N658AA

Part: BATTERY — DISCHARGED (CABIN) · airframe 71,540 hrs · 24,811 cycles

COACH SEAT EMER PATH LIGHTS INOPERATIVE AT ALL SEATS. R & R BATTERY & CHARGER ASSEMBLY AT M10800 IAW 33-51-07. SYS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 71,536 hrs · 24,810 cycles

COACH SEAT EMER PATH LIGHTS INOPERATIVE AT ALL SEATS. R & R BATTERY & CHARGER ASSEMBLY AT M10801 IAW 33-51-07. SYS CHECKED NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 71,536 hrs · 24,810 cycles

FIRST CLASS SEAT MOUNTED EMER PATH LIGHTS INOPERATIVE AT ALL SEATS. R & R BATTERY CHARGER ASSEMBLY AT M10798 IAW AMM 33-51-07. SYS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 71,540 hrs · 24,811 cycles

COACH SEAT EMER PATH LIGHTS INOPERATIVE AT ALL SEATS. R & R BATTERY & CHARGER ASSEMBLY AT M10799 IAW 33-51-07. SYS CHECKED NORMAL.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 70,043 hrs · 24,266 cycles

UPPER CHORD COMMON TO STATION 231.25 & BL 0 DAMAGED. ACCOMPLISHED NESTED ANGLE REPAIR IAW EA B757-53-034845.

Part: DOOR FRAME — CRACKED (L2 DOOR) · airframe 70,043 hrs · 24,266 cycles

LEFT NR 2 DOOR UPPER HINGE CUT OUT IS CRACKED. INSTALLED REPAIR DOUBLER & STOP PIN FITTING IAW SRM 52-10-02-2R-1 & EA COMP-52-034741.

Part: SKIN — CRACKED (NR 1 PYLON) · airframe 68,897 hrs · 23,854 cycles

DURING ACCOMPLISHMENT OF THE AFT HINGE FITTING PREVENTATIVE MODIFICATION, ECO F1566, ON THE NR 1 PYLON ONE FASTENER HOLE THROUGH THE FITTING & STRUCTURE WAS OVERSIZED & HFEC INSPECTED. REMOVED CRACK BY ENLARGING HOLE, VERIFIED CRACK REMOVAL BY HFEC INSPECTION, INSTALLED FREEZE PLUGS & INSTALLED REPAIR DOUBLER IAW EA B757-54-032771.

Part: ENGINE — FAILED (RIGHT) · airframe 66,448 hrs · 22,971 cycles

PLS - INFLIGHT SJU-MIA. CREW REPORTED HYDRAULIC OVERTEMP INDICATION AND LOSS OF RIGHT HYDRAULIC QUANTITY FOLLOWED. RIGHT ENGINE OIL FILTER CLOG LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT DIVERTED PLS LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE AT PLS ON 03/04/2013. SYSTEM GROUND CHECK NORMAL OPERATION (OPEN)

Part: LENS — BROKEN (CABIN) · airframe 64,043 hrs · 22,098 cycles

LEFT NUMBER 4 DOOR EMERGENCY LIGHT LENS BROKEN. REPLACED LENS FOR LEFT NUMBER 4 DOOR EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,043 hrs · 22,098 cycles

LEFT NUMBER 4 DOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR LEFT NUMBER 4 DOOR EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: ACTUATOR — LEAKING (RT MLG TRUCK) · airframe 63,189 hrs · 21,779 cycles

SJO - CREW REPORTED MAIN LANDING GEAR DOOR OPEN EICAS MESSAGE. FLIGHT RETURNED SJO LANDED WITHOUT INCIDENT. FOUND LANDING GEAR HYDRAULIC FUSE TRIPPED. REPLACED RIGHT GEAR TRUCK TILT ACTUATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 62,170 hrs · 21,410 cycles

HUMP IN PREVIOUS REPAIRS ON FLOORBEAM. PERFORM TEE CAP REPAIR PER EA B757-53-018541.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,170 hrs · 21,410 cycles

BOTTOM OF WEB CORRODED AT FASTENER HOLE. REPAIRED WEB PER AARD 51-20-00-1 REPAIR 1, S/O-KTH0, BOEING DOCUMENT 146N87225-63 AND SRM 51-10-02 OG.

