N78008

Part: LAVATORY — FAULTED (ZONE 100) · airframe 122,761 hrs · 12,705 cycles

ALL A/C LEFT LAVS INCLUDING 3L CENTER LAVS STOPPED WORKING FOUND ALL LAVS ON LEFT SIDE, INCLUDING 3L CENTER LAVS TO BE OPERATING NORMALLY. FOUND LAV H CLOGGED WITH LARGE AMOUNTS OF PAPER TOWELS AND TOLIET PAPER JAMMED IN TOLIET BOWL. REMOVED AND CLEARED CLOG. LAV H OPERATES NORMALLY. REF AMM 38-32-00. FLUSHED ADD EMP:U092712 ALL LAVS WITH CRUSHED ICE AND VINEGAR. WAITING ON LAV SERVICE FOR PRECHARGE AND FINAL OPS CHECKS OF TANK INDS. ACCOMPLISHED AA AUTO ZERO - ADJUSTMENT TASK 38-33-00-710-801. ALSO ACCOMPLISHED THE LCM BITE OPS TEST, TASK 38-33-00-740-801. BOTH TEST PASSED ON ALL 3 TANKS. ALL TANKS SHOWING EMPTY. AFTER ICE & VINAGER, TANKS NR 1 , 3 ALL SHOW ONE GREEN BAR, AND TANK NR 2 HAS NO BARS. AWAITING LAV SERVICE. CMS WASTE TANK QTY INDICATION- OPS TEST TASK 38-33-00-710-802 TEST PASSED. VERIFIED ALL A/CS LEFT LAVS INCLUDING 3L CENTER OPERATE NORMALLY REF AMM 38-32-00-700-802.

Part: PRESSURE SENSOR — FAULTED (RT ENGINE) · airframe 121,475 hrs · 12,576 cycles

BLEED OFF ENG R EICAS ADVISORY RIGHT ENGINE BLEED VALVE CLOSED FOR SYSTEM FAULT OR SWITCH OFF, AND THE ENGINE IS NOT SHUTDOWN. FIM TASK REF : FIM TASK REFERENCE NOT FOUND CMC MSG# 3610470 AIR SUPPLY & CABIN PRES SURE CONTROLLER (R) IP SENSOR FAIL 36-10470 FIM TASK 36-21 TASK 804 CARRIED OUT. SHOP FAULTS 56 EA, HPSOV FAIL OPEN 36-10370 FIM TASK 36-11 TASK 802. BOTH MSG POINT TOWARDS FAULTY IP SENSOR. WIRING CHECKS CARRIED OUT I.A.W WDM 36-21-12. VOLTAGE 15.25 STABLE AND GOOD GND WIRE SHAKE TEST PASS. REMOVAL/ INSTALLATION OF IP SENSOR M36212 IAW AMM 36-21-03. AIR SUPPLY CONTROL SYSTEM MAT TEST PASS. HPSOV ACTIVATED IAW 36-11-07-860-012-001. PART POWER ENG RUN CARRIED OUT I.A.W 71-00-00. ENG AIR SUPPLY OP TEST PASS I.A.W 36-10-00. ... ALL PARAMETERS NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (ZONE 800) · airframe 121,316 hrs · 12,557 cycles

DOOR FLIGHT LOCK 3R EICAS STATUS NR 3 RIGHT PASSENGER ENTRY DOOR FLIGHT LOCK COMMAND/FLT LK RLY/SEN SOR DISAGREEMENT. FOLLOWED FIM 52-11 TASK 806. PERFORMED FLIGHT LOCK OPS TEST SEVERAL TIMES, LOCK ENGAGES NORMALLY. MAINTENANCE MESSAGE DOES NOT SHOW. CLEANED ASSOCIATED PROXIMITY SENSORS AS PRECAUTIONARY. OK FOR SERVICE AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION (FLT LOCK) · airframe 121,201 hrs · 12,544 cycles

DOOR FLIGHT LOCK 3R EICAS STATUS #3 RIGHT PASSENGER ENTRY DOOR FLIGHT LOCK COMMAND /FLT LK RLY/SEN SOR DISAGREEMENT. FIM TASK REF : FIM TASK REFERENCE NOT FOUND CMC MSG# 5211330. PSEU 2 (R2) WHEN ACFT ARRIVAL AMT ON BOARD CHK NO EXISTING FAULT, ONLY GOT PRESENT LEG FAULT MMSG 52-11330 & 52-12210, BOTH MMSG ARE NOT ACTIVE. PER FIM 52-11 TASK 806 AND 52-11 TASK 809, THIS WAS AN INTERMITTENT FAULT. PERFORM FLIGHT LOCK CONTROL TEST PER AMM 52-11-26-200-801, TEST PASSED, STATUS MSG GONE.

