N645AA

Part: BUSHING — CORRODED (NR 1 PYLON) · corrosion level 2 · airframe 69,810 hrs · 24,153 cycles

NR 1 PYLON INBD SIDELOAD FITTING BUSHING CORRODED. ACCOMPLISHED REPAIR IAW EA B757-57-032247 & SR 3-2509941736.

Part: FITTING — DAMAGED (NACELLE) · airframe 69,810 hrs · 24,153 cycles

MID BULKHEAD TO LOWER SPAR FITTING HOLE OVERSIZED. INSTALLED FREEZE PLUG IN LOWER SPAR CHORD FITTING IAW SR 3-2513303349 & EA B757-54-032537.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 69,810 hrs · 24,153 cycles

LT HAND WING UPPER SKIN CORRODED. ACCOMPLISHED REPAIR IAW B757-57-032528.

Part: SPLICE PLATE — CORRODED (RT HORIZ STAB) · corrosion level 3 · airframe 69,810 hrs · 24,153 cycles

CORROSION ON RT HAND LOWER INNER STABILIZER PIVOT SPLICE PLATE. REMOVED CORROSION & ACCOMPLISHED REPAIR IAW EA B757-55-032260.

Part: CONTROL PANEL — INOPERATIVE (RUDDER TRIM) · airframe 69,234 hrs · 23,963 cycles

MIA CREW REPORTED RUDDER TRIM ISSUE. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED AILERON RUDDER TRIM CONTROL PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: SLIDE — OUT OF POSITION (L4 DOOR) · airframe 67,642 hrs · 23,378 cycles

A MEMBER OF THE CABIN SERVICE WENT TO OPEN THE LEFT NUMBER 4 DOOR WITH THE SLIDE HANDLE LEFT IN THE ARMED POSITION. SLIDE FELL ONTO CABIN SERVICE TRUCK AND DID NOT FULLY DEPLOY. REPLACED LEFT NUMBER 4 SLIDE.

Part: HYDRAULIC LINE — LEAKING (NLG) · airframe 67,212 hrs · 23,218 cycles

SJU - CREW REPORTED LEFT HYDRAULIC QUANTITY LOSS. EMERGENCY DECLARED FLIGHT RETURNED SJU LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED STEERING FLEX HOSE IN NOSE GEAR WHEEL WELL. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: ACTUATOR — INOPERATIVE (LT MLG) · airframe 67,045 hrs · 23,149 cycles

MIA - CREW REPORTED LEFT GEAR DOOR WARNING LIGHT ILLUMINATED ALONG WITH AN EICAS MESSAGE. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND LOOSE CONDUIT ON LEFT GEAR. REPLACED LEFT MAIN LANDING GEAR ACTUATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: ACCESS DOOR — SEPARATED (HYDRAULIC SYS) · airframe 66,123 hrs · 22,816 cycles

JFK - CREW REPORTED DURING CLIMBOUT, THERE WERE REPORTS OF VIBRATIONS COMING FROM THE LEFT FLOOR IN THE ROWS JUST BEHIND THE WING, THEN A LOUD BANG AND CENTER SYSTEM FLUID LOSS. EMERGENCY DECLARED FLIGHT RETURNED JFK LANDED WITHOUT INCIDENT. UPON ARRIVAL, INSPECTION OF THE AIRCRAFT REVEALED THE HYDRAULIC SERVICING ACCESS DOOR HAD SEPARATED FROM THE AIRCRAFT DAMAGING THE CENTER SYSTEM SUPPLY LINE AND RESERVOIR. AIRCRAFT REMOVED FROM SERVICE. REPLACED HYDRAULIC SYSTEM SERVICE DOOR AND CENTER HYDRAULIC SYSTEM RESERVOIR SUCTION LINE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 65,799 hrs · 22,691 cycles

EMERGENCY LIGHT FROM ROW 26DEF TO 36DEF INOPERATIVE. REPLACED BATTERY PACK OVER RIGHT AFT LAVATORY. OPS CHECK NORMAL.

