N668AA

Part: ACTUATOR — INOPERATIVE (LE SLAT) · airframe 62,851 hrs · 21,985 cycles

MIA - CREW REPORTED LEADING EDGE SLAT DISAGREE MESSAGE ON APPROACH. EMERGENCY DECLARED FLIGHT LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER 20 ROTARY SLAT DRIVE ACTUATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: COUPLING — BROKEN (BLEED AIR SYS) · airframe 61,064 hrs · 21,310 cycles

MCO - CREW REPORTED LEFT BLEED DUCT LEAK INDICATION AND DUCT LEAK LOW PRESSURE STATUS MESSAGE. EMERGENCY DECLARED FLIGHT LANDED MCO WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED BROKEN COUPLING AT LEFT ENGINE UPPER STRUT / PNEUMATIC DUCT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: DOOR — DENTED (CARGO BAY) · airframe 60,956 hrs · 21,267 cycles

DENT WITH SCRATCH ON NUMBER 1 CARGO DOOR. DOUBLER INSTALLED PER SRM 52-30-01-02R AND ESO 90114.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 60,956 hrs · 21,267 cycles

DAMAGE AT LOWER FORWARD CORNER ON NUMBER 2 CARGO DOOR. ACCOMPLISHED REPAIR PER ESO 90121.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,956 hrs · 21,267 cycles

SUPPORT AT STATION 1681 CORRODED. ACCOMPLISHED REPAIR PER AARD 51-10-05-1.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,956 hrs · 21,267 cycles

SUPPORT CORRODED AT STATION 1650. REPLACED SUPPORT PER SRM 51-40-02-0G.

Part: SKIN — DAMAGED (CARGO DOOR) · corrosion level 2 · airframe 60,956 hrs · 21,267 cycles

NUMBER 2 CARGO DOOR LOWER AFT OUTER SKIN IS DAMAGED. INSTALLED STRAP DOUBLER LOCATED ON THE ANGLE TO REINFORCE AREA OF SHORT EDGE DISTANCE PER EA COMP-52-019501.

Part: SLAT — CORRODED (RT WING) · corrosion level 2 · airframe 60,956 hrs · 21,267 cycles

NUMBER 8 SLAT 58.25 INCHES FROM INBOARD END CORRODED. CORROSION REMOVED PER SRM 51-10-02-0G. FABRICATED AND INSTALLED FLUSH DOUBLERS PER AARD 57-43-00-1.

Part: SLAT — CORRODED (RT WING) · corrosion level 2 · airframe 60,956 hrs · 21,267 cycles

NUMBER 8 SLAT 44.5 INCHES FROM OUTBOARD END CORRODED. FABRICATED AND INSTALLED FLUSH DOUBLERS PER AARD 57-43-00-1.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 60,956 hrs · 21,267 cycles

NUMBER 2 CARGO DOOR LOWER AFT OUTER SKIN IS DAMAGED. CUT OUT DAMAGED AREA OF OUTER SKIN AT LOWER AFT CORNER AND INSTALLED REPAIR DOUBLER PER ESO 90121.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 60,956 hrs · 21,267 cycles

UPPER SKIN ON NUMBER 8 LEADING EDGE SLAT CORRODED AT OUTBOARD TRACK. CORROSION REMOVED PER SRM 51-10-02-0G. FABRICATED AND INSTALLED FLUSH DOUBLERS PER AARD 57-43-00-1.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 60,956 hrs · 21,267 cycles

LEFT WING NUMBER 2 SLAT HAS CORROSION ON LOWER SKIN AT OUTBOARD MAIN TRACK APPROXIMATELY 30 INCHES INBOARD FROM OUTBOARD END OF SLAT. REMOVED CORROSION FROM SKIN PER SRM 57-43-01-1A AND INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 60,956 hrs · 21,267 cycles

LEFT WING NUMBER 2 SLAT HAS CORROSION ON LOWER SKIN AT OUTBOARD MAIN TRACK APPROXIMATELY 30 INCHES INBOARD FROM OUTBOARD END OF SLAT. INSTALLED FLUSH DOUBLER PER AARD 57-43-00-1.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 60,956 hrs · 21,267 cycles

