N361AA

Part: DIODE — ERRATIC (CABIN PRESSURE) · airframe 111,959 hrs · 18,243 cycles

CREW REPORTED CABIN AUTO PRESSURIZATION FAULT. AN EMER WAS DECLARED. THE FLIGHT DIVERTED & LANDED WITHOUT INCIDENT. THE ACFT WAS GNDED. R & R DIODE R206. AS A PRECAUTION, ALSO REPLACED RELAYS K147, K716, K211 & K148, ALL CHECKED OK. WORK ACCOMPLISHED IAW MM 21-31-02, AMM 32-09-02, SWPM 20-90-11 & SWPM 20-81-26. TESTED SYS AS REQUIRED, ALL CHECKED OK. SEE ALSO AALA20151015008.

Part: CONTROLLER — FAULTED (CABIN PRESSURE) · airframe 111,959 hrs · 18,243 cycles

CABIN AUTO PRESSURIZATION FAULT. AN EMERGENCY WAS DECLARED. FLIGHT DIVERTED & LANDED WITHOUT INCIDENT. ACFT GROUNDED. R & R NR 1 CABIN PRESS CONTROLLER. WORK ACCOMPLISHED IAW MM 21-31-02, AMM 32-09-02, SWPM 20-90-11 & SWPM 20-81-26. TESTED SYS AS REQUIRED, ALL CHECKED OK.

Part: BPCU — FAULTY (ELECTRICAL SYS) · airframe 111,867 hrs · 18,225 cycles

AT CRUISE, BOTH UTILITY BUSS OFF LIGHTS ILLUMINATED. ACCOMPLISHED QRH PROCEDURE, BUSSES REMAINED OFF. REPLACED BPCU IAW AMM 24-41-03. ALL OPERATIONS & INDICATIONS NORMAL.

Part: SLAT SYSTEM — FALSE INDICATION · airframe 111,367 hrs · 18,134 cycles

DURING APPROACH LE SLAT ASYMMETRY DISPLAYED ON EICAS. LANDING ABORTED, EMERGENCY DECLARED, AND LANDING UNEVENTFUL. ACCOMPLISHED FIM 27-81-00, CHECKED LE SENSORS FROM PSEU RACK PLUG. ALL SENSORS OHMED NORMAL, SENSOR GAPS NORMAL. COULD NOT DUPLICATE ON GND. SYS CHECKED NORMAL.

Part: STRINGER — DENTED (FUSELAGE) · airframe 109,551 hrs · 17,835 cycles

FUSELAGE DENTED AT STATION 512 BETWEEN STRINGERS 36 RT & 37 RT. REPAIRED STRINGERS IAW SRM 53-00-01-2R-12 & EA 53-038171 DATED 1/26/2015.

Part: SKIN — DENTED (FUSELAGE) · airframe 109,551 hrs · 17,835 cycles

FUSELAGE DENTED AT STATION 512 BETWEEN STRINGERS 36 RT & 37 RT. REPAIRED AREA IAW SRM 53-00-01-2R-12 & EA -53-038171 DATED 1/26/2015.

Part: WEB — CRACKED (FUSELAGE) · airframe 109,551 hrs · 17,835 cycles

WEB BETWEEN STATIONS 500 & 522 UNDER PDU 5C IS CRACKED. R & R WEB IAW 51-10-02-0G.

Part: SKIN — CORRODED (RT HORIZ STAB) · corrosion level 2 · airframe 109,551 hrs · 17,835 cycles

RIGHT HORIZONTAL STABILIZER UPPER SKIN CORRODED AT REAR SPAR STATION 170. REPAIRED SKIN IAW EA 55-038299 DATED 1/24/2015.

Part: STIFFENER — CRACKED (LT PYLON) · airframe 109,551 hrs · 17,835 cycles

LEFT PYLON OTBD VERTICAL STIFFENER & UPPER ATTACH ANGLE CRACKED FWD OF OTBD MIDSPAR FITTING. INSTALLED NEW LT PYLON OTBD STIFFENER & UPPER ANGLE IAW SRM 51-10-02 & AARD 51-00-05.

