N14061

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT ROWS 7G TO 18G INOPERATIVE. REPLACED BATTERY PACK AT NUMBER TWO DOOR FOR EMERGENCY LIGHT AT SEAT 7G TO 18G. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

MIA - EMERGENCY LIGHTS AT SEAT ROWS 19G TO 28G INOPERATIVE. REPLACED BATTERY PACK AT NUMBER THREE DOOR FOR EMERGENCY LIGHTS AT SEAT ROWS 19G TO 28G. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: JACKSCREW — INOPERATIVE (SLATS)

JFK INFLIGHT - SLATS DID NOT EXTEND FOR LANDING. LANDED JFK WITHOUT INCIDENT. REPLACED NUMBER SIX LEFT JACKSCREW. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT LEFT NUMBER THREE DOOR INOPERATIVE. REPLACED BATTERY PACK AND MODULE ASSEMBLY FOR INOPERATIVE EMERGENCY LIGHT AT LEFT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — BROKEN (EMERGENCY LIGHTS)

MIA - EMERGENCY LIGHT AT SEAT 22C INOPERATIVE. REPAIRED BROKEN WIRE FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — BROKEN (CABIN)

MIA - EMERGENCY LIGHT AT SEAT 12C BROKEN. REPLACED EMERGENCY LIGHT ASSEMBLY FORE SEAT 12C. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHTS AT SEATS 21G AND 22G INOPERATIVE. REPLACED CONNECTOR FOR INOPERATIVE EMERGENCY LIGHTS AT SEATS 21G AND 22G. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

JFK - FOUND RIGHT HAND AISLE EMERGENCY LIGHTS DIM BETWEEN SEATS 19 TO 31. REPLACED BATTERY PACK FOR RIGHT HAND SECTION THREE EMERGENCY PATH LIGHTING BETWEEN SEATS 19 TO 31. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

JFK - SEAT MOUNTED EMERGENCY LIGHTS IN RIGHT HAND MID CABIN AND LEFT HAND FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACKS FOR SEAT MOUNTED EMERGENCY LIGHTS IN RIGHT HAND MID CABIN AND LEFT HAND FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — BROKEN (CABIN)

MIA - EMERGENCY LIGHT AT SEAT 15C BROKEN. REPLACED EMERGENCY LIGHT ASSEMBLY FOR SEAT 15C. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: DRIVE UNIT — INOPERATIVE (LE SLATS)

MIA - AIRCRAFT DIVERTED TO MIA WITH DUAL LEADING EDGE INDICATION PROBLEMS. REPLACED POWER DRIVE UNIT AND NUMBER THREE JACKSCREW. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SOCKET — INOPERATIVE (EMERGENCY LIGHT)

JFK - EMERGENCY LIGHT OUT OF ITS SOCKET AT SEAT 27G. REPLACED EMERGENCY LIGHT SOCKET AT SEAT 27G. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: COMPUTER — INOPERATIVE (FEEL LIMITER)

SJU - INFLIGHT T661 ON CLIMB FLIGHT RECEIVED A DUAL RUDDER LIMITER FAULT. RETURNED TO SJU AND LANDED WITHOUT INCIDENT. NO EMERGENCY AND NOT OVERWEIGHT. REPLACED NUMBER 1 FEEL LIMITER COMPUTER AND RESET NUMBER 2 COMPUTER. SYSTEM GROUND CHECKED NORMAL OPERATION. SECOND AIR INTERRUPT ON DEPARTURE FOR DUAL RUDDER LIMITER FAULT. RETURNED TO SJU AND LANDED WITHOUT INCIDENT. REPLACED NUMBERS 1 AND 2 FEEL LIMITER COMPUTERS AND RELAYS AND VARIABLE STOP ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PUMP — INOPERATIVE (RT WING)

AIRCRAFT DIVERTED TO MIA DUE TO RT WING FUEL DISTRIBUTION PROBLEM. REMOVED AND REPLACED RT CENTER PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE HARNESS — FAULTY (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 23G INOPERATIVE. REPLACED SEAT HARNESS AT SEATS 23G AND 28G. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — INOPERATIVE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 9G INOPERATIVE. SECURED EMERGENCY EXIT LIGHT WIRE CONNECTOR AT 9G. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — INOPERATIVE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 28G INOPERATIVE. SECURED EMERGENCY EXIT LIGHT PLG AT SEAT 28G. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

MIA - FOUND EMERGENCY LIGHT AT SEAT 28G INOPERATIVE. SECURED CONNECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: RIB — CORRODED (KRUEGER FLAP)

KRUEGER FLAP JACK RIB HORIZONTAL SUPPORT FITTING CORRODED ON AFT SIDE BETWEEN ACT ATTACH POINTS. REMOVED CORROSION, TREATED IAW ESO 30595.