NUMBER 2 CARGO DOOR- LOWER FORWARD CORNER OF OUTER SKIN IS DAMAGED. TRIMMED OUT DAMAGE FABRICATED DOUBLER AND INSTALLED PER ESO 90101.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 60,956 hrs · 21,267 cycles

LEFT WING NUMBER 2 SLAT HAS CORROSION ON LOWER SKIN AT INBOARD MAIN TRACK APPROXIMATELY 31 INCHES OUTBOARD FROM INBOARD END OF SLAT. INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 60,956 hrs · 21,267 cycles

LEFT WING NUMBER 2 SLAT HAS CORROSION ON LOWER SKIN AT INBOARD MAIN TRACK APPROXIMATELY 31 INCHES OUTBOARD FROM INBOARD END OF SLAT. REMOVED CORROSION FROM SKIN PER SRM 57-43-01-1A AND INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 60,956 hrs · 21,267 cycles

NUMBER 1 CARGO DOOR OUTER SKIN HAS DENT WITH A SCRATCH IN IT APPROXIMATELY 12 INCHES FORWARD OF AFT EDGE 3 INCHES BELOW NUMBER 4 BEAM. INSTALLED DOUBLER PER SRM 52-30-01-2 R.

Part: STRUCTURE — CRACKED (R2 DOOR) · airframe 60,956 hrs · 21,267 cycles

RIGHT NUMBER 2 DOOR CHORD AT UPPER HINGE CUTOUT IS CRACKED. INSTALLED DOUBLER REPAIR PER EA COMP 52-019343.

Part: SIGN — PEELING (CABIN) · airframe 58,660 hrs · 20,441 cycles

LEFT NUMBER 2 DOOR AFT EXIT MARKER PEELING. INSTALLED NEW EXIT MARKER AT LEFT NUMBER DOOR 2 AFT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,660 hrs · 20,441 cycles

SEAT 25D ESCAPE PATH LIGHT ONE LAMP INOPERATIVE. REPLACED LAMP FOR ESCAPE PATH LIGHT AT SEAT 25D. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,660 hrs · 20,441 cycles

SEAT 19D ESCAPE PATH LIGHT ONE LAMP INOPERATIVE. REPLACED LAMP FOR ESCAPE PATH LIGHT AT SEAT 19D. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 58,660 hrs · 20,441 cycles

EXIT SIGN AT FLIGHT DECK ENTRY INOPERATIVE. REPLACED ALL THE LAMPS IN THE FPRWARD CABIN CENTER EXIT SIGN AT FLIGHT DECK ENTRY. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,660 hrs · 20,441 cycles

SEAT 24D ESCAPE PATH LIGHT ONE LAMP INOPERATIVE. REPLACED LAMP FOR ESCAPE PATH LIGHT AT SEAT 24D. OPS CHECK NORMAL.

Part: LENS — MISSING (CABIN) · airframe 58,660 hrs · 20,441 cycles

SEAT 12D ESCAPE PATH LIGHT MISSING LENS. REPLACED LIGHT ASSEMBLY FOR ESCAPE PATH LIGHT AT SEAT 12D. OPS CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,660 hrs · 20,441 cycles

SEAT 14D ESCAPE PATH LIGHT ONE LAMP INOPERATIVE. REPLACED LAMP FOR SEAT 14D ESCAPE PATH LIGHT. OPS CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,660 hrs · 20,441 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,474 hrs · 19,698 cycles

CRACK IN FLOORBEAM STATION 700 LEFT BUTTLINE 24 AND LEFT BUTTLINE 48. INSTALLED DOUBLER PER AARD 53-30-51-2 REPAIR 2 AND CARD 53-98-01.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 56,474 hrs · 19,698 cycles

PREVIOUS BLENDOUT OF CORROSION ON NUMBER 8 SLAT 91 INCHES FROM OUTBOARD END. INSTALLED FLUSH DOUBLER ON UPPER SKIN 91 INCHES FROM OUTBOARD END PER AARD 57-43-00-1.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,971 hrs · 19,179 cycles

SEAT MOUNTED EMERGENCY LIGHTS ROW 9 TO 15 INOPERATIVE DURING TEST. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS ROW 9 TO 15.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

JFK EMERGENCY SLIDE LIGHT AT EXTERIOR RIGHT NUMBER 1 DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY SLIDE LIGHT AT EXTERIOR RIGHT NUMBER 1 DOOR.

