N623AA

Part: RADIO ALTIMETER — MALFUNCTIONED (COCKPIT) · airframe 72,605 hrs · 25,810 cycles

MIA CREW REPORTED SMOKE IN THE CABIN DURING DESCENT. EMERGENCY DECLARED FLIGHT LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND CAPTAINS RADIO ALTIMETER PRODUCING THE SMOKE. REPLACED LT RADIO ALTIMETER, SYSTEM GND CHECKED NORMAL OPERATION CLOSED.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 3 · airframe 70,079 hrs · 24,900 cycles

CORROSION FROM STATIONS 1697 TO 1701 STRINGER 24 LEFT. INSTALLED A NEW STRINGER AND SPLICE IN THE AFT CARGO AREA PER SRM 53-60-03 AND EA B757-53-029491.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 70,079 hrs · 24,900 cycles

RIGHT TRANSITION PANEL - 4 ATTACH HOLES IN SILL CHORD ANGLE (STRINGER 27R AT STATION 1440) DAMAGED. REPAIRED HOLES PER EA B757-53-029513 DATED.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 69,004 hrs · 24,483 cycles

EMERGENCY EXIT LIGHTS FROM ROW 27 AFT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AND CHARGER. OPS CHECK NORMAL.

Part: MODULE — INOPERATIVE (CABIN) · airframe 68,290 hrs · 24,220 cycles

EMERGENCY LIGHTS FROM SEATS 26D TO 36D AND LEFT AND RIGHT AFT DOOR EXIT SIGNS INOPERATIVE. REPLACED MODULE AND BATTERY AT M10801, OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,290 hrs · 24,220 cycles

AFT CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR AFT CABIN EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: SWITCH — INTERMITTENT (CABIN) · airframe 68,290 hrs · 24,220 cycles

EMERGENCY TEST SWITCH AT LEFT NUMBER 1 FLIGHT ATTENDANT PANEL INTERMITTANT. REPLACED EMERGENCY TEST SWITCH AT LEFT NUMBER 1 FLIGHT ATTENDANT PANEL. OPS CHECK NORMAL.

Part: MODULE — INOPERATIVE (CABIN) · airframe 68,290 hrs · 24,220 cycles

SEAT MOUNTED EMERGENCY EXIT LIGHTS FROM SEAT ROWS 26 AND AFT WILL NOT TURN OFF. REPLACED MODULE AT M10801. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,290 hrs · 24,220 cycles

EXTERIOR RIGHT NUMBER 4 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LAMP FOR EXTERIOR RIGHT NUMBER 4 DOOR EMERGENCY EXIT LIGHT. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,290 hrs · 24,220 cycles

MID CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR MID CABIN EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 68,290 hrs · 24,220 cycles

EXTERIOR LEFT NUMBER 2 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LAMP FOR EXTERIOR LEFT NUMBER 2 DOOR EMERGENCY EXIT LIGHT. OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 68,290 hrs · 24,220 cycles

SEAT 26D TO 36D EMERGENCY LIGHTS AND AFT DOOR EXIT SIGN INOPERATIVE. REPLACED BATTERY AND CHARGER 0736 AND 0737 IN AFT GALLEY, OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 67,333 hrs · 23,884 cycles

EMERGENCY LIGHT AT AFT RIGHT SERVICE DOOR (OUTSIDE FUSELAGE) DID NOT COME ON WHEN TESTED. REPLACED LIGHT BULB. OPS CHECK NORMAL.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 66,798 hrs · 23,674 cycles

AFT GALLEY DECK PLATE DOUBLER DAMAGED. REPAIRED DECK PLATE BY REPLACING DOUBLER PER SRM 53-60-51-2. REPAIR 2 AND EA B757-53-0020036.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,798 hrs · 23,674 cycles

REMOVED RE-ENFORCING ANGLES FROM FORWARD SIDE OF LATERAL I BEAM/FLOOR SUPPORT TO FACILITATE CORROSION REMOVAL, STATION 1680, WATERLINES 206 TO 207.8. REINFORCED LATERAL I BEAM/FLOOR SUPPORT BY INSTALLING NEW REINFORCING ANGLES ON THE FORWARD SIDE OF I BEAM PER SRM 53-00-51-2, REPAIR 2.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 66,798 hrs · 23,674 cycles

