N381AN

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 101,198 hrs · 16,315 cycles

SEAT EMERGENCY LIGHTS WERE INOPERATIVE AT SEAT ROWS 32 HJ TO 41 HJ. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK, AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: FAN — CONTAMINATED (LAVATORY) · airframe 101,052 hrs · 16,279 cycles

AIRCRAFT WAS GROUNDED: SHORT TERM ACRID LIKE ODOR IN COCKPIT AND CABIN, DISSIPATED RAPIDLY. FLIGHT ATTENDANTS NOTICED SAME ODOR UPON GATE ARRIVAL. WHILE TROUBLESHOOTING, FOUND LAVATORY WASTE FLUID DRIPPING INTO LEFT HAND RECIRCULATION AIR FILTER AND LEFT HAND RECIRCULATION FAN. MAINTENANCE REPLACED RECIRCULATION FAN BECAUSE OF CONTAMINATION FROM LEAK, REPLACED PER MM 21-25-01 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 100,958 hrs · 16,258 cycles

LEFT FLIGHT ATTENDANT SEAT FLASHLIGHT WAS INOPERATIVE. REPLACED THE FLASHLIGHT BATTERY IAW AMM 25-60-00. OPS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 100,544 hrs · 16,172 cycles

FORWARD RT GALLEY, FLIGHT ATTENDANT SEAT FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE FLASHLIGHT BATTERY AND PERFORMED A SATISFACTORY OPERATIONAL CHECK IAW MM 25-64-00.

Part: WINDOW — DAMAGED (COCKPIT R2) · airframe 99,093 hrs · 15,881 cycles

R2 COCKPIT WINDOW. DAMAGED AREA THE SIZE OF A NICKEL IN GLASS WITH DARK STREAK EMANATING FROM BOTH SIDES. REMOVED AND REPLACED THE R2 WINDOW IAW AMM 56-11-02.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 98,615 hrs · 15,797 cycles

COCKPIT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE COCKPIT EMERGENCY LIGHT ASSEMBLY IAW MM 33-51-02 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 98,075 hrs · 15,708 cycles

EMERGENCY FLASHLIGHT AT THE FLIGHT ATTENDANT R2 SEAT IS INOPERATIVE. REPLACED THE FLASHLIGHT BATTERY IAW MM 25-60-00.

Part: FLASHLIGHT — MISSING (CABIN) · airframe 97,918 hrs · 15,678 cycles

AIRCRAFT WAS NOT GROUNDED. R2 JUMP SEAT FLASH LIGHT MISSING. REPLACED MISSING FLASH LIGHT.

Part: RELAY — NO TEST (OVERWING SLIDE) · airframe 97,672 hrs · 15,622 cycles

OVERWING ESCAPE SLIDE SYSTEM DOES NOT TEST. REMOVED AND REPLACED THE RELAY K3, RIGHT OVERWING ESCAPE SYSTEM AFT DOOR MODULE M1136 IAW WDM 25-65-12. OPERATIONAL CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 97,663 hrs · 15,621 cycles

EMERGENCY LIGHT LENS BY THE L1 DOOR, DETACHED. REMOVED AND REPLACED THE LIGHT ASSEMBLY IAW AMM 33-51-01. OPS CHECKED GOOD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 97,208 hrs · 15,541 cycles

AIRCRAFT IN BASE MAINTENANCE. MULTIPLE PATH EMERGENCY LIGHTS, INOPERATIVE. REPLACED BATTERY AND CHARGER (M732)AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK. (SEE AALA20170815001 FOR BATTERY).

Part: BATTERY — DISCHARGED (CABIN) · airframe 97,208 hrs · 15,541 cycles

AIRCRAFT IN BASE MAINTENANCE. MULTIPLE PATH EMERGENCY LIGHTS, INOPERATIVE. REPLACED BATTERY (M732)AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK. (SEE AALA201708169036 FOR CHARGER).

Part: CLAMP — DETERIORATED (ZONE 200) · airframe 97,205 hrs · 15,539 cycles

AIRCRAFT WAS NOT GROUNDED. DETERIORATED RIGHT HAND SLIDE DEPLOYMENT CABLE CLAMPS. REPLACED CLAMP PER AMM 25-65-04.

Part: ACTUATOR — DEPLOYED (LT SPOILER) · airframe 97,205 hrs · 15,539 cycles

AIRCRAFT WAS NOT GROUNDED. FOUND LEFT WING SPOILER OVERRIDE ACTUATOR DEPLOYED. REPLACED LEFT WING SPOILER OVERRIDE ACTUATOR PER AMM 25-65-20.

Part: ACTUATOR — CORRODED (ZONE 800) · airframe 97,205 hrs · 15,539 cycles

AIRCRAFT WAS GROUNDED. RIGHT OVERWING SLIDE DOOR RELEASE ACTUATOR REQUIRES REPLACEMENT. REPLACED SLIDE COMPARTMENT DOOR LATCH ACTUATOR PER MM 25-65-11.

Part: ACTUATOR — FAULTY (EVAC SLIDE) · airframe 97,205 hrs · 15,539 cycles

AIRCRAFT WAS NOT GROUNDED. RIGHT OVERWING SLIDE DOOR SNUBBER ACTUATORS, REQUIRE REPLACEMENT. REPLACED DOOR OPENING ACTUATORS PER AMM 25-65-10. (SEE ALSO 201708079011).

Part: ACTUATOR — FAULTY (EVAC SLIDE) · airframe 97,205 hrs · 15,539 cycles

AIRCRAFT WAS NOT GROUNDED. RIGHT OVERWING SLIDE DOOR SNUBBER ACTUATORS, REQUIRE REPLACEMENT. REPLACED AFT DOOR OPENING ACTUATOR PER AMM 25-65-10. (SEE ALSO 201708079010).

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 96,877 hrs · 15,471 cycles

SMOKE DETECTOR IN LAVATORY M2 EMITTED AN AURAL WARNING BRIEFLY. ACCOMPLISHED SMOKE DETECTOR TEST IAW AMM 26-13-00. OPERATIONAL CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 96,729 hrs · 15,445 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIDEWALL LIGHT AT SEAT 21J IS BURNT OUT. **SUPPLEMENTAL - 06/16/17 - RE-LAMPED SIDEWALL LIGHT IAW AMM 33-21-00. OPERATIONAL CHECK GOOD. (CLOSED)

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 96,713 hrs · 15,443 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT ON THE LEFT SIDE MID GALLEY WALL HAS A MISSING LENS. REPLACED LENS IAW AMM 33-15-05. OPERATIONAL CHECKED GOOD.

