N640A

Part: POWER SUPPLY — DEFECTIVE (CABIN) · airframe 73,158 hrs · 25,985 cycles

SEAT MOUNTED EMER PATH LIGHTS DIM BETWEEN SEATS 16D & 25D. R & R EMER PATH LIGHT POWER SUPPLY IAW AMM 33-51-07. SYS CHECKED NORMAL.

Part: UNKNOWN — ODOR (CABIN & COCKPIT) · airframe 72,963 hrs · 25,906 cycles

ELECTRICAL ODOR IN THE CABIN & COCKPIT. ODOR STOPPED WHEN UTILITY BUSES WERE TURNED OFF. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. INSPECTED ACFT WITH UTILITY BUSES & RECIRCULATION FANS ON WITH NO FAULTS NOTED. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 71,721 hrs · 25,458 cycles

RIGHT NR 2 DOOR EXTERNAL SLIDE SPOT LIGHT INOPERATIVE. R & R RT NR 2 DOOR EXTERNAL SLIDE SPOT LIGHT. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,363 hrs · 24,962 cycles

BULLNOSE EMERGENCY LIGHT AT 5E INOPERATIVE. REPLACED LAMP FOR BULLNOSE EMERGENCY LIGHT AT 5E. OPERATIONS CHECKED NORMAL.

Part: SUPPORT FITTING — CORRODED (FLAP TRACK) · corrosion level 2 · airframe 69,982 hrs · 24,831 cycles

RT WW AFT BULKHEAD RBL 29 INBD MAIN FLAP TRACK SUPPORT FITTING CORRODED. ACCOMPLISHED REPAIR TO RT WW AFT BULKHEAD RBL 29 INBD MAIN FLAP TRACK SUPPORT FITTING IAW REO-G16658 REVISION C FIG 3 & AA EA B757-57-031566.

Part: CONNECTOR — DIRTY (CABIN) · airframe 67,459 hrs · 23,925 cycles

SEAT 25D EMERGENCY LIGHT INOPERATIVE. CLEANED AND RESEATED CONNECTORS UNDER SEAT AREA. OPS CHECK NORMAL.

Part: SLAT — DAMAGED (NR 4) · airframe 64,696 hrs · 22,895 cycles

NUMBER 4 LEADING EDGE SLAT HAS A TEAR IN THE TRAILING EDGE, IN SAME AREA OF YELLOW LIFE RAFT BRACKET ON TOP OF LEFT WING. HOT BONDED CORE AND DOUBLERS PER SRM 51-70-10.

Part: TERMINAL — FAULTY (ELECTRICAL SYS) · airframe 64,134 hrs · 22,689 cycles

LAX - CREW REPORTED IMMEDIATELY AT ROTATION BATTERY DISCHARGE LIGHT STARTED FLASHING, TEMPORARY LOSS OF SOME INSTRUMENT LIGHTING, AND SEVERAL AMBER EICAS MESSAGES. EMERGENCY DECLARED FLIGHT RETURNED LAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND FAULTY A AND C PHASE TERMINALS OF BUS TIE RELAY C902. REPLACED TERMINALS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: TRANSMITTER — INOPERATIVE (HYDRAULIC SYS) · airframe 63,839 hrs · 22,574 cycles

JFK - CREW REPORTED LOSS OF CENTER HYDRAULIC SYSTEM. EMERGENCY DECLARED FLIGHT RETURNED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED CENTER HYDRAULIC FLUID QUANTITY TRANSMITTER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONTROL MODULE — FAULTY (STABILIZER TRIM) · airframe 63,612 hrs · 22,487 cycles

MIA - CREW REPORTED STAB TRIM EICAS DURING CLIMBOUT. FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT STABILIZER TRIM CONTROL MODULE THAT WAS FAULTY. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 63,318 hrs · 22,378 cycles

CEILING EMERGENCY LIGHTS ABOVE AFT FLIGHT ATTENDANT SEAT INOPERATIVE. REPLACED CHARGER AND BATTERIES FOR CEILING EMERGENCY LIGHTS ABOVE AFT FLIGHT ATTENDANT SEAT. OPS CHECKS OK.

