N392AN

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 82,019 hrs · 13,386 cycles

AIRCRAFT NOT GROUNDED: PILOT REPORTS ON APPROACH, FLAPS SELECTED 25 DEGREES, AIRCRAFT ROLLED RIGHT REQUIRING 2 UNITS LEFT AILERON TO FLY LEVEL. MAINTENANCE DEPLOYED ALL FLIGHT CONTROL DEVICES AND INSPECTED FOR DAMAGE, NO DEFECTS FOUND. ACCOMPLISHED BITE TEST OF ALL FLT. CONTROL MODULES AND OPERATIONAL CHECK FOR THE FLAP SYSTEM IAW AMM 27-51-00. SYSTEM CHECK NORMAL.

Part: CONTROL UNIT — FAILED (AUTOBRAKE SYS) · airframe 81,312 hrs · 13,262 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS DURING ROLL OUT, AUTO BRAKE DISARMED JUST AFTER TOUCHDOWN. AUTOBRAKE WERE IN POSITION 3. MAINTENANCE ACCOMPLISHED FIM TASK 32-42-00 AND REPLACED AUTOBRAKE ANTISKID UNIT IAW AMM 32-42-01. OPS CHECKS GOOD.

Part: TRANSFORMER — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,896 hrs · 12,965 cycles

EXTERIOR EMERGENCY LIGHT, LEFT WING GROUND ILLUMINATION, WAS INOPERATIVE. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE LIGHT TRANSFORMER IAW AMM 33-41-00.

Part: WINDOW — LACK OF LUBE (COCKPIT) · airframe 78,465 hrs · 12,662 cycles

CAPTAIN'S WINDOW WOULD NOT OPEN. MAINTENANCE LUBRICATED THE WINDOW TRACKS AND PERFORMED A SATISFACTORY OPERATIONAL CHECK IAW AMM 56-11-02.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 78,205 hrs · 12,607 cycles

EMERGENCY BATTERY PACK M737 LOST ITS CHARGE. REPLACED THE BATTERY PACK.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 77,044 hrs · 12,396 cycles

R1 DOOR EXIT LENS FELL OFF. LIGHT LENS AND BEZEL DAMAGED. REPLACED EXIT SIGN LIGHT ASSEMBLY R1 DOOR PER AAMM 33-51-00 AND AAMM 33-51-01. OK FOR SERVICE.

Part: COVER — DETACHED (CABIN) · airframe 76,931 hrs · 12,372 cycles

AIRCRAFT WAS NOT GROUNDED. L4 DOOR EXIT SIGN COVER IS OFF OF LIGHT PANEL. REINSTALLED LIGHT COVER PER AMM 25-25-00.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 76,809 hrs · 12,348 cycles

R1 DOOR BOTTOM EXIT SIGN LENS WAS FALLING OFF. MAINTENANCE INSTALLED EXIT SIGN LENS AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 76,322 hrs · 12,263 cycles

AIRCRAFT WAS GROUNDED. TRAILING EDGE FLAP DISAGREE MESSAGE WHEN FLAPS WERE SELECTED TO 15. AN EMERGENCY WAS DECLARED. THE FLIGHT PERFORMED A "GO-AROUND" AND ACCOMPLISHED QRH PROCEDURES. FLIGHT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE FOR INSPECTION AND REPAIR. FSEU BITE TEST PROCEDURE PERFORMED IAW FIM 27-51-00-815-809 NO EXISTING FAULT FOUND. T/S FIM TASK 27-51-00-815-810 FIGURE 105 NO DEFECT FOUND SYSTEM WORKS NORMALLY.

Part: SIGN — LOOSE (EMERGENCY LIGHTS) · airframe 76,245 hrs · 12,249 cycles

EXIT SIGN AT THE R1 DOOR BOTTOM IS LOOSE. SECURED THE SIGN. OPS TESTED GOOD IAW MM 33-50-00.

Part: HYDRAULIC LINE — LEAKING (LT MLG) · airframe 75,774 hrs · 12,171 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. CENTER HYDRAULIC SYSTEM PRESSURE CAUTION LIGHT ILLUMINATED. LANDING UNEVENTFUL. REMOVED AND REPLACED LEFT MAIN LANDING GEAR HYDRAULIC HOSE ASSEMBLY (LINE) PER AMM 20-10-10. LEAK AND OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (SEAT 3A) · airframe 75,701 hrs · 12,160 cycles

SEAT 3A MOUNTED EMERGENCY LIGHT FOUND INOPERATIVE. REMOVED AND REPLACED THE LIGHT IAW AMM 33-51-00. OPS CHECKED GOOD.

