N588AA

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 62,935 hrs · 26,686 cycles

SEAT MOUNTED EMERGENCY LIGHT AT 14D INOPERATIVE. REMOVED AND REPLACED SIDEWALL TO SEAT CONNECTOR AT 14DEF. OPS CHECK NORMAL.

Part: PISTON — DEFECTIVE (NLG) · airframe 61,945 hrs · 26,193 cycles

DFW - CREW REPORTED AFTER TAKEOFF NOSE GEAR WOULD NOT RETRACT AND CABIN PRESSURIZATION WENT INTO STANDBY. EMERGENCY DECLARED LANDED DFW WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR PISTON THAT WAS BAD. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: ADC — MALFUNCTIONED (COCKPIT) · airframe 59,804 hrs · 25,176 cycles

LAX - CREW REPORTED AFTER TAKEOFF THE AUTOPILOT AUTOTHROTTLES DISENGAGED AND THE CAPTAINS FLIGHT MANAGEMENT ANNUNCIATOR/ALTIMETER WENT BLANK. EMERGENCY DECLARED RETURNED LAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED CAPTAINS CENTRAL AIR DATA COMPUTER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,858 hrs · 24,323 cycles

FRAME STATION 1446 OUTBOARD OF LONGERON 2L IS CRACKED. REPAIRED FRAME UNDER EA MD80-53-007119 AND SRM 53-03-00.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 57,858 hrs · 24,323 cycles

SHEAR TIE IS CRACKED L1-L2L. REPLACED SHEAR TIE UNDER SRM 51-30-05.

Part: MOUNT — CORRODED (GALLEY) · corrosion level 2 · airframe 57,858 hrs · 24,323 cycles

GALLEY NUMBER TWO INBOARD FORWARD TIE DOWN FITTING HAS CORROSION. INSTALLED NEW GALLEY MOUNT UNDER SRM 51-30.

Part: LONGERON — CRACKED (ZONE 200) · airframe 57,858 hrs · 24,323 cycles

LONGERON 2R IS CRACKED AT STATION 1418 APPROXIMATELY .75 INCHES LONG. REPLACED SECTION ON LONGERON 2R UNDER AARD 53-30-002.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 57,858 hrs · 24,323 cycles

SHEAR TIE CRACKED AT STATION 1451 FROM STRINGER L1L TO L2L. REPLACED SHEAR TIE UNDER AARD 51-00-00-12.

Part: FRAME — CRACKED (ZONE 200) · airframe 57,858 hrs · 24,323 cycles

FRAME IS CRACKED AT STATION 1418 LONGERON 2R AND LONGERON 2L. INSTALLED REPAIR UNDER EA MD80-53-007027 AND SRM 53-03 FIGURE 31A.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,858 hrs · 24,323 cycles

LEFT TRACK SPLICE HAS CORROSION. INSTALLED NEW TRACK SPLICE UNDER SRM 51-30-05.

Part: CUSP WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 57,858 hrs · 24,323 cycles

CUSP CORROSION AT STATION 200 RIGHT BUTTLINE 10. INSTALLED DOUBLER UNDER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,858 hrs · 24,323 cycles

CORROSION ON RIGHT CUSP MEMBRANE STATION 160-200. INSTALLED DOUBLER REPAIR UNDER AARD 53-20-00-16.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 57,858 hrs · 24,323 cycles

REMOVED FLOORBOARD SUPPORT AT RIGHT BUTTLINE 8. FOUND FLANGE CORRODED BEYOND LIMITS. INSTALLED NEW FLOORBOARD SUPPORT UNDER SRM 51-01.

Part: CARGO TRACK — CORRODED (BS 1212-1320) · corrosion level 2 · airframe 57,858 hrs · 24,323 cycles

RIGHT AFT TIE DOWN TRACK HAS CORROSION BETWEEN STATION 1212-1320 OUT OF LIMITS. INSTALLED NEW TIE DOWN TRACK UNDER AARD 51-00-00-012.

Part: BEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 57,858 hrs · 24,323 cycles

AFT CARGO DOOR BEAM CORRODED. INSTALLED DOUBLER REPAIR UNDER AARD 53-10-00-3

Part: PAN — CORRODED (ZONE 100) · corrosion level 2 · airframe 57,858 hrs · 24,323 cycles

CORROSION BELOW NUMBER ONE GALLEY AT DRAIN PAN AREA BETWEEN FLOORBEAMS STATION 148-160. INSTALLED DOUBLER UNDER AARD 53-20-00-16.

