N176AA

Part: STRAP — OUT OF POSITION (R1 DOOR) · airframe 56,351 hrs · 15,852 cycles

AIRCRAFT WAS GROUNDED: PILOT REPROTS WIRING BUNDLE HANGING DOWN BELOW SLIDE PACK ON 1R DOOR. MAINTENANCE FOUND SURVIVAL KIT ATTACH STRAP HANGING DOWN, RESTOWED ATTACH STRAP, REENGAGED GIRT BAR TO GIRT BAR HANDLING MECHANISM IAW AMM 25-66-10. ACCOMPLISHED SYSTEM TEST OF GIRT BAR MECHANISM IAW AMM 52-11-25. TEST GOOD.

Part: FLASHLIGHT — INOPERATIVE (MID LAVATORY) · airframe 56,024 hrs · 15,763 cycles

AIRCRAFT NOT GROUNDED: FLASH LIGHT AT MID LAV WILL NOT TEST. REMOVED AND REPLACED FLASH LIGHT AT MID LAV IAW AMM 25-60-00.

Part: STRAP — UNSECURE (R4 DOOR) · airframe 55,740 hrs · 15,696 cycles

AIRCRAFT WAS GROUNDED: 4R DOOR WOULD NOT ARM. MAINTENANCE RESECURED SLIDE STRAP PER AMM 25-61-01.

Part: STRAP — FAULTY (R4 DOOR) · airframe 55,740 hrs · 15,696 cycles

AIRCRAFT WAS GROUNDED: 4R DOOR WOULD NOT ARM. MAINTENANCE RESECURED SLIDE STRAP PER AMM 25-61-01.

Part: GIRT BAR — DEFECTIVE (R4 DOOR) · airframe 55,690 hrs · 15,688 cycles

AIRCRAFT WAS GROUNDED: MAINTENANCE REPORTS DURING REPLACEMENT OF SLIDE DUE TO DEPLOYMENT, INSPECTION OF GIRT BAR FOUND SPRING LEAF NOT PROVIDING ENOUGH PRESSURE TO GIRT FITTING. MAINTENANCE REMOVED AND REPLACED R4 DOOR GIRT BAR IAW AMM 25-66-10. OPS CHECK OK.

Part: WEB — CORRODED (BS 1718) · corrosion level 2 · airframe 55,679 hrs · 15,683 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON WEB AT BS 1718 BETWEEN RBL 22 AND RBL 26. REPAIRED WEB PER SRM 53-60-51-2R-17.

Part: SEAT TRACK — CORRODED (BS 860) · corrosion level 2 · airframe 55,679 hrs · 15,683 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SEAT TRACK #4 AT BS 860. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 860) · corrosion level 2 · airframe 55,679 hrs · 15,683 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SEAT TRACK #3 AT BS 860. REPLACED SEAT TRACK.

Part: ANGLE — CORRODED (BS 860) · corrosion level 2 · airframe 55,679 hrs · 15,683 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON CREASE BEAM ANGLE AT BS 860 AND RBL 57. REPAIRED CREASE BEAM ANGLE PER AARD 53-30-13-1.

Part: ACTUATOR — MALFUNCTIONED (RT MLG) · airframe 55,343 hrs · 15,582 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS GEAR DOORS CAUTION LIGHT ON UPON GEAR EXTENSION. MAINTENANCE RETRACTED AND EXTENDED THE LANDING GEAR IAW AMM 32-32-00 AND FOUND THAT THE RH DOWN LOCK ACTUATOR AND RH GEAR DOOR ACTUATOR WAS NOT WORKING PROPERLY. REMOVED AND REPLACED THE RH GEAR DOOR ACTUATOR IAW AMM 32-32-12. SEE SDR AALA201904029011.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,343 hrs · 15,582 cycles

AIRCRAFT IN BASE VISIT: MAINTENANCE FOUND THE SEAT MOUNTED EMERGENCY LIGHTS FROM 1E THRU 4E INOP. REPLACED BATTERY PACK AND CHARGER M10798 IAW AMM 33-51-07. SEAT MOUNDED LIGHTS OPS CHECK GOOD.