Part: LIGHT — CRACKED (SEAT 5A) · airframe 96,558 hrs · 15,407 cycles

DIM AND CRACKED EMERGENCY LIGHT ASSEMBLY AT SEAT 5A. REPLACED SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY IAW AMM 33-60-98. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK. THE AIRCRAFT WAS GROUNDED.

Part: LENS — LOOSE (EXIT SIGN) · airframe 96,384 hrs · 15,376 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGN BY FLOOR NEAR R4 DOOR HAS A LOOSE LENS COVER. REMOVED AND REPLACED LENS COVER IAW AMM 33-51-01. OPERATIONAL CHECK GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 96,346 hrs · 15,372 cycles

SEAT MOUNTED EMERGENCY LIGHT ON SEAT 7J SIDE PANEL HAS DAMAGED WIRES. REMOVED AND REPLACED THE LIGHT ASSEMBLY IAW AMM 33-51-10. OPS CHECKED GOOD.

Part: LENS — MISSING (CABIN) · airframe 96,345 hrs · 15,372 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT LEFT SIDE OF GALLEY BETWEEN ROWS 13 AND 17 HAS A MISSING LENS COVER. INSTALLED LENS COVER IAW AMM 33-51-09. OPERATIONAL CHECK GOOD.

Part: PUMP — FAULTY (FUEL OVERIDE) · airframe 96,328 hrs · 15,369 cycles

LEFT CENTER TANK FUEL PUMP EICAS MESSAGE. TURNED OFF PUMP PER PROCEDURES. REMOVED AND REPLACED FUEL OVERRIDE PUMP IAW AMM 28-22-05. OPS CHECKED GOOD.

Part: UFI — MALFUNCTIONED (FUEL SYSTEM) · airframe 96,057 hrs · 15,330 cycles

AIRCRAFT WAS NOT GROUNDED. LEFT CENTER FUEL PUMP IS INOPERATIVE. LIGHT ILLUMINATED WITH EICAS MESSAGE. TURNED OFF PUMP FOR TAKEOFF. ACCOMPLISHED FIM 28-22-99 WITH NO FAULTS FOUND. ACCOMPLISHED RESET OF THE UNIVERSAL FAULT INTERRUPTER. OPERATIONAL CHECK GOOD. (CLOSED)

Part: BATTERY — FAULTY (FLASHLIGHT) · airframe 95,933 hrs · 15,305 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT R1 JUMPSEAT WILL NOT TURN OFF. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW ECO C3324AA. OPERATIONAL CHECK GOOD.

Part: LIGHT — BROKEN (SEAT 7J) · airframe 95,734 hrs · 15,268 cycles

SEAT MOUNTED EMERGENCY LIGHT AT SEAT 7J IS BROKEN. REPLACED THE LIGHT ASSEMBLY IAW AMM 33-51-00. OPS CHECKED GOOD.

Part: MODULE — FAULTY (STAB TRIM) · airframe 95,547 hrs · 15,235 cycles

STABILIZER TRIM INDICATION. EMERGENCY DECLARED, RETURNED TO DEPARTURE, AND THE AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED STABILIZER TRIM CONTROL MODULE IAW AMM 27-09-00. OPS CHECKED GOOD.

Part: O-RING — CUT (HYD SYSTEM) · airframe 95,518 hrs · 15,224 cycles

DURING FLIGHT HYDRAULIC SYSTEM A FLUID QUANTITY LOSS WAS OBSERVED. AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. MAINTENANCE FOUND A CUT O-RING UNDER THE A SYSTEM ALTERNATION CURRENT MOTOR PUMP PRESSURE AND CASE DRAIN FILTER MODULE DIFFERENTIAL PRESSURE INDICATOR PLUG. REMOVED AND REPLACED O-RING IAW AMM 20-10-19. LEAK AND OPERATIONAL CHECK NORMAL.

Part: HOUSING — RECESSED (EMERGENCY LIGHT) · airframe 95,310 hrs · 15,183 cycles

EMERGENCY EXIT SIGN AT THE L1 DOOR IS UNSECURE DUE TO HOUSING RECESSED. SECURED EXIT SIGN IAW AMM 33-51-01. OPERATIONAL CHECK GOOD.

Part: LENS — DETACHED (EXIT SIGN) · airframe 95,227 hrs · 15,168 cycles

AIRCRAFT NOT GROUNDED. EMERGENCY EXIT SIGN AT L1 DOOR HAS A DETACHED LENS COVER. SECURED LENS COVER. OPERATIONAL CHECK GOOD.

Part: ENGINE — LEAKING (NR 1) · airframe 92,871 hrs · 14,775 cycles

DURING CRUISE, THE NR 1 ENGINE OIL QTY DECREASED. BORESCOPE OF THE COMPRESSOR REAR FRAME INDICATED COKING BUT WAS UNABLE TO CONFIRM SOURCE. THE AIRCRAFT WAS GROUNDED.

Part: IDG — FAILED (NR 1 ENGINE) · airframe 92,199 hrs · 14,652 cycles

LEFT GEN FAILED 55 MINUTES AFTER TAKEOFF. DEFINITE JOLT FELT. ATTEMPTED ONE RESET WITH SAME INTENSITY JOLT FELT. GEN DID NOT RESET. AN EMER WAS DECLARED & THE FLIGHT RETURNED WITHOUT FURTHER INCIDENT. R & R NR 1 IDG IAW AMM 24-11-01. OPERATIONAL & LEAK CHECKED OK. THE ACFT WAS GNDED.

Part: LENS — DETACHED (EXIT SIGN) · airframe 92,146 hrs · 14,639 cycles

EXIT SIGN BY 42C HAS FALLEN OFF. FOUND EXIT SIGN LENS IN AFT GALLEY & INSTALLED AT AREA 42C AS REQUIRED. OPERATIONS CHECKED EMER LIGHTS OK IAW AMM 33-51-00, OK FOR SERVICE. THE ACFT WAS NOT GNDED.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,978 hrs · 14,604 cycles

AIRCRAFT WAS IN BASE MX. BELL FRAME AT FS 762 IS CORRODED, BETWEEN STRINGER 36L & 39L. REPAIRED FRAME IAW SRM 53-00-07.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 91,978 hrs · 14,604 cycles

AIRCRAFT WAS IN BASE MX. CABIN FLOOR INTERCOSTAL UPPER ANGLE IS CRACKED, BETWEEN FS 1197.22 & 1197.44 AT LBL 42. R & R ANGLE IAW SRM 63-60-51, AARD 51-00-05 & DWG 146T5400.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 91,978 hrs · 14,604 cycles

AIRCRAFT WAS IN BASE MX. CABIN FLOOR INTERCOSTAL UPPER ANGLE, BETWEEN FS 1241 & 1263 AT LBL 36 IS CRACKED. R & R ANGLE IAW SRM 63-60-51, AARD 51-00-05 & DWG 146T5400.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,978 hrs · 14,604 cycles

AIRCRAFT WAS IN BASE MX. UPPER CHORD OF CABIN FLOORBEAM AT FS 764, IS CORRODED AT RBL 26. REPAIRED FLOORBEAM IAW SRM 53-00-51-2R-1 & EA 257609.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,978 hrs · 14,604 cycles

AIRCRAFT WAS IN BASE MX. CABIN SEAT TRACK NR 8 IS CORRODED, BETWEEN FS 390 & 397. R & R SEAT TRACK SECTION IAW AARD 51-00-05 & DWG 141T5121.

