N1439A

Part: SKIN — CRACKED (ZONE 200) · airframe 79,041 hrs · 19,399 cycles

LH FWD ENTRY DOOR CUTOUT AFT LOWER CORNER SKIN CRACKED.

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 79,041 hrs · 19,399 cycles

FLC DOOR CUTOUT UPPER TRANSITION AND CEILING PANEL CRACKED AT CENTER AND GOUGES AT FWD CORNER. REPLACED FLC DOOR CUTOUT CENTER AND FWD CORNER SUPPORT ANGLES IAW B767-300 SRM 51-40-02 PARA 7. P/N 453T1654-28 AND P/N 453T1654-18.

Part: ROLLER TRAY — CORRODED (ZONE 100) · corrosion level 2 · airframe 79,041 hrs · 19,399 cycles

ROLLER TRAY CORRODED AT STA 654+88 RBL 20 AT LOCK. COMPLETED ROLLER TRAY SPLICE REPAIR IAW B767 SRM 53-00-53 REPAIR 1 DETAIL 4 REF. AMES DOC 47574REA01.

Part: LONGERON CLIP — CRACKED (ZONE 400) · airframe 79,041 hrs · 19,399 cycles

#1 PYLON HAS TWO CRACKED LONGERON CLIPS ON THE O/B AND I/B SIDE OF WEB LOCATED JUST AFT OF HYD BAY DOORS . REMOVED AND REPLACED LONGERON CLIPS IN #1 PYLON . IAW B767 SRM 51-40-02 PARA 7

Part: ROLLER TRAY — CORRODED (ZONE 100) · airframe 79,041 hrs · 19,399 cycles

ROLLER TRAY CORRODED AT STA. 478 RBL44

Part: WINDOW — UNKNOWN (UNKNOWN) · airframe 78,659 hrs · 19,248 cycles

SUPPLEMENTAL-5 JULY 2023-KILN DUE TO SYSTEM OUTAGE, REPORT PREVIOUSLY SUBMITTED VIA ALTERNATE EMAIL PROCEDURES. LEFT FORWARD WINDOW EICAS DISPLAYED. NO OTHER INDICATIONS NOTED. CAPTAIN'S WINDOW SHATTERED AT 35,000 FEET. DIVERSION TO KSMF WITH AN EMERGENCY DECLARATION. LANDING WAS UNEVENTFUL WITH NO ADDITIONAL PRECAUTIONARY ACTIONS. ON ARRIVAL, AIRCRAFT WAS GROUNDED FOR UNSCHEDULED MAINTENANCE. L1 WINDOW ASSEMBLY AND WINDOW HEAT CONTROLLER REMOVED AND REPLACED IAW B767 AMMS 56-11-01 AND 30-40-01 RESPECTIVELY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — CRACKED (LT WING) · airframe 77,321 hrs · 18,738 cycles

LH LE WING STA 616.2 CRACKED

Part: ROLLER TRAY — CORRODED (ZONE 100) · corrosion level 2 · airframe 79,041 hrs · 19,399 cycles

ROLLER TRAY CORRODED AT STA 478, RBL44

Part: STIFFENER — CRACKED · airframe 74,880 hrs · 17,901 cycles

WEB ON STIFFENER AT STATION 971 LBL 90 HAS DAMAGED HOLE. REMOVED, FABRICATED AND REPLACED NEW STIFFNER AT STATION 971 LBL 90 IAW ENGINEERING ORDER 74783FAB01.

Part: SKIN — DELAMINATED · airframe 74,880 hrs · 17,901 cycles

RIGHT SIDE VERTICAL BETWEEN THE AUX SPAR AND FRONT SPAR THE COMPOSITE SKIN PANEL IS DELAMINATED. REPAIRED RIGHT SIDE VERT STAB PANEL BETWEEN THE AUX SPAR AND FT SPAR IAW B767 SRM 51-70-10 R4.

Part: FLAP — DELAMINATED · airframe 74,880 hrs · 17,901 cycles

LEFT WING TRAILING EDGE INBOUND TRAILING EDGE PLAP HAS DELAM AREA ON INBOUND EDGE. LAYED UP AND CURED IAW B767 SRM 51-70-10.

Part: FAILSAFE — CRACKED · airframe 74,880 hrs · 17,901 cycles

RIGHT FAILSAFE STRAP AT STA 955 HAS A CRACK INDICATION ON ULTRASOUND NDT INSPECTION. REPAIRED FAILSAFE STRAP AT STATION 955 IAW AMES ENGINEERING ORDER 472070RD04.

Part: BEAM — CRACKED · airframe 74,880 hrs · 17,901 cycles

INBOUND HYD BAY LATCH CHANNEL IS CRACKED AT #3 LATCH MOUNT AREA. REMOVED AND REPLACED BEAM IAW B767 SRM 51-40-02.

Part: WEB — CRACKED · airframe 74,880 hrs · 17,901 cycles

FWD DOUBLER ON FAIRING SUPPORT WEB AT TA 1081 CRACKED, FABRICATED AND REPLACED NEW DOUBLER IAW B767 SRM 51-10-02.

Part: DOUBLER — CRACKED · airframe 74,880 hrs · 17,901 cycles

AFT DOUBLER ON FAIRING SUPPORT WEB AT STA 1081 CRACKED. FABRICATED AND REPLACED NEW DOUBLER IAW B767 SRM 51-10-02.

Part: NONE — CRACKED · airframe 74,880 hrs · 17,901 cycles

RIGHT STUB BEAM CRACKED AT STATION 903.5 RBL89.REPAIRED RIGHT CRACKED STUB BEAM AT STATION 903.5 RBL 89 IAW ENGINEERING ORDER 53-767-7702.

Part: FORMER — CRACKED · airframe 74,880 hrs · 17,901 cycles

NOSE FORMER IS CRACKED BY #9 SLAT INBOUND AUX TRACK AT WING LEADING STATION 562. REMOVED AND REPLACED DAMAGE NOSE FORMER IAW B767 SRM 51-40-02.

Part: RIB — CRACKED · airframe 74,880 hrs · 17,901 cycles

LEFT WING LEADING EDGE AT APPROXIMATELY LES 563.0 HAS CRACKED NOSE RIB. REMOVED AND REPLACED NOSE RIB ON LEFT WING LEADING EDGE AT WS STA 565.9 IAW B767 51-40-02.

Part: CHANNEL — CRACKED · airframe 74,880 hrs · 17,901 cycles

#2 AFT STRUT FAIRING WEB OUTBOARD "U" CHANNEL CRACKED AT BOTTOM IN RADIUS. REMOVED CHANNEL AND MATCH DRILLED NEW "U" CHANNEL IAW B767 SRM 51-40-05 AND INSTALLED IAW B767 SRM 51-40-02. IN #2 PYLON AFT OF FAIRING WEB.

Part: NONE — CRACKED · airframe 74,880 hrs · 17,901 cycles

#2 AFT STRUT FAIRING SMALL ANGLE ON BACK SIDE OF HYD COMPT OUTBOARD SIDE CRACKED. REMOVED AND REPLACED SMALL "C" ANGLE ON #2 AFT STRUT FAIRING FWD SIDE JUST AFT OF HYD COMPT IAW B767 SRM 51-40-02

Part: STIFFENER — CRACKED · airframe 74,880 hrs · 17,901 cycles

#2 AFT STRUT FAIRING ANGLE ON INBOUND FORWARD SIDE OF AFT WEB RUNNING FORE AND AFT IS CRACKED. REMOVED AND REPLACED STRUT FAIRING ANGLE IAW B767 SRM 51-40-02.

Part: BULKHEAD — CRACKED · airframe 74,880 hrs · 17,901 cycles

#1 PYLON PANEL 437DB V FRAME CRACKED. REMOVED DAMAGED V FRAME AND INBD CHANNEL MATCH DRILLED HOLES IAW B767 1-40-05 AND REINSTALLED CHANNELS AND V FRAME IAW B767 SRM 51-40-02 PARA 4 AND PARA 7.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 72,406 hrs · 17,149 cycles

RIGHT FLIGHT DECK EMERGENCY FLASHLIGHT IS INOPERATIVE. CENTER FLASHLIGHT IS OPERATIONAL. INITIATED DEFERRAL MAINTENANCE ITEM-17342. REMOVED AND REPLACED RIGHT FLIGHT DECK EMERGENCY FLASHLIGHT AND BATTERY, IAW B767 AMM 25-05-03. OPERATIONAL CHECK SATISFACTORY. FAULT NOT DUPLICATED. DEFERRAL MAINTENANCE ITEM 17342 CLEAR.

Part: CLAMP — NOT SEATED (BLEED AIR SYS) · airframe 70,243 hrs · 16,456 cycles

"LEFT BLEED DUCT LEAK" CAUTION EICAS MSG. COMPLETED ASSOCIATED QRH PROCEDURE. INSPECTED LEFT PACK CROSS OVER DUCT, ISO VALVE, AND ACM AREA CLAMPS WITH BAY DOORS OPEN AND CLOSED. NO EICAS MSG NOTED. OK FOR SVC REF AMM 21-50-00. LP 1069086 - ITEM 1: DEFERRED TO MDDR 117700 PER MEL 21-51-01-01, CAT 'C'. DDG COMPLIED WITH. MCC NOTIFIED. LP 1069092 - M3: T/S IAW FIM 21-51 FAULT TREE 804. FOUND RAM OUTLET ACTR TO BE AT FAULT. PLACED PART ON BOARD. DMI 117700 REMAINS OPEN. LP 1069094 - M3: REMOVED & REPLACED "RAM AIR EXHAUST DOOR ACTUATOR" LT PACK IAW AMM 21-53-04, STILL INOP, PROBLEM STILL EXISTS. SWAPPED PACK TEMP CONTROLLERS FOR TROUBLESHOOTING, SWAPPED BACK TO ORIGINAL POSITIONS. PROBLEM STILL EXISTS IAW AMM 21-51-14. MEL STILL OPEN. LP 1069099 - M8: RE-SEATED CLAMPS. RAN PACK FOR 2+ HOURS, NO DEFECTS OR LEAKS NOTED AT THIS TIME, REF AMM 36-11-00. RAN BITE TEST, NO DEFECTS NOTED. EXHAUST DOOR ACTUATES AS IT SHOULD, NO DEFECTS NOTED AT THIS TIME. THIS CLEARS DMI 117700. PLACARDS REMOVED AND MCC NOTIFIED.