Part: PLUG — DEFECTIVE (OIL SYSTEM) · airframe 65,714 hrs · 22,662 cycles

PLS - INFLIGHT STT-MIA. CREW REPORTED LEFT ENGINE OIL QUANTITY AND PRESSURE LOSS. LEFT ENGINE WAS SHUTDOWN (SINGLE ENGINE TIME 25 MINS). EMERGENCY DECLARED FLIGHT DIVERTED PLS LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. AIRCRAFT FERRIED TO MIA. REPLACED CORE PLUG ON BOTTOM OF HORIZONTAL STABILIZER BUTTOCK LINE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 65,552 hrs · 22,595 cycles

EMERGENCY PATH LIGHTING FROM ROWS 26 THRU 36 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY PATH LIGHTING FROM ROWS 26 THRU 36. OPS CHECK NORMAL.

Part: WIRE — PULLED (EMERGENCY LIGHT) · airframe 65,281 hrs · 22,489 cycles

SEAT 35D EMERGENCY PATH LIGHT WIRING PULLED AWAY FROM LENS COVER. REPLACED EMERGENCY LIGHT ASSEMBLY FOR SEAT 35D EMEREGNCY LIGHT. OPS CHECK NORMAL.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 64,546 hrs · 22,224 cycles

VVI - INFLIGHT MIA-LPB. CREW REPORTED LEFT HYDRAULIC PUMP AND POWER TRANSFER UNIT FAILED IN FLIGHT. FLIGHT DIVERTED VVI LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE DRIVEN PUMP. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: MODULE — INOPERATIVE (CABIN) · airframe 63,954 hrs · 22,004 cycles

FOUND AFT SEAT EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY MODULE FOR AFT SEAT EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: FAN — INOPERATIVE (CABIN) · airframe 62,692 hrs · 21,543 cycles

MIA - CREW REPORTED ELECTRICAL ODOR IN CABIN AND COCKPIT. CAPTAIN REPORTED THAT RIGHT RECIRC FAN INOPERATIVE THEN ODOR. EMERGENCY DECLARED FLIGHT LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT RECIRCULATION FAN. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: ACCELEROMETER — INOPERATIVE (RT ENGINE) · airframe 61,720 hrs · 21,201 cycles

PTY - INFLIGHT LIM-MIA. CREW REPORTED RIGHT ENGINE VIBRATION AND UNABLE TO MAINTAIN CRUISE POWER. EMERGENCY DECLARED FLIGHT DIVERTED PTY LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE ACCELEROMETER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,705 hrs · 21,194 cycles

CORROSION STATIONS 1380 TO 1440 AFT CARGO T-ANGLE. INSTALLED NEW T-CAP ANGLE PER AARD 51-10-02-0G.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,705 hrs · 21,194 cycles

CREASE ANGLE CORRODED STATION 1031. REPLACED ANGLE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,705 hrs · 21,194 cycles

CORROSION AT STATION 670 RIGHT BUTTLINE 24. ACCOMPLISHED SEAT TRACK SPLICE REPAIR.

Part: SKIN — GOUGED (E&E DOOR) · airframe 61,705 hrs · 21,194 cycles

ADL0034 LOWER FUSELAGE MAIN EMERGENCY EQUIPMENT COMPARTMENT DOOR HAS GOUGE. REMOVED AND REPLACED SKIN PER EA NUMBER COMP52-013894.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,705 hrs · 21,194 cycles

CORROSION STATION 680 LEFT BUTTLINE 14. ACCOMPLISHED SPLICE REPAIR PER SRM 53-00-51-2R.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,705 hrs · 21,194 cycles

CORROSION ON FLOORBEAM SUPPORT AT STATION 683 RIGHT BUTTLINES 24 TO 48. REPLACED FLOORBEAM SUPPORT PER SRM 51-10-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,705 hrs · 21,194 cycles

CORROSION STATION 363 LEFT BUTTLINE 12 TO RIGHT BUTTLINE 53. REPLACED T-CAP PER SRM 53-00-51-2R 3.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,705 hrs · 21,194 cycles

