N190AA

Part: STRUCTURE — LEAKING (RT WING DRY BAY) · airframe 63,957 hrs · 16,126 cycles

AIRCRAFT WAS GROUNDED: RIGHT WING HAS 3 STAINS OFF FUEL COMING FROM DRY BAY DRAIN HOLE. MAINTENANCE DESEALED, CLEANED, AND RESEALED RIGHT WING DRY BAY STRUCTURE AS REQUIRED. SATISFACTORY LEAK CHECK ACCOMPLISHED.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 63,375 hrs · 15,937 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT AT SEAT 4E ON SIDE OF SEAT INOPERABLE. MAINTENANCE SECURED LOOSE CONNECTOR AND PERFORMED SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00.

Part: UNKNOWN — MALFUNCTIONED (ENGINE) · airframe 63,202 hrs · 15,886 cycles

AIRCRAFT WAS GROUNDED: PILOT ABORTED TAKEOFF DUE TO AIRCRAFT PULLED TO THE LEFT, THE RIGHT ENGINE ACCELERATES FASTER THAN THE LEFT ENGINE. RUDDER AND NOSEWHEEL STEERING USED. ACFT WT 204,000. NO REVERSERS, NO AUTOBRAKES, SPEED LESS THAN 3OKTS. MAINTENANCE REPORTS REMOVED AND REPLACED LT AND RT NOSE TIRES IAW AMM 32-45-02. LUBRICATED NOSE LANDING GEAR IAW AMM 12-21-12. ACCOMPLISHED ENGINE RUN UP IAW AMM 71-00-00, FOUND NORMAL. TAXIED A/C FOUND STEERING NORMAL.

Part: LIGHT — INOPERATIVE (L1 DOOR SLIDE) · airframe 63,006 hrs · 15,835 cycles

AIRCRAFT NOT GROUNDED: PILOT RPEORTS 1L DOOR SLIDE ARMED LIGHT INOPERATIVE. MAINTENANCE REPLACED 1L DOOR SLIDE ARMED LIGHT ASSY, OPS CHECKS GOOD.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 62,770 hrs · 15,764 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT MOUNTED EMERGENCY LIGHTS INOPERABLE AT SEAT 1EF. MAINTENANCE FOUND LOOSE CONNECTION AT WALL AND RECONNECTED CONNECTOR PER MM 33-51-11.

Part: CONTROL MODULE — MALFUNCTIONED (ZONE 100) · airframe 62,527 hrs · 15,705 cycles

AIRCRAFT WAS NOT GROUNDED: SPOILER MESSAGE APPEARED AFTER TAKE OFF, WOULD NOT CLEAR, QRH COMPLIED WITH. MAINTENANCE ACCOMPLISHED BITE PROCEDURE OF SPOILER CONTROL MODULES AND ACCOMPLISHED RESET OF #3 LEFT SCM. FAULT ERASED AND PERFORMED SATISFACTORY OPERATIONAL CHECK PER FIM PROCEDURE 27-61-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,935 hrs · 15,555 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY MARKERS AT 4L AND 4R (SEE AALA201905169012) DOOR INOPERATIVE. MAINTENANCE PERFORMED SATISFACTORY OPERATIONAL CHECK OF 4L AND 4R DOOR MARKERS PER AMM 33-51-10.

Part: BATTERY — DISCHARGED (CABIN) · airframe 61,935 hrs · 15,555 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT MOUNTED EMERGENCY LIGHTS 26D THROUGH 36D INOPERATIVE. MAINTENANCE REPLACED CHARGER (SEE AALA201905169007) AND BATTERY ASSEMBLY PER AMM 33-51-07.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 61,935 hrs · 15,555 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT MOUNTED EMERGENCY LIGHTS 26D THROUGH 36D INOPERATIVE. MAINTENANCE REPLACED CHARGER AND BATTERY ASSEMBLY (SEE AALA201905169013) PER AMM 33-51-07.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,935 hrs · 15,555 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY MARKERS AT 4L (SEE AALA201905169006) AND 4R DOOR INOPERATIVE. MAINTENANCE PERFORMED SATISFACTORY OPERATIONAL CHECK OF 4L AND 4R DOOR MARKERS PER AMM 33-51-10.

Part: BATTERY — DISCHARGED (CABIN) · airframe 61,935 hrs · 15,555 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT MOUNTED EMERGENCY LIGHTS IN FIRST CLASS WERE VERY DIM. MAINTENANCE REPLACED CHARGER (SEE AALA201905169005) AND BATTERY ASSEMBLY PER AMM 33-51-07.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 61,935 hrs · 15,555 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT MOUNTED EMERGENCY LIGHTS IN FIRST CLASS WERE VERY DIM. MAINTENANCE REPLACED CHARGER AND BATTERY (SEE AALA201905169011) ASSEMBLY PER AMM 33-51-07.

