N187AN

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 65,607 hrs · 16,354 cycles

AIRCRAFT NOT GROUNDED: MAINTENANCE REPORTS SEAT ROW 2EF EMERGENCY PATH LIGHTS WILL NOT ILLUMINATE. REMOVED AND REPLACED SEAT ROW 2EF EMERGENCY PATH LIGHTING CONNECTOR AT THE SIDEWALL IAW SWPM 20-42-01. OPS CHECKED GOOD.

Part: BATTERY — NO TEST (FLASHLIGHT) · airframe 64,648 hrs · 16,066 cycles

AIRCRAFT WAS NOT GROUNDED: FLASH LIGHT AT MID RIGHT HAND FLIGHT ATTENDANT SEAT INOPERABLE. MAINTENANCE REPLACED BATTERY IAW AMM 25-64-00.

Part: MODULE — INOPERATIVE (CABIN) · airframe 63,796 hrs · 15,833 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT MOUNTED EMERGENCY LIGHTS 20D THROUGH 25D WERE VERY DIM. MAINTENANCE REPLACED CHARGER AND BATTERY (MODULE) PER AMM 33-51-07.

Part: LIGHT — BROKEN (SEAT 2E) · airframe 63,189 hrs · 15,643 cycles

AFT EMERGENCY LIGHT AT SEAT 2E WAS BROKEN. REPLACED THE AFT EMERGENCY LIGHT & OPS CHECKED GOOD IAW MM 33-51-00.

Part: A/C PACK — OVERHEATED (RIGHT) · airframe 63,031 hrs · 15,593 cycles

ON APPROACH, CREW REPORTED A RIGHT PACK OVERHEAT, WHICH RESULTED IN A LOSS OF CABIN PRESSURE. THE MASKS DID NOT DEPLOY. AN EMERGENCY WAS DECLARED AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS GROUNDED.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 61,863 hrs · 15,274 cycles

LEFT OVERWING FWD, LOWER EMERGENCY EXIT SIGN IS INOPERATIVE. SECURED A LOOSE CONNECTOR FOR THE LIGHT ASSEMBLY. ACCOMPLISHED AN OPS TEST IAW AMM 33-51-10. THE EXIT SIGN CHECKED NORMAL.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 61,863 hrs · 15,274 cycles

SEAT 2E EMERGENCY LIGHTS WERE INOPERATIVE. SECURED THE LOOSE CONNECTOR FOR THE LIGHT ASSEMBLY. ACCOMPLISHED OPERATIONS TEST IAW AMM 33-51-11. CHECKED GOOD.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,420 hrs · 15,171 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON L4 DOOR GUTTER BOX (SUPPORT) IN TWO PLACES BETWEEN STA 1163-1771. REPLACED GUTTER BOX (SUPPORT) PER DRAWING 146N5230 AND 51-00-05-1.

Part: COLLAR — DAMAGED (L2 DOOR) · airframe 60,869 hrs · 15,030 cycles

L2 DOOR HOLD OPEN LATCH RELEASE LEVER COLLAR IS DAMAGED. REPLACED THE COLLAR IAW 52-11-08.

Part: SPLICE — DAMAGED (EMERGENCY LIGHT) · airframe 60,004 hrs · 14,783 cycles

EMERGENCY LIGHT AT RIGHT FIRST CLASS BULKHEAD, FWD SEAT 1E FOUND INOPERATIVE. REPLACED THE CONTACT SPLICE BEHIND AIR GRILLE AT SEAT 1E IAW SWPM 20-30-12. OPS CHECKED OK IAW AMM 33-51-11.

Part: BULB — UNSECURE (EMERGENCY LIGHT) · airframe 60,002 hrs · 14,782 cycles

EXTERIOR SLIDE LIGHT AT L4 DOOR IS INOPERATIVE. SECURED THE BULB IAW AMM 33-51-06.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 60,002 hrs · 14,782 cycles

SEAT MOUNTED EMERGENCY LIGHTS AT ROW 27D ARE INOPERATIVE. SECURED THE CONNECTOR. OPS CHECKED OK IAW AMM 33-51-11.

