N1093A

Part: WARNING MESSAGE — ILLUMINATED (RT A/C PACK) · airframe 93,462 hrs · 15,802 cycles

WHEN ADVANCING THRUST LEVERS FOR TAKEOFF, "RIGHT PACK TEMP" EICAS MESSAGE APPEARED. A/C ABORTED TAKE-OFF (ATO) AND RETURNED TO GATE (BTB). MTX GROUNDED A/C, MTX DEFERRED RIGHT HAND PACK IAW ABX-MEL 21-51-1-1 MX ACTION C/W AND PLACARD INSTALLED A/C RELEISED NO ETOPS ,MX ACTION PROCEDURE 21-51-2 C/W . AND RETURNED A/C TO SERVICE.

Part: START VALVE — FAULTED (LT ENGINE) · airframe 93,415 hrs · 15,782 cycles

ON TAXI OUT, LEFT ENGINE START VALVE DISCREET LIGHT ON. AIRCRAFT RETURNED TO BLOCKS (BTB). MAINTENANCE ACTUATED START VALVE IAW B767 AMM 80-11-02 DUE TO FAILED START. NO FURTHER DEFECTS NOTED A/C REMAINS NO ETOPS. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (ZONE 400) · airframe 93,325 hrs · 15,748 cycles

DURING TAXI OUT L REV ISLN VALVE LIGHT ILLUMINATED ON GROUND A/C RETURNED TO THE GATE(BTB0 AND MTX GROUNDED A/C. MTX PERFORMED THRUST REVERSER BITE TEST AND MSG. CLEARED IAW B767 AMM 78-36-07. MTX RETURNED A/C TO SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 92,012 hrs · 15,244 cycles

DURING TAXI, ICE DET OFF EICAS MESSGAE AFTER ENGINE START. A/C RETURNED TO GATE (BTB) AND MTX GROUNDED A/C , MTX. PERFORMED OPS CHECK AND SYSTEM CHECKED OK IAW AMM 30-81-00. RETURNED A/C TO SERVICE .

Part: UNKNOWN — LEAKING (FUEL) · airframe 91,374 hrs · 15,006 cycles

AFTER PUSH BACK GROUND CREW REPORTED FUEL LEAKING FROM #2 ENGINE A/C RETURNED TO THE GATE (BTB) AND MTX GROUNDED AC. MTX THEN RAN ENGINE AND PERFORMED POWERPLANT TEST NO 3. IAW B767 AMM 71-00-00. FUEL LEAK STOPED. NO DEFECTS NOTED AT THIS TIME. A/C REMAINS NO ETOPS.MTX RETURNED AC TO SERVICE.

Part: PUMP — LOW PRESSURE (FUEL BOOST) · airframe 91,359 hrs · 15,000 cycles

DURING TAXI THE CTR R FUEL PUMP EICAS MESSAGE APPEARED , AC RETURNED TO GATE(BTB) AND MTX GROUNDED AC . MTX VERIFIED LOW FUEL IN CENTER TANK. TRANSFERRED FUEL OUT OF CENTER TANK IAW 28-26-00. RH CENTER PUMP OPERATES NORMAL. A/C REMAINS NO ETOPS.AND RETURNED AC TO SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (BLEED SYS) · airframe 91,359 hrs · 15,000 cycles

DURING TAXI RH BLEED OFF AFTER START . AC RETURNED TO GATE (BTB) AND MTX GROUNDED AC . MTX RAN RH ENGINE AND RESET RT BLEED AIR IAW AMM 71-00-00 OPS CHECK GOOD AC REMAINS NO ETOPS 180 . MTX RETURNED AC TO SERVICE .

Part: SHUTOFF VALVE — MALFUNCTIONED (RT ENGINE) · airframe 91,268 hrs · 14,966 cycles

DURING TAXI OUT , RH ENGINE BLEED VALVE OFF REGARDLESS OF THE POSITION AFTER STARTING ENGINE. AC RETURNED TO GATE(BTB) AND MTX GROUNDED AC , TROUBLE SHOT AND REPLACED RH PRSOV IAW AMM 36-11-09 OPS CK AND LEAK CK GOOD. INSPECTED HPSOV, PRC AND PRV LINES AND FITTING NO DEFECT FOUND. A/C REMAIN NO ETOPS. AND RETURNED AC TO SERVICE

Part: WARNING MESSAGE — ILLUMINATED (COOLING FAN) · airframe 91,247 hrs · 14,958 cycles

DURING TAXI OUT  FWD EQUIPMENT SUPPLY FAN #1 STATUS MESSAGE APPEARED AND AC RETUNED TO GATE (BTB) AND MTX GROUNDED AC , MTX DEFERRED FOR DEPARTURE IAW MEL ABX-21-58-3-2-1 . AND RETURNED AC TO SERVICE .

Part: WARNING MESSAGE — FALSE ACTIVATION (ACCESS DOOR) · airframe 91,124 hrs · 14,911 cycles

E/E ACCESS DOOR EICAS MSG ON T/O RTF PER FLIGHT CONTROL AND MX CONTROL. EVENT OCCURED BETWEEN 700 - 1500 FEET AGL (ATB) AND MTX GROUNDED AC . MTX INSPECTED AC AND DEFERRED MEC DOOR INDICATION FOR DEPATURE IAW MEL ABX -52-71-1-1 AND RETURNED AC TO SERVICE .

Part: ANTI-ICE VALVE — FAULTED (RT ENGINE) · airframe 91,090 hrs · 14,894 cycles

DURING TAXI WITH BOTH ENGINES RUNNING AND ENGINE ANTI-ICE SELECTED ON WE OBSERVED THE RIGHT ENGINE ANTI-ICE VALVE LIGHT ILLUMINATED AND A RIGHT ENGINE ANTI-ICE AMBER MESSAGE AC RETURNED TO GATE( BTB) AND MTX GROUND AC . TROUBLESHOT AND FOUND MX PROCEDURES FOR MEL 36-11-8-1-1A-1 NOT C/W CORRECTLY (PRV WAS LOCKED CLOSED, HPSOV NOT LOCKED, OVERPRESSURE SWITCH NOT DISCONNECTED CAPPED AND STOWED) APPLIED/REAPPLIED DEACTIVATION PROCEDURES PER ABX MPM 36-11-8-1-1A-1. OPS CHECK GOOD. DI REMAINS OPEN. A/C REMAINS NO ETOPS..MTX RETURNED AC TO SERVICE

Part: BRAKE ASSY — FIRE (ZONE 700) · airframe 90,734 hrs · 14,751 cycles

AS AC TAXIED INTO GATE MTX NOTICED LH GEAR WAS SMOKING , MTX CALLED FOR FIRE RESCUE TO EXTINGUISH . AFTER ALL WAS GOOD AND BRAKES AND WHEELS COOLED MTX GROUNDED AC . MTX REPLACED REMOVED #1 AND #5 WHEELS AND BRAKES .. C/W B767 AMM 05-51-14 BRAKE TEMPS AT BLOCK IN WERE NOT OBSERVED ON EICAS B767 AMM SUBTASK CONDITIONAL INSPECTION IF FUSES MELTED 05-51-14-882-110 NO DEFECTS FOUND ON ANY AXEL ON LH TRUCK NO DEFECTS. REPLACED #1 AND #5 WHEEL AND BRAKES IAW AMM 32-41-00 AND 32-45-00. C/W ANTI- SKID TEST PER B767 AMM 32-42-00-705-027 NO DEFECTS . C/W PARKING BRAKE OPS TEST IAW AMM 32-44-00-730-801 NO DEFECTS .C/W FLIR DIGITAL IMAGING SCAN OF LH MLG BRAKES AFTER HEAVY BRAKING PER 767 AMM 20-10-75-750-801 , ALL VALUES WITHIN LIMITS PER AMM 32-46-00 NO BRAKE WAS OVER 470 DEG C OR LEVEL 5 .AC WAS RETURNED TO SERVICE.

Part: PITOT TUBE — MALFUNCTIONED (ZONE 200) · airframe 90,618 hrs · 14,702 cycles

DURING TAXI FOR EVAL. FLIGHT CAPTIANS PITOT HEAT EICAS MSG APPEARED AND AC RETURNED TO GATE AND MTX GROUNDED AC , AFTER TROUBLE SHOOTING FOUND HEATER COIL FOR CAPTS. UPPER PITOT PROBE SHORTED TO GROUND. REMOVED AND REPLACED LH UPPER PITOT STATIC PROBE IAW B767 AMM 30-31-00 AND 34-11-01. OPS CHECK GOOD . AC WAS RETURNED TO SERVICE .

Part: DRIVE ASSY — LEAKING (LT SLAT) · airframe 90,615 hrs · 14,701 cycles

LEFT WING POWER DRIVE UNIT ASSY LE SLAT WITH EVIDENCE OF LEAK(<P>LEFT WING POWER DRIVE UNIT ASSY L/E SLAT WAS REPLACED I.A.W. AMM 27-81-10-424-023 REV. 142 DATE 22 APR 24. TORQUE APPLIED 67 LB-IN, 125 LB-IN AND 70 LB-IN TORQUE N/S 0224902084 DATE 21 FEB 25, TORQUE N/S 1123126455 DATE 28 NOV 24. ADJUSTMENT AND OPERATIONAL TEST WERE SATISFACTORY. NO LEAK FOUND.</P>)

Part: FUEL TANK — LEAKING (ZONE 100) · airframe 90,615 hrs · 14,701 cycles

FUEL LEAK ON LOWER SURFACE OF CENTER TANK RIGHT SIDE AT RBL 97.42(<P>FUEL LEAK ON LOWER SURFACE OF CENTER TANK RIGHT SIDE AT RBL 97.42 WAS REPAIRED IAW AMM 28-11-00-308-013 REV 142 22APR24. THE FUEL LEAK TEST WAS SATISFACTORY.</P>)

Part: SWITCH — INOPERATIVE (THRUST REVERSERS) · airframe 90,615 hrs · 14,701 cycles

ENG 1 RH T/R INOPERATIVE CDU T/R POSITION SWITCH(<P>ENG 1 RH T/R, CDU T/R POSITION SWITCH WAS REPLACED PER AMM 78-36-01-404-008. NO FURTHER DEFECTS NOTED.</P>)

Part: ANTENNA — CORRODED (FWD VHF) · corrosion level 2 · airframe 90,615 hrs · 14,701 cycles

CORROSION ON UPPER FORWARD VHF ANTENNA(<P>REPLACEMENT OF UPPER FWD VHF ANTENNA&NBSP; WAS PERFORMED IAW AMM 23-12-03- 000-801-001 AND AMM 23-12-03-400-801-001. NO FURTHER DEFECTS NOTED.</P>)

Part: REINFORCEMENT — MECHANIC ERROR (LT WING) · airframe 90,615 hrs · 14,701 cycles

LH WING REINFORCEMENT ANGLE AT STR L-11 BETWEEN RIB 10 AND 11 WITH MIS DRILL HOLES(<P>MIS DRILL HOLES ON REPAIRED LH WING REINFORCEMENT ANGLE AT STR L-11 BETWEEN RIB 10 AND 11 WERE REPAIRED IAW FVCI EO NO. 24097-1 REV. IR. NO FURTHER DEFECTS NOTED.</P>)

Part: ACCESS PANEL — LEAKING (LT WING) · airframe 90,615 hrs · 14,701 cycles

LH WING, ACCESS PANEL 533AB, INNER DRY BAY, ON RIB 6, WITH EVIDENCE FUEL LEAK(<P>LH WING, ACCESS PANEL 533AB, INNER DRY BAY, ON RIB 6, WITH EVIDENCE FUEL LEAK. THE FUEL LEAK WAS REPAIRED IAW AMM 28-11-00-308-013 REV 142 22APR24, FUEL LEAK TEST WAS SATISFACTORY.</P>)

Part: SAMPLE PORT — CONTAMINATED (SMOKE DETECTION) · airframe 90,615 hrs · 14,701 cycles

MAIN DECK SMOKE DETECTION SYSTEM SAMPLING PORTS WITH CONTAMINATION(<P>SMOKE DETECTION SYSTEM SAMPLING PORTS OF MAIN DECK WERE CLEANED IAW AMM 26-19-01-400-801 REV 142, DATE 22 APR 24. NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — DELAMINATED (LT TE FLAP) · airframe 90,615 hrs · 14,701 cycles

DELAMINATION ON LEFT WING, INBOARD MAIN FLAP, LOWER SURFACE(<P>LEFT WING, INBOARD MAIN FLAP, LOWER SURFACE WAS REPAIRED IAW SRM 57-53-01-2R-1 FIG 201 SHEET 2 AND 51-70-03-0G-0 PAR 5A , 25 REV 125 APR 15/2024. NO FURTHER DEFECTS NOTED.&NBSP;</P>)

Part: SKIN — DELAMINATED (ZONE 300) · airframe 90,615 hrs · 14,701 cycles

DELAMIATION ON SKIN OF VETRICAL STABILIZER 3" ABOVE FSS 1195.390 AND NEAR LEADING EDGE(<P>VETRICAL STABILIZER 3" ABOVE FSS 1195.390 AND NEAR LEADING EDGE WAS REPAIRED IAW SRM 55-30-01-2R-1 FIG 201 SHEET 1 NOTE F PAG 1-2 AND SRM 51-70-10-2R--4 REPAIR 4 FIG 201 SHEET 2 PAG 1,4 REV 125 APR 15/2024. NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — DELAMINATED (LEFT TE FLAP) · airframe 90,615 hrs · 14,701 cycles

DELAMINATION ON LEFT WING, INBOARD MAIN FLAP, LOWER SURFACE(<P>LEFT WING, INBOARD MAIN FLAP, LOWER SURFACE WAS REPAIRED IAW SRM 57-53-01-2R-1 FIG 201 SHEET 2 AND 51-70-03-0G-0 PAR 5A , 25 REV 125 APR 15/2024. NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — DELAMINATED (RT NR 9 SLAT) · airframe 90,615 hrs · 14,701 cycles

DELAMINATION ON RIGHT WING, SLAT NO 9, MULTIPLE DENTS ON UPPER SKIN OF TRAILING EDGE WEDGE(<P>&NBSP;RIGHT WING, SLAT NO 9 WAS REP AIRED IAW SRM 57-43-02-2R-1 REP 1 FIG 201 SHEET 2 AND SRM 51-70-10-2R-4 REP AIR 4 FIG 202 SHEET 1 REV 125 APR 15/2024</P>)

Part: LIGHT — UNKNOWN (UNKNOWN) · airframe 88,907 hrs · 14,094 cycles

EMER LIGHTS "UNARMED" LIGHT BROKEN(<P>R/R UNARMED LIGHT IAW B767 AMM 33-11-00. OPS CKS GOOD</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,156 hrs · 13,828 cycles

TWO INERTIA DESCENT DEVICE REELS BROKEN #1 AND #7(<P>PLACED ON DEFERRAL 185160 PER MEL 25-61-01-01 CAT C DUE DATE 17MAY23</P>)

Part: SPRING — UNKNOWN (UNKNOWN) · airframe 88,077 hrs · 13,807 cycles

TWO ESCAPE REELS FELL OUT DURING TAKE OFF. R/R HOLDING SPINGS FOR #2 AND #3 INERTIA REEL IAW SRM 51-40-02 AND AMM 25-61-00. OPS CHECK GOOD AT THIS TIME.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 87,862 hrs · 13,735 cycles

EXIT SIGN BY DOOR HANDLE FELL OFF(<P>RE-INSTALED EXIT SIGN IAW B767 AMM 25-63-00. NO FURTHER DEFECTS NOTED</P>)

Part: NONE — NONE · airframe 87,798 hrs · 13,702 cycles

SUSPECTED HARD LANDING(<P>COMPLETED PHASE 1 INSPECTION IAW B-767 AMM 05-51-01 PER MCC, NO DEFECTS NOTED AT THIS TIME.</P>)

Part: NONE — NONE · airframe 87,776 hrs · 13,690 cycles

LH MLG DOOR WITH PUNCTURE DAMAGE ON INNER SKIN AT 30 INCH FROM DOOR LEADING EDGE AND 4 INCH FROM LOWER EDGE.(<P>IT WAS REPAIRED BY SRM 52-80-02-2R-1 / SRM 51-70-03-0G-0 AND BOEING SR 4-5739242265.</P>)

Part: NONE — NONE · airframe 87,776 hrs · 13,690 cycles

BULK CARGO DOOR SURROUND STRUCTURE - LOWER SILL - EXISTING EDGE REWORK AT LIGHTENING HOLE OF FLOOR PLATE.(<P>IT WAS REPAIRED PER BOEING SR 4-5708956820.</P>)

Part: NONE — NONE · airframe 87,776 hrs · 13,690 cycles

LH PYLON - UPPER SKIN - WEAR DAMAGE BETWEEN NAC STA 149.43 TO NAC STA 139.73 FOUND OUT OF LIMITS (IT WAS EXCEEDED THE MAXIMUM DEPTH).(<P>IT WAS REPAIRED PER BOEING SR&NBSP;4-5704143162</P>)

Part: NONE — NONE · airframe 87,776 hrs · 13,690 cycles

LOOSE SHIM LOCATED IN THE HOUSING ASSY (112T1018-1) FROM FWD TRUNNION SUUPORT, LH MAIN LANDING GEAR(<P>REMOVED THE HOUSING ASSY (112T1018-1) TO REPLACE FILLERS / SHIMS PER AMM 32-11-01/401, AIPC 57-53-15 AND DWG 112T1717</P>)

Part: NONE — NONE · airframe 87,776 hrs · 13,690 cycles

LH WING #6 L/E SLAT (P/N 114T3100-401G, S/N 000010) SKIN BIRD STRIKE DENT DAMAGE - TIME LIMIT REPAIR(<P>IT WAS REPAIRED IN ACCORDANCE WITH ATLAS EO 1957A609 / SRM 57-43-01-2R-2 REPAIR 2</P>)

Part: NONE — NONE · airframe 87,776 hrs · 13,690 cycles

RH WING, SPOILER #9, TRAILING EDGE LOWER SURFACE (OUTBOARD CORNER), CLOSE TO WSTA 616.2.(<P>IT WAS REPAIRED PER SRM 57-70-01-2R-1 AND SRM 51-70-04-0G-0.</P>)