Part: CHARGER — INOPERATIVE (ZONE 200) · airframe 120,199 hrs · 12,436 cycles

AFT LEFT EMERGENCY POWER SUPPLY BATTERY (M33407) INOP. REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY BATTERY PACK AT THE L4 DOOR IAW B777 AMM 33-51-06-960-802. OPS CHK GOOD.

Part: STATIC WICK — MISSING (ZONE 600) · airframe 119,048 hrs · 12,314 cycles

PDA 1 REF TO LP# 3518143 RIGHT HAND WING TIP ONE (1) STATIC DISCHARGER MISSING TOMC HAS BEEN NOTIFIED.RT SIDE MISSING STATIC WICK ONE STATIC DISCHARGER MISSING ON RH WING TIP. DEFERRED IAW RELATED MEL ONE STATIC DISCHARGER MISSING ON RH WING TIP. DEFERRED IAW RELATED MEL RT SIDE WING TIP MISSING STATIC WICK INSTALLED NEW STATIC WICK AT RIGHT WING TIP. REF AMM 23-61-01-400-801

Part: SPRING — MISSING (LT MLG UPLOCK) · airframe 118,967 hrs · 12,306 cycles

PDA 2 FOUND LH MAIN GEAR ASSY UPLOCK SPRING MISSING.REMOVED AND REPLACED LH MAIN GEAR ASSY UPLOCK SPRINGS PER AMM 32-32-20. OK TO CONTINUE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 115,209 hrs · 11,888 cycles

M/D R2 DOOR 1EA EMER LT POWER PACK (M33098) FOUND LOW CAPACITY,O RIGINATED BY , REF TO HAECO NON ROUTINE NO.9479563, SPE C NO.B777-25-3-7250. PERFORMED BY , REPLACED M/D R2 DOOR M33098 EMER LT POW ER PACK AND C/O NEW POWER PACK TEST,THE RESULT FOUND NORMAL AS P ER AMM 33-51-06-960-803 REV 100.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 115,209 hrs · 11,888 cycles

M/D L4 DOOR 1EA EMER LT POWER PACK (M33407) FOUND LOW CAPACITY,O RIGINATED BY, REF TO HAECO NON ROUTINE NO.9479556 SPE C NO.B777-25-3-7250. PERFORMED BY , REPLACED M/D L4 DOOR M33407 EMER LT POW ER PACK AND C/O NEW POWER PACK TEST. THE RESULT FOUND NORMAL AS P ER AMM 33-51-06-960-803 REV 100.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 115,209 hrs · 11,888 cycles

M/D R1 DOOR CEILING PANEL M33094 EMER LT POWER PACK FOUND LOW CA PACITY,ORIGINATED BY, REF TO HAECO NON ROUTINE NO.948 1100 SPEC NO.B777-25-3-7250. PERFORMED BY , REPLACED THE M/D R1 DOOR CEILING PANEL M33094 EMER LT POWER PACK AND C/O THE NEW POWER PACK TEST THE RE SULT FOUND NORMAL AS PER AMM 33-51-06-960-803 REV 100,IDT .

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 115,209 hrs · 11,888 cycles

M/D L1 DOOR CEILING PANEL M33093 EMER POWER PACK FOUND LOW CAPAC ITY,ORIGINATED BY , REF TO HAECO NON ROUTINE NO.948110 1 SPEC NO.B777-33-3-7019. PERFORMED BY, REPLACED M/D L1 DOOR CEILING PANEL M330 93 EMER POWER PACK AND C/O TEST OF THE NEW POWER PACK,THE RESULT FOUND NORMAL,AS PER AMM 33-51-06-960-803 REV 100.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 115,209 hrs · 11,888 cycles

M/D L2 DOOR 1EA EMER LT POWER PACK (M33099) FOUND LOW CAPACITY,O RIGINATED BY , REF TO HAECO NON ROUTINE NO.9479561 SPE C NO.B777-25-3-7250. REPLACED M/D L2 DOOR M33099 EMER LT POW ER PACK AND C/O NEW POWER PACK TEST,THE RESULT FOUND NORMAL AS P ER AMM 33-51-06-960-803 REV 100,IDT BY.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 115,209 hrs · 11,888 cycles

M/D L3 DOOR 1EA EMER LT POWER PACK (M33405) FOUND LOW CAPACITY,O RIGINATED BY ,REF TO HAECO NON ROUTINE NO.9479572 SPE C NO.B777-33-3-7019. REPLACED M/D L3 DOOR M33405 EMER LT POW ER PACK AND C/O NEW POWER PACK TEST,THE RESULT NORMAL AS PER AMM 33-51-06-960-803 REV 100,