Part: SKIN — CORRODED (FUEL TANK) · corrosion level 2 · airframe 91,978 hrs · 14,604 cycles

AIRCRAFT WAS IN BASE MX. CORROSION ON UPPER SURFACE OF CTR FUEL TANK, UPPER SKIN AT FS 955 & BL 0. REPAIRED SKIN IAW SRM 51-10-02 & EA 257525 DATED 01 29 2016.

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 91,729 hrs · 14,560 cycles

EMERGENCY LIGHTING ON LT AFT ENTRY DOOR EXIT SIGNS UPPER & LOWER IS INOPERATIVE. AIRCRAFT WAS GROUNDED. R & R CHARGER ASSEMBLY M1210 IAW AMM 33-51-07. SYS CHECKED NORMAL.

Part: LIGHT — SHORTED (CABIN) · airframe 91,729 hrs · 14,560 cycles

EMERGENCY LIGHTING ON SEATS 25 - 31 LT SIDE ARE INOPERATIVE. AIRCRAFT WAS GROUNDED. FOUND LIGHT ASSEMBLY SHORTED AT 25B. R & R LIGHT ASSEMBLY IAW AMM 33-51-10 & PERFORMED OPERATIONAL CHECK. SYS CHECKED NORMAL.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 91,729 hrs · 14,560 cycles

EMERGENCY LIGHTING ON RT & LT AFT ENTRY DOOR EXIT SIGNS UPPER & LOWER IS INOPERATIVE. AIRCRAFT WAS GROUNDED. R & R CHARGER & BATTERY ASSEMBLIES M1210 IAW AMM 33-51-07. SYS CHECKED NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 91,714 hrs · 14,554 cycles

EMERGENCY LIGHTS FROM ROW 25AB - 31AB INOPERATIVE. REPLACED BATTERY & CHARGER BPS7-3 AT ROW 25AB IAW AMM 33-51-07. OPERATIONS NORMAL, THE ACFT WAS GNDED.

Part: ENGINE — LEAKING (RIGHT) · airframe 91,570 hrs · 14,529 cycles

DURING FLIGHT, RT ENG LOST 10 QUARTS OF OIL IN 5.5 HRS. FLIGHT DIVERTED & LANDED WITHOUT FURTHER INCIDENT. ACFT WAS REMOVED FROM SERVICE. TROUBLE SHOT SYS & FOUND TUBE B SCAVENGE LEAKING THRU GASKET IAW IPC IAW 79-21-00-01 DETAIL N ITEM 112. REPLACED GASKET. ENG STILL LEAKS OIL. FERRIED ACFT. R & R RT ENG IAW 719301 WC.

Part: SELECTOR PANEL — FAILED (COCKPIT) · airframe 91,021 hrs · 14,436 cycles

AFTER ROTATION ON TAKEOFF, EICAS MSG CABIN AUTO INOPERATIVE. TROUBLE SHOT IAW FIM 21-31-00-815-803, FOUND NR 1 CONTROLLER FAILING THE SELECTOR. REPLACED CABIN PRESS SELECTOR PANEL IAW AMM 21-31-01. OPERATIONALLY CHECKED NORMAL.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 91,021 hrs · 14,436 cycles

AFTER ROTATION ON TAKEOFF, EICAS MSG CABIN AUTO INOPERATIVE. TROUBLE SHOT IAW FIM 21-31-00-815-803, FOUND NR 2 CONTROLLER FAILING ITSELF. REPLACED NR 2 AUTO PRESS CONTROLLER IAW 21-31-02 AMM. SYS OPERATIONS NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 90,211 hrs · 14,312 cycles

R1 EXTERIOR EMER LIGHT & OVERWING OPERATE FOR ONLY 4 SECONDS ON AIRPLANE EXTERIOR. R & R M731 EMER BATTERY & CHARGER. PERFORMED OPERATIONAL CHECK IAW AMM 33-50-00. SYSTEM CHECKED NORMAL.

Part: BATTERY — WEAK (CABIN) · airframe 90,211 hrs · 14,312 cycles

R1 DOOR EXIT EMER LIGHT & OVERWING LIGHTS OPERATE FOR ONLY 4 SECONDS ON AIRPLANE EXTERIOR. R & R M731 EMER BATTERY & CHARGER. PERFORMED OPERATIONAL CHECK IAW AMM 33-50-00. SYS CHECKED NORMAL.

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 90,143 hrs · 14,301 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CRUISE BOTH PRESS CONTROLLERS INOPERATIVE IN AUTO MODE. R & R PRESS OUTFLOW VLV IAW AMM 21-31-03. PERFORMED OPERATIONAL CHECK. SYS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 89,952 hrs · 14,268 cycles

BATTERY PACK M1209 FOR THE OVERWING EXIT LIGHTS IS INOPERATIVE. REMOVED, REPLACED & PERFORMED GOOD OPERATIONAL TEST OF BATTERY PACK M1209 FOR THE OVERWING EXIT LIGHTS IAW AMM 33-51-07.

Part: SLAT SYSTEM — MALFUNCTIONED (WINGS) · airframe 89,774 hrs · 14,244 cycles

DURING FLAP RETRACTION RECEIVED EICAS, LE FLAP DISAGREE, MESSAGE. EMERGENCY DECLARED, LANDING UNEVENTFUL. INTERROGATED FLAP & SLAT ELEC UNIT WITH NO LAST LEG FAULTS SHOWN. FLAPS & SLAT CYCLED FULL RANGE SEVERAL TIMES WITH ALL INDICATIONS NORMAL IAW AMM 27-51-00-862-056 & 27-51-01-404-130 PARA 22. SYS CHECKED NORMAL.