Part: SKIN — CORRODED (WING)

INTERGRANULAR CORROSION IN WING SKIN BETWEEN RIBS 28-29 JUST AFT OF REAR SPAR. AREA WAS BLENDED, FLAP, PEENED AND TREATED IAW FSO 30595.

Part: ADC — FAULTY (E/E BAY)

MIA - FLT 1901 - EN ROUTE MAI-SDQ - LEFT CAPTAINS AIRSPEED ABOUT 50 KNOTS SLOW AT 250 KNOTS. 20 KNOTS SLOW AT 150 KNOTS. RETURNED AND LANDED MIA WITHOUT INCIDENT. REPLACED NR 1 AIR DATA COMPUTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (R1 DOOR)

JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT R1 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT R1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (L4 DOOR)

JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L4 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT L4 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: HOSE — LEAKING (HYD SYSTEM)

JFK - FLT 1152 - EN ROUTE MIA-JFK, ON SHORT FINAL GREEN HYDRAULIC SYSTEM DECREASED TO ZERO. HYDRAULIC PUMPS WERE IMMEDIATELY SHUT OFF. LANDED JFK WITHOUT FURTHER INCIDENT. REPLACED LEFT SIDE MAIN LANDING GEAR PRESSURE FLEXIBLE HOSE. SERVICED GREEN SYSTEM. NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PIN — LOOSE (L1 DOOR)

JFK - DURING OVERNIGHT MAINTENANCE, FORWARD EMERGENCY EXIT LIGHT AT L1 DOOR INOPERATIVE. RE-SECURED PIN AT FORWARD EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: TRACK — CORRODED (CABIN) · airframe 32,964 hrs · 13,073 cycles

TUL - TRACK ''D'', LEFT, IS CORRODED FORWARD OF FRAME 74. BLENDED OUT CORROSION TO A DEPTH OF .065 INCH. REPAIRED PER ESO 30595 DATED 5-18-00. (X)

Part: SEAT TRACK — CORRODED (CABIN) · airframe 32,963 hrs · 13,073 cycles

TUL - CORROSION ON NR 1 SEAT TRACK AT FOWARD OUTBOARD LAVATORY MOUNT. REMOVED AND BLENDED OUT CORROSION PER SRM 51-74-10. ALODINED, PRIMED, AND PAINTED FORWARD OUTBOARD MOUNT HOLE. (X)

Part: BULKHEAD — CORRODED (CARGO BAY) · airframe 32,963 hrs · 13,073 cycles

TUL - CORROSION ON FORWARD CARGO BULKHEAD FR 39 BETWEEN L53R AND L54R. CUT OUT CORROSION AND REPAIRED PER SRM 53-15-17, PAGES 206 AND 208. (X)

Part: SEAT TRACK — CORRODED (CABIN) · airframe 32,963 hrs · 13,073 cycles

TUL - CORROSION ON AFT LAVATORY MOUNT OUTBOARD FRAME 33 TRACK NR 1. REMOVED CORROSION AND BLENDED. INSTALLED DOUBLER STRAP PER A300 AARD 53-20-00. ALODINED, PRIMED AND PAINTED. (X)

Part: RIB — CORRODED (RT PYLON) · airframe 32,964 hrs · 13,073 cycles

TUL - RIB CORRODED ON BOTH SIDES LOWER OUTBOARD FAIRING BOLT HOLE. REMOVED AND REPLACED WITH NEW RIB, RIB 17A, RIGHT PYLON. (X)

Part: TRACK — CORRODED (CABIN FLOOR) · airframe 32,964 hrs · 13,073 cycles

TUL - TRACK ''E'' IS CORRODED BETWEEN FRAMES 71-72. BLENDED OUT CORROSION PER SRM 51-7440-2 TO .017 INCH. ALODINED, PRIMED AND PAINTED BLENDED AREA PER 51-21-00 AND PER ESO 30595 DATED 5-18-00. (X)

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 32,964 hrs · 13,073 cycles

NR 2 SEAT TRACK AT LAVATORY MOUNT HOLES CORRODED. REMOVED CORROSION, TREATED, PRIMED, PAINTED, AND INSTALLED STRUCTURAL STRAPS ON THE FORWARD AND AFT LAVATORY MOUNT HOLES PER AARD 53-20-00. (X)