Part: APU — ODOR (APU BAY) · airframe 115,093 hrs · 11,876 cycles

CREW REPORTED ELECTRICAL BURNING SMELL TOWARDS END OF FLIGHT. CONTACT TOMC A/C EXTENSIVELY EXAMINED, UNABLE TO LOCATE BURNING SMELL. APU STARTED AND AIR CONDITIONING PACKS OPERATED, SMELL WAS VERY OBVIOUS THROUGHOUT A/ C AND FLIGHTDECK WITH AIR CONDITIONING OPERATING, SUSPECT APU BLEED AS BURNING SMELL. MEL REQUIRED FOR APU BLEED DEFERRAL. FOR INFO. CABIN CREW SMOKE/ODOR QUESTIONAIRE ATTACHED. MEL 4952A SEPERATE LOG PAGE FOR APU BLEED REF PARA E (3) NIL EVIDENCE OF FLUID INGESTION. NIL DAMAGE NOTED TO APU INLET SCREEN. APU CHECK VALVE REMOVED FOR ACCESS, APU BLEED DUCT DOES NOT APPEAR WET OR EVIDENCE OF RESIDUAL OIL. CHECK VALVE REFITTED REF AMM 49-52-03 APU CONTROL SURGE VALVE REMOVED AS PER AMM 49-53-01-000-801. NO LEAK OR OIL RESIDUE APPARENT INSIDE VALVE AND CONNECTING DUCTS. PICTURE ADDED FOR REFERENCE. ACP''D CONDITIONAL INSPECTION 05-51-58-800-801-C3. SEE LOG 6969429. CONTINUED FROM SECTION E., (1), (A), BOTH ENG RUN AND PACKS OPERATED FOR MORE THAN 2 HOURS. SMOKE/ODOR DID NOT DISSIPATE. REF FIM 21-00 TASK 808, ACP''D ITEMS D., (10), EXCEPT FOR FURTHER INFO, ALSO SEE LP 6969429 FOR CONDITIONAL INSPECTION 05-51-58-800-801-C3 UP TO PARAGRAPH ''E'' LP 6961664 SHOWS APU OIL LEVEL SERVICED ON ARRIVAL TO LHR AND LP 6972130 SHOWS ANOTHER 4 QTYS ADDED TO APU POST ENGINE RUNS. SEE LP 6974034 FOR APU MAG CHIP INSPECTION APU. APU CONTROL SURGE VALVE REFITTED AS PER AMM 49-53-01 UNLOCKING FOR FIX OIL SMELL VERIFIED TO BE FROM DEFECTIVE APU BLEED.

Part: TIRE — LOW PRESSURE (LEFT NLG) · airframe 111,628 hrs · 11,503 cycles

LEFT NOSE TIRE LOW PRESSURE FOUND LEFT NLG TIRE WITH 53 PSI, REMOVED AND REPLACED LEFT NLG WHEEL ASSY IAW AMM TASK 32-45-02/401. PARTS USED: 1983092,QTY :1 ADD EMP:U312251,U362187 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1983092 SN OFF 0973 IPC REFERENCE # 32-45-02-05C WHEEL, ASSY, NL OFF 0000 ON 25-3245-9-0001 8973

Part: BATTERY PACK — INOPERATIVE (R4 DOOR) · airframe 108,673 hrs · 11,174 cycles

TEST FOUND DOOR R4(M33409) EMERGENCY LT CAN NOT STAY ON FOR 15 MINUTES REFER HAECO NON-ROUTINE NO.9494656 - ORIGIANTED BY EMP V905359 SPEC NO.B777-33-3-7019 REPLACED EMERGENCY LT BATT PACK AT DOOR R4 (M33409) AND TESTED FOUND NORMAL PER AMM 33-51-06-960-802 REV 96,PERFORMED BY EMP V9 05359 IDT BY EMP V905466.(ON PN ADD717-01-100 SN 297136;OFF PN A DD 717-01-100 SN 177950)

Part: BATTERY PACK — NO TEST (L2) · airframe 108,673 hrs · 11,174 cycles

TEST FOUND DOOR L2 (M33096) EMERGENCY LT CAN NOT STAY ON FOR 15 MINUTES REFER HAECO NON-ROUTINE NO.9494652 - ORIGINATED BY EMP V 905359 SPEC NO.B777-33-3-7019 REPLACED EMERGENCY LT BATT PACK AT DOOR L2 (M33096) AND TESTED FOUND NORMAL PER AMM 33-51-06-960-802 REV 96,PERFORMED BY EMP V9 05359 IDT BY EMP V905466.(ON PN ADD717-01-100,SN 297122;OFF PN A DD717-01-100 SN 231393)

Part: BATTERY PACK — NO TEST (R2 DOOR) · airframe 108,673 hrs · 11,174 cycles

TEST FOUND DOOR R2 (M33098) EMERGENCY LT CAN NOT STAY ON FOR 15 MINUTES REFER HAECO NON-ROUTINE NO.9494653 - ORIGINATED BY EMP V905359 SPEC NO.B777-33-3-7019 REPLACED EMERGENCY LT BATT PACK AT DOOR R2 (M33098) AND TESTED FOUND NORMAL PER AMM 33-51-06-980-802 REV 96,PERFORMED BY EMP V9 05359 IDT BY EMP V905466.(ON PN ADD717-01-100 SN 213162;OFF PN A DD 717-01-100 SN 206127)