Part: STIFFENER — CRACKED (LT PYLON) · airframe 109,551 hrs · 17,835 cycles

LEFT PYLON OTBD HORIZONTAL STIFFENER CRACKED. R & R STIFFENER IAW SRM 51-10-02-0G & DWG 311T2400.

Part: FRAME — CRACKED (RT PYLON) · airframe 109,551 hrs · 17,835 cycles

RIGHT PYLON NACELLE STRUT INBD FRAME CHORD IS CRACKED AT AFT OTBD RADIUS, APPROX 4 INCHES FROM TOP. R & R FRAME IAW SRM 51-10-02-0G & DWG 311T2350.

Part: LIGHT — BROKEN (CABIN) · airframe 109,524 hrs · 17,831 cycles

ON CABIN INSPECTION FOUND EPM EMER LIGHT BROKEN & LENS MISSING AT FLOOR LEVEL AT 4R DOOR. REPLACED R4 DOOR EPM EMER LIGHT ASSEMBLY. ALL OPERATIONS OK.

Part: BEZEL — MISSING (CABIN) · airframe 106,733 hrs · 17,381 cycles

EMERGENCY LIGHT BEZEL MISSING AT UPPER LT AFT GALLEY AISLE. REPLACED BEZEL, OPERATIONS CHECKED NORMAL.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 106,364 hrs · 17,324 cycles

SMOKE DETECTOR IN F1 LAVATORY INTERMITTENTLY ACTIVATES WITH NO SIGN OF SMOKE. ACCOMPLISHED SMOKE DETECTOR CHECK IAW MM 26-13-00-501 & RESET. OPERATIONS CHECKED NORMAL.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 105,160 hrs · 17,112 cycles

SMOKE DETECTOR ACTIVATED AT LAVATORY FS 3, LAVATORY WAS EMPTY. RESET SMOKE DETECTOR AT FS 3 LAVATORY & NO FURTHER ALARM SOUND. OPERATIONS CHECKED NORMAL.

Part: TERMINAL — BROKEN (EVAC SLIDE) · airframe 104,540 hrs · 17,015 cycles

BOTH LT & RT EMERGENCY ESCAPE SQUIB TEST 1 SLIDE & SQUIB TEST 2 SPOILER FAILED. FOUND A BROKEN WIRE TERMINAL FROM RT SIDE BATTERY PACK. R & R TERMINAL. OPERATIONS CHECKED NORMAL.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 104,130 hrs · 16,947 cycles

CORROSION AT STATION 955 ON THE OTBD SURFACE OF FAILSAFE STRAP. REMOVED CORROSION & ACCOMPLISHED REPAIR IAW EA B767-53-030937.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 104,130 hrs · 16,947 cycles

FS SKIN DAMAGED AT STATION 1569 & STRINGER 21 RT. INSTALLED DOUBLER IAW SRM 53-00-01-2R-1 & EA B767-53-030914.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 104,130 hrs · 16,947 cycles

FS SKIN FROM STATIONS 325 TO 347 & STRINGERS 21 & 12 LT DENTED & GOUGED. INSTALLED DOUBLERS IAW EA B767-53-030930.

Part: ENGINE — FAILED (RIGHT) · airframe 103,593 hrs · 16,856 cycles

INFLIGHT, CREW REPORTED RT ENGINE OIL FILTER CLOG LIGHT ILLUMINATED. CREW SHUTDOWN RT ENGINE (SINGLE ENGINE TIME 27 MINUTES). EMERGENCY DECLARED FLIGHT DIVERTED RDU LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. ACFT FERRIED FOR MX. REPLACED RT ENGINE ON 06/04/2013. SYS GROUND CHECK NORMAL OPERATION.

