N196AA

Part: WINDSHIELD — ARCED (COCKPIT L1) · airframe 56,968 hrs · 17,547 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK L1 WINDSHIELD ARCING. REPLACED WINDSHIELD PER AMM 56-11-01-400.

Part: CHARGER — NO TEST (EMERGENCY LIGHTS) · airframe 55,257 hrs · 17,074 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY LIGHT OUTSIDE L1 DOOR INOPERATIVE. MAINTENANCE REPLACED BATTERY CHARGER PER STANDARD PRACTICES AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: CHARGER — NO TEST (EMERGENCY LIGHTS) · airframe 55,257 hrs · 17,074 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD GALLEY LOWER EXIT SIGN INOPERATIVE. MAINTENANCE REPLACED BATTERY CHARGER PER STANDARD PRACTICES AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: DECK PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,257 hrs · 17,074 cycles

AIRCRAFT IN BASE VISIT: FOUND CORROSION OUT OF LIMITS ON AFT DECK PLATE. INSTALLED SRM REPAIR IAW 53-60-51-2R-18.

Part: SKIN — CORRODED (TE FLAP) · corrosion level 2 · airframe 55,257 hrs · 17,074 cycles

AIRCRAFT IN BASE VISIT: LEFT WING INBOARD MAIN FLAP LOWER SKIN AFT EDGE HAS A FOUR INCH BY ONE INCH AREA OF CORROSION, REPAIRED FOLLOWING INSTRUCTION OF EA 294003.

Part: TRANSMISSION — FAILED (LT WING TE FLAPS) · airframe 55,075 hrs · 17,015 cycles

A TRAILING EDGE FLAP DISAGREE LIGHT ILLUMINATED ON FINAL AS FLAPS MOVED FROM 15 TO 20. FLAPS STOPPED MOVING AT APPROXIMATELY 18. ALTERNATE FLAPS 20 SELECTED AS NON-NORMAL ACCOMPLISHMENT FLAPS WENT TO 20 IAW THE CHECKLIST. FLAPS LEFT IN 20 FOR LANDING AND AT THE GATE. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE OUTBOARD NR 5 FLAP TRANSMISSION IAW AMM 27-51-06. OPS CHECKED GOOD.

Part: CONTROL VALVE — MALFUNCTIONED (TE FLAPS) · airframe 55,016 hrs · 17,000 cycles

ON FINAL, WITH FLAPS AT 20 DEGREES. SELECTED 25 DEGREES AN IMMEDIATE TE FLAPS DISAGREE EICAS MESSAGE. QRH COMPLETE, 20 DEGREES FLAP, LANDING NORMAL, NORMAL BRAKING. AFTER TROUBLESHOOTING, MAINTENANCNE REMOVED AND REPLACED THE FLAP CONTROL MODULE VALVE IAW AMM 27-51-28. OPS CHECKED GOOD.

Part: FLAP TRACK — LACK OF LUBE (LT WING TE FLAP) · airframe 55,243 hrs · 15,550 cycles

THE PILOT REPORTED THAT ON FINAL WITH FLAPS 20 SELECTED, FLAPS STOPPED AT 17 DEGREES. ABORTED LANDING, RAN THE FLAP INDICATION CHECKLIST. FLAPS EXTENDED TO 20 IN THE ALTERNATE MODE. THE AIRCRAFT WAS GROUNDED. MAINTENANCE FOUND THE FLAP DISAGREE FAULT CODE 305. THE LT FLAP TRANSMISSION WASINSPECTED AND FOUND NOT TRIPPED. ON FURTHER INSPECTION, FOUND COMPLETELY DRY GREESE FITTINGS AND TRACKS. COMPLETED A TRAILING EDGE LUBRICATION, OPS CHECKED IAW AMM 27-50-00. NO FLAP MESSAGES ACTIVE.