CORROSION STATION 1640 RIGHT BUTTLINE 6 TO LEFT BUTTLINE 39. REPLACED T-CAP FLOOR SUPPORT BEAM PER SRM 53-00-51-2R 3.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,705 hrs · 21,194 cycles

CORROSION CREASE ANGLE STATIONS 758 TO 790. REPLACED ANGLE PER SRM 53-30-13-01.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 61,705 hrs · 21,194 cycles

CRACKED FLOOR SUPPORT AT STATIONS 343 TO 363 RIGHT BUTTLINE 25. REPLACED SUPPORT PER SRM 51-10-02-0G.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,705 hrs · 21,194 cycles

CREASE ANGLE CORRODED. REPLACED ANGLE.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,705 hrs · 21,194 cycles

CREASE ANGLE STATIONS 680 TO 740 CORRODED. REPLACED CREASE ANGLE PER SRM 51-40-02.

Part: SLAT — CORRODED (LT WING) · corrosion level 2 · airframe 61,705 hrs · 21,194 cycles

NUMBER 7 SLAT CORROSION FOUND AROUND FASTENER HEAD APPROXIMATELY 50 INCHES FROM THE OUTBOARD END AND 7 INCHES FROM INBOARD END (MARKED). INSTALLED REPAIR PER AARD 57-43-01.

Part: SKIN — CORRODED (TE FLAP) · corrosion level 2 · airframe 61,705 hrs · 21,194 cycles

CORROSION ON OUTBOARD FLAP LOWER LEADING EDGE INBOARD OF NUMBER 8 FLAP TRACK. INSTALLED FLUSH DOUBLER AND FILLER PER SRM 57-53-01 2R3.

Part: SKIN — DAMAGED (LE SLAT) · corrosion level 2 · airframe 61,705 hrs · 21,194 cycles

DEEP BLEND IN BLIND FASTENER ON NUMBER 9 SLAT (MARKED) RIGHT WING. REMOVED COVE SKIN CUTOUT DAMAGED AND FABRICATED DOUBLERS. ALODINED AND PRIMED DOUBLERS AND FILLER PER AARD 57-43-00-1 AND SRM 51-20-01.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 61,705 hrs · 21,194 cycles

LAVATORY FLOOR SUPPORT BRACKET CRACKED AND GOUGED. REPLACED SUPPORT PER SRM 51-10-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,705 hrs · 21,194 cycles

FLOOR SUPPORT CORRODED STATIONS 377 TO 395 RIGHT BUTTLINE 60. REPLACED FLOOR SUPPORT PER SRM 51-10-02.

Part: SLAT — CORRODED (LT WING) · corrosion level 2 · airframe 61,705 hrs · 21,194 cycles

LEFT WING NUMBER 4 SLAT UPPER CORROSION AT TRAILING EDGE WEDGE 24 INCH INBOARD OF OUTBOARD END. LEFT WING NUMBER 4 SLAT BLENDED AREA OUT OF LIMITS. INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,484 hrs · 21,117 cycles

THE 21DEF BULLNOSE EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR 21DEF BULL NOSE EMERGENCY LIGHT. OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,484 hrs · 21,117 cycles

RIGHT NUMBER 4 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 3 DOOR EMERGENCY LIGHT. OPS CHECKED NORMAL.

Part: PUMP — FAILED (ENGINE) · airframe 59,927 hrs · 20,560 cycles

MIA - INFLIGHT JFK-CUN. CREW REPORTED LEFT HYDRAULIC PRESSURE ON EICAS AND ON OVERHEAD PANEL THEN LEFT ENGINE HYDRAULIC PUMP INDICATED ON EICAS AND OVERHEAD PANEL. APPROXIMATELY 2 HOURS LATER HYDRAULIC SYSTEM PRESSURE LOW ILLUMINATED AND ELECTRIC PUMP PRESSURE LIGHT ILLUMINATED. IMMEDIATELY LOST ALL PRESSURE AND HAD TO USE ALTERNATE FLAP AND ALTERNATE GEAR EXTENSION. EMERGENCY DECLARED DIVERTED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED ENGINE DRIVEN PUMP. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 59,068 hrs · 20,244 cycles

EMERGENCY LIGHT AT SEAT 31D INOPERATIVE. REPLACED LAMP.

