N374AA

Part: SLIDING WINDOW — OUT OF ADJUST (COCKPIT) · airframe 96,318 hrs · 15,214 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. FIRST OFFICER'S SLIDING WINDOW VERY DIFFICULT TO MOVE TO THE FORWARD POSITION AND OVERCOME MECHANISM SPRINGS AFT. ADJUSTED INBOARD AND OUTBOARD LINK ARM, AFT CORNER OF WINDOW, AFT ROLLER CLUSTER AND CAMBLOCK ON #2 OPENABLE WINDOW. REMOVED AND REINSTALLED LATCH HANDLE LOWER AFT AND TOP COVER. OPERATIONAL CHECK GOOD PER AMM 56-11-02.

Part: WINDOW — FAILED (COCKPIT) · airframe 96,318 hrs · 15,214 cycles

AIRCRAFT IN BASE MAINTENANCE. LEFT HAND WINDSHIELD CRACKED, SHATTERED WITH WINDOW HEAT ON. REPLACED WINDSHIELD PER AMM 56-11-01.

Part: SPAR — DAMAGED (VERTICAL STAB) · airframe 96,318 hrs · 15,214 cycles

AIRCRAFT IN BASE MAINTENANCE, HOLE ON THE VERTICAL STABILIZER AUX SPAR WAS ELONGATED BETWEEN FSS 54 AND FSS 61, LHS. REPAIRED PER EA NR 271511.

Part: PANEL — DELAMINATED (VERTICAL STAB) · airframe 96,318 hrs · 15,214 cycles

DELAMINATION ON RIGHT VERTICAL STABILIZER BETWEEN THE AUXILIARY SPAR AND FRONT SPAR, VSS 195 TO 270. REMOVED AND REPLACED THE PANEL IAW SRM 51-70-10-2R, AND SRM 51-40-02.

Part: PANEL — DELAMINATED (ZONE 300 - STABS) · airframe 96,318 hrs · 15,214 cycles

DELAMINATION ON RIGHT VERTICAL STABILIZER BETWEEN THE AUXILIARY SPAR AND FRONT SPAR, STABILIZER STATIONS 39 TO 92 REMOVED AND REPLACED PANEL PER SRM 51-70-10-2R AND SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 96,318 hrs · 15,214 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON CENTER WING SECTION FLOOR BEAM BETWEEN FUSELAGE STATIONS 800 AND 845, LBL11.5. ACCOMPLISHED SPLICE REPAIR PER SRM 53-00-51-2R-3.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 96,318 hrs · 15,214 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON UPPER CHORD FLOORBEAM UNDER STRAP AND AT SPLICE STRAP, FUSELAGE STATION 1480, BETWEEN RBL65 AND RBL88. REPAIRED PER SRM 53-00-51-2R-1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 96,318 hrs · 15,214 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON UPPER CHORD FLOORBEAM AT FUSELAGE STATION 325, BETWEEN RBL20 AND RBL40. REPAIRED T-CHORD AT STATION 325 BETWEEN LBL50 AND RBL50 PER SRM 53-00-51-2R-1.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 96,318 hrs · 15,214 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON FUSELAGE SKIN LAP SEAM AT THE 5:00 POSITION BEHIND THE RIGHT MAIN LANDING GEAR WHEEL WELL, FUSELAGE STATION 1197+44 TO 1197+70, STRINGER 36R. REPAIRED PER SRM 53-00-01-2R-12.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 96,318 hrs · 15,214 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON MAIN DECK FLOOR BEAM UPPER CHORD AT FUSELAGE STATION 764 BETWEEN LBL64 AND LBL80. REPAIRED IAW SRM 53-00-51-2R-1 FIGURE 1.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 96,318 hrs · 15,214 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON AFT PIT STRINGER 36R BETWEEN FUSELAGE STATIONS 1197+22 TO 1197+44. REMOVED AND REPLACED STRINGER SEGMENT IAW SRM 53-00-03-2R-2.