Part: BATTERY PACK — NO TEST (L1 DOOR) · airframe 108,673 hrs · 11,174 cycles

TEST FOUND L/H DOOR 1 AREA EMER LT CAN NOT STAY ON FOR 15 MINITE S (M33424) REFER HAECO NON-ROUTINE NO.9493056 - ORIGINATED BY EM P V903689 SPEC NO.B777-33-3-7019 REPLACED LH DOOR 1 EMERGENCY LT BATT PACK M33424 AND TESTED FND NORMAL PER AMM 33-51-06-960-802 REV 96,PERFORMED BY EMP V905359 IDT BY V905466.(ON PN ADD717-01-100,SN 187236;OFF PN D717-01-100 SN 423479)

Part: BATTERY PACK — NO TEST (L4 DOOR) · airframe 108,673 hrs · 11,174 cycles

TEST FOUND DOOR L4(M33407) EMERGENCY LT CAN NOT STAY ON FOR 15 MINUTES REFER HAECO NON-ROUTINE NO.9494655 - ORIGINATED BY EMP V905359 SPEC NO.B777-33-3-7019 REPLACED EMERGENCY LT BATT PACK AT DOOR L4 (M33407) AND TESTED FOUND NORMAL PER AMM 33-51-06-960-802 REV 96,PERFORMED BY EMP V9 05359,IDT BY V905466.(ON PN ADD717-01-100,SN 29111;OFF PN ADD717 -01-100,SN 156268)

Part: BATTERY PACK — NO TEST (L3 DOOR) · airframe 108,673 hrs · 11,174 cycles

TEST FOUND DOOR L3 (M33406) EMERGENCY LT CAN NOT STAY ON FOR 15 MINUTES REFER HAECO NON-ROUTINE NO.9494654 - ORIGINATED BY EMP V 905359 SPEC NO.B777-33-3-7019 REPLACED EMERGENCY LT BATT PACK AT DORO L3(M33406) AND TESTED FO UND NORMAL PER AMM 33-51-06-960-802 REV 96,PERFORMED BY EMP V905 359,IDT BY V905466.(ON PN ADD717-01-100 SN 297123;OFF PN D717-01 -100 SN 317944)

Part: NONE — LEAKING (ENG2) · airframe 105,143 hrs · 10,639 cycles

OIL PRESSURE INDICATION (ENGINE) AMBER FIM TASK REF : G1 79-98 TASK 803 CMC MSG# 7931492 FLIGHT STATUS: A INTERMITTENCE CODE: M PH: CRUISE NARRATIVE: ELECTRONIC ENG CONTROL (FADEC)(R ENG,CH A) CMC MSG# 7931492 FLIGHT STATUS: A INTERMITTENCE CODE: M PH: CRUISE NARRATIVE: UPON INSPECTION OF #2 ENG, FOUND 1 ANTI-LEAK VALVE CAP FOR MAIN INSPECTION AS REQUIRED. REF AMM 79-21-12 FOR DMS SENSOR DURING IDLE RUN WAS STABLE @ 32PSI. #2 ENG OIL QTY STABLE AND OIL TANK LINE AT 6OCLOCK POS ON BOTTOM OF FAN COWL AND VALVE INSPECTION, NO DEBRIS NOTED, TEST PASSED. REF AMM 79-21-08 FOR FULL. IMAGE OF #2 ENG INDICATIONS DURING IDLE LEAK CHECK ADDED LEAKING ENG OIL. 2ND ANTI LEAK VALVE @6 OCLOCK POSTION FOUND NO ANTI-LEAK VALVE AND CAP R&R AT 6 OCLOCK POSTION UNDER UNDER FAN TO LOG PAGE. DISCREPENCIES, BUT CHANGED DUE TO PRECAUTIONARY MEASURES. REF COWL. PERFORMED ENG IDLE LEAK TEST AS NEEDED FOR VALVE, CAP R&R LOG PAGE 71-00-00-200-812-G00, PERFORMED INFLIGHT WINDMILLING AND DMS SENSOR INSPECTION. NO LEAKS NOTED. #2 ENG OIL PRESSURE

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 103,547 hrs · 10,338 cycles

AD 2018-14-02 SUPPORT TASK- DR 4R EMER LIGHT PWR SUPPLY M33408 T EST FAIL.REFER NR L/P:9131218 DR 4R EMER LIGHT BATTERY PACK AND CHARGER REPLACED AS PER AMM 33-51-06 AND TESTED NORMAL AS PER AMM 33-51-06.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 103,547 hrs · 10,338 cycles

AD 2018-14-02 SUPPORT TASK- DR 2R EMER LIGHT PWR SUPPLY M33097 T EST FAIL. REFER NR L/P:9131217. REPLACED DR 2R EMER LIGHT BATTERY PACK AND TESTED NORMAL AS PER AMM 33-51-06.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 103,547 hrs · 10,338 cycles

