N633AA

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,549 hrs · 26,275 cycles

FOUND EMER LIGHT AT SEAT 34 & 35 ABC INOPERATIVE. R & R LAMP AT SEAT 34 & 35 ABC. SYS CHECKED NORMAL.

Part: CONTROL MODULE — DEFECTIVE (CABIN) · airframe 73,549 hrs · 26,275 cycles

SEAT MOUNTED EMER LIGHTS FROM ROW 16 THRU ROW 25 INOPERATIVE. R & R CONTROL MODULE AT SEAT 16 IAW AMM 33-51-00. SYS CHECKED NORMAL.

Part: BATTERY PACK — DEFECTIVE (CABIN) · airframe 73,549 hrs · 26,275 cycles

FIRST CLASS EMER LIGHTS WILL NOT SHUTOFF. R & R EMER LIGHT POWER SUPPLY & BATTERY AT LOCATION M10799 IAW AMM 33-51-07. PERFORMED OPERATIONAL CHECK IAW AMM 33-51-00-715-039. SYS CHECKED NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 73,549 hrs · 26,275 cycles

SEAT MOUNTED EMER LIGHT AT 12D INOPERATIVE. FOUND LOOSE CONNECTOR, RECONNECTED & SECURED PLUG. SYS CHECKED NORMAL.

Part: CONTROL MODULE — FAULTY (CABIN) · airframe 73,415 hrs · 26,221 cycles

FIRST CLASS EMER LIGHTS TURN ON WHEN POWER IS TURNED OFF. R & R AISLE PATH LIGHTING CONTROL MODULE IAW MM 33-51-07. SYS CHECKED NORMAL.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 73,415 hrs · 26,221 cycles

FIRST CLASS EMER LIGHTS TURN ON WHEN POWER IS TURNED OFF. R & R BATTERY PACK & POWER SUPPLY IAW AMM 33-51-07.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,400 hrs · 26,215 cycles

L1 DOOR LOWER SIDEWALL EXIT LIGHTS INOPERATIVE LT & RT SIDE. R & R BATTERY PACK IAW MM 33-51-00. SYS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,400 hrs · 26,215 cycles

EXIT LIGHT IN AISLE LOWER BULKHEAD BY FIRST CLASS INOPERATIVE. R & R BATTERY PACK IAW MM 33-51-00. SYS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,400 hrs · 26,215 cycles

R1 DOOR LOWER SIDEWALL EXIT LIGHTS INOPERATIVE LT & RT SIDE. R & R BATTERY PACK IAW MM 33-51-00. SYS CHECKED NORMAL.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 71,864 hrs · 25,635 cycles

EMERGENCY EXIT LIGHT AT SEAT 36D INOPERATIVE. SECURED CONNECTOR & REPLACED LAMP FOR SEAT 36D EMERGENCY EXIT LIGHT. OPS CHECKED NORMAL.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 71,864 hrs · 25,635 cycles

EMERGENCY EXIT LIGHT AT SEAT 28D INOPERATIVE. SECURED CONNECTOR & REPLACED LAMP FOR SEAT 28D EMERGENCY LIGHT. OPS CHECKED NORMAL.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 71,864 hrs · 25,635 cycles

EMERGENCY EXIT LIGHT AT SEAT 34D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 34D. OPS CHECKED NORMAL.

Part: WEDGE — DAMAGED (LE SLAT) · airframe 70,265 hrs · 25,070 cycles

HOLE ON LOWER SURFACE OF WEDGE 34 INCHES FROM INBD. ACCOMPLISHED HOT BOND REPAIR.

Part: SPRING — MISSING (LT MLG UPLOCK) · airframe 70,067 hrs · 24,996 cycles

DFW CREW REPORTED AMBER GEAR LIGHT REMAINED ILLUMINATED & WAS ACCOMPANIED BY GEAR DISAGREE MESSAGE. EMERGENCY DECLARED FLIGHT RETURN DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. LT MLG UPLOCK ASSEMBLY FORWARD SPRING WAS MISSING. REPLACED UPLOCK SPRING FOR LT MLG & CONTROL LEVER MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,015 hrs · 24,974 cycles

AFT CARGO DOOR ESCAPE PATH LIGHT INOPERATIVE. REPLACED LAMP FOR AFT CARGO DOOR ESCAPE PATH LIGHT. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,015 hrs · 24,974 cycles

MID LAVATORY FLOOR ESCAPE PATH LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR MID LAVATORY FLOOR ESCAPE PATH LIGHT. OPERATIONS CHECKED NORMAL.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,386 hrs · 24,039 cycles

CORROSION ON THE FLOORBEAM AT 1660, RIGHT BUTTLINE. ACCOMPLISHED SPLICE REPAIR PER DRAWING LOR 53005, REPAIR 3 AND EA B757-53-024612.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,386 hrs · 24,039 cycles

CORRODED T-CAP AT STATION 1640 LEFT BUTTLINE 5 TO RIGHT BUTTLINE 4. REPLACED T-CAP PER SRM 53-00-51-2R-3.