Part: BATTERY — WEAK (EMERGENCY LIGHTS) · airframe 60,391 hrs · 15,089 cycles

SEAT MOUNTED EMERGENCY LIGHTS AT 9D THRU 14D WERE VERY DIM. TROUBLESHOT AND REPLACED THE BATTERY PACK IAW AMM 33-51-07. SYSTEM OPS NORMALLY.

Part: CHARGER — UNKNOWN (EMERGENCY LIGHTS) · airframe 60,393 hrs · 15,090 cycles

SEAT MOUNTED EMERGENCY LIGHTS AT 9D THRU 14D WERE VERY DIM. TROUBLESHOT AND REPLACED THE CHARGER IAW AMM 33-51-07. SYSTEM OPS NORMALLY.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 60,061 hrs · 14,998 cycles

CORROSION ON THE LEFT WING UPPER SURFACE SKIN NEAR THE OVERWING FILL PORT. REPAIRED THE SKIN IAW SRM 57-20-01, REPAIR 6, AND EA 283845.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 60,061 hrs · 14,998 cycles

CORROSION WAS FOUND ON THE RIGHT WING UPPER SURFACE SKIN NEAR THE OVERWING FILL PORT. REPAIRED THE SKIN IAW SRM 57-20-01, REPAIR 6, AND EA 283832.

Part: SKIN — CRACKED (RT WING) · airframe 60,061 hrs · 14,998 cycles

RIGHT WING SKIN HAD A CRACK INDICATION AT DIAGONAL BRACE FASTENER HOLE NR 4. REPAIRED THE WING SKIN IAW EA 283659.

Part: DOUBLER — CORRODED (BS 1681) · corrosion level 2 · airframe 60,061 hrs · 14,998 cycles

CORROSION FOUND ON BACK DECK DOUBLER LOCATED AT BS 1681, RBL 52. REPLACED DOUBLER IAW SRM 53-60-51-2R-10, AND SRM 51-40-02.

Part: SKIN — DELAMINATED (LT AILERON) · airframe 59,904 hrs · 14,955 cycles

THE LEFT WING AILERON HAD TWO WATER INGRESSION DELAMINATION AREAS AT THE INBOARD EDGE. THE AIRCRAFT WAS GROUNDED. REPLACED THE AILERON IAW AMM 27-11-21.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 59,594 hrs · 14,881 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY FLASHLIGHT TESTS RED LOCATED IN THE FLIGHT ATTENDANT STATION 2R CABIN ENTRY DOOR. REPLACED EMERGENCY FLASHLIGHT BATTERY.

Part: FMC — MALFUNCTIONED (FIRST OFFICER'S) · airframe 59,152 hrs · 14,773 cycles

WHILE TRYING TO SELECT DIRECT TO A WAYPOINT ON THE LEGS PAGE AT THE F/OS CDU BOTH FMCS LOCKED UP WITH STANDBY ONE DISPLAYED. ON OTHER MESSAGES, BOTH FMC COMPUTES LOADED CORRECT SOFTWARE AND NAV DATABASE. ALL CHECKED NORMAL PER AMM 34-61-01. THE AIRCRAFT WAS GROUNDED.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 59,149 hrs · 14,772 cycles

SEAT MOUNTED EMERGENCY LIGHT AT 34D INOPERATIVE. MAINTENANCE RESEATED A LOOSE CONNECTOR UNDER SEAT 34D AND PERFORMED A SATISFACTORY OPS CHECKED IAW AMM 33-51-11.

Part: LIGHT — BROKEN (SEAT 2J) · airframe 58,943 hrs · 14,716 cycles

SEAT 2J EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT IAW AMM 33-51-11.

Part: SPACER — MISSING (L2 DOOR SLIDE) · airframe 58,669 hrs · 14,634 cycles

L2 DOOR SLIDE RELEASE STRAP IS MISSING TWO SPACERS AND LINKS IAW AMM 25-66-01-404-044 VIEW A, FIG 405. REPLACED THE SPACERS AND LINKS IAW AMM 25-66-01-404-044, VIEW A, FIG 405. OK FOR SERVICE.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 58,605 hrs · 14,619 cycles

EMERGENCY LIGHT LENS MISSING AT SEAT 2EF. REPLACED THE LENS IAW AMM 33-50-00 .

Part: UNKNOWN — MALFUNCTIONED (RT ENGINE) · airframe 58,463 hrs · 14,574 cycles

DURING CRUISE, THE AIRCRAFT EXPERIENCED A THROTTLE SPLIT AND THE RIGHT HAND ENGINE. THE ENGINE WOULD NOT MAKE POWER. THE AIRCRAFT DIVERTED TO PTY AND LANDED WITHOUT FURTHER INCIDENT. CONTRACT MAINTENANCE IS TROUBLESHOOTING THE FAULT. THE AIRCRAFT WAS GROUNDED.