Part: LENS — MISSING (CABIN) · airframe 75,346 hrs · 12,102 cycles

AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED EMERGENCY ESCAPE PATH WHITE LIGHT ON SEAT 20B, LOWER PART BY AISLE, HAS A MISSING CAP. REPLACED LENS COVER (CAP). OPERATIONAL CHECK GOOD.

Part: GIRT BAR — OBSTRUCTED (R4 DOOR) · airframe 75,239 hrs · 12,086 cycles

AIRCRAFT WAS NOT GROUNDED. R4 DOOR IS DIFFICULT TO ARM/DISARM. EXTRA PRESSURE REQUIRED ON GREEN BUTTON AND LEVER. INSPECTED DOOR PER AMM 52-05-03 AND REMOVED DEBRIS FROM GIRT BAR MECHANISM. OPERATIONAL CHECK GOOD.

Part: SIGN — LOOSE (CABIN) · airframe 75,239 hrs · 12,086 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGN BY THE L4 DOOR IS LOOSE. READJUSTED EXIT SIGN PER AMM 33-51-01. OPERATIONAL CHECK GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 75,054 hrs · 12,058 cycles

AIRCRAFT WAS NOT GROUNDED. SEAT 3J TRIM PANEL EMERGENCY LIGHT PLUG WIRE, BROKEN. RESECURED SEAT 3J TRIM PANEL PER ESO 12323 AND CMM 25-20-08.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 74,607 hrs · 11,980 cycles

EMERGENCY LIGHT BY THE R1 DOOR, NEAR THE FLOOR IN THE FIRST CLASS GALLEY HAS A DETACHED LENS. INSTALLED THE LENS. OPS CHECKED GOOD.

Part: LENS — MISSING (CABIN) · airframe 74,030 hrs · 11,894 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT ON CEILING IN AISLE BY SEAT 7A HAS A MISSING LENS COVER. INSTALLED LENS COVER. OPERATIONAL CHECK GOOD.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 73,918 hrs · 11,875 cycles

EMERGENCY LIGHT AT THE L4 DOOR HAS A DETACHED LENS COVER. REINSTALLED LENS COVER IAW AMM 33-51-01. OPERATIONAL CHECK GOOD.

Part: LENS — DETACHED (CABIN) · airframe 73,846 hrs · 11,853 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT OVER L1 DOOR HAS A DETACHED LENS COVER. REMOVED AND REPLACED LIGHT ASSEMBLY IAW AMM 33-51-09. OPERATIONAL CHECK GOOD.

Part: SKIN PANEL — DAMAGED (LE SLAT) · airframe 73,724 hrs · 11,828 cycles

AIRCRAFT WAS GROUNDED. LEFT WING LEADING EDGE NR 6 SLAT LOWER CLOSURE PANEL HAS A DAMAGED SECTION ENCLOSING AN AREA OF APPROXIMATELY 2 INCHES BY 1.5 INCHES. REPAIRED IAW AARD 57-43-02-2. OPERATIONAL CHECK GOOD.

Part: LENS — MISSING (CABIN) · airframe 73,701 hrs · 11,823 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGN AT L4 DOOR HAS A MISSING LENS COVER. INSTALLED LENS COVER IAW AMM 33-51-00. OPERATIONAL CHECK GOOD.

Part: RECEPTACLE — SMOKE (CABIN) · airframe 73,223 hrs · 11,726 cycles

AIRCRAFT NOT GROUNDED. DURING FLIGHT FROM LHR, A PASSENGER IN SEAT 8G PLUGGED IN HIS ELECTRONIC CHARGER INTO THE POWER PORT PRODUCING A POPPING NOISE AND A PUFF OF SMOKE. NO FURTHER SMOKE OR FIRE. OPERATIONAL CHECK IAW AMM 25-25-11 SATISFACTORY. (CLOSED)

Part: SENSOR — FAULTY · airframe 73,154 hrs · 11,716 cycles

DURING CRUISE RECIEVE A "L PACK TEMP" EICAS MESSAGE. ACCOMPLISHED QRH CHECKLIST AND TURNED LEFT PACK OFF. EMERGENCY DECLARED. RETURNED TO FIELD. AIRCRAFT WAS GROUNDED. MAINTENANCE REMOVED AND REPLACED COMPRESSOR OUTLET SENSOR IAW AMM 21-51-06, TEMPURATURE CONTROL VALVE IAW 21-51-12 AND RAM AIR INLET ACTUATOR IAW AMM 21-53-03. OPERATIONAL AND LEAK CHECKS NORMAL. SEE ALSO AALA20161216010 AND AALA20161216011.

