N399AN

Part: PUMP — UNRELIABLE (RT ENGINE OIL) · airframe 77,436 hrs · 12,991 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS ON DESCENT, RIGHT ENGINE OIL PRESSURE WENT INTO YELLOW THEN RED AT LOW THRUST POWER SETTING. AS FLIGHT PROGRESSED IT TOOK HIGHER THRUST SETTINGS TO KEEP OIL PRESSURE OUT OF THE CAUTION RANGE. RIGHT ENGINE SHUT DOWN UPON LANDING. MAINTENANCE REMOVED AND REPLACED RIGHT HAND ENGINE LUBE AND SCAVANGE PUMP IAW AMM 79-21-03. OPS TEST & LEAK CHECK GOOD.

Part: FLASHLIGHT — MISSING (CABIN) · airframe 75,924 hrs · 12,649 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY FLASHLIGHT MISSING ON LEFT SIDE OF MID GALLEY. MAINTENANCE REPLACED FLASHLIGHT PER AMM 25-64-00.

Part: SENSOR — UNRELIABLE (CIT) · airframe 75,581 hrs · 12,572 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS TWO COMPRESSOR STALLS BELOW 500 WHILE ON APPROACH TO MIA . THE FIRST ONE FELT LIKE THE LEFT ENGINE THE SECOND ONE SOUNDED LIKE THE RIGHT ENGINE. MAINTENANCE TROUBLESHOT AND ACCOMPLISHED FIM TASK 71-05-00. REMOVED AND REPLACED THE L/H ENG & R/H CIT SENSOR IAW AMM 73-21-02. ACCOMPLISHED HIGH POWER ASSURANCE RUN AT ALL POWER SETTING IAW 71-00-00, ALL PARMETERS WERE NORMAL, NO EICAS MESSAGES NOTED. (SEE SDR # AALA201906089002)

Part: SENSOR — UNRELIABLE (CIT) · airframe 75,581 hrs · 12,572 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS TWO COMPRESSOR STALLS BELOW 500 WHILE ON APPROACH TO MIA . THE FIRST ONE FELT LIKE THE LEFT ENGINE, THE SECOND ONE SOUNDED LIKE THE RIGHT ENGINE. MAINTENANCE TROUBLESHOT AND ACCOMPLISHED FIM TASK 71-05-00. REMOVED AND REPLACED THE L/H & R/H ENGINE CIT SENSOR IAW AMM 73-21-02. ACCOMPLISHED HIGH POWER ASSURANCE RUN AT ALL POWER SETTING IAW 71-00-00, ALL PARMETERS WERE NORMAL. NO EICAS MESSAGES NOTED. (SEE SDR # AALA201906119014)

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 75,285 hrs · 12,491 cycles

AIRCRAFT WAS NOT GROUNDED: DURING PS CHECK, EMERGENCY LIGHTS ON OVERHEAD CEILING PANELS, FROM STATION 871.5 TO STATION 1197+66, LEFT AISLE FAILED OT ILLUMINATE DURING VISUAL TEST. MAINTENANCE REPLACED EMERGENCY LIGHTING BATTERY PER STANDARD PRACTICES AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 75,285 hrs · 12,491 cycles

AIRCRAFT WAS NOT GROUNDED: DURING PS CHECK, AFT LEFT DOOR EXTERIOR EMERGENCY LIGHT FAILED TO ILLUMINATE. MAINTENANCE REPLACED BATTERY PACK PER STANDARD PRACTICES AND PEFORMED SATISFACTORY OPERATIONAL CHECK.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,219 hrs · 12,473 cycles

THE FORWARD DOOR EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE BATTERY PACK AND CHARGER. OPS CHECKED GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,219 hrs · 12,473 cycles

THE FORWARD DOOR EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE BATTERY PACK AND CHARGER. OPS CHECKED GOOD.

Part: SIGN — DETACHED (EMERGENCY LIGHT) · airframe 74,951 hrs · 12,404 cycles

EXIT SIGN AT THE L4 DOOR DETACHED. MAINTENANCE INSTALLED THE EXIT SIGN AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: IRU — FAULTY (RIGHT) · airframe 74,351 hrs · 12,260 cycles

DURING CRUISE, THE CENTER AUTOPILOT DISCONNECTED WITH ACCOMPANING EICAS MESSAGE FOR INERTIAL REFERENCE UNIT ON DIRECT CURRENT. FIRST OFFICIER`S ATTITUDE DIRECTION INDICATOR WENT INOPERATIVE AT THE SAME TIME. CENTER IRU DISPLAYED ALIGN ON OVERHEAD IRU CONTROL PANEL. COMPLIED WITH THE QRH PROCEDURES, BUT CENTER IRU REMAINED IN ALIGN MODE, INERTIAL REFERECNE SYSTEM IN MOTION MESSAGE DISPLAYED ON THE FMC. EMERGENCY DELCARED, FLIGHT RETURNED TO DEPARTURE, AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS GROUNDED. ACCOMPLISHED FIM 34-21-815, AND FOUND RIGHT IRU AT FAULT. REPLACED RIGHT IRU IAW AMM 34-21-01. OPERATIONS CHECKED NORMAL.

