N657AM

Part: SLIDE — DEPLOYED (L1 DOOR) · airframe 70,164 hrs · 24,358 cycles

FLIGHT ATTENDANT OPENED LT NR 1 DOOR WHILE IT WAS STILL ARMED & SLIDE DEPLOYED UNSUCCESSFULLY. REPLACED DOOR ASSIST RESERVOIR & SLIDE PACK. OPERATIONS CHECKED NORMAL.

Part: WIRE — DAMAGED (CABIN) · airframe 69,608 hrs · 24,139 cycles

EMERGENCY LIGHTS FROM ROWS 26 TO 36 INOPERATIVE. FOUND DAMAGED WIRES ON L759 EXIT LIGHT. R & R LIGHT FIXTURE L759. OPERATIONS CHECKED NORMAL.

Part: LIGHT — DAMAGED (CABIN) · airframe 69,608 hrs · 24,139 cycles

EMERGENCY EXIT LIGHT AT LT NR 4 DOOR DAMAGED. REPLACED LIGHT ASSEMBLY AT LT NR 4 DOOR. OPERATIONS CHECKED NORMAL.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,608 hrs · 24,139 cycles

CORROSION AT STATION 1661 & RBL 37 ON TOP OF BEAM. INSTALLED DOUBLER IAW SRM 53-00-51-2R-11.

Part: FITTING — DAMAGED (NR 1 PYLON) · airframe 69,474 hrs · 24,089 cycles

NUMBER 1 PYLON ONE FASTENER HOLE HAD A CRACK INDICATION DURING HFEC INSPECTION. THE SUBJECT HOLE WAS IN THE AFT FITTING, INBD SIDE, UPPER AFT HOLE. THE HOLE ON THE SKIN ONLY WAS OVERSIZED TO REMOVE DAMAGE & A FREEZE PLUG WAS INSTALLED.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 69,466 hrs · 24,086 cycles

LT FWD OVERWING DOOR EMERGENCY LIGHT FWD BULB INOPERATIVE. REPLACED LAMP FOR LT FWD OVERWING DOOR EMERGENCY LIGHT, OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 69,466 hrs · 24,086 cycles

LT FWD OVERWING DOOR EMERGENCY LIGHT AFT BULB INOPERATIVE. REPLACED LAMP FOR LT FWD OVERWING DOOR EMERGENCY LIGHT, OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 69,466 hrs · 24,086 cycles

RT OVERWING FWD EMERGENCY LIGHT UPPER LAMP INOPERATIVE. REPLACED LAMP FOR RT OVERWING FWD UPPER EMERGENCY LIGHT, OPERATIONS CHECKED NORMAL.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 69,466 hrs · 24,086 cycles

FIRST CLASS ESCAPE PATH LIGHT INOPERATIVE. REPINED CONNECTOR AFT EMERGENCY ESCAPE PATH LIGHT, OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 69,466 hrs · 24,086 cycles

RT FWD OVERWING DOOR EMERGENCY LIGHT AFT BULB INOPERATIVE. REPLACED LAMP FOR RT FWD OVERWING DOOR EMERGENCY LIGHT, OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 69,466 hrs · 24,086 cycles

LT AFT OVERWING DOOR EMERGENCY LIGHT FWD BULB INOPERATIVE. REPLACED FWD LAMP FOR LT AFT OVERWING DOOR EMERGENCY LIGHT, OPERATIONS CHECKED NORMAL.

Part: FRAME — GOUGED (FUSELAGE) · airframe 65,719 hrs · 22,700 cycles

DEEP GOUGE IN FRAME, FORWARD SIDE OF E AND E ACCESS DOOR CUTOUT. INSTALLED DOUBLER REPAIR PER EA B757-53-027257.

Part: SKIN — DENTED (FUSELAGE) · airframe 65,719 hrs · 22,700 cycles

DENT IN FUSELAGE SKIN AT STATIONS 1540 TO 1560 AND STRINGERS 26 AND 27 RIGHT. INSTALLED REPAIR DOUBLER PER EA B757-53-027315.