Part: CONNECTOR — BURNED (SPOILER) · airframe 61,843 hrs · 21,864 cycles

DFW - CREW REPORTED RIGHT WING SPOILERS WOULD NOT STOW ON APPROACH. EMERGENCY DECLARED LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND BURNED PLUG ON NUMBER 3 SPEED BRAKE POWER CONTROL MODULE. REPLACED PLUG. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONNECTOR — LOOSE (CABIN) · airframe 61,594 hrs · 21,778 cycles

SEATS 1EF ESCAPE PATH LIGHT INOPERATIVE. SECURED LOOSE CONNECTOR AT SEATS 1EF. OPS CHECKED NORMAL.

Part: SKIN — DAMAGED (LE SLAT) · airframe 61,398 hrs · 21,701 cycles

RIGHT WING HAS SEVERAL PITS IN THE EXTERNAL SKIN AT THE INBOARD END OF LEADING EDGE SLAT. REMOVED PITTED SKIN AND INSTALLED NEW SKIN ON INBOARD END OF SLAT PER ESO 90401.

Part: SLAT — CORRODED (LT WING) · corrosion level 2 · airframe 61,398 hrs · 21,701 cycles

LEFT WING THERE IS CORROSION AROUND A RIVET HEAD ON THE NUMBER FOUR SLAT AT THE OUTBOARD DRIVE TRACK. REMOVED FASTENER AND REMOVED CORROSION BY BLENDING THEN INSTALLED STRAP DOUBLER PER EA 757-27-012256.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 61,398 hrs · 21,701 cycles

LEFT WING THERE IS DELAMINATION OF THE TRAILING EDGE WEDGE ON THE NUMBER FOUR SLAT APPROXIMATELY 4 INCHES FROM THE OUTBOARD END OF THE SLAT. REMOVED DAMAGE AND INSTALL NEW TRAILING EDGE WEDGE PER ESO 90248.

Part: SLAT — CORRODED (LT WING) · corrosion level 2 · airframe 61,398 hrs · 21,701 cycles

LEFT WING THERE IS CORROSION ON THE NUMBER ONE SLAT APPROXIMATELY 2 INCHES FROM THE OUTBOARD END OF THE SLAT. REMOVED CORROSION AND INSTALLED FLUSH DOUBLER PER AARD 57-43-00-1.

Part: SKIN — DAMAGED (LE SLAT) · airframe 61,398 hrs · 21,701 cycles

LEFT WING: THERE IS DELAMINATION OF THE TRAILING EDGE WEDGE ON THE NUMBER ONE SLAT AT THE INBOARD END OF THE SLAT. CUT OUT DAMAGED AREA OF SKIN AND CORE. SHAPED NEW SECTION OF CORE. READY TO HOT BOND THE FIRST STAGE OF A TWO STAGE CURE PER SRM 51-70-10-2R FIGURE 209. INSTALLED BONDED PERMANENT REPAIR PER SRM 51-70-10-2R.

Part: SLAT — DAMAGED (WING) · airframe 61,398 hrs · 21,701 cycles

NUMBER 7 SLAT HAS A BLIND FASTENER AT RIB WHERE A PREVIOUS BLEND-OUT WAS ACCOMPLISHED. CUT OUT DAMAGED AREA AND INSTALLED REPAIR PER AARD 57-43-00-1 PAGE TWO.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,569 hrs · 21,374 cycles

RIGHT TRANSITION PANEL CORRODED STATIONS 636 TO 644. REMOVED AND REPLACED TRANSITION PANEL WITH SERVICEABLE PANEL PER SRM 51-70-00-06.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 60,569 hrs · 21,374 cycles

FLOORBEAM CRACKED STATION 700 LEFT BUTTLINE 24 TO LEFT BUTTLINE 45.5. INSTALLED DOUBLER PER AARD 53-30-51-2.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,569 hrs · 21,374 cycles