CRACKED FLOORBEAM AT STATION 700 LEFT BUTTLINES 24 TO 48. INSTALLED DOUBLER PER SRM 53-00-51-2R.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,798 hrs · 23,674 cycles

HAT SECTION FLOORBOARD SUPPORT CORRODED AT BUTTLINE 0, STATIONS 1660 TO 1680. INSTALLED NEW FLOORBOARD SUPPORT PER SRM 51-10-02-0G.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,798 hrs · 23,674 cycles

CENTER HAT SECTION FLOORBOARD SUPPORT IS CORRODED AT STATIONS 1640 TO 1660 BUTTLINE 0. REMOVED AND REPLACED SECTION OF FLOOR SUPPORT PER SRM 51-10-02-0G.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,798 hrs · 23,674 cycles

STATION 1640 UPPER FLOORBEAM REPAIR UPPER DOUBLER AND FRAME CORRODED LEFT BUTTLINE 6 TO RIGHT BUTTLINE 12. REPAIRED LATERAL I BEAM/FLOOR SUPPORT BY INSTALLING T CAP REPAIR PER SRM 53-00-51-2, REPAIR 3.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,798 hrs · 23,674 cycles

CORROSION ON FLOORBEAM FROM RIGHT BUTTLINES 12 TO 56 AT STATION 1680. ACCOMPLISHED NESTED ANGLE REPAIR PER SRM 53-00-51-2, REPAIR 2.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,798 hrs · 23,674 cycles

AFT GALLEY DECK PLATE "CENTER HAT SECTION" SUPPORT IS CORRODED AT BUTTLINE 0, STATIONS 1685 TO 1715. INSTALLED NEW CENTER HAT SECTION AR BUTTLINE 0 STATIONS 1685 TO 1715 PER SRM 51-10-02-G9.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,798 hrs · 23,674 cycles

Z-ANGLE IS CORRODED AT BOTH ENDS ON THE AFT GALLEY DECK PLATE LEFT BUTTLINE 50 STATIONS 1680 TO 1715. REPLACED Z-ANGLE PER SRM 51-10-02-0G.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,798 hrs · 23,674 cycles

Z-ANGLE SUPPORT CORRODED AT STATIONS 1680, RIGHT BUTTLINE 50. REPLACED Z-ANGLE PER SRM 51-10-02-0G, PARAGRAPH 9.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 66,798 hrs · 23,674 cycles

NUMBER 9 SLAT HAS CORROSION ALONG BLEND, UPPER SKIN SURFACE ABOVE INBOARD SLAT TRACK. REPAIRED PER AARD 57-43-00-1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,798 hrs · 23,674 cycles

CORROSION ON FLOORBEAM AT STATION 365 RIGHT BUTTLINES 0 TO 64. REPAIRED FLOORBEAM PER SRM 53-00-51-2R-5.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,798 hrs · 23,674 cycles

LEFT NUMBER 4 DOOR GUTTER BOX DRAIN SUPPORT CORRODED. REPLACED LEFT NUMBER 4 GUTTER BOX DRAIN SUPPORT PER SRM 51-10-02-0G.

Part: SHUTOFF VALVE — FAULTY (BLEED AIR SYS) · airframe 64,534 hrs · 22,838 cycles

LAX - CREW REPORTED LEFT ENGINE HIGH STAGE LIGHT ILLUMINATED DURING FLIGHT. EMERGENCY DECLARED FLIGHT RETURNED LAX LANDED WITHOUT INCIDENT. PLACARD LEFT ENGINE HIGH PRESSURE SHUT-OFF VALVE PER MEL 36-2. REPLACED VALVE AT LAX ON 02/08/2011. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: COMPUTER — FAILED (COCKPIT) · airframe 62,657 hrs · 22,176 cycles