Part: CONNECTOR — BROKEN (CABIN) · airframe 64,470 hrs · 22,241 cycles

EMERGENCY LIGHT IN CEILING OVER LEFT WING EXIT FOUND INOPERATIVE. FOUND BAD PIN RETAINER ON THE QUICK DISCONNECT. REPLACED QUICK DISCONNECT. OPS CHECK NORMAL.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 61,839 hrs · 21,249 cycles

STRINGER 15 LEFT CRACKED UNDER SKIN DENT. CUT OUT DAMGE AND DID STRINGER REPAIR PER SRM 51-10-02.

Part: STRAP — CRACKED (FUSELAGE) · airframe 61,839 hrs · 21,249 cycles

CRACK IN STRAP AT STATION 345 BUTTLINE 0. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-10-51.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,839 hrs · 21,249 cycles

CORROSION AROUND FLOORBOARD HOLES ON STATION 1640 FLOORBEAM FROM RIGHT BUTTLINE 40 TO 56. REPLACED BEAM PER EA B757-53-017884 DATED 07/24/11.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,839 hrs · 21,249 cycles

STATIONS 1500 TO 1520 STRINGERS 30 LEFT AND RIGHT WEB CORRODED. ACCOMPLISHED REPAIR PER AARD 51-10-05-1.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 61,839 hrs · 21,249 cycles

INTERCOSTAL CRACKED STATIONS 1620 TO 1640 RIGHT BUTTLINE 20. INSTALLED NEW INTERCOSTAL PER SRM 51-10-02-0G.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 61,839 hrs · 21,249 cycles

RIGHT NUMBER 1 DOOR CUTOUT FORWARD FUSELAGE FRAME CRACKED AT STATION 329 BETWEEN STRINGER 11 AND 12 RIGHT. INSTALLED DOUBLER PER EA B757 53-017917 AND SRM 51-70-11-0G.

Part: WEB — CORRODED (LT MLG WW) · corrosion level 2 · airframe 61,839 hrs · 21,249 cycles

LEFT WHEEL WELL AREA JUST ABOVE AFT END OF KEEL BEAM, 4 TO 6 INCHES FROM AFT BULKHEAD STATION 1180 CORRODED. CORRODED AREA REPAIRED PER EA 757-53-017624 DATED 07/19/2011.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 61,839 hrs · 21,249 cycles

SCUFF PLATE CRACKED STRINGER 17 RIGHT. INSTALLED SCUFF PLATE PER AMM 53-13-01-4.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,839 hrs · 21,249 cycles

CORROSION ON VERTICAL LEG OF T-CAP AT FORWARD SIDE OF STATION 1440. REPLACED T-CAP PER AARD 51-10-05-1.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,839 hrs · 21,249 cycles

FOUND CORROSION AT AFT CARGO DOOR CUTOUT WEB STATION 1382 AND ABOVE STRINGER 26 RIGHT AFTER T-CAP AND FITTING REMOVED. INSTALLED NEW WEB PER AARD 51-10-05-1.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 61,839 hrs · 21,249 cycles

STATION 460 TO 480, RIGHT BUTTLINE 15, WEB TOP CAP DAMAGED. REPLACED INTERCOSTAL PER SRM 51-40-03 AND SRM 53-00-51.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,839 hrs · 21,249 cycles

CORROSION ON THE FLOORBOARD ANGLE AT STATION 1675 AND LEFT BUTTLINE 53. INSTALLED NEW ANGLE PER SRM 51-10-02-G.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,839 hrs · 21,249 cycles

LEFT NUMBER 4 DOOR SCUFF PLATE MOUNT CORRODED AT STATION 1681. REMOVED AND REPLACED L ANGLE PER SRM 51-10-02-0G.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,839 hrs · 21,249 cycles

IN THE CABIN AT STATION 1604 THE RIGHT AFT LAVATORY MOUNT IS CORRODED AT RIGHT BUTTLINE 25. INSTALLED NEW LAVATORY MOUNT PER SRM 51-10-02-0G.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,839 hrs · 21,249 cycles

IN THE CABIN AT STATION 1638 THE RIGHT AFT LAVATORY MOUNT IS CORRODED AT RIGHT BUTTLINE 25. INSTALLED NEW LAVATORY MOUNT PER SRM 51-10-02-0G.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,839 hrs · 21,249 cycles

STATION 1604 THE RIGHT AFT LAVATORY MOUNT IS CORRODED AT RIGHT BUTTLINE 46. INSTALLED LAVATORY MOUNT AND SUPPORT PER SRM 51-40-02-02 51-10-02-OG IPC 53-01-54-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,839 hrs · 21,249 cycles