Part: WEB — DAMAGED (FUSELAGE) · airframe 57,858 hrs · 24,323 cycles

WEB INBOARD OF CARGO BEAM HAS DEEP TOOL MARKS. REMOVED DAMAGE AND INSTALLED DOUBLER REPAIR UNDER SRM 51-70-04 FIGURE 2 SHEET 2.

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 57,858 hrs · 24,323 cycles

CORROSION ON WEB ABOVE AFT CARGO DOOR BEAM STATION 1209. INSTALLED DOUBLER UNDER SRM 51-70-04.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,858 hrs · 24,323 cycles

CUSP CORROSION FROM STATION 1250 TO 1309 OUT OF LIMITS. INSTALLED NEW CUSP PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 57,858 hrs · 24,323 cycles

LEFT CUSP STATION 1285 CRACKED. INSTALLED CUSP DOUBLER REPAIR PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 57,858 hrs · 24,323 cycles

LEFT CUSP STATION 1290 CRACKED. INSTALLED CUSP DOUBLER REPAIR PER AARD 53-20-00-16.

Part: STRUCTURE — CORRODED (ZONE 100) · corrosion level 2 · airframe 57,858 hrs · 24,323 cycles

SUB FLOOR STATION 200 FORWARD OF NUMBER SIX TRACK IS CORRODED. INSTALLED DOUBLER UNDER AARD 53-20-00-16.

Part: STRAP — DAMAGED (CARGO BAY) · airframe 57,858 hrs · 24,323 cycles

MID CARGO AFT DOOR FRAME AFT STRAP IS DAMAGED BELOW THE RIGHT TIE DOWN TRACK INBOARD LANDING AT STATION 702 LONGERON 30R-26R. REPLACED STRAP UNDER AARD 53-00-00-012.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 57,858 hrs · 24,323 cycles

AFT CARGO LEFT AFT TIE DOWN TRACK CORRODED. INSTALLED NEW LEFT TIE DOWN TRACK STATION 1079-1320 UNDER SRM 51-30-01.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 57,858 hrs · 24,323 cycles

RIGHT SIDE CRACK IN CUSP AT FASTENER HOLE STATION 844. REPAIRED CRACK WITH DOUBLER UNDER AARD 53-20-00-16.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,858 hrs · 24,323 cycles

SUB FLOOR HAS CORROSION STATION 180-160 INBOARD OF NUMBER 5 SEAT TRACK AND UNDER NUMBER 1 GALLEY. INSTALLED DOUBLER UNDER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 57,858 hrs · 24,323 cycles

LEFT CUSP CRACKED STATION 225. REPLACED CUSP SHEET UNDER AARD 53-20-00-16.

Part: RIB — CRACKED (LE SLAT) · airframe 57,858 hrs · 24,323 cycles

HIGH FREQUENCY EDDY CURRENT INDICATES CRACKS ON RIGHT WING LEADING EDGE NUMBER FIVE SLAT AT BOTH OUTBOARD AND SECOND FROM OUTBOARD MOST SLAT RIBS. REPLACED BOTH NUMBER FIFTEEN OUTBOARD AND NUMBER FOURTEEN SECOND FROM OUTBOARD DAMAGED RIBS WITH NEW RIBS ON SLAT 1021 IAW SRM-57-50-13.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 57,858 hrs · 24,323 cycles

AFT CARGO DOOR NUMBER ONE BEAM AFT STOP FITTING CRACKED. REMOVED AND REPLACED AFT STOP FITTING PER ESO 80174.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 57,858 hrs · 24,323 cycles

AFT CARGO DOOR NUMBER ONE BEAM FORWARD STOP FITTING CRACKED. REMOVED AND REPLACED STOP FITTING PER ESO 80174.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 57,858 hrs · 24,323 cycles

AFT CARGO DOOR EXTERIOR SKIN HAS DENT AND GOUGE 14 INCHES FROM TOP EDGE AND 18 INCHES FROM AFT EDGE. REMOVED DENTED AND GOUGED SKIN FROM OUTER SKIN, FABRICATED REPAIR DOUBLER FROM .050" 2024 T-3, AND INSTALLED REPAIR DOUBLER WET WITH B-1422 UNDER SRM 52-05-00 FIG 1.

