N643AA

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,903 hrs · 21,510 cycles

CORROSION ON TOP ANGLE AFT END OF THRESHOLD LEFT NUMBER 4 DOOR. REPLACED ANGLE PER SRM 51-10-02-G9.

Part: STIFFENER — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 61,903 hrs · 21,510 cycles

NUMBER 2 CARGO DOOR 2ND STIFFENER FROM LOWER AFT CORRODED. REMOVED CORRODED STIFFENER AND INSTALLED NEW STIFFENER PER ESO 90121.

Part: WEB — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 61,903 hrs · 21,510 cycles

NUMBER 2 CARGO DOOR 3RD WEB FROM LOWER AFT CORRODED. REMOVED CORRODED WEB AND INSTALLED NEW WEB PER ESO 90121.

Part: WEB — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 61,903 hrs · 21,510 cycles

NUMBER 2 CARGO DOOR 1ST WEB FROM LOWER FORWARD CORRODED. REMOVED CORRODED WEB AND INSTALLED NEW WEB PER ESO 90121.

Part: BEAM — DENTED (CARGO DOOR) · airframe 61,903 hrs · 21,510 cycles

NUMBER 2 CARGO DOOR LOWER EDGE ASSEMBLY DENTED AND WORN. REMOVED DAMAGED EDGE BEAM AND INSTALLED NEW EDGE BEAM PER ESO 90121.

Part: WEB — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 61,903 hrs · 21,510 cycles

NUMBER 2 CARGO DOOR 2ND FROM AFT LOWER WEB CORRODED. REMOVED CORRODED WEB AND INSTALLED NEW WEB PER ESO 90121.

Part: WEB — BENT (CARGO DOOR) · airframe 61,903 hrs · 21,510 cycles

NUMBER 2 CARGO DOOR FORWARD LOWER WEB BENT. REMOVED BENT WEB AND INSTALLED NEW WEB PER ESO 90121.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,903 hrs · 21,510 cycles

CORROSION ON UPPER DOOR SILL IN AFT CARGO. REPLACE PANEL PER SRM-51-10-02-0G.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,903 hrs · 21,510 cycles

CORROSION ON STIFFENING ANGLE AT STATION 1720 ON THE FORWARD RIGHT SIDE. REPLACED T-ANGLE PER SRM 51-10-02-G8.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,903 hrs · 21,510 cycles

CORRODED, REPLACED BATHTUB FITTING.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,903 hrs · 21,510 cycles

LEFT NUMBER 4 DOOR THRESHOLD ANGLE CORRODED. REPLACED ANGLE PER SRM 51-10-02-G9.

Part: PLATE — CORRODED (FUSELAGE) · airframe 61,903 hrs · 21,510 cycles

AFT GALLEY AFT DECK REPAIR DOUBLERS BUTT UP AGAINST PRESSURE DECK CHORD ANGLE STATION 1720 LEFT BUTTLINE 60 TO RIGHT BUTTLINE 60. INSTALLED NEW DOUBLER PER EA B757-53-012525.

Part: FITTING — CORRODED (CARGO BAY) · corrosion level 2 · airframe 61,903 hrs · 21,510 cycles

T-CAP CORRODED IN AFT CARGO. REPLACED T-CAP PER SRM 51-10-02-0G.

Part: WEB — CORRODED (CARGO BAY) · corrosion level 2 · airframe 61,903 hrs · 21,510 cycles

WEB CORRODED IN AFT CARGO. REPLACED WEB PER SRM 51-10-02.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,903 hrs · 21,510 cycles

RIGHT CREASE ANGLE HAS CORROSION AT STATION 770 RIGHT BUTTLINE 63 TO 64 WATERLINE 208. INSTALLED NEW CREASE ANGLE SECTION AND SPLICE PER AARD 53-30-13-1, SRM 51-20-01-0G, SRM 51-40-01-0G.