STATION 1590 THE RIGHT OUTBOARD FLOORBOARD SUPPORT IS CORRODED. REPLACED CREASE ANGLE PER SRM 51-70-12-0G AND AARD 53-60-13-1.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,839 hrs · 21,249 cycles

GUTTER SUPPORT CORRODED AT STATIONS 1640 TO 1660 AND RIGHT BUTTLINE 57. INSTALLED NEW SUPPORT PER SRM 51-10-02-G.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,839 hrs · 21,249 cycles

CORROSION ON THE GUTTER SUPPORT AT STATIONS 1660 TO 1680 RIGHT BUTTLINE 57. INSTALLED NEW GUTTER SUPPORT PER SRM 51-10-02-G.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,839 hrs · 21,249 cycles

CREASE ANGLE CORRODED AT STATION 1675 AND RIGHT BUTTLINE 53. INSTALLED NEW CREASE ANGLE PER SRM 51-10-02-G.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,839 hrs · 21,249 cycles

STRINGER 17 LEFT STATIONS 1700 TO 1720 WEB CORRODED. REPLACED STRINGER WEB PER AARD 51-10-05-1.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 3 · airframe 61,839 hrs · 21,249 cycles

CORROSION ON AFT CARGO WEB BETWEEN STATIONS 1600 AND 1620 AT STRINGER RIGHT OF STRINGER 30. REPLACED WEB PER AARD 51-10-05-1.

Part: WEDGE — DEBONDED (LE SLAT) · airframe 61,839 hrs · 21,249 cycles

DISBOND FOUND ON NUMBER 8 RIGHT OUTBOARD SLAT TRAILING EDGE WEDGE. REPLACED TRAILING EDGE WEDGE.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,839 hrs · 21,249 cycles

FLOORBOARD TO WEB ANGLE CORRODED AFT OF RIGHT NUMBER 2 DOOR STATIONS 745 TO 755. REPLACED CREASE ANGLE PER SRM 51-10-02-0G.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,839 hrs · 21,249 cycles

WEB CORRODED STATIONS 1600 TO 1620. REPLACED WEB PER AARD 51-10-05-1.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,839 hrs · 21,249 cycles

ENTRY DOOR THRESHOLD SUPPORT CORRODED. ACCOMPLISHED REPAIR PER SRM 51-10-02-G9.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,839 hrs · 21,249 cycles

CREASE ANGLE WEB CORRRODED STATIONS 960 TO 980 AND STRINGER 17 RIGHT, RIGHT BUTTLINE 60. REPLACED WEB PER SRM 51-10-02-0G.

Part: DOOR — CRACKED (R2) · airframe 61,839 hrs · 21,249 cycles

RIGHT NUMBER 2 DOOR UPPER HINGE CUTOUT CRACKED. ROUTED OUT CRACK AND INSTALLED DOUBLER PER EA COMP-52-017690 DATED 6/24/2011.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,839 hrs · 21,249 cycles

FLOORBOARD SUPPORT CORRODED. REPLACED SUPPORT PER SRM 51-10-02 AND AARD 51-10-05.

Part: BEAM — BENT (CARGO DOOR) · airframe 61,839 hrs · 21,249 cycles

FORWARD CARGO DOOR LOWER EDGE BEAM BENT IN TWO AREAS. REPLACED LOWER EDGE BEAM PER ESO 90114.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,839 hrs · 21,249 cycles

OUTBOARD GALLEY SUPPORT CORRODED. REMOVED CORROSION, ALODINED, PRIMED, FILLED WITH BMS 5-92 AND PAINTED PER AARD 53-10-51-3.

Part: STRAP — CRACKED (FUSELAGE) · airframe 61,839 hrs · 21,249 cycles

CEILING STRAP CRACKED AT STATION 377.7 AND APPROXIMATELY LEFT BUTTLINE 24. REPLACED STRAP PER SRM.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,839 hrs · 21,249 cycles

LAVATORY MOUNT STATION 1604 LEFT BUTTLINE 25 CORRODED. INSTALLED NEW LAV MOUNT PER SRM 51-10-02-0G.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,839 hrs · 21,249 cycles

AFT DECK STATIONS 1681 TO 1720 CORRODED. REPLACED AFT DECK PER SRM 53-10-02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,839 hrs · 21,249 cycles

T-CLIP STATION 1720 CORRODED. REPLACED T-CLIP FITTING PER SRM 51-10-02-G.