Part: FUEL FILTER — FAULTY (RT ENGINE) · airframe 58,463 hrs · 14,574 cycles

THE AIRCRAFT WAS GROUNDED. AT CRUISE, THE AIRCRAFT EXPERIENCED A THROTTLE SPLIT AND THE RIGHT HAND ENGINE. THE ENGINE WOULD NOT MAKE POWER. THE AIRCRAFT DIVERTED TO PTY AND LANDED WITHOUT FURTHER INCIDENT. CONTRACT MAINTENANCE IS TROUBLESHOOTING THE FAULT. *** SUPPLEMENTAL REPORT TO UPDATE SECTIONS 4 AND 5. REPLACED NR 2 ENGINE FUEL FILTER PER MM 73-11-10. *** (CLOSED) (SEE CONTROL AALA20180125007 AND AALA201801309025) (MICS 70265023 AND 34049409)

Part: GOVERNOR — FAULTY (RT ENGINE) · airframe 58,463 hrs · 14,574 cycles

THE AIRCRAFT WAS GROUNDED. AT CRUISE, THE AIRCRAFT EXPERIENCED A THROTTLE SPLIT AND THE RIGHT HAND ENGINE. THE ENGINE WOULD NOT MAKE POWER. THE AIRCRAFT DIVERTED TO PTY AND LANDED WITHOUT FURTHER INCIDENT. CONTRACT MAINTENANCE IS TROUBLESHOOTING THE FAULT. *** SUPPLEMENTAL REPORT TO UPDATE SECTIONS 4 AND 5. REPLACED NR 2 ENGINE FUEL FLOW GOVERNOR PER MCM CARD 73-94-01. *** (CLOSED) (SEE CONTROL #AALA20180125007 AND #AALA201801309026) (MICS 70265023 AND 34049409)

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 58,360 hrs · 14,543 cycles

AIRCRAFT WAS NOT GROUNDED. FIRST CLASS EMERGENCY AISLE LIGHTS ON SEATS INOPERABLE. REPLACED POWER SUPPLY AND BATTERY IAW MM 33-51-07.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 58,357 hrs · 14,542 cycles

AIRCRAFT WAS NOT GROUNDED: MID GALLEY AREA FLIGHT ATTENDANT SEAT, LEFT HAND EMERGENCY FLASH LIGHT INOPERABLE. MAINTENANCE REPLACED FLASH LIGHT PER AMM 25-64-00 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 58,045 hrs · 14,445 cycles

AIRCRAFT WAS NOT GROUNDED. FIRST CLASS FORWARD FLIGHT ATTENDANT SEAT EMERGENCY FLASHLIGHT WAS INOPERATIVE. REPLACED THE FIRST CLASS FORWARD FLIGHT ATTENDANT SEAT EMERGENCY FLASHLIGHT IAW AMM 25-64-00.

Part: GROUND WIRE — DISCONNECTED (ZONE 200) · airframe 57,008 hrs · 14,159 cycles

AIRCRAFT WAS GROUNDED. 30 MINUTES AFTER TAKEOFF AT FL 380, GOT INCREASING ELECTRICAL SMELL. LASTED 2 MINUTES THEN WENT AWAY. ODOR IN COCKPIT ONLY. MAINTENANCE FOUND GROUND WIRE DISCONNECTED FROM GROUND STUD ON P11 OVERHEAD PANEL, LEFT HAND SIDE METAL FRAME. RE-ATTACHED GROUND WIRE PER AMM SWPM 20-20-00. ACCOMPLISHED SIC 05-96-70 ALL SYSTEMS AND LIGHTS NORMAL, NO ODOR NOTED.

Part: BATTERY — NO TEST (FLASHLIGHT) · airframe 56,816 hrs · 14,103 cycles

FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT THE L2 JUMPSEAT IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-64-00. OPERATIONAL CHECKED GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 56,642 hrs · 14,066 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT BY THE L4 DOOR IS BROKEN. REMOVED AND REPLACED LIGHT ASSEMBLY IAW AMM 33-51-01. OPERATIONAL CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 56,207 hrs · 13,951 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT NR 1 EMERGENCY FLASHLIGHT LED IS NOT FLASHING. REMOVED AND REPLACED FLASHLIGHT ASSEMBLY IAW AMM 25-64-00. OPERATIONAL CHECK GOOD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 55,948 hrs · 13,868 cycles

AIRCRAFT WAS GROUNDED. DURING OPERATIONAL CHECK OF S10035, FOUND EMERGENCY ESCAPE PATH LIGHTS FROM SEAT 9 TO 15, EMERGENCY EXIT INDICATOR L752 AT L2 DOOR, AND EMERGENCY EXIT INDICATOR L751 AT R2 DOOR INOPERATIVE. REMOVED AND REPLACED BATTERY PACK (AALA201703209041) AND CHARGER ASSEMBLY AT M10952 IAW AMM 33-51-07. OPERATIONAL CHECK GOOD. ALSO REFERENCE AALA201703209044

