N866DA

Part: BATTERY — DISCHARGED (ZONE 200) · airframe 90,035 hrs · 10,931 cycles

BOTH L1 AND R2 HAD THEIR EPAS BATTERIES DEPLETED, REPLACED PER AMM.

Part: BATTERY PACK — FAULTED (ZONE 200) · airframe 89,969 hrs · 10,904 cycles

DURING THE EMERGENCY LIGHT CHECKS FOUND DOOR 1R 1 EACH BATTERY PACK WOULD NOT EXCEPT CHARGE (M33094).

Part: FITTING — LACK OF LUBE (GIRT BAR) · airframe 87,890 hrs · 10,620 cycles

(AIRCRAFT 7007, L/P 5276994) R1 DOOR HARD TO OPEN AND CLOSE. CORRECTIVE ACTION: LUBRICATED FWD AND AFT GIRT BAR FITTINGS (LOCK DOWN) PER B777 AMM 12-21-24.

Part: HANDLE — OUT OF SEQUENCE (L2 DOOR) · airframe 86,958 hrs · 10,530 cycles

L2 DOOR DIFFICULT TO CLOSE. FOUND OUTSIDE HANDLE OUT OF SEQUENCE, DOOR NOW OPERATES NORMAL.

Part: LENS — MISSING (CABIN) · airframe 86,525 hrs · 10,487 cycles

(AIRCRAFT 7007, L/P 1250584) EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING / LOCATIONS:904 / ACARS TEXT: FRC 335102904 / INTERIOR. REPLACED MISSING EMERGENCY EXIT LENS COVER IN CREW REST AREA PER CMM 33-21-89. OPS CHECK GOOD.

Part: LENS — DAMAGED (CABIN) · airframe 85,833 hrs · 10,414 cycles

(AIRCRAFT 7007, L/P 1168520) EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:901 / INTERIOR. REPLACED LENS AT EMERGENCY LIGHT 901. OK FOR SVC PER MM 33-50.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 84,326 hrs · 10,263 cycles

(AIRCRAFT 7007, L/P 5723650) EXTERIOR EMERGENCY LIGHTS L1 AND R4 DOOR INOP. REMOVED AND REPLACED R4 LAMP- OPS CK OK. REMOVED AND REPLACED L1 LAMP. FOUND FUSES BAD. REPLACED FUSES PER B777 AMM 33-51-06. OPS CHECK GOOD.

Part: LENS — MISSING (CABIN) · airframe 83,738 hrs · 10,203 cycles

(AIRCRAFT 7007, L/P 5272497) EMERGENCY PATH PROXIMITY LIGHT LENS COVER MISSING AT 25R 4L GALLEY BY 57B FWD SIDE 3L LAV CLEAR. 4R DOOR AREA AFT SIDE OF GALLEY RED. AOG ORDERED P/N 0203173-001 CLEAR 10 EA AND P/N 0203173-002 RED FROM MSP DOMESTIC STORES TO AIRCRAFT. WIP 589048 1/18/19. INSTALLED ALL MISSING LIGHT COVERS LIGHTS. OPS CKS GOOD.

Part: FUSE — BLOWN (POWER SUPPLY) · airframe 83,738 hrs · 10,203 cycles

(AIRCRAFT 7007, L/P 5272498) OVHD EMERGENCY LIGHTS INOP AT 35R AND 40R. REPLACED FUSE IN POWER SUPPLY REF WDM 33.51. CHECKS OK.

Part: LOCK — FAILED (L3 DOOR) · airframe 80,945 hrs · 9,917 cycles

L3 DOOR FLIGHT LOCK STATUS MESSAGE ILLUMINATED IN FLIGHT. REPLACED L3 FLIGHT LOCK ACTUATOR IAW AMM 52-11.

Part: TARGET — OUT OF POSITION (R4 DOOR SENSOR) · airframe 80,351 hrs · 9,856 cycles

R4 DOOR TARGET LOCK IS OUT OF POSITION. R & R THE LOCK SENSOR S52215 IAW AMM 52-71, OPS CHECKED GOOD.

Part: OXYGEN BOX — OPEN (ROW 32 DEF) · airframe 79,997 hrs · 9,822 cycles

AFTER PUSH BACK FROM GATE, OXYGEN MASK DOOR AT ROW 32 DEF OPENED AND MASK FELL OUT. RESET AND CLOSED THE OXYGEN MASK DOOR AND CHEKED NORMAL IAW AMM 35-21-02.