Part: SKIN — CORRODED (BS 1087-1131) · corrosion level 2 · airframe 96,318 hrs · 15,214 cycles

AIRCRAFT IN BASE MAINTENANCE. AFT CARGO STATION 1087 TO 7 INCHES AFT OF STATION 1109, BETWEEN STRINGER 37L AND 39L, INNER SKIN HAS THREE AREAS OF CORROSION. REPAIRED INNER SKIN PER EA 270774.

Part: SKIN — CORRODED (FUSELAGE) · airframe 96,316 hrs · 15,213 cycles

LAP SEAM AT STRINGER 36R CORRODED AT FS 1197.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 95,548 hrs · 15,089 cycles

4L & 4R DOOR EMER EXIT SIGNS ARE INOPERATIVE. R & R BATTERY PACK IAW AMM 33-51-07. OPERATIONS TESTED OK IAW AMM 33-51-00.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 91,844 hrs · 14,441 cycles

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

Part: CAP — CORRODED (CARGO BAY) · airframe 91,434 hrs · 14,380 cycles

CORROSION FOUND ON J CAP IN FWD CARGO AT STATION 566 & LBL 40. SPLICED IN NEW J CAP SECTION IAW SRM 53-00-07.

Part: REFLECTOR — DEFECTIVE (EXTERIOR LIGHT) · airframe 91,434 hrs · 14,380 cycles

EXTERIOR EMERGENCY LIGHT AT LT NR 4 DOOR FAILED TEST. REPLACED LAMP HOLDER REFLECTOR, OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 91,434 hrs · 14,380 cycles

EXTERIOR EMERGENCY LIGHT AT RT NR 1 DOOR FAILED TEST. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT RT NR 1 DOOR, OPERATIONS CHECKED NORMAL.

Part: WIRE HARNESS — DEFECTIVE (EGT) · airframe 90,831 hrs · 14,286 cycles

JFK INFLIGHT ORD-LHR CREW REPORTED LT HAND ENG EXHAUST GAS TEMPERATURE ERRATIC. FLIGHT DIVERTED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED GREEN CORE HARNESS, SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: PRESSURE SWITCH — INOPERATIVE (HYDRAULIC SYS) · airframe 90,299 hrs · 14,193 cycles

MIA CREW REPORTED CTR HYD SYS HAD LOSS PRESSURE LIGHT & EICAS MESSAGE. FLIGHT LANDED MIA WITHOUT INCIDENT. REPLACED CTR HYD PUMP PRESSURE SWITCH. SYSTEM GND CHECKED NORMAL OPERATION CLOSED.

Part: FITTING — DAMAGED (RT PYLON) · airframe 89,882 hrs · 14,118 cycles

RT PYLON WAS FOUND TO HAVE TWO OVERSIZED HOLES. THE HOLES ARE COMMON TO THE AFT BULKHEAD, SIDE LOAD FITTING INBD & OTBD, & MIDSPAR FITTING INBD & OTBD. REAMED TWO EACH HOLES TO DIAMETER .625 & INSTALLED FREEZE PLUG IAW EA B767-54-032579.

Part: SPAR — DAMAGED (LT PYLON) · airframe 89,882 hrs · 14,118 cycles

LT HAND PYLON WAS FOUND TO AN OVERSIZED HOLE COMMON TO THE INBD MIDSPAR FITTING, MIDSPAR WEB & T-CHORD FITTING & STRAP. ACCOMPLISHED REPAIR IAW EA 767-54-032580 & ECO C3369. REMOVED HOLE THRU MIDSPAR WEB & MID SPAR CHORD ROUND & TRUE AT A DIAMETER OF .625 & INSTALLED FREEZE PLUGS.

Part: BULKHEAD — DAMAGED (LT PYLON) · airframe 89,882 hrs · 14,118 cycles

LT PYLON WAS FOUND TO AN OVERSIZED HOLE IN THE AFT BULKHEAD, COMMON TO THE MID SPAR FITTING. REMOVED HOLE IN BULKHEAD ROUND & TRUE TO DIAMETER OF .625 & INSTALLED FREEZE PLUG IAW EA B767-54-032583.

