N641AA

Part: BULKHEAD — CORRODED (RT MLG WW) · corrosion level 2 · airframe 65,490 hrs · 23,026 cycles

CORROSION ON RIGHT WHEEL WELL CENTER BULKHEAD STATION 1090, 17 INCHES ABOVE KEEL BEAM. INSTALLED DOUBLER PER EA B757-53-020485.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 65,490 hrs · 23,026 cycles

IN THE AFT CARGO BELOW THE CABIN FLOOR, THE INTERCOSTALS TOP "L" ANGLE BETWEEN STATIONS 1320 TO 1340 IS CRACKED BY THE SECOND FROM AFT NUT PLATE. REMOVED AND REPLACED INTERCOSTAL PER BOEING DWG 146N5180 AND AMM 51-10-02-OG.

Part: SLAT — CORRODED (LE SLAT) · corrosion level 2 · airframe 65,490 hrs · 23,026 cycles

LEFT WING NUMBER 3 SLAT CORRODED AROUND FASTENER 33 INCHES FROM OUTBOARD END. INSTALLED REPAIR DOUBLER PER AARD 57-43-00-1.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 65,490 hrs · 23,026 cycles

INTERCOSTAL WEB DAMAGED STATIONS 540 TO 560 BUTTLINE 0. INSTALLED NEW WEB PER SRM 51-10-02-0G.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 65,490 hrs · 23,026 cycles

LEFT WING, NUMBER 3 SLAT CORRODED AROUND FASTENER ON TOP SKIN APPROXIMATELY 33 INCHES FROM OUTBOARD END. REMOVED CORROSION AND INSTALLED REPAIR DOUBLERS PER AARD 57-43-00-1.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 65,490 hrs · 23,026 cycles

CORROSION ON NUMBER 9 SLAT SKIN AROUND FASTENER OUTBOARD DRIVE TRACK AREA. REMOVED CORROSION AND INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.

Part: RECEIVER — FAILED (WEATHER RADAR) · airframe 64,670 hrs · 22,710 cycles

MIA (REPEAT ITEM) CREW REPORTED ON CLIMBOUT WEATHER RADAR FAILED. FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RECEIVER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 63,942 hrs · 22,448 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 (EXTERIOR) · airframe 63,942 hrs · 22,448 cycles

RIGHT NUMBER 2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 2 DOOR EXTERIOR EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: WIRE HARNESS — INOPERATIVE (CABIN) · airframe 62,302 hrs · 21,850 cycles

AFT EMERGENCY LIGHT AT SEAT 18DEF INOPERATIVE. REPLACED EMERGENCY LIGHT HARNESS AT SEAT ROW 18DEF. OPS CHECK NORMAL.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,385 hrs · 21,540 cycles

DRAIN MAST BRACKET CORRODED IN AFT CARGO COMPARTMENT STATION 1670 BETWEEN STRINGERS 25 RIGHT AND 26 RIGHT. INSTALLED REPAIR DOUBLER PER EA B 757-53-011579.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,385 hrs · 21,540 cycles

CORROSION ON DITCHING PANEL/WEB, BELOW THE 14TH LEFT VIEW WINDOW, FRAME STATIONS 756 TO 760 LEFT BUTTLINES 64 TO 66, WATERLINE 208, STRINGER 17 LEFT. REMOVED AND REPLACED WEB/DITCHING PANEL PER SRM 51-10-02-0G, PARAGRAPH 8 AND 9.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 61,385 hrs · 21,540 cycles

INTERCOSTAL DAMAGED FROM STATIONS 660 TO 680 LEFT BUTTLINE 45. REPLACED INTERCOSTAL FROM STATIONS 660 TO 680 LEFT BUTTLINE 45 SRM 51-10-02-G9.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 61,385 hrs · 21,540 cycles

CRACK IN FLOORBEAM STATION 700 LEFT BUTTLINE 24. INSTALL SPLICE REPAIR PER AARD 53-30-51-2.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 61,385 hrs · 21,540 cycles

