N607AM

Part: TRANSMISSION — MALFUNCTIONED (TE FLAP) · airframe 55,049 hrs · 18,780 cycles

MIA CREW REPORTED FLAP DISAGREE MESSAGE. EMERGENCY DECLARED FLIGHT LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED OTBD LT WING FLAP TRANSMISSION. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,311 hrs · 18,161 cycles

ROWS 17 THRU 25 SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. REPLACED THE BATTERY PACK. OPS CHECK NORMAL.

Part: INDICATOR — MALFUNCTIONED (COCKPIT) · airframe 52,559 hrs · 17,896 cycles

SEA - CREW REPORTED LEADING EDGE SLAT DISAGREE LIGHT. EMERGENCY DECLARED FLIGHT LANDED SEA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. RESET LEFT OUTBOARD OVERLOAD INDICATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: RADAR — FAILED (ZONE 100) · airframe 52,177 hrs · 17,771 cycles

MIA - CREW REPORTED WEATHER RADAR FAILED. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED WEATHER RADAR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN PANEL — DENTED (RT HORIZ STAB) · airframe 52,081 hrs · 17,736 cycles

NUMEROUS HAIL DENTS TO TOP OF RIGHT HORIZONTAL FORWARD PANELS. PERFORMED HIGH FREQUENCY EDDY CURRENT SURFACE SCAN ON EXTERNAL SKIN AT DENTS; NO CRACKS INDICATED. APPLIED STRUCTURAL ADHESIVE AS PER SRM 51-70-01, REPAIR 1, DENT FILL PROCEDURE AND EA B757-55-025759.

Part: SKIN PANEL — DENTED (LT HORIZ STAB) · airframe 52,081 hrs · 17,736 cycles

NUMEROUS HAIL DENTS ON TOP OF LEFT HORIZONTAL FORWARD OUTBOARD PANEL. PERFORMED HIGH FREQUENCY EDDY CURRENT SURFACE SCAN ON EXTERNAL SKIN AT DENTS, NO CRACKS INDICATED. APPLIED STRUCTURAL ADHESIVE PER 757 SRM 51-70-01, REPAIR 1, DENT FILL PROCEDURE AND EA B757-55-025757.

Part: SKIN PANEL — DENTED (LT HORIZ STAB) · airframe 52,081 hrs · 17,736 cycles

NUMEROUS HAIL DENTS TOP OF LEFT HORIZONTAL FORWARD PANELS. PERFORMED HIGH FREQUENCY EDDY CURRENT SURFACE SCAN ON EXTERNAL SKIN AT DENTS; NO CRACKS INDICATED. APPLIED STRUCTURAL ADHESIVE AS PER SRM 51-70-01, REPAIR 1, DENT FILL PROCEDURE AND EA B757-55-025756.

Part: STRUCTURE — CRACKED (R2 DOOR) · airframe 52,081 hrs · 17,736 cycles

RIGHT NUMBER 2 DOOR, UPPER HINGE CUTOUT IS CRACKED. INSTALLED DOUBLER REPAIR PER SRM 52-10-02-2R 1 AND EA COMP 52-025737.

Part: STRAP — CRACKED (FUSELAGE) · airframe 52,081 hrs · 17,736 cycles

TWO CRACKS IN STABILIZER STRAP AT FLOORBEAMS STATION 377.7 AND LEFT BUTTINE 24. ACCOMPLISHED NESTED ANGLE REPAIR PER SRM 53-10-51-2R 1.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 49,663 hrs · 16,841 cycles

ACCIDENTAL IMPACT AT FUSELAGE SKIN AT APPROXIMATE STATION 1545 AT STRINGER 22 RIGHT. INSTALLED EXTERNAL DOUBLER PER EA B757-53-020017.

Part: PAN — GOUGED (DOOR) · airframe 49,555 hrs · 16,807 cycles

HANDLE PAN GOUGED. INSTALLED NEW HANDLE PAN PER ESO 90284.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 49,210 hrs · 16,672 cycles

AIRCRAFT WAS DAMAGED BETWEEN STATIONS 1640 AND 1661 BELOW STRINGER 20 RIGHT. DAMAGED SKIN COMPLETELY TRIMMED OUT AND A LAP SKIN DOUBLER INSTALLED OVER TRIMMED OUT SECTION PER 757-200 SRM 53-00-01 FIGURE 201. REPAIRED PER 757 SRM 53-00-01 FIG 201 AND EA B757-53-018988.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,252 hrs · 16,348 cycles

CRACK AT STATION 1400 STRINGER 26 LEFT. ACCOMPLISHED DOUBLER REPAIR PER SRM 53-00-07-2R 5.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,252 hrs · 16,348 cycles

L-ANGLE SUPPORT CORRODED AT RIGHT NUMBER 4 DOOR. ACCOMPLISHED REPAIR PER SRM 51-10-02-G8.