Part: TRANSMISSION — LACK OF LUBE (LT WING TE FLAP) · airframe 54,972 hrs · 16,986 cycles

PILOT REPORTED THAT AN EMERGENCY WAS DECLAIRED INBOUND, DUE TO A FLAP DISAGREE WARNING WHILE GOING FROM 20 DEGREES OF FLAPS TO 25 DEGREES. THE FLAPS REMAINED AT 20 DEGREES FOR LANDING. MAINTENANCE TROUBLESHOT IAW FIM 27-51-00-815-808 AND ACCOMPLISHED AN FSEU BITE TEST, FOUND THE NR 1 FLAP TRANSMISSION OVERLOAD INDICATOR TRIPPED. THE INDICATOR WAS RESET AND THE FLAP TRANSMISSION WAS LUBRICATED AND SERVICED.

Part: DUCT — LEAKING (HP 2) · airframe 53,974 hrs · 16,701 cycles

LEFT ENGINE FIRE WARNING ACTIVEATED INTERMITTENTLY, EVENTUALLY STOPPED BEFORE ENGINE SHUTDOWN. EMERGENCY DECLARED AND LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED HP2 AND HP6 DUCTS IAW MM 36-11-01, AND ACCOMPLISHED HIGH POWER RUN IAW MM 71-00-00. NO FIRE LOOP FAULTS OCCURED.

Part: DUCT — LEAKING (HP 6) · airframe 53,974 hrs · 16,701 cycles

LEFT ENGINE FIRE WARNING ACTIVATED INTERMITTENTLY, EVENTUALLY STOPPED BEFORE ENGINE SHUTDOWN. EMERGENCY DECLARED AND FLIGHT LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED HP2 AND HP6 DUCTS IAW MM 36-11-01 AND ACCOMPLISHED HIGH POWER RUN IAW MM 71-00-00. NO FIRE LOOP FAULTS OCCURED.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 53,829 hrs · 16,658 cycles

RIGHT AFT FLIGHT ATTENDANT SEAT EMERGENCY FLASHLIGHT WAS INOPERATIVE. REPLACED THE FLASHLIGHT BATTERY IAW AMM 25-64-00. OPS CHECKED OK.

Part: SKIN — DELAMINATED (LT WING SLAT) · airframe 53,663 hrs · 16,616 cycles

LEFT WING NR 1 LEADING EDGE SLAT DELAMINATED. THE AIRCRAFT WAS GROUNDED. REPLACED SLAT IAW AMM 27-81-02.

Part: TRANSMITTER — FAULTY (ZONE 100) · airframe 53,576 hrs · 16,592 cycles

AIRCRAFT WAS GROUNDED: REJECTED TAKEOFF AT 75 KNOTS, MAXIMUM GROUND SPEED 90 KTS DUE TO ENGINE PRESSURE RATIO. RIGHT ENGINE PRESSURE RATIO BLANKED AT 70 KNOTS. MAINTENANCE PERFORMED E-58 9768713, TROUBLESHOT RIGHT HAND ENGINE PRESSURE RATIO TRANSMITTER PER AMM 77-11-01 AND FIM 77-11-01-815-802-R00, REPLACED TRANSMITTER, AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: TRANSMITTER — FAILED (RT ENGINE) · airframe 53,576 hrs · 16,592 cycles

AIRCRAFT ABORTED TAKEOFF FOR AN EPR MESSAGE ON RIGHT ENGINE. RIGHT ENGINE EPR BLANKED AT 70 KTS. IAW E-58 9768713, TROUBLESHOT THE EPR TRANSMITTER IAW AMM 77-11-01, AND FIM 77-11-01-815-802-R00. REPLACED THE RIGHT ENGINE EPR TRANSMITTER IAW AMM 77-11-01. ALL TEST PASSED AND AIRCRAFT IS OK FOR SERVICE.

