N185AN

Part: TRACK — DIRTY (SLIDING WINDOW) · airframe 65,073 hrs · 16,383 cycles

AIRCRAFT WAS NOT GROUNDED: FIRST OFFICERS SLIDING WINDOW DIFFICULT TO OPEN AND CLOSE. MAINTENANCE CLEANED AND LUBRICATED WINDOW TRACKS AND PERFORMED SATISFACTORY OPERATIONAL CHECK PER STANDARD PRACTICES.

Part: GUST LOCK — LACK OF LUBE (L1 DOOR) · airframe 65,064 hrs · 16,380 cycles

AIRCRAFT NOT GROUNDED: 1L DOOR GUST LOCK INOPERATIVE. CHECKED AND APPLIED LPS-3 LUBE TO GENERAL AREA IAW AMM GEN STND PRACTICES AND AMM 52-11-00 CYCLED DOOR GUST LOCK SEVERAL TIMES, OK FOR SERVICE.

Part: CHARGER — NO TEST (EMERGENCY LIGHTS) · airframe 65,044 hrs · 16,372 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT MOUNTED EMERGENCY LIGHT IN FIRST CLASS VERY DIM. MAINTENANCE REPLACED CHARGER (M10798) PER AMM 33-51-07.

Part: MODULE — WEAK (EMERGENCY LIGHT)

SEAT MOUNTED EMERGENCY LIGHT IN FIRST CLASS VERY DIM. REPLACED BATTERY AND CHARGER REF AMM 33-51-07. FIRST CLASS SEAT MOUNTED EMERGENCY LIGHTS CHECK NORM. BATTERY PACK EQUIPTMENT M10798.

Part: BATTERY PACK — WEAK (EMERGENCY LIGHTS)

SEAT MOUNTED EMERGENCY LIGHT IN FIRST CLASS VERY DIM. REPLACED BATTERY AND CHARGER REF AMM 33-51-07. FIRST CLASS SEAT MOUNTED EMERGENCY LIGHTS CHECK NORM. BATTERY PACK EQUIPTMENT M10798.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 65,044 hrs · 16,372 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT MOUNTED EMERGENCY LIGHT IN FIRST CLASS VERY DIM. MAINTENANCE REPLACED BATTERY PER AMM 33-51-07.

Part: COLLAR — UNRELIABLE (L1 DOOR) · airframe 64,502 hrs · 16,204 cycles

AIRCRAFT WAS GROUNDED: MAINTENANCE REPORTS DOOR 1L GUST LOCK DOOR NOT ENGAGE. REPLACED HOLD OPEN LOCK COLLAR IAW AMM 52-11-08. OPS CHECK OK.

Part: OVEN — ODOR (GALLEY) · airframe 64,466 hrs · 16,191 cycles

AIRCRAFT WAS GROUNDED: ON TAXI OUT FAS REPORTED ELECTRICAL ODOR, SAID IT WAS STRONG. JUMPSEATER WENT BACK AND CONFIRMED ODOR, AND FOUND IT TO BE STRONGEST IN FIRST CLASS, LEFT SIDE, SECOND OR THIRD ROW. PAX REPORTED OILY SMELL. MAINTENANCE REPORTS UPON FURTHER EVALUATION, FOUND ELECTRICAL/ MILD BURNING SMELL WHEN FIRST CLASS GALLEY OVEN IS IN OPERATION AFTER 10 MINUTES OF USE AND PERSISTED THROUGH-OUT THE TIME IT IS ON. CYCLED OVEN SEVERAL TIMES WITH SAME OUTCOME. REMOVED AND REPLACED FIRST CLASS GALLEY OVEN IAW AMM 25-31-05. RAN OVEN IN EXCESS OF ONE HOUR AND COULD NOT REPLICATED ODOR.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 64,077 hrs · 16,055 cycles