Part: LIGHT — NOT SEATED (CABIN) · airframe 102,264 hrs · 16,653 cycles

LEFT NUMBER 4 DOOR LOWER EXIT PORTION OF SIGN AT BOTTOM LOCATION LAMPS INOPERATIVE. RESEAT LIGHT ASSEMBLY CONTACT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 100,468 hrs · 16,364 cycles

LOWER AFT RIGHT SIDE EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LOWER AFT RIGHT SIDE EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 100,468 hrs · 16,364 cycles

LOWER FORWARD RIGHT SIDE EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LOWER FORWARD RIGHT SIDE EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: CONTROLLER — INOPERATIVE (BLEED AIR SYS) · airframe 99,167 hrs · 16,153 cycles

JFK - CREW REPORTED RIGHT ENGINE HIGH PRESSURE SHUT-OFF VALVE EICAS MESSAGE ACCOMPANIED BY RIGHT ENGINE BLEED OVERHEAD ANNICIATOR LIGHT. QRH PROCEDURES ACCOMPLISHED. FLIGHT LANDED JFK WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED HIGH PRESSURE CONTROLLER AND YELLOW CORE HARNESS ON RIGHT ENGINE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LENS — MISSING (ZONE 200) · airframe 99,019 hrs · 16,127 cycles

LEFT AFT LAVATORY WALL EMERGENCY LIGHT ILLUMINATOR LENS MISSING. REPLACED LENS FOR LEFT AFT LAVATORY WALL EMERGENCY LIGHT ILLUMINATOR. OPS CHECK NORMAL.

Part: SLAT — DEBONDED (RT WING) · airframe 98,583 hrs · 16,053 cycles

NUMBER 8 SLAT AT INBOARD END, JUST OUTBOARD OF RIGHT PYLON DISBONDED. INSTALLED DOUBLER PER SRM 51-70-10.

Part: SKIN — DEBONDED (LE SLAT) · airframe 98,583 hrs · 16,053 cycles

DISBOND ON NUMBER 3 SLAT, OUTBOARD UPPER CORNER, UPPER AND LOWER SURFACES. INSTALLED DOUBLER PER SRM 51-70-10-2R.

Part: SKIN — DEBONDED (LE SLAT) · airframe 98,583 hrs · 16,053 cycles

DISBOND ON NUMBER 3 SLAT, INBOARD UPPER CORNER, UPPER AND LOWER SURFACES. INSTALLED DOUBLER PER SRM 51-70-10-2R.

Part: SKIN — DEBONDED (LE SLAT) · airframe 98,583 hrs · 16,053 cycles

NUMBER 10 SLAT INBOARD END LOWER SKIN DISBONDED. INSTALLED DOUBLER PER SRM 51-70-10.

Part: SLAT — DEBONDED (RT WING) · airframe 98,583 hrs · 16,053 cycles

NUMBER 11 SLAT OUTBOARD UPPER CORNER AREA DISBONDED. INSTALLED DOUBLER PER SRM 51-70-10.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 98,041 hrs · 15,962 cycles

RIGHT AFT/MID FUSELAGE EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 97,636 hrs · 15,904 cycles

EMERGENCY LIGHT AT LEFT NUMBER 4 DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT NUMBER 4 DOOR. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 97,636 hrs · 15,904 cycles

EMERGENCY LIGHT AT RIGHT NUMBER 4 DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER 4 DOOR. OPS CHECK NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 97,241 hrs · 15,837 cycles

SEAT EMERGENCY LIGHTS AT SEATS 25HJ TO 29HJ INOPERATIVE. RESET CONNECTOR UNDER SEAT 27HJ. OPS CHECK NORMAL.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 96,699 hrs · 15,756 cycles

LEFT AFT EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED BATTERY FOR LEFT AFT EMERGENCY FLASHLIGHT. OPS CHECK NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 96,317 hrs · 15,697 cycles

LEFT NUMBER 4 DOOR EMERGENCY EXIT SIGN INOPERATIVE. REPLACED BATTERY CHARGER FOR LEFT NUMBER 4 DOOR EMERGENCY EXIT SIGN. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 96,317 hrs · 15,697 cycles