Part: SKIN — DENTED (FUSELAGE) · airframe 57,858 hrs · 24,323 cycles

TWO DENTS OUT OF LIMITS DUE TO BEING IN THE SAME BAY NOT MEETING SEPARATION REQUIREMENTS UNDER SRM 53-04-00 FIGURE 3B. INSTALLED DOUBLER UNDER SRM 53-04 FIGURE 12B AND AARD 53-30-00-9.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 57,858 hrs · 24,323 cycles

TUL - FORWARD CARGO DOOR FORWARD STOP BRACKET (STOP PAD FITTING) AT NUMBER THREE BEAM CRACKED. REMOVED AND REPLACED STOP BRACKET (STOP PAD FITTING) UNDER ESO 80174.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 57,858 hrs · 24,323 cycles

TUL - FORWARD CARGO DOOR AFT STOP PAD FITTING AT NUMBER ONE BEAM CRACKED. REMOVED AND REPLACED STOP PAD FITTING PER ESO 80174.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,858 hrs · 24,323 cycles

LEFT HAND WINDOW PAN STATION 1060 HAS THE UPPER AFT EAR CRACKED. INSTALLED REPAIR ANGLE UNDER AARD 53-10-00-25.

Part: WEB — CRACKED (FUSELAGE) · airframe 57,858 hrs · 24,323 cycles

WEB CRACKED AT STATION 207 L-15L. INSTALLED DOUBLER UNDER AARD 53-10-00-11.

Part: HYDRAULIC LINE — LOOSE (HYDRAULIC SYS) · airframe 57,435 hrs · 24,122 cycles

DFW - LANDING GEAR SLOW TO LOWER AND RIGHT HYDRAULIC PRESS LIGHT ILLUMINATED. LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND HYDRAULIC LEAK IN RIGHT SYSTEM TAIL. TIGHTENED HYDRAULIC LINE ON LEFT HYDRAULIC THRUST REVERSE CONTROL VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: GENERATOR — FAULTED (NR 1) · airframe 55,948 hrs

LGA INFLIGHT - CREW REPORTED NR 1 ENGINE DRIVEN GENERATOR CYCLED ON AND OFF AFTER TAKEOFF FOLLOWED BY NAVIGATION DATA AND DISPLAY GUIDANCE COMPUTER INPUT LOST. RETURNED TO LGA AND LANDED WITHOUT INCIDENT. REPLACED NR 1 ENGINE DRIVEN GENERATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,276 hrs

MIA - EMERGENCY LIGHT AT SEAT 18D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · 43,415 cycles

MIA EMERGENCY LIGHT AT SEAT 33D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 33D. SYSTEM GROUND CHECKED NORMAL OPS.

Part: BULKHEAD — DEFORMED (FUSELAGE) · airframe 54,183 hrs · 22,707 cycles

TUL - AFT PRESSURE BULKHEAD WEB DEFORMED AT STATION 1338. AREA OF DISCREPANCY IS 45 INCHES BY 28.5 INCHES. REPAIRED BULKHEAD DOME PER SRM 53 03 FIGURE 33 VIEW C ON BOTH SIDES OF AIRCRAFT PER ESO 80559.

Part: WEB — CORRODED (FUSELAGE) · airframe 54,183 hrs · 22,707 cycles

TUL - LOWER WEB AT AFT LAVATORY SERVICE COMPARTMENT AFT END AFT CARGO HAS CORROSION AT STATION 1300 TO 1320. REPLACED FOUR INSIDE DOUBLERS IN ACCORDANCE WITH ENGINEERING SPECIFICATION ORDER 80559 DATED 23 APR 2008.

Part: HOSE — LEAKING (HYD SYSTEM)

AUS INFLIGHT T1960/18NOV, RIGHT HYDRAULIC SYSTEM LOST FLUID AT CRUISE. NORMAL GEAR EXTENSION WAS USED. LANDED AUS WITHOUT INCIDENT. FOUND RIGHT HYDRAULIC RETURN LINE LEAKING AT AFT CARGO RIGHT WALL. REPLACED RIGHT HYDRAULIC RETURN LINE AT AFT CARGO RIGHT WALL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT)

SFO - FOUND EMERGENCY LIGHT AT SEAT 27D INOPERATIVE. REPINNED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 27D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT)

SFO - FOUND EMERGENCY LIGHT AT SEAT 18D INOPERATIVE. REPINNED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - FOUND TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR TAILCONE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — PINCHED (EMERGENCY LIGHT)

DFW EMERGENCY EXIT DOUBLE ARROW LIGHT ASSEMBLY ON FORWARD GALLEY AISLE WALL NEAR FLOOR INOPERATIVE. FOUND WIRE PINCHED BEHIND ONE OF CONNECTORS. CUT OFF PINCHED WIRE AND REINSTALLED CONNECTOR FOR EMERGENCY EXIT LIGHT AT FORWARD GALLEY WALL NEAR FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW CEILING EMERGENCY LIGHTS AT ROWS 3 TO 7 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROWS 3 TO 7. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT)

