N611AM

Part: IDG — FAILED (LT ENGINE) · airframe 67,811 hrs · 24,695 cycles

LAS - INFLIGHT SFO-MIA. CREW REPORTED LEFT ENGINE GENERATOR FAILED AND AUXILIARY POWER UNIT FAULTED. EMERGENCY DECLARED FLIGHT DIVERTED LAS LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT INTEGRATED DRIVE GENERATOR. REPLACED APU AT LAX ON 06/28/2011. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: TANK — DEFECTIVE (FUEL SYSTEM) · airframe 66,919 hrs · 24,384 cycles

MCO - INFLIGHT EWR-MIA. CREW REPORTED LEFT FUEL QUANTITY INDICATION ISSUE. EMERGENCY DECLARED FLIGHT DIVERTED MOC LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. PLACARD LEFT MAIN TANK, LEFT WING FUELING PANEL AND FUEL TOTALIZER INOPERATIVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,313 hrs · 23,792 cycles

LEFT NUMBER 4 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 4 DOOR EMERGENCY LIGHT. OPS CHECKED NORMAL.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,353 hrs · 23,454 cycles

NUMEROUS AREAS OF CORROSION ALONG STATION 1680 FLOORBEAM T-CAP LEFT BUTTLINE 54 TO RIGHT BUTTLINE 54. REMOVED AND REPLACED ENTIRE FLOORBEAM T-CAP PER EA B757-53-009489.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,353 hrs · 23,454 cycles

AFT CABIN DECK STATION 1720 RIGHT BUTTLINE 63 THE WEB UNDER BATH TUB FITTING IS CORRODED. INSTALLED NEW WEB PER SRM 51-40-02.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,353 hrs · 23,454 cycles

LEFT NUMBER 4 DOOR AFT GUTTER BOX HAS CORROSION AROUND NUT PLATES. REMOVED CORROSION AND RE-INSTALLED GUTTER BOX.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,353 hrs · 23,454 cycles

RIGHT NUMBER 4 DOOR LOWER SILL SUPPORT AT STATION 1657 CORRODED. INSTALLED LOWER SUPPORT AT RIGHT NUMBER 4 STATION 1657 PER SRM 51-10-02-0G.

Part: SLAT — CRACKED (LT WING) · airframe 64,353 hrs · 23,454 cycles

LEFT WING LEADING EDGE NUMBER 2 SLAT HAS CRACK ACROSS FASTENER IN COVE AREA FORWARD OF INBOARD MAIN DRIVE TRACK ARM MARKED. STOP-DRILLED CRACK PER AARD 57-43-00-4. ACCOMPLISHED HIGH FREQUENCY EDDY CURRENT AROUND STOP DRILL. NO CRACK INDICATION BEYOND STOP DRILL. INSTALLED DOUBLER PER AARD 57-43-00-4.

Part: SKIN — GOUGED (LE SLAT) · airframe 64,353 hrs · 23,454 cycles

LEFT WING NUMBER 2 SLAT TOP AFT HAS ALUMINUM TAPE OVER HOLE. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 51-70-10-2R.

Part: SLAT — CRACKED (LT WING) · airframe 64,353 hrs · 23,454 cycles

LEFT WING LEADING EDGE NUMBER 2 SLAT HAS CRACK ACROSS FASTENER IN COVE AREA FORWARD OF OUTBOARD MAIN DRIVE TRACK ARM MARKED. STOPPED DRILLED CRACK PER AARD 57-43-00-4. ACCOMPLISHED HIGH FREQUENCY EDDY CURRENT AROUND STOP DRILL. NO CRACK INDICATION BEYOND STOP DRILL. INSTALLED DOUBLER PER AARD 57-43-00-4.

Part: MODULE — INOPERATIVE (CABIN)

DFW - FIRST CLASS ESCAPE PATH EMERGENCY LIGHTING DIM. REPLACED MODULE FOR FIRST CLASS ESCAPE PATH EMERGENCY LIGHTING.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS)

DFW - AFT OVERWING EMERGENCY LIGHT IN ROW 18DEF INOPERATIVE. REPLACED LAMP IN AFT OVERWING EMERGENCY LIGHT IN ROW 18DEF.