Part: SUPPORT BRACKET — CORRODED (CABIN) · airframe 32,964 hrs · 13,073 cycles

TUL - SUPPORT BETWEEN RIGHT TRACK D AND E CORRODED FORWARD OF FRAME 72. BLENDED OUT CORROSION TO A DEPTH OF .017 INCH ALODINED, PRIMED AND PAINTED PER SRM 51-21-40 AND PER ESO 30595 DATED 5-18-00. (X)

Part: FITTING — CORRODED (CARGO BAY) · airframe 32,964 hrs · 13,073 cycles

TUL - CORROSION ON ROLLER TRAY SUPPORT FITTING UNDER NR 1 ROLLER TRAY AT FR 38.2. INSTALLED NEW ROLLER TRAY SUPPORT FITTING PER SRM 51-72-10-0 PAGE 1. (X)

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 32,964 hrs · 13,073 cycles

TUL - NR 3 SEAT TRACK CORRODED. REMOVED AND REPLACED SECTION OF SEAT TRACK PER SRM 51-72-10 AND INSTALLED SPLICE PER SRM 53-10-16. (X)

Part: SUPPORT BRACKET — CORRODED (CABIN) · airframe 32,964 hrs · 13,073 cycles

TUL - LAVATORY L CORRODED ON INBOARD TIE-DOWN SUPPORT AT FORWARD AND AFT MOUNT HOLES. REMOVED AND REPLACED LAVATORY TIE-DOWN SUPPORT PER SRM 51-72-10, FRAMES 31-33. (X)

Part: TRACK — CORRODED (CABIN) · airframe 32,964 hrs · 13,073 cycles

TUL - TRACK ''C'', RIGHT, HAD CORROSION AFT OF FRAME 74. BLENDED OUT CORROSION PER SRM 51-74-10, .080 INCH KEEP. REPAIRED PER ESO 30575 DATED 5-18-00. (X)

Part: GALLEY TRACK — CORRODED (AFT CABIN FLOOR) · airframe 32,964 hrs · 13,073 cycles

TUL - TRACK ''B'', LEFT, HAD CORROSION AT AFT GALLEY MOUNT HOLE. BLENDED OUT CORROSION ,045 INCH DEEP, REPAIRED PER ESO 30595 DATED 5-18-00, FRAMES 79-80. (X)

Part: TRACK — CORRODED (CABIN) · airframe 32,964 hrs · 13,073 cycles

TUL - RIGHT TRACK ''D'' AFT OF FRAME 73 HAD CORROSION. BLENDED CORROSION PER SRM 51-74-10-2 TO A DEPTH OF .020 INCH. REPAIRED PER ESO 30595 DATED 5-18-00. (X)

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 32,964 hrs · 13,073 cycles

TUL - NR 8 SEAT TRACK CORRRODED. REMOVED AND REPLACED SEAT TRACK AND SEALED AROUND BRACKETS PER SRM 51-72-10-0. FRAME 33, STA 1870 TO STA 2135. (X)

Part: SEAT TRACK — CORRODED (CABIN) · airframe 32,964 hrs · 13,073 cycles

TUL - CORROSION ON NR 2 TRACK, FRAME 33, AFT LAVATORY MOUNT. REMOVED AND BLENDED CORROSION. REF: SRM 51-74-10. INSTALLED STRAP ON AREA PER AARD 53-20-00-2 ON AFT MOUNT. TREATED AND PRIMED AND PAINTED. (X)

Part: TRACK — CORRODED (CABIN) · airframe 32,964 hrs · 13,073 cycles

TUL - TRACK ''B'', LEFT, HAD CORROSION AT GALLEY MOUNT HOLE. BLENDED OUT CORROSION .050 INCH DEEP, REQUIRED PER ESO 30595 DATED 5-18-00. (X)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND TRACK D RIGHT IS CORRODED BETWEEN FRAME 73-74. INSTALLED NEW TRACK PER SRM 51-72-10-0. (M)

Part: PRIORITY VALVE — LEAKING (FUSELAGE)

JFK - FLT 679 - AFTER TAKEOFF, CREW REPORTED SMOKE IN THE CABIN. RETURNED AND LANDED JFK WITHOUT FURTHER INCIDENT. REPAIRED HYDRAULIC LEAK AT PRIORITY VALVE UNION. SYSTEM GROUND CHECK NORMAL OPERATION. PERFORMED PACK BURNOUT AND REPLACED COALESCER BAGS. REPLACED ALL THREE SMOKE DETECTORS AS A PRECAUTION. (M)

