N660AM

Part: SKIN — CRACKED (NR 2 PYLON) · airframe 68,007 hrs · 23,547 cycles

NUMBER 2 ENG PYLON HAS A CRACK INDICATION AT INBD UPPER AFT THRUST REVERSER HINGE MOUNT FASTENER HOLE, ALUMINUM SKIN LAYER ONLY. REMOVED CRACK BY ENLARGING HOLE TO .831 INCHES IN ALUMINUM SKIN LAYERS ONLY & INSTALLED FREEZE PLUG. INSTALLED DOUBLER IAW B757-54-034406.

Part: PROBE — INOPERATIVE (LT FUEL TANK) · airframe 66,141 hrs · 22,887 cycles

AUS REPEAT ITEM. CREW REPORTED UNWANTED FUEL TRANSFER. AIRCRAFT FERRIED TO DFW FOR ADDITIONAL MAINTENANCE. REPLACED LT TANK COMPENSATOR NR 6 PROBE & DENSITOMETER. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: RADAR — FAILED (ZONE 200) · airframe 64,767 hrs · 22,400 cycles

DFW - INFLIGHT LAX-MIA. CREW REPORTED WEATHER RADAR FAILED. FLIGHT DIVERTED DFW LANDED WITHOUT INCIDENT. REPLACED WEATHER RADAR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: HOUSING — CRACKED (HYDRAULIC PUMP) · airframe 64,433 hrs · 22,273 cycles

MIA - CREW REPORTED RIGHT HYDRAULIC SYSTEM FAILURE. EMERGENCY DECLARED FLIGHT LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED ENGINE DRIVEN PUMP HOUSING THAT WAS CRACKED. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SWITCH — MALFUNCTIONED (COCKPIT) · airframe 63,777 hrs · 22,050 cycles

VVI INFLIGHT MIA-LPB CREW REPORTED SMOKE AND ODOR IN THE COCKPIT AND HIGH ALTITUDE SWITCH SHORTED. FLIGHT DIVERTED VVI LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. PLACARD HIGH ALTITUDE SWITCH PER MEL. FLIGHT CONTINUED TO DESTINATION. REPLACED HIGH ALTITUDE SWITCH ASSEMBLY AT MIA ON 09/07/2012. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PIN — BACKED OUT (FUEL SYSTEM) · airframe 62,293 hrs · 21,510 cycles

JFK - CREW REPORTED RIGHT FUEL TANK AND TOTALIZER BLANKED DURING CLIMB. FLIGHT RETURNED JFK LANDED WITHOUT INCIDENT. PLACARD RIGHT FUEL TANK INDICATION AND TOTALIZER PER MEL. FOUND PIN 9 PUSHED BACK ON CONNECTOR D6884. RESET PIN. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,955 hrs · 21,004 cycles

IN THE CABIN AT STATION 1681 UNDER THE FORWARD LIP OF THE FLOORBEAM THE NUT PLATE MOUNT IS CORRODED AT RIGHT BUTTLINE 24. REMOVED DAMAGE AND INSTALLED DOUBLER PER AARD 53-60-51-5 AND EA B757-53-019192.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 60,955 hrs · 21,004 cycles

STATION 1400, STRINGER 24 LEFT EXTERNAL REPAIR DOUBLER DAMAGED. INSTALLED DOUBLER PER SRM 53-00-03-2R 1, EA PRELIM5 AND EA B757-53-019188.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,955 hrs · 21,004 cycles

FRAME AT STATION 1380 BETWEEN STRINGERS 27 AND 28 RIGHT CORRODED. INSTALLED REPAIR DOUBLER PER SRM 51-70-11-0G FIGURE 1.

Part: WEB — CRACKED (FUSELAGE) · airframe 60,955 hrs · 21,004 cycles

IN THE CABIN THE NEXT STRINGER END RUNOUT PIECE ABOVE STRINGER 12 RIGHT FORWARD OF THE RIGHT NUMBER 2 DOOR OPENING IS CRACKED IN THE OUTBOARD RADIUS AT THE JOGGLE, STATION 681. REMOVED AND REPLACED WEB PER SRM 51-10-02-0G AND EA B757-53-019128.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 60,955 hrs · 21,004 cycles

LEVELING COMPOUND CRACKED AND DISTORTED INSIDE STRINGER 29 RIGHT AT STATION 1420. PERFORMED STRINGER SPLICE REPAIR PER SRM 53-00-03-2R 1.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,955 hrs · 21,004 cycles