AIRCRAFT WAS NOT GROUNDED: 1L DOOR EXTERIOR SLIDE LIGHT INOPERABLE. MAINTENANCE RELAMPED LIGHT PER AMM 33-51-06.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 63,854 hrs · 15,982 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT WING #2 SLAT COVE SKIN CRACKED. REPAIRED SLAT COVE SKIN PER AARD 57-43-00-4

Part: CHARGER — FAULTY (CABIN) · airframe 63,682 hrs · 15,936 cycles

AIRCRAFT NOT GROUNDED: SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE FROM SEATS 16D THRU 25D. REPLACED BATTERY AND CHARGER M10953 REF AMM 33-51-07. SEAT MOUNTED EMERGENCY LIGHTS 16D-25D CHECK NORM.

Part: CHARGER — FAULTY (CABIN) · airframe 63,682 hrs · 15,936 cycles

AIRCRAFT NOT GROUNDED: SEAT MOUNTED EMERGENCY LIGHTS DIM FROM SEATS 9D THRU 15D. REPLACED BATTERY AND CHARGER M10952 IAW AMM 33-51-07. SEAT MOUNTED LIGHTS 9D THRU 15D CHECK NORM.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 63,466 hrs · 15,878 cycles

AIRCRAFT NOT GROUNDED: SEAT 33D EMERGENCY PATH LIGHT INOPERATIVE. RECONNECTED CONNECTOR AND SECURED UNDER SEAT 33D IN REF TO AMM 33-51-11. OPS CHECK GOOD.

Part: CONNECTOR — SHORTED (EMERGENCY LIGHTS) · airframe 62,340 hrs · 15,584 cycles

AIRCRAFT WAS GROUNDED: MAINTENANCE FOUND EMERGENCY SEAT ESCAPE PATH LIGHTING AT SEAT 26DEF RH TO LAST ROW LIGHTS INOP. MAINTENANCE FOUND LIGHT CONNECTOR AT 33F SHORT. REMOVED AND REPLACED CONNECTOR IAW SWPM 20-42-01. ACCOMPLISHED EMERGENCY LIGHT OPS CHECK IAW AMM 33-51-00. OPS CHECK GOOD.

Part: WIRE — SEPARATED (EMERGENCY LIGHT) · airframe 62,155 hrs · 15,525 cycles

MAINTENANCE FOUND THE EMERGENCY LIGHT AT ROW 28D INOPERATIVE. FOUND SEPARATED WIRES FROM EMERGENCY LIGHT CONNECTOR AT SIDEWALL SEAT 28D. REPAIRED THE CONNECTOR WIRES AND INSTALLED NEW SOCKETS IAW 33-51-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,155 hrs · 15,525 cycles

EMERGENCY LIGHT AT THE AFT CARGO DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT AND PERFORMED A SATISFACTORY OPERATIONAL CHECK IAW 33-40-00.

Part: SPRING — BROKEN (L1 GUST LOCK) · airframe 61,365 hrs · 15,287 cycles

L1 DOOR GUST LOCK BROKEN, AND WILL NOT LOCK. THE AIRCRAFT WAS GROUNDED. REPLACED THE GUST LOCK SPRING AND TRIGGER ON THE DOOR IAW AMM 52-11-08. OPS CHECKED NORMAL.

Part: STRAP — TORN (L1 DOOR) · airframe 61,348 hrs · 15,283 cycles

THE AIRCRAFT WAS NOT GROUNDED. L1 DOOR SLIDE RELEASE STRAP HARNESS LOWER STRAP AREA FABRIC TORN, HARNESS ON AOG CPN: 4105750. REPLACED L1 DOOR SLIDE STRAP PER AMM 25-66-01. OPERATIONS CHECK OK.

Part: SPRING — BROKEN (L1 GUST LOCK) · airframe 61,328 hrs · 15,275 cycles

L1 DOOR GUST LOCK WAS FOUND BROKEN. REPLACED GUST LOCK SPRING AND TRIGGER IAWMM 52-11-08. OPS CHECKED NORMAL.