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,948 hrs · 13,868 cycles

DURING OPERATIONAL CHECK OF S10035, FOUND EMERGENCY LIGHTS FROM SEAT 9 - 15, EMERGENCY EXIT INDICATOR L752 AT L2 DOOR, AND EMERGENCY EXIT INDICATOR L751 AT R2 DOOR INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK AND CHARGER ASSEMBLY IAW AMM 33-51-07. OPERATIONAL CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: SWITCH — FAULTY (ZONE 200) · airframe 55,948 hrs · 13,868 cycles

AIRCRAFT WAS GROUNDED. MIA-UIO FLIGHT RETURNED TO MIA ACCOUNT CABIN EMERGENCY EXIT LIGHTS CYCLING ON AND OFF INTERMITTENTLY. NO EMERGENCY DECLARED. UNEVENTFUL LANDING. REMOVED AND REPLACED NOSE LANDING GEAR EMERGENCY LIGHT TEST SWITCH AT S10035 IAW WDM 33-51-11. OPERATIONAL CHECK GOOD. REFERENCE AALA201703209041 AND AALA20170318001.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 55,893 hrs · 13,854 cycles

EMERGENCY EXIT SIGN BY L4 DOOR HAS A MISSING LENS COVER. REPLACED LENS. OPS CHECKED GOOD.

Part: CONTROLLER — UNSERVICEABLE (WINDOW HEAT) · airframe 55,605 hrs · 13,773 cycles

AIRCRAFT WAS GROUNDED. DURING CRUISE, THE RIGHT FORWARD PILOT/CO-PILOT WINDOW PANE CRACKED. AIRCRAFT PRESSURE WAS MAINTAINED. REMOVED AND REPLACED THE R1 WINDOW ASSEMBLY IAW AMM 56-11-01 (AALA20170202021) AND THE WINDOW HEAT CONTROLLER UNIT IAW AMM 30-41-01. OPERATIONAL CHECK GOOD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 55,605 hrs · 13,773 cycles

AIRCRAFT WAS GROUNDED. DURING CRUISE, THE RIGHT FORWARD PILOT/CO-PILOT WINDOW PANE CRACKED. AIRCRAFT PRESSURE WAS MAINTAINED. REMOVED AND REPLACED THE R1 WINDOW ASSEMBLY IAW AMM 56-11-01 AND THE WINDOW HEAT CONTROLLER UNIT IAW AMM 30-41-01 (AALA20170202022). OPERATIONAL CHECK GOOD.

Part: SEAL — DIRTY (COCKPIT) · airframe 55,577 hrs · 13,766 cycles

AIRCRAFT NOT GROUNDED. FIRST OFFICERS SLIDING WINDOW IS DIFFICULT TO CLOSE. CLEANED STICKY RESIDUE OFF WINDOW SEAL. WINDOW OPERATING WITHIN LIMITS IAW AMM 56-11-02. (CLOSED)

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 55,564 hrs · 13,759 cycles

SEAT MOUNTED EMERGENCY LIGHTS FOR ROWS 26 THROUGH 36 ARE INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-07. OPERATIONAL CHECKED GOOD.

Part: SWITCH — FAULTY (ZONE 200) · airframe 55,533 hrs · 13,747 cycles

AIRCRAFT WAS GROUNDED. LEFT ENGINE FUEL CONTROL WOULD NOT SHUT DOWN ENGINE. REMOVED AND REPLACED LEFT ENGINE FUEL CONTROL SWITCH IAW AMM 76-11-02 AND SWPM 20-61-11. OPERATIONAL CHECK GOOD.

Part: CHARGER — FAULTY (ZONE 100) · airframe 55,244 hrs · 13,668 cycles

AIRCRAFT WAS GROUNDED. JFK, AIR INTERRUPT, JKF-BHX. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT OVERWEIGHT. DURING FLIGHT AND EICAS MAIN BATTERY CHARGER MESSAGE WAS GENERATED. STANDBY POWER SWITCH WAS CYCLED TO BATTERY THEN BACK TO AUTO TWICE. MESSAGE DID NOT CLEAR. REMOVED AND REPLACED MAIN BATTERY CHARGER IAW AMM 24-31-02. OPERATIONAL TEST NORMAL IAW AMM 24-31-01.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 53,522 hrs · 13,230 cycles

AIRCRAFT WAS NOT GROUNDED. EXTERIOR EMERGENCY LIGHT AT R4 DOOR IS INOPERATIVE. R & R LIGHT ASSEMBLY. OPS CHECK NORMAL.