Part: HANDLE — BROKEN (L1 DOOR) · airframe 73,962 hrs · 12,178 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR ASSIST HANDLE, AT DOOR 1L, WAS BROKEN. MAINTENANCE REPLACED DOOR ASSIST HANDLE PER MM 52-11-00 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 73,742 hrs · 12,133 cycles

RIGHT EMERGENCY LIGHTS, FORWARD CABIN SEATS 8H -21H WERE INOPERATIVE. REPLACED THE POWER SUPPLY IAW AMM 33-51-07. OPS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 73,708 hrs · 12,125 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT FLASHLIGHT DOES NOT TEST CORRECTLY. REPLACED FLASHLIGHT BATTERY LIGHT ILLUMINATES AND LIGHT NOW TURNS GREEN WHEN PRESS TO TEST BUTTON IS PUSHED AMM REF 25 25 03.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 73,540 hrs · 12,091 cycles

AFT EMERGENCY LIGHT EXIT COVERS MISSING. REPLACED THE COVER IAW AMM 35-51-10.

Part: LAMP — INOPERATIVE (SIGN) · airframe 73,507 hrs · 12,086 cycles

SEAT 17H FASTEN SEAT BELT SIGN INOPERATIVE, SIGN FALLING OFF. REPLACED THE LAMPS AND INSTALLED THE ASSEMBLY IAW AMM 33-24-00.

Part: PRESSURE SWITCH — LEAKING (HYD SYSTEM) · airframe 73,269 hrs · 12,044 cycles

DURING FLIGHT CREW REPORTED THAT THE CENTER HYDRAULIC SYSTEM WAS LOOSING QUANTITY AND WOULD LIKELY BE EMPTY UPON ARRIVAL INTO ORD. CAPTAIN DELCARED EMERGENCY AND LANDED WITHOUT INCIDENT. TROUBLE SHOOTING FAULTY/LEAKING DELTA-P AT PRESSURE AND CASE DRAIN FILTER AC MOTOR PUMP C2. REPLACED DELTA P ASSEMBLY PER AMM 29-11-18. OPERATIONS AND LEAK CHECK GOOD. AC OK FOR SERVICE. AIRCRAFT WAS GROUNDED.

Part: FILTER — LEAKING (HYD SYSTEM) · airframe 73,269 hrs · 12,044 cycles

DURING FLIGHT CREW REPORTED THAT THE CENTER HYDRAULIC SYSTEM WAS LOOSING QUANTITY AND WOULD LIKELY BE EMPTY UPON ARRIVAL INTO ORD. DELCARED EMERGENCY AND LANDED WITHOUT INCIDENT. TROUBLESHOT THE FAULTY/LEAKING DELTA-P AT PRESSURE AND CASE DRAIN FILTER AC MOTOR PUMP C2. REPLACED CASE DRAIN FILTER IAW AMM 29-11-18. OPS AND LEAK CHECKED GOOD. AC OK FOR SERVICE. THE AIRCRAFT WAS GROUNDED.

Part: BOTTLE — LOW PRESSURE (LT WING SLIDE) · airframe 72,517 hrs · 11,891 cycles

LEFT WING ESCAPE SLIDE INFLATION BOTTLE PRESSURE BELOW GREEN BAND ON LOW SIDE. REMOVED AND REPLACED THE CYLINDER IAW AMM 25-65-02. THE AIRCRAFT WAS GROUNDED.

Part: ANNUNCIATOR — NO TEST (EMERGENCY LIGHTS) · airframe 71,334 hrs · 11,679 cycles

EMERGENCY DOOR LIGHT WILL NOT TEST ON OVERHEAD PANEL. REPLACED OVERHEAD ANNUNCIATOR PANEL IAW AMM 33-16-02.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 71,050 hrs · 11,620 cycles

AIRCRAFT IN BASE MAINTENANCE. FOUND CRACK ON STIFFENER AT STATION 246. REPLACED STIFFNER PER SRM 53-10-51-2R-3.