Part: THRESHOLD — DAMAGED (FUSELAGE) · airframe 48,252 hrs · 16,348 cycles

RIGHT NUMBER 4 DOOR THRESHOLD WEB DAMAGED. INSTALLED SPLICE DOUBLER PER SRM 51-70-13-0G.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,252 hrs · 16,348 cycles

LEFT NUMBER 4 DOOR THRESHOLD DRAIN SUPPORT IS CORRODED 2 EACH. ACCOMPLISHED REPAIR PER SRM 51-10-02-0G.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,252 hrs · 16,348 cycles

CABIN FLOOR SUPPORT INBOARD OF THE RIGHT NUMBER 4 DOOR THRESHOLD IS CORRODED RIGHT BUTTLINE 55 BETWEEN STATIONS 1640 TO 1660. REPLACED SUPPORT PER SRM 51-10-02-0G.

Part: STRUCTURE — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,252 hrs · 16,348 cycles

AFT MAIN DECK STRUCTURE CORRODED. ACCOMPLISHED REPAIR PER SRM 53-60-51-2K-2.

Part: SUPPORT CHANNEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,252 hrs · 16,348 cycles

AFT MAIN DECK HAT CHANNEL CORRODED. ACCOMPLISHED REPAIR PER SRM 51-10-02-0G.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 48,252 hrs · 16,348 cycles

LEFT MAIN INBOARD TRAILING EDGE FOUND DELAMINATION ON TOP SKIN WEDGE APPROXIMATELY 29 INCHES FROM INBOARD END AND 27 INCHES AFT OF LEADING EDGE OF FLAP. REMOVED DELAMINATED AREA OF UPPER SKIN ON AFT WEDGE AND INSTALLED A PERMANENT REPAIR USING HOT-BONDED PRE-PREG FIBERGLASS PER SRM 57-53-01-2R FIGURE 201 AND SRM 51-70-07-0G.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,252 hrs · 16,348 cycles

CABIN FLOOR SUPPORT CORRODED STATIONS 1660 TO 1680 AND BUTTLINE 0. REPLACED SUPPORT PER SRM 51-10-02-0G.

Part: SUPPORT — CORRODED (R1 DOOR) · corrosion level 2 · airframe 48,252 hrs · 16,348 cycles

RIGHT NUMBER 1 DOOR DRAIN SUPPORT CORRODED. REPLACED SUPPORT PER SRM 51-10-02-0G.

Part: SUPPORT — CORRODED (R1 DOOR) · corrosion level 2 · airframe 48,252 hrs · 16,348 cycles

RIGHT NUMBER 1 DOOR FORWARD DRAIN SUPPORT CORRODED. REPLACED SUPPORT PER SRM 51-10-02-0G.

Part: WEDGE — DENTED (LE SLAT) · airframe 48,252 hrs · 16,348 cycles

NUMBER 6 SLAT HAS DENT ON WEDGE AREA APPROXIMATELY 5 INCHES LONG BY 1 INCH WIDE APPROXIMATELY 48 INCHES FROM OUTBOARD END AND 3 INCHES FROM SLAT SKIN. REMOVED DAMAGED AREA REMOVED CORE. INSTALLED NEW CORE AND EXTERNAL DOUBLER PER SRM 51-70-10-2R.

Part: PAN — DAMAGED (L2 DOOR) · airframe 48,252 hrs · 16,348 cycles

LEFT NUMBER 2 DOOR HANDLE PAN GOUGED. REPLACED PAN PER ESO 90282.

Part: COMPRESSOR — STALLED (RT ENGINE) · airframe 47,039 hrs · 15,899 cycles

MIA - CREW REPORTED RIGHT ENGINE COMPRESSOR STALLED ON CLIMB. RIGHT ENGINE SHUTDOWN FOR APPROXIMATELY 10 SECONDS THEN RE-STARTED AND SET AT IDLE FOR LANDING. EMERGENCY DECLARED RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED BOROSCOPE AND ENGINE CHANGE DECLARED. REPLACED RIGHT ENGINE AT MIA ON 11/04/2010. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: GUARD — BROKEN (CABIN) · airframe 46,379 hrs · 15,670 cycles