Part: LAMP — INOPERATIVE (EMERGENCY LGIHT) · airframe 59,950 hrs · 14,768 cycles

AFT EMERGENCY LIGHT INOPERATIVE AT SEAT 2E. MAINTENANCE REPLACED THE LAMP IAW AMM 33-51-11 AND PERFORMED SUCCESSFUL OPERATIONAL CHECK.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 59,948 hrs · 14,767 cycles

AFT EMERGENCY LIGHT MISSING LENS AT SEAT 3E. MAINTENANCE REPLACED LENS IAW AMM 33-51-11, AND PERFORMED A SUCCESSFUL OPS CHECKED.

Part: SIGN — DETACHED (CABIN) · airframe 59,922 hrs · 14,756 cycles

AIRCRAFT NOT GROUNDED. 2R DOOR EXIT SIGN FELL OFF. REINSTALLED EMERGENCY EXIT SIGN AT 2R DOOR PER MM 33-51-01. OPERATIONS CHECK NORMAL.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 59,763 hrs · 14,713 cycles

EMERGENCY LIGHT AT SEAT 27D IS INOPERATIVE. SECURED A LOOSE CONNECTOR UNDER SEAT 27D. OPERATIONAL CHECKED GOOD IAW AMM 33-51-00.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 59,040 hrs · 14,519 cycles

THE AIRCRAFT WAS NOT GROUNDED. FOUND 1R SLIDE CYLINDER PRESSURE BELOW LIMITS. REMOVED AND REPLACED R1 SLIDE IAW MCM 25-94-34 OK FOR SERVICE.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 58,818 hrs · 14,471 cycles

FIRST CLASS SEAT 2E BOTH EMERGENCY LIGHTS ARE INOPERATIVE. FOUND CONNECTOR AT 2E WALL DISCONNECTED. CONNECTED IAW AMM 33-51-11.

Part: MODULE — NOT SEATED (CABIN) · airframe 58,598 hrs · 14,408 cycles

AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT 20D IS INOPERATIVE. RESEATED LIGHT MODULE PER AMM 33-51-11. OPERATIONAL CHECK GOOD.

Part: LENS — BROKEN (CABIN) · airframe 58,110 hrs · 14,265 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGN OVER R2 DOOR HAS A BROKEN LENS COVER. REMOVED AND REPLACED LENS COVER. OPERATIONAL CHECK GOOD.

Part: STRAP — FRAYED (EVAC SLIDE) · airframe 58,110 hrs · 14,265 cycles

AIRCRAFT WAS NOT GROUNDED. L1 DOOR EMERGENCY ESCAPE SLIDE D-RING STRAP IS FRAYED. REMOVED AND REPLACED STRAP IAW AMM 25-66-01. OPERATIONAL CHECK GOOD.

Part: LIGHT — NOT SEATED (ZONE 200) · airframe 58,060 hrs · 14,248 cycles

AIRCRAFT WAS NOT GROUNDED. R1 DOOR EMERGENCY EVACUATION SLIDE LIGHT IS INOPERATIVE. RESEATED LIGHT IN SOCKET. OPERATIONAL CHECK GOOD.

Part: LENS — DETACHED (EXIT SIGN) · airframe 58,060 hrs · 14,248 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGN OVER R2 DOOR HAS A DETACHED LENS COVER. RESECURED LENS COVER. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 58,052 hrs · 14,244 cycles

EMERGENCY LIGHTS AT SEATS 20D AND 26D THROUGH 36D ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AND CONTROL MODULE AT M10801 IAW AMM 33-51-11. OPS CHECKED GOOD.

Part: MODULE — NO TEST (EMERGENCY LIGHTS) · airframe 58,051 hrs · 14,244 cycles

EMERGENCY LIGHTS AT SEATS 20D AND 26D THROUGH 36D ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AND CONTROL MODULE AT M10801 IAW AMM 33-51-11. OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 57,693 hrs · 14,150 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGNS AT L4/R4 DOORS ARE DIM. RECHARGED EMERGENCY LIGHTS SYSTEM IAW AMM 33-51-00. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 57,686 hrs · 14,148 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AFT CABIN RIGHT OUTERMOST SEAT IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-60-00. OPERATIONAL CHECK GOOD.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 56,874 hrs · 13,921 cycles

AIRCRAFT NOT GROUNDED. SEAT MOUNTED ESCAPE PATH LIGHT AT SEAT 4D IS INOPERATIVE. CLEANED AND SECURED ILLUMINATOR CONNECTOR IAW AMM 33-51-00. OPERATIONAL CHECK GOOD.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 56,874 hrs · 13,921 cycles

AIRCRAFT NOT GROUNDED. SEAT MOUNTED ESCAPE PATH LIGHT AT SEAT 16D IS INOPERATIVE. CLEANED AND SECURED ILLUMINATOR CONNECTOR IAW AMM 33-51-00. OPERATIONAL CHECK GOOD.

