N637AM

Part: ROTARY ACTUATOR — MALFUNCTIONED (LE SLAT) · airframe 65,362 hrs · 23,093 cycles

PAP (REPEAT ITEM) CREW REPORTED LEADING EDGE SLAT ASYMMETRY. EMERGENCY DECLARED FLIGHT LANDED PAP WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND LEADING EDGE SLAT POWER DRIVE UNIT OUTBOARD OVERLOAD INDICATOR TRIPPED AND NUMBER 10 LEADING EDGE SLAT ACTUATOR OVERLOAD INDICATOR ACTIVATED. REPLACED NUMBER 10 LEADING EDGE SLAT ROTARY ACTUATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BOLT — LOOSE (LE SLAT) · airframe 65,360 hrs · 23,092 cycles

MIA - CREW REPORTED LEADING EDGE ASYMMETRY ISSUE ON TAKEOFF. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND NUMBER 10 ROTARY ACTUATOR MOUNT BOLT LOOSE. REPLACED MOUNT BOLT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,569 hrs · 21,769 cycles

EMERGENCY LIGHTS AT ROW 24DEF INOPERATIVE. REPLACED SEAT MOUNTED LIGHT ASSEMBLY AT 24DEF. OPS CHECKED NORMAL.

Part: SKIN — DAMAGED (LE SLAT) · airframe 59,645 hrs · 21,086 cycles

NUMBER 8 SLAT TWO {2} SCREWS INSTALLED ON THE LEADING EDGE SKIN AT THE AFT END 32 INCHES FROM THE OUTBOARD END. REMOVED FASTENERS AND INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.

Part: SKIN — DAMAGED (LE SLAT) · airframe 59,645 hrs · 21,086 cycles

NUMBER 8 SLAT HAS A BLENDED AREA WITH A BLIND FASTENER INSTALLED IN THE LEADING EDGE SKIN 45 .75 INCHES FROM THE INBOARD END. REMOVED DAMAGED AREA AND INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 59,645 hrs · 21,086 cycles

NUMBER 7 SLAT HAS A CORROSION BLISTER NEXT TO THE FASTENER 63 .75 INCHES FROM THE OUTBOARD END ON THE LEADING EDGE SKIN. REMOVED AFFECTED AREA AND INSTALLED FLUSH REPAIR AS PER SRM 57-43-01-2R AND AARD 57-43-00-1.

Part: SKIN — DAMAGED (LE SLAT) · airframe 59,645 hrs · 21,086 cycles

NUMBER 8 SLAT HAS A SCREW IN THE LEADING EDGE SKIN 34 INCHES FROM THE INBOARD END. REMOVED FASTENER AND INSTALLED FLUSH DOUBLER PER AARD 57-43-00-1.

Part: SKIN — DAMAGED (LE SLAT) · airframe 59,645 hrs · 21,086 cycles

NUMBER 8 SLAT HAS PREVIOUS BLEND AROUND FASTENER ON NOSE SKIN {TOP}. REMOVED DAMAGED AREA OF SKIN AND INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 59,645 hrs · 21,086 cycles

NUMBER 7 SLAT HAS CORROSION AROUND FASTENER 32 INCHES FROM OUTBOARD END ON NOSE {TOP}. REMOVED AFFECTED AREA AND INSTALLED FLUSH REPAIR AS PER SRM 57-43-01-2R AND AARD 51-43-00-1.

Part: SKIN — CORRODED (LLE SLAT) · corrosion level 2 · airframe 59,645 hrs · 21,086 cycles

NUMBER 7 SLAT HAS CORROSION ON SKIN FROM INBOARD END. REMOVED AFFECTED AREA AND INSTALLED FLUSH REPAIR AS PER SRM 57-43-01-2R AND AARD 51-43-00-1.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 59,645 hrs · 21,086 cycles

NUMBER 8 SLAT HAS CORROSION AROUND FASTENER 18.5 INCHES FROM OUTBOARD END ON NOSE SKIN {TOP}. REMOVED DAMAGED SKIN AND INSTALLED FLUSH REPAIR PER AARD 57-43-00-1.