Part: FRAME — GOUGED (FUSELAGE) · airframe 62,170 hrs · 21,410 cycles

FRAME GOUGED, LEFT SIDE STATION 1640 BETWEEN STRINGERS 7 AND 8. INSTALLED DOUBLER PER EA B757-53-018531 AND BOEING REPAIR SKETCH AAL/AAL-11-1981-01C.

Part: FRAME — GOUGED (FUSELAGE) · airframe 62,170 hrs · 21,410 cycles

FRAME GOUGED, LEFT SIDE STATION 1640 BETWEEN STRINGERS 6 AND 7. INSTALLED DOUBLER AS PER EA. B757-53-018531 AND BOEING REPAIR SKETCH AAL/AAL-11-1981-01C.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 62,170 hrs · 21,410 cycles

CUTOUT 2 INCHES SECTION OF 1380 FRAME LOWER CHORD, LOWER FLANGE RUNNING ON TOP OF LOWER T-CHORD TO FOM TO ACCESS CORROSION. INSTALLED REPAIR DOUBLERS, FILLER, SHIMS AND RELATED STRUCTURE AT STATION 1380 FRAME, OUTER CHORD PER SRM 51-70-12-0G AND EA B757-53-018500.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 62,170 hrs · 21,410 cycles

LEFT INTERCOSTAL DAMAGED. REPLACED INTERCOSTAL AND STRINGER PER SRM 51-10-02 OG.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,170 hrs · 21,410 cycles

CORROSION ON T-CORD WEB APPROXIMATE STATION 1420 STRINGER 26 RIGHT ON OUTBOARD FACE. INSTALLED SERVICEABLE WEB PER AARD 51-10-05-1.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,170 hrs · 21,410 cycles

AFT CARGO DOOR CUTOUT LOWER UPPER T-CHORD FROM STATIONS 1380 TO 1440 HAS CORROSION AROUND NUT PLATES. REPLACED UPPER CHORD PER AARD 51-10-05-1.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,170 hrs · 21,410 cycles

LAVATORY MOUNT CORRODED. REPLACED LAVATORY MOUNT PER SRM 51-10-02 OG.

Part: STRUCTURE — DEFECTIVE (FUSELAGE) · airframe 62,170 hrs · 21,410 cycles

AFT DECK WILL NOT EXTEND UNDERNEATH THE ANGLE AT STATION 1720. REPLACED AFT DECK PER SRM 51-10-02 OG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,170 hrs · 21,410 cycles

CORROSION ON CREASE LEFT BEAM. REPLACED SECTION OF BEAM AND ACCOMPLISHED SPLICE REPAIR PER AARD 53-60-13-1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,170 hrs · 21,410 cycles

CORROSION IN NUMEROUS PLACES ON PREVIOUS REPAIRS TO THE FLOORBEAM AT 1640 AND LEFT BUTTLINE 48 TO RIGHT BUTTLINE 30. REPLACE THE UPPER CHORD OF T CAP ON FLOORBEAM FRAME STATION 1640 PER BOEING DRAWING LOR5L53005 REPAIR 5.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,170 hrs · 21,410 cycles

WEB CORRODED STATION 1380 TO 1400 STRINGER 17 RIGHT. REPLACED WEB PER SRM 51-10-02-0G.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,170 hrs · 21,410 cycles

STATION 682 Z-ANGLE CORRODED. REPLACED Z-ANGLE PER SRM 51-10-02-OG.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 62,170 hrs · 21,410 cycles

LEFT SIDE STATION 1701, STRINGER 10 LEFT INTERCOSTAL DAMAGED. INSTALLED STRINGER/INTERCOSTAL PER SRM 51-10-02-0G PARAGRAPH NUMBER 9.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,170 hrs · 21,410 cycles

STATION 567.3, FORWARD CARGO DOORSILL AREA, FITTING FOR THRESHOLD SUPPORT CORRODED. INSTALLED FITTING ASSEMBLY PER SRM 51-10-02-0G AND IPC 53-33-63-01.