Part: GEARBOX — WORN (NR 2 ENGINE) · airframe 58,662 hrs · 20,093 cycles

INFLIGHT MIA TO JFK. CREW REPORTED RIGHT ENGINE OIL PRESSURE WENT BELOW 10 POUNDS PER SQUARE INCH. CREW SHUT DOWN NUMBER TWO ENGINE. LANDED RDU WITHOUT INCIDENT. SINGLE ENGINE TIME 20 MINUTES. FOUND EXCESSIVE METAL ON GEARBOX CHIP DETECTORS AND OIL LEAK AT RADIAL DRIVE SHAFT. REPLACED NUMBER TWO ENGINE ON 02 OCT AT RDU DUE TO OIL LEAK.

Part: PIN — LOOSE (CONNECTOR) · airframe 58,065 hrs · 19,894 cycles

SJU - FIRST CLASS EMERGENCY LIGHT INOPERATIVE. RE-LOCK PUSH OUT PIN AT SEAT 5E-F CONNECTOR. OPS CHECKED NORMAL WD 33-51-01.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,907 hrs · 19,839 cycles

WEB CORRODED AT KEEL BEAM. REPAIRED IAW EA B757-53-006402.

Part: WIRE — BROKEN (EMERGENCY LIGHTS)

BOS - EMERGENCY ESCAPE PATH LIGHT AT SEAT 34D INOPERATIVE. REPAIRED BROKEN WIRE ON HARNESS FOR EMERGENCY ESCAPE PATH LIGHT AT SEAT 34D.

Part: HOSE — DAMAGED (HYD SYSTEM)

JFK TEST FLIGHT T9640/06SEP - AFTER TAKEOFF CREW REPORTED MAIN LANDING GEAR UNSAFE LIGHT. FOLLOWED BY LEFT SYSTEM HYDRAULIC LOSS. LANDED JFK WITHOUT INCIDENT. AFTER LANDING RIGHT GEAR DOOR WAS EXTENDED AND WHEEL WELL WAS SATURATED WITH HYDRAULIC FLUID. FOUND FLEX LINE TO RIGHT MAIN LANDING GEAR DOOR ACTUATOR WITH HOLE IN LINE. REPLACED HOSE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: GEARBOX — FAILED (RIGHT ENGINE)

RIGHT ENGINE OIL PRESSURE WENT TO ZERO DURING CLIMB AT 24000 FEET. THE ENGINE SHUT DOWN. OIL QUANTITY AND TEMPERATURE NORMAL. SINGLE ENGINE TIME 18 MINUTES. RETURNED TO UIO AND LANDED WITHOUT INCIDENT. REPLACED RIGHT ENGINE DUE TO GEARBOX FAILURE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ACM — ODOR (LEFT)

ORD - ON CLIMBOUT SMOKE AND FUMES ENTERED COCKPIT AND FIRST CLASS GALLEY AREA. ACCOMPLISHED RED BOX ITEMS AND ACRID SMELL DISSIPATED AND THEN CAME BACK. SMOKE AND FUMES WERE GONE BY THE TIME THE AIRCRAFT LANDED 15 MINUTES LATER. RETURNED ORD AND LANDED WITHOUT INCIDENT. FOUND LEFT HAND AIR CONDITIONING PACK AIR CYCLE MACHINE INTERMITTENTLY SHUTTING OFF. REPLACED LEFT HAND AIR CYCLE MACHINE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

MIA - OVERHEAD EMERGENCY EXIT LIGHT AT ROWS 17 AND 18 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY EXIT LIGHT AT ROWS 17 AND 18. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ENGINE — STALLED (LEFT)