Part: HORN — DEFECTIVE (EMER EXIT DOOR)

JFK - DURING OVERNIGHT MAINTENANCE R3 DOOR EMERGENCY EXIT HORN INOPERATIVE. REPLACED EMERGENCY EXIT HORN AT R3 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: ROLLER TRAY — CORRODED (FRAME 56)

TUL - NR 6 ROLLER TRAY AT FRAME 56, FORWARD TRAY CORRODED AT FASTENER AT FRAME 56. ROLLER TRAY REPLACED, REF AARD 51-10-00-3, TREATED PRIMED AND PAINTED TRAY REF SRM 51-21-00-01. (M)

Part: ROLLER TRAY — CORRODED (FRAME 58)

TUL - NR 6 FORWARD ROLLER TRAY SEGMENT CORRODED FRAME 58 SPLICE. REPLACED ROLLER TRAY SECTION REF AARD 51-10-00-3, TREATED, PRIMED AND PAINTED REF SRM 51-21-00-0. (M)

Part: STRINGER — CORRODED (FRAME 72-73)

TUL - FOUND CORROSION ON LOWER ANGLE OF STRINGER 55 FROM FRAME 72-73. REPAIRED STRINGER PER E20 30575, DATED 3-24-98. (M)

Part: STRINGER — CORRODED (FRAME 54.54.1)

TUL - FOUND CORROSION ON STRINGER 53R BETWEEN FRAME 54 AND 54.1. CUT OUT SECTION OF STRINGER 53R AND SPLICED IN NEW SECTION PER SRM 53-10-14. (M)

Part: STRINGER — CORRODED (FRAME 72-73)

TUL - FOUND CORROSION ON STRINGER 56L. INSTALLED DOUBLER REPAIR PER SRM 53-10-14-2. (M)

Part: STRINGER — CORRODED (FRAME 59)

TUL - FOUND STRINGER 55R HAS SURFACE CORROSION ON SHEAR TIE AND STRINGER. INSTALLED NEW STRINGER SECTION PER SRM 53-10-1A PAGE 210. (M)

Part: STRINGER — CORRODED (FRAME 71/72)

TUL - FOUND CORROSION AROUND LOWER ANGLE OF STRINGER 56L BETWEEN FRAME 71 AND 72. INSTALLED DOUBLER REPAIR PER SRM 53-10-14-2. (M)

Part: STRINGER — CORRODED (CARGO COMPT)

TUL - FOUND CORROSION ON STRINGER 57 BETWEEN FRAME 54 AND 54.1. INSTALLED STRINGER SPLICE AND DOUBLERS PER SRM 53-10-14. (M)

Part: STRINGER — CORRODED (FRAME 70-71)

TUL - FOUND CORROSION ON STRINGER 57 BETWEEN FRAME 70 AND 71. INSTALLED DOUBLER ON STRINGER PER SRM 53-10-14 AFTER CORROSION WAS REMOVED. (M)

Part: FLOORBEAM — CORRODED (FRAME 58)

TUL - FOUND CORROSION ON FLOORBEAM IN AFT CARGO AT FRAME 58 BELOW NR 6 ROLLER TRAY. REPAIRED PER ESO 30595 DATED 3-18-98, AFTER CORROSION REMOVED PER SRM 51-74-10-2. (M)

Part: STRINGER — CORRODED (FRAME 60-61)

TUL - FOUND STRINGER 52L HAS CORROSION BETWEEN FRAME 60 AND FRAME 61 AFT CARGO. REPAIRED STRINGER 52L PER SRM 53-10-14. REMOVED CORROSION PER SRM 51-74-10-2. (M)

Part: FLOORBEAM — CORRODED (FRAME 56)

TUL - FLOORBEAM IN AFT CARGO AT FRAME 56 HAS CORROSION BELOW ROLLER TRAY NR 6. REMOVED CORROSION PER SRM 51-74-10-2. REPAIRED PER ESO 30595 STEP A DATED 3-19-98. (M)

Part: FLOORBEAM — CORRODED (FRAME 64)

TUL - FOUND FLOORBEAM IN BULK CARGO HAS CORROSION AT FRAME 64 RT SIDE WALL TO NR 5 ROLLER TRAY. REPAIRED PER ESO 30595, DATED 3-18-98, AFTER CORROSION REMOVED PER SRM 51-74-10-2. (M)