Part: LIGHT — MISSING (EXIT SIGN) · airframe 88,223 hrs · 13,985 cycles

LEFT NR 1 DOOR EMER EXIT SIGN, ABOVE INSIDE DOOR HANDLE, THREE LIGHTS MISSING. REPLACED EMER EXIT SIGN. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 88,136 hrs · 13,975 cycles

LEFT SIDE WING TO BODY FAIRING EMER LIGHT INOPERATIVE. REPLACED LAMP HOLDER ASSEMBLY. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 87,898 hrs · 13,930 cycles

COCKPIT EMER LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR COCKPIT EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: GROUND WIRE — BROKEN (CABIN) · airframe 87,898 hrs · 13,930 cycles

LEFT NR 1 DOOR THRESHOLD EMER LIGHT GND WIRE BROKEN OFF. REPAIRED BROKEN GND WIRE AT LT NR 1 THRESHOLD LIGHT ASSEMBLY. OPERATIONS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 87,809 hrs · 13,915 cycles

EMERGENCY LIGHTS FROM SEATS 20AB TO 24AB FAILED TEST. REPLACED BATTERY & CHARGER. OPERATIONS CHECKED NORMAL.

Part: WIRE — LOOSE (CABIN) · airframe 87,809 hrs · 13,915 cycles

EMERGENCY PATH LIGHT ON SEAT 30H INOPERATIVE. FOUND WIRES PULLED LOOSE. RECONNECTED CONNECTOR FOR EMER PATH LIGHT AT SEAT 30H. OPERATIONS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 87,809 hrs · 13,915 cycles

OVERHEAD LT EMER LIGHTS FROM ROWS 20 TO 34 INOPERATIVE. REPLACED BATTERY & CHARGER. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 87,809 hrs · 13,915 cycles

AFT OVERHEAD EMER LIGHT NEXT TO A5 LAVATORY INOPERATIVE. REPLACED LAMP FOR AFT OVERHEAD EMER LIGHT NEXT TO A5 LAVATORY. OPERATIONS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 87,809 hrs · 13,915 cycles

LEFT OVERHEAD EMER LIGHT AT SEAT 13AB INOPERATIVE. REPLACED BATTERY & CHARGER. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 85,570 hrs · 13,580 cycles

RT NR DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RT NR 2 DOOR EXTERIOR EMERGENCY LIGHT, OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 85,161 hrs · 13,507 cycles

RT NR 2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RT NR 2 DOOR EXTERIOR EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 85,161 hrs · 13,507 cycles

SEAT MOUNTED EMERGENCY LIGHT AT 17AB INOPERATIVE. SECURED LOOSE CONNECTOR UNDER SEAT 17AB. OPERATIONS CHECKED NORMAL.

Part: LENS — MISSING (CABIN) · airframe 84,264 hrs · 13,368 cycles

MID GALLEY AISLE LOWER EMERGENCY EXIT MARKER SIGN LENS COVER MISSING. REPLACED LENS COVER FOR MID GALLEY AISLE LOWER EMERGENCY EXIT MARKER SIGN. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 84,264 hrs · 13,368 cycles

BULKHEAD MOUNTED EMERGENCY EXIT LIGHT FORWARD OF SEAT 20G INOPERATIVE. REPLACED LAMP FOR BULKHEAD MOUNTED EMERGENCYC EXIT LIGHT FORWARD OF SET 20G. OPS CHECK NORMAL

Part: LIGHT — INOPERATIVE (CABIN) · airframe 82,702 hrs · 13,121 cycles

SEAT 23B, EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT 23B EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 82,702 hrs · 13,121 cycles

SEAT 34H, EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT 34H EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 81,681 hrs · 12,956 cycles

CEILING EMERGENCY LIGHT ABOVE SEAT 40B INOPERATIVE. REPLACED LAMP FOR CEILING EMERGENCY LIGHT ABOVE SEAT 40B. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 81,681 hrs · 12,956 cycles

EMERGENCY EXIT SIGNS AT DOORS LEFT AND RIGHT NUMBER 1 INOPERATIVE. REPLACED LEFT NUMBER 1 BATTERY PACK BENEATH FLIGHT ATTENDANT SEAT. OPS CHECK NORMAL.

Part: LENS — MISSING (CABIN) · airframe 81,681 hrs · 12,956 cycles

EMERGENCY LIGHT ON SEAT 40H MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 40H. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 81,681 hrs · 12,956 cycles

LOWER POSITION OF LEFT NUMBER 2 DOOR AFT EMERGENCY EXIT SIGN INOPERATIVE. REPLACED LAMP FOR LOWER POSITION OF LEFT NUMBER 2 DOOR AFT EMERGENCY EXIT SIGN. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 81,681 hrs · 12,956 cycles

LEFT NUMBER 1 DOOR LOWER PORTION OF UPPER EMERGENCY EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK FOR LEFT NUMBER 1 DOOR. OPS CHECK NORMAL.

Part: SELECTOR VALVE — LEAKING (BRAKE SYSTEM) · airframe 81,681 hrs · 12,956 cycles

MSP INFLIGHT SFO-JFK. CREW REPORTED CENTER HYDRAULIC SYSTEM QUANTITY LOSS. EMERGENCY DECLARED FIGHT DIVERTED MSP LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEAKING ALTERNATE BRAKE SELECTOR VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: COFFEEMAKER — MALFUNCTIONED (GALLEY) · airframe 78,312 hrs · 12,425 cycles

CREW REPORTED SMELL OF BURNING FROM COFFEE MAKER 7. CREW DEACTIVATED COFFEE MAKER BY PULLING CIRCUIT BREAKER. ODOR CLEARED. INSPECTED AREA BEHIND COFFEE MAKER. NO EVIDENCE OF BURNING OR ARCING. DEFERRED COFFEE MAKER 7 PER NEF 25-32A AUTH 4-1312NEF-C.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 77,580 hrs · 12,310 cycles

R2 DOOR EXIT EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY M733. OPS CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 77,580 hrs · 12,310 cycles

RIGHT FUSELAGE EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY M733. OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,663 hrs · 12,173 cycles

SEAT 14 HJ EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT 14 HJ EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,663 hrs · 12,173 cycles

EMERGENCY LIGHT AT SEAT 6AB INOPERATIVE. REPLACED LAMP FOR SEAT 6AB EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 76,663 hrs · 12,173 cycles

EMERGENCY LIGHT AT SEAT 12HJ INOPERATIVE. RE-SECURED PLUG FOR LIGHT ASSEMBLY AT SEAT 12HJ EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: BATTERY PACK — MALFUNCTIONED (CABIN) · airframe 76,663 hrs · 12,173 cycles

EMERGECNY LIGHTS AT LEFT NUMBER 1 DOOR BOTH SIGNS DO NOT TEST. RESET BATTERY PACK & CHARGER. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,663 hrs · 12,173 cycles

EMERGENCY LIGHT ABOVE SEAT 4AB INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT ABOVE SEAT 4AB. OPS CHECK NORMAL.