Part: ACTUATOR — UNRELIABLE (MLG DOORS) · airframe 55,343 hrs · 15,582 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS GEAR DOORS CAUTION LIGHT ON UPON GEAR EXTENSION. MAINTENANCE RETRACTED AND EXTENDED THE LANDING GEAR IAW AMM 32-32-00 AND FOUND THAT THE RH DOWN LOCK ACTUATOR AND RH GEAR DOOR ACTUATOR WAS NOT WORKING PROPERLY. REMOVED AND REPLACED THE RH GEAR LOCK ACTUATOR IAW AMM 32-32-02. SEE SDR AALA201904059010.

Part: CONTROLLER — DEFECTIVE (CABIN PRESSURE) · airframe 55,069 hrs · 15,495 cycles

RETURNED TO DEPARTURE, BOTH CABIN AUTO PRESSURE CONTROLLERS FAILED IN FLIGHT. AIRCRAFT WAS GROUNDED. AUTO1 CABIN ALT BITE TEST SHOWS TO REPLACE THE CABIN PRESSURE CONTROL UNIT IAW 21-30-00-815-802 FIM. REMOVED AND REPLACED THE NR 1 AND 2 PRESSURE CONTROLLERS IAW AMM 21-31-02, AND REMOVED AND REPLACED OUTFLOW VALVE ACTUATOR MOTOR IAW MM 21-31-05.

Part: CONTROLLER — FAILED (NR 2) · airframe 54,784 hrs · 15,412 cycles

CABIN PRESSURIZATION FAILED DURING CLIMB. AUTOMATIC PRESSURE CONTROLLER NR 2 WAS IN USE. AUTOMATIC PRESSURE CONTROLLER NR 1 WAS ON PLACARD. EMERGENCY DECLARED, FLIGHT LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS GROUNDED. MAINTENANCE ACCOMPLISHED FIM 21-30-00, FOUND THE NR 2 AUTOMATIC PRESSURE CONTROLLER WOULD NOT WORK ON POWER. REPLACED THE NR 2 CONTROLLER IAW AMM 21-31-02, AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 54,065 hrs · 15,205 cycles

RIGHT WING OUTBOARD TRAILING EDGE FLAP UPPER AND LOWER SURFACES HAVE MUTIPLE AREAS OF MOISTURE INGRESSION. THE AIRCRAFT WAS GROUNDED. REPAIRED FLAP IAW EA 285896.

Part: SWITCH — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 53,719 hrs · 15,126 cycles

WHEN THE EMERGENCY LIGHT SWITCH GUARD IS CLOSED, THE UNARMED LIGHT ILLUMINATES. REPLACED EMERGENCY LIGHT SWITCH GUARD. OPERATIONS CHECK GOOD. PER AMM 33-51-00-715-004.

Part: GIRT BAR — DISENGAGED (R4 DOOR) · airframe 53,641 hrs · 15,108 cycles

R4 DOOR SLIDE LIGHT BURNED OUT. FOUND R4 GIRT BAR NOT ENGAGING PROPERLY. INSTALLED THE GIRT BAR IAW AMM 25-16-10. ACCOMPLISHED REQUIRED CHECKS. SLIDE ENGAGE LIGHT CHECKS NORMAL.

Part: COLLAR — BROKEN (L1 DOOR) · airframe 53,054 hrs · 14,969 cycles

AIRCRAFT WAS NOT GROUNDED. L1 DOOR FOLD OPEN LOCKING COLLAR BROKEN. REPLACED HOLD OPEN LOCK COLLAR ON L1 DOOR PER AMM 52-11-08. ALL OPERATIONS CHECKS NORMAL. OK FOR SERVICE.

Part: LENS — MISSING (LIGHT) · airframe 52,556 hrs · 14,845 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT IDENTIFIER FORWARD OF SEAT 17A MISSING DECAL. REPLACED EXIT IDENTIFIER LENS PER AMM 33-51-10.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 52,556 hrs · 14,845 cycles

EMERGENCY FLASHLIGHT INOPERATIVE AT THE MID CABIN LT JUMPSEAT. REPLACED THE FLASHLIGHT BATTERY.