Part: SENSOR — FAULTY (LT A/C PACK) · airframe 73,154 hrs · 11,716 cycles

DURING CRUISE RECIEVE A "L PACK TEMP" EICAS MESSAGE. ACCOMPLISHED QRH CHECKLIST AND TURNED LEFT PACK OFF. EMERGENCY DECLARED. RETURNED TO FIELD. AIRCRAFT WAS GROUNDED. MAINTENANCE REMOVED AND REPLACED COMPRESSOR OUTLET SENSOR IAW AMM 21-51-06, TEMPURATURE CONTROL VALVE IAW 21-51-12 AND RAM AIR INLET ACTUATOR IAW AMM 21-53-03. OPERATIONAL AND LEAK CHECKS NORMAL.

Part: VALVE — FAULTY (INLET) · airframe 73,154 hrs · 11,716 cycles

DURING CRUISE RECIEVE A "L PACK TEMP" EICAS MESSAGE. ACCOMPLISHED QRH CHECKLIST AND TURNED LEFT PACK OFF. EMERGENCY DECLARED. RETURNED TO FIELD. AIRCRAFT WAS GROUNDED. MAINTENANCE REMOVED AND REPLACED COMPRESSOR OUTLET SENSOR IAW AMM 21-51-06, TEMPURATURE CONTROL VALVE IAW 21-51-12 AND RAM AIR INLET ACTUATOR IAW AMM 21-53-03. OPERATIONAL AND LEAK CHECKS NORMAL. SEE ALSO AALA20161215034 AND AALA20161216011.

Part: WIRE — SHORTED (MICROPHONE) · airframe 71,637 hrs · 11,475 cycles

DURING CLIMB CREW REPORTED UNABLE TO TRANSMIT ON VHF NR 1, 2 OR LT SATCOM FROM CAPTAIN`S, FIRST OFFICER`S OR JUMPSSEAT COMMMUNICATION PANEL. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT GROUNDED. MAINTENANCE FOUND THE CAPTAIN"S MICROPHONE CORD SHORTED AT THE STRAIN RELIEF. REMOVED AND REPLACED MICROPHONE AND ACCOMPLISHED OPERATIONAL CHECK IAW AMM 23-51-00 AND 23-12-00. SYSTEM CHECK NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 70,723 hrs · 11,301 cycles

AIRCRAFT WAS NOT GNDED. FIRST CLASS FRONT LT CABIN EMER LIGHTS INOPERATIVE. R & R IAW AMM 33-51-00. SYS CHECKED NORMAL.

Part: RELAY — FAULTY (EVAC SLIDE) · airframe 70,416 hrs · 11,234 cycles

THE EMER EVACUATION SLIDES WOULDN`T PRESS TO TEST. ONE OF THE DISABLE SWITCHES FAULTED TRIGGERING THE ASSIST BOTTLE SQUIB & THE CONSEQUENT SUCCESSFUL LT OVERWING SLIDE DEPLOYMENT. R & R THE K3 & K5 RELAYS IAW SSM 25-65-01. SQUIB TEST PASSED IAW AMM 25-65-00. THE ACFT WAS GNDED.

Part: CHILLER — ODOR (GALLEY) · airframe 69,135 hrs · 10,991 cycles

STRONG ELEC BURNING ODOR IN CABIN ON DESCENT. HE ODOR DISAPPEARED WHEN THE UTILITY BUSSES WERE DISCONNECTED. THE AFT GALLEY RT CHILLER WAS MORE HOT THAN AFT LT CHILLER & THE AFT RT CHILLER CB KEPT POPPING OUT. R & R AFT GALLEY RT CHILLER IAW MM 25-33-02. OPS CHECKED NORMAL. THE ACFT WAS GROUNDED.