Part: BOTTLE — EMPTY (R1 DOOR) · airframe 61,836 hrs · 21,248 cycles

ON WALKAROUND FOUND THAT THE RIGHT NUMBER 1 DOOR ASSIST BOTTLE EMPTY. REPLACED THE RIGHT NUMBER 1 DOOR ASSIST BOTTLE. OPS CHECK NORMAL.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 61,079 hrs · 21,008 cycles

PROX LIGHT AT SEAT 24D INOPERATIVE. SECURED CONNECTOR AT WALL FOR SEAT 24D PROXIMITY LIGHT. OPS CHECK NORMAL.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 61,079 hrs · 21,008 cycles

PROXIMITY LIGHT AT SEAT 33D INOPERATIVE. SECURED CONNECTOR FOR PROXIMITY LIGHT AT SEAT 33D. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,079 hrs · 21,008 cycles

AFT WING SLIDE LIGHTS INOPERATIVE (1 ON EACH WING). REPLACED BATTERY PACK M10770 FOR SLIDE PROXIMITY LIGHTING. OPS CHECK NORMAL.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 61,079 hrs · 21,008 cycles

PROXIMITY LIGHT AT SEAT 31D INOPERATIVE. SECURED CONNECTOR FOR PROXIMITY LIGHT AT SEAT 31D. OPS CHECK NORMAL.

Part: UNKNOWN — ODOR (CABIN) · airframe 60,352 hrs · 20,751 cycles

PLS - INFLIGHT MIA-SJU. FLIGHT ATTENDANT REPORTED BURNING ODOR IN CABIN AROUND ROW 30. EMERGENCY DECLARED FLIGHT DIVERTED PLS LANDED WITHOUT INCIDENT. RESET INFLIGHT ENTERTAINMENT SYSTEM CIRCUIT BREAKERS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PLACARD — MISSING (CABIN) · airframe 60,234 hrs · 20,703 cycles

NUMBER ONE DOOR FORWARD EMERGENCY LIGHT MISSING EXIT PLACARD. INSTALLED EXIT PLACARD ON 1 DOOR FORWARD EMERGENCY LIGHT. OPS CHECKED NORMAL.

Part: PLACARD — MISSING (CABIN) · airframe 60,234 hrs · 20,703 cycles

FORWARD RIGHT NUMBER 2 DOOR MISSING EMERGENCY LIGHT EXIT PLACARD. REPLACED FORWARD RIGHT NUMBER 2 DOOR EMERGENCY LIGHT PLACARD. OPS CHECK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,154 hrs · 20,679 cycles

AREA FLOOD EMERGENCY LIGHT IN BULLNOSE ABOVE SEAT 19ABC IS INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT IN BULLNOSE ABOVE SEAT 19ABC. OPS CHECKS NORMAL.

Part: FAN — MALFUNCTIONED (CABIN) · airframe 60,113 hrs · 20,661 cycles

MIA - FLIGHT ATTENDANT REPORTED BURNING PLASTIC OIL RUBBER SMELL IN FIRST CLASS ABOUT 15 MIN INTO FLIGHT. NO FIRE OR SMOKE INDICATION IN COCKPIT BUT FLIGHT ATTENDANT ALSO REPORTED WARM SPOTS ON FLOOR AT ROWS 1 AND 2 HJ SIDE EMERGENCY DECALS. EMERGENCY DECLARED RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT RECIRCULATION FAN AND BOTH EQUIPMENT COOLING FANS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PLACARD — DAMAGED (CABIN) · airframe 59,704 hrs · 20,510 cycles

RIGHT AFT OVERWING EXIT STICKER DAMAGED. REPLACED RIGHT AFT OVERWING EXIT STICKER.

Part: PLACARD — DAMAGED (CABIN) · airframe 59,704 hrs · 20,510 cycles

LEFT AFT OVERWING EXIT STICKER DAMAGED. REPLACED LEFT AFT OVERWING EXIT STICKER.