MIA - DURING CLIMBOUT LEFT ENGINE VIBRATION INDICATED 3.4 ON N3. PULLED THROTTLE BACK AND CAUTION INDICATION WENT OUT. AFTER ADVANCING THROTTLE LEFT ENGINE EXPERIENCED A COMPERSSOR STALL. PULLED THROTTLE BACK AND LEFT ENGINE STABILIZED AND OPERATIVE NORMALLY AT THE REDUCED POWER SETTING. REPLACED NUMBER ONE ENGINE AT MIA. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MODULE — INOPERATIVE (CABIN)

SFO - EMERGENCY LIGHTS FROM ROWS 15 TO 2 LEFT DOOR INOPERATIVE. REPLACED MODULE AT LOCATION M10799 FOR EMERGENCY LIGHTS FROM ROWS 15 TO 2 LEFT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, LEFT SIDE PASSENGER FORWARD DOOR SLIDE LIGHT INOPERATIVE. REPLACED LEFT SIDE PASSENGER FORWARD DOOR SLIDE LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: HYDRAULIC LINE — PUNCTURED (HYD SYSTEM)

MIA - FLT 938 - EN ROUTE CCS-MIA, EICAS MESSAGE DISPLAYED LOSS OF HYDRAULIC QUANTITY OF CENTER HYDRAULIC SYSTEM. LEFT AND RIGHT CENTER ELECTRIC HYDRAULIC PUMP SWITCHES TURNED OFF. CAPTAIN DECLARED EMERGENCY AND LANDED AT MIA WITHOUT INCIDENT. INSPECTED AND FOUND PUNCTURED LINE FROM THE NR 1 CENTER ELECTRIC PUMP TO FILTER MODULE. REPLACED HYDRAULIC LINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

MIA - L1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. RESECURED LOOSE CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 34 DEF INOPERATIVE. SECURED EMERGENCY EXIT LIGHT HOLDER AT SEAT 34 DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, RIGHT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — CORRODED (WING)

TUL - FOUND CORROSION ON UPPER SKIN SURFACE AT ROOT NUMEROUS AREAS UNDER WALKWAY PAINT, WS 70 TO WS 177. REPAIRED PER ESO 90309 DATED 5-18-01. (M)

Part: SKIN — CORRODED (RT WING)

TUL - FOUND CORROSION ON UPPER RIGHT WING SKIN SPLICE AT L/E STATION WS 95 TO WS 565.50. REPAIRED PER ESO 90309 DATED 5-18-01. (M)

Part: SKIN — CORRODED (WING)

TUL - FOUND CORROSION UNDER BLACK STRIP AROUND WING WALK AREA FOR EMERGENCY ESCAPE PATH, RBL 70.50 WBL 250. REPAIRED PER ESO90309 DATED 5-18-01. (M)

Part: SKIN — CORRODED (RT WING)

TUL - FOUND CORROSION ON UPPER RIGHT WING SKIN AT TRAILING EDGE SPLICE WS 100.50 TO WS 369.50. REPAIRED PER ESO 90309 DATED 5/18/2001. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND TWO SMALL DENTS IN FUSELAGE SKIN 6 INCHES FORWARD AND 8 INCHES TO THE RIGHT OF E/E COMPT DOOR. REMOVED DAMAGE AND INSTALLED DOUBLE PER SRM 53-00-01-2. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND TWO DENTS IN FUSELAGE SKIN 6 INCHES FORWARD AND 8 INCHES TO THE RIGHT OF E/E COMP DOOR. DOUBLER INSTALLED PER SRM 53-00-01-2. (M)

Part: BATTERY — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, COCKPIT EMERGENCY EXIT LIGHT DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PUMP — LEAKING (RT ENGINE)

LAX - FLT 181 - EN ROUTE BOS-LAX, DETECTED RIGHT SIDE HYDRAULIC QUANTITY LOSS. LANDED LAX WITHOUT FURTHER INCIDENT. REPLACED RIGHT SIDE HYDRAULIC PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