Part: FAN — FAULTY (CABIN) · airframe 52,755 hrs · 13,040 cycles

AIRCRAFT WAS GNDED. LT RECIRCULATION FAN INOPERATIVE LIGHT ILLUMINATED. ACCOMPANIED BY A REPORT OF SMOKE & ODOR IN THE AFT CABIN. LEFT RECIRCULATION FAN SWITCHED TO OFF. R & R THE LT RECIRCULATION FAN IAW AMM 21-25-01. SYS CHECKED NORMAL.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,660 hrs · 12,796 cycles

CORRODED APU INLET DOOR FWD LANDING STRAP AT STATION1790, BETWEEN STRINGER 3R - 6R. R & R LANDING STRAP IAW AARD 51-00-05-1 REPAIR 1 & AMM 49-15-08.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,660 hrs · 12,796 cycles

CORROSION ON AFT DECK WEB, BETWEEN STATIONS 1708 & 1720 FROM RBL 52 TO LBL 52. REMOVED CORROSION & APPLIED DOUBLER IAW SRM 53-60-51-2R & 53-51-51-2R.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 49,592 hrs · 12,326 cycles

EMERGENCY AISLE LIGHTS 9DE TO 15D DIM. R & R THE BATTERY AT M10952, FS 692. PERFORMED OPS CHECK IAW AMM 33-51-00. SYS CHECKED NORMAL.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 49,384 hrs · 12,279 cycles

CREW REPORTED AUTO SPEED BRAKE FAULT, LIGHT ILLUMINATED. NO EMERGENCY DECLARED, LANDING UNEVENTFUL. LIGHT EXTINGUISHED AFTER LANDING & FLIGHT CONTINUED TO DESTINATION.

Part: PIN — BACKED OUT (CABIN) · airframe 49,140 hrs · 12,217 cycles

SEAT MOUNTED EMER LIGHT AT 36D IS INOPERATIVE. FOUND PUSHED BACK PINS AT WALL TO SEAT CONNECTOR. REPAIRED IAW SWPM 20-42-01. SYS CHECKED NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 48,085 hrs · 11,977 cycles

EMERGENCY EXIT PATHWAY LIGHT AT SEAT 10D INOPERATIVE. FOUND LOOSE CONNECTOR AT SIDEWALL. RECONNECTED CONNECTOR FOR SEAT MOUNTED EMER LIGHT AT 10D. OPERATIONS CHECKED NORMAL.

Part: COMPUTER — INOPERATIVE (ZONE 100) · airframe 47,520 hrs · 11,840 cycles

RIGHT FLIGHT MANAGEMENT COMPUTER FAILED IN FLIGHT. FLIGHT DIVERTED & LANDED WITHOUT INCIDENT. ACCOMPLISHED DEFERRAL OF FLIGHT MANAGEMENT COMPUTER IAW MEL. REPLACED RT CONTROL DISPLAY UNIT MPN 4077880908 ON 07/20/2014.

Part: SKIN — CORRODED (LT WING) · airframe 47,154 hrs · 11,732 cycles

LEFT WING UPPER SKIN AT BLACK & YELLOW STRIPE CORRODED. BLENDED OUT CORROSION, NDT PERFORMED FPI & HFEC, FLAPPER PEENED, TREATED, PRIMED & PAINTED.

Part: SKIN — DENTED (LE SLAT) · airframe 47,154 hrs · 11,732 cycles

FOUND MULTIPLE DENTS ON NR 6 SLAT LE SKIN AT FSS 231. CUT OUT DAMAGED AREA, INSTALLED INTERNAL DOUBLER & FILLER, THEN INSTALLED FLUSH PATCH ON COVE SKIN.

Part: ANTI-ICE VALVE — INOPERATIVE (LT ENGINE) · airframe 46,279 hrs · 11,521 cycles

JFK CREW REPORTED LT HAND ENG ANTI ICE EICAS MESSAGE. EMERGENCY DECLARED FLIGHT RETURNED JFK LANDED WITHOUT INCIDENT. PLACARDED VLV INOPERATIVE IAW MEL 30-04B AUTH 02-922DC-C. FLIGHT CONTINUED TO DESTINATION. REPLACED LT ENG COWL ANTI ICE VLV AT JFK ON 02/25/20140. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: STIFFENER — CORRODED (LT WING) · corrosion level 2 · airframe 41,495 hrs · 10,398 cycles

LEFT WING REAR SPAR STIFFENER WS 202.92 CORRODED AT BONDING JUMPER. ACCOMPLISHED NESTED ANGLE REPAIR PER EA B757-57-026844.

Part: GATE — CORRODED (R4 DOOR) · corrosion level 2 · airframe 41,495 hrs · 10,398 cycles

RIGHT NUMBER 4 DOOR LOWER GATE HAS PITTING CORROSION ON LOWER EXTERNAL LIP AREA. REPAIRED R4 DOOR LOWER GATE PER EA 757-52-026716 AND G15490 REVISION D.