Part: THERMOCOUPLE — UNSECURE (RT ENGINE) · airframe 70,561 hrs · 11,527 cycles

EMERGENCY DECLARED. FLIGHT RETURNED TO DEPARTURE DUE TO A RIGHT ENGINE BLEED DUCT LEAK WARNING INDICATION. OVERWEIGHT LANDING UNEVENTFUL. ACCOMPLISHED LEAK CHECK PER MCM 36-96-02. RESECURED FIRE LOOP THERMOCOUPLES PER SRM 51-30-01. LEAK AND OPERATIONAL CHECK GOOD. AIRCRAFT WAS GROUNDED.

Part: LENS — MISSING (CABIN) · airframe 70,341 hrs · 11,483 cycles

AIRCRAFT WAS NOT GROUNDED. MISSING OVERHEAD EMERGENCY LIGHTING LENS COVER AT SEAT 25H. INSTALLED NEW EMERGENCY LIGHT LENS (BEZEL) PER AMM 33-51-04.

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 69,401 hrs · 11,298 cycles

AIRCRAFT WAS GROUNDED. CAPTAIN REPORTED RIGHT MAIN TANK LOST 1500 LBS OF FUEL AND THE FUEL CONFIGURATION LIGHT ILLUMINATED. RIGHT PUMPS SHUT OFF TO EMPTY CENTER TANK. AFTER CENTER TANK WAS AT 0 IT ROSE AGAIN TO 400 LBS WHEN RIGHT TANK PUMPS WERE TURNED ON AGAIN. ACCOMPLISHED FIM 28-22-00 AND FIM 28-21-00 WITH NO FUEL TRANSFER NOTED. OPERATIONAL CHECK GOOD.

Part: LIGHT — CRACKED (CABIN) · airframe 69,300 hrs · 11,280 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT FLOOR PROXIMITY AISLE LIGHT AT SEAT 21HJ IS CRACKED. REMOVED AND REPLACED LIGHT ASSEMBLY IAW AMM 33-51-09. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 69,238 hrs · 11,271 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AFT SEAT ACROSS AISLE FROM SEAT 17B IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-64-01. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 69,155 hrs · 11,259 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT LEFT FORWARD MID GALLEY IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-64-01. OPERATIONAL CHECK GOOD.

Part: LENS — DETACHED (EXIT SIGN) · airframe 67,930 hrs · 11,015 cycles

AIRCRAFT NOT GROUNDED. L1 DOOR EMERGENCY EXIT SIGN LENS COVER DETACHED. INSTALLED LENS COVER. OPERATIONAL CHECK GOOD.

Part: WINDOW — LEAKING (COCKPIT) · airframe 67,403 hrs · 10,939 cycles

VERY LOUD SQUEAL FROM CAPTAIN`S SIDE WINDOW. STARTED CLIMBING THROUGH 10,000 FT AND CONTINUED TO FL350. STOPPED DESCENDING THROUGH 14,000 FT, DIFFERENTIAL PRESSURE OF 6.3 PSI. THE FLIGHT DECLARED AN EMERGENCY AND RETURNED TO JFK WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED L2 WINDOW AND SEAL AS PER AMM 56-11-11. NO LEAKS FOUND, OK FOR SERVICE. THE AIRCRAFT WAS GROUNDED.

Part: LINE — LOOSE (PITOT SYSTEM) · airframe 67,247 hrs · 10,913 cycles

DURING TAKE OFF, CAPTAIN`S AIRSPEED FAILED. STANDBY AND FO`S NORMAL . AFTER TAKEOFF, RECEIVED A MASTER CAUTION, LT & RT EEC, RUDDER RATIO, AILERON LOCKOUT. THE FLIGHT DECLARED AN EMERGENCY AND RETURNED TO FIELD WITHOUT FURTHER INCIDENT. FOUND PITOT LINE LOOSE AND UNLOCKED. SECURED THE PITOT LINE, OPS CHECKED NORMAL IAW MM 34-12-00 AND 34-12-01. OPS CHECK OF BOTH ENGINES IAW MM 71-00-00, RUDDER RATIO IAW MM 27-21-00, AND AILERON LOCKOUT IAW MM 27-11-00, ALL OPSS TESTED OK. THE AIRCRAFT WAS GROUNDED.

