N1487A

Part: CONTROL MODULE — FAULTED (SPOILERS) · airframe 96,870 hrs · 21,055 cycles

SPOILER EICAS MESSAGE. PERFORMED FIM 27-09 FT 803 & FIM 27-09 FT 808, FOUND PCA FAULTING ON SCM #3 MSG. R & R #4 SPOILER PCA IAW AMM 27-61-02. DURING OPS CHECK FOUND #4 PCA STUTTERING WHILE DEPLOYING, SUSPECT BFS PCA. R & R #4 SPOILER PCA IAW AMM 27-61-02, NO HELP, MSG REMAINS. DURING DEPLOYMENT OF SPOILERS, FOUND #4 & #9, SUSPECT BAD SCM. R & R #3 SCM IAW AMM 27-09-00, OPS OK, NO MSG NOTED. PERFORMED SPOILERS OPS TEST IAW AMM 27-61-00, OPS CHECK GOOD, NO EICAS MSG NOTED, NO SPOILER DISCREET LIGHT NOTED & NO MSG FOUND ON ALL SCM'S. A/C OK FOR SVC. VERIFIED PART PER IPC 27-01-01-01.

Part: MODULE — FAULTED (WARNING SYS) · airframe 96,867 hrs · 21,054 cycles

AIR TURN BACK FOR SPOILER ADVISORY MESSAGE. UPON ARRIVAL, PERFORMED MULTIPLE OPS TEST IAW AMM 27-61-00, COULD NOT DUPLICATE. PERF FIM 31-51 FT 809. R/R PCA TAKEOFF CONFIG WARNING MODULE (M620) IAW AMM 31-51-04, BIT ALL SCM'S WITH NO FAULTS PRESENT IN PREVIOUS FAULTS. PERF MCDP TEST IAW FIM 22-04FT 810, NO FAULTS NOTED. PERF OPS TEST OF SPOILERS IAW AMM 27-61-00, OPS CHECK GOOD. NO ADV PER ENGINEERING. ALL TEST COMPLETED. PART EFFECTIVE PER IPC.

Part: LIGHT — UNKNOWN (CABIN) · airframe 95,804 hrs · 20,672 cycles

OVERHEAD EMERGENCY LIGHTS 1 PAX PANEL BACKLIGHT INOP,(<P>PERFORMED OPS CHECK ON OVERHEAD BACKLIGHTING IAW AMM 33-13-00. OPS CHECK GOOD AT THIS TIME.</P>)

Part: TAT PROBE — FAULTED · airframe 95,797 hrs · 20,670 cycles

EICAS MESSAG "TAT PROBE" FOLOWED BY 'AUTOPILOT DISCONNEC' LNAV AND VNAV BECAME INOP(<P>PERFORMED T/S PER FIM 30-33 FT805, SUSPECTING TAT, RELAY K514 AND RELAY K411 TO BE FAULTINGREMOVED AND REPLACED TAT PROBE IAW AMM 34-12-02. REMOVED AND REPLACED RELAYS K 411 AND K514. OPS CHECKED GOODIAW AMM 34-12-02.&NBSP;</P>)

Part: ELT — UNKNOWN (UNKNOWN) · airframe 95,566 hrs · 20,590 cycles

CHORD ON ELT NEAR ENTRANCE DOOR UNRAVELED AND CARDBOARD SPLIT OPEN. SCOTCH TAPE HOLDING CARDBOARD TOGETHER(<P>REMOVED PORTABLE ELT FROM GALLEY AND INSTALLED SERVICEABLE ELT PER AMM 25-63-03. NO FURTHER DEFECTS NOTED.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,308 hrs · 20,502 cycles

RH WING PANEL 651VB BROKEN AND PORTION MISSING FROM AIRCRAFT(<P>TIME-LIMITED REPAIR OF PANEL 651VB INSTALLED IAW EA 6757A0030 REV 0 DVI OF REPAIR AND SURROUNDING AREAS REQUIRED EVERY 1 F/C. REPLACE SPEED TAPE AS REQUIRED. REINSPECT TRANSFERRED TO MDDR 196842</P>)

Part: PCA — UNKNOWN (UNKNOWN) · airframe 95,064 hrs · 20,431 cycles

ON TAKEOFF OUT OF CVG AND MHT, THERE WAS A VIBRATION THAT FELT RAPID BUT SUBTLE PTCH OSCILLATION, ALL ENGINE GUAGES WERE NORMAL.(<P>R/R LH ELEVATOR CENTER PCA IAW B767 AMM 27-31-05. OPS CHECK &AMP; LEAK CHECK GOOD AT THIS TIME. MCC NOTIFIED</P>)

Part: FLASHLIGHT ASSY — NONE · airframe 93,530 hrs · 19,918 cycles

GALLEY FLASH LIGHT INOP(<P>R/R FLASHLIGHT IAW AMM 25-64-00. R/R FLASHLIGHT HOLDER/BRACKET IAW SRM 51-40-02. OPS CHECK NORMAL. DMI 181380 CLOSED</P>)

Part: NONE — NONE · airframe 93,502 hrs · 19,909 cycles

LOWER FUSELAGE, EXTERNAL SKIN WITH LIGHTNING STRIKE BETWEEN STA 172.5 AT 3.700" ABOVE STG 21RH(<P>LOWER FUSELAGE, EXTERNAL SKIN&NBSP; BETWEEN STA 172.5 AT 3.700" ABOVE STG 21RH, LIGHTNING STRIKE WAS REPAIRED IAW SRM 53-00-01-2R-8 REPAIR 8 SECTION II REV. 121 15/DEC/22</P>)

Part: NONE — NONE · airframe 93,502 hrs · 19,909 cycles

LOWER FUSELAGE, EXTERNAL SKIN WITH LIGHTNING STRIKE BETWEEN STA 157 AND 164.7 AT STG 21RH (3EA)(<P>LOWER FUSELAGE, EXTERNAL SKIN BETWEEN STA 157 AND 164.7 AT STG 21RH, THREE LIGHTNING STRIKES WERE REPAIRED IAW SRM 53-00-01-2R-8 REPAIR 8</P>)

Part: NONE — NONE · airframe 93,502 hrs · 19,909 cycles

DELAMINATION ON INTERNAL / EXTERNAL AREA OF LH ACCESS PANELS FROM VERTICAL STABILIZER BETWEEN FSS 118.75 TO FSS 246.653 AND FRONT SPAR TO AUXILIARY SPAR.(<P>REPAIRED THE AFFECTED AREA PER SRM 55-30-01-2R-1 FIG. 201 PAGE 1-7 AND SRM 51-70-10-2R-4 FIG. 201 SHEET 2.</P>)

Part: NONE — NONE · airframe 93,502 hrs · 19,909 cycles

LOWER FUSELAGE, EXTERNAL SKIN WITH LIGHTNING STRIKE ON STA 287 AT 9.5" ABOVE STG 21RH.(<P>LOWER FULSELAGE, EXTERNAL SKIN ON STA 287 AT 9.5" ABOVE STG 21RH. LIGHTNING STRIKE WAS REPAIRED IAW SRM 53-00-01-2R-8 REPAIR 8 SECTION II REV. 121 15/DEC/22</P>)

Part: WIRE — NONE · airframe 93,502 hrs · 19,909 cycles

AFT CARGO, DIAGONAL WALL RH SIDE, UNDER PANEL, SEVERAL ELECTRICAL WIRES BROKEN(<P>ELECTRICAL WIRES WERE REPLACED PER SWPM 20-10-13. OPS CHECK GOOD</P>)

Part: NONE — NONE · airframe 93,502 hrs · 19,909 cycles

DELAMINATION ON EXTERNAL AREA OF RH ACCESS PANELS FROM VERTICAL STABILIZER BETWEEN FSS 118.75 TO FSS 246.653 AND FRONT SPAR TO AUXILIARY SPAR.(<P>REPAIRED THE AFFECTED AREA PER SRM 55-30-01-2R-1 FIG. 201 SHEET 1 AND SRM 51-70-10-2R-4 FIG. 201 SHEET 1.</P>)

Part: NONE — NONE · airframe 93,502 hrs · 19,909 cycles

LOWER HALF OF FUSELAGE, EXTERNAL SKIN WITH LIGHTNING STRIKE EVIDENCE ON STA 522 BETWEEN STG 19 AND 20RH.(<P>LOWER HALF OF FUSELAGE, EXTERNAL SKIN&NBSP; ON STA 522 BETWEEN STG 19 AND 20RH WITH LIGHTNING STRIKE WAS REPAIRED IAW SRM 53-00-01-2R-8 REPAIR 8 SECTION II REV.121 15/DEC/22</P>)

Part: BOTTLE — LEAKING · airframe 92,104 hrs · 19,464 cycles

SUSPECT PAX O2 BOTTLE LEAKING(REMOVED AND REPLACED PAX O2 BOTTLE AMM 12-15-08, NO LEAKS NOTED)

Part: NONE — NONE · airframe 91,775 hrs

#2 OXYGEN BOTTLE PRESSURE REGULATOR LEAKING(<P><SPAN>REMOVED AND REPLACED #2 OXYGEN PRESSURE REGULATOR IAW AMM 35-11-03. OPS AND LEAK CHECK GOOD AT THIS TIME.</SPAN></P>)

Part: NONE — NONE

O2 BOTTLE NEAR L1 DOOR MISSING GLASS OVER PRESSURE GUAGE.(<P>PLACED ITEM ON DMI 158497 IAW MEL 35-31-01.</P> / <P>LP 1617077 ITEM 5 - REMOVED AND REPLACED L1 PORTABLE OXY BOTTLE IAW B767 AMM 35-31-01.</P>)

Part: MASK — NONE · airframe 91,044 hrs

FIRST OFFICER MASK IS NOT FLOWING O2 PROPERLY. EXTREMELY HARD TO BREATH THROUGH NEEDS TO BE REPLACED.(<P><SPAN>R&AMP;R FO O2 MASK IAW 35-11-51</SPAN></P>)

Part: DIODE — NONE

R ENG OIL PRESS LIGHT INOP(<P>TRANSFERRED TO MDDR 156702 PER MEL 79-33-01-01 CAT C. DUE DATE 23NOV21</P> / <P>14NOV21 - LOG PAGE 1373448 - ITEM #4 - SCK - : REMOVED AND REPLACED R ENGINE OIL PRESSURE ANNUNCIATOR DIODE/FUSE CARD REF B767 AMM 33-16-02-962-007. OPS CHECK NORMAL AT THIS TIME. MCC ADVISED. THIS CLEARS MDDR #156702. PLACARDS REMOVED.</P>)

Part: NONE — NONE

STATUS MSG L ENG EEC C1(<P>TRANSFERRED TO MDDR 156734 IAW DDG 73-21-01-05 CAT A DUE DATE 20DEC21</P>)

Part: NONE — NONE · airframe 90,908 hrs · 19,065 cycles

L ENG BLEED EICAS CAME ON 5 TIMES ON/OFF APPROACH TO LANDING(<P>PERFORMED BITE CHECK OF AIR SUPPLY. NO FAULTS AT THIS TIME IAW AMM 36-23-00.</P>)

Part: FIRE LOOP — MALFUNCTIONED (LT ENGINE) · 19,063 cycles

L ENG FIRE LP 1 INTERMITTENTLY APPEARING ON STATUS PAGE. PERFORMED FIM 26-11 P/T 804 UP TO BLOCK 52. ALL RESISTANCE CHECKS WITHIN LIMITS PER TABLE A. UPON DOING THE RESISTANCE CHECKS FOUND LOOSE TERMINAL END ON LOWER & AFT FIRE DETECTOR TERMINAL TS45. RESECURED IAW 26-11-02 &AMP; WDM 26-11-11. OPS CHECK GOOD. PERF ENG RUN IAW AMM 71-00-00. NO MSG NOTED. PERF DVI & WIRE SHAKE DOWN OF LH ENG FIRE LP1 IAW AMM 20-60-03. NO DEFECTS NOTED AT THIS TIME. PERF ENGINE RUN IAW AMM 71-00-00. NO STATUS MSG DISPLAYED AT THIS TIME.

Part: NONE — NONE · airframe 90,761 hrs · 19,021 cycles

L ENG EEC C1 STATUS(<P>PERFORMED UP TO STEP 4 OF FIM 73-21 FAULT TREE 885. UNABLE TO PERFORM REST OF THE FIM. TRANSFERRED TO MDDR # 155587 PER DDG MEL # 73-21-01-05. DUE 24NOV21, CAT "A". MCC NOTIFIED.</P> / <P>L/P 1422396: C/W FIM 71-01 F/T 810, PIMU BITE WITH NO FAULTS FOUND PER SHEET 4 BLOCK 27. THIS CLEARS MDDR 155587.</P> / <P>LOG PAGE 1373429: R/R STATOR GENERATOR IAW AMM 71-00-00. TEST NO. 3 IDLE TEST SUCCESSFUL. NO ACTIVE MSGS, NO FAULTS ON PIMU.</P>)

Part: NONE — NONE

LEFT WEATHER RADAR FAILED WXR FAIL MSG ON EICAS(<P>PERFORMED WEATHER RADAR SYSTEM OPERATIONAL TEST IAW B767 AMM 34-43-00 715-026-002. OPS CKS NORMAL AT THIS TIME. COULD NOT DUPLICATE ON GROUND.</P>)

Part: FIRE DETECTOR — INTERMITTENT (LT ENGINE) · 18,994 cycles

INTERMITTENT LENG FIRE LOOP 1 STATUS MSG. REMOVED AND REPLACED L/H ENGINE UPPER AFT FIRE LOOP DETECTOR ELEMENT IAW AMM 26-11-02. OPS CHECK GOOD AT THIS TIME,

Part: NONE — NONE · airframe 90,661 hrs · 18,993 cycles

STATUS MESSAGE "L ENG EEC C1"(<P>MSG CLEARED IAW AMM 72-00-00. OPS CKD IAW 72-10-00.</P>)

Part: NONE — NONE · airframe 90,614 hrs · 18,978 cycles

AFT CABIN TEMP ADVISORY MSG DISPLAYED IN FLIGHT.(<P>PERFORMED BITE ON ZONE TEMP CONTROLLER REF FIM 21-61 FT 803, NO FAULTS PRESENT AT THIS TIME.</P>)

Part: CONTROLLER — FAULT MESSAGE

AFT CABIN TEMP CAUTION MSG IN FLIGHT @FL390 CABIN ALT 7000 CABIN DIFFERENTIAL PRESS 8.4 PSI. T/S IAW FIM 21-61 FAULT TREE 803 AND AMM 21-61-03. REMOVED AND REPLACED ZONE TEMP CONTROLLER UNIT IAW AMM 21-61-03. OPS TEST GOOD. STATUS MSG CLEARED.

Part: CONTROLLER — FALSE INDICATION

DURING CRUISE, AFT CABIN TEMP MESSAGE PERFORMED BITE CHECK OF ZONE TEMP CONTROLLER IAW FIM 21-61 FT 803. NO DEFECTS NOTED. A/C OK FOR SERVICE.

Part: CONTROL PANEL — WARNING MESSAGE · airframe 90,598 hrs · 18,973 cycles

"AFT CABIN TEMP" EICAS MESSAGE OBSERVED IN FLIGHT.(<P>PERF BITE OF ZONE CONTROL PANEL IAW AMM 21-61-03. NO CURRENT FAULTS NOTED. REF OPS CHECK OF AFT CABIN TEMP, OPS NORMAL AT THIS TIME.</P>)

Part: CONTROLLER — ERRATIC · 18,973 cycles

AFT CABIN TEMP EICAS MSG ABOUT 3 HOURS IN CRUISE. RAN QRH TEMP IN ZONE DROPPED A COUPLE OF DEGREES TO 21C. PERFORMED BITE TEST OF THE ZONE TEMP CONTROLLER IAW B767AMM 21-61-00. OPS CKS GOOD. COULD NOT DUPLICATE.