Part: GATE — CRACKED (L4 DOOR) · airframe 59,645 hrs · 21,086 cycles

LEFT NUMBER FOUR DOOR UPPER GATE CRACKED. INSTALLED NEW UPPER GATE PER ESO 90108.

Part: TORQUE BOX — CRACKED (R2 DOOR) · airframe 59,645 hrs · 21,086 cycles

RIGHT NUMBER TWO PASSENGER DOOR HANDLE TORQUE BOX IS CRACKED. REPLACED RIGHT NUMBER TWO PASSENGER DOOR HANDLE TORQUE BOX PER ESO 90282.

Part: GATE — CRACKED (L1 DOOR) · airframe 59,645 hrs · 21,086 cycles

LEFT NUMBER ONE DOOR UPPER GATE CRACKED AT ROD END BOLT HOLE. REMOVED CRACKED UPPER GATE AND INSTALLED NEW UPPER GATE PER ESO 90283.

Part: GATE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 59,645 hrs · 21,086 cycles

RIGHT NUMBER TWO PASSENGER DOOR LOWER GATE HAS HEAVY CORROSION ON LOWER END. REPLACED LOWER GATE PER ESO 90282.

Part: GATE — CORRODED (L1 DOOR) · corrosion level 2 · airframe 59,645 hrs · 21,086 cycles

LEFT NUMBER ONE PASSENGER ENTRY DOOR LOWER GATE ASSEMBLY CORRODED. REPLACED WITH NEW LOWER GATE ASSEMBLY PER ESO 90283.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 86,572 hrs

JFK - AFT EVACUATION LIGHTS AND ROW 20 LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT ROW 20 AFT.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - LOWER AFT FUSELAGE EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LOWER AFT FUSELAGE EMERGENCY LIGHT.

Part: MODULE — INOPERATIVE (CABIN) · airframe 58,310 hrs

ORD - EMERGENCY LIGHTS ON SIDES OF SEATS 9D TO 16D INOPERATIVE. REPLACED MODULE AND BATTERY AT OVERHEAD ROW 9.

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,380 hrs · 20,651 cycles

CABIN, CORROSION ON FLOOR WEB LEFT BODY LINE 50 TO RIGHT BODY LINE 40 AT STATION 1714 TO 1718. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-60-51-2R.

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,382 hrs · 20,652 cycles

CABIN, CORROSION ON WEB BENEATH Z CHANNEL AT LEFT BODY LINE 50. INCORPORATED INTO PRE-EXISTING DOUBLER PER SRM 53-60-51-2R ALTERNATIVE -2.

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,382 hrs · 20,652 cycles

CORROSION ON WEB ABOVE FLOORBEAM STATION 1680 RIGHT BODYLINE 3. INSTALLED DOUBLER PER SRM 53-60-51-2R2.

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,382 hrs · 20,652 cycles

CORROSION ON WEB ABOVE FLOORBEAM STATION 1680 LEFT BODYLINE 5 TO 24. INSTALLED DOUBLER PER SRM 53-60-51-2R2.

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,382 hrs · 20,652 cycles

CORROSION ON WEB ABOVE FLOORBEAM STATION 1680 LEFT BODYLINE 33 - 40. INSTALLED DOUBLER PER SRM 53-60-51-2R2.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,382 hrs · 20,652 cycles

CORROSION ON WEB ABOVE FLOORBEAM STATION 1680 RIGHT BODYLINE 12. INSTALLED DOUBLER PER SRM 53-60-51-2R2.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,382 hrs · 20,652 cycles

CORROSION ON FLOORBEAM AT STATION 1680 LEFT BODYLINE 12 FORWARD SIDE. INSTALLED FLOORBEAM DOUBLER PER AARD 53-60-51-5 REFERENCE EA B757-53-006144.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,382 hrs · 20,652 cycles

CORROSION ON FLOORBEAM STATION 1680 LEFT BODYLINE 25 FORWARD SIDE. INSTALLED DOUBLER PER AARD 53-60-51-5 REF EA 757-53-006144.