Part: NONE — NONE · airframe 87,776 hrs · 13,690 cycles

ENGINE #1, INLET COWL LIP SKIN WAS FOUND WITH GOUGE OUT OF LIMITS AT 8 O CLOCK POSITION(<P>IT WAS REPAIRED PER COLLINS REPAIR FORMAT #CV23-01267-REPAIR AND BOEING SR 4-5692112122.</P>)

Part: NONE — NONE · airframe 87,776 hrs · 13,690 cycles

DEBONDED TWO AREAS ON LH PANEL OUTER SKIN LOCATED AT FRONT SPAR AND BETWEEN FSS145.128 TO FSS 270.784 FROM VERTICAL STABILIZER.(<P>IT WAS REPAIRED PER SRM 55-30-01-2R-1 REPAIR 1 FIG. 201 PAGE 2 AND SRM 51-70-10-2R-4 REPAIR 4 FIG. 201 SHEET 1 PAGE 1-3 REV. 121 DEC15/22</P>)

Part: NONE — NONE · airframe 87,776 hrs · 13,690 cycles

DEBONDED TWO AREAS ON RH PANEL OUTER SKIN LOCATED AT FRONT SPAR AND BETWEEN FSS145.128 TO FSS 270.784 FROM VERTICAL STABILIZER.(<P>IT WAS REPAIRED PER SRM 55-30-01-2R-1 REPAIR 1 FIG. 201 PAGE 2 AND SRM 51-70-10-2R-4 REPAIR 4 FIG. 201 SHEET 1 PAGE 1-3 REV. 121 DEC15/22</P> / <P>&NBSP;</P>)

Part: WINDOW — NONE · airframe 87,776 hrs · 13,690 cycles

FLIGHT COMPARTMENT WINDOW, LH WINDOW (#3) WITH CRACKING(<P>IT WAS REPLACED PER AMM 56-11-10. OPS CHECK GOOD.</P>)

Part: NONE — NONE · airframe 87,776 hrs · 13,690 cycles

DURING A ZONAL INSPECTION, MISSING RIVETS ON THE ANGLE ON THE FLOOR BEAM LOWER CHORD LOCATED AT STA 654+121, S-20LH AND STA 676, S-20LH.(<P>IN ACCORDANCE WITH IAI CUSTOMER SERVICE - REPAIR INSTRUCTION #CS-30111-001 IS NECESSARY TO REMOVE THE AFFECTED ANGLES FROM FRAME AND FLOOR STRUCTURE. NOTE: SEE MXA EO #TRE6753580</P>)

Part: BATTERY PACK — NONE · airframe 87,228 hrs · 13,510 cycles

EMERGENCY LIGHT AT L1 DOOR INOP.(<P>T/S PER FIM 33-51 F/T, FOUND BATTERY PACK AT FAULT, ORDEDED 2013-1A SEE ITEM M7 FOR CORRECTIVE ACTION.</P> / <P>M7 CORRECTIVE ACTION - T/S PER FIM 33-51 F/T 803 FOUND BATTERY PACK AT FAULT, ORDERED P/N 2013-1A . REMOVED AND REPLACED BATERRY PACK M735, OPS CHECK NORMAL IAW AMM 33-51-07</P>)

Part: BATTERY PACK — NONE · airframe 87,228 hrs · 13,510 cycles

EMERGENCY LIGHT RIGHT SIDE OVERHEAD COCKPIT INOP(<P>T/S PER FIM 33-51 F/T 803, FOUND BATTERY PACK AT FAULT, ORDERED P/N 2013-1A.&NBSP; REMOVED AND REPLACED BATTERY PACK M735, OPS CHECK NORMAL IAW AMM 33-51-07</P>)

Part: SIGN — DETACHED · airframe 86,968 hrs · 13,428 cycles

DURING COCKPIT OBSERVATION, I FOUND EXIT SIGN ON LIFE RAFT GALLEY COMPUTER NEAR BUTTON BROKEN OFF.(<P>RESECURED EXIT SIGN IN PLACE IAW AMM 25-00-00. OPS CHECK GOOD</P>)

Part: NONE — NONE · airframe 85,557 hrs · 12,978 cycles

UPON DOOR CLOSURE L1 PUSH BUTTON FOR ESCAPE SLIDE WAS NOT CENTERED IN PRECUT PANEL(<P>TRIMMED AND ADJUSTED PRECUT PANEL IAW SRM 51-70-16-06-0 PUSH BUTTON EXTENDS NORMAL .OPS CKS GOOD&NBSP;</P>)

Part: NONE — NONE · airframe 85,130 hrs · 12,843 cycles

FO SIDE OUTLET / NO HEAT.(<P>PERF PACK TEMP CONTROL TEST IAW AMM 21-51-16. OPS CHECK GOOD. AIR TEMP FROM ALL FLIGHT DECK VENTS BLOWS WARM EVENLY. NO DEFECTS AT THIS TIME.</P>)

Part: NONE — NONE

RIGHT FWD WINDOW EICAS(<P>PERFORMED RH FWD WINDOW BITE TEST IAW FIM 30-41 FAULT TREE 804 FIG 104. NO FAULTS NOTED.</P>)

Part: NONE — NONE · 12,839 cycles

APU FAULT ON START ON GROUND(<P>PERFORMED APU BITE IAW FIM 49-11 FIG 103. NO FAULTS NOTED.</P>)

Part: NONE — NONE

R2 WINDOW FWD WINDOW HEAT INOP ( FLIGHT DECK WINDOW HEAT SYSTEMS, NO. 2 (SIDE) WINDOWS )(<P><SPAN>DEFFERED IAW MEL 30-40-01-02. DUE 18 NOV 21, MDDR # 156473 CAT C, PERF RT BITE IAW FIM 30-41 FT 804, RT WINDOW #2 FAULTED.</SPAN></P>)

Part: NONE — NONE

APU FAILED TO START(<P>T/S PER FIM 49-11 FT 980 TO BLOCK 13 SHEET 2, FOUND GRND ON RELAY K442 PIN 7, BLOCK 34 REPLACE ECU RECOMMENDED, PERF CONT CHECK OF CONNECTOR D40813 PIN&NBSP; H7 TO RELAY K442 PIN 7, CHECK GOOD, MCC UPDATED, ECU ON ORDER.</P>)

Part: NONE — NONE · 12,833 cycles

R FWD WINDOW EICAS MESSAGE ON LANDING(<P>PERFORMED FIM TASK 30-41 TASK 802 RESISTANCE VALUES FOUND TO BE WITHIN LIMITS. REMOVED AND REPLACED WHCU AS PER CUSTOMER REQUEST. AMM 30-41-01. CHECKS OK.</P>)

Part: NONE — NONE

RT FWD WINDSHIELD EICAS ON LANDING. REPEAT WRITEUP.(<P>PERFORMED FIM 30-41 FAULT TREE 804. FOUND NO WIRING DEFECTS AND SENSORS TO BE WITHIN LIMITS. REMOVED AND REPLACED WINDOW HEAT CONTROL PANEL IAW AMM 30-41-02.</P>)

Part: NONE — NONE

AFTER STARTING, FWD RT WINDOW HEAT AND FWD LT WINDOW HEAT INOP CAME ON. AFTER LANDING, FWD LT WINDOW HEAT INOP CAME ON.(<P>PERFORMED BITE ON WHCU IAW AMM 30-41-01 AND WH TEST PER AMM 30-41-02. COUND NOT DUPLICATE FAULT ON GROUND. MCC ADVISED AND TECH SUPPORT. OK FOR CONTINUED SERVICE.</P>)

Part: NONE — NONE

R FWD WINDOW EICAS MSG AND INOP ANNUNCIATED ON OVERHEAD PANEL AFTER LANDING.(<P>FOUND LOOSE CONNECTION ON BOTTOM WINDOW HEAT ELEMENT. RESECURED CONNECTION IAW AMM 30-41-01. OPS CHECK GOOD.</P>)

Part: NONE — NONE · airframe 85,094 hrs · 12,830 cycles

LEFT PACK TEMP EICAS AFTER CLOSING DOOR BEFORE BLOCK OUT.(<P><SPAN>TRANSFER TO MDDR 155917 IAW MEL 21-51-01-01, CAT C.</SPAN></P> / <P><SPAN>LP 1431368: PERFORMED FIM 21-51 TASK 877 AND FOUND NO FAULTS. PERFORMED OPERATIONAL TEST AND BITE CHECK FOR THE LH PACK TEMP IAW AMM 21-51-00. FOUND NO FAULT AND EICAS MESSAGES. OPS CHECK GOOD AT THIS TIME. THIS CLEARS DMI #155917.</SPAN></P>)

Part: NONE — NONE · 12,830 cycles

R FWD WINDOW HEAT EICAS AFTER LANDING.(<P>NO MESSAGES PRESENT. BITE TEST WINDOW HEAT CONTROL UNIT. NO FAULTS BITE TEST OK PER AMM 30-41-010404-007. WINDOW HEAT OPS CK GOOD.</P>)

Part: NONE — NONE

R FWD WINDOW HEAT MSG AFTER LANDING(<P>PERF FIM 30-41 FT 804, NO FAULTS ON WHCU. PERF RESISTANCE CHK FROM R/H FWD WINDOW 10.352 WITHIN LIMITS. PERF CONTINUITY CHK FROM R/H FWD WINDOW SENSORS J1/J4/J5 TO CONNECTOR D2898B PINS 4 &AMP; 5 PER WDM 30-41-12. NO WIRING DAMAGE FOUND. SWAPPED R/H FWD WINDOW SENSOR J3 TO SPARE SENSOR J2 ON TB324 IAW WDM 30-41-12. OPS CHK NORM. NO FAULTS NOTED ON BITE TEST.</P>)

Part: NONE — NONE

RIGHT FWD WINDOW HEAT(<P>REMOVED AND REPLACED R FWD WINDOW HEAT CONTROL UNIT IAW B767 AMM 30-41-01. OPS CHECK GOOD.</P>)

Part: NONE — NONE

RIGHT FWD WINDOW HEAT.(<P>BITE TESTED RIGHT WINDOW HEAT CONTROL UNIT PER AMM 30-41-01. NO FAULTS NOTED. NO MESSAGES PRESENT. OK TO CONTINUE.</P>)

Part: UNKNOWN — ODOR (COCKPIT) · airframe 84,925 hrs · 12,778 cycles

COCKPIT HAS DIRTY SOCK ODOR DURING CLIMB OUT & DESCENT. PER AMM 05-51-56, FUMES SMELL CAN NOT DUPLICATE. SYSTEM OK.

Part: VALVE — ILLUMINATED · 12,755 cycles

AFT CABIN TEMP EICAS MSG PERFORMED FIM TASK 21-60 FT 803. FOUND AFT ZONE TRIM VALVE ILLUMINATED. REMOVED AND REPLACED TRIM VALVE IAW AMM 21-67-07. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: PLUG — DISLODGED · airframe 84,804 hrs · 12,747 cycles

LEFT ENGINE OIL QUANTITY INDICATION REMAINDED AT 23 QTS FOR ENTIRE FLIGHT AS WELL AS ON SHUTDOWN.(<P>PERF FIM 79-31 FT 805, FOUND CANNON PLUG DT675 BACKED OFF. RE-SEATED DT675; CLEARED PER SWPM 20-60-00, OPS CHECK GOOD PER AMM 79-31-00. NO DEFECTS NOTED AT THIS TIME.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN TEMP)

AFT CABIN TEMP EICAS MESSAGE(<P>TRANSFERRED TO MDDR&NBSP;<SPAN>153269 IAW MEL 21-61-00.</SPAN></P> / <P><SPAN>PERFORMED ZONE TEMP CONTROL SYSTEM OPERATIONAL TEST IAW B767 AMM 21-61-00. OPS CHECK GOOD AT THIS TIME. THIS CLEARS DMI 153269. REMOVED ALL PLAC.</SPAN></P>)

Part: START VALVE — DAMAGED (RIGHT)

DAMAGE FOUND ON RH ENG STARTER VALVE BRACKET &AMP; STARTER INOP(<P>TRANSFERRED TO MDDR# 153226 IAW MEL 80-00-02-01, CAT C.</P> / <P>REMOVED AND REPLACED ENGINE START VALVE IAW 80-11-02 OPS &AMP; LEAK CHECK GOOD. THIS CLOSES MDDR 153226 PLAC REMOVED.</P>)

Part: STARTER — FAULTED (RT ENGINE) · 12,715 cycles

UNABLE TO START RH ENGINE. ENG START VALVE LIGHT REMAINS ON WITH ENG START SW IN GND NO N2 ROTATION(<P>REMOVED AND REPLACED RH ENG STARTER IAW AMM 80-11-01. OPS CHECK GOOD.</P>)

Part: ACCELEROMETER — FAULTED (NR 2 ENGINE)

#2 ENG EXCESSIVE VIBRATIONS DURING INITIAL CLIMB ON (LPT), RANGING FROM 0.5 TO 5.0(<P>TRANSFERRED TO MDDR 153024 IAW MEL 77-31-01-01, CAT C.</P> / <P>REMOVED AND REPLACED REAR FRAME ACCELEROMETER. IAW AMM 77-31-02. IDLE RUN. IAW AMM 71-00-00. BY INDICATION GOOD. THIS CLEAR MDDR #153024. SD@2303Z</P>)

Part: CONTROL CARD — FAULTED (LT ENG FIRE LOOP)

L ENG FIRE LP 2(<P>TRANS TO MDDR 151988 CAT "C" DUE DATE 26AUG21 IAW MEL # 26-11-01-01. MCC NOTIFIED. T.I: TJ @ 1530Z.</P> / <P>LP 1476270 ITEM M3: REMOVED &AMP; REPLACED LFT ENG #2 LOOP CONTROL CARD (FIRE) IAW AMM 26-10-01. OPS TEST GOOD. THIS CLEARS DMI 151988. PLACARDS REMOVED. CD 0052Z</P>)

Part: ANGLE — CRACKED (NR 6 SLAT) · airframe 84,312 hrs · 12,605 cycles

CRACKED #16 ANGLE AT RADIUS AFT SIDE OF SLAT #6 COVE(<P>REMOVED AND REPALCED ANGLE #16 AT RADIUS AFT SIDE OF SLAT #16 COVE IAW B767 SRM 51-40-02</P>)

Part: ANGLE — CRACKED (LT NR 6 SLAT) · airframe 84,312 hrs · 12,605 cycles

CRACKED RADIUS ANGLE #15 AFT SIDE OF SLAT #6 LEFT WING(<P>REMOVED AND REPLACED&NBSP; ANGLE #15 AFT SIDE OF SLAT #6 LEFT WING IAW B767 SRM 51-40-02</P>)

Part: ANGLE — CRACKED (LT NR 6 SLAT) · airframe 84,312 hrs · 12,605 cycles

CRACKED RADIUS ANGLE #14 AFT SIDE #6 SLAT LEFT WING(<P>REMOVED AND REPLACED ANGLE #14 AFT SIDE #6 SLAT LEFT WING IAW B767 SRM 51-40-02</P>)

Part: SKIN — GOUGED (RT WING SLAT) · airframe 84,312 hrs · 12,605 cycles

R/H WING #9 SLAT UPPER T/E WEDGE SKIN GOUGED AT W.S. 616.2 DUE TO PROTRUDING SCREW(<P>UPON FURTHER EVALUATION OF #9 SLAT UPPER TE WEDGE, FOUND OUT OF LIMITS IAW B767 SRM 51-10-02.&NBSP; REPAIRED #9 SLAT UPPER TE WEDGE IAW B767 SRM 51-70-10-2R-4</P>)

Part: SKIN — DAMAGED (RT LE FLAP) · airframe 84,312 hrs · 12,605 cycles

EXPOSED COMPOSITE RIGHT OUTBOARD FLAP LEADING EDGE, WS 680.(<P>UPON FURTHER EVALUATION OF RH OB FLAP LE WS 680, FOUND DELAM AND OUT OF LIMITS IAW B767 SRM 51-10-06. REPAIRED RH OB FLAP LE WS 680 IAW B767 SRM 57-53-01-2R-1, 51-70-17-0G-0. RESTORED PROTECETIVE FINISHES IAW B767 AMM 51-24-22</P>)

Part: FLAP — DAMAGED (LT WING) · airframe 84,312 hrs · 12,605 cycles

MULTIPLE AREAS OF DAMAGE ON LH IB FLAP ASSY, FOUND OUT OF LIMITS IAW B767 SRM 51-10-02. CUSTOMER REQUEST FLAP REPLACEMENT. REMOVED AND REPLACED LH IB FLAP ASSY AND OPS CHECK GOOD IAW B767 AMM 27-51-06-422-059.