Part: WARNING LIGHT — FALSE ACTIVATION (DOOR LOCK) · airframe 79,883 hrs · 9,809 cycles

L3 DOOR FLIGHT LOCK STATUS MESSAGE. TROUBLESHOT IAW FIM 52-11-00-810-805. ACFT OK FOR SERVICE.

Part: HANDLE — LACK OF LUBE (R1 DOOR) · airframe 79,570 hrs · 9,782 cycles

R1 DOOR DIFFICULT TO OPEN USING INTERIOR HANDLE. EXTERIOR HANDLE ROTATES BUT WOULD NOT ENGAGE. LUBRICATED THE DOOR HANDLE MECHANISM. DOOR OPERATES NORMALLY. OK FOR SERVICE.

Part: LIGHT — HOT (CREW REST) · airframe 77,508 hrs · 9,566 cycles

FORWARD CREW REST UPPER ENTRY CLOSET, CAPTAIN'S SIDE CLOSET LIGHT BULB BURNED THROUGH LENS COVER (DEFORMED BY HEAT). REPLACED LIGHT BULB AND LIGHT SWITCH.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,588 hrs · 9,463 cycles

EMERGENCY LIGHTS INOPERATIVE IN ZONE 2. REPLACED THE BATTERY AND POWER SUPPLY IAW AMM 33-51. EMERGENCY LIGHTS TESTED NORMAL.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 76,250 hrs · 9,427 cycles

EMERGENCY EXIT LENS MISSING. I NSTALLED THE LENS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 75,782 hrs · 9,381 cycles

THE EMERGENCY LIGHT AT 10B INOPERATIVE AND LENS MISSING. REPLACED THE LAMPED AND LENS.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,214 hrs · 9,326 cycles

AFT GALLEY 4 CTR EMERGENCY LIGHTS INOPERATIVE. R & R THE BATTERY CHARGER IAW AMM 33-51.

Part: SKIN — PUNCTURED (NR 4 SLAT) · airframe 75,064 hrs · 9,312 cycles

NR 4 LE SLAT HAS A PUNCTURE APPROXIMATELY .5 INCHES IN DIAMETER ON UPPER SURFACE. REPAIRED IAW SRM 57-43-02 FIG 201 REPAIR 2.

Part: LIGHT — MISSING · airframe 74,992 hrs · 9,304 cycles

EMERGENCY LIGHT MISSING JUST FORWARD OF OF ACFT RIGHT SIDE. REPLACED THE LIGHT.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 74,946 hrs · 9,300 cycles

EMERGENCY EXIT SIGN COVER LOOSE. FIXED EXIT SIGN COVER.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 74,825 hrs · 9,288 cycles

AFT GALLEY F/A JUMP SEAT EMERGENCY WHITE LIGHTS INOP. REPLACED M33409 PWR SUPPLY AND RE-PIN LEFT AFT GALLEY CART LIGHT ASSY.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 74,804 hrs · 9,286 cycles

AFT GALLEY ACROSS FROM R4 DOOR AT FLOOR LEVEL EMERGENCY LIGHT LENS MISSING. INSTALLED LENS.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 74,804 hrs · 9,286 cycles

AFT GALLEY ACROSS FROM L4 DOOR AT FLOOR LEVEL EMERGENCY LIGHT LENS MISSING. INSTALLED LENS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 74,804 hrs · 9,286 cycles

SEAT 11C EMERGENCY LIGHT INOPERATIVE AND LENS MISSING. REPLACED THE LAMP AND INSTALLED LENS.

Part: BAND — CHAFED (THRUST REVERSER) · airframe 71,436 hrs · 8,952 cycles

MAINTENANCE TASK NR 2 ENGINE OTBD THRUST REVERSER V-BAND GROOVE LOWER AREA FOUND CHAFED. PERFORMED BLEND OUT REPAIR IAW PRI 543523-14, REV 0, DATED 01FEB16, 1015 HRS & PRI 543523-14AD, REV 0.