Part: HANDLE — OBSTRUCTED (DOOR) · airframe 51,475 hrs · 14,541 cycles

ARMING HANDLE BINDING WHEN RETRACTED. CLEARED DEBRIDS FROM THE TRACK IAW ESO 90938.

Part: WINDOW — CRACKED (L1 DOOR) · airframe 51,031 hrs · 14,406 cycles

AIRCRAFT WAS GROUNDED. L1 DOOR MOUNTED WINDOW HAS A POSSIBLE CRACK. REMOVED AND REPLACED DOOR WINDOW PER AMM 56-31-02. LEAK AND OPERATIONAL CHECK GOOD.

Part: BATTERY — INOPERATIVE (AFT FLASHLIGHT) · airframe 50,604 hrs · 14,302 cycles

FLIGHT ATTENDANT FLASHLIGHT AFT LEFT IS INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT BATTERY IAW AMM 25-64-00. OPS CHECKED GOOD.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 50,494 hrs · 14,280 cycles

LEFT SIDE EMERGENCY EXIT DOOR SIGN HAS A BROKEN LENS. REPLACED THE LENS IAW AMM 25-21-06. OPS CHECKED GOOD.

Part: COVER — UNSECURE (EXIT SIGN) · airframe 50,455 hrs · 14,271 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGN COVER FELL OFF. REATTACHED EMERGENCY EXIT LIGHT COVER AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: LENS — MISSING (EXIT SIGN) · airframe 50,445 hrs · 14,267 cycles

AIRCRAFT WAS NOT GROUNDED. EXIT SIGN MISSING AIRCRAFT RIGHT (WINDOW). REPLACED EXIT SIGN LENS FOR RIGHT WINDOW PER AMM 33-51-01.

Part: WARNING MESSAGE — ILLUMINATED (HYD QTY) · airframe 49,544 hrs · 14,018 cycles

EMERGENCY DECLARED. RETURNED TO FIELD. DURING FLIGHT RECEIVED EICAS HYD QTY LOW MESSAGE ACCOMPLANIED BY AN INDICATION OF SLOW LOSS OF FLUID INDICATED. IT WAS DETERMINED THAT THE LEFT HYDRAULIC QUANTITY INDICATION WAS ON MEL AND PLACARDED PER 29-9 AUTH: 4-421DC-C.

Part: PRESSURE SWITCH — FAULTY (HYDRAULIC SYS) · airframe 49,235 hrs · 13,945 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. SXM-JFK FLIGHT DIVERTED TO SJU ACCOUNT LEFT HYDRAULIC QUANTITY LOW RESERVOIR LIGHT ILLUMINATED AND LEFT HYDRAULIC QUANTITY EICAS MESSAGE. OVERWEIGHT LANDING UNEVENTFUL. REMOVED AND REPLACED LEFT HYDRAULIC RESERVOIR PRESSURE SWITCH IAW AMM 29-35-01. OPERATIONAL CHECK GOOD.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 48,867 hrs · 13,832 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. EMERGENCY PATH LIGHT ON SEAT ROW 27DEF IS INOPERATIVE. FOUND PLUG DISCONNECTED AT SIDEWALL. RECONNECTED PLUG. OPERATIONAL CHECK NORMAL IAW AMM 33-51-00

Part: GOVERNOR — FAULTY (LT ENGINE) · airframe 48,808 hrs · 13,814 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. JFK-SKB FLIGHT RETURNED TO JFK. DURING CLIMB, THE CREW REPORTED A LEFT ENGINE PRESSURE RATIO INDICATION PROBLEM, THROTTLE FULL FORWARD WOULD NOT GO ABOVE 1.41. REMOVED AND REPLACED LEFT ENGINE FUEL FLOW GOVERNOR ASSEMBLY IAW SIC 73-94-01. LEAK AND OPERATIONAL CHECK GOOD.

Part: BULB — UNSECURE (L3 DOOR SLIDE) · airframe 48,807 hrs · 13,813 cycles

L3 DOOR EMERGENCY EVACUATION SLIDE EXIT LIGHT INOPERATIVE. SECURED THE BULB IAW AMM 33-51-06. OPS CHECKED GOOD.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 48,290 hrs · 13,676 cycles

R1 DOOR EMERGENCY POWER RESERVOIR LOW. REMOVED AND REPLACED RESERVOIR ASSEMBLY IAW AMM 52-11-30. OPS CHECKED GOOD.