Part: PSEU — FAULTED (TAILSKID) · airframe 66,969 hrs · 10,857 cycles

TAIL SKID DISAGREE LIGHT ILLUMINATED WHEN GEAR HANDLE PLACED IN UP POSITION. LEFT MAIN GEAR INDICATED DOWN AND LOCKED WHEN GEAR HANDLE PLACED IN OFF POSITION. LANDING GEAR DOOR LIGHTS REMAINED ILLUMINATED WHEN GEAR HANDLE PLACED IN DOWN POSITION. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT GROUNDED. MAINTENANCE ACCOMPLISHED BITE CHECK OF PSEU WITH HARD FAILURE CARD 011 FAULT RETURNED. REMOVED AND REPLACED PSEU AND ACCOMPLISHED TEST IAW AMM 32-09-04. SYSTEM CHECKS NORMAL.

Part: COUPLING — LOOSE (LE SLAT) · airframe 65,596 hrs · 10,633 cycles

AIRCRAFT WAS GNDED. EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING POST CHECK FUNCTIONAL CHECK FLIGHT THE LE ASYMMETRY LIGHT ILLUMINATED AT FLAPS 30. FOUND BROKEN SAFETY WIRE & BACKED OUT SET SCREWS ON TORQUE TUBE COUPLING INBD NR 5 SLAT OFFSET GEARBOX. INSTALLED COUPLING, SET GAPS & PERFORMED OPERATIONAL CHECK IAW AMM 27-81-24.. SYS CHECKED NORMAL.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,595 hrs · 10,632 cycles

NUMBER 2 GALLEY AFT INBD MOUNT CORRODED STATION 368, RBL 41 - 15. REPLACED NR 2 GALLEY AFT INBD MOUNT IAW AARD 51-00-05-1. ACFT IN BASE MX.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,595 hrs · 10,632 cycles

NUMBER 2 GALLEY FWD INBD MOUNT CORRODED, STATION 347, RBL 41-15. REPLACED NR 2 GALLEY FWD INBD MOUNT AT STATION 347, RBL 41-15 IAW AARD 51-00-05-1. ACFT IN BASE MX.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,595 hrs · 10,632 cycles

NUMBER 1 GALLEY FWD OTBD MOUNT CORRODED. REPLACED NR 1 GALLEY FWD OTBD MOUNT IAW SRM 51-10-02-0G. ACFT IN BASE MX.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,595 hrs · 10,632 cycles

NUMBER 1 GALLEY AFT OTBD MOUNT CORRODED. REPLACED CORRODED GALLEY MOUNT IAW SRM 51-10-02-0G. ACFT IN BASE MX.

Part: HOLDER — LOOSE (EXTERIOR) · airframe 65,595 hrs · 10,632 cycles

EXTERIOR EMER LIGHT NEAR R1 IS INTERMITTENT. REPLACED LAMP HOLDER ASSEMBLY. ACFT IN BASE MX.

Part: CHARGER — INTERMITTENT (CABIN) · airframe 65,595 hrs · 10,632 cycles

EXTERIOR EMER LIGHT, L391, NEAR THE RT WING TE IS INTERMITTENT. REPLACED CHARGER M733 & OPERATIONS CHECK IAW MM 33-51-07, TESTED OK. ACFT IN BASE MX.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,595 hrs · 10,632 cycles

CORROSION ON THE FWD CARGO DOOR SILL SUPPORT STRUCTURE, LOWER SURFACE AROUND POD LOCK & STOP MOUNT BOLT NUTS, STATION 506, RBL45. REMOVED CORROSION IAW EA 258563. ACFT IN BASE MX.

Part: CONNECTOR — LOOSE (CABIN) · airframe 64,634 hrs · 10,449 cycles

SEAT 20H EMER EXIT LIGHTS ARE INOPERATIVE. SECURED LOOSE SEAT CONNECTOR AT 20H IAW 33-51-10. SYS CHECKED NORMAL.

Part: MODULE — FAULTY (TE FLAP) · airframe 64,198 hrs · 10,378 cycles

AFTER TAKEOFF, AT 5000 FEET, FLAPS ON EICAS WITH CONFIG WARNING HORN BEING INTERMITTENT UNTIL LANDING. FLIGHT DECLARED AN EMER & LANDED WITHOUT FURTHER INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED RELAY K215 IAW SWPM 20-81-22 & SENSOR S266 AS A PRECAUTION IAW AMM 32-09-08. R & R CTR FLAP & STAB POSITION MODULE M839 AT P50 ELEC SYSTEM CARD FILE IAW MM 27-58-01.