AD 2018-14-02 SUPPORT TASK - DR 1R EMER LIGHT PWR SUPPLY M33094 TEST FAIL REF NR LP 9131215 DR 1R EMER LIGHT PWR SUPPLY M33094 BATTERY REPLACED AND TESTED N ORMAL AS PER AMM 33-51-06 ADD EMP:V896958

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 103,547 hrs · 10,338 cycles

B777-33-3-7019 DR 3L EMER LIGHT POWER SUPPLY M33405 BATTERY PACK CAPACITY CHECK FAIL REF NR LP 9130101 DR 3L EMER LIGHT POWER SUPPLY M33405 BATTERY REPLACED AND TESTED NORMAL AS PER AMM 33-51-06 ADD EMP:V896958

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 103,547 hrs · 10,338 cycles

AD 2018-14-02 SUPPORT TASK - DR 2R EMER LIGHT PWR SUPPLY M33098 TEST FAIL REF NR LP 9131216 DR 2R EMER LIGHT PWR SUPPLY M33098 BATTERY REPLACED AND TESTED NORMAL AS PER AMM 33-51-06 ADD EMP:V896958

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 103,547 hrs · 10,338 cycles

B777-33-3-7019 - DR 3L EMER LIGHT POWER SUPPLY M33400 BATTERY CA PACITY CHECK FAIL REF NR LP 9130102 DR 3L EMER LIGHT POWER SUPPLY M33400 BATTERY REPLACED AND TESTED NORMAL AS PER AMM 33-51-06 ADD EMP:V896958

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 103,547 hrs · 10,338 cycles

B777-33-3-7019 DR 2L EMER LIGHT POWER SUPPLY M33099 BATTERY PACK CAPACITY CHECK FAIL REF NR LP 9130100 DR 2L EMER LIGHT POWER SUPPLY M33099 CHARGER AND BATTERY REPLACE D AND TESTED NORMAL AS PER AMM 33-51-06 ADD EMP:V896958

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 103,547 hrs · 10,338 cycles

B777-33-3-7019 DR 3R EMER LIGHT POWER SUPPLY M33401 BATTERY PACK CAPACITY CHECK FAIL REF NR LP 9130103 DR 3R EMER LIGHT POWER SUPPLY M33401 BATTERY AND CHARGER REPLACE D AND TESTED NORMAL AS PER AMM 35-51-06 ADD EMP:V896958

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 101,855 hrs · 10,118 cycles

B777-33-3-7031 DR R3 M33404 EMER LIGHT POWER SUPPLY BATTERY CAPA CITY LOW REF NR LP 9130154 DR R3 M33404 EMER LIGHT POWER SUPPLY CHARGER BATTERY REPLACED AN D TESTED NORMAL AS PER AMM 33-51-06

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 101,855 hrs · 10,118 cycles

B777-33-3-7031 DR R1 EMER LIGHT POWER SUPPLY M33094 BATTERY PACK CAPACITY LOW REF NR L/P 9130151 DR R1 EMER LIGHT POWER SUPPLY M33094 BATTERY PACK REPLACED AND T ESTED NORMAL AS PER AMM 33-51-06.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 101,855 hrs · 10,118 cycles

B777-33-3-7031 DR L2 EMER LIGHT POWER SUPPLY M33099 BATTERY PACK CAPACITY LOW REF NR LP 9130153 DR L2 EMER LIGHT POWER SUPPLY M33099 BATTERY PACK REPLACED AND T ESTED NORMAL AS PER AMM 33-51-06.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 101,855 hrs · 10,118 cycles

B777-33-3-7031 DR R3 M33401 EMER LIGHT POWER SUPPLY BATTERY PACK CAPACITY LOW REF NR LP 9130152 DR R3 M33401 EMER LIGHT POWER SUPPLY BATTERY PACK REPLACED AND T ESTED NORMAL AS PER AMM 33-51-06 ADD EMP:V898181 IDT INSPECTION OK