Part: DECK PLATE — CORRODED (BS 1706-1720) · corrosion level 2 · airframe 47,555 hrs · 13,486 cycles

CABIN AFT DECK PLATE HAS SEVERAL AREAS OF CORROSION BETWEEN BS 1710 - 1720 FROM RBL 8 TO LBL 52. REPAIRED THE DECK PLATE IAW SRM 53-60-51-ER-18 AND AARD 53-60-51-3.

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 46,277 hrs · 13,175 cycles

AIRCRAFT WAS NOT GNDED. DURING DESCENT FROM FL340 TO FL200 RECEIVED CABIN ALTITUDE WARNING. CABIN ALTITUDE WENT TO 10500. INITIATED IMMEDIATE DESCENT TO 10000. ACCOMPLISHED AMM 21-31-02 TEST ON BOTH CABIN ALTITUDE CONTROLLERS WITH NO FAULT FOUND. OK FOR SERVICE.

Part: CONTROL MODULE — DEFECTIVE (CABIN) · airframe 46,039 hrs · 13,123 cycles

WHILE ACCOMPLISHING A CHECK, FOUND NUMEROUS FIRST CLASS ESCAPE PATH LIGHTS INOPERATIVE. TROUBLE SHOT TO DEFECTIVE AISLE PATH LIGHTING CONTROL MODULE. REPLACED & TESTED NORMAL IAW MM 33-51-11. THE ACFT WAS NOT GNDED. SEE ALSO AALA20160305004.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,039 hrs · 13,123 cycles

WHILE ACCOMPLISHING A CHECK, FOUND NUMEROUS FIRST CLASS ESCAPE PATH LIGHTS INOPERATIVE. TROUBLE SHOT TO DEFECTIVE BATTERY PACK. REPLACED & TESTED NORMAL IAW MM 33-51-11. THE ACFT WAS NOT GNDED. SEE ALSO AALA20160307004.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 45,925 hrs · 13,094 cycles

FIRST CLASS SEAT EMER LIGHTS INOPERATIVE. R & R POWER SUPPLY IAW AMM 33-51-07. THE ACFT WAS NOT GNDED.

Part: FSEU — FAULTY (ZONE 100) · airframe 45,092 hrs · 12,900 cycles

WHILE CONFIGURING FOR LANDING, TE FLAP ASYM AND LE DISAGREE MSGS WITH FLAP INDICATOR SHOWING LESS THAN 1. AN EMER WAS DECLARED & THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. ACFT WAS REMOVED FROM SERVICE. R & R FSEU 2 IAW MM 27-51-01. CYCLED FLAPS UP & DOWN, NO FAULTS NOTED. IAW SDR CONTROL AALA20151120005.

Part: SWITCH — FAULTY (TE FLAP) · airframe 45,092 hrs · 12,900 cycles

WHILE CONFIGURING FOR LANDING, TE FLAP ASYM & LE DISAGREE MSGS WITH FLAP INDICATOR SHOWING LESS THAN 1. AN EMER WAS DECLARED & THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. ACFT WAS REMOVED FROM SERVICE. ACCOMPLISHED FIM 27-51-02, FOUND FAULT WITH DEPRESSURIZATION MODULE PRES SWITCH. R & R SWITCH IAW MM 27-51-29, OPERATIONALLY & LEAK CHECKED OK. REFERENCE ALSO SDR CONTROL AALA20151123009.

Part: CIRCUIT CARD — FAULTY (ZONE 100) · airframe 44,575 hrs · 12,785 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB RECEIVED A TAT PROBE EICAS MSG, NO AUTO THROTTLE/LNAV/VNAV/NO ICE PROTECTION, ACCOMPANIED BY THE RT EEC INOPERATIVE LIGHT ILLUMINATING. ACCOMPLISHED FIM 30-33-00-815 802, FOUND RT ENG SPEED CARD M10311 FAULTING. R & R SPEED CARD IAW AMM 77-12-03. PERFORMED OPERATIONAL CHECK IAW AMM 30-33-00-715-00. SYS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 43,799 hrs · 12,614 cycles

FORWARD DOOR LIGHTS DIM. CHARGED BATTERIES. SYS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 43,799 hrs · 12,614 cycles

LIGHTS AT SEVERAL SEATS INOPERATIVE. R & R BATTERY. SYS CHECKED NORMAL.