Part: SKIN — DAMAGED (TE FLAP) · airframe 67,386 hrs · 24,039 cycles

LEFT OUTBOARD AFT FLAP LOWER SKIN TRAILING EDGE WEDGE HAS DELAMINATED DENT APPROXIMATELY 2 INCHES IN DIAMETER, 21 INCHES FROM OUTBOARD END OF FLAP AND 4.5 INCHES FROM TRAILING EDGE. REMOVED DELAMINATED SKIN AND CORE TO 0.5 DEPTH. BONDED IN NEW CORE PLUG. HOT BONDED GRAPHITE PRE-PREG LAY-UP PERMANENT REPAIR OVER CORE PLUG PER SRM 51-70-04-0G.

Part: SKIN — DAMAGED (TE FLAP) · airframe 67,386 hrs · 24,039 cycles

LEFT OUTBOARD AFT FLAP BOTTOM SIDE HAS AREA DELAMINATION JUST AFT OF THIRD TRACK FROM INBOARD END. REMOVED DELAMINATED SKIN AND CORE TO 0.5 DEPTH. BONDED IN NEW CORE PLUG. HOT BONDED GRAPHITE PRE-PREG LAY-UP PERMANENT REPAIR OVER CORE PLUG PER SRM 51-70-04-0G.

Part: TURBINE — DAMAGED (RT ENGINE) · airframe 66,137 hrs · 23,575 cycles

MIA - CREW REPORTED HIGH RIGHT ENGINE VIBRATION AT 32000 FEET AND HIGH EXHAUST GAS TEMPERATURE. PRECAUTIONARY ENGINE SHUT DOWN (SINGLE ENGINE TIME 25 MINS). FOUND PIECES OF LOW PRESSURE TURBINE BLADES IN THE TAIL PIPE. REPLACED RIGHT ENGINE ON 01/07/2012 AT MIA. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LENS — BROKEN (CABIN) · airframe 64,522 hrs · 22,968 cycles

RIGHT NUMBER 4 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REPLACED LENS FOR RIGHT NUMBER 4 DOOR EMERGENCY EXIT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,147 hrs · 22,834 cycles

FORWARD EXIT EMERGENCY LIGHT OVER LEFT WING IS INOPERATIVE. REPLACED LAMP FOR FORWARD EXIT EMERGENCY LIGHT OVER LEFT WING. OPS CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,147 hrs · 22,834 cycles

LEFT FORWARD OVERWING EMERGENCY EXIT AFT EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT FORWARD OVERWING EMERGENCY EXIT AFT EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,222 hrs · 22,511 cycles

BULL NOSE LIGHT AT ROW 25D INOPERATIVE. REPLACED LAMP FOR BULLNOSE LIGHT AT ROW 25D. OPS CHECK NORMAL.

Part: PLACARD — DAMAGED (CABIN) · airframe 63,222 hrs · 22,511 cycles

RIGHT FORWARD OVERWING EXIT MARKER DECAL DAMAGED. REPLACED DECAL. OPS CHECK NORMAL.

Part: PLACARD — DAMAGED (CABIN) · airframe 63,222 hrs · 22,511 cycles

LEFT FORWARD OVERWING EXIT DECAL DAMAGED. REPLACED DECAL. OPS CHECK NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 63,222 hrs · 22,511 cycles

SEAT MOUNTED EMERGENCY LIGHTS DIM SEAT ROW 15. REPLACED BATTERY AND CHARGER FOR SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROW 15. OPS CHECK NORMAL.

Part: PLACARD — DAMAGED (CABIN) · airframe 63,222 hrs · 22,511 cycles

LEFT AFT OVERWING EXIT DECAL DAMAGED. REPLACED DECAL. OPS CHECK NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 63,222 hrs · 22,511 cycles

FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY AND CHARGER FOR FIRST CLASS LIGHTS. OPS CHECK NORMAL.