Part: SKIN — CRACKED (BS 508) · airframe 101,035 hrs · 10,036 cycles

REF LP 3522239 LIGHTNING STRIKE DEFERRED PER OPERATIONAL LIMITS WILL NEED SRM REPAIR INSTALLED HFEC PERFORMED REF STEP B (2) PERFORMED STEPS A,B AND C OF SRM 53-00-01 REPAIR 4 PARA 4, NEED INSPECTED AREA PER SRM 53-00-01 REPAIR 4 PARA 4 STEPS A, B,C. HFEC C/W PER NDT 6-51-00-01. NO CRACKS FOUND. STA. 508 STR 46R. 2024-T3 CLAD PO# 9944459 REF SRM 53-00-01 REPAIR 4 NEED TO VERIFY REPAIR DOUBLER AND FILLER MATERIAL AS 0.100" 53-00-01 REPAIR 4. VERIFIED MATERIAL AS 0.100 " 2024-T3 CLAD . PO: 9944459. SRM REPAIR 4 STEP 4.F.(1) AND SRM 51-10-02. ZERO-TIMED EXISTING HOLES IN CRITICAL ROW REF. SRM 53-00-01 REF. SRM 53-00-01 REPAIR 4.F.(1) AND SRM 51-10-02. PERFORMED OPEN FASTENER HOLE HFEC OF EXISTING HOLES IN THE CRITICAL ROW PER 777 NDT MANUAL PART 6 51-00-02 PROCEDURE 3. COMPLIED W STEPS D,E, F, AND G OF SRM 53-00-01 REPAIR 4 PARA 4. C/W STEP 4H OF REPAIR 4 SRM 53-00-01. NEED OK TO TREAT AND PRIME REPAIR PARTS. T AND PRIME REPAIR PARTS.. VERIFIED C/W SRM 53-00-01 REPAIR 4, STEPS 4.D THRU H. OK TO TREA DOES NOT APPLY TO THIS REPAIR PER FIG. 204 REPAIR DOUBLER THICKNESS & FASTENER SIZE ELIMINATES PRODUCTION COUNTERSINKS. COMPLIED WITH STEPS 4 I & J PER SRM 53-00-01 REPAIR 4. STEP 4K PRODUCTION COUNTERSINKS. REF: REPAIR FIG. 204. OK TO INSTALL PARTS. VERIFIED C/W STEPS 4.I & J. OF SRM 53-00-01 REPAIR 4. STEP 4.K DOES NOT APPLY TO THIS REPAIR. OVERSIZE FASTENER ELIMINATES COMPLIED WITH STEPS 4. L, M, N, & O PER SRM 53-00-01 REPAIR 4. REPAIR 4. VERIFIED COMPLIANCE WIT

Part: NOT REPORTED — LEAKING (WASTE WATER) · airframe 99,428 hrs · 9,867 cycles

WATER LEAKING FROM BELLY OF AFT CARGO PIT. LOWER AFT FUSELAGE LEAKING GRAY WATER FROM AFT AND BULK CARGO COMPARTMENT FUSELAGE DRAINS. SPILL COVERAGE AREA IS FROM STA. 1455 TO STA. 2062 AND FROM S-47(L) TO S-47(R). C/W IMEDIATE CLEANUP REF ECRA 2011-01000 CARGO COMP SPILL SECTION 2.B 1-10. APPROX AREA OF SPILL FROM BODY STA. 1455 TO STA. 2062 AND BL47(L) AND BL47(R). WILL REQUIRE INDEPTH CLEAN UP. REQUEST W/I 7 DAYS ACCP ECRA2011-01000AA CARGO COMP SPILL SEC 2. B, INDEPTH CLEANUP, IN APPROX AREA FROM BS1455 TO BS 2062 BTWN BL 47(L) TO BL 47(R). ACCOMPLISH IN DEPTH CLEANUP WITHIN 7 DAYS. TOMC-APPROVAL. RECORDS UPDATE. REMOVED FOR ACCESS THREE CENTER ROWS OF AFT PIT FLOORBOARDS FROM FWD BLKHD TO BALL MAT AND FWD CTR BALL MAT. TOMCQC REV PERFORMED. ACCOMPLISHED IN DEPTH CLEANUP FROM BS1455 TO BS2062 BL47L TO BL4. 7R ALL REMOVED FLOORBOARDS INCLUDING BULK PIT INSTALLED. REF ECRA 2011-01000 AND AMM 25-80-99 AND 25-52-10

Part: BATTERY PACK — LOW (CABIN) · airframe 94,805 hrs · 9,391 cycles

OHAR EMER LT POWER SUPPLY BATTERY CAPACITY LOW. OHAR EMER LT POWER SUPPLY BATTERY PACK REPLACED AND TESTED NORMAL AS PER AMM 33-51-06.

Part: BATTERY PACK — LOW (CABIN) · airframe 94,805 hrs · 9,391 cycles

DOOR R3 EMER LIGHT POWER SUPPLY M3 3404 BATTERY CAPACITY LOW. DOOR R3 EMERG LIGHT POWER SUPPLY M33404 BATTERY PACK REPLACED AND TESTED NORMAL AS PER AMM 33-51-06.

Part: BATTERY — LOW (CABIN) · airframe 94,805 hrs · 9,391 cycles

DOOR 2R EMER LIGHT POWER SUPPLY M3 3097 BATTERY LOW CAPACITY. DOOR 2R EMERG LIGHT POWER SUPPLY M33097 BATTERY PACK REPLACED AND TESTED NORMAL AS PER AMM 33-51-06.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 94,805 hrs · 9,391 cycles

EMER LT POWER SUPPLY CHARGER (M33093) FOUND INOP. EMER LT POWER SUPPLY CHARGER REPLACED AND TESTED NORMAL AS PER AMM 33-51-06.