INTERCOSTAL DAMAGED FROM STATIONS 660 TO 680 LEFT BUTTLINE 24. REPLACED INTERCOSTAL AT STATIONS 660 TO 680 LEFT BUTTLINE 24 PER SRM 51-10-02-0G,9.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,385 hrs · 21,540 cycles

CORROSION ON WEB OUTBOARD OF CREASE ANGLE AT STATIONS 1022 TO 1038 RIGHT BUTTLINES 65 TO 66. INSTALLED NEW WEB STATIONS 1020 TO 1040 RIGHT PER SRM 51-10-02-0G 8 AND 9.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,385 hrs · 21,540 cycles

LIGHT CORROSION ON AND AROUND FASTENERS ON CREASE ANGLE WEBS-RIGHT SIDE STATIONS 1400 TO 1460. REMOVED AND REPLACED DITCHING PAN FROM STATIONS 1400 TO 1460 PER SRM 51-10-02-0G 9.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,385 hrs · 21,540 cycles

LIGHT CORROSION ON AND AROUND FASTENERS ON CREASE ANGLE WEBS RIGHT SIDE STATIONS 1400 TO 1460. REMOVED AND REPLACED DITCHING PAN FROM STATIONS 1400 TO 1460 PER SRM 51-10-02-0G 9.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,385 hrs · 21,540 cycles

LEFT CREASE ANGLE, HEAVY CORROSION AT STATIONS 755 TO 765 MARKED. REPAIRED WITH REPLACEMENT SECTION OF CREASE BEAM AND REPAIR SPLICE. SPLICE MPN CBE1851, PER AARD 53-30-13-1.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 61,385 hrs · 21,540 cycles

MAIN EMERGENCY EQUIPMENT CEILING INTERCOSTAL CRACKED STATIONS 480 TO 500. INSTALLED NEW ANGLE AND FASTENERS PER SRM 51-40-02-0G AND SRM 51-10-02-0G 8.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 61,385 hrs · 21,540 cycles

FLOORBEAM CRACKED STATION 660. INSTALLED TEE-CAP REPAIR PER SRM 53-00-51-2R-3.

Part: STRAP — DAMAGED (FUSELAGE) · airframe 61,385 hrs · 21,540 cycles

LOWER FLOORBEAM STRAP, AFT SIDE OF 660 LEFT BUTTLINE 45, HAS DAMAGED HOLES. INSTALLED REPAIR DOUBLER PER SRM 53-10-51-2R 1.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,385 hrs · 21,540 cycles

CHORD ANGLE LEFT SIDE STATIONS 660 TO 780 CORRODED. REPLACED ANGLE PER SRM 51-10-02-G 8.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,385 hrs · 21,540 cycles

CORROSION ON WEB OUTBOARD OF CREASE ANGLE AT STATIONS 980 TO 982 RIGHT BUTTLINES 66 TO 68. REMOVED CORROSION BY REMOVING THE CORRODED ANGLE ATTACHED TO THE WEB. INSTALLED NEW ANGLE, PER SRM 51-10-02-0G ARTICLE 8.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,385 hrs · 21,540 cycles

FLOORBOARD SUPPORT ANGLE CORRODED INBOARD OF RIGHT NUMBER 4 DOOR THRESHOLD. REMOVED AND REPLACED FLOORBOARD SUPPORT ANGLE PER SRM 53-00-51-2R.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,385 hrs · 21,540 cycles

AFT DRAIN SUPPORT CORRODED INBOARD OF RIGHT NUMBER 4 DOOR. REMOVED AND REPLACED AFT DRAIN SUPPORT PER SRM 51-10-02-0G ARTICLE 8.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,385 hrs · 21,540 cycles