Part: VALVE — FAULTED (RT A/C PACK) · airframe 84,310 hrs

R/H PACK STANDBY MODE INOP(<P>TRANS TO MDDR # 149157 IAW MEL 21-51-03-02 CAT C DUE: 05JUL21. BM @ 0040Z</P> / <P>28JUN, CVG MX: LP 1466262, ITEM M4:&NBSP; REMOVED &AMP; REPLACED LOW LIMIT VALVE&NBSP; IAW AP-20223 &AMP; AMM 21-51-11. OPS CHECK GOOD AT THIS TIME. THIS C/W AP-20223 REV 0. THIS CLEARS DMI 149157 MCC NOTIFIED. PLACARDS REMOVED.</P>)

Part: ADI — MALFUNCTIONED (FIRST OFFICER'S) · airframe 84,278 hrs

DURING TAKEOFF ROLL AFTER THRUST ADVANCE F/O'S ADI BLANKED, PERFORMED LOW SPEED REJECTED T/O AND TAXIED BACK TO BLOCKS.(<P>REMOVED AND REPLACED RIGHT ADI IAW B767 AMM 34-27-03 AND 34-33-00 OPS CHECK GOOD.</P>)

Part: OIL SYSTEM — LOW (APU) · airframe 84,201 hrs

APU FAULT WHEN TRYING TO START APU AFTER LANDING(<P>PERFORMED APU BITE PROCEDURE IAW FIM TASK 49-11 FT 987, LOW OIL PRESSURE FAULT, FOUND APU OIL LOW, SERVICED TO FULL IAW AMM 12-13-04, PERFORMED OPS CHECK OF APU 3X TIMES IAW AMM 49-11-00, OPS CHECK GOOD, APU HRS @ 1407.4 @ APU SERVICING</P>)

Part: LINE — OUT OF POSITION (PRESSURE HOSE) · airframe 84,142 hrs · 12,557 cycles

LEFT ENGINE BLEED OFF MSG AFTER START. COMPLETED QRH MSG REMAINS.(<P>PERFORMED AIR SUPPLY BITE TEST IAW 767 AMM 36-23-00, SUSPECT BAD PRV. REMOVED &AMP; REPLACED PRV IAW 767 AMM 36-11-18. PERFORMED ENGINE RUNS IAW 767 AMM 71-00-00, OPS CHECK FAILED, LEFT ENGINE NO DUCT PRESSURE.</P><P>LP 1466400, ITEM M4: REMOVED AND REPLACED PRV CONTROLLER IAW AMM 36-11-19, S/N OFF: 2017070012, P/N OFF: 792755-15. OPS CHECK FAILED.</P><P>LP 1466401, ITEM M7: REF B767 WDM 36-11-61 FOUND OPEN WIRE BETWEEN CONNECTOR P4156P AND PRV VVALVE V325, PIN 7-TERMINAL 3. REPLACED WIRE BUNDLE FROM CONNECTOR D4156P TO LEFT ENG PRV V325, IAW B767 SWPM 20-10-11. LEFT ENGINE BLEED OPS CHECK NML, WIRES CHK OK.</P><P>LP 1466402, ITEM M10: REMOVED AND REINSTALLED PRV ACTUATOR SUPPLY PRESSURE HOSE AND PRECOOLER REGULATED PRESSURE LINE IN CORRECT POSITION. IAW AMM 20-11-00, OPS CHECK &AMP; LEAK CHECK GOOD AT THIS TIME IAW BAMM 36-11-15. BAMM 36-11-18 AND BAMM 36-11-19</P>)

Part: SMOKE DETECTOR — FALSE ACTIVATION (FWD CARGO) · airframe 84,144 hrs · 12,558 cycles

FWD CARGO DET 2 EICAS MSG DISPLAYED.(<P>DEFERRED FWD CARGO SMOKE DET# 2 IAW DDG 26-16-01-01-01 AND TRANSFERRED TO DMI 148237, PLACARD INSTALLED.</P><P>TPA MX, 11JUN, LP 1466405, ITEM M6: REMOVED AND REPLACED FWD CARGO SMOKE DETECTOR #2(M325) IAW AMM 26-16-01, OPS NORMAL.

Part: OXYGEN MASK — INOPERATIVE (COCKPIT) · airframe 84,031 hrs · 12,517 cycles

FIRST OBSERVER SEAT O2 INOP(<P>PLACED ITEM ON DMI 147544 IAW MEL 25-11-02-01A CAT A. DUE 2 FLIGHT DAYS. AUTH: JD 0438L</P><P>CVG, 26MAY, LP 1306002, ITEM M3: REMOVED AND REPLACED IST. OBS O2 MASK ASSY IAW B767 AMM 35-11-51. OPS CHECK GOOD AT THIS TIME. THIS CLEARS DMI 147544. PLACARDS REMOVED. MCC NOTIFIED. T.I.: 1239Z YK.</P>)

Part: MICROPHONE — NO TEST (F/O O2 MASK) · airframe 84,028 hrs · 12,516 cycles

FO O2 MASK WILL NOT CHECK FOR MICROPHONE OPERATION.(<P>RE-PACKED FO O2 MASK IAW AMM 35-11-57. OPS CHECK OK.</P>)

Part: FMC — UNKNOWN (RIGHT) · airframe 84,010 hrs · 12,511 cycles

AFTER ENGINE START AND APU SHUTDOWN, A/C SCREENS UPPER/LOWER EICAS, CA SIDE ADI AND RIGHT FMC FLICKERED AND GLITCHED AS IF POWER WAS TRANSFERING(<P>RAN BOTH ENGINES TO OBSERVE IDG LEADS ISOLATED EACH TDG AND NOTED NO FAULTS AFTER 30 MINUTES. OPS CHECK GOOD IAW B767 AMM 71-00-00<BR /></P>)

Part: PRESSURE SWITCH — FAULTED (FUEL SYSTEM) · airframe 83,996 hrs · 12,505 cycles

L AFT FUEL PUMP CAUTION MESSAGE IN FLIGHT. QRH COMPLETE.(<P>DEFERRED PER MEL 28-22-01, CAT C. TRANSFERRED TO MDDR # 147093. MCC NOTIFIED. EXP 27MAY21. DL 1013A</P><P>20MAY21 - LP 1306097 - M5 - CVG -&NBSP;REMOVED AND REPLACED PRESSURE SWITCH IAW AMM 28-42-01/401. THIS CLEARS MDDR 147093.</P>)

Part: RELAY — FAULTED (FWD CROSSFEED) · airframe 83,997 hrs · 12,506 cycles

FWD CROSSFEED VALVE INOP.(<P>TRANSFERRED TO MDDR 146979 IAW MEL 28-22-03B, CAT C.</P><P>REMOVED AND REPLACED RELAY K2152 IAW FIM 28-22 FT 821 AND WDM 28-22-31, OPS CHECK GOOD. THIS CLEARS DMI 146979. MCC NOTIFIED.&NBSP;</P>)

Part: PUMP — WARNING MESSAGE (LEFT) · airframe 83,960 hrs · 12,495 cycles

L AFT FUEL PUMP EICAS MESSAGE DISPLAYED AS WELL AS L AFT PRESS LIGHT IN OVHD PANEL, LIGHT REMAINED ILLUMINATED WITH SWITCH SELECTED ON(<P>RESET LEFT AFT FUEL PUMP IAW AMM 28-20-05 NO FIX. DEFERRED PER MEL 28-22-01, TRANSFERRED TO MDDR #146737.</P><P>LP 1237929 - ITEM #3: REMOVED AND REPLACED FUEL PANEL IAW 28-21-17, NO FIX, REINSTALLED ORIGINAL FUEL PANEL. DMI 146737 REMAINS OPEN.</P><P>ITEM #4: REMOVED AND REPLACED L AFT FUEL BOOST PUMP IAW AMM 28-22-03. OPS CHECK GOOD IAW AMM 28-22-00. NO LEAKS DETECTED AT THIS TIME. THIS CLEARS DMI 146737. MCC NOTIFIED, PLACARDS REMOVED, DDG MX PROCEDURE REVERSED. ETOPS STATUS UPGRADED.</P>)

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 83,951 hrs · 12,491 cycles

CABIN ALTITUDE 2 INOP ( AUTO CABIN PRESSURE CONTROL SYSTEMS, ONE INOPERATIVE )(<P>ITEM TRANSFERRED TO MDDR 146448 PER 21-31-01A CAT C DUE DATE 15MAY21.</P><P>LP 1453662: REMOVED AND REPLACED&NBSP;AUTOMATIC PRESSURE CONTROLLER IAW AMM 21-31-02, OPS CHECK GOOD, THIS CLEARS MDDR 146448. PLACARDS REMOVED</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 83,924 hrs

STATUS MSG CABIN ALT AUTO 2 IN DECENT(<P>OPS CHECK IAW B767-300 AMM TASK 21-33-00-705-001. COULD NOT DUPLICATE ON GROUND&NBSP;</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 83,903 hrs

CABIN ALT 2 STATUS MSG(<P>PERF. FIM 21-31 FT 810 STATUS MSG CLEARED. NO FAULTS NOTED SYS CK NORMAL.

Part: CONTROL PANEL — MALFUNCTIONED (ENGINE IGNITION) · airframe 83,951 hrs · 12,491 cycles

RT FUEL VALVE INDICATION INOP, . REMOVED AND REPLACED ENGINE IGNITION AND STARTING PANEL IAW B767 AMM 80-11-51. OPS CHECK GOOD. THIS CLEARS MDDR 146335. ALL PLACARDS REMOVED.

Part: PRESSURE SWITCH — MALFUNCTIONED (FUEL SYSTEM) · airframe 83,847 hrs · 12,456 cycles

L AFT PUMP PRESS LT REMAINED ON WITH SWITCH ON BEFORE START. AFTER A/NC & CYCLING SWITCH BACK TO PRESS LIGHT WENT OUT. T/S PER FIM 28-22 FT 819, REMOVED LH AFT FUEL PRESSURE SWITCH TO BLEED PRESSURE SENSE LINE PER FIM. REINSTALLED LH AFT FUEL PRESSURE SWITCH AND OPS CHECKED IAW AMM 28-42-01. OPS CHECK GOOD, PRESSURE LIGHT FUNCTIONS CORRECTLY. THIS CLEARS DMI 146049, PLACARD REMOVED.

Part: PRIORITY VALVE — MALFUNCTIONED (RT BLEED SYS) · airframe 83,759 hrs · 12,432 cycles

AFTER PUSHBACK AND START RT ENG BLEED OFF MSG COMPLIED W/ QRH RETURNED TO GATE.(<P>BITE AIR SUPPLY MODULE PER 36-20-00. FOUND PRVC FAULT. REMOVED AND REPLACED PRVC PER AMM 36-11-19. PERFORMED R ENG IDLE RUN PER AMM 72-00-00. OPS CHECK GOOD. NO FAULTS NOTED.</P>)

Part: STATUS MESSAGE — FALSE INDICATION (NR 1 FIRE DET) · airframe 83,541 hrs · 12,378 cycles

DURING TAXI OUT TWO STATUS MESSAGES, 1 LEFT ENGINE FIRE DET, LEFT FUEL QUANTITY.&NBSP;(<P>PERFORMED OPS TEST OF ENGINE FIRE LOOPS PER AMM 26-11-00. OPS CHECK GOOD AT THIS TIME.</P>)

Part: CIRCUIT CARD — MALFUNCTIONED (AFLOTS) · airframe 83,507 hrs · 12,363 cycles

FWD AND AFT CARGO SWITCH LIGHT NOT ILLUM AND EICAS MESSAGE NOT DISPLAYED DURING FIRE/OVHT TEST.(<P>T/S IAW FIM 26-16 F/T 806 AND ENDED AT BLOCK 102 ON SHEET 2. REMOVED AND REPLACED AFOLTS NO 6 CARD IAW AMM 26-10-01. OPS CHECK GOOD AT THIS TIME.</P>)

Part: INDICATOR — MALFUNCTIONED (HYD PRESSURE) · airframe 83,417 hrs · 12,341 cycles

L HYD LOW IN FLIGHT, L HYD PRIMARY PUMP EICAS IN FLIGHT.(<P>FOUND DIFFERENTIAL PRESSURE INDICATOR LEAKING HYD FLUID. REMOVED AND INSPECTED CASE DRAIN FILTER FOR METAL, NO METAL FOUND. REPLACED FILTER IAW 29-11-17. NSN, P/N OFF: 654T0035-3.</P><P>ITEM 2: REMOVED LT HYD CASE DRAIN FILTER DIFF PRESS INDICATOR IAW AMM 29-17-24, INSTALLED DIFF PRESSURE INDICATOR AMM 29-17-24, NO LEAKS NOTED.</P>)

Part: FITTING — STRIPPED (VALVE) · airframe 83,278 hrs · 12,297 cycles

AFTER ENG START RT ENG BLEED OFF LIGHT WOULDN’T EXTINGUISH. TRANSFERRED TO MDDR 142467 IAW MEL 36-11-01-01A, CAT C, DUE DATE 25FEB21. PER FIM TASK PERFORMED BITE OF AIR SUPPLY MODULE FOUND PRV LISTED. UPON GVI OF PRV FOUND AIR SUPPLY LINE FITTING STRIPPED AND LOOSE. PRV ON ORDER. REMOVED AND INSTALL PRV AMM 36-11-18. OPS CHECK GOOD. THIS CLEARS DMI NR 142467.

Part: WARNING MESSAGE — FALSE INDICATION (BLEED SYSTEM) · airframe 83,281 hrs · 12,298 cycles

RIGHT ENG BLEED OFF INDICATION ON OVERHEAD AND EICAS AFTER ENGINE START(PERFORMED OPERATION CHECK OF RT ENG BLEED OFF LIGHT; FOUND RT ENG BLEED TO OPERATE NORMAL AT THIS TIME IAW 767 MM 71-00-00)

Part: RADAR — MALFUNCTIONED (WX SYSTEM) · airframe 83,227 hrs · 12,279 cycles

WX RADAR ISN'T GIVING A CORRECT RETURN ON LEFT SIDE OF SWEEP - BOTH L &AMP;R SYSTEMS - VERY WEAK(<P>PERFORMED OPS TEST OF WXR SYSTEM RT WXR OKAY, NO FAULTS. LEFT WXR SYSTEM FAULTY - TRANSFERRED LEFT WXR TO MDDR 142145 IAW DDG 34-43-01 CAT D DUE 08JUN21</P><P>DATE 09FEB - LP 1316246 ITEM 4 - ONT -&NBSP;PERFORMED WXR RADAR SYS TEST IAW AMM 34-43-00 , AND WXR BITE PROCEDURE IAW FIM TASK 34-43 FT 805 ALL SYSTEMS GOOD. NO DEFECTS NOTED. THIS CLEARS MDDR 142145 TI: RS @1303 FOR REMOVAL.</P>)

Part: REGULATOR — FAILED (OXYGEN SYS) · airframe 83,142 hrs · 12,254 cycles

SUPERNUMERARY O2 PRESSURE INDICATION BETWEEN EICAS AND O2 GAUGE OUT OF LIMITS. REMOVED AND REPLACED REGULATOR/TRANSDUCER, IAW AMM 35-11-04. OPERATIONS CHECKS NORM AT THIS TIME.

Part: GENERATOR — MALFUNCTIONED (LEFT) · airframe 83,042 hrs · 12,219 cycles

LEFT GEN DROPPING OFFLINE AFTER ENGINE START AND DURING TAXI MOMENTARILY, OCCURRED THREE TIMES, GEN CAME BACK ONLINE EVERY TIME. TRANSFERRED TO DMI 140758, IAW MEL 24-00-01-01, CAT B. PERFORMED OPERATIONS CHECK ON LEFT IDG, IAW B767 AMM 24-11-00. NO MESSAGE ON BPCU, OPERATIONS CHECK GOOD. THIS CLEARS DMI 140758.

Part: CONTROL PANEL — MALFUNCTIONED (APU START) · airframe 82,959 hrs · 12,184 cycles

APU START SELECTOR DOES NOT SPRING BACK FROM START TO ON POSITION WHEN SELECTED. TRANSFERRED TO MDDR 140101, IAW MEL 49-11-01A, CAT C, DUE 06JAN21. REMOVED AND REPLACED APU CONTROL PANEL, IAW BOEING 767 AMM 49-41-81. OPERATIONS TEST GOOD. THIS CLEARS DMI 140101. PLACARDS REMOVED. MCC NOTIFIED.

Part: MODULATING VALVE — MALFUNCTIONED (AFT CABIN TEMP) · airframe 82,698 hrs · 12,095 cycles

AFT CABIN TEMP INOPERABLE EICAS AND AFT CAB AUTO ANNUNCIATOR LIGHT ON OVERHEAD PANEL. TRANSFERRED TO DMI 137977, IAW MEL 21-61-01-02, CAT C, DUE 27NOV20. GTC 0950Z. C/W W/O 73354, REMOVED AND REPLACED AFT TRIM AIR MODULATING VALVE, IAW AMM 21-61-07. OPERATIONS CHECK GOOD. THIS CLEARS MDDR 137977. MCC NOTIFIED DISP: DL 1010Z.

Part: UNKNOWN — UNKNOWN (RT WX RADAR) · airframe 82,683 hrs · 12,090 cycles

RT WX RADAR INOPERABLE. RT WX RADAR SYSTEM TEST CARRIED OUT, IAW AMM 34-43-00. OPERATIONS CHECK GOOD.

Part: STARTER — FAILED · airframe 82,634 hrs · 12,071 cycles

RT ENGINE STARTER WOULD NOT ACCEPT OIL DURING STARTER OIL CHANGE, WC A-80-301-00-02 AS PART OF WO 72732. REMOVED AND REPLACED RT STARTER ASSEMBLY, IAW 80-11-01. STARTER OIL SERVICED, IDLE LEAK TEST GOOD, REF 71-00-00.

Part: NONE — NONE (LT ENGINE) · airframe 82,602 hrs · 12,062 cycles

IN FLIGHT, FL 370 1700Z SAT -50 DEG C, LEFT ENGINE VIBE MONITOR INDICATED "FAN" 5.0 (FULL SCALE DEFLECT). TRANSFERRED TO MDDR NR 137066, IAW MEL 77-31-01, CAT C DUE DATE 11NOV20. MCC NOTIFIED EH. PLACARDS INSTALLED. T+I 2108Z CW. PERFORMED LT ENGINE VIBRATION SURVEY, IAW AMM 71-00-00. ALL ENGINE PARAMETERS ARE WITHIN OPERATIONAL LIMITS. THIS CLEARS MDDR 137066.

Part: OXYGEN MASK — FAILED (CAPTAIN'S) · airframe 82,585 hrs · 12,057 cycles

CAPTAINS O2 MASK HARNESS BLOWN. SWAPPED LEFT MASK JUMPSEAT O2 MASK (S/N:105712) FOR BROKEN MASK (S/N:21800) AND PLACED ON DMI: 126891, IAW MEL 35-11-03-02A. LEFT MOST JUMPSEAT UNUSEABLE. REMOVED AND REPLACED LT SUPER NUMERARY (JUMPSEAT) CREW O2 MASK, IAW AMM 35-11-51. THIS CLEARS MDDR 136891. MCC NOTIFIED, PLACARD REMOVED. OPS CHECK GOOD. DISPATCH TJ 1545Z.

Part: ACCELEROMETER — MALFUNCTIONED (LT ENGINE) · airframe 82,583 hrs · 12,056 cycles

IN FLIGHT LEFT VIB INDICATOR ERRATIC INDICATIONS FROM .5-5.0 NO ACTUAL VIB FELT. ALL OTHER INDICATIONS NORMAL. TRANSFERRED TO MDDR 136877, IAW DDG 77-31-01 CAT "C", DUE 08NOV20. INSTALLED ALTERNATE/EXTERNAL NR 1 ACCELEROMETER, IAW AMM 77-31-01 (LT ENGINE). PERFORMED OPERATIONS CHECK, IAW AMM 77-31-00. OPERATIONS CHECK GOOD. THIS CLEARS DMI 136877. PLACARD REMOVED, MCC NOTIFIED.