Part: RELEASE MECH — OUT OF ADJUST (COCKPIT) · airframe 56,612 hrs · 13,842 cycles

AIRCRAFT NOT GROUNDED. CAPTAIN’S SLIDING WINDOW IS JAMMED AND WILL NOT OPEN. ADJUSTED LATCH HANDLE RELEASE BUTTON IAW 56-11-02. OPERATIONAL CHECK GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (SPEEDBRAKES) · airframe 55,864 hrs · 13,649 cycles

DURING FLIGHT THE AUTO SPEEDBRAKE EICAS AND AUTO SPEED BRAKE DISCREET WARNING LIGHT ILLUMINATED. EMERGENCY DECLARED, AND LANDING UNEVENTFUL. MAINTENANCE ACCOMPLISHED AUTO SPEEDBRAKE OPS TEST IAW AMM 27-62-00. MESSAGE CLEARED. SYSTEM CHECKED NORMAL.

Part: BOTTLE — DISCHARGED (R4 DOOR) · airframe 54,601 hrs · 13,363 cycles

FOUND R4 AFT DOOR EMER POWER RESERVOIR BOTTLE DISCHARGED. R & R EMER POWER ASSIST RESERVOIR ON R4 DOOR IAW AMM 52-11-30. THE ACFT WAS GNDED.

Part: SENSOR — OUT OF ADJUST (ZONE 800) · airframe 54,599 hrs · 13,362 cycles

RIGHT AFT ENTRY DOOR WILL NOT ARM. CLEANED GIRT BAR SENSORS & MADE ADJUSTMENT TO RT GIRT BAR SENSOR IAW AMM 25-66-10. OPERATIONS CHECKED GOOD, ARMING LIGHT ILLUMINATED. THE ACFT WAS GNDED.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 54,330 hrs · 13,305 cycles

AIRCRAFT WAS NOT GNDED. R2 DOOR EXTERIOR EMER LIGHT INOPERATIVE. R & R BATTERY PACK & CHARGER IAW AMM 33-51-07. OPERATIONAL CHECKED GOOD. SEE ALSO AALA 20160322013.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,330 hrs · 13,305 cycles

AIRCRAFT WAS NOT GNDED. R2 DOOR EXTERIOR EMER LIGHT INOPERATIVE. R & R BATTERY PACK & CHARGER IAW AMM 33-51-07. OPERATIONAL CHECKED GOOD. SEE ALSO AALA 20160323003.

Part: IDG — FAILED (LT ENGINE) · airframe 52,329 hrs · 12,841 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CRUISE, LT ENG GEN DRIVE FAILED & APU AUTO SHUTDOWN DURING START ATTEMPT. R & R LT ENG INTEGRATED DRIVE GEN IAW AMM 24-11-01. PERFORMED LEAK & OPERATIONAL CHECKS. SYS CHECKED NORMAL. FOR APU NO START SEE AALA20150827006 & AALA20150827007.

Part: BATTERY — FAULTY (APU) · airframe 52,329 hrs · 12,841 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CRUISE, LT ENG GEN DRIVE FAILED & APU AUTO SHUTDOWN DURING START ATTEMPT. R & R APU BATTERY & CHARGER IAW AMM 24-31-03 & AMM 24-31-04. APU START & OPERATIONAL CHECK NORMAL. SEE ALSO AALA20150827006, FOR IDG FAILURE SEE AALA20150825002.

Part: CHARGER — FAULTY (APU) · airframe 52,329 hrs · 12,841 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CRUISE, LT ENG GEN DRIVE FAILED & APU AUTO SHUTDOWN DURING START ATTEMPT. R & R APU BATTERY & CHARGER IAW AMM 24-31-03 & AMM 24-31-04. APU START & OPERATIONAL CHECK NORMAL. SEE ALSO AALA20150827007, FOR IDG FAILURE SEE AALA20150825002.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,848 hrs · 12,725 cycles

FLOORBEAM AT FS 1640 IS CORRODED BETWEEN RBL 3 & LBL 56. REPAIRED IAW SRM 757 53-00-51-2R-8 & EA 252602.