Part: BATTERY — DISCHARGED (CABIN) · airframe 94,805 hrs · 9,391 cycles

EMER LT POWER SUPPLY (M33093) BATTERY FOUND LOW CAPACITY. EMER LT POWER SUPPLY BATTERY REPLACED AND TESTED NORMAL AS PER AMM 33-51-06.

Part: BATTERY — DISCHARGED (CABIN) · airframe 94,805 hrs · 9,391 cycles

EMER LT POWER SUPPLY (M33401) BATTERY FOUND LOW CAPACITY. EMER LT POWER SUPPLY BATTERY REPLACED AND TESTED NORMAL AS PER AMM 33-51-06.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 91,587 hrs · 9,062 cycles

EXTERIOR EMERGENCY LIGHT INOPERATIVE AT THE L4 DOOR. REPLACED THE LAMPS. OPS CHECKED GOOD.

Part: BATTERY PACK — FAULTED (EMERGENCY LIGHTS) · airframe 89,165 hrs · 8,837 cycles

EMERGENCY LIGHTS COME ON INTERM AT L4 AND R4 DOORS. REPLACED BATTERY PACK AND TESTED OK IAW AMM TASK 33-51 -06-960-802.

Part: SKIN — DENTED (BS 355) · airframe 88,514 hrs · 8,785 cycles

FOUND A DENT AT BS 355 JUST FWD OF THE E & E DOOR, JUST BELOW STRINGER 47R. COMPLIED WITH FPI INSPECTION OUTSIDE ONLY IAW ESC170314-0008. PERFORMED STEPS 5 & 6 OF ESC 170314-00081A -1, STEP 3. NO CRACK INDICATIONS NOTED.

Part: FUSE — FAILED (POWER SUPPLY) · airframe 85,319 hrs · 8,510 cycles

ON CHECK FOUND TWO AISLE EMERGENCY LIGHTS NOT ILLUMINATED AT BS 1800 . M33409 POWER SUPPLY FUSE REPLACED IAW AMM 33-51-06-960-801 AND TESTED OK

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 76,041 hrs · 7,693 cycles

DOOR 3 LT EMER LIGHT FOUND DIM. REPLACED & TESTED NORMAL IAW AMM 33-51-06.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 76,041 hrs · 7,693 cycles

DOOR 4 RT EMER LIGHT FOUND DIM. REPLACED & TESTED NORMAL IAW AMM 33-51-06.

Part: VIDEO MONITOR — OVERHEATED (CABIN) · airframe 74,680 hrs · 7,579 cycles

SEAT 38D IFE SCREEN BECAME HOT & HAD A METRICALLY BURNING SMELL. FOLLOWED THE CHECKLIST & SOLVED THE PROBLEM. REPLACED VIDEO MONITOR AT SEAT 38D, OPERATIONS CHECKED OK.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 69,617 hrs · 7,143 cycles

R2 DOOR EMERGENCY LIGHT BATTERY FOUND TO HAVE FAILED. BATTERY REPLACED AND OPS CHECKED NORMAL IAW AMM 33-51-06.

Part: BATTERY — NO TEST (R-3 DOOR) · airframe 69,617 hrs · 7,143 cycles

R3 DOOR EMERGENCY LIGHT BATTERY PACK CAPACITY CHECK FAILED. BATTERY PACK REPLACED AND OPS CHECKED NORMAL IAW AMM 33-51-06.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 69,617 hrs · 7,143 cycles

L2 DOOR EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. BATTERY PACK REPLACED AND OPS CHECKED NORMAL AS IAW AMM 33-51-06.

Part: BATTERY PACK — FAILED (L1 DOOR) · airframe 69,617 hrs · 7,143 cycles

CABIN L1 DOOR EMERGENCY LIGHT BATTERY CAPACITY CHECK FAILED. BATTERY REPLACED AND OPS CHECKED NORMAL IAW AMM 33-51-06.

Part: BATTERY — NO TEST (L3 DOOR) · airframe 69,617 hrs · 7,143 cycles

L3 DOOR EMERGENCY LIGHT BATTERY CAPACITY CHECK FAILED. BATTERY PACK REPLACED AND OPS CHECKED NORMAL IAW AMM 33-51-06.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 69,617 hrs · 7,143 cycles

R4 DOOR EMERGENCY LIGHT BATTERY CHECK FAILED. BATTERY REPLACED AND OPS CHECKED NORMAL IAW AMM 33-51-06.

Part: SKIN — DENTED (NR 4 SLAT) · airframe 67,598 hrs · 6,970 cycles

DENT ON L/E OF NR 4 SLAT, APPROX 48" FROM INBD END. PERFORMED INTERIM REPAIR IAW PART 1 OF EC/RA 5743-01131.

