N647GT

Part: ELT — UNKNOWN (UNKNOWN) · airframe 85,046 hrs · 24,230 cycles

FOUND PORTABLE ELT SEAL BROKEN ON PRE-FLIGHT(<P>REMOVED AND REPLACED PORTABLE ELT REF AMM 25-63-03</P>)

Part: BATTERY — UNKNOWN (UNKNOWN) · airframe 85,001 hrs · 24,207 cycles

CREW REPORTS FLASHLIGHT IN GALLEY, RED LIGHT NOT FLASHING.(<P>R/R FLASHLIGHT BATTERY IAW 767 AMM 25-00-00. OPS CHECK GOOD</P>)

Part: OXYGEN MASK — UNKNOWN (UNKNOWN) · airframe 84,842 hrs · 24,123 cycles

FO COMM INOP(<P>R/R FO OXYGEN MASK ASSY IAW 35-11-51. OPS &AMP; LEAK CHECK GOOD. DMI 194696 CLOSED.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 84,747 hrs · 24,069 cycles

CLIMBING THROUGH FL 300 CABIN ALTITUDE EICAS PRESENTED FOLLOWED SHORTLY BY MAIN CARGO DOOR WARNING LIGHT ON FIRST OFFICER FWD PANEL. DECLARED MAYDAY DUE TO INABILITY TO MAINTAIN CABIN PRESS.(<P>FOUND ON ARRIVAL, MAIN CARGO DOOR VENT PANEL IN OPEN POSITION, FOUND MAIN CARGO DOOR IN UNLOCK POSITION ON CARGO DOOR CONTROL PANEL IN GALLEY. INSPECTED CARGO DOOR FOR DEFECTS AND OPERATIONAL GVI. DOOR OPERATES AND FUNCTIONS NORMAL IAW BOEING 767 AMM 52-31-00. NO DEFECTS NOTED. DOOR LOCKS VISUALLY CHECKED CLOSED AND LEAKED. INDICATIONS SYSTEMS OPS NORMAL. PERFORMED CABIN PRESSUE LEAK TEST IAW BOEING 767 AMM 05-51-24. NO EXCESSIVE LEAKS NOTED, DIFFRENTIAL PRESSURE TAKEN TO 4.0 PSI SYSTEM. OPS CHECK NORMAL.&NBSP;</P>)

Part: SWITCH — UNKNOWN (UNKNOWN) · airframe 84,587 hrs · 23,993 cycles

EMERGENCY LT "UNARMED" LT HALF LT NOT ILLUMINATED (RELAMPED NO HELP) & CAP DEFORM(<P>1) CHECK DRAWER DAMAGED AND "UNARMED" CAP DEFORM REP IPC 33-16-02-03 ITEM 12 &AMP; 40. 2) IAW SWPM 20-84-18 R/R SW AND OPS CHECK OK IAW AMM 33-51-00.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 84,286 hrs · 23,844 cycles

DURING T/O, ESCAPE REEL CAME OUT, NEEDS RE-STOW(<P>FOUND ONE OF THE ESCAPE REELS UNLATCHED. RE-STOWED ESCAPE REEL. LATCHED AND CLOSED REEL PER AMM 25-61-02</P>)

Part: ELT — DAMAGED · airframe 83,581 hrs · 23,343 cycles

ELT BROKEN SEAL(<P>R/R ELT IAW AMM 25-63-03. OPS CHECK GOOD. MDDR 169983 CLOSED.</P>)

Part: NONE — NONE · airframe 83,178 hrs

FOUND BROKEN WIRE ON OXYGEN #2 TRANSDUCER (WIRE BROKEN FROM BIN)(<P><SPAN>REPIN CONNECTOR D25006 (D) IAW SWPM 20-63-01. OPS CHECK GOOD IAW AMM 35-11-00.</SPAN></P>)

Part: ESCAPE REEL — NONE · airframe 83,124 hrs

FLIGHT DECK, ONE INERTIAL REEL ACCIDENTALLY DEPOYED, 6 REMAIN OPERATIONAL(REMOVED FROM THE A/C).(<P>TRANSFER TO MDDR 162932, PER MEL 25-61-01-01, CAT "C", DUE DATE: 31MAR22. DISP: JA @ 1601Z.</P> / <P>CVG MX-21MAR: LP 1543129, ITEM M4: INSTALLED #1 DESCENT DEVICE IAW AMM 25-61-05. THIS CLEARS DMI # 162932. MCC NOTIFIED, PLACARDS REMOVED. TIME AND INITIALS: 1929Z, JOL.</P>)

Part: ESCAPE REEL — NONE · airframe 83,124 hrs

FOUND #4 DESCENT DEVICE UNREELED.(<P>REMOVED AND REPLACED #4 DESCENT DEVICE IAW AMM 25-61-05.</P>)

Part: BATTERY — NONE · airframe 82,800 hrs

BOTH FLASHLIGHT AND FLASHLIGHT HOLDERS INOP ( (FLIGHT ATTENDANT FLASHLIGHT/HOLDER ASSEMBLIES) )(<P>TRANSFERRED TO MDDR 157940, CAT C, DUE 14DEC21 IAW MEL 25-63-04B.</P> / <P>05DEC21 - LP 1371933 - ITEM# 6 - CVG - REMOVED AND REPLACED BATTERIES IN BOTH EMERGENCY FLASHLIGHTS IAW CMM 25-60-02, OPS CHECK GOOD. THIS CLEARS MDDR 157940, PLACARD REMOVED.</P>)

Part: NONE — NONE

PACKS SEEM TO STAY ON HIGH FLOW(<P><SPAN>RESET PACKS IAW AMM 21-51-14. OPS CHECK GOOD AT THIS TIME</SPAN></P>)

Part: CIRCUIT CARD — FAILED (FIRE DETECTION)

MAIN CARGO FIRE EICAS ON CLIMB OUT. PERFORMED QRH PROCEDURE AND RETURNED TO CVG. MSG WENT AWAY ON SHORT FINAL. PERFORMED MAIN DECK CARGO FIRE TEST. SUSPECT M10427 FIRE OVHT LOGIC TEST CARD. REMOVED AND REPLACED M10427 FIRE OVHT LOGIC TEST CARD IAW 26-10-01. OPS CKS GOOD.

Part: BLOWER — NONE · 22,582 cycles

CARGO DET AIR STATUS MESSAGE(<P>REMOVED AND REPLACED #2 FWD CARGO SMOKE DETECTION BLOWER. OPS CHECK GOOD IAW AMM 26-16-02.</P>)

Part: DETECTOR — NONE

DURING POST FLT INSP DISCOVERED FWD CARGO DET 2 STATUS MESSAGE(<P>TRANSFERRED TO MDDR 155876 IAW MEL 26-16-01-01-01, CAT C.&NBSP;</P> / <P>REMOVED AND REPLACED FWD CARGO DETECTOR IAW AMM 26-16-01. OPS CHECK GOOD. THIS CLEARS MDDR 155876.</P>)

Part: NONE — NONE · airframe 82,670 hrs · 22,567 cycles

T-R UNIT STATUS MESSAGE DISPLAYED.(<P>RESET C/B 6AG ON P6 PANEL IAW B767 FIM 24-32 FAULT TREE 803. NO EICAS MSG SHOWING AT THIS TIME. SYSTEM TEST OK.</P>)

Part: NONE — NONE · airframe 82,643 hrs · 22,550 cycles

THREE CRACKS WERE FOUND ON FLOOR STRUCTURE SUPPORT STRINGER P/N 146T5004-103 FROM BULK CARGO BETWEEN STA 1461 TO STA 1502 AND RBL 25.09 / RBL 36.91(<P>IT WAS REPAIRED PER B767 SRM 53-60-53-2R-0 AND&NBSP;<SPAN>51-70-11 (TYPICAL FORMED SECTION REPAIRS)</SPAN></P>)

Part: NONE — NONE · airframe 82,643 hrs · 22,550 cycles

FRETTING DAMAGE BY CHAFFING BETWEEN THE VERTICAL STABILIZER FAIRINGS AND FUSELAGE SKIN AT STA 1582 TO STA 1640 AND S-2 LH &AMP; RH.(<P>IT WAS REWORKED PER BOEING SR# 4-5226413756</P>)

Part: NONE — NONE · airframe 82,643 hrs · 22,550 cycles

CRACKS WERE FOUND ON FLOOR STRUCTURE SUPPORT STRINGER P/N 146T5006-6 FROM BULK CARGO BETWEEN STA 1439 TO STA 1518 AND LBL 24.20 / LBL 29.36(<P><SPAN>IT WAS REPAIRED PER B767 SRM 53-60-53-2R-0 AND 51-70-11 (TYPICAL FORMED SECTION REPAIRS)</SPAN></P>)

Part: NONE — NONE · airframe 82,643 hrs · 22,550 cycles

DURING NOSE LANDING GEAR SEALS REPLACEMENT, THE NLG WAS DISASSEMBLED AND THE NLG INNER CYLINDER WAS REMOVED. ONCE REMOVED, CORROSION (PITTING) WAS FOUND IN SOME AREAS OF OUTER CYLINDER (SHOCK STRUT)(<P><SPAN>NOSE LANDING GEAR OUTER CYLINDER (SHOCK STRUT) WAS REPAIRED PER LOCAL BLENDING IAW BOEING SR# 4-5205743050.</SPAN></P>)

Part: NONE — NONE · airframe 82,643 hrs · 22,550 cycles

TWO LIGHTNING STRIKES ON THE DIVERTER STRIP OF VERTICAL STABILIZER TIP(<P><SPAN><SPAN>&NBSP;</SPAN><SPAN>DIVERTER STRIP OF VERTICAL STABILIZER TIP WAS REPAIRED BY BLEND-OUT IAW BOEING SR# 4-5219944422</SPAN></SPAN></P>)

Part: SENSOR — NONE

STATUS MESSAGE "NOSE A/G DISAGREE"(<P>TROUBLESHOT PER 767 FIM. NOT COMPRESSED SENSOR S266 WAS REPLACED PER 767 AMM 32-09-08-402-037. OPS CHECK GOOD ON GEAR SWING.</P>)

Part: NONE — NONE · airframe 82,650 hrs · 22,554 cycles

LIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN BETWEEN STA 1373 TO STA 1351 AND S-3RH TO S-4RH(<P><SPAN>DAMAGE ON FUSELAGE SKIN WAS REPAIRED BY BLEND-OUT IAW BOEING SR# 4-5220752308</SPAN></P>)

Part: NONE — NONE · corrosion level 2 · airframe 82,643 hrs · 22,550 cycles

CORROSION DAMAGE ON INBD FACE OF 451T1604-4 SUPPORT BEAM WEB AT STA 478 AND RBL 42.05(<P><SPAN><SPAN>451T1604-4 SUPPORT BEAM WEB WAS REPAIRED BY DOUBLER IAW BOEING SR# 4-5206382380</SPAN></SPAN></P>)

Part: ROD — NONE

DAMAGE OUT OF LIMITS ON INPUT ROD ASSY OF OUTBD, CENTER AND INBD PCA OF RH ELEVATOR(<P>ROD ASSEMBLIES<SPAN>&NBSP;WERE REPLACED</SPAN></P>)

Part: STATUS MESSAGE — ILLUMINATED (FWD CARGO)

FWD CARGO DET 2 STATUS MSG(<P>TRANSFERRED TO DMI 152903 PER MEL 26-16-01-01-01, CAT C, DUE 12SEP21. PLACARD INSTALLED. MCC NOTIFIED.</P>)

Part: WARNING MESSAGE — FALSE INDICATION (FWD CARGO)

FWD CARGO PACK EICAS MESSAGE IMMEDIATELY AFTER TAKEOFF(<P>PERFORMED FIM 21-61 FT 803. NO DEFECT NOTED. AIRCRAFT OK FOR SERVICE.</P>)

Part: SMOKE DETECTOR — FAULTED (FWD CARGO)

FWD CARGO DET 2 STATUS MESSAGE. TRANSFERRED TO MDDR 152088 IAW MEL 26-16-01-01, CAT C, DUE 28AUG21. MCC NOTIFIED. PLACARDS INSTALLED.</P> / <P>REMOVED AND REPLACED #2 FORWARD CARGO SMOKE DETECTOR IAW 767 AMM 26-16-01. OPS CHECK GOOD. THIS CLEARS DMI 152088. MCC NOTIFIED. PLACARDS REMOVED.</P>)

Part: ENGINE — VIBRATION (LEFT) · airframe 81,935 hrs · 22,043 cycles

DURING FLIGHT LEFT ENGINE VIBES , MUCH HIGHER THAN RIGHT ENGINE FAN 3.1 OCCURRED ON MULTIPLE LEGS(<P>PER AMM 71-00-00 POWER PLANT OPERATION LIMITATIONS. FAN VIB OF 3.1 IS WITHIN LIMITS FOR CONTINUED OPERATION.

Part: WARNING MESSAGE — FALSE ACTIVATION

ON DEPT AND IN FLT R BLEED OFF EICAS MSG INTERMITTANT FOR PROLONGED PERIODS. COMPLETED W/ QRH. REPEAT WRITE UP. SEE LP 1461467(<P>REF MEL 21-51-01-01 OPERATION STEP 5, FAULT MSG NML. NO MX ACTION REQUIRED.</P>)

Part: ACM — FAULTED (RIGHT) · airframe 82,439 hrs · 22,405 cycles

R/H PACK INOP MIX MANIFOLD FAULT(<P>DEFERRED R/H PACK IAW MEL 21-51-01-01. CAT C, DMI # 150027, MAINTENANCE FUNCTION C/W, DUE DATE 22 JUL 21. MCC NOTIFIED. PLACARDS INSTALLED.</P> / <P>LP 1362144: REMOVED AND REPLACED ACM PER B767 AMM 21-51-03-004-001 21-51-03-404-016. REACTIVATED PACK FLOW CONTROL SOV PER TASK 21-00-00-00-449-378. OPS CHECK GOOD. THIS CLEARS MDDR 150027.

Part: WARNING LIGHT — FALSE ACTIVATION (FWD CARGO) · airframe 82,439 hrs · 22,405 cycles

FWD CGO BACKUP EICAS MSG ON AIPT, RAN QRH MEASSAGE AND NO ASSOCIATED "FAULT" LIGHT ON OVERHEAD PANEL CLEARED ON ITS OWN.(<P>NO FAULT PRESENT AT THIS TIME FIM 21-61 TREE 922. NO FURTHER ISSUE. OPS CKS OK ON GROUND.</P>)

Part: OIL SYSTEM — LOW (APU) · 22,394 cycles

APU FAULT UPON START ON TAXI IN. APU WOULD NOT START.(<P>OIL QTY LOW. SERVICED APU OIL TO FULL IAW AMM 12-13-04-613-06. APU OPS NORMAL.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT WINDOW)

L FWD WINDOW EICAS MESSAGE, CYCLED SWITCH AND EICAS MESSAGE REMAINED.(<P>PERFORMED OPS CHECK FOR L FWD WINDOW HEAT EICAS MSG IAW AMM 30-41-00. OPS CHECK GOOD.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 82,412 hrs

FWD CGO BACKUP ADVISORY MESSAGE ON DEPARTURE. QRH COMPLETE. MESSAGE CLEARED ON IT'S OWN(<P>PERFORMED FIM 21-61 TREE 922 AND OPS CHECK IAW AMM 21-22-00. NO FAULTS RECORDED AT THIS TIME.&NBSP;</P>)

Part: SMOKE DETECTOR — MALFUNCTIONED (FWD CARGO) · airframe 82,286 hrs

FWD CARGO DET 2 STATUS MSG APU POWER. NO MSG PRESENT ON EXT POWER(<P>DEFERRED TO MDDR# 147806.</P><P>31MAY21 - LOG# 783943 - ITEM 5 - CVG - REMOVED AND REPLACED CARGO SMOKE DETECTOR M325 IAW AMM 26-16-01. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. THIS CLEARS DMI#147806. MCC EDGAR NOTIFIED. PLACARDS REMOVED.</P><P><BR DATA-MCE-BOGUS="1" /></P>)

Part: ENVIRON SYS — FAULTED (FWD CARGO) · airframe 82,277 hrs · 22,291 cycles

AFTER TAKEOFF "FWD CARGO BACKUP" CAUTION MSG. COMPLIED WITH QRH PROCEDURE(<P>PERFORMED OPS CHECK OF FWD CARGO AC SYSTEM IAW AMM 21-28-00. OPS CHECKS GOOD AT THIS TIME</P>)

Part: SHUTOFF VALVE — FAULTED (RIGHT) · airframe 82,213 hrs · 22,243 cycles

AFTER BOTH ENGINES STARTED WITH ISOLATION VALVE CLOSED AND AIR COND PACKS IN AUTO, RT SIDE MANIFOLD PRESS STAYED OPSI WITH ENGINE RUN UP &GT;807. N2. REMOVED AND REPLACED RH PRSOV IAW AMM 36-11-09, LEAK CHECK AND OPS CHECK GOOD. PERFORMED TAKEOFF POWER ENGINE RUN IAW AMM 71-00-00, 36-11-09, PRSOV OPS CHECK GOOD.

Part: SHUTOFF VALVE — FAULTED (RT ENGINE) · airframe 82,207 hrs · 22,239 cycles

"R ENG HPSOV" MESSAGE ON EICAS IN FLIGHT, TRANSFERRED TO MDDR 146639 AS PER MEL36-11-02-02, LOG PAGE 1477650. REMOVED AND REPLACED RT ENGINE HPSOV IAW AMM 36-11-07. LEAK CHECK GOOD, OPS CHECK GOOD. THIS CLEARS DMI 146639. P/N 802170-10 S/N 2006100098. PER FIM 36-10 FT 837 REMOVED AND REPLACED RT HPC IAW AMM 36-11-08. NO LEAKS NOTED, OPS CHECK GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENG BLEED) · airframe 82,204 hrs

R ENG BLEED CAUTION MESSAGE CAME ON AFTER R ENG START, MESSAGE CLEARED ON IT'S OWN AFTER 2 MINS. NO FURTHER DISCEPANCY.(<P>NO MSG PRESENT ON ARRIVAL. PERFORMED OPS CHECK PER AMM 36-11-07 HPSOV/HPC. OPS CHECK NORMAL IAW FIM 36-10&NBSP; F/T 954. NO MSG'S PRESENT.<BR /></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENG BLEED) · airframe 82,204 hrs

R ENG BLEED CAUTION MESSAGE CAME ON AFTER ENG START. MESSAGE CLEARED AFTER PACKS, AUTO, AND ISOLATION VALVE CLOSED.(<P>PERFORMED BITE TEST ON AIR SUPPLY CONTROL SYSTEM IAW B767 AMM 36-23-00. NO FAULT NOTED AT THIS TIME. NO MSG DISPLAY.<BR /></P>)

Part: HEATER — MALFUNCTIONED (R2 WINDOW) · airframe 82,189 hrs

R2 SIDE WINDOW HEAT INOP ( FLIGHT DECK WINDOW HEAT SYSTEMS, NO. 2 (SIDE) WINDOWS )(<P>TRANSFERRED TO DMI# 146048. CAT C DUE 08MAY21. MEL 30-41-01-02. PLACARD INSTALLED.</P><P>29APR21 - 1476651 - ITEM# 4 - CVG -&NBSP;TROUBLESHOT R2 WINDOW HEAT. FOUND RESISTANCE IS OUT OF LIMITS. READING 30 OHMS. TROUBLESHOOTING DONE IAW FIM 30-41 FAULT TREE 803. WINDOW REPLACEMENT REQUIRED DMI 146048 REMAINS OPEN.</P><P><SPAN>2MAY2021 - 1476665: REMOVED &AMP; REPLACED R2 WINDOW PER 56-11-02, OPS CHECK OK, WINDOW HEAT TEST OK, MDDR CLEARED.&NBSP;</SPAN></P>)

Part: NONE — NONE · airframe 82,171 hrs · 22,211 cycles

DURING WALK AROUND FOUND EVIDENCE OF BIRD STRIKE ON RH ENGINE INLET. PERFORMED HPC BOROSCOPE THROUGH PLUGS B1-0, B1-1, B1-6 AND B1-12 IAW AMM 72-00-00-706-146-110. NO DAMAGE NOTED.

Part: WIRE — LOOSE (WINDOW HEAT) · airframe 82,161 hrs · 22,204 cycles

R SIDE WINDOW HEAT INOP ON PREFLIGHT CHECK. (REPEAT WRITE UP)(<P>TRANSFERRED TO MDDR 145899 IAW MEL 30-41-01-02, CAT C, DUE 05MAY21. PLACARD INSTALLED.</P><P>26APR, ATL MX, LP 1481761, ITEM M4: T/S IAW B767 FIM 30-41-801 AND WDM 30-41-11, FOUND WINDOW (R2) SENSOR CORD LOOSE. SECURED SYSTEM, OPS NML. IAW 30-41-00. THIS CLEARS MDDR 145899. MCC NOTIFIED. PLACARD REMOVED. YM 1641Z</P>)

Part: CONTROLLER — MALFUNCTIONED (WINDOW HEAT) · airframe 82,166 hrs · 22,207 cycles

RH SIDE WINDOW HEAT LIGHT "INOP" ILLUMINATED. R2 WINDOW HEAT INOP.(<P>TRANSFERRED TO DMI #145755 IAW MEL 30-41-01-02. CAT C, DUE 03MAY21. MCC NOTIFIED. PLACARD INSTALLED, MX ACTION C/W.</P><P>REF LOG 1477427 ITEM #5: REMOVED AND REPLACED WINDOW HEAT CONTROLLER IAW AMM 30-41-01. OPS CHECK GOOD, THIS CLEARS DMI 145755. MCC NOTIFIED, PLACARD REMOVED.</P>)

Part: IGNITER — FAILED (RT ENGINE) · airframe 82,161 hrs · 22,204 cycles

R ENG IGNITOR 2 STATUS. RIGHT ENGINE WOULD NOT LIGHT IN SINGLE(<P>PLACED ON MEL 74-00-01B, MDDR 145735, CAT C - DUE 02 MAY 2021. PLACARD INSTALLED.</P><P>REMOVED AND REPLACED #2 IGNITOR PLUG REF B767 AMM 74-21-02/401. PERFORMED IGNITION SYSTEM AUDIBLE TEST PER 767 AMM 74-00-00-730-803-H03. SYSTEM OK FOR SERVICE. THIS CLEARS DMI 145735. MCC NOTIFIED. YC 1830Z</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT SHUTOFF VALVE) · airframe 82,120 hrs · 22,173 cycles

RT ENG HPSOV. PERFORMED BITE TEST ON AIR SUPPLY MODULE IAW B767 AMM 36-11-07. NO FAULTS NOTED AT THIS TIME. NO MSG DISPLAY.</P>)

Part: PACKING — DAMAGED (RT IDG) · airframe 82,127 hrs · 22,178 cycles

R GEN DRIVE EICAS MESSAGE DURING INITIAL CLIMB. MESSAGE CLEARED WHEN LEVELING AT 10,000 FT ABOUT 90 SECONDS LATER(<P>REMOVED AND REPLACED&NBSP;PACKING ON RH IDG FILL PORT IAW AMM 20-11-00. NO LEAKS NOTED AT THIS TIME. SERVICED IDG IAW AMM 12-13-03 AND PERFORMED OPS CHECK IAW AMM 24-11-00. NO DEFECTS NOTED.&NBSP;<BR /></P>)

Part: IDG — UNDERSERVICED (RIGHT) · airframe 82,095 hrs · 22,154 cycles

RECEIVED R GEN DRIVE ON TAKEOFF ROLL. MESSAGE CLEARED ON CLIMBOUT OF 10000(<P>SERVICED IDG WITH 1QT IAW 12-13-03-613-027. NO LEAKS NOTED. OK FOR SERVICE.</P>)

Part: SWITCH — MALFUNCTIONED (SMOKE DETECTION) · airframe 82,078 hrs

CARGO DET AIR STATUS MSG.(<P>TRANSFERRED TO MDDR 144723 PER DDG 26-16-01-03-01, CAT C, DUE 12APR21.</P><P>04 APR 21 - LP 1456865 ITEM 13 CVG -&NBSP;REMOVED &AMP; REPLACED SMOKE DET PRESS SWITCH AMM 26-16-03.&NBSP;<SPAN>REMOVED &AMP; REPLACED</SPAN><SPAN>&NBSP;FWD CARGO BLOWER MOTOR IAW AMM 26-16-02.&NBSP;</SPAN><SPAN>REMOVED &AMP; REPLACED</SPAN><SPAN>&NBSP;K331 RELAY SWPM 20-81-12. ALL OPS GOOD.&NBSP;</SPAN></P>)

Part: SMOKE DETECTOR — WARNING MESSAGE (FWD CARGO) · airframe 82,077 hrs · 22,141 cycles

FWD CARGO DETECTOR MSG ON EICAS(<P>TRANSFERRED TO MDDR 144669 IAW MEL 26-16-01-01. PLACARD INSTALLED.</P><P>LP 1456855 - M5 - CVG - REMOVED AND REPLACED AFT CARGO DETECTOR IAW 767 AMM 26-16-01. OPS CHECK GOOD. THIS CLEARS DMI# 144669, PLACARDS REMOVED. MCC NOTIFIED.</P>)

Part: NONE — NONE · airframe 81,979 hrs · 22,073 cycles

DURING THE WALK AROUND THE CREW NOTICED FLUID COMPING FROM APU BAY AREA. UPON INSPT OF APU AND AREA NO LEAK WAS FOUND, ACCUMULATION OF OIL DUE TO AC SITTING. LEAK AND OPS CKS GOOD IAW AMM 49-11-00.