Part: DOUBLER — DENTED (CARGO DOOR) · airframe 62,170 hrs · 21,410 cycles

AFT CARGO DOOR- DENT IN OUTER SKIN 18 INCHES AFT OF FORWARD EDGE AND 4 INCHES UP FROM LOWER EDGE WITH ADL DOT NEXT TO IT. AFT CARGO DOOR CUT AND REMOVED DAMAGED AREA OF SKIN. COMPLETED DOUBLER INSTALLATION PER SRM 52-30-01-2R 4.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,170 hrs · 21,410 cycles

AFT CARGO INTERCOSTAL CORRODED. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-10-02-G9.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,170 hrs · 21,410 cycles

AFT CARGO INTERCOSTAL CORRODED STATIONS 1500 TO 1520 STRINGER 30. REPLACED INTERCOSTAL PER SRM 51-10-02-0G.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,170 hrs · 21,410 cycles

AFT CARGO INTERCOSTAL STATION 1500 CORRODED. REPLACED INTERCOSTAL PER SRM 51-10-02-G9.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,170 hrs · 21,410 cycles

WEB CORRODED STATIONS 1420 TO 1440. REPLACED WEB PER SRM 51-10-03-09.

Part: SKIN — CRACKED (LE SLAT) · airframe 62,170 hrs · 21,410 cycles

CRACK IN COVE SKIN 29 INCHES FROM END OF NUMBER 9 SLAT. STOPPED DRILLED END OF CRACK. HFEC SURFACE SCAN CONFIRMS CRACK TERMINATION AT STOP DRILL. FABRICATED AND INSTALLED REPAIR PER AARD 57-43-00-4.

Part: PAN — DAMAGED (L1 DOOR) · airframe 62,170 hrs · 21,410 cycles

LEFT NUMBER 1 DOOR, OUTER HANDLE PAN HAS DEEP GOUGE. REPLACED HANDLE PAN AND RE-INSTALLED TORQUE BOX PER ESO 90283.

Part: LIGHT — INOPERATIVE (CARGO DOOR) · airframe 61,837 hrs · 21,290 cycles

AFT CARGO DOOR MOUNTED EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR AFT CARGO DOOR MOUNTED EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 61,837 hrs · 21,290 cycles

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

Part: MODULE — INOPERATIVE (CABIN) · airframe 61,837 hrs · 21,290 cycles

ALL EMERGENCY LIGHTS IN MODULE M10699 CIRCUIT FAIL WITHIN 15 SECONDS OF OPERATION. REMOVED AND REPLACED M10699. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,338 hrs · 21,107 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 61,338 hrs · 21,107 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,621 hrs · 20,518 cycles

LEFT NUMBER 1 EMERGENCY EXIT FLOOD LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 1 EMERGENCY EXIT FLOOD LIGHT. OPS CHECKED NORMAL.

Part: PLACARD — PEELING (CABIN) · airframe 59,621 hrs · 20,518 cycles

LEFT EMERGENCY EXIT LIGHT LENS PLACARD IS PEELING. REPLACED PLACARD.

Part: SLIDE — OUT OF POSITION (L3 DOOR) · airframe 59,116 hrs · 20,336 cycles

LEFT NUMBER 3 DOOR SLIDE INADVERTENTLY UNSUCCESSFULLY DEPLOYED. SLIDE FELL FROM HOUSING AND ASSIST BOTTLE DISCHARGED. REPLACED LEFT NUMBER 3 DOOR SLIDE. OPS CHECK NORMAL.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 57,991 hrs · 19,949 cycles

SKIN CORRODED AT NUMBER THREE SLAT HI-LOK 72 INCHES FROM INBOARD END AND 16 INCHES FROM TRAILING EDGE. DAMAGED AREA REMOVED AND DOUBLERS INSTALLED PER ARRD 57- 43-00-01 AND ESO 90246.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,991 hrs · 19,949 cycles

INBOARD COVE SKIN CRACKED ON NUMBER 1 SLAT AT INBOARD AUXILIARY ARM TRACK. INSTALLED EXTERNAL DOUBLER ON COVE SKIN PER AARD 57-43-00-4.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,991 hrs · 19,949 cycles

BOTH TRAILING EDGE SKINS ARE CRACKED ON NUMBER 1 SLAT AT OUTBOARD DRIVE TRACK. INSTALLED EXTERNAL DOUBLER ON COVE SKIN PER AARD-57-43-00-4.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,991 hrs · 19,949 cycles

BOTH TRAINING EDGE SKINS ARE CRACKED ON NUMBER THREE SLAT AT INBOARD DRIVE TRACK. INSTALLED EXTERNAL DOUBLER REPAIR AT COVE SKIN AT INBOARD DRIVE TRACK UNDER SRM 57-43-00-4 AND ESO 90246.