Part: IDG — FAILED (RT ENGINE) · airframe 76,471 hrs · 12,148 cycles

GYE - INFLIGHT SCL-MIA. CREW REPORTED ACCT RIGHT ENGINE GENERATOR INOPERATIVE WITH AUXILIARY POWER UNIT ON MEL. EMERGENCY DECLARED FLIGHT DIVERTED GYE LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT INTEGRATED DRIVE GENERATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: STRAP — DAMAGED (FUSELAGE) · airframe 76,252 hrs · 12,117 cycles

FLOORBEAM STABILIZATION STRAP AT RIGHT BUTTLINE 39 AND JUST FORWARD OF STATION 347 WAS FOUND SEVERED ALONG THE EDGE OF FLOORBEAM LOWER CHORD. REPLACED STRAP PER EA B767-53-019870.

Part: VIDEO MONITOR — MALFUNCTIONED (CABIN) · airframe 75,788 hrs · 12,054 cycles

LHR - INFLIGHT ZRH-JFK. CREW REPORTED 10H VIDEO MONITOR BILLOWING BLUE SMOKE AND EXTREMELY HOT. EMERGENCY DECLARED FLIGHT DIVERTED LHR LANDED WITHOUT INCIDENT. CONFIRMED BULKHEAD MONITOR AT 10HJ AS SOURCE OF FUMES. MONITOR DEFERRED INOPERATIVE PER NEF 23-33C AUTH NBR 9-118NEF-C. REPLACED MONITOR AT 10H AT JFK ON 09/03/2011. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 73,769 hrs · 11,747 cycles

DFW - INFLIGHT MIA-LAX. CREW REPORTED FIRST OFFICERS WINDSHIELD CRACKED IN FLIGHT WITH WINDOW HEAT ON. FLIGHT DIVERTED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT FORWARD WINDSHIELD. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SENSOR — OUT OF LIMITS (LE SLAT) · airframe 73,420 hrs · 11,692 cycles

DFW - AFTER CLIMBOUT CREW ATTEMPTED TO RETRACT FLAPS TO ZERO, FLAP INDICATOR NEEDLES FOR LEFT AND RIGHT FLAPS STUCK BETWEEN 0 AND ONE, WITH A SLAT ASSEMBLY. LIGHT AND SLAT ASSYMETRY EICAS MESSAGE. CREW ATTEMPTED TO LOWER FLAPS TO 20 FOR LANDING WITH NO INDICATION OR CHANGE INFLIGHT CHARACTERISTICS. EMERGENCY DECLARED, FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT LANDED WITH NO FLAPS. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEADING EDGE SLAT SENSOR 303 AT THE NUMBER 9 RIGHT SLAT. SYSTEM GROUND CHECK NORMAL OEPRATION.

Part: LENS — MISSING (CABIN) · airframe 72,297 hrs · 11,499 cycles

EMERGENCY LIGHT LEFT SIDE OF MID GALLEY MISSING LENS. REPLACED EMERGENCY LIGHT ASSEMBLY LEFT SIDE MID GALLEY. OPS CHECKS NORMAL.

Part: IDG — FAULTY (LEFT) · airframe 72,004 hrs · 11,445 cycles

GIG - CAPTAIN REPORTED FLAP INDICATION FAULT DURING FLIGHT. EMERGENCY DECLARED RETURNED GIG LANDED WITHOUT INCIDENT. FOUND LEFT INTEGRATED DRIVE GENERATOR PHASE LEAD BURNT T2 AND T3. REPLACED LEFT ENGINE INTEGRATED DRIVE GENERATOR AND BUS POWER CONTROL UNIT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: IDG — FAULTY (LT ENGINE) · airframe 72,004 hrs · 11,445 cycles

GIG - CAPTAIN REPORTED FLAP INDICATOR WOULD INTERMITTENTLY INDICATE FLAPS ONE WITH SERVO SOUNDS COMING FROM THROTTLE QUADRANT. EMERGENCY DECLARED FLIGHT RETURNED GIG LANDED WITHOUT INCIDENT. INSPECTED AND FOUND LEFT ENGINE INTEGRATED DRIVE GENERATOR PHASELEADS T2 AND T3 BURNT. REPLACED LEFT INTEGRATED DRIVE GENERATOR AND BUS POWER CONTROL UNIT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,534 hrs · 11,170 cycles

CORROSION ON FUSELAGE SKIN INNER SURFACE BETWEEN STATIONS 1080 AND 1085 AND STRINGER 38 LEFT CENTERED AT LEFT BUTTLINE 15. ACCOMPLISHED REPAIR PER EA 010233.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 70,534 hrs · 11,170 cycles

TOP LEFT AFT FASTENER TWO HOLES SHOW CRACK INDICATIONS. REAM HOLE TO TRANSITION FIT PER 767-300 SRM 51-40-0G. INSTALLED A OVERSIZE FASTENER PER EA B767-53-010232.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 70,534 hrs · 11,170 cycles

LEFT STATION 1809.5 OUTER CHORD HFEC OPEN-HOLE FASTENER INSPECTION, FOUND CRACK INDICATIONS ON THE AFT TWO HOLES. ACCOMPLISHED BORE/FASTENER REWORK PER EA 010232.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,368 hrs · 10,962 cycles

EMERGENCY LIGHT AT SEAT 25B INOPERATIVE. REPLACED LAMP.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,368 hrs · 10,962 cycles

EMERGENCY LIGHT AT LEFT AND RIGHT NUMBER ONE DOORS INOPERATIVE. REPLACED BATTERY PACK M1208.

Part: SHUTOFF VALVE — LEAKING (RT MLG WW) · airframe 68,526 hrs · 10,818 cycles

MIA - CENTRAL HYDRAULIC QUANTITY EICAS MESSAGE DURING CRUISE WITH STATUS MESSAGE "RF" ON CENTER HYDRAULIC QUANTITY. COMPLETED QRH PROCEDURE OF DEPRESSURINZING CENTER HYDRAULIC SYSTEM AT CRUISE. ALTERNATE GEAR EXTENSION PROCEDURAL STEP: GEAR HANDLE DOWN CAUSED LOSS OF CENTER HYDRAULIC SYSTEM. COMPLIED QRH PROCEDURE LANDED FLAPS 10 DEGREES. FOUND HYDRAULIC LEAK AROUND FLAP SLAT HYDRAULIC SHUTOFF VALVE IN RIGHT WHEEL WELL AFT WALL. REPLACED FLAP/SLAT MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SOCKET — INOPERATIVE (CABIN) · airframe 68,277 hrs · 10,779 cycles

FORWARD SEAT 20H RIGHT NEAR CLOSET EMERGENCY LIGHT INOPERATIVE. REPLACED CONNECTION SOCKET AND REPLACED LAMP.