SEAT 29D ESCAPE PATH LIGHT GUARD BROKEN. REPLACED SEAT 29D ESCAPE PATH LIGHT GUARD. OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,379 hrs · 15,670 cycles

SEAT 17D AFT ESCAPE PATH LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT 17D AFT ESCAPE PATH LIGHT. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 45,867 hrs · 15,498 cycles

LEFT SIDE EMERGENCY LIGHTS AT RIGHT NUMBER 2 AND LEFT NUMBER 2 DOOR INOPERATIVE. REPLACED BATTERY PACK FOR LEFT SIDE EMERGENCY LIGHTS AT RIGHT NUMBER 2 AND LEFT NUMBER 2 DOOR. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 45,867 hrs · 15,498 cycles

EMERGENCY LIGHTS FROM ROWS 9 TO 15 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FROM ROWS 9 TO 15. OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,867 hrs · 15,498 cycles

EMERGENCY LIGHT AT 17DEF INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHTS AT 17DEF. OPS CHECKED NORMAL.

Part: SKIN — DENTED (LE SLAT) · airframe 45,433 hrs · 15,349 cycles

NUMBER 10 SLAT HAS DENT BELOW SRM LIMITS ABOUT 1.5 INCHES FROM OUTBOARD END ON LEADING EDGE. CUT OUT DAMAGED AREA AND FABRICATED DOUBLERS PER AARD 57-43-00-1.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,899 hrs · 15,149 cycles

EMERGENCY LIGHT EICAS MESSAGE AND EMERGENCY LIGHT SYSTEM ILLUMINATED IN AFT SECTION OF MAIN CABIN WITH EMERGENCY LIGHT SWITCH UNARMED. REPLACED BATTERY PACK POSITION M10801 RIGHT AFT CEILING PANEL. OPS CHECKED NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 44,899 hrs · 15,149 cycles

EMERGENCY LIGHT EICAS MESSAGE AND EMERGENCY LIGHT SYSTEM ILLUMINATED IN AFT SECTION OF MAIN CABIN WITH EMERGENCY LIGHT SWITCH UNARMED. REPLACED CHARGER POSITION M10801 RIGHT AFT CEILING PANEL. OPS CHECKED NORMAL.

Part: WIRE — SHORTED (CABIN) · airframe 44,744 hrs · 15,095 cycles

FOUND LIGHT ASSEMBLY WIRE CUT/SHORTED DUE TO UNKNOWN IMPACT WITH SEAT ASSEMBLY INBOARD PANEL. REPLACED 34DEF LIGHT ASSEMBLY. OPS CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,744 hrs · 15,095 cycles

FOUND LIGHT ASSEMBLY WIRE CUT/SHORTED DUE TO UNKNOWN IMPACT WITH SEAT ASSEMBLY INBOARD PANEL CAUSING DISCHARGE TO AFT BATTERY PACK. REPLACED AFT BATTERY PACK AND POWER SUPPLY. OPS CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,296 hrs · 14,945 cycles

EMERGENCY PROXIMITY LIGHTS AND LIGHTS AT LEFT AND RIGHT NUMBER FOUR DOOR INOPERATIVE. REPLACED BATTERY PACK.

Part: SKIN — CRACKED (RT WING) · airframe 43,604 hrs · 14,697 cycles

CRACK ON RIGHT WING INBOARD LEADING EDGE BULLNOSE SKIN. INSTALLED EXTERNAL DOUBLER REPAIR UNDER ESO 90309 AND SRM 57-41-01-2R.

Part: SKIN — CRACKED (LT WING) · airframe 43,604 hrs · 14,697 cycles

CRACK AT LEFT WING IN BULLNOSE SKIN OVER PYLON INBOARD BEND. REPLACED UNDER ESO 90309 AND AARD 51-00-00-1.

Part: SKIN — CRACKED (RT WING) · airframe 43,604 hrs · 14,697 cycles

CRACK FOUND IN RIGHT WING BULLNOSE SKIN OVER PYLON INBOARD BEND. REPLACED UNDER AARD 51-41-01-01 PG 1 AND SRM 57-41-01-01 PG 1, FIG 1.

Part: FSEU — FAILED (LE SLAT) · airframe 43,589 hrs · 14,691 cycles

LEADING EDGE SLATS DISAGREE EICAS MESSAGE WHEN SELECTED FLAPS 1 ON APPROACH. LANDED SEA WITHOUT INCIDENT. FOUND NUMBER 1 FLAP SLAT ELECTRONIC UNIT FAULTED. REPLACED NUMBER 1 FLAP SLAT ELECTRONIC UNIT.