CORROSION ON CREASE ANGLE STATION 680 TO 740. REMOVED CREASE ANGLE AND INSTALLED NEW SECTION ON CARD 53-98-01 ITEM 63.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 60,569 hrs · 21,374 cycles

INTERCOSTAL CRACKED AT STATION 660 LEFT BUTTLINE 48. REPLACED INTERCOSTAL PER SRM 51-10-02.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,569 hrs · 21,374 cycles

CORROSION ON CREASE ANGLE STATIONS 760 TO 864. REMOVED AND REPLACED CREASE ANGLE PER AARD 53-30-13-1.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 60,569 hrs · 21,374 cycles

INTERCOSTAL CRACKED AT LEFT BUTTLINE 24 AND STATIONS 660 TO 680. INSTALLED NEW INTERCOSTAL PER SRM 51-10-02-0G.

Part: SHEAR TIE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 60,569 hrs · 21,374 cycles

FORWARD CARGO DOOR LOWER EDGE AT STATION 580 SHEAR TIE IS CORRODED. REMOVED AND REPLACED SHEAR TIE WITH SERVICEABLE SHEAR TIE PER SRM 51-70-00-0G.

Part: BULLNOSE — CRACKED (RT WING) · airframe 60,569 hrs · 21,374 cycles

NUMBER 2 ENGINE WING BULLNOSE CRACKED ON INBOARD SIDE. INSTALLED DOUBLER PER AARD 57-41-01-6.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,052 hrs · 21,182 cycles

AFT SECTION OF SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 57,152 hrs · 20,126 cycles

LAX - INFLIGHT SNA-ORD - RIGHT ENGINE COMPRESSOR STALLED ON TAKEOFF. EMERGENCY DECLARED, LANDED LAX WITHOUT INCIDENT WITH RIGHT ENGINE AT REDUCED POWER. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER 2 ENGINE ON FEBRUARY 15TH AT LAX. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONTROL UNIT — INOPERATIVE (BLEED AIR VALVE) · airframe 57,147 hrs · 20,124 cycles

ORD - CREW REPORTED ON CLIMBOUT IN FLIGHT SHUTDOWN OF RIGHT ENGINE, SINGLE ENGINE TIME 9 MINUTES. EMERGENCY DECLARED, RETURNED ORD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED BLEED VALVE CONTROL UNIT AND TRANSIT PRESSURE UNIT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 56,514 hrs

MIA - EMERGENCY LIGHTS IN FIRST CLASS DIM. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRUCTURE — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,247 hrs · 19,799 cycles

AFT GUTTER BOX CORRODED. REPAIRED IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,247 hrs · 19,799 cycles

FLOORBEAM CORRODED. REPAIRED IAW EA B757-53-004738.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,247 hrs · 19,799 cycles

FLOORBEAM CORRODED. REPAIRED IAW EA B757-53-004838 DATED 10/24/2008.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHTS AT SEAT ROWS 9 TO 15 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 9 TO 15. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT RIGHT NR TWO DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT RIGHT NR TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT LEFT NR TWO DOOR SIDEWALL INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT LEFT NR TWO DOOR SIDEWALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: LIGHT — INOPERATIVE (ROW 31 ABC)

DFW - EMERGENCY LIGHT AT SEAT ROW 31ABC INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT ROW 31ABC. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DFW - EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY BULL NOSE LIGHT AT FORWARD LEFT INOPERATIVE. REPLACED LAMPS FOR EMERGENCY BULL NOSE LIGHT AT FORWARD LEFT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT LEFT AFT OVERWING EXIT INOPERATIVE. REPLACED LAMP AND REMOVED LIGHT CORROSION FOR EMERGENCY LIGHT AT LEFT AFT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WINDOW — CRACKED (COCKPIT)