Part: TRANSCEIVER — INOPERATIVE (WX RADAR SYS) · airframe 67,896 hrs · 10,716 cycles

GIG - AIRCRAFT'S WEATHER RADAR FAILED INFLIGHT. RETURNED GIG WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED WEATHER RADAR TRANSCEIVER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LINE — LEAKING (ANTI ICE SYS) · airframe 67,326 hrs · 10,613 cycles

INFLIGHT RDU-LHR. NO ANTI-ICE ON LT ENGINE GOING INTO ICY CONDITIONS. EMERGENCY DECLARED LANDED JFK WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND PRV MUSCLE LINE LEAKING. RESEATED TIGHTENED LINE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: TRANSCEIVER — FAILED (WX RADAR SYS) · airframe 66,065 hrs

GIG INFLIGHT. CREW REPORTED WEATHER RADAR WENT INOPERATIVE DURING FLIGHT. RETURNED TO GIG AND LANDED WITHOUT INCIDENT. REPLACED WEATHER RADAR TRANSCEIVER. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: LAMP — MISSING (EMERGENCY LIGHT) · airframe 65,840 hrs

JFK - EMERGENCY LIGHT AT SEAT 23B MISSING LAMP. REPLACED LAMP AT SEAT 23B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

JFK - EMERGENCY LIGHT EXIT SIGNS AT LT AND RT OVERWING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT EXIT SIGNS AT LT AND RT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: PSEU — FAULTY (L/E SLAT) · airframe 63,840 hrs

MIA INFLIGHT T381/04MAY - CREW REPORTED ALERT TWO LEADING EDGE ASYMMETRY MESSAGE. LANDED MIA WITHOUT INCIDENT. FOUND NUMBER FIVE SLAT INBOARD PROXIMITY SWITCH ELECTRONIC UNIT FAULTING. REPLACED PROXIMITY SWITCH ELECTRONIC UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FSEU — MALFUNCTIONED (E&E BAY) · airframe 63,673 hrs

CDG INFLIGHT T44/19APR - CREW REPORTED LEADING EDGE SLAT ASSEMBLY EICAS MESSAGE AND LEADING EDGE CAUTION LIGHT WHEN MOVING FLAP HANDLE TO 1 AT 205 KNOTS. COULD NOT LOWER FLAPS NORMALLY. DECLARED EMERGENCY AND LANDED CDG WITHOUT INCIDENT. RESET FLAP SLAT ELECTRONIC UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SIGN — BROKEN (EMERGENCY LIGHTS)

MIA - BI DIRECTIONAL EMERGENCY EXIT IDENTIFIER FORWARD OF SEAT 20G IS BROKEN. REPLACED BI DIRECTIONAL EMERGENCY EXIT SIGN ASSEMBLY FORWARD OF SEAT 20G. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — LOOSE (EMERGENCY LIGHTS)

ORD - EMERGENCY LIGHTS AT SEAT ROWS 31H TO 36H INOPERATIVE. SECURED WIRE CONNECTION AT SEAT ROW 32H FOR INOPERATIVE EMERGENCY LIGHTS AT SEAT ROWS 31H TO 36H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHTS AT SEAT ROW 22H INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT ROW 22H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT 32H INOPERATIVE. RELAMPED EMERGENCY PATH LIGHT AT SEAT 32H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SIGN — WORN (CABIN)

DFW - EMERGENCY EXIT LIGHT IDENTIFIER AT LEFT NUMBER FOUR DOOR WORN. REPLACED EMERGENCY EXIT LIGHT IDENTIFIER AT LEFT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

JFK - EXTERIOR EMERGENCY LIGHTS IN FOURTH POSITION LEFT SIDE INOPERATIVE. REPLACED LIGHT ASSEMBLY AT NUMBER FOUR POSITION LEFT HAND SIDE FOR EXTERIOR EMERGENCY LIGHTS IN FOURTH POSITION LEFT HAND SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: GIRT BAR — NOT SEATED (L1 DOOR)

SFO - THE LEFT ONE DOOR SLIDE GIRT BAR IS NOT INSTALLED IN THE GIRT BAR RECEIVER. INSTALLED GIRT BAR IN THE GIRT BAR RECEIVER FOR LEFT ONE DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (COCKPIT)

DFW - EMERGENCY LIGHT OVER COCKPIT DOOR INOPERATIVE. REPLACED EMERGENCY LIGHT OVER COCKPIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS)

EMERGENCY LIGHTS AT SEAT ROWS 22 TO 24 RT HAND SIDE INOPERATIVE. REPLACED BATTERY PACK FOR SEAT ROWS 22 TO 24 RT HAND SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SENSOR — INOPERATIVE (SLATS)

HNL - INFLIGHT T270/12 ON INITIAL CLIMBOUT BEFORE FLAP HANDLE MOVED LEADING EDGE FLAP ASYMMETRY LIGHT CAME ON. RETURNED TO HNL AND LANDED WITHOUT INCIDENT. DUPLICATED FAULT WITH SLATS. FOUND FAULT ASSOCIATED WITH NUMBER SIX SLAT SENSOR. REPLACED SENSOR SWITCH FOR NUMBER 6 INBOARD SLAT LEFT WING SENSOR NUMBER 281. REPLACED PROXIMITY SWITCH ELECTRONICS UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PSEU — INOPERATIVE (WING SLAT)

HNL INFLIGHT T296/11 LEADING EDGE SLAT ASYMMETRY WITH FLAP INDICATION BETWEEN ONE AND UP. RETURNED TO HNL AND LANDED OVERWEIGHT WITHOUT INCIDENT. OVERWEIGHT INSPECTION ACCOMPLISHED IAW WORK CARD 05 96 11 WITH NO DISCREPANCIES FOUND. REPLACED FSEU AND PSEU. BITE CHECKED IAW AMM 32 09 04 4. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) NOTE: EXTENDED RANGE EVENT REPORT 1491.

Part: FLOORBEAM — CORRODED (FUSELAGE)

AFW - FLOORBEAM AT STATION 325 (G1 GALLEY AREA) HAS CORROSION REMOVAL ON UPPER AND LOWER SURFACES. MATERIAL REMAINING IS BEYOND SRM LIMITS. AREA IS 1 INCH BY 1 INCH AND DEPTH IS 0.23 INCH. REMOVED CORROSION AND VERIFIED. FABRICATED REPAIR STRAP, ALODINED ALL BARE ALUMINUM SURFACES AND FINISHED BLENDS AND REPAIR STRAP WITH PRIMER. FILLED BLENDS WITH BMS595 SEALANT AND INSTALLED REPAIR STRAP WITH SEALANT PROSEAL 870 AND FASTENERS.