Part: PSEU — MALFUNCTIONED (LE SLAT) · airframe 69,049 hrs · 10,974 cycles

LEADING EDGE SLAT ASYMMETRY EICAS MSG & LE LIGHT ON. FLAPS STOPPED BETWEEN OPS 1 DEGREE. FLIGHT DECLARED AN EMER & RETURNED TO FIELD WITHOUT FURTHER INCIDENT. ACFT REMOVED FROM SERVICE. ACCOMPLISHED FIM 27-81-00-815-809, FAULT CODE 27-81021 NOTED. PSEU BITE FAULT CODE 5301 RT SLAT NR 1 NOTED. ACCOMPLISHED RESET ON FSEU & PSEU. NO FAULTS NOTED. OPERATIONAL CHECK OF LE SLAT SYS IAW AMM 27-81-00. OPERATIONAL CHECKED GOOD, NO FAULTS NOTED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,823 hrs · 10,928 cycles

CABIN FLOORBEAM AT STATION 347 IS CORRODED BETWEEN RBL 28 & RBL 54. REPAIRED FLOORBEAM IAW SRM REPAIR 53-00-51-2R-1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,823 hrs · 10,928 cycles

TOP OF FLOORBEAM AT STATION 325 & LBL 14 IS CORRODED. REPAIRED FLOORBEAM IAW SRM 53-00-51-2R-2.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,196 hrs · 10,668 cycles

SEAT MOUNTED EMER PATH LIGHT AT 5J INOPERATIVE. R & R LIGHT ASSEMBLY. SYS CHECKED NORMAL.

Part: MONITOR — FAULTY (HYDRAULIC SYS) · airframe 67,219 hrs · 10,673 cycles

AIR INTERRUPT, RETURNED & EMER DECLARED. LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING CLIMB RECEIVED EICAS MSG FOR LT HYD QTY READING .03. R & R HYD QTY MONITOR UNIT. PERFORMED OPERATIONAL CHECK IAW AMM 29-33-01. SYS CHECKED NORMAL.

Part: LENS — MISSING (CABIN) · airframe 66,796 hrs · 10,610 cycles

EMERGENCY PATH LIGHTING ILLUMINATOR MISSING CLEAR LENS FWD OF SEAT 2A. INSTALLED NEW LENS. PERFORMED OPERATIONAL CHECK. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 66,352 hrs · 10,544 cycles

EMERGENCY EGRESS FLOOD LIGHT AT BS 251 LT SIDE IS INOPERATIVE. RELAMPED IAW AMM 33-51-06. OPERATION CHECKED NORMAL.

Part: SHROUD — DEFECTIVE (CABIN) · airframe 66,291 hrs · 10,533 cycles

SEAT 28B EMER LIGHT SHROUD. REPLACED 28B EMER LIGHT SHROUD. OPERATIONS CHECKED GOOD.

Part: SHROUD — DEFECTIVE (CABIN) · airframe 66,291 hrs · 10,533 cycles

SEAT 29B EMER LIGHT SHROUD. REPLACED 29B EMER LIGHT SHROUD. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 65,477 hrs · 10,390 cycles

LEFT AFT WING SLIDE EMER LIGHT INOPERATIVE. REPLACED LAMP FOR LT AFT WING SLIDE EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: LENS — UNSECURE (CABIN) · airframe 65,477 hrs · 10,390 cycles

RIGHT NR 1 DOORWAY EMER LIGHT LENS HANGING DOWN. SECURED LENS FOR EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,477 hrs · 10,390 cycles

EMERGENCY LIGHT AT SEAT 39H INOPERATIVE. REPLACED LAMP FOR EMER LIGHT AT SEAT 39H. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 65,477 hrs · 10,390 cycles

INTERIOR RT AFT OVERWING EXIT SIGN INOPERATIVE. REPLACED LAMP FOR INTERIOR RT AFT OVERWING EXIT SIGN. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 65,477 hrs · 10,390 cycles

INTERIOR LT AFT OVERWING EXIT SIGN INOPERATIVE. REPLACED LAMP FOR INTERIOR LT AFT OVERWING EXIT SIGN. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 64,993 hrs · 10,317 cycles

RIGHT WING EXTERIOR ESCAPE PATH LIGHT CTR INOPERATIVE. REPLACED LAMP FOR RT WING EXTERIOR ESCAPE PATH LIGHT CTR. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,032 hrs · 10,174 cycles

EMERGENCY LIGHT AT CEILING PANEL ABOVE SEAT 4H INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT CEILING PANEL ABOVE SEAT 4H. OPERATIONS CHECKED NORMAL.