Part: ACTUATOR — FAULTY (SPOILERS) · airframe 60,010 hrs · 14,944 cycles

EICAS MESSAGE FOR THE SPOILERS AND SPOILERS LIGHT IS ILLUMINATED. THE AIRCRAFT DUMPED FUEL AND RETURNED TO DEPARTURE. TROUBLESHOT THE SYSTEM AND FOUND THE NR 9 SPOILER PCA HAS OPEN RESISTANCE. REPLACED SPOILER PCA IAW AMM 27-61-02. OPS AND LEAK CHECKED NORMAL. THE AIRCRAFT WAS GROUNDED.

Part: GIRT BAR — FAULTY (R4 DOOR) · airframe 59,971 hrs · 14,932 cycles

CATERER DISCOVERED DETACHED HARDWARE ON THE R4 DOOR GIRT BAR. REPLACED THE GIRT BAR IAW AMM 25-66-10.

Part: MECHANISM — BROKEN (WINDOW) · airframe 59,885 hrs · 14,910 cycles

AIRCRAFT WAS NOT GROUNDED. FIRST OFFICERS WINDOW DIFFICULT TO CLOSE FULLY USING CRANK. REPLACED FIRST OFFICERS WINDOW OPERATING MECHANISM PER M/M 56-11-04.

Part: GIRT BAR — OUT OF ADJUST (R4 DOOR SLIDE) · airframe 59,430 hrs · 14,795 cycles

R4 DOOR SLIDE ARM LIGHT INOPERATIVE. ADJUSTED THE GIRT BAR FLOOR FITTING IAW AMM 52-11-25.

Part: GUST LOCK — LACK OF LUBE (L2 DOOR) · airframe 59,028 hrs · 14,686 cycles

L2 DOOR HARD TO CLOSE. LUBRICATED THE GUST LOCK ASSEMBLY. DOOR OPS CHECKED NORMAL IAW AMM 52-11-00.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,947 hrs · 14,663 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT HAND TRANSITION PANEL AROUND FASTENER HOLES BETWEEN STA 1440 TO STA 1480. REPLACED TRANSITION PANEL PER 51-00-05-1 AND DRAWING 146N-15391.

Part: MOUNT — CRACKED (CABIN) · airframe 58,568 hrs · 14,550 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT AT THE R4 DOOR HAS A CRACKED MOUNT. REMOVED AND REPLACED LIGHT ASSEMBLY PER AMM 33-51-10. OPERATIONAL CHECK GOOD.

Part: SEAL — LEAKING (HYD MODULE) · airframe 58,533 hrs · 14,540 cycles

CENTER HYDRAULIC SYSTEM QUANTITY LOSS INDICATION, APU LOW DUCT PSI. CHECKED AND FOUND CENTER HYDRAULIC MODULE SEAL LEAKING. THE SEAL WAS REPLACED. SYSTEM PRESSURIZED, NO LEAKS FOUND IAW 29-11-13 & 12-12-01. AIRCRAFT WAS GROUNDED.

Part: SIGN — UNSECURE (EMERGENCY LIGHT) · airframe 58,527 hrs · 14,538 cycles

THE EXIT SIGN OVER THE R2 DOOR WAS LOOSE. THE EXIT SIGN SECURED IAW MM 33-51-00.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 56,997 hrs · 14,126 cycles

EMERGENCY EXIT LIGHTS BETWEEN BS 700 AND 720 WERE DIM. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51-07. OPERATIONAL CHECKED GOOD.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 56,821 hrs · 14,080 cycles

SEAT MOUNTED EMERGENCY LIGHT AT SEAT 24D IS INOPERATIVE. SEATED LOOSE CONNECTOR IAW AMM 33-51-06. OPERATIONAL CHECK GOOD.

Part: BULB — LOOSE (EMERGENCY LIGHT) · airframe 56,821 hrs · 14,080 cycles

L2 DOOR EMERGENCY EVACUATION SLIDE LIGHT IS INOPERATIVE. RESEATED BULB IAW AMM 33-51-06. OPERATIONAL CHECKED GOOD.