Part: ENGINE — INOPERATIVE (NR 1) · airframe 41,841 hrs · 14,083 cycles

MIA - NUMBER ONE ENGINE OIL QUATITY AND PRESSURE WENT TO ZERO AND THE CREW SHUTDOWN THE ENGINE. SINGLE ENGINE TIME 10 MINUTES. EMERGENCY DECLARED, RETURNED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER 1 ENGINE ON MARCH 3,2009 AT MIA. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 40,870 hrs

MCO INFLIGHT - EMERGENCY FLOOR LIGHTING FLICKERED ON AND OFF DURING FLIGHT. REPLACED BATTERY PACK AT STATION 1095. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW EMERGENCY LIGHT AT RT FORWARD OVERWING INOPERATIVE. REPLACED EMERGENCY LAMP FOR EMERGENCY LIGHT AT RT FORWARD OVERWING. SYSTEM GROUND CHECKED NORMAL OPS.

Part: SLIDE — PARTIAL INFLATE (R4 DOOR)

MIA - RIGHT NR 4 DOOR SLIDE INADVERTENTLY UNSUCCESSFULLY DEPLOYED WHEN OPENED FROM THE INSIDE. SLIDE FELL OUT OF COVER BUT DID NOT INFLATE AND DOOR BOTTLE DISCHARGED. REPLACED RIGHT NUMBER FOUR DOOR SLIDE AND ASSIST BOTTLE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT 10D INOPERATIVE. REPAIRED PIN ON CONNECTOR FOR EMERGENCY LIGHT AT SEAT 10D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: HOSE — LEAKING (HYD SYSTEM)

MIA INFLIGHT T1818/22AUG - ON SHORT FINAL, LOST LEFT HYDRAULIC QUANTITY DOWN TO .22. LANDED MIA WITHOUT INCIDENT. REPLACED MAIN LANDING GEAR DOWN LOCK ACTUATOR HOSE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS)

MIA - EMERGENCY LIGHT AT SEAT 18D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR INOPERATIVE. REPLACED LIGHT BULB FOR INOPERATIVE EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — DAMAGED (CABIN)

DFW - SEAT MOUNTED EMERGENCY LIGHT AT FORWARD SEAT 5E LENS AND SHROUD DAMAGED. REPLACED DAMAGED LENS AND SHROUD AT FORWARD SEAT 5E. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

SFO FIRST CLASS EMERGENCY LIGHTS ON SEATS INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 4EF. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

BOS - EMERGENCY LIGHTS IN FIRST CLASS SECTION INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN FIRST CLASS SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: HYDRAULIC LINE — LOOSE (HYD SYSTEM)

MIA - FLT 1193 - EN ROUTE JFK-MBJ, PASSENGER REPORTED WHITE STREAK COMING OFF LEFT WING DURING CRUISE. CREW INVESTIGATED SHUTDOWN LEFT ENGINE PER FUEL LEAK CHECK LIST. LANDED AT MIA WITHOUT INCIDENT. INSPECTED AND FOUND HYDRAULIC LINE LEAKING. TIGHTENED LEAKING LINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 34 INOPERATIVE. SECURED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT 34D INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGH MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 34D INOPERATIVE. RE-SEATED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 34D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 34D INOPERATIVE. RESECURED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 34D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: MODULE — DEFECTIVE (CABIN)

DFW - FLT 2328 - DURIGN CRUISE, THE FLOOR EMERGENCY LIGHT ILLUMINATED FOR APPROXIMATELY 35 MINUTES. REPAIRED LOOSE EMERGENCY AISLE PATH LIGHTING GROUND WIRE AND REPLACED CONTROL MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: MODULE — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS ILLUMINATED INTERMITTENTLY. REPLACED EMERGENCY FLOOR LIGHT MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: MODULE — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS WERE INOPERATIVE. REPLACED EMERGENCY FLOOR PATH LIGHTING FORWARD MODULE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: CONNECTOR — BROKEN (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT RIGHT AISLE FROM BULKHEAD BACK TO PAX SEAT ROW 14D INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHTS STRIP CONNECTOR BY PAX SEAT ROW 14D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FUEL GOVERNOR — DEFECTIVE (NR 2 ENGINE)

SJU - FLT 1470 - ON DESCENT TO SJU, THE NR 2 ENGINE WOULD NOT ADVANCE FROM IDLE POSITION. LANDED SJU WITHOUT INCIDENT. REPLACED NR 2 ENGINE FUEL GOVERNOR AND THROTTLE ANGLE TRANSDUCER. RAN ALL NECESSARY RUN-UP CHECKS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)