WEB CORRODED BETWEEN STATIONS 1600 AND 1620 AT STRINGER 28. ACCOMPLISHED REPAIR PER SRM 51-10-02-G9.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,955 hrs · 21,004 cycles

IN THE CABIN AT THE RIGHT NUMBER 2 DOOR THRESHOLD THE Z ANGLE, TO THE CREASE BEAM, BETWEEN STATIONS 675 AND 755 IS CORRODED. REPLACED Z-ANGLE TO THE RIGHT CREASE BEAM STATIONS 675 TO 755, RIGHT BUTTLINES 63 TO 64, WATERLINE 208 PER SRM 51-10-02-0G SECTION 9 AND EA B757-53-019029.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,955 hrs · 21,004 cycles

MAIN CABIN, FLOOR STRUCTURE, CREASE ANGLE WEB CORRODED RIGHT SIDE STATIONS 940 TO 960. REPLACED WEB PER SRM 51-10-02-0G.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,955 hrs · 21,004 cycles

FLOORBOARD SUPPORT CORRODED STATIONS 1640 TO 1661, WATERLINES 206 TO 208. INSTALLED FLOORBOARD SUPPORT AND VERTICAL STIFFENER PER SRM 51-10-02-0G.

Part: PRESSURE DECK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,955 hrs · 21,004 cycles

THE CABIN REAR PRESSURE DECK HAS A DOUBLER ON TOP THAT IS CORRODED IN SEVERAL PLACES BETWEEN STATIONS 1701 AND 1720 AND LEFT BUTTLINE 1 AND RIGHT BUTTLINE 54. INSTALLED DECK FILLER AND DOUBLER PER SRM 53-60-51-2R 2.

Part: SLAT — CRACKED (LE SLAT) · airframe 60,955 hrs · 21,004 cycles

NUMBER 10 SLAT COVE SKIN CRACKED AT OUTBOARD DRIVE TRACK. INSTALLED NEW SLAT SKIN PER ESO 90253.

Part: SUPPORT FITTING — DAMAGED (FUSELAGE) · airframe 60,955 hrs · 21,004 cycles

LEFT AFT G4 GALLEY MOUNT SUPPORT FITTING HAS TWO (2) DRILL STARTS IN UPPER SURFACE OF FITTING. REMOVED DAMAGED FITTING AND INSTALLED NEW FITTING IAW SRM 51-10-02-0G.

Part: SPAR — CRACKED (SERVICE DOOR) · airframe 60,955 hrs · 21,004 cycles

UPPER OUTER SPAR CHORD IS CRACKED ON RIGHT NUMBER 2 DOOR. ROUTED OUT DAMAGE, OVERSIZED 2 EACH OVERSIZED HOLES AND INSTALLED REPAIR PER ESO 90282 AND EA COMP- 52-018851.

Part: SKIN — DAMAGED (LE SLAT) · airframe 60,955 hrs · 21,004 cycles

BLIND FASTENER AND DEEP BLEND ON NUMBER 8 SLAT UPPER SKIN. REMOVED DAMAGED SKIN AND INSTALLED DOUBLER REPAIR PER AARD 57-43-00-1.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 60,955 hrs · 21,004 cycles

INTERCOSTAL CRACKED STATION 1580 TO 1600. REPLACED INTERCOSTAL PER SRM 51-10-02 OG.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,955 hrs · 21,004 cycles

WEB CORRODED STATION 1020. REPLACED WEB PER SRM 51-10-02-OG.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,955 hrs · 21,004 cycles

LEFT NUMBER 4 DOOR THRESHOLD HAT CHANNEL AT STATION 1672 LEFT BUTTLINE 60 CORRODED. INSTALLED NEW HAT CHANNEL AT LEFT NUMBER 4 DOOR AT STATION 1672 LEFT BUTTLINE 60 PER SRM 51-10-02-0G.

Part: TEE FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,955 hrs · 21,004 cycles

T-FITTING LOCATED ON AFT DECK PLATE FRAME STATION 1720, LEFT BUTTLINE 5 CORRODED - ATTACHES IN BETWEEN THE 2 LEFT BATH TUB FITTINGS. INSTALLED T-ANGLE FITTING, PER SRM 51-10-02-0G.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,858 hrs · 20,253 cycles

ROW 16AB EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR ROW 16AB OVERHEAD BIN EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,821 hrs · 19,498 cycles

WEB CORRODED IN AFT CARGO FROM STATIONS 1360 TO 1380. WEB WAS REPLACED PER SRM 51-10-02-0G.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,821 hrs · 19,498 cycles

CHORD ANGLE CORRODED FROM STATIONS 730 TO 740. ANGLE WAS REPLACED PER 51-1-02-0G.