Part: SMOKE DETECTOR — INOPERATIVE (LAVATORY) · airframe 63,680 hrs · 10,126 cycles

CREW REPORTED LAVATORIES F1, M1 & A6 SMOKE DETECTORS HAD RANDOM FALSE WARNINGS DURING FLIGHT. FLIGHT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED F1, M1 & A6 LAVATORY SMOKE DETECTORS IAW AMM26-13-01. SYS GROUND CHECKED NORMAL.

Part: LIGHT — MISSING (CABIN) · airframe 63,604 hrs · 10,116 cycles

CABIN EMERGENCY LIGHT MISSING LAMP. REPLACED LAMP FOR CABIN EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.

Part: LIGHT — MISSING (CABIN) · airframe 62,683 hrs · 9,951 cycles

RT NR 2 DOOR EMERGENCY LIGHT ABOVE THE HANDLE FLOOD LIGHT ASSEMBLY MISSING. REPLACED LIGHT ASSEMBLY FOR RT NR 2 EMERGENCY LIGHT ABOVE THE HANDLE FLOOD FLIGHT. OPERATIONS CHECK NORMAL.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 61,943 hrs · 9,836 cycles

CABIN EMERGENCY LIGHT DIM. REPLACED FOR CABIN EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 59,375 hrs · 9,451 cycles

LEFT NUMBER 4 DOOR EXTERNAL EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY. OPS CHECK NORMAL.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 59,264 hrs · 9,429 cycles

FLIGHT ATTENDANT REPORTED M1 LAVATORY SMOKE DETECTOR CHIMED INTERMITTENTLY. REPLACED M1 LAVATORY SMOKE DETECTOR. OPS CHECK NORMAL.

Part: SKIN — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 58,364 hrs · 9,274 cycles

CORROSION FOUND ATOP HORIZONTAL STABILIZER AT RIGHT BUTTLINE 25.5 AND 13 INCHES BACK FROM LEADING EDGE. INSTALLED SKIN DOUBLER PER EA B767-55-026005.

Part: INTERCOSTAL — DAMAGED (RT PYLON) · airframe 58,364 hrs · 9,274 cycles

RIGHT PYLON NACELLE STRUT FRAME INBOARD CHORD AFT SIDE MID LOWER AREA HAS DEEP TOOLING MARK. REPLACED INTERCOSTAL PER SRM 51-4-0-02.

Part: COVER — MISSING (CABIN) · airframe 57,215 hrs · 9,098 cycles

SEAT 40B EMERGENCY LIGHT LENS COVER MISSING. REPLACED THE SEAT 40B EMERGENCY LIGHT LENS COVER. OPS CHECK NORMAL.

Part: FAN — OVERHEATED (E&E BAY) · airframe 56,402 hrs · 8,952 cycles

SNN - INFLIGHT CDG-DFW. CREW REPORTED ODOR IN AFT GALLEY AND AFT CABIN READING LIGHTS FLICKERING. EMERGENCY DECLARED FLIGHT DIVERTED SNN LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FORWARD EQUIPMENT COOLING EXHAUST FAN. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PLUG — LEAKING (SPOILER ACTUATOR) · airframe 55,614 hrs · 8,822 cycles

MIA - CREW REPORTED LOSS OF LEFT HYDRAULIC SYSTEM. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER 1 SPOILER ACTUATOR DRAIN PLUG THAT WAS LEAKING. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,309 hrs · 8,768 cycles

EMERGENCY LIGHT ON SEAT 10AB INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT ON SEAT 10AB. OPS CHECK NORMAL.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 51,982 hrs · 8,254 cycles

SMOKE ALARM FORWARD LAVATORY CAME ON. NO SMOKE DETECTED AND LAV WAS NOT OCCUPIED AT THE TIME. DEFERRED SMOKE/FIRE ALARM AT FWD LAV PER MEL 26-13 WITH AUTH NBR 02-433D-C. DISCONNECTED POWER CONNECTOR. REPLACED LAV F1 SMOKE DETECTOR. OPS CHECK NORMAL.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 51,944 hrs · 8,248 cycles

SMOKE DETECTOR IN FORWARD LAVATORY IS SOUNDING CONTINUOUSLY WITH NO SMOKE. CLEANED CONNECTOR AND REPLACED FORWARD LAVATORY SMOKE DETECTOR. OPS CHECK NORMAL.