Part: TRANSMITTER — FAULTED (RT ENGINE EPR) · airframe 53,576 hrs · 16,592 cycles

ABORTED TAKE OFF AT 90 KNOTS DUE TO A LOSS OF EPR INDICATION, RIGHT ENGINE. FLIGHT RETURNED TO GATE. EPR BLANKED AT 70 KNOTS. REJECTED TAKEOFF AT 75 KNOTS. MAXIMUM GROUND SPEED 90 KNOTS. THE AIRCRAFT WAS GROUNDED. TROUBLESHOOTING RIGHT ENGINE EPR TRANSMITTER IAW AMM 77-11-01 AND FIM 77-11-01-815-802-R00. ALL TESTS PASSED, AIRCRAFT OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (MLG) · airframe 52,727 hrs · 16,387 cycles

BELOW 7000 FT ABOVE GROUND LEVEL, GEAR NOT DOWN AND CONFIGURATION WARNING, TEMPORARY ILLUMINATION. MAINTENANCE ACCOMPLISHED GEAR NOT DOWN CONFIGURATION WARNING TEST IAW FIM 31-51-00 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 52,665 hrs · 16,372 cycles

FOUND THE L1 DOOR SLIDE DISLODGED FROM DOOR. REPLACED THE SLIDE IAW 25-66-01.

Part: CHARGER — NO TEST (EMERGENCY LIGHTS) · airframe 52,603 hrs · 16,356 cycles

L1 DOOR UPPER EXIT SIGN INOPERATIVE DURING A TEST. REPLACED THE BATTERY CHARGER M731 IAW AMM 33-51-07.

Part: LIGHT — BROKEN (CABIN) · airframe 51,630 hrs · 16,093 cycles

AIRCRAFT WAS NOT GROUNDED: EXIT IDENTIFIER AT 4L DOOR, LENS WAS MISSING AND BROKEN. MAINTENANCE REPLACED BROKEN 4L EXIT IDENTIFIER SIGN AS REQUIRED AND PERFORMED SATISFACTORY OPERATIONAL CHECK PER M/M 33-51-00.

Part: VALVE — UNSERVICEABLE (WATER SYSTEM)

THE AIRCRAFT WAS GROUNDED. NO WATER IN LAVATORIES OR COFEE MAKERS. THE FLIGHT DIVERTED. AN EMERGENCY WAS DECLARED DUE TO OVERWEIGHT LANDING. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE EVALUATED AIRCRAFT AND FOUND EVIDENCE OF ICE ON EXTERIOR OF FUSELAGE, AFT OF THE FORWARD WATER SERVICE DOOR, THE POTABLE WATER SYSTEM WAS PLACED ON MEL DEFERRAL. WATER TANK FILL VALVE REPLACED PER MM 38-11-02. LEAK CHECK AND OPERATIONS CHECK GOOD.

Part: LENS — MISSING (CABIN) · airframe 50,974 hrs · 15,887 cycles

THE AIRCRAFT WAS NOT GROUNDED. THE SEAT 2E ESCAPE PATH LIGHTING LENS WAS MISSING. INSTALLED LENS IN THE SEAT 2E ESCAPE PATH LIGHTING IAW TECH REF, MAINTENANCE OR REPAIR DONE IN PREVIOUS UPDATE.

Part: SIGN — LOOSE (ROW 17DEF) · airframe 50,843 hrs · 15,858 cycles

THE EXIT SIGN AT ROW 17DEF FOUND LOOSE. REPLACED THE SIGN.

Part: LENS — DAMAGED (CABIN) · airframe 50,699 hrs · 15,829 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT AT ROW 18 ABC OVERWING EXIT SIDEWALL HAS A DAMAGED PLACARD. REPLACED LENS COVER (PLACARD) PER AMM 33-51-10. OPERATIONAL CHECK GOOD.

Part: LENS — DAMAGED (CABIN) · airframe 50,699 hrs · 15,829 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT AT ROW 17 DEF OVERWING EXIT SIDEWALL HAS A DAMAGED PLACARD. REPLACED LENS COVER (PLACARD) PER AMM 33-51-10. OPERATIONAL CHECK GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 50,699 hrs · 15,829 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT AT THE R4 GALLEY RIGHT SIDEWALL IS BROKEN. REMOVED AND REPLACED LIGHT ASSEMBLY PER AMM 33-51-10 AND WDM 33-51-15. OPERATIONAL CHECK GOOD.

Part: LENS — MISSING (CABIN) · airframe 50,699 hrs · 15,829 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT AT ROW 17 ABC OVERWING SIDEWALL HAS A MISSING LENS PLACARD. REPLACED LENS COVER (PLACARD) PER AMM 33-51-10. OPERATIONAL CHECK GOOD.