Part: HOOK — BINDING (L2 DOOR) · airframe 64,065 hrs · 8,190 cycles

L2 DOOR WILL NOT DISARM. L 2 DOOR ARM-DISARM LEVER FOUND BINDING. SLIDE RAFT REMOVED AND L2 DOOR DECLARED INOPERATIVE. FOUND DOOR ASSIST BOTTLE LOW R & R DOOR ASSIST BOTTLE IAW AMM 52-11. REPLACED HOOK ASSY IAW AMM 52-11, OPS CHECKED GOOD. INSTALLED SLIDE IAW AMM 25-66. OPS CHECKED GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 61,747 hrs · 7,956 cycles

FLT 252, DURING CRUISE, CABIN FLOOR EMERGENCY EXIT LIGHTS ILLUMINATED FOR A FEW MINUTES THEN EXTINGUISHED. NO RELATED PRESENT LEG FAULTS AND /OR EXISTING FAULTS OPS CHECK, TEST EMERGENCY LIGHT NORMAL. OK TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,209 hrs · 7,805 cycles

EMERGENCY LIGHTS INOPERATIVE, FROM ROW 10 THRU 14 LT AND RT SIDE ISLES. R & R POWER SUPPLY. OPS CHECKED GOOD IAW 33-51-06. OK FOR SERVICE.

Part: BATTERY — INOPERATIVE (DOOR ASSIST) · airframe 56,445 hrs · 7,472 cycles

EMERGENCY POWER ASSIST SYSTEM AT R1 DOOR FAILED TEST. REPLACED BATTERY AS PER AMM 52-11-20-401. OPS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (DOOR ASSIST) · airframe 56,445 hrs · 7,472 cycles

EMERGENCY POWER ASSIST SYSTEM AT L4 DOOR FAILED TEST. REPLACED BATTERY AS PER AMM 52-11-20-401. OPS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (DOOR ASSIST) · airframe 56,445 hrs · 7,472 cycles

EMERGENCY POWER ASSIST SYSTEM AT R4 DOOR FAILED TEST. REPLACED BATTERY AS PER AMM 52-11-20-401. OPS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (DOOR ASSIST) · airframe 56,445 hrs · 7,472 cycles

EMERGENCY POWER ASSIST SYSTEM AT L3 DOOR FAILED TEST. REPLACED BATTERY AS PER AMM52-11-20-401. OPS CHECKED GOOD.

Part: SKIN — DAMAGED (BS 2118) · airframe 60,077 hrs · 7,795 cycles

POSSIBLE LIGHTNING STRIKE, BS 2118 S5-30R. REMOVED DAMAGED AREA OF FUSELAGE SKIN IAW PRI 504672-14, REV O. PERFORMED HFEC OF CUTOUT IAW NDT 51-00-00, PART 6 NO DEFECTS NOTED. FABRICATED REPAIR PARTS IAW SRM 53-00-01, REPAIR 4. TREATED & PAINTED REPAIR PARTS IAW SRM 53-00-01 REPAIR 4. INSTALLED REPAIR SRM 53-00-01, REPAIR 4.

Part: SKIN — DAMAGED (BS 2115) · airframe 60,077 hrs · 7,795 cycles

POSSIBLE LIGHTNING STRIKE, BS 2115 S29R. REMOVED DAMAGED AREA OF SKIN IAW SRM 53-00-01 REPAIR NR 4. PERFORMED HFEC OF CUTOUT IAW NDT 51-00-00 PRT 6, NO DEFECTS NOTED. FABRICATED REPAIR DOUBLER IAW SRM 53-00-01 REPAIR NR 4.

Part: SKIN — DAMAGED (BS 2018) · airframe 60,077 hrs · 7,795 cycles

LIGHTNING STRIKE DAMAGE FOUND AT BS 2018 AND JUST BELOW STRINGER 4. REPAIRED IAW SRM 53-00-01, REPAIR 4 .

Part: SKIN — DAMAGED (BS 2067) · airframe 60,077 hrs · 7,795 cycles

LIGHTNING STRIKE AT BS 2067 S30R. INSTALLED FASTENER IAW SRM 53-00-01, REPAIR 8.

Part: SENSOR — FAULTY (AC BAY) · airframe 54,235 hrs · 7,265 cycles

DIV, FLT 295 NRT LEFT PACK INOPERATIVE INFLIGHT AT 32000 FT. FLIGHT DIVERTED TO DTW DUE TO LEFT PACK CYCLING. LEFT LOWER PACK FLOW CONTROL VALVE AND LEFT PACK FLOW CONTROL SENSOR WAS REPLACED. ETOPS CATEGORY 'B': DIVERSION OR TURNBACK

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,395 hrs · 7,169 cycles

DURING A MAINTENANCE VISIT, THE EMERGENCY FLOOR PROXIMITY LIGHTS AT SEATS 10B, 10C AND 12B WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE FLOOR PROXIMITY LIGHT ASSEMBLY. SYSTEM OPERATION WAS NORMAL AFTER THE FLOOR PROXIMITY LIGHTS WERE REPLACED.