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 70,217 hrs · 16,447 cycles

LP 1100481 (MIA) - SPAR VALVE CHECK FAILS DURING ENG START - RT ENG - RETURN TO BLOCKS. LP 1100482 (CVG) - INFO ONLY - DURING RT ENG START SPAR VALVE CYCLES NORMALLY. THIS AFTER RETURN TO BLOCKS DUE TO NO CYCLING . INDICATION AND LATER DEFERRAL. LP 1100481 (MIA) - VERIFIED SPAR VLV OPERATIONAL, CW WITH DDG 28-40-02 ITEM -TRANSFERRED TO MDDR 117472 CAT C - EXP 18SEP19. LP 1100482 (CVG) - PERFORMED OPS CHECK OF RT SPAR VALVE IAW AMM 28-22-04-404 SUBPART F. OPS CHECK GOOD AT THIS TIME. THIS CLOSES DMI 117472.

Part: OIL SYSTEM — UNDERSERVICED (APU) · airframe 70,150 hrs · 16,425 cycles

"APU FAULT" EICAS, 2 ATTEMPTS UNSUCCESSFUL. SERVICED APU OIL IAW AMM 12-13-04. OPS CHECK OK, START ON FIRST ATTEMPT PER AMM 49-11-00.

Part: PRESSURE SWITCH — FAILED (APU) · airframe 70,118 hrs · 16,414 cycles

APU FAULT, SHUTDOWN DURING POWER TRANSFER. BIT CHECKED THE APU ECU AND FOUND IT WAS FLAGGING LOW OIL PRESSURE IAW FIM 49-11 FT 987. REMOVED AND REPLACED APU LOW OIL PRESSURE SWITCH, IAW AMM 49-94-02. OPS CHECKED OK. CLEARED APU FAULT AND DOOR STATUS FAULT.

Part: WARNING MESSAGE — FALSE ACTIVATION (EXHAUST FAN) · airframe 70,130 hrs · 16,417 cycles

AFT EQ EXH FAN 2 STATUS MESSAGE. T/S PER FIM 21-26 FAULT TREE 808. MESSAGE CLEARED, OPS CHECK NORMAL.

Part: DISPLAY — MALFUNCTIONED (WX RADAR SYSTEM) · airframe 70,009 hrs · 16,375 cycles

RADAR DISPLAYS SCATTERED RETURNS ACROSS ENTIRE DISPLAY WITH NO PRECIP IN VICINITY. PERFORMED WX RADAR OPERATIONAL TEST IAW AMM 34-43-00. OPS TEST OK, NO DEFECTS NOTED AT THIS TIME.

Part: SHUTOFF VALVE — UNKNOWN (RT ENGINE) · airframe 69,984 hrs · 16,366 cycles

EICAS AND STATUS MSG: R ENG HPSOV. PERFORMED RIGHT ENGINE RUN, NO MESSAGE DISPLAYED AT THIS TIME. PACK PRESSURE HOLDS GOOD. THERE ARE NO DEFECTS FOUND AT THIS TIME, OPS CHECK PERFORMED IAW 71-00-00. REMOVED AND REPLACED R ENGINE HPSOV IAW AMM 36-11-02. LEAK CHECKED GOOD. BITE TEST GOOD IAW 36-23-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENG HPSOV) · airframe 69,980 hrs · 16,364 cycles

RIGHT ENGINE HPSOV DISPLAYED ON STATUS PAGE. PERFORMED A BITE TEST, NO FAULTS FOUND. SYSTEM OPS CHECKED GOOD IAW AMM 36-00-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT SHUTOFF VALVE) · airframe 69,955 hrs · 16,356 cycles

RIGHT ENGINE HPSOV MESSAGE DISPLAYED ON EICAS, IN FLIGHT. PERFORMED AIR SUPPLY BITE PROCEDURE IAW FIM 36-20-00/101. FOUND RH SYS PRV LIGHT ILLUMINATED. PERFORMED MX ACTIONS IAW DDG VOL. 2 36-11-08-01-01A. REACTIVATED R HPSOV. PERFORMED BITE AIR SUPPLY MODULE, NO DEFECTS NOTED IAW AMM 36-20 FT 804. OPS CHECK GOOD, NO MSGS. PERFORMED ENG RUN IAW AMM 71-00-00, NO FAULTS NOTED.

Part: SWITCH — FAULTY (FIRE WARNING) · airframe 69,935 hrs · 16,348 cycles

FWD CARGO FIRE SWITCH LIGHT ON THE P-8 PANEL WOULD NOT TEST DURING SYSTEM OR BRIGHT LIGHT TEST. (BULB GOOD) FWD CARGO FIRE SYSTEM PLACED ON MEL DEFERRAL IAW DDG 26-23-01. MDDR 115416. LP 1053596 - M7: REMOVED AND REPLACED FWD LOWER CARGO FIRE SWITCH IAW SWPM 20-84-15. MDDR 115416 CLEARED. PLACARD REMOVED AND MCC NOTIFIED.

Part: CONTROL VALVE — MALFUNCTIONED (AC BAY) · airframe 69,930 hrs · 16,346 cycles

L BLEED DUCT LEAK. (<P>TRANSFERRED TO DMI 115382 PER MEL 21-51-01-01, CAT 'C', DUE DATE: 05-AUG-19. PLACARDS INSTALLED AND MX ACTION C/W.&NBSP;</P><P>LP 1053595 - M5: REMOVED AND REPLACED LEFT PACK TEMP CONTROL VALVE REF AMM 21-51-12. OPS CHECK NORMAL. THIS CLEARS MDDR 115382. PLACARD REMOVED.&NBSP;</P>)

Part: OIL SYSTEM — LOW (APU) · airframe 69,903 hrs · 16,335 cycles

APU WOULD NOT START. &NBSP;(<P>PERFORMED B767 FIM 49-11 FT 987 APU BITE PROCEDURES. SERVICED OIL, CLEARED FAULTS. OPS CHECK GOOD.&NBSP;&NBSP;</P>)

Part: BRAKE — FIRE (LT MLG) · airframe 69,868 hrs · 16,321 cycles

ON EXITING RW, TWR ADVISED SMOKE &AMP; FIRE EMANATING FROM LEFT MAIN GEAR. EMERGENCY VEHICLES RESPONDED &AMP; SPRAYED GEAR.(<P>REMOVED AND REPLACED #6 BRAKE ASSY IAW AMM 32-41-08, OPS CHECK GOOD. PERFORMED ANTI-SKID OPERATIONAL TEST AND BITE TEST IAW AMM 32-42-00, NO FURTHER DEFECTS NOTED AT THIS TIME . INSPECTED AXLE, NO DEFECTS NOTED.&NBSP;</P><P>LP 1058502 - M4: AS PRECAUTION, REMOVED AND REPLACED #5 MWA IAW AMM 32-45-01. VERIFIED AXLE WASHER INSTALLATION OK. </P><P>LP 1058502 - M6: PERFORMED HIGH ENERGY STOP INSPECTION IAW AMM 05-51-14. NO DEFECTS NOTED AT THIS TIME.</P>)

Part: BLEED AIR SYS — MALFUNCTIONED (APU) · airframe 69,831 hrs · 16,309 cycles

NO DUCT PRESSURE DURING APU OPERATION.(<P>TRANSFERRED TO MDDR 114602 PER 49-11-01-01 CAT C DUE 21JUL19 VALVE LOCKED OUT PER DDG 36-11-01.</P><P>LP 1080383 - M2:&NBSP;PUT THE AIRPLANE BACK IN ITS USUAL CONFIGURATION. PERFORMED FIM 36-10 FAULT TREE 839. NO FAULTS NOTED. RAN BOTH PACK AIR VALVES AND DRY MOTORED AN ENGINE WITH NO FAULTS. APU BLEED OPERATES AS NORMAL. SEE ITEM 3</P><P>LP 1080383 - M3:&NBSP;PER CUSTOMER REQUEST, R&AMP;R APU ECU IAW AMM 49-61-05. OPS CHECK GOOD. THIS CLEARS DMI 114602. PLACARDS REMOVED. NO OTHERS DEFECTS NOTED AT THIS TIME.</P>)

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 69,835 hrs · 16,311 cycles

NO APU DUCT PRESSURE ON STARTUP AFTER LANDING. (<P><SPAN>RE-STARTED APU DUCT PRESSURE NORMAL, NO FAULTS FOUND REF AMM 49-11-00 DUCT PRESSURE REF 49-52-00.</SPAN><BR DATA-MCE-BOGUS="1" /></P>)

Part: EEC — MALFUNCTIONED (RT ENGINE) · airframe 69,793 hrs · 16,294 cycles

NO LIGHT OFF ON RIGHT ENGINE START. SELECTED BOTH, SECOND ATTEMPT SUCCESSFUL.&NBSP;(<P>RT ENGINE IGN. 1(A) INOP, DEFERRED IGN 1(A) PER MEL 74-00-01B CAT 'C'. THIS OPENS DMI # 114171, PLACARD INSTALLED AND MCC NOTIFIED.</P><P>LP 1054226 - M5:&NBSP; T/S PER SRM 74-31-01. INPUT VOLTAGE FROM PINS 8 TO 7 GOOD. SHOT WIRES FROM J1 ON EEC 103.9 TO EXCITER PINS A &AMP; B. VOLTAGE CHECK GOOD. NO OUTPUT VOLTAGE. SUSPECT EEC ON RT ENG. P/N: 0748250CN1820M33P14.</P><P>REMOVED RT ENGINE EEC AS PER AMM 73-21-50. OPS CHECKED GOOD AS PER AMM 71-00-00 GROUND TESTS EEC'S<BR DATA-MCE-BOGUS="1" /></P>)

Part: LIGHT — INTERMITTENT (BLEED WARNING) · airframe 69,750 hrs · 16,279 cycles

RIGHT ENG BLEED OFF BACKLIGHTING, NO ILLUMINATION WITH ENG SHUT DOWN. FOUND DURING COCKPIT PRE-FLIGHT. RESET RT ENG BLEED SWITCH IAW AMM 36-20-00. OFF LIGHT CAME BACK ON. OPS CHECKED GOOD.