LEFT NUMBER 1 DOOR EMERGENCY EXIT SIGN INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 1 DOOR EMERGENCY EXIT SIGN. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 94,955 hrs · 15,480 cycles

RIGHT NUMBER 1 EXTERIOR EMERGENCY SLIDE LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 1 EXTERIOR EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: FAN — FAULTY (E&E BAY) · airframe 91,895 hrs · 14,921 cycles

JFK - FUMES DETECTED IN COCKPIT EN ROUTE. FORWARD EQUIPMENT EXHAUST FAN EICAS MESSAGE APPEARED AND CIRCUIT BREAKER WAS FOUND POPPED OUT. FLIGHT LANDED JFK WITHOUT INCIDENT. REPLACED FORWARD EQUIPMENT COOLING FAN. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FITTING — CRACKED (HYDRAULIC SYS) · airframe 91,434 hrs · 14,844 cycles

JFK - INFLIGHT DFW-CDG. CREW REPORTED LEFT HYDRAULIC SYSTEM QUANTITY LOST. DIVERTED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND YAW DAMPER LEFT SERVO RETURN ELBOW CRACK. REPLACED FITTING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 91,263 hrs · 14,813 cycles

INFLIGHT ZRH TO JFK. LEFT HYDRAULIC SYSTEM PRESSURE EICAS MESSAGE ILLUMINATED WITH COMPLETE LOSS OF HYDRAULIC FLUID. LANDED LHR WITHOUT INCIDENT. REPLACED FLEX HYDRAULIC HOSE TO RUDDER RATIO CHANGER. INSPECTED AND REPLACED CASE DRAIN FILTERS FOR BOTH THE EDP AND ELEC HYD PUMP, ALL OK. REPLACED HYD LINE SECURING CLIPS FOUND DAMAGED PER IPC 27-21-13-05 ITEMS 10, 15, 20, 25.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 90,741 hrs · 14,717 cycles

EMERGENCY LIGHTS LEFT SIDE FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR LEFT FIRST CLASS.

Part: WATER HEATER — MALFUNCTIONED (LAVATORY) · airframe 88,258 hrs

DUB - SMOKE DETECTOR IN LAVATORY 2 WENT OFF. NO VISIBLE SMOKE. NO FAULT ON SMOKE DETECTOR. FOUND LAVATORY WATER HEATER INOPERATIVE. REPLACED WATER HEATER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LAX - EMERGENCY LIGHT AT LT NR THREE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT LT NR THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: FIRE DETECTOR — INOPERATIVE (NR 2) · airframe 84,901 hrs

DFW INFLIGHT T2421/29APR - CREW REPORTED RIGHT NUMBER TWO FIRE LOOP INDICATION ON CLIMB-OUT. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND LOWER FORWARD FIRE DETECTOR OPEN. REPLACED LOWER FORWARD FIRE DETECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 84,528 hrs

DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 10H INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 10H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 84,030 hrs

ORD - EMERGENCY EXIT LIGHT AT MID GALLEY RIGHT CEILING INOPERATIVE. REPLACED BATTERY LAMP FOR EMERGENCY EXIT LIGHT AT MID GALLEY RIGHT CEILING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 83,766 hrs

DFW EXTERNAL EMERGENCY LIGHT AT LEFT NUMBER FOUR DOOR INOPERATIVE. REPLACED LAMPS FOR EXTERNAL EMERGENCY LIGHT AT LEFT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 83,766 hrs

DFW - EMERGENCY LIGHT AT LEFT AFT OVERWING EXIT INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT LEFT AFT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — BROKEN (EMERGENCY LIGHTS)

ORD - EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR HAD BROKEN LENS. REPLACED LENS FOR EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHT)

CDG - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR EXIT SIGN MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — LOOSE (CABIN)