Part: SWITCH — MALFUNCTIONED (RT GENERATOR) · airframe 81,971 hrs · 22,067 cycles

RIGHT GENERATOR IDG DRIVE LIGHT INOP. R ENG GENERATOR INOP(<P>TRANSFERRED TO MDDR 143311, CAT B, IAW MEL 24-00-01-01. PLACARD INSTALLED. AIRCRAFT OK FOR SERVICE.</P><P>ITEM 2: DEFERRAL MDDR 143310 AND MEL 24-11-01-01-01B TRANSFERRED TO MDDR 143311 IAW MEL 24-00-01.</P><P>LP 1229712: REMOVED AND REPLACED RH GEN DRIVE KORRY SW IAW SWPM 20-84-18. OPS CK GOOD. THIS CLEARS MDDR 143311.&NBSP;</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (RT ENGINE) · airframe 81,924 hrs · 22,035 cycles

RIGHT ENG HPSOV STATUS MESSAGE DISPLAYED (PERFORMED BITE PROCEDURE IAW 767 AMM 36-11-00. NO DEFECTS NOTED AT THIS TIME. PERFORMED ENGINE RUNS IAW 71-00-00. OPS CHECKS GOOD.)

Part: SMOKE DETECTOR — MALFUNCTIONED (FWD CARGO) · airframe 81,904 hrs · 22,020 cycles

FWD CARGO DET 2 MSG. REMOVED AND REPLACED FWD CARGO DETECTOR 2 IAW AMM 26-16-01. OPS CHECKS GOOD AT THIS TIME.

Part: FIRE LOOP — MALFUNCTIONED (NR 2 ENGINE) · airframe 81,869 hrs · 21,993 cycles

R. ENG FIRE LP 2. PLACARD INSTALLED. UPON INSPECTION FOUND LOWER AFT FIRE LOOP TERMINAL BROKEN. REMOVED AND REPLACED LOWER AFT FIRE LOOP ASSY ON #2 ENGINE IAW AMM 26-11-02, OPS CHECK GOOD. AP 18887 C/W, THIS CLEARS DMI 142113. MCC NOTIFIED. PLACARDS REMOVED.</P>)

Part: SMOKE DETECTOR — FALSE INDICATION (FWD CARGO) · airframe 81,872 hrs · 21,995 cycles

FWD CARGO DET 2 STATUS MESSAGE(<P>TRANSFERRED TO MDDR # 142124 MEL 26-16-01-01-01 CAT "C" DUE 18FEB21 DT 0935</P><P>DATE 10FEB21 - LP 1333272 ITEM 6 - CVG-&NBSP;REMOVED AND REPLACED FWD CARGO SMOKE DETECTOR 2 IAW AMM 26-16-01. NO DEFECTS NOTED AT THIS TIME. THIS CLEARS DMI 142124. MCC NOTIFIED. PLACARDS REMOVED.</P>)

Part: DUCT — LEAKING (PNUEMATIC SYSTEM) · airframe 81,838 hrs · 21,970 cycles

STATUS MSG "R ENG FIRE LOOP 1 ON CLIMB OUT THEN CLEARED ON TAXI IN(<P>ITEM TRANSFERRED TO MDDR # 141650 IAW MEL 26-11-01-01, CAT C, DUE 09FEB21. PLACARD INSTALLED.</P><P>DATE 31JAN21- LP 1333247 ITEM 8 - CVG - TROUBLESHOT RH ENGINE FIRE DETECTION SYSTEM IAW FIM 26-11 FAULT TREE 804. FOUND PNUEMATIC DUCT LEAK IN PRECOOLER DUCTING. TIGHTENED V-BAND IAW AMM 36-11-15 STEP F21. NO FAULTS FOUND AT THIS TIME. THIS CLEARS DMI 141650. PLACARD RMVD.</P>)

Part: FIRE LOOP — FALSE ACTIVATION (RT ENGINE) · airframe 81,834 hrs · 21,967 cycles

STATUS MESSAGE "RT ENGINE FIRE L1" AFTER ROTATION GOES AWAY AT THE TOP OF DESCENT. HAPPENED LAST TWO FLIGHT LEGS. DUE TO HISTORY AND PREV ACTIONS/TS TAKEN. RESET FIRE DETECT. CARD M689. NO PRESENT LEG FAULT, IAW AMM 26-11-00.

Part: CONNECTOR — LOOSE (FIRE LOOP) · airframe 81,828 hrs · 21,962 cycles

RT ENGINE FIRE LOOP 1 STATUS MESSAGE DISPLAYED ENGINE FIRE DETECTION SYSTEMS, DETECTION LOOPS (ER RESTRICTED 120). TRANSFERED TO MDDR 141557, IAW DDG 26-11-01-01, CAT C, DD 07FEB21. FOUND LOOSE CONNECTOR AT LOWER LOOP RT SIDE, SECURED CONNECTOR. OPERATIONS CHECK OK, MDDR 141557 IS CLOSED.

Part: VALVE — LEAKING (IDG OIL PRESSURE) · airframe 81,823 hrs · 21,959 cycles

RIGHT GEN DRIVE LIGHT ILLUMINATED AFTER ENGINE START. TRANSFERRED TO MDDR 141517 24-00-01-01. PLACARD INSTALLED. DATE 31JAN21 LP 1333247 ITEM 9 CVG. INSPECTED AND FOUND IDG OIL PRESSURE RELIEF VALVE LEAKING. R & R IDG OIL PRESSURE RELIEF VALVE IAW B767 AMM 24-11-18. OPS CHECK AND LEAK CHECK GOOD. ACTIONS REVERSED. THIS CLEARS DMI 141517. MCC NOTIFIED, PLACARDS REMOVED.

Part: FIRE LOOP — CHAFED (NR 1) · airframe 81,814 hrs · 21,953 cycles

RT ENGINE FIRE LP 1 STATUS MESSAGE. T/S IAW FIM 26-11 FT 808 & FT 804. FOUND RT ENGINE LOOP 1 CHAFING AGAINST ENGIEN STRUT. RELOCATED LOOP, PERFORMED BITE CHECK, MESSAGE CLEARED. NO OTHER FAULTS NOTED. A/C OK FOR SERVICE.

Part: IDG — FAILED (RT GENERATOR) · airframe 81,811 hrs · 21,952 cycles

DURING TAKEOFF ROLL, INITIATED A LOW SPEED AT 55 KTS, REJECTED TAKEOFF FOR RT GEN OFF AND RT GEN DRIVE EICAS MESSAGES. TRANSFERED TO MDDR 141408, REF POLAR DDG 24-00-01-01, CAT B, DUE 28 JAN21. MCC NOTIFIED, PLACARDS INSTALLED. MX ACTION C/W. REMOVED AND REPLACED RT ENGINE IDG, OPERATIONS & LEAK CHECK SATISFACTORY, REF AMM 24-11-01. THIS CLEARS MDDR 141408. PLACARD REMOVED.

Part: CIRCUIT CARD — MALFUNCTIONED (FIRE LOOP 1) · airframe 81,811 hrs · 21,952 cycles

RT ENGINE FIRE LP 1 EICAS MESSAGE. REMOVED AND REPLACED FIRE DETECTION CARD FILE, PRINTED CIRCUIT BOARD, IAW AMM 26-10-01. OPERATIONS CHECKS GOOD. EICAS MESSAGE NO LONGER VISIBLE.

Part: CIRCUIT CARD — MALFUNCTIONED (FIRE LOOP 2) · airframe 81,811 hrs · 21,952 cycles

RT ENGINE FIRE LP 2 EICAS MESSAGE. REMOVED AND REPLACED FIRE DETECTION CARD FILE, PRINTED CIRCUIT BOARD, IAW AMM 26-10-01. OPERATIONS CHECKS GOOD. EICAS MESSAGE NO LONGER VISIBLE.

Part: STATUS MESSAGE — FALSE ACTIVATION (FIRE LOOP 1) · airframe 81,807 hrs · 21,950 cycles

RT ENGINE FIRE LP 1 STATUS MESSAGE ON TAKEOFF. PERFORMED OPERATIONAL CHECK OF RT ENGINE FIRE LP 1, IAW B767 AMM 26-11-00. NO FAULTS FOUND AT THIS TIME.

Part: STATUS MESSAGE — FALSE ACTIVATION (FIRE LOOP 1) · airframe 81,806 hrs · 21,949 cycles

RIGHT ENGINE FIRE LOOP 1 STATUS MESSAGE. NO ACTIVE MESSAGE SHOWN ON EICAS. PERFORMED FIRE DETECTION BITE PROCEDURE, IAW B767 FIM 26-11-00/101. OPERATIONS CHECKS GOOD AT THIS TIME.

Part: OIL SYSTEM — LOW (NR 2 IDG) · airframe 81,806 hrs · 21,949 cycles

RT GEN OFF ON TAKEOFF. DEFERRED PER MEL 24-00-01-01, DMI 141247, 25JAN21, CAT B. PLACARD INSTALLED. UPON VISUAL INSPECTION FOUND THE NR 2 IDG LOW ON OIL, SERVICED IDG WITH 3 QTS, IAW AMM 12-13-03. THIS CLEARS DMI 141247. MCC NOTIFIED AND PLACARD REMOVED.

Part: ENGINE — DAMAGED (RIGHT) · airframe 81,807 hrs · 21,950 cycles

OIL FOUND IN RT EXHAUST CONE AND SPINNER DAMAGED. RT ENGINE CHANGE COMPLETE, IAW WORK CARD A-71-999-09-02. ENGINE RUNS ARE GOOD AT THIS TIME.

Part: TRU — MALFUNCTIONED (APU) · airframe 81,807 hrs · 21,950 cycles

APU ABORT START. PERFORMED FIM 49-11 FT 989 TO SHEET 3 BLOCK 25. REMOVED AND REPLACED APU TRU, IAW AMM 24-32-04. OPERATIONS CHECK GOOD.

Part: MODULE — MALFUNCTIONED (AUX PITOT ANNUNC) · airframe 81,794 hrs · 21,942 cycles

RT AUX PITOT IND INOPERABLE. TRANSFERRED TO MDDR 140941, PER MEL 30-31-02 CAT B DUE 18JAN21. REMOVED AND REPLACED RT AUX PITOT ANNUNCIATOR LIGHT MODULE, IAW AMM 33-16-02. OPERATIONS CHECK GOOD. THIS CLEARS MDDR 140941.

Part: CIRCUIT BREAKER — TRIPPED (RT BOOST PUMP) · airframe 81,740 hrs · 21,906 cycles

RT AFT FUEL PUMP EICAS MESSAGE CIRCUT BREAKER POPPED ON ENGINE START. PER DDG/MEL 28-22-01, CAT C, ITEM TRANSFERRED TO MDDR NR 140429. OPENED AND COLLARED RIGHT AFT MAIN BOOST PUMP CB ROW G-21 MCC AND DISPATCH NOTIFIED. C/B RESET AND C/O OPERATIONS CHECK STATISFACTORY, IAW AMM 28-31-00. C/W OPERATIONS CHECK WITH ENGINE RUNNING AND NO FAULTS NOTED DURING POWER TRANSFER, IAW AMM 71-00-00. C/W 77893 AND AP-19303. T/S IAW FIM 28-22 FT 831 AND 802. PULLED C/B'S FOR R AFT BOOST PUMP. INSPECTED WIRING IAW FT 831 AND WDM 28-22-11. NO FAULTS FOUND. RESET CB'S, PERFORMED OPS CK IAW FIM 28-22 FT 831 STEPS 1-5. OPS CK GOOD. AIRCRAFT OK FOR SERVICE.THIS CLEARS W/O 77893.

Part: PUMP — MALFUNCTIONED (LT FUEL BOOST) · airframe 81,740 hrs · 21,906 cycles

CTR L FUEL PUMP EICAS MESSAGE ON DEPARTURE. TRANSFERED TO MDDR NR 140434, IAW DDG 28-22-02A, CAT C, MX PROCEDURES C/W. REMOVED AND REPLACED CTR-L PUMP AND C/O OPERATIONS CHECK AND LEAK CHECK OK, IAW AMM 28-22-05 AND AMM 28-31-00. MDDR 140434 CLOSED.

Part: DUCT — DAMAGED (APU SURGE VALVE) · airframe 81,669 hrs · 21,858 cycles

DURING APU MAINTENANCE FOUND APU SURGE VALVE DUCT DAMAGED. TRANSFERRED TO MDDR 139394, IAW DDG 49-11-01A, CAT C, DUE 22DEC20. REMOVED AND REPLACED APU SURGE BLEED DUCT, IAW AMM 20-11-00. APU OPERATIONS CHECK GOOD, NO DEFECTS NOTED AT THIS TIME, IAW AMM 49-11-00. THIS CLEARS DMI 139394, MCC NOTIFIED, PLACARDS REMOVED.

Part: SHUTOFF VALVE — WARNING MESSAGE (LT ENGINE) · airframe 81,519 hrs · 21,749 cycles

LT ENGINE HPSOV STATUS MESSAGE. T/S IN REF TO FIM 36-10/833, LT HPSOV THUMB TEST OK VALVE SWITCHES WRANG. CHECKED FOUND 28V AT HPC-OK. CLEANED AND RE-CONNECTED PLUG AT HPC, LT SYSTEM PNEU OPERATIONS CHECKS, OK DURING ENGINE RUN, PER AMM 36-11-00.

Part: MODULE — FAILED (ANNUNCIATOR LGHT) · airframe 81,497 hrs · 21,732 cycles

LEFT ENGINE FUEL VALVE LIGHT INOPERABLE. TRANSFERRED TO MDDR 137160, IAW MEL 73-21-03-01, CAT: C EXP: 13NOV20 MX PROCEDURE COMPLIED WITH. MZ AT 1424 05NOV20. REMOVED AND REPLACED ANNUNCIATOR LIGHT MODULE, PER AMM 33-16-02. CHECKS OK. THIS CLEARS MDDR 137160. PLACARD REMOVED.

Part: PIN — MISSING (OXYGEN MASK) · airframe 81,427 hrs · 21,687 cycles

F/O OXYGEN MASK PIN IS MISSING. RE-SECURED F/O O2 MASK, IAW B767-300 AMM 35-11-51.

Part: WARNING LIGHT — FALSE INDICATION (FUEL PUMP) · airframe 81,394 hrs · 21,662 cycles

LEFT AFT FUEL PUMP ILLUMINATED ON EICAS THEN EXTINGUISHED WHILE IN CRUISE. PERFORMED OPERATIONAL CHECK OF THE LEFT AFT FUEL PUMP, IAW AMM 28-22-00. OPERATIONAL NORMAL, NO DEFECTS NOTED AT THIS TIME.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 81,339 hrs · 21,612 cycles

EXTERIOR EMERGENCY LIGHTS INOPERABLE. REMOVED AND REPLACED EXTERIOR LIGHTING BATTERY IAW AMM 33-51-07. OPS CHECKS GOOD AT THIS TIME. BATTERY EQUIPMENT # M736.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 81,339 hrs · 21,612 cycles

INTERIOR EMERGENCY LIGHTS INOPERABLE. REMOVED AND REPLACED INTERIOR LIGHTING BATTERY IAW AMM 33-51-07. OPS CHECKS GOOD AT THIS TIME. BATTERY EQUIPMENT # M735.

Part: LAMP — INOPERATIVE (INDICATOR) · airframe 81,317 hrs · 21,589 cycles

RIGHT ENGINE SPAR VALVE LIGHT INOPERABLE. RELAMPED RT SPAR VALVE LIGHT IAW B767 AMM 33-13-00. OPS CHECK GOOD.

Part: FAULT MESSAGE — FALSE ACTIVATION (APU) · airframe 81,309 hrs · 21,580 cycles

APU FAULT ON EICAS, LEFT ENGINE START OCCURED PRIOR TO ANY MOVEMENT OF APU SELECTOR. PERFORMED APU ECU BITE CHECK IAW AMM 49-61-05. PERFORMED APU START AND SHUTDOWN PROCEDURES IAW AMM 49-11-00. NO DEFECTS NOTED.

Part: CONTROL VALVE — FAILED (APU) · airframe 81,309 hrs · 21,580 cycles

APU INOPERATIVE. REMOVED AND REPLACED THE SURGE CONTROL VALVE IAW AMM 49-53-01, BITE CHECKED GOOD. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 81,309 hrs · 21,580 cycles

ON CLIMB/DEPARTURE FWD CGO BACKUP EICAS MSG AND FAULT LIGHT ILLUMINATED(<P>RAN QRH FWD CGO BACKUP MSG CLEARED - NO FAULT ACTIONS. PERFORMED OPERATIONAL CHECK OF THE COMPLETED OPS CHECK GOOD. FORWARD CARGO A/C IAW AMM 21-28-00. PERFORMED ZONE TEMPERATURE CONTROLLER BITE PROCEDURE IAW FIM 21-60 FAULT TREE 804. NO FAULTS FOUND AT THIS TIME. SYSTEM CHECKS NORMAL.<BR /></P>)

Part: RADAR — MALFUNCTIONED (WEATHER) · airframe 81,215 hrs · 21,495 cycles

RADAR DISPLAY HEAVY PRECIPITATION WITH NO PRECIPITATION AHEAD, WITH TILT AT +15. THIS WAS ON BOTH LT & RT SYSTEMS AND MODE WX & WXT. PERFORMED SYSTEM OPERATIONAL CHECK IAW AMM 34-43-00. NO DEFECTS NOTED.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 81,181 hrs · 21,465 cycles

CARGO TRIM AIR STATUS MSG. OPS CHECKED CARGO TRIM AIR IAW AMM 21-51-04. OPS CHECK GOOD, STATUS MESSAGE CLEARED. NO FURTHER DEFECT NOTED.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 81,181 hrs · 21,465 cycles

LT FWD WINDOW HEAT LIGHT INOP. REMOVED AND REPLACED WINDOW HEAT CONTROL PANEL IAW AMM 30-41-02. OPS CHECK GOOD.

Part: CLAMP — LOOSE (FIRE LOOP) · airframe 81,153 hrs · 21,439 cycles

RH ENG FIRE LP 1 INOP(<P>TRANSFER TO MDDR 128549 IAW DDG 26-11-01-01, CAT 'C'.&NBSP;</P><P>LP 896779 - M2: FOUND SEVERAL CLAMPS LOOSE. RE-SECURED IAW AMM 26-11-00, OPERATIONAL TEST OK. THIS CLEARS MDDR 128549.</P>)

Part: SHUTOFF VALVE — NOT REPORTED (BLEED AIR SYS) · airframe 81,140 hrs · 21,426 cycles

RIGHT ENG HPSOV.(<P>REMOVED AND REPLACED RIGHT ENGINE HPSOV IAW AMM 36-11-07. OPS TEST OK. PERFORMED&NBSP; BITE TEST AIR SUPPLY CONTROL SYSTEM.<BR /></P>)

Part: CONTROLLER — MALFUNCTIONED (CABIN TEMP) · airframe 81,142 hrs · 21,429 cycles

FWD CARGO A/C EICAS MESSAGE DISPLAYED AFTER BLOCK OUT.(<P>REMOVED AND REPLACED AUX ZONE TEMP CONTROLLER IAW AMM 21-61-12, OPS CHECK GOOD AT THIS TIME.<BR /></P>)

Part: RCCB — FAULTY (APU BATTERY) · airframe 81,097 hrs · 21,388 cycles

STATUS MESSAGE : APU BATT NO STBY(<P>TRANSFERRED TO MDDR 127229 IAW MEL 49-11-01A CAT C DUE 28APR20. </P><P>LP 1190116: REMOVED AND REPLACED MAIN APU BATTERY TIE REMOTE CONTROL CIRCUIT BREAKER IAW AMM 24-33-05. OPS CHECKS GOOD. THIS CLEARS DMI 127229. PLACARD REMOVED. MCC NOTIFIED.</P>)

Part: CIRCUIT BREAKER — PULLED (IGNITION SYS) · airframe 81,089 hrs · 21,379 cycles

STATUS MESSAGES "LH ENG IGNITOR 1" AND "RH ENG IGNITOR 2".(<P>FOUND LH IGN. AND RH IGN. CBS PULLED. CLOSED CBS, OPS CHECK NML IAW B767 AMM 74-11-01.</P>)

Part: CONTROLLER — MALFUNCTIONED (CABIN TEMP) · airframe 80,990 hrs · 21,336 cycles

AFT CABIN TEMP EICAS MSG.(<P>TRANSFER TO MDDR 125899 IAW DDG 21-61-01-02, CAT 'C'.</P><P>LP 952878 - M2: RESET TEMP CONTROLLER AND ACCOMPLISHED TEST IAW AMM 21-61-00. SYSTEM FOUND OK. THIS CLEARS MDDR 125899.</P>)

Part: SKIN — CRACKED (LE SLAT) · airframe 80,973 hrs · 21,333 cycles

CRACK - SKIN, OUTBD SIDE OF L/H WING NO. 4 SLAT EXTERNAL SKIN, OSS 641.945.(<P>REPAIRED THE DAMAGED AREA IAW SRM 57-43-01-2R-2 REPAIR 2 REV. 112. JOB COMPLETED.</P>)

Part: SIGNAL COND UNIT — FAILED (VIBE MONITOR) · airframe 80,973 hrs · 21,333 cycles

FOUND THE ENGINE VIBRATION MONITOR FUNCTION FAIL.(<P>IAW AMM 77-31-03-004-002-1-100, 77-31-03-404-004-1-100 REV. 129 REPLACED THE SIGNAL CONDITIONER. IAW AMM 77-31-00-715-001-1-100, 77-31-00-705-103-1-100 REV. 129 PERFORMED OPERATIONAL TEST AND SELF TEST. RESULT WAS SATISFACTORY.</P>)

Part: FIRE DETECTOR — BROKEN (NR 1 ENGINE) · airframe 80,973 hrs · 21,333 cycles

FOUND THE TS00682 FIRE DETECTOR ASSY CONNECTOR BROKEN.(<P>IAW AMM 26-11-02-024-001 AND AMM 26-11-02-424-033 REV. 129 REPLACED FIRE DETECTOR AT NO. 1 ENG (TS00682). IAW AMM 26-11-02-424-033 REV. 129 PERFORMED INSTALLATION TEST AND RESULT WAS SATISFACTORY.</P>)

Part: CONTROLLER — MALFUNCTIONED (BLEED AIR SYS) · airframe 80,973 hrs · 21,333 cycles

FOUND #2 ENG HPC PHH, PHL PH-PC AND PC PRESSURE SWITCH OPERATION TEST FAIL, WHEN SUPPLY PRESSURE BETWEEN 117-140 PSIG, BIT 16 DOES NOT CHANGE TO 1.(<P>IAW AMM 36-11-08-004-006-007 REV. 129 AND AMM 36-11-08-404-014-007 REV. 129 REPLACED HPC AT NO. 2 ENG. IAW AMM 36-11-08-404-014-007 REV. 129 PERFORMED HPC INSTALLATION TEST, CHECK RESULT = NORMAL AND NO LEAK FOUND. IAW AMM 36-23-00-715-001 REV. 129 PERFORMED AIR SUPPLY CONTROL SYSTEM BITE TEST, CHECK RESULT = NORMAL.</P>)

Part: SKIN — CRACKED (LE SLAT) · airframe 80,973 hrs · 21,333 cycles

CRACK - SKIN, OUTBD SIDE OF L/H WING NO. 3 SLAT EXTERNAL SKIN, OSS 792.537.(<P>REPAIRED THE DAMAGED AREA IAW SPM 57-43-01-2R-2 REPAIR 2, REV 112. JOB COMPLETED.</P>)