Part: TRANSMITTER — FAILED (TE FLAP) · airframe 64,198 hrs · 10,378 cycles

AFTER TAKEOFF, AT 5000 FEET, FLAPS ON EICAS WITH CONFIG WARNING HORN BEING INTERMITTENT UNTIL LANDING. FLIGHT DECLARED AN EMER & LANDED WITHOUT FURTHER INCIDENT.. ACFT REMOVED FROM SERVICE. REPLACED RELAY K215 IAW SWPM 20-81-22 & SENSOR S266 AS A PRECAUTION IAW AMM 32-09-08. R & R NR 4 FLAP POSITION TRANSMITTER & ACCOMPLISHED ADJUSTMENT TEST IAW MM 27-51-45.

Part: FSEU — FAULTY (TE FLAP) · airframe 64,198 hrs · 10,378 cycles

AFTER TAKEOFF, AT 5000 FEET, FLAPS ON EICAS WITH CONFIG WARNING HORN BEING INTERMITTENT UNTIL LANDING. FLIGHT DECLARED AN EMER & LANDED WITHOUT FURTHER INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED RELAY K215 IAW SWPM 20-81-22 & SENSOR S266 AS A PRECAUTION IAW AMM 32-09-08. REPLACED FSEU IAW AMM 27-51-01.

Part: MODULE — FAULTY (TE FLAP) · airframe 64,198 hrs · 10,377 cycles

AFTER TAKEOFF, AT 5000 FEET, FLAPS ON EICAS WITH CONFIG WARNING HORN. AN EMER WAS DECLARED & THE FLIGHT RETURNED TO FIELD. WARNING & LIGHT WERE INTERMITTENT & WARNING CONTINUED UNTIL LANDING. ACFT WAS REMOVED FROM SERVICE. FOUND FSEU FAULT, LT FLAP STAB POS NR 27-51018. REPLACED FLAP STAB POSITION MODULE M838. ALL TEST PASSED IAW 27-58-11. OPERATIONALLY CHECKED OK.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 61,872 hrs · 9,982 cycles

EMERGENCY DECLARED, RETURNED TO DEPARTURE, & LANDED UNEVENTFULLY. FOUND HYDRAULIC LINE BROKEN. REPLACED HYDRAULIC LINE ON RIGHT MAIN LANDING GEAR IAW AMM 20-10-10. OPS AND LEAK CHECKED GOOD.

Part: LIGHT — INOPERATIVE (ZONE 100) · airframe 61,725 hrs · 9,955 cycles

LEFT SLIDE EMER LIGHT L645 INOPERATIVE. R & R LAMP IAW AMM 33-51-00. SYS CHECKED NORMAL.

Part: IRU — FAILED (ZONE 200) · airframe 61,704 hrs · 9,950 cycles

AIR INTERRUPT, RETURNED & DECLARED EMER. LANDING UNEVENTFUL. ACFT WAS OVERWEIGHT. DURING CLIMB FIRST OFFICERS FLIGHT DIRECTOR PROVIDED ERRONEOUS INFORMATION, FURTHER INVESTIGATION REVEALED NO INFORMATION AVAILABLE FROM RT OR CTR INERTIAL REFERENCE UNITS. PERFORMED DIAGNOSTIC TEST IAW FIM 22-02-00-810-801. FOUND RT & CTR INERTIAL REFERENCE UNITS FAULTED. R & R UNITS IAW AMM 34-21-01. PERFORMED GND TEST IAW AMM 22-00-02. SYS CHECKED NORMAL.

Part: LIGHT — BROKEN (R1 DOOR) · airframe 60,974 hrs · 9,838 cycles

RIGHT NR 1 DOOR LOWER EMER LIGHT IS BROKEN. REPLACED RT NR 1 DOOR LOWER EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: SLIDE — UNWANTED DEPLOY (OVERWING EXIT) · airframe 60,974 hrs · 9,838 cycles

LEFT OVERWING SLIDE DEPLOYED WHEN ARMING HANDLE, LT FWD HATCH WAS MOVED FROM SAFE TO ARMED POSITION. REPLACED LT OVERWING SLIDE.

Part: CONTACT — DIRTY (EXTERIOR LIGHT) · airframe 60,974 hrs · 9,838 cycles

EXTERIOR EMER EXIT LIGHT AFT OF THE LT NR 4 DOOR INOPERATIVE. CLEANED CONTACTS & REPLACED LAMP. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 59,760 hrs · 9,643 cycles

LEFT NR 4 DOOR EXTERIOR EMER SLIDE LIGHT INOPERATIVE. REPLACED LAMP FOR LT NR 4 DOOR EXTERIOR EMER SLIDE LIGHT. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 57,987 hrs · 9,366 cycles

LT NR 4 DOOR EXTERIOR SLIDE EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LT NR 4 DOOR EXTERIOR SLIDE EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 57,098 hrs · 9,226 cycles

LT FS EXTERIOR EMERGENCY LIGHT BY LT NR 4 DOOR INOPERATIVE. REPLACED LAMP FOR LT FS EXTERIOR EMERGENCY LIGHT AT LT NR 4 DOOR. OPERATIONS CHECKED NORMAL.