Part: RADAR — INTERMITTENT

RADAR WILL NOT MAINTAIN TILT/STABLE IN AUTO MODE.(<P>TRANSFERED TO MDDR# 153823 MEL 34-43-01-02 CAT C.</P> / <P>20 SEP 21 - LP 1287025 ITEM 8 - AFW - OPS CHECK PER AMM 34-43-00-715-002. NO FAULT FOUND COULD NOT DUPLICATE ON GROUND. THIS CLOSED DMI 153823. PLACARDS REMOVED.</P>)

Part: AUTOTHROTTLE SYS — FALSE INDICATION · airframe 90,520 hrs

AUTO THROTTLE DISCONNECT EICAS MSG DURING CLIMB 10,000 FT FROM INTERMEDIATE LEVEL.OFF AT 290 AFTER PRESSING ALT BUTTON TO CONTINUE CLIMB VNAV TO 350.SELECTED FL CH AND AUTO THROTTLE REENGAGED. ERROR DID NOT REPEAT(<P>PERFORMED AUTO FLIGHT FLIGHT FAULT BITE PROCEDURE IAW FIM 22-02 FT 801. NO FLT FAULTS INDICATED.</P>)

Part: DOOR SEAL — CORRODED · corrosion level 2 · airframe 9,051,034 hrs · 18,945 cycles

BULK CARGO DOOR CUT-OUT, UPPER SEAL HAS SEVERAL AREAS OF CORROSION.(<P>UPON FURTHER EVAL CORROSION FOUND TO BE OUT OF LIMITS IAW B767 53-00-15-1A-1. REMOVED AND REPLACED BULK CARGO LOWER SILL FLOOR PLATE IAW B767 DWG 146T8211 REV. B,R, B767 SRM 51-40-02</P>)

Part: SKIN — CRACKED · airframe 90,510 hrs · 18,945 cycles

WHILE PERFORMING HFEC INSP ON PART 1-2 OF ORIGINATING TASK CARD. VISUALLY NOTED A CRACK AND CONFIRMED WITH HFEC ON THE RH WING LOWER SURFACE STR L-9.5, 22ND FASTENER FROM MOST O/B FASTENER ON STR AT 12 O'CLOCK POSITION LOOKING UP/FWD, APPROX 1/8" LONG.(<P>REPAIRED CRACK AT RH WING LOWER SURFACE STR L-9.5 HOLE #45 AND REMOVED AND REPLACED RH WING STR L-9.5 IAW B767 FAS EA 21070&NBSP; REV:IR, EO:6757A139PT4, DWG: 767-9420, SRM 51-40-02, 51-40-05, 51-20-01, AMM 51-24-22, 28-11-00</P>)

Part: SKIN — CRACKED · airframe 90,510 hrs · 18,945 cycles

CRACK NOTED ON RH WING LOWER SURFACE STR L-6.5 MOST I/B FASTENER AT 6 O'CLOCK POSITION LOOKING UP/FWD. APPROX 1/4" LONG.(<P>REPAIRED CRACK AT RH WING LOWER SURFACE STR L-6.5 MOST I/B FASTENER HOLE BTW WSTA 990.2 AND 1046.2 IAW B767 FAS EA 21069-P1 REV:IR, SRM 51-10-02, 51-40-02, 51-40-05, 51-20-01, AMM 51-24-22, 28-11-00, DWG:767-9470, AND EO: 6757A140 PT 4.</P>)

Part: SENSOR — FAILED (CABIN TEMP)

AFT CABIN TEMP EICAS MESSAGE.(<P>ITEM TRANSFERRED TO DMI 152434 PER MEL 21-61-01-02. CAT C. DUE 03SEP21. PERFORMED ZONE TEMP BITE IAW FIM 21-61-00. FOUND AFT ZONE SENSOR BAD. TJ @ 1704Z.</P> / <P>24AUG, SCK MX, LP 1386751, ITEM M2: CLEANED TEMP SENSOR IAW B767 AMM 21-65-04. AFT ZONE TEMP CONTROL OPS CHECK GOOD. THIS CLEARED DMI 152434. T/I: GTC @ 0408Z.</P>)

Part: CONTROLLER — FAULTED (AFT CABIN TEMP) · 18,944 cycles

AFT CABIN TEMP EICAS DURING CRUISE. FOLLOWED NON NORMAL CK LIST(<P>PERF BITE ON ZONE TEMP CONTROLLER.IAW AMM 21-61-00. RESET CONTROLLER. MSG AND FAULT CLEARED. OPS CK NORMAL.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT PRV)

STATUS MSG R ENG PRV(<P>C/W FIM 36-10- FAULT TREE 847, OPS CHECK NORMAL.</P>)

Part: TRANSCEIVER — FAULTED (WX RADAR)

R "WX SYS FAIL" AND "WXR SYS" STATUS MSG.(<P>TRANSFERRED TO DMI 152042 IAW MEL 34-43-01, CAT D.</P> / <P>REMOVED AND REPLACED RIGHT WEATHER RADAR TRANSCEIVER IAW B767 AMM 34-43-01-404-005. PERFORMED OPERATIONAL TEST IAW B767 AMM 34-43-00-715-026-002. OPS CHECK GOOD. NO DEFECTS NOTED. THIS CLEARS DMI 152042.</P>)

Part: APU — FAULTED · airframe 5,549 hrs

AFTER LANDING APU WOULD NOT START (3 ATTEMPTS MADE)(<P>APU GRND STARTED BY MAINT W/ NO FAULTS NOTED. BITE AND SELF TEST PER AMM 49-61-05. NO FAULTS NOTED.</P>)

Part: APU — UNKNOWN · airframe 90,432 hrs

APU FAILED TO START ON GND(<P>PERFORMED BITE AND SELF TEST OF ECU IAW AMM 49-61-05.&NBSP; NO FAULTS FOUND.&NBSP; APU START 1ST ATTEMPT.&NBSP; OPS CHECK NORMAL.</P>)

Part: CHARGER — FAILED (APU BATTERY)

APU FAILED TO START AFTER LANDING 3 ATTEMPTS(<P>T/S PER FIM 49-11 F/T 987, FOUND FAULT CODE 34 ON ALL LEGS. FOUND APU BATTERY CHARGER TO BE AT FAULT. REMOVED AND REPLACED APU BATTERY CHARGER IAW AMM 24-31-05. OPS CHECKS GOOD.</P>)

Part: WARNING LIGHT — FALSE ACTIVATION (APU)

APU FAULT EICAS MSG DISPLAYED DURING ATTEMPTED APU START AFTER LANDING, QRH COMPLETED. FAULT LIGHT DOES NOT REMAIN DISPLAYED WITH APU SWITCH OFF.(<P><SPAN>PERFORMED BITE TEST NO FAULTS NOTED PER FIM 49-11 FT 987, OPS CHECK GOOD AT THIS TIME</SPAN></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENGINE)

R ENG PRV STATUS MSG DISPLAY AFTER ENGINE START(<P>PERFORMED FIM 36-20-00/101 AIR SUPPLY BITE. NO FAULTS NOTED AT THIS TIME. MSG CLEARED. OK FOR SERVICE.</P>)

Part: ECU — DIRTY (APU) · airframe 90,384 hrs

APU FAULT ON TAXI IN(<P><SPAN>PERFORMED APU BITE IAW AMM 49-61-05. CLEARED ECU. APU START NORMAL ON 1ST ATTEMPT. OK FOR SERVICE</SPAN></P>)

Part: OIL SYSTEM — LOW (APU)

APU FAULT AFTER LANDING(<P>PERFORMED ECU BITE IAW FIM TASK 49-11 FT 987. START ABORTED FAULT, FOUND APU OIL LOW, SERVICED APU OIL TO FULL IAW AMM 12-13-04, PERFORMED OPS CHECK OF APU IAW AMM 49-11-00, OPS CHECK GOOD</P>)

Part: LINE — LEAKING (HYD SYSTEM) · airframe 90,280 hrs

FOUND PUDDLE OF OIL IN RIGHT ENGINE COWL AND OIL DRIPPING FROM ENGINE(<P>FOUND&NBSP; ENGINE HYDRALIC LEAK,TIGHT AND TORQUE HYD LINE FROM PYLON TO ENG IAW AMM 71-00-00.&NBSP; SERVICED R HYD IAW AMM 12-00-00&NBSP; NO LEAK AT THIS TIME.&NBSP; A/C OK TO RELEASE</P>)

Part: ENGINE — OIL CONSUMPTION (NR 2) · 18,868 cycles

REF MDDR 150225 ETOPS RESTRICTED FOR OIL CONSUMPTION(<P>REPLACED #2 ENG SEE LP 1188465 ITEM 12. AC RETURNED TO ETOPS 180 STATUS</P>)

Part: A/C PACK — CONTAMINATED

ALL DURING PREFLIGHT AND TAKE OFF AND CLIMB THRU FL350 AND DESCEND THRU FL 280 AND BELOW A STRONG OILY SMELL WAS PREDOMINANT INSIDE FLT DECK, SMELL DECREASED DURING CRUISE(<P>PERFORMED INSPECTION IAW 05-51-56. CONTAMINATION REMOVED FROM PACK AND PRECOOLER..</P> / <P>&NBSP;</P>)

Part: ECS — CONTAMINATED · airframe 90,269 hrs · 18,862 cycles

AT ROTATION DURING TAKEOFF A LIGHT HAZE OR SMOKE WAS OBSERVED AROUND THE FIRST OFFICER POSITION ALONG WITH A SOUR SMELL. THE HAZE DISSIPATED IMMEDIATELY AND THE SMELL SUBSIDED AFTER A FEW MINUTES(<P>PERFORMED INSPECTION IAW 05-51-56 -202-001 CONTAMINATION REMOVED FROM AIR CONDITIONING AND PNEUMATIC SYTEM . OPS CHECKS OK, ACFT OK TO CONTINUE&NBSP;</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (APU BATTERY)

UPON MX ARRIVAL TO FD, FOUND APU BAT CHG STATUS MSG(<P><SPAN>APU TURNED OFF BY INBOUND CREW. RESTARTED APU + FOLLOWED FAULT TREE 49-11-FT-958. APU OPS NORMAL, MSG CLEARED.</SPAN></P>)

Part: APU — FAULTED · airframe 90,178 hrs · 18,830 cycles

APU FAULT ON START UP RPM WOULD NOT EXCEED 27%(<P>PERF APU BITE IAW FIM 49-11 FT 986 NO FAULTS NOTED PERF INSP OF APU OIL FOUND APU OIL TO BE OVER SERVICED. DRAINED APU OIL IAW AMM 12-13-04. RAN APU SEVERAL TIMES IAW AMM 49-11-00 NO FURTHER DEFECTS NOTED AT THIS TIME.&NBSP;</P>)

Part: ECS — CONTAMINATED · airframe 89,888 hrs · 18,742 cycles

OCCASIONAL ELECTRICAL SMOKE SMELL ON DESCENT(<P>PERFORMED INSPECTION OF EQUIPMENT COOLING SYSTEM IAW AMM 21-58-00. NO DEFECTS NOTED. PERFORMED VISUAL INSPECTION OF WATER SPRAY NOZZLES IAW AMM 21-53-05. NO DEFECTS NOTED. AC OK FOR CONTINUED SERVICE. RAN BOTH PACKS AT FULL HOT FOR 30 MINUTES, NO FUMES NOTED. REMOVED CONTAMINATION FROM AIR CONDITIONING SYSTEM IAW AMM 21-00-00-21. PERFORMED EWIS INSPECTION IN MEC IAW AMM 05-51-56 AND 20-60-04. NO DEFECTS NOTED.</P>)

Part: COUPLER — DAMAGED (HF SYSTEM) · airframe 89,888 hrs · 18,742 cycles

LOST SATCOM ON FLIGHT. UNABLE TO RESET THROUGH CENTER CDU. WITH NO WORKING HF'S HAD TO PULL CB'S TO RESET SYSTEM, SATCOM WORKING INTERMITTENT ON PLANE.(<P>REMOVED AND REPLACED&NBSP;LEFT AND RIGHT HF COUPLERS. PERFORMED OPS CHECK OF SATCOM IAW AMM 23-25-00. OPS CHECK GOOD. NO DEFECTS NOTED. PER ENGINERRING CONDUCTED L &AMP; R SATCOM VOICE CALLS. OPS CHECK GOOD.</P><P>OFF PART: PN 964-0453-001, SN 03249</P>)

Part: OXYGEN MASK — FAULTED (COCKPIT OXYGEN) · airframe 89,842 hrs · 18,724 cycles

CAPT O2 MASK NOT WORKING PROPERLY, EXTREMELY HARD TO BREATHE THROUGH, NEEDS TO BE REPLACED.(<P>SWAPPED O2 MASK WITH LEFT OBSERVERS. LEFT OBS SEAT UNUSEABLE. PART # INSTALLED CAPT POSITION NOW MC10-08-109 S/N 19290. CURRENT OBS MASK P/N MC10-08-109 S/N 73962.</P><P>ITEM #2: TRANSFER TO MDDR 146898, MEL 35-11-03, CAT C, DUE 23MAY21.</P><P>LP 1478064 ITEM #4: REMOVED AND REPLACED L OBSV OXY MASK PER AMM 35-11-51, OPS CHECK GOOD, THIS CLEARS DMI 146898.</P><P><BR /></P>)

Part: INDICATOR — MALFUNCTIONED (CABIN PRESSURE) · airframe 89,765 hrs

CABIN RATE INDICATOR NEEDLE VIBRATES AND INDICATES CLIMB IN ALL PHASES OF FLIGHT.ONLY STABLE DURING DESCENT.(<P>TRANSFERRED TO MDDR 146207,CAT C DUE 11MAY21. PER DDG 21-33-01A. PLACARD INSTALLED MCC NOTIFIED. P/N S231N210-14 ON ORDER WITH MCC. </P><P>2MAY2021 - 1465393 ITEM #6 - REMOVED AND REPLACED CABIN PRESSURE INDICATOR PANEL IAW AMM 21-33-01. OPS CHECK GOOD. THIS CLEARS MDDR 146207</P>)

Part: LENS — DETACHED (INDICATOR LIGHT) · airframe 89,765 hrs

R OIL PRESSURE INDICATOR LIGHT FELL OFF(<P>TRANSFERRED TO MDDR 146103 PER MEL 79-33-01-01 CAT C DUE 9 MAY 21 </P><P>2MAY2021 - 1465393 ITEM #4 - REMOVED AND REPLACED RT ENG OIL PRESS LIGHT LENS CAP ASSY PER SWPM 20-84-14 OPS CHECK PER AMM 33-16-00 OIL FOR SVC CLEAR DMI 146103.</P>)

Part: CONNECTOR — DAMAGED (RT PACK TEMP) · airframe 89,726 hrs · 18,688 cycles

FOUND CONNECTOR D10140 ON TS5135 COMP OUTLET TEMP SENSOR 2 BAD BACKSHELL. RH PACK TEMP CONTROL STANDBY MODE SYSTEM INOP TRANSFERRED TO MDDR 145718 IAW DDG 21-51-03-02. CAT C DUE 02MAY21. CONNECTOR D10140 ON TS5135 CAPPED AND STOWED. EH 1346Z. REMOVED AND REPLACED CONNECTOR D10140 ON RIGHT PACK IAW B767 SWPM 20-60-03 TABLE 6. OPS CHECK RIGHT PACK ON STANDBY MODE, OPS CHECKS OK AT THIS TIME. THIS CLEARS MDDR 145718.