Part: EXCITER — MALFUNCTIONED (RT ENGINE) · airframe 69,733 hrs · 16,273 cycles

ITEM 1 - INFO, FIRST START ATTEMPT ON RIGHT ENGINE NO LIGHT OFF. ITEM 2 - STATUS MESSAGE: R ENG IGNITER 1(<P>RT ENG #1 IGNITION INOP. PLACED ON MEL 74-00-01B DMI #113663, SELECT BOTH TO START ENGINE.&NBSP;</P><P>LP 1080536 - M2:&NBSP;REMOVED AND REPLACED RT ENG #1 IGNITER PLUG IAW AMM 74-21-02. NO FIX. DMI # 113663 REMAINS OPEN.</P><P>LP 1080539 - M4: INITIALLY, RT ENG #1 IGN FAILED AUDIBLE TEST PER AMM 74-00-00, CLEANED AND RE-SEATED IGN EXCITER #1 CONNECTOR (M7196). AUDIBLE TEST PASSED, CHECKED WIRES FROM EEC TO IGN #1 EXCITER PER SWPM 20-10-06, NO DEFECTS NOTED. R/R RELAY K1231 PER SWPM 20-81-22. RAN RT ENGINE ISOLATING L ENG, OPS CHECKED GOOD PER AMM 71-00-00 DMI REMAINS OPEN.</P><P>LP 1054203 - M5:&NBSP;PERF. ENGINE #2 IDLE RUN IN SINGLE IGNITION POSITION IAW AMM 71-00-00-712-168-H03. OPERATION NORMAL. DMI REMAINS. MCC ADVISED.</P><P>LP 1054211 - M6:&NBSP;REMOVED AND REPLACED RT ENGINE #1 LEAD IAW AMM 74-21-01. OPS CHECK, NOT GOOD. DMI 113663 REMAINS OPEN, NEED FURTHER T/S.&NBSP;</P><P>LP 1054220 - M6: REMOVED AND REPLACED #1 AND #2 EXCITER BOXES ON RIGHT ENGINE IAW AMM 74-11-01. OPS CHECK NORMAL. ENGINE START NORMAL (#1 AND #2) SYSTEM EMS. NOT EICAS MESSAGE.&NBSP;THIS CLEARS&NBSP;MDDR 113663.&NBSP; </P><P>2ND OFF PART (P/N 10-631045-3B, S/N: LFW354)</P>)

Part: SWITCH — BROKEN (OXYGEN TEST) · airframe 69,716 hrs · 16,268 cycles

CAPTAIN`S OXYGEN TEST RESET SWITCH BROKEN. REMOVED AND REPLACED CAPT OXYGEN STOWAGE PER ASSY AS REQ, LEAK CHECKED GOOD IAW AMM 35-11-51.

Part: EXCITER — MALFUNCTIONED (NR 2 ENGINE) · airframe 69,683 hrs · 16,259 cycles

# 2 ENGINE DID NOT START WITH SINGLE IGNITER , SWITCHED TO BOTH FOR BOTH ENGINE STARTS. PERFORMED NO.2 SYS IGNITION AUDIBLE TEST. CONFIRMED ONLY ONE IGNITER IS OPERATING WITH SWITCH SET TO 'BOTH'. A/C DOWNGRADED TO ER 60. PLACARDS INSTALLED. REMOVED AND REPLACED #1 IGN EXCITER & #1 IGN PLUG ON #2 ENG IAW AMM 74-11-01 & 74-21-02. PERFORMED OPS CHECK IAW AMM 71-00-00, OPS CHECK GOOD AT THIS TIME.

Part: VALVE — UNKNOWN (APU DUCT PRESS) · airframe 69,567 hrs · 16,225 cycles

NO APU DUCT PRESSURE. PERFORMED OPS CHECK PER AMM 49-11-00. CYCLED APU VALVE AND GOT DUCT PRESSURE. NO FURTHER DEFECTS NOTED.

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 69,519 hrs · 16,208 cycles

DURING TAXI OUT, FUEL PANEL IN OVHD PNL, ALL QTYS BLANKED AS WELL AS TEMP &AMP; TOTAL. DURING RETURN TO GATE,&NBSP; DISPLAY BECAME INTERMITTENT. MOMENTARY FUEL QTY BITE STATUS MSG DISPLAYED.(<P>PERFORMED FUEL QTY BITE PROCEDURE IAW FIM 28-41 FT 847. RECEIVED "NO PRESENT FAULTS" MSG. FUEL QTY INDICATORS OPERATING / INDICATING NORMAL AT THIS TIME IAW AMM 28-41-00.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 69,507 hrs · 16,204 cycles

AFT CARGO OVHT CAUTION MSG ON TAXI OUT. (<P>TRANSFERRED TO MDDR #112207 IAW MEL 21-40-01-01. (M) C/W, PLACARD INSTALLED AND MCC NOTIFIED. CAT 'C' DUE 4 JUN 19.</P><P>LP 1024647 - M2:&NBSP;OPS CHECK 21-44-00, NO DEFECTS NOTED AT THIS TIME. PLACED RELAY K229 ON ORDER WITH MCC, P/N BACR13CF2AB PRECAUTIONARY.&NBSP; RELAY REMOVED AND STOWED IN OVERHEAD BIN IAW 21-40-01-01. DMI REMAINS OPEN.</P><P>LP 1066208: REMOVED AND REPLACED AFT OVER HEAT RELAY K229 IAW AMM 21-44-11. OPS CHECK GOOD.&NBSP;</P>)

Part: SWITCH — MALFUNCTIONED (CARGO BAY) · airframe 69,492 hrs · 16,199 cycles

AFT CARGO OVER HEAT INDICATION. (<P>REMOVED AND REPLACED AFT CARGO OVER HEAT SWITCH IAW AMM 21-44-05.</P>)

Part: EXCITER — ARCED (NR 1 ENGINE) · airframe 69,492 hrs · 16,199 cycles

ENGINE #1 UPPER IGNITION LEAD SYSTEM #1 HAS ARC MARKS AND PITTING AT EXCITER CONNECTION. (<P>REMOVED AND REPLACED #1 ENGINE UPPER IGNITION EXCITER BOX IAW AMM 74-11-01. OPS CHECK NORMAL.</P>)

Part: IGNITION LEAD — ERODED (NR 1 ENGINE) · airframe 69,492 hrs · 16,199 cycles

ENGINE #1 LOWER IGNITION EXCITER BOX. EXCITER #1 LEAD CONNECTION HAS EROSION ON PIN. (<P>REMOVED AND REPLACED ENGINE #1 LEAD IGNITION LOWER CONNECTION IAW AMM 74-21-01. OPS CHECK NORMAL.</P>)

Part: VALVE — MALFUNCTIONED (APU) · airframe 69,455 hrs · 16,186 cycles

APU BLEED AIR INOP. WILL NOT SUPPLY PRESSURE.(<P>RESET APU BLEED AIR VALVE IAW AMM REF 36-11-00. APU BLEED NORMAL.</P>)

Part: ECU — FAULTY (APU) · airframe 69,436 hrs · 16,181 cycles

APU DUCT PRESS INTERMITTENT 0-15 PSI.(<P>REMOVED AND REPLACED APU ECU AND OPS CHECK IS GOOD AT THIS TIME IAW AMM 49-01-05.<BR /></P>)

Part: CONTROLLER — MALFUNCTIONED (AC BAY) · airframe 69,398 hrs · 16,170 cycles

RIGHT PACK TEMP IN AUTO MODE INOP.&NBSP;(<P>TRANSFERRED TO MDDR 111374 PER MEL 21-51-03-01 CAT "C". </P><P>LP 1053418 - REMOVED AND REPLACED PACK TEMP CONTROLLER IAW AMM 21-51-14.</P>)

Part: CONTROLLER — MALFUNCTIONED (AC BAY) · airframe 69,398 hrs · 16,170 cycles

AFT CARGO OVHT MESSAGE ILLUMINATED.(<P>TRANSFERRED TO MDDR# 111378 PER MEL 21-40-02-01-01B CAT C DUE 19MAY19.&NBSP;&NBSP;</P><P><SPAN>LOG PAGE 1053418 - M4: PERFORMED BITE TEST OF RT PACK CONTROLLER. FOUND CONTROLLER FAULT LIGHT ILLUMINATED. REMOVED AND REPLACED RT CONTROLLER WITH SERVICEABLE UNIT. OPS CHECK IS GOOD.&NBSP;&NBSP;THIS CLEARS DMI # 111374. PLACARDS REMOVED. MCC NOTIFIED. REF AMM 12-51-14.</SPAN><BR DATA-MCE-BOGUS="1" /></P><P><SPAN>LOG PAGE 1053418 - M5:&NBSP;REF LP 1053418, ITEM 4 FOR REPLACEMENT OF RT PACK CONTROLLER. PERFORMED OPS CHECK OF AFT CARGO HEAT. OPS CHECK IS GOOD. NO MESSAGES DISPLAYED. THIS CLEARS DMI # 111378. REF AMM 21-44-00. MCC NOTIFIED. PLACRADS REMOVED.&NBSP;</SPAN></P>)