Part: SKIN — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 55,043 hrs · 8,893 cycles

UPPER SKIN CORROSION HORIZONTAL STABILIZER AT STRINGER 3 AND RIGHT BUTTLINE 20. ACCOMPLISHED REPAIR PER EA B767-55-029688.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 55,043 hrs · 8,893 cycles

SEAT 20H EMERGENCY LIGHT INOPERATIVE. RESEATED LIGHT ASSEMBLY PLUG FOR SEAT 20H EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: INDICATOR — LEAKING (HYDRAULIC SYS) · airframe 54,436 hrs · 8,798 cycles

JFK - INFLIGHT ORD-LHR. CREW REPORTED LEFT HYDRAULIC SYSTEM QUANTITY STATUS MESSAGE. EMERGENCY DECLARED FLIGHT DIVERTED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND LEFT HYDRAULIC DIFFERENTIAL PRESSURE INDICATOR LEAKING ON LEFT PYLON CASE DRAIN FILTER MODULE. REPLACED HYDRAULIC DIFFERENTIAL PRESSURE INDICATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LENS — MISSING (CABIN) · airframe 53,486 hrs · 8,660 cycles

EMERGENCY ESCAPE PATH LIGHT LENS COVER AT FLIGHT ATTENDANT JUMPSEAT RIGHT SIDE IN THE MID GALLEY MISSING. REPLACED LENS FOR EMERGENCY ESCAPE PATH LIGHT AT FLIGHT ATTENDANT JUMPSEAT. OPS CHECK NORMAL.

Part: LIGHT — SHORTED (CABIN) · airframe 53,054 hrs · 8,596 cycles

MIA - CREW REPORTED ELECTRICAL SMELL FROM POWER PORT/LIGHT AT SEAT 4B. LIGHT BETWEEN SEATS 5A/B FLICKERED TOGETHER ON AND OFF. TURNED POWER PORT OFF BUT SMELL CAME BACK. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND READING LIGHT AT SEAT 5B SHORTED OUT. REPLACED 5B WORK TABLE LIGHT AND SWITCH. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 52,405 hrs · 8,491 cycles

THE 4AB EMERGENCY LIGHTS INOPERATIVE. SECURED CONNECTION FOR EMERGENCY LIGHTS AT 4AB. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,173 hrs · 8,459 cycles

SEAT MOUNTED ESCAPE PATH LIGHT ON SEAT 39B IS INOPEATIVE. REPLACED LAMP FOR SEAT 39B ESCAPE PATH LIGHT. OPS CHECK NORMAL.

Part: LENS — MISSING (CABIN) · airframe 51,723 hrs · 8,383 cycles

SEAT 27AB EMERGENCY LIGHT MISSING LENS. REPLACED LENS FOR SEAT 27AB EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: CONTACT — DIRTY (EXTERIOR LIGHT) · airframe 51,723 hrs · 8,383 cycles

LEFT NUMBER 4 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. CLEANED CONTACT ON LEFT NUMBER 4L DOOR EXTERIOR EMERGENCY. OPS CHECK NORMAL.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 51,483 hrs · 8,342 cycles

LEFT ROW 26 CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT ROW 26 CEILING EMERGENCY LIGHT. OPS CHECKED NORMAL.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 51,483 hrs · 8,342 cycles

RIGHT ROW 37 CEILING EMERGENCY LIGHT MISSING LENS COVER. REPLACED LENS COVER FOR RIGHT ROW 37 CEILING EMERGENCY LIGHT. OPS CHECKED NORMAL.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 51,483 hrs · 8,342 cycles

AFT RIGHT DOOR EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. REPLACED LAMP FOR AFT RIGHT DOOR EXTERIOR EMERGENCY LIGHT. OPS CHECKED NORMAL.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 51,483 hrs · 8,342 cycles

LEFT ROW 32 CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT ROW 32 CEILING EMERGENCY LIGHT. OPS CHECKED NORMAL.