Part: SIGN — BROKEN (CABIN) · airframe 43,409 hrs · 12,525 cycles

EMERGENCY EXIT SIGN AT SEAT 17A IS BROKEN. R & R SIGN IAW AMM 33-51-01.

Part: COOLING FAN — MALFUNCTIONED (ZONE 100) · airframe 42,468 hrs · 12,304 cycles

DURING CRUISE NOTED ODOR IN COCKPIT WITH AN EQUIP OVERHEAT EICAS MSG. ODOR DISSIPATED WHEN EQUIPMENT COOLING FAN WAS SHUT OFF. NO FURTHER INCIDENTS WAS REPORTED. R & R THE NR 1 EQUIP COOLING FAN IAW AMM 21-58-06-414-007. SYS CHECKED NORMAL.

Part: BEAM — CORRODED (THRUST REVERSER) · corrosion level 2 · airframe 42,279 hrs · 12,262 cycles

UPPER INNER BEAM OF THE OTBD THRUST REVERSER WAS CORRODED SIX INCHES FWD OF THE AFT HINGE. REMOVED CORROSION & REPAIRED FOLLOWING INSTRUCTIONS OUTLINED IN EA COMP-78-038167 DATED 1/16/2014.

Part: COMPRESSOR — STALLED (RT ENGINE) · airframe 40,541 hrs · 11,856 cycles

REPEAT ITEM, DURING FUNCTIONAL CHECK FLIGHT, RT ENG COMPRESSOR STALLED DURING CLIMB OUT. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. REPLACED RT ENG. SYS GND CHECKED NORMAL OPERATION OPEN.

Part: COMPRESSOR — STALLED (RT ENGINE) · airframe 40,543 hrs · 11,855 cycles

DURING FUNCTIONAL CHECK FLIGHT RT ENG COMPRESSOR STALLED. ENG STABILIZED WHEN THROTTLE REDUCED TO MID-POINT. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACCOMPLISHED BORESCOPE WITH NO FAULTS FOUND. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: ACTUATOR — FAULTY (RUDDER) · airframe 40,543 hrs · 11,854 cycles

CREW REPORTED FLIGHT CONTROL PROBLEMS & ACFT WAS SHAKING. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED RT UPPER RUDDER POWER CONTROL ACTUATOR. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,261 hrs · 11,773 cycles

LEFT NR 3 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LT NR 3 DOOR, OPERATIONS CHECKED NORMAL.

Part: CONTROL MODULE — INOPERATIVE (CABIN) · airframe 37,460 hrs · 11,132 cycles

AFT EMERGENCY LIGHTS WILL NOT TURN OFF. REPLACED MODULE CONTROL FOR AFT EMERGENCY LIGHTS. OPERATIONS CHECKED NORMAL.

Part: FRAME — DENTED (FUSELAGE) · airframe 37,460 hrs · 11,132 cycles

FRAME DENTED AT FORWARD PIT OF LT SIDE AT BS 540 & STRINGER 25 LT. ACCOMPLISHED REPAIR FOR FRAME IAW REO-G16336 REVISION C & EA B757-53-030495.

Part: DOOR — DENTED (R4) · airframe 37,460 hrs · 11,132 cycles

DENT IN RIGHT NR 4 DOOR IN WHITE STRIPE AFT OF LOWER HINGE. ACCOMPLISHED DOUBLER REPAIR IAW EA B757-52-030464 & REO-G16339 REVISION B.

Part: SKIN — SCRATCHED (CARGO DOOR) · airframe 37,460 hrs · 11,132 cycles

FOUND TWO SCRATCHES ON FORWARD CARGO DOOR LOWER SKIN. BLENDED DAMAGE AND FOUND TO BE OUT OF LIMITS PER SRM 53-30-01. REPAIRED DAMAGED SKIN PER SRM 53-30-01-2R REPAIR 4.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 37,460 hrs · 11,132 cycles

AFT PIT FRAME DENTED & PUNCTURE AT BS 1440 & STRINGER 25 LT. REMOVED DAMAGE & INSTALLED REPAIR SPLICE ANGLE & REPAIR STRINGER CLIP IAW SRM 53-00-07-2R-5 FIGURE 201 DETAIL III.