Part: GOVERNOR — FAULTY (RT ENGINE) · airframe 56,508 hrs · 13,993 cycles

AIRCRAFT WAS GROUNDED. RIGHT ENGINE DID NOT SHUT DOWN WITH THE FUEL CUTOFF SWITCH. FOUND LOOSE CONNECTOR ON THE FUEL FLOW GOVERNOR SHUTOFF SWITCH. CLEANED AND RESEATED CONNECTOR. PROBLEM REPEATED ON 2/13/17 PHL FLIGHT 203. REMOVED AND REPLACED RIGHT FUEL FLOW GOVERNOR IAW SIC 73-94-01. OPERATIONAL CHECK GOOD.

Part: SKIN PANEL — CORRODED (TE FLAP) · corrosion level 2 · airframe 56,405 hrs · 13,957 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. RIGHT INBOARD MAINT FLAP HAS SEVERAL SMALL AREAS OF CORROSION ON THE UPPER SKIN PANEL. REPAIRED SKIN PANEL IAW SRM SRM 51-70-10-2R 2 AND EA 266869.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,716 hrs · 13,773 cycles

INTERIOR EMERGENCY EXIT SIGNS AT L1 AND R1 DOOR ARE EXTREMELY DIM. REMOVED AND REPLACED EMERGENCY POWER SUPPLY AND BATTERY AT M10798 IAW AMM 33-51-07. SYSTEM CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,716 hrs · 13,773 cycles

SEAT MOUNTED EMERGENCY LIGHTS FROM SEAT 26 DEF TO SEAT 36 DEF AND EXIT SIGNS AT L4 AND R4 DOORS ARE EXTREMELY DIM. REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY AT M10801 IAW AMM 33-51-07. SYSTEM CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,716 hrs · 13,773 cycles

SEAT MOUNTED EMERGENCY LIGHTS AT SEAT 1E THROUGH SEAT 15 DEF ARE EXTREMELY DIM. REMOVED AND REPLACED EMERGENCY POWER SUPPLY AND BATTERY AT M10952 IAW AMM 33-51-07. OPS CHECKED NORMAL.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,716 hrs · 13,773 cycles

SEAT MOUNTED EMERGENCY LIGHTS FROM SEAT 26 DEF TO SEAT 36 DEF AND EXIT SIGNS AT L4 AND R4 DOORS ARE EXTREMELY DIM. REMOVED AND REPLACED EMERGENCY POWER SUPPLY AND BATTERY AT M10801 IAW AMM 33-51-07. SYSTEM CHECKED NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,716 hrs · 13,773 cycles

SEAT MOUNTED EMERGENCY LIGHTS AT SEAT 1E THROUGH SEAT 15 DEF ARE EXTREMELY DIM. REMOVED AND REPLACED EMERGENCY POWER SUPPLY AND BATTERY AT M10952 IAW AMM 33-51-07. OPERATIONAL CHECK NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,716 hrs · 13,773 cycles

INTERIOR EMERGENCY EXIT SIGNS AT L1 AND R1 DOOR ARE EXTREMELY DIM. REMOVED AND REPLACED EMERGENCY POWER SU.. SEE ALSO AALA20161103006.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,378 hrs · 13,443 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY PATH LIGHTING IS INOPERATIVE BETWEEN ROWS 2 AND 15. R & R EMERGENCY LIGHT POWER SUPPLY AND BATTERY IAW AMM 33-51-00. OPS CHECK NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 54,378 hrs · 13,443 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY PATH LIGHTING IS INOPERATIVE BETWEEN ROWS 2 AND 15. R & R EMERGENCY LIGHT POWER SUPPLY AND BATTERY IAW AMM 33-51-00. OPS CHECK NORMAL.