Part: STRINGER — CORRODED (FRAME 54 57-58)

TUL - STRINGERS 54L AND 55L HAVE CORROSION AFT CARGO BETWEEN FRAME 57.3 AND 58. REMOVED CORROSION PER SRM 51-74-10-2. REPAIRED PER ESO 30595 DATED 3-18-98 AND SRM 51-72-10-0. (M)

Part: LONGERON — CORRODED (FRAME 54)

TUL - FOUND CORROSION ON STRINGER 56L BETWEEN FRAME 54 AND 54.1. REMOVED CORRODED MATERIAL PER 51-74-10-2 AND INSTALLED DOUBLER PER SRM 53-10-14. (M)

Part: STRINGER — CORRODED (FRAME 54)

TUL - FOUND STRINGER 56L UNDER FRAME 54.2 HAS CORROSION. REMOVED CORROSION PRIMED AND TREATED. INSTALLED DOUBLER IAW SRM 53-10-14. (M)

Part: LONGERON — CORRODED (FRAME 54.1)

TUL - FOUND CORRODED LONGERON AROUND FRAME 54.1. REMOVED CORRODED SECTION OF LONGERON, SPLICED IN NEW PIECE PER SRM 53-10-14. (M)

Part: STRINGER — CORRODED (FRAME 64-65)

TUL - FOUND STRINGER 54R BETWEEN FRAMES 64 AND 65 HAS CORROSION. REMOVED CORROSION PER SRM 51-74-10-2. REPAIRED PER ESO 30595, DATED 3-18-98. (M)

Part: LONGERON — CORRODED (FRAME 58-59)

TUL - FOUND LONGERON 56R BETWEEN FRAMES 58 AND 59 HAS CORROSION ON THE LOWER SIDE. REMOVED CORRODED LONGERON SECTION AND INSTALLED NEW PIECE PER SRM 53-10-14-2. (M)

Part: STRINGER — CORRODED (FRAME 58)

TUL - FOUND CORROSION ON STRINGER 55L BETWEEN FRAME 58 AND 64. REMOVED AND REPLACED STRINGER 55L BETWEEN FRAME 58 AND 64 PER SRM 51-72-10-0. (M)

Part: STRINGER — CORRODED (FRAME 57)

TUL - FOUND CORROSION ON INBOARD FLANGE OF STRINGER 56R BETWEEN FRAME 57.2 AND 57.3. INSTALLED DOUBLER ON STRINGER PER SRM 53-10-14. (M)

Part: STRINGER — CORRODED (FRAME 58-64)

TUL - FOUND CORROSION ON STRINGER 54L FROM FRAME 58 TO 64. REMOVED AND REPLACED STRINGER 54L FROM FRAME 58 TO FRAME 64 PER SRM 51-72-10-0. (M)

Part: SPLICE — CORRODED (FRAME 65)

TUL - FOUND CORROSION ON STRINGER SPLICE ON STRINGER 55L AT FRAME 65. REMOVED AND REPLACED STRINGER SPLICE ON STRINGER 55L AT FRAME 65 PER SRM 51-72-00-10. (M)

Part: STRINGER — CORRODED (FRAME 58-59)

TUL - FOUND STRINGER 49L HAS CORROSION LOWER FLANGE AT FASTENERS BETWEEN FRAMES 58 AND 59. REMOVED SECTION OF STRINGER AND REPAIRED WITH SPLICE IAW SRM 53-10-14-2. (M)

Part: SHEAR TIE — CORRODED (FRAME 58)

TUL - FOUND CORROSION ON SHEAR TIE AT FRAME 58 BETWEEN STRINGER 52R AND 53R. REMOVED AND REPLACED SHEAR TIE PER SRM 51-72-10-0. (M)

Part: FLOORBEAM — CORRODED (FRAME 61)

TUL - FOUND CORROSION ON FLOORBEAM END FITTING RT SIDE AT FRAME 61. REMOVED AND REPLACED FLOORBEAM END FITTING PER SRM 51-72-10-0. (M)

Part: STRINGER — CORRODED (FRAME 57.3-58)

TUL - FOUND CORROSION ON STRINGER 49L BETWEEN FRAME 57.3 AND 58. REMOVED SECTION OF STRINGER AND REPAIRED WITH SPLICE IAW SRM 53-10-14-2. (M)