ORD INFLIGHT T2242/06SEP - RIGHT FORWARD WINDOW HEAT FAILED. TURNED OFF POWER TO WINDOW HEAT AND SECONDS LATER FIRST OFFICERS WINDOW DEVELOPED LARGE CRACK. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED FIRST OFFICERS NUMBER ONE WINDOW. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

MIA - EMERGENCY LIGHTS AT FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

MIA - EMERGENCY LIGHTS AT FORWARD TO MID COACH INOPERATIVE. REPLACED BATTERY PACK AT RIGHT NUBMER TWO DOOR FOR EMERGENCY LIGHTS AT FORWARD TO MID COACH. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS)

MIA - EMERGENCY LIGHT AT SEAT 3E INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 3E. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SWITCH — MALFUNCTIONED (NR 2 ENGINE)

MIA - RECEIVED A BRIEF RIGHT ENGINE FIRE LIGHT/BELL AND A STATUS RIGHT ENGINE OVERHEAT TURBINE DETECTION 2. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. AIRCRAFT TAKEN OUT OF SERVICE FOR EVALUATION. REPLACED NUMBER 2 ENGINE TURBINE OVERHEAT DETECTION SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT 1L INOPERATIVE. REPLACED CONNECTORS FOR EMERGENCY LIGHT AT 1L. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DISCONNECTED (CABIN)

DFW EMERGENCY EXIT LIGHT MOUNTED ON SEAT 34D INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY EXIT LIGHT AT SEAT 34D SIDEWALL PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SPRING — OUT OF ADJUST (GIRT BAR)

DURING ACCOMPLISHMENT OF ENGINEERING REQUEST OT CHECK GIRT BAR SPRINGS TO EACH PASSENGER DOOR POSITION, FOUR GIRT BAR SPRINGS OUT OF ADJUSTMENT. ADJUSTED FOUR GIRT BAR SPRINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, LOWER OVERWING EMERGENCY EXIT LIGHTS AT SEAT 16D INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ACTUATOR — LEAKING (SPOILER)

ACTUATOR, EN ROUTE, SJC-BOS RIGHT SYSTEM HYDRAULIC QUANTITY MESSAGE ON EICAS. HYDRAULIC QUANTITY INDICATED .47. SECURED RIGHT SYSTEM PER OPERATIONS MANUAL. AIR INTERRUPTED MSP AND LANDED WITHOUT INCIDENT. REPLACED NUMBER 7 SPOILER POWER CONTROL ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — NOT SEATED (CABIN)

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

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 22 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT ROW 22. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — NOT SEATED (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT AT 22D INOPERATIVE. RE-SEATED EMERGENCY EXIT LIGHT CONNECTOR AT 22D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PIN

MIA - DURING OVERNIGHT MAINTENANCE FOUND EMERGENCY EXIT LIGHT AT SEAT 22D INOPERATIVE. RE-SEATED EMEREGNCY EXIT PIN AT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 24D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 24D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: HOSE — RUPTURED (MLG)

PHL - FLT 1463 - EN ROUTE DFW-PHX - UPON LANDING, LOST LEFT SIDE HYDRAULIC SYSTEM. LANDED PHX WITHOUT FURTHER INCIDENT. REPLACED LEFT SIDE MLG PRESSURE HOSE. SERVICED HYDRAULIC SYSTEM. LEAK CHECKS GOOD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WINDOW — OVERHEATED (COCKPIT)

ORD - FLT 259 - EN ROUTE BOS-SJC, DETECTED STRONG SMELL AND LIGHT SMOKE IN RIGHT SIDE COCKPIT. DECLARED EMERGENCY, DIVERTED ORD AND LANDED WITHOUT FURTHER INCIDENT. REPLACED FIRST OFFICER''S WINDOW. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PUMP — LEAKING (LT ENGINE)