Part: PITOT TUBE — MALFUNCTIONED (CAPTAIN'S) · airframe 50,674 hrs · 15,823 cycles

EMERGENCY DECLARED. FLIGHT RETURNED TO DEPARTURE DUE TO ALTIMETER UNRELIABLE AND AIRSPEED INDICATION DISAGREE. LANDING UNEVENTUL. REMOVED AND REPLACED CAPTAINS PITOT PROBE IAW AMM 34-11-01. LEAK AND OPERATIONAL CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 50,239 hrs · 15,709 cycles

ROW 17H EXIT SIGN LENS IS LOOSE. MAINTENANCE SECURED THE EXIT SIGN LENS AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 50,069 hrs · 15,659 cycles

THE R1 DOOR EMERGENCY EXIT SIGN LENS MISSING. REPLACED SIGN LENS IAW-AMM 33-51-10.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 50,069 hrs · 15,659 cycles

THE AIRCRAFT WAS NOT GROUNDED. SEAT ROW 35DEF EMERGENCY LIGHT, AISLE SEAT IS OUT. INSPECTED AND FOUND A BROKEN CONNECTORS, REPAIRED AND INSTALLED A NEW CONNECTORS IAW AMM 20-12-13, OPS CHECKED NORMAL.

Part: LENS — MISSING (CABIN) · airframe 49,342 hrs · 15,450 cycles

AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT 4C HAS A MISSING LENS COVER. INSTALLED LENS COVER IAW AMM 33-51-05. OPERATIONAL CHECK GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 49,179 hrs · 15,403 cycles

FLOOR PROXIMITY EMERGENCY EXIT FLOODLIGHT IN THE FORWARD GALLEY HAS A MISSING LENS COVER. REPLACED LENS . OPERATIONAL CHECKED GOOD.

Part: CONNECTOR — LOOSE (CABIN) · airframe 48,843 hrs · 15,300 cycles

AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTS AT SEATS 2E AND 2F ARE INOPERATIVE. SECURED CONNECTOR IAW AMM 33-51-11. OPERATIONAL CHECK GOOD.

Part: POTABLE WATER — LOW · airframe 46,855 hrs · 14,820 cycles

DURING CRUISE CREW REPORTED A TOTAL LOSS OF POTABLE WATER. EMERGENCY DECLARED. LANDING UNEVENTFUL. SERVICED POTABLE WATER. NO LEAKS NOTED. OPS CHECKED NORMAL.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,091 hrs · 14,618 cycles

AIRCRAFT WAS IN BASE MX. CABIN FLOORBEAM AT FS 1640 IS CORRODED AT LBL 58. REPAIRED FLOORBEAM T CAP, BETWEEN LBL 34 & 61 IAW SRM 53-00-51-2R-8.

Part: LINE — LOOSE (CREW O2) · airframe 45,915 hrs · 14,579 cycles

AIRCRAFT WAS NOT GNDED. AIR INTERRUPT, EMER WAS DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING CRUISE, FLIGHT CREW O2 PRESS GRADUALLY DECREASED. PRESS WAS AT 40 ON LANDING. ACCOMPLISHED AMM TASK 35-11-00-206-023 & FOUND A LOOSE LINE BEHIND OBSERVERS MASK STORAGE BOX. TIGHTENED LINE & ACCOMPLISHED AMM TASK 12-15-08-603-001 LEAK CHECK WITH NO LEAKS NOTED.

Part: LENS — MISSING (EXIT SIGN) · airframe 45,729 hrs · 14,535 cycles

AFT GALLEY LT SIDE LIGHT LENS MISSING FOR EMER EXIT SIGN JUST AFT OF DOOR. INSTALLED NEW EMER EXIT SIGN LIGHT LENS AT AFT LT GALLEY JUST AFT OF DOOR IAW AMM 33-51-10. THE ACFT WAS NOT GNDED.

