N665AA

Part: UNKNOWN — ODOR (CABIN) · airframe 70,948 hrs · 24,754 cycles

RETURNED, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB AT 2600 FEET FLIGHT ATTENDANT REPORTED STRONG BURNING ELEC SMELL BETWEEN L2 & R2 DOORS. PERFORMED ENG & APU RUNS WITH NO FINDINGS. INSPECTED RECIRCULATION FANS & FILTERS, ALL CABIN LIGHTS, INFLIGHT ENTERTAINMENT & POWER PORTS WITH NO FINDINGS. R & R OXYGEN & HALON EXTINGUISHER BOTTLES. ALL CHECKED NORMAL & NO ODOR PRESENT WHILE PERFORMING ENG RUNS. ACFT FERRIED WITH NO ODOR REPORTED.

Part: HOUSING — DIRTY (CABIN) · airframe 70,948 hrs · 24,754 cycles

RETURNED, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB AT 5000 FEET FLIGHT ATTENDANT REPORTED STRONG BURNING ELEC SMELL BETWEEN L2 & R2 DOORS. CHECKED ALL CABIN LIGHTS, POWER PORTS, ELEC EQUIP, ELEC EQUIP BAY & CARGO COMPARTMENTS. NO EVIDENCE OF ELEC SMELL FOUND. PERFORMED DUAL ENG RUN. SYSTEMS CHECKED NORMAL. ELEC SMELL FOUND ONLY AT DOG HOUSE BEHIND SEAT 5AB. CLEANED DOG HOUSE & SMELL CLEARED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,417 hrs · 24,557 cycles

LEFT NR 3 DOOR EMER LIGHT INOPERATIVE. REPLACED LAMP FOR LT NR 3 DOOR EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: PRESSURE DECK — CORRODED (FUSELAGE) · airframe 69,614 hrs · 24,270 cycles

CORROSION IN THE RT WW ON THE LOWER SURFACE OF THE PRESS DECK AT STATION 1160. REMOVED CORROSION, ACCOMPLISHED HFEC INSPECTION & INSTALLED DOUBLER.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,878 hrs · 24,006 cycles

EMERGENCY LIGHTS IN FIRST CLASS SECTION INOPERATIVE. REPLACED BATTERY PACK FOR FIRST CLASS EMERGENCY LIGHTS, OPERATIONS CHECKED NORMAL.

Part: HINGE — DAMAGED (THRUST REVERSER) · airframe 68,826 hrs · 23,982 cycles

NR 2 ENG THRUST REVERSER AFT HINGE INBD FASTENER HOLE DAMAGED. INSTALLED FREEZE PLUGS & DOUBLER IAW EA B757-54-033589 & SRM 54-50-00.

Part: CONTROL MODULE — FAULTY (SPOILER) · airframe 67,495 hrs · 23,496 cycles

SAP INFLIGHT MIA-TGU CREW REPORTED SPOILER EICAS MESSAGE ON DESCENT. FLIGHT DIVERTED SAP LANDED WITHOUT INCIDENT. PLACARDED FLIGHT SPOILER SYSTEM IAW MEL. FLIGHT CONTINUED TO DESTINATION. REPLACED 1L SPOILER CONTROL MODULE AT MIA ON 08/04/2013. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 65,987 hrs · 22,928 cycles

DFW - CREW REPORTED NUMBER 2 CENTER HYDRAULIC OVERHEAT MESSAGE FOLLOWED BY EICAS MESSAGE AND LOSS OF SYSTEM. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER 2 CENTER ELECTRONIC HYDRAULIC PUMP. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BALLAST — INOPERATIVE (CABIN) · airframe 64,430 hrs · 22,357 cycles

THE 18ABC EMERGENCY HATCH DOOR LIGHT LEFT AFT INOPERATIVE. REMOVED AND REPLACED LEFT HATCH DOOR LIGHT BALLAST. OPS CHECK NORMAL.

Part: TEAR STRAP — CRACKED (FUSELAGE) · airframe 62,390 hrs · 21,591 cycles

TEARSTRAP CRACKED BOTTOM OF FLOORBEAM STATION 365 AND LEFT BUTTLINE 47. INSTALLED DOUBLER PER SRM 53-10-51-2R 1.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,390 hrs · 21,591 cycles

AFT GALLEY DECK PLATE FORWARD RIGHT DOUBLER OUTBOARD OF CENTER CORRODED. REPLACED DOUBLER PER SRM 53-60-51-2R2.