Part: MOUNT — DAMAGED (RT ENGINE)

TUL - FOUND LIGHT DAMAGE ON RT ENGINE PYLON FORWARD ATTACH FITTING LOWER FWD RT SIDE. BLENDED PER ESO 30595, DATED 3-16-98 AND FLAPPER PEENED WORK AREA PER SRM 51-29-00 (AA SPECIFICATION PAGE 16-19) PRIMED AND PAINTED. (M)

Part: SHEAR TIE — CORRODED (FRAME 58)

TUL - FOUND CORROSION ON SHEAR TIE AT FRAME 58 BETWEEN STRINGER 54R AND 55R. REMOVED AND REPLACED SHEAR TIE PER SRM 51-72-10-0. (M)

Part: TIE DOWN — CORRODED (FRAME 68-69)

TUL - FOUND CARGO FLOOR, THIRD TIE DOWN FROM DOOR FLOOR BRACKET HAS CORROSION. SPLICED IN REPAIR PER SRM 53-10-15-2. (M)

Part: STRINGER — CORRODED (FRAME 54-54.2)

TUL - FOUND CORROSION ON STRINGER 53L BETWEEN FRAME 54 AND 54.2. INSTALLED STRINGER SPLICE AT 53L AND INSTALLED NEW STRINGER 53L BETWEEN FRAME 54 AND FRAME 54.2 IAW SRM 53-10-14.2. (M)

Part: STRINGER — CORRODED (FRAME 71)

TUL - FOUND CORROSION ON STRINGER 54L AT FRAME 71. INSTALLED NEW SECTION OF STRINGER PER SRM 51-72-10-0. (M)

Part: BRACKET — CORRODED (LT WING)

TUL - KRUEGER FLAP BRACKET EXFOLIATED AT LOWR OUTBOARD MOUNT BORE, OUTBOARD MOUNT PAD AND FLAP TO ARM ATTACH POINT. INSTALLED NEW MOUNT PER MM 27-87-11, OPS CHECK OK. (M)

Part: SPLICE — CORRODED (FRAME 65)

TUL - FOUND CORROSION ON STRINGE R56L SPLICE AT FRAME 65. REMOVED AND REPLACED STRINGER SPLICE PER SRM 51-72-10-0. (M)

Part: SPLICE — CORRODED (FRAME 64-65)

TUL - FOUND CORROSION ON STRINGER SPLICE AT STRINGER 51L, 53L 54L AND 55L BETWEEN FRAME 64 AND 65. REMOVED AND REPLACED STRINGER SPLICED AT 51L, 53L, 54L, AND 55L PER SRM 51-72-10-0. (M)

Part: TRAY — CORRODED (CARGO COMPT)

TUL - FOUND CENTER CARGO NR 6 ROLLER TRAY HAS CORROSION DAMAGE. REMOVED AND REPLACED SECTION OF ROLLER TRAY PER SRM 51-72-10-0. (M)

Part: ANGLE — CRACKED (FUSELAGE)

TUL - RIGHT PICKUP ANGLE CRACKED. REPAIRED PICKUP ANGLE PER ESO 30595, DATED 3-11-98. (M)

Part: DOOR — CORRODED (CARGO COMPT)

TUL - FOUND NUT PLATE HOLES CORRODED AROUND FWD LOWER CORNER OF FORWARD CARGO DOOR, DOOR INNER STRUCTURE. REMOVED AND REPLACED DOUBLER PER SRM 51-72-10. (M)

Part: DOOR — CORRODED (CARGO COMPT)

TUL - FOUND NUT PLATE HOLES CORRODED AROUND FORWARD LOWER CORNER OF FORWARD CARGO DORO, DOOR INNER STRUCTURE. REMOVED AND REPLACED DOUBLER PER SRM 51-72-10. (M)

Part: SKIN — GOUGED (BS 4044)

TUL - FOUND GOUGE IN AIRCRAFT, CROWN SKIN STATION 4044 BETWEEN STRINGER 5 AND 6 LEFT SIDE. REPAIRED DAMAGED SKIN PER SRM 53-10-12 FIG 203, INSTALLED DOUBLER. (M)

Part: SUPPORT — CORRODED (FRAME 60)

TUL - FOUND CORROSION ON FLOORBEAM SUPPORT AT FRAME 60 FROM ROLLER TRAY NR 4 TO THE CARGO DOOR SILL. REMOVED AND REPLACED FLOOR CROSSBEAM PER SRM 51-72-10-0. (M)