Part: IDG — FAILED (LT ENGINE) · airframe 44,183 hrs · 14,180 cycles

LEFT IDG FAILED ON CLIMB OUT, DISCONNECTED LT IDG IAW QRH. THE FLIGHT RETURNED, AN EMER WAS DECLARED & THE FLIGHT LANDED OVERWEIGHT. THE ACFT WAS REMOVED FROM SERVICE. R & R LT IDG IAW AMM 24-11-01, NO LEAKS FOUND. ACCOMPLISHED ALL REQUIRED TESTS, OK FOR SERVICE.

Part: VALVE — FAULTY (ZONE 400) · airframe 43,731 hrs · 14,085 cycles

DURING TAKEOFF ROLL, AT APPROXIMATELY 1.73 EPR, THE RT ENGINE N2 REACHED 103.1 FOR FIVE SECONDS. TAKEOFF ABORTED AT APPROX 90 TO 95 KNOTS. R & R HP 3 & HP 3 BLEED VALVES IAW AMM 75-32-04. R & R HP 3 & HP 2 SOLENOIDS IAW AMM 75-32-05. ACCOMPLISHED HIGH POWER ASSURANCE TEST & TEST NR 3 IAW AMM 71-00-00. SYS CHECKED NORMAL.

Part: SOLENOID — FAULTY (ZONE 400) · airframe 43,731 hrs · 14,085 cycles

DURING TAKEOFF ROLL, AT APPROXIMATELY 1.73 EPR, THE RT ENG N2 REACHED 103.1 FOR FIVE SECONDS. TAKEOFF ABORTED AT APPROXIMATELY 90 TO 95 KNOTS. R & R HP 3 & HP 3 BLEED VALVES IAW AMM 75-32-04. R & R HP 3 & HP 2 SOLENOIDS IAW AMM 75-32-05. ACCOMPLISHED HIGH POWER ASSURANCE TEST & TEST NR 3 IAW AMM 71-00-00. SYSTEM CHECKED NORMAL.

Part: SOLENOID — FAULTY (ZONE 400) · airframe 43,731 hrs · 14,085 cycles

DURING TAKEOFF ROLL, AT APPROXIMATELY 1.73 EPR, THE RT ENGINE N2 REACHED 103.1 FOR FIVE SECONDS. TAKEOFF ABORTED AT 90 TO 95 KNOTS. R & R HP 3 & HP 3 BLEED VALVES IAW AMM 75-32-04. R & R HP 3 & HP 2 SOLENOIDS IAW AMM 75-32-05. ACCOMPLISHED HIGH POWER ASSURANCE TEST & TEST NR 3 IAW AMM 71-00-00. SYS CHECKED NORMAL.

Part: SHUTOFF VALVE — FAULTY (RT ENGINE) · airframe 43,731 hrs · 14,085 cycles

DURING TAKEOFF ROLL, AT APPROXIMATELY 1.73 EPR, THE RT ENGINE N2 REACHED 103.1 FOR FIVE SECONDS. TAKEOFF ABORTED AT APPROXIMATELY 90 TO 95 KNOTS. R & R HP 3 & HP 3 BLEED VALVES IAW AMM 75-32-04. R & R HP 3 & HP 2 SOLENOIDS IAW AMM 75-32-05. ACCOMPLISHED HIGH POWER ASSURANCE TEST & TEST NR 3 IAW AMM 71-00-00. SYS CHECKED NORMAL.

Part: WINGLET — CORRODED (LT WING) · corrosion level 2 · airframe 41,564 hrs · 13,572 cycles

LEFT WING WINGLET TIP CORRODED BEYOND SRM LIMITS. R & R LT WINGLET TIP IAW AMM 57-31-03-402.

Part: SKIN — WORN (TE FLAP) · airframe 41,564 hrs · 13,572 cycles

WEAR ON LE SKIN OF RT INBD MAIN FLAP AT WS 231. REPAIRED SKIN & PROVIDED CLEARANCE FROM PANEL FWD OF FLAP IAW EA COMP-57-037721.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 37,967 hrs · 12,690 cycles

FLIGHT CREW ENTRANCE DOOR EMERGENCY EXIT SIGN INOPERATIVE. REPLACED EMERGENCY EXIT SIGN BATTERY PACK. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 37,869 hrs · 12,662 cycles