Part: FITTING — CORRODED (CARGO BAY) · corrosion level 2 · airframe 56,821 hrs · 19,498 cycles

AFT CARGO TIE DOWN CORRODED. TIE DOWN ASSEMBLY WAS REPLACED.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,821 hrs · 19,498 cycles

NUMBER 2 SLAT COVE SKIN IS CRACKED ADJACENT TO BOTH DRIVE TRACKS INBOARD OF ACCESS PANELS 524 CB AND OUTBOARD OF ACCESS PANELS 524 FB. STOPPED DRILLED CRACK AND INSTALLED EXTERNAL DOUBLER ON COVE SKIN INBOARD OF ACCESS PANEL 524 CB AND OUTBOARD OF ACCESS PANEL 524 FB PER AARD 57-43-04.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,522 hrs · 19,386 cycles

EMERGENCY LIGHTS AT SEAT 17B INOPERATIVE. REPLACED LIGHT ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,506 hrs · 19,382 cycles

SEAT MOUNTED EMERGENCY LIGHTS WILL NOT ILLUMINATE FROM ROW 16 THRU 25 ON TEST. FOUND EMERGENCY LIGHT AT SEAT 17DEF DEFECTIVE. REPLACED LIGHT ASSEMBLY.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,200 hrs · 19,277 cycles

EMERGENCY LIGHT AT SEAT ROWS 16DEF TO 22DEF INOPERATIVE. REPLACED BATTERY PACK ABOVE SEAT ROW 20DEF.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,129 hrs · 19,248 cycles

EMERGENCY LIGHTS AT SEAT ROW 16 INOPERATIVE. REPLACED BATTERY PACK.

Part: WIRE — UNSECURE (CABIN)

DFW EMERGENCY LIGHT WIRE AT 3EF SIDEWALL NOT SECURED. RESECURED EMERGENCY LIGHT WIRE AT 3EF.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,309 hrs

SJU - RIGHT FLOOR EMERGENCY LIGHTS AND COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED NUMBER 2 DOOR OVERHEAD LIGHT MODULE.

Part: UNKNOWN — SMOKE (LAVATORY) · airframe 50,907 hrs

EWR INFLIGHT T164/15FEB - CREW REPORTS MID LAVATORY SMOKE DETECTORS ACTIVATED FOLLOWED BY SMOKE AND ODOR IN CABIN. LANDED EWR WITHOUT INCIDENT. REPLACED SMOKE DETECTOR IN MID LAVATORY. AIRCRAFT FERRIED TO TUL FOR FURTHER EVALUATION AND REPAIRS.

Part: A/C PACK — CONTAMINATED (LEFT) · airframe 50,853 hrs

BWI INFLIGHT T775/03FEB LGA TO MIA AT FLIGHT LEVEL 400 FLIGHT ATTENDANT REPORTED AFT AND MID LAVATORY SMOKE DETECTORS ACTIVATED FOLLOWED BY VISIBLE SMOKE AND SMELL IN CABIN AND COCKPIT. SMOKE BECAME MODERATE IN AFT CABIN AND SMOKE BEGAN TO DISSIPATE ON DESCENT AND AFTER LEFT AIR CONDITIONER PACK TURNED OFF. LANDED BWI WITHOUT INCIDENT. FOUND LEFT AIR CONDITIONING PACK AND MIX MANIFOLD CONTAMINATED WITH OIL. REPLACED LEFT AIR CYCLE MACHINE AND REHEATER AND CLEANED LEFT AND RIGHT AIR CONDITIONING PACK PNEUMATIC DUCTS AND MIX MANIFOLDS. ACCOMPLISHED PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: A/C PACK — CONTAMINATED · airframe 52,732 hrs

DTW INFLIGHT T398/01FEB ORD TO LGA - CREW REPORTED SMOKE IN CABIN WITH LEFT HYDRAULIC PRESSURE INDICATION AND RUDDER RATIO LIGHT ILLUMINATED. LANDED DTW WITHOUT INCIDENT. FOUND GLYCOL INGESTED INTO AIR CONDITIONING. PERFORMED PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LINE — LEAKING (HYD SYSTEM)