FORWARD DRAIN SUPPORT INBOARD OF RIGHT NUMBER 4 DOOR STATIONS 1640 TO 1660 CORRODED. REMOVED AND REPLACED FORWARD DRAIN SUPPORT PER SRM 51-10-02-0G ARTICLE 8.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,385 hrs · 21,540 cycles

RIGHT NUMBER 4 DOOR THRESHOLD MOUNT CORROSION STATION 1680. REPLACED OF R-4 THRESHOLD MOUNT ANGLE STATION 1680 COMPLETED IAW SRM 51-10-02-OG. 8.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,385 hrs · 21,540 cycles

FORWARD DRAIN SUPPORT INBOARD OF RIGHT NUMBER FOUR DOOR STATION 1640-1660 CORRODED. REPLACED DRAIN SUPPORT WITH NEW PART PER SRM 51-10-02-0G, PARAGRAPH 8.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,385 hrs · 21,540 cycles

CORROSION ON WEBBING PANEL. REPLACED WEB.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,385 hrs · 21,540 cycles

CORROSION ON AFT DECK STATION 1715. INSTALLED DOUBLER REPAIR PER SRM 53-60-51-2R-2.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,385 hrs · 21,540 cycles

CORROSION ON WEB OUTBOARD OF CREASE ANGLE AT STATIONS 963 TO 965 RIGHT BUTTLINES 67 TO 68. REMOVED WEB AT STATIONS 960 TO 980 RIGHT BUTTLINES 67 TO 68 AND INSTALLED NEW WEB PER SRM 51-40-02-0G AND 51-10-02-0G.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,385 hrs · 21,540 cycles

CORROSION ON AFT GALLEY DECK PLATE DOUBLER RIGHT BULLTINE 12 STATION 1715. REMOVED OLD DOUBLER AND INSTALLED NEW DOUBLER PER SRM 53-60-51-2 REPAIR NUMBER 2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,385 hrs · 21,540 cycles

AT THE RIGHT NUMBER 1 DOOR AREA STATIONS 345 TO 365 THERE IS CORROSION ON THE LONGITUDAL FLOORBOARD SUPPORT RIGHT BUTTLINE 62. INSTALLED FLOOR SUPPORT PER SRM 51-10-02-0G, TREATED AND PRIMED AS REQUIRED PER SRM 51-20-01-0G.

Part: SKIN — DAMAGED (LE SLAT) · airframe 61,385 hrs · 21,540 cycles

LEFT WING NUMBER 1 SLAT STATION 711 HAS 2 EACH PROTRUDING HEAD BLIND FASTENERS (MARKED). LEFT WING NUMBER 1 SLAT REMOVED DAMAGED AREA OF SKIN AND INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,385 hrs · 21,540 cycles

AT THE RIGHT NUMBER 1 DOOR AREA STATIONS 324 TO 345 THERE IS CORROSION ON THE LONGITUDAL FLOORBOARD SUPPORT RIGHT BUTTLINE 62. INSTALLED FLOOR SUPPORT PER SRM 51-10-02-0G, TREATED AND PRIMED AS REQUIRED PER SRM 51-20-01-0G.

Part: SLAT — CORRODED (LT WING) · corrosion level 2 · airframe 61,385 hrs · 21,540 cycles

LEFT WING NUMBER 1 SLAT STATION 707 HAS 1 EACH 3/16 CHERRY MAX FASTENER IN BLENDED AREA. LEFT WING NUMBER 1 SLAT REMOVED FASTENER AND CORRODED AREA. INSTALLED A FLUSH DOUBLER REPAIR PER AARD 57-43-01. MRT# 026729.

Part: MODULE — INOPERATIVE (CABIN) · airframe 61,151 hrs · 21,460 cycles

ESCAPE PATH LIGHTS FROM ROWS 16 TO 24 INOPERATIVE. REPLACED MODULE CHARGER M10800 FOR ESCAPE PATH LIGHTING FROM ROWS 16 TO 24. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,151 hrs · 21,460 cycles

ESCAPE PATH LIGHTS INOPERATIVE FROM ROWS 16 TO 24. REPLACED BATTERY PACK FOR ESCAPE PATH LIGHTS FROM ROWS 16 TO 24. OPS CHECKED NORMAL.