Part: PLACARD — DAMAGED (CABIN) · airframe 63,222 hrs · 22,511 cycles

RIGHT AFT OVERWING EXIT MARKER DECAL DAMAGED. REPLACED DECAL. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,862 hrs · 22,392 cycles

CENTER RIGHT EMERGENCY EXIT DOOR LIGHT INOPERATIVE. REPLACED LAMP FOR CENTER RIGHT EMERGENCY EXIT DOOR. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,862 hrs · 22,392 cycles

AFT LEFT EMERGENCY EXIT DOOR LIGHT INOPERATIVE. REPLACED AFT LEFT EMERGENCY EXIT DOOR LIGHT ASSEMBLY. OPS CHECK NORMAL.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 62,229 hrs · 22,158 cycles

EMERGENCY LIGHTS AT SEAT ROW 10 DEF DO NOT LIGHT UP. FOUND A BROKEN WIRE IAW MCM CARD 2800. REPLACED EMERGENCY LIGHT HARNESS AT THE END OF SEAT 10 DEF AND PERFORMED OPS CHECK. OPS CHECK NORMAL.

Part: GOVERNOR — FAULTY (LT ENGINE) · airframe 61,552 hrs · 21,929 cycles

DFW - CREW REPORTED ON DESCENT LEFT ENGINE STUCK IN IDLE. EMERGENCY DECLARED LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE FUEL FLOW GOVERNOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: OVEN — MALFUNCTIONED (GALLEY) · airframe 60,859 hrs · 21,680 cycles

EWR - FLIGHT ATTENDANT REPORTED SMOKE COMING FROM FIRST CLASS GALLEY OVEN. OVEN WAS TURNED OFF AND SMOKE DISSIPATED. FLIGHT LANDED EWR WITHOUT INCIDENT. REPLACED FIRST CLASS OVEN. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: COMPUTER — FAILED (EICAS) · airframe 60,380 hrs · 21,510 cycles

MIA - CREW REPORTED UPPER EICAS SCREEN FAILED DURING CLIMB. FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. FOUND BURNT PIN ON UPPER EICAS DISPLAY SCREEN JACK. REPLACED LEFT EICAS COMPUTER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,206 hrs · 21,088 cycles

SEAT 17-24 RIGHT SIDE EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK ABOVE SEAT 20 HJ. ALL CHECKS NORMAL.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,865 hrs · 20,971 cycles

WEB CORRODED UNDER FLOOR AFT CARGO. REPAIRED IAW SRM 53-60-04-2R.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,865 hrs · 20,971 cycles

WEB CORRODED UNDER FLOOR OF AFT CARGO. REPAIRED IAW SRM 53-60-04-2R.

Part: PAN — WORN (L1 DOOR) · airframe 58,865 hrs · 20,971 cycles

TUL - LEFT NUMBER ONE DOOR HAS WEAR AREA 6 O`CLOCK POSITION CENTER OF PAN. REMOVED AND REPLACED PAN PER ESO90283.

Part: PAN — GOUGED (R1 DOOR) · airframe 58,865 hrs · 20,971 cycles

TUL - RIGHT NUMBER ONE DOOR HANDLE PAN IS GOUGED. REMOVED AND REPLACED HANDLE PAN UNDER ESO-90284.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 58,711 hrs

DFW - EXIT IDENTIFIER SIGNS AT LEFT NUMBER 2 AND RIGHT NUMBER 2 DOOR WILL NOT ILLUMINATE. REPLACED CHARGER FOR EXIT IDENTIFIER SIGNS AT LEFT NUMBER 2 AND RIGHT NUMBER 2 DOOR.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,711 hrs

DFW - EXIT IDENTIFIER SIGNS AT LEFT NUMBER 2 AND RIGHT NUMBER 2 DOOR WILL NOT ILLUMINATE. REPLACED BATTERY PACK FOR EXIT IDENTIFIER SIGNS AT LEFT NUMBER 2 AND RIGHT NUMBER 2 DOOR.

Part: LIGHT — BROKEN (CABIN) · airframe 57,983 hrs

SFO - MID EMERGENCY EXIT DOOR FORWARD LIGHT INOPERATIVE. REPLACED FORWARD LIGHT ASSEMBLY AT MID CABIN EXIT DOOR.

Part: WIRE HARNESS — UNSECURE (EMERGENCY LIGHTS) · airframe 57,983 hrs

SFO - EMERGENCY LIGHTS AT SEAT 14 AND SEAT 15 INOPERATIVE. RESECURED EMERGENCY LIGHT HARNESS AT SEAT 14 AND 15.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 57,228 hrs · 20,404 cycles

FLOORBEAM CORRODED, REPAIRED FLOORBEAM IAW SRM 53-0-51-2R3.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 57,228 hrs · 20,404 cycles

INTERCOSTAL CORRODED, REPAIRED INTERCOSTAL IAW SRM 51-40-02.

Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 57,228 hrs · 20,404 cycles

AFT MAIN DECK PLATE CORRODED, REPAIRED AFT DECK PLATE IAW SRM 53-60-51-2R2 AND EA B757-53-00-4996.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 57,228 hrs · 20,404 cycles

CORROSION ON FORWARD EDGE AND BETWEEN TEE CAP OF BEAM, REPAIRED FLOORBEAM TEE CAP IAW SRM 53-60-51-2R2 AND AARD 53-60-51-5

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 54,848 hrs

MIA - EMERGENCY LIGHT AT SEAT 15D INOPERATIVE. RESECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 15D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,708 hrs

DFW - EMERGENCY LIGHT FOR L1 SLIDE INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT L1 SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,708 hrs

DFW - EMERGENCY LIGHT AT SEAT 13D INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 13D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — BROKEN (CABIN)

MIA - EMERGENCY LIGHT AT SEAT 18D AFT IS BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 18D AFT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SLIDE — INOPERATIVE (L1 DOOR)

MIA - LEFT NUMBER ONE DOOR SLIDE FELL OUT OF HOUSING WHEN DOOR OPENED. UNSUCCESSFUL DEPLOYMENT. FOUND DEBRIS AT GIRT BAR. CLEARED DEBRIS FROM GIRT BAR AREA AND REINSTALLED LEFT NUMBER ONE DOOR SLIDE AND POWER ASSIST BOTTLE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

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

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT ON AFT CARGO DOOR INOPERATIVE. REPLACED LIGHT BULB FOR INOPERATIVE EMERGENCY LIGHT ON AFT CARGO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT 13D INOPERATIVE. REPLACED WIRE HARNESS CONNECTOR AND PINS AT SEAT 13D FOR EMERGENCY ESCAPE PATH LIGHT AND SEAT 13D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PUMP — INOPERATIVE (FUEL SYSTEM)

MIA - AFTER APPROXIMATELY ONE HOUR AT 35000 CRUISE ALL INDICATIONS NORMAL. BEGAN CLIMB TO FINAL CRUISE ALTITUDE OF 37000. RIGHT FUEL FLOW ON 2.2 LEFT 5.1. UNABLE TO MAINTAIN ALTITUDE. DESCENDED TO FLIGHT LEVEL 250 AND FUEL FLOWS MATCH. 4.8 AND 4.8 AT 320 KNOTS. LANDED MIA WITHOUT INCIDENT. REPLACED RIGHT ENGINE FUEL GOVERNOR AND FUEL PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHT AT ROW 26 RIGHT SIDE INOPERATIVE. SECURED PLUG FOR EMERGENCY LIGHTS AT ROW 26 RIGHT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT)

MIA - SEAT MOUNTED EMERGENCY EXIT LIGHT AT 31DEF INOPERATIVE. FOUND SEAT TO SIDEWALL CONNECTOR DISCONNECTED. RECONNECTED CONNECTOR FOR SEAT MOUNTED EMERGENCY EXIT LIGHT AT 31DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (CABIN)

MIA SEAT MOUNTED PATH LIGHT AT SEATS 13DEF INOPERATIVE. RESECURED LOOSE CONNECTOR FOR SEAT MOUNTED PATH LIGHT AT SEATS 13DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED

Part: SHUTOFF VALVE — DEFECTIVE (ANTI SKID SYS)

AFTER TAKEOFF, RIGHT HYDRAULIC SYSTEM BEGAN LOOSING QUANTITY. AIRCRAFT RETURNED TO SJU WITHOUT FURTHER INCIDENT. REPLACED BOTH ANTI-SKID SHUTOFF VALVES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: ODOR — DETECTED (CABIN)

CREW OBSERVED BURNED PLASTIC ODOR IN CABIN. EMERGENCY DECLARED AND RETURNED TO PIT WITHOUT FURTHER INCIDENT. GROUND RAN AIRCRAFT WITH BOTH AIR CONDITIONING PACKS ON HIGH. INSPECTED E/E BAY, CARGO BAYS, AFT ACCESSORY COMPARTMENT, AND BOTH MAIN LANDING GEAR BAYS. CHECKED CABIN LIGHTS BALLASTS. CHECKED LAVATORIES AND TRASH BINS. UNABLE TO DUPLICATE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: HYDRAULIC LINE — LEAKING (HYD SYSTEM)

DFW - FLT 742 - EN ROUTE DFW-LGA, LEFT HYDRAULIC QUANTITY LOW CAUTION FOLLOWED BY LEFT HYDRAULIC PRESSURE FAILURE. RETURNED AND LANDED DFW WITHOUT INCIDENT. FOUND LEFT MAIN GEAR DOWN LOCK FLEX LINE LEAKING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (SEAT 13)