Part: FLOORBEAM — CORRODED (FUSELAGE)

AFW - FLOORBEAM AT STATION 347 AT G1 GALLEY AREA HAS CORROSION REMOVAL ON UPPER AND LOWER SURFACES. MATERIAL REMAINING IS BEYOND SRM LIMITS. AREA IS 2 INCH BY 1 INCH AND A DEPTH OF 0.55 INCHES. REMOVED CORROSION AND VERIFIED FABRICATED REPAIR STRAP, ALODINED ALL BARE ALUMINUM SURFACES AND FINISHED BLENDS AND REPAIR STRAP WITH PRIMER. FILLED BLENDS WITH BMS 595 SEALANT AND INSTALLED REPAIR STRAP WITH SEALANT PROSEAL 870 AND FASTENERS.

Part: FLOORBEAM — BROKEN (FUSELAGE)

AFW - FLOORBEAM AT STATION 325 AT RBL 86 (VERY OUTBOARD END) BROKEN OFF, AREA IS 1 INCH SQUARE. SMOOTHED AND BLENDED BROKEN EDGE OF CHORD. TWO REPAIR ANGLES MACHINED, EXTRUSION INSTALLED. ANGLES ATTACHED WITH FLUSH HI-LOKS (UPPER FASTENER) AND PROTRUDING HI-LOKS IN LOWER HOLE LOCATIONS. EXISTING FASTENER LOCATIONS REPLACED WITH SAME TYPE AND SIZE AS ORIGINAL.

Part: FLOORBEAM — CRACKED (FUSELAGE)

AFW - FLOORBEAM AT STATION 287 AT RBL 86 AT VERY OUTBOARD END HAS CRACK ON H3 FLANGE. AREA OF FLANGE CONTAINING CRACK WAS REMOVED. TWO REPAIR ANGLES MACHINED FROM 0,063 INCH 7075T6 EXTRUSION AND FILLER WERE INSTALLED WITH STAINLESS HI-LOKS.

Part: TAPE — BURNED (ANTI-ICE SYS)

AFW - HEATER TAPE FOR WATER OR DRAIN LINE WAS BURNT IN HALF. INSULATION WRAPPER WAS SLIGHTLY CHARRED. WATER AND DRAIN LINE ARE WRAPPED TOGETHER WITH 2 RIBBONS (PART NUMBER 304311040280 MFR COX AND COMPANY), AREA WAS .5 INCH BY 16 INCHES AT AFT CARGO AT STATION NUMBER 1410 THROUGH 1420 ABOVE STRINGER 536R. CAPPED AND STOWED HEATER TAPE POWER WIRE. REMOVED BURNT SECTION OF HEATER TAPE AND WRAPPED NEW INSULATION AROUND DRAIN LINE AND WATER LINE PER PATTERN CARD 1231 STEP 3 NOTE 3. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — DAMAGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING AT 2B INOPERATIVE. REPAIRED EMERGENCY EXIT PATH LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DAMAGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING AT 3B INOPERATIVE. REPAIRED EMERGENCY EXIT PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PIN — UNSECURE (CONNECTOR)

ORD - EMERGENCY FLOOR LIGHT AT SEAT 25H WILL NOT ILLUMINATE. RESECURED PIN AT 25H SEAT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: COMPUTER — MALFUNCTIONED (EICAS SYSTEM)

JFK - FLT 38 - EN ROUTE DFW-ZRH, TWO AND ONE-HALF HOURS INTO FLIGHT, BLUE CARGO DOOR EICAS MESSAGE CAME ON THEN BEGAN FLICKERING ON AND OFF FOR 30 MINUTES. WHILE CALLING TECH GOT THE BULK CARGO DOOR EICAS STEADY AGAIN AND A QUICK BELL AND TWO QUICK RED EICAS MESSAGES WHICH WENT OUT BEFORE IT WAS READ. THIS WAS ALSO FOLLOWED BY EICAS DISAGREE AND LEFT EICAS COMPUTER WHITE MESSAGES. LANDED JFK WITHOUT INCIDENT. REPLACED LEFT EICAS COMPUTER AND ACCOMPLISHED CHECK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE LIGHTS AT SEAT 22H INOPERATIVE. CLEANED EMERGENCY ESCAPE LIGHT CONNECTORS AT SEAT 22H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (AFT CARGO)

SFO - DURING OVERNIGHT MAINTENANCE, EXTERNAL EMERGENCY EXIT LIGHT FORWARD OF AFT CARGO PIT DOOR INOPERATIVE. ADJUSTED EXTERNAL EMERGENCY EXIT LIGHT SOCKET FORWARD OF AFT CARGO PIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LIGHTING AT 24B INOPERATIVE. RECONNECTED LOOSE CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PUMP — INOPERATIVE (HYD SYSTEM)

DFW - FLT 2342 - EN ROUTE DFW-ORD, AFTER TAKEOFF GEAR HANDLE PUT IN RETRACT POSITION 'C' HYDRAULIC PRESSURE DROPPED TO 710 PSI AND BOTH ELECTRICAL PUMP INOPERATIVE LIGHTS ILLUMINATED. AIRCRAFT RETURNED DFW LANDING WITHOUT INCIDENT. AIRCRAFT REMOVED AND FROM SERVICE FOR FURTHER EVALUATION. DFW MAINTENANCE REPLACED THE AIR DRIVEN PUMP AND PRESSURE REGULATOR SHUTOFF VALVE PER MM. ALL OPERATIONAL CHECKS NORMAL. SYSTEM GROUND CHECK OPERATION NORMAL. (M)

Part: SKIN — TORN (FUSELAGE)

AFW - FOUND FUSELAGE SKIN TORN AT FORWARD CARGO DOOR CUT OUT FORWARD LOWER CORNER. DAMAGE CUT OUT. FABRICATE FILLERS. FABRICATE DOUBLERS. ALODINED AND PRIME SURFACES. DOUBLER TO BE INSTALLED WET. REPLACE EXISTING FASTENERS. FILLERS TO BE ATTACHED TOGETHER WITH DOUBLE FLUSH RIVETS. (M)

