT FUSELAGE GND SCAN EMERGENCY LIGHT, OPERATIONS CHECKED NORMAL.

Part: LENS — MISSING (CABIN) · airframe 89,897 hrs · 14,295 cycles

EMERGENCY LIGHT AT LT NR 1 DOOR MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT LT NR 1 DOOR, OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 89,609 hrs · 14,241 cycles

RT & LT MID GALLEY EMERGENCY LIGHT PATH LOWER ARROWS INOPERATIVE. R & R BATTERY PACK POWER SUPPLY. OPERATIONS CHECKED NORMAL.

Part: SIGN — DAMAGED (CABIN) · airframe 89,609 hrs · 14,241 cycles

EMERGENCY PATH MARKER ARROW DOUBLE SIGN AT FWD RT AISLE ON WALL OF FWD RT GALLEY DAMAGED. INSTALLED NEW LIGHT ASSEMBLY. OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 89,609 hrs · 14,241 cycles

RT & LT MID LAVATORY EMERGENCY LIGHT PATH LOWER ARROWS INOPERATIVE. R & R BATTERY PACK POWER SUPPLY. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 88,214 hrs · 14,007 cycles

RT SIDE OVERWING NR 3 SLIDE ILLUMINATION LIGHT INOPERATIVE. REPLACED LAMP FOR RT SIDE OVERWING NR 3 SLIDE ILLUMINATION LIGHT. OPERATIONS CHECKED NORMAL

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 87,431 hrs · 13,869 cycles

LAVATORY A5 HALLWAY DIRECTIONAL EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK M1210. OPERATIONS CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 87,431 hrs · 13,869 cycles

LAVATORY A6 HALLWAY DIRECTIONAL LIGHT INOPERATIVE. REPLACED POWER SUPPLY M739. OPERATION CHECKED NORMAL.

Part: WIRE — DISCONNECTED (CABIN) · airframe 87,431 hrs · 13,869 cycles

FORWARD ROW 20B CLOSET EMERGENCY LIGHT INOPERATIVE. FOUND WIRE OF THE WALL DISCONNECTED & CAPPED. RECONNECTED WIRES TO THE LIGHT L001. OPERATION CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 87,431 hrs · 13,869 cycles

RT NR 2 INTERIOR DOOR TOP & BOTTOM EXIT EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY M739. OPERATION CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 87,431 hrs · 13,869 cycles

LAVATORY A5 HALLWAY DIRECTIONAL EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY M739. OPERATION CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 87,431 hrs · 13,869 cycles

LT NR 2 INTERIOR DOOR TOP & BOTTOM EXIT LIGHT INOPERATIVE. REPLACED POWER SUPPLY M739. OPERATION CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 87,431 hrs · 13,869 cycles

LT AFT DOOR OUTSIDE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK M00738. OPERATION CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 87,431 hrs · 13,869 cycles

LT AFT SEAT MOUNT & CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY M739. OPERATION CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 87,431 hrs · 13,869 cycles

LT NR 2 EXIT EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR LT NR 2 EXIT EMERGENCY LIGHT. OPERATION CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 85,835 hrs · 13,596 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 85,835 hrs · 13,596 cycles

SEAT 24H FORWARD EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR 24H FORWARD EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 85,835 hrs · 13,596 cycles

SEAT 34B EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT 34B FORWARD EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 85,835 hrs · 13,596 cycles

SEAT 4H FORWARD EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT 4H FORWARD EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — FAULTY (CABIN) · airframe 85,835 hrs · 13,596 cycles

LEFT NUMBER 1 DOOR ENTRY EMERGENCY LIGHT FLICKERS. REPLACED LAMP FOR LEFT NUMBER 1 DOOR ENTRY EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: IRU — INOPERATIVE (ZONE 200) · airframe 85,835 hrs · 13,596 cycles

JFK - INFLIGHT MIA-LHR. CREW REPORTED CAPTAINS STANDBY ATTITUDE DISPLAY BLANKED DURING CRUISE. EMERGENCY DECLARED FLIGHT DIVERTED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED INERTIAL REFERENCE UNIT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — CORRODED (HORIZ STAB) · corrosion level 3 · airframe 85,687 hrs · 13,569 cycles

CORROSION ON HORIZONTAL CENTER BOX UPPER SKIN LEFT BUTTLINE 13 STRINGER 1 TO REAR SPAR. INSTALLED EXTERNAL DOUBLER PER EA B767-55-027802.