DFW - DURNIG OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHT AT SEAT 13 INOPERATIVE. SECURED LOOSE CONNECTOR AT SEAT 13. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: SKIN — WORN (BS 1862)

AFW - LEFT SIDE FUSELAGE SKIN AT STATION 1862 HAS SMALL AREA OF WEAR BEYOND SRM LIMITS. BLENDED SHARP EDGES, PERFORMED DYE PENETRANT INSPECTION FOR CRACKS, NONE FOUND. REPLACED ONE FASTENER IAW MRB 1511. (M)

Part: SPAR — DISBONDED (RUDDER)

AFW - RUDDER FRON SPAR SKIN SHOWS DISBOND INDICATIONS AT STATION 226.5-228. CUTOUT DELAMINATION. PUT DRY CYCLE AND CUTOUT REPAIR PLYS, LAYUP AND COOK. TOP CHECK OK. (M)

Part: SILL — CORRODED (BS 1383)

AFW - LOWER SILL INNER CHORD HAS CORROSION BLENDED BEYOND SRM LIMITS. REPAIRED BLENDED AREA WITH STRAP PER MRB 757-1509, TREATED AND PRIMED. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS DISLODGED. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AND BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: AIR DISTR — ODOR (CABIN)

DFW - FLT 458 - AFTER TAKEOFF DFW DURING CLIMB-OUT, FLIGHT ATTENDANT REPORTED HOT SMELL AND SMOKE IN CABIN. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. CHECKED CABIN AND CARGO COMPARTMENTS, RECIRCULATION FANS AND EQUIPMENT COOLING FANS WITH NO ODOR OR DEFECTS NOTED. SUSPECTED CAUSE WAS NORMAL CYCLING OF PACK ANTI-ICE SYSTEM. PRECAUTIONARY ACCOMPLISHED PACK BURNOUT PROCEDURE. SYSTEMS GROUND CHECKED NORMAL OPERATION WITH NO HOT SMELL OR SMOKE NOTED. (M)

Part: WIRE — LOOSE (CABIN)

DFW - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS AT STATION 880L INOPERATIVE. REPAIRED GROUND WIRE, SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLOOR BEAM — CORRODED (BS 324)

AFW - FLOOR BEAM HAD CORROSION BLENDED BEYOND SRM LIMITS AT STATION 324 RBL 60, PER MRB 757-608. (M)

Part: FLOOR BEAM — CORRODED (BS 1640)

AFW - FLOOR BEAM HAD CORROSION BLENDED BEYOND SRM LIMITS, STATION 1640 RBL 54, LBL 54, PER MRB 757-607. (M)

Part: PLATE — CORRODED (DECK)

AFW - CORROSION BLENDED BEYOND SRM LIMITS IN SEVERAL AREAS OF THE DECK PLATE, PER MRB 757-611. (M)

Part: FLOOR BEAM — CORRODED (BS 365)

AFW - FLOOR BEAM HAD CORROSION BLENDED BEYOND SRM LIMITS AT STATION 365, LBL 10, RBL 14 AND RBL 61, PER MRB 757-610. (M)

Part: SKIN — DENTED (HORIZ STAB)

AFW - RIGHT HORIZ SKIN PANEL HAS DENT ON LOWER SURFACE (HONEYCOMB PANEL), PER MRB 757-616. (M)

Part: EEL WIRE — BROKEN (CABIN)

DFW - DURING OVERNIGHT CHECK, FOUND L3 DOOR EMERGENCY EXIT IDENTIFIER MARKER INOPERATIVE. REPAIRED BROKEN WIRE ON EMERGENCY EXIT IDENTIFIER MARKER. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: TRANSDUCER — DEFECTIVE (NR 1 ENGINE)

DFW - FLT 1366 - DESCENT THROUGH 26,000 FEET, A FUEL SMELL WAS NOTICED IN COCKPIT AND CABIN. ON LEVEL OFF AT 24,000 FEET, NR 1 ENGINE APPEARED TO HAVE FLAMED OUT. DID ENGINE SHUT DOWN PROCEDURE FOLLOWED BY IN-FLIGHT RE-START PER QRH PROCEDURES. ENGINE OPERATED NORMALLY FOR REST OF FLIGHT. LANDED DFW WITHOUT INCIDENT. REPLACED THROTTLE ANGLE TRANSDUCER. REMOVED AND REPLACED BLEED VALVE CONTROL UNIT. ALL TESTS COMPLETED SATISFACTORILY. ENGINE RUN ACCOMPLISHED. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)