Part: CHARGER — FAILED (CABIN) · airframe 59,263 hrs · 20,779 cycles

EMERGENCY PATH LIGHTING AT LEFT SECTION OF SEATS INOPERATIVE. REPLACED BATTERY CHARGER ASSY AT M10801, OPS CHECKS GOOD.

Part: INDICATOR — INOPERATIVE (AIRSPEED) · airframe 58,960 hrs · 20,677 cycles

JFK - CAPTAIN DECLARED FIRST OFFICER LOST HIS AIRSPEED INDICATOR. EMERGENCY DECLARED LANDED JFK WITHOUT INCIDENT. REMOVED AND REPLACED AIRSPEED INDICATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (CABIN) · airframe 58,908 hrs · 20,656 cycles

SEAT 26D EMERGENCY LIGHT INOPERATIVE. RECONNECTED LOOSE CONNECTION FOR EMERGENCY LIGHT AT SEAT 26D.

Part: PCA — LEAKING (HYDRAULIC SYS) · airframe 58,635 hrs · 20,563 cycles

BOS - CREW REPORTED LOSS OF RIGHT HYDRAULIC QUANTITY. EMERGENCY DECLARED, RETURNED TO BOS WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND POWER CONTROL ACTUATOR LEAKING. REPLACED POWER CONTROL ACTUATOR AND ANTI-SKID CONTROL.

Part: PUMP — LEAKING (RT FUEL) · airframe 58,224 hrs · 20,436 cycles

BOS - AIRCRAFT WAS LEAKING FLUID FROM RIGHT ENGINE DURING TAKEOFF. RETURNED BOS WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LOW PRESSURE FUEL PUMP.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS)

DFW - RIGHT NUMBER 4 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 4 DOOR EMERGENCY LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN)

LAX- EMERGENCY LIGHTS AT LEFT NUMBER ONE DOOR ARE DIM. REPLACED BATTERY PACK AT LEFT NUMBER ONE DOOR.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,842 hrs · 19,936 cycles

FLOORBEAM CORRODED, REPAIRED FLOORBEAM IAW SRM 53-00-51.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,842 hrs · 19,936 cycles

FLOORBEAM CORRODED, REPAIRED FLOORBEAM IAW SRM 53-0-51.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,482 hrs · 19,936 cycles

CORROSION UNDER R NR 4 PASSENGER/SERVICE DOOR, REPAIRED R 4 DOOR DRAIN SUPPORT IAW SRM 53-00-51.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,842 hrs · 19,936 cycles

FLOOR SUPPORT CORRODED, REPAIRED FLOOR SUPPORT IAW SRM 53-00-51.

Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,842 hrs · 19,936 cycles

AFT MAIN DECK PLATE CORRODED, REPAIRED IAW SRM 53-60-51-2R2.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,842 hrs · 19,936 cycles

LEFT NR 4 PASSENGER/SERVICE DOOR AFT FLOOR SUPPORT CORRODED, REPAIRED SUPPORT IAW SRM 53-00-51.

Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,842 hrs · 19,936 cycles

AFT MAIN DECK PLATE CORRODED; REPAIRED IAW SRM 53-60-51-2R2.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,842 hrs · 19,936 cycles

FLOOR SUPPORT CORRODED, REPAIRED FLOOR SUPPORT IAW SRM 53-00-51.

Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,842 hrs · 19,936 cycles

AFT MAIN DECK PLATE CORRODED, REPAIRED IAW SRM 53-60-51-2R2.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,842 hrs · 19,936 cycles

FLOOR SUPPORT CORRODED, REPAIRED SUPPORT IAW SRM 53-00-51.

Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,842 hrs · 19,936 cycles

AFT MAIN DECK PLATE CORRODED, REPAIRED IAW SRM 53-60-51-2R2.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,842 hrs · 19,936 cycles

BATHTUB FITTING CORRODED, REPLACED FITTING IAW SRM 53-00-51.

Part: TEE FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,842 hrs · 19,936 cycles

TEE FITTING CORRODED, REPLACED FITTING IAW SRM 53-00-51.

Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,842 hrs · 19,936 cycles

AFT MAIN DECK PLATE CORRODED. REPAIRED IAW SRM 53-60-51-2R2.

Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,842 hrs · 19,936 cycles

AFT MAIN DECK PLATE CORRODED; REPAIRED IAW SRM 53-60-51-2R2.

Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,842 hrs · 19,936 cycles

AFT MAIN DECK PLATE CORRODED. REPAIRED IAW SRM 53-60-51-2R2.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 56,807 hrs

LGA - EMERGENCY LIGHT AT R3 DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT R3 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 56,807 hrs

LGA - EMERGENCY LIGHT AT LEFT NUMBER THREE DOOR INOPERATIVE. REPLACED LAMP AT LEFT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 56,807 hrs

LGA - EMERGENCY LIGHT AT R2 DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT R2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,815 hrs

DFW - EMERGENCY LIGHT AT RIGHT SEAT ROW 25 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT SEAT ROW 25. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: GEARBOX — LEAKING (LEFT ENGINE)

DEN INFLIGHT T1425/31JUL - LEFT GENERATOR FAIL INDICATION ILLUMINATED AND LEFT ENGINE LOW OIL PRESSURE INDICATION ILLUMINATED. SHUT DOWN LEFT ENGINE. LANDED DEN WITHOUT INCIDENT. SINGLE ENGINE TIME 10 MINUTES. FOUND OIL LEAKING FROM LEFT ENGINE GEARBOX. CHIP DETECTOR WAS CONTAMINATED WITH METEL. REPLACED LEFT ENGINE GEARBOX PER MAINTENANCE CHECK MANUAL 72 94 02. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

LGA - EMERGENCY EXIT LIGHT AT AFT RIGHT DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT AFT RIGHT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SFO - SEAT MOUNTED EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK M10789 FOR SEAT MOUNTED EMERGENCY LIGHTS IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

LGA - RIGHT NUMBER TWO DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED RIGHT NUMBER TWO DOOR EXTERIOR EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

LGA - EMERGENCY EGRESS LIGHT AT SEAT ROW 5 FORWARD INOPERATIVE. RELAMPED EMERGENCY EGRESS LIGHT AT SEAT ROW 5 FORWARD. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (LAVATORY)

DFW - CEILING EMERGNECY LIGHT AT LEFT AFT LAVATORY INOPERATIVE. REPLACED CEILING EMERGENCY LIGHT AT LEFT HAND AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY LIGHT AT R2 DOOR INOPERATIVE. REPLACED EMERGENCY LIGHT AT R2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — BROKEN (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT 22D LENS BROKEN. REPLACED CLEAR LENS FOR EMERGENCY LIGHT AT SEAT 22D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — BROKEN (LT OVERWING)

DFW - EMERGENCY EXIT LIGHT AT FORWARD LEFT HAND OVERWING EXIT MARKER BROKEN. REPLACED THE LIGHT ASSEMBLY FOR THE EMERGENCY EXIT LIGHT AT FORWARD LEFT HAND OVERWING EXIT MARKER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

DFW - BULLNOSE EMERGENCY LIGHT AT SEAT ROW 31 INOPERATIVE. RELAMPED THE BULLNOSE EMERGENCY LIGHT AT SEAT ROW 31. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY PATH LIGHTING FROM ROWS 1 TO 6 AND 25 TO 36 INOPERATIVE. REPLACED BATTERY PACKS FOR INOPERATIVE EMERGENCY PATH LIGHTING FROM ROWS 1 TO 6 AND 25 TO 36. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHTS AT RIGHT NUMBER TWO AND NUMBER FOUR DOORS INOPERATIVE. RELAMPED EMERGENCY LIGHTS AT RIGHT NUMBER TWO AND NUMBER FOUR DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SOCKET — INOPERATIVE (EMERGENCY LIGHT)