Part: CIRCUIT BREAKER — TRIPPED (FUEL PUMP) · airframe 89,696 hrs · 18,679 cycles

R AFT FUEL PUMP CIRCUIT BRK(<P>PERF R AFT FUEL PUMP TEST PER AMM 28-22-00. VERIFIED GFI RIGHT NOT POPPED & INSPECTED RIGHT AFT FUEL PUMP FOR ANY LEAKS, FOUND NONE. RESET C/B R AFT FUEL PUMP & OPS CHECK GOOD PER GMM 3.8.1, PER FIM 28022 FT 820, COULD NOT FIND ANY DISCREPANCIES.</P>)

Part: PURGE CAN — INOPERATIVE (RT AFT FUEL) · airframe 89,700 hrs · 18,680 cycles

R AFT FUEL PUMP INOP(<P>TRANSFERRED TO MDDR 145638 IAW MEL 28-22-01, CAT C.&NBSP;<BR /></P><P>CVG MX, 21APR, LP 1145778: REMOVED &AMP; REPLACED AFT RIGHT FWD PUMP IAW AMM 28-22-03, OPS CHECK GOOD. THIS CLEARS DMI 145638. GTC 2244Z</P>)

Part: SEAL DEPRESSOR — DAMAGED (CARGO DOOR) · airframe 89,617 hrs · 18,650 cycles

MAIN CARGO DOOR SEAL DEPRESSOR DAMAGE LOWER FWD INSP PER SRM 53-00-15-1A-1 WITHIN LIMITS .(<P>REMOVED DAMAGED SEAL DEPRESSOR LOCATED, DRILLED DEBURRED AND INSTALLED NEW SEAL DEPRESSOR AT MAIN CARGO DOOR CUT OUT FWD LOWER PER B767-300 DRM 51-40-02-0G-0.</P>)

Part: SEAL DEPRESSOR — DAMAGED (CARGO DOOR) · airframe 89,617 hrs · 18,650 cycles

MAIN CARGO DOOR AFT SEAL DEPRESSOR UPPER SECTION DAMAGED(<P>REMOVED DAMAGED SEAL DEPRESSOR LOCATED DRILLED DEBURRED AND INSTALLED NEW SEAL DEPRESSOR MAIN CARGO DOOR CUT OUT AFT SIDE UPPER PER B767-300 SRM 51-40-02-0G-0.</P>)

Part: SEAL DEPRESSOR — DAMAGED (CARGO DOOR) · airframe 89,617 hrs · 18,650 cycles

MAIN CARGO DOOR FWD SEAL DEPRESSOR UPPER SECTION DAMAGED.(<P>REMOVED DAMAGED SEAL DEPRESSOR LOCATED, DRILLED DEBURRED AND INSTALLED NEW SEAL&NBSP; DEPRESSOR AT MAIN CARGO DOOR CUT OUT FWD UPPER SIDE PER B767-300 SRM 51-40-02-0G-0.</P>)

Part: ANTENNA — DAMAGED (COCKPIT ELT) · airframe 89,617 hrs · 18,650 cycles

COCKPIT SUPERNUMERARY ELT HAS DAMAGED ANTENNA HOLDER(<P>REMOVED AND REPLACED COCKPIT SUPERNUMERARY ELT AS PER B767-300F AMM 25-63-03</P>)

Part: CONTAINMENT BAG — DAMAGED (COCKPIT) · airframe 89,617 hrs · 18,650 cycles

COCKPIT CONTAINMENT BAG VACUUM SEAL IS BROKEN(<P>REMOVED AND REPLACED COCKPIT AVSAX CONTAINMENT BAG AS PER B767-300F AMM 25-60-00.</P>)

Part: ACOUSTIC PANEL — DAMAGED (NR 1 ENGINE) · airframe 89,617 hrs · 18,650 cycles

# 1 ENG. HAS DEAMAGED ACOUSTIC PANEL AFT OF 1ST STAGE BLADES (7 O' CLOCK POSITION)(<P>REMOVED AND REPLACED DAMAGED ACOUSTIC PANEL AT #1 ENG. BY 7 O' CLOCK POS. PER B767-300 AMM 72-33-01-004-001-H00, AMM 72-33-01-404-011-H00.</P>)

Part: DISPLAY — FAILED (COCKPIT) · airframe 89,617 hrs · 18,650 cycles

AFTER RUN UP, UPPER DISPLAY FAILED(<P>REMOVED AND REPLACED UPPER EICAS DISPLAY UNIT N10013 &AMP; OPS CHECK DISPLAY UNIT TEST OK AMM 31-41-01</P>)

Part: BLOCKER DOOR — DELAMINATED (THRUST REVERSER) · airframe 89,617 hrs · 18,650 cycles

#1 ENG I/B T/REV BLOCKER DOOR IS DELAMINATED AT BOTTOM #1 POS.(<P>REMOVED AND REPLACED #1 ENG. I/B T/REV BLOCKER DOOR AT POS. #1 AS PER B767 AMM 78-31-14. OPS CHK NORMAL.</P>)

Part: BATTERY — INOPERATIVE (APU) · airframe 89,617 hrs · 18,650 cycles

APU BATTERY FAIL REF WORK CARD 6749A012(<P>REMOVED AND REPLACED APU BATTERY PER MM 24-31-04-404-005. OPS CHECK GOOD.</P>)

Part: HANDLE — DAMAGED (L1 DOOR) · airframe 89,617 hrs · 18,650 cycles

L-1 ENTRANCE DOOR LOWER HANDLE DAMAGED.(<P>REMOVED AND REPLACED DAMAGED HANDLE AT L-1 ENTRANCE DOOR LOWER SIDE PER B767-300 AMM 20-11-00-910-802.</P>)

Part: BLOWER — INOPERATIVE (EVAS) · airframe 89,617 hrs · 18,650 cycles

COC PILOT'S EVAS BLOWER INOP(<P>REMOVED AND REPLACED COC PILOT'S EVAS BLOWER AS PER B767 AMM 25-60-99. OPS CHECK OK .&NBSP;</P>)

Part: VALVE — FAULTED (TRIM AIR) · airframe 89,582 hrs · 18,636 cycles

FWD CABIN TEMP ADVISORY MSG ON EICAS(<P>TRSNSFERRED TO MDDR 144401 IAW MEL 21-61-04-02, CAT C, DATED 05APR21. C/B PULLED AND COLLARED TRIM AIR VALVE LOCKED OUT, MCC NOTIFIED.</P><P>27 MAR - LP 1254532 ITEM 3 - ONT - PERFORMED FIM 21-61 FT 803 AND FOUND FWD TRIM VALVE AT FAULT, REMOVED AND REPLACED RELAY K239 (P37) PER SWPM 20-81-22. NO FIX. REMOVED AND REPLACED FWD TRIM VALVE IAW AMM 21-61-07. OPS CHECK GOOD. THIS CLEARS DMI 144401. PLACARD REMOVED. MCC NOTIFIED.</P>)

Part: A/C PACK — MALFUNCTIONED (CABIN TEMP) · airframe 89,392 hrs · 18,575 cycles

FWD CABIN TEMP INOP 10 MINS PRIOR TO TOP OF DESCENT(<P>PERFORMED FIM TASK 21-61 FT 803 FOUND NO FAULTS. PERFORMED OPS CHECK IAW AMM 21-61-00. OPS CHECK GOOD.

Part: DRIVE UNIT — FAILED (WX RADAR) · airframe 89,342 hrs · 18,562 cycles

ON CLIMB OUT GOT WX FAIL ON LOWER DISPLAYS ACCOMPANIED BY WXR SYS STATUS MSG. THIS IS A RECURRING PROBLEM AND HAS BEEN WRITTEN UP MULTIPLE TIMES.(REMOVED AND REPLACED WX RADAR DRIVE UNIT IAW AMM 34-43-07. OPS CHECK GOOD. T/S PER FIM 34-43 FT 805 TO B18.50. ANTENNA FAIL.)

Part: WARNING MESSAGE — FALSE ACTIVATION (WX RADAR SYS) · airframe 89,342 hrs · 18,562 cycles

WXR SYS STATUS MESSAGE EN-ROUTE (PERF BITE OF WXR SYS IAW FIM 34-43 FT 805 SYS. OPS CHECK GOOD, NO DEFECTS NOTED AT THIS TIME.)

Part: SMOKE DETECTOR — FAILED (CARGO BAY) · airframe 89,339 hrs · 18,560 cycles

SMOKE DETECTOR A2 CARGO FAIL(<P>TRANSFERED TO MDDR #142633 IAW MEL 26-16-01-01, CAT C, DUE DATE 01MAR21.</P><P>19FEB21 - 1253816 - ITEM# 8 - CVG - ACFT ARRIVED WITH NO AMBER LIGHTS ILLUMINATED ON CARGO FIRE BOX. ACCOMPLISHED FIM 26-16 FT. 806, NO FAULTS NOTED, SYSTEM IS OK. PER MX CTRL, THIS CLEARS DMI 142633, PLACARDS REMOVED.</P>)

Part: RADAR — MALFUNCTIONED (WX SYSTEM) · airframe 89,234 hrs · 18,524 cycles

WXR FAIL DISPLAYED INTERMITTENTLY ON MFD WITH EITHER L OR R SYS SELECTED. WXR SYS STATUS MSG DISPLAYED.(<P>PERFORMED WXR BITE PROCEDURE IAW FIM TASK 34-43 FT 805. SYSTEM OK, OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.</P>)

Part: PRESSURE SWITCH — MALFUNCTIONED (RT ENG ANTI ICE) · airframe 89,199 hrs · 18,516 cycles

RIGHT ENG TAI EICAS MESSAGE.(<P>TRANSFERRED TO MEL 30-21-01-04-02, MDDR 141976, CAT "C". DUE DATE 15FEB21. T&AMP;I TJ: 21:42Z.</P><P>05JAN, RIV, LP 1246922, ITEM M3: REMOVED AND REPLACED RT ENGINE ANTI-ICE VALVE IAW AMM 30-21-03. OPS CHECK IS GOOD AT THIS TIME. IT DID NOT FIX THE PROBLEM. DMI REMAINS OPEN, REF TO ITEM M4 FOR CONTINUATION. P/N OFF: 2790583-108, S/N OFF: 4273F.</P><P>LP 1246923, ITEM M4: FOUND PIN 1 DAMAGED ON R/H ENG TAI PRESS SWITCH. REMOVED AND REPLACED R/H TAI PRESS SWITCH IAW AMM 30-21-01. OPS CHECK GOOD, NO DEFECTS NOTED AT THIS TIME. THIS CLEARS DMI# 141976. PLACARDS REMOVED, MCC NOTIFIED. HPSOV REACTIVATED IAW AMM 36-00-00-440. DISPATCH: SD @ 21:05Z.</P>)

Part: CONTROLLER — INOPERATIVE (CABIN) · airframe 89,172 hrs · 18,508 cycles

FORWARD CABIN TEMP INOPERATIVE. CABIN COMPT TEMP CONTROL SYSTEM, ALL CARGO CONFIGURATION. TRANSFERRED TO MDDR 141789 PER DDG 21-61-01-02, CAT C, DUE 12 FEB 21. MX ACTION COMPLIED WITH. PLACARDS INSTALLED. 02FEB21 LOG PG 1272386 ITM 3 CVG RESET CB R-15 PER AMM 21-61-03. CABIN ZONE TEMP CONTROL ASSY R & R. THIS CLEARS MDDR 141789.

Part: GCU — FAILED (APU) · airframe 89,165 hrs · 18,506 cycles

DUE TO PREVIOUS FAULT CT LOOP FAIL, CHANGE APU GCU. R & R APU GCU IAW AMM 24-22-01, OPS CHECK OK.

Part: ISOLATION VALVE — LEAKING (PNUE REG SYSTEM) · airframe 89,165 hrs · 18,506 cycles

BLEED AIR LEAK RT PYLON VISUALLY CHECKED PRESSURE REGULATING VALVE FOR LEAKS. NO LEAKS NOTED. OPERATED CENTER ISOLATION VALVE PER AMM 36-11-00 AND L/R ISOLATION VALVE PER AMM 36-11-00. NO AIR LEAKS SOUNDS NOTED.

Part: CONTROLLER — INOPERATIVE (COCKPIT TEMP) · airframe 89,121 hrs · 18,489 cycles

FWD COMPT TEMP CONTROL SYS INOPERABLE. TRANSFERRED TO DMI 141282, IAW MEL 21-61-01-02, CAT C. REMOVED AND REPLACED CABIN ZONE TEMP CONTROLLER ASSEMBLY, IAW AMM 21-61-03. OPERATIONS CHECK NORMAL. NO EICAS MESSAGES NOTED. THIS CLEARS DMI 141282. MCC NOTIFIED. PLACARD REMOVED.

Part: OXYGEN MASK — MISINSTALLED (FIRST OFFICER'S) · airframe 88,941 hrs · 18,418 cycles

F/O'S ROCKER SWITCH IS STUCK IN INTERCOM EVEN WHEN SWITCH IS IN OFF POSITION. FOUND F/O OXYGEN MASK IMPROPERLY STOWED. STOWED IAW 767 AMM 35-11-51. OPERATIONS CHECK GOOD, PER AMM 23-51-00.

Part: GROUND WIRE — BROKEN (OXYGEN SYSTEM) · airframe 88,912 hrs · 18,408 cycles

CREW O2 PRESS IND INOPERABLE. TRANSFERRED TO DMI 139696, IAW MEL 35-11-02-01, CAT B. FOUND GROUND BROKEN OFF AT CONNECTOR D752. REPAIRED IAW SWPM 20-30-00. PERFORMED OPERATIONAL CHECK IAW AMM 35-11-00, NO FAULTS NOTED.

Part: CONTROLLER — MALFUNCTIONED (CABIN TEMP) · airframe 88,908 hrs · 18,406 cycles

FWD CABIN TEMP EICAS MESSAGE DISPLAYED AT GATE. CABIN COMPT TEMP CONTROL SYSTEM ALL CARGO CONFIGURATION. TRANSFERRED TO MDDR 139627, IAW MEL 21-61-01-02, CAT C. 16DEC20-LG PG 1188070 ITEM 5-CVG-REF. MDDR 139627. REMOVED AND REPLACED ZONAL TEMP CONTROLLER, IAW AMM 21-61-03. OPERATIONS CHECK, IAW AMM 21-61-03. OPERATIONS CHECK GOOD. MDDR 139627 CLEARED.

Part: CONTROLLER — MALFUNCTIONED (CABIN TEMP) · airframe 88,898 hrs · 18,403 cycles

FWD CABIN TEMP EICAS MESSAGE. FWD CABIN TEMP CONTROLLER INOPERABLE LIGHT ON, IAW MEL 21-61-01-02 CAT C DUE 25DEC20. TRANSFERRED TO MDDR 139550 PLACED ON MEL. PLACARDS INSTALLED. 15DEC20-LG PG 1188066-ITEM 3-PDX-PERFORMED ZONE TEMP CONTROLLER BITE, IAW FIM 21-61 FT 803. CONTROLLER FAULT FOUND, PER MCC REQUEST R & R ZONE TEMP CONTROLLER, IAW AMM 21-61-03. OPERATIONS TEST GOOD, MCC NOTIFIED. PLACARDS REMOVED, THIS CLEARS DMI 139550.

Part: WARNING MESSAGE — NO INDICATION (FUEL QTY) · airframe 88,816 hrs · 18,379 cycles

DID NOT RECEIVE EICAS MESSAGE TO TURN OFF CENTER FUEL PUMPS WHEN CENTER TANK QUANTITY REDUCED TO 0.0. PERFORMED OPERATIONS CHECK, IAW AMM 28-22-00/501. NO DEFECTS NOTED AT THIS TIME.

Part: STARTER — INOPERATIVE (APU) · airframe 88,599 hrs · 18,315 cycles

APU FAILED TO START (3 ATTEMPTS) APU INOPERABLE, DOOR CLOSED. TRANS TO DMI 137350, PER MEL 49-11-01B CAT "B" DUE 09NOV20 DISP T/R 2154Z SP 07NOV20. T/S APU AND FOUND APU STARTER INOPERABLE. REMOVED AND REPLACED APU STARTER, IAW AMM 49-41-01. OPERATIONS TEST OK AND CLEARS DMI 137350. PLACARD REMOVED.