Part: SENSE LINE — DETERIORATED (ZONE 400) · airframe 53,270 hrs · 13,198 cycles

STATUS MSG, RT ENG OVERHEAT LP2 5 MINUTES AFTER TAKEOFF. RT ENG OVERHEAT EICAS MSG 15 MINUTES AFTER TAKEOFF. THE MSG WENT OUT WHEN ACCOMPLISHING THE CHECKLIST. THE CREW DECLARED AN EMER & RETURNED WITHOUT FURTHER INCIDENT. THE ACFT WAS GNDED. REPLACED RT HP6 DIFFUSER DUCT, NO HELP. REPLACED RT HPSOV SENSE LINE. ENG RUN & OPERATIONS CHECKED GOOD.

Part: CONNECTOR — LOOSE (CABIN) · airframe 52,237 hrs · 12,955 cycles

EMERGENCY LIGHT AT SEAT ROW 24 INOPERATIVE. RESEATED LOOSE CONNECTOR AT SEAT & RELAMPED SEAT IAW 33-51-11, LIGHT TEST CHECKED OK.

Part: SKIN — WORN (TE FLAP) · airframe 51,329 hrs · 12,773 cycles

LEFT INBOARD FLAP HAS WEAR ON LEADING EDGE APPROX 74" FROM INBOARD LEADING EDGE. TRIMMED OUT 5" X 7.5", INSTALLED DOUBLER, REPAIR PLATE & FIBERGLASS OVERLAY IAW SRM 57-53-01.

Part: CONTACT — DEFECTIVE (ZONE 200) · airframe 51,088 hrs · 12,717 cycles

EMERGENCY PATH LIGHT AT SEAT 29D IS INOPERATIVE. INSTALLED NEW SOCKET PIN AT CONNECTOR & PERFORMED OPERATIONAL CHECK IAW AMM 20-42-01 & AMM 33-51-00.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 49,871 hrs · 12,416 cycles

SEAT 15D EMER EXIT LIGHT INOPERATIVE. RESEATED CONNECTOR FOR EMER LIGHT AT SEAT 15D. PERFORMED OPERATIONAL CHECK IAW AMM 33-51-00. SYS CHECKED NORMAL.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 49,871 hrs · 12,416 cycles

SEAT 32D EMER EXIT LIGHT INOPERATIVE. RESEATED CONNECTOR FOR EMER LIGHT AT SEAT 32D. PERFORMED OPERATIONAL CHECK IAW AMM 33-51-00. SYS CHECKED NORMAL.

Part: TIRE — FAILED (MLG) · airframe 49,026 hrs · 12,215 cycles

RETURNED & EMER DECLARED. LANDING UNEVENTFUL. ACFT NOT OVERWEIGHT. DURING TAKEOFF MLG TIRE 6 BURST FOLLOWED BY LOSS OF LT HYD SYS QTY. R & R MLG TIRES 5 & 6 IAW AMM 32-45-01. R & R BRAKE PRESS LINE, GEAR PRESS LINE & GEAR DOWN RETURN LINE IAW AMM 20-10-09. R & R LT ENG DRIVEN PUMP IAW AMM 29-11-05 & ASSOCIATED FILTERS IAW 29-11-15. PERFORMED LEAK & TAXI CHECKS. SYS CHECKED NORMAL.

Part: SLIDE — DEFECTIVE (L1 DOOR) · airframe 48,919 hrs · 12,194 cycles

1L DOOR OPENED WHILE ARMED. THE SLIDE FELL OFF THE DOOR & DID NOT DEPLOY. R & R SLIDE.