Part: LENS — MISSING (CABIN)

DFW - AFT LAVATORY EMERGENCY EXIT LIGHT MISSING LENS. REPLACED LENS FOR AFT LAVATORY EMERGENCY EXIT LIGHT.

Part: HOSE — LEAKING (HYD SYSTEM) · airframe 50,959 hrs

MCO INFLIGHT T2064/25MAY. LEFT HYDRAULIC SYSTEM QUANTITY LOSS ON SHORT FINAL. LANDED MCO WITHOUT INCIDENT. FOUND FLEX LINE FAILURE AT LEFT WHEEL WELL. REPLACED HYDRAULIC FLEX LINE, ENGINE DRIVEN PUMP AND FILTERS. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: LINE — LEAKING (FUEL SYSTEM) · airframe 50,007 hrs

RDU INFLIGHT T1671/01FEB JFK TO CUN - FUEL DISAGREE LIGHT ILLUMINATED. SUSPECT FUEL LEAK IN LEFT ENGINE. LANDED RDU WITHOUT INCIDENT. REPLACED LEFT ENGINE HIGH PRESSURE FUEL LINE AND O-RINGS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,966 hrs

DFW - EMERGENCY LIGHT AT LEFT BULLNOSE AT SEAT ROW 12 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT BULLNOSE AT SEAT ROW 12. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,966 hrs

DFW - EXTERNAL EMERGENCY LIGHT AT LOWER AFT DOOR INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY LIGHT AT LOWER AFT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,966 hrs

DFW - EMERGENCY EXIT LIGHT AT RIGHT AND LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK AT M10758 FOR EMERGENCY LIGHT AT RIGHT AND LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

MIA - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 13D INOPERATIVE. REPLACED LAMP FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 13D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHTS)

MIA - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 13D MISSING LENS. REPLACED LENS FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 13D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (CABIN)

DFW - EMERGENCY LIGHT AT SEAT 14D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 14D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT 35D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 35D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (CABIN)

SFO CEILING EMERGENCY LIGHTS FROM ROWS 28 TO 32 INOPERATIVE. REPLACED BATTERY PACK B5 107 FOR CEILING EMERGENCY LIGHTS FROM ROWS 28 TO 32. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: TRANSDUCER — INOPERATIVE (ANTI-SKID SYS)

MIA - INFLIGHT AFTER TAKEOFF UPPER EICAS ANTI-SKID MESSAGE AND LIGHT CAME ON ANNUNCIATOR PANEL. AFTER GEAR DOWN, LIGHT AND MESSAGE STAYED ON THROUGH ROLL OUT. BOTH ARE INTERMITTENT. REPLACED NUMBER 7 TRANSDUCER FOR ANTI-SKID AUTOBRAKE CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SPRING — DAMAGED (GIRT BAR)

DURNG ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, ONE GIRT BAR SPRING NEEDS REPLACEMENT. REPLACED ONE GIRT BAR SPRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: HOSE — CRACKED (MLG ACTUATOR)

DFW - FLT 1265 - EN ROUTE SAT-DFW, COMPLETE LOSS OF LEFT HYDRAULIC SYSTEM QUANTITY. EMERGENCY DECLARED. LANDED DFW WITHOUT INCIDENT. REPLACED RIGHT MLG LOCK ACTUATOR HOSE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: HYDRAULIC LINE — CRACKED (HYD SYSTEM)

DFW - FLT 1089 - EN ROUTE DFW-PDX, LEFT HYDRAULIC QUANTITY LOSS. RETURNED AND LANDED DFW WITHOUT INCIDENT. REPLACED LEFT MLG SIDE STRUT ACTUATOR DOWN HOSE WITH TEMPORARY HOSE. SERVICED LEFT HYDRAULIC SYSTEM RESERVOIR. LEAK AND OPERATIONS CHECKED NORMAL. (M)

Part: LIGHT — INOPERATIVE (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT DOOR 1R INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT 1R DOOR. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: MODULE — DEFECTIVE (CABIN)

SNA - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST AND COACH CLASS WERE INOPERATIVE. REPLACED EMERGENCY FLOOR PATH LIGHTING FORWARD AND AFT MODULES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PAN — GOUGED (R4 DOOR)