RT FWD OVERWING EXIT EMERGENCY FWD LIGHT INOPERATIVE. REPLACED LAMP FOR RT FWD OVERWING EXIT EMERGENCY FWD LIGHT. OPERATIONS CHECKED NORMAL.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 35,772 hrs · 12,140 cycles

EXTERNAL FUSELAGE REPAIR DOUBLER LOCATED BODY STATIONS 334 TO 340 BETWEEN STRINGERS 17 AND 18 LEFT DAMAGED. REMOVED FLOORBOARD AND ACCOMPLISHED REPAIR PER REO G16170 REVISION A AND INSTALLED FLOORBOARD PER AMM 53-01-01.

Part: SKIN — SCRATCHED (LT WING) · airframe 35,772 hrs · 12,140 cycles

LEFT WING LOWER SKIN HAS 4 SCRATCHED AREAS WITHIN 1.5 INCHES OF FASTENERS THAT HAVE BEEN BURNISHED AND PAINTED BETWEEN STATIONS 954 AND 775. ACCOMPLISHED REPAIRED PER REO-G16161 REVISION C AND EA B757-57-029550.

Part: ACCESS PANEL — DENTED (LT WING) · airframe 35,772 hrs · 12,140 cycles

INTERIM REPAIR TO LOWER LEFT WING DAMAGED AT ACCESS PANEL 534AB. REPAIRED PER REO-G16161 REVISION C AND EA B757-57-029550.

Part: GATE — CORRODED (R4 DOOR) · corrosion level 2 · airframe 35,772 hrs · 12,140 cycles

RIGHT NUMBER 4 DOOR LOWER GATE EDGE CORRODED. ACCOMPLISHED REPAIR PER EA COMP-52-029472.

Part: DOOR FRAME — DENTED (FUSELAGE) · airframe 35,772 hrs · 12,140 cycles

FORWARD E AND E DOOR FRAME DENT AT POINT LATCHING MECHANISM INTERSECTS FROM STATIONS 231 AND BUTTLINE 0. REMOVED DAMAGE AND INSTALLED REPAIR ANGLE REO-G16140 REVISION A.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,772 hrs · 12,140 cycles

FORWARD CARGO COMPARTMENT, LOWER DOOR SILL FITTING AT STATION 607.3 IS CORRODED. REPLACED FITTING PER SRM 51-10-02 SECTION 9.

Part: STRINGER — DENTED (FUSELAGE) · airframe 35,772 hrs · 12,140 cycles

AFT CARGO COMPARTMENT AT STATION 1420 AND STRINGER 25 LEFT DENTED. REMOVED LEFT TRANSITION PANEL FROM STATIONS 1410 TO 1530. CUT OUT DAMAGE AND INSTALLED REPAIR SPLICE AND 2 EACH REPAIR STRINGER CLIPS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,602 hrs · 11,649 cycles

EMERGENCY AISLE LIGHT AT SEAT 10D INOPERATIVE. REPLACED LAMP FOR SEAT 10D EMERGENCY AISLE LIGHT. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 33,461 hrs · 11,620 cycles

ROWS 26 TO 37 SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR ROWS 26 TO 37 SEAT MOUNTED EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 33,155 hrs · 11,510 cycles

LEFT NUMBER 1 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 1 DOOR EMERGENCY LIGHT. OPS CHECKED NORMAL.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 33,155 hrs · 11,510 cycles

LEFT NUMBER 1 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 1 DOOR EMERGENCY LIGHT. OPS CHECKED NORMAL.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 33,155 hrs · 11,510 cycles

R4 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR R4 DOOR EMERGENCY LIGHT. OPS CHECKED NORMAL.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 33,155 hrs · 11,510 cycles

R1 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 1 DOOR EMERGENCY LIGHT. OPS CHECKED NORMAL.