Part: RELAY — FAILED (SPOILER SYSTEM) · airframe 48,309 hrs · 12,041 cycles

CREW REPORTED AUTO SPOILER EICAS MSG DISPLAYED DURING CRUISE. FLIGHT DIVERTED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. PLACARDED FLIGHT SPOILER SYS INOPERATIVE IAW MEL. REPLACED RELAYS K10385 & K10386 ON 07/31/2014. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,484 hrs · 11,833 cycles

EMERGENCY FLOOD LIGHT OVER SEAT 27C INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY FLOOD LIGHT OVER SEAT 27C. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,246 hrs · 11,300 cycles

SEAT 4EF EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT 4EF EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 42,936 hrs · 10,787 cycles

SEAT ROW 29DGE EMERGENCY LIGHT INOPERATIVE. SECURED CONNECTOR AT ROW 29DGE. OPS CHECK NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 42,936 hrs · 10,787 cycles

SEAT 29DEF EMERGENCY LIGHT INOPERATIVE. SECURED CONNECTOR AT SEAT 29DEF. OPS CHECK NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 42,328 hrs · 10,624 cycles

ROW 15D SEAT EMERGENCY LIGHT INOPERATIVE. RESEATED LOOSE CONNECTOR AT SEAT 15D. OPS CHECK NORMAL.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 40,887 hrs · 10,316 cycles

AFT CARGO DOOR EXTERIOR SKIN LOWER FORWARD CORNER DAMAGED. INSTALLED DOUBLER AND FILLER PER ESO 90121 AND SRM 52-30-01-2R.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 40,887 hrs · 10,316 cycles

AFT CARGO DOOR EXTERIOR SKIN LOWER AFT SIDE DEEP BLENDED AREAS. INSTALLED DOUBLER PER SRM 51-30-01-2R.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 40,887 hrs · 10,316 cycles

AFT CARGO DOOR, EXTERIOR SKIN LOWER AFT SIDE HAS DEEP BLENDED AREAS. INSTALLED REPAIR DOUBLER PER SRM 52-30-01-2R FIGURE 201.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,887 hrs · 10,316 cycles

CORRODED FLOORBEAM AT STATION 1640. SPLICE REPAIR TO UPPER FLOORBEAM T-CAP.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,887 hrs · 10,316 cycles

RIGHT NUMBER 4 GUTTER SUPPORT CORRODED. REPLACED GUTTER SUPPORT PER AARD 51-00-05-01.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,887 hrs · 10,316 cycles

CORRODED GUTTER SUPPORT FROM STATIONS 1640 TO 1660 RIGHT BUTTLINE 56. REPLACED SUPPORT PER AARD 51-00-05-1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,887 hrs · 10,316 cycles

CORROSION ON T-CAP OF FLOORBEAM AT STATION 1660. ACCOMPLISHED NESTED ANGLE REPAIR PER SRM 53-00-51-2R 3.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,887 hrs · 10,316 cycles

CHANNEL AT STATION 1714 CORRODED. REPLACED CHANNEL.

Part: SKIN — DAMAGED (LE SLAT) · corrosion level 2 · airframe 40,887 hrs · 10,316 cycles

DEEP BLEND ON NUMBER 8 SLAT UPPER SKIN APPROXIMATELY 36 INCHES FROM OUTBOARD END. REMOVED DAMAGED SKIN AND INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 40,887 hrs · 10,316 cycles

AFT CARGO DOOR EXTERIOR SKIN LOWER FORWARD CORNER DAMAGED. DOUBLER AND FILLER INSTALLED PER ESO 90121 AND SRM 52-30-01-2R.

Part: TACH GENERATOR — FAILED (RT ENGINE) · airframe 38,829 hrs · 9,890 cycles

MIA - CREW REPORTED RIGHT N-3 ROLLED BACK TO 0 ACCOMPANIED BY RIGHT ENGINE BLEED MESSAGE. CENTER RIGHT FUEL PUMP AND LEFT YAW DAMPER INOPERATIVE. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED N3 TACHOMETER GENERATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 35,679 hrs · 9,240 cycles

INTERCOSTAL HAS CORROSION AT STATIONS 1640 TO 1661 BUTTLINE 0. INSTALLED NEW INTERCOSTAL PER SRM 53-60-15.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 35,679 hrs · 9,240 cycles

ALL GALLEY MOUNTS FROM STATIONS 1681 TO 1720 CORRODED. REMOVED AND REPLACED GALLEY MOUNTS PER SRM 51-40-2.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 35,679 hrs · 9,240 cycles

DURING INSPECTION OF AFT DECK FOUND 7 AREAS OF CORROSION AT STATIONS 1681 TO 1718, RIGHT BUTTLINES 6 TO 47. INSTALLED DOUBLER AND SPLICE PER EA B757-53-014322 DATED 12/6/2010, SRM 53-60-51-3 AND SRM 53-60-51-2R-2.