Part: LIGHT — LOOSE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 20H INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT AT SEAT 20H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 39 INOPERATIVE. REPAIRED EMERGENCY EXIT WIRE AT SEAT 39 ELECTRICAL CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — SHORTED (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS AT SEAT 39B INOPERATIVE. REPAIRED WIRE AT SEAT 39B. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: WIRE — BROKEN (SEAT 36)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT PATH LIGHT AT SEAT 36H INOPERATIVE. REPAIRED WIRING AT SEAT 36H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: WIRE — BROKEN (ROW 21)

DFW - DURING OVERNIGHT, MAINTENANCE EMERGENCY EXIT SEAT LIGHTS AT SEAT 21 AB INOPERATIVE. REPAIRED WIRE TO EMERGENCY EXIT SEAT LIGHTS AT 21 AB. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: SWITCH — DEFECTIVE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHTS COULD NOT BE TURNED OFF USING THE SWITCH AT THE FORWARD FLIGHT ATTENDANT'S STATION. REPLACED FORWARD FLIGHT ATTENDANT EMERGENCY EXIT SEAT LIGHT SWITCH. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: WIRE — FAILED (ROW 22)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT SEAT ROW 22B INOPERATIVE. REPAIRED EMERGENCY EXIT SEAT LIGHT WIRING AT SEAT ROWS 22B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLOORBEAM — CORRODED (BS 764)

AFW - FLOORBEAM AT STATION 764 HAD CORROSION BLENDED BEYOND SRM LIMITS. ALODINE ALL BARE ALUMINUM SURFACES FINISH BLENDED AREAS WITH 2 COATS OF PRIMER. FILL BLEND WITH BMS5-95. (M)

Part: SEAT TRACK — CORRODED (BS 740-746)

AFW - SEAT TRACKS AT RBL AND LBL 11 HAD CORROSION BLENDED BEYOND SRM LIMITS. ALODINE ALL BARE ALUMINUM SURFACES. FINISH WITH 2 COATS PRIMER. FILL BLENDS WITH BMS5-95 AFTER SHIMMING PER SRM. (M)

Part: FLOORBEAM — CORRODED (BS 347)

AFW - FLOORBEAM AT STATION 347 HAD CORROSION BLENDED BEYOND SRM LIMITS. ALODINE AND FINISH THE BLENDED AREAS WITH 2 COATS PRIMER. FILL BLENDS WITH BMS5-95 AND INSTALLED SKIN AS REQUIRED. (M)

Part: FLOORBEAM — CORRODED (BS 906)

AFW - FLOORBEAM AT LBL 54.81 STATION 906 HAD CORROSION BLENDED BEYOND SRM LIMITS. BLEND OUT CORROSION AND ROTO PEEN THE REWORKED AREA PER SRM. ALODINE ALL BARE ALUMINUM SURFACES. FINISH BLENDED AREAS WITH 2 COATS PRIMER. FILL BLENDS WITH BMS5-95. (M)

Part: FLOORBEAM — CORRODED (BS 797)

AFW - FLOORBEAMS AT LBL AND RBL 11 HAD CORROSION BLENDED BEYOND SRM LIMITS. BLEND OUT CORROSION AND ROTO PEEN THE REWORKED AREA PER SRM. ALODINE ALL BARE ALUMINUM SURFACES. FINISH BLEND AREAS WITH 2 COATS PRIMER. FILL BLENDS WITH BMS 5-95. (M)

Part: FLOORBEAM — CORRODED (BS 797)

AFW - FLOORBEAMS AT LBL AND RBL 33 HAD CORROSION BLENDED BEYOND SRM LIMITS. BLEND OUT CORROSION AND ROTO PEEN THE REWORKED AREA PER SRM. ALODINE ALL BARE ALUMINUM SURFACES. FINISH BLENDED AREAS WITH 2 COATS PRIMER. FILL BLENDS WITH BMS5-95. (M)

Part: FLOORBEAM — CORRODED (BS 325)

AFW - FLOORBEAM AT STATION 325 HAD CORROSION BLENDED BEYOND SRM LIMITS. ACCOMPLISHED IAW SKETCHES. ALODINE AND PRIME STRAP TO INSTALL. (M)

Part: FLOORBEAM — CORRODED (BS 347)

AFW - FLOORBEAM AT STATION 347 HAD CORROSION BLENDED. FABRICATE REPAIR STRAP. ALODINE ALL BARE ALUMINUM SURFACES. FINISH BLEND AND REPAIR PARTS WITH 2 COATS PRIMER. INSTALL STRAP WET WITH SEALANT. (M)

Part: DUCT — LOOSE (LT ENGINE)

MIA - FLT 2101 -DURING CLIMB AT ABOUT 20,000 FT LEFT ENGINE OVERHEAT WARNING APPEARED. RAN PROCEDURE AND WHEN RETARDING LEFT THROTTLE BELOW 70 PERCENT THE ENGINE OVERHEAT LIGHT EXTINGUISHED. CHECKED ALL PNEUMATIC DUCTS FOR CONDITION, ALL OK. CHECKED CLAMPS, FOUND ONE CLAMP LOOSE ON DUCT. TIGHTENED CLAMP. RAN ENG AT 97 PERCENT N1. OPS CHECK NORMAL. LT ENGINE OVERHEAT LOOP DET 5407 REPLACED. PERFORMED GROUND OPS CHECK OF DET SYSTEM CHECKS NORMAL. (M)

Part: WIRE — BROKEN (CABIN)

LHR - DURING OVERNIGHT CHECK, DISCOVERED EMERGENCY EXIT LIGHT AT PASSENGER SEAT 36HJ INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT WIRE AT PASSENGER SEAT 36HJ. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: WIRE — BROKEN (CABIN)

SFO - DURING MAINTENANCE, EMERGENCY EXIT LIGHT AT PAX SEAT 34H INOPERATIVE. REPAIRED BROKEN WIRE AND REPLACED PIN AND CONNECTOR FOR EMERGENCY EXIT LIGHT AT PAX SEAT 34H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LAMP ASSY — SHORTED (CABIN)

EZE - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEATS 22H, 23H AND 24H INOPERATIVE. PROBLEM DETERMINED TO BE SHORTED LIGHT SOCKET AT SEAT 23H. ISOLATED LIGHT AT SEAT 23H AND REINSTATED SYSTEM WITH SEAT LIGHT 22H AND 24H FUNCTIONING NORMALLY. PLACARDED EMERGENCY EXIT LIGHT AT PAX SEAT 23H. SUBSEQUENTLY REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT PAX SEAT 23H AND REMOVED PLACARD AT MIA/12. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SEAT TRACK — CORRODED (FS 772)

FOUND CORROSION ON INBOARD FLANGE OF SEAT TRACK LBL 1106 STATION 772. REPAIRED PER MRB 767-908 DATED 4/23/95. (M)