Part: FASTENER — LOOSE (ACOUSTIC PANEL) · airframe 82,556 hrs · 12,046 cycles

RIGHT ENGINE VIBRATION INDICATOR SHOWING 0.2-3.1 FOR 30 SECONDS DURING CLIMB. OSCILLATING, NO VIBRATIONS FELT. PERFORMED EXTERNAL ENGINE INSPECTION, IAW AMM 72-00-00. FOUND LOOSE FASTENERS ON INNER ACOUSTIC PANELS, SECURED FASTENERS, IAW AMM 72-53-01.

Part: CONNECTOR — DAMAGED (LT ENGINE) · airframe 82,530 hrs · 12,037 cycles

IN CRUISE AT FL370 LEFT ENGINE FAN VIB INDICATIONS RANGED ERRATICALLY FROM 0.4-5.0 FOR APPROXIMATELY THREE MINUTES. NO ACTUAL VIBRATION FELT. TRANSFERRED TO MDDR 136585 MEL 77-31-01, CAT C DUE DATE 01NOV20. RS 2107Z 25OCT, ILN MX. REMOVED AND REPLACED ENGINE VIBE MONITOR, IAW AMM 77-31-03 (OFF PART: PN 241-256-000-131, SN EF480). OPERATIONS CHECK GOOD. THIS CLEARS DMI NR 136585 Y.I.- RS 0137Z. IN FLIGHT FAN VIB INDICATOR ERRATIC INDICATIONS FROM .6 -5. REOPENED MDDR 136585, IAW DDG 77-31-01. MX ACTION COMPLIED WITH. PLACARD NSTALLED. MCC NOTIFIED YK 1430Z. REMOVED AND REPLACED CONNECTOR D10994, IAW SWPM 20-60-00. OPERATIONS CHECK GOOD, IAW AMM 77-31-00. T/I BA 1621Z.

Part: FIRE DETECTOR — INOPERATIVE (LT ENGINE) · airframe 82,517 hrs · 12,031 cycles

LT ENGINE FIRE LOOP NR 2 INOPERABLE ENGINE FIRE DETECTION SYSTEMS, DETECTION LOOPS (ER RESTRICTED 120). TRANSFERRED TO MDDR 136490. 22OCT2020, LOG 1274401, ITEM 4, CVG. REMOVED AND REPLACED LT ENGINE UPPER AFT FIREWALL FIRE DETECTOR, IAW AMM 36-11-02. OPERATIONS TEST GOOD. THIS CLEARS MDDR 136490. PLACARDS REMOVED. MCC NOTIFIED. LEON DISPATCH EH 1527A.

Part: CIRCUIT CARD — MALFUNCTIONED (FIRE LOOP NR 2) · airframe 82,507 hrs · 12,027 cycles

LT ENGINE FIRE LOOP NR 2 INOPERABLE. PLACED ON MDDR 136244, IAW DDG 26-11-01-01. MIA MX, 17OCT. T/S REMOVED/REPLACED NR 2 LOOP DET CARD M682 LT ENGINE, PER AMM 26-10-01. OPERATIONS TEST LT ENGINE FIRE/OVERHEAT SYSTEM OK, PER AMM 26-11-00/718. MDDR 136244 CLEARED ST/1953Z.

Part: CIRCUIT CARD — MALFUNCTIONED (OVERHEAT SYSTEM) · airframe 82,511 hrs · 12,028 cycles

"FIRE/OVERHEAT SYSTEM" EICAS MESSAGE. ACCOMPLISHED QRH AND MESSAGE CLEARS BUT COMES BACK WITHIN 2-3 MINS. REMOVED/REPLACED AFOLT CARD M10224 ENGINE RT; PERFORMED FIRE/OVERHEAT ENGINE SYSTEM TEST OK, AMM 26-10-01.

Part: RADAR — MALFUNCTIONED (WX SYSTEM) · airframe 82,511 hrs · 12,028 cycles

WX RADAR STUCK IN TEST MODE. PERFORMED WEATHER RADAR SYSTEM TEST, IAW B767 AMM 34-43-00-735-033-002, ALL SYSTEMS TEST GOOD, INCLUDING MODE SWITCHING FUNCTION. PERFORMED 30S/40S TEST, IAW 22-00-02. NO FAULTS PRESENT AT THIS TIME. A/C OK FOR CAT IIIB OPERATIONS.

Part: RADAR — STUCK (WEATHER) · airframe 82,502 hrs · 12,025 cycles

WX RADAR STUCK IN TEST MODE. PERFORMED WEATHER RADAR SYSTEM TEST, IAW B767 AMM 34-43-00-735-033-022. ALL SYSTEMS TEST GOOD, INCLUDING MODE SWITCHING FUNCTION. PERFORMED 30S/40S TEST, IAW 22-00-02. NO AUTOFLIGHT FAULTS PRESENT AT THIS TIME. A/C OKAY FOR CAT III B OPERATIONS.

Part: CABLE — DAMAGED (LT ENGINE) · airframe 82,502 hrs · 12,025 cycles

LT ENGINE W11 AND W12 CABLE ASSEMBLYS HAVE HEAT DAMAGE IN THE AREA NEAR BOTH COUPLING SEAT OF 8TH STAGE MANIFOLD. REMOVED AND REPLACED W11 CABLE, IAW B767 AMM 73-21-18-804-099-H00, 73-21-18-004-088-H00, 73-21-18-404-92-H00, NO FAULTS NOTED. REMOVED AND REPLACED W12 CABLE ASSEMBLY, IAW B767 AMM 73-21-18-804-049-H00, 73-21-18-004-088-H00, 73-21-18-404-92-H00. NO FAULTS NOTED. P/N OFF: 1853M63G01, S/N OFF: LMDC8313.

Part: SEAL — LEAKING (LT ENGINE DUCT) · airframe 82,499 hrs · 12,024 cycles

LT ENGINE FIRE LP 2 STATUS MESSAGE. REMOVED AND REPLACED E-SEALS ON DUCTING OF 8TH STAGE LPT MANIFOLD, PER B767 AMM 36-11-01. ENGINE RUN UP AND OPERATIONS CHECK GOOD AND LEAK CHECK GOOD.

Part: SEAL — DAMAGED (LT ENGINE) · airframe 82,499 hrs · 12,024 cycles

LT ENGINE OH LP 1 STATUS MESSAGE INTERMITTENT. T/S PER FIM 26-11 FT 804 AND MM 36-11-01. CONTINUITY FOUND IN ALL DETECTOR ELEMENTS. NO LEAKS FOUND IN PNEUMATIC DUCTS LT ENGINE FOUND HEAT DAMAGED WIRING HARNESS ENDING AT P11 AND P12 ECU. MCC NOTIFIED. PARTS ORDERED. REMOVED AND REPLACED E-SEALS ON DUCTING OF 8TH STAGE LPT MANIFOLD, PER B767 AMM 36-11-01. ENGINE RUN UP AND OPERATIONS CHECKED GOOD. REPLACED DUE TO PREVIOUS EVIDENCE OF LEAKAGE.

Part: DUCT — LEAKING · airframe 82,499 hrs · 12,024 cycles

FIRE/OVERHEAT SYSTEM ADVISORY MESSAGE IN FLIGHT. RAN QRH MESSAGE CLEARED THEN RE APPEARED. T/S PER FIM 26-11 FT 804, WDM 26-11-11 & AMM 26-11-00. FOUND DUCT NOT SEATED PROPERLY, RESECURED. RAN ENGINE, REF 71-00-00 TO 35% N1 FOR 20 MIN, NO FAULTS NOTED.

Part: DUCT — LEAKING (LT ENGINE) · airframe 82,499 hrs · 12,024 cycles

LT ENGINE LOOP 1 STATUS MESSAGE INTERMITTENT IN FLIGHT. T/S PER FIM 26-11 FT 804, WDM 26-11-11 & AMM 26-11-00. FOUND DUCT NOT SEATED PROPERLY, RESECURED. RAN ENGINE, REF 71-00-00 TO 35% N1 FOR 20 MIN, NO FAULTS NOTED.

Part: DUCT — LOOSE · airframe 82,494 hrs · 12,023 cycles

LEFT ENGINE DETECTION LOOP 2 INOPERABLE. ENGINE FIRE DETECTION SYSTEMS, DETECTION LOOPS (ER RESTRICTED 120). TRANSFERRED TO MDDR 135801, IAW MEL 26-11-01-01, CAT C. TROUBLESHOT PER FIM 26-11 FT 804, WIRING DIAGRAM 26-11 AND AMM 26-11-00. FOUND DUCT LOOSE, RESECURED, RAN ENGINE UP TO 35 PERCENT FOR 20 MINUTES. NO FAULTS NOTED. MCC NOTIFIED. THIS CLEARS MDDR 135801.

Part: FAN — FAILED (EQUIP EXHAUST) · airframe 82,444 hrs · 12,010 cycles

STATUS MESSAGE AT FL340 AFT EQ EXHAUST FAN 1. TRANSFERRED TO MDDR 135629 AS PER MEL 21-58-05. CAT C DUE 17 OCT 2020. REMOVED FWD EQUIPMENT EXHAUST FAN, IAW AMM 21-58-00. RE-INSTALLED FWD EXHAUST FAN, IAW AMM 21-58-06. OPERATIONS CHECK NORMAL. THIS CLEARS MDDR 135629, PLACARD REMOVED.

Part: BYPASS VALVE — BROKEN · airframe 82,439 hrs · 12,009 cycles

DURING REMOVAL OF LEFT ISOLATION VALVE FOUND ISOLATION BY-PASS CHECK VALVE BROKE. REMOVED AND REPLACED, IAW 36-11-05 LEFT BYPASS CHECK VALVE. OPS CHECK GOOD.

Part: ISOLATION VALVE — LEAKING · airframe 82,439 hrs · 12,009 cycles

SINGLE ENGINE TAXI IN, OPENED BOTH ISOLATION VALVES AND GET AN "L ISLN BLD VLV" EICAS AS THE LT ISOLATION VALVE DIDN`T OPEN. RAN FIM 36-10 FT 827 UP TO STEP 14, PROBLEM NOT INDICATION, SUSPECTED SLIGHT LEAK FROM ISOLATION VALVE LEFT. REMOVED AND REPLACED LT ISOLATION VALVE, IAW 36-11-04. OPS CHECK GOOD.

Part: PRESSURE SWITCH — MALFUNCTIONED (FUEL SYSTEM) · airframe 82,434 hrs · 12,008 cycles

LEFT AFT FUEL PUMP EICAS ILLUMINATED WITH LEFT AFT FUEL PRESS FLICKERS. PERFORMED FIM 28-22-43819. UNABLE TO DUPLICATE EICAS MESSAGE. LEFT AFT FUEL PRESS LIGHT FLICKERS. INSTALLED DMI 135536, IAW MEL 28-42-01-01. M/P C/W. MCC EC 1012 DISP JD 1012. RIV MX, 05OCT. REMOVED AND REPLACED LEFT AFT FUEL PRESSURE SWITCH, IAW 28-42-01. OPS CHECK GOOD, LEAK CHECK GOOD. DMI NR 135536 CLEARED. LC @ 1750Z.

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PUMP) · airframe 82,418 hrs · 12,004 cycles

LT AFT FUEL PUMP "EICAS" ILLUMINATED DURING PREFLIGHT NUMEROUS TIMES & OVERHEAD LT AFT FUEL PUMP PRESS CYCLES. OPS CHECKED LT AFT BOOST PUMP, IAW 28-22-00. OPS CHECK NORMAL AT THIS TIME, NO FURTHER DEFECTS NOTED.

Part: MODULATING VALVE — MALFUNCTIONED (BLEED OVERHEAT) · airframe 82,370 hrs · 11,990 cycles

LT ENG BLEED OVERHEAT. REMOVED FAV ASSY NR 1 ENGINE, IAW AMM 36-11-16. INSTALLED & OPERATIONS CHECKED FAMV NR 1 (LT), IAW AMM 36-11-16. LEAK & OPERATIONS CHECKED GOOD, PER SAME. REQUIRES HIGH POWER ENGINE RUN, PER MCC REQUEST. REMOVED AND INSTALLED 31 ENGINE PRSOV, IAW AMM 36-11-09, OPERATIONS CHECK NORMAL, IAW AMM 36-11-09. LEAK CHECK NORMAL, IAW AMM 36-11-09. S/N OFF: 990403, P/N OFF: 799801-4. PERFORMED MPA ENGINE RUNS, PER MM 71-00-00 TEST 5, ALL OPERATIONS FOUND NORMAL.

Part: LINE — LEAKING (PUMP) · airframe 82,379 hrs · 11,993 cycles

RIGHT ENGINE EDP PRESSURE LINE HAS LEAK AT FLEX LINE TO FIREWALL. REMOVED AND REPLACED PRESSURE FLEX LINE ON RIGHT ENGINE EDP FIREWALL, IAW MM 20-10-09 AND 70-50-00. LEAK CHECK GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 82,348 hrs · 11,981 cycles

DIRTY SOCK SMELL ON CLIMBOUT THROUGH 10,000' AND AGAIN DESCENDING THROUGH 10,000'. PERFORMED INSPECTION OF LT COOLING PACK, IAW AMM 21-51-00. HEAT EXCHANGERS, CONDENSORS, DUCTS ARE CLEAR OF FOD, NO SIGN OF FOUL SMELL. CLEANED OUT WATER FROM WATER SEPARATOR DRAIN, IAW 21-51-21. SUPPLIED CONDITIONED AIR, IAW AMM 21-00-00. NO ODOR AT THIS TIME.

Part: WIRE — SHORTED (FIRE LOOPS) · airframe 82,310 hrs · 11,968 cycles

LT ENG FIRE LP1 STATUS MESSAGE ENROUTE. FOUND WIRES BETWEEN D4230P TS681, TS 682 AND TS683 FIRE LOOPS SHORTED TO SHIELD. REMOVED AND REPLACED WIRES W5324-452R-16, -451R-16, -454R-16, -453R-16, -456R-16, -455R-16 IAW WDM 26-11-11 SWPM 20-10-06. PERFORMED OPS CHECK OF NR 1 FIRE LOOP ON LT ENG, IAW AMM 26-11-01. OPS CHECK GOOD AT THIS TIME.

Part: MANIFOLD — DAMAGED (LT ENGINE) · airframe 82,310 hrs · 11,968 cycles

LEFT ENGINE TCC DUCT IS DAMAGED. ITEM TRANSFERRED TO MDDR 134586, IAW DDG 75-24-01, CAT C DUE 27SEP20. LT ENGINE TURBINE COOLING SYSTEM INOPERABLE. REMOVED DAMAGED INLET MANIFOLD AND INSTALLED NEW INLET MANIFOLD, IAW AMM 75-24-03-404-037-H00; 75-24-03-004-001-H00. ASSOCIATED BRACKETS INSTALLED SAFETY WIRED. COMPLETED INSTALLATION OF TCC COOLING DUCT, IAW MM 75-24-03.

Part: FIRE LOOP — MALFUNCTIONED (LT ENGINE) · airframe 82,282 hrs · 11,960 cycles

MULTIPLE WRITE UPS (3) STATUS "LT ENG FIRE LP 1". TRANSFERRED FIRE LOOP 1 LT ENG TO DMI # 134384 MEL # 26-11-01-01. REMOVED AND REPLACED ENG NR 1 LOWER AFT LOOP DETECTOR ASSY, IAW 26-11-02. DURING INSTALL, LOOP 2 TERMINAL LUG DAMAGED. REPLACED LOOP 2 ON DETECTOR ASSY, IAW 26-11-02. PERFORMED FIRE DETECTOR OPS TEST, IAW 26-11-00, NO FAULTS NOTED. PERFORMED DVI ON ALL CLAMPS, NO DEFECTS NOTED. THIS CLEARS MDDR 134384. PLACARD REMOVED.

Part: FIRE LOOP — OUT OF ADJUST (LT ENGINE) · airframe 82,287 hrs · 11,962 cycles

UPON ARRIVAL, CREW REPORTS LEFT ENG FIRE LOOP 1 INTERMITTENT DURING CRUISE, NO MESSAGE ON ARRIVAL. PERFORMED SYSTEM TEST, IAW FIM 26-11 504, NO DEFECTS NOTED. PERFORMED LOAD LIGHT CHECK AT CANISTER D7792P TO DETECTOR RJ TERMINAL AT 28 WDC, NO DEFECT NOTED. FOUND LOWER AFT LOOP GROUND TO FROM IN TOW PLACED. ADJUSTED LOOP, NO DEFECT NOTED.

Part: UNKNOWN — UNKNOWN (SHUTOFF VALVE) · airframe 82,276 hrs · 11,957 cycles

LEFT HPSOV CLOSE COMMAND WAS NOT DETECTED. PERFORMED AIR SUPPLY CONTROL SYSTEM BITE TEST, OK AMM 36-23-00/715. LT ENGINE RUN UP OK, NO MSG AMM 71-00-00-735.

Part: UNKNOWN — UNKNOWN (SHUTOFF VALVE) · airframe 82,276 hrs · 11,957 cycles

RIGHT HPSOV CLOSE COMMAND WAS NOT DETECTED. PERFORMED AIR SUPPLY CONTROL SYSTEM BITE TEST, OK AMM 36-23-00-715. RT ENGINE RUN UP OK, NO MSG AMM 71-00-00-715.

Part: SEAL — LEAKING (FAN SHAFT) · airframe 82,276 hrs · 11,957 cycles

NR 2 ENGINE 1ST STAGE ROTO DISK FAN SHAFT HAS OIL LEAKS. REMOVED AND REPLACED NR 2 ENGINE FAN HUB MANIFOLD SEAL, PER MM 72-31-03-404-005-H00. OPERATED ENGINE PER MM 71-00-00-862-053-H03. NO LEAKS NOTED.

Part: PACKING — LEAKING (DISK SHAFT) · airframe 82,276 hrs · 11,957 cycles

NR 1 ENGINE 1ST STAGE ROTO DISK SHAFT HAS OIL LEAKS. REMOVED AND REPLACED NR 1 BEARING MANIFOLD PACKING ON NR 1 ENGINE, IAW 767 AMM 72-31-03. PENDING ENGINE IDLE, RUN LEAK TEST. OPERATED ENGINE PER MM 71-00-00-862-053-H03. NO LEAKS NOTED.