Part: SKIN — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 85,687 hrs · 13,569 cycles

CORROSION WAS FOUND ON THE OUTER UPPER SKIN OF THE CENTER HORIZONTAL STABILIZER BOX APPROXIMATELY 17.5 INCHES FORWARD OF THE AFT SPAR AND LEFT BUTTLINE 18.5. INSTALLED EXTERNAL DOUBLER PER EA B767-55-027801.

Part: SKIN — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 85,687 hrs · 13,569 cycles

CORROSION WAS FOUND ON THE CENTER STABILIZER BOX LOWER OUTER SKIN AT THE AFT SPAR AT APPROXIAMTELY RIGHT BUTTLINE 12. INSTALLED EXTERNAL DOUBLER PER EA B767-55-027803.

Part: SKIN — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 85,687 hrs · 13,569 cycles

CORROSION ON HORIZONTAL BOX UPPER SKIN RIGHT BUTTLINE 13.833 TO 32.67, STRINGER 2 TO 3. INSTALLED EXTERNAL DOUBLER PER EA B767-55-027800.

Part: SKIN — DENTED (FUSELAGE) · airframe 85,687 hrs · 13,569 cycles

DENT IN FUSELAGE SKIN AT STATION 1197 AT STRINGER 24 RIGHT. REPAIRED PER SRM 53-00-01-2R-6.

Part: LIGHT — DAMAGED (CABIN) · airframe 83,343 hrs · 13,207 cycles

RIGHT NUMBER 1 EMERGENCY LIGHT FOR THRESHOLD AND DOOR HANDLE IS DAMAGED. REPLACED L287 RIGHT NUMBER 1 EMERGENCY LIGHT ASSEMBLY. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 83,343 hrs · 13,207 cycles

LEFT NUMBER 4 THRESHOLD EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 4 THRESHOLD EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: TRANSMITTER — INOPERATIVE (LT ENGINE) · airframe 81,945 hrs · 12,977 cycles

ATL INFLIGHT MIA-ORD. CREW REPORTED HIGH OIL PRESSURE ON LEFT ENGINE. EMERGENCY DECLARED FLIGHT DIVERTED ATL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT ENGINE OIL PRESSURE TRANSMITTER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — BROKEN (CABIN) · airframe 81,463 hrs · 12,897 cycles

SIDE DOOR EMERGENCY EXIT SIGN AT LEFT NUMBER 1 DOOR LOWER LIGHT INOPERATIVE. REPLACED EXIT LIGHT ASSEMBLY. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 81,463 hrs · 12,897 cycles

RIGHT NUMBER 4 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 4 DOOR EXTERIOR EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 81,463 hrs · 12,897 cycles

EMERGENCY LIGHT ON ROW 27A INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT ROW 27A. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 81,463 hrs · 12,897 cycles

LEFT OVERWING EMERGENCY LIGHT AT TRAILING EDGE INOPERATIVE. REPLACED LAMP FOR LEFT OVERWING EMERGENCY LIGHT AT TRAILING EDGE OF FLAP. OPS CHECK NORMAL.

Part: FSEU — INOPERATIVE (ZONE 100) · airframe 80,790 hrs · 12,796 cycles

MIA - CREW REPORTED LEADING EDG SLAT ASYMMETRY LIGHT ILLUMINATED DURING FLAP EXTENSION. EMERGENCY DECLARED FLIGHT LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FLAP SLAT ELECTRONIC UNIT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FSEU — FAULTED (ZONE 100) · airframe 78,538 hrs · 12,471 cycles

MIA - CREW REPORTED ON APPROACH LEADING EDGE SLAT DISAGREE AT HANDLE POSITION 25. FLIGHT LANDED MIA WITHOUT INCIDENT. REPLACED FLAP/SLAT ELECTRONICS UNIT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 75,013 hrs · 11,833 cycles

DURING AN A CHECK, WHILE PERFORMING THE EMERGENCY LIGHT TEST, DISCOVERED THAT THE LEFT OVERWING EMERGENCY ESCAPE LIGHTING PATH WOULD NOT TEST, THE 3 LEFT OVERWING EMERGENCY LIGHTS WILL NOT LIGHT UP DURING THE TEST. REPLACED BATTERY PACK. OPS CHECKED NORMAL.