CDG - EMERGENCY DOOR EXIT SIGN LIGHT AT LEFT NUMBER ONE DOOR UNSECURED. SECURED LOOSE DOOR EXIT SIGN FOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

LAX - EMERGENCY LIGHT AT RIGHT OVERWING EXIT SLIDE INOPERATIVE. RELAMPED EMERGENCY LIGHT AT RIGHT OVERWING EXIT SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - OVERHEAD EMERGENCY AISLE LIGHTS AT SEAT ROWS 25 AND 28 INOPERATIVE. REPLACED BATTERY PACK M737 FOR OVERHEAD EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MODULE — INOPERATIVE (EMERGENCY SIGN)

LAX EMERGENCY LIGHT AT RIGHT ONE EXIT IDENTIFIER SIGN INOPERATIVE. REPLACED MODULE IN EMERGENCY LIGHT EXIT IDENTIFIER SIGN AT RIGHT ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (CABIN)

EZE - EMERGENCY LIGHTS AT ROWS 20HJ AND 21HJ INOPERATIVE. REPLACED BATTERY PACK AT ROW 20 FOR EMERGENCY LIGHTS AT ROWS 20HJ AND 21HJ. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SKIN — CRACKED (FUSELAGE)

DUB - AIRCRAFT MAINTENANCE DISCOVERED A ONE INCH CRACK BETWEEN TWO RIVETS AT STRINGER 37 LEFT AT STATION 1219. ACCOMPLISHED TEMPORARY REPAIR FABRICATE REPAIR DOUBLER OF 2024T3 0.063 TO 0.080 THICK. INSTALL WET WITH SEALANT. INSTALL USING 3/16 PROTRUDING HEAD BLIND RIVETS USING EXISTING FASTENER PATTERNS. INSTALL AT MINIMUM TWO ROWS OF FASTENERS PAST CRACK IN EACH DIRECTION TO AIRCRAFT SKIN CRACK AT STATION 1219 STRINGER 37 LEFT PER SRM/AFW ENGINEERING INSTRUCTIONS FOR FERRY FLIGHT TO AFW BASE FOR FURTHER EVALUATION AND PERMANENT REPAIR. ACCOMPLISHED PERMANENT REPAIR PER MRB 767 2697.

Part: SPRING — INOPERATIVE (PAX DOOR SLIDE)

AFW - SPRING ON RIGHT NR 1 DOOR PER AD 2001 26 19 WILL NOT STAY IN COTTER PIN. FORWARD SPRING RIGHT NUMBER ONE DOOR ON GIRT BAR. REPLACED GIRT BAR ON RIGHT NUMBER ONE DOOR.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHTS AT L391, L644 AND L392 INOPERATIVE. REPLACED BATTERY PACK M733 FOR EMERGENCY LIGHTS AT L391, L644 AND L392. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - OUTSIDE OVERWING RIGHT HAND EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER EQUIPMENT NUMBER M731 FOR OUTSIDE OVERWING RIGHT HAND EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

AFW - FLOOR SUPPORT TEE AT LEFT 4 DOOR HAS CORROSION REMOVAL ON H3 HINGE. VERIFIED CORROSION WAS COMPLETELY REMOVED. DYE CHECKED AREA FOR CRACKS AND REFINISHED THE BLENDED AREA WITH ALODINE AND TWO COATS OF BMS10-11 PRIMER. APPLIED CORROSION INHIBITING COMPOUND TO FLOOR SUPPORT TEE. FILLED BLEND WITH BMS5-99 SEALENT.

Part: FRAME — CUT (FUSELAGE)

AFW - WHILE ACCOMPLISHING C1945CB STEP E3 FRAME WAS CUT AT .30 INCH FROM UPPER FASTENER OF REMAINING FRAME, NOT .46 INCH AS ECO STATES. AREA WAS ONE INCH BY ONE INCH AT A DEPTH OF 1.3 INCHES. FILLED GAP WITH BMS595 SEALANT AND COMPLETE REPAIR PER ECO C1945 INSTRUCTIONS.