Part: WEB — CORRODED (CARGO BAY) · corrosion level 2 · airframe 61,903 hrs · 21,510 cycles

WEB CORRODED IN AFT CARGO. REPLACED WEB PER SRM 51-10-02.

Part: DOUBLER — DENTED (FUSELAGE) · airframe 61,903 hrs · 21,510 cycles

CLENCHED RIVETS IN FOUR AND A HALF INCH CIRCLE. DOUBLER REPAIR AT STATION 1630 RIGHT SIDE NEXT TO DRAIN MAST PER SRM 53-00-01-2R (5).

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,903 hrs · 21,510 cycles

FLOORBOARD SUPPORT IS CORRODED ON BOTTOM SIDE AT 1510 BUTTLINE 3 LEFT. INSTALLED FLOORBOARD STRINGER SPLICE DOUBLER PER AARD 53-60-53-7.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 61,903 hrs · 21,510 cycles

NUMBER 7 SLAT TRAILING EDGE WEDGE DELAMINATED. INSTALLED NEW TRAILING EDGE WEDGE PER ESO 90248.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 61,903 hrs · 21,510 cycles

STATION 700 FLOORBEAM CRACK LEFT BUTTLINE 24 TO LEFT BUTTLINE 45. REPAIRED PER SRM 53-00-51.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,903 hrs · 21,510 cycles

WEB CORRODED STRINGER 27 RIGHT STATION 1437 BEHIND DOORWAY CASTING. REMOVED AND REPLACED WEB PER SRM 51-10-02.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,903 hrs · 21,510 cycles

WEB CORRODED STRINGER 27 RIGHT STATION 1383. REMOVED AND REPLACED WEB PER SRM 51-10-02-G8.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,903 hrs · 21,510 cycles

LEFT CREASE ANGLE HAS CORROSION AT STATION 770. INSTALLED SPLICE REPAIR PER AARD 53-30-13-1.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,903 hrs · 21,510 cycles

TRANSITION PANEL CORROSION STATIONS 1530 TO 1640 RIGHT BUTTLINE 16.25 TO 23.5 STRINGER 26 RIGHT. REPLACED TRANSITION PANEL PER SRM 51-10-02.

Part: SKIN — CRACKED (LE SLAT) · airframe 61,903 hrs · 21,510 cycles

LEFT WING SLAT NUMBER 2 SKIN IS CRACKED OUT FROM FASTENERS AT TRACK CUTOUT. STOP DRILLED HOLE AT END OF CRACK IN COVE SKIN PER AARD 57-43-00-4. FABRICATED AND DRILLED REPAIR DOUBLER. INSTALLED DOUBLER PER AARD 57-43-00-4.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,281 hrs · 21,288 cycles

EMERGENCY PATHWAY LIGHT AT SEAT 32D IS INOPERATIVE. REPLACED LAMP FOR EMERGENCY PATHWAY LIGHT AT SEAT 32D. OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 61,281 hrs · 21,288 cycles

EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER 4 DOOR IS INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER 4 DOOR. OPS CHECKED NORMAL.

Part: CONNECTOR — BROKEN (CABIN) · airframe 61,281 hrs · 21,288 cycles

EMERGENCY LIGHTS AT SEAT 6EF ARE INOPERATIVE. REPAIRED BROKEN CONNECTOR LIGHT FOR EMERGENCY LIGHTS AT SEAT 6EF. OPS CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,783 hrs · 21,114 cycles

LEFT OVERWING EMERGENCY EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK FOR LEFT OVERWING EMERGENCY EXIT SIGN. OPS CHECKED NORMAL.

Part: TAT PROBE — INOPERATIVE (ZONE 100) · airframe 60,696 hrs · 21,080 cycles

DFW - INFLIGHT LAX-STL. CREW REPORTED TOTAL AIR TEMPERATURE PROBE HEAT FAILURE IN CRUISE. FLIGHT DIVERTED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED TOTAL AIR TEMPERATURE PROBE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,294 hrs · 20,935 cycles

FOUND CORROSION ON Z-ANGLE. REMOVED AND REPLACED PER SRM 51-10-02.