Part: GENERATOR — FAILED (RT ENGINE) · airframe 59,613 hrs · 20,475 cycles

MIA - CREW REPORTED ON CLIMBOUT RIGHT GENERATOR FAILED WITH AUXILIARY POWER UNIT ALREADY ON PLACARD. EMERGENCY DECLARED RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT GENERATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,143 hrs · 20,308 cycles

EMERGENCY LIGHTS FOR ROWS 9 THRU 14 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FOR ROWS 9 THRU 14. OPS CHECK OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,667 hrs · 20,138 cycles

BULLWISE EMERGENCY LIGHT AT 27ABC INOPERATIVE. REPLACED LAMP FOR BULLWISE AT 27ABC EMERGENCY LIGHT. OPS CHECKED NORMAL.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 57,693 hrs · 19,802 cycles

LEFT WING NUMBER 3 SLAT UPPER SKIN CORRODED AROUND FASTENERS APPROX 33 INCHES FROM OUTBOARD END. REMOVED DAMAGED SKIN AND INSTALLED DOUBLER PER AARD 57-43-00-4.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 57,693 hrs · 19,802 cycles

LEFT WING SLAT NUMBER 3 UPPER SKIN CORRODED AROUND FASTENERS 3 FEET FROM RIB END AT TRAILING EDGE WEDGE JOINT. REMOVED DAMAGED SKIN AND INSTALLED DOUBLER PER AARD 57-43-0-4.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,693 hrs · 19,802 cycles

NUMBER 2 SLAT INNER COVE SKIN HAS CRACK AT OUTBOARD TRACK ATTACH POINT. FABRICATED, PRIMED, PAINTED AND INSTALLED NEW COVE SKIN PER AARD 51-20-00-1 REPAIR 1.

Part: ANGLE — CORRODED (LE SLAT) · corrosion level 2 · airframe 57,693 hrs · 19,802 cycles

RIGHT WING NUMBER 8 SLAT COVE ANGLE HAS AREAS OF CORROSION. REMOVED COVE ANGLE AND INSTALLED NEW COVE ANGLE PER AARD 57-43-00-3.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,423 hrs · 19,699 cycles

EMERGENCY LIGHT AT AFT CABIN SECTION DIM. REPLACED BATTERY PACK.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 54,620 hrs

SFO - AFT EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,650 hrs · 53,650 cycles

DFW - EMERGENCY LIGHT AT SEAT 21D INOPERATIVE. REPLACED CONNECTOR AT SIDEWALL FOR EMERGENCY LIGHT AT SEAT 21D. SYSTEM GROUND CHECKED NORMAL OPERATION. (S)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,151 hrs

DFW - EMERGENCY LIGHTS AT SEAT ROW 20 TO AFT OF CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROW 20 TO AFT OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SLIDE — DISLODGED (L4 DOOR)

MIA FLIGHT 2190/15AUG - LEFT NUMBER FOUR DOOR SLIDE FELL OFF DOOR WHEN CATERING OPENING UNARMED DOOR. SLIDE WAS DISLODGED AND DID NOT DEPLOY. REPLACED SLIDE FOR LEFT NUMBER FOUR DOOR AND ASSIST BOTTLE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHT AT SEAT 28D INOPERATIVE. RECONNECTED SIDEWALL CONNECTOR FOR EMERGENCY LIGHT AT SEAT 28D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: TRANSMITTER — MALFUNCTIONED (EPR)

SEA INFLIGHT T1661/29MAR - EMERGENCY DECLARED ON DESCENT INTO SEA DUE TO LEFT ENGINE PRESSURE RATIO FLUX. UNABLE TO CONTROL ENGINE THRUST. LANDED SEA WITHOUT INCIDENT. REPLACED LEFT ENGINE PRESSURE RATIO TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGE NCY LIGHT)

MIA - FOUND EMERGENCY LIGHT AT SEAT 33D INOPERATIVE. SECURED LOOSE CONNECTOR AT SEAT 33D FOR EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY LIGHT AT SEAT 18D INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — BROKEN (EMERGENCY SIGN)

MIA - LEFT ONE DOOR TWO EACH EMERGENCY EXIT LIGHTS ARE BROKEN. REPLACED TWO EMERGENCY EXIT SIGNS AT LEFT ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY EXIT SIGN ABOVE LEFT AFT DOOR NUMBER 4 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN ABOVE LEFT AFT DOOR NUMBER 4. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ODOR — DETECTED (CABIN)