AFW - R-4 DOOR HANDLE PAN HAS A SMALL GOUGE. AFTER BLENDING, IS BEYOND SRM LIMITS. REFINISH THE BLEND OUT PER REF 'C', SRM SECTION. TST: 14,753.23 HOURS. CYCLES, 5,396. (X)

Part: SILL — CORRODED (CARGO DOORWAY)

AFW - AFT CARGO DOOR LOWER SILL INNER CHORD HAD CORROSION. BLENDED BEYOND SRM LIMITS. BLEND OUT IAW 757 SRM 5-10-00. ALODINE AND APPLY TWO COATS OF PRIMER. FILL BLENDED AREA WITH BMS5-92 TYPE 10R3. APPLY DINOL OVER AREA. REINSTALL SAME TYPE FASTENER AS REMOVED. TST: 14,753.23 HOURS. CYCLES, 5,396. (X)

Part: FLOOR BEAM — CORRODED (BS 324)

AFW - FLOOR BEAM AT STA 324 HAS CORROSION ON UPPER SURFACE. MATERIAL REMAINING IS BEYOND SRM ALLOWABLE LIMITS. BLEND OUT CORROSION. ALODINE, APPLY TWO COATS PRIMER AND FILL WITH BMS5-92. TST: 14,753.23 HOURS. CYCLES, 5,396. (X)

Part: FLOORBEAM — CORRODED (BS 365)

AFW - FOUND FLOORBEAM AT STATION 365 HAD 2 AREAS OF CORROSION BEYOND SRM LIMITS. ALODINED ALL BLENDED AREAS. FABRICATE STRAPS USING .050 301.5 HARD STAINLESS STEEL. APPLY 2 COATS PRIMER TO STRAPS AND BEAM. FILL ALL BLEND AREAS WITH BMS5-92. INSTALL STRAPS USING BACBACRN616 HI-LOCKS. (M)

Part: FLOORBEAM — CORRODED (BS 324)

AFW - FOUND FLOOR BEAM AT STATION 324 HAS CORROSION BEYOND SRM LIMITS. ALODINED ALL BLENDED AREAS. FABRICATE STRAPS FROM .050 301.5 HARD STAINLESS STEEL. APPLY TWO COATS PRIMER TO STRAPS AND BEAM FILL BLEND AREA WITH AMS 5092. INSTALL STRAP WITH BACB30NN6 HI-LOKS. (M)

Part: FLOOR BEAM — CORRODED (BS 1640)

AFW - FLOOR BEAM AT STA 1640 HAS CORROSION ON UPPER SURFACE. MATERIAL REMAINING IS BEYOND SRM ALLOWABLE LIMITS. ALODINE ALL BLENDED AREAS. FABRICATE STRAPS FROM .050 INCH 301 1/2 HARD STAINLESS STEEL. APPLY TWO COATS PRIMER TO STRAPS AND FLOOR BEAM. FILL ALL BLENDED AREAS WITH MS5-92 TYPE 10R3. INSTALL STRAPS USING BACB30NW6 HILOCKS. TST: 14,753.23 HOURS. CYCLES, 5,396. (X)

Part: FLOOR BEAM — CORRODED (BS 377)

AFW - FLOOR BEAM AT STA 377 HAS CORROSION. ALODINE BLENDED AREAS, FABRICATE STRAPS .050 INCH 301 1/2 HARD STAINLESS STEEL. APPLY TWO COATS PRIMER TO STRAP AND FLOOR BEAM. FILL BLENDED AREA WITH BMS 5-92. INSTALL STRAP USING BACB 30NW6 HILOCKS. TST: 14,753.23 HOURS. CYCLES, 5,396. (X)

Part: SUPPORT — CORRODED (FUSELAGE)

AFW - FLOOR SUPPORT STRUCTURE IN SEC 41 HAS CORROSION. MATERIAL REMAINING IS BEYOND SRM ALLOWABLE LIMITS. BLENDED OUT CORROSION AT ALL LOCATIONS. ALODINED, APPLY TWO COATS PRIMER AND FILL WITH BMS5-92. TST: 14,753.23 HOURS. CYCLES, 5,396. (X)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, FOUND THE FORWARD COACH SECTION EMERGENCY EXIT FLOOR PATH EXIT PLACARD LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)