Part: FUSE — BLOWN (CABIN) · airframe 52,679 hrs · 7,098 cycles

DURING A MAINTENANCE VISIT, THE EMERGENCY LIGHTS AT ROWS 31DF THROUGH 42DF WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND A BAD FUSE IN THE BATTERY PACK AND REPLACED M33404 NR 4 PER B777 AMM 33-50. SYSTEM OPERATION WAS NORMAL AFTER M33404WAS REPLACED.

Part: SKIN — CRACKED (L4 DOOR) · airframe 50,829 hrs · 6,923 cycles

FOUND L4 DOOR OUTER SKIN LWR AFT CORNER BENT AND CRACKED REPAIRED L4 DOOR IAW ERA 489082 -14.

Part: SKIN — DENTED (FUSELAGE) · airframe 50,829 hrs · 6,923 cycles

FOUND DENT IN FUSELAGE OUT OF LIMITS AT STA 2040 BETWEEN S-39R AND S-40R. REPAIRED DENT IAW ERA 489083-14 REV O.

Part: ANTENNA — FAILED (WEATHER RADAR) · airframe 45,403 hrs · 6,366 cycles

IRREG WEATHER RADAR FAILED. R & R WX ANTENNA DRIVE UNIT IAW MM. ALL TEST OK LRU REPLACEMENT TEST OK IAW MM. OK FOR SERVICE. BORROWED PART, MFG P/N 622-5136-202. ETOPS CATEGORY 'B': DIVERSION OR TURNBACK.

Part: CIRCUIT BREAKER — TRIPPED (NR 2 ENGINE) · airframe 43,239 hrs · 6,165 cycles

DURING TAXI AFTER ENG START RECEIVED EICAS MSG, ENG REVERSE LIMITED R-. RTB NO ASSOCIATED FAULTS ON MAT. RAN ENGINE CYCLED REVERSER CHECK GOOD PER AMM.

Part: PUMP — LOOSE (NR 1 HYD SYSTEM) · airframe 42,480 hrs · 6,108 cycles

DURING NR 1 ENG RUN FOUND HYD PUMP BACKING OUT AT THE 2 O`CLOCK POSITION. REMOVED HYD PUMP FOR ACCESS TO DAMAGED STUD. REMOVED AND REPLACED NR 1 ENG PER TRANSMITTAL 11T003.

Part: PUMP — INTERMITTENT (LT ENG FUEL) · airframe 42,180 hrs · 6,085 cycles

ON PUSH BACK CENTER FUEL PUMP L EICAS MSG CAME ON. MX MSG 28-11002.28-11030 T/S PER FIM 28-22-00-810-838 BOTH MSG INTERMITTENT FAULT.

Part: ENGINE — MAKING METAL (APU) · airframe 40,331 hrs · 5,944 cycles

REMOVED AND REPLACED APU DUE TO METAL ON CHIP DETECTOR. POST MTC IN-FLT START IN FLT RELEASE. FOUND EXCESSIVE METAL ON MAIN CHIP DET. REMOVED AND REPLACED APU PER M/M OPS GOOD.

Part: ENGINE — MAKING METAL (NR 1) · airframe 35,794 hrs · 5,573 cycles

NR 1 ENGINE, FOUND SMALL QUANTITY OF FINDS ON THE MASTER CHIP DETECTOR. RAN ENGINE PER PFHB. FOUND METAL ON NR 1 ENG CHIP DETECTOR AND EGB AND SAGB CHIP DETECTORS 984543. DUE NR 1 ENGINE CHANGE. REPLACED NR 1 ENGINE PER TRANS 11T003.

Part: BEARING — FAILED (STARTER) · airframe 34,856 hrs · 5,483 cycles

DURING ENG START GND CREW REPORTED SPARKS IN NR 2 ENG THEN SIGNALED A TAIL PIPE FIRE ENG AUTO SHUTDOWN CK LIST ACCOMPLISHED. INSPECTED TAIL PIPE NO DEFECTS NOTED. FOUND NR 2 ENG STARTER BEARINGS FAILED. REMOVED AND REPLACED NR 2 ENG STARTER PER M/M. LEAK CK AND OPS CKS GOOD, MFG P/N 3505788-7, S/N OFF 489C, S/N ON 593C.