Part: ROTARY ACTUATOR — INOPERATIVE (TE FLAP) · airframe 51,747 hrs · 8,216 cycles

AFW - INFLIGHT JFK-DFW. DURING FUNCTIONAL CHECK FLIGHT FOR TRAILING EDGE FLAP DISAGREE MESSAGE CONDITION, THE EICAS SYSTEM DISPLAYED FLAP DISAGREE MESSAGE AGAIN. EMERGENCY DECLARED FLIGHT DIVERTED AFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER 1 AND 8 FLAP ROTARY ACTUATORS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SWITCH — OUT OF ADJUST (TE FLAP) · airframe 51,490 hrs · 8,166 cycles

LHR - CREW REPORTED TRAILING EDGE FLAP DISAGREE INDICATION. EMERGENCY DECLARED LANDED LHR WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. ADJUSTED SWITCH M604. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,842 hrs · 7,738 cycles

EMERGENCY LIGHT AT LEFT AFT OVERWING INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT AFT OVERWING.

Part: O-RING — DEFECTIVE (APU) · airframe 48,354 hrs · 7,651 cycles

PHX - INFLIGHT SFO-MIA. CREW REPORTED AUXILIARY POWER UNIT OIL QUANTITY ON EICAS STATUS THEN APU FAULT. LEFT ENGINE GENERATOR ALREADY ON PLACARD. FLIGHT DIVERTED PHX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED O-RING ON BLANKING PLATE ON BOTTOM OF APU GEARBOX. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONTROL MODULE — INOPERATIVE (TE FLAP) · airframe 47,723 hrs · 7,539 cycles

LAX - TRAIL EDGE FLAP DISAGREE LIGHT ILLUMINATED WHEN FLAPS SELECTED FROM 1 DEGREE TO 5 DEGREES POSITION. EMERGENCY DECLARED, LANDED LAX WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND CONTROL MODULE M531 INOPERATIVE. REPLACED MODULE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,002 hrs · 7,249 cycles

FLOORBEAM CORRODED AT STATION 325 RIGHT BUTTLINE 36. REMOVED CORROSION AND INSTALLED PART REINFORCEMENT REPAIR STRAP UNDER ENGINEERING AUTHORIZATION 767-006777 AND SRM 51.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,002 hrs · 7,249 cycles

CORROSION AT STATION 347 FLOORBEAM. REPAIRED STRAP BETWEEN RIGHT BUTTLINE 29 AND RIGHT BUTTLINE 58 UNDER EA 006778. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BUSHING — MIGRATED (LT PYLON) · airframe 46,002 hrs · 7,249 cycles

LEFT PYLON STRUT HAS MIGRATING BUSHING ON THE INBOARD LUG OF THE LEFT PYLON FORWARD UPPER SPAR FITTING. REPAIRED PER ENGINEER AUTHORIZATION.

Part: RVDT — INOPERATIVE (TE FLAP) · airframe 44,381 hrs

SAN - AIRCRAFT HAD A FLAP DISAGREE INDICATION. EMERGENCY DECLARED, LANDED SAN WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED M603 FLAP HANDLE ROTARY VARIABLE DIFFERENTIAL TRANSDUCERS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

MIA - EXTERIOR EMERGENCY LIGHT AT FORWARD LEFT CARGO DOOR INOPERATIVE. REPLACED LAMP. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CYLINDER — FAILED (BRAKE SYSTEM) · airframe 43,972 hrs

GIG - HYDRAULIC LEAK ON NUMBER EIGHT BRAKE. FOUND ONE BRAKE CYLINDER FAILED CAUSING THE LEAK AND SMOKE AFTER LANDING AND CAUSING BRAKE TO OVERHEAT. REPLACED BRAKE AND WHEEL ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: RELAY — FAULTED (TE FLAPS) · airframe 43,782 hrs