Part: MODULE — FAILED (APU FLOW) · airframe 69,287 hrs · 16,140 cycles

APU SHUTDOWN WHILE ON THE GROUND (UNCOMMANDED).(<P>PERFORMED APU BITE IAW FIM 49-11 FT 987. FOUND PT SENSOR FAULTY. PERFORMED PT SENSOR FIM 49-11 F/T A15 BLOCK 1. R/R FLOW SENSING MODULE IAW AMM 49-53-08. OPS CHECK GOOD AND NO FURTHER DEFECTS NOTED.</P><P>LP 1078502 - M5: ACCOMPLISHED APU COLD SOAK START VERIFICATION SATISFACTORY INTO MIA. THIS CLEARS DMI 110816.</P>)

Part: CHARGER — INOPERATIVE (APU BATTERY) · airframe 69,205 hrs · 16,116 cycles

APU BATTERY CHARGER STATUS MSG. REMOVED AND REPLACED APU BATTERY CHARGER IAW AMM 24-31-05-004-001. OPS CHECK GOOD. T

Part: BATTERY — FAULTED (APU) · airframe 69,187 hrs · 16,107 cycles

UNABLE TO START APU WHILE TAXI IN. TRIED TWO ATTEMPTS. APU INOP. PERFORMED FIM 49-11FT 987 & 988. FOUND FAULTS WITH THE ECU. PERFORMED FIM 49-11 FAULT TREE 988, FOUND APU BATTERY CHARGER TO BE SUSPECTED AT FAULT. PERFORMED FIM 49-11 FT 988, VERIFIED BATTERY CHARGER AT FAULT. REMOVED AND REPLACED APU BATTERY CHARGER IAW AMM 24-31-05-424-007. REMOVED AND REPLACED THE APU BATTERY IAW AMM 24-31-04-004-001.

Part: APU — FAULTED · airframe 69,184 hrs · 16,106 cycles

APU FAULT AFTER LANDING. 2 ATTEMPTS MADE, BOTH UNSUCCESSFUL STARTS.&NBSP;(<P>PERFORMED FIM 49-11 FT 987 APU BITE PROCEDURE, "START ABORTED" FAULT, CLEARED MESSAGE. PERFORMED OPS CHECK OF APU IAW AMM 49-11-00. OPS CHECK GOOD. NO MESSAGE PRESENT, RAN FOR 15 MINUTES 2X TIMES.</P>)

Part: OIL SYSTEM — LOW (APU) · airframe 69,174 hrs · 16,103 cycles

APU FAULT EICAS DURING APU START AFTER LANDING, ATTEMPTED 2 STARTS.(<P>FOUND APU OIL LOW. APPLIED 1 QT OF OIL INTO THE APU PER AMM 12-10-00. OPS CHECK OK.</P>)

Part: SENSOR — MALFUNCTIONED (APU) · airframe 69,114 hrs · 16,079 cycles

NO APU BLEED AIR PRESSURE AFTER APU START. REMOVED AND INSTALLED SERVICEABLE P2 SENSOR ON APU IAW AMM 49-61-04 OPS CHECKED AND FOUND OPERATING NORMAL AT THIS TIME. REMOVED AND REPLACED APU FLOW SENSING MODULE, OPS CHECK OF MODULE SATISFACTORY REF AMM 49-53-08, ALSO CHECKED IGV FOR PLAY AND PROPER PUSH/PULL LIMITS. TENSION IS WITHIN LIMITS. PERFORMED ECM ACTION ITEMS 1-5, NO FAULTS FOUND, R & R APU ECU IAW AMM 49-61-05. PERFORMED FIM 49-11 FAULT TREE A05. NO HELP. ACCOMPLISHED W/O 49770 REPLACED APU I.A.W AMM 49-11-01 OPS CHECK NORMAL.

Part: CONTROL PANEL — DEFECTIVE (ELECTRICA.L SYS) · airframe 69,114 hrs · 16,079 cycles

LT UTILITY LIGHT INOP&NBSP;(<P>REMOVED AND REPLACED ELECTRICAL SYSTEM CONTROL PANEL IAW AMM 24-22-01 OK&NBSP;</P>)

Part: WIRE — ARCED (P61) · airframe 69,090 hrs · 16,072 cycles

FWD EQUIP SUPPLY FAN 1 STATUS MSG(<P>TRANSFERRED TO MDDR # 108940 IAW MEL 21-58-03-02-01 CAT C DUE 29MAR19. MX PROCEDURES C/W.</P><P><BR /></P><P>FOUND 3 WIRES BEHIND P61 TO BE ARCHING, REF LP 1065470 ITEM 3 FOR SIGN OFF. PERFORMED OPS CHECK OF SUPPLY EXH FAN FAN IAW AMM 21-58-02. OPS CHECK NORMAL AT THIS TIME. THIS CLEARS DMI # 108940 AND PLACARD REMOVES.&NBSP;<BR /></P>)

Part: WIRE — ARCED (P61) · airframe 69,090 hrs · 16,072 cycles

AFTER LIFTOFF, TAT EICAS DISPLAYED A/T KICKED &AMP; L NAV VNAV INOP(<P>FOUND 3 WIRES BEHIND P61 TO BE ARCHING REF LP 1065470 ITEM 3&NBSP; FOR SIGN OFF. PERFORMED TEST 30/40 IAW FIM 22-03 FT 818,819 NO DEFECTS NOTED AT THIS TIME.&NBSP;</P><P>ITEM (3) SPLICED WIRE W62-51N-12, W62-5IR-12 ,W62-56M-22 IAW SWPM 20-30-12 NO DEFECTS NOTED SPLICES ARE LOCATED APPROXIMATELY 3 INCHES FROM CONNECTOR D05934P POS 8.</P>)

Part: WIRE — ARCED (P61) · airframe 69,090 hrs · 16,072 cycles

R CENTER TANK PUMP EICAS(<P>TRANSFER TO MDDR 108944 IAW MEL 28-22-02A CAT C DUE DATE 29-MAR-19</P><P>FOUND 3 WIRES BEHIND P61 TO BE ARCHING, REF LP 1065470 ITEM 3 FOR SIGN OFF. PERFORMED OPS CHECK OF CENTER TANK FUEL PUMP IAW AMM 28-00-00. OPS CHECK NORMAL AT THIS TIME. CLEARED MDDR 108944 AND PLACARD REMOVED.&NBSP;<BR /></P>)

Part: PRESSURE SWITCH — FAULTY (ANIT-ICE SYS) · airframe 68,995 hrs · 16,037 cycles

RT ENG TAI EICAS MSG.(<P>R&AMP;R RT ENG TAI PRESSURE SWITCH IAW AMM 30-21-01 OPS CHECK GOOD.<BR /></P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 69,010 hrs · 16,041 cycles

L BLEED ISLN VAL AFTER LANDING(<P>PERFORMED OPERATIONAL TEST OF L ISO BLEED VALVE IAW AMM REF 36-11-04-404-013. OPS CHECK GOOD.</P>)

Part: CONTROL PANEL — MALFUNCTIONED (GENERATOR) · airframe 68,962 hrs · 16,026 cycles

R GEN DRIVE LIGHT INOP.(<P>TRANSFERED TO MDDR #107761 IAW MEL 24-00-01-01 DUE 26FEB19. REMOVED AND REPLACED GEN CONTROL PANEL IAW AMM 24-22-01 OPS CHECKED GOOD THIS CLEARS MDDR 107761 PLACARD REMOVED. LOG PAGE 929242, R&AMP;R GEN CONTROL PANEL IAW AMM 24-22-01 ALL CHECKS GOOD THIS CLEARS MDDR 107761, PLACARDS REMOVED MCC NOTIFIED JL 1435Z<BR /></P>)

Part: ENGINE — VIBRATION (RIGHT) · airframe 68,877 hrs · 16,000 cycles

HIGH RIGHT ENG VIBRATION ( FAN IND 4.7) ON CLIMB 11,500' AT 280 KIAS EVENT RECORD @1149Z(<P>C/W FIM 71-05 FT 852 TO STEP 6. PERFORMED AND CW THE TRIM BALANCE OF THE FAN ROTOR IAW B767 AMM 72-31-00 AND VIBRATION SURVEY IAW B767 AMM 71-00-00. OPS CHECKS GOOD. NO DEFECTED NOTED AT THIS TIME.</P>)

Part: UNKNOWN — VIBRATION (AIRFRAME) · airframe 68,877 hrs · 16,000 cycles

SUBSTANTIAL AIRFRAME VIBRATION WHEN ENGINES SPOOL UP FROM IDLE IN FLIGHT. NO VIBRATION INDICATION ON ENGINE PAGE.(<P>PERFORMED AIRFRAME VIBRATION CONDITIONAL INSPECTION I.A.W A.M.M 05-51-38. NO ABNORMALITIES OR DEFECTS NOTED<BR /></P>)

Part: BLADE — DAMAGED (NR 2 ENGINE FAN) · airframe 68,871 hrs · 15,997 cycles

FOUND MULTIPLE BLADES (FAN) WITH DAMAGE ON #2 ENG.(<P>ALL BLADES IDENTIFIED IN SERVICE CHECKAND NEW DISCREPANCIES NOTED.<BR /></P>)