Part: STIFFENER — DAMAGED (FUSELAGE) · airframe 35,679 hrs · 9,240 cycles

FOUND TOOLING MARKS ON STIFFENER AT STATION 1720 AFTER REMOVAL FOR OTHER MAINTENANCE. INSTALLED NEW STIFFENER PER SRM 51-40-2.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 35,679 hrs · 9,240 cycles

DURING INSPECTION OF AFT GALLEY DECK FOUND 5 AREAS OF CORROSION AT STATION 1681. INSTALLED DOUBLER PER EA B757-53-014322 DATED 12/6/2010, AARD 53-60-51-3, SRM 53-00-51 AND SRM 53-60-51-2R-2.

Part: GENERATOR — FAILED (RT ENGINE) · airframe 33,690 hrs · 8,827 cycles

SJU - INFLIGHT MIA-SSA. CREW REPORTED RIGHT ENGINE DRIVEN GENERATOR FAILED AND RIGHT CENTER FUEL PUMP LOW PRESSURE LIGHT ILLUMINATED IN FLIGHT. EMERGENCY DECLARED FLIGHT DIVERTED SJU LANDED WITHOUT INCIDENT. REPLACED RIGHT ENGINE GENERATOR AND RESET RIGHT CENTER FUEL PUMP UFI CONTROLLER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 32,728 hrs · 8,563 cycles

EMERGENCY EGRESS LIGHTS AT SEAT ROW 17DEF INOPERATIVE. SECURED CONNECTOR.

Part: ACTUATOR — OUT OF ADJUST (LT MLG) · airframe 32,502 hrs · 8,507 cycles

GEAR DOOR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. GEAR DOORS ANNUNCIATED ON EICAS. GEAR LOWERED NORMALLY. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. ACCOMPLISHED PRE-FERRY BOW ALL CHECKS OK. AIRCRAFT FERRIED TO JFK PER S/M 12-044 DATED 12-11-09. ADJUSTED LEFT MAIN LANDING GEAR DOOR ACTUATOR AND RIGHT HYDRAULIC FUSE. REPLACED RIGHT MAIN LANDING GEAR DOOR POSITIONER ACTUATOR.

Part: CONNECTOR — LOOSE (CABIN) · airframe 32,231 hrs · 8,441 cycles

EMERGENCY LIGHT AT SEAT 17C INOPERATIVE. RE-INSTALLED CONNECTOR PLUG AT SEAT 17C.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,889 hrs · 8,332 cycles

SEAT MOUNTED EMERGENCY LIGHTS FROM ROW 16 THRU 25 INOPERATIVE. REPLACED BATTERY PACK, OPS CHECK OK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,889 hrs · 8,332 cycles

SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 26 TO 36 DIM. REPLACED BATTERY PACK, OPS CHECK OK.

Part: PIN — BROKEN (CONNECTOR) · airframe 31,686 hrs · 8,288 cycles

EMERGENCY PATH LIGHT AT 17D INOP. REPAIRED BROKEN PIN AT CONNECTOR. OPS CHECK OK PER M/M 33-51-00-5.

Part: LIGHT — INOPERATIVE (EXTERIOR)

DFW RIGHT NUMBER 4 EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 4 EXTERIOR EMERGENCY LIGHT.