DFW - DOOR FOUR LEFT EMERGENCY SLIDE LIGHT AT L56 INOPERATIVE. REPLACED THE SOCKET ASSEMBLY FOR THE L56 EMERGENCY SLIDE LIGHT AT DOOR FOUR LEFT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — LOOSE (EMERGENCY LIGHT)

EMERGENCY LIGHT AT SEAT 26D INOPERATIVE. FOUND LOOSE WIRE. RESECURED LOOSE WIRE FOR EMERGENCY LIGHT AT SEAT 26D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: O-RING — DAMAGED (HYD SYSTEM)

DFW EN ROUTE FLL-LAX CENTER HYDRAULIC SYSTEM DROPPED TO .34. LANDED DFW WITHOUT INCIDENT. REPLACED LEAKING CENTER HYDRAULIC SYSTEM ELECTRIC PUMP O-RING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SOCKET — INOPERATIVE (EMERGENCY LIGHT)

SFO - DURING OVERNIGHT MAINTENANCE, OBSERVED EMERGENCY LIGHT INOPERATIVE AT AFT PASSENGER DOOR. CLEANED AND TIGHTENED LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SENSOR — DEFECTIVE (COCKPIT)

PHX - FLT 612 - EN ROUTE SNA-DFW, DETECTED SMOKE IN CABIN AND COCKPIT. DIVERTED PHX AND LANDED WITHOUT FURTHER INCIDENT. REPLACED WINDOW HEAT SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SMOKE DETECTOR — ACTIVATED (AFT LAVATORY)

LAX - FLT 207 - EN ROUTE MIA-LAX - DETECTED SMOKE/FIRE AT AFT LAVATORY. LANDED LAX WITHOUT FURTHER INCIDENT. REPLACED FIRE EXTINGUISHER. PERFORMED OPERATIONS CHECK OF SMOKE DETECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SOCKET — DAMAGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATHWAY LIGHT AT SEAT ROW 25 INOPERATIVE. RE-PINNED EMERGENCY EXIT PATHWAY LIGHT WALL PLUG. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS AT SEAT 26D INOPERATIVE. RECONNECTED LOOSE CONNECTOR AT SEAT 26D. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: LIGHT — BROKEN (CABIN)

TPA - DURING OVERNIGHT MAINTENANCE, BULKHEAD EMERGENCY EXIT LIGHT AFT OF DOOR R4 BROKEN. REPLACED BULKHEAD EMERGENCY EXIT LIGHT ASSEMBLY AFT OF DOOR R4. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: LIGHT — DEFECTIVE (CABIN)

MIA - FLT 442 - DURING OVERNIGHT MAINTENANCE SECTION OF EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT ROW 19A INOPERATIVE. REPLACED SECTION OF EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT ROW 19A. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, R2 AFT EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. REPLACED R2 AFT EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: DECK PLATE — CORRODED (BS 1720)

AFW - DECK PLATE HAS CORROSION REMOVED BEYOND SRM LIMITS ON UPPER SURFACE, PER MRB 757-721. TST: 15,773 HRS. CYCLES: 5,917. (X)

Part: FLOOR BEAM — CORRODED (BS 324)

AFW - CORROSION WAS BLENDED BEYOND SRM LIMITS ON FLOOR BEAM AT STA 324, RBL 58, PER MRB 757-723. TST: 15,773. CYCLES: 5,917. (X)

Part: SUPPORT — CORRODED (LT AILERON)

AFW - LEFT WING AILERON HINGE SUPPORT, RIB NR 1 AT STA 817.27, HAS CORROSION REMOVED AROUND NUTPLATE BEYOND SRM LIMITS, PER MRB 757-726. (X)