LGA - ON FINAL APPROACH CREW REPORTED TRAILING EDGE LIGHT ILLUMINATED, FLAP DISAGREE ON EICAS. FOLLOWED PROCEDURES AND CHECKLIST AND LANDED WITH NORMAL FLAPS 30 DEGREES. CYCLED FLAP/SLATS WITH BOTH HYDRAULICS AND ELECTRICAL. VERIFIED FLAP OVERLOAD INDICATORS NOT POPPED. REPLACED RIGHT FLIGHT CONTROL COMPUTER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SLIDE — DISLODGED (L3 DOOR) · airframe 61,434 hrs · 21,743 cycles

LEFT NUMBER 3 DOOR SLIDE WAS DISLODGED. SLIDE DEPLOYMENT WAS UNSUCCESSFUL. REPLACED LEFT NUMBER 3 DOOR SLIDE. OPS CHECK NORMAL.

Part: MODULE — INOPERATIVE (CABIN) · airframe 61,318 hrs · 21,705 cycles

EMERGENCY LIGHTS AT FORWARD FIRST CLASS ARE DIM. REPLACED MODULE AND BATTERY PACK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,961 hrs · 21,578 cycles

EMERGENCY LIGHT AT SEAT ROW 29 INOPERATIVE. REPLACED LIGHT ASSEMBLY.

Part: CONNECTOR — WORN (CABIN) · airframe 60,961 hrs · 21,578 cycles

SEAT 28 EGRESS LIGHT INOP. REPLACED WALL CONNECTOR AND REPAIRED LIGHT ASSY SOCKET. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,961 hrs · 21,578 cycles

EMERGENCY LIGHT AT SEAT ROW 22 INOPERATIVE. REPLACED LAMP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,055 hrs · 21,257 cycles

EMERGENCY LIGHT AT SEAT ROW 23D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT ROW 23D PER MM. OPS CHECK GOOD. OK FOR SERVICE.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 58,330 hrs

MIA EMERGENCY LIGHTS FROM ROW 17D TO 25D INOPERATIVE. RESECURED CONNECTOR FOR EMERGENCY LIGHTS FROM ROW 17D TO 25D.

Part: ACTUATOR — FAILED (T/E FLAP) · airframe 56,547 hrs

ORD INFLIGHT T1624/05MAY - CREW REPORTED LEADING EDGE SLAT ASYMMETRY AND LIGHT INDICATION. FLAP INDICATION STOPPED AT .05. TRAILING EDGE LIGHT ALSO ILLUMINATED. TRAILING EDGE FLAPS OPERATED WITH ALTERNATE SWITCH. LANDED ORD WITHOUT INCIDENT. FOUND NUMBER 12 RIGHT WING ROTARY ACTUATOR OVERLOADED. REPLACED NUMBER 12 ROTARY ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: TRANSMITTER — INOPERATIVE (L/E SLAT) · airframe 56,543 hrs

LAX INFLIGHT T1913/04MAY - CREW REPORTED LEADING EDGE SLAT DISAGREE INDICATION ON APPROACH. REPLACED LEADING EDGE DRIVE TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,508 hrs

DFW - EMERGENCY LIGHT EXIT MARKERS AT LEFT AND RIGHT NUMBER TWO DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT EXIT MARKERS AT LEFT AND RIGHT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,508 hrs

DFW EMERGENCY LIGHTS AT SEAT ROWS 26D TO 36D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 26D TO 36D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,508 hrs

DFW - SEAT EMERGENCY LIGHT EXIT MARKERS AT LEFT AND RIGHT NUMBER FOUR DOOR AND AFT GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT EXIT MARKERS AT LEFT AND RIGHT NUMBER FOUR DOOR AND AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 56,508 hrs

DFW - EMERGENCY LIGHTS AT SEAT ROWS 9D TO 16D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 9D TO 16D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,353 hrs

MIA - EMERGENCY LIGHT AT SEAT 22D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PRINTER — SMOKE (COCKPIT)

ORD INFLIGHT T844/30AUG - ACARS PRINTER STARTED SMOKING. PULLED PRINTER CIRCUIT BREAKERS ON OVERHEAD PANEL. OPENED PRINTER AND PAPER ROLL NOT BURNED. LANDED ORD WITHOUT INCIDENT. REPLACED ACARS PRINTER AND INSPECTED AREA. NO DAMAGE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHT AT OVERHEAD RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS)