Part: STATUS MESSAGE — FALSE ACTIVATION (FIRE LOOP) · airframe 82,218 hrs · 11,936 cycles

LT ENG FIRE LOOP 1 STATUS MSG DISPLAYS INTERMITTENTLY, BEGAN DURING CRUISE. TRANSFERRED TO MDDR 133668 PER MEL 26-11-01-01, CAT C, DUE SEPT 10 2020. T/S LT ENG LOOP 1 PER W/D 26-11-11 UPPER AFT WIRE DET T681 WIRE W5324-002R-16 SHORTED TO GND. REPAIRED AND INSTALLED TERMINAL, PER SWPM 20-30-11. PERFORMED LT ENG FIRE DET SYS OPS TEST, OK PER AMM 26-11-00/715. MDDR 133668 CLEARED UP, PLACARD REMOVED.

Part: LOGIC CARD — MALFUNCTIONED (FIRE LOOP) · airframe 82,196 hrs · 11,929 cycles

L ENG FIRE LP 1 STATUS MSG INTERMITTENT IN FLIGHT. ISSUED DMI #133495 PER MEL CH. 26-11-01-01, CAT "C", PER MOCC: AM. REMOVED AND REPLACED LOGIC TEST FIRE/OVERHEAT CARD 1 AT P54 PANEL OPS CHECK GOOD NO FAULTS NOTED AT THIS TIME IAW AMM 26-11-01.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT A/C PACK) · airframe 82,158 hrs · 11,917 cycles

"R PACK OFF" EICAS MESSAGE @ 4000'. PERFORMED BITE OPERATIONAL CHECK OF PACK SYSTEM PER AMM 21-00-00. OPS CHECK GOOD, NO MESSAGES. COULD NOT DUPLICATE AT THIS TIME

Part: CIRCUIT CARD — MALFUNCTIONED (FIRE LOOP) · airframe 82,125 hrs · 11,906 cycles

STATUS MSG L ENG FIRE LOOP 1(<P>ISSUED MDDR 133103 IAW MEL 26-11-01-01, CAT C, DUE 29AUG20.</P><P>LP 1297199: PERFORMED VISUAL INSPECTION ON LOWER FWD ENG #1 FIRE DETECTOR. FOUND DETECTOR ELEMENT TOUCHING THE SUPPORT TUBE IAW FIM 26-11 FT 802. READJUSTED ELEMENT AWAY FROM SUPPORT TUBE. PERFORMED FIM 26-11 FT 805. OPS CHECKS NORMAL. NO FAULTS OR STATUS MESSAGE NOTED. THIS CLEARS MDDR 133103. MCC NOTIFIED.</P><P>LP&NBSP;1297200:&NBSP;TRANSFERRED (RE-OPENED) TO DMI 133103 PER MEL 26-11-01-01 CAT "C". DDPG PROCEDURES C/W.</P><P>LP 1274715, ITEM M11: REMOVED AND REPLACED FIRE CARD M681. OPS CK GOOD IAW 767MM 20-41-01 &AMP; 26-11-00. PERFORMED WIRING CHECK OF DETECTORS, NO DEFECTS NOTED IAW 767 WDM 26-11-01. THIS ITEM CLEARS DMI # 133103. PLACARDS REMOVED. MCC JESUS NOTIFIED. T/I: TJ @ 15:19Z.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENG FIRE LOOP) · airframe 82,116 hrs · 11,903 cycles

L ENG FIRE LOOP 1 STATUS MSG CARRIED OUT TEST IAW FIM 26-11 FAULT TREE 805 (EICAS MESSAGE L ENG FIRE LP 1(LP2) DISPLAYED, FIGURE 105+104, MESSAGE NOT SHOWN.

Part: ISOLATION VALVE — MALFUNCTIONED (LEFT) · airframe 82,049 hrs · 11,882 cycles

LEFT ISOLATION VALVE DOESN'T OPEN WITHOUT REPETITIVE RE-CYCLING OF BUTTON. PERFORMED LEFT ISOLATION VALVE TEST IAW AMM 36-11-04-214-022 AND FOUND GOOD.

Part: OXYGEN MASK — INOPERATIVE (SEAT) · airframe 81,913 hrs · 11,837 cycles

RIGHT SUPERNUMERARY SEAT O2 MASK INOP (SUPERNUMERARY OXYGEN SYSTEM. ASSOCIATED SEAT NOT OCCUPIED. REMOVED AND REPLACED O2 BOX AT RH SUPERNUMERY SEAT. OPS CK AND LEAK CHECK GOOD. IAW AMM 35-11-51.

Part: WARNING MESSAGE — FALSE ACTIVATION (WX RADAR) · airframe 81,900 hrs · 11,833 cycles

WXR SYS STATUS MESSAGE DISPLAYED ON BLOCK-IN. WXR FAIL DISPLAYED MOMENTARILY ENROUTE. PERFORMED WX RADAR BITE PROCEDURE PER FIM 34-43- FT 805, OPS CHECKED GOOD.

Part: PRESSURE SWITCH — INOPERATIVE (RT FUEL BOOST) · airframe 81,887 hrs · 11,828 cycles

RIGHT AFT FUEL BOOST PUMP INOPERATIVE. REMOVED AND REPLACED PRESSURE SWITCH IAW AMM 28-42-01. OPS NORMAL.

Part: INDICATION SYS — FALSE INDICATION (ENG VIBRATION) · airframe 81,891 hrs · 11,829 cycles

DURING TAKEOFF AND CLIMBOUT THE LEFT VIBRATION INDICATOR PEGGED AT 5.0 UNITS FOR A COUPLE SECONDS THEN WENT AWAY, THEN CAME BACK, THEN WENT AWAY. PERFORMED TROUBLESHOOTING IAW FIM 71-05, FAULT TREE 852, AND PERFORMED AN ENGINE VIBRATION SURVEY IAW AMM 71-00-00/501 AND VIB FOUND NORMAL.

Part: RADAR — MALFUNCTIONED (WX SYSTEM) · airframe 81,867 hrs · 11,819 cycles

THE WX RADAR IS PAINTING RANDOM SOUTHS, OR THE RIGHT SIDE FROM 1-3 O'CLOCK POSITIONS. THE WX IS VFR WITH NO PRECIP. PERFORMED OPERATIONAL TEST OF WX RADAR IAW AMM 34-43-00, TEST GOOD AT THIS TIME.

Part: IDG — MALFUNCTIONED (LEFT) · airframe 81,861 hrs · 11,816 cycles

L GEN OFF, AFTER ENGINE START. REMOVED AND REPLACED THE LT ENG IDG IAW AMM 24-11-01-404-002-004. OPERATIONAL TEST DONE IAW AMM 24-11-00-715-005, LEAK CHECKED GOOD. REMOVED AND REPLACED LEFT GENERATOR CONTROL UNIT IAW TASK 24-22-02-004-010.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 81,853 hrs · 11,813 cycles

L ENG HPSOV EICAS DURING DESENT. FAULT CLEARED PER AMM 31-41-00. C/W AIR SUPPLY BITE PER AMM 36-23-00 AND RAN ENGINE PER AMM 71-00-00. NO FAULTS, NO LEAKS.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 81,718 hrs · 11,766 cycles

HYD GEN ON STATUS MESSAGE DISPLAYED. PERFORMED TROUBLESHOOTING AS PER FIM 24-25 FAULT TREE 804 AND THE SYSTEM IS OK AT THIS TIME.

Part: FAN — WARNING MESSAGE (FWD E/E BAY) · airframe 81,713 hrs · 11,764 cycles

FWD EQUIP COOLING EXHAUST FAN EICAS MESSAGE DISPLAYED. REMOVED AND REPLACED THE FWD EQUIPMENT COOLING EXHAUST FAN AND OPS CHECKED GOOD. EICAS MESSAGE ERASED.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 81,448 hrs · 11,673 cycles

STATUS MSG AFT EQ EXH FAN 2(<P>PERFORMED T/S PER FIM 21-58 FT A02, NO DEFECTS NOTED. SYSTEM OPS CHECK NORMAL.</P>)

Part: TRU — ACTIVATED (COCKPIT) · airframe 81,438 hrs · 11,670 cycles

APU FAILED TO START ON 03 ATTEMPTS ON PRE-FLIGHT - FAULT LIGHT ON.(<P>ITEM TRANSFERRED TO MDDR 128488 IAW MEL 49-11-01A DUE 27MAY20, CAT 'C'.&NBSP;FURTHER T/S REQUIRED.</P>) REMOVED AND REPLACED APU TRU IAW AMM 24-32-04 AND PERFORMED OPERATIONAL CHECK AND FOUND GOOD. THIS CLEARS DMI #128488. MCC NOTIFIED, PLACARD REMOVED.<BR DATA-MCE-BOGUS="1" /></P>)

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 81,424 hrs · 11,665 cycles

STATUS MESSAGE FWD CARGO DET 2(<P>TRANSFERRED TO MDDR 128429 IAW DDG 26-16-01-01-01, CAT "C", DUE 26MAY 20.</P><P><SPAN>LP&NBSP;</SPAN><SPAN>1147381:&NBSP;</SPAN>T/S IAW FIM 26-16 FT 806, BLOCK 110 RECOMMENDS CHANGING FWD CARGO DET #2 DETECTOR M325 . <SPAN>REMOVED AND REPLACED FWD CARGO DET #2 M325 DETECTOR IAW B767AMM 26-16-01.OPS CHECK GOOD. THIS CLEARS DMI 128429. MCC NOTIFIED, PLACARDS REMOVED.</SPAN></P>)

Part: OXYGEN MASK — INOPERATIVE (COCKPIT) · airframe 81,420 hrs · 11,663 cycles

SUPERNUMERARY SEAT O2 MASK INOP.(<P>TRANSFERRED TO MDDR 128370 IAW MEL&NBSP;35-11-03-02A, CAT 'C'</P><P>16MAY20, CVG, LP 1141045, ITEM M4: REMOVED AND REPLACED O2 MASK ASSY PER AMM 35-11-04. THIS CLEARS DMI #128370. MCC NOTIFIED, PLACARDS REMOVED.</P>)

Part: PUMP — LEAKING (NR 1 ENGINE) · airframe 81,411 hrs · 11,661 cycles

DURING ROUTINE MX FOUND #1 ENG DRIVEN PUMP LEAKING FUEL(<P>REMOVED AND REPLACED&NBSP;LH ENGINE FUEL PUMP ASSY PER AMM 73-11-01/401, PERFORMED FUEL LEAK CHECK ON LH ENG DUE TO ENGINE FUEL PUMP REPLACEMENT, RAN ENG AT ALL POWER SETTING IAW 71-00-00, NO LEAKS.</P>)

Part: IDG — LOW (LT ENGINE) · airframe 81,382 hrs · 11,652 cycles

EICAS "LH GEN OFF" ON FINAL APPROACH(<P>SERVICED IDG PER 12-13-03-613-027. PERFORMED FIM 24-20 FT 801. FOUND LAST RUN HIGH FREQ TRIP, IDG PMG WIRING, IDG LOW OIL PRESS, IDG HIGH RISE TEMP. RAN #1 ENG. NO OTHER FAULTS NOTED. OPS CHECK GOOD.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 81,223 hrs · 11,597 cycles

LEFT BLEED ISOLATION VALVE EICAS IN FLIGHT.(<P>CYCLED ISOLATION VALVE MULTIPLE TIMES WITH PRESSURE AND WITHOUT PRESSURE. VALVE OPENED AND CLOSED NORMALLY WITH NO FAULTS. OPS CHECK GOOD IAW AMM 36-11-04.</P>)

Part: OXYGEN MASK — BROKEN (COCKPIT) · airframe 81,095 hrs · 11,553 cycles

CAPT O2 MASK BROKEN.(<P>REMOVED AND REPLACED CAPT'S O2 MASK IAW B767 AMM 35-11-51. OPS CHECK GOOD. NO DEFECTS NOTED.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 81,091 hrs · 11,551 cycles

IDLE DISAGREE EICAS MESSAGE ON TAXI - IN.(<P>VERIFIED IDLE TRA ALL READ THE SAME (34.0) AND PERFORMED MCDP TEST 52. OPS CHECK GOOD. NO FAULTS FOUND PER B767 AMM 73-21-11.</P>)

Part: PRINTED CKT BOARD — DEFECTIVE (BLEED AIR SYS) · airframe 81,054 hrs · 11,538 cycles

R ENG PRV MESSAGE(<P>TRANSFERRED TO MDDR #126215 I.A.W MEL 36-11-08-01-01A, CAT 'C'.&NBSP;</P><P>LOG PAGE 1120934: REMOVED AND REPLACED #2 ENG PRINTED CIRCUIT ASSY BLEED AIR I.A.W AMM 36-11-12. OPS TEST OK, MDDR #126215 CLOSED.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 81,042 hrs · 11,534 cycles

L WXR SYS INOP DISPLAYED WXR FAIL.(<P>PERFORMED FIM PROCEDURE 34-43 TABLE 801. OPS TEST NORMAL. NO DEFECTS. OK TO CONTINUE.</P>)

Part: WIRE HARNESS — DEFECTIVE (RT ENGINE) · airframe 81,044 hrs · 11,535 cycles

R ENG VIB MONITOR DISPLAYS LPT W/ INDICATIONS BETWEEN 0.8 TO 5.0 (MAX SETTLE) NO OTHER ENG ABNORMAL.(<P>TRANSFERRED TO MDDR 126194 IAW MEL 77-31-01-01, CAT C, DUE 03APR20. PLACARD INSTALLED. MX ACTIONS C/W.</P><P>LOG PAGE 1120940: REMOVED AND REPLACED RH ENGINE COMPRESSOR REAR FRAME VIB SENSOR WIRE # 5322 ( HARNESS ) I.A.W SWPM 20-10-11, PERFORMED RH ENGINE RUN I.A.W AMM 77-31-00 AND VIBRATION MONITOR AMM 77-31-00 &AMP; 71-00-00. MDDR 126194 CLOSED.</P>)

Part: UNKNOWN — ODOR (CABIN) · airframe 81,036 hrs · 11,531 cycles

AIR FROM GASPER VENTS SMELLS LIKE WET SOCKS DURING TAKEOFF / CLIMBOUT AND DECENT AND LANDING.(<P>RAN A/C SYSTEM THRU FULL TEMP RANGE IAW 767 AMM 21-00-21. NO DISCREPANCIES NOTED. OPS CHECK GOOD.<BR /></P>)

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 81,032 hrs · 11,530 cycles

LEFT RADAR MANUAL TILT CONTROL IS INTERMITTENT&NBSP;(<P>PERFORMED OPS TEST OF RADAR TILT CONTROL I.A.W AMM 34-43-00. NO DISCREPANCY FOUND.</P>)

Part: UNKNOWN — ODOR (AC SYSTEM) · airframe 81,010 hrs · 11,523 cycles

REPEAT WRITE UP. A/C SMELLS LIKE DIRTY SOCKS, ONLY WHEN ON A/C PNEUMATIC AIR SOURCE.(<P>PERFORMED B767 FIM 21-00-21 TO CLEAR CONTAMINATION FROM THE AIR CONDITIONING SYSTEM, NO DEFECTS NOTED.<BR /></P>)

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 81,003 hrs · 11,520 cycles

TILT CONTROL INOP USING LEFT RADAR SYSTEM.(<P>PERFORMED WEATHER RADAR TEST ON GND IAW AMM 34-43-05. TEST PASS.<BR /></P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 80,982 hrs · 11,512 cycles

RIGHT ENGINE PRV STATUS MESSAGE.(<P>PERFORMED FIM 36-10 FT 847, NO DEFECTS NOTED. BITE SUPPLY MODULE SHOWS NO FAULTS - EICAS MESSAGE CLEARED.</P>)

Part: SUPPORT BRACKET — NOT REPORTED (COCKPIT) · airframe 80,926 hrs · 11,496 cycles

FO AND CAPTAIN EVAS SYSTEM INOP.(<P>TRANSFERRED TO MDDR 125170 PER MEL 25-63-06, CAT 'D'. MCC NOTIFIED. ALL PLACARDS INSTALLED.</P><P>REF LOG PG&NBSP;1182595&NBSP;- ITEM 11: REMOVED AND REPLACED RETRACTABLE TABLE SUPPORT BRACKET AS PER EO 6725A222, REV 3, PART 3. THIS CLEARS DMI 125170. MCC NOTIFIED. PLACARD REMOVED.</P>)

Part: EVA SYSTEM — INOPERATIVE (COCKPIT) · airframe 80,926 hrs · 11,496 cycles

FO AND CAPTAIN EVAS SYSTEM INOP.(<P>TRANSFERRED TO MDDR 125170 PER MEL 25-63-06, CAT 'D'. MCC NOTIFIED. ALL PLACARDS INSTALLED.</P>)

Part: DUCT — DAMAGED (ANTI-ICE) · airframe 80,883 hrs · 11,481 cycles

DURING WALK-AROUND, FOUND L/H WING SLAT PANEL 525AT DAMAGED. THERMAL ANTI-ICE DUCT REQUIRES REPLACEMENT.&NBSP;(<P>REMOVED AND REPLACED THERMAL ANTI-ICE DUCT PER AMM 27-81-02 AND 30-11-06/401, OPS CHECK PER TAI DUCT LEAK TEST 30-11-00-790-801, OPS CHECK GOOD.</P>)

Part: WARNING LIGHT — FALSE ACTIVATION (RT ENGINE PRV) · airframe 80,841 hrs · 11,464 cycles

RIGHT ENG PRV EICAS MOMENTARY ILLUMINATED AFTER RIGHT ENG START.(<P>PERFORMED BITE TEST PER AMM 36-23-00. NO FAULTS NOTED. NO EICAS MESSAGE REMAINED.</P>)

Part: HOOK AND LOOP — MISSING (COCKPIT EVAS) · airframe 80,795 hrs · 11,449 cycles

COCKPIT EVAS SYSTEM INOP (COCKPIT SMOKE VISION SYSTEM (CSVS) (STC ST00731LA))(<P>TRANSFERRED TO MDDR #124452 PER ATLAS DDG 25-63-06, CAT "D".</P><P>LP&NBSP;1190645: INSTALLED MISSING VELCRO IAW AMM 23-30-01. THIS CLEARS MDDR 124452. PLACARD REMOVED.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (ISOLATION VALVE) · airframe 80,782 hrs · 11,444 cycles

"L BLD ISOLATION VALVE" EICAS MSG AFTER LANDING. QRH COMPLETE.(<P>PERFORMED AIR SUPPLY BITE PER FIM 36-20 FT 804, NO FAULTS NOTED. ALSO PERFORMED L BLEED ISOLATION VALVE TEST IAW AMM 36-11-04. OPS CHECK GOOD. NO EICAS MSG OR VALVE LIGHT PRESENT.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT PRV) · airframe 80,661 hrs · 11,402 cycles

"R ENGINE PRV" EICAS MESSAGE AND BLEED INDICATION LIGHT APPEARED AFTER R ENGINE START.&NBSP; MESSAGE AND LIGHT EXTINGUISHED. "R ENG PRV" STATUS MESSAGE APPEARED.(<P>PERFORMED AIR SUPPLY CONTROL SYSTEM BITE TEST, NO FAULTS&NBSP;NOTED. EICAS MESSAGE CLEARED IAW AMM 36-23-00.</P>)

Part: MODULE — INOPERATIVE (APU) · airframe 80,528 hrs · 11,357 cycles

APU GENERATOR FIELD OFF LIGHT INOP. REMOVED AND REPLACED THE MODULE ASSY IAW AMM 33-13-00.