Part: STRAP — BROKEN (ZONE 100) · airframe 17,878 hrs · 777 cycles

CEILING STRAP BROKEN IN MAIN E/E COMPARTMENT LT TUNNEL. REPAIRED IAW SRM 53-10-51 PAGE 1.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,489 hrs

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

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: CONNECTOR — LOOSE (CABIN)

JFK - EMERGENCY LIGHT AT FIRST CLASS CABIN INOPERATIVE. SECURED CONNECTOR AT BATTERY PACK FOR EMERGENCY LIGHT AT FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

SFO - SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROWS 16DEF TO 26DEF INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROWS 16DEF TO 26DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHTS)

SFO - SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROWS 16DEF TO 26DEF INOPERATIVE. REPLACED MODULE FOR EMERGENCY LIGHTS AT SEAT ROWS 16DEF TO 26DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: VALVE — LEAKING (LEFT ENGINE)

LAX INFLIGHT T267/15JUL - NUMBER ONE ENGINE OVERHEAD EICAS MESSAGE AND NUMBER ONE ENGINE OVERHEAT WARNING ILLUMINATED. REDUCED LEFT ENGINE TO IDLE AND LANDED LAX WITHOUT INCIDENT. NO FIRE FOUND. FOUND HIGH PRESSURE VALVE LEAKING AT LOWER FLANGE. REPLACED HIGH STAGE VALVE SEALS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CLAMP — LOOSE (LEFT ENGINE)

LAX INFLIGHT T192/08JUL - ON CLIMB, RECEIVED LEFT ENGINE OVERHEAT INDICATION AND EICAS MESSAGE. RETURNED TO LAX AND LANDED WITHOUT INCIDENT. FOUND CLAMPS ON HIGH STAGE BLEED VALVE ON NUMBER ONE ENGINE LOOSE AND LEAKING. RETIGHTENED CLAMPS AND ACCOMPLISHED OVERWEIGHT LANDING INSPECTION. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHTS AT LEFT AND RIGHT FORWARD OVERWING HATCH INOPERATIVE. RELAMPED EMERGENCY LIGHTS AT LEFT AND RIGHT FORWARD OVERWING HATCH. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT ROW 6AB OVERHEAD FIRST CLASS CLOSET INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT ROW 6AB OVERHEAD FIRST CLASS CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHTS AT LEFT AND RIGHT AFT OVERWING HATCH INOPERATIVE. RELAMPED EMERGENCY LIGHTS AT LEFT AND RIGHT AFT OVERWING HATCH. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LAX - EMERGENCY LIGHT AT SEATS 1E TO 6E INOPERATIVE. REPLACED CHARGER AND BATTERY PACK M10798 FOR INOPERATIVE EMERGENCY LIGHTS AT SEATS 1E TO 6E. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (EXTERIOR)

DFW - EMERGENCY LIGHTS OUTSIDE OF LEFT NUMBER FOUR DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHTS OUTSIDE OF LEFT NUMBER FOUR DOOR. SYSTEM GROUND OPERATIONS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY OVERHEAD LIGHT IN BIN BULL NOSE AT SEATS 29DEF INOPERATIVE. RELAMPED EMERGENCY OVERHEAD LIGHTS IN BIN BULL NOSE AT SEATS 29DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - SEAT MOUNTED EMERGENCY LIGHTS FROM ROW 26 TO 36 INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR SEAT MOUNTED EMERGENCY LIGHTS FROM ROW 26 TO 36. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

MIA - SEAT MOUNTED EMERGENCY LIGHTS AT SEAT 24D INOPERATIVE. FOUND CONNECTOR LOOSE UNDER SEAT 24D. RECONNECTED CONNECTOR FOR SEAT MOUNTED EMERGENCY LIGHTS AT SEAT 24D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT)

DFW - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHTS FOR FIRST CLASS AND TWO IN COACH INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: TRANSMITTER — INOPERATIVE (AFT ACCY)

MIA - FLT 922 - EN ROUTE MIA-LPB, STABILIZER TRIM EICAS MESSAGE AND STABILIZER TRIM CAUTION LIGHT ILLUMINATED. RETURNED TO MIA LANDING WITHOUT INCIDENT. REPLACED RIGH STABILIZER TRIM MODULE TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)