Part: SKIN — DENTED (TAILCONE) · airframe 74,823 hrs · 11,798 cycles

DENT ON FUSELAGE TAIL CONE SKIN AT STATION 1845 NEAR STRINGER 3 LEFT APPROXIMATELY 12 IN FORWARD OF THE RUDDER TRAILING EDGE LEFT SIDE. THE DENT MEASURES 1.5 BY .073 EXCEEDING THE SRM LIMITS OF 30. HIGH FREQUENCY EDDY CURRENT INSPECTION FOUND NO CRACKS. THE SKIN IN THIS AREA IS A BONDED ASSEMBLY OF TWO SHEETS OF 0.016 2024-T3 CLAD. REPAIRED PER EA B767-53-008820.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 74,823 hrs · 11,798 cycles

TOOLING DAMAGE WAS FOUND ADJACENT TO A HI-LOK COLLAR ON STRINGER 8 RIGHT AT THE D STATION 111 FRAME. THE DAMAGE CONSISTED OF A DEEP GOUGE TO THE AFT SIDE OF THE HOLE. THE DAMAGE WAS REMOVED BY COUNTERBORING THE FASTENER HOLE TO 0.437€? AND INSTALLING A FREEZE PLUG PER THE EA 008861.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,026 hrs · 11,487 cycles

EMERGENCY LIGHT AT SEAT 23B INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 23B.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - READING LIGHTS AT SEATS 21G, 20J, 40J, AND 38L INOPERATIVE. REPLACED LAMPS AT SEATS 21G, 20J, 40J, AND 38L.

Part: STIFFENER — DAMAGED (MLG WW) · airframe 68,583 hrs

AFW MAIN LANDING GEAR PRESSURE DECK LONGITUDINAL STIFFENER HAS A HOLE IN THE UPPER OUT BOARD FLANGE AT RT BUTTLINE 5.75 STATION 1045. REPAIRED PER MRB 767 3250. (CLOSED)

Part: STIFFENER — DAMAGED (MLG WW) · airframe 68,583 hrs

AFW MAIN LANDING GEAR PRESSURE DECK LONGITUDINAL STIFFENER HAS A HOLE IN THE UPPER OUT BOARD FLANGE AT RT BUTTLINE 5.75 STATION 1060. REPAIRED PER MRB 767 3250. (CLOSED)

Part: LENS — MISSING (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT SEAT 12B MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 12B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (COCKPIT)

SFO - EMERGENCY EXIT LIGHT IN COCKPIT INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY EXIT LIGHT IN COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

SFO - EMERGENCY LIGHTS IN FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK M738 FOR EMERGENCY LIGHTS IN FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHT)

SFO- EMERGENCY LIGHT AT MID GALLEY RIGHT SIDEWALL MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT MID GALLEY RIGHT SIDEWALL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — BROKEN (CABIN)

DFW - EMERGENCY SEAT MOUNTED LIGHTS AT SEAT 23AB IS DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY SEAT MOUNTED LIGHTS AT SEAT 23AB. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 23AB INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 23AB. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

LAX - EMERGENCY LIGHTS AT SEATS 22HJ THROUGH 24HJ INOPERATIVE. SECURED LOOSE CONNECTOR FOR INOPERATIVE EMERGENCY LIGHTS AT SEATS 22HJ THROUGH 24HJ. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: DOOR — INFLT SEPARATION (LT A/C PACK)

WHILE CLIMBING THROUGH 11000 FEET A LOUD BANG AND AIRCRAFT SHUDDER WAS HEARD AND FELT IN AIRFRAME. VIBRATIONS AND RUMBLE COULD BE FELT IN AIRFRAME. POST FLIGHT REVEALED LEFT PACK DOOR HAD DEPARTED AIRCRAFT. LEFT PACK DOOR REPLACED AND STRUCTURE REPAIRED PER BILL OF WORK DATED 26MAY2005 AT AFW. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

SFO - EMERGENCY LIGHT AT SEAT 35H INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 35H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PIN — LOOSE (EMERGENCY LIGHT)