Part: ATTACH FITTING — CRACKED (LT WING) · airframe 41,495 hrs · 10,398 cycles

LEFT WING WINGLET ADAPTER PLUG ATTACH FLANGE CRACKED. REMOVED DAMAGE AND INSTALLED ANGLE, FILLER AND NUT PLATE CHANNEL PER EA 757-57-026567 REVISION A.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,495 hrs · 10,398 cycles

CORROSION ON SUBFLOOR AT STATION 1680, LEFT BUTTLINE 10. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER PER B757 SRM 53-60-51-2R.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,495 hrs · 10,398 cycles

MAIN CABIN FLOOR SHEAR WEB CORRODED FROM BODY STATIONS 1711 TO 1717, LEFT BUTTLINES O TO 48. INSTALLED REPAIR DOUBLER PER SRM 51-40-02.

Part: SKIN — DENTED (FUSELAGE) · corrosion level 2 · airframe 41,495 hrs · 10,398 cycles

EXTERIOR FUSELAGE SKIN DENTED/GOUGED TWO PLACES ADJACENT TO SOLID PLUG RIVET BODY STATION 515, STRINGERS 28 TO 29 RIGHT. TRIMMED OUT DAMAGE SECTION OF SKIN AND INSTALLED DOUBLER PER SRM 53-00-01 2R FIGURE 201.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,495 hrs · 10,398 cycles

MAIN CABIN FLOOR SHEAR WEB SURFACE FROM BODY STATIONS 1711 TO 1717, RIGHT BUTTLINE 1.5 TO RBL 48. CORROSION REMOVED AND INSTALLED DOUBLER PER SRM 51-40-02.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,495 hrs · 10,398 cycles

MAIN CABIN FLOOR SHEAR WEB SURFACE FROM BODY STATIONS 1711 TO 1717, RIGHT BUTTLINES 48 TO 53 CORRODED. INSTALLED DOUBLER PER SRM 51-40-02.

Part: FRAME — DENTED (FUSELAGE) · airframe 41,495 hrs · 10,398 cycles

AFT CARGO COMPARTMENT FRAME HAS DENT AT BODY STATION 1480, STRINGERS 26 TO 27 LEFT. REMOVED AND RE-INSTALLED TRANSITION PANEL, INTERCOSTAL CLIPS AND TIE DOWN FITTING PER SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,495 hrs · 10,398 cycles

CORROSION ON FLOOR SUPPORT ANGLE AT STATION 1700, RIGHT BUTTLINE 44. REPLACED ZEE CHANNEL PER SRM 51-40-02.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,495 hrs · 10,398 cycles

CORROSION ON FLOOR ATTACH CHANNEL AT STATION 1660, RIGHT BUTTLINE 54. REMOVED AND REPLACED CHANNEL PER SRM 51-40-02 DRAWING 146N5246.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,495 hrs · 10,398 cycles

MAIN CABIN FLOOR SHEAR WEB STIFFENER CORRODED FROM BODY STATIONS 1716 TO 1714, LEFT BUTTLINE 1.5 TO RIGHT BUTTLINE 1.5. REMOVED AND REPLACED WEB STIFFENER PER SRM 51-40-02.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,495 hrs · 10,398 cycles

CORROSION ON FLOOR ATTACH CHANNEL AT STATION 1673 LEFT BUTTLINE 54. REMOVED CORRODED CHANNEL AND INSTALLED NEW CHANNEL PER SRM 51-40-02.

Part: STRAP — CRACKED (FUSELAGE) · airframe 41,495 hrs · 10,398 cycles

FORWARD CARGO COMPARTMENT LEFT TUNNEL AREA, FLOORBEAM STRAP CRACKED AT LOWER CHORD OF FLOORBEAM BODY STATION 560, LEFT BUTTLINE 42. INSTALLED REPAIR DOUBLER, AND REMOVED AND RE-INSTALLED STRAP PER SRM 53-10-51-2R AND 51-40-02.

Part: SKIN — GOUGED (FUSELAGE) · airframe 41,495 hrs · 10,398 cycles

FUSELAGE SKIN AT BODY STATION 1540 AND STRINGER 9 LEFT IS GOUGED. TRIMMED OUT DAMAGE AND REPAIRED WITH DOUBLER PER SRM 53-00-01 FIGURE 101, EA B757-53-026754 AND REO G15494 REVISION C (TIMCO).

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,495 hrs · 10,398 cycles

MAIN CABIN INTERCOSTAL AT RIGHT NUMBER 1 DOOR CORRODED. REPLACED INTERCOSTAL PER SRM 51-40-02.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,495 hrs · 10,398 cycles

STATIONS 1661 TO 1680 RIGHT NUMBER 4 DOOR DRAIN SUPPORT CORRODED. REMOVED AND REPLACED SUPPORT PER SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,495 hrs · 10,398 cycles

CORROSION ON FLOOR SUPPORT CHANNEL AT STATION 1660 LEFT BUTTLINE 54. REMOVED CORROSION PER SRM 53-60-15-1A. REMOVED DRAIN PAN AND CORRODED CHANNEL. INSTALLED NEW CHANNEL AND RE-INSTALLED DRAIN PAN PER SRM 51-40-02.