Part: SEAL — DEBONDED (ENGINE SPINNER) · airframe 51,399 hrs · 12,613 cycles

AIR INTERRUPT, EMER DECLARED. LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CRUISE, LT ENG VIBRATION INCREASED TO 4.1 AFTER 30 MINUTES OF FLIGHT. BRINGING THROTTLE TO NEAR IDLE BROUGHT INDICATIONS IN LIMITS. RECEIVED EICAS MSG, L ENG VIB, L ENG BB. FOUND SPINNER SEALS DISBONDED FROM SPINNER. R & R SPINNER IAW AMM 72-35-01. PERFORMED VIBRATION SURVEY TEST IAW AMM 71-00-00. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,992 hrs · 12,503 cycles

SEAT 33D EMER LIGHT INOPERATIVE. RELAMPED SEAT 33D EMER LIGHT. SYS CHECKED NORMAL.

Part: FLUID — LOW (LAVATORY) · airframe 49,849 hrs · 12,248 cycles

DIVERTED, EMER DECLARED & LANDING UNEVENTFUL. ACFT WAS OVERWEIGHT. DURING CRUISE CABIN CREW REPORTED ALL LAVATORIES WOULD NOT FLUSH. FOUND ALL LAVATORIES WITH MINIMAL TO NO FLUID IN THEM. CONFIRMED NO LEAKS ON ACFT AT ANY LAVATORY SERVICE STATION. ALL LAVATORIES SERVICED. SYS CHECKED NORMAL.

Part: PIN — DEFECTIVE (CABIN) · airframe 49,515 hrs · 12,187 cycles

SEAT 35D EMER LIGHT INOPERATIVE. REPLACED PINS FOR SEAT 35D EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: PIN — DEFECTIVE (CABIN) · airframe 49,515 hrs · 12,187 cycles

SEAT 4E EMER LIGHT INOPERATIVE. REPLACED PINS FOR SEAT 4E EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,257 hrs · 12,131 cycles

EMERGENCY LIGHT IN FIRST CLASS FAILED TEST. REPLACED LAMP FOR EMER LIGHT IN FIRST CLASS. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,257 hrs · 12,131 cycles

EMERGENCY LIGHT AT SEAT 13C FAILED TEST. REPLACED LAMP FOR EMER LIGHT AT SEAT 13C. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,257 hrs · 12,131 cycles

EMERGENCY LIGHT AT SEAT 33D FAILED TEST. REPLACED LAMP FOR EMER LIGHT AT SEAT 33D. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,257 hrs · 12,131 cycles

EMERGENCY LIGHT AT SEAT 36D FAILED TEST. REPLACED LAMP FOR EMER LIGHT AT SEAT 36D. OPERATIONS CHECKED NORMAL.

Part: WIRE — BROKEN (CABIN) · airframe 48,321 hrs · 11,883 cycles

EMERGENCY LIGHT AT SEAT 10DEF BROKEN WIRE AT OTBD SEAT FRAME. REPAIRED WIRE & INSTALLED NEW PIN. OPERATIONS CHECKED NORMAL.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 46,932 hrs · 11,567 cycles

AFT CARGO DOOR FWD LOWER CORNER DAMAGED. INSTALLED EXTERNAL SKIN DOUBLER REPAIR IAW SRM 52-30-01-2R-4.

Part: CONTROL PANEL — MALFUNCTIONED (AUTOPILOT SYS) · airframe 45,886 hrs · 11,315 cycles

SNN INFLIGHT JFK-DUB CREW REPORTED SEVERAL AUTOPILOT RELATED ISSUES INCLUDING, LAND 2 MODE ANNUNCIATED, BANK LIMITED TO 5 DEGREE ALT CAPTURE INOPERATIVE. FLIGHT LEVEL CHANGE INOPERATIVE. FLIGHT DIVERTED SNN LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED MODE CONTROL PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: SERVO — LEAKING (AUTOPILOT SYS) · airframe 45,855 hrs · 11,305 cycles

MIA CREW REPORTED LT HYD FLUID LOSS IN FLIGHT. FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. SERVICED THE LT HYD SYSTEM. REPLACED THE LT A/P SERVO. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: SIGN — INOPERATIVE (CABIN) · airframe 43,220 hrs · 10,724 cycles

AFT GALLEY EXIT SIGN INOPERATIVE. REPLACED AFT GALLEY EXIT SIGN. OPS CHECK NORMAL.