Part: SKIN — DAMAGED (LT PYLON) · airframe 89,882 hrs · 14,118 cycles

LT HAND PYLON WAS FOUND TO AN OVERSIZED HOLE IN THE INBD SKIN, COMMON TO THE SIDE LOAD FITTING, NEAR A GSE FITTING. ACCOMPLISHED REPAIR IAW EA B767 54-032581 & ECO C3369. HFEC OPEN HOLE INSPECTED WITH NO CRACK INDICATION NOTED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 86,294 hrs · 13,530 cycles

FORWARD CARGO BODY FRAME STATION 500 UPPER FLANGE IS BENT AND HAS A LONG CRACK, ABOVE AND AROUND STRINGER 31 LEFT. FABRICATED NEW SECTION OF FRAME UPPER FLANGE PER AARD 51-20-00-1 AND INSTALLED PER SRM 51-10-02.

Part: CAP — CORRODED (CARGO BAY) · corrosion level 2 · airframe 86,294 hrs · 13,530 cycles

SHORT J-CAP AT LOWER DOOR CUTOUT IN FORWARD CARGO HAS CORROSION ON BOTTOM SIDE AT NUT PLATE STATION 504. REPLACED J-CAP PER SRM 51-10-02.

Part: TORQUE BOX — CRACKED (LT PYLON) · airframe 86,294 hrs · 13,530 cycles

LEFT PYLON UPPER TORQUE BOX SKIN CRACKED AT GENERATOR FEEDER CABLE PASS THROUGH, OUTBOARD AFT NUT PLATE. INSTALLED DOUBLER REPAIR PER AARD 54-52-01.

Part: STRUCTURE — CRACKED (RT PYLON) · airframe 86,294 hrs · 13,530 cycles

RIGHT PYLON INSIDE FORWARD TORQUE BOX ACCESS, UPPER SKIN AT CUTOUT FOR POWER FEEDER CABLES CRACKED AT NUT PLATE AT AFT INBOARD SIDE. INSTALLED DOUBLER PER AARD 54-52-01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 86,294 hrs · 13,530 cycles

STATION 1219 CARGO FLOOR INNER J FRAME CORRODED. INSTALLED REPAIR STRAP PER SRM 53-00-07-2R.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 86,294 hrs · 13,530 cycles

UPPER FUSELAGE SKIN ON RIGHT SIDE OF VERTICAL STABILIZER BETWEEN STATIONS 1605 AND 1629 DAMAGED. INSTALLED EXTERNAL DOUBLER PER SRM 530-00-01-2R 1.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 86,294 hrs · 13,530 cycles

GOUGE/DELAMINATION TO NUMBER 6 SLAT TRAILING EDGE WEDGE, UNDER SIDE. LOCATED 8.5 INCHES INBOARD OF OUTBOARD END. ACCOMPLISHED METAL BOND REPAIR PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 86,294 hrs · 13,530 cycles

CRACK IN NUMBER 10 LEADING EDGE SLAT SKIN, 42 INCHES FROM INBOARD END. INSTALLED FLUSH DOUBLER REPAIR PER SRM 57-43-01-2R 2.

Part: SLAT — CRACKED (RT WING) · airframe 86,294 hrs · 13,530 cycles

CRACK IN NUMBER 9 LEADING EDGE SLAT, 42 INCHES FROM INBOARD END. INSTALLED FLUSH DOUBLER REPAIR PER SRM 57-43-01-2R 2.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 86,117 hrs · 13,503 cycles

EXTERIOR EMERGENCY LIGHTS 1 TO 4 FAILED TO ILLUMINATE. REPLACED LAMP. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 85,907 hrs · 13,469 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 85,907 hrs · 13,469 cycles