Part: FAN — MALFUNCTIONED (CABIN) · airframe 32,976 hrs · 5,299 cycles

BURNING RUBBER SMELL IN FWD CABIN AREA FOLLOWED APPROX 30 SECONDS LATER WITH A RECIRC FAN STATUS MESSAGE. CHECKED MX INFO DISPLAY AND SHOWED FWD UPPER RECIRC FAN OFF. SMELL CLEARED IN LESS THAN ONE MINUTE. ATL MX ASKED THAT THE UPPER RECIRC SWITCH TO BE TURNED OFF. NO FURTHER INDICATIONS. REPLACED FAN CKS GOOD. REINSTALLED CEILING PANELS, REMOVED MCO PLAC P/N 4100945A.

Part: SWITCH — DEFECTIVE (E/E BAY LIGHTS) · airframe 32,893 hrs · 5,291 cycles

UNUSUALLY STRONG ODOR NOTED IN MAIN E/E COMPARTMENT. COULD NOT POSITIVELY IDENTIFY NATURE OF ODOR. PERFORMED INSP OF E/E ELECTRICAL COMPONENTS AND WIRING. NO TROUBLE FOUND. ALL C/B-S IN. INSPECT FWD CARGO BIN. ALL OKAY. ODOR DISSIPATED AFTER 2 HOURS. MAIN E/E COMPARTMENT LIGHTS NOTED TO GO INTERMITTENTLY DIM THEN BRIGHT. AFTER 2 HOURS LIGHTS INTERMITTENTLY UNCONTROLLABLE FROM E/E LIGHTS SWITCHES IN BOTH ON OR OFF POSITIONS. FWD TO MCO AND PLAC 33-31-01. C/B PULLED AND COLLARED. REPLACED DEFECTIVE SWITCH. E AND E LIGHTS WORKING NORMAL. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: START VALVE — FAILED (NR 1 ENGINE) · airframe 28,660 hrs · 4,823 cycles

ENGINE START VALVE L EICAS MSG DURING START, RTB. REPLACED NR 1 ENG START VALVE. OPS CHECK OK.

Part: BATTERY — DISCHARGED (L1 DOOR) · airframe 28,052 hrs · 4,755 cycles

CREW REPORT FLASHLIGHT RED LIGHT NOT FLASHING AT 1L DOOR. REPLACED BATTERY. OPS CHECK NORMAL.

Part: AOA — UNKNOWN (STALL WARNING) · airframe 27,021 hrs · 4,643 cycles

LEFT AND RIGHT AOA VANE SHOWS ON STATUS. ERASED FAULT AT CH 31.DID NOT RETURN. OK FOR SERVICE.

Part: FUSE — BLOWN (EMERGENCY LIGHT) · airframe 26,621 hrs · 4,601 cycles

ROWS 30 THRU 40 IN SEAT EMERGENCY LIGHTS INOP. REPLACED FUSE IN PWR SUPPLY.

Part: OVEN — ODOR (NR 3 GALLEY) · airframe 25,598 hrs · 4,478 cycles

AFT OVEN, STRONG ELECTRICAL ODOR AS WELL AS ELECTRICAL SMOKE. NO FAULT LIGHT, NO POPPED CIRCUIT BREAKERS. REPLACED OVEN.

Part: BULB — BURNED (CABIN LIGHTS) · airframe 24,720 hrs · 4,368 cycles

HALOGEN LIGHT IN 2R BUNK AREA IN AFT CREW REST SHORTED OUT. FOUND FLUORESCENT BULB SOCKET IN AFT FLIGHT ATTENDANT CREW REST AFT BUNK RIGHT SIDE BURNED AND PIN ON BULB BURNED. NO FURTHER DAMAGE FOUND. REPLACED BALLAST AND BULB

Part: SWITCH — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 21,472 hrs · 3,890 cycles

EMERGENCY LIGHT SWITCH AT 4RT INTERMITTANT CAUSING EMERGENCY LIGHTS TO FLICKER. REPLACED SWITCH.

Part: ENGINE — BIRD INGESTION (NR 2) · airframe 19,913 hrs · 3,647 cycles

BIRD INGESTION AT TAKEOFF. SURGE AND ENGINE EXCEEDENCE. ENGINE CHANGED.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,373 hrs · 3,281 cycles

ZONE 3 SEAT MOUNTED EMERGENCY LIGHTS NOT ILLUMINATING. REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK, OPS NORMAL.