Part: PRESSURE SWITCH — LEAKING (APU OIL SYSTEM) · airframe 88,338 hrs · 18,231 cycles

UPON WALK AROUND DISCOVERED OIL LEAKING FROM APU COWL. FOUND OIL LEAKING FROM LOW OIL PRESSURE SWITCH. REMOVED AND REPLACED LOW OIL PRESSURE SWITCH, IAW AMM 49-94-02. OPERATIONS CHECK GOOD, NO LEAKS NOTED AT THIS TIME.

Part: BUSS — FAULTED (LT & RT) · airframe 88,329 hrs · 18,229 cycles

UTILITY BUS LT & RT WILL NOT RESET. UNABLE TO OPEN CARGO DOORS. PERFORMED COCKPIT RESET, PER AMM 24-00-00. CHECKED FUSES, PER AMM 24-41-02. RESET BPCU, PER AMM 24-41-03 AND CYCLED UTILITY BUS SWITCHES, PER AMM 24-00-00-769-075. OPS CHK GOOD.

Part: VALVE — MALFUNCTIONED (A/C PACK) · airframe 88,298 hrs · 18,221 cycles

RT TEMP PACK EICAS. ISSUED MDDR 134974, IAW DDG 21-51-03-01, CAT C, EXPIRES 05/OCT/20. NO MX ACTION REQUIRED. PLACARDS INSTALLED. PERFORMED BITE OF RT PACK TEMP CONTROLLER, IAW FIM 21-51 FT803. FAULTED RT PACK CONTROL VALVE. REMOVED AND REPLACED RT PACK TEMP CONTROL VALVE, IAW AMM 21-51-12. OPS CHECK GOOD, NO FAULTS NOTED. THIS CLEARS DMI 134974, MCC NOTIFIED. PLACARD REMOVED. DISPATCH- CW @ 1853Z.

Part: CONTROLLER — MALFUNCTIONED (CABIN TEMP) · airframe 88,278 hrs · 18,215 cycles

FWD CABIN TEMP, PLACED ON DEFERRAL REF DMI 134796 IAW DDG 21-61-01-02, CAT C, DUE 02 OCT. VALVE IN CLOSED POSITION. .25SEP20, LP1289762 ITEM M8: R/R ZONE TEMP CONTROLLER IAW AMM 21-611-03. OPS GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME. THIS CLEARS DMI 134796. ALL PLACARDS REMOVED. CW 1853Z- DISPATCH.

Part: FAULT LIGHT — FALSE ACTIVATION (APU) · airframe 88,218 hrs · 18,200 cycles

APU FAULT ON TAXI IN. APU STARTED W/ NO FAULTS OR DEFECTS NOTED, IAW AMM 49-00-00.

Part: APU — MALFUNCTIONED · airframe 88,192 hrs · 18,191 cycles

APU RELIABILITY COLD START ACCOMPLISHED ON FLT 1 EA TPC-SCK SAT -54C FL 380, START. UNSUCCESSFUL ON 3RD ATTEMPT. PERFORMED BITE ON ECU, IAW FIM 49-11 FL 987. NO FAULTS NOTED, APU OPERATION NORMAL.

Part: CIRCUIT BREAKER — TRIPPED (APU) · airframe 88,140 hrs · 18,167 cycles

AFTER LANDING, APU DID NOT STSRT (3 TRIES)&NBSP;(<P>UPON INVESTIGATION NOTED CIRCUIT BREAKER #CB1 ON RH GEN CONTROL UNIT. RESET BREAKER &AMP; CIRCUIT BREAKER DID NOT POP AGAIN. PERFORMED APU ECU BITE &AMP; OPS CHECK AS REQUIRED PER FIM 49-11 FAULT TREE 805. NO FAULTS NOTED AT THIS TIME. OPS CHECK GOOD&NBSP;</P>)

Part: APU — UNKNOWN · airframe 88,132 hrs · 18,165 cycles

APU FAULT LIGHT ON 2 START ATTEMPTS(<P>OPS CHECKED APU START. STARTED 05 CONSECUTIVE TIME WITH NO ISSUES. IAW AMM 49-11-00 OPS GOOD&NBSP;</P>)

Part: ECU — MALFUNCTIONED (APU) · airframe 88,121 hrs · 18,162 cycles

NO APU START AFTER 3 ATTEMPTS. PERFORMED APU BITE REF FIM 49-11 FT 987, OBSERVED MINI FLAG 34. REMOVED AND REPLACED APU ECU IAW 49-61-05. STARTED APU 4 TIMES, NO FLTS, FLAGS ON ECU. PLACED LOAD ON APU. PERFORMED A DRY MOTOR 32 ENG IAW AMM 71-00-00. NO FAULTS NOTED. OPER NORMAL AT THIS TIME.

Part: VALVE — INOPERATIVE (CABIN TEMP) · airframe 88,121 hrs · 18,162 cycles

AFT CABIN ZONE TEMP VALVE INOP(<P>PERFORMED ZONE TEMP CONTROLLER BITE IAW AMM 21-61-03 FOUND AFT ZONE TRIM VALVE FAULT.

Part: MODULATING VALVE — MALFUNCTIONED (CABIN TEMP) · airframe 88,121 hrs · 18,162 cycles

AFT CABIN ZONE TEMPERATURE VALVE INOPERABLE. PERFORMED ZONE TEMPERATURE CONTROLLER BITE IAW AMM 21-61-03. FOUND AFT ZONE TRIM VALVE FAULT. TRANSFERRED TO MDDR 133363 PER MEL 21-61-04-02, CAT C, DUE 03 SEP 20 18:47Z DC, PLACARDS INSTALLED. CB'S COLLARED. LP 1274161 ITEM 5: REMOVED AND REPLACED TRIM AIR MODULATING VALVE AFT V3, OPERATIONS CHECK NORMAL IAW AMM 21-61-07, THIS CLEARS MDDR # 133363.

Part: APU — FAULTED · airframe 88,109 hrs · 18,159 cycles

APU FAULT TWO START ATTEMPTS PERFORMED FIM TASK 49-11 FAULT TREE 991. FOUND NO FAULT AT THIS TIME. PERFORMED REPETITIVE SUCCESSFUL RUN AND SHUTDOWN PROCEDURES IAW AMM 49-11-00. NOTIFIED MCC

Part: CHIP DETECTOR — BROKEN (STARTER) · airframe 88,109 hrs · 18,159 cycles

NR 1 ENG STARTER MAGNETIC CHIP DETECTOR BROKEN. REMOVED AND REPLACED THE MAGNETIC DRAIN PLUG ASSY IAW AMM 80-11-01-004. LEAK CHECKED GOOD.

Part: BLADE — DAMAGED (LT ENGINE) · airframe 88,109 hrs · 18,159 cycles

L/H ENG ACOUSTICAL PANEL SHOWING HONEY COMB AT 8 O'CLOCK POSITION EVALUATED LH ENG, FOUND PANEL OUT OF LIMITS. REMOVED SPINNER BLADES 1-7 AND ACOUSTIC PANELS IAW B767 AMM 72-33-01. PANELS, BLADES AND SPINNER INSTALLATION STILL REQ. M4 ENTRY CONTINUED ON LOG PAGE 1269583 M13. LP 1269583 M13: INSTALLED #6 AND #8 ACOUSTIC LINERS IAW AMM 72-33-01. SEE ENTRY M13 & M14 FOR PART TRANSACTIONS. FAN BLADES 1-7 AND SPINNER INSTALLATION REMAIN. M4 &AMP; M13 ENTRIES CONTINUED ON LOG PAGE 1269583 M14. LP1269583 M14 INSTALLED BLADES 1-7 ON LH ENG IAW B767 AMM 72-31-02 AND INSTALLED SPINNER ON LH ENG IAW B767 AMM 72-31-02. OPS GOOD.

Part: APU — UNKNOWN · airframe 88,109 hrs · 18,159 cycles

APU FAULTS EICAS, 2 ATTEMPTS UNSATISFACTORY. PERFORMED APU OPS CHECK. 3 GOOD STARTS. NO DEFECTS NOTED PER AMM 49-11-00

Part: WARNING LIGHT — FALSE ACTIVATION (RT A/C PACK) · airframe 88,089 hrs · 18,151 cycles

R PACK TEMP LIGHT ILLUMINATED ON CLIMB OUT PERFORMED B.I.T.E TEST IAW AMM REF 21-51-00. NO FAULTS FOUND. SYSTEM OPS NORMAL.

Part: DRAIN MAST — MISSING (NR 2 ENGINE) · airframe 88,060 hrs · 18,140 cycles

ON WALK AROUND FOUND # 2 ENG DRAIN MAST MISSING(<P>IAW AMM 71-71-01 INSTALLED DRAIN MAST ON #2 ENG. OPS NORMAL AT THIS TIME.<BR /></P>)

Part: UNKNOWN — UNKNOWN (APU) · airframe 88,060 hrs · 18,140 cycles

APU FAULT. WOULD NOT START IN RAMP(<P>PERFORMED APU OPS CHECK THREE CONSECUTIVE GOOD STARTS, NO DEFECTS NOTED IAW AMM 49-11-01&NBSP; (NOTE: AN APU COLD SOAK START VERIFICATION DMI&NBSP; DDG 25-AP-01 WAS OPENED AFTER ABOVE ACTION).</P>)

Part: OIL SYSTEM — LEAKING (RT ENGINE) · airframe 88,039 hrs · 18,130 cycles

DURING WALK AROUND FOUND EXCESSIVE OIL LEAK ON RH ENGINE&NBSP;(<P>REF ISSUED WO 19313 FOR NR 2 ENGINE UER. WORK ORDER C/W IAW ASSOCIATED JOB CARDS, NR 2 ENGINE REMOVED AND REPLACED (AMM 71-00-02/401).</P>)

Part: CIRCUIT CARD — MALFUNCTIONED (RT ENGINE BLEED) · airframe 88,039 hrs · 18,130 cycles

R ENG BLEED OFF LITE & EICAS ILLUMINATED AFTER ENG START. REMOVED AND REPLACED RT ENGINE BLEED AIR CONTROL CARD IAW AMM 36-11-12/401. OPS CHECKED GOOD.

Part: CIRCUIT CARD — MALFUNCTIONED (LT ENGINE BLEED) · airframe 88,038 hrs · 18,129 cycles

LEFT ENG BLEED AIR INOPERATIVE REMOVED AND REPLACED L/H AIR SUPPLY CONTROL CARD IAW AMM 26-11-12. PERFORMED ENG IDLE RUN IAW 71-00-00. OPS CHECK NORMAL AT THIS TIME.

Part: PRIORITY VALVE — MALFUNCTIONED (RT ENGINE) · airframe 88,039 hrs · 18,130 cycles

RIGHT ENG BLEED OFF EICAS AFTER ENGINE START. REMOVED AND REPLACED THE RT PRSOV IAW AMM 36-11-09. PERFORMED IDLE ENGINE RUN IAW AMM 71-00-00, OPS CHECKED GOOD IAW AMM 36-11-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENG BLEED) · airframe 88,026 hrs · 18,125 cycles

RIGHT ENGINE BLEED OFF EICAS MESSAGE DISPLAYED AND OVERHEAD ANNUNCIATOR ILLUMINATED IN FLIGHT. COMPLIED WITH AIR SUPPLY BITE IAW FIM 36-20 TASK 804. TEST INDICATED PRSOV. VERIFIED NO CURRENT FAULTS. ERASED. RAN ENGINE IAW AMM 71-00-000. RT ENG BLEED OPS CHECKED NORMAL IAW AMM 36-10-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENGINE) · airframe 88,028 hrs · 18,126 cycles

R ENG BLEED OFF EICAS. COMPLIED WITH THE SUPPLY BITE IAW FIM 36-20, TASK 804. VERIFIED NO CURRENT FAULTS. PERFORMED ENGINE RUNS IAW AMM 71-00-00. RT ENG BLEED OPS CHECKED NORMAL IAW AMM 36-10-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENGINE) · airframe 88,039 hrs · 18,130 cycles

RIGHT ENGINE BLEED OFF EICAS MESSAGE DISPLAYED AND OVERHEAD ANNUNCIATOR ILLUMINATED IN FLIGHT. COMPLIED WITH AN AIR SUPPLY BITE IAW FIM 36-20 TASK 804. TEST INDICATED PRSOV, VERIFIED NO CURRENT FAULTS. ERASED AND RAN ENGINE IAW AMM 71-00-00. RT ENG BLEED OPS CHECKED NORMAL IAW AMM 36-10-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (C/P&CABIN TEMP) · airframe 88,018 hrs · 18,122 cycles

COCKPIT, FWD, AND AFT CABIN TEMP EICAS MESSSAGE. COMPLIED WITH TEMP CONTROLLER BITE TEST. ALL PASSED. OK FOR CONTINUED SERVICE IAW AMM 21-61-03.

Part: APU — FAULTED · airframe 88,005 hrs · 18,117 cycles

APU FAULT AFTER 3 START ATTEMPTS ON THE GROUND. FOUND BPCU CB IN THE OPEN POSITION. RESET CB, THEN PERFORMED BPCU BITE. NO FAULTS. STARTED APU IN THE FIRST ATTEMPT. NO FAULTS NOTED. REF AMM 24-22-00.

Part: APU — UNKNOWN · airframe 87,986 hrs · 18,110 cycles

APU FAULTS AFTER 3 START ATTEMPT ON GROUND.(<P>PERFORMED ECU BITE IAW B767 AMM 49-61-05-742-027. NO FAULTS NOTED. STARTED APU AND APPLIED BOTH ELECTRIC AND BLEED AIR LOAD. NO FAULTS.<BR /></P>)

Part: WARNING LIGHT — FALSE ACTIVATION (RT ENGINE BLEED) · airframe 87,986 hrs · 18,110 cycles

AFTER ENGINE START RT ENG BLEED OFF LIGHT ILLUMINATED, RT ENG BLEED OFF EICAS MSG. ON GVI OF PNEUMATIC VALVES ON R/H ENG, FOUND ANTI-ICE VALVE TO BE LOOSE. RESECURED ANTI-ICE VALVE, RAN #2 ENG PERFORMED AND RT ENG BLEED VALVE OPS CHECK LEAKS GOOD IAW B767 AMM 36-11-09.

Part: APU — FAULTED · airframe 87,952 hrs · 18,100 cycles

APU FAULT ON THREE START ATTEMPTS, AFTER LANDING GROUND OPS CHECKED GOOD. APU CONT UNIT BITE CHECKED GOOD, APU COLD SOAK REQ DUE TO MX, REF ITEM M-4, REF AMM 49-00-00.

Part: PITOT TUBE — FAILED (CAPTAIN'S) · airframe 87,929 hrs · 18,092 cycles

CAPTAIN`S PITOT EICAS MESSAGE DISPLAYED IN FLIGHT. RAN FIM 30-31, FT 805 UP TO STEP 21, REMOVED AND REPLACED THE RELAY F241 IAW SWPM 20-81-00, NO HELP, PLACED ORIGINAL RELAY BACK IAW 20-81-00, PER FIM. REMOVED AND REPLACED THE CAPTAIN`S PITOT TUBE IAW 34-11-01, OPS AND LEAK CHECKED GOOD.

Part: APU — UNKNOWN · airframe 87,910 hrs · 18,085 cycles

APU DID NOT START AFTER LANDING. TWO ATTEMPTS UNSUCCESSFUL. PERFORMED APU ECU BITE CHECK. NO FAULTS NOTED. APU STARTED FIRST ATTEMPT. NO FAULTS. REF AMM 49-61-00.