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

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 85,907 hrs · 13,469 cycles

LEFT NUMBER 2 DOOR LOWER EMERGENCY LIGHT ON UPPER SIGN INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 2 DOOR LOWER EMERGENCY LIGHT ON UPPER SIGN. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 85,907 hrs · 13,469 cycles

EMERGENCY EXIT LIGHT ABOVE DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY IN COCKPIT FOR EMERGENCY EXIT LIGHT ABOVE DOOR. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 85,907 hrs · 13,469 cycles

LEFT NUMBER 1 DOOR LOWER EMERGENCY LIGHTS ON UPPER SIGN INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 1 DOOR LOWER EMERGENCY LIGHTS ON UPPER SIGN. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 85,398 hrs · 13,396 cycles

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

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 83,406 hrs · 13,067 cycles

EMERGENCY EXIT SIGN LENS MISSING AT SEAT 21G. REPLACED LENS FOR EMERGENCY EXIT SIGN AT SEAT 21G. OPS CHECKED NORMAL.

Part: ENGINE — FAILED (LEFT) · airframe 83,339 hrs · 13,055 cycles

MIA - CREW REPORTED LEFT ENGINE OIL LOSS. LEFT ENGINE SHUTDOWN (SINGLE ENGINE TIME 20 MINS). EMERGENCY DECLARED FLIGHT LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE AT MIA ON 02/14/2012. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 83,079 hrs · 13,008 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 82,121 hrs · 12,844 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 82,121 hrs · 12,844 cycles

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

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 81,837 hrs · 12,803 cycles

SEAT 33H EMERGENCY LIGHT INOPERATIVE. REPINNED SEAT 33H EMERGENCY LIGHT CONNECTOR OPS CHECK NORMAL.

Part: SWIVEL FITTING — CORRODED (LT MLG) · corrosion level 2 · airframe 80,533 hrs · 12,609 cycles

CORROSION ON THE LEFT MAIN LANDING GEAR SIDE STRUT SWIVEL FITTING. THE CORROSION IS LIMITED TO THE OUTBOARD LUG OUTBOARD FACE OF THE MAIN PIVOT JOINT TO THE MAIN LANDING GEAR SIDE STRUT. ACCOMPLISHED REPAIR PER EA B767-57-017039.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 79,988 hrs · 12,515 cycles

DEN - INFLIGHT JFK-SFO. CREW REPORTED FLIGHT DECK O2 PRESSURE DROPPING DURING FLIGHT. FLIGHT DIVERTED DEN LANDED WITHOUT INCIDENT. CAPTAINS O2 MASK FOUND TO BE LEAKING. REPLACED CAPTAINS O2 MASK WITH 2ND OBSERVERS MASK AND PLACARD 2ND OBSERVERS SEAT INOPERATIVE PER MEL 25-19D AUTH 1103-C. REPLACED SECOND OBSERVERS O2 MASK AT SFO ON 03/25/2011. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 78,852 hrs · 12,327 cycles

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

Part: COVER — MISSING (EXIT SIGN) · airframe 77,179 hrs · 12,055 cycles

RIGHT FORWARD OVERWING ESCAPE HATCH EXIT SIGN COVER MISSING. REPLACED OVERWING EXIT SIGN. OPS CHECKED NORMAL.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,953 hrs · 11,670 cycles

FOUND CORROSION ON THE FUSELAGE SKIN INNER SURFACE BETWEEN STATION 1094 AND 1128 COMMON TO THE LEFT WING-TO-BODY FAIRING ATTACH POINTS. REMOVED CORROSION AND REPAIRED UNDER ENGINEERING AUTHORIZATION B767-53-008096.

Part: STRUCTURE — CORRODED (CARGO BAY) · corrosion level 2 · airframe 74,953 hrs · 11,670 cycles

FOUND CORROSION ON FORWARD CARGO DOOR LOWER INNER AND OUTER CHORD. REMOVED CORROSION AND REPAIRED UNDER SRM 53-00-15-1A AND ENGINEERING AUTHORIZATION B767-53-008069.