JFK - MAINTENANCE ENTRY BEFORE OVERNIGHT CHECK, FIRST CLASS EMERGENCY EXIT LIGHT IN FIRST CLASS STAYS ILLUMINATED WITH SWITCH IN OFF POSITION. PERFORMED TEST OF EMERGENCY LIGHT SYSTEM UNABLE TO DUPLICATE. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: WIRE — OPEN (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS INOPERATIVE. REPAIRED WIRE ON EMERGENCY EXIT FLOOR PATH LGIHTS IN FIRST CLASS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: CONNECTOR — DEFECTIVE (CABIN)

JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING IN FIRST CLASS FROM 1R DOOR TO 2R DOOR INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: LIGHT — DAMAGED (ROW 1)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT STRIP NEAR SEAT ROW 1 MISSING 18 INCH SECTION. REPLACED EMERGENCY FLOOR PATH LIGHTING STRIP AT SEAT ROW 1. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, LEFT FORWARD EXTERIOR OVERWING EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. CLEANED AND RESECURED CONNECTOR TO LEFT FORWARD EXTERIOR OVERWING EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATIONS. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, R2 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. RESEATED R2 DOOR EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

ORD - DURING OVERNIGHT CHECK, LEFT FORWARD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LEFT FORWARD EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, FORWARD EMERGENCY EXIT FLOOR LIGHT FOUND INOPERATIVE. REPLACED LIGHT STRIP AT FORWARD EMERGENCY EXIT FLOOR. SYSTEM FOUND CHECKED, NORMAL OPERATION. (X)

Part: FAN — DEFECTIVE (E/E COMPT)

MIA - FLT 2142 - EN ROUTE CCS/MIA - DURING CRUISE, FUMES NOTED COMING FROM COCKPIT INSTRUMENT PANEL. AIRCRAFT PROCEEDED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED NR 1 EQUIPMENT SUPPLY FAN AND FILTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLOOR BEAM — CORRODED (BS 345)

AFW - FOUND FLOOR BEAM AT STATION 345 HAS CORROSION REMOVED ON UPPER SURFACE. MATERIAL REMAINING IS BEYOND SRM LIMITS, PER MRB 757-820. (M)

Part: FLOOR BEAM — CORRODED (BS 365)

AFW - FOUND FLOOR BEAM AT STATION 365 HAS CORROSION ON UPPER SURFACE BLENDED BEYOND SRM LIMITS, PER MRB 757-821. (M)

Part: FLOOR BEAM — CORRODED (BS 377)

AFW - FOUND FLOOR BEAM AT STATION 377 HAD 6 AREAS OF CORROSION BLENDED BEYOND SRM LIMITS, PER MRB 757-822. (M)

Part: FLOOR BEAM — CORRODED (BS 342)

AFW - FOUND FLOOR BEAM AT STATION 324 HAS CORROSION REMOVED ON UPPER SURFACE. MATERIAL REMOVED IS BEYOND SRM LIMITS, PER MRB 757-819. (M)

Part: DECK PLATE — CORRODED (BS 1720)

AFW - FOUND DECK PLATE HAS SEVERAL AREAS OF CORROSION BLENDED BEYOND SRM LIMITS, PER MRB 757-824. (M)

Part: FLOOR BEAM — CORRODED (BS 1640)

AFW - FOUND FLOOR BEAM AT STATION 1640 HAS CORROSION REMOVED BEYOND SRM LIMITS, PER MRB 757-826. (M)

Part: FLOOR BEAM — CUT (BS 1640)

AFW - WHILE CUTTING THE TOP CAP OFF FLOOR BEAM 1640 FOR SRM REPAIR, EO WAS LOST ON THE 5 MOST OUTBOARD RIGHT FASTENERS AT FRAME, PER MRB 757-827. (M)

Part: SILL — CORRODED (CARGO DOOR)

AFW - FOUND LOWER MAIN SILL, UPPER CHORD, NR 2 CARGO DOOR CUTOUT HAS CORROSION REMOVED ON UPPER AND LOWER SURFACES. CORROSION REMOVED IS BEYOND SRM LIMITS, PER MRB 757-831. (M)

Part: EEL CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 1 THROUGH 6 INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR BY PASSENGER SEAT ROW 1. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)