Part: FRAME — DENTED (FUSELAGE) · airframe 37,460 hrs · 11,132 cycles

FRAME DENTED AT FORWARD PIT LT HAND SIDE BS 720 & STRINGER 24 LEFT. REMOVED DAMAGE & INSTALLED REPAIR ANGLE IAW SRM 51-40-09-0G & SRM 53-00-07-2R-5.

Part: SKIN — DENTED (FUSELAGE) · airframe 37,460 hrs · 11,132 cycles

DENT IN FUSELAGE SKIN AT BS 415 & STRINGER 19 RT. REPAIRED SKIN IAW SRM 53-00-01-2R-2.

Part: LIGHT — INOPERATIVE (ZONE 800) · airframe 37,408 hrs · 11,116 cycles

LEFT NR 2 DOOR SLIDE LIGHT INOPERATIVE. REPLACED LAMP FOR LT NR 2 DOOR SLIDE LIGHT. OPS CHECK NORMAL.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 33,228 hrs · 10,164 cycles

CORROSION ON T-CAP AT STATION 1640 AND BUTTLINE 0. REMOVED CORROSION PER SRM 51-10-02-0G. REPLACED T-CAP PER BOEING DRAWING LOR 5L53005 AND EA B757-53-022669.

Part: PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 33,228 hrs · 10,164 cycles

CORROSION ON AFT DECK PLATE BETWEEN BS 1680 TO 1720. REPLACED AFT DECK PLATE PER 51-00-05-1 AND EA B757-53-022697.

Part: STRAP — BROKEN (FUSELAGE) · airframe 33,228 hrs · 10,164 cycles

FLOORBEAM STABILIZATION STRAP BROKE AT STATION 365, LEFT BUTTLINE 25. INSTALLED REPAIR STRAP PER SRM 53-10-51-2R.

Part: SKIN — DENTED (FUSELAGE) · airframe 33,228 hrs · 10,164 cycles

FUSELAGE DENT STATION 397 AND STRINGER 15 RIGHT. INSTALLED DOUBLER REPAIR PER SRM 53-00-01-2R2.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 31,404 hrs · 9,782 cycles

RIGHT AFT SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT AFT SERVICE DOOR EXTERIOR EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,061 hrs · 9,719 cycles

FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FIRST CLASS EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,960 hrs · 8,861 cycles

RIGHT NUMBER 4 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 4 DOOR EMERGENCY LIGHT. OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,960 hrs · 8,861 cycles

LEFT NUMBER 4 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 4 DOOR EMERGENCY LIGHT. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 24,014 hrs · 8,150 cycles

EMERGENCY LIGHTS AT SEAT ROWS 9 TO 15 INOPERATIVE. REPLACED BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 22,865 hrs

JFK - RIGHT NUMBER 2 DOOR BATTERY PACK INOPERATIVE. REPLACED BATTERY PACK FOR RIGHT NUMBER 2 DOOR.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT 13DEF INOPERATIVE. REPLACED LAMP AT SEAT ROW 13DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 19,062 hrs

DFW - EXTERIOR EMERGENCY LIGHT AT LEFT AFT OVERWING EXIT INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LEFT AFT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS)

MIA - EMERGENCY LIGHTS AT SEAT ROWS 16 TO 25 INOPERATIVE. CHARGED BATTERY FOR EMERGENCY LIGHT SYSTEM FOR EMERGENCY LIGHTS AT SEAT ROWS 16 TO 25. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS)

MIA - EMERGENCY LIGHTS IN FIRST CLASS CABIN INOPERATIVE. CHARGED BATTERY FOR EMERGENCY LIGHT SYSTEM FOR EMERGENCY LIGHTS IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — DISCHARGED (CABIN)

DFW - FOUND EXTERIOR EMERGENCY LIGHT AT RIGHT AFT ENTRY DOOR INOPERATIVE. CLEANED SOCKET AND REPLACED BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)