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,382 hrs · 20,652 cycles

CORROSION ON WEB ABOVE FLOORBEAM STATION 1680 LEFT BODYLINE 48 TO 52. INSTALLED DOUBLER PER SRM 53-60-51-2R2.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,382 hrs · 20,652 cycles

CORROSION ON FLOORBEAM STATION 1680 LEFT BODYLINE 4-5 AT SCREW HOLE FORWARD SIDE. INSTALLED DOUBLER PER AARD 53-60-51-5 REFERENCE EA B757-53-006144.

Part: MOUNT — CORRODED (GALLEY) · corrosion level 2 · airframe 58,382 hrs · 20,652 cycles

CORROSION ON GALLEY TIE DOWN FITTING BODY LINE 0 STATION 1686. INSTALLED NEW TIE DOWN FITTING PER SRM 51-10-02.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,245 hrs · 20,601 cycles

CABIN FLOORBEAM HAS CORROSION AT STATION 1640 RIGHT BODY LINE 42 TO LEFT BODY LINE 17. REMOVED AND REPLACED FLOORBEAM UPPER CHORD RIGHT BODY LINE 42 TO LEFT BODY LINE 17 PER SRM 53-00-51-2R.

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,245 hrs · 20,601 cycles

CABIN FLOOR HAS CORROSION ON WEB STATION 1680 AT RIGHT BODY LINE 32 TO RIGHT BODY LINE 45.

Part: PLACARD — DAMAGED (CABIN)

DFW RIGHT HAND AFT LEFT SIDE OF OVERWING EXIT PLACARD DAMAGED. INSTALLED SERVICEABLE EXIT PLACARD.

Part: LIGHT — INOPERATIVE (CABIN)

DFW EMERGENCY LIGHT AT BULL NOSE 2E INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT BULL NOSE 2E.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS)

LGA - EMERGENCY LIGHT AT SEAT 12D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 12D.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,484 hrs

JFK- EMERGENCY EXIT SIGN BASE AT RIGHT NUMBER 2 DOOR INOPERATIVE. REPLACED LEFT NUMBER 2 DOOR EMERGENCY LIGHT. RIGHT NUMBER 2 DOOR CHECKED NORMAL.

Part: COUPLING — LEAKING (HYD SYSTEM) · airframe 57,482 hrs · 20,311 cycles

RDU INFLIGHT JFK TO CUN - CREW REPORTED RIGHT HYDRAULIC SYSTEM QUANTITY LOSS. LANDED RDU WITHOUT INCIDENT. FOUND HYDRAULIC LEAK AT RIGHT ENGINE HYDRAULIC PUMP RETURN LINE AND PRESSURE COUPLING. REPLACED COUPLING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,029 hrs

DFW - EMERGENCY LIGHT AT SEAT 12DEF INOPERATIVE. REPLACED LIGHT ASSEMBLY AT SEAT ROW 12DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW EMERGENCY LIGHT AT AFT LT OVERWING HATCH INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT AFT LT OVERWING HATCH. SYSTEM GROUND CHECKED NORMAL OPS.

Part: BLADE — FAILED (COMPRESSOR) · airframe 55,427 hrs

ORD INFLIGHT T780/30MAY. NR ONE ENGINE COMPRESSOR STALL DURING TAKEOFF POWER. CREW HEARD TWO LOUD REPORTS AND FELT AIRCRAFT VIBRATE. CABIN CREW AND PASSENGERS REPORTED BURST OF FLAME. ALL INDICATIONS NORMAL. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. NO SECONDARY INDICATIONS FOR ENGINE FLAME. FOUND MULTIPLE STAGE THREE HIGH PRESSURE COMPRESSOR BLADES DAMAGED. REPLACED NR ONE ENGINE ON 30 MAY AT ORD. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,174 hrs