Part: SKIN — DENTED (LE SLAT) · airframe 57,991 hrs · 19,949 cycles

DENT IN SLAT WITH HOLE AT 89 INCHES FROM INBOARD END NUMBER 5 SLAT TRAILING EDGE WEDGE SURFACE ON LEFT WING. HOT BONDED REPAIR DOUBLER PER SRM 51-70-10-2R, 2, FIG 203A.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 57,782 hrs · 19,868 cycles

EMERGENCY AISLE LIGHTS AT SEATS 16D TO 26D WILL NOT TURN OFF. REPLACED BATTERY PACK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,677 hrs · 19,822 cycles

LEFT NUMBER THREE DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LAMP.

Part: MODULE — INOPERATIVE (CABIN)

DFW MID COACH ZONE EMERGENCY LIGHTS ARE DIM. REPLACED MODULE AND BATTERY FOR MID COACH ZONE EMERGENCY LIGHTS.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 5,513,528 hrs

JFK - EMERGENCY FLOOR PATH LIGHTS AT ROWS 19 TO 26 VERY DIM. REPLACED BATTERY PACK FOR ROWS 19 TO 26.

Part: IDG — FAILED (NR 1 ENGINE) · airframe 55,109 hrs · 18,878 cycles

MIA INFLIGHT. CREW REPORTED LOSS OF LEFT HAND GENERATOR AND OVER BOARD EXHAUST VALVE OPEN INDICATION. APU FAILED WITH FAULT LIGHT AT 24000 FEET. CREW ALSO REPORTED HEARING A LOUD BANG NOISE IN COCKPIT THAT STOPPED WHEN SPEED DECREASED TO 280 KNOTS. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED NUMBER ONE ENGINE INTEGRATED DRIVE GENERATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,998 hrs

SEA- EMERGENCY AISLE LIGHTS FROM ROW 16 THRU 25 INOPERATIVE. REPLACED BATTERY PACK FOR ROW 16 THRU 25.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · 53,970 cycles

LOWER RT AND LT EMERGENCY LIGHT EXIT SIGNS AT OVERWING EXIT DOORS AND SEAT ROWS 16DEF TO 25DEF INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 20DEF FOR LOWER RT AND LT EMERGENCY LIGHT EXIT SIGNS AT OVERWING EXIT DOORS AND SEAT ROWS 16DEF TO 25DEF. SYSTEM GROUND CHECKED NORMAL OPS.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR EXIT SIGN INOPERATIVE. RECONNECTED CONNECTOR FOR EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: B-NUT — LOOSE (HYD LINE)

MSY INFLIGHT T9404/15SEP DFW TO FLL - LEFT HYDRAULIC QUANTITY LOSS IN FLIGHT. DIVERTED TO MSY AND LANDED WITHOUT INCIDENT. TIGHTENED LOOSE B NUT ON PYLON HYDRAULIC LINE. SERVICED LEFT HYDRAULIC SYSTEM. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SOCKET — INOPERATIVE (EMERGENCY LIGHTS)

JFK - RED EMERGENCY SEAT PATH LIGHT AT SEAT 17D INOPERATIVE. FOUND WIRE BROKEN AT SOCKET. REPLACED SOCKET ASSEMBLY FOR RED EMERGENCY SEAT PATH LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS)

MIA - FOUND EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER FOUR DOOR INOPERATIVE. RELAMPED EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONTROLLER — INOPERATIVE (THRUST REVERSER)

MIA - DURING TAKEOFF ROLL LEFT HAND ENGINE BLEED OFF LIGHT ILLUMINATED FOLLOWED BY EICAS LEFT ENGINE BLEED OFF MESSAGE. TURNED ENGINE BLEED OFF IN ACCORDANCE WITH FLIGHT MANUAL. AFTER LIFT OFF THERE WAS A STRONG FUEL SMELL FOR APPROXIMATELY FIVE SECONDS. STATUS MESSAGE AFTER LANDING LEFT REVERSER. RETURNED AND LANDED MIA WITHOUT INCIDENT. REPLACED REVERSER FLOW CONTROLLER FOR LEFT ENGINE THRUST REVERSER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ACTUATOR — INOPERATIVE (SPEED BRAKES)

INFLIGHT - AUTO SPEEDBRAKES FAILED TO DEPLOY ON LANDING. REPLACED AUTO SPOILER ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - OVERHEAD EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHTS IN AFT LEFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN AFT LEFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