Part: BULKHEAD — GOUGED (FUSELAGE) · airframe 74,953 hrs · 11,670 cycles

BULKHEAD WEB NEAR LEFT STATION 1809 OUTER CHORD WAS GOUGED. BLENDED WEB UNDER ENGINEERING AUTHORIZATION B767-53-008055.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 74,953 hrs · 11,670 cycles

CRACK INDICATIONS WERE FOUND ON THE FORWARD LOWER HOLE COMMON TO THE BULKHEAD LEFT FORWARD OUTER CHORD AND STRINGER 12A LEFT TENSION FITTING AT STATION 1809.5. THE FASTENER HOLE WAS OVERSIZED TO 0.2782 INCHES. BOEING APPROVED THE OVERSIZED HOLE TO 2ND OVER WITHOUT COLD-WORKING THE HOLE.

Part: BULKHEAD — CRACKED (HORIZ STAB) · airframe 74,953 hrs · 11,670 cycles

CRACK INDICATIONS WERE FOUND ON THE AFT UPPER HOLE COMMON TO THE OUTER CHORD AND S-12A RIGHT TENSION FITTING AT BULKHEAD RT FWD OUTER CHORD. THE FASTENER HOLE WAS OVERSIZED TO 0.2782 TO REMOVE ANY INDICATIONS. BOEING APPROVED THE OVERSIZED HOLE TO 2ND OVER WITHOUT COLD-WORKING THE HOLE.

Part: LENS — MISSING (CABIN)

SFO EMERGENCY LIGHT AT SEAT 21B MISSING LENS. REPLACED LENS AT SEAT 21B.

Part: CONNECTOR — LOOSE (CABIN) · airframe 72,269 hrs

SFO AISLE EMERGENCY LIGHT AT ROW 38 INOPERATIVE. SECURED SEAT CONNECTOR.

Part: LAMP — BROKEN (EMERGENCY LIGHTS) · airframe 72,115 hrs

SFO - EMERGENCY LIGHT AT SEAT 28H BROKEN APART. REPLACED LAMP AT SEAT 28H.

Part: SHROUD — BROKEN (EMERGENCY LIGHTS) · airframe 72,115 hrs

SFO - EMERGENCY LIGHT AT SEAT 28H BROKEN APART. REPLACED SHROUD AT SEAT 28H.

Part: LENS — BROKEN (EMERGENCY LIGHTS) · airframe 72,115 hrs

SFO - EMERGENCY LIGHT AT SEAT 28H BROKEN APART. REPLACED LENS AT SEAT 28H.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,811 hrs · 69,811 cycles

JFK - EMERGENCY LIGHT SIGNS AT NR 2 EXIT DOORS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT SIGNS AT NR 2 EXIT DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (S)

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 69,599 hrs

DFW - EXTERIOR EMERGENCY LIGHT AT AFT LT DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT AFT LT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,481 hrs

MIA - EMERGENCY LIGHT AT SEAT 5H INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 5H. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: LIGHT — MISSING (CABIN) · airframe 68,854 hrs

SFO - EMERGENCY LIGHT AT SEAT 29B MISSING. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 29B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: DOOR — MALFUNCTIONED (RT OVERWING)

SFO - RIGHT OVERWING SLIDE DID NOT SUCCESSFULLY DEPLOY. UNABLE TO DEACTIVATE BOTTLE. OUTER DOOR DID NOT OPEN PROPERLY AT TIME OF SLIDE DEPLOYMENT. REPLACED RIGHT OVERWING SLIDE AND DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — BROKEN (CABIN) · airframe 68,619 hrs

SFO - EMERGENCY LIGHT AT SEAT 29B BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT LEFT SEAT 29B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 4B INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 4B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

MIA - EMERGENCY SEAT MOUNTED LIGHT AT SEAT 21H INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY SEAT MOUNTED LIGHT AT SEAT 21H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS)