SJU - EMERGENCY LIGHTS AT SEAT ROWS 16D TO 25D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 16D TO 25D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,174 hrs

SJU - 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 — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,174 hrs

SJU - EMERGENCY LIGHTS AT SEAT ROWS 9D TO 15D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 9D TO 15D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

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

Part: PIN — LOOSE (LIGHT CONNECTOR)

MIA - EMERGENCY LIGHT AT SEAT 29D INOPERATIVE. RESET LOOSE PIN AT EMERGENCY LIGHT CONNECTOR FOR SEAT 29D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT 32D INOPERATIVE. SECURED WIRES AT CONNECTOR FOR EMERGENCY LIGHT AT SEAT 32D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LINE — FAILED (UPLOCK ACTUATOR)

DFW - TWENTY MINUTES AFTER TAKEOFF LEFT HYDRAULIC SYSTEM LOST ALL FLUID. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED RIGHT MAIN LANDING GEAR UNLOCK ACTUATOR PRESSURE LINE. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

JFK - EMERGENCY LIGHTS AT SEATS 26D TO 36D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEATS 26D TO 36D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SKIN — SCRATCHED (FUSELAGE)

TUL - SCRATCH ON THE CROWN SKIN AT STATION 700 JUST INBOARD OF, AND ADJACENT TO, STRINGER 2L. AFTER SCRATCH WAS BLENDED THE DEPTH OF THE BLEND MEASURED 0.027 INCH. REPAIRED PER REPAIR DOUBLER ESO 90309.

Part: SPRING — OUT OF ADJUST (GIRT BAR)

DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, TWO GIRT BAR SPRINGS OUT OF ADJUSTMENT. ADJUSTED TWO GIRT BAR SPRINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEPARTED (FUSELAGE)

DFW - FLT 2075 - EN ROUTE MCO-DFW, EMERGENCY EXIT LIGHT FOR L-3 DOOR FELL OFF IN FLIGHT. AIRCRAFT LANDED IN DFW WITHOUT INCIDENT. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

DFW - FOUND EMERGENCY EXIT SIGN BETWEEN AFT LAVATORIES INOPERATIVE. REPAIRED BROKEN WIRE AT R4 DOOR FORWARD SIDEWALL FLOOR LEVEL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (ROW 16D)

TPA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ON SIDE OF SEAT 16D WILL NOT TEST. RECONNECTED SEAT TO WALL CONNECTOR FOR SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: DECK PLATE — CORRODED (BS 1681/1720)

AFW - DECK PLATE HAS CORROSION BLENDED BEYOND SRM LIMITS. CYCLES, 5,937. (X)

Part: FLOOR BEAM — CORRODED (BS 365)

AFW - FLOOR BEAM AT STA 365 FROM RBL 6 TO RBL 18 HAS CORROSION REMOVED BEYOND SRM LIMITS. PER MRB 757-646. CYCLES, 5,937. (X)

Part: HANDLE PAN — GOUGED (L-1 DOOR)

AFW - L-2 DOOR HANDLE PAN HAS SMALL GOUGE. AFTER BLENDING, IS BEYOND LIMITS. PER MRB 757-648. CYCLES, 5,937. (X)

Part: SUPPORT — GOUGED (T/E FLAPS)

AFW - BEAM-BELL CRANK SUPPORT-INBOARD MAIN FLAP RT WING HAS GOUGE BLENDED. PARENT MATERIAL 0.130 INCH, MINIMUM MATERIAL 0.117 INCH. PER MRB 757-647. CYCLES, 5,937. (X)

Part: FLOOR BEAM — CORRODED (BS 1640)

AFW - TWO AREAS OF CORROSION REMOVED ON FLOOR BEAM STA 1640, LBL 2 AND RBL 57 BEYOND SRM LIMITS. CYCLES, 5,937. (X)