Part: LIGHT — NOT SEATED (CABIN) · airframe 51,047 hrs · 8,254 cycles

LEFT NUMBER 2 DOOR EXIT EMERGENCY LIGHT INOPERATIVE. RESEATED BULB FOR LEFT NUMBER 2 DOOR EXIT EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: SHUTOFF VALVE — LEAKING (HYDRAULIC SYS) · airframe 49,962 hrs · 8,078 cycles

LHR - CREW REPORTED CENTER HYDRAULIC QUANTITY SLOWLY DECREASING ALONG WITH EICAS MESSAGE. EMERGENCY DECLARED FLIGHT RETURNED LHR LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND FLAP/SLAT SHUT-OFF VALVE MODULE IN RIGHT GEAR WHEEL WELL LEAKING. REPLACED MODULE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: INDICATOR — LEAKING (HYDRAULIC SYS) · airframe 45,071 hrs · 7,265 cycles

MIA - CREW REPORTED RIGHT HYDRAULIC SYSTEM LOSS INFLIGHT. EMERGENCY DECLARED, LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND RIGHT ENGINE PYLON MODULE LEAKING. REPLACED PRESSURE DIFFERENTIAL INDICATOR AND O-RING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FRAME — DENTED (FUSELAGE) · airframe 43,939 hrs · 7,087 cycles

DURING THE CURRENT €ŒC€? CHECK AAL FOUND A TYPICAL DENTS TO THE STATION 500 FUSELAGE FRAME INNER CHORD BETWEEN STRINGER 30 LEFT AND 31 LEFT DUE TO IMPACT DAMAGE FROM CARGO PALLETS. THE DAMAGE WAS FOUND DURING ROUTINE GVI INSPECTIONS OF THE CARGO FLOOR STRUCTURE AND IS TYPICAL TO THE DAMAGE FOUND PER SR 1-1568143824. EA B767-53-011014, REPAIRED PER MAJOR EA NUMBER B767-53-011014 DATED 10JUN10.

Part: CONNECTOR — MISALIGNED (ENGINE) · airframe 43,117 hrs · 6,939 cycles

MAD - RIGHT EICAS AND SECONDARY EXHAUST GAS TEMPERATURE INDICATION FLUCTUATING TO FULL SCALE DEFLECTION. FLIGHT RETURNED MAD LANDED WITHOUT INCIDENT. FOUND MISALIGNED CONNECTOR (9 O`CLOCK POS) ON EGT JUNCTION BOX. CLEANED AND RE-SECURED JUNCTION BOX CONNECTORS. DURING IDLE RUN BY CREW ALL INDICATIONS NORMAL AND STABLE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 42,750 hrs · 6,864 cycles

SEAT 9A POWER PORT HAD ELECTRICAL ODOR. REPLACED POWER PORT OUTLET. OPS CHECKED NORMAL.

Part: CIRCUIT BREAKER — POPPED (COCKPIT) · airframe 39,847 hrs

FCO - ELECTRICAL MALFUNCTION. FOUND LEFT CIRCUIT BREAKER DC BUS SECTION ONE POPPED. RESET CIRCUIT BREAKER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: UNKNOWN — ODOR (WEATHER RADAR) · airframe 39,271 hrs · 6,288 cycles

BSB - INFLIGHT MIA-GIG - HEAVY ACRID SMELL IN COCKPIT AFTER APU SHUTDOWN. LANDED WITHOUT INCIDENT BSB. AIRCRAFT REMOVED FROM SERVICE. THE WEATHER RADAR SYSTEM WAS ERASED AND WXR CHECKED OKAY FOR SERVICE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS)

MIA - EMERGENCY LIGHT AT SEAT 37B INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT 37B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,246 hrs

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LAX - EMERGENCY LIGHTS AT CEILING AND FLOOR AT LEFT AISLE SEAT ROWS 30 TO AFT OF CABIN INTERMITTENTLY ON AND OFF THROUGH OUT FLIGHT. LANDED LAX WITHOUT INCIDENT. REPLACED BATTERY PACK AND CHARGER AT SEAT 39AB FOR EMERGENCY LIGHTS AT CEILING AND FLOOR AT LEFT AISLE SEAT ROWS 30 TO AFT OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — LOOSE (CABIN)

DFW - EMERGENCY LIGHT ASSEMBLY LOOSE AT SEAT 25H. RESECURED EMERGENCY LIGHT ASSEMBLY AT SEAT 25H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY EXIT LIGHT AT OVERHEAD ABOVE SEAT 5H INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT AT OVERHEAD ABOVE SEAT 5H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY LIGHTS AT SEAT ROW 22 INOPERATIVE. REPAIRED LIGHT ASSEMBLY AT SEAT ROW 22 FOR INOPERATIVE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

EMERGENCY LIGHTS AT SEAT ROW 21 INOPERATIVE. REPAIRED LOOSE CONNECTION AT SEAT ROW 21 FOR INOPERATIVE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: CONNECTOR — DISCONNECTED (CABIN)