Part: LENS — DIRTY (EMERGENCY LIGHT) · airframe 33,155 hrs · 11,510 cycles

EMERGENCY LIGHT LENS AT SEAT 12DEF HAS RESIDUE OBSTRUCTING LIGHT. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 12DEF. OPS CHECKED NORMAL.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 33,155 hrs · 11,510 cycles

P62 PANEL, EMERGENCY LIGHT TEST SWITCH INOPERATIVE. FOUND PIN TO GROUND PUSHED BACK IN CONNECTOR D40488. LOCKED PIN. OPS CHECKED NORMAL.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 33,155 hrs · 11,510 cycles

L4 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR L4 DOOR EMERGENCY LIGHT. OPS CHECKED NORMAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,166 hrs · 11,131 cycles

CRACK IN MAIN FRAME AT STATION 395 AND LEFT BUTTLINE 24. PERMANENT REPAIR ACCOMPLISHED PER EA B757-53-020928.

Part: BUSHING — CORRODED (LT MLG TRUNNION) · corrosion level 2 · airframe 32,092 hrs · 11,105 cycles

CORROSION AROUND LEFT FORWARD TRUNNION OUTBOARD UPPER BUSHING. REMOVED CORROSION AND REPLACED BUSHING PER EA B757-57-020367.

Part: BUSHING — CORRODED (LT MLG TRUNNION) · corrosion level 2 · airframe 32,092 hrs · 11,105 cycles

CORROSION AROUND LEFT FORWARD TRUNNION INBOARD LOWER BUSHING. REMOVED CORROSION AND REPLACED BUSHING PER EA B757-57-020367.

Part: BUSHING — CORRODED (RT MLG TRUNNION) · corrosion level 2 · airframe 321,092 hrs · 11,105 cycles

CORROSION AROUND RIGHT FORWARD TRUNNION OUTBOARD LOWER BUSHING. REMOVED CORROSION AND REPLACED BUSHING PER EA B757-57-020367.

Part: BUSHING — CORRODED (LT MLG TRUNNION) · corrosion level 2 · airframe 32,092 hrs · 11,105 cycles

CORROSION AROUND LEFT TRUNNION UPPER BUSHING. REMOVED CORROSION AND REPLACED BUSHING PER EA B757-57-020367.

Part: BUSHING — CORRODED (LT MLG TRUNNION) · corrosion level 2 · airframe 32,092 hrs · 11,105 cycles

CORROSION AROUND LEFT FORWARD TRUNNION OUTBOARD LOWER BUSHING. REMOVED CORROSION AND REPLACED BUSHING PER EA B757-57-020367.

Part: BUSHING — CORRODED (RT MLG TRUNNION) · corrosion level 2 · airframe 32,092 hrs · 11,105 cycles

CORROSION AROUND RIGHT FORWARD TRUNNION INBOARD UPPER BUSHING. REMOVED CORROSION AND REPLACED BUSHING PER EA B757-57-020367.

Part: BUSHING — CORRODED (RT MLG TRUNNION) · corrosion level 2 · airframe 32,092 hrs · 11,105 cycles

CORROSION AROUND RIGHT FORWARD TRUNNION INBOARD LOWER BUSHING. REMOVED CORROSION AND REPLACED BUSHING PER EA B757-57-020367.

Part: BUSHING — CORRODED (RT MLG TRUNNION) · corrosion level 2 · airframe 32,092 hrs · 11,105 cycles

CORROSION AROUND RIGHT FORWARD TRUNNION OUTBOARD UPPER BUSHING. REMOVED CORROSION AND REPLACED BUSHING PER EA B757-57-020367.

Part: GCU — INOPERATIVE (ZONE 600) · airframe 31,968 hrs · 11,063 cycles

JFK - CREW REPORTED RIGHT ENGINE GENERATOR FAILED. EMERGENCY DECLARED FLIGHT RETURNED JFK LANDED WITHOUT INCIDENT. PLACARDED RIGHT INTEGRATED DRIVE GENERATOR INOPERATIVE. FLIGHT CONTINUED TO AUA. REPLACED GENERATOR CONTROL UNIT AT TUL ON 11/1/2011. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,337 hrs · 10,487 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,337 hrs · 10,487 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,337 hrs · 10,487 cycles

LEFT NUMBER 2 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 2 DOOR EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,020 hrs · 9,317 cycles

RIGHT NUMBER 1 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 1 DOOR EMERGENCY LIGHT. OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,020 hrs · 9,317 cycles

LEFT NUMBER 1 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 1 DOOR EMERGENCY LIGHT. OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,020 hrs · 9,317 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 25,840 hrs · 8,894 cycles

ALL FIRST CLASS FWD GALLEY EXIT MARKER DIM. REPLACED BATTERY PACK AND CHARGER ASSEMBLY.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 25,840 hrs · 8,894 cycles

AFT GALLEY EMERGENCY EXIT MARKERS DIM. REPLACED BATTERY PACK AND CHARGER ASSEMBLY.