Part: FRAME — CUT (TAIL)

AFW - WHILE ACCOMPLISHING C1945CB STEP E 3 CHORD WAS CUT AT 0.30 INCH FROM UPPER FASTENER OF REMAINING CHORD NOT 0.46 INCH AS ECO INSTRUCTS. AREA IS 1 INCH BY 1 INCH AT A DEPTH OF 1.3 INCHES. FILLED GAP WITH BMS5 95 SEALANT AND COMPLETED REPAIR PER ECO C1945 INSTRUCTIONS.

Part: FAILSAFE — CORRODED (FUSELAGE)

AFW - SECTION 43 FORWARD CARGO, INNER CHORD ANGLE OF FAILSAFE CHORD FORWARD CARGO DOOR HAS CORROSION REMOVAL BLENDOUTS ON THE LOWER SURFACE IN 2 LOCATIONS AT FASTENERS. STA 591 IS 1.5 INCH DIAGONAL WITH DEPTH OF .030 INCHES & STA 527.65 IS 1.2 INCHES DIAGONAL WITH DEPTH OF .021 INCH DEEP. CORROSION REMOVED, PERFORM EDDY CURRENT, & ROTOPEEN BLENDED AREA. REFINISH BLENDED AREA WITH ALODINE & 2 COATS OF PRIMER. INSTALLED FAILSAFE STRAP, FABRICATE REPAIR STRAPS. STRAP MUST EXTEND A MINIMUM OF .5 INCH BEYOND CENTER OF EACH FASTENER HOLE. FINISH STRAP WITH ALODINE & 2 COATS OF BMS1011 PRIMER. INSTALL A STRAP AT EACH BLENDED LOCATION. ADJUST GRIP LENGTH OF BOLTS TO ACCOMODATE REPAIR STRAP.

Part: FAILSAFE — CORRODED (CARGO DOORFRAME)

FAILSAFE FWD CARGO DOOR CUTOUT ANGLE HAS CORROSION REMOVAL BLENDOUTS ON LOWER SURFACE 2 LOCATIONS AT FASTENERS. DEPTH IS 0.030 INCH BY 0.021 INCH STA 591 & 527.65 SECTION 43 FWD CARGO. PERFORMED HIGH FREQUENCY EDDY CURRENT TO INSURE CRACK FREE. ROTOPEEN BLENDED AREA AND REFINISH THE BLENDED AREA WITH ALODINE AND 2 COATS OF BMS10 11 PRIMER. AFTER INSTALLATION OF FAILSAFE STRAP FABRICATE REPAIR STRAPS FROM 7075T7351 PLATE A MINIMUM OF 0.190 THICK. STRAP EXTENDS A MINIMUM OF .5 INCH BEYOND CENTER AT EACH FASTENER HOLE. FINISHED STRAP WITH ALODINE AND 2 COATS OF BMS10 11 PRIMER AND INSTALLED A STRAP AT EACH BLENDED LOCATION. ADJUST RIP LENGTH OF BOLTS TO ACCOMMODATE REPAIR STRAP.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHT)

MIA EMERGENCY LIGHT AT SEAT 26B INOPERATIVE. REPLACED WIRE ON HARNESS FOR EMERGENCY LIGHT AT SEAT 26B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — BROKEN (EMERGENCY LIGHT)

EMERGENCY LIGHT AT SEAT 26B INOPERATIVE. REPAIRED BROKEN WIRE ON HARNESS FOR EMERGENCY LIGHT AT SEAT 26B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — LOOSE (CABIN)

LAX LEFT HAND AFT DOOR EMERGENCY FLOOR FLOOD LIGHT BASE ASSEMBLY LENS LOOSE. REPLACED LEFT HAND AFT DOOR EMERGENCY FLOOR FLOOD LIGHT BASE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — BROKEN (EMERGENCY LIGHT)