Part: UNKNOWN — ODOR · airframe 80,437 hrs · 11,322 cycles

RIGHT PACK TURNED ON BEFORE TAKEOFF, ODOR OF "WET PAINT" NOTICED IN COCKPIT. NOTICED ODOR AGAIN DURING DESCENT WITH THRUST CHANGES.(<P>PERFORMED R PACK CONDITIONAL INSPECTION PER AMM 05-51-56. PLACED RH PACK ON MEL PER MCC REQUEST MDDR #120585, MEL # 21-51-01-01, CAT 'C', DUE 24NOV19.</P><P>LP 1218630: OPERATED PACK AT HOT TEMPS. INSPECTED. NO SMELL NOTED. THIS CLEARS MDDR 120585. PLACARDS REMOVED.&NBSP;</P>)

Part: CIRCUIT CARD — DEFECTIVE (BLEED AIR SYS) · airframe 80,382 hrs · 11,301 cycles

R ENG PRV EICAS MSG AFTER ENGINE START.(<P>ITEM 1: REMOVED AND REPLACED HIGH PRESSURE SHUTOFF VALVE IAW B767 MM 36-11-07 AND 36-11-08, NO HELP. OFF PART (PN: 790270-14, SN 880417H).</P><P>ITEM M3: REMOVED AND REPLACED HIGH PRESS CONTROLLER IAW B767 AMM 36-11-07, NO HELP.&NBSP; OFF PART (PN: 773289-15, SN: 2018011638).</P><P>ITEM M2: REMOVED AND REPLACED R ENG BLEED CARD IAW B767 AMM REF 20-41-01. RAN ENG SEVERAL TIMES, NO FAULTS NOTED AT THIS TIME.</P>)

Part: UNKNOWN — ODOR (CABIN) · airframe 80,282 hrs · 11,264 cycles

STRONG FUME SMELL DURING TAKE OFF WITH ENGINES AT T/O THRUST, POSSIBLE BURNING OIL FUMES.&NBSP;(<P>PERFORMED ENG + PNEUMATIC SYSTEM OIL BURN OUT REF B767 FIM 20-00 TASK 801 &AMP; 802. NO FURTHER ODOR DETECTED AT THIS TIME. PERFORMED VISUAL INSPECTION OF PACK R/H AREA, NO OIL OR SUBSTANCES NOTED.</P>)

Part: LEAD — FAULTED (LT ENGINE) · airframe 80,284 hrs · 11,265 cycles

ITEM 1: STATUS MSG L ENGINE IGNITER 1.&NBSP; ITEM 2: INFO ONLY - NO LIGHTOFF L ENG, FIRST START USED BOTH IGNITERS. 2ND START GOOD, ENG START SWITCH REMAINS IN BOTH.&NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP;(<DIV>TRANSFERRED TO MDDR 119429 PER MEL 74-00-01B, CAT 'C', DUE: 31-OCT-2019.</DIV><DIV>LP 1214199 - M5:&NBSP;PERFORMED BITE ON L PIMU, NO FAULTS NOTED. PERFORMED SINGLE IGNITER ENGINE START X2 IAW AMM 71-00-00, BOTH STARTS GOOD. (DMI REMAINS OPEN)</DIV><DIV>REF LOG PAGE 1214213 ITEM M4; REMOVED AND REPLACED LEFT ENGINE #1 IGNITION EXCITER IAW 74-11-01. SEE PAGE 1214214 ITEM M9 FOR FURTHER ACTION PERFORMED P/N OFF 10-631045-2B&NBSP; S/N OFF UNNEP111</DIV><DIV>REF LOG PAGE 1214214 ITEM M9; REMOVED AND REPLACED LEFT ENGINE#1 IGNITION LEAD IAW AMM 74-21-01. THIS CLEARS MDDR 119429.&NBSP;</DIV>)

Part: SMOKE DETECTOR — FALSE ACTIVATION · airframe 80,273 hrs · 11,260 cycles

DURING PRE-FLIGHT INSPECTION, CARGO LOOP 3A, AMBER.(<P>TRANSFERRED TO MDDR 119369 PER MEL 26-16-02-02, CAT 'C', DUE DATE: 29-OCT-2019.</P><P>LP 1086689 - ITEM 2:&NBSP;PERFORMED CARGO/FIRE OVERHEAT TEST PER DDG. #3 A LOOP AMBER LIGHT REMAINS ILLUMINATED. #3 B LOOP TEST GOOD. DMI 119369 REMAINS OPEN</P><P>LP 1214191 - ITEM 2:&NBSP;REMOVED AND REPLACED CARGO SMOKE DETECTOR ASSY 3A REF AMM 26-16-01. OPS CHECK GOOD, NO MESSAGE DISPLAYED. DMI #119369 IS CLEARED. PLACARD REMOVED AND MCC NOTIFIED.&NBSP;<BR /></P>)

Part: UNKNOWN — ODOR (CABIN) · airframe 80,275 hrs · 11,261 cycles

DURING T/O, CLIMB, AND DESCENT; DETECTED A "DIRTY SOCKS" SMELL FROM THE RIGHT PACK/BLEED SYSTEM. SUSPECTED AEROSOLIZED ENG OIL IN BLEED SYSTEM.(<P>RAN RIGHT ENGINE PER AMM 71-00-00. OPERATED RT PACK, NO SMELLS NOTED. AIRCRAFT OK FOR SERVICE.</P><P>NOTE: PERFORMED VISUAL INSPECTION OF RT PACK AREA, NO EVIDENCE OF OIL IAW AMM 21-23-00 AND AMM 21-51-00.</P>)

Part: UNKNOWN — ODOR (CABIN) · airframe 80,277 hrs · 11,262 cycles

DURING TAKEOFF AND CLIMB, DETECTED A "DIRTY SOCK SMELL" FROM THE RIGHT PACK/BLEED SYSTEM. MOST PROMINENT DURING HIGH THRUST CHANGES.(<P>RAN ENGINES PER AMM 71-00-00. OPERATED R/H PACK, NO SMELLS NOTED. AIRCRAFT OK FOR SERVICE. NOTE: PERFORMED VISUAL INSPECTION OF R/H PACK AREA, NO FAULTS OR LEAKS FOUND.</P>)

Part: SWITCH — MALFUNCTIONED (RT BUSS TIE) · airframe 80,260 hrs · 11,256 cycles

RIGHT BUS TIE SWITCH WILL NOT ILLUMINATE.(<P>TRANSFERRED TO MDDR 119253 PER MEL 24-27-04, CAT 'C', DUE 27-OCT-19. MCC NOTIFIED.&NBSP;</P><P>LP 1086681 - M8:&NBSP;PERFORMED RE-LAMP OF RH BUS TIE SWITCH REF AMM 24-27-00, NO HELP. MCC NOTFIED. PARTS ON ORDER. DMI # 119253 REMAINS OPEN.</P><P>LP 1214213 - M5: REMOVED AND REPLACED RIGHT BUS TIE ISOLATION KORRY SWITCH ASSY. OPS TEST GOOD IAW 33-16-02. THIS CLEARS MDDR 119253. MCC NOTIFIED.</P>)

Part: CONTROLLER — MALFUNCTIONED (R2 WINDOW HEAT) · airframe 80,201 hrs · 11,235 cycles

R2 WINDOW HEAT INOP. PERFORMED BITE PROCEDURE ON WINDOW HEAT CONTROL UNITS IAW FIM 30-41 FT 804. NO FAULTS OR DEFECTS NOTED. REMOVED AND REPLACED LEFT FWD AND RT SIDE WINDOW HEAT CONTROLLER UNIT IAW AMM 30-41-01, OPS CHECKED GOOD.

Part: ELT — BROKEN (COCKPIT) · airframe 80,189 hrs · 11,230 cycles

ELT SEAL BROKEN AT L1 DOOR POSITION. REMOVED AND REPLACED COCKPIT PORTABLE ELT REF B767 AMM 25-63-03. NO DEFECTS NOTED AT THIS TIME.

Part: START VALVE — MALFUNCTIONED (LT ENGINE) · airframe 80,104 hrs · 11,199 cycles

INTERMITTENT "LEFT STARTER CUTOUT" MESSAGE WHILE IN FLIGHT&NBSP;(<P>REMOVED AND REPLACED LEFT ENGINE STARTER VALVE IAW B767 AMM 80-11-02. OPS CHECK GOOD AT THIS TIME.&NBSP;</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 80,089 hrs · 11,192 cycles

AFT EQ EXH FAN 1 STATUS MSG.(<P>PLACED EQUIP COOLING MODE SELECTOR ON PANEL TO "STBY" THEN BACK TO "AUTO". ERASED MESSAGE PER FIM 21-26 FT 805.</P>)

Part: GENERATOR — MALFUNCTIONED (APU) · airframe 80,084 hrs · 11,191 cycles

APU COLD SOAK START FAILED. APU COLD SOAK START PERFORMED, APU STARTED, RAN FOR 10 MIN. ALT 38,000; TIME: 2100Z. START FAILED. PERFORMED APU EXTERNAL INSPECTION IAW AMM 49-21-00-206-001. FOUND OIL LEAKING FROM APU GENERATOR HOUSING. SERVICED APU OIL TO FULL, NO HELP. PERFORMED BOEING FIM 49-11 FT 995. SERVICED APU WITH 1/2 QUART OF OIL. CHECKED FOR BITE FAULTS, NONE PRESENT. RAN APU FOR 2 HOURS, RE-CHECKED FOR FAULTS, NONE PRESENT. INSPECTED FOR LEAKS, NONE NOTED AFTER SHUTDOWN. NO EICAS MESSAGE PRESENT. R/R APU GENERATOR IAW AMM 24-21-01. OPS CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (LT ENGINE) · airframe 80,037 hrs · 11,179 cycles

LT ENG, NO LIGHT OFF 1ST ATTEMPT. STARTED SUCCESSFULLY ON 2ND ATTEMPT WITH IGNITION IN BOTH. PERFORMED IGNITION SYSTEM AUDIBLE TEST, LEFT ENGINE PER AMM 74-00-00-705-104-H03. OPS CHECK GOOD, NO DEFECTS NOTED.

Part: RELAY — FAILED (FUEL CROSSFEED) · airframe 79,866 hrs · 11,122 cycles

WHEN OPERATING THE FWD X-FEED, THE VALVE DISAGREE LIGHT DOES NOT ILLUMINATE. (LIGHT TEST OK)(<P>REMOVED AND REPLACED RELAY K2151 IAW FIM 28-22 FT 821 AND SWPM. 20-81-11. OPS CHECK NORMAL.

Part: HEAT EXCHANGER — CONTAMINATED (RIGHT ECS) · airframe 79,813 hrs · 11,104 cycles

A DIRTY SOCK SMELL WAS DETECTED AFTER STARTUP UNTIL TOC. PERFORMED AMM 21-00-21-302-030, REMOVAL OF OIL CONTAMINATION FROM AIR CONDITIONING AND PNEUMATIC SYSTEMS. DURING ENGINE RUN, AFTER SELECTING R PACK TO ON, NOTICED FAINT ODOR COMING FROM GASPER VENTS. PERFORMED CHECK, FOUND AND REMOVED DEBRIS INSIDE RT PRIMARY HEAT EXCHANGER. OPS TEST RT PACK IAW AMM 21-51-00, NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: ECS — CONTAMINATED · airframe 79,802 hrs · 11,101 cycles

AFTER START, A FAINT DIRTY SOCK SMELL WAS DETECTED BUT EBBED. DURING TAKEOFF, THRU FL 250, ODOR RETURNED AND INTENSIFIED. SUSPECT PARTICLIZED ENG OIL ENTERING BLEED SYSTEM. PERFORMED TASK B767 AMM 05-51-56 AND 21-00-21-102-030, REMOVAL OF OIL CONTAMINATION FROM AIR CONDITIONING AND PNEUMATIC SYSTEMS. COULD NOT DUPLICATE DISCREPANCY. A/C OK FOR SERVICE.

Part: MODULATING VALVE — MALFUNCTIONED (HYD SYSTEM) · airframe 79,739 hrs · 11,077 cycles

HYD CTR DEMANDS CAUTION FLASHES WITH EACH FLAP MOVEMENT. REMOVED AND REPLACED PRESS REGULATOR AND S/O VALVE, AND VALVE ASSY MODULATION IAW AMM 29-11-30. OPS CHECKED NORMAL.

Part: SENSOR — MALFUNCTIONED (TAT) · airframe 79,739 hrs · 11,077 cycles

PER ENGINE CONDITION MONITORING ALERT ITEM 2019P-334, REPLACE TAT SENSOR, COMPLIED WITH ITEM 2019P-334 ATTACHED. REMOVED AND REPLACED TAT SENSOR PER AMM 34-12-02.

Part: WIRE HARNESS — FAILED (FUEL VALVE) · airframe 79,739 hrs · 11,077 cycles

PERFORM TROUBLESHOOTING OF THE LEFT ENGINE FUEL VALVE EICAS MESSAGE. REPLACE THE W7 AND W8 HARNESS, THEN PERFORM ENG TEST PER AMM 71-00-00, TEST 2 AND 3. REMOVED AND REPLACED W7 AND W8 HARNESS IAW AMM 73-21-18. TEST 2 AND 3 NORMAL.

Part: STARTER — INOPERATIVE (NR 2 ENGINE) · airframe 79,739 hrs · 11,077 cycles

NR 2 ENGINE STARTER INOPERATIVE. REMOVED AND REPLACED THE STARTER IAW AMM 80-11-01.

Part: ISOLATION VALVE — INOPERATIVE (APU) · airframe 79,695 hrs · 11,060 cycles

APU DID NOT MAKE 21 PSI FOR ENGINE START.(<P>TRANSFER TO MDDR 115491 IAW MEL 49-11-01A CAT C DUE 08AUG19.</P><P>LP 1097989 - M4: PERFORMED APU ECU BITE PROCEDURE IAW B767 AMM 49-61-05. DISCOVERED "APU CONTROL UNIT" FAULTS IN RECENT FAULT HISTORY. SUSPECT BAD APU ECU. DMI #115491 REMAINS OPEN.</P><P>LP 1097990 - M1: REMOVED AND REPLACED APU ECU IAW AMM 49-61-05. DID NOT FIX FAULT. DMI #115491 REMAINS OPEN. OFF PART (P/N: 2117342-20, S/N: 59-B0129)</P><P>LP 0994610 - M2:&NBSP;TROUBLESHOT APU BLEED FAULT IAW FIM 36-10 FAULT TREE 840. AS PER FIM, SUSPECTED FAULTY RIGHT ENG START VALVE. R&AMP;R RIGHT ENG START VALVE IAW AMM 80-11-02. NO FIX. THIS DOES NOT CLEAR DMI 115491. DMI REMAINS OPEN.</P><P>LP 0994615 - M7: REMOVED AND REPLACED RH PNEUMATIC ISOLATION VALVE, LEAK CHECK OK IAW B767 AMM 36-11-04. REMOVED AND REPLACED APU SURGE VALVE, LEAK CHECK AND OPS CHECK GOOD&NBSP;PER AMM 49-53-01. THIS CLEARS DMI 115491, PLACARD REMOVED.</P><P><BR /></P><P>APU SURGE VALVE OFF PART (PN: 979806-12, SN: P-690C)&NBSP;&NBSP;</P><P>NOTE: ACCOMPLISHED DURING A-CHECK (MIA), REFERENCE NRC: 00012</P>)

Part: GASKET — NOT REPORTED (APU) · airframe 79,648 hrs · 11,045 cycles

APU ONLY DEVELOPS 14 PSI DURING FIRST ENGINE START. (<P>TRANSFERRED TO MDDR 115030 IAW DDG 49-11-01-01. (M) PROCEDURES C/W. PLACARDS INSTALLED. NO OTHER DEFECTS NOTED AT THIS TIME.&NBSP;&NBSP;</P><P>LP 1097588 - M4:&NBSP;REMOVED AND REPLACED THE APU FLOW SENSOR GASKET IAW AMM 49-53-08. (M) PROCEDURES REVERSED. PLACARDS REMOVED. OPS CHECK GOOD, NO OTHER DEFECTS NOTED AT THIS TIME. THIS CLEARS MDDR 115030.<BR /></P>)

Part: TRANSCEIVER — MALFUNCTIONED (WEATHER RADAR) · airframe 79,445 hrs · 10,977 cycles

L WXR SYS INOP, AMBER WXR FAIL CAPTION SHOWS ON EHSI.(<P>PERFORMED FIM 34-43-FT 805, FOUND NO DEFECTS, OPS CHECK NORMAL. PLACED WX RADAR TRANSCEIVER&NBSP; P/N 066-50008-0408 ON ORDER WITH MCC, PRECAUTIONARY.