PHX - FLT 77 - EN ROUTE IAD-LAX - LEFT SIDE HYDRAULIC SYSTEM FAILED WITH COMPLETE LOSS OF FLUID. AIR INTERRUPTED, DIVERTED AND LANDED PHX WITHOTU FURTHER INCIDENT. REPLACED LEFT SIDE HYDRAULIC PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: MODULE — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS WERE INOPERATIVE. REPLACED EMERGENCY DOOR PATH LIGHTING MODULES AT SEAT ROWS 3 AND 9. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: CONNECTOR — BROKEN (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT AFT SECTION OF MAIN CABIN FOUND INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT STRIP CONNECTOR AT AFT SECTION OF MAIN CABIN. SYSTEM GROUND CHECK, NORMAL OPERATION. (X0

Part: FUEL GOVERNOR — DEFECTIVE (LT ENGINE)

MCO - FLT 638 - DURING APPROACH TO MCO, LEFT ENGINE FLAMEOUT 500 FEET BEFORE LANDING. ACCOMPLISHED ABNORMAL PROCEDURES AND AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED LEFT ENGINE FUEL FLOW GOVERNOR, TRANSIENT PRESSURE UNIT, BLEED VALVE CONTROL UNIT, IP BLEED VALVE, AND IP SOLENOID VALVE. ACCOMPLISHED GROUND ENGINE RUN WITH NO DEFECTS FOUND. SYSTEM LEAK AND GROUND CHECKED NORMAL OPERATION. (M)

Part: WHEEL BEARING — FAILED (NLG)

SNA - FLT NR 1689 - AFTER GATE ARRIVAL, LEFT NOSE WHEEL/TIRE FOUND TO BE MISSING WITH NO ABNORMAL INDICATIONS DURING LANDING, ROLLOUT OR TAXI. REPLACED LEFT NOSE WHEEL/TIRE ASSEMBLY. ALSO, REPLACED RIGHT NOSE WHEEL/TIRE ASSEMBLY. AIRCRAFT MAINTENANCE FERRY SNA/AFW. REPLACED NOSE LANDING GEAR STRUT INNER CYLINDER ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLOOR BEAM — CORRODED (BS 365)

AFW - FLOOR BEAM AT STA 365 HAS CORROSION BLENDED BEYOND SRM LIMITS, PER MRB 757-687. TST, 15,514.52 HOURS. CYCLES, 5,884. (X)

Part: DOOR FRAME — GOUGED (OVERWING)

AFW - AFT LT OVERWING EXIT DOOR FRAME LOWER SIDE HAD DEEP GOUGE. GOUGE IS BLENDED BEYOND SRM LIMITS, PER MRB 757-200. TST, 15,512.52. CYCLES, 5,884. (X)

Part: FLOOR BEAM — CORRODED (BS 1640)

AFW - CORROSION BLENDED ON TOP SURFACE OF FLOOR BEAM AT STA 1640, LBL 57, LBL 53, BL ZERO, AND RBL 57. BLENDS ARE BEYOND SRM LIMITS, PER MRB 757-686. TST, 15,514.52. CYCLES, 5,884. (X)

Part: DOOR PAN — GOUGED (R4 DOOR)

AFW - R-4 DOOR HANDLE PAN HAS GOUGE BEYOND SRM LIMITS, PER MRB 757-200. TST, 15,514.52 HOURS. CYCLES, 5,884. (X)

Part: DECK PLATE — CORRODED (BS 1681)

AFW - DECK PLATE HAS CORROSION REMOVED ON UPPER SURFACE AT VARIOUS LOCATIONS, PER MRB 757-685. TST, 15,514.52 HOURS. CYCLES, 5,884. (X)

Part: DOOR PAN — GOUGED (L4 DOOR)

AFW - L-4 DOOR HANDLE PAN HAS A GOUGE BEYOND SRM LIMITS, PER MRB 757-692. TST, 15,514.52 HOURS. CYCLES, 5,884. (X)

Part: FLOOR BEAM — MISDRILLED (BS 1701)

AFW - FLOOR BEAM AT STA 1701, RBL 50, HAD TWO HOLES MISDRILLED, PER MRB 757-693. TST, 15,514.52 HOURS. CYCLES, 5,884. (X)