Part: SOCKET — INOPERATIVE (CABIN) · airframe 25,840 hrs · 8,894 cycles

EMERGENCY LIGHT AT RIGHT NUMBER THREE DOOR SLIDE INOPERATIVE. REPLACED SOCKET.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 25,840 hrs · 8,894 cycles

FIRST CLASS SEAT MOUNTED EMERGENCY LIGHTS DIM. REPLACED BATTERY PACK AND CHARGER ASSEMBLY.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 25,840 hrs · 8,894 cycles

SEAT MOUNTED EMERGENCY LIGHTS IN COACH ARE DIM. REPLACED BATTERY PACK AND CHARGER ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,840 hrs · 8,894 cycles

EMERGENCY LIGHT AT RIGHT FORWARD OVERWING EXIT INOPERATIVE. REPLACED LAMP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,626 hrs · 8,821 cycles

LEFT NUMBER FOUR DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LEFT NUMBER FOUR DOOR SLIDE LIGHT.

Part: LENS — MISSING (CABIN) · airframe 25,288 hrs · 8,702 cycles

EMERGENCY EXIT LIGHT SIGN COVER MISSING AT RIGHT NUMBER FOUR DOOR IN AFT GALLEY. REPLACED MISSING LIGHT COVER. OP CHECK OK.

Part: CONNECTOR — BURNED (P1 PROBE) · airframe 23,972 hrs · 8,265 cycles

VVI INFLIGHT MIA-LPB - RIGHT ENGINE PRESSURE RATIO PROBLEM. LANDED VVI WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND ENGINE P1-PROBE WITH BURNT PINS AND P1 PROBE CONNECTOR WITH TWO SOCKETS BURNED. REMOVED AND REPLACED P1 PROBE CONNECTOR. REPLACED ENGINE PRESSURE RATIO TRANSMITTER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — MALFUNCTIONED (ZONE 200) · airframe 23,747 hrs

MIA ESCAPE PATH LIGHTING FOR SEATS 26D TO 30D VERY DIM. RECHARGED LIGHT SYSTEM FOR ESCAPE PATH LIGHTING FOR SEATS 26D TO 30D.

Part: CONNECTOR — LOOSE (CABIN) · airframe 22,396 hrs

MIA - EMERGENCY LIGHT AT SEAT 9D INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 22,396 hrs

MIA - EMERGENCY LIGHT AT SEAT 32D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 32D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,279 hrs

DFW - EXTERIOR EMERGENCY LIGHT AT LT NR FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LT NR FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,279 hrs

DFW - EXTERIOR EMERGENCY LIGHT AT RT NR FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT RT NR FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: LIGHT — INOPERATIVE (ROW 12) · airframe 21,279 hrs

DFW - EMERGENCY LIGHT AT SEAT ROW 12 INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT ROW 12. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,279 hrs

DFW - EXTERIOR EMERGENCY LIGHT AT LT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LT NR TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR SLIDE INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SJU - EMERGENCY LIGHTS FROM SEAT ROWS 9D TO 15D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FROM SEAT ROWS 9D TO 15D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHTS AT SEAT ROW 16DEF INOPERATIVE. RECONNECTED WIRING AT WALL FOR EMERGENCY LIGHTS AT SEAT ROW 16DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (CABIN)

DFW - OVERWING EMERGENCY LIGHTS AT RIGHT HAND FORWARD AND LEFT HAND AFT LIGHT INOPERATIVE. REPLACED BATTERY PACKS FOR OVERWING EMERGENCY LIGHTS AT RIGHT HAND FORWARD AND LEFT HAND AFT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.