Part: FITTING — BROKEN (THRUST REVERSER) · airframe 80,973 hrs · 21,333 cycles

BROKEN - FITTING, NO. 1 ENG R/H T/R TRANS COWL UPPER SIDE GUIDE FITTING.(<P>IAW AMM 78-31-00-802-190 REV. 129 AND AMM 70-50-00-912-001 REV. 129 AND AMM 78-31-00-402-131 REV. 129 REPLACED THE NO. 1 ENG R/H T/R TRANSLATING COWL UPPER COWL GUIDE FITTING WITH SERVICEABLE PARTS. CONDITION CHECK NORMAL.</P>)

Part: CHECK VALVE — NOT REPORTED (AC BAY) · airframe 80,973 hrs · 21,333 cycles

REQUEST INSTALL L/H R/H PACK TRIM AIR SUPPLY CHECK VALVE.(<P>IAW AMM 21-61-05-404-015 REV. 129 INSTALL L/H R/H TRIM AIR SUPPLY CHECK VALVE.</P>)

Part: GUIDE — MISSING (THRUST REVERSER) · airframe 80,973 hrs · 21,333 cycles

MISSING - GUIDE, NO. 1 ENG RH T/R TRANS COWL UPPER SIDE.(<P>IAW AMM 78-31-00-802-190-1-100 REV. 129 AND AMM 70-50-00-912-001-1-100 REV. 129 AND AMM 78-31-00-402-131-1-100 REV. 129 INSTALLED NO. 1 ENG T/R TRANSLATING COWL UPPER COWL GUIDE WITH SERVICEABLE PARTS. CONDITION CHECK NORMAL.</P>)

Part: PROBE — DAMAGED (EGT) · airframe 80,973 hrs · 21,333 cycles

FOUND EGT THERMOCOUPLE PROBE DAMAGE AT NO. 1 ENG (SIX O'CLOCK).(<P>IAW AMM 77-21-01-404-011 AND 77-21-01-004-010 REV. 129, REPLACED THE EGT PROBE FOR #1 ENG. IAW AMM 77-21-00-715-012 REV. 129 PERFORM EGT INDICATING SYS OPERATIONAL TEST, RESULT TEST NORMAL. COMPLETED THIS JOB AND CONDITION CHECK SATISFACTORY.</P>)

Part: SKIN — CRACKED (LE SLAT) · airframe 80,973 hrs · 21,333 cycles

CRACK - SKIN, LWR FACE OF R/H WING NO. 9 SLAT L/E SKIN NEAR OUTBD TRACK, OSS 641.945(<P>REPAIRED THE DAMAGED AREA IAW SRM 57-43-01-2R-2 REPAIR 2, REV. 112. JOB COMPLETED.&NBSP;</P>)

Part: ACCELEROMETER — MALFUNCTIONED (VIBE MONITOR) · airframe 80,973 hrs · 21,333 cycles

FOUND NO. 1 ENG N2 VIBRATION SENSOR FAIL.(<P>IAW AMM 77-31-02-004-001 AND 77-31-02-404-006 REV. 129 REPLACED THE ACCELEROMETER WITH SERVICEABLE PARTS FOR NO. 1 ENG. IAW AMM 71-00-00-712-168 REV. 129 PERFORM DRY MOTORING TEST, RESULT CONDITION NORMAL. COMPLETED THIS JOB AND CONDITION CHECK SATISFACTORY.</P>)

Part: TUBE — DENTED (FUEL SYSTEM) · airframe 80,973 hrs · 21,333 cycles

FOUND #2 PYLON FUEL TUBE WEAR AND DENT WITHOUT LIMIT.(<P>IAW AMM 28-22-07-404-104 REV. 129 AND AMM 28-22-07-404-126 REV. 129 REPLACED THE #2 PYLON FUEL TUBE WITH SERVICEABLE PARTS. TRANSFER TO FORM T2031 ITEM #4.</P>)

Part: TUBE — DENTED (FUEL SYSTEM) · airframe 80,973 hrs · 21,333 cycles

FOUND #1 PYLON FUEL TUBE SCRATCH AND DENT WITHOUT LIMIT.(<P>IAW AMM 28-22-07-404-104 REV. 129 AND AMM 28-22-07-404-126 REV. 129 REPLACED OF THE #1 PYLON FUEL TUBE WITH SERVICEABLE PARTS. TRANSFER TO FORM T2031 ITEM #4.</P>)

Part: SEAL — BROKEN (NR 2 PYLON) · airframe 80,973 hrs · 21,333 cycles

BROKEN SEAL ASSY, NO. 2 PYLON AFTER FAIRING SIDE PANEL (PNL NO. 446CR) LOWER EDGE.(<P>IAW AMM 71-00-02-004-002 REV. 129 REMOVED THE PANEL NO. 446CR. REMOVED DAMAGED PARTS IAW SRM 51-40-02 REV. 112. INSTALL NEW PARTS IAW SRM 51-40-02 REV. 112 AND DWG NO. 311T2570 SH1 REV. 1. IAW AMM 71-00-02-404-049 REV. 129 INSTALLED THE PANEL NO. 446CR. CONDITION CHECK NORMAL.</P>)

Part: COUPLER — WORN (FUEL SYSTEM) · airframe 80,973 hrs · 21,333 cycles

FOUND BOTH PYLON FUEL TUBE COUPLINGS WORN.(<P>IAW AMM 28-22-07-404-104 REV. 129 AND AMM 28-22-07-404-126 REV. 129 REPLACED BOTH PYLON FUEL TUBE COUPLINGS WITH SERVICEABLE PARTS.</P>)

Part: PLUG — CRACKED (NR 1 EXHAUST) · airframe 80,973 hrs · 21,333 cycles

FOUND #1 ENG EXHAUST PLUG CRACK(<P>IAW AMM 78-11-02-004-001 REV. 129 REMOVED THE #1 ENG EXHAUST PLUG. REFER TO J/C ATTACHING SHEET CONTROL NO. 0243072.0198389. IAW AMM 78-11-02-404-006 REV. 129 INSTALLED THE #1 ENG EXHAUST PLUG. CONDITION CHECK NORMAL.</P>)

Part: SEAL — BROKEN (RT COWLING) · airframe 80,973 hrs · 21,333 cycles

BROKEN - SEAL, NO. 1 ENG R/H FAN COWL BETWEEN NO. 2 KEEPER AND TE.(<P>IAW AMM 71-11-04-712-014 REV. 129 AND AMM 71-11-04-412-007 REV. 129 REPLACED SEAL AT #1 ENG R/H FAN COWL. CONDITION CHECK SATISFACTORY.</P>)

Part: SKIN — CRACKED (LE SLAT) · airframe 80,973 hrs · 21,333 cycles

CRACK - SKIN, LWR FACE OF R/H WING NO. 9 SLAT L/E SKIN NEAR INBD TRACK, OSS 572.549.(<P>REPAIRED THE DAMAGED AREA IAW SRM 57-43-01-2R-2, REPAIR 2, REV. 112. JOB COMPLETED.&NBSP;</P>)

Part: DRAIN LINE — CHAFED (NR 2 ENGINE) · airframe 80,973 hrs · 21,333 cycles

CHAFING - TUBE, NO. 2 ENG L/H OIL DRAIN MODULE CAP WITH DRAIN TUBE UPPER SURFACE.(<P>IAW AMM 70-50-00-912-001 REV. 129 REPLACE THE OIL DRAIN TUBE FOR #2 ENG. IAW AMM 71-71-00-796-067 REV. 129, PERFORM DRAIN CHECK, RESULT COND NORMAL AND NO LEAK FOUND. COMPLETED THIS JOB AND CONDITION CHECK SATISFACTORY.</P>)

Part: PACKING — DAMAGED (NR 1 ENGINE) · airframe 80,973 hrs · 21,333 cycles

FOUND #1 ENG A-SUMP OIL LEAK.(<P>IAW AMM 72-31-03-004-001 REV. 129 AND AMM 72-31-02-404-005 REV. 129 REPLACED THE PACKING WITH SERVICEABLE PARTS AT NO. 1 ENG A-SUMP. TRANSFER TO FORM T2031 ITEM #6.</P>)

Part: SEAL — BROKEN (NR 2 PYLON) · airframe 80,973 hrs · 21,333 cycles

BROKEN - SEAL ASSY, NO. 2 PYLON AFTER FAIRING SIDE PANEL (PNL NO. 446CL) LOWER EDGE.(<P>IAW AMM 71-00-02-004-002 REV. 129 REMOVED THE PANEL NO. 446CL. REMOVED DAMAGED PARTS IAW SRM 51-40-02 REV. 112. INSTALL NEW PARTS IAW SRM 51-40-02 REV. 112 AND DWG NO. 311T2570 SH1 REV. 1. IAW AMM 71-00-02-404-049 REV. 129 INSTALLED THE PANEL NO. 446CL. CONDITION CHECK NORMAL.<BR /></P>)

Part: ACOUSTIC LINER — DEBONDED (NR 1 ENGINE) · airframe 80,973 hrs · 21,333 cycles

DISBOND - HONEYCOMB, NO. 1 ENG FWD ACOUSTIC LINER ON 6:00.(<P>IAW AMM 72-33-01-004-001 REV. 129 AND AMM 72-33-01-404-011 REV. 129 REPLACED THE NO. 1 ENG FWD ACOUSTICAL LINER WITH SERVICEABLE PARTS. COMPLETED THIS JOB AND CONDITION CHECK NORMAL.</P>)

Part: CONTROLLER — MALFUNCTIONED (BLEED AIR SYS) · airframe 80,973 hrs · 21,333 cycles

FOUND NO. 2 ENG PRVC OPERATION TEST FAIL, REFERENCE PRESSURE OUT OF THE REQUIRED LIMITS.(<P>IAW AMM 36-11-19-004-001-002 REV. 129 AND AMM 36-11-19-404-014-002 REV. 129 REPLACED PRVC AT NO. 2 ENG. IAW AMM 36-11-19-404-014-002 REV. 129 PERFORMED #2 ENG PRVC INSTALLATION TEST, CHECK RESULT. TEST NORMAL AND NO LEAK FOUND.<BR /></P>)

Part: BULB — MISSING (AC BAY) · airframe 80,973 hrs · 21,333 cycles

FOUND LH PACK INLET AIR TEMP BULB IS NOT INSTALLED ON THE DUCT AND IS DAMAGED.&NBSP;(<P>IAW AMM 21-52-08-004-025 REV. 12P AND AMM 21-52-08-404-010 REV. 12P, REPLACED PACK INLET AIR TEMP BULB. CONDITION CHECK NORMAL, AND JOB COMPLETED.&NBSP;</P>)

Part: CONTROLLER — MALFUNCTIONED (BLEED AIR SYS) · airframe 80,973 hrs · 21,333 cycles

FOUND #1 ENG PRVC OPERATION TEST FAIL REFERENCE PRESSURE OUT OF THE REQUIRED LIMITS.(<P>IAW AMM 36-11-19-004-001-002 REV. 129 AND AMM 36-11-19-404-014-002 REV. 129 REPLACED PRVC AT NO. 1 ENG. IAW AMM 36-11-19-404-014-002 REV. 129 PERFORMED #1 ENG PRVC INSTALLATION TEST, CHECK RESULT. TEST NORMAL AND NO LEAK FOUND.</P>)

Part: CONNECTOR — DAMAGED (NR 1 ENGINE) · airframe 80,973 hrs · 21,333 cycles

FOUND BACKSHELL DAMAGE AT NO. 1 ENG (D10970)(<P>IAW WDM 80-11-11 REV. 28, SWPM 20-25-12, REV. 73, SWPM 20-61-11 REV. 71, REPLACED THE BACKSHELL AND CONNECTOR (D10970) (OFF PN: BACC63CM1005). IAW WDM 80-11-11 REV. 28 PERFORMED THE CONTINUITY CHECK AND THE RESULT WAS SATISFACTORY. IAW AMM 71-00-00-995-229-1-103 REV. 129 PERFORMED POWER PLANT TEST - REFERENCE TABLE START VALVE AND THE RESULT WAS SATISFACTORY.</P>)

Part: DRAIN LINE — DENTED (NR 2 ENGINE) · airframe 80,973 hrs · 21,333 cycles

DENT - TUBE, NO. 2 ENG L/H HYDRAULIC OIL DRAIN TUBE CONNECTION ACCESSORY DRIVE MODULE.(<P>IAW AMM 70-50-00-912-001 REV. 129, REPLACE THE HYD DRAIN TUBE FOR #2 ENG, IAW AMM 71-71-00-796-067 REV. 129, PERFORM DRAIN CHECK, RESULT COND NORMAL AND NO LEAK FOUND. COMPLETED THIS JOB AND CONDITION CHECK SATISFACTORY.</P>)

Part: SKIN — CRACKED (LE SLAT) · airframe 80,973 hrs · 21,333 cycles

CRACK - SKIN, INBD SIDE OF L/H WING NO. 3 SLAT EXTERNAL SKIN, OSS 723.941.(<P>REPAIRED THE DAMAGED AREA IAW SRM 57-43-01-2R-2 REPAIR 2, REV. 112. JOB COMPLETED.&NBSP;</P>)

Part: RUB STRIP — MISSING (THRUST REVERSER) · airframe 80,973 hrs · 21,333 cycles

MISSING - WEARSTRIP, NO. 1 ENG R/H T/R NO. 3 BLOCKER DOOR, TOTAL: 1EA.(<P>IAW AMM 78-31-14-004-001 &AMP; 78-31-14-404-008 REV. 129 &AMP; CMM 78-32-03 REPAIR 003, REV. 58, COMPLETED THE WEARSTRIP REPAIR. IAW AMM 71-00-00-700-807 REV. 129 PERFORMED T/R OPERATIONAL TEST, RESULT: NORMAL. COMPLETED THIS JOB AND CONDITION CHECK SATISFACTORY.</P>)

Part: PAINT — PEELING (NR 1 ENGINE) · airframe 80,973 hrs · 21,333 cycles

PEEL OFF - PAIN, NO. 1 ENG SPINNER CONE PEEL OFF.(<P>CLEAN UP SURFACE AND APPLY THE COATING IAW GE CF6-80C2 ESM 72-21-10 REPAIR 004 AND REPAIR 006 REV. 89. CONDITION CHK NORMAL.</P>)

Part: RIB — CRACKED (RT WING) · airframe 80,973 hrs · 21,333 cycles

CRACK - RIB, UPPER SIDE AFT EDGE OF R/H WING INBD T/E COMPARTMENT RIB, WS 468.11, ACCESS PANEL NO 661BB.(<P>REPAIR DAMAGED AREA IAW SRM 57-51-02-2R-3 REPAIR 3. JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

Part: DUCT — BROKEN (ANTI-ICE SYS) · airframe 80,973 hrs · 21,333 cycles

FOUND ANTI-ICE INTERSTITIAL DUCT BRK BETWEEN #4-#5, #8-#9 SLAT.(<P>IAW AMM 30-11-06-004-001 REV. 129 AND AMM 30-11-06-404-009 REV. 129 REPLACE ANTI-ICE INTERSTITIAL DUCT BETWEEN #4-5 SLAT AND #8-9 SLAT.</P>)

Part: SKIN — DAMAGED (ACCESS DOOR) · airframe 80,973 hrs · 21,333 cycles

BROKEN CHAFING AND DEFORM DAMAGES ON SKIN EDGE OF ELEC/ELEX ACCESS DOOR PANEL ASSY 141T6301-77.(<P>REPAIRED DAMAGED AREA IAW EI NO T2020A52M-749, REV. 1. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: BLOWER — FAULTY (SMOKE DETECTOR) · airframe 80,973 hrs · 21,333 cycles

FOUND STATUS MSG "CARGO DET AIR"(<P>REPLACED AFT CARGO SMOKE DETECTOR BLOWER 2 IAW AMM 26-16-02-000-801-002. CONDITION CHECK NORMAL.</P>)

Part: LATCH — WORN (RT COWLING) · airframe 80,973 hrs · 21,333 cycles

WORN - LATCH, NO. 1 ENG R/H FAN COWL OIL TANK SVC DOOR MID.(<P>REMOVE DAMAGED PARTS IAW SRM 51-40-02 REV. 112. INSTALL NEW PARTS IAW SRM 51-40-02 REV. 112 AND GOODRICH CMM 71-13-22 REV. 44. JOB COMPLETED AND CONDITION NORMAL.</P>)

Part: DRAIN LINE — DENTED (NR 1 ENGINE) · airframe 80,973 hrs · 21,333 cycles

DENT - TUBE, NO. 1 ENG FUEL-MANIFOLD DRAIN TUBE UNDER A.G.B 6:00.(<P>IAW AMM 70-50-00-912-001 REV. 129, REPLACE THE FUEL MANIFOLD DRAIN TUBE FOR #1 ENG. IAW AMM 71-71-00-796-067 REV. 129, PERFORM DRAIN CHECK, RESULT CONDITION NORMAL AND NO LEAK FOUND. COMPLETED THIS JOB AND CONDITION CHECK SATISFACTORY.</P>)

Part: SKIN — CRACKED (LE SLAT) · airframe 80,973 hrs · 21,333 cycles

CRACK - SKIN, LWR FACE OF R/H WING NO. 10 SLAT L/E SKIN NEAR OUTBD TRACK, OSS 792.537.(<P>REPAIRED THE DAMAGED AREA IAW SRM 57-43-01-2R-2 REPAIR 2, REV. 112. JOB COMPLETED.&NBSP;</P>)

Part: SKIN — CRACKED (LE SLAT) · airframe 80,973 hrs · 21,333 cycles

CRACK - SKIN, LWR FACE OF R/H WING NO. 10 SLAT L/E SKIN NEAR INBD TRACK, OSS 723.941.(<P>REPAIRED THE DAMAGED AREA IAW SRM 57-43-01-2R-2, REPAIR 2, REV. 112. JOB COMPLETED.</P>)

Part: DIODE — DEFECTIVE (APU) · airframe 80,973 hrs · 21,333 cycles

FOUND THE APU INOP.(<P>IAW SRM 24-31-02, 49-00-04 REV. 28 AND WDM 24-32-41, 49-14-11, 49-15-11, 49-41-11, 49-61-11 REV. 28 PERFORMED WIRING CHECK, THE RESULT WAS SATISFACTORY. FOUND DIODE R65 APU SHUTDOWN ISOLATION FUNCTION. IAW WDM 49-61-11 REV. 28 AND SWPM 20-90-11 REV. 73 REPLACED R65 DIODE WITH UNUSED DIODE. IAW AMM 49-11-00-802-002 REV. 129 PERFORMED APU STARTING AND OPERATION. THE CONDITION CHECKED NORMAL. IAW AMM 49-61-05-742-045, REV. 129, PERFORMED APU CONTROL UNIT BITE TEST. THE RESULT WAS SATISFACTORY.</P>)

Part: COWLING — ERODED (NR 2 ENGINE) · airframe 80,973 hrs · 21,333 cycles

EROSION - L/E, NO. 2 ENG R/H FAN COWL EXTERIOR FWD SURROUND SURFACE.(<P>IAW AMM 71-11-04-714-001 REV. 129 REMOVED THE 2R FAN COWL. REFER TO J/C ATTACHING SHEET CTRL NO. 0249896. IAW AMM 71-11-04-714-002 REV. 129 INSTALLED THE 2R FAN COWL. CONDITION CHECK NORMAL.</P>)

Part: GUIDE VANE — BROKEN (NR 1 ENGINE) · airframe 80,973 hrs · 21,333 cycles

BROKEN - METAL L/E, NO. 1 ENG O.G.V ON 11, 2~5 O'CLOCK.(<P>IAW AMM 72-33-00-308-043 REV. 129 REPAIRED METAL L/E NO. 1 ENG O.G.V ON 11, 2~5 O'CLOCK. CONDITION CHECK NORMAL.</P>)

Part: GUIDE — WORN (THRUST REVERSER) · airframe 80,973 hrs · 21,333 cycles

WORN - GUIDE ASSY, NO. 2 ENG L/H TRANSLATING COWL UPPER SIDE.(<P>IAW AMM 78-31-00-802-190 AND AMM 70-50-00-912-001 AND AMM 78-31-00-402-131 REV. 129, REPLACED THE GUIDE WITH NEW FOR 2L TRANS COWL. COMPLETED THIS JOB AND CONDITION CHECK NORMAL.<BR /></P>)

Part: PAINT — PEELING (NR 2 ENGINE) · airframe 80,973 hrs · 21,333 cycles

PEEL OFF - PAINT, NO. 2 ENG FAN ROTOR SPINNER CONE.(<P>CLEAN UP SURFACE AND APPLY THE COATING IAW GE CF6-80C2 ESM 72-21-10 REPAIR 004 AND REPAIR 006, REV. 89. CONDITION CHECK NORMAL.</P>)

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 80,973 hrs · 21,333 cycles

FLASHLIGHT AT L1 DOOR AREA RED LIGHT NOT FLASH.(<P>TRANSFERRED TO MDDR 124565 AS PER MEL 25-20-01, CAT E, DUE 11JUN2020.</P>)

Part: SWITCH — STICKING (OXYGEN MASK) · airframe 80,843 hrs · 21,304 cycles

CAPT'S O2 MASK RESET/TEST SWITCH STICKS WHEN TESTED, DOES NOT RETURN TO ORIGINAL POSITION.(<P>CLEANED RESET/TEST SWITCH AND CAPT'S O2 MASK, OPERATIONAL CHECKS OK IAW AMM 35-11-51.</P>)

Part: TEST SWITCH — STICKING (OXYGNE MASK) · airframe 80,835 hrs · 21,300 cycles

OBSERVER O2 MASK RESET TEST SWITCH STICKS WHEN RELEASED.(<P>IAW AMM 35-11-51, ADJUSTED AND LUBED RESET TEST SWITCH AND OPERATIONAL TEST NORMAL.</P>)

Part: TEST SWITCH — STICKING (OXYGEN MASK) · airframe 80,835 hrs · 21,300 cycles

CAPT'S O2 MASK RESET TEST SWITCH STICKS WHEN RELEASED, WHICH PREVENTS CAPTAIN'S INTERCOM SWITCH FROM WORKING.(<P>IAW AMM 35-11-51, ADJUSTED AND LUBED RESET TEST SWITCH AND OPERATIONAL TEST NORMAL.</P>)

Part: RADAR — MALFUNCTIONED (WEATHER) · airframe 80,831 hrs · 21,298 cycles

RADAR UNABLE/DOESN'T SHOW WEATHER EVEN THOUGH WE COULD SEE CELLS VISUALLY.(<P>IAW AMM 34-43-00-715-001-001, OPERATIONAL TEST OF WEATHER RADAR SYS CONDITION NORMAL. NO FAULT FOUND.</P>)

Part: APU — FAILED · airframe 80,779 hrs · 21,286 cycles

DUCT PRESSURE WENT TO ZERO AND SHORTLY AFTER APU AUTO SHUTDOWN AT THE GATE. REMOVED AND REPLACED THE APU ASSEMBLY. PERFORMED OPS CHECK, NORMAL. NO FAULTS FOUND ON BITE PROCEDURE IAW AMM 49-11-01.

Part: CONNECTOR — DIRTY (OIL SYSTEM) · airframe 80,790 hrs · 21,292 cycles

DURING CLIMBOUT FROM ICN WITH RIGHT OIL PRESSURE INDICATION - BLANKED THEN TO NORMAL REPEATEDLY. LEFT OIL PRESSURE BLANKED / RED / AMBER INDICATIONS REPEATEDLY. CLEANED BOTH ENGINE OIL PRESSURE TRANSMITTER CONNECTORS IAW AMM 79-32-01, PERFORMED BOTH ENGINE RUNS, C/W ALL INDICATIONS, CHECKED NORMAL IAW AMM 71-00-00.