Part: SUPPORT — CORRODED (FRAME 60)

TUL - FLOORBOARD SUPPORT AT FRAME 60 BETWEEN ROLLER TRAYS 2 AND 3 HAS CORROSION AROUND FASTENER HOLES TOP AND BOTTOM. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-72-10-0, SPLICED PER SRM 53-10-15-2. (M)

Part: SUPPORT — CORRODED (FRAME 60)

TUL - FOUND FLOOR SUPPORT AROUND FRAME 60 BETWEEN NR 1 AND NR 2 ROLLER TRAYS HAS CORROSION. REMOVED AND REPLACED CROSSBEAM PER SRM 51-72-10-0. (M)

Part: SUPPORT — CORRODED (CARGO COMPT)

TUL - FLOOR BOARD SUPPORT AT FRAME 66 HAS CORROSION AROUND FASTENER HOLES TOP AND BOTTOM. INSTALLED DOUBLER ON FLOOR SUPPORT AT OUT OF LIMIT AREA PER SRM 53-10-15. (M)

Part: SUPPORT — CORRODED (CARGO COMPT)

TUL - FLOOR SUPPORT FRAME HAS CORROSION FROM DOOR TO NR 5 ROLLER TRAY AT FRAME 63. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-72-10-0. (M)

Part: END CAP — CORRODED (CARGO COMPT)

TUL - FOUND CORROSION ON STRINGER 57 END CAP BETWEEN FRAME 65 AND 66. REMOVED AND REPLACED STRINGER END CAP PER SRM 51-72-20. (M)

Part: FLOORBEAM — CORRODED (CARGO COMPT)

TUL - FOUND CORROSION ON FLOORBEAM AT FRAME 58 UNDER NR 3 AND NR 4 ROLLER TRAYS. SPLICE IN NEW SECTION OF FLOORBEAM PER SRM 53-10-15-2. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND SEAT TRACK NR 3 BETWEEN FRAME 31 AND 32 HAS DEEP CORROSION. INSTALLED NEW SEAT TRACK FROM FRAME 25 - FRAME 33 PER AARD 51-10-00-3 AND 51-70-00-1 AND 51-40-00-1 AND SRM 51-21-20 AND 51-22-00 AND 51-24-00 AND 51-72-10-0 AND 51-40-30 AND 53-10-16-2. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOND CORROSION NR 10 SEAT TRACK BETWEEN FRAME 27 AND 28. INSTALLED NEW SEAT TRACK PER AARD 51-10-00-3 AND 51-20-00-1 AND SRM 51-10-00-0 AND 53-10-16-2 AND 51-10-00-1 AND 51-22-00. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND CORROSION UNDER LAV 'M' SUPPORT, CENTER BEAM AT FRAME 31 AND 32. REPLACED CORRODED SEAT TRACK STRUCTURE PER SRM 51-10-00-0, 53-10-16-2, 53-10-00-1, 51-22-00. (M)

Part: STRINGER — CORRODED (BS 1938-4040)

TUL - FOUND CORROSION ON STRINGER 55RT BETWEEN FRAME 59 TO FRAME 61. FABRICATED AND DRILLED SPLICE PIECES (DOUBLER) AND INSTALLED PER SRM 53-10-14-2 TREATED PRIMED AND PAINTED. (M)

Part: STRINGER — CORRODED (CABIN)

TUL - FOUND STRINGER SPLICE AND STRINGER 51L FORWARD SIDE OF FRAME 65 HAS CORROSION. REMOVED AND REPLACED STRINGER END SPLICE WITH NEW PART PER SRM 51-72-10-0. (M)

Part: SPLICE — CORRODED (CARGO COMPT)

TUL - FOUND STRINGER SPLICE 51L FORWARD OF FRAME 65 HAS CORROSION. REMOVED AND REPLACED STRINGER SPLICE 51L PER SRM 51-72-10-0. (M)

Part: STRINGER — CORRODED (CARGO COMPT)

TUL - STRINGER 56 RT HAS CORROSION LOWER FLANGE AROUND FASTENER. REMOVED CORROSION, INSTALLED SPLICES PER SRM 53-10-14-2. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - NR 7 SEAT TRACK CORRODED BETWEEN FRAME 15 AND 16. NR 7 SEAT TRACK CORRODED BETWEEN FRAME 16 AND 16A. REPLACED NR 7 SEAT TRACK FROM FRAME 15A TO FRAME 19 PER SRM 51-72-10-0. (M)