Part: BLADES — DAMAGED (RT ENGINE) · airframe 79,407 hrs · 10,965 cycles

FOUND BLADE #5, #8, #10, #34, #35 DAMAGED ON RT ENG. ALL DAMAGE IS WITHIN LIMITS IAW AMM 72-31-02. (LENGTH X DEPTH) : / #5 BLADE 1" X .04", #8 BLADE 1.5" X .06", #10 BLADE 1.75" X .11", #34 BLADE 2" X .12", #35 BLADE 2" X .12"(<P>TRANSFER TO MDDR 113488 NON-MEL INFO. DUE 16DEC20.</P>)

Part: SOLENOID — MALFUNCTIONED (FUEL SHUTOFF) · airframe 79,362 hrs · 10,950 cycles

L ENG FUEL VALVE EICAS AND LIGHT AFTER FUEL CONTROL SET FROM CUTOFF TO RUN. REMOVED AND REPLACED FUEL S/O SOLENOID IAW AMM 73-21-20. OPS CK AND LEAK CKS IAW AMM 71-00-00 TEST 3, OPS NORMAL, NO LEAKS.

Part: CONTROLLER — MALFUNCTIONED (A/C PACK) · airframe 79,346 hrs · 10,943 cycles

AFT CABIN TEMP MESSAGE ON EICAS.(<P>PERFORMED BITE CABIN PACK CONTROLLER. NO MSG'S AT THIS TIME. OPS CHECK NORMAL IAW B767 AMM 21-44-00.</P>)

Part: ACM — MALFUNCTIONED (LEFT) · airframe 79,334 hrs · 10,939 cycles

LEFT PACK INOP EICAS MESSAGE DISPLAYED.(<P>TRANSFER TO MDDR # 112784 IAW DDG 21-51-01-01 CAT C.</P><P>LOG PAGE 1050947 ITEM M5: REVERSED DDG. T/S PER AMM 21-51-14. LH PACK TEMP CONTROLLER. RAN PACK FOR 2 HRS, CYCLED SWITCH NUMEROUS TIMES DURING OPERATION. ALSO RAN ENGINES TO TRY AND DUPLICATE FAULT. NO FAULTS OR MSGS NOTED. OPS CK GOOD. THIS CLEARS DMI 112784.</P>)

Part: SOLENOID VALVE — MALFUNCTIONED (LT ENGINE) · airframe 79,220 hrs · 10,902 cycles

WHEN L FUEL CONTROL SWITCH TO CUT OFF, LT ENGINE REMAINED RUNNING FOR 15/20 SEC, THEN L ENGINE VALVE ANNUNCIATOR LIGHT ILLUMINATED. (<P>REMOVED FUEL SHUTOFF SOLENOID IAW AMM 73-21-20-004-001-H00. INSTALLED SERVICEABLE SOLENOID VALVE - HMU IAW AMM 73-21-20-404-007-H00.&NBSP; OPS AND LEAK CHECKS GOOD.&NBSP;</P>)

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 79,105 hrs · 10,870 cycles

RADAR IS NOT DEPICTING THE RIGHT WEATHER. (<P>PERFORMED OPERATIONAL TEST ON WEATHER RADAR SYSTEM IAW AMM 34-43-00. OPS CHECK GOOD AT THIS TIME.<BR /></P>)

Part: GASKET — FAILED (HMU) · airframe 78,950 hrs · 10,814 cycles

DURING LEAK CHECK OF HMU FOUND FUEL METER LEAKING FUEL AT GASKET SPLIT LINE.(<P>REMOVED AND PERFORMED FUEL AND HEAT EXCHANGER GASKET AS PER AMM CH 79-21-01. LEAK CHECK GOOD. PERFORMED ENGINE #2 TEST IDLE RUN AS PER AMM 71-00-00 .CHECKS NORMAL, REF ITEM LOG PG 1024117.&NBSP;<BR /></P>)

Part: SHUTOFF VALVE — FAILED · airframe 78,947 hrs · 10,813 cycles

AFTER START OF RIGHT ENGINE. THE RIGHT ENGINE FAILED ( SLOWLY ROLLED BACK) THE EICAS MESSAGE RIGHT ENGINE FUEL VALVE WAS OBSERVED AND THE ENGINE VALVE LIGHT FLICKERED&NBSP;(<P>REMOVED AND REPLACED RIGHT FUEL CUTOFF SOLENOID VALVE IAW AMM REF 73-21-20. NO HELP. SEE LOG PAGE 1024117 ITEM M4 P/N OFF 2718799 S/N OFF 78081-3751. REMOVED AND REPLACED HMU #2 ENGINE IAW AMM 73-21-01. NO HELP ( NOTE PENDING LEAK CHECK). PERFORMED LEAK CHECK OF HMU AS PER 73-21-01. CHECK OK. P/N OFF 442634 S/N OFF BACK3047. LP 1024118: REMOVED AND REPLACED RIGHT FUEL SPAR SHUTOFF VALVE AS PER AMM 28-22-11. OPS CHECK GOOD PER SAME.&NBSP; P/N OFF MA30A1017&NBSP; S/N OFF AA655662. LP 1024120: REMOVED AND REPLACED RIGHT ENGINE FUEL SHUTOFF VALVE PER AMM 28-22-01, P/N OFF 125334D-1&NBSP; S/N OFF T54260&NBSP; INSPECTED INSIDE THE FUEL TANK BEFORE CLOSING. CLOSED ALL FUEL TANK PANELS AS REQUIRE AS PER AMM 28-11-01. LEAK CHECK IAW AMM 28-11-21, NO LEAKS NOTED.&NBSP;&NBSP;</P>)

Part: TRANSCEIVER — MALFUNCTIONED (WEATHER RADAR) · airframe 78,888 hrs · 10,791 cycles

REF W/O 49066 LEFT WEATHER RADAR INOP(<P>REMOVED AND REPLACED LEFT WEATHER RADAR TRANSCEIVER IAW AMM 34-43-01 OPS CHK GOOD</P>)

Part: RADAR — FAILED · airframe 78,763 hrs · 10,753 cycles

LEFT WEATHER RADAR FAIL.(<P>PERFORMED FIM 34-43 F/T 805 OPERATIONAL CHECK GOOD AT THIS TIME.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 78,768 hrs · 10,754 cycles

WINDSHEAR SYS EICAS MESSAGE. WXR FAIL MESSAGE ON HSI AFTER TAKEOFF.(<P>DURING TEST FOUND LEFT WXR FAILED. TRANSFER TO MDDR # 108269 IAW MEL 34-43-01 CAT D DUE DATE 04-JULY-2019. PLACARD INSTALLED.</P><P><BR /></P><P>LP 957878-M5: PERFORMED OPS CHECK ON BOTH L AND R WEATHER RADAR SYSTEMS IAW AMM 34-43-00, OPS CHECK GOOD @ THIS TIME. PERFORMED BITE ON BOTH L AND R TRANSCEIVER IAW FIM 34-43 FT 805, NO FAULTS NOTED. THIS CLEARS MDDR 108269 AND PLACARD REMOVED.<BR /></P>)

Part: COMPUTER — MALFUNCTIONED (WINDSHEAR SYS) · airframe 78,809 hrs · 10,767 cycles

WINDSHEAR SYS EICAS MSG @FL 400(<DIV>RERACKED EGPWS COMPUTER ALL AURAL WARNINGS AND LIGHTS TEST NML IAW FIM 34-46 FAULT TREE 804 NO FAULTS NOTED.</DIV>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 78,751 hrs · 10,749 cycles

WINDSHEAR SYSTEM EICAS MSG(<P>PERFORMED GROUND TEST, NO FAULTS NOTED IAW AMM 34-43-00.</P>)

Part: DRIVE UNIT — FAILED (WEATHER RADAR) · airframe 78,727 hrs · 10,741 cycles

RIGHT WX RADAR SYSTEM FAILED STATUS MESSAGE&NBSP;&NBSP;(<P>TRANSFERRED&NBSP;TO MDDR 107978 PER MEL 34-43-01.</P><P>LOG PAGE 1053932 REMOVED AND REPLACED WX RADAR DRIVE UNIT IAW AMM 34-43-05 OPS AND SYSTEM CHECK GOOD, MDDR # 107978 CLOSED.&NBSP;</P>)

Part: IDG — FAULTY (LT ENGINE) · airframe 78,713 hrs · 10,736 cycles

LEFT IDG INOP.(<P>TRANSFERRED TO MDDR 107852. PERFORMED&NBSP;OIL SERVICE OF THE IDG PER AMM 12-13-03. THEN PERFORMED OPS TEST OF LEFT&NBSP; IDG PER AMM 24-11-00. NO FAULTS. PERFORMED BPCU BITE PER FIM 24-20 FT 801, NO FAULTS. PERFORMED ENGINE RUN ISOLATED ELEC PWR TO LEFT IDG NO FAULTS. </P><P>LP 1022451: REPLACED IDG PER AMM 24-11-01-404-003-003. OPS CKS GOOD. THIS CLEARS DMI 107852. PLACARDS REMOVED AND MCC NOTIFIED.&NBSP;<BR /></P>)

Part: FIRE LOOP — FALSE ACTIVATION (LT ENGINE) · airframe 78,666 hrs · 10,722 cycles

L ENG FIRE LOOP 1 ON EICAS(<P>PLACED FIRE LOOP 1 ON MEL 26-11-01-01 CAT C MDDR# 107623 DUE DATE 03MAR19.</P><P>LP 1053935:&NBSP;<SPAN>REPLACED LOWER AFT FIRE LOOP PER AMM 26-11-02 OPS GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (GENERATOR DRIVE) · airframe 78,662 hrs · 10,721 cycles

ELEC GEN DRIVE L MESSAGE DISPLAYED AFTER ENGINE START(<P>TRANSFERRED TO MDDR&NBSP;PER MEL 24-00-01-01&NBSP;DMI 107569&NBSP;DUE 22FEB19</P><P>LP 1085774-M8: SERVICED IDG OIL PER AMM 12-13-03.&NBSP;PERFORMED ENGINE RUN IAW B767 AMM 71-00-00 AND OPS CHECK THE LEFT IDG FOR FIVE MINUTES IAW B767 AMM 24-11-00.&NBSP;BPCU BITE GOOD. ALL SYSTEM OPS CHECK NORMAL AND THIS CLEARS MDDR 107569, PLACARD REMOVED.</P>)

Part: FIRE LOOP — FAILED (LT ENGINE) · airframe 78,623 hrs · 10,707 cycles

L ENG FIRE LOOP 1(<P>TRANSFER TO MDDR 107354 IAW DDG 26-11-01-01 CAT C DUE 25FEB19.</P><P>LP 1085769: REMOVED AND REPLACED #1 LOOP IAW B767 AMM 26-11-02.&NBSP;</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (WX RADAR SYSTEM) · airframe 78,587 hrs · 10,696 cycles

WXR SYS STATUS MESSAGE.(<P>PERFORMED WEATHER BITE SYSTEM TEST OPS CHECK OK IAW AMM 34-43-01 NO FAULTS NOTED.&NBSP;</P>)

Part: IDG — DISCONNECTED (LEFT) · airframe 78,585 hrs · 10,695 cycles

&NBSP; (LH IDG INOP) REF. DMI 107084(<P>&NBSP;PERFORMED BPCU BITE IAW FIM 24-20 TASK 804 FOUND IDG DISCONNECT MSG. RECONNECTED IDG IAW 24-11-01 AND RAN ENGINES FOR 10 MIN IAW 71-00-00 MSG DID NOT RETURN, LEFT GEN OUTPUT NORMAL NO FURTHER DEFECTS NOTED. .</P>)

Part: OIL FILTER — WARNING MESSAGE (RIGHT) · airframe 78,585 hrs · 10,695 cycles

STATUS MSG RH OIL FILTER(<P>R&AMP;R RH ENGINE OIL FILTER I.A.W A.M.M 79-21-04 PERFORMED ENGINE RUN FOR 10 MIN I.A.W 71-00-00 MESSAGE DID NOT RETURN, LEAK CHECK GOOD. NO FURTHER DEFECTS NOTED. VERIFIED MASTER CHIP DETECTOR WITHIN LIMITS</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (SHUTOFF VALVE) · airframe 78,581 hrs · 10,694 cycles

STATUS MESSAGE LEFT ENGINE PRV LEFT ENGINE HPSOV(<P>PERFORMED FIM BITE IAW FIM36-20-00 NO DEFECTS NOTED OPS TEST GOOD IAW AMM 36-11-18<BR /></P>)

Part: SHUTOFF VALVE — UNKNOWN (LEFT) · airframe 78,581 hrs · 10,694 cycles

DURING T/O EICAS MESSAGE LEFT ENGINE HPSOV(<P>REMOVED AND REPLACED LEFT ENGINE HPSOV IAW AMM 36-11-07 OPS CHECK NORMAL<BR /></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (SHUTOFF VALVE) · airframe 78,606 hrs · 10,702 cycles

L ENG HPSOV EICAS MESSAGE PERFORMED QRH PROCEDURES.(<P>PERFORMED BITE TEST PER FIM 36-20-00 NO DEFECTS NOTED. PERFORMED OPS CHECK OF HPSOV PER AMM 36-11-07. NO DEFECTS NOTED AT THIS TIME NO PREVIOUS HISTORY FOUND. EICAS MESSAGE CLEARED.<BR /></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (WEATHER RADAR) · airframe 78,559 hrs · 10,685 cycles

WXR SYS STATUS MSG.(<P>RESET WXR CB AND TESTED WXR SYSTEM IAW 34-43-00, OPS CHECK NORMAL.<BR /></P>)

Part: SEAL — LEAKING (MAIN CARGO DOOR) · airframe 78,575 hrs · 10,690 cycles

WHILE PRESSURIZING AIRCRAFT FOUND LEAK AT MAIN CARGO DOOR AFT CORNER.(<P>CLEANED AND LUBRICATED MCD SEAL AT LOWER AFT CORNER IAW B767 AMM 52-32-00,PRESSURIZATION OP'S CHECK NORMAL,NO LEAKS NOTED IAW AMM 21-31-00.</P>)

Part: SWITCH — BROKEN (FUELING PANEL) · airframe 78,556 hrs · 10,684 cycles

FUELING PANEL LEFT MAIN TANK SET BUTTON BROKEN.(<P>R/R LOAD SELECT SWITCH IAW AMM 28-21-11,OPS CHECK NORMAL.</P>)

Part: BACK LIGHT — INOPERATIVE (FUEL INDICATOR) · airframe 78,556 hrs · 10,684 cycles

FUELING PANEL LEFT LOAD SELECT INDICATOR BACK LIGHT INOP.(<P>R/R FUEL PANEL LEFT LOAD SELECT INDICATOR IAW AMM 28-41-06 OPS CK NORMAL.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 78,481 hrs · 10,652 cycles

STATUS : RT OIL FILTER&NBSP; (EICAS MSG)&NBSP;(<P>PERFORMED ENGINE RAN PER AMM 71-00-00-967-053-G03, CHECK MAIN OIL CHIP DETECTOR PER 79-21-05-002-002-H00 NO METAL CHIPS FOUND. ALSO RAN FIM 79-35 FT 803 NO FAULTS FOUND. OK FOR SERVICE MCC NOTIFIED</P>)

Part: CONTROL PANEL — FAULTY (EXTERNAL POWER) · airframe 78,459 hrs · 10,647 cycles

LT BUS TIE ISLN LIGHT INOP.(<P>R&AMP;R AC EXTERNAL POWER&NBSP;PANEL ASSY OPS CK GOOD IAW AMM 24-22-01. OPS CKD NML.<BR /></P>)

Part: BATTERY — INOPERATIVE (MAIN) · airframe 78,379 hrs · 10,616 cycles

RIGHT BUS TIE INOP A/C HAS NO POWER ON RIGHT BUS. REMOVED AND REPLACED A/C MAIN BATTERY. OPS CHECKS GOOD IAW AMM 24-31-01. RT AND LT BUS TIE SYSTEMS OPS CHECK GOOD IAW AMM 24-33-00 AND 24-50-00.

Part: EXCITER — MALFUNCTIONED (APU) · airframe 78,204 hrs · 10,557 cycles

APU DIDN'T START. REMOVED AND REPLACED APU IGNITION EXCITER IAW AMM 49-41-03. OPS CHECK GOOD.

Part: IDG — ABNORMAL (LT ENGINE) · airframe 78,209 hrs · 10,559 cycles

LEFT GEN FIELD LIGHT OFF A/C LOST AC POWER WHILE PARKING W/ENGINES RUNNING. REMOVED AND REPLACED NR 1 ENGINE IDG IAW AMM 24-11-01. OPS CHECKED GOOD.

Part: PROBE — DEFECTIVE (ICE DETECTOR) · airframe 78,126 hrs · 10,525 cycles

ICE DETECTOR ON WHEN IN NO ICING SKIES WERE CLEAR REMAINED ON ENTIRE FLIGHT(<P>REMOVED AND REPLACED ICE DETECTOR PROBE IAW AMM 30-81- 01 TEST NORMAL</P>)

Part: WARNING LIGHT — FALSE ACTIVATION (ISOLATION VALVE) · airframe 78,113 hrs · 10,519 cycles

ON LANDING, EICAS FOR THE LT BLEED ISOLATION VALVE. ENGINE ANTI-ICE WAS ON AT TIME OF LANDING. PERFORMED APU RUN AND CYCLED THE LT BLEED ISOLATION VALVE AND FOUND IT TO OPERATE NORMAL IAW MM 49-00-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI-ICE SYSTEM) · airframe 78,113 hrs · 10,519 cycles

RECEIVED AN ICE DETECTION ON, ICE DETECTION OFF INTERMITTENTLY DURING FLIGHT. PERFORMED AN OPS CHECK OF THE ICE DETECTION SYSTEM IAW AMM 30-81-00, NO MESSAGES INDICATED.

Part: UNKNOWN — VIBRATION (LT ENGINE) · airframe 78,041 hrs · 10,495 cycles

LEFT ENGINE N2 VIBRATION INCREASED TO 4.2 WITH THRUST AT IDLE, DECREASED WITH THRUST ADVANCED. PERFORMED AVM SYSTEM TEST IAW AMM 77-31-00-770-015-H00, NO FAULTS FOUND, VIBRATION WITHIN LIMITS.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 77,949 hrs · 10,461 cycles

STATUS: WXR SYS LEFT WX AFTER TAKE OFF "FAIL" SHOWN ON HSI. PERFORMED BIT TEST IAW FIM 34-43 F/T 805. OPS NML AT THIS TIME.