Part: BLADE — DAMAGED (NR 1 ENGINE) · airframe 68,871 hrs · 15,997 cycles

FOUND MULTIPLE BLADES (FAN) WITH DAMAGE ON #1 ENG.(<P>BLADES REQ REWORK DUE TO DAMAGE BLADE 34 REMOVED 1.2 IN BEND LEADING EDGE TO TRAILING. BLADE 30 REMOVED .7 IN BEND LEADING TO TRAILING. BLADE #4 CONTOURED .4 - 3" FROM LEADING EDGE BLADE 1 CONTOURED .2 IN&NBSP;BEND .4 FROM LEADING EDGE IAW AMM 767-72-31-02-308-055-H00. ALL WITHIN LIMITS.<BR /></P>)

Part: BLADE — DAMAGED (NR 2 ENGINE) · airframe 68,868 hrs · 15,995 cycles

#2 ENGINE LP BLADE #36 DAMAGED.(<P>INSPECTED #36 BLADE IAW B767 AMM 72-31-02,DAMAGED FOUND TO BE WITHIN ALLOWABLE LIMITS WITH NO FURTHER ACTION REQUIRED.</P>)

Part: BLADE — DAMAGED (NR 2 ENGINE) · airframe 68,868 hrs · 15,995 cycles

#2 ENGINE LP BLADE #27 DAMAGED.(<P>BLENDED DAMAGED AREA IAW B767 AMM 72-31-02,FOUND TO BE WITHIN ALLOWABLE LIMITS.</P>)

Part: BLADE — DAMAGED (NR 2 ENGINE) · airframe 68,868 hrs · 15,995 cycles

#2 ENGINE LP BLADE #31 DAMAGED.(<P>REMOVED AND REPLACED #31 BLADE IAW B767 AMM 72-31-02.</P>)

Part: BLADE — DAMAGED (NR 2 ENGINE) · airframe 68,868 hrs · 15,995 cycles

#2 ENGINE LP BLADE #18 DAMAGED.(<P>REMOVED AND REPLACED #18 BLADE IAW B767 AMM 72-31-02.</P>)

Part: BLADE — DAMAGED (NR 2 ENGINE) · airframe 68,868 hrs · 15,995 cycles

#2 ENGINE LP BLADE #11 DAMAGED.(<P>INSPECTED BLADE #11 IAW&NBSP; B767 AMM 72-31-02,DAMAGED FOUND TO BE WITHIN ALLOWABLE LIMITS WITH NO FURTHER ACTION REQUIRED.</P>)

Part: BLADE — DAMAGED (NR 2 ENGINE) · airframe 68,868 hrs · 15,995 cycles

#2 ENGINE LP BLADE #32 DAMAGED.(<P>BLENDED DAMAGED AREA IAW B767 AMM 72-31-02,FOUND TO BE WITHIN ALLOWABLE LIMITS.</P>)

Part: BLADE — DAMAGED (NR 2 ENGINE) · airframe 68,868 hrs · 15,995 cycles

#2 ENGINE LP BLADE #3 DAMAGED.(<P>REMOVED AND REPLACED #3 BLADE IAW B767 AMM 72-31-02.</P>)

Part: ROD — DAMAGED (NACELLE DOOR) · airframe 68,868 hrs · 15,995 cycles

#2 ENGINE I/B COWL HOLD OOPEN ROD DAMAGED.(<P>REMOVED AND REPLACED #2 ENGINE I/B CORE COWL HOLD OPEN ROD IAW B767 AMM 20-11-00,ASSET #0019776.</P>)

Part: BLADE — DAMAGED (NR 2 ENGINE) · airframe 68,868 hrs · 15,995 cycles

#2 ENGINE LP BLADE #25 DAMAGED.(<P>BLENDED DAMAGED AREA IAW B767 AMM 72-31-02,FOUND TO BE WITHIN ALLOWABLE LIMITS.</P>)

Part: BLADE — DAMAGED (NR 2 ENGINE) · airframe 68,868 hrs · 15,995 cycles

#2 ENGINE LP BLADE #13 DAMAGED.(<P>BLENDED DAMAGED AREA IAW AMM 72-31-02,FOUND TO BE WITHIN ALLOWABLE LIMITS.</P>)

Part: BLADE — DAMAGED (NR 2 ENGINE) · airframe 68,868 hrs · 15,995 cycles

#2 ENGINE LP BLADE #26 DAMAGED.(<P>REMOVED AND REPLACED #26 BLADE IAW B767 AMM 72-31-02.</P>)

Part: BLADE — DAMAGED (NR 2 ENGINE) · airframe 68,868 hrs · 15,995 cycles

#2 ENGINE LP BLADE #28 DAMAGED.(<P>BLENDED DAMAGED AREA IAW B767 AMM 72-31-02 FOUND TO BE WITHIN ALLOWABLE LIMITS.</P>)

Part: BLADE — DAMAGED (NR 2 ENGINE) · airframe 68,868 hrs · 15,995 cycles

#2 ENGINE LP BLADE #14 DAMAGED.(<P>BLENDED DAMAGED AREA IAW B767 AMM 72-31-02 FOUND TO BE WITHIN ALLOWABLE LIMITS.</P>)

Part: APU — FAULTED · airframe 68,868 hrs · 15,995 cycles

APU FAULT WHEN ATTEMPTING TO START.(<P>PERFORMED MULTIPLE APU START UPS &AMP; SHUTDOWNS WITH APU ECU BITE PROCEDURE IAW B767 AMM 49-61-05,NO DEFECTS NOTED.</P>)

Part: BLADE — DAMAGED (NR 2 ENGINE) · airframe 68,868 hrs · 15,995 cycles

#2 ENGINE LP BLADE #19 DAMAGED.(<P>BLENDED DAMAGED AREA IAW B767 AMM 72-31-02 FOUND TO BE WITHIN ALLOWABLE LIMITS.</P>)

Part: APU — FAULTED · airframe 68,860 hrs · 15,990 cycles

APU FAULT WHEN ATTEMPTING START.(<P>TRANSFER TO MDDR # 107038 PER MEL 49-11-01A. PLACARD INSTALLED. MCC NOTIFIED, CAT C EXP 17FEB19, TI: ST@ 1916Z.</P><P>LP 1041293-M1: BITE CHECKED ECU, CLEARED FAULTS.&NBSP;<SPAN>PERFORMED MULTIPLE APU START UPS &AMP; SHUT DOWNS WITH APU ECU BITE PROCEDURE IAW B767 AMM 49-61-05. NO DEFECTS NOTED, THIS CLEARS DMI #107038.</SPAN></P>)

Part: CONTROL VALVE — MALFUNCTIONED (APU SURGE) · airframe 68,809 hrs · 15,968 cycles

AIR PRESSURE FROM APU NOT STABLE DURING ENGINE START.UNABLE TO GET STABILIZED N2(<P>TRANSFERRED TO MDDR 106753 IAW DDG 49-11-01A, CAT C DUE 11FEB19 .</P><P>R/R SURGE CONTROL VALVE PER AMM 49-53-01. OPS CK GOOD.

Part: CONTROLLER — MALFUNCTIONED (CABIN TEMP) · airframe 68,791 hrs · 15,961 cycles

FWD CABIN TEMP CONTROLLER EICAS(<P>RESET SYSTEM PER ZONE TEMP CONTROLLER AMM 21-00-00-449 OPS CHECK NORMAL</P>)

Part: MODULATING VALVE — FAULTY (AC BAY) · airframe 68,793 hrs · 15,962 cycles

REMOVE AND REPLACE FWD ZONE TRIM AIR MODULATING VALVE PER MCC(<P>REMOVED AND REPLACED FWD ZONE TRIM AIR MODULATING VALVE PER MCC IAW AMM 21-61-07 AND OPS CHECK IS GOOD AT THIS TIME.</P>)

Part: ECU — MALFUNCTIONED (APU) · airframe 68,784 hrs · 15,958 cycles

APU WON'T STAY RUNNING(<P>T/S APU MINI FLAG 48 &AMP; 99 R&AMP;R APU ECU IAW AMM 49-61-05<BR />ALL CHECKS GOOD AT THIS TIME. <BR /></P>)

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 68,763 hrs · 15,948 cycles

SPAR VALVE FAILED OPEN ON NR 1 ENG START(<P>PERFORMED NR 1 ENG RUN TO VERIFY SPAR VALVE OPERATION IAW AMM 71-00-00 SPAR VALVE OPS NORMAL&NBSP;</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 68,700 hrs · 15,926 cycles

"FLIGHT DECK TEMP" MSG IN FLIGHT FOLLOWED QRH PROCEDURE AND TURNED OFF TRIM AIR VALVE THEN "TRIM AIR" AFT CABIN TEMP AND FWD CABIN TEMP MSG DISPLAYED.(<P>PERFORMED OPS CHECK OF SYSTEM IAW AMM 21-61-00. OPERATIONAL TEST CHECKS GOOD AT THIS TIME. CANNOT DUPLICATE MSG AT THIS TIME.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 68,678 hrs · 15,919 cycles

STATUS MSG RT ENG PRV.(<P>PERFORMED BITE ON AIR SUPPLY BITE MODULE PER AMM 36-23-01 NO FAULTS FOUND OK TO CONTINUE SERV. MSG ERASED.<BR /></P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (EXHAUST FAN) · airframe 68,632 hrs · 15,904 cycles

STATUS MSG AFT EQ EXAST FAN 2(<P>PERFORMED FIM 21-26- FAULT TREE 808 SYSTEM CHECK NORMAL AT THIS TIME&NBSP;</P>)