Part: GASKET — MISSING (APU FLW SENS MOD) · airframe 87,915 hrs · 18,086 cycles

APU PNEUMATICS INOPERATIVE. FOUND A GASKET MISSING FROM THE FLOW SENSING MODULE. REPLACED THE GASKET IAW AMM 49-53-08, OPS NORMAL. OBSERVED APU BULK PRESSURE @ 30PSI, PERFORMED ENG RUNS IAW AMM 71-00-00. OPS GOOD.

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 87,870 hrs · 18,072 cycles

APU FAULT. TRIED TWICE TO START ON GROUND, MAX RPM 2ND ATTEMPT 29. PERFORMED APU OPERATIONAL START PROCEDURE WITH NO DEFECTS NOTED, IAW AMM 49-11-00, APU OPERATES NORMAL.

Part: AIR FILTER — DIRTY (WEATHER RADAR) · airframe 87,862 hrs · 18,068 cycles

WEATHER RADAR INOP. WXR XCVR RIGHT AIR FILTER CLEANED, PERFORMED WXR BITE TEST, TEST PASS. NO FAULTS FOLLOWED. MSG CLEARED. REF FIM 34-43 FT 805.

Part: WIRE — KINKED (WINDOW HEAT) · airframe 87,830 hrs · 18,058 cycles

R SIDE WINDOW HEAT INOP LIGHT AND EICAS MSG. FOUND KINKED WIRE FROM NR 3 SIDE WINDOW. REPAIRED PER SWPM 20-10-13. OPS NORMAL AT THIS TIME. NO FURTHER DEFECTS NOTED.

Part: FAULT MESSAGE — ILLUMINATED (APU) · airframe 87,801 hrs · 18,050 cycles

APU FAULT MESSAGE. THREE ATTEMPTS. PERFORMED ECU BITE TEST, CHECKED OK, INSPECTED APU FOR LEAKS, NO LEAKS FOUND, APU OIL VISUAL CHECKED OK, APU ECU BITES OK IAW 49-11, FAULT TREE 987, APU LEAK CHECKED OK IAW AMM 49-16-00. APU CHIP DETECTORS OK IAW 49-27-04, APU OPS OIL CHECKED OK IAW AMM 12-13-04.

Part: OIL SYSTEM — LOW (APU) · airframe 87,781 hrs · 18,044 cycles

APU FAULT LITE ON START ATTEMPT. SERVICED APU OIL IAW MM CH 12-13-04. APU POWER GENERATION CK'S GOOD IAW MM CH 24-21-00 ALSO RESET CB 2 AND C/W BITE TEST OF EPCU TEST PASS IAW MM 24-22-00.

Part: TRANSCEIVER — MALFUNCTIONED (WEATHER RADAR) · airframe 87,736 hrs · 18,029 cycles

WX RADAR DOES NOT APPEAR TO PAINT SIGNIFICANT WEATHER AS EXPECTED. REMOVED AND REPLACED RIGHT WX RADAR TRANSCEIVER IAW AMM 34-43-01. OPS CHECK NORMAL.

Part: PRESSURE SWITCH — MALFUNCTIONED (APU) · airframe 87,736 hrs · 18,029 cycles

TWICE (2X) APU FAULT, NO FURTHER ATTEMPTS. REMOVED AND REPLACED APU GENERATOR FILTER DIFFERENTIAL PRESSURE SWITCH IAW AMM 49-27-15 OPS CHECK GOOD. THIS CLEARS MDDR 130465. NOTE: AN APU COLD SOAK DMI 130584 WAS ALSO OPENED IN THE AIRCRAFT PER ETOPS MNL REQUIREMENT.

Part: SHUTOFF VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 87,707 hrs · 18,019 cycles

WHEN ATTEMPTING TO X BLEED START THE LEFT ENG EICAS MESSAGE R ENG BLEED OFF AND OFF LIGHT IN R ENG BLEED SWITCH SHOWED. FOUND R ENG PRSOV AT FAULT. REPLACED PER AMM 36-11-09-402-508-001. OPS GOOD.

Part: FILTER — FAULTY (APU) · airframe 87,707 hrs · 18,019 cycles

APU INOP (AUXILIARY POWER UNIT (APU), ER OPERATIONS NOT ALLOWED. T/SHOOTING REPLACED GENERATOR FILTER IAW AMM 49-27-07. SYSTEM TESTED OK. THIS CLEARS MDDR 130054.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 87,605 hrs · 17,986 cycles

APU FAULT EICAS MESSAGE WHEN ATTEMPTED START ON TAXI IN. PERFORMED BITE CHECK ON APU ECU, NO FAULTS FOUND. APU STARTED FIRST ATTEMPT REF AMM 49-11-00/49-61-05.

Part: CONTROLLER — MALFUNCTIONED (CABIN TEMP) · airframe 87,342 hrs · 17,914 cycles

FLIGHT DECK TEMP EICAS MSG(<P>TRANSFER TO MDDR #128109 IAW DDG 21-61-02-03, CAT 'C', DUE DATE 18 MAY 2020.</P><P>LP 1140486: REMOVED AND REPLACED CABIN ZONE TEMP CONTROLLER IAW AMM 21-61-03. THIS CLEARS MDDR 128109.<BR DATA-MCE-BOGUS="1" /></P>)

Part: CONTROLLER — MALFUNCTIONED (CABIN TEMP) · airframe 87,342 hrs · 17,914 cycles

AFT CABIN AND FORWARD CABIN TEMP EICAS MSG(<P>ISSUED MDDR #128108 PER MEL CH 21-61-01-02, CAT 'C'.</P><P>LP 1140486: REMOVED AND REPLACED CABIN ZONE TEMP CONTROLLER IAW AMM 21-61-03. THIS CLEARS MDDR 128108.<BR DATA-MCE-BOGUS="1" /></P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 87,342 hrs · 17,914 cycles

L PRV STATUS MSG(<P>PERFORMED AIR SUPPLY CONTROL MODULE BITE TEST REF AMM 36-20-00-815-804. TEST PASSED AT THIS TIME. MSG CLEARED. OK FOR RTS.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 87,332 hrs · 17,911 cycles

LH ENG PRV STATUS(<P>PERFORMED AIR SUPPLY BITE IAW FIM 36-20 FT 804, PREVIOUS FAULTS STORED. CLEARED FAULTS. PERFORMED ENGINE RUN IAW AMM 72-00-00. TROUBLE SHOOTING IAW FIM 36-10 FT 847 &AMP; FT 848, NO FAULTS NOTED, NO EICAS MESSAGES. PERFORMED AIR SUPPLY BITE IAW 36-20-00. NO FAULTS STORED. OPS CHECK GOOD.</P>)

Part: SHUTOFF VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 87,321 hrs · 17,907 cycles

STATUS MESSAGE LH ENG. PRV(<P>REMOVED AND REPLACED HIGH PRESSURE SHUT OFF VALVE ON #1 ENG IAW AMM 36-11-18. OPS CHECK GOOD.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 87,297 hrs · 17,901 cycles

STATUS MSG L ENG PRV(<P>PERFORMED BITE TEST IAW FIM 36-11-18 FAULT TREE 847, NO FAULTS NOTED. PERFORMED PRV LEAKAGE TEST IAW AMM 36-11-18. NO LEAKS, OPS CHECK GOOD.</P>)

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 87,270 hrs · 17,885 cycles

AFT CABIN TEMP DISPLAYED ON EICAS DURING DESCENT(<P>TRANSFERED TO MDDR 126626 IAW MEL 21-61-01-02, CAT "C", DUE 13APR2020.</P>)

Part: MODULE — FAULTY (APU) · airframe 87,168 hrs · 17,854 cycles

APU AUTO SHUTDOWN (PRIOR TO DEPARTURE).(<P>APU PLACED ON DEFERRAL (DDG 49-11-01A), MDDR 125904, CAT 'C'.</P><P>LOG PAGE 1130021: REMOVED AND REPLACED FLOW CONTROL SENSOR MODULE IAW AMM REF 49-53-04, OPS CHECK GOOD. DMI 125904 CLEARED, PLACARDS REMOVED.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 87,170 hrs · 17,856 cycles

APU FAULT AFTER TAXI TO GATE.(<P>PERFORMED APU START I/A/W AMM 49-11-00. NO DEFECTS NOTED, OPS CHECK NORMAL.<BR /></P>)

Part: MODULATING VALVE — FAULTY (CABIN TEMP) · airframe 87,095 hrs · 17,829 cycles

AFT CABIN TEMP EICAS MESSAGE(<P>TRANSFERRED TO MDDR 125561 IAW MEL 21-61-01-02, CAT 'C'. MCC NOTIFIED. PLACARDS INSTALLED.</P><P><SPAN>LP&NBSP;1206930 - M2: REMOVED AND REPLACED AFT CABIN TRIM AIR MODULATING VALVE IAW AMM 21-61-07. OPS TEST GOOD. THIS CLEARS MDDR 125561. PLACARDS REMOVED.</SPAN></P><P><BR DATA-TEMP="1" /></P><P><BR DATA-TEMP="1" /></P>)

Part: KNOB — STUCK (CABIN PRESSURE) · airframe 87,035 hrs · 17,808 cycles

PRESSURIZATION LANDING ALTITUDE SELECTOR KNOB STUCK(<P>REMOVED AND REPLACED CABIN ALTITUDE CONTROL IAW AMM 21-31-01-004-001. OPS CK GOOD.</P>)

Part: VALVE — FAILED (CABIN TEMP) · airframe 87,002 hrs · 17,800 cycles

AFT CABIN TEMP MESSAGE ON LANDING.(<P>TRANSFERRED TO DMI 124984 IAW DDG 21-61-04-02, CAT C, DUE 04MAR20. MX ACTIONS COMPLIED WITH.</P><P>LP 1207060: REMOVED AND REPLACED AFT ZONE TRIM VALVE V3 IAW AMM 21-61-02. PERFORMED OPS CHECK, OPS GOOD. NO FURTHER DEFECTS NOTED. THIS CLEARS DMI 124984. ALL PLACARDS REMOVED.</P>)

Part: VALVE — MALFUNCTIONED (CABIN TEMP) · airframe 87,028 hrs · 17,806 cycles

PRIOR TO BLOCK OUT AFT CABIN TEMP EICAS.(<P>DEFERRED TO DMI #124935, DDG 21-61-01-02, CAT C. PLACARD APPLIED.</P><P>LOG PAGE 1169158: REMOVED AND REPLACED AFT CARGO TRIM VALVE ASSY IAW IAW B767 AMM 21-61-07. OPS CHECKED GOOD AT THIS TIME. THIS CLEARS MDDR 124935.</P>)

Part: SURGE VALVE — FAILED (APU) · airframe 86,936 hrs · 17,774 cycles

DURING SHUTDOWN APU BLEED VALVE WOULD NOT GO ABOVE 10 PSI, CYCLED BLEED SWITCH, NO CHANGE.(<P>TRANSFERRED TO MDDR 124676 PER MEL 49-11-01-01, CAT C, DUE DATE: 24FEB20. DISPATCH JL @ 17:10Z.</P><P><SPAN>LP&NBSP;</SPAN><SPAN>1169147:&NBSP;</SPAN><SPAN>REMOVED AND REPLACED APU SURGE CONTROL VALVE IAW AMM 49-53-01 AND OPS CHECK IS GOOD AT THIS TIME. THIS CLEARS MDDR 124676. MCC NOTIFIED AND STICKERS REMOVED.</SPAN></P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 86,699 hrs · 17,699 cycles

AFT EQUIPMENT EXHAUST FAN 2 STATUS MESSAGE. T/S PER FIM 21-26 FT 808. MESSAGE ERASED. NO FURTHER FAULTS AT THIS TIME.

Part: CONTROL VALVE — INOPERATIVE (APU) · airframe 86,688 hrs · 17,694 cycles

APU PNEUMATIC FUNCTION INOPERATIVE. REMOVED AND REPLACED APU BLEED CONTROL VALVE IAW AMM 36-11-10. OPS CHECKED OK IAW AMM 49-11-00.

Part: PNEUMATIC SYSTEM — MALFUNCTIONED (APU) · airframe 86,544 hrs · 17,648 cycles

APU PNEUMATIC INOPERATIVE. PERFORMED PACK CONTROLLER BITE IAW AMM 21-51-14, NO FAULTS FOUND. PERFORMED APU BITE IAW FIM 49-11 FT 987, NO FAULTS FOUND. MONITORED APU WITH PACKS ON FOR TWO HOURS, NO ISSUES. OPS CHECK GOOD IAW AMM 49-11-00.

Part: APU — SHUTDOWN · airframe 86,555 hrs · 17,650 cycles

APU UNSCHEDULED SHUTDOWN BEFORE START CHECK. RESTART OK. PERFORMED OPS CHECK OF APU IAW AMM 49-11-01. NO DEFECTS NOTED AT THIS TIME.

Part: SWITCH — STICKING (WX RADAR F/O) · airframe 86,486 hrs · 17,624 cycles

F/O WXR RADAR SWITCH (CENTER PEDESTAL) STICKS IN POSITION OFTEN WHEN SELECTING AND DESELECTING.(<P>REMOVED DEBRIS FROM SWITCH, PERFORMED OPS CHECK PER AMM 34-43-00/501, OPS GOOD.</P>)

Part: OIL SYSTEM — LOW (ENGINE) · airframe 86,470 hrs · 17,617 cycles

AFTER 05:55 FLIGHT, FOLLOWING DAILY CHECK, AIRCRAFT BLOCK-IN WITH 18 QTS OIL QUANTITY. FOUND NO LEAKS AROUND ENGINES. SERVICED ENGINE OILS TO PROPER OPERATING LEVEL IAW AMM 12-13-01.

Part: BLEED AIR SYS — SURGES (APU) · airframe 86,447 hrs · 17,610 cycles

APU AIR SURGING UP AND DOWN WITH PACKS RUNNING. PERFORMED APU WIRE PROCEDURE PER FIM 49-11 FT 987 AND NO FAULTS CODE FOUND.