EMERGENCY EXIT LIGHT INOPERATIVE AT SEAT 26G. BATTERY PACK FAILED DUAL FEED CHECK. REPAIRED BROKEN WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS WERE INOPERATIVE AT ROW 32AB. RECONNECTED LOOSE CONNECTOR AT SEAT 32AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

EMERGENCY EXIT ILGHTS INOPERATIVE AT ROW 32AB. BATERY PACK FAILED DUAL FEED CHECK. RECONNECTED LOOSE CANNON PLUG AT SEAT 32AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FILTER — CLOGGED (IDG)

ON DEPARTURE CLIMB-OUT, THE GENERATOR LIGHT FLICKERED WITH ACCOMPANIED EICAS MSG RT GENERATOR DRIVE, DISCONNECTED RIGHT GENERATOR. CHECKED RT IDG AND FOUND OIL OVER FILLED AND DIFF PRESS POP OUT. REPLACED OIL IDG PRESS FILTER AND SERVICED IDG IAW MM 12 RUN UP PERFORMED ALL INDICATIONS ARE NORMAL OK FOR SERVICE. NO DEBRIS FOUND. (M)

Part: LIGHT — MALFUNCTIONED (CABIN)

LHR - FLT 46 - EN ROUTE ORD-LHR, DURING FLIGHT EMERGENCY EXIT LIGHTS ILLUMINATED FOR 2 MINUTES THEN EXTINGUISHED. LANDED LHR WITHOUT INCIDENT. CYCLED EMERGENCY EXIT LIGHT SWITCH OFF THEN ARMED AND ACCOMPLISHED EMERGENCY EXIT LIGHT TEST, ALL LIGHTS FUNCTION AS NORMAL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (APU)

APU FAULT LIGHT CAME ON AT FL320. ACCOMPLISHED APU FAULT PROCEDURE WITH RESTART AND LIGHT REMAINED ILLUMINATED. RESEATED ELECTRICAL CONNECTOR ON APU LOW OIL PRESSURE SWITCH SERVICED APU TO FULL ACCOMPLISHED GROUND CHECKS AND OIL CONSUMPTION CHECK ALL OK INSPECTED OIL FILTERS AND MAGNETIC CHIP DETECTORS ALL CLEAN APU OK FOR FURTHER SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

LFW - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LIGHTING AT ROWS 22, 23, 24 INOPERATIVE. REPLACED SEAT CONNECTOR AT ROW 23 AND BATTERY PACK EQUIPMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LIGHTING SEAT 20-24B INOPERATIVE. SECURED POWER SUPPLY PLUG AT SEAT 20-24B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LIGHTING SEAT 10B INOPERATIVE. SECURED POWER SUPPLY PLUG AT SEAT 10B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT AT ROWS 18 THROUGH 21 INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PIN — DEFECTIVE (CONNECTOR)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 33H INOPERATIVE. REPLACED CONNECTOR PIN ON SEAT 33H EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PUMP — DEFECTIVE (NR 2 ENGINE)

MIA - FLT 912 - EN ROUTE MIA-LAX, DETECTED AIRCRAFT INTERMITTENTLY OSCILLATING SIDE TO SIDE. OSCILLATION INCREASED DURNIG CLIMB. RETURNED MIA AND LANDED WITHOUT FURTHER INCIDENT. REPLACED RIGHT SIDE HIGH PRESSURE FUEL PUMP. ACCOMPLISHED LEAK AND POWER ASSURANCE CHECK. NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONTACT — DIRTY (EXIT LIGHT)

DFW - DURING OVERNIGHT MAINTENANCE, 1L DOOR JAM EMERGENCY EXIT LIGHT FAILED LIGHT TEST. CLEANED BULB CONTACT. SYSTEM GRUOND CHECKED NORMAL OPERATION. (M)

Part: ROD — BROKEN (RT LE SLAT)