Part: OXYGEN MASK — MALFUNCTIONED (COCKPIT) · airframe 80,767 hrs · 21,280 cycles

CENTER JUMPSEAT O2 MASK DOES NOT TEST.(<P>PULLED OUT AND RESTORED O2 MASK AND BOX, TEST OK IAW AMM 35-11-00/501.<BR /></P>)

Part: ADI — MALFUNCTIONED (COCKPIT) · airframe 80,763 hrs · 21,279 cycles

FIRST OFFICER'S PRIMARY FLIGHT DISPLAY FAILED ON TAKEOFF ROLL AT 30 KNOTS.(<P>F/O ADI REMOVED AND INSPECTED. FOUND DEBRIS ON EQUIP COOLING SCREEN, ADI REPLACED, REF AMM 34-22-03.</P>)

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 80,751 hrs · 21,277 cycles

RADAR UNABLE TO SHOW RETURNS OF KNOWN WEATHER.(<P>WX C/B'S CYCLED, AND OPS TEST PASS IAW AMM 34-43-00.</P>)

Part: CONTROL VALVE — MALFUNCTIONED (APU) · airframe 80,741 hrs · 21,276 cycles

APU AUTO SHUTDOWN(<P>REMOVED AND REPLACED APU CONTROL UNIT (OFF PART: PN&NBSP;2117342-20, SN&NBSP;33-B0380) PER AMM 49-61-05, BUT NO HELP. ITEM DEFERRED PER MEL 49-11-01B, CAT 'B', MDDR #122862.</P><P>LOG PAGE 1105254 - M2: REPLACED SURGE CONTROL VALVE AND OPERATIONAL CHK FUNCTION NORMAL, IAW AMM 49-53-01. MEL AND MDDR 122862 CLOSED. PLACARD REMOVED.</P>)

Part: BATTERY — INOPERATIVE (C/P FLASHLIGHT) · airframe 80,721 hrs · 21,271 cycles

TWO FLIGHT DECK FLASHLIGHT HOLDERS WERE INOPERATIVE. REMOVED AND REPLACED THE BATTERIES IAW CMM 25-60-02. OPS CHECKED GOOD.

Part: ECU — MALFUNCTIONED (APU) · airframe 80,681 hrs · 21,245 cycles

APU AUTO SHUTDOWN(<P>TRANSFERRED TO MDDR 122058 IAW MEL 49-11-01A, CAT 'C', DUE 24DEC19. PLACARD INSTALLED. MCC NOTIFIED.</P><P>LP 1097764 - M2: REMOVED AND REPLACED APU ECU IAW AMM 49-61-05. THIS CLOSES DMI 122058. MCC NOTIFIED AND PLACARD REMOVED.</P>)

Part: OXYGEN BOX — NO TEST (CAPTAIN'S) · airframe 80,553 hrs · 21,129 cycles

CAPTAIN`S OXYGEN MASK YELLOW CROSS DOES NOT SHOW DURING TEST. REMOVED AND REPLACED THE CAPTAIN`S OXYGEN MASK BOX IAW AMM 35-11-51.

Part: CONTROLLER — MALFUNCTIONED (AUX TEMP) · airframe 80,551 hrs · 21,127 cycles

AFTER TAKEOFF, , RECEIVED A FWD CGO BACKUP EICAS MESSAGE AND PANEL FAULT LIGHT. WENT AWAY 5 MINUTES LATER. REMOVED AND REPLACED AUX TEMP CONTROLLER IAW AMM 21-61-12, OPS CHECKED GOOD. TROUBLESHOT (WIRING CHECK), FROM D5602P PIN 11 TO PIN 10 FOUND 0.5 VOLT DROP, FROM D5602P PIN 11 TO D7052P PIN 13, FOUND A 0.4 VOLT DROP. REMOVED AND REPLACED RELAYS K1222 & K1221 IAW SWPM 20-81-22.VERIFIED 26 VDC AT D13570 PINS 4 & 12, VERIFIED 114.5 VAC VOLTAGE DROP BETWEEN D5988P PINS 49 AND 50. VERIFIED 26VDC VOLTAGE DROP BETWEEN D5988P PINS 47 AND 48.

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN TEMP) · airframe 80,549 hrs · 21,125 cycles

AFTER TAKEOFF, RECEIVED A FWD CARGO BACKUP EICAS AND PANEL FAULT LIGHT. WENT AWAY ON ITS OWN. PERFORMED ZONE TEMP CONTROLLER BITE PROCEDURE IAW AMM 21-61-00. PERFORMED LT AND RT PACK TEMP CONTROLLER BITE PROCEDURE IAW AMM 21-51-00, NO FAULTS FOUND. BOTH SYSTEMS FUNCTION NORMAL AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 80,506 hrs · 21,082 cycles

AFTER TAKEOFF, RECEIVED "FWD CARGO BACKUP" EICAS MESSAGE. WENT AWAY BY 10,000'. PERFORMED FIM 21-61 FT 803. NO FAULT INDICATIONS FOUND AND COULD NOT DUPLICATE THE FAULT. FIM 21-61 TASK 803 C/W, NO DEFECTS NOTED.

Part: PITOT HEAD — MALFUNCTIONED (CAPTAIN'S) · airframe 80,473 hrs · 21,050 cycles

CAPT PITOT EICAS MESSAGE ON ENGINE START. T/S PER FIM 30-31 FT 803, FOUND DISCONTINUITY FROM CAPTAINS PITOT. REMOVED AND REPLACED CAPTAIN PITOT IAW AMM 34-11-01. OPS CHECK IAW AMM TASK 30-31-00-715-008. LEAK TEST IAW AMM 34-11-00-730-811. OPS CHECK GOOD. T

Part: START VALVE — FAILED (LT ENGINE) · airframe 80,450 hrs · 21,029 cycles

ON LEFT ENGINE START, LEFT STARTER CUTOUT MESSAGE AFTER NORMAL START WITH ENGINE START SELECTOR SWITCH WENT TO AUTO AND VALVE LIGHT EXTINGUISHED NORMALLY. EICAS MESSAGE WAS ON FOR 55 SECOND. REMOVED AND REPLACED LEFT ENGINE STARTER VALVE IAW AMM 80-11-02. PERFORMED OPERATIONAL TEST IAW AMM 80-11-00-705-003-H00. SYSTEM OPS CHECK NORMAL.

Part: CONNECTOR — DIRTY (STARTER) · airframe 80,450 hrs · 21,028 cycles

ON LEFT ENGINE START, "LEFT STARTER CUTOUT" MESSAGE AFTER START. AFTER 30 SECONDS, MESSAGE CLEARED WITHOUT CREW ACTION. ENGINE START AUTOMATICALLY WENT TO AUTO. CLEANED THE CONNECTOR PLUG ON LEFT ENGINE START VALVE IAW SWPM 20-60-01. PERFORMED OPS CHECK IAW B767 AMM 80-11-00. OPS CHECK GOOD AT THIS TIME.

Part: SWITCH — MALFUNCTIONED (CARGO TEMP) · airframe 80,450 hrs · 21,029 cycles

OVERHEAT AFT CARGO LIGHT ILLUMINATED. REMOVED AND REPLACED AFT CARGO TEMPERATURE SWITCH IAW AMM 21-44-05.

Part: IGNITION LEAD — BROKEN (APU) · airframe 80,434 hrs · 21,015 cycles

APU IGNITION LEAD BROKEN. (<P>REMOVED AND REPLACED APU IGNITION LEAD IAW AMM 49-41-04.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 80,426 hrs · 21,007 cycles

FWD EQUIPMENT OVERHEAT EICAS MESSAGE ON TAKEOFF.&NBSP; (<P>TRANSFERRED TO MDDR 115154&NBSP;IAW&NBSP;21-58-01-01&NBSP;DDG PROCEDURES, CAT 'C', DUE DATE: 01-AUG-19.&NBSP;</P><P>LP 1090375 - M5: PERFORMED T/S IAW FIM TASK 21-58-00 FAULT TREE 912. ON BLOCK 25, WE WERE ABLE TO DETERMINE THAT THE SYSTEM WORKED PERFECTLY FINE. OPS CHECK GOOD. NO STATUS MESSAGE. THIS ITEM CLEARS DMI 115154. MCC NOTIFIED.<BR /></P>)

Part: DUCT — BROKEN (CARGO BAY) · airframe 80,414 hrs · 20,997 cycles

AFT CARGO HEAT INOP. AFT CARGO HEAT DUCT BROKEN IN FOUR PLACES BETWEEN STA 1100 AND STA 1200.(<P>TRANSFER TO MDDR 114885, CAT "C", DUE DATE 27-JUL-19. PLACARD INSTALLED AND MCC NOTIFIED.</P><P>LP 1091275 - M7: REMOVED AND REPLACED BROKEN SECTION OF CARGO HEAT DUCT AT STA 1200 IAW AMM 21-40-01. DMI #114885 REMAINS OPEN FOR FURTHER DUCT REPLACEMENT. OFF PART (P/N:&NBSP;214T6113-56, S/N: NSN).&NBSP;</P><P>LP 1090373 - M8: INSTALLED AFT CARGO HEAT DUCTS PER AMM 21-41-01. OPS CHECK GOOD AT THIS TIME. THIS CLEARS MDDR #114885. MCC NOTIFIED. PLACARDS REMOVED.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 80,411 hrs · 20,994 cycles

FWD EQPT OVHT EICAS MESSAGE AFTER TAKE OFF, LIGHT DID NOT STAY ON AFTER QRH WAS RUN. (<P>PLACED EQUIP COOLING SELECTOR BACK TO AUTO IAW AMM 21-58-00.</P><P>LP 1091265 - M7: PERFORMED OPS CHECK OF EQ. COOLING SYSTEM IAW 21-58-00, OPS GOOD AT THIS TIME.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 80,404 hrs · 20,990 cycles

FWD CGO BACKUP EICAS (<P><SPAN>PERFORMED BITE ON XONE TEMP MODULE IAW FIM 21-61 FT 804. NO DEFECTS NOTED AT THIS TIME.</SPAN></P>)

Part: VALVE — FAULTY (CABIN TEMP) · airframe 80,394 hrs · 20,978 cycles

&NBSP;FWD CABIN TEMP EICAS MESSAGE APPEARED DURING CRUISE&NBSP;(<P>UPON INSPECTION FOUND INOP LIGHT ILLUMINATED T/S PER FIM 21-60 FT 806 BITE CHECK ZONE TEMP CONTROLLER. FOUND FWD CABIN ZONE TRIM AIR VALVE LIGHT ON. ITEM TRANSFERRED TO MDDR 114274 PER DDG 21-61-04-02 CAT "C"&NBSP;</P><P>R/R TRIM AIR VALVE IAW AMM&NBSP;</P>)

Part: SCREEN — DIRTY (TEMP SENSOR) · airframe 80,386 hrs · 20,970 cycles

"FWD CABIN TEMP" EICAS WITH FWD CAB INOP LIGHT ALSO ILLUMINATED. (<P>CLEANED FWD CABIN TEMP SENSOR SCREEN IAW AMM 21-61-00. OPS CHECK GOOD AT THIS TIME.</P>)

Part: VALVE — MALFUNCTIONED (E/E BAY) · airframe 80,377 hrs · 20,963 cycles

FWD EQUIPMENT VALVE ADVISORY MESSAGE. REMOVED AND REPLACED DAMAGED EQUIPMENT COOLING EXHAUST DUCT IN FWD LOWER CARGO FLOOR WITH NEW. LEAK CHECKS GOOD IAW AMM 27--58-05. REMOVED AND REPLACED OVERBOARD EXHAUST VALVE IAW AMM 21-58-05 OPS AND CHECKS LEAK CHECKED GOOD.

Part: TERMINAL — LOOSE (OVERHEAT LOOP) · airframe 80,371 hrs · 20,957 cycles

RH ENG OVERHEAT LOOP 1 STATUS MSG. T/S IAW FIM 26-11 FT 804, TESTED FIRE DETECTION SYSTEM, NO FAULTS OR MESSAGES FOUND. INSP FIRE O/H CARDS, RE-RACKED AND SECURED. NO FAULTS FOUND. T/S PER WDM 26-11-22. CONTINUITY AND MEG CHECK OF WIRE OK. REMOVED AND REPLACED TERMINAL ON T5684 DETECTOR IAW SWPM 20-30-11. OPS CHECKED OK IAW AMM 26-11-00.

Part: FIRE DETECTOR — FAULTED (RT ENGINE) · airframe 80,359 hrs · 20,948 cycles

R ENG OH LP 1 STATUS MESSAGE PRIOR TO BLOCK OUT. REMOVED UPPER FWD FIRE DETECTOR IAW AMM 26-11-02-024-001. REPLACED DETECTOR IAW AMM 26-11-02-141-038. PERFORMED OPS CK PER AMM SUBTASK 26-11-02-861-002, OPS CK GOOD. THIS ACTION CLEARS MDDR 113417.</P>)

Part: CONTROLLER — MALFUNCTIONED (CABIN TEMP) · airframe 80,362 hrs · 20,951 cycles

FWD CABIN TEMP EICAS. RESET ZONE TEMP CONTROLLER IAW AMM 21-61-00. NO DEFECTS NOTED.

Part: CLAMP — MISSING (BLEED AIR) · airframe 80,313 hrs · 20,908 cycles

RH ENG OVHT LP 1 STS MSG. A/C FLEW FOR TWO DAYS WITH OUT REPEAT STATUS MESSAGE. OPS CHECK IAW 26-10-00 SUCCESSFUL. PERFORMED VISUAL INSPECTION OF FIRE LOOP 1 FOUND 3 CLAMPS MISSING ON O/B AFT LWR LOOP IAW AMM 26-11-02. NOTIFIED MCC OF FINDINGS. INSTALLED MISSING CLAMPS IN AFT LWR LOOP. FOUND FWD UPPER LOOP TOUCHING METAL IN DIFFERENT PLACES. ADJUSTED FWD UPPER LOOP PER AMM 26-11-00/501. OPERATIONAL TEST FIRE SYS. IAW AMM 26-11-00. MSG CLEARED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 80,315 hrs · 20,910 cycles

ON CLIMBOUT, FWD CGO BACKUP EICAS MSG RAN APPROPRIATE NNC, MESSAGE REMAINED. MESSAGE DISAPPEARED FIVE MINUTES LATER.(<P>TROUBLESHOT FAULT MSG FOR FWD CARGO BACKUP IAW FIM TASK 21-61-43-803, OPS CHECK GOOD. NO DEFECTS AT THIS TIME.</P>)

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 80,294 hrs · 20,892 cycles

"APU FAULT" ON TAXI IN.(<P>ECU FAULT "NO LIGHT". TRANSFERRED TO DMI 111843 IAW MEL 49-11-01A. YM @ 15:01.(M) PROCEDURE C/W. EXPIRES 28MAY19.</P><P>LP 0994059 - M2: PERFORMED T/S IAW FIM 49-11 FT 988. PERFORMED APU BITE, NO MSG OR FAULTS FOUND. STARTED APU, OPS CHECK NORMAL. THIS CLEARS MDDR 111843. PLACARD REMOVED AND&NBSP;MCC ADVISED.&NBSP;</P><P>ALSO OPENED MDDR 111857 - APU COLD SOAK START REQUIRED (DDG 25-AP-01)&NBSP;<BR /></P>)

Part: DUCT — DAMAGED (APU) · airframe 80,264 hrs · 20,866 cycles

"APU FAULT" ON TAXI IN(<P>ECU FAULT "NO LIGHT". TRANSFERRED TO DMI 111170 IAW MEL 49-11-01A, NT 1418Z. MX PROCEDURE C/W, EXPIRES 14MAY19.</P><P>LP 958478 - M2: FOUND HOLE IN APU AIR SURGE DUCT.&NBSP; REMOVED AND REPLACED AIR SURGE DUCT IAW AMM 20-11-01 AND 49-11-01. PERFORMED OPS AND LEAK CHECK, OPS CHECK GOOD. THIS CLEARS MDDR 111170. PLACARD REMOVED AND MCC NOTIFIED.&NBSP;</P>)

Part: CONTROL VALVE — FAULTY (AC BAY) · airframe 80,271 hrs · 20,870 cycles

LT PACK INOP.(<P>TRANSFERRED TO MDDR 111166 MEL 21-51-01-01.</P><P>REF LOG PAGE 958476 ITEM M3; REMOVED AND REPLACED ACM IAW AMM 21-51-03. ACM CHECK NORMAL. PER SUBTASK 21-51-031-744-047 BITE CHECK LEFT PACK TEMP CONTROL. FOUND TEMP CONTROL VALVE FAULTY. ACM OFF S/N 33-2729&NBSP; &NBSP;OFF P/N 680540-4</P><P>REF LOG PAGE 9548480 ITEM M2; REMOVED AND REPLACED LEFT PACK TEMP CONTROL VALVE IAW AMM 21-51-12. OPS CHECK GOOD. THIS CLEARS DMI 111166.&NBSP;</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 80,271 hrs · 20,870 cycles

L PACK TEMP EICAS MESSAGE IN FLIGHT(<P>PERFORMED BITE TEST OF THE LEFT PACK TEMP CONTROLLER OPS CHECKED GOOD AT THIS TIME IAW FIM 21-51-00 TREE 805</P>)

Part: VALVE — DAMAGED (RT IDG) · airframe 80,215 hrs · 20,821 cycles

RIGHT ENGINE IDG COOLING VALVE MUCSLE LINE DAMAGED. REMOVED AND REPLACED R/H ENG COOLING VALVE. OPS CHECK NORMAL IAW AMM 24-11-07.</P>)

Part: LAMP — INOPERATIVE (FIRE BOTTLE) · airframe 80,123 hrs · 20,744 cycles

AFT CARGO COMPARTMENT SQUIB TEST 2 AND FIRE BOTTLE 1 INOP.(<P>RELAMPED AND RESET C/B FOR AFT CARGO COMPARTMENT SQUIB TEST 2 OPS CHECK GOOD PER AMM 26-23-00 MDDR. #107863 CLEARED.</P>)

Part: CONNECTOR — DIRTY (FLOW CONTROL) · airframe 79,984 hrs · 20,649 cycles

FLT DECK AIRFLOW NOISE IS EXCESSIVE DIFFICULT TO COMMUNICATE(<P>ACCOMPLISHED CHECK OF LEFT PACK FLOW CONTROL VALVE AS PER FIM FAULT CODE 21-20 01-00 AND FOUND V16 CONNECTOR&NBSP; DISRTY ,CLEANED AND E INSTALLED CONNECTOR&NBSP; AS PER AMM 21-51-01 OPS CHECK NORMAL&NBSP; NO NOISE IN THE COCKPIT&NBSP;</P>)

Part: PRESSURE SWITCH — INOPERATIVE (FUEL BOOST) · airframe 79,946 hrs · 20,600 cycles

LEFT AFT BOOST PUMP PRESSURE LIGHT INOP.(<P>REMOVED AND REPLACED L/H AFT FUEL PUMP PRESSURE SWITCH IAW B767 AMM 28-42-01, OPS CHECK GOOD AT THIS TIME.</P>)

Part: PRESSURE SWITCH — FAILED (FUEL SYSTEM) · airframe 79,939 hrs · 20,593 cycles

WITH FUEL PUMPS IN OFF POSITION LH FUEL SYS PRESS EICAS CAUSIOIN MSG DOESNT COME ON . LH FWD PUMP PRESS LIFHT ON EICAS MESSAGE WILL NOT DISPLAY, EVEN WITH THE CB PULLED AND COLLARD BY MTX.&NBSP; &NBSP;(NOTE - LH FWD FUEL PMP PRESS ALREADY ON DEFERRAL ON MDDR 104147)(<P>REMOVED AND REPLACED LH FWD FUEL PRESSURE SWITCH IAW ATLAS B767 AMM 28-42-01 OPS CHECK GOOD. THIS CLEARS MDDR 104147. REMOVED PLACARDS NOTIFIED MCC&NBSP;</P>)

Part: PRESSURE SWITCH — MALFUNCTIONED (FUEL SYSTEM) · airframe 79,939 hrs · 20,593 cycles

L/H FWD FUEL PRESSURE LIGHT INOP. REMOVED AND REPLACED LH FWD FUEL PRESSURE SWITCH IAW ATLAS B767 AMM 28-42-01, OPS CHECK GOOD.

Part: LIGHT — INTERMITTENT (FUEL PUMP) · airframe 79,935 hrs · 20,588 cycles

L AFT FUEL PUMP PRESS LIGHT INOP.(<P>TRANSFER TO MDDR 104048 AS PER MEL 28-42-01-01 CAT C.</P><P>LP 815713-M2 PERFORMED OPS CHECK OF LH AFT&NBSP; FUEL PUMP PRESS LIGHT IAW AMM 28-42-01 OPS CHECK GOOD&NBSP; THIS CLEARED MDDR 104048&NBSP;</P>)

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 79,930 hrs · 20,580 cycles

AIRCRAFT CABIN PRESSURIZES AT REATES OF 2000+ FEET PER MINUTE ON THE GROUND WHEN APU BLEED SWITCH IS SELECTED - OUTFLOW VALVE SHOULD BE FULL OPEN AT ALL TIMES WITH WEIGHT ON WHEELS. HURTS EARS(<P>PERFORMED FIM TASK 21-31 FT 803 AND OPS CHECK CABIN PRESS SYST. IAW B767 AMM 21-31-00 NO DEFECTS NOTED AT THIS TIME. ACFT OK FOR SERVICE.</P>)

Part: STARTER — FAILED · airframe 79,908 hrs · 20,566 cycles

ENGINE STARTER FAILED(<P>R&AMP;R ENGINE STARTER IAW AMM 80-11-01. OPS CHECK &AMP; LEAK CHECKS GOOD.&NBSP;<BR /></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT STARTER) · airframe 79,887 hrs · 20,553 cycles

DURING CLIMB LEFT ENGINE STARTER EICAS. START VALVE LIGHT NOT ILLUMINATED&NBSP;(<P>ACCOMPLISHED MOTORIZED THE ENGINE IAW B767 AMM 71-00-00 START VALVE OPERATED NORMAL REF AMM ENGINE START SYSTEM TEST IAW 80-11-00</P>)

Part: START VALVE — WARNING MESSAGE (LEFT) · airframe 79,887 hrs · 20,553 cycles

LEFT STARTER CUTOUT CAUTION, LEFT ENGINE STARTER ADVISORY&NBSP;(<P>TRANSFERRED TO MDDR 103217 PER DDG 80-00-02-01 CAT "C"&NBSP;</P><P>LOG PAGE 815279 REMOVED AND REPLACED L ENG START VALVE AS PER AMM 80-11-02 OPS CHECKED GOOD AT THIS TIME , MDDR # 103217 CLOSED&NBSP;</P>)

Part: CONTROLLER — MALFUNCTIONED (HP) · airframe 79,861 hrs · 20,517 cycles

L ENG HPSOV STATUS MSG(<P>TRANSFER TO MDDR 102441 IAW MEL 36-11-02-02 CAT DUE DATE 18 NOV18</P><P><BR DATA-MCE-BOGUS="1" /></P><P>REMOVED &AMP; REPLACED HP CONTROLLER IAW AMM 36-11-08 OPS CK &AMP; ENG RUNS NML IAW AMM 71-00-00</P>)

Part: CIRCUIT CARD — FALSE INDICATION (NR 1 FIRE LOOP) · airframe 79,860 hrs · 20,516 cycles

L ENG FIRE LP 1 STATUS MSG.(<P>TRANSFERRED TO MDDR # 102390 PER MEL 26-11-01, CAT C. DUE 17NOV18. DISPATCH YM @ 1233Z</P><P>LP 1017027 -M3 REMOVED AND REPLACED M10224 FIRE&NBSP; OVERHEAT CARD&NBSP; IAW AMM 26-10-01 OPS CHECK GOOD&NBSP; CLEARED MDDR&NBSP;</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (LT ENG FIRE LOOP) · airframe 79,860 hrs · 20,516 cycles

L ENG OH LP1 STATUS MSG.(<P>TRANSFERRED TO MDDR 102391 PER MEL 26-11-02-01. CAT C. DISPATCH YM @ 1233Z</P><P>LP 1017028 REFERENCES&NBSP; LOG PAGE&NBSP; 1017027 ITEM M3 FOR DMI CLOSURE PERFORMED FIRE LOOP TEST IAW AMM 26-10-01 TEST OK</P>)

Part: MAGNETIC SEAL — MALFUNCTIONED (NR 2 ENGINE) · airframe 79,844 hrs · 20,495 cycles

CAPPED # 2 ENGINE DRAIN LINES STARTER, IDG,FUEL PUMP,HMU AND HYDRAULIC PUMP AS PER AMM 71-71-00 &AMP; ECM 2018P-704 FOR 10 FC ( ACTUAL FC 20490 ) ( DUE TO HIGH OIL CONSUMPTION )(<P>TRANSFER TO NON MEL&NBSP; MDDR 101809 FOR AMM 71-71-00 FOR 10 FC</P><P><BR DATA-MCE-BOGUS="1" /></P><P>LOG PAGE 1017004:REPLACED CARBON SEAL AND MAGNETIC SEAL ASSEMBLY IAW AMM72-64-02-404, CAP REMOVED FROM DRAIN REPLACED<BR DATA-MCE-BOGUS="1" /></P><P><BR /></P>)

Part: SHUTOFF VALVE — FAULTY (BLEED AIR SYS) · airframe 79,814 hrs · 20,457 cycles

LEFT DUCT PRESSURE CYCLING BETWEEN 40-10 PSI BELOW 10000 FEET ON CLIMB AND DESCENT. REMOVED AND REPLACED LEFT PRSOV IAW AMM 36-11-00. OPS CK NORMAL.