Part: PIN — BROKEN (A/C PACK TEMP) · airframe 86,419 hrs · 17,598 cycles

LEFT PACK AUTO TEMP CONTROLLER INOPERATIVE, FAILED LOW LIMIT VALVE BITE. STANDBY CONTROLLER BITE CHECKED GOOD. T/S PER WDM 21-51-14. FOUND PIN 21 ON D1432P BROKEN AND SHORTED. REPLACED THE PIN IAW SWPM 20-61-00. OPS CHECKED IAW AMM 21-51-00. NO DEFECTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (APU) · airframe 86,413 hrs · 17,595 cycles

APU FAULT.(<P>PERFORMED BITE CHECK OF THE APU IAW FIM 49-11 FT 987, MESSAGE CLEARED.</P>)

Part: TRANSDUCER — FAILED (APU) · airframe 86,371 hrs · 17,577 cycles

APU INOP.(<P>TRANSFERRED TO MDDR #120796 PER MEL 49-11-01A, CAT 'C,' DUE DATE: 28NOV19. MCC NOTIFIED AND PLACARDS INSTALLED.</P><P>LP 1113302 - M4: STARTED APU AND PERFORMED BITE TEST, NO FAULTS NOTED. RAN L AND R PACKS, AND WITH LT PACK ONLY ON, THE DUCT PRESSURE SURGES. REQUIRES FURTHER TROUBLESHOOTING IAW B767-300 FIM 49-11 FT 987.&NBSP;</P><P>LP 1113320 - M4: REMOVED &AMP; REPLACED TOTAL PRESSURE TRANSDUCER (OFF PART: PN: 3876084-2, SN: NSN)&NBSP;&AMP; DIFF PRESSURE TRANSDUCER. OPS CHECK COMPLETE, NO DEFECTS NOTED AT THIS TIME IAW AMM 49-53-02 AND AMM 49-53-04. THIS CLEARS DMI 120796. PLACARDS REMOVED AND MCC NOTIFIED.</P>)

Part: APU — MALFUNCTIONED · airframe 86,353 hrs · 17,570 cycles

APU INOPERATIVE.(<P>LP 1215769 - M1: PERFORMED BITE TEST ON APU ECU, TEST PASSED IAW AMM 49-61-05. APU OPS CHECK NORMAL IAW AMM 49-11-00.<BR /></P><P>LP 1215769 - M2:&NBSP;APU COLD SOAK REQUIRED DUE TO APU WORK. TRANSFERRED TO DMI 120637, DEFERRED PER DDG 25-AP-01, CAT 'N', ETOPS RESTRICTED.</P><P>LP 1215771 - ITEM 1: APU RELIABILITY COLD START BWI-PDX, SAT -57 C, FL 360, START SUCCESSFUL ON 1ST ATTEMPT. NOTED BY MX, THIS CLEARS MDDR #120637. PLACARDS REMOVED.</P>)

Part: APU — FAULTED · airframe 86,309 hrs · 17,559 cycles

APU FAULT ON TAXI IN, TRIED TO START 3 TIMES.(<P>PERFORMED SELF AND BITE CHECK OF THE ECU IAW AMM B767 49-61-05, NO FAULTS FOUND. ABORTED START MESSAGE, APU STARTED ON FOURTH ATTEMPT. OPS CHECK GOOD AT THIS TIME (1ST ATTEMPT BY MX). BATTERY RECOVERED FROM EARLIER&NBSP;CREW ATTEMPTS. APU OPERATION NORMAL, BATTERY SHOWED 28&NBSP;VOLTS AND 3&NBSP;AMPS CHARGING.</P>)

Part: OIL SYSTEM — LOW (APU) · airframe 86,250 hrs · 17,539 cycles

APU FAULT EICAS MSG, TWO ATTEMPTS MADE.(<P>PERFORMED BITE CHECK OF APU IAW B767 AMM 49-61-05 AND SELF TEST, NO FAULTS FOUND.&NBSP;DISCOVERED APU OIL WAS LOW, SERVICED OIL IAW AMM 12-13-04 (REF ITEM M3). APU START SUCCESSFUL THIRD ATTEMPT.<BR /></P><P><BR /></P><P>NOTE: LP 1092172 -&NBSP;AS PER ATLAS AIR GMM, APU REQUIRED COLD SOAK DUE TO APU WORK DONE.&NBSP;ITEM TRANSFERRED TO MDDR 120098 PER ATLAS AIR ETOPS MM IAW MEL- 25-AP-01, OPTION C, CAT N, DUE DATE 03NOV20. PLACARD INSTALLED.</P>)

Part: IGNITER — FAILED (NR 1 ENGINE) · airframe 86,232 hrs · 17,533 cycles

OVERTEMP ON #1 DURING RELIGHT, SHUTDOWN AT FL 400. RELIGHT AT FL 310. VIA QRH "IN FLIGHT". REF ITEM #1: CREW REPORTED THAT AIRCRAFT WAS APPROACHING FUEL IMBALANCE. CREW SHUT OFF L FUEL PUMPS, FORGOT TO SELECT CROSSFEED. AS THEY WERE GOING TO SELECT CROSSFEED, LEFT ENG FLAMED OUT. ON FIRST ENG RESTART, EGT EXCEEDED LIMITS. 788 EGT FOR 13 SECONDS TOTAL. CREW SHUTDOWN ENG, EGT WAS AT 30 DEGREES C AT SECOND ENG RESTART, ATTEMPT SUCCESSFUL.&NBSP;&NBSP;(<P>C/W FIM 71-06 FT 825, INSPECTION FOUND NO FAULTS. REMOVED AND REPLACED #1 AND #2 IGNITER PLUGS IAW AMM 74-21-02. C/W FIM 71-10 FT 810, ALL CHECKS GOOD.</P><P>ITEM M2: NO FUEL MIGRATION NOTED DURING GROUND TIME.&NBSP;</P><P>LP 1092157 - M6: L ENG FUEL SUCTION FEED SYSTEM TEST PERFORMED IAW AMM 28-22-00. ALL CHECKS GOOD, NO DECAY IN ENGINE PARAMETERS.</P><P>LP 1092157 - M7:&NBSP;UNUSUAL CONDITION INSPECTION PERFORMED IAW AMM 72-00-00. ENGINE WINDMILL, ALL CHECKS GOOD.</P>)

Part: APU — FAULTED · airframe 86,158 hrs · 17,506 cycles

APU FAULT ON START ATTEMPT.(<P>PERFORMED APU BITE TEST IAW AMM 49-61-05 AND RESTARTED APU. OPS CHECKS GOOD AT THIS TIME.</P>)

Part: IGNITER — WARNING MESSAGE (LT ENGINE) · airframe 86,033 hrs · 17,463 cycles

STATUS MESSAGE FOR THE LT ENGINE IGNITER 1. REMOVED AND REPLACED THE LT ENGINE IGNITER NR 1 IAW AMM 74-21-02, OPS CHECKED NORMAL. REMOVED AND REPLACED THE LT ENGINE NR 1 IGNITING EXCITER IAW AMM 74-11-01, OPS CHECKED GOOD.

Part: BATTERY — FAILED (APU) · airframe 86,009 hrs · 17,455 cycles

THREE ATTEMPTS TO START APU, EICAS APU FAULT. PERFORMED BITE CHECK OF APU ECU I.A.W AMM 49-61-00 AND FOUND NO MINIFLAGS , START ABORT OR PREVIOUS LEGS SHOW SEE MAINTENANCE MANUAL , REMOVED AND REPLACED APU BATTERY IAW AMM 24-31-04. OPS NORMAL.,

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 85,999 hrs · 17,452 cycles

APU WILL NOT START ON GROUND, AT THE END OF FLIGHT.&NBSP;(<P>PERFORMED 3 SUCCESSFUL APU STARTS, NO DEFECTS NOTED. ALL PARAMETERS NORMAL ON APU HEALTH CHECK, APU OPS TEST GOOD IAW AMM 49-11-00. APU BITE, NO FAULTS.&NBSP;</P>)

Part: CONTROL VALVE — FAULTY (AC BAY) · airframe 85,987 hrs · 17,447 cycles

WHEN SELECTING L PACK OFF FOR ENGINE START, THE EICAS MSG, "L PACK OFF" NOT DISPLAYED ON EICAS. PACK OFF SWITCH LIGHT DID NOT ILLUMINATE.(<P>TRANSFERRED TO MEL 118320 PER DDG 21-51-01-01, CAT 'C'.&NBSP; PLACARD INSTALLED AND MCC NOTIFIED.<BR /></P><P>LP 1051364 - M4:&NBSP;PERFORMED BITE CHECK ON LT PACK TEMP CONTROLLER, FAULTING LOW LIMIT VALVE PER AMM 21-51-14. SUSPECT BAD PACK TEMP CONTROLLER BOX DUE TO LOW LIMIT VALVE BEING REPLACED, PN 625934-6 ON ORDER WITH MCC.</P><P>LP 1051365 - M2:&NBSP;R/R L/H PACK FLOW CIRCUIT CARD IAW 21-51-09. FAILED OPS CHECK, LIGHT REMAINED OFF. L/H PACK FLOW CONTROL VALVE IS MANUALLY CLOSED. DMI REMAINS OPEN.</P><P>LP 1051367 - M3:&NBSP;REMOVED AND REPLACED FLOW CONTROL VALVE ASSY IAW B767 AMM 21-51-01. PART INSTALLED IS FOR WRONG EFFECTIVITY A/C, BUT IS RIGHT PART FOR A/C. FLOW CONTROL VALVE WITH PROPER EFF. IS MISSING CANNON PLUG ON CANNISTER. PER MCC, ORIGINAL PART IS TO BE RE-INSTALLED UNTIL ENGINEERING IS NOTIFIED.&NBSP;</P><P>LP 1051368 - M4: (RE)REMOVED AND REPLACED NEW FLOW CONTROL VALVE ASSY IAW B767 AMM 21-51-01. OPS CHECK GOOD AT THIS TIME. THIS CLEARS DMI # 118320. PLACARD REMOVED AND MCC NOTIFIED. EH @ 17:25Z</P>)

Part: OIL SYSTEM — LOW (APU) · airframe 85,990 hrs · 17,448 cycles

EICAS MESSAGE "APU FAULT" ON START. SECOND START ATTEMPT UNSUCCESSFUL.(<P>PERFORMED FIM TASK 49-11 FT 987, APU BITE PROCEDURE. "SEE MAIN MANUAL" ON BITE. INSPECTED APU, FOUND OIL TO BE LOW. EICAS APU OIL LEVEL CONFIRMED AT .50. SERVICED APU OIL IAW AMM 12-13-04. APU STARTS AND RUNS AS REQUIRED IAW AMM 49-11-00. OPS CHK GOOD. COULD NOT DUPLICATE DISCREPANCY. APU HRS @ 1735.4</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 85,966 hrs · 17,437 cycles

STATUS MSG "AFT EQ EXH FAN 2". PERFORMED FIM 21-26 FT 808, SYSTEM OPERATES NORMAL PER BLOCK 40. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 85,952 hrs · 17,431 cycles

APU FAULT EICAS MESSAGE AFTER LANDING. APU DEFERRED PER MEL 49-11-01A. THIS BECOMES MDDR 118053, CAT 'C', DUE O1-OCT-19. MCC NOTIFIED. LP 1076160 - M3; REMOVED AND REPLACED APU IAW WORK ORDER #56763. REF LOG PAGE 1051351 ITEM #4. OPS CHECK GOOD AT THIS TIME. THIS CLEARS MDDR 118053. MCC NOTIFIED AND PLACARDS REMOVED.

Part: VALVE — FAULTY (AC BAY) · airframe 85,941 hrs · 17,427 cycles

LT PACK "OFF" LIGHT WILL NOT ILLUMINATE WHEN LT PACK SWITCH IS IN OFF POSITION. TRANSFERRED TO DMI 117977 IAW MEL 21-51-01-01, CAT 'C', DUE DATE 29SEP19. PLACARDS INSTALLED AND MX ACTION C/W. FLOW CONTROL SHUT OFF VALVE LOCKED IN CLOSED POSITION AND SATISFIED. LP 1076141 - M4: REMOVED AND REPLACED LOW LIMIT VALVE IAW AMM 21-51-11, OPS CHECK GOOD. THIS CLEARS MDDR 117977. MCC NOTIFIED AND PLACARD REMOVED. TI: RS @ 18:13Z.

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 85,929 hrs · 17,424 cycles

3 APU FAULT / START DURING SHUT DOWN. TRANSFERRED TO MDDR #117876 PER DDG 25-AP-01, OPTION C, CAT N, DUE 09-16-20. LP 1076132 - M2: PERFORMED APU BITE TEST IAW FIM 49-11 FT 958, NO FAULTS NOTED. (2) TWO SUCCESSFUL STARTS. MDDR 117876 REMAINS OPEN PER DDG 25-AP-01, OPTION C, CAT N. LP 1076135 - ITEM 1: APU RELIABILITY COLD START OAT -36C, FL 330, 1X SUCCESSFUL START. NOTED BY MX. THIS ACTION CLEARS DMI 117876. PLACARD REMOVED.

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 85,920 hrs · 17,422 cycles

APU NO START AFTER LANDING, ATTEMPTED 2X. PERFORMED APU BITE PROCEDURE, NO FAULTS NOTED. COMPLETED 3 SUCCESSFUL STARTS WITH NO ISSUES. WORK DONE IAW FIM 49-11 FT 958, ALL OPS CHECKS GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 85,912 hrs · 17,420 cycles

EICAS MSG: APU FAULT. PERFORMED BITE OF APU ECU, NO FAULTS FOUND. OPS CHECK GOOD REF AMM 49-61-05.

Part: CONTROLLER — MALFUNCTIONED (AC BAY) · airframe 85,870 hrs · 17,404 cycles

AFT CABIN TEMP EICAS MSG FWD CABIN TEMP EICAS. RESET PACK TEMP CONTROLLER AND OPS TESTED PACKS IAW AMM 21-51-00. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 85,870 hrs · 17,404 cycles

APU FAULT ON TAXI IN UNSUCCESFUL START THREE TIME. PERFORMED APU OPERATION CHECK WITH LOAD IAW AMM 49-11-00. FOUND SATISFACTORY AT THIS TIME.

Part: SMOKE DETECTOR — DEFECTIVE · airframe 85,818 hrs · 17,388 cycles

ON P8 AFT CONTROL PANEL CCP, CHANNEL B LED LIGHT AMBER, IS ON ALL THE TIME. TEST FAILED. REPLACED #7B SMOKE DETECTOR IAW AMM 26-14-01, OPS CHECK NORMAL.

Part: INDICATOR — FAULTY (FUEL SYSTEM) · airframe 85,818 hrs · 17,388 cycles

CENTER FUEL TANK QUANTITY INDICATOR READING IN ERROR AT FUEL PANEL. REMOVED AND REPLACED CENTER FUEL TANK QTY INDICATOR AT FUEL PANEL. OPS CHECKED NORMAL IAW AMM 28-43-00.<

Part: CONTROL VALVE — MALFUNCTIONED (APU) · airframe 85,812 hrs · 17,386 cycles

APU FAILED TO START AFTER 3 ATTEMPTS, APU FAULT LIGHT DISPLAYED. PERFORMED ECU BITE IAW B767 FIM 49-11 F/T 987, NO FAULTS NOTED. RESET PER FIM, APU STARTS FIRST ATTEMPT IAW AMM 49-11-00. PACK AND ELECTRICAL LOAD NORMAL. APU INOP DUE TO AUTO SHUTDOWN. REMOVED AND REPLACED APU SURGE CONTROL VALVE IAW AMM 49-53-01. OPS CHECK NORMAL, NO LEAKS NOTED.

Part: APU — MALFUNCTIONED · airframe 85,801 hrs · 17,382 cycles

APU WOULD NOT START AFTER LANDING, TWO ATTEMPTS. APU FAULT EACH TIME. PERFORMED ECU BITE IAW FIM 49-11 FT 987. RESET ECU, APU OPERATION NORMAL.

Part: OIL SYSTEM — LOW (APU) · airframe 85,781 hrs · 17,376 cycles

APU WOULD NOT START AFTER LANDING. APU OIL QUANTITY LOW. SERVICED APU OIL PER AMM 12-13-04. RESTARTED APU, RAN NORMAL, OPS CHECKED GOOD. A/C GOOD FOR CONTINUED SERVICE.

Part: SMOKE DETECTOR — FAULTED (MAIN DECK CARGO) · airframe 85,754 hrs · 17,366 cycles

MAIN DECK CARGO A1 AMBER LIGHT. PERFORMED FIM 26-14-00, MAIN DECK CARGO FIRE DETECTION SYSTEM PROCEDURE IAW B767 IAI SUPPLEMENTAL MX MANUAL. FOUND NR 1A SMOKE DETECTOR AT FAULT. REMOVED AND REPLACED 1A LOOP SMOKE DETECTOR IAW IAI SUPPLEMENTAL MX MANUAL 26-14-01. NO FAULTS NOTED.