Part: CONNECTOR — DEFECTIVE (CABIN)

MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS FROM PAX SEAT ROW 6B TO 11B INOPERATIVE. REPAIRED BROKEN EMERGENCY FLOOR LIGHT STRIP CONNECTOR AT PAX SEAT ROW 6B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

MIA - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT PAX SEATS 2AB THROUGH 5AB INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 2AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BALLAST — DEFECTIVE (CABIN)

JFK - DURING OVERNIGHT CHECK, L2 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED L2 DOOR OVERHEAD EMERGENCY EXIT LIGHT BALLAST. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — BROKEN (CABIN)

MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS FORWARD OF LAVATORY Z INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT STRIP CONNECTORS FORWARD OF LAVATORY Z. SYSTEM GRUOND CHECKED NROMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

MIA - DURING OVERNIGHT CHECK, RIGHT AISLE EMERGENCY FLOOR LIGHTS INOPERATIVE. RESECURED RIGHT AISLE EMERGENCY FLOOR LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BRACKET — CORRODED (BS 5262)

TUL - BRACKET THAT HOLDS THE CARGO DOOR HOLD-OPEN ROD SEVERELY CORRODED. NO OTHER CORROSION FOUND IN SURROUNDING AREA. REPLACED PER SRM 52-30-14-11. TST: 21,374.47 HRS. CYCLES, 8,539. (X)

Part: FRAME — CORRODED (FRAME 63)

TUL - FOUND CORROSION ON TOP OF FRAME AT LT OUTBOARD ROLLER TRAY ATTACH FRAME 63 AND APPROXIMATELY 5 INCHES OUTBOARD ON VERTICAL ANGLE. REMOVED 1 INCHES SECTION OF ROLLER TRAY, FABRICATED AND INSTALLED NEW SECTION PER SRM 53-10-15, REMOVED CORRODED TOP OF FRAME PER 53-10-13 AND INSTALLED NEW FRAME, ALODINED, PRIMED AND PAINTED ALL NEW PIECES. (M)

Part: SUPPORT — CORRODED (BS 1180-1200)

TUL - FOUND STRIP ON SEAT TRACK SUPPORT NR 8, 6 INCHES BELOW FORWARD GALLEY MOON MAT IS CORRODED. REMOVED OUT OF LIMITS T-ANGLE AND INSTALLED MANUFACTURED T-ANGLE IAW SRM 53-10-13. (M)

Part: ROLLER TRAY — CORRODED (FRAME 28-35)

TUL - FOUND NUMEROUS AREAS OF CORROSION FROM FRAME 28 TO FRAME 35 ON TRAY NR 4. INSTALLED NEW SECTION OF ROLLER TRAY PER SRM 53-10-10 FIG 202. (M)

Part: SEAT TRACK — CORRODED (BS 1764-2241)

TUL - FOUND CORROSION ON SEAT TRACK JUST INBOARD OF LAV M ON SEAT TRACK NR 8, A PON OPEN UP ENTIRE LENGTH OF SEAT TRACK 8 FROM STATION 1764 TO STATION 2241. INSTALLED NEW SEAT TRACK NR 8 JUST INBOARD OF LAV M, SPLICE TO SPLICE. (M)

Part: SKIN — CORRODED (BS 4740)

TUL - FOUND CORROSION AROUND 14 FASTENERS ON AIRCRAFT OUTER SKIN BELOW THRESHOLD. REMOVED CORROSION AS PER AA SRM 51-74-10-2. TREATED PRIMED AND TOP COATED AREA. (M)

Part: WEB — CORRODED (L1 DOOR)

TUL - CORROSION ON WEB INBOARD L1 DOOR SILL AFT FORWARD GIRT BAR FITTING. REPAIRED AREA PER ESO 3095. CORROSION REMOVED, INHIBITED, AND PAINTED. TST: 21,374.47 HRS. CYCLES, 8,539. (X)

Part: SUPPORT — CORRODED (BS 1180-1230)

TUL - CORROSION ON FLOOR SUPPORT INBOARD R1 DOOR. REMOVED AND INSTALLED NEW T-ANGLE FLOOR SUPPORT AND DOUBLER PER SRM 53-10-16. (X)

Part: EEL PIN — LOOSE (CABIN)

JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS ILLUMINATED WITH SWITCH IN DISARM POSITION AND NO POWER ON THE AIRCRAFT. RESECURED PIN '0' ON BURNDY BLOCK 5702VT BLOCK 10. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)