Part: ECU — MALFUNCTIONED (APU) · airframe 68,631 hrs · 15,903 cycles

APU INOP&NBSP; &NBSP;- (NOTE: PNEUMATIC PRESSURE OSCILATING WITH OR WITHOUT PACKS ON)(<P>APU DEFERRED IAW MEL 49-11-01A . R&AMP;R APU ECU OPS CHECK OK.</P>)

Part: RADAR — MALFUNCTIONED (WEATHER SYSTEM) · airframe 68,618 hrs · 15,899 cycles

WX RADAR PAINTS INTERMITTENT RETURNS IN CLEAR CONDITIONS AT ALL TILT POSITIONS.(<P>PERFORMED SYSTEM TEST OF THE WX RADAR IAW AMM 34-43-00/501. NO DISCREPANCIES NOTED AT THIS TIME.</P>)

Part: TEST SWITCH — INOPERATIVE (OXYGEN SYSTEM) · airframe 68,632 hrs · 15,904 cycles

RESET/TEST SWITCH NOT FUNCTIONING PROPERLY WHEN PRESSED ONCE. TEST OCCURS MASK WILL NOT TEST AGAIN AFTERWARDS UNLESS INFLATED(<P><SPAN>REPACKED / MASK OPS OK IN REF TO AMM 35-11-00</SPAN></P>)

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 68,475 hrs · 15,850 cycles

APU INOP, NO DUCT PRESSURE. ACCOMPLISHED OPERATIONAL CHECK OF THE APU IAW AMM 49-11-00. AND ECU BITE CHECK NO FAULTS FOUND AT THIS TIME. APU ARRIVED WORKING AND PERFORMED 3 GOOD STARTS WITH NO FAULT.

Part: PUMP — INOPERATIVE (FUEL SYSTEM) · airframe 68,454 hrs · 15,840 cycles

RT CENTER FUEL PUMP INOP. T/S AMM 28-26-00 FILLED CTR TANK WITH 2500 LBS TRANSFERRED OUT, L/R PUMP LIGHTS ON P5 NEVER / STAYED ON FOR MORE THAN 3 SECONDS. REMOVED AND REPLACED RT CENTER OVER RIDE PUMP PER AMM 28-22-05. OPS CHECK NORMAL.

Part: GENERATOR — MALFUNCTIONED (RIGHT) · airframe 68,374 hrs · 15,812 cycles

RIGHT GEN OFF AFTER START.RESET UNSUCCESSFUL(<P>RESET GEN FIELD IAW 24-11-00. OPS CHECK GOOD</P>)

Part: IDG — DEFECTIVE (RT ENGINE) · airframe 68,365 hrs · 15,808 cycles

RIGHT GEN OFF AFTER START. REMOVED AND REPLACED RIGHT IDG IAW AMM 24-11-01. OPS AND LEAKS CHECK GOOD.

Part: VALVE — INOPERATIVE (CABIN TEMP) · airframe 68,341 hrs · 15,798 cycles

AFT CABIN TEMP CONTROL INOP / ( CABIN COMPT TEMP CONTROL SYSTEM / ALL CARGO CONFIGURATION )(<P>PLACED ON MDDR 103188</P><P>FOUND ZONE TRIM VALVE IN-OP. DOES NOT ROTATE. EVEN WITH MANUAL KNOB.NEEDS A TRIM VALVE P/N 398786-5<BR /></P><P>REF LOGPAGE 0974275 - REMOVED AND REPLACED TRIM AIR MODULATING VALVE AND PERFORMED SYSTEM TEST PER AMM 21-61-07; MDDR 103188 CLEARED AT THIS TIME.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (SPAR VALVE) · airframe 68,297 hrs · 15,785 cycles

EICAS MSG L FUEL SPAR VAL AFTER ENGINE START ENGINE SHUT DOWN AFTER UNCOMMANDED EGT RISE(<P>PERFORMED OPERATIONAL CHECK OF ENGINE SHUT OFF VALVE, NORMAL ON VALVE ON, FLIGHT DECK INDICATION NORMAL IAW AMM 28-22-01. ENG IDLE PWR RUN CKS NORMAL 72-00-00<BR /></P>)

Part: WARNING LIGHT — ILLUMINATED · airframe 68,287 hrs · 15,782 cycles

WITH R ENG BLEED SELECTED ON AND PACK SELECTED ON IN ANY MODE, "R ENG BLEED AIR OFF" LIGHT ILLUMINATED AT ALL POWER SETTINGS, CONTRARY TO DDG.(<P>PER DDG 36-11-02 UNDER OPERATION LIGHT ILLUMINATING IS NORMAL.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (IDLE) · airframe 68,287 hrs · 15,782 cycles

IDLE DISAGREE MESSAGE DURING ENTIRE DESCENT PHASE. PERFORMED A BITE TASK L AND R PIMU IAW AMM 77-35-00. TESTED GOOD.

Part: ANTI-ICE VALVE — MALFUNCTIONED (RT ENGINE) · airframe 68,280 hrs · 15,779 cycles

RIGHT ENGINE ANTI-ICE EICAS MESSAGE. REMOVED AND REPLACED INLET TAI VALVE IAW AMM 30-21-03. COMPLETED UP TO 30-21-03-714-062. OPS CHECKED NORMAL.

Part: SEAL — FAILED (A/C PACK) · airframe 68,228 hrs · 15,761 cycles

PNEUMATIC COUPLING ABOVE THE LOW LIMIT VALVE HAS A LARGE AIR LEAK ON THE LEFT PACK. R & R THE DUCT SEALS IAW AMM 21-51-11, OPS CHECKED NORMAL.

Part: ACM — LEAKING (RIGHT) · airframe 68,228 hrs · 15,761 cycles

RIGHT ACM HAD AN AIR LEAK AT THE MATING SURFACE. R & R THE RT ACM IAW AMM 21-51-03. OPS CHECKED OK.

Part: SEAL — MISSING (NR 2 NACELLE) · airframe 68,228 hrs · 15,761 cycles

NR 2 ENGINE INBD SIDE OF PYLON PANEL 447AL WAS MISSING THE AFT PART OF THE SEAL. REMOVED AND REPLACED THE SEAL IAW AMM 51-40-02.

Part: QUICK DISCONNECT — INOPERATIVE (THRUST REVERSER) · airframe 68,231 hrs · 15,762 cycles

NR 2 ENGINE OTBD THRUST REVERSER COWLING OPEN QUICK DISCONNECT WAS INOPERATIVE. R & R THE QUICK DISCONNECT IAW AMM 72-00-53.

Part: QUICK DISCONNECT — INOPERATIVE (THRUST REVERSER) · airframe 68,231 hrs · 15,762 cycles

NR 1 ENGINE OTBD THRUST REVERSER COWL QUICK DISCONNECT WAS INOPERATIVE. R & R THE QUICK DISCONNECT IAW AMM 72-00-57.

Part: FEEDER CABLE — DETERIORATED (RT IDG) · airframe 68,231 hrs · 15,762 cycles

RIGHT IDG POWER FEEDERS COLD SHRINK SLEEVES DETERIORATED.(<P>R/R PWR FEEDER COLD SHRINK SLEEVES IN RIGHT IDG IAW AMM 20-10-14.</P>)

Part: FEEDER CABLE — DETERIORATED (LT IDG) · airframe 68,231 hrs · 15,762 cycles

LEFT IDG POWER FEEDERS COLD SHRINK SLEEVES WERE DETERIORATED. R & R LEFT ENGINE IDG POWER FEEDERS COLD SHRINK SLEEVES IAW AMM 20-10-14.</P>)

Part: STRUCTURE — PEELING (THRUST REVERSER) · airframe 68,228 hrs · 15,761 cycles

LEFT ENGINE LEFT THRUST REVERSER LOWER HALF WIRE MESH WAS PEELING. REPAIRED THE THRUST REVERSER LOWER HALVE WIRE MESH IAW EO 6778A019, PART 3, AND CMM 78-32-32.

Part: GAUGE — INOPERATIVE (REFUEL PANEL) · airframe 68,231 hrs · 15,762 cycles

CENTER TANK FUEL GAUGE, INTERNAL LIGHT WAS INOPERATIVE ON THE REFUELING PANEL.. R & R CENTER TANK FUAL GAUGE IAW AMM 28-41-08.

Part: WARNING MESSAGE — FALSE ACTIVATION (WX RADAR SYS) · airframe 68,214 hrs · 15,755 cycles

WXR SYS ADVISORY MESSAGE DISPLAYED, WILL NOT WORK INDEPENDENTLY. COMPLIED WITH EO 6734A156, LT AND RT WEATHER RADAR SYSTEMS OPERATED NORMAL IAW MM 34-43-00, MESSAGE CLEARED.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 68,211 hrs · 15,753 cycles

CA WXR FAIL DISPLAY STATUS MESSAGES WXR SYSTEM. PERFORMED SYSTEM TEST IAW AMM 34-43-00 FOUND NORMAL.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 68,212 hrs · 15,754 cycles

WEATHER RADAR SYSTEM ADVISORY MESSAGE DISPLAYED WILL NOT WORK INDEPENDENTLY. COMPLIED E/O 6734A156 LT AND RT WXR SYSTEM OPERATES NORMAL PER AMM 34-43-00, MESSAGE CLEARED.