Part: ENGINE — FAILED (LEFT) · airframe 42,537 hrs · 10,546 cycles

BGR - INFLIGHT MAN-JFK. CREW REPORTED LEFT ENGINE OIL PRESSURE LOSS. ACCOMPLISHED IN-FLIGHT SHUTDOWN OF LEFT ENGINE (SINGLE ENGINE TIME 30 MINUTES). EMERGENCY DECLARED FLIGHT DIVERTED BGR LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE AT BGR ON 11/06/2012. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: HINGE — CRACKED (THRUST REVERSER) · airframe 41,030 hrs · 10,227 cycles

NUMBER 1 ENGINE INBOARD THRUST REVERSER HINGE HAS A CRACK IN THE AFT UPPER MOUNT HOLE. OVER SIZED HOLE AND INSTALLED FREEZE PLUG PER EA B757-54-024386.

Part: ANGLE — WORN (LT MLG WW) · airframe 41,030 hrs · 10,227 cycles

ANGLE AT LEFT WING WHEEL WELL AT FALSE SPAR AND FUSELAGE WORN. INSTALLED NEW ANGLE PER SRM 51-70-12-0G.

Part: ANGLE — CHAFED (LT MLG WW) · airframe 41,030 hrs · 10,227 cycles

LEFT WING LEFT WHEEL WELL AT FALSE SPAR AND FUSELAGE WORN. INSTALLED DOUBLER REPAIR PER SRM 51-70-12-0G.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,030 hrs · 10,227 cycles

LEFT NUMBER 4 DOOR ENTRY SCUFF PLATE DRAIN SUPPORT HAS CORROSION. REPLACED LEFT NUMBER 4 DOOR ENTRY SCUFF PLATE DRAIN SUPPORT PER SRM 51-10-02 AND AARD 51-00-05.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,030 hrs · 10,227 cycles

FLOORBEAM AT STATION 1640 HAS CORROSION ON TOP OF LEFT BUTTLINE TO RIGHT BUTTLINE 4. INSTALLED T CAP, ANGLE AND STRAPS PER SRM 53-00-51-2R 3.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,030 hrs · 10,227 cycles

AFT DECK HAS NUMEROUS ARES CORRODED BEYOND LIMITS. INSTALLED DOUBLER REPAIR COVERING FROM STATIONS 1710 TO 1720, LEFT BUTTLINE 28 TO RIGHT BUTTLINE 53 PER SRM 51-20-01.

Part: SKIN — GOUGED (FUSELAGE) · airframe 41,030 hrs · 10,227 cycles

FUSELAGE GOUGED AT STATION 630L AND STRINGER 17 LEFT. INSTALLED DOUBLER REPAIR PER EA B757-53-023893.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,030 hrs · 10,227 cycles

LEFT Z-ANGLE AT LEFT BUTTLINE 50, STATIONS 1680 TO 1720, CORRODED. INSTALLED LEFT Z-ANGLE PER AARD 51-10-02.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,030 hrs · 10,227 cycles

STATION 1686 TO 1720 BUTTLINE 0 CORRODED. REPLACED HAT CHANNEL PER SRM 51-10-02.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 40,894 hrs · 10,190 cycles

SEAT MOUNTED EGRESS EMERGENCY LIGHTING AT SEAT 2E INOPERATIVE. SECURED CONNECTOR UNDER SEAT 2E. OPS CHECK NORMAL.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 39,401 hrs · 9,875 cycles

DELAMINATION ON OUTBOARD AFT FLAP LOWER SKIN OUTBOARD OF NUMBER 1 FLAP TRACK. ACCOMPLISHED SKIN REPAIR PER EA COMP 57-020872.