Part: UNKNOWN — ODOR (CABIN) · airframe 61,012 hrs · 6,366 cycles

STRONG ODOR EMANATING FROM AREA OF ROW 38F-J ZONE. PASSENGERS IN THAT AREA COMPLAINED OF EYE IRRITANTS. NO ODOR AND NO CONTAMINATION OF PESTICIDE OR FERTILIZER. CHECKED THESE AREA, OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,410 hrs · 6,206 cycles

SOME CEILING EMERGENCY EXIT LIGHT CONTINUE TO ILLUMINATE AFTER NUMEROUS RESETS. FIVE ADJACENT LIGHT BEHIND DOOR 2L STAY ON EMERGENCY LIGHT SYSTEM NOT OPERATING CORRECTLY CHANGED ATA 3300 TO 3320. RESET DONE ON ELEC PLUG DM33099 BATTERY PACK CHECK FOR OPER IAW M/M 33-51-06 SYS OK.

Part: PSU — INOPERATIVE (CREW REST) · airframe 48,353 hrs · 5,209 cycles

DURING TEST FLIGHT O2 MASK DID NOT DEPLOY IN CREW REST OVERHEAD AREA AFT POSITION. PSU ASSY REPLACED AND DROP TEST PERFORMED FOUND NORMAL AMM 35-21-15.

Part: NOZZLE — FAILED (ENGINE)

ENGINE SUFFERED AN OVERTEMP AND HPC/HPT ROTOR VIBRATION EXCCEEDANCE. THE CUSTOMER REPORTED METAL PARTICLES IN THE EXHAUST. DURING ENGINE MODULE DISASSEMBLY AT MFG, IT WAS NOTED THAT THE HPT STAGE 2 NOZZLE ASSY EXHIBITED SIGNIFICANT HARDWARE DAMAGE TO THE NOZZLE SEGMENTS, STAGE 1 AND STAGE 2 SHROUDS. (K)

Part: SCREEN — CLOGGED (IFE COOLING) · airframe 24,942 hrs · 2,924 cycles

THE FLIGHT CREW REPORTED THAT THE IFE (INFLIGHT ENTERTAINMENT) CMT UNIT WAS OVERHEATING WHILE EN ROUTE FROM TLV TO EWR. THE AIRCRAFT WAS DIVERTED TO MXP WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THAT THE FORWARD IFE AIR VENT SCREEN OVER IFE CONTROL STATION WAS PLUGGED WITH LINT AND DIRT IN THE OVERHEAD AREA. THIS PREVENTED THE IFE CMT UNIT FROM GETTING COOLING AIR. THERE WERE NO SIGNS OF ELECTRICAL BURNING AND BOTH IFE FANS WERE WORKING. THE CMT WAS REPLACED. THE AIR VENT SCREEN WAS CLEANED. OPERATION OF THE IFE COOLING SYSTEM CHECKED GOOD IAW MM 21-27-700-803. AN FCD WAS ISSUED TO INSPECT THE REST OF THE FLEET.

Part: STRUT — CRACKED (RT MLG) · airframe 24,216 hrs · 2,835 cycles

INSPECTION FOUND THE RT MLG SHOCK STRUT LEAKING FLUID FROM TOP OF THE OUTER CYLINDER. THE INNER AND OUTER CYLINDERS WERE REMOVED. THE ORIFICE SUPPORT TUBE WAS REMOVED FROM THE OUTER CYLINDER AND FOUND TO BE CRACKED THROUGH. THE INSIDE DIAMETER OF THE OUTER CYLINDER WAS INSPECTED AND NO DAMAGE WAS FOUND. A NEW ORIFICE SUPPORT TUBE WAS INSTALLED ON THE EXISTING OUTER CYLINDER WHICH WAS REINSTALLED. THE SHOCK STRUT WAS FULLY SERVICED AND LEAK AND OPERATIONAL CHECKS WERE GOOD. THE ORIFICE SUPPORT TUBE WAS SENT TO BOEING FOR INVESTIGATION AND ANALYSIS.

Part: SKIN — DENTED (FUSELAGE) · airframe 19,234 hrs · 2,222 cycles

INSPECTION FOUND FUSELAGE SKIN DENTED AT FORWARD LT SIDE THREE FEET FORWARD OF L-2 DOOR AT BS 678, STRINGER 27L. THE SKIN WAS REPAIRED IAW SRM 53-00-01, REPAIR 4. A DIP WAS INITIATED TO REINSPECT THE REPAIR AT 30,000 FLIGHT CYCLES WITH INTERVALS OF 16,000 FLIGHT CYCLES.

Part: BEAM — DENTED (CARGO DOOR) · airframe 19,238 hrs · 2,223 cycles

INSPECTION FOUND FORWARD CARGO DOOR UPPER EDGE BEAM WEB DENTED. REPAIRED IAW ECRA 5230-01721.

Part: SKIN — DEFORMED (CARGO DOOR) · airframe 19,234 hrs · 2,222 cycles

INSPECTION FOUND AFT CARGO DOOR FORWARD LOWER CORNER SKIN DEFORMED. REPAIRED IAW SRM 52-30-01, FIGURE 202, REPAIR 17, SHEET 5.