Part: SKIN — DAMAGED (TE FLAP) · airframe 60,294 hrs · 20,935 cycles

LEFT INBOARD TRAILING EDGE AFT FLAP HAS A HOLE IN THE LOWER SKIN. REMOVED 2.75 INCH DIAMETER DAMAGED BOTTOM SKIN AND CORE. TOP SKIN UNDAMAGED. FABRICATED NEW CORE AND INSTALLED PER SRM 51-70-17-0G PARAGRAPH 4C FIGURE 11 SECTION B-B.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,294 hrs · 20,935 cycles

FOUND CORROSION ON LAVATORY MOUNT FITTING. REMOVED AND REPLACED MOUNT FITTING PER SRM 51-10-02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,294 hrs · 20,935 cycles

FOUND CORROSION ON GALLEY TIE DOWN. REMOVED AND REPLACED TIE DOWN PER SRM 51-10-02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,294 hrs · 20,935 cycles

FOUND CORROSION ON GALLEY TIE DOWN. REMOVED AND REPLACED TIE DOWN PER SRM 51-10-02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,294 hrs · 20,935 cycles

FOUND CORROSION ON GALLEY TIE DOWN. REMOVED AND REPLACED TIE DOWN PER SRM 51-10-02.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,294 hrs · 20,935 cycles

FOUND CORROSION ON LAVATORY MOUNT FITTING. REMOVED AND REPLACED MOUNT FITTING PER SRM 51-10-02.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,294 hrs · 20,935 cycles

FOUND CORROSION ON GALLEY FLOOR. INSTALLED DOUBLER PER SRM 53-60-51.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,294 hrs · 20,935 cycles

FOUND CORROSION ON LAVATORY MOUNT FITTING. REMOVED AND REPLACED MOUNT FITTING PER SRM 51-10-02.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,294 hrs · 20,935 cycles

FOUND CORROSION ON LAVATORY MOUNT FITTING. REMOVED AND REPLACED PER SRM 51-10-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,294 hrs · 20,935 cycles

FOUND CORROSION ON FLOORBOARD SUPPORT. REMOVED AND REPLACED SUPPORT PER SRM 51-10-02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,294 hrs · 20,935 cycles

FOUND CORROSION ON GALLEY TIE DOWN FITTING. REMOVED AND REPLACED FITTING PER SRM 51-10-02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,294 hrs · 20,935 cycles

FOUND CORROSION ON GALLEY TIE DOWN. REMOVED AND REPLACED TIE DOWN PER SRM 51-10-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,294 hrs · 20,935 cycles

FOUND CORROSION ON FLOORBOARD SUPPORT. REMOVED AND INSTALLED NEW SUPPORT PER SRM 51-10-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,294 hrs · 20,935 cycles

FOUND CORROSION ON FLOORBOARD SUPPORT. REMOVED AND REPLACED SUPPORT PER SRM 51-10-02.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,294 hrs · 20,935 cycles

FOUND CORROSION ON LAVATORY MOUNT FITTING. REMOVED AND REPLACED MOUNT FITTING PER SRM 51-10-02.

Part: LENS — MISSING (CABIN)

DFW BULLNOSE EMERGENCY LIGHT AT SEAT 27C MISSING LENS. REPLACED LENS FOR BULLNOSE EMERGENCY LIGHT AT SEAT 27C.

Part: LIGHT — INOPERATIVE (CABIN)

DFW EMERGENCY PATH LIGHTING AT SEAT 32D INOPERATIVE. REPLACED LAMP FOR EMERGENCY PATH LIGHT AT SEAT 32D.

Part: LIGHT — INOPERATIVE (CABIN)

DFW BULLNOSE EMERGENCY LIGHT ABOVE 3B INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT BULLNOSE ABOVE 3B.