Part: UNKNOWN — MALFUNCTIONED (COCKPIT) · airframe 68,206 hrs · 15,751 cycles

WEATHER RADAR INOP. PERFORMED SYSTEM TEST PER AMM TASK 34-43-00-735-033-002 CHKS OK TO CONTINUE SRVC.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 68,169 hrs · 15,739 cycles

LT IDG VALVE STATUS MSG. COULD NO DUPLICATE STATUS MSG AT THIS TIME. PERFORMED TEST IAW AMM 24-11-01.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 68,183 hrs · 15,743 cycles

AFT EQ EXH FAN2 STATUS MSG AFTER ENGINE START. PERFORM OPS CHECK. FAN OPERATES NRM PERFORMED MAINTENANCE ERASE PROCEDURE PER FIM 31-41-00/101. A/C IN NRM CONDITION AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 68,169 hrs · 15,739 cycles

APU FIRE LOOP 1 MESSAGE PRIOR TO START. APU FIRE DETECTION BITE PROCEDURE NO FAULTS NOTED. CANNOT DUPLICATE FAULT.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 68,169 hrs · 15,739 cycles

WX SYS STATUS MSG. PERFORMED ADJUST TEST ON WEATHER RADAR SYSTEM IAW AMM 34-43-00. BOTH RADAR SWITCHES NEED TO BE ON TO TEST OPS CHECK GOOD.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 68,168 hrs · 15,738 cycles

WXR SYSTEM STATUS MESSAGE. PERFORMED OPS CHECK IAW AMM 34-34-43-0 OPS CHECK NORMAL.

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 68,183 hrs · 15,743 cycles

APU INOP. APU OPS CONDITION NORMAL.

Part: LIGHT — INOPERATIVE (SWITCH) · airframe 68,183 hrs · 15,743 cycles

EMER DOOR SWITCH INDICATOR LIGHT INOP. R&R LIGHT IAW AMM 33-13-00, OPS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 68,158 hrs · 15,735 cycles

FO WRX FAIL. PERFORMED OPERATIONAL TEST OF WRX SYS. FOUND NO FAULTS AT THIS TIME IAW AMM 34-43-00, OPS CHECKED GOOD AT THIS TIME.

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 68,139 hrs · 15,727 cycles

WX RADAR FAILED. PERFORM OPS CHECK IAW AMM 34-43-00, OPS CHECK GOOD AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 68,120 hrs · 15,720 cycles

EICAS "RT ENG ANTI ICE" WHEN RT ENG ANTI ICE SELECTED OFF, ABOVE EICAS MESSAGE AND VALVE LIGHT ON. VALVE SEEMS STUCK ON. PERFORMED OPERATIONAL CHECK OF THE ENG THERMAL ANTI ICE VALVE ON THE NR 2 ENG. OPS CHECK NORMAL IAW AMM 30-21-00.

Part: ANTI-ICE VALVE — MALFUNCTIONED (RT ENGINE) · airframe 68,080 hrs · 15,707 cycles

ON APPROACH EICAS MESSAGE RT ENGINE ANTI-ICE AND RIGHT ENGINE ANTI-ICE VALVE LIGHT ILLUMINATED. REMOVED AND REPLACED RT ENGINE ANTI-ICE VALVE IAW AMM 30-21-03-004-001 OPS CHECK NORMAL.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 68,069 hrs · 15,702 cycles

WX RADAR STATUS MESSAGE ON LANDING. PERFORMED OPS TEST OF WEATHER RADAR SYSTEM, OPS CHECK GOOD IAW AMM 34-43-00.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 68,072 hrs · 15,703 cycles

WXR SYS STATUS MESSAGE. PERFORMED OPS CHECK IAW AMM 34-43-00, NO DEFECT NOTED AT THIS TIME.

Part: FIRE LOOP — DEFECTIVE (NR 2 ENGINE) · airframe 68,026 hrs · 15,687 cycles

STATUS MESSAGE RT ENG FIRE LP2. REMOVED AND REPLACED NR 2 ENGINE FIRE LOOP 2 IAW AMM 26-11-02, OPERATIONAL CHECK IS GOOD, NO FURTHER DEFECTS NOTED. FAULT CLEARED.

Part: CIRCUIT CARD — UNSECURE (FIRE WARNING) · airframe 68,020 hrs · 15,685 cycles

STATUS MESSAGES, RT ENG FIRE LP2. RERACKED ENG FIRE LOOP CARD REF AMM 20-41-01 AND PERFORMED GROUND TEST REF AMM 26-11-00, OPS CHECK GOOD NO IRREGULARITY NOTED AT THIS TIME.

Part: BLEED AIR SYS — MALFUNCTIONED (APU) · airframe 68,020 hrs · 15,685 cycles

APU WILL NOT PROVIDE AIR ON THE GND IN BWI, APU VALVE LIGHT INTERMITTENT. RESTARTED APU, BLEED AIR OK PER AMM 49-52-00.

Part: CIRCUIT CARD — UNSECURE (BLEED AIR SYS) · airframe 68,004 hrs · 15,680 cycles

RT BLEED DUCT LEAK EICAS MESSAGE ON PREFLIGHT WITH RIGHT PACK ON. RERACKED AIR SUPPLY CONTROL CARD M691 IAW AMM 36-11-12, NO FAULT OR MSG. FOUND LEAK AT ISO BYPASS CHECK VLV UPPER CLAMP AREA. TIGHTEN CLAMP AND LEAK CKD GOOD IAW AMM 36-11-05.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 67,989 hrs · 15,674 cycles

STATUS MSG "WXR SYS" WX RADAR FAIL MSG ENROUTE. PERFORMED OPS CHECK, MSG CLEARED, OPS NORMAL PER AMM 34-43-00.

Part: SENSOR — FAULTY (CABIN TEMP) · airframe 67,947 hrs · 15,658 cycles

FWD CABIN TEMP EICAS. REMOVED AND REPLACED FWD CABIN TEMP SENSOR IAW AMM 21-61-02. OPS CHECK GOOD AT THIS TIME.

Part: HOLDER — OUT OF POSITION (COCKPIT) · airframe 67,912 hrs · 15,645 cycles

CAPT NR 2 WINDOW IS FOGGING UP. ACCOMPLISHED FIM 30-41-00 FT 804 AND 802. NO FAULTS NOTED. WINDOW RESISTANCE IS 22.3 OMS (WITHIN LIMITS). VERIFIED AIR FLOW FROM WINDSHIELD DIFFUSERS PER AMM 25-22-00. SUSPECT AIRFLOW RESTRICTED BY CAPT'S TABLET HOLDER. REPOSITIONED HOLDER TO MIDDLE OF L2 WINDOW. L2 WINDOW HEAT OPS CHECKS GOOD PER AMM 30-41-60.

Part: BLEED AIR SYS — INOPERATIVE (APU) · airframe 67,912 hrs · 15,645 cycles

APU BLEED INOP. REMOVED AND REPLACED APU CONTROL UNIT IAW AMM 49-61-05, OPS CHECK FAILED PN OFF: 2117342-20, SN OFF: 129-1274. MDDR REMAINS OPEN.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 67,914 hrs · 15,646 cycles

WXR SYS STATUS MESSAGES. PERFORMED OPERATIONAL TEST IAW AMM 34-21-00, MESSAGES CLEARED.

Part: A/C PACK — MALFUNCTIONED (AC BAY) · airframe 67,914 hrs · 15,646 cycles

RT DUCT LEAK EICAS. ACCOMPLISHED QRH RT DUCT LEAK AND MESSAGES EXTINGUISHED 3 MIN LATER. RESET RIGHT PACK AND LIGHT EXTINGUISHED NO DEFECTS NOTES AT THIS TIME IAW AMM 36-00-00.

Part: TRANSCEIVER — MALFUNCTIONED (WEATHER RADAR) · airframe 67,893 hrs · 15,638 cycles

STATUS WXR SYS WX RADAR INOP. REMOVED AND REPLACED WXR TRANSCEIVER IAW AMM 34-43-01 OPS CHECK GOOD.

Part: EXCITER — FAILED (APU) · airframe 67,888 hrs · 15,636 cycles

APU RELIABILITY COLD START ACCOMPLISHED ON FLT LEG TPA- SCK SAT -54C FL 410 UNSUCCESSFUL AFTER 3 START ATTEMPTS. REMOVED AND REPLACED IGNITION EXCITER IAW AMM 49-41-03. PERFORMED OPS CHECK, OPS CHECK SATISFACTORY.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 67,881 hrs · 15,634 cycles

WXR SYS STATUS MSG. PERFORMED OPS CHECK OF WEATHER RADAR SYSTEM IAW AMM 34-43-00-715-026-002, NO DEFECTS NOTED AT THIS TIME.

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 67,875 hrs · 15,630 cycles

WEATHER RADAR FAILED. PERFORMED OPERATIONAL TEST OF WEATHER RADAR SYSTEM IAW MM 34-43-00-715-001-001. WEATHER RADAR OPERATES NORMAL AT THIS TIME.

Part: SENSOR — DIRTY (CABIN TEMP) · airframe 67,872 hrs · 15,628 cycles

BULK CARGO TEMP READOUT ERRATIC +8 TO -56 IN FLIGHT. CLEANED AFT ZONE TEMP SENSOR (BULK PIT) IAW AMM 21-61-09. OPS CHECK GOOD AND READING STABLE.

Part: MONITOR — INOPERATIVE (COCKPIT) · airframe 67,872 hrs · 15,628 cycles

ENGINE VIBE DISPLAY INOP. REMOVED AND INSTALLED A SERVICABLE ENGINE VIBE MONITOR UNIT IAW AMM 77-31-03. SELF TEST CHECK GOOD IAW AMM 77-31-00.

Part: MONITOR — INOPERATIVE (COCKPIT) · airframe 67,870 hrs · 15,627 cycles

ENGINE VIBE DISPLAY INOP. REMOVED AND INSTALLED ENGINE VIBE MONITOR UNIT IAW AMM 77-31-03, SELF TEST CHECK GOOD IAW AMM 77-31-00.