Part: CIRCUIT CARD — DEFECTIVE (FIRE WARNING) · airframe 79,807 hrs · 20,448 cycles

RT ENG FIRE LOOP 1 STATUS MSG(<P>ITEM PLACED ON MEL 26-11-01-01 CAT C MDDR 101012 DUE DATE 22OCT18.</P><P>T/S PER FIM 26-11 FT 804. PER BLOCK 104B BELL/CHIME AURAL WARNING MODULE(M1000) + ALFOTS NR 2 CARD (M10274) REQUIRE REPLACEMENT, REPLACED M10274 IAW AMM 26-10-01. TEST GOOD PER AMM 26-10-01. THIS CLEAR DMI# 101012.</P>)

Part: UNKNOWN — MALFUNCTIONED (BLEED AIR SYS) · airframe 79,807 hrs · 20,448 cycles

ON CLIMB OUT DUCT PRESS FLUCTUATES BETWEEN 30 AND 40 PSI TIL 10,500' ON APPROACH SHUT R PACK OFF, LEFT DUCT SURGED.(<P>PERFORMED AIR SUPPLY BITE TEST IAW 36-23-00 NO DEFECTS NOTED AT THIS TIME. PER AMM 36-10-00 DUCT PRESS IS REGULATED BETWEEN 30 PSI AND 50 PSI.</P>)

Part: FILTER — DIRTY (BLEED AIR SYS) · airframe 79,800 hrs · 20,438 cycles

LEFT DUCT PRESSURE FLUCTUATES DURING CLIMB(<P>PER FIM 36-10 FAULT TREE 831. INSPECTED AND CLEANED NR 1 PRSOV AIR FILTERS IAW AMM 36-11-04. OPS CHECK GOOD AT THIS TIME. <BR /></P>)

Part: UNKNOWN — MALFUNCTIONED (BLEED AIR SYS) · airframe 79,800 hrs · 20,438 cycles

LEFT DUCT PRESSURE FLUCTUATES BETWEEN 10 PSI TO 30 PSI ON CLIMB OUT(<P>PERFORMED BITE TEST ON AIR SUPPLY, NO FAULTS IN IAW AMM 36-20-00. NO FAULTS NOTED AT THIS TIME. A/C OK FOR SERVICE <BR /></P>)

Part: PIN — CORRODED (WINDOW HEAT) · airframe 79,782 hrs · 20,414 cycles

REF MDDR 100135 - RT SIDE WINDOW HEAT&NBSP;(<P>RANG WIRES OUT, FOUND PIN ON RT WINDOW SENSOR TO BE CORRODED. REMOVED AND REPLACED PIN IAW SWPM 20-10-11 OPS CHECK GOOD . MCC ADVISED PLACARDS REMOVED&NBSP;</P>)

Part: BLEED AIR SYS — SURGES · airframe 79,769 hrs · 20,398 cycles

AFTER TAKE OFF DUCT PRESSURES SURGE BETWEEN 20&AMP;40 PSI FOR SEVERAL CYCLES THEN STABILIZED(<P>PERFORMED BITE TEST OF AIR SUPPLY MODULE IAW B767 AMM 36-23-00. BITE TEST OK NO DEFECTS NOTED AT THIS TIME</P>)

Part: BLEED AIR SYS — ABNORMAL · airframe 79,770 hrs · 20,399 cycles

AFTER&NBSP; TAKE OFF DUCT PRESSURE SOURCE BETWEEN 20 AND 40 PSI FOR SEVERAL CYCLES THEN STABILIZED(<P>PERFORMED BITE TEST OF AIR SUPPLY MODULE IAW AMM 36-23-00 BITE TEST OK&NBSP; NO DEFECTS NOTED&NBSP;</P>)

Part: ENGINE — ABNORMAL (NR 1) · airframe 79,769 hrs · 20,398 cycles

#1 ENGINE TRIM BALANCE REQUIRED.(<DIV>PERFORMED #1 ENGINE TRIM BALANCE IAW 72-31-00-705-119. PER MCC GLEN ITEM IS NOT RII.</DIV>)

Part: HEATER — INOPERATIVE (RT WINDOW) · airframe 79,768 hrs · 20,397 cycles

RH SIDE WINDOW HEAT INOP(<P>PLACED RH SIDE WINDOW HEAT ON MEL 30-41-01-02 CAT C DUE&NBSP; DATE 05OCT18 MDDR # 100135 .&NBSP;</P>)

Part: UNKNOWN — MALFUNCTIONED (AC PACK) · airframe 79,752 hrs · 20,374 cycles

LEFT AC PACK SURGES DURING T/O AND ON APPROACH. PERFORMED BITE CHECK ON LT PACK CONTROLLER IAW AMM 21-51-00 NO FAULTS FOUND. RUN LT PACK IAW AMM 21-51-00 WITH NO SURGES. OK FOR SERVICE.

Part: PACKING — DAMAGED (NR 1 ENGINE) · airframe 79,736 hrs · 20,371 cycles

SEEPING OIL NO 1 ENG AND LOWER SIDE AT FWD HORIZONTAL DRIVE SHAFT HOUISING OIL SEEPING. IAW AMM 80-11-02-002-001 AND 80-1-02-402-009 AND 72-63-02-0040995 AND 72-63-02-404-016 AND 80-11-01-004-001 AND 80-11--01-404-012 REV 125 REPLACED PACKING. IAW AMM 71-00-00-712-68 AND 71-00-00-795-034 REV 125 PRF THE LEAK CHECK AND NO LEAK WAS FOUND. COMPLETED THIS JOB AND CONDITION CHECK SATISFACTORY.

Part: PACKING — DAMAGED (NR 1 ENGINE) · airframe 79,736 hrs · 20,371 cycles

FOUND NR 1 ENG A-SUMP OIL LEAK. IAW AMM 72-31-03-004-001 & 72-31-03-404-005 REV 125 REPLACED PACKING. IAW 71-00-00-795-034 REV 125 PERFORM IDLE LEAK CHK RESULT. NO LEAK FOUND 3. COMPLETED THIS JOB AND CONDITION CHECK NORMAL.

Part: RIVET — LOOSE (NR 2 COWLING) · airframe 79,726 hrs · 20,366 cycles

LOOSE RIVET NR 2 ENG RT CORE COWL 4E WEAR STRIP NEAR 3 O'CLOCK. REMOVE DAMAGE RIVET IAW SRM 51-40-02 REV 108. INSTALL NEW RIVET IAW SRM 51-40-02 REV 108 AND CMM 71-13-24 REV 43. JOB COMPLETED AND COND CHK NML.

Part: COWLING — DENTED (NR 2 ENGINE) · airframe 79,736 hrs · 20,371 cycles

DENT, INNER BARREL NR 2 ENG NOSE COWL NEAR 10 O'OCLOCK. REPLACE NR 2 ENG INLET COWL.

Part: SENSOR — ABNORMAL (AC BAY) · airframe 79,736 hrs · 20,371 cycles

BITE TEST ON STANDBY CONTROLLER FOUND R/K COMPT SENSOR NO GO. IAW AMM 21-51-23 REV 18 PERFORM WRONG CHECK. RESULT WAS NORMAL. IAW AMM 21-51-06-004-001/404-011 REV 125 RPL SENSOR TS 5135. IAW AMM 21-51-14-700-802-001 REV 125 PFM PACK STANDY CONTROLLER BITE, RESULT WAS SATISFACTORY.

Part: BRACKET — WORN (NR 2 COWLING) · airframe 79,726 hrs · 20,366 cycles

WORN STOP PLATE NR 2 ENG RT CORE COWL PRESSURE RELIEF DOOR 2EA LATCH. REMOVE DAMAGE PARTS IAW SRM 51-40-02 REV 108. INSTALL NEW PARTS IAW SRM 51-40-02 REV 108 AND CMM 71-13-24 REV 43. JOB COMPLETED AND COND CHK NML.

Part: BUSHING — WORN (NR 2 COWLING) · airframe 79,726 hrs · 20,366 cycles

WORN BUSHING AND PIN NR 2 ENG RT CORE COWL PRESSURE RELIEF DOOR 2EA HINGE. REMOVE DAMAGE PART IAW SRM51-40-02 REV 02 REV 108. INSTALL NEW PART IAW SRM 51-40-02 REV 108 AND CMM 71-13-24. JOB COMPLETED AND COND CHK NML.

Part: DETECTOR — DEFORMED (COOLING SYS) · airframe 79,726 hrs · 20,366 cycles

FOUND E&E COOLING LOW FLOW DETECTOR CONNECTOR BASE DEFORM. IAW AMM 21-58-17-022-001 AND AMM 21-58-17-422-008 REV 125. RPL AND PFM INSTALLATION TEST RESULT PASSED. COND CHK NML.

Part: RUB STRIP — BROKEN (NR 2 COWLING) · airframe 79,726 hrs · 20,366 cycles

BROKEN RUB STRIP NR 2 ENG NOSE COWL T/E, NEAR 3 O'CLOCK POSITION. REPLACE THE WEAR STRAP WITH NEW IAW SRM 51-40-02-06-0 REV 108 AND CMM 71-11-16 FIGURE 8 REV 45 AND SPM 70-13-01 REV 107. JOB COMPLETED AND COND CHK NML.

Part: STRAP — WORN (LT COWLING) · airframe 79,736 hrs · 20,371 cycles

RIVET NR 1 ENG LT CORE COWL INNER AFT UPPER WEAR STRAP RIVET WORN. REMOVE DAMAGE PARTS IAW SRM 51-40-02 REV 108. INSTALL NEW PARTS IAW SRM 51-40-02 REV 108 AND CMM 71-13-23 REV 40. JOB COMPLETED AND COND CHK NML.

Part: ADAPTER — WORN (NR 2 COWLING) · airframe 79,726 hrs · 20,366 cycles

WORN BRACKET AND ADAPTER NR 2 ENG RT CORE COWL HOLD OPEN ROD. REMOVE DAMAGE PARTS IAW SRM 51-40-02 REV 108. INSTALL NEW PARTS IAW SRM 51-40-02 REV 108 AND CMM 71-13-24. JOB COMPLETED AND COND CHK NML.

Part: RELAY — FAILED · airframe 79,726 hrs · 20,366 cycles

FOUND RELAY K835 FUNCTION FAIL DURING COOLING FAN OPERATIONAL TEST. IAW SWPM20-81-22 REV 68 REPLACED RELAY K835. IAW AMM 21-58-41-400-801-002 REV 125 PERFORMED OP TEST, AFT CGO EQUIP COOLING FAN SYS, SATISFY.

Part: ACOUSTIC LINER — BROKEN (NR 2 ENGINE) · airframe 79,726 hrs · 20,366 cycles

BROKEN MID ACOUSTIC LINER NR 2 ENG FAN CASE NEAR 12 O'CLOCK. IAW AMM 72-33-01-004-001 AND AMM 72-33-01-404-011 REV 125 REPLACED NR 2 ENG MID ACOUSTIC LINER.

Part: BRACKET — CHAFED (NR 1 COWLING) · airframe 79,726 hrs · 20,366 cycles

CHAFING BRACKET NR 1 ENG LT CORE COWL INNER FWD SUPPORT BRACKET CHAFING. REMOVE DAMAGE PARTS IAW SRM 51-40-02 REV 108. INSTALL NEW PARTS IAW SRM 51-40-02 REV 108 AND CMM 71-13-23 REV 40. JOB COMPLETED AND COND CHK NML.

Part: NUT PLATE — MISSING (NR 2 COWLING) · airframe 79,726 hrs · 20,366 cycles

MISSING NUTPLATE NUT PLATE NR 2 ENG NOSE COWL HR FWD 2EA HOIST POINT. REINSTALL NUTPLATE REFER TO JOB CARD ATTACHING SHEET NR 0137453. JOB DONE COND CHK NML.

Part: LATCH — WORN (NR 1 COWLING) · airframe 79,726 hrs · 20,366 cycles

WORN LATCH NR 1 ENG RT FAN COWL OIL TANK ACCESS DOOR LATCH WORN TOTAL 2EA. REMOVE DAMAGE WEARSTRIP IAW SRM51-40-02 REV 108. INSTALL NEW WEARSTRIP IAW SRM 51-40-02 REV 108 AND CMM 71-13-22 REV 43. REMOVE DAMAGE LATCH IAW SRM 51-40-02 REV 108. INSTALL NEW LATCH IAW SRM 51-40-02 REV 108 AND AIPC 71-11-10-51 REV 35. JOB COMPLETED AND COND CHK NML.

Part: BRACKET — WORN (NR 2 COWLING) · airframe 79,726 hrs · 20,366 cycles

WORN BRACKET AND ADAPTER NR 2 ENG LT CORE COWL HOLD OPEN ROD. REMOVE DAMAGE PARTS IAW SRM 51-40-02 REV 108. INSTALL NEW PARTS IAW SRM 51-40-02 REV 108 AND CMM 71-13-23 REV 40. JOB COMPLETED AND COND CHK NML.

Part: RIVET — MISSING (NR 2 COWLING) · airframe 79,726 hrs · 20,366 cycles

MISSING RIVETS NR 2 ENG LT CORE COWL T/E UPPER SIDE WEAR STRIP. INSTALL NEW RIVETS IAW SRM 51-40-02-04-0 REV 108 AND CMM 71-13-24 REV 43. JOB COMPLETED AND COND CHK NML.

Part: NUT PLATE — WORN (TRANSLATING COWL) · airframe 79,726 hrs · 20,366 cycles

WORN NUTPLATE NR 1 ENG RT T/R TRANSLATING COWL FWD LOCKOUT PLATE NUTPLATE WORN AT LOWER AND MID LOCKOUT PLATE. REMOVE DAMAGE NUTPLATE IAW SRM 51-40-02-06-0 REV 108. INSTALL NEW NUTPLATE IAW SRM 51-40-02-06-0 REV 108 AND IPC 78-32-32 FIGURE 1A SHEET 4. REV 80. JOB COMPLETED AND COND CHK NML.

Part: ACOUSTIC LINER — BROKEN (NR 2 ENGINE) · airframe 79,726 hrs · 20,366 cycles

NR 2 ENG FAN CASE FWD ACOUSTIC LINER PLASTIC COVER BROKEN. IAW AMM 72-33-01-004-001 REV 125 RMV ACOUSTIC LINER. RBF J/C ATTACHING SHEET 0137454 REPAIR ACOUSTIC LINER. IAW AMM 72-33-01-404-011 REV 125 INSTALL ACOUSTIC LINER.

Part: SKIN — SCRATCHED (NR 1 COWLING) · airframe 79,726 hrs · 20,366 cycles

SCRATCH SURFACE NR1 ENG CORE COWL LGH EXTERNAL SURFACE SRATCH. ACCOMPLISHED DAMAGE AREA IAW EO NO 1971A191 REV 0. JOB COMPLETED COND CHK NML.

Part: SKIN — CRACKED (NR 2 COWLING) · airframe 79,726 hrs · 20,366 cycles

CRACK OUTER SURFACE NR 2 ENG RT CORE COWL NAC UTA-273 TO 295 NEAR 2 O'CLOCK. ACCOMPLISHED DAMAGE AREA IAW ED NO 1971A190 REV 0. JOB COMPLETED AND COND CHK NML.

Part: PRESSURE SWITCH — DEFECTIVE (ANTI-ICE SYS) · airframe 79,726 hrs · 20,366 cycles

NR 1 ENG TAI PRESSURE SW FAIL TEST. IAW AMM 30-21-01-004-001 AND AMM 30-21-01-404-022 REV 125 REPLACED NR 1 ENG TAI PRESSURE SW AND TEST PASSED ALL COND CHK NML.

Part: SHUTOFF VALVE — FAILED (BLEED AIR SYS) · airframe 79,736 hrs · 20,371 cycles

PFM NR 1 ENG HEALTH CHK FOR PRSOV FOUND REGULATED FUNCTIONAL FAIL. IAW AMM 36-11-09-002-033-001 REV 125 AND AMM 36-11-09-402-058-001 REV 125 REPLACED NO 1 ENG PRSOV. IAW AMM 36-11-09-402-058 REV 125 STEP G PRM PRSOV TEST RESULT NORMAL. IAW AMM 36-11-09-402-058 REV 125 STEP N PUT THE AIRCRAFT BACK TO USUAL CONDITION.

Part: SKIN — CRACKED (NR 2 COWLING) · airframe 79,726 hrs · 20,366 cycles

CRACK OUTER SURFACE NR 2 ENG RT CORE COWL T/E NEAR 4 O'CLOCK POSITION QTY 2 EA. ACCOMPLISH EO NR 1971A188 REV 0. JOB COMPLETED AND COND CHK NML.

Part: RIVET — WORN (NR 1 COWLING) · airframe 79,726 hrs · 20,366 cycles

WORN RIVETS NR 1 ENG LT CORE COWL INNER AFT FRAME RIVET WORN. REMOVE DAMAGE RIVETS IAW SRM 51-40-02 REV 108. INSTALL NEW RIVETS IAW SRM 51-40-02 REV 108 AND SRM 54-42-02-2R-1 REV 108. COMPLETED AND COND CHK NML.

Part: SEAL — CHAFED (NR 2 COWLING) · airframe 79,726 hrs · 20,366 cycles

CHAFING SPRING SEAL NR 2 ENG RT CORE COWL UPPER SIDE. REMOVE DAMAGE PART IAW SRM 51-40-02 REV 108. INSTALL NEW PARTS IAW SRM 51-40-02 REV 108 AND CMM 71-13-24 REV 43. JOB COMPLETED AND COND CHK NML.

Part: EXTRACTOR — LEAKING (AC BAY) · airframe 79,726 hrs · 20,366 cycles

FOUND AIRLEAK AT EXTRACTOR DUCT OF LT PACK. IAW AMM 21-51-04-004-001 AND AMM 21-51-04-404-015 REV1.25 RPL THE EXTRACTOR. IAW AMM 21-00-00-0862-024 REV 125 PFM LEAK CHECK RESULT NO LEAK FOUND AND JOB COMPLETED.

Part: PRESSURE SWITCH — FAILED (NR 1 ENGINE) · airframe 79,736 hrs · 20,371 cycles

FOUND NR 1 ENG FUEL FILTER DIFFERENTIAL PRESSURE SWITCH FUNCTION TEST FAIL. IAW AMM 73-34-01-024-001 REV 125 AND AMM 73-34-01-424-008 REV 125 REPLACE NR 1 ENG FUEL FILTER DIFFERENTIAL PRESSURE SWITCH WITH NEW PARTS. IAW AMM 71-00-00-712-168 REV 125 NR 1 ENG FUEL FILTER DIFFERENTIAL PRESSURE SWITCH LEAK CHECK AND NO LEAK WAS FOUND. COMPLETED THIS JOB AND CONDITION CHECK NORMAL.

Part: NUT PLATE — MISSING (NR 1 COWLING) · airframe 79,726 hrs · 20,366 cycles

NR 1 ENG NOSE COWL RT UPPER SIDE HINGE POINT NUTPLATE MISSING. IAW AMM 71-11-01-004-002 AND AMM 71-11-01-404-005 REV 125 REPLACE NR 1 ENG INLET COWL. COND CHK NML.

Part: FRAME — CRACKED (NR 1 COWLING) · airframe 79,726 hrs · 20,366 cycles

CRACK EDGE NR 1 ENG LT CORE COWL EXTERNAL AFT EDGE AT LOWER SIDE CRACK. ACCOMPLISHED CRACK AREA REPAIR IAW EO NR1971A189 REV 0. REMOVE DAMAGED FRAME IAW 514002 REV108. INSTALL NEW FRAME IAW SRM 51-40-02 REV 108 AND CMM 71-13-23 REV 40. JOB COMPLETED COND CHK NML.

Part: LATCH — BROKEN (NR 2 COWLING) · airframe 79,726 hrs · 20,366 cycles

BROKEN CUTOUT EDGE NR 2 RT FAN COWL OIL TANK ACCESS DOOR FWD LATCH. REPAIRED DAMAGE AREA IAW CMM 71-13-22 REPAIR NR 11 REV 43. COND CHK NML JOB COMPLETE.

Part: RIVET — WORN (NR 1 COWLING) · airframe 79,726 hrs · 20,366 cycles

WORN RIVET NR1 ENG CORE COWL EXTERNAL RIVET WORN AT LOWER SIDE. REMOVED DAMAGED RIVET IAW SRM 51-40-02 REV 108. INSTALL NEW RIVET IAW SRM 51-40-02 REV 108 AND CMM 71-13-23 REV 40. JOB COMPLETED COND CHK NML.

Part: PRESSURE SWITCH — DEFECTIVE (ANTI-ICE SYS) · airframe 79,726 hrs · 20,366 cycles

NR 2 ENG INLET TAI PRESSURE SW TEST FAIL. IAW AMM 30-21-01-004-001 AND AM 30-21-01-404-002 REV125 REPLACED NR 2 ENG TAI PRESSURE SW AND TEST PASSED 2. COND CHK NML.

Part: BRACKET — CHAFED (NR 1 COWLING) · airframe 79,726 hrs · 20,366 cycles

CHAFING BRACKET NR 1 ENG RT CORE COWL INNER FWD SUPPORT ROD BRACKET CHAFING. REMOVE DAMAGE PARTS IAW SRM 51-40-02 REV 108. INSTALL NEW PARTS IAW SRM 51-40-02 REV 108 AND CMM 71-13-24 REV 43. JOB COMPLETED AND COND CHK NML.

Part: RIVET — WORN (APU BAY) · airframe 79,726 hrs · 20,366 cycles

LOOSEN RIVET LT APU DOOR INNER FWD LOWER FIRE DETECTOR SUPPORT BRACKET RIVET WORN. REMOVE DAMAGE RIVET IAW SRM 51-40-02-06-0 REV 108. INSTALL NEW RIVET IAW SRM 51-40-02-06-0 REV 108 AND DWG NUMBER 355T5200 SHEET 1 REV A. JOB DONE COND CHK NML.

Part: PRECOOLER — DAMAGED (BLEED AIR SYS) · airframe 79,736 hrs · 20,371 cycles

FOUND NR 2 ENG PRECOOLER OUTLET FINS FLAKED AWAY. IAW AMM 36-11-15-004-003-001 REV125 AND AMM 36-11-15-404-020-001 REV125 REPLACED NR 2 ENG PRE-COOLER. IAW AMM 36-11-09-782-138-001 REV 125 NO2 ENG PRE-COOLER LEAK CHECK.

Part: RIVET — WORN (NR 1 COWLING) · airframe 79,726 hrs · 20,366 cycles

WORN RIVET NR 1 ENG NOSE COWL AFT FLANGE WEAR STRAP RIVET WORN AT RT. REPLACE DAMAGE RIVET WITH NEW IAW SRM 51-40-02-06-0 REV 108 AND CMM 71-11-16 FIGURE 8 REV 45 AND 70-13-01 REV 107. JOB COMPLETED ABD COND CHK NML.

Part: COWLING — ERODED (NR 1 ENGINE) · airframe 79,726 hrs · 20,366 cycles

EROSION 4E NR1 ENG LT FAN COWL 4E LOWER SIDE EROSION. REMOVE DAMAGE MATERIAL AND CLEAN. MEASURE DAMAGE SIZE (=.6 IN, W=0.3IN) AT NR 1 ENG LT FAN COWL LEADING EDGE LOWER SIDE. BOND EDGE PROTECTOR W/ ADHESIVE, CURE AT 140F FOR 1HR IAW CMM 71-17-21 REPAIR NR 9 REV 42. COND CHK NML.

Part: FASTENER — LOOSE (LT COWLING) · airframe 79,726 hrs · 20,366 cycles

REPLACEMENT LOOSE FASTENERS ON NR 2 ENG LT CORE COWL. ACCOMPLISHED EI NO 72018A71M-4869 REV 0. JOB COMPLETED AND COND CHK NML.