CUN INFLIGHT T1688 - LEFT HYDRAULIC QUANTITY MESSAGE APPEARED FOLLOWED BY LEFT HYDRAULIC PRESSURE MESSAGE INDICATIONS. VERIFIED LOSS OF LEFT HYDRAULIC FLUID AND PRESSURE. USED ALTERNATE GEAR AND FLAP EXTENSION. RETURNED TO CUN AND LANDED WITHOUT INCIDENT. FOUND ONE HYDRAULIC LINE AT RIGHT WHEEL WELL LEAKING. REPLACED HYDRAULIC LINE AND HYDRAULIC PRESSURE FILTER. SERVICED LEFT HYDRAULIC SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - SEAT MOUNTED EMERGENCY LIGHTS FROM SEAT ROWS 15 TO 23 INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS FROM SEAT ROWS 15 TO 23. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHTS AT OVERHEAD ROWS 11 AND 34 INOPERATIVE. RELAMPED EMERGENCY LIGHTS AT OVERHEAD ROWS 11 AND 34. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY EXIT LIGHT AT LEFT NR 1 DOOR INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT AT LEFT NR 1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PLACARD — MISSING (EMERGENCY EXIT)

DFW - EMERGENCY EXIT LIGHT AT RIGHT HAND WING AFT MISSING DECAL. INSTALLED EXIT ARROW DECAL FOR EMERGENCY EXIT LIGHT AT RIGHT HAND WING AFT SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — BROKEN (EMERGENCY LIGHT)

DFW - AFT MOUNTED EMERGENCY LIGHT CLEAR PLASTIC SHROUD IS BROKEN. REPLACED CLEAR SHROUD FOR AFT MOUNTED EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT LEFT HAND OVERWING EXIT INOPERATIVE. RELAMPED EMERGENCY LIGHT AT LEFT HAND OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (EXTERIOR)

DFW - EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR INOPERATIVE. RELAMPED OUTSIDE EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - SEAT MOUNTED EMERGENCY LIGHTS AT SEATS 16D TO 25D INOPERATIVE. REPLACED BATTERY PACK AND CHARGER AT STATION 1070 AND CHANGED WIRE HARNESS AT SEAT 17D FOR INOPERATIVE SEAT MOUNTED EMERGENCY LIGHTS AT SEATS 16D TO 25D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMEGENCY LIGHT)

SFO - SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 16 TO 25 INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 16 TO 25. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (SEAT 2E)

DFW- AFT EMERGENCY PATH LIGHT AT SEAT 2E INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY PATH LIGHT AT SEAT 2E. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SLIDE — FAILED (L1 DOOR)

MIA - EMERGENCY ESCAPE SLIDE AT DOOR 1L FELL OFF ITS HOLDER AND DID NOT DEPLOY WHEN ARMED DOOR WAS OPENED. POWER ASSIST BOTTLE WAS BLOWN. JETBRIDGE WAS ATTACHED. REPLACED POWER ASSIST BOTTLE AND INSTALLED NEW SLIDE AT 1L DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CLAMP — LOOSE (BLEED AIR)

CCS - FLT 2140 - EN ROUTE CCS-MIA, RIGHT ENGINE FIRE WARNING/OVERHEAT LIGHT ILLUMINATED. RETARDED THROTTLE LIGHT EXTINGUISHED AFTER A FEW MINUTES. ADVANCED THROTTLE AGAIN OVERHEAT LIGHT ILLUMINATED. SHUTDOWN RIGHT ENGINE AS A PRECAUTION, NO OVER TEMPERATURE INDICATIONS THEN NOTED. RETURNED AND LANDED CCS WITHOUT INCIDENT. REPLACED PRECOOLER CLAMP AND THE SENSE LINE BETWEEN THE PRESSURE SHUTOFF VALVE AND THE PRECOOLER ON RIGHT ENGINE. RAN ENGINE AND ALL CHECKS WERE NORMAL. LEAK CHECKED OK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: TRANSMISSION — LACK OF LUBE (T/E FLAP)

MIA - FLT 2040 - EN ROUTE DEN-MIA - TRAILING EDGE FLAP DISAGREE WHEN FLAP HANDLE WAS MOVED FROM 15 TO 20 DEGREES. FLAPS STUCK AT 17 DEGREES INITIALLY. FLAPS AT 20 DEGREES FOR LANDING. LANDED MIA WITHOUT INCIDENT. FLAP TRANSMISSION INDICATOR CIRCUIT BREAKER POPPED AT NR 2 FLAP TRANSMISSION, LEFT WING. RESET FLAP TRANSMISSION INDICATOR AND ADVISED TECH SERVICES. FOUND NR 1, 2 AND 5 FLAP TRANSMISSION REQUIRED SERVICING. SERVICED TRANSMISSIONS AND CYCLED FLAPS SEVERAL TIMES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CHARGER — FAILED (CABIN)