Part: NOZZLE — OBSTRUCTED (EXTINGUISHER) · airframe 85,637 hrs · 17,327 cycles

AFT LOWER CARGO HAS 3 FIRE EXTINGUISHER NOZZLES BLOCKED.(<P>REMOVED LINER AND TAPE OBSTRUCTION PER AMM 26-23-00 AND AMM 25-52-01 ON ALL 3 NOZZLES. ALL OTHER NOZZLES CLEAR.</P><P><BR /></P>)

Part: SMOKE DETECTOR — INOPERATIVE (MAIN DECK CARGO) · airframe 85,633 hrs · 17,325 cycles

MAIN DECK CARGO # 7 SMOKE DETECTOR INOP.&NBSP;(<P>TRANSFERRED TO MDDR # 115824 AS PER MEL 26-16-02-01, CAT 'C', DUE DATE 15AUG19.&NBSP;</P><P>LP 1091652 - M2:&NBSP;REMOVED AND REPLACED 7B CARGO SMOKE DETECTOR AND OPS CHECK STILL FAILS. DMI # 15824 REMAINS OPEN. FURTHER T/S NEEDED IAW 767 AMM 26-16-02.</P><P>LP 1091654 - M3:&NBSP;T/S SMOKE DET. #7 CHANNEL B, FOUND DET. OPERATIONAL &AMP; FOUND 28VDC ON PINS 4 &AMP;12 ON CONNECTOR D20298. REQ FUTHER T/S MDDR #115824 REMAINS OPEN.</P><P>LP 1091657 - M1:&NBSP;REINSPECTED FIRE CARGO LIGHT LOOP LIGHTS IAW DMI # 26-16-02-01. ALL CHECKS ARE GOOD. DMI 115824 REMAINS OPEN.</P><P>LP 1091659 - M4:&NBSP;REMOVED AND RE-INSTALLED FOR T/S MAIN CARGO SMOKE DET CONTROL PANEL. FOUND LOOSE CONNECTOR, RE-SECURED CONNECTOR IAW AMM 26-14-00. SYSTEM OPERATES NORMAL. THIS CLEARS MDDR 115824, PLACARDS REMOVED.</P>)

Part: STARTER — FAILED (APU) · airframe 85,623 hrs · 17,321 cycles

APU RELIABILITY COLD START ACCOMPLISHED ON FLIGHT LEG ONT-RFD SAT -46, FL 410, 3 ATTEMPTS UNSUCCESSFUL.(<P>NOTED BY MX. THIS CLOSES MDDR 115734, APU DEFERRED. REF LP 1091648 - ITEM 7.</P><P>LP 1091648 - M7: TRANSFERRED TO MDDR # 115774 IAW DDG 49-11-01A, CAT 'C', DUE DATE: 14-AUG-2019. PLACARDS INSTALLED.&NBSP;</P><P>LP 1091649 - M2:&NBSP;BIT ECU IAW 49-11 FT 987, RECEIVED SEE MAINT MANUAL ON SHUT DOWN 1 TO 4, NO FAULTS NOTED ON ECU SELF TEST. MINI FLAGS 36 38 42 66 OBSERVED. DUE TO IGV ACTUATOR PREVIOUSLY REPLACED, PLACED ECU ON ORDER WITH MCC. DMI 115774 REMAINS OPEN.</P><P>LP 1091667 - M4: REMOVED AND REPLACED APU STARTER MOTOR REF AMM 49-41-01. LEAK &AMP; CHECK GOOD.

Part: ACTUATOR — FAILED (APU) · airframe 85,620 hrs · 17,320 cycles

APU COLD SOAK START FL 380, -43 C, THREE ATTEMPTS UNSUCCESSFUL. PERFORM APU BITE CHECK IAW FIM 49-11- FT 987. FOUND MINI FLAG 36, 38, 42, 66. FAULTS ECU SCV DRIVER SHORTED, ECU IGV ACTUATOR FAIL AND POSITION OF IGV NOT MATCHING. R & R APU IGV ACTUATOR IAW AMM 49-52-02. PERFORMED FIM 49-11 FT 987 APU BITE PROCEDURE, NO FAULTS NOTED. NO FLAGS NOTED. PERFORMED OPS CHECK OF APU IAW AMM 49-11-00, OPS CHECKED GOOD.

Part: WARNING LIGHT — MALFUNCTIONED (FIRE DETECTION) · airframe 85,620 hrs · 17,319 cycles

MAIN CARGO FIRE DETECTION PANEL ANNUNCIATOR LIGHT REMAINS ILLUMINATED AT LOCATION 7B. C/W PROCEDURES IAW MEL 26-16-02-01 AND AMM 26-00-00/901. OPS CHECK GOOD, NO FURTHER DEFECTS NOTED.

Part: APU — MALFUNCTIONED · airframe 85,567 hrs · 17,300 cycles

APU INOP, 3 ATTEMPTS. PERFORMED APU ECU BIT CHECK. MINI FLAGS 21,26,29,36,38,42,48 AND 66 DISPLAYED. FURTHER T/S REQUIRED. SUCCESSFUL APU START 1 OF 3 ATTEMPTS. IAW AMM 49-11-00 + 49-61-05. REMOVED & REPLACED APU ECU. OPS CK GOOD. 3 SUCCESSFUL STARTS. DURING 3RD RUN APU AUTO SHUTDOWN. ECU FAULTED REVERSE FLOW REF AMM 29-22-02 &AMP; 49-61-05. REMOVED AND REPLACED REVERSE FLOW MODULE IAW AMM 49-53-08, NO FIX REMOVED AND REPLACED APU INLET TEMP SENSOR IAW AMM 49-61-03, NO FIX. SUSPECT FAULTY CHECK VALVE. PERFORMED FIM 49-11 FAULT TREE A04 AND FOUND ECU TO BE FAULTY, NO ECU IN STOCK AT CVG, REMOVED AND REPLACED APU& ECU IAW AMM 49-61-01. OPS CHECK GOOD AT THIS TIME.

Part: SOLENOID VALVE — MALFUNCTIONED (APU) · airframe 85,559 hrs · 17,298 cycles

APU INFLT START ATTEMPT, FAILED 3 TIMES FL 40000, MAX RPM NOTED 48. OAT -45. (<P>MCC NOTIFIED. THIS BECOMES DMI 115399 MEL 49-11-01A, CAT 'C', DUE: 06AUG19.</P><P>LP 1080632 - M5: REMOVED AND REPLACED DE-OIL SOLENOID VALVE WITH OVERHAULED UNIT REF AMM 49-27-08. OPS &AMP; LEAK CHECKS ARE GOOD. THIS CLEARS DMI #115399.&NBSP; PLACARDS REMOVED. MCC NOTIFIED.&NBSP;</P>)

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 85,555 hrs · 17,297 cycles

APU RELIABILITY COLD START ACCOMPLISHED ON FLIGHT LEG ONT-RFD SAT -47&NBSP; FL 410, START UNSUCCESSFUL ON 3 ATTEMPTS.(<P>C/W OPS CHECK OF APU. NO DEFECTS NOTED, APU STARTS SUCCESSFULLY.&NBSP; APU COLD START MDDR 115327 REMAINS OPEN IAW AMM 49-11-00.</P><P>LP 1090199 - DUE TO APU FAILED TO START ON 3 ATTEMPTS. APU WAS PLACED ON DEFERRAL.&NBSP;</P>)

Part: UNKNOWN — MALFUNCTIONED (COCKPIT TEMP) · airframe 85,555 hrs · 17,297 cycles

FLIGHT DECK TRIM AIR VALVE POSITION INDICATOR WILL NOT MOVE TO FULL COLD POSITION WHEN FLIGHT DECK COMPARTMENT TEMPERATURE CONTROL IS MOVED TOWARD "C".(<P>PERFORMED OPS CHECK OF FLIGHT DECK TEMP CONTROL SYSTEM. OPS CHECK NORMAL. ALSO VERIFIED TRIM AIR VALVE OPERATES NORMALLY. ALL WORK IAW AMM 21-51-00.</P>)

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 85,545 hrs · 17,294 cycles

APU RELIABILITY COLD START FAILED ON FLT LEG BWI-PDX SAT -42 FL 400. UNSUCCESSFUL 3RD ATTEMPT. (<P>PERFORMED BITE CHECK OF APU PER AMM 49-00-00. NO FAULTS NOTED. APU START SUCCESSFUL 1ST ATTEMPT ON GROUND.<BR /></P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 85,500 hrs · 17,279 cycles

APU FAULT EICAS MESSAGE. (<P>PERFORMED ECU BITE IAW AMM 49-61-05, NO FAULTS NOTED. TEST OK, APU START 2ND ATTEMPT. PILOT WAS 1ST ATTEMPT.<BR /></P>)

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 85,485 hrs · 17,276 cycles

RT SIDE WINDOW EICAS MSG. (<P>PER MGT REQUEST, SWAPPED L AND R WINDOW HEAT CONTROLLERS. R FWD - L SIDE (PN 624066-4, SN 034C-558), L FWD - R SIDE (PN 624066-5, SN 0830-2675) REF AMM 30-41-01. BITE CK GOOD.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 85,469 hrs · 17,270 cycles

EICAS "R SIDE WINDOW", QRH DID NOT CLEAR. (<P>PERFORMED BOEING 767 FIM 30-41 FT 803, NO DEFECTS NOTED. OPERATED WITH NO EICAS MSG.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 85,463 hrs · 17,267 cycles

R SIDE WINDOW EICAS MESSAGE.(<P>PERFORMED FIM 30-41 FT 803, LEFT FWD OR RIGHT SIDE WINDOW ANTI-ICING BITE PROCEDURE. NO FAULTS NOTED, NO EICAS MSG PRESENT.<BR /></P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (EXHAUST FAN) · airframe 85,381 hrs · 17,240 cycles

AFT EQUIPMENT EXHAUST FAN 2 STATUS MESSAGE. PROCEDURES COMPLIED WITH FIM CH 21-26-00 FT 808. NO OTHER ISSUES NOTED, OK FOR CONTINUED SERVICE.

Part: CONNECTOR — UNSECURE (SHUTOFF VALVE) · airframe 85,375 hrs · 17,238 cycles

RIGHT ENG BLEED EICAS MESSAGE.(<P>RE-RACKED BLEED AIR CONTROL CARD, VISUALLY INSPECTED RH ENGINE PRSOV, REMOVED CONNECTORS, CLEANED, AND RE-SECURED CONNECTORS. PERFORMED BITE TEST TO PNEUMATIC CONTROL, ALL FAULTS CLEARED. OPS CHECK NORMAL, REF B767 FIM 36-10 FOR WORK PERFORMED.</P>)

Part: ACTUATOR — FAULTY (APU BAY) · airframe 85,371 hrs · 17,237 cycles

APU DOOR STATUS MSG.(<P>PERFORMED OPS CHECK&NBSP; IAW AMM 49-11-00 OPS CHECK GOOD AT THIS TIME.</P><P>LP 1084011 - M8: TRANSFERRED TO MDDR 113785</P><P>LP 1084015 - M2:&NBSP;TROUBLESHOOTED IAW WDM 49-15-11. FOUND GROUND @ PIN 1 OF K547. W/ APU INLET DOOR OPEN. INTERNAL SWITCHING OF APU INLET DOOR ACTUATOR FAULTY. DMI # 113785 REMAINS OPEN.</P><P>LP 1084018 - M2: REMOVED AND REPLACED THE APU&NBSP;AIR INTAKE DOOR ACTUATOR IAW AMM 49-15-06. OPS CHECK GOOD AT THIS TIME. THIS CLEARS MDDR 113785.</P>)

Part: BLADE — NICKED (RT ENGINE FAN) · airframe 85,259 hrs · 17,199 cycles

FOUND TWO NICKS IN R ENGINE, FAN BLADES 4 AND 5.(<P>NICKS DEPTH WERE 1/16 (TH) INCH. MAX BLEND ALLOWED IS 1/2 INCH. BLENDED PER B767 AMM 72-31-02 AREA C. COMPLETED FPI INSPECTION PER B767 AMM 70-11-06-232-001-H00.

Part: GASKET — LEAKING (FUEL PANEL) · airframe 85,264 hrs · 17,201 cycles

FOUND FUEL LEAKING FROM PANEL 541QB. REMOVED AND REPLACED FUEL PANEL SEALS IAW AMM 28-11-10. LEAK CHECK GOOD, NO FURTHER DEFECTS. DUE TO LEAKING FUEL FUEL PANEL CHANGED FUEL PANEL GASKET IAW 28-11-01. LEAK CHECK GOOD, NO FURTHER DEFECTS NOTED.

Part: ECU — MALFUNCTIONED (APU) · airframe 85,253 hrs · 17,196 cycles

FOUND APU NOT SUPPLYING DUCT PRESSURE WITH VALVE ON.(<P>REMOVED AND REPLACED THE ECU IAW AMM 49-61-05. OPS CHECK GOOD.

Part: SKIN — GOUGED (BS 1228-1229) · airframe 85,236 hrs · 17,191 cycles

GOUGE ON AIRCRAFT SKIN AT STA 1229, S 27 RBL AND S 26 RBL.(<P>PERFORMED INSPECTION OF DAMAGE, FOUND TO BE WITHIN LIMITS IAW SRM 53-00-01. DENT GOUGE REMOVED IAW SRM 51-10-02. NO FURTHER DEFECTS NOTED.&NBSP;</P><P>LP 1074740 - M5: HFEC NDT INSPECTION REQUIRED. TRANSFERRED TO NON-MEL 112528.</P><P>LP 1074741:&NBSP;DAMAGED AREA CLEAN OUT PERFORMED ON LP 1074743 - ITEM M7 AND EDDY CURRENT INSPECTION DONE ON LP 1074742 - ITEM M6. DAMAGE FOUND TO BE IN ALLOWABLE LIMITS. THIS CLEARS NON-MEL 112528 AND MCC NOTIFIED.&NBSP;</P>)

Part: IDG — UNKNOWN (LT ENGINE) · airframe 85,227 hrs · 17,188 cycles

DUE TO HISTORY OF LEFT GEN DRIVE LIGHT SLOW TO EXTINGUISH AND REQUEST, REMOVE AND REPLACE LT ENG IDG. (<P>REMOVED AND REPLACED&NBSP;LT ENG IDG IAW AMM 24-11-01. OPS CHECKED IAW AMM 24-11-00, OPS CHECK GOOD. LEAK CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.</P>)

Part: SENSOR — FAILED (INLET PRESSURE) · airframe 85,227 hrs · 17,188 cycles

NO APU DUCT PRESSURE. T/S APU, BITE THE ECU PER AMM/FIM 49-11 FT 98. FOUND P2 SENSOR FAULT. CLEARED ECU, CLEANED P2 SENSOR, RAN APU AND DUCT PRESSURE WAS 30/30 WITH 1 PACKS ON, 2 PACKS ON 25/26. REMOVED AND REPLACED INLET PRESSURE (P2) SENSOR IAW AMM 49-61-04. OPS CHECK AND BITE TEST GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 85,211 hrs · 17,184 cycles

L GEN DRIVE LIGHT AND EICAS L GEN DRIVE STAY ON FOR APPROX 1 MINUTE, THEN GO AWAY. (<P>PERFORMED ENGINE (LT) IDLE RUN IAW AMM 71-00-00. OPS CHECKED LT GENERATOR PER AMM 24-10-00. OPS CHECK&NBSP;NORMAL.</P>)

Part: SMOKE GOGGLES — MISSING (COCKPIT) · airframe 84,477 hrs · 16,971 cycles

COCKPIT SMOKE GOGGLES MISSING 3RD SUPERNUMERARY SEAT. (<P>INSTALLED SMOKE GOGGLES AT 3RD SUPERNUMERARY SEAT PER AMM 25-64-00. CHECK OK.</P>)

Part: SWITCH — FAULTY (RAM AIR TURBINE) · airframe 84,477 hrs · 16,971 cycles

RAT UNLOCKED ONCE LANDED. (<P>REMOVED AND REPLACED RAT UP LIMIT SW S369 PER AMM 29-21-17. ACCOMPLISHED RAT SYSTEM TEST OK. AMM&NBSP; 29-21-00.</P>)

Part: STARTER — DEFECTIVE (NR 2 ENGINE) · airframe 84,477 hrs · 16,971 cycles

#2 ENGINE STARTER HAS NO ACCEPTABLE METAL PARTICLES. (<P>REMOVED AND REPLACED #2 ENGINE STARTER. PER AMM 80-11-01 OPS AND LEAK CHECK NORMAL.</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 85,162 hrs · 17,168 cycles