Part: LIGHT — INOPERATIVE (EXTERIOR)

DFW - EXTERIOR EMERGENCY LIGHT AT LEFT OVERWING INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LEFT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - EMERGENCY SEAT MOUNTED LIGHTS AND EDIT MARKER LIGHTS ARE DIM FROM SEAT ROW 26 TO AFT OF CABIN. REPLACED BATTERY PACK FOR DIM EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (EXTERIOR)

DFW EXTERNAL EMERGENCY SLIDE LIGHT AT LEFT NUMBER FOUR DOOR IS INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY SLIDE LIGHT AT LEFT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SOCKET — LOOSE (CABIN)

DFW EMERGENCY LIGHT AT AFT SEAT 16D INOPERATIVE. SECURED SOCKET IN SEAT HARNESS CONNECTOR FOR EMERGENCY LIGHT AT AFT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,259 hrs

JFK - EMERGENCY LIGHT AT RT AFT OVERWING INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RT AFT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: CONTACT — DAMAGED (EMERGENCY LIGHT) · airframe 55,259 hrs

JFK - EMERGENCY LIGHT AT RT AFT OVERWING INOPERATIVE. REPLACED CLIP FOR EMERGENCY LIGHT AT RT AFT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LAX - EMERGENCY EXIT SIGN LIGHT AT RIGHT SIDE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN LIGHT AT RIGHT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

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

Part: BULB — BURNED OUT (EMERGENCY LIGHTS)

DFW - FOUND EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR SLIDE INOPERATIVE. RELAMPED EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT ROW 24 INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT ROW 24. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FITTING — DISCONNECTED (LEFT ENGINE)

DFW INFLIGHT - CLIMBING THROUGH APPROXIMATELY FLIGHT LEVEL 180 LEFT HAND ENGINE PRESSURE RATIO N1, N2 AND N3 WERE RAPIDLY DECREASING AND LEFT HAND ENGINE WAS PUTTING OUT SIGNIFICANTLY LESS POWER. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND FITTING ON P1 LINE BELOW OIL TANK OFF. ATTACHED LINE AND SAFE TIED. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHTS AT SEAT ROWS 25 TO 36 INOPERATIVE. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS AT ROWS 25 TO 36. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SIGN — BROKEN (EMERGNECY LIGHT)

DFW - AFT RIGHT HAND CABIN DOOR EXIT ARROW MARKER SIGN LIGHT AFT OF THE DOOR IS BROKEN. REPLACED THE AFT RIGHT HAND CABIN DOOR INTERIOR EXIT ARROW MARKER SIGN LIGHT AFT OF THE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PUMP — FAILED (HYD SYSTEM)

ENROUTE CUN-MIA AND APPROACHING MIA FOR LANDING LOST ENTIRE LEFT HYDRAULIC SYSTEM. LANDED WITHOUT FURTHER INCIDENT. REPLACED ENGINE DRIVEN HYDRAULIC PUMP. PERFORMED LEAK AND SYSTEM GROUND CHECKED NORMAL OPERATION. (SW21200401054)

Part: COMPRESSOR WHEEL — DAMAGED (RT ENGINE)

AIRCRAFT VIBRATION FELT AND LOUD THUMP WAS HEARD AT 20,000 ON CLIMB-OUT. RIGHT ENGINE VIBRATED INTO THE AMBER RANGE. RETARDED THROTTLE BACK INTO NORMAL RANGE ATTEMPTS TO ADVANCE THE THROTTLE CAUSED VIBRATION TO RETURN INITIAL THUMP WITH SLIGHT CONTROL MOVEMENT. SLIGHT BURNED SMELL. ALL OTHER INDICATIONS NORMAL. DAMAGE FOUND TO ENGINE C1 DISK, NOSE COWLING AND THRUST REVERSERS. REMOVED AND REPLACED THR NR 2 ENGINE. SYSTEM GROUND OPERATIONS AND LEAK CHECKED CONDUCTED NORMAL FOR OPERATION. (M)