Part: SIGN — BROKEN (CABIN) · airframe 41,002 hrs · 10,293 cycles

AFT RIGHT DOOR EMERGENCY EXIT MARKER SIGN BROKEN AND LENS MISSING. REPLACED EMERGENCY EXIT SIGN ASSEMBLY AT AFT RIGHT DOOR. OPS CHECK NORMAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 38,564 hrs · 9,785 cycles

THREE LIGHTING STRIKES AT STATION 438 AND BETWEEN STRINGERS 9 AND 10. INSTALLED DOUBLER PER SRM 53-00-01-2R3.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 38,564 hrs · 9,785 cycles

THREE EACH LIGHTNING STRIKES AROUND FASTENER AT STATION 438 STRINGERS 9 AND 10 RIGHT REMOVED DAMAGE. PERFORMED HFEC FOR CRACK INDICATION. PERFORMED DIGITAL THICKNESS READING, .043 THICKNESS REMAINING. PERFORMED HOLE PROBE HFEC, NO CRACK INDICATIONS. INSTALLED DOUBLER PER SRM 53-00-01-2R 3.

Part: BUSHING — CORRODED (LT MLG TRUNNION) · corrosion level 2 · airframe 38,563 hrs · 9,784 cycles

LEFT MAIN LANDING GEAR FORWARD TRUNNION AIRFRAME ATTACH POINTS - FOUND SEALANT BROKEN AT SIX O`CLOCK POSITION OF BUSHING HAT AREA. REMOVED THE SECTION OF THE SEALANT THAT SEPARATED FROM BUSHING AND CORROSION AROUND THIS AREA, INBOARD SIDE OF THE UPPER OUTBOARD BUSHING. INSTALLED NEW BUSHING PER EA B757-57-021000.

Part: BUSHING — CORRODED (RT MLG TRUNNION) · corrosion level 2 · airframe 38,563 hrs · 9,784 cycles

RIGHT MAIN LANDING GEAR FORWARD TRUNNION AIRFRAME ATTACH POINTS - PITTING AT SIX O`CLOCK POSITION AT EDGE OF BUSHING HAT LANDING ON THE INBOARD SIDE OF THE LOWER OUTBOARD BUSHING. INSTALLED NEW BUSHING PER EA B757-57-021000.

Part: BUSHING — CORRODED (RT MLG TRUNNION) · corrosion level 2 · airframe 38,563 hrs · 9,784 cycles

RIGHT MAIN LANDING GEAR FORWARD TRUNNION CORRODED AROUND BUSHING BORE EDGE INBOARD SIDE OF THE LOWER INBOARD BUSHING. INSTALLED NEW BUSHING PER EA B757-57-021000.

Part: BUSHING — CORRODED (RT MLG TRUNNION) · corrosion level 2 · airframe 38,563 hrs · 9,784 cycles

RIGHT MAIN LANDING GEAR FORWARD TRUNNION CORRODED AROUND BUSHING BORE EDGE OUTBOARD SIDE OF THE LOWER INBOARD BUSHING. INSTALLED NEW BUSHING PER EA B757-57-021000.

Part: BUSHING — CORRODED (LT MLG TRUNNION) · corrosion level 2 · airframe 38,563 hrs · 9,784 cycles

CORROSION ON LEFT LOWER INBOARD FORWARD TRUNNION ATTACH BUSHING. INSTALLED NEW BUSHING PER EA B757-57-021000.

Part: BUSHING — DAMAGED (RT MLG TRUNNION) · airframe 38,563 hrs · 9,784 cycles

RT MLG FWD TRUNNION AIRFRAME ATTACH POINTS - FOUND A GROOVE IN METAL (WITH PRIMER ON IT) AT THE FOUR O`CLOCK POSITION AT THE AREA WHERE THE HAT OF THE BUSHING LANDS, OUTBOARD SIDE OF THE LOWER INBOARD BUSHING. ROTO-PEENED SPOT FACED HAT LANDING TO INTENSITY OF 0.016A COVERAGE 2.0 PER EA B757-57-021000.

Part: BUSHING — CORRODED (RT MLG TRUNNION) · corrosion level 2 · airframe 38,563 hrs · 9,784 cycles

RIGHT MAIN LANDING GEAR FORWARD TRUNNION CORRODED AROUND BUSHING BORE EDGE INBOARD SIDE OF THE UPPER INBOARD BUSHING. INSTALLED NEW BUSHING PER EA B757-57-021000.