Part: STRAP — CRACKED (FUSELAGE) · airframe 62,390 hrs · 21,591 cycles

STABILIZER STRAP CRACKED STATION 1380 RIGHT BUTTLINE 45. INSTALLED DOUBLER.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,390 hrs · 21,591 cycles

WEB CRACKED STATION 700 BELOW NUMBER 4 SEAT TRACK. ACCOMPLISHED SPLICE REPAIR.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 3 · airframe 62,390 hrs · 21,591 cycles

WEB INBOARD OF AFT CARGO DOOR SILL AT STATIONS 1410 TO 1420 CORRODED. REPLACED WEB.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 3 · airframe 62,390 hrs · 21,591 cycles

WEB OUTBOARD OF STRINGER 29 RIGHT IS CORRODED AT STATIONS 1620 TO 1640. REPLACED WEB PER AARD 51-20-00-1.

Part: SLAT — CORRODED (RT WING) · corrosion level 2 · airframe 62,390 hrs · 21,591 cycles

NUMBER 9 SLAT HAS CORROSION AROUND HI-LOK FASTENER, 65 INCHES FROM OUTBOARD END. INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,390 hrs · 21,591 cycles

AFT PRESSURE DECK DOUBLER AT STA 1715 BUTTLINE 35 LEFT HAS CORROSION. REMOVED DOUBLER AND REINSTALLED REPAIR PER SRM 53-60-51-2R.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 62,390 hrs · 21,591 cycles

FORWARD CARGO DOOR, OUTER DOOR SKIN EDGE BENT AT LOWER AFT CORNER. INSTALLED DOUBLER REPAIR ON LOWER AFT CORNER OUTER SKIN PER SRM 52-30-01 PAGE 1 AND EA COMP-52-019297.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 62,390 hrs · 21,591 cycles

STATION 1540 TO 1560 STRINGER 30 RIGHT DAMAGED. INSTALLED DOUBLER REPAIR SRM 53-00-01-2R-3.

Part: STRUCTURE — CRACKED (R2 DOOR) · airframe 62,390 hrs · 21,591 cycles

RIGHT NUMBER 2 PASSENGER DOOR INNER CHORD UPPER HINGE CUTOUT IS CRACKED. INSTALLED DOUBLER REPAIR PER EA 52-019135 DATED 09/20/2011.

Part: INTERCOSTAL — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 62,390 hrs · 21,591 cycles

FORWARD CARGO DOOR 2ND INTERCOSTAL AFT OF FORWARD EDGE HAS CORROSION. INSTALLED NEW INTERCOSTAL PER ESO 90114.

Part: INTERCOSTAL — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 62,390 hrs · 21,591 cycles

FORWARD CARGO DOOR, 4TH INTERCOSTAL AFT OF FORWARD EDGE HAS CORROSION. INSTALLED NEW INTERCOSTAL PER ESO 90114.

Part: INTERCOSTAL — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 62,390 hrs · 21,591 cycles

FORWARD CARGO DOOR, 3RD INTERCOSTAL AFT OF FORWARD EDGE HAS CORROSION. INSTALLED NEW INTERCOSTAL PER ESO 90114.

Part: SKIN — BENT (CARGO DOOR) · airframe 62,390 hrs · 21,591 cycles

NUMBER 2 CARGO DOOR, THE OUTER EDGE OF THE SKIN IS BENT AT THE LOWER FORWARD CORNER OF THE DOOR. STRAIGHTENED THE DAMAGED AREA ALONG THE OUTER EDGE OF THE SKIN CORNER. DYE CHECKED: NO CRACKS INDICATED. FABRICATED DOUBLER AND INSTALLED PER SRM 52-30-01-2R.

Part: SKIN — BENT (CARGO DOOR) · airframe 62,390 hrs · 21,591 cycles

NUMBER 2 CARGO DOOR LOWER FORWARD CORNER DOOR SKIN BENT. DYE CHECKED AREA AND INSTALLED A DOUBLER REPAIR AT THE LOWER FORWARD CORNER OF THE NUMBER 2 CARGO DOOR PER SRM 52-30-01-2R.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 62,390 hrs · 21,591 cycles

FLOOR SUPPORT STRINGER BENT AND DENTED STATION 1430. REPLACED FLOOR SUPPORT STRINGER PER AARD 51-10-05-01.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,390 hrs · 21,591 cycles

SUPPORT ANGLE UNDER CREASE ANGLE AT STATION 1720 CORRODED. REPLACED SUPPORT ANGLE.