Part: RIVET — WORN (NR 1 COWLING) · airframe 79,726 hrs · 20,366 cycles

WORN RIVET NR 1 ENG LT CORE COWL INNER AFT UPPER WEAR STRAP RIVET WORN. REMOVE DAMAGE PARTS IAW SRM 51-40-02 REV 108. INSTALL NEW PARTS IAW SRM 51-40-02 REV 108 AND CMM 71-13-23 REV 40. JOB COMPLETED AND COND CHK NML.

Part: COWLING — DENTED (NR 2 ENGINE) · airframe 79,736 hrs · 20,371 cycles

DENTS INNER BARREL NR 2 ENG NOSE COWL FROM 5 TO 7 O'CLOCK. IAW AMM 71-11-01-004-002 AND 71-11-01-404-005 REV125 REPLACED NR 2 ENG INNER COWL. COMPLETED THIS JOB AND CONDITION CHECK SATISFACTORY.

Part: ACCESS DOOR — DAMAGED (NR 1 COWLING) · airframe 79,726 hrs · 20,366 cycles

DOOR NR 1 ENG RT FAN COWL OIL TANK ACCESS DOOR EDGE DAMAGE. REPAIR DAMAGE AREA IAW CMM 71-13-22 REPAIR NR 11 REV 43. .COND CHK NML, JOB COMPLETE.

Part: LATCH — WORN (NR 1 COWLING) · airframe 79,726 hrs · 20,366 cycles

WORN LATCH NR 1 ENG RT CORE COWL PRESSURE RELIEF DOOR LATCH WORN BOTH. REMOVE DAMAGE PARTS IAW SRM 51-40-02-06-0 REV 108. INSTALL PARTS IAW SRM 51-40-02-06-0 REV 08 AND AIPC 71-11-08-51 REV35. JOB COMPLETED COND CHK NML.

Part: RIVET — LOOSE (TRANSLATING COWL) · airframe 79,726 hrs · 20,366 cycles

LOOSEN RIVETS NR 2 LT TRANSLATING COWL LOWER SIDE FAIRING. REMOVE DAMAGE RIVETS IAW SRM 51-40-02-06-0 REV 108. INSTALL NEW RIVETS IAW SRM 51-40-02-06-0 REV 108 AND IPC 78-32-31 REV 80. JOB COMPLETED AND COND CHK.

Part: INVERTER — NOT REPORTED · airframe 79,628 hrs · 20,316 cycles

STBY INVERTER REMOVED AND REPLACED. STATIC INVERTER PER AMM 24-33-03. OPS CHECK OK.

Part: CONTROLLER — FAILED (APU) · airframe 79,625 hrs · 20,315 cycles

APU BLEED AIR NO BLEED AIR PRESSURE FROM APU. REPLACED APU INLET GUIDE VANE ACTUATOR IAW AMM 49-52-02. P/N A64847-5 S/N1514 APU OPER STILL NO PNEUMATIC FUNCTION. APUC BITE P2 SENSEN FAULT REF FIM 49-11 FT A21. REPLACED APUC IAW 49-01-04. OPERATED APU PACKS. ADP ENG START MODE ALL FUNCTION SATISFACTORY.

Part: ISOLATION VALVE — FAILED (BLEED AIR SYS) · airframe 79,625 hrs · 20,315 cycles

LEFT BLEED ISOLATION VALVE STATUS MESSAGE. SWAPPED LEFT ISOLATION VALVE WITH CENTER ISOLATION VALVE AND TESTED LEFT ISOLATION VALVE IAW AMM 36-11-04 OPS CHECK GOOD. REMOVED AND REPLACED CTR ISOLATION VALVE IAW AMM 36-11-04 TEST OK.

Part: CHECK VALVE — MALFUNCTIONED (APU) · airframe 79,561 hrs · 20,306 cycles

APU PNEUMATIC FUNCTION INOP. REMOVED AND REPLACED APU PNEUMATIC CHECK VALVE IAW AMM 36-11-11. OPS CHECK GOOD AT THIS TIME.

Part: RELIEF VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 79,528 hrs · 20,290 cycles

RT ENGINE BLEED/PACK OFF LIGHT REMAINS ON AFTER ENGINE START DUCT PRESSURE RT 0 UNTIL THRUST IS INCREASED. IAW AMM 36-11-18 REMOVED AND REPLACED RT ENGINE PRV AND PERFORMED LEAK CHECK NORMAL IAW AMM 36-13-00 PERFORM AIR SUPPLY CONTROL BITE TEST AND NO FAULTS FOUND IAW AMM 71-00-00 PERFORMED ENGINE RUN TEST CHECK NORMAL.

Part: SHUTOFF VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 79,528 hrs · 20,290 cycles

RT ENGINE BLEED OFF EICAS MSG AFTER START, NO BLEED PRESSURE. PER AMM 36-11-09 REPLACED RIGHT ENGINE PRSOV AND LEAK CHECK, NO LEAK LEAK FOUND.

Part: PACKING — DAMAGED (BLEED AIR SYS) · airframe 79,524 hrs · 20,288 cycles

RT ENGINE BLEED LIGHT STAYS ON AFTER START UNTIL POWER IS INCREASED. INSPECTION FOUND PRV MUSCLE AIR TUBE DAMAGE, REMOVED AND REPLACED PACKING AND PERFORM LEAK TEST OK IAW AMM 36-11-18.

Part: SHUTOFF VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 79,518 hrs · 20,285 cycles

RT ENG BLEED LIGHT STAYS ON AFTER START UNTIL POWER IS INCREASED. RT ENG HPSOV PFM THUMB TEST ONLY. 10 SEC, R&R RT ENG HPSOV PFM ENG RUN TEST, NO LEAK FND. COND CHK NML IAW AMM 36-11-07, 71-00-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 79,515 hrs · 20,283 cycles

RT ENG STARTER CUTOUT AFTER START, SHUT DOWN ENGINE, MSG CLEARED. NORMAL START- 2ND ATTEMPT. RT ENG SAV OPERATION CHECK NORMAL WITH MOTORING IAW AMM 71-00-00.

Part: FIRE DETECTOR — FAULTY (RT ENGINE) · airframe 79,498 hrs · 20,275 cycles

RT ENG FIRE LP 2 STATUS MESSAGE. REMOVED AND REPLACED RT ENGINE UPPER AFT FIRE DETECTOR. OPERATIONAL TEST PASSED IAW AMM 26-11-02.

Part: CONTROLLER — NOT SEATED (APU BLEED SYS) · airframe 79,453 hrs · 20,269 cycles

APU BLEED INOP. RE-RACKED APUC & OPS CHK OK AS PER AMM TASK 49-11-00-802-002.

Part: CONTACT — DIRTY (FIRE WARNING) · airframe 79,453 hrs · 20,269 cycles

RT ENG FIRE LP 2. PERFORMED FIRE TEST & INSPECTION. CAK CONTACTED CLEANED, OPS CHK AS PER AMM TASK 26-11-00-16501.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 79,428 hrs · 20,264 cycles

RT ENG FIRE LP2 STATUS MSG. PERFORMED CHECK PER FIM 26-11 FAULT TREE 804 AND CHK NML.

Part: FIRE WARNING — ACTIVATED (COCKPIT) · airframe 79,375 hrs · 20,243 cycles

STATUS MSG "R ENG FIRE LP 2.

Part: BOTTLE — INOPERATIVE (EXTINGUISHER) · airframe 79,349 hrs · 20,235 cycles

EICAS FOR THE ENG BOTTLE NR 2. FOUND PRESSURE SWITCH ON THE BOTTLE INOPERATIVE, REMOVED AND REPLACED THE EXTINGUISHER BOTTLE IAW AMM 26-21-03-004-094. OPS CHECKED GOOD.

Part: PUMP — INOPERATIVE (FUEL BOOST) · airframe 79,359 hrs · 20,236 cycles

LEFT CENTER FUEL PUMP WAS INOPERATIVE. OPEN

Part: PUMP — UNKNOWN (FUEL BOOST) · airframe 79,344 hrs · 20,234 cycles

LEFT CENTER FUEL PUMP IS NOT INHIBITED, ON GROUND PRIOR TO ENGINE START. PERFORMED AN OPS CHECK OF THE LEFT CTR FUEL BOOST PUMP IAW AMM 28-22-00. OPS CHECK NORMAL.

Part: SHUTOFF VALVE — FAILED (NR 2) · airframe 79,334 hrs · 20,226 cycles

RIGHT PACK OFF EICAS MESSAGE, RESULTED FROM LOSS OF THE RT ENGINE BLEED. REMOVED & REPLACED THE NR 2 ENGINE PRSOV IAW AMM 36-11-09. CHECKED OK.

Part: SHUTOFF VALVE — FAILED (NR 2) · airframe 79,334 hrs · 20,226 cycles

RIGHT ENGINE BLEED OFF EICAS MESSAGE. REMOVED AND REPLACED THE NR 2 ENGINE PRSOV. OPS CHECKED GOOD IAW AMM 36-11-09.

Part: BLEED VALVE — MALFUNCTIONED (RT ENGINE) · airframe 79,330 hrs · 20,220 cycles

AFTER ENGINE SHUTDOWN, THE RIGHT ENGINE BLEED DOES NOT SHUT OFF. OPS CHECKED THE ENGINE BLEED AND CYCLED THE PRSOV IAW AMM 36-11-09. VALVE OPERATED NORMALLY. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 79,325 hrs · 20,213 cycles

AFTER ENGINE START, THE CABIN AUTO INOPERATIVE EICAS MESSAGE ACTIVATED. PERFORMED A BITE CHECK FOR FAULTS ON CABIN PRESSURE CONTROLLER. EICAS MESSAGE CLEARED IAW FIM 21-31, FAULT TREE 803.

Part: ANTI-ICE VALVE — WARNING MESSAGE (LEFT) · airframe 79,315 hrs · 20,203 cycles

WHEN TURNING THE LT ENGINE ANTI-ICE SWITCH FROM ON TO AUTO, THE LT ENG ANTI-ICE EICAS MESSAGE ILLUMINATED. REPLACED THE ANTI-ICE VALVE. OPS CHECKED IAW AMM 30-21-03. OPS & LEAK CHECKED GOOD.

Part: CONTROL UNIT — FAILED (BUSS) · airframe 79,307 hrs · 20,200 cycles

DURING PRE-DEPARTURE, FOUND THE LT UTILITY BUSS INOPERATIVE LIGHT ILLUMINATED. REMOVED AND REPLACED THE BUSS POWER CONTROL UNIT IAW AMM 24-22-00. OPS CHECKED GOOD IAW AMM 24-22-00, OK FOR SERVICE.

Part: COOLING FAN — FAULTY (E&E BAY) · airframe 79,291 hrs · 20,192 cycles

DURING PRE-FLIGHT - EICAS MSG - FWD EQP EXHAUST FAN ON STATUS PAGE. REMOVED AND REPLACED FWD EQUIPMENT COOLING FAN IAW AMM 21-58-06. OPS CHECK GOOD.

Part: FILTER — WARNING MESSAGE (RT ENGINE FUEL) · airframe 79,289 hrs · 20,189 cycles

RIGHT ENGINE FUEL FILTER STATUS MESSAGE. REMOVED AND REPLACED THE FUEL FILTER IAW AMM 73-11-03 . LEAK AND OPS CHECKED NORMAL.

Part: IDG — INOPERATIVE (RT GENERATOR) · airframe 79,267 hrs · 20,165 cycles

RIGHT GENERATOR OFF. REMOVED AND REPLACED THE RT IDG IAW AMM 24-11-01. OPS AND LEAK CHECKED GOOD,

Part: WARNING MESSAGE — FALSE ACTIVATION (FIRE LOOP) · airframe 79,258 hrs · 20,157 cycles

RIGHT ENGINE FIRE LOOP 1 STATUS MESSAGE. TROUBLE SHOT THE SYSTEM, FOUND NO FAULT IAW AMM 26-11 F/T 804, FIG 104, STEP 55.

Part: FIRE LOOP — MALFUNCTIONED (RT ENGINE) · airframe 79,256 hrs · 20,156 cycles

RIGHT ENGINE FIRE LOOP 1 STATUS MESSAGE. R & R THE AFT UPPER LOOP ASSY IAW AMM 26-11-02. OPS CHECKED NORMAL..

Part: RELAY — FAILED (COCKPIT HEAT) · airframe 79,256 hrs · 20,156 cycles

FLT DECK TEMP CONTROL INOPERATIVE IN AUTO, CYCLED FROM FULL HOT TO FULL COLD. EICAS ACTIVATED FOR A FEW MINUTES. R & R THE FLIGHT DECK ZONE DUCT OVERHEAT RELAY K238 IAW AMM 21-61-00. OPS CHECKED NORMAL IAW SWPM 20-81-13, AND AMM 21-61-00.

Part: TRANSMITTER — MALFUNCTIONED (APU OIL SYSTEM) · airframe 79,244 hrs · 20,151 cycles

APU OIL LEVEL INDICATED LOW. REMOVED AND REPLACED APU OIL QTY TRANSMITTER IAW AMM 49-9-04/401, LEAK CHECKED GOOD, OPS CHECKED GOOD.

Part: CONNECTOR — DIRTY (NR 2 FIRE DETECT) · airframe 79,244 hrs · 20,151 cycles

RIGHT ENGINE FIRE LOOP 1 SATUS MESSAGE. PERFORMED FIM 26-11 FT 806, NO DEFECTS NOTED. INSPECTED AND CLEANED THE NR 2 FIRE LOOP CONNECTOR. OPS CHECKED GOOD, NO STATUS MESSAGE ON EICAS.

Part: UNKNOWN — MALFUNCTIONED (GENERATOR SYS) · airframe 79,197 hrs · 20,132 cycles

APU GEN OFF EICAS MSG. APU GEN FIELD MAN RE-SET NO HELP TRANSFER TO MDDR 91311 IAW DDG 49-11-01A. APU HEALTH CHECK PER EO 6749A003, ALL PERFORMED SATISFACTORY. PERFORMED APU OPS CHECK PER AMM 49-21-00 NO DEFECTS NOTED.

Part: CHARGER — MALFUNCTIONED (APU BATTERY) · airframe 79,185 hrs · 20,127 cycles

STATUS MESSAGE FOR THE APU BATTERY CHARGER. TRIED TO RESET THE APU BATTERY CHARGER CIRCUIT BREAKER BUT NO HELP. REMOVED AND REPLACED APU BATTERY IAW AMM 24-31-04, AND REMOVED AND REPLACED THE APU BATTERY CHARGE IAW AMM 24-31-05, TESTED OK.

Part: WARNING MESSAGE — ILLUMINATED (CABIN TEMP) · airframe 79,136 hrs · 20,106 cycles

FWD CABIN TEMP EICAS MESSAGE DURING CLIMB. COMPLETED RQH NON-NORMAL CHECKLIST. ON GROUND NOTED FWD CABIN IND 32C, SUSPECT TEMP TX FAULT.

Part: WARNING MESSAGE — ILLUMINATED · airframe 79,136 hrs · 20,106 cycles

FWD CARGO BACKUP EICAS MESSAGE AFTER TAKE OFF. COMPLETED QRH NON NORMAL CHECKLIST. FIM 21-61 FAULT TREE 812 FOLLOWED. AUX ZONE CONT UNIT, NO FAULTS SHOWN AND BITE TEST PASSED. RESET GOOD. NO RECENT HISTORY.

Part: GASKET — LEAKING (HEAT EXCHANGER) · airframe 79,041 hrs · 20,065 cycles

LEFT ENGINE FUEL/OIL HEAT EXCHANGER FOUND LEAKING. THE HEAT EXCHANGER GASKET WAS REPLACED IAW AMM 79-21-01. ENGINE IDLE TEST. FOUND NORMAL IAW AMM 71-00-00.

Part: MOTOR — FAILED (APU STARTER) · airframe 79,002 hrs · 20,048 cycles

APU FAULT EICAS, APU FAILED TO START. REMOVED AND REPLACED THE START MOTOR AND CLUTCH ASSY. APU STARTING OPS TESTED OK IAW AMM 49-41-00 AND 49-41-06.

Part: WARNING MESSAGE — FALSE ACTIVATION (EQUIP EXHAUST) · airframe 78,997 hrs · 20,046 cycles

AFT EQUIPMENT EXHAUST FAN STATUS MESSAGE. OPS TESTED, CLEARED OUT AND THE RESULT WAS NORMAL IAW AMM 21-58-00.

Part: STARTER — FAILED (APU) · airframe 78,969 hrs · 20,034 cycles

APU FAULT ON EICAS, APU FAILED TO START. TROUBLESHOT AND REPLACED THE K197 RELAY IAW FIM 49-11, BLOCK22. BUT PROBLEM CONTINUED. APU ECU BITE SELF TEST PASSED BUT FAULT ON BITE CHANGED AS APU STARTER.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENGINE FIRE) · airframe 78,967 hrs · 20,033 cycles

AFTER SHUTDOWN OF THE LT ENGINE HAD A STATUS MESSAGE FOR LT ENGINE FIRE LOOP 1 AND LT ENGINE OVERHEAT LOOP 1. PERFORMED FIRE / OVERHEAT TEST, TEST PASSED IAW AMM 26-10-00. ACFT OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 78,905 hrs · 20,006 cycles

EICAS FWD CARGO BACKUP. PERFORMED FWD CARGO AIR CON TEST IAW AMM 21-28-00. CHECKED OK AND BITE CHECKED THE AUX TEMP CONTROLLER NO FAULTS IAW FIM 21-61-FT 812.

Part: UNKNOWN — UNKNOWN (COCKPIT TEMP) · airframe 78,808 hrs · 19,964 cycles

FLT DECK TEMP CONTROL IN AUTO TOO COLD EVEN WITH FULL WARM POSITION AND TOO HOT IN MANUAL WITH TRIM AIR VALVE IN FULL COLD&NBSP;(<P>PERFORMED FIM 21-61 FT 802 RESEAT K238AND PERFORMED ZONE TEMP CONTROL BITE , ALL TEST PASSED AND A/C OK FOR SERVICE&NBSP;</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (FWD CARGO) · airframe 78,803 hrs · 19,962 cycles

FWD CGO BACKUP EICAS DISPLAYED DURING CLIMBOUT, QRH NON-NORMAL PROCEDURE ACCOMPLISHED(<P>AUX ZONE TEMP CONTROLLER BITE TEST SHOW NO FAULTS PER AMM 21-61-12. AND ZONE TEMP CONTROLLER RESET.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENGINE BLEED) · airframe 78,803 hrs · 19,962 cycles

RIGHT ENGINE BLEED OFF EICAS MSG AT APPROX. 100KTS ON T.O ROLL QRH ACCOMPLISHED&NBSP;(<P>PERFORMED ASBM BITE PROCEDURE AND NO FAULTS NOTED , ALSO REVIEW HISTORY SHOWS R ENG BLEED NORMAL , NO MSG ON EICAS PER AMM 71-00-00 , A/C OK FOR SERVICE&NBSP;</P>)

Part: WARNING LIGHT — INOPERATIVE (PITOT SYSTEM) · airframe 78,769 hrs · 19,947 cycles

RIGHT AUX PITOT WARNING LIGHT INOP. TRANSFERRED TO MDDR 86607 CAT "B" PER MEL 30-31-02.

Part: WARNING MESSAGE — FALSE ACTIVATION (CARGO TEMP) · airframe 78,690 hrs · 19,912 cycles

AT ROTATION THE FWD CARGO TEMP 29C MESSAGE, CLEARED DURING CRUISE. ZONE TEMP CONTROLLER BITE TESTED WITH NO FAULTS NOTED IAW AMM 21-61-03.

Part: COVER — BROKEN (FIRE HANDLE) · airframe 78,653 hrs · 19,896 cycles

APU FIRE HANDLE COVER BROKEN. SECURED APU FIRE HANDLE COVER AND CHECK OK IAW AMM 26-15-01.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 78,651 hrs · 19,895 cycles

EICAS MESSAGE FWD CARGO BACKUP. CHECKED, NO RELATED FAULTS. ON GROUND PERFORMED FIM 21-61 F/T 812 - BLK 47, RESEATED RELAY K1222 AS A PRECAUTION. AUX ZONE TEMP CONTROLLER BITE TEST PASSED.

Part: WARNING LIGHT — FALSE ACTIVATION (FUEL FILTER) · airframe 78,644 hrs · 19,892 cycles

STATUS MESSAGE FOR THE LT ENGINE FUEL FILTER. REMOVED THE FUEL FILTER AND INSPECTED, NO DEFECT NOTED. REMOVED AND REPLACED THE FUEL FILTER ELEMENT IAW AMM 73-11-02 AS A PRECAUTION AND CLEANED FUEL FILTER DIFFERENTAL PRESSURE SWITCH IAW AMM 73-34-01. OK IAW AMM 71-00.

Part: ESCAPE REEL — MALFUNCTIONED (CABIN) · airframe 78,626 hrs · 19,884 cycles

ON ARRIVAL, CHECKED ESCAPE REELS AND DEPLOYED WHEN UPON LATCH COVER WAS OPENED. NO TENSION ON REEL. REMOVED AND REPLACED THE ESCAPE REEL. CHECKED OK IAW AMM 25-61-03.

Part: ESCAPE REEL — UNWANTED DEPLOY (CABIN) · airframe 78,621 hrs · 19,882 cycles

ESCAPE REELS DEPLOYED ON LANDING. INSTALLED AND CHECKED OK.

Part: FITTING — LEAKING (PUMP) · airframe 78,614 hrs · 19,879 cycles

RIGHT ENGINE INBOARD THRUST REVERSER COWL, PUMP FITTING FOUND LEAKING. TIGHTENED THE PUMP FITTING IAW AMM 70-50-00, NO LEAKS REVEALED.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 78,607 hrs · 19,876 cycles

FWD CARGO BACK UP EICAS MESSAGE CAME ON AFTER TAKEOFF BUT WENT OUT 10 OR 20 SECONDS LATER. PERFORMED BITE TEST OF AUX ZONE TEMP CONTROLLER, CHECKED OK IAW FI 21-21 FAULT TREE 801, PERFORMED A TEST OF AUX SHUTOFF VALVE IAW AMM 28-21-01. PERFORMED A CHECK OF THE FORWARD CARGO TRIM HEAT VALVE, CLEANED AND CHECKED OK IAW AMM 21-45-01. PERFORMED TEST OF TRIM AIR MODULATING VALVE, CLEANED AND TESTED OK IAW AMM 21-61-07.

Part: RELAY — MALFUNCTIONED (TEMP) · airframe 78,593 hrs · 19,870 cycles

FWD CARGO BACKUP EICAS SHORTLY AFTER TAKE OFF, EICAS EXTINGUISHED AFTER 3 MINUTES. PERFORMED A BITE TEST OF THE AUX TEMP CONTROLLER, TESTED OK. REMOVED THE AUX TEMP CONTROLLER AND INSPECTED CONNECTORS, ALL CHECKED OK. REMOVED AND INSPECTED K1222 RELAY AND CHECKED GOOD, SYSTEM OPS CHECKED GOOD IAW FIM 21-61-FAULT TREE 812. REMOVED THE CONNECTOR ON FWD CARGO SHUTOFF VALVE AND INSPECTED PINS, ALL CHECKED OK. CLEANED CONNECTOR AND REINSTALLED. REMOVED AND REPLACED RELAY K1212, CARGO AC SHUTOFF VALVE SYSTEM CHECKED GOOD IAW AMM 21-28-01.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 78,600 hrs · 19,873 cycles

FWD CARGO BACKUP EICAS MESSAGE CAME ON SHORTLY AFTER TAKEOFF, WENT OUT WITH IN 20 MINUTES AFTER TAKEOFF. ZONE TEMP CONTROLLER BITE TEST COMPLIED WITH IAW FIM 21-61-00. NO DEFECTS NOTED.

Part: WARNING LIGHT — FALSE ACTIVATION (CARGO TEMP) · airframe 78,582 hrs · 19,865 cycles

FWD CARGO BACKUP EICAS AFTER TAKEOFF, EICAS EXTINGUISHED AFTER ABOUT 1 HOUR IN FLIGHT. PERFORMED A BITE TEST OF AUX ZONE TEMP CONTROLLER, NO FAULTS NOTED. EICAS SHOWS NO FAULTS OR MESSAGES, SYSTEM TESTED OK IAW AMM 21-61-00.