EMERGENCY LIGHTS BETWEEN ROWS 27HJ AND 30HJ INOPERATIVE. RECONNECTED CONNECTOR PLUG AT SEATS 25HJ AND 28HJ FOR INOPERATIVE EMERGENCY LIGHTS BETWEEN ROWS 27HJ AND 30HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHTS FROM SEAT 31H TO 36H INOPERATIVE. RESECURED LOOSE CONNECTOR FOR EMERGENCY LIGHTS FROM SEAT 31H TO 36H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT)

CDG - EMERGENCY ESCAPE PATH LIGHTS BETWEEN 28AB AND 36AB INOPERATIVE. FOUND CONNECTOR AT 37AB DISCONNECTED. RECONNECTED CONNECTOR AT 37AB FOR EMERGENCY ESCAPE PATH LIGHTS BETWEEN 28AB AND 36AB. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

LAX - SEAT MOUNTED ESCAPE PATH LIGHTS AT SEATS 21H TO 23H INOPERATIVE. SECURED LOOSE WIRE CONNECTOR ON SEAT 20H LIGHTS FOR SEAT MOUNTED ESCAPE PATH LIGHTS AT SEATS 21H TO 23H. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: LIGHT — INOPERATIVE (SEAT 24G)

DFW EMERGENCY LIGHT AT SEAT 24G DAMAGED. REPAIRED EMERGENCY LIGHT ASSEMBLY FOR SEAT 24G. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: COVER — BROKEN (EMERGENCY LIGHT)

MIA - EMERGENCY EXIT LIGHT COVER MISSING MID GALLEY. FOUND ASSEMBLY BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

SFO - EMERGENCY ESCAPE PATH LIGHTING AT SEATS 21 AND 22AB INOPERATIVE. RESEATED LOOSE CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHTING FOR SEATS 21 AND 22AB. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — BROKEN (LAVATORY)

DFW - EMERGENCY LIGHT ON WALL AT AFT LEFT LAVATORY BROKEN. REPLACED EMERGENCY LIGHT ON WALL AT AFT LEFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY SEAT AISLE LIGHTS AT 3B, 4B, 5B, AND 6B INOPERATIVE. REPLACED PACK AT M735. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

EMERGENCY LIGHTS INOPERATIVE ON SEATS 31B AND 32B. SECURED LOOSE CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

LAX - MAINTENANCE OBSERVED EMERGENCY LIGHTS INOPERATIVE FROM SEAT ROWS 2 THROUGH 13. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT PATH LIGHT AT SEAT 28B INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 28B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT PATH LIGHTING AT SEAT 19B INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY EXIT PATH LIGHTING AT SEAT 19B ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS AT SEATS 9H/10H INOPERATIVE. TIGHTENED EMERGENCY LIGHT CONNECTOR AT SEAT 9H/10H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

EMERGENCY LIGHT INOPERATIVE AT SEATS 31HJ, 30HJ, 29HJ, AND 27HJ ARE INOPERATIVE. RECONNECTED PLUG AT 27HJ. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — FAULTY (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 19B THROUGH 22B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 19B, 20B, AND 22B INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT 19B, 20B, AND 22B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: INDICATOR — SHORTED (GALLEY)

ORD - FLT 42 - AFTER TAKEOFF, FIRST CLASS GALLEY POWER ON INDICATOR LIGHT SHORTED CAUSING SMOKE IN GALLEY. CIRCUIT BREAKER PULLED AND POWER TO GALLEY SECURED FOR DURATION OF FLIGHT. REPLACED FIRST CLASS GALLEY POWER ON INDICATOR LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: UNKNOWN — ODOR (CABIN)

GIG - 904 - AFTER TAKEOFF, FLIGHT ATTENDANT REPORTED FUEL VAPORS IN CABIN, PILOT WENT BACK AND VERIFIED ODOR. FUMES WERE STRONGEST AT ROW 22. FUMES REMAINED CONSTANT THROUGHOUT FLIGHT AND ON GROUND AFTER LANDING. INSPECTED APU FUEL SUPPLY LINE AND SHROUD, INSPECTED BOTH ENGINE FUEL FEED SYSTEM, INSPECTED APU DRAIN MAST, CLOSE THE ENTRY DOORS, RAN APU WITH PACKS ON. THE SAME WITH LEFT AND RIGHT ENGINES ISOLATED. NO EVIDENCE OF LEAK/OR FUEL ODORS. SYSTEM GROUND CHECK NORMAL OPERATION. (M)