Part: ACTUATOR — MALFUNCTIONED (FUEL SYSTEM) · airframe 67,855 hrs · 15,623 cycles

NR 2 ENGINE SPAR VALVE LIGHT FAILED TO ILLUMINATE WHEN FUEL CONTROL WAS SELECTED TO RUN. REMOVED AND REPLACED RT ENG FUEL SHUTOFF VALVE ACTUATOR IAW AMM 28-22-11. PERFORMED OPS CHECK IAW AMM 28-22-11. GOOD, NO FAULTS AT THIS TIME.

Part: STARTER — MALFUNCTIONED (LT ENGINE) · airframe 67,832 hrs · 15,615 cycles

LT STARTER WOULD NOT CUT OUT. R&R LT ENGINE STARTER IAW AMM 80-11-01. OPS GOOD.

Part: FIRE LOOP — OPEN (LT ENGINE) · airframe 67,832 hrs · 15,615 cycles

"L ENG FIRE 1P 2" STATUS MSG. T/S IAW WDM 26-11-11. FOUND OPEN ON LOOP 2 DETECTOR T5681. ROBBED LOOP & INSTALLED IAW AMM 26-11-02. OPS CK GOOD PER AMM 26-11-02.

Part: ACTUATOR — FAULTY (FUEL SYSTEM) · airframe 67,823 hrs · 15,612 cycles

RT ENG SPAR VALVE DID NOT CYCLE DURING START. R&R RT ENGINE FUEL SHUTOFF VALVE ACTUATOR IAW AMM 28-22-11. OPS CHECK GOOD.

Part: INDICATION SYS — MALFUNCTIONED (COCKPIT) · airframe 67,827 hrs · 15,613 cycles

LOWER EICAS LEFT & RIGHT VIBE INDICATIONS BLANK. CYCLED VIBE CIRCUIT BREAKERS IAW AMM 20-60-01. PERFORMED ENGINE RUN IAW AMM 71-00-00. VIBE INDICATION OPS CHECK NORMAL. OK FOR SERVICE.

Part: ACTUATOR — FAULTY (FUEL SYSTEM) · airframe 67,823 hrs · 15,612 cycles

LEFT HAND SPAR VALVE LIGHT DID NOT COME ON FOR ENGINE START. REMOVED AND REPLACED ENGINE FUEL SHUTOFF VALVE ACTUATOR IAW AMM 28-22-11. OPS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 67,819 hrs · 15,610 cycles

DURING DESCENT AT 18000 FT GOT WXR FAIL STATUS MESSAGE ON F/O ND. PERFORMED OPS TEST OF WEATHER RADAR AS PER AMM 34-43-00, NO MESSAGES PRESENT. OPS CHECK GOOD.

Part: RELAY — FAILED (LT IDG) · airframe 67,802 hrs · 15,604 cycles

LT IDG VALVE. SERVICED BOTH IDG TO FULL IAW AMM 12-13-03. PERFORMED FIM 24-20-FT 802 REMOVED AND REPLACED RELAY IAW SWPM 20-81-11 K468. NO FAULTS NOTED AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 67,819 hrs · 15,610 cycles

WHEN CAPT SELECTS WXR OFF FROM EFIS CONTROL PANEL, FO RECEIVES WXR FAIL ON EHSI WHEN FO SELECT WXR OFF ON EFIS CONTROL PANEL, CAPT RECEIVES WXR FAIL ON EHSI. CARRIED OUT WEATHER RADAR OPERATIONAL TEST AS PER AMM 34-43-00 FOUND GOOD AT THIS TIME.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 67,819 hrs · 15,610 cycles

ON SHUT DOWN WXR SYSTEM STATUS MSG. NO STATUS MSG PRESENT, PERFORMED GROUND TEST NO DEFECTS AT THIS TIME AS PER AMM 34-43-00.

Part: LIGHT — INOPERATIVE (FUEL SYSTEM) · airframe 67,802 hrs · 15,604 cycles

RIGHT SPAR VALVE LIGHT DID NOT CYCLE WHILE STARTING THE RIGHT ENGINE. REPLACED RT SPAR VALVE LIGHT ASSY AS PER SWPM 20-84-18, OPS CHECK GOOD AT THIS TIME.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 67,790 hrs · 15,600 cycles

AFTER FIRST ENGINE START, RT AUX PITOT EICAS REMAINED ILLUMINATED, AFTER SECOND ENGINE START, RT AUX PITOT STILL REMAINED ILLUMIINATED. DEFERRED PER MEL 30-31-02 DMI 96358.

Part: PROBE — FAULTY (PITOT/STATIC SYS) · airframe 67,790 hrs · 15,600 cycles

AFTER FIRST ENGINE START RIGHT AUX PITOT EICAS REMAINS ILLUMINATED AFTER SECOND ENGINE START RIGHT AUX PITOT EICAS STILL REMAINED ILLUMINATED. REMOVED AND REPLACED PROBE ASSY PITOT STATIC RT SIDE LOWER IAW AMM 34-11-01. PERFORMED HIGH RANGE LEAK CHECK REF TASK 34-11-01-407-017 CA/C EQUIPPED WITH QUICK DISCONNECT FITTING, LEAK CHECK GOOD.

Part: CIRCUIT CARD — DEFECTIVE (OVERHEAT SYS) · airframe 67,790 hrs · 15,600 cycles

RIGHT DUCT LEAK LOOP INOP. REPLACED WW O/H CARD PER AMM 26-10-01 CHKS GOOD NO FAULTS.

Part: CONTROL VALVE — FAULTY (NR 2 ENGINE) · airframe 67,790 hrs · 15,600 cycles

STARTING NR 2 ENGINE IN CVG THE START VALVE DID NOT EXTINGUISH UNTIL AFTER START CUTOUT. REMOVED AND REPLACED START CONTROL VALVE. OPS CHECK GOOD REF AMM 80-11-02.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 67,790 hrs · 15,600 cycles

ON LANDING EICAS MESSAGE RIGHT AUX PITOT HEAT. PERFORMED OPS CHECK PER FIM 30-31 FAULT TREE 806 ALL TEST PASS OK TO CONTINUE SERVICE, 0 FAULTS.

Part: SWITCH — CONTAMINATED (FUEL SYSTEM) · airframe 67,778 hrs · 15,597 cycles

NR 2 ENGINE FUEL SPAR VALVE INOP. SUSPECT LOW SWITCH SPRING TENSION, UPON FURTHER INSPECTION FOUND THE SWITCH DIODE CONTACTS TO BE CONTAMINATED WITH DEBRIS. CLEANED IAW AMM 20-60-06. OPS CHK IAW AMM 28-22-00. CHK GOOD.

Part: ACTUATOR — MALFUNCTIONED (APU) · airframe 67,772 hrs · 15,594 cycles

UPON POST FLIGHT INSPECTION FOUND APU HAS NO DUCT PRESSURE. REMOVED AND REPLACED IGV ACTUATOR IAW AMM 49-52-02. OPS CHECKED GOOD.

Part: SWITCH — INOPERATIVE (FUEL SYSTEM) · airframe 67,717 hrs · 15,578 cycles

RIGHT FWD FUEL PUMP INOP. REMOVED AND REPLACED SWITCH 33-13-00 OPS CHECK NORMAL.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 67,685 hrs · 15,567 cycles

STATUS MSG "WX SYS". PERFORMED FIM 34-43 FAULT TREE 805. NO FAULTS FOUND. OPS CHECK GOOD.

Part: PANEL — DEFECTIVE (WEATHER RADAR) · airframe 67,683 hrs · 15,566 cycles

CAPT WXR INOP. CORRECTION ACTION EFIS PANEL REPLACED. PERFORMED WEATHER RADAR SYSTEM TEST REF 34-43-00. OPS CHECK OK AT THIS TIME.

Part: RELAY — FAULTY (APU) · airframe 67,681 hrs · 15,565 cycles

APU INOP. PFM FIM TASK 49-11, NO DEFECTS NOTED. REMOVED AND REPLACED RELAY K442. FAULTY RELAY PER SWPM 20-22. OPS CHECK OK IN ALL MODES.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 67,681 hrs · 15,565 cycles

CAPT WX RADAR INTERMITTENT WX FAIL. REMOVED AND REPLACED EFIS CONTROL PANEL PER 34-22-02. OPS CHECKED NORMAL.

Part: SLIDE — DISCHARGED (PAX DOOR)

BOS - FLT 592 - DURING OVERNIGHT CHECK, L1 DOOR SLIDE PRESSURE OUT OF GREEN BAND. REPLACED SLIDE, SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHT AT ARROW MARKER INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PROBE — DEFECTIVE (RT MAIN TANK)

BNA - FLT 1451 - DURING CRUISE, WITHIN 5 MINUTES OF NORMAL FUEL CHECK A FUEL ASYMMETRY BETWEEN RIGHT AND LEFT MAIN TANKS WAS NOTED. CREW DECLARED AN EMERGENCY AND DIVERTED TO BNA AND LANDED WITHOUT FURTHER INCIDENT. BNA MAINTENANCE DEFERRED RIGHT MAIN FUEL TANK QTY AND TOTALIZER PER MEL PROCEDURES. AIRCRAFT OVERNIGHTED DFW AND THE FUEL SYSTEM WAS TROUBLESHOT. MAINTENANCE FOUND RIGHT MAIN TANK FUEL PROBE TO BE THE FAULT CAUSE. REPLACED RIGHT MAIN TANK FUEL PROBES. SYSTEM OPERATED NORMAL WITH NO LEAKS. PLACARD REMOVED FROM SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (RT OVERWING)

ORD - DURING OVERNIGHT MAINTENANCE, RIGHT OVERWING UPPER EMERGENCY LIGHTS INOPERATIVE. REPLACED RIGHT OVERWING UPPER EMERGENCY LIGHT ASSEMBLIES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL STRIP — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BY FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)