Part: SHUTOFF VALVE — MALFUNCTIONED (RT ENGINE) · airframe 78,545 hrs · 19,849 cycles

STATUS MESSAGE FOR THE RT ENGINE HPSOV. REMOVED AND REPLACED HPSO IAW AMM 36-11-02, OPS CHECKED OK. LEAK CHECKED OK, PERFORMED IDLE ENG RUN CHECK OK. PERFORMED BITE TEST OF AIR CONTROLLER, FOUND HPSOV ON HPC MESSAGE, CLEARED MESSAGE REACTIVATED THE RT THRUST REVERSER, BUT OPS CHECKED BAD, RT ENG THRUST REVERSER WILL NOT DEPLOY. REPLACED THE HPSOV. CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (CARGO) · airframe 78,543 hrs · 19,848 cycles

EICAS MESSAGE AFTER TAKE OFF, FWD CARGO BACKUP EICAS MESSAGE, EXTINGUISHED DURING CLIMB. PERFORMED A BITE TEST OF ZONE TEMP CONTROLLER. TESTED OK IAW 21-61-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (CARGO TEMP) · airframe 78,538 hrs · 19,846 cycles

EICAS MESSAGE AFTER TAKEOFF. FWD CARGO BACKUP; THEN EXTINGUISHED DURING CLIMB. PERFORMED A BITE TEST OF ZONE TEMP. CONTROLLER TEST OK.

Part: WARNING MESSAGE — FALSE ACTIVATION (CARGO TEMP) · airframe 78,538 hrs · 19,846 cycles

EICAS MESSAGE AFTER TAKEOFF, FWD CARGO BACKUP EICAS MESSAGE. EXTINGUISHED DURING CLIMB. PERFORMED A BITE TEST OF ZONE TEMP CONTROLLER, TESTED OK IAW AMM 21-61-00.

Part: VENT — MALFUNCTIONED (COCKPIT AIR) · airframe 78,516 hrs · 19,836 cycles

CAPTAIN`S SIDEWALL VENT VALVE WILL NOT OPEN AND CLOSE PROPERLY. CLEANED AND CHECKED THE AIR VENT VALVE. WORKS NORMAL IAW AMM 21-24-00.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 78,511 hrs · 19,834 cycles

FORWARD CARGO BACK EICAS MESSAGE. NO REPEAT ON THIS LEG AND UNABLE TO DUPLICATE ON GROUND BUT AS PRECAUTIONARY, REPLACED REPLACED K1219 RELAY AND CHECKED OK IAW AMM 21-41-00.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (TEMP) · airframe 78,497 hrs · 19,828 cycles

EICAS MESSAGE FOR FWD CARGO BACKUP. CHECKED TEMP CONTROLLER & BITE TEST CARRIED OUT. NO RELATED FAULTS NOTED. EICAS MESSAGE SELF CLEARED IAW AMM 21-61-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN TEMP) · airframe 78,490 hrs · 19,825 cycles

FWD CARGO BACKUP EICAS AFTER TAKE OFF, THIRD RIGHT UP. TEMP CONTROLLER CIRCUIT BREAKER RESET AND BITE TEST PERFORMED IAW AMM 21-61-00, OK.

Part: CONTROLLER — MALFUNCTIONED (CABIN TEMP) · airframe 78,485 hrs · 19,823 cycles

EICAS MESSAGE FWD CARGO BKUP. RESET ZONE TEMP CONTROL SYS AND ZONE TEMP CONTROLLER BITE TEST PERFORMED AS PER AMM 21-61-00 'OK' & NIL FAULTS NOTED.

Part: RELAY — FAILED · airframe 78,483 hrs · 19,822 cycles

EICAS MESSAGE FOR THE FWD CARGO BKUP. THE FWD CARGO DUCT OVERHEATT& RELAY K1222 REPLACED IAW WDM 21-61-81 ,. BITE TEST CARRIED OUT SATISFACTORY.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 78,483 hrs · 19,822 cycles

FWD CARGO BACKUP EICAS ALERT , SECOND OCCURANCE IN TWO CONSECUTIVE LEGS. PERFORMED TROUBLESHOOTING IAW FIM 21-61, F/T 922, AND FOUND THIS TO BE AN INTERMITTENT FAULT, NO FURTHER MX ACTION REQUIRED.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 78,483 hrs · 19,822 cycles

AFTER TAKEOFF, AN EICAS MESSAGE FOR THE FWD CARGO BACKUP. RESET ZONE TEMP CONTROL SYSTEM AND PERFORMED ZONE TEMP CONTROLLER BITE TEST SHOWN GO LIGHT IAW AMM 21-61-00. SYSTEM OK FOR CONTINUE SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PUMP) · airframe 78,434 hrs · 19,801 cycles

RT AFT FUEL PUMP ADVISORY APPEARS INTERMITTENTLY DURING FLIGHT. PERFORMED SYSTEM TEST OF RIGHT AFT FUEL PUMP IAW AMM 28-22-00 NO DEFECTS NOTED SYSTEM OK.

Part: CONNECTOR — DIRTY (FIRE LOOP) · airframe 78,418 hrs · 19,794 cycles

RT ENGINE FIRE LOOP 1 STATUS MESSAGE. CHECKED THE FIRE LOOP, MESSAGE DISSAPEARED INTERMITTENTLY. CLEANED AND TIGHTENNED ALL FIRE LOOP CONNNECTORS AT THE RT ENGINE, TESTED OK IAW AMM 26-11-01.

Part: WARNING MESSAGE — FALSE ACTIVATION (FIRE LOOP) · airframe 78,408 hrs · 19,790 cycles

INTERMITTENT STATUS MESSAGE FOR RT ENGINE FIRE LOOP 1 IN FLIGHT. PERFORMED SYSTEM TEST OF RIGHT ENGINE FIRE DETECTION SYSTEM IAW 26-11-00 SYSTEM TESTED OK.

Part: WARNING MESSAGE — FALSE ACTIVATION (EQUIP COOLING) · airframe 78,403 hrs · 19,788 cycles

RECEIVED A STATUS MESSAGE FOR THE AFT EQ EXHAUST FAN NR 1. EQUIPMENT COOLING BITE TEST COMPLIED WITH AND WAS SATISFACTORY IAW AMM 21-58-41. EQUIPMENT COOLING SYSTEM OP CHECKED OK.

Part: APU — OIL CONSUMPTION · airframe 78,390 hrs · 19,782 cycles

MAGENTA ADD DISPLAY ON STATUS PAGE FOR APU. SERVICED APU WITH 3 QTS IAW AMM 12-49-01. REPLACED IAW AMM 49-11-01, OPS AND LEAK CHECKED NORMAL.

Part: PACKING — DEFECTIVE (APU) · airframe 78,334 hrs · 19,758 cycles

APU OIL QTY LOW AT ARRIVAL. REPLACED PACKING AT CAP AND ADJUSTED HANDLE TENSION CHECKS NORMAL PER AMM 49-11-00.

Part: O-RING — LEAKING (APU OIL SYS) · airframe 78,315 hrs · 19,750 cycles

ON ARRIVAL APU OIL INDICATES .50 QTY. CHECKS SIGHT GUAGE AND JUST ABOVE ADD LEVEL(<P>SERVICED 3 QTS OF OIL AND OPERATED 1 HRS 45 MINS. NO OIL LEAK FOUND IN APU COMPARTMENT TAIL PIPE AND COOLING AIR DUCT DISCHARGE DUCT. NO OIL FOUND BUT APU INOPERATIVE. REMOVED AND REPLACED APU OIL CAP ORING. LEAK CHECKED GOOD IAW AMM 49-21-00-206

Part: OIL SYSTEM — LOW (APU OIL SYS) · airframe 78,313 hrs · 19,749 cycles

APU OIL QUANTITY 0.25 WITH ADD ANNUNCIATED. APU OIL SERVICING UPLIFT 2 QTS IAW AMM 12-13-02. APU OPERATING TEST PERFORMED OIL INDICATION AND PARAMETERS DATA NORMAL IAW AMM 49-11-00.

Part: FIRE DETECTOR — FAILED (RT NACELLE) · airframe 78,297 hrs · 19,742 cycles

RIGHT ENGINE FIRE LOOP STATUS MESSAGE. REMOVED AND REPLACED THE FIRE DETECTOR ASSY IAW AMM 26-11-02.

Part: CONTROL VALVE — LEAKING (APU OIL SYS) · airframe 78,297 hrs · 19,742 cycles

FOUND APU OIL DROPPED LOW LEVEL. FOUND APU OIL WAS LEAKING FROM THE TEMP CONTROL VALVE ASSY. R & R THE CONTROL VALVE.

Part: FAN — MALFUNCTIONED (EQUIP EXHAUST) · airframe 78,297 hrs · 19,742 cycles

AFT EQUIPMENT EXHAUST FAN 1 STATUS MESSAGE. RESET THE CIRCUIT BREAKER AND EQUIPMENT COOLING SYSTEM OPERATIONAL TEST PASSED IAW AMM 21-58-00/501 TASK 205-120-006.

Part: FIRE DETECTOR — FAILED (RT ENGINE) · airframe 78,283 hrs · 19,736 cycles

DURING PRE FLIGHT CHECK MX FOUND R ENG. FIRE LP1 MSG. REMOVED AND REPLACED THE LWR AFT THERE DETECTOR ELEMENT AND CHECKED NORMAL IAW AMM 26-11-02 AND OBSERVED 8 LEGS WITHOUT FAULT REPORTED.

Part: INDICATOR — MALFUNCTIONED (APU FIRE) · airframe 78,228 hrs · 19,712 cycles

APU BLT EICAS MESSAGE. APU BLT DISCHARGE INDICATION. REMOVED AND REPLACED THE APU BOTTLE ARM LIGHT ASSY. OP CHECKED OK. REMOVED CIRCUIT BREAKER COLLAR FROM APU REMOTE FIRE INDICATION IAW 26-22-21.

Part: CONTROLLER — MALFUNCTIONED (CARGO TEMP) · airframe 78,193 hrs · 19,697 cycles

AFTER T/O RECEIVED EICAS "FWD CARGO BACKUP" ACCOMPLISHED QRH, PERFORMED FIM 21-61-812 FIG 112 AND RESET AUX TEMP CONTROLLER. BITE TEST SHOWS GOOD SYSTEM OK FOR CONT SERVICE.

Part: DISPLAY — MALFUNCTIONED (EICAS) · airframe 78,181 hrs · 19,692 cycles

AFTER TAKE OFF, RECEIVED AN EICAS, THE FWD CARGO BACKUP EICAS BLANKED 45 SECONDS LATER. PERFORMED FIM 21-61 FT 812 & THE AUX ZONE TEMP CONTROL BITE PROCEDURE FOUND OK IAW AMM 21-61-12.

Part: CONTROL PANEL — MALFUNCTIONED (RADAR DISPLAY) · airframe 78,181 hrs · 19,692 cycles

FIRST OFFICER'S RADAR DISPLAY DIM. REMOVED AND REPLACED THE EFIS CONTROL PANEL, OPS CHECKED OK IAW AMM 34-22-02, 34-22-02-002-010 AND 34-22-02-402-020.

Part: TERMINAL — LOOSE (FIRE LOOP) · airframe 78,149 hrs · 19,678 cycles

DURING PRE-FLIGHT CHECK, FOUND THE LT ENG FIRE LOOP 2 EICAS MESSAGE. ALL DETECTOR ELEMENTS WERE RESISTANCE, INSULATION CHECKED ,FWD TERMINAL LUG AT LWR FWD ELEMENT LOOSE. ALL TERMINAL TIGHTENED, FIRE TESTED GOOD.

Part: HYDRAULIC SYSTEM — LEAKING · airframe 78,156 hrs · 19,681 cycles

HYD QTY RIGHT SIDE ILLUMINATED. CHECKED RT HYD SYSTEM LOST ALL HYDRAULIC FLUID, TROUBLESHOT AND FOUND LEAKING FLUID FROM PRESSURE FILTER & DIFFERENTIAL PRESSURE INDICATOR. FILTER REPLACED AND DPI REPLACED, PERFORMED LEAK CHECK, NO LEAKAGE NOTED IAW AMM 29-11-17-4 & 29-11-00-5. REPLACED THE RT PRESSURE FILTER ELEMENT & INSPECTED THE OLD FILTER, NO METAL PARTICLES NOTED IAW AMM 29-11-17-4, & 29-11-00-6. REPLACED THE RT PRESSURE FILTER DIFFERENTIAL INDICATOR & LEAK CHECKED, NO LEAKING NOTED. REPLACED THE RT ENGINE DRIVEN PUMP ASSEMBLY & LEAK CHECKED, OPS CHECKED NORMAL, N LEAKS NOTED IAW AMM 29-11-05-4. REPLACED THE RT EDP HYD SUPPLY LINE COUPLER FITTING ASSEMBLY AND LEAK CHECKED, N LEAKS NOTED.

Part: PIN — MISSING (RT NACELLE) · airframe 78,135 hrs · 19,672 cycles

DURING WALKAROUND CHECK, FOUND PIN MISSING IN THE INTERPHONE AREA, RIGHT ENGINE, RIGHT SIDE. APPLIED 2 LAYERS OF SPEED TAPE IAW EO1971A138 AND INSPECTED IAW EO 1971A138. INSPECTED IAW AMM 05-51-59.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT FIRE LOOP) · airframe 78,126 hrs · 19,668 cycles

DURING PRE FLIGHT CHECK BY MAINT, FOUND THE LT ENGINE FIRE LOOP 2 MESSAGE. OPS CHECKED NORMAL IAW AMM 26-00-00.

Part: CIRCUIT CARD — NOT SEATED (RT ENGINE) · airframe 78,122 hrs · 19,666 cycles

EICAS MESSAGE DURING OFF, LOADING RT ENGINE SPEED CARD. SEATED THE RIGHT ENGINE SPEED AND PERFORMED N2 CARD TEST, PASSED IAW AMM 73-21-54 & MESSAGE CLEARED.

Part: RELAY — FAILED · airframe 78,099 hrs · 19,656 cycles

FWD CARGO BACKUP, EICAS MESSAGE DISPLAYED DURING DEPARTURE. QRH PROCEEDURE COMPLETED AND MESSAGE EXTINGUISHED. REMOVED AND REPLACED THE RELAY K1222 IN P37 MISC PANEL IAW FIM 21-61 FAULT TREE 812 & AMM 21-61-81, SYS OP CHECKED OK.

Part: RELAY — MISINSTALLED (EQUIPMENT VALVE) · airframe 78,085 hrs · 19,650 cycles

FWD EQUIPMENT VALVE EICAS MESSAGE AND VALVE LIGHT DISPLAYED AFTER START, WITH VALVE SWITCH IN THE STANDBY POSITION. PERFORMED TROUBLESHOOTING IAW FIM 21-58 FT 899. FOUND RELAY K1005 INSTALLED INCORRECTLY. SYSTEM TESTED OK.

Part: BUTTON — INOPERATIVE (WX RADAR) · airframe 78,089 hrs · 19,652 cycles

GCS BUTTON ON WX RADAR PANEL IS INOPERATIVE. RT SYSTEM TESTED OK IAW AMM 34-43-00.

Part: FIRE LOOP — OUT OF POSITION (LT NACELLE) · airframe 78,087 hrs · 19,651 cycles

LEFT ENGINE FIRE LOOP 2 STATUS MESSAGE. POSITIONED THE LEFT ENGINE FIRE LOOP 2 AND CLEANED ALL TERMINAL CONNECTORS. SYSTEM CHECKED OK IAW 26-11-00.

Part: PIN — WORN (RT NACELLE) · airframe 78,015 hrs · 19,620 cycles

RIGHT ENGINE INBD CORE COWL HOLD OPEN ROD STOWAGE PIN FOUND WORN. REPLACED THE IAW AMM 70-50-00, REV 120A.

Part: SKIN — DENTED (RT NACELLE) · airframe 78,015 hrs · 19,620 cycles

RIGHT NACELLE O/B CORE COWL BELOW PRECOOLER EXHAUST, FOUND A DENT. FOUND WITHIN LIMITS IAW SRM 54-42-01-1A-1, FIG.101, REV 104.

Part: HEAT EXCHANGER — LEAKING (RT ENGINE) · airframe 78,015 hrs · 19,620 cycles

RIGHT ENGINE IDG AIR/OIL HEAT EXCHANGER FOUND LEAKING. AIR/OIL HEAT EXCHANGER REPLACED IAW AMM 24-11-04, REV 120A.

Part: SKIN — WORN (NR 1 NACELLE) · airframe 78,015 hrs · 19,620 cycles

NR 1 NACELLE LT CORE COWL INTERIOR AFT UPPER SKIN FOUND WORN. REPAIRED IAW SRM 51-40-02, REV 104.

Part: VALVE — INOPERATIVE (HMG) · airframe 78,015 hrs · 19,620 cycles

DURING HMG OP TEST, FOUND HMG VALVE UNABLE TO CLOSE WHEN TEST SWITCH RETURN TO NORMAL POSITION. REMOVED AND REPLACED HMG VALVE IAW AMM 24-25-03, REV 120. CARRIED OUT HMG SYSTEM OPS TEST IAW AMM 24-25-00, REV 120, FOUND SATISFACTORY.

Part: FIRE LOOP — MALFUNCTIONED (NR 1) · airframe 78,015 hrs · 19,620 cycles

STATUS MESSAGE FOR THE LT ENGINE FIRE LOOP. THE FIRE LOOP WAS REMOVED, REPLACED AND TESTED IAW AMM 26-11-02, REV 120A, FOUND SATISFACTORY.

Part: ACTUATOR — CORRODED (TE FLAP SYS) · airframe 78,015 hrs · 19,620 cycles

DURING A TE FLAP ROTARY ACTUATOR AND REACTION RING INSPECTION, FOUND CORROSION ON THE NR 4 TE FLAP ROTARY ACTUATOR. THE ACTUATOR WAS REMOVED AND REPLACED IAW EO 6727A007.

Part: PIN — MISSING (NR 1 NACELLE) · airframe 78,015 hrs · 19,620 cycles

NR 1 ENGINE LH FAN COWL FWD HINGE PIN MISSING. THE HINGE PIN WAS INSTALLED IAW AMM 71-11-04, REV 120A.

Part: ACTUATOR — CORRODED (TE FLAP SYS) · airframe 78,015 hrs · 19,620 cycles

DURING A TE FLAP ROTARY ACTUATOR AND REACTION RING INSPECTION, FOUND CORROSION ON THE NR 2 TE FLAP ROTARY ACTUATOR. THE ACTUATOR WAS REMOVED AND REPLACED IAW EO 6727A007.

Part: DUCT — TORN (APU BLEED) · airframe 78,015 hrs · 19,620 cycles

APU SURGED, BLEED DUCT. FLEXIBLE DUCTING FOUND TORN. REMOVED AND REPLACED THE APU SURGE BLEED DUCT FLEXIBLE DUCTING IAW AMM 49-53-01, REV 120, CARRIED OUT A LEAK CHECK IAW AMM 49-11-00, REV 120, FOUND SATISFACTORY.

Part: ACTUATOR — CORRODED (TE FLAPS) · airframe 78,015 hrs · 19,620 cycles

TE FLAP ROTARY ACTUATOR AND REACTION RING INSPECTION, FOUND CORROSION ON POSITION NR 7 TE FLAP ROTARY ACTUATOR. THE ACTUATOR WAS REMOVED AND REPLACED IAW 8017-579, AND EO 6727A007.

Part: CONNECTOR — CRACKED (HMG) · airframe 78,015 hrs · 19,620 cycles

HMG SHUTOFF VALVE CONNECTOR FOUND CRACKED. THE CONNECTOR WAS REPLACED IAW SWPM 20-61-11, REV 64, WDM 24-25-11 AND 24-25-13, REV 11.

Part: FASTENER — WORN (NR 1 NACELLE) · airframe 78,015 hrs · 19,620 cycles

NR 1 NACELLE RT CORE COWL EXTERIOR AFT UPPER SKIN FOUND WITH TWO FASTENER HEADS WORN. REMOVED AND REPLACED THE FASTENERS IAW SRM 51-40-02, REV 104.

Part: ACTUATOR — CORRODED (TE FLAP SYS) · airframe 78,015 hrs · 19,620 cycles

TE FLAP ROTARY ACTUATOR AND REACTION RING INSPECTION, FOUND CORROSION ON THE NR 5 TE FLAP ROTARY ACTUATOR. THE ACTUATOR WAS REMOVED AND REPLACED IAW 8017-579, AND EO 6727A007.

Part: PIN — WORN (RT NACELLE) · airframe 78,015 hrs · 19,620 cycles

RT ENGINE OTBD FAN COWL FORWARD AND AFT HOLD OPEN ROD STOWAGE PIN FOUND WORN. THE PIN WAS REPLACED IAW AMM 70-50-00, REV 120A.

Part: SKIN — SCRATCHED (NR 1 NACELLE) · airframe 78,015 hrs · 19,620 cycles

NR 1 NACELLE, RT CORE COWL EXTERIOR SKIN WITH SCRATCHES. MINOR SCRATCHES REMOVED IAW SRM 51-10-02, REV 104. FOUND WITHIN LIMIT IAW SRM 54-42-01-1A-1, FIG 101, REV 104.

Part: COVER — MISSING (TERMINAL LUG) · airframe 78,015 hrs · 19,620 cycles

DURING INSPECTION FOUND COCKPIT WINDOWS NR 1 AND 2 HEATER TERMINAL LUG COVER MISSING. THE COVER WAS REPLACED IAW SWPM 20-61-11, REV 64.

Part: SKIN — ERODED (NR 1 NACELLE) · airframe 78,015 hrs · 19,620 cycles

NR 1 ENG NOSE COWL EXTERIOR SKIN AFT OF NOSE COWL LIP FOUND EROSION CIRCUMFERENTIALLY. NR 1 NOSE COWL EXTERIOR SKIN AFT OF NOSE COWL LIP REPAIRED IAW SRM 54-12-01-2R-11 REPAIR 11, REV 104, AND PAINTED IAW AMM 51-21-10, REV 120.

Part: SUPPORT FITTING — CRACKED (THRUST REVERSER) · airframe 78,015 hrs · 19,620 cycles

NR 1 ENG RT THRUST REVERSER CENTER ACTUATOR SUPPORT FITTING FOUND CRACKED. THE SUPPORT FITTING WAS REPAIRED IAW AMM 78-31-10-308-014-H00, REV 120A.

Part: SEAL — LEAKING (IDG) · airframe 78,015 hrs · 19,620 cycles

OIL LEAKED FROM LEFT ENGINE IDG CARBON SEAL. CAPPED LEFT ENGINE IDG OIL DRAIN LINE AND NO LEAKAGE FOUND IAW AMM 71-71-001601. REMOVED THE NR 1 IDG IAW AMM 24-11-01, REV 120A, AND REPLACED IDG CARBON SEAL ASSY IAW AMM 72-64-02, REV 120A, AND INSTALLED IDG ASSY IAW AMM 24-11-01, REV 120A, AND CARRIED OUT IDG OIL LEAK CHECK IAW AMM 71-71-00, REV 120A, FOUND NO LEAK AND IDG OPERATION TEST CARRIED OUT IAW AMM 24-11-00, REV 120A, FOUND SATISFACTORY.

Part: SPINNER — DAMAGED (NR 1 ENGINE) · airframe 78,015 hrs · 19,620 cycles

NR 1 ENGINE SPINNER PAINT FLAKED OFF. PAINTED IAW AMM 72-31-01, REV 120.

Part: SUPPORT FITTING — CRACKED (THRUST REVERSER) · airframe 78,015 hrs · 19,620 cycles

NR 1 ENGINE, LT THRUST REVERSER LOWER ACTUATOR SUPPORT FITTING FOUND CRACKED. THE SUPPORT FITTING WAS REPAIRED IAW AMM 78-31-10-308-014-H00, REV 120A.

Part: ACTUATOR — CORRODED (TE FLAP SYS) · airframe 78,015 hrs · 19,620 cycles

DURING A TE FLAP ROTARY ACTUATOR AND REACTION RING INSPECTION, FOUND CORROSION ON THE NR 3 TE FLAP ROTARY ACTUATOR. THE ACTUATOR WAS REMOVED AND REPLACED IAW EO 6727A007.

Part: WARNING MESSAGE — ILLUMINATED · airframe 78,071 hrs · 19,644 cycles

STATUS MESSAGE FOR LT ENGINE SPEED & RT ENGINE SPEED CARD DISPLAYED. SPEED CARD TEST C/OUT IAW AMM 73-21-04.

Part: CARBON SEAL — LEAKING (LT IDG) · airframe 78,008 hrs · 19,619 cycles

OIL LEAKED FROM LEFT ENGINE IDG CARBON SEAL. CAPPED LEFT ENGINE IDG DRAIN LINE AND NO LEAKAGE FOUND IAW AMM 71-71-00/001.