WXR SYS STATUS MESSAGE. &NBSP;(<P>T/S PER FIM 34-43 FT 801. CLEARED MSG, NO FURTHER FAULTS NOTED AT THIS TIME.&NBSP;</P>)

Part: SHUTOFF VALVE — MALFUNCTIONED (APU) · airframe 85,155 hrs · 17,166 cycles

APU AIR INOP&NBSP;(<P>CHECKED AND DEFERRED TO MDDR 111916. CAT C APU AIR INOP PER DDG 49-11-01-01, APU VALVE LOCKED CLOSED PER DDG 36-11-01. </P><P>LP 1079436 - M6:&NBSP;T/S PER AMM 49-11-00.OPS CHECK APU WITH NO FAULTS NOTED. PER MCC DMI 111916 CONTINUES. C/W MEL 36-11-04 MX ACTIONS.</P><P>LP 1079441 - M4: R&AMP;R APU AIR SUPPLY SHUTOFF VALVE IAW AMM 36-11-10, OPS CHECK GOOD. THIS CLEARS DMI 111916. PLACARD REMOVED. MCC NOTIFIED.&NBSP;JL @ 14:25Z.</P>)

Part: IDG — LOW (LT ENGINE) · airframe 85,167 hrs · 17,169 cycles

AFTER ENGINE START, "L GEN DRIVE" EICAS MSG WITH L DRIVE OVHD LIGHT AND L GEN OFF LIGHT. REMOVED ILLUMINATED FOR ABOUT 30 SEC AFTER L ENG AT IDLE THEN WENT OUT.(<P>BITE BPCU IAW FIM 24-20 FAULT TREE 801. L GEN OIL LOW MESSAGE FAULT DISPLAYED. SERVICED IDG OIL IAW AMM 12-13-02. OIL LEVEL CHECK GOOD.<BR /></P>)

Part: CONTROLLER — MALFUNCTIONED (WINDOW HEAT) · airframe 85,011 hrs · 17,126 cycles

L3 WINDOW HEAT INOP.(<P>TRANSFER TO MDDR 111036 IAW DDG 30-41-01-03CAT C DUE DATE 11 MAY-19.</P><P>LP 1050441: REMOVED AND REPLACED&NBSP;WINDOW HEAT CONTROLLER FOR L3 WINDOW IAW AMM 30-41-01. OPS CHECK OK. THIS CLEARS MDDR 111036. DISPATCH SK@0412Z<BR /></P>)

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 84,980 hrs · 17,118 cycles

APU WOULD NOT START AFTER LANDING. APU FAULT DISPLAYED, ATTEMPTED START 3 TIMES WITH SAME FAULT.&NBSP;(<P>BITE CHECK FCM PER AMM 49-11-00. NO FAULTS DISPLAYED, PERFORMED APU START, 1 ATTEMPT SUCCESSFUL PER AMM 49-11-00. OPS CHECK GOOD.&NBSP;</P>)

Part: CONNECTOR — BROKEN (WINDOW HEAT) · airframe 84,914 hrs · 17,101 cycles

RH SIDE WINDOW HEAT INOP. FOUND BROKEN CONTACT AT RT SIDE WINDOW HEAT, PLACED P/N CW02-2010 TERM C KIT02-2010 PER TABLE 5 IAW SWPM 20-64-16. REMOVED AND REPLACED R2 WINDOW CONNECTOR D1906 J-B IAW WDM 30-41-11 AND SWPM 20-30-12. OPS CHECK GOOD IAW AMM 30-41-00 AT THIS TIME.

Part: OIL SYSTEM — LOW (LT IDG) · airframe 84,885 hrs · 17,095 cycles

LEFT GENERATOR TOOK APPROX. 2 MINUTES TO COME ONLINE AFTER ENGINE START WITH ASSOCIATED EICAS L GEN DRIVE OFF. PERFORMED BPCU BITE IAW FIM 24-20 TASK 801. FOUND IDG LOW OIL PRESSURE. SERVICED PER AMM 12-13-03. PERFORMED ENG RUN PER AMM 71-00-00. FOUND NO FAULTS, IDG LEAK CHECKS GOOD. BPCU BITE, FOUND NO FAULTS. IDG OPS CHECKS GOOD. NO FURTHER DEFECTS.

Part: OIL SYSTEM — LOW (IDG) · airframe 84,885 hrs · 17,095 cycles

LEFT GENERATOR TOOK APPROX. 2 MINUTES TO COME ONLINE AFTER ENGINE START WITH ASSOCIATED EICAS L GEN DRIVE OFF.(<P>PERFORMED BPCU BITE IAW FIM 24-20 TASK 801. FOUND IDG LOW OIL PRESSURE. SERVICED PER AMM 12-13-03. PERFORMED ENG RUN PER AMM 71-00-00. FOUND NO FAULTS, IDG LEAK CHECKS GOOD. BPCU BITE, FOUND NO FAULTS. IDG OPS CHECKS GOOD. NO FURTHER DEFECTS.</P>)

Part: SWITCH — STUCK (FUEL PUMP) · airframe 84,877 hrs · 17,092 cycles

DURING INSIDE DAILY CHECK, FOUND LEFT FWD FUEL PUMP SWITCH STUCK.(<P><SPAN>REMOVED AND REINSTALLED SWITCH, CLEANED DEBRIS FROM CASE, AND RELAMPED. OPS CHECK OK PER B767 REF AMM 33-13-00.</SPAN><BR /></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT GENERATOR) · airframe 84,814 hrs · 17,077 cycles

L GEN DRIVE EICAS MESSAGE AFTER LEFT ENGINE START FOR APPROX 45 SECONDS(<P>LEFT ENGINE IDG OIL LEVEL FULL AND OPS CHECK GENERATOR DRIVE SYSTEM IAW AMM 24-11-02 TEST GOOD</P>)

Part: CONTROLLER — FAULTED (CABIN PRESSURE) · airframe 84,563 hrs · 16,998 cycles

CABIN ALT. AUTO 2 STATUS MESSAGE.&NBSP;(<P>PERFORMED FIM 21-31 FT 803 AT STEP 2 FOUND CONTROLLER M119 FAULT CONTROLLER. SWAPPED CONTROLLER M118 AND M119 PER B767 AMM 21-31-02 FAULT FOLLOWS, CONTROLLER ORDERED. TRANSFERRED MDDR 107776 AS PER DDG 21-21-01A CAT "C"&NBSP;&NBSP;R&AMP;R AUTO PRESSURE UNIT ASSY. NO 2 REF.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (WINDOW HEAT) · airframe 84,533 hrs · 16,990 cycles

R SIDE WINDOW EICAS IN CRUISE. CYCLED R SIDE WINDOW HEAT SWITCH. AS PER QRH, FAULT CLEARED(<P>PERFORMED BIT CHECK ON R2 WINDOW HEAT CONTROLLER, NO FAULTS NOTED AT THIS TIME. SYSTEM OPS CKS NORMAL IAW AMM 30-41-00.</P>)

Part: BLOWER — FAILED (SMOKE DETECTOR) · airframe 84,479 hrs · 16,972 cycles

CARGO DET AIR, FWD DET FAN EICAS MESSAGE(<P>R/R M716 FWD DET BLOWER IAW AMM 26-16-02. OPS CHECK NORMAL&NBSP;</P>)

Part: BLOWER — LEAKING (SMOKE DETECTOR) · airframe 84,479 hrs · 16,972 cycles

NO.2 FWD CARGO SMOKE DET BLOWER (M717) HAD GLUE FLUID LEAKING FROM CASE.&NBSP;(<P>PERFORMED OPS CHECK TO M717, FOUND NORMAL IAW AMM 26-16-02. CLEANED AREA FROM GLUE ON ASSEMBLY IAW 20-30-02.</P>)

Part: GENERATOR — TRIPPED (APU) · airframe 84,443 hrs · 16,957 cycles

APU GEN DROPPING OFF LINE. DROPPED OFF LINE 4 TIMES AT LEAST.(<P>PERFORMED OPERATIONAL TEST ON APU GEN IAW AMM 49-00-00. OPS CHK NORMAL.</P>)

Part: GCU — INOPERATIVE (APU GENERATOR) · airframe 84,433 hrs · 16,954 cycles

APU GEN INOP. FREQ LOW, AIR OK(<P>TRANSFERRED TO MDDR # 106940 AS PER MEL 49-11-01A CAT C&NBSP;</P><P>LP 1053779-3 (RIV) -&NBSP;PFMD BPCU BITE IAW FIM 24-20 FT 801 FOUND APU&NBSP; GENERATOR CONTROL UNIT FAULTING. REMOVED AND REPLACED APU GCU IAW AMM 24-22-02 OPS CHECK GOOD NO FURTHER DEFECT NOTED. MCC ADVISED - PLACARDS REMOVED.</P><P>NOTE: NO NEED FOR APU COLD SOAK START VERIFICATION DUE FAULT ONLY INVOLVING APU GENERATION (NOT STARTING CIRCUIT)&NBSP;</P><P><BR /></P>)

Part: GCU — MALFUNCTIONED (LEFT) · airframe 84,302 hrs · 16,907 cycles

LEFT ENG GEN OFF LIGHT&NBSP;(<P>TRANSFERRED TO MDDR # 105940 AS PER MEL 24-00-01-01 CAT B&NBSP;</P><P>LOG PAGE 706715&NBSP;ACCOMPLISHED BPCU BITE PER FIM 24-20/801 NO FAULTS NOTED, SERVICE LEFT IDG PER AMM 12-13-03, RAN ENGINES PER AMM 71-00-00 NO FAULTS , REMOVED AND REPLACED LEFT GCU PER AMM 24-22-02 , LEFT GENERATOR OPS CHECK GOOD PER AMM 24-22-00 , MDDR CLOSED ,&NBSP;</P>)

Part: SWITCH — DEFECTIVE (OIL SYSTEM) · airframe 84,326 hrs · 16,916 cycles

L ENG OIL PRESS DISAGREE LIGHT WILL NOT ILLUMINATE.(<P>R&AMP;R L-ENG KORY SWITCH IAW AMM 79-33-01 OPS CHECK GOOD. NO FURTHER FAULT AT THIS TIME.<BR /></P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 84,194 hrs · 16,869 cycles

CABIN ALT AUTO #2 STATUS MESSAGE(<P>BITE CHECK CABIN ALT 2 CONTROLLER IAW B767 AMM 21-31-00, BITE &AMP; OPS CHECKED GOOD</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 84,056 hrs · 16,816 cycles

STATUS MESSAGE AFT EQ EXH FAN 2. T/S IAW FIM 21-26 FAULT TREE 808, NO FAULTS FOUND. SYSTEM OPS CHECK NORMAL.

Part: STARTER — FAULTY (APU) · airframe 84,052 hrs · 16,815 cycles

APU INOP. FAULT FOUND WITH STARTER MOTOR. REMOVED AND REPLACED STARTER IAW AMM 49-11-01, OPS CHECK NORMAL.

Part: CONTROL UNIT — FAULTY (APU) · airframe 84,037 hrs · 16,811 cycles

APU EGT OVERTEMP. REMOVED AND REPLACE APU CONTROL UNIT IAW AMM 49-61-05. OPS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 84,032 hrs · 16,809 cycles

APU FAULT. PERFORMED APU BITE AND OPS CHECK PER AMM 49-11-00. OPS CHECKED GOOD.

Part: APU — INOPERATIVE (APU BAY) · airframe 84,029 hrs · 16,808 cycles

APU INOP. TRANSFERRED TO MDDR 104068, AS PER DDG 49-11-01A CAT 'C".

Part: ACTUATOR — FAULTY (APU) · airframe 84,032 hrs · 16,809 cycles

APU INOP. PERFORMED BITE PROCEDURE OF APU ECU IAW AMM 49-61-05. ECU WAS FOUND TO HAVE FLAGS 38,42, & 66. FLAGGING LRU INDICATE IGV ACTUATOR FAULTING. R&R APU IGV ACTUATOR IAW AMM 49-52-02. OPS CHECK GOOD.

Part: EGT INDICATION — FAULTED (APU) · airframe 83,998 hrs · 16,799 cycles

APU WOULD NOT START, 3 ATTEMPTS EICAS MSG APU FAULT. APU START ON FIRST ATTEMPT FOUND PREVIOUS FAULTS EGT OVERHEAT AND START ABORTED NO OTHERS FAULTS. OPS CHECK GOOD.

Part: CIRCUIT CARD — FAULTY (OVERHEAT SYS) · airframe 83,958 hrs · 16,782 cycles

AFTER START FIRE/OVHT SYS EICAS CAUTION. R&R RT ENG FIRE OVERHEAT CARD IAW AMM 26-10-01. OPS CHECK GOOD. DMI REMAINS OPEN FOR FURTHER T/S. P/N OFF: 6445-01, S/N OFF: 15325. THE STATUS MESSAGE HAS BEEN CLEARED AND NEVER SHOWED BACK.

Part: WARNING LIGHT — FALSE ACTIVATION (LT GENERATOR) · airframe 83,942 hrs · 16,774 cycles

FOUND LEFT ENGINE GENERATOR FIELD OFF LIGHT ILLUMINATED ON P61 PANEL&NBSP;(<P>RESET GENERATOR LEFT ENGINE AND RON LEFT AT IDLE. NO DEFECTS NOTED IAW AMM 71-00-00&NBSP;</P>)

Part: ACTUATOR — NOT REPORTED (APU) · airframe 83,933 hrs · 16,769 cycles

APU PLACED ON DEFERAL&NBSP;DUE TO BLEED ISSUES&NBSP;(<P>OPENED MEL 49-11-01 MDDR 103112</P><P>REF LOGPAGE 1008682 - REMOVED AND REPLACED IGV ACTUATOR PER AMM 49-53-02; MDDR 103112 CLEARED AT THIS TIME.</P>)

Part: FIRE LOOP — MALFUNCTIONED (RT ENGINE) · airframe 83,933 hrs · 16,769 cycles

R ENG FIRE LP 1 STATUS MSG(<P><SPAN>REMOVED / AND REPLACED UPPER AFT FIRE LOOP ON #2 ENG IAW B767 AMM 26-11-02-424.&NBSP; OPS / CHECK GOOD</SPAN></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (APU) · airframe 83,912 hrs · 16,758 cycles

APU FAULT MESSAGE DISPLAYED DURING A START ATTEMPT AFTER LANDING. APU STARTED NORMAL, NO FAULT MESSAGE DISPLAYED, NO DEFECTS NOTED IAW AMM 49-11-00.

Part: ECU — MALFUNCTIONED (APU) · airframe 83,908 hrs · 16,756 cycles

APU HAD NO BLEED AIR. REMOVED AND REPLACED THE APU ECU IAW AMM 49-61-05. APU OPS CHECKED GOOD.

Part: FIRE LOOP — OUT OF POSITION (RT ENGINE) · airframe 83,892 hrs · 16,751 cycles

STATUS MESSAGE RIGHT ENGINE FIRE LOOP 1. TRANSFERRED TO MMDR 102578 REFERENCE DDG 26-11-01-01 CAT "C". PERFORMED VISUAL INSPECTION OF RIGHT ENGINE FIRE LP1 FOUND&NBSP; LOOP TOUCHING METAL IN NUMEROUS SOTS REPOSITION LOOP AWAY&NBSP; FROM CONTACT OPS CHECK SYSTEM&NBSP; CHECK NORMAL IAW AMM 26-11-00.

Part: SELECTOR — FAILED (CABIN TEMP) · airframe 83,886 hrs · 16,748 cycles

AFT CABIN TEMP INOPERATIVE PRIOR TO START. REMOVED AND REPLACED CABIN ZONE TEMP SELECTOR IAW AMM 21-61-04 AND SEATED THE CABIN TRIM AIR VALVE CONNECTOR IAW AMM 21-61-07. OPS CHECKED GOOD.