Part: PUMP — INOPERATIVE (LT ENGINE) · airframe 38,011 hrs · 9,672 cycles

SJU - INFLIGHT MIA-BSB. CREW REPORTED LEFT ENGINE HYDRAULIC OVERHEAT MESSAGE. EMERGENCY DECLARED FLIGHT DIVERTED SJU LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SEVRICE. REPLACED LEFT ENGINE DRIVEN HYDRAULIC PUMP. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PUMP — INOPERATIVE (LT ENGINE) · airframe 37,997 hrs · 9,667 cycles

MIA - CREW REPORTED LEFT ENGINE HYDRAULIC OVERHEAT. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE DRIVEN HYDRAULIC PUMP. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,698 hrs · 9,224 cycles

THE 3E SEAT EMERGENCY LIGHT INOPERATIVE. REPLACE 3E SEAT EMERGENCY LIGHT ASSEMBLY. OPS CHECK NORMAL.

Part: CHARGER — FAULTED (MAIN) · airframe 33,132 hrs · 8,683 cycles

YQX - INFLIGHT BOS-CDG. CREW REPORTED BATTERY CHARGER STATUS MESSAGE ILLUMINATED DURING FLIGHT. EMERGENCY DECLARED DIVERTED YQX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED MAIN BATTERY AND MAIN CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,873 hrs · 8,120 cycles

EMERGENCY LIGHT ABOVE SEAT 3E INOPERATIVE. RELAMPED LIGHT AT SEAT 3E. OPS CHECK OK.

Part: CONNECTOR — DEFECTIVE (BOOST PUMP) · airframe 30,341 hrs · 7,996 cycles

LAX - INFLIGHT SFO-HNL. CENTER BOOST PUMP FAILED IN FLIGHT. EMERGENCY DECLARED LANDED LAX WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED THE RIGHT CENTER BOOST PUMP CONNECTOR AND THE K10012 RELAY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 29,543 hrs

MIA - EMERGENCY LIGHT AT SEAT 20D INOPERATIVE. RESEATED LIGHT CONNECTOR FOR EMERGENCY AISLE LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN)

LAX- SEAT MOUNTED EMERGENCY LIGHTS AT SEAT 18D AND 19D INOPERATIVE. REPLACED BATTERY PACK AT SEAT 18D AND SEAT 19D.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · 27,224 cycles

LAX EXTERIOR EMERGENCY LIGHT AT RT NR 3 DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT RT NR 3 DOOR. SYSTEM GROUND CHECKED NORMAL OPS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,756 hrs

DFW - EMERGENCY LIGHT AT AFT GALLEY INOPERATIVE. REPLACED LIGHT ASSEMBLY L762 FOR EMERGENCY LIGHT AT AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: O-RING — LEAKING (HYD SYSTEM)

LAX INFLIGHT T162/24SEP - LEFT HYDRAULIC QUANTITY EICAS MESSAGE WITH RESERVOIR ANNUNCIATION. GEAR AND FLAPS LOWERED NORMALLY. QUANTITY STABILIZED AT 0.27. LANDED LAX WITHOUT INCIDENT. FOUND DELTA P LEAKING ON LEFT PYLON. REPLACED O-RING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — BROKEN (EMERG;ENCY LIGHT)

EMERGENCY LIGHT LENS AT SEAT 15D BROKEN. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 15D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: OVEN — DIRTY (CABIN)

SNN - REPORT OF SMOKE FROM DOOR SEAL AT NUMBER 3 OVEN IN AFT GALLEY. SMOKE STOPPED WHEN OVEN SWITCHED OFF. CLEANED OVENS IN AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

SFO - EMERGENCY LIGHTS FROM SEAT 16D TO 25D INOPERATIVE. REPLACED BATTERY PACK AT M10953 FOR EMERGENCY LIGHTS FROM SEAT 16D TO 25D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LANDING GEAR — MALFUNCTIONED (NLG)

DFW - NOSE LANDING GEAR WOULD NOT RETRACT ON TAKEOFF OUT OF TULSA. LANDED DFW WITHOUT INCIDENT. NOSE LANDING GEAR INSPECTED WITH NO DEFECTS NOTED. SWUNG GEAR SEVERAL TIMES, COULD NOT DUPLICATE WRITE UP. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LANDING GEAR — MALFUNCTIONED (NOSE)

AFTER TAKEOFF FROM TUL, NOSE LANDING GEAR FAILED TO RETRACT. INSPECTED NOSE LANDING GEAR WITH NO DEFECTS NOTED. CYCLED GEAR SEVERAL TIMES. COULD NOT DUPLICATE WRITE UP. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — DISCHARGED (CABIN)

LAX - FLT 297 - ON TAXI TO THE RUNWAY, EMERGENCY LIGHTS CAME BETWEEN ROWS 9 AND 15. RETURNED TO THE GATE. REPLACED M10952 BATTERY MODULE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)