Part: PIN — NOT SEATED (BATTERY MODULE) · airframe 58,674 hrs · 20,328 cycles

EMERGENCY LIGHTS INOPERATIVE FROM 26D THRU AFT DOORS. RESET PIN 23 AT LEFT NUMBER 4 DOOR EMERGENCY BATTERY MODULE LOCATED BETWEEN RIGHT AND LEFT LAVATORY. OPS CHECKED NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 58,542 hrs · 20,280 cycles

EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. RE-SECURED CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHTING. OPS CHECKED NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 58,532 hrs · 20,276 cycles

THE 23D SEAT MOUNTED ESCAPE PATH LIGHT INOPERATIVE. SECURED CONNECTOR FOR 23D SEAT MOUNTED ESCAPE PATH LIGHT. OPS CHECKED NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 58,532 hrs · 20,276 cycles

THE 17ABC OVERWING EMERGENCY LIGHT INOPERATIVE. RE-SECURED CONNECTOR FOR 17ABC OVERWING EMERGENCY LIGHT. OPS CHECKED NORMAL.

Part: MODULE — INOPERATIVE (CABIN) · airframe 58,532 hrs · 20,276 cycles

ROWS 26 TO 36 EMERGENCY LIGHTS AND LEFT AND RIGHT AFT ENTRY DOOR EXIT SIGN INOPERATIVE. REPLACED MODULE FOR ROWS 26 TO 36 EMERGENCY LIGHTS AND LEFT AND RIGHT AFT ENTRY DOOR EXIT SIGN. OPS CHECKED NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 58,532 hrs · 20,276 cycles

THE 17ABC OVERWING EMERGENCY LIGHT INOPERATIVE. SECURED CONNECTOR FOR 17ABC OVERWING EMERGENCY LIGHT. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,532 hrs · 20,276 cycles

ROWS 26 TO 36 EMERGENCY LIGHTS AND LEFT AND RIGHT AFT ENTRY DOOR EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK FOR ROWS 26 TO 36 EMERGENCY LIGHTS AND LEFT AND RIGHT AFT ENTRY DOOR EXIT SIGN. OPS CHECKED NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 58,532 hrs · 20,276 cycles

SEAT 11D EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. SECURED LOOSE CONNECTOR FOR SEAT 11D EMERGENCY ESCAPE PATH LIGHT. OPS CHECKED NORMAL.

Part: CLAMP — LOOSE (AC PACK) · airframe 57,878 hrs · 20,059 cycles

JFK - INFLIGHT LGA-MIA. CREW REPORTED PRESSURIZATION LOSS AFTER TAKEOFF. PROBLEM STARTED WITH LEFT BLEED FAULT. WHEN LEFT BLEED WAS SHUT DOWN, ALTITUDE WARNING ON PRESSURIZATION SYSTEM RIGHT PACK COULD NOT MAINTAIN CABIN PRESSURE. EMERGENCY DECLARED FLIGHT DIVERTED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND CLAMP LOOSE ON RIGHT PACK CHECK VALVE BOOT. REPOSTIONED BOOT AND INSTALLED NEW CLAMP.

Part: LUG — CORRODED (DOOR) · corrosion level 2 · airframe 57,779 hrs · 20,027 cycles

CORROSION ON LUGS OF UPPER CASTING GATE ROD ATTACHMENT. REPAIRED PER EA 757-52-009071.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,779 hrs · 20,027 cycles

THE NUMBER 9 SLAT BACK SKIN IS CRACKED AT THE INBOARD DRIVE TRACK FITTING AREA. REPAIRED SLAT PER AARD 57-43-00-4.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,779 hrs · 20,027 cycles

THE NUMBER 8 SLAT BACK SKIN HAS TWO CRACKS AT THE INBOARD DRIVE TRACK FITTING AREA. REPAIRED SLAT PER AARD 57-43-00-4.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,779 hrs · 20,027 cycles

THE NUMBER 9 SLAT BACK SKIN IS CRACKED AT THE OUTBOARD DRIVE TRACK FITTING AREA. REPAIRED SLAT PER AARD 57-43-00-4.