STL RIGHT AND LEFT EMERGENCY LIGHT AT FORWARD OVERWING EXIT INOPERATIVE. SECURED LOOSE WIRE TERMINAL ON FORWARD OVERWING EMERGENCY LIGHT POWER SUPPLY AT SEAT 20D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND FUSELAGE SKIN CRACKED AT RIVET STATION 1380 1 INCH ABOVE LEFT PYLON. INSTALLED DOUBLER PER 53-01-00, AARD 53-30-00-02. (M)

Part: WEB — DAMAGED (FUSELAGE)

TUL - FOUND LEFT TEMP CONTROL VALVE HAS WORN THROUGH DOUBLER AND INTO STATION 1380 WEB. REMOVED AND REPLACED DOUBLER ON STATION 1380 WEB BY LEFT TEMP CONTROL VALVE IAW AARD 53-40-00-28. (M)

Part: SHEAR TIE — CRACKED (FUSELAGE)

TUL - FOUND BOTH LEFT AND RIGHT SHEAR TIE DOUBLERS ON AFT SIDE OF FRAME 1451 CRACKED BELOW VERTICAL STAB ATTACH ANGLES. REPLACED SHEAR TIE DOUBLERS WITH NEW PARTS. REMOVED AND REPLACED PER SRM 53-01-00. (M)

Part: WEB — DAMAGED (FUSELAGE)

TUL - FOUND .5 INCH HOLE IN CUSP UNDER SEAT TRACK NR 1 AT STATION 1197. INSTALLED DOUBLER PER AARD 53-00-00-02. (M)

Part: WEB — DAMAGED (FUSELAGE)

TUL - FOUND SUBFLOOR DAMAGED IN SEVERAL AREAS STATION 213-217 RBL 10-19. INSTALLED REPAIR DOUBLER PER AARD 53-00-00-2. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

TUL - FOUND STATION 200, SEAT TRACK 5-6, FLOOR/GALLEY SUPPORT ANGLE CORRODED. INSTALLED NEW SERVICEABLE FLOORBOARD SUPPORT ANGLE AT STATION 200. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 1 SEAT TRACK CORRODED AT NUTPLATE ATTACH AREA FOR TIE DOWN BOLT. INSTALLED PLUG PER SRM 51-10-3. (M)

Part: STRUCTURE — CRACKED (FUSELAGE)

TUL - FOUND CRACK AND CORROSION UNDER G-1 GALLEY DRAIN PAN ALONG AND UNDER BUTT JOINT. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-00-00-02. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND DENT IN FUSELAGE STATION 1198 LONGERON 17L. INSTALLED TWO NEW DOUBLER PER SRM 53-04 FIG 38. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON RIGHT CUSP AT STATION 488, LOWER SIDE. INSTALLED DOUBLER AT RT CUSP STATION 488 PER SRM 53-01 53-01-FIG 4-3. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON RIGHT CUSP AT STATION 565, LOWER SIDE. INSTALLED DOUBLER PER SRM 53-00-00-02. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 2 SEAT TRACK CORRODED INSIDE TRACK AT STATION 1190. INSTALLED SEAT TRACK PLUG IN SEAT TRACK NR 2 STATION 1190 PER AARD 53-20-00-10. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT AT 20F INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SOCKET — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHT AT SEAT 15D INOPERATIVE. REPLACED EMERGENCY EXIT ESCAPE PATH LIGHT SOCKET AT SEAT 15D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SELECTOR — DEFECTIVE (COCKPIT)

DFW - FLT 1110 - AFTER LEVELING OFF AT 33,000 FT FOR ABOUT 2 MINUTES THE MASTER WARNING LIGHT ILLUMINATED FROM THE CABIN ALTIMETER WARNING LIGHT. THE CABIN WAS CLIMBING AT ABOUT 600 FT PER MINUTE. STARTED EMERGENCY DESCENT AND CAUGHT THE CABIN AT ABOUT 12,500 FT. LEVEL AT 10,000 FT. MANUAL WOULD AFFECT THE PRESSURIZATION BUT NOT TO THE EXTENT IT SHOULD HAVE. LANDED DFW WITHOUT INCIDENT. REPLACED PRESSURIZATION SELECTOR PANEL, OUTFLOW VALVE ACTUATOR AND MOTOR, AND NUMBER 1 PRESSURIZATION CONTROLLER. ACCOMPLISHED BITE AND OPERATIONS CHECKS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BYPASS HANDLE — NOT CLOSED (COCKPIT)

YUL - FLT T2037 - AFTER TAKEOFF YUL EN ROUTE ORD, LANDING GEAR WOULD NOT RETRACT WITH GEAR HANDLE IN UP POSITION. RETURNED AND LANDED YUL WITHOUT INCIDENT. STOWED GEAR DOOR BYPASS HANDLE IN FULL CLOSED LOCKED POSITION. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)