JFK - EMERGENCY LIGHT AFT OF MID GALLEY RIGHT SIDE INOPERATIVE. RECONNECTED LOOSE PLUG FOR EMERGENCY LIGHT AFT OF MID GALLEY RIGHT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMEGENCY LIGHTS)

MIA - EMERGENCY LIGHT AT SEAT ROW 31H OVERHEAD INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 31H OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

MIA - EMERGENCY LIGHT AT OVERHEAD COCKPIT ENTRY EXIT SIGN INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT OVERHEAD COCKPIT ENTRY EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT EXIT MARKER AT RIGHT NUMBER ONE DOOR MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT EXIT MARKER AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS)

JFK - EMERGENCY LIGHT AT CEILING RIGHT SIDE NEXT TO FLIGHT ATTENDANT READING LIGHT INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT CEILING RIGHT SIDE NEXT TO FLIGHT ATTENDANT READING LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FLASHLIGHT — INOPERATIVE (CABIN)

SFO - EMERGENCY FLASHLIGHT AT RIGHT AFT FLIGHT ATTENDANT SEAT INOPERATIVE. REPLACED EMERGENCY FLASHLIGHT AT RIGHT AFT FLIGHT ATTENDANT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHIELD — LOOSE (EMERGENCY LIGHTS)

CDG - FOUND EMERGENCY LIGHT AT SEAT 20CEG BULKHEAD HAS A LOOSE COVER. SECURED EMERGENCY LIGHT COVER AT SEAT 20CEG BULKHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

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

Part: WIRE — DISCONNECTED (CABIN)

ORD - EMERGENCY LIGHTS AT RIGHT AISLE JUST AFT OF FORWARD GALLEY INOPERATIVE. RECONNECTED WIRES FOR EMERGENCY LIGHTS AT RIGHT AISLE JUST AFT OF FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHT AT SEAT 35H INOPERATIVE. REPLACED CONNECTOR AND RELAMPED FOR EMERGENCY LIGHT AT SEAT 35H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - SEAT MOUNTED EMERGENCY LIGHTS FROM ROW 23 RIGHT SIDE TO ROW 34 RIGHT SIDE INOPERATIVE. REPLACED BATTERY PACK M1209 FOR EMERGENCY LIGHTS AT ROW 23 RIGHT HAND TO ROW 34 RIGHT HAND. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LINE — LEAKING (HYD SYSTEM)

JFK - LEFT HYDRAULIC FLUID LOW AND DROPPING, SYSTEM WAS SHUT DOWN. LANDED JFK WITHOUT INCIDENT. SECURED HYDRAULIC LINE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — DISCONNECTED (CABIN)

DFW - EMERGENCY EXIT LIGHT AT RIGHT HAND FORWARD GALLEY INOPERATIVE. FOUND LOOSE WIRE. RECONNECTED WIRE FOR EMERGENCY EXIT LIGHT AT RIGHT HAND FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — BROKEN (CABIN)

SFO - EMERGENCY LIGHT AT LOWER END OF RIGHT HAND FIRST CLASS GALLEY HAS BROKEN BASE AND MISSING LENS COVER. REPLACED BASE AND LENS COVER FOR EMERGENCY LIGHT AT LOWER END OF RIGHT HAND FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY LIGHTING INOPERABLE FROM ROWS 20 TO 24. REPLACED BATTERY PACK AT 23A/B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — DAMAGED (CABIN)

LAX FORWARD GALLEY RT AISLE EMERGENCY FLOOR FLOOD LIGHT INOPERATIVE. REPAIRED WIRING FOR FORWARD GALLEY RT AISLE EMERGENCY FLOOR FLOOD LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED

Part: SEAT TRACK — CORRODED (FUSELAGE)