Part: CONNECTOR — DIRTY (VIBRATION SYS) · airframe 77,802 hrs · 10,410 cycles

HIGH SPEED REJECTED T/O DUE TO EXCESSIVE VIBRATION NOISE. INITIATED REJET AT 118 KNOTS. VIBRATION INCREASED WITH AIRSPEED INCREASE. LEFT ENGINE VIBES VARIED FROM 0.5 TO 4.7 AFTER VACATING RUNWAY. INSPECTED CORE VIBE ACC WIRES, CLEANED CONNECTOR ON FAN VIBE ACC. PERFORMED OPERATIONAL TEST OK AVM SYSTEM PER MM 71-31-00 WITH ENG RUN IAW AMM 71-00-00, ALL INDICATIONS STEADY.

Part: TRU — FAULTY (APU) · airframe 77,536 hrs · 10,313 cycles

APU INOP ECU BITE FAULTING A/C START CIRCUIT AND MINI FLAGS 23,24. REMOVED AND REPLACED APU START TRU IAW AMM 24-34-04. OPS CHECK GOOD.

Part: OIL SYSTEM — LEAKING (APU) · airframe 77,522 hrs · 10,307 cycles

APU OIL LEAK LEFT SIDE DUCT. TRANSFERRED TO MDDR 96488 PER MEL 49-11-01A CAT.

Part: INDICATOR — FAULTY (COCKPIT) · airframe 77,517 hrs · 10,306 cycles

STBY ENG INDICATOR HAS FAILED FLAG INDICATIONS. REMOVED AND REPLACED STBY ENG INDICATOR ( SEI ) AS PER AMM 77-41-01.

Part: SHUTOFF VALVE — FAULTY (FUEL SYSTEM) · airframe 77,517 hrs · 10,306 cycles

LEFT ENGINE VALVE INDICATION INOP. REMOVED AND REPLACED LEFT ENGINE FUEL SHUTOFF VALVE ACTUATOR IAW AMM 28-22-11. OPS CHECK GOOD AT THIS TIME.

Part: OIL SYSTEM — LOW (APU) · airframe 77,493 hrs · 10,298 cycles

AFTER LANDING APU WOULD NOT START AND "APU FAULT" EICAS. PERFORMED APU ECU BIT CK IAW AMM 49-61-05 SHUT DOWN/NO START DUE TO LOW OIL PRESS. CLEARED FAULTS ECU CKS GOOD. SERVICED APU OIL 5 QTS TO FULL IAW AMM 12-13-04.

Part: CONTROL BOX — MALFUNCTIONED (CANI TEMP) · airframe 77,480 hrs · 10,292 cycles

FWD ZONE TEMP CONTROLLER. REMOVED AND REPLACED FWD ZONE TEMP CONTROL BOX. PERFORMED BITE TEST SYS TEST NORMAL AT THIS TIME.

Part: SHUTOFF VALVE — FAILED (BLEED AIR SYS) · airframe 77,480 hrs · 10,292 cycles

NR 2 ENGINE PRSOV FAILED ENGINE PNEUMATIC HEALTH CHECK. REMOVED AND REPLACED PRSOV ON NR 2 ENGINE PER AMM 36-11-09.

Part: SKIN — DENTED (FUSELAGE) · airframe 77,480 hrs · 10,292 cycles

FOUND TWO DENTS ADJACENT TO EACH OTHER AT RIGHT UPPER HALF OF FUSELAGE APPROX AT STA 1197 BETWEEN STRINGER 3R-4R, BELOW JOINT LAP. REMOVED 3EA FASTENERS BETWEEN 1197+88 AND STA 1197+132 STR 2R AND 4R, HFEC AREA NO CRACKS NOTED, RE-INSTALLED 3EA FASTENERS AT AREA IAW EA18144 REV IR.

Part: STARTER — DEFECTIVE (APU) · airframe 77,480 hrs · 10,292 cycles

APU MOTOR WIRES LOOSE AT APU COMPARTMENT. REMOVED AND REPLACED APU STARTER PER AMM 49-41-01.

Part: RADAR — MALFUNCTIONED (WEATHER SYS) · airframe 77,432 hrs · 10,272 cycles

WEATHER RADAR TILTS TO MINUS 15 IN AUTO. RESET THE CIRCUIT BREAKER FOR WEATHER RADAR SYSTEM, MESSAGE CLEARED. PERFORMED A SYSTEM TEST, SYSTEM TESTED NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (FIRE LOOP) · airframe 77,290 hrs · 10,222 cycles

APU FIRE LOOP 1 STATUS MESSAGE. ACCOMPLISHED FIM 26-15 FT 803 & 804. APU FIRE DETECTION BITE PROCEDURE MESSAGE CLEARED. OPS CHECKED NORMAL,

Part: RADAR — MALFUNCTIONED (WX SYSTEM) · airframe 77,157 hrs · 10,165 cycles

WEATHER RADIO FAIL FLAG ON BOTH MFDS, SWITCHED TO RT WEATHER RADAR SYSTEM. WEATHER RADAR SYSTEM STATIS MESSAGE AFTER LANDING. ACCOMPLISHED FIM 34-43-00/201 TK 801, FAULT ERASED. WEATHER RADAR OPS CHECKED GOOD IAW AMM 34-43-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT A/C PACK) · airframe 77,106 hrs · 10,151 cycles

LEFT PACK TEMP EICAS MESSAGE. RAN THE PACK FOR SEVERAL MINUTES, NO TEMP ISSUES AT THIS TIME, NO EICAS MESSAGES IAW AMM 21-61-00, AND 36-00-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT A/C PACK) · airframe 76,959 hrs · 10,093 cycles

LEFT PACK TEMP EICAS MESSAGE, COMPLETED QRH PROCEDURES. EICAS CONTROL MESSAGE INOPERATIVE LIGHT EXTINGUISHED. PERFORMED AN OPS CHECK OF THE LT PACK , OPS CHECKED GOOD IAW AMM 21-51-00-705-161. PERFORMED A BITE CHECK OF THE LT PACK TEMP CONTROLLER, BITE CHECKED GOOD IAW AMM 21-51-00-705-001.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT A/C PACK) · airframe 76,917 hrs · 10,077 cycles

AFTER ENGINE START, LEFT PACK EICAS MESSAGE. COMPLIED WITH QRH. FOUND RAM AIR INLET DOOR ACTUATOR FAULTED ON PACK TEMP CONTROLLER. CLEARED FAULT, RAN BITE TEST IAW MM 21-51-14, NO FAULTS FLAGGED. RAN LT PACK IN AUTO ON FULL HOT NO DEFECTS NOTED. GOOD FOR SERVICE.

Part: BLOWER — FAILED · airframe 76,677 hrs · 9,985 cycles

AFT DET FAN & AND FWD DET FAN MAINTENANCES MESSAGES DISPLAYED. R & R THE NR 1 BLOWER IAW AMM 26-16-02. OPS CHECKED GOOD. NO MESSAGES DISPLAYED.

Part: WARNING MESSAGE — FALSE ACTIVATION (WX RADAR SYS) · airframe 76,670 hrs · 9,981 cycles

STATUS MESSAGE FOR THE WEATHER RADAR SYS, DISPLAYED. PERFORMED A WEATHER RADAR SYS TEST IAW AMM 34-43-00, OPS CHECKED GOOD, MESAGES CLEARED AND DID NOT RETURN.

Part: VALVE — NO TEST (NR 1 ENG FAN) · airframe 76,670 hrs · 9,981 cycles

NR 1 ENGINE FAN AIR VALVE FAILED A PNEUMATIC TEST. REMOVED AND REPLACED THE NR 1 ENGINE FAN AIR VALVE IAW AMM 36-11-16. OPS CHECKED NORMAL.

Part: DUCT — CRACKED (LT MLG WW) · airframe 76,670 hrs · 9,981 cycles

LEFT WHEEL WELL FWD DUCT CRACKED(<P>REMOVED AND REPLACED L/H WHEEL WELL FWD DUCT IAW AMM 36-11-01 OPS CHECK NORMAL</P>)

Part: WINDOW — FAILED (R1) · airframe 76,670 hrs · 9,981 cycles

R1 WINDOW HAS SIGNS OF MOISTURE AND ARCING. REMOVED AND REPLACED THE R1 WINDOW IAW AMM 56-11-01.

Part: RADAR — MALFUNCTIONED (WX SYSTEM) · airframe 76,659 hrs · 9,975 cycles

WEATHER RADAR SYS STATUS MESSAGE. PERFORMED A WEATHER SYSTEM TEST, OPS CHECKED OK IAW AMM 34-43-00.

Part: ECS — MALFUNCTIONED (AFT CABIN) · airframe 76,457 hrs · 9,917 cycles

AFT CABIN TEMP CONTROL INOP(<P>TRANSFERRED TO MDDR 87017 PER MEL 21-61-04-02 CAT C DUE 19DEC17</P><P>REACTIVATED VALVE AND OPS CHECK SYSTEM PER AMM 21-61-00 ZONE TEMP OPS CHECK. ALL OPS CHECK NORMAL MDDR 87017 CLEARED.</P>)

Part: SWITCH — MALFUNCTIONED (RT ENGINE) · airframe 76,269 hrs · 9,864 cycles

RIGHT ENGINE BLEED OFF LIGHT INOPERATIVE. REMOVED AND REPLACED THE SWITCH IAW SWPM 20-84-15. OPS CHECKED NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT A/C PACK) · airframe 76,139 hrs · 9,829 cycles

DURING DESCENT, A RIGHT PACK OFF MESSAGE ILLUMINATED. PERFORMED A BITE ON THE RT PACK CONTROLLER IAW AMM 21-51-24, NO FAULTS FOUND. PACK OPS OK.

Part: VALVE — LEAKING (LT ENGINE) · airframe 76,130 hrs · 9,827 cycles

LEFT ENGINE HAS A SMALL FUEL SEEPAGE FROM THE HPT TURBINE COOLING VALVE SHROUD DRAIN. REMOVED AND REPLACED LEFT ENG TCC VALVE IAW AMM 75-24-01 , TEST RAN THE NR 1 ENGINE FOR LEAK CHECK , NO LEAKS FOUND, OPS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 76,088 hrs · 9,814 cycles

DURING RETURN TO SMF R PACK INTERMITTENTLY DISPLAYED PACK OFF. PERFORMED PACK SYSTEM TEST IAW AMM 21-51-00 ALL OPS NORMAL OK FOR SERVICE.

Part: CONTROLLER — MALFUNCTIONED (CABIN TEMP) · airframe 76,047 hrs · 9,800 cycles

AFT CABIN TEMP EICAS MESSAGE ON CLIMBOUT. PERFORMED A BITE TEST ON THE TEMP CONTROLLER, ALL CHECKED GOOD IAW 21-51-00.

Part: VALVE — FAILED (CABIN TEMP) · airframe 76,047 hrs · 9,800 cycles

AFT CABIN AUTO INOPERATIVE LIGHT. REMOVED AND REPLACED THE TRIM AIR VALVE IAW AMM 21-61-07, OPS CHECKED GOOD, LEAK CHECKED GOOD. NO FURTHER DEFECTS NOTED.

Part: PUMP — FAILED (FUEL BOOST) · airframe 76,036 hrs · 9,797 cycles

LEFT AFT FUEL PUMP CAUTION MESSAGE. REMOVED AND REPLACED THE FUEL BOOST PUMP IAW AMM 28-22-03, OPS & LEAK CHECKED OK.

Part: SHIELD — WORN (ENGINE FUEL) · airframe 76,006 hrs · 9,788 cycles

LEFT ENGINE FUEL SUPPLY HOSE COVER WORN. REMOVED AND REPLACED LEFT ENGINE FUEL SUPPLY HOSE COVER. IAW AMM 73-11-07</P>)

Part: VALVE — LEAKING (DRAIN MAST) · airframe 76,006 hrs · 9,788 cycles

LEFT DRAIN MAST LEAK FROM TCC VALVE. TIGHTENED TCC VALVE FUEL LINES ON LEFT ENGINE. NO LEAKS NOTED IAW AMM 70-80-00.

Part: INSULATION — TORN (TERMINAL) · airframe 76,006 hrs · 9,788 cycles

LEFT IDG, 2 TERMINAL INSULATORS WORN. REPLACED SILICONE TAPE ON LEFT IDG ELECTRICAL TERMINALS. IAW SWPM 20-10-11</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (APU FIRELOOP) · airframe 75,841 hrs · 9,739 cycles

STATUS MESSAGE FOR APU FIRE LOOP 1. ACCOMPLISHED FIM 26-15-FT 804, MESSAGES CLEARED SYSTEM NORMAL.

Part: RADAR — UNKNOWN (WX SYSTEM) · airframe 75,751 hrs · 9,712 cycles

WEATHER RADAR SPIKING INTERMITTENTLY AT ALTITUDE. COULD NOT DUPLICATE, ALL OPS CHECKED NORMAL IAW AMM 34-43-01.

Part: WARNING MESSAGE — FALSE ACTIVATION (STANDBY INVERTER) · airframe 75,721 hrs · 9,705 cycles

STATUS MESSAGE FOR THE STANDBY INVERTER. PERFORMED FIM 24-33, FT 808, STEP 2. OPS CHECKED NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (WX RADAR) · airframe 75,678 hrs · 9,693 cycles

LEFT WEATHER RADAR FAIL INDICATION WHEN SELECTED. PERFORMED OPERATIONAL CHECK IAW 34-43-00. NO FAULTS NOTED AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION (APU FIRE LOOP) · airframe 75,662 hrs · 9,688 cycles

APU FIRE LOOP 1 STATUS MESSAGE. PERFORMED AN APU FIRE TEST IAW AMM 26-15-00. SYSTEM TESTED NORMAL, NO STATUS MESSAGES REMAIN. APU STARTED NORMALLY.

Part: LAMP — INOPERATIVE (INSTRUMENT PANEL) · airframe 75,633 hrs · 9,679 cycles

RIGHT GENERATOR DRIVE DISC LIGHT FAILED TO ILLUMINATE AFTER RIGHT ENGINE SHUTDOWN IN BLOCKS. REPLACED THE LAMPED IN THE GENERATOR DRIVE LIGHT IAW AMM 33-13-00 OPS CHECKED GOOD.

Part: FIRE LOOP — FALSE INDICATION (APU) · airframe 75,603 hrs · 9,670 cycles

APU FIRE LOOP 2 MESSAGE. REMOVED AND REPLACED APU FIRE LOOP 2. OPS CHECKED GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (FIRE LOOP) · airframe 75,599 hrs · 9,669 cycles

AP FIRE LOOP 2 STATUS MESSAGE. PERFORMED OPS CHECK IAW AMM 26-15-00. MESSAGE CLEARED. OPS CHECKED GOOD.

Part: VALVE — FAILED (CABIN TEMP) · airframe 75,467 hrs · 9,627 cycles

AFT CABIN TEMP CAUTION MESSAGE. REMOVED AND REPLACED AFT TRIM VALVE IAW AMM 21-61-07 FAULT CLEARED. PERFORMED ZONE TEMP CONTROLLER BITE PROCEDURE IAW FIM 21-61 FT 803 NO FAULTS NOTED .

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 75,230 hrs · 9,544 cycles

ENGINE VALVE LIGHT INOPERATIVE ON PEDESTAL. ENGINE VALVE LIGHT OPERATES NORMAL IAW AMM 28-22-00.

Part: PRESSURE SWITCH — FAILED (RT ENGINE OIL) · airframe 75,174 hrs · 9,525 cycles

RIGHT ENGINE LOW OIL PRESSURE LIGHT INOPERATIVE. REMOVED AND REPLACED RIGHT ENGINE LOW OIL PRESSURE SWITCH & OPS LEAK CHECKED NORMAL IAW AMM 79-33-01.

Part: CONTROL PANEL — FAILED (WX RADAR) · airframe 75,178 hrs · 9,526 cycles

WX RADAR AUTO TILT POSITION IS INOPERATIVE. REMOVED AND REPLACED WEATHER RADAR CONTROL PANEL IAW 34-43-02.

Part: TRANSMITTER — INOPERATIVE (RT ENGINE OIL) · airframe 75,166 hrs · 9,523 cycles

RIGHT ENGINE OIL PRESSURE LIGHT INOPERATIVE. REMOVED AND REPLACED THE NR 2 ENGINE OIL TRANSMITTER IAW AMM 79-32-01. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENGINE IGN) · airframe 75,091 hrs · 9,500 cycles

STATUS MESSAGE LT ENGINE IGNITER. PERFORMED AUDIBLE CHECK, NO DEFECTS NOTED IAW AMM 74-00-00.

Part: WIRE — CHAFED (BOOST PUMP) · airframe 75,079 hrs · 9,496 cycles

LEFT AFT FUEL PUMP LOW PRESSURE LIGHT ILLUMINATED. PERFORMED TROUBLESHOOTING IAW FIM 28-22. FAULT TREE 819 AND FIG 114 FOUND. REPAIRED CHAFED WIRE WITH BACK SHELL AT AFT LEFT BOOST PUMP CONNECTOR D1542 IAW SWPM 20-10-11.

Part: CONTROLLER — MALFUNCTIONED (BLEED AIR SYS) · airframe 75,076 hrs · 9,494 cycles

STATUS MSG R ENG PRV. REMOVED AND INSTALLED RT ENGINE PRV CONTROLLER ASSY IAW 36-11-19 ERF M3 FOR LEAK CK AND INSTALLATION TEST 36-11-19-714.

Part: RELAY — MALFUNCTIONED (FUEL SYSTEM) · airframe 75,037 hrs · 9,482 cycles

LEFT AFT FUEL PUMP EICAS MESSAGE DISPLAYED ON PUSHBACK. REMOVED AND REPLACED GFI RELAY K10705 IAW SWPM 20-81-22. OPS CHECKED GOOD.

Part: RELAY — NOT SEATED (FUEL PUMP) · airframe 75,007 hrs · 9,472 cycles

LEFT AFT FUEL PUMP EICAS MESSAGE ON APPROACH, QRH COMPLETE. RESEATED RELAY K10705 BOOST PUMP OPERATED NORMAL. NO EICAS MESSAGE DISPLAYED IAW AMM 28-22-03.

Part: CONNECTOR — DISCONNECTED (RT A/C PACK) · airframe 74,968 hrs · 9,458 cycles

EICAS RT PACK TEMP AFTER DEPARTURE CLIMBING THROUGH 18000 FT. RAN QRH PROCEDURE AND RESET