DW - FLT 0070 - DURING CLIMB-OUT, SLATS WERE RETRACTED AND A SLAT ASYMMETRY EICAS MESSAGE ILLUMINATED. CREW RETURNED TO DFW AND LANDED OVERWEIGHT WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE OUTBOARD CONTROL ROD FOR NR 7 SLAT BROKEN. MAINTENANCE REPLACED NR 7 CONTROL ROD AND ADJUSTED/OPERATED SLATS FLAPS SEVERAL TIMES WITH NO MESSAGES OR FAULTS ON FSEU OR PROXIMITY BOX. OVERWEIGHT LANDING WAS ACCOMPLISHED WITH NO ABNORMAL FINDINGS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: MODULE — DEFECTIVE (RT LE SLAT)

DFW - FLT 945 - DURING CLIMB-OUT, SLATS WERE RETRACTED AND A SLAT ASYMMETRY EICAS MESSAGE ILLUMINATED. CREW RETURNED TO DFW AND LANDED OVERWEIGHT WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND RIGHT SLAT CONTROL MODULE FAULTY. REPLACED RIGHT SLAT CONTROL MODULE. ACCOMPLISHED REQUIRED OPERATIONAL AND LEAK CHECKS. OVERWEIGHT LANDING WAS ACCOMPLISHED WITH NO ABNORMAL FINDINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — BROKEN (ROW 32-41)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY PATH EXIT LIGHTS BETWEEN SEAT ROWS 32HJ THROUGH 41HJ INOPERATIVE. MAINTENANCE FOUND A FAULTY CONNECTOR. REPLACED CONNECTOR TO EMERGENCY EXIT PATH LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — FAILED (ROW 21AB)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT ROW 21AB INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT ROW 21AB. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: LIGHTS — INTERMITTENT (CABIN)

LHR - FLT 136 - DURING CRUISE, EMERGENCY EXIT LIGHTS ILLUMINATED FOR SEVERAL MINUTES AND EXTINGUISHED. MAINTENANCE CHECKED AND TESTED EMERGENCY EXIT LIGHT SYSTEM UNABLE TO DUPLICATE INTERMITTENT FAULT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

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

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 32A/B FOUND INOPERATIVE. RECONNECTED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEAT 32A/B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: FRAME — CORRODED (FUSELAGE)

AFW - FOUND FRAME INNER CHORD CORRODED. FOUND BEYOND SRM LIMITS AFTER BLENDING. REFINISHED BLENDED AREAS PER SRM 53-00-07 FIG 101. APPROVED FOR CONTINUED SERVICE BY ENGINEERING PER MRB 767-1280. (M)

Part: FRAME — WORN (BS 1175)

AFW - FOUND WEAR ON AFT CARGO J CAP FRAME. FOUND WEAR TO EXCEED SRM ALLOWABLE LIMITS. BLENDED DAMAGED AREAS, ALODINED AND PRIMED. APPROVED BY ENGINEERING WITH NOTED CONDITION PER MRB 767-1244. (M)

Part: FRAME — CORRODED (BS 1197)

AFW - FOUND AFT CARGO J CAP FRAME CORRODED. AFTER BLENDING FOUND TO BE BEYOND SRM LIMITS. BLENDOUTS ARE 20:01 RATIO. ALODINED AND PRIMED. APPROVED BY ENGINEERING PER MRB 767-1243. (M)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 41H INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 41H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: STRAP — CORRODED (BS 524-593)

AFW - FOUND AND BLENDED CORROSION ON FORWARD CARGO FAIL/SAFE STRAP IN THREE PLACES. AFTER BLENDING, FOUND EACH AREA TO BE BEYOND SRM LIMITS. ALODINED, PRIMED AND PAINTED EACH AREA. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1241. (M)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT LEFT AISLE BETWEEN PAX SEAT ROWS 8 TO 11 INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT LEFT AISLE PAX SEAT ROW 11. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)

Part: EEL STRIP — BROKEN (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING RIPPED FROM FLOOR AT SEAT 4H. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (Z)

Part: EEL ASSY — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT PASSENGER SEAT 15B FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT ASSEMBLY AT PASSENGER SEAT 15B. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)