Part: PLACARD — DAMAGED (CABIN)

DFW - EMERGENCY EXIT MARKER DECAL AT LEFT NUMBER TWO DOOR DAMAGED. REPLACED DECAL FOR EMERGENCY EXIT MARKER AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EXTERIOR)

DFW - EXTERNAL EMERGENCY LIGHT AT LEFT HAND FORWARD OVERWING AFT INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY LIGHT AT LEFT HAND FORWARD OVERWING AFT POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — DAMAGED (EMERGENCY LIGHTS) · airframe 58,178 hrs

DFW - EMERGENCY LIGHT AT SEAT 33D HAS DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 33D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)

MIA - EMERGENCY LIGHT AT OVERHEAD SEAT 12ABC INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 12ABC. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — CUT (EMERGENCY LIGHTS)

MIA - EMERGENCY LIGHT EXIT ARROW SIGN AT RIGHT SIDE LOWER AFT GALLEY INOPERATIVE. FOUND CUT WIRES BEHIND LAVATORY. REPAIRED PER E58 9376176. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LAX - EMERGENCY LIGHT AT MID COACH INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT MID COACH. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

MIA - EMERGENCY EXIT UNARMED LIGHT INOPERATIVE. RELAMPED EMERGENCY EXIT UNARMED LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ENGINE — LEAKING (RIGHT)

ABQ - RIGHT HAND ENGINE OIL PRESSURE LOSS. IN FLIGHT SHUT DOWN OF ENGINE. SINGLE ENGINE TIME 15 MINUTES. LANDED ABQ WITHOUT INCIDENT. FOUND OIL LEAK. FLIGHT DATA RECORDER DOWNLOADED. REPLACED NUMBER TWO ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: VALVE — INOPERATIVE (LT MLG)

SDQ - THE LEFT HAND MAIN LANDING GEAR DOOR WOULD NOT CLOSE ON LANDING. REPLACED THE SERVO CALVE OF THE LEFT HAND MAIN LANDING GEAR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SEAL — LEAKING (FUEL PORT)

DEN - AFTER TAKEOFF PASSENGER REPORTED FUEL LEAKING FROM RIGHT OVERWING FUEL CAP. LANDED DEN WITHOUT INCIDENT. REPLACED FUEL CAP, O-RING SEALS AT RIGHT WING OVERWING FUEL PORT HOUSING ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CAP — LEAKING (FUEL STORAGE)

MIA - INFLIGHT T671/17 RIGHT HAND WING FUEL LEAK. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED CAP AND O-RING FOR RIGHT HAND FUEL TANK. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (SEAT 17D)

AFT EMERGENCY PATH LIGHT ON SEAT 17D INOPERATIVE. REPLACED AFT EMERGENCY PATH LIGHT ASSEMBLY ON SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SPRING — DAMAGED (GIRT BAR)

DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, FOUR GIRT BAR SPRINGS NEEDING REPLACED. REPLACED FOUR GIRT BAR SPRINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SWITCH — DEFECTIVE (NR 2 ENGINE)

TUL - FLT 1805 - EN ROUTE TUL-DFW, DETECTED RIGHT SIDE HYDRAULIC QUANTITY LOW. RETURNED TUL GATE WITHOUT FURTHER INCIDENT. REPLACED NR 2 SIDE ENGINE DIFFERENTIAL PRESSURE SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: UNKNOWN — ODOR (CABIN)

ABQ - FLT 160 - EN ROUTE SAN-JFK, DETECTED A STRONG SMELL AT L2 AND R2 DOORS. DIVERTED ABQ AND LANDED WITHOUT FURTHER INCIDENT. CLEANED ENTIRE PACK SYSTEM. ACCOMPLISHED ADJUSTMENT SYSTEM TEST ON RIGHT SIDE ENGINE BLEED SYSTEM. PERFORMED HIGH POWER ENGINE RUN UP. NO SMELL NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

LAX - DURING OVER-NIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS AT SEATS 22 THROUGH 26 INOPERATIVE. SECURED LOOSE CONNECTOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: WIRE — BROKEN (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS AT COFFEE BAR IN FIRST CLASS INOPERATIVE. REPAIRED EMERGENCY EXIT ESCAPE PATH LIGHT WIRING AT COFFEE BAR. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: CONNECTOR — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS IN FIRST CLASS SEAT ROWS 5E AND 6E INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT STRIP CONNECTOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)