LAX - EMERGENCY ESCAPE PATH LIGHTING AT 37H INOPERATIVE. FOUND PUSH BACK PIN AT CONNECTOR NEXT TO SIDEWALL. RESECURED PINS FOR EMERGENCY ESCAPE PATH LIGHTING AT 37H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — FAULTY (CABIN)

SFO - EMERGENCY LIGHT AT 37H INOPERATIVE. REPLACED CONNECTOR AT FOR EMERGENCY LIGHT AT 37H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FLOORBEAM — CORRODED (FUSELAGE)

AFW - FLOORBEAM AT STATION 347, ON THE BOTTOM SURFACE OF THE UPPER FLOORBEAM AT APPROXIMATELY RBL 73, HAD CORROSION IN AN AREA OF 0.8 INCHES BY 0.5 INCHES AND A DEPTH OF 0.026 AND WAS BEYOND SRM LIMITS. BLENDED OUT CORROSION IN AN AREA OF 0.80 BY 0.50 INCHES MAXIMUM DEPTH OF 0.026 INCHES. PARENT MATERIAL THICKNESS IS 0.090 INCHES. TOTAL THICKNESS LOSS IS 28.9 PERCENT. AREA ALODINED AND FINISHED WITH TWO COATS OF BMS10-11 PRIMER. BLENDED AND FILLED WITH BMS5-95.

Part: LIGHT — DAMAGED (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 20G BULKHEAD DAMAGED. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 20G. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 31H INOPERATIVE. RE-SECURED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 31H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: GENERATOR — INOPERATIVE (APU)

SFO - FLT 1402 - EN ROUTE SFO-DFW, APU AUTO SHUTDOWN RESULTING IN APU GENERATOR GOING OFFLINE. AIR INTERRUPTED AND DECLARED EMERGENCY. LANDED WITHOUT INCIDENT. REPLACED RIGHT IDG, WHICH HAD BEEN PREVIOUSLY MEL'D. ALSO REPLACED APU ELECTRONIC CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SWITCH — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, LEFT SIDE EMERGENCY EXIT LIGHT AT TEST SWITCH INOPERATIVE. REPLACED LEFT SIDE EMERGENCY EXIT LIGHT SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (ROWS 24 AND 37)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT PATH LIGHTS AT 37B AND 24H INOPERATIVE. REPAIRED WIRE FOR EMERGENCY EXIT SEAT PATH LIGHTS AT 37B AND 24H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: CONNECTOR — FAILED (ROW 29B)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT 29B INOPERATIVE. REPAIRED CONNECTOR TO EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT 29B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: FITTING — DEFECTIVE (NR 1 BRAKE)

GRU - FLT 998 - UPON LANDING AT GRU FROM MVD, NR 1 MAIN LANDING GEAR TIRE BLOWOUT. REPLACED NR 1 WHEEL AND TIRE ASSY AND ADJACENT NR 2 MAIN WHEEL AND TIRE ASSY. NR 1 BRAKE SEIZED DURING TEST AFTER WHEEL AND TIRE REPLACEMENT. REPLACED FAULTY HYDRAULC FLUID QUICK DISCONNECT VALVE TO NR 1 BRAKE AND PRECAUTIONARY REPLACEMENT OF NR 1 BRAKE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PROX ELECT UNIT — DEFECTIVE (E/E COMPT)

MIA - FLT 2101 - ON TAKEOFF UPON RAISING THE GEAR, THE GEAR DOOR AMBER WARNING LIGHT REMAINED ILLUMINATED. EICAS MESSAGE ILLUMINATED WHEN GEAR HANDLE WAS PLACED TO OFF POSITION AND THE LEFT GEAR EXTENDED AND LOCKED IN THE DOWN POSITION. AIRCRAFT AIR INTERRUPTED AND RETURNED TO MIA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED REQUIRED CHECKS OF DOOR AND LOCK MECHANISMS WITH NO FAULTS NOTED. MAINTENANCE REPLACED GROUND PROXIMITY ELECTRONIC UNIT. ACCOMPLISHED LANDING GEAR CONTROL ADJUSTMENT AND SWUNG GEAR WITH NO MESSAGES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: ACTUATOR — MALFUNCTIONED (LT MLG)