Part: FAIRING — CRACKED (LT ENGINE) · airframe 57,663 hrs · 19,985 cycles

LAS - INFLIGHT LAX-STL. CREW REPORTED LEFT ENGINE VIBRATION. EMERGENCY DECLARED DIVERTED LAS LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE NOSE CONE FAIRING DUE TO A CRACK FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (CABIN) · airframe 57,479 hrs · 19,919 cycles

EMERGENCY LIGHT AT SEAT 18D MISSING LENS. REPLACED LENS.

Part: CONNECTOR — LOOSE (CABIN)

MIA - EMERGENCY LIGHT AT SEAT 12D INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 12D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — BURNED (PILOT VALVE)

VVI INFLIGHT, AT CRUISE CREW REPORTED STRONG ELECTRICAL BURNING ODOR. FIRST OFFICER LOST AIRSPEED INDICATOR AND ALTIMETER WAS ERRATIC. CREW RECEIVED RUDDER RATIO AND MACH SPEED TRIM INDICATIONS. RETURNED TO VVI AND LANDED WITHOUT INCIDENT. FOUND LEFT DUCT PRESSURE LOW AND LEFT STAGE PILOT VALVE CONNECTOR BURNED. PLACARDED THE NR 1 ENGINE HIGH PRESSURE SHUTOFF VALVE INOPERATIVE. REPLACED THE NR 1 ENGINE PNEUMATIC SENSOR LINE FROM PILOT VALVE TO HIGH STATE VALVE ON 05 MAR 08 IN MIA. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS)

MIA - EMERGENCY EXIT LIGHT AT LEFT NUMBER FOUR DOOR INOPERATIVE. REPLACED LAMP FOR INOPERATIVE EMERGENCY EXIT LIGHT AT LEFT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: A/C PACK — SMOKE

CCS - INFLIGHT AIRCRAFT ARRIVED WITH ACRID SMELL IN COCKPIT AND NUMBER ONE FLIGHT ATTENDANT REPORTED A HAZY SMOKE IN FIRST CLASS CABIN. INSPECTED MAIN CABIN AND FIRST CLASS CABIN AND NO EVIDENCE OF ACRID SMELL. ACCOMPLISHED PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT BY RIGHT AFT LAVATORY INOPERATIVE. FOUND WIRE DISCONNECTED AT EMERGENCY LIGHT RIGHT HAND AFT LAVATORY. REPOSITIONED WIRE FOR EMERGENCY LIGHT AT RIGHT HAND AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BOTTLE — DISCHARGED (ESCAPE SLIDE)

ORD - R1 DOOR SLIDE BOTTLE INDICATES ZERO PSI. REPLACED SLIDE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — INOPERATIVE (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 21D INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 21D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DIRTY (L2 DOOR)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L2 DOOR INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT CONNECTOR AT L2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (SEAT 11)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT 11D INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT 11D. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: FLOOR BEAM — CORRODED (BS 377)

AFW - FLOOR BEAM AT STATION 377 HAS CORROSION, REMOVAL ON UPPER SURFACE MATERIAL REMAINING IS BEYOND SRM LIMITS. REPAIR PER MRB 980. (M)

Part: FLOOR BEAM — DAMAGED (BS 365)

AFW - FLOOR BEAM AT STATION 365 HAS DRILL MARK BLENDOUT, MATERIAL REMAINING IS BEYOND SRM ALLOWABLE LIMITS. REPAIR PER MRB 757-981. (M)

Part: PAN — GOUGED (R4 DOOR)

AFW - R-4 DOOR HANDLE PAN HAS GOUGE BEYOND SRM LIMITS. GOUGE WAS BLENDED. REPAIRED PER MRB 757-983. (M)

Part: FRAME — CORRODED (BS 1480)

AFW - FUSELAGE FRAME AT STATION 1480 HAS CORROSION REMOVED, REMAINING MATERIAL IS BEYOND ALLOWABLE SRM LIMITS. REPAIR PER MRB 757-986. (M)

Part: INTERCOSTAL — CORRODED (BS 395-418)

AFW - INTERCOSTAL BETWEEN STATION 395 AND 418 HAS CORROSION REMOVAL, REMAINING MATERIAL IS BEYOND ALLOWABLE SRM LIMITS. REPAIR PER MRB 757-979. (M)

Part: FLOOR BEAM — CORRODED (BS 1640)

AFW - FLOOR BEAM AT STATION 1640 HAS CORROSION REMOVAL, REMAINING MATERIAL IS BEYOND SRM ALLOWABLE LIMITS. REPAIR PER MRB 757-982. (M)