MXP - TRAILING EDGE FLAP DISAGREE INDICATION WHEN FLAPS SELECTED TO 20. ALTERNATE METHOD TO SET FLAPS TO 20 FOR LANDING. LANDED WITHOUT INCIDENT. REPLACED RELAY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,314 hrs

SFO - EXTERNAL EMERGENCY LIGHT AT LEFT OVERWING EXIT INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY LIGHT AT LEFT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — BROKEN (EMERGENCY LIGHT)

MIA - SEAT MOUNTED EMERGENCY EXIT LIGHT AT SEAT ROW 5H INOPERATIVE. REPAIRED BROKEN WIRE FOR SEAT MOUNTED EMERGENCY EXIT LIGHT AT SEAT ROW 5H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRAP — BROKEN (FLASHLIGHT)

MIA - EMERGENCY FLASHLIGHT AT RIGHT MID GALLEY FLIGHT ATTENDANT SEAT HAS BROKEN STRAP. REPLACED STRAP FOR EMERGENCY FLASHLIGHT AT RIGHT MID GALLEY FLIGHT ATTENDANT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRAP — BROKEN (FLASHLIGHT)

MIA - EMERGENCY FLASHLIGHT BREAK STRAP SEAL AT RIGHT BUSINESS CLASS GALLEY BROKEN. REPLACED STRAP FOR EMERGENCY FLASHLIGHT BREAK STRAP SEAL AT RIGHT BUSINESS CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MODULE — INOPERATIVE (CABIN)

MIA - EMERGENCY LIGHTS AT SEATS 32H TO 40 INOPERATIVE. REPLACED MODULE M734 AND SEVERAL LAMPS FOR EMERGENCY LIGHTS AT SEATS 32H TO 40. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE HARNESS — INOPERATIVE (FIRE LOOP)

INFLIGHT T1486/21AUG IN CLIMB OUT LT ENGINE FIRE LOOP NR 2 ILLUMINATED INTERMITTENTLY. RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. REPLACED LT ENGINE FIRE LOOP NR 2 HARNESS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: WIRE HARNESS — DAMAGED (CABIN)

DFW - SEAT MOUNTED EMERGENCY LIGHTS AT SEAT 12H INOPERATIVE. REPAIRED BROKEN WIRE ON SEAT HARNESS FOR EMERGENCY LIGHT AT SEAT 12H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

JFK - LAST THREE LEFT AFT EMERGENCY OUTSIDE LIGHTS INOPERATIVE. RESET BATTERY PACK M738 FOR LAST THREE LEFT AFT EMERGENCY OUTSIDE LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BALLAST — INOPERATIVE (EMERGENCY LIGHT)

SFO - RIGHT AFT EMERGENCY EXIT SIDEWALL LIGHT INOPERATIVE. REPLACED BALLAST FOR RIGHT AFT EMERGENCY EXIT SIDEWALL LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — MISSING (CABIN)

LAX FLIGHT DECK DOOR EMERGENCY LIGHT ASSEMBLY MISSING. INSTALLED NEW FLIGHT DECK DOOR EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 37H INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, AFT SEAT MOUNTED EMERGENCY PATH LIGHTING AT SEAT 2H INOPERATIVE. REPLACED AFT SEAT MOUNTED EMERGENCY PATH LIGHTING ASSEMBLY AT SEAT 2H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: HARNESS — DAMAGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING AT SEAT 20C INOPERATIVE. REPLACED EMERGENCY EXIT PATH LIGHTING WIRE HARNESS AT SEAT 20C. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — NOT SEATED (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING SYSTEM AT 17B INOPERATIVE. RESEATED CONNECTOR UNDER SEAT 17B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE EMERGENCY ESCAPE PATH LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGHTS BATTERY PACK FOR FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: HARNESS — INOPERATIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT ON SEAT 31B INOPERATIVE. RECONNECTED HARNESS TO SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SENSOR — DIRTY (LT MLG)

RDU - FLT 2485 - AFTER TAKEOFF, EN ROUTE RDU-DFW, GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. CREW HAD TO DEPRESS THE LOCK OVERRIDE BUTTON TO RETRACT THE LANDING GEAR. RETURNED TO RDU AND LANDED WITHOUT INCIDENT. CLEANED LEFT MAIN LANDING GEAR TILT SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)