Part: OIL SYSTEM — LOW QUANTITY (LEFT ENGINE) · airframe 77,999 hrs · 19,618 cycles

REPORTED THAT LEFT ENGINE HAS LOW OIL DURING FLIGHT. SERVICED ENGINE OIL 3 QTS IAW AMM 12-13-01 INSPECTED LEFT ENGINE IAW AMM 71-05-03. NO DEFECTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (EXHAUST FAN) · airframe 78,192 hrs · 20,061 cycles

STATUS MESSAGE FOR AFT EQ EXHAUST FAN 2 DURING PRE-FLIGHT. PERFORMED AN OPS CHECK OF THE NR 2 AFT EQUIPMENT EXHAUST FAN IAW SUPPLEMENT MANUAL 21-58-41, OPS CHECKED GOOD.

Part: VALVE — INOPERATIVE (LT IDG) · airframe 77,987 hrs · 19,610 cycles

LEFT ENGINE IDG VALVE INOPERATIVE. REMOVED AND REPLACED THE IDG VALVE IAW AMM 24-11-07, OPS CHECKED NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENGINE BLEED) · airframe 77,986 hrs · 19,608 cycles

LEFT ENGINE BLEED OFF EICAS MESSAGE. PERFORMED A SUPPLY SYSTEM BITE TEST IAW AMM 36-23-00-00, NO FAULTS NOTED.

Part: SHUTOFF VALVE — MALFUNCTIONED (LT BLEED SYS) · airframe 77,983 hrs · 19,604 cycles

LEFT ENGINE BLEED AIR MESSAGE. REPLACED PRSOV IAW AMM 36-11-09. OPS CHECKED OK IAW AMM 71-00-00.

Part: REGULATOR VALVE — FAILED (LT ENGINE) · airframe 77,966 hrs · 19,583 cycles

AFTER ENGINE START, THE LEFT ENGINE BLEED OFF EICAS MESSAGE DISPLAYED, ASSOCIATED LEFT PACK OFF. REMOVED AND REPLACED PRESSURE REGULATING VALVE IAW AMM 36-11-09 OPS CHECKED NORMAL.

Part: OIL SYSTEM — LOW (APU) · airframe 77,962 hrs · 19,579 cycles

APU AUTO SHUTDOWN IN FLIGHT, STATUS MESSAGE APU OIL QUANTITY, OIL QUANTITY INDICATES ADD. SERVICED THE APU OIL IAW AMM 12-13-04, OPS CHECKED GOOD IAW AMM 49-11-00.

Part: PACKING — TORN (PLUG) · airframe 77,921 hrs · 19,531 cycles

LEFT DUCT PRESSURE SURGES BETWEEN 20 TO 50 PSI DURING CHANGES IN ENGINE POWER SETTINGS. DISCOVERED LT ENGINE PRSOV INLINE FILTER FREE OF DEBRIS, PLUG HAD TORN PACKING. REMOVED AND REPLACED PACKING. PRSOV OPS CHECK AND DUCT PRESSURE MODULATION CORRECTED ON ENGINE RUN IAW FIM 36-10-01.

Part: WARNING MESSAGE — FALSE ACTIVATION (ENGINE) · airframe 77,897 hrs · 19,499 cycles

EICAS MESSAGE IDLE DISAGREE. PERFORMED ENGINE RUNS IAW AMM 71-00-00. OPS CHECKED GOOD, NO DEFECTS NOTED.

Part: ROD — DETACHED (NR 8 LE SLAT) · airframe 77,882 hrs · 19,480 cycles

RTO AT APROXIMATELY 100 KIAS, CONFIGURATION FLAPS. FOUND NR 8 LEADING EDGE SUPPORT ROD DETACHED. ATTACHED THE NR 8 L/E SLAT SUPPORT ROD IAW AMM 27-81-02, PERFORMED OPS CHECKS, NO DEFECTS NOTED.

Part: INERTIA REEL — UNWANTED DEPLOY (CABIN) · airframe 77,883 hrs · 19,481 cycles

INERTIAL REELS DEPLOYED DURING TAXI AFTER LANDING. REMOVED AND REPLACED THE DESCENT DEVICES IAW AMM 25-61-03

Part: CONTROL UNIT — MALFUNCTIONED (APU) · airframe 77,876 hrs · 19,472 cycles

APU AUTO SHUTDOWN. REMOVED AND REPLACED APU CONTROL UNIT IAW AMM 49-61-05. OPS CHECKED OK.

Part: BLEED VALVE — MALFUNCTIONED (RT ENGINE) · airframe 77,874 hrs · 19,469 cycles

ON ENGINE SHUTDOWN, RIGHT ENGINE BLEED VALVE DID NOT CLOSE. PERFORMED AN OPS CHECK IAW AMM 36-11-09. OPS CHECK GOOD, NO FAULTS NOTED.

Part: WARNING LIGHT — FALSE ACTIVATION (ANTI ICE VALVE) · airframe 77,858 hrs · 19,450 cycles

LEFT ENGINE ANTI-ICE VALVE EICAS MESSAGE AFTER LANDING, MSG CLEARED ON GROUND IAW AMM 30-21-00, ENG RUN FOUND TO BE OK.

Part: SKIN — CRACKED (LT ELEVATOR) · airframe 77,845 hrs · 19,435 cycles

LEFT INBD ELEVATOR, TOP SKIN HAS A ONE INCH CRACK, PUNCTURE IN THE TOP SKIN, 31 INCHES FROM THE OB END, 4 INCHES FROM THE TRAILING EDGE. ACCOMPLISHED INTERIM REPAIR IAW PMO-T25-16-0031-03B.

Part: PUMP — MALFUNCTIONED (FUEL BOOST) · airframe 77,790 hrs · 19,369 cycles

NR 1 LEFT FWD FUEL PUMP EICAS MESSAGE. REMOVED AND REPLACED THE LT FWD. FUEL BOOST PUMP IAW AMM 28-22-03. OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 77,721 hrs · 19,310 cycles

LEFT FORWARD FUEL PUMP EICAS MESSAGE, STARTED TO RUN QRH PROCEDURE AND EICAS MESSAGE WENT OUT, CANNOT DUPLICATE MESSAGE. OPS CHECK OF ENGINE FUEL FEED SYSTEM GOOD IAW AMM 28-22-011.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 77,713 hrs · 19,301 cycles

FORWARD CARGO BACKUP EICAS MSG, FIM 21-61, FT 922, BITE PROCEDURE C/O, NO FAULT FOUND ON THE GROUND. OPS CHECKED SERVICEABLE.

Part: RADOME — DAMAGED (FUSELAGE) · airframe 77,709 hrs · 19,297 cycles

BIRD STRIKE ON NOSE OF ACFT. RADOME REPLACED IAW 53-12-01.

Part: DRAIN MAST — MISSING (LT ENGINE) · airframe 77,703 hrs · 19,291 cycles

UPON INITIAL PREFLIGHT, LT ENGINE MISSING LOWER FLUID DRAIN MAST. INSTALLED LT ENGINE DRAIN MAST IAW AMM 20-11-00.

Part: CONTROL PANEL — DEFECTIVE (COCKPIT) · airframe 77,714 hrs · 19,701 cycles

LEFT SIDE WINDOW HEAT ON LIGHT INOPERATIVE. R & R WINDOW HEAT CONTROL PANEL IAW AMM 30-41-00.

Part: MONITOR — ERRATIC (LT ENGINE) · airframe 77,677 hrs · 19,263 cycles

LEFT ENGINE LPT VIBRATION MONITOR SYSTEM ERRATIC AND URELIABLE.

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 77,679 hrs · 19,265 cycles

RIGHT DUCT PRESSURE DURING CLIMB THRUST 70 PSIL, NORMAL AT 40 PSI. DURING CRUISE LT & RT 36 PSI. PRESSURIZED LT AND RT PNEUMATIC SYS DURING CH 71 TEST NR 1, 3, 4, 5, 8, 9,& 10. NO FLUCTUATIONS NOTED. OPS CHECKED FOUND TO BE SATISFACTORY IAW AMM 36-00-00-862-047.

Part: GENERATOR — MALFUNCTIONED (RIGHT) · airframe 77,666 hrs · 19,252 cycles

RT ENGINE GENERATOR DRIVE LIGHT INOPERATIVE. R & R THE GENERATOR IAW AMM 24-11-01. OPS NORMAL IAW AMM 71-00-00.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 77,661 hrs · 19,246 cycles

RT ENGINE GENERATOR DRIVE LIGHT INOPERATIVE TRANSFER TO MDDR 69145 IAW MEL, CAT B, DUE DATE 08-13-16. PLACARD INSTALLED C/W MEL PROCEDURES.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 77,659 hrs · 19,243 cycles

FORWARD CARGO BACK UP EICAS MSG DISPLAYED FORWARD CARGO AC FAULT DISCRETE LIGHT ILLUMINATED FORWARD CARGO TEMP 39C. PERFORMED FIM 21-61, FAULT TREE 922, NO FAULTS FOUND, CHECKS SERVICEABLE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 77,659 hrs · 19,243 cycles

LT FORWARD FUEL PUMP EICAS MESSAGE. LEFT FORWARD FUEL PUMP PRESSURE LIGHT DISPLAYED. LEFT FORWARD FUEL BOOST PUMP TESTED IAW AMM 28-22-00. NO FAULTS FOUND, CHECK SERVICEABLE.

Part: WIRE — DAMAGED (HEAT EXCHANGER) · airframe 77,659 hrs · 19,243 cycles

LEFT SECONDARY HEAT EXCHANGER OUT TEMP SHOWING ERRATIC, NO EICAS ECM/MSG. WIRE, W508-211R REPAIRED AT SPLICE SMS WDM 21-57-31 CHECKS SERVICEABLE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 77,651 hrs · 19,235 cycles

EICAS MESSAGE CENTER LT FUEL PUMP AND ENGINE FUEL FEED SYS. OPS TEST IAW AMM 28-22-00/501, NO FAULT FOUND.

Part: RELAY — FAULTY (OVERHEAT SYS) · airframe 77,652 hrs · 19,236 cycles

BULK CARGO OVERHEAT LIGHT ILLUMINATED. DEFER BULK CARGO OVERHEAT LIGHT ILLUMINATED MDDR 68835. FOUND RELAY K729 FAULTY , RELAY REPLACED IAW SWPM 20-81-00.

Part: NUT — DETACHED (SLAT LINKAGE) · airframe 77,603 hrs · 19,187 cycles

ON ARRIVAL, LEFT NR 5 SLAT WING LEADING EDGE SLAT LINKAGE FOUND NUT DETACHED ITEM 3 LEADING EDGE NR 5 SLOT WING PANEL DAMAGE, AND FOUND HARDWARE MISSING REINSTALLED AS REQUIRED IAW AMM 27-80 ITEM 3. TEMPORARY REPAIR COMPLETED IAW SRM 57-41-01-2R-1 NOTED A & D, DRAWING 114T2400 SHT 2 REV N.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 77,601 hrs · 19,183 cycles

RT GENERATOR DRIVE DISC, DRIVE LIGHT NOT ON WITH ENGINE SHUTDOWN. LIGHT TEST OK. RELAMPED RT GEN DRIVE DISC, SWITCH IAW AMM 33-13-00. PERFORMED OPS CHECK TEST OK, RT IDG IAW AMM 24-11-01. OPS CHECK GOOD.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 77,585 hrs · 19,169 cycles

LEFT PACK TEMP EICAS MSG ON TAXI PLACED LT PACK ON MDDR 67656 IAW MEL 21-51-01-01. MAINTENANCE PROCEDURES C/W PLACARD INSTALLED. LT PACK WILL NOT RESET IN AUTO OR STANDBY. REMOVED AND REPLACED LT ACM MM 21-51-07. REMOVED AND REPLACED HOT AIR SUPPLY TUBE IAW M/M 21-51-10 OPS CK OK. NO LEAKS MDDR 67656 CLEARED.

Part: UNKNOWN — ODOR · airframe 77,585 hrs · 19,169 cycles

VERY STRONG SMOKE ODOR ON TAXI. INSPECTED UPPER CARGO COMPARTMENT, LWR FWD AND AFT CARGO COMPARTMENT. INSPECTED LT AND RT PACK COMPARTMENT. NO EVIDENCE OF SMOKE FOUND IAW AMM 05-51-56.

Part: RELAY — FAILED (FUEL SYSTEM) · airframe 77,585 hrs · 19,169 cycles

LEFT FWD FUEL BOOTS PUMP AUTOMATIC FUNCTION INOPERATIVE. TRANSFER TO MEL 28-22-01-01. T/S SYSTEM USING WIRING DIAGRAM 28-25-11, 28-22-11, AND FIM TASK 28-25, FAULT TREE 808. REPLACED LT FWD PUMP PWR SENSE RELAY K513 IAW SWPM CH 20-81-19, SYSTEM CK'S GOOD IAW MM 49-11-00. THIS CLEARS MDDR, PLACARD REMOVED.

Part: CONTROLLER — MALFUNCTIONED (RT ENGINE) · airframe 77,576 hrs · 19,160 cycles

RIGHT ENGINE PRV STATUS MSG. R & R RT ENGINE PRV AND PRV CONTROLLER IAW AMM LEAKS AND OPS CHECK GOOD, AMM 36-11-18 AND AMM 36-11-19.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 77,565 hrs · 19,148 cycles

AUTOMATIC FUNCTION OF LT FWD PUMP WHEN APU RUNNING LOW PRESSURE LIGHT REMAINS ILLUMINATED. ACCOMPLISHED SUCESSFUL OPS CHECK OF FWD LT BOOST PUMP REF AMM 49-11-00. OPS GOOD ON SEVERAL CYCLES. NO PREVIOUS HISTORY. OK FOR SERVICE.

Part: ESCAPE ROPE — UNWANTED DEPLOY (CABIN) · airframe 77,561 hrs · 19,144 cycles

NR 2 & NR 4 DESCEND DEVICES FOUND DEPLOYED UPON ARRIVAL. R & R DESCENT DEVICES IAW SMM 25-61-63.

Part: WARNING MESSAGE — FALSE ACTIVATION (DUCT PRESSURE) · airframe 77,495 hrs · 19,079 cycles

DURING CLIMBOUT, LEFT DUCT PRESSURE NOTED AT 55 PSI. RIGHT INDICATED NORMAL PRESSURE AT 35. NO EICAS MESSAGE WAS DISPLAYED. PRESSURE NORMALIZED DURING CRUISE FLIGHT. AIR SUPPLY BITE PROCEDURE C/O IAW FIM 36-20 WITH NO FAULT NOTED, AS WELL AS ENGINE GROUND RUN C/O SERVICEABLE.

Part: PLUG — LOOSE (NR 1 ENGINE) · airframe 77,495 hrs · 19,079 cycles

DURING WALK AROUND, FOUND OIL LEAK NR 1 ENGINE FOUND PLUG ON NR 1 ENGINE FUEL/OIL COOLER LOOSE, TIGHTENED PLUG TO 45 FT/LB AND SAFE TIED. REF 79-21-01. LEAK CHECKED OK AT THIS TIME.

Part: SWITCH — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 77,405 hrs · 18,989 cycles

EMERGENCY LIGHTS COME ON WHEN A/C POWER IS SHUTOFF. EMERGENCY LIGHTS SWITCH WAS IN OFF. REPLACED EMERGENCY LIGHT SWITCH IAW WDM 33-51-11. SYSTEM OPS CHECKED GOOD IAW AMM 33-51-00.

Part: EXCITER — FAULTED (APU) · airframe 77,390 hrs · 18,974 cycles

PERFORMED APU COLD SOAK START, DID NOT START. APU FAULT EICAS APPEARED. LP 696503, ITEM 1: ITEM TRANSFERRED DO DMI MDDR 64015, PLACARD INSTALLED. APU INOPERATIVE ER OPERATIONS NOT ALLOWED. T/S ECU- IGN UNIT FAULTY. ITEM M3: R & R EXCITER BOX IAW 49-41-03. OPS CHECK GOOD. THIS ITEM IS NOW CLOSED. PLACARD REMOVED, MAINTENANCE NOTIFIED.

Part: PROXIMITY SWITCH — MALFUNCTIONED (RT MLG) · airframe 77,376 hrs · 18,960 cycles

PROBE HEAT EICAS WOULD NOT CLEAR AFTER ENGINE START. REPLACED RT MLG PROXIMITY SWITCH IAW AMM 32-09-07-002. OPS CHECK GOOD.

Part: ANTI-ICE VALVE — MALFUNCTIONED (RT ENGINE) · airframe 77,335 hrs · 18,924 cycles

STATUS MSG, "RT ENGINE TAI VALVE. R & R RT ENGINE TAI VALVE IAW AMM 30-21-03. ACCOMPLISHED GROUND OPS CHECK, SYSTEM OPS CHECK NORMAL.

Part: TERMINAL — LOOSE (WINDOW) · airframe 77,344 hrs · 18,927 cycles

EICAS MESSAGE LT FWD WINDOW. FOUND WINDOW POWER INPUT TERMINAL LUG BOLT, ONE SIZE TOO BIG, CONNECTOR FOUND LOOSE AND ARCING. REPLACED BOLT, OPS CHECK GOOD REF AMM 56-11-01 FOR TERMINAL INSTALLATION.

Part: CONTROLLER — MALFUNCTIONED (WINDOW HEAT) · airframe 77,340 hrs · 1,892,639 cycles

LEFT FWD WINDOW HEAT INOPERATIVE. TS LT FWD WINDOW HEAT INOPERATIVE, FOUND POPPED CIRCUIT BREAKER ON P36. RESET CB IAW MCC, REPLACED WHCU FOR LT FWD WINDOW. OPS CHECKS GOOD IAW AMM 30-41-01.

Part: BLEED VALVE — MALFUNCTIONED (APU) · airframe 77,335 hrs · 18,924 cycles

APU AUTOSHUTDOWN, FAULT LIGHT ILLUMINATED. ECU BITE SHOWED REVERSE FLOW MSG. APU BLEED SURGE VALVE REPLACED IAW AMM 49-53-01 OPS CHECK OK NEW ECU BITE NO FAULTS.

Part: WINDOW — FAILED (COCKPIT) · airframe 77,332 hrs · 18,921 cycles

LT FWD WINDOW HEAT INOPERATIVE. INTERMITTENT FAILURE. REMOVED L1 WINDOW AND TEMP INSTALLED NEW WINDOW IAW MM 56-11-01-004-039. COMPLETED INSTALL OF L1 WINDOW IAW AMM 56-11-01, OPS CHECK GOOD AT THIS TIME. COMPLETED STEP 17 AT 1401.

Part: CONTROLLER — INOPERATIVE (WINDOW HEAT) · airframe 77,330 hrs · 18,919 cycles

LEFT FWD WINDOW INOPERATIVE. R & R CONTROL UNIT IAW MM 30-41-00, OPS CHECK GOOD AT THIS TIME.

Part: SHUTOFF VALVE — WARNING MESSAGE (RT ENGINE) · airframe 77,295 hrs · 77,322 cycles

RIGHT ENGINE HPSOV, RT ENGINE TAI VALVE STATUS MESSAGE. R & R RT ENGINE HPSOV IAW AMM 36-11-07. OPS AND LEAK CK GOOD THIS CLEARS MDDR 62780 PLACARDS. REMOVED MCC NOTIFIED.

Part: IDG — FAILED (LT GENERATOR) · airframe 77,320 hrs · 18,908 cycles

LOSS OF LT GENERATOR AT 1500 FT. ALL SHORT FINAL. ATTEMPTED ONE RESET. WOULD NOT RECONNECT. R & R LT IDG IAW AMM 24-11-01, OPS CHECKS GOOD, NO OTHER DEFECT NOTED AT THIS TIME.

Part: CONTROL UNIT — MALFUNCTIONED (APU) · airframe 77,320 hrs · 18,908 cycles

APU AUTO SHUTDOWN, MINI FLAG 17. T/S TO FAULT ECU, R & R APU ECU IAW AMM 49-61-05, OPS CHECK OK. R & R APU OIL SCAVENGE FILTER, LEAK CHECK OK. R & R APU GENERATOR OIL FILTER DIFFERENTIAL PRESSURE SWITCH, PN: 3876048-3, SN: 99071691539D, OPS CHECK OK.

Part: RECEPTACLE — LOOSE (WINDOW HEAT) · airframe 77,315 hrs · 18,903 cycles

FWD L1 WINDOW INOP, HEAT, PERFORMED FIM TEST 30-41, FTR 803, AMBER CONTROL LIGHT CAME ON. IAW TABLE 102, MEASURED RESIST FROM J4 & J5-10.2 OHM. REMOVED CONTROLLER. NOTED REAR RECEPTACLE LOOSE. SECURED; REINSTALLED IAW AMM 30-41-01, TESTED.

Part: SKIN — DAMAGED (BS 196) · airframe 77,295 hrs · 18,898 cycles

SCRATCHES ON FUSELAGE SKIN, BUTT JOINT AND LAP JOINT, AT BS 196.5, STR 21R, REF IAI NRC M0315. REPAIR PERFORMED IAW IAI REA MF01084R0113, REV, NEW, AND AS INSTRUCTED BY SR 4-2989086791. THIS REPAIR, RELATED TO AD 2010-06-16, SB 767 53A193, R2 AND SRM 53-00-01.

Part: STRINGER — CRACKED (BS 368) · airframe 77,295 hrs · 18,898 cycles

CRACK ON STRINGER 1L LOCATED AT FUSELAGE BS-368, REF IAI NRC C0028. REPAIRED SRM 53-00-03, FIG 201, REPAIR 1 AS CATEGORY A, PERMANENT REPAIR. THIS REPAIR CLASSIFIED AS MAJOR BY EO 6753A258, REV 0.

Part: SKIN — DAMAGED (BS 390-412) · airframe 77,295 hrs · 18,898 cycles

DEEP ABRASION DAMAGE REPAIR AT FUSELAGE SKIN BS 390-412, STR 22L-23L, REF IAI NRC M0022, REPAIR PERFORMED IAW SRM 53-00-01, FIG 201, REPAIR 29 IAW REF SRM THIS REPAIR IS A CATEGORY B: REPAIR. INITIAL INSPECTION THRESHOLD IS AT 37500 FC, TOTAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 77,295 hrs · 18,898 cycles

FWD BATTERY PACK EMERGENCY LIGHT INOPERATIVE, REF IAI NRC M0568. REINSTALL BATTERY PACK EMERGENCY LIGHT IN FWD POS IAW J/C 371-25-C5066-001-AV, CHECK OK, AFTER CAPACITY TESTED AND INSPECTED IN SHOP.

Part: STRUT — CRACKED (NR 2 NACELLE) · airframe 77,296 hrs · 18,898 cycles

CRACK REPAIR ON STRUT NR 2 INBD SIDE SKIN PANEL, NAC BS 221.25 TO 237.5, REF NRC M0538, REPAIR PERFORMED IAW REA MF01084R0148, REV NEW, DATED 29 OCT 15, REA MF0108R0148, REV A, DATED 15 NOV 15 AND AS INSTRUCTED BY SR 4-3029397194, MESSAGE.

Part: HINGE FITTING — DAMAGED (NR 1 NACELLE) · airframe 77,295 hrs · 18,898 cycles

HINGE FITTING ASSY, WEAR DAMAGE REPAIR ON ENGINE'S NR1 FAN COWL BS 188.2, REPAIR PERFORMED IAW REA MF01084R0071, REV A DATED 13OCT15.

Part: FLOORBEAM — CORRODED (BS 246) · corrosion level 2 · airframe 77,295 hrs · 18,898 cycles

CORROSION DAMAGE AT FUSELAGE BS 246 MAIN DECK FLOORBEAM - MID CHORD, PN 141T5814-158, WL200, BETWEEN RBL 55 AND RBL 73, REF IAI NRC M0066. REPAIR PERFORMED IAW SRM 53-10-51, FIGURE 201, REPAIR 2, AS CATEGORY A, PERMANENT REPAIR. THIS REPAIR CLASSIFIED AS MAJOR, EO NR 6753A266, REV 0.

Part: SKIN — DAMAGED (BS 434-654) · airframe 77,295 hrs · 18,898 cycles

PERFORMED REPAIR OF MULTIPLE EXTERNAL SKIN DAMAGES ON FUSELAGE SECTION 43 AND 46, BS 434 TO 654+44 B/T S-39L AND S-39R, BS 1197+110 TO 1480 B/T S-26R AND S-36R AND AT S-31L, REF NRC M0023-M0026, M0033, M0035 AND M0036. REPAIR PERFORMED IAW REA MF01084R0094, REV NEW, REA MF01084R0094, REV. A,