DFW - FLT 964 - AFTER TAKEOFF GRU, RAISED GEAR HANDLE AND RECEIVED GEAR DISAGREE MESSAGE ON EICAS. LOWERED HANDLE AND NOSE AND RIGHT MLG LIGHTS ILLUMINATED. RAISED GEAR HANDLE RECEIVED SAME INDICATIONS AS AFTER TAKEOFF. AFTER ABOUT 2 MINUTES LEFT MAIN GEAR INDICATED DOWN AND LOCKED. PUT GEAR HANDLE DOWN, GOT 3 GREEN LIGHTS. RAISED HANDLE AND RECEIVED NORMAL INDICATIONS. CONTINUED FLIGHT AND LANDED DFW WITHOUT INCIDENT. REPLACED LEFT SIDE BRACE LOCK ACTUATOR AND MAIN TRUCK POSITIONER ACTUATOR. PERFORMED GEAR RETRACTION FIVE TIMES. ACCOMPLISHED LEAK CHECK AND PERFORMED PSEU BITE TEST. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLOORBEAM — CORRODED (BS 764)

AFW - FLOORBEAM AT STATION 764 HAS CORROSION REMOVAL ON UPPER SURFACE. ALODINE BLENDED AREA. FABRICATE STRAP FROM STAINLESS STEEL. APPLY TWO COATS PRIMER TO STRAP AND FLOORBEAM. FILL BLENDED AREA WITH BMS5-92 TYPE 1. (M)

Part: CONNECTOR — BROKEN (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT PATH LIGHT AT PASSENGER SEAT 36B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEAT 36B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SOCKET — BROKEN (PASSENGER SEAT)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT PATH LIGHT AT PASSENGER SEAT 35 AB INOPERATIVE. REPLACED BROKEN EMERGENCY EXIT LIGHT SOCKET AT PASSENGER SEAT 35 AB. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: LIGHT — MALFUNCTIONED (CABIN)

ORY - FLT 0062 - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH MARKING LIGHTS INOPERATIVE AT PASSENGER SEAT 36H. PERFORMED EMERGENCY EXIT TEST, UNABLE TO DUPLICATE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: LATCH — BROKEN (SLIDE COMPT)

ORD - FLT 0361 - DURING OVERNIGHT MAINTENANCE, LEFT HAND OVER WING SLIDE COMPARTMENT DOOR WOULD NOT OPEN NORMALLY. LATCH LINKAGE AT CENTER LATCH WAS FOUND BROKEN. REPLACED CENTER LATCH ON LEFT HAND OVER WING SLIDE COMPARTMENT AND AS A PRECAUTION, REPLACED AFT ACTUATOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: OVERHEAT LOOP — DIRTY (LT ENGINE)

LAX - FLT 0032 - DURING DEPARTURE FROM LAX, LEFT ENGINE OVERHEAT EICAS MESSAGE APPEARED, THROTTLE WAS RETARDED. WHEN THROTTLE WAS ADVANCED, THE MESSAGE APPEARED ONCE AGAIN. AIR INTERRUPTED AND RETURNED TO LAX, LANDED WITHOUT FURTHER INCIDENT. CHECKED RESISTANCE OF BOTH OVERHEAT LOOPS AND WERE FOUND NORMAL. CLEANED AND RESEATED PYLON PLUG. SYSTEM GROUND CHECKED NORMAL OPERATION. ACCOMPLISHED ENGINE RUN AT TAKEOFF POWER FOR ONE MINUTE, NO OVERHEAT MESSAGE. (X)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 31B INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 31B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT ON PASSENGER SEAT 23B FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEAT 23B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: WIRE — BROKEN (CABIN)

SFO - DURING OVERNIGHT CHECK, EMREGENCY EXIT LIGHTS AT PASSENGER SEAT 20B FOUND INOPERATIVE. REPAIRED BROKEN EMERGENCY EXIT LIGHT WIRE AT PASSENBER SEAT 20B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: WIRE — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS ON LEFT SIDE OF FIRST CLASS AND BUSINESS CLASS CABIN INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT WIRE AT PAX SEAT 2B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 7H AND 21H INTERMITTENT. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR AT PAX SEAT ROW 3H. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)