Part: VALVE — FAILED (WATER SYS) · airframe 15,485 hrs · 2,991 cycles

AFTER TAKEOFF NO WATER PRESSURE IN GALLEYS OR LAVS. FOUND PRESELECT OVERFLOW VALVE FAILED AND REPLACED SAME.

Part: ENGINE — FAILED (NR 1) · airframe 13,903 hrs · 2,747 cycles

LT ENGINE VIBRATION WENT TO 5.0 ON CLIMBOUT ACCOMPLISHED BY ENGINE SURGE STALL. RETURNED TO MAN NOTICEABLE AIRFRAME BUFFETING OPERATED ENG AT IDLE TO NO OTHER ABNORMAL INDICATIONS. REPLACED NBR 1 ENG PER ROUTINE CARD DECK

Part: ENGINE — FAILED (NR 1) · airframe 13,903 hrs · 2,747 cycles

ATB-NR 1 ENGINE VIBRATES N2 5.0 AND COMPRESSOR STALL. METAL FOUND IN TAILPIPE ON ARRIVAL IN MAN.

Part: ACM — UNSERVICEABLE (LEDT PACK) · airframe 13,356 hrs · 2,638 cycles

GOT SMELL OF OIL WITH VIBRATION AFTER T/O 30 MINUTES LATER L PACK MODE EICAS MESSAGE AND STATUS MESSAGE ECON COOL VALVE L INSPECTED L PACK ACM FOUND BLADE MISSING FROM ACM TURBINE SECTION FWD TO MCO/PLAC PER MEL 21-52-01 C/P DISCONNECTED CLEARED STATUS MESSAGE INSPECTED L PACK ACM - FOUND BLADED MISSING FROM ACM TURBINE SECTION - FWD TO MCO/PLAC PER MEL 21-52-01 - C/P DISCONNECT - CLEARED STATUS MSG OK ETOPS CATEGORY 'B': DIVERSION OR TURNBACK

Part: WARNING SYSTEM — ACTIVATED (SPEED BRAKES) · airframe 12,577 hrs · 2,484 cycles

AT APPLICATION OF TAKE OFF POWER CREW RECEIVED CONFIGURATION SPEEDBRAKE EICAS WARNING AND ASSOCIATED AURAL WARNING CREW DISCONNECTED T/O BELOW 5 KTS. PERFORMED MAT TEST ON WARNING ELECTRONICS SYSTEM AND SPEED BRAKE TEST. NO DEFECTS NOTED NO MESSAGES OR FAULTS AT THIS TIME.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 12,410 hrs · 2,450 cycles

"C" SYSTEM HYDRAULIC QUANTITY LEVEL DECREASED IN FLIGHT. EMERGENCY LANDING DECLARED TO AIRPORT. AIRCRAFT LANDED WITHOUT INCIDENT.AIRCRAFT TOWED TO GATE. FOUND C2 ELECTRIC HYDRAULIC PUMP LEAKING. PUMP REPLACED.

Part: ODOR — DETECTED (SEAT 11H) · airframe 8,500 hrs · 1,793 cycles

CREW REPORTS POSSIBLE ELECTRICAL SMELL, SEAT 11-H. SEAT OPERATION NORMAL, NO ELECTRICAL SMELL NOTED. INSPECTED WIRES, ALL CHECKS OK.

Part: COMPRESSOR — OVERHEATED (CABIN) · airframe 4,213 hrs · 1,001 cycles

A/C DIVERTED TO LGW DUE TO RUBBER SMELL IN AFT CABIN. FOUND POTABLE WATER COMPRESSOR OVERHEATED.

Part: STRUCTURE — BIRD STRIKE (FUSELAGE) · airframe 3,302 hrs · 858 cycles

FLT RETURNED TO JFK DUE TO POSSIBLE BIRD STRIKE. PERFORMED BIRD STRIKE INSPECTION, FOUND SMALL AMOUNT OF BLOOD ON LOWER FUSELAGE JUST AFT OF RIGHT NOSE GEAR DOOR. ALSO SMALL SPOT OF BLOOD ON RIGHT INBOARD TRAILING EDGE FLAP. OTHERWISE THERE WAS NO PHYSICAL DAMAGE TO THESE AREAS. INSPECTION OF THE REST OF THE AIRCRAFT WAS ALL OK.