JFK - FOUND EMERGENCY LIGHTS AT SEATS 17-23 ARE INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY AND BATTERY CHARGER MODULE M10800. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WINDOW — CRACKED (COCKPIT)

ORD - FLT 1876 - EN ROUTE LAX-ORD, CRUISING AT 37,000 FEET, FRONT RIGHT COCKPIT WINDOW BEGAN TO ARC AND BURNED LINE THROUGH LAMINATE. WINDOW HEAT WAS TURNED OFF SHORTLY AFTER A LOAD POP AND LAMINATE OR OUTER PAIN SHATTERED. PERFORMED EMERGENCY DESCENT AND SLOWED TO 250 KNOTS AND CONTINUED TO ORD. LANDED ORD WITHOUT INCIDENT. REPLACED R-1 WINDOW PER MM 56-11-01-4. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONTROL PANEL — DEFECTIVE (COCKPIT)

SJU - FLT 495 - EN ROUTE MIA-SJU, DETECTED ELECTRICAL SMOKE IN COCKPIT. TURNED OFF COCKPIT LIGHTS. SMOKE CEASED. RETURNED SJU AND LANDED WITHOUT FURTHER INCIDENT. REPLACED VOR PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PANEL — SEPARATED (NACELLE)

BOS - FLT 1183 - EN ROUTE BOS-STT SHORTLY BEFORE TAKEOFF DETECTED NR 2 ENGINE SHUTDOWN DUE TO INGESTION FROM ACOUSTICAL PANEL AT NACELLE. RETURNED BOS GATE WITHOUT FURTHER INCIDENT. REPLCED NR 2 ENGINE DUE TO FOD FROM DETACHED PANEL. SYSTEM IS CURRENTLY UNDER INVESTIGATION. (M)

Part: FLOOR BEAM — CORRODED (BS 1640)

AFW - FLOOR BEAM HAD 2 AREAS OF CORROSION BLENDED BEYOND SRM LIMITS. REPAIRED PER MRB 757-998. (M)

Part: ANGLE — CORRODED (BS 360)

AFW - ANGLE HAS CORROSION REMOVAL ON UPPER SURFACE, MATERIAL REMAINING IS BEYOND SRM LIMITS. REPAIRED PER MRB 757-995. (M)

Part: FLOOR BEAM — CORRODED (BS 324)

AFW - FLOOR BEAM HAS CORROSION REMOVAL, MATERIAL REMAINING IS BEYOND ALLOWABLE SRM LIMITS. REPAIRED PER MRB 757-997. (M)

Part: SUPPORT — CORRODED (BS 403)

AFW - FLOOR SUPPORTS IN SECTION 41 HAVE CORROSION REMOVAL, MATERIAL REMAINING IS BEYOND SRM ALLOWABLE LIMITS. REPAIRED PER MRB 757-994. (M)

Part: FLOOR BEAM — CORRODED (BS 377)

AFW - FLOOR BEAM HAS CORROSION REMOVAL MATERIAL, REMAINING IS BEYOND SRM ALLOWABLE LIMITS. REPAIRED PER MRB 757-1000. (M)

Part: SILL — CORRODED (CARGO DOORWAY)

AFW - AFT CARGO DOOR SURROUND STRUCTURE LOWER SILL HAD CORROSION BLEND BEYOND SRM LIMITS. REPAIRED PER MRB 757-999. (M)

Part: FLOOR BEAM — CORRODED (BS 310)

AFW - FLOOR BEAM HAS CORROSION REMOVAL, MATERIAL REMAINING IS BEYOND SRM ALLOWABLE LIMITS. REPAIRED PER MRB 757-996. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, FOUND THE RIGHT AFT OVER WATER EMERGENCY EXIT IDENTIFIER INOPERATIVE. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: DOOR PAN — GOUGED (L-4 DOOR)

AFW - FOUND L-4 DOOR HANDLE PAN HAD GOUGE BLENDED BEYOND SRM LIMITS. PER MRB 757-818. (M)

Part: EEL WIRE — BROKEN (CABIN)

DFW - EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 17D TO 26D INOPERATIVE. REPAIRED BROKEN EMERGENCY FLOOR LIGHT WIRE BY PASSENGER SEAT ROW 17D. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)