MIA - EMERGENCY LIGHT AT SEAT 23D INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT 23D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

MIA - EMERGENCY LIGHT AT SEAT 13D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 13D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

MIA - EMERGENCY LIGHT AT SEAT 20D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 20D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: GEARBOX — FAILED (LT ENGINE)

ORD APPROXIMATELY 25 MINUTES OUT OF ORD LEFT ENGINE OIL QUANTITY BEGAN TO DECREASE. OIL QUANTITY WENT TO ZERO IN ABOUT THREE MINUTES. OIL PRESSURE SUBSEQUENTLY DECREASED TO ZERO. CREW SHUT LEFT ENGINE DOWN. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. SINGLE ENGINE TIME 20 MINUTES. REPLACED LEFT ENGINE ON 26 NOV 2006 AT ORD DUE TO GEARBOX FAILURE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ACTUATOR — INOPERATIVE (RUDDER TRIM)

MIA - INFLIGHT RUDDER TRIM INTERMITTANT. LANDED MIA WITHOUT INCIDENT. REPLACED RIGHT HAND RUDDER TRIM ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: COMPUTER — LOOSE (ADCS)

SFO - INFLIGHT T044 JUST PRIOR TO A/C ROTATION LOST BOTH AIRSPEED INDICATORS, BOTH ALTIMETERS, BOTH VSI, BOTH FDS, AUTOTHROTTLES, AUTO PRESS 1&2, BOTH EEC, RUDDER RATIO, MACH TRIM, TCAS, ALT REPORTING, AUDIO ALTS. UNABLE TO RESTORE ANY SYSTEM. AFTER LANDING ON ROLLOUT SYSTEMS RETURNED TO NORMAL. FOUND BOTH CADCS, SERIAL NUMBERS LEFT HAND 82080237 AND RIGHT HAND 01056148, NOT SECURED IN RESPECTIVE RACKS. REPLACED BOTH ADCS AS PRECAUTIONARY AND PERFORMED REQUIRED PITOT/STATIC CHECKS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SFO - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY LIGHTS AT ROWS 17 TO 23 INOPERATIVE. REMOVED AND REPLACED M10800 BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

BOS - MAINTENANCE OBSERVED SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE FROM ROWS 16 TO 23. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PCU — FAULTY (RUDDER)

DFW - FLT 1507 - EN ROUTE DFW-YVR - AFTER TAKEOFF, AIRCRAFT BEGAN A SEVERE FISHTAILING MOTION FOR ABOUT 30 SECONDS. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED ALL THREE RUDDER POWER CONTROL UNITS. SYSTEM GROUND AND FLIGHT CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DAMAGED (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY PATH LIGHTS FROM ROW 17 TO REAR OF AIRCRAFT INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

SJU - FLT 1894 - DURING FLIGHT, EMERGENCY EXIT PATH LIGHTS ILLUMINATED INTERMITTENTLY. RECONNECTED END CONNECTOR ON AFT FLOOR LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — DISCHARGED (CABIN)

BOS - FLT 148 - DURING FLIGHT, EMERGENCY EXIT LIGHTS BY 2L AND 2R INTERMITTENTLY ILLUMINATED. REPLACED MODULE AND BATTERY PACK FOR EMERGENCY EXIT LIGHTS AT 2R AND 2R DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: MODULE — DEFECTIVE (INSTRUMENT PANEL)

BWI - FLT 600 - DURING APPROACH TO BWI WHEN LANDING GEAR EXTENDED, LEFT MAIN LANDING GEAR GREEN LIGHT FAILED TO ILLUMINATE. RECYCLED LANDING GEAR WITH SAME RE SULTS. ACCOMPLISHED ABNORMAL PROCEDURE AND AIRCRAFT LANDED BWI WITHOUT INCIDENT. REPLACED LANDING GEAR LEVER MODULE AND LT MAIN LANDING GEAR ANNUNCIATOR LIGHT CAPSULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)