Part: FAN — OVERHEATED (CABIN) · airframe 35,179 hrs · 9,025 cycles

MAD - CREW REPORTED ELECTRICAL BURNING SMELL IN CABIN, CREW ISOLATED PROBLEM TO RIGHT RECIRC FAN. WHEN SWITCHED OFF SMELL DISSIPATED. FLIGHT LANDED MAD WITHOUT INCIDENT. REPLACED RIGHT RECIRCULATION FAN. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: VALVE — FAULTY (PARKING BRAKE) · airframe 34,990 hrs · 8,990 cycles

MAD - CREW REPORTED PARKING BRAKE LIGHT ILLUMINATED DURING FLIGHT. EMERGENCY DECLARED LANDED MAD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED PARKING BRAKE VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 34,439 hrs · 8,880 cycles

EMERGENCY LIGHTS IN AFT CABIN DIM DURING TEST. REPLACED BATTERY PACK AT M10801.

Part: MODULE — INOPERATIVE (CABIN) · airframe 33,759 hrs · 8,728 cycles

EMERGENCY LIGHTS FROM SEAT ROW 11 TO 25 FAILED TO TEST. REPLACED MODULE FOR EMERGENCY LIGHTS FROM SEAT ROW 11 TO 25.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 33,759 hrs · 8,728 cycles

EMERGENCY LIGHTS FROM SEAT ROW 11 TO 25 FAILED TO TEST. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FROM SEAT ROW 11 TO 25. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 32,930 hrs · 8,511 cycles

SEAT MOUNTED EMERGENCY LIGHT AT ROWS 16 TO 25 INOPERATIVE. REPLACED BATTERY PACK AT M10800.

Part: WIRE — LOOSE (COCKPIT) · airframe 32,564 hrs · 8,410 cycles

FIRST OBSERVERS MAP LIGHT CAME UNATTACHED AND WAS TOUCHING THE CIRCUIT BREAKER PANEL MAKING SPARKS. LANDED BRU WITHOUT INCIDENT. FOUND SHORT CIRCUIT IN FIRST OBSERVER MAP LIGHT. BREAKER UTILITY PULLED AND SECURED IAW MEL 33-1A 12-352D-C. SECURED WIRING TO GROUND AT JFK.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 32,223 hrs · 8,331 cycles

RIGHT AFT EXTERNAL OVERWING EMERGENCY LIGHT IS INOPERATIVE. REPLACED LAMP.

Part: CONNECTOR — LOOSE (CABIN) · airframe 31,907 hrs · 8,247 cycles

EMERGENCY LIGHT AT SEAT 27D INOPERATIVE. SECURED CONNECTOR AT SEAT 27D. OPS CHECK OK.

Part: LIGHT — DAMAGED (ZONE 200)

DFW - EMERGENCY PATH LIGHT ASSEMBLY AT SEAT 24D IS DAMAGED. REPLACED EMERGENCY PATH LIGHT ASSEMBLY AT SEAT 24D.

Part: OXYGEN MASK — FAILED (CABIN) · airframe 29,570 hrs

AMA INFLIGHT EGE TO DFW - AT FL410, RIGHT CIRCULATION FAN FAILED FOLLOWED BY RIGHT PACK OVERHEAT INDICATION FOLLOWED BY LEFT PACK OVERHEAT INDICATION. EMERGENCY DESCENT ACCOMPLISHED. OXYGEN MASKS IN CABIN DEPLOYED MANUALLY. FLIGHT ATTENDANT REPORTED SLIGHT BURNING ODOR. REPORTED SOME OXYGEN MASKS IN CABIN DID NOT DEPLOY. INSPECTED AIRCRAFT AND PREPARED FOR FERRY FLIGHT TO DFW FOR REPAIRS AND REPLACEMENT OF OXYGEN GENERATORS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,508 hrs

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

Part: MODULE — FAULTED (STAB TRIM) · airframe 29,215 hrs

LAX INFLIGHT - MACH SPEED TRIM INDICATIONS AT 16000 FEET. AUTOPILOT WAS OFF AIRSPEED ABOUT 270 KNOTS INDICATED AIR SPEED. RETURNED TO LAX AND LANDED WITHOUT INCIDENT. REPLACED RIGHT STABILIZER TRIM ASYMMETRY MODULE AND RIGHT STABILIZER TRIM CONTROL MODULE BRAKE PRESSURE SWITCH (MPN 10605525). SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DFW EMERGENCY LIGHT EXIT SIGN AT LT NR 3 DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT EXIT SIGN AT LT NR 3 DOOR. SYSTEM GROUND CHECKED NORMAL OPS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DFW EMERGENCY LIGHT EXIT SIGN AT RT NR 3 DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT EXIT SIGN AT RT NR 3 DOOR. SYSTEM GROUND CHECKED NORMAL OPS.