EWR - AFT AIRCRAFT EMERGENCY LIGHTS ON FLOOR, RIGHT AND LEFT HAND EXIT DOOR INOPERATIVE. REPLACED BATTERY PACK AT M736 AND M737 FOR AFT EMERGENCY LIGHTS ON FLOOR, RIGHT AND LEFT HAND EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — BROKEN (EXIT SIGN)

DFW - EMERGENCY EXIT LIGHT AT DOOR 2L IS BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT DOOR 2L. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — DISCHARGED (CABIN)

MIA) ABOVE DOOR EMERGENCY EXIT SIGN INOPERATIVE AT L2 INTERIOR SIDE. REPLACED POWER SUPPLY M733 FOR ABOVE DOOR EMERGENCY EXIT SIGN AT L2 INTERIOR SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED

Part: BATTERY — DISCHARGED (CABIN)

MIA) EXTERIOR EMERGENCY EXIT LIGHT AT L2 INOPERATIVE. REPLACED POWER SUPPLY M733 FOR EXTERIOR EMERGENCY EXIT LIGHT AT L2. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED

Part: WIRE — LOOSE (COCKPIT)

LAX - DURING OVERNIGHT MAINTENANCE, ALL CABIN EMERGENCY EXIT LIGHTS REMAIN ON EVEN THOUGH THE EMERGENCY LIGHT SWITCH IS IN THE OFF POSITION. SECURED WIRE ON EMERGENCY LIGHT SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: RECEPTACLE — INOPERATIVE (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT 9D LIGHT INOPERATIVE. RESECURED EMERGENCY EXIT SEAT LIGHT RECEPTACLE AT 11D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SOCKET — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT ROW 4 INOPERATIVE. REPLACED AFT LIGHT SOCKET ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE RED LIGHT AT SEAT 16D BROKEN. REPLACED EMERGENCY EXIT ESCAPE RED LIGHT ASSEMBLY AT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS FORWARD OF COACH CLASS INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP FORWARD OF COACH CLASS. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT IN FORWARD CABIN UNDER EXIT SIGN INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: FLOOR — CORRODED (BS 377)

AFW - AFTER BLENDING CORROSION THE REMAINING MATERIAL IS BEYOND SRM LIMITS. REPAIRED PER MRB 757-945. (M)

Part: FLOOR BEAM — CORRODED (BS 345)

AFW - AFTER REMOVING CORROSION THE REMAINING MATERIAL IS BEYOND SRM LIMITS. REPAIRED PER MRB 757-942. (M)

Part: INTERCOSTAL — CORRODED (BS 331)

AFW - AFTER BLENDING CORROSION THE REMAINING MATERIAL IS BEYOND SRM LIMITS. REPAIRED PER MRB 757948. (M)

Part: DOOR PAN — GOUGED (R4 DOOR)

AFW - AFTER BLENDING GOUGE IN DOOR PAN REMAINING MATERIAL IS BEYOND SRM LIMITS. REPAIRED PER MRB 757-941. (M)

Part: HINGE RIB — CORRODED (LT WING)

AFW - FOUND LEFT WING AILERON ATTACH HINGE RIB WAS BLENDED TO REMOVE CORROSION, REMAINING MATERIAL IS BEYOND SRM LIMITS. REPAIRED PER MRB 757952. (M)

Part: FLOOR — CORRODED (BS 418)

AFW - AFTER BLENDING CORROSION THE REMAINING MATERIAL IS BEYOND SRM LIMITS. REPAIRED PER MRB 757-943. (M)

Part: FLOOR BEAM — CORRODED (BS 365)

AFW - AFTER BLENDING CORROSION THE REMAINING MATERIAL IS BEYOND SRM LIMITS. REPAIRED PER MRB 757-944. (M)

Part: HANDLE PAN — GOUGED (L4 DOOR)

AFW - AFTER BLENDING GOUGE ON L-4 DOOR HANDLE PAN, REMAINING MATERIAL IS BEYOND SRM LIMITS. REPAIRED PER MRB 757-950. (M)

Part: SILL — CORRODED (BS 1385-1441)

AFW - AFTER BLENDING CORROSION AT AFT CARGO DOOR CUT OUT LOWER SILL, INNER CHORD, MATERIAL REMAINING IS BEYOND SRM LIMITS. REPAIRED PER MRB 757-953. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT SIDE MARKER LIGHT AT DOOR 2R INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT SIDE MARKER LIGHT AT DOOR 2R. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)