FOUND SEAT TRACK AT STATION 764 LBL 11 HAD CORROSION BLENDED ON UPPER SURFACE OF FLANGES. BLEND OUT CORROSION. DYE CHECK FOR CRACKS. ALODINE THE BLENDED AREA. APPLY 2 COATS OF PRIMER. REINSTALL FASTENERS PER MRB 767-2527 DATED 10/07/2003. (M)

Part: SKIN — CORRODED (FUSELAGE)

FOUND FUSELAGE SKIN ON INNER SIDE HAD CORROSION BLEND BEYOND SRM LIMITS. BLEND OUT CORROSION PER ATTACHED SKETCH. DYE CHECK TO ENSURE CRACK FREE. ROTO PEEN BLENDED AREA. REFINISH THE BLENDED AREA PER SRM. FILL BLENDED AREA WITH BMS 5-95. SHIM AS REQUIRED TO REINSTALL THE DRAIN BRACKETS TO THEIR PREVIOUS LOCATIONS PER MRB 767-2528. (M)

Part: IDG — FAILED (RT ENGINE)

RIGHT GENERATOR DRIVE LEFT ILLUMINATED, IDG DISCONNECTED AS PER OM. UNABLE TO REMOVED QAD RING FOR IDG. REPLACEMENT, PLACARDED RIGHT IDG AS PER MEL 24-01 AUTH LGWA-354DC-A. REMOVED AND REPLACED RIGHT IDG PER MM. OPS CHECK GOOD. NO LEAKS NOTED REMOVED MEL 24-01. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTS ROW 26H AND AFT INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGHTS BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DAMAGED (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LIGHTING AT SEAT 36H INOPERATIVE. REPAIRED SEAT CONNECTOR AT SEAT 36H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHT AT 25H INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGHT CONNECTOR AT SEAT 25H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LIGHTING SEAT 40H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY DUE TO BROKEN WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — DISCONNECTED (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY EXIT LIGHT COVER MISSING AND WIRES DISCONNECTED AT SET 7B. REPLACED EMERGENCY EXIT LIGHT COVER AND RECONNECTED WIRES TO SEAT 7B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 25 A/B INOPERATIVE. TIGHTENED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 25 A/B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 25B INOPERATIVE. SECURED LOOSE CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — INOPERATIVE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 28B INOPERATIVE. RE-SECURED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 28B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 23H INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT SEAT 23H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 28B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 22H INOPERATIVE. SECURED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 22H. SYSTEM GROUND CHECKED NORMAL OPERATION. M)

Part: CONNECTOR — DAMAGED (CABIN SEAT)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 20B INOPERATIVE. RE-PIN EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 20B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

SFO - DURING OVER-NIGHT, MAINTENANCE EMERGENCY EXIT ESCAPE PATH LGIHTS AT SEATS 22H, 24A, AND 26A INOPERATIVE. REPAIRED BROKEN WIRE AT SEAT 24A. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: FIRE LOOP — DEFECTIVE (LT ENGINE)

LAX - FLT 898 - AFTER TAKEOFF LAX, MIA LEFT ENGINE FIRE LOOP NR 2 LIGHT ILLUMINATED FOLLOWED BY LOOP NR 1 LIGHT. AIRCRAFT RETURNED TO LAX AND LANDED WITHOUT INCIDENT. REPLACED LEFT ENGINE UPPER AFT FIRE DETECTION LOOP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FRAME J CAP — CORRODED (BS 1285)

AFW - CHORD (J-CAP) HAS CORROSION REMOVAL IN UPPER AND LOWER SURFACE. MATERIAL REMAINING IS BEYOND SRM LIMITS. REMOVED ALL CORROSION, ENSURED BLENDOUTS IN AREA OF NUTPLATES ARE FLAT TO ALLOW PROPER SEATING WHEN INSTALLED. REFINISHED BLENDED AREA PER SRM 53-00-07, FIG 1D1. TST: 27,816.53 HOURS. CYCLES: 4,326. (X)

Part: FLOORBEAM — CORRODED (BS 347)