FLIGHT ATTENDANT AT MID CABIN NOTICED AN ELECTRICAL ODOR AT 1,200 FT DECLARED EMERGENCY AND LANDED AT FJK. FLIGHT ATTENDANT REPORTED THAT THE ODOR WAS WORSE AT HIGHER POWER SETTING (CLIMB). RAN BOTH ENGINES WITH AND WITHOUT PACKS AT TAKEOFF POWER. NO ABNORMAL ODORS NOTED AIRCRAFT OK FOR SERVICE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FILTER — DIRTY (CABIN)

EN ROUTE, ACRID FUMES NOTED IN FIGHT DECK AND CABIN. COMPLETED CHECKLIST. THE RIGHT RE-CIRCULATION FAN WAS OBSERVED TO BE OFF. DIVERTED MSY AND LANDED WITHOUT INCIDENT. CLEANED LOOSE DUST FROM RE-CIRCULATION FAN FILTER. REINSTALLED CANNON PLUG ON RE-CIRCULATION FAN. RESET CIRCUIT BREAKERS. PERFORMED RE-CIRCULATION TEST AS REQUIRED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LINE — BROKEN (PRESSURE LINE)

ENROUTE, CUN-JFK ON DEPARTURE, LEFT HYDRAULIC SYSTEM QUANTITY LOSS. RETURNED AIRCRAFT TO CUN AND LANDED WITHOUT INCIDENT. REPLACED RIGHT GEAR MAIN DOOR SEQUENCE VALVE PRESSURE LINE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SIGNS AT MAIN ENTRY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGNS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (ROW 36)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT ROW 36 INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT ROW 36. SYSTEM GROUND CHECK NORMAL OPERATION.. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS NEAR AFT LAVATORY INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP NEAR AFT LAVATORY. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: FLOOR BEAM — CORRODED (BS 1640)

AFW - AFTER REMOVING CORROSION, THE MATERIAL REMAINING IS BEYOND SRM LIMITS. REPAIRED PER MRB 757-931. (M)

Part: FRAME — CORRODED (BS 1480)

AFW - FOUND AFTER REMOVING CORROSION FROM FRAME THE REMAINING MATERIAL IS BEYOND SRM LIMITS. REPAIRED PER MRB 757-934. (M)

Part: FRAME — CORRODED (BS 1645)

AFW - AFTER REMOVING CORROSION THE REMAINING MATERIAL IS BEYOND SRM LIMITS. REPAIRED PER MRB 757-933. (M)

Part: FLOOR — CORRODED (BS 417)

AFW - AFTER REMOVING CORROSION, FOUND REMAINING MATERIAL IS BEYOND SRM LIMITS. REPAIRED PER MRB 757-929. (M)

Part: DOOR PAN — GOUGED (L4 DOOR)

AFW - FOUND GOUGE AT DOOR PAN IS BEYOND SRM LIMITS. REPAIRED PER MRB 757-935. (M)

Part: RIB — CORRODED (LT WING)

AFW - FOUND AFTER REMOVING CORROSION THE REMAINING MATERIAL IS BEYOND SRM LIMITS. REPAIRED PER MRB 757-932. (M)

Part: FLOOR BEAM — CORRODED (BS 324)

AFW - AFTER REMOVING CORROSION, FOUND THE REMAINING MATERIAL IS BEYOND SRM LIMITS. REPAIRED PER MRB 757-928. (M)

Part: FLOOR BEAM — CORRODED (BS 365)

AFW - FOUND AFTER REMOVING CORROSION, REMAINING METAL THICKNESS IS BEYOND SRM LIMITS. REPAIRED PER MRB 757-927. (M)

Part: FLOOR — CORRODED (BS 300)

AFW - FOUND AFTER REMOVING CORROSION, THE REMAINING MATERIAL IS BEYOND SRM LIMITS. REPAIRED PER MRB 757-930. (M)

Part: FLOOR BEAM — CORRODED (BS 377)

AFW - FOUND AFTER BLENDING CORROSION, REMAINING METAL BEYOND SRM LIMITS. REPAIRED PER MRB 757-926. (M)

Part: EEL CONNECTOR — BROKEN (CABIN)

BWI - FLT NR 2030 - DURING OVERNIGHT CHECK, EMEREGNCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 2 THROUGH 17 INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR BY PASSENGER SEAT ROW 2. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)