Part: PLACARD — DAMAGED (CABIN)

DFW EMERGENCY LIGHT EXIT MARKER DECALS AT RT HAND OVERWING DAMAGED. REPLACED EXIT DECALS FOR EXIT MARKER AT RT HAND OVERWING. SYSTEM GROUND CHECKED NORMAL OPS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DFW EMERGENCY LIGHT EXIT SIGN AT LT NR 7 DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT EXIT SIGN AT LT NR 7 DOOR. SYSTEM GROUND CHECKED NORMAL OPS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DFW EMERGENCY LIGHT EXIT SIGN AT RT NR 7 DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT EXIT SIGN AT RT NR 7 DOOR. SYSTEM GROUND CHECKED NORMAL OPS.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT)

DFW EMERGENCY LIGHT AT SEAT 26D INOPERATIVE. REPLACED DAMAGED PIN AT SIDEWALL CONNECTOR FOR EMERGENCY LIGHT AT SEAT 26D. SYSTEM GROUND CHECKED NORMAL OPS.

Part: FIRE WARNING — MALFUNCTIONED (NR 2 ENGINE)

VVI INFLIGHT T9222/15MAY MIA TO LPB. NR 2 ENGINE FIRE WARNING OVERHEAT EICAS MESSAGE AND ASSOCIATED LIGHTS AND BELLS. LANDED VVI WITHOUT INCIDENT. NO EVIDENCE OF FIRE. PERFORMED ADJUSTMENT AND TEST OF NR 2 ENGINE FIRE WARNING SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) (A)

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - EMERGENCY LIGHTS AT SEAT ROWS 16 TO 25 DIM. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 16 TO 25. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PLACARD — DAMAGED (CABIN)

DFW - EMERGENCY EXIT DECAL AT AFT LEFT FORWARD GALLEY DOOR DAMAGED. REPLACED DECAL FOR EMERGENCY EXIT LIGHT AT AFT LEFT FORWARD GALLEY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PLACARD — DAMAGED (CABIN)

DFW - EMERGENCY EXIT DECAL AT AFT LEFT AFT GALLEY DOOR DAMAGED. REPLACED DECAL FOR EMERGENCY EXIT LIGHT AT AFT LEFT AFT GALLEY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT SEAT 10D INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 10D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT SEAT 22D INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 22D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS)

LAX - EMERGENCY EXIT SIGN LIGHT AT RIGHT FORWARD OVERWING INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY EXIT SIGN LIGHT AT RIGHT HAND FORWARD OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

LAX - EMERGENCY EXIT SIGN LIGHT AT LEFT AFT OVERWING INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY EXIT SIGN LIGHT AT LEFT AFT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — BURNED (WINDOW HEAT)

LAX - INFLIGHT RETURNED TO LAX DUE TO SMOKE AND ELECTRICAL ODOR IN COCKPIT. LANDED WITHOUT INCIDENT. FOUND WIRE TO LEFT NUMBER ONE WINDOW HEAT CONNECTION BURNED. REPAIRED WIRE AND REPLACED LEFT NUMBER ONE WINDOW. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

SFO - EMERGENCY LIGHT AT SEAT 20D INOPERATIVE. RELAMPED INOPERATIVE EMERGENCY LIGHT AT SEAT 20D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

SFO - EMERGENCY LIGHTS AT LEFT HAND WING AFT ESCAPE HATCH INOPERATIVE. REPLACED BULBS FOR EMERGENCY LIGHTS AT LEFT HAND WING AFT ESCAPE HATCH. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

JFK - EMERGENCY EXIT SIGN AT LEFT AFT MAIN ENTRY DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY EXIT SIGN AT LEFT AFT MAIN ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SLIDE — FAILED (CABIN)

DFW UNSUCCESSFUL SLIDE DEPLOYMENT. DIRECTIONAL EXIT HANDRAIL DID NOT FULLY INFLATE AND DID NOT STAY INFLATED. REPLACED RIGHT HAND MAIN OFFWING EVACUATION SLIDE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.