AFW - FLOORBEAM AT STA 347 HAS CORROSION REMOVAL ON UPPER SURFACE. ALODINED BLENDED AREA. FABRICATED STRAP FROM STAINLESS STEEL. APPLIED 2 COATS PRIMER TO STRAP AND FLOORBEAM AND BLENDED AREA. INSTALLED STRAP WET WITH SEALANT WITH HI-L0KS. TST: 27,816.33 HOURS. CYCLES: 4,326. (X)

Part: MLG — FAILED (LEFT)

ORD - FLT 0037 - ON TAKEOFF UPON RAISING THE GEAR, THE GEAR DOOR WARNING LIGHT REMAINED ILLUMINATED. FOLLOWED ABNORMAL PROCEDURES. THE GEAR DOOR WARNING LIGHT REMAINED ILLUMINATED EVEN WHEN THE GEAR WAS DOWN AND LOCKED. GEAR WAS LEFT IN THE DOWN AND LOCKED POSITION AND AN EMERGENCY LANDING AT ORD WAS ACCOMPLISHED WITHOUT INCIDENT. REPLACED MLG ASSY. SWUNG GEAR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT 21B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT SEAT 21B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: IDG — MALFUNCTIONED (NR 2 ENGINE)

R GEN DRIVE EICAS MESSAGE WITH ASSOCIATED DRIVE LIGHT ON, GEN DRIE DISCONNECTED AS PER ABNORMAL CHECKLIST. PLACARDED RT IDG INOP PER MEL 24-1 AUTH NR 5-49DC-B ENT IN MIC. BOTH IDGS SERVICED AND APU OIL QTY READS FULL. NO SERVICE REQUIRED. REMOVED AND REPLACED NR 2 ENGINE IDG OPS AND LK CHECK GOOD 374240236/1854. (M)

Part: CONNECTOR — BROKEN (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 27H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEAT 27H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: CONNECTOR — BROKEN (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 39B INOPERATIVE. REPLACED BROKEN EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 39B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — BROKEN (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT PAX SEATS 37B AND 40H INOPERATIVE. REPLACED BROKEN EMERGENCY EXIT LIGHT CONNECTORS AT PAX SEATS 37B AND 40H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — FAILED (E/E COMPT)

CCS - MAIN BATTERY CHARGER EICAS MESSAGE RECEIVED IN FLIGHT. MAIN BATTERY CHARGER AND APU SWAPPED. REPLACED MAIN BATTERY. PLACARDED APU INOP PER MEL. ENTERED MIS SHEET. APU AND BATTERY CHARGER OPS TEST PERFORMED. SYSTEM BACK TO NORMAL. OK FOR SERVICE. REMOVED PLACARD. MEL 49-01 AUTH NR 6-447DC-C. MIS SHEET CLEARED. (M)

Part: WIRE — LOOSE (RT FWD DOOR)

SFO - DURING OVERNIGHT MAINTENANCE, FOUND THE RIGHT FORWARD ENTRY DOOR OUTSIDE EMERGENCY EXIT LIGHT INOPERATIVE. TIGHTENED LOOSE GROUND WIRE ON RIGHT FORWARD ENTRY DOOR OUTSIDE EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLOORBEAM — CORRODED (BS 800/840)

AFW - FLOORBEAM IS BEYOND SRM LIMITS AFTER BLEND OUT OF CORROSION AND GOUGES. FLAP PEEN, BLEND, DYE-CHECK, ALODINE, PRIME, FILL WITH BMS 5-28 SEALANT AND PAINT PER ENGINEERING MRB 767-988. T.S.T. 14,105. CYCLES, 2,184. (X)

Part: SKIN — CHAFED (TE FLAP)

AFW - FLAP NOSE SKIN IS CHAFED BEYOND SRM LIMITS. BLENDED DYE-CHECKED ALODINED, PRIMED, FILLED WITH BMS 5-28 SEALANT AND PAINTED AREA PER ENGINEERING MRB 767-287. T.S.T. 14,105. CYCLES, 2,184. (X)