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, AFT FACING CLASS DIVIDER EMERGENCY EXIT SIGN INOPERATIVE. CONNECTED EMERGENCY EXIT SIGN QUICK DISCONNECT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — BROKEN (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 17D BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: VALVE — LEAKING (LT ACM BAY)

SNA - FLT 1409 - EN ROUTE DFW-SNA UPON LANDING, TOWER REPORTED SMOKE AT RIGHT SIDE TIRES. LANDED SNA WITHOUT FURTHER INCIDENT. REPLACED LEFT SIDE SLAT BYPASS VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

BOS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT PATH LIGHTING AT SEAT 24DEF THROUGH 24 DEF INOPERATIVE. RECONNECTED EMERGENCY EXIT SEAT PATH LIGHTING CONNECTOR AT SEAT 27 DEF. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE AFT CABIN EMERGENCY EXIT FLOOR PATH LIGHTING HAS A BULB INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHTING STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: SWITCH — FAILED (CABIN)

ORD - FLT 861 - DURING TURNAROUND, MAINTENANCE FOUND EMERGENCY EXIT LIGHT PANEL UNARMED SWITCH CAPSULE BROKEN. REPLACED EMERGENCY EXIT LIGHT PANEL UNARMED SWITCH CAPSULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — FAILED (CABIN)

MIA - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTING IN FIRST CLASS SECTION TO COACH CLASS INOPERATIVE. REPAIRED WIRE SPLICE CONNECTOR AT COACH CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: STRUCTURE — CORRODED (BS 1434)

AFW - AFT CARGO LOWER SILL SURROUND STRUCTURE HAS CORROSION REMOVED ON THE LOWER SURFACE OF THE INNER CHORD. PER MRB 757-706. TST, 15,723.22 HOURS. CYCLES, 5,740. (X)

Part: FLOOR BEAM — MISDRILLED (FS 1640)

AFW - FLOOR BEAM AT STA 1640, RBL 24, WAS DRILLED IN RADIUS OF THE LOWER FLANGE, AFT SIDE PER MRB 757-714 TST, 15,723.22 HOURS. CYCLES, 5,740. (X)

Part: FLOOR BEAM — CORRODED (BS 377)

AFW - FLOOR BEAM AT STA 377 HAS CORROSION REMOVED ON UPPER SURFACE BEYOND SRM LIMITS. PER MRB 757-703. TOTAL CYCLES, 15,723.22 HOURS. CYCLES, 5,740. (X)

Part: FLOOR BEAM — CORRODED (FS 324)

AFW - FLOOR BEAM AT STA 324 HAS CORROSION ON UPPER SURFACE REMOVED BEYOND SRM LIMITS. PER MRB 757-700. TST, 15,723.22 HOURS. CYCLES, 5,740. (X)

Part: DOOR PAN — GOUGED (R4 DOOR)

AFW - R-4 DOOR PAN HAS A GOUGE BEYOND SRM LIMITS. PER MRB 757-709. TST, 15,723.22 HOURS. CYCLES, 5,740. (X)

Part: FLOOR BEAM — CORRODED (BS 365)

AFW - FLOOR BEAM AT STA 365, RBL 25, HAS CORROSION BLENDED BEYOND SRM LIMITS. PER MRB 757-702. TST, 15,723.22 HOURS. CYCLES, 5740. (X)

Part: DECK PLATE — CORRODED (BS 1720)

AFW - DECK PLATE HAS CORROSION REMOVED ON UPPER SURFACE AT SEVERAL LOCATIONS. CORROSION REMOVED IS BEYOND SRM LIMITS. PER MRB 757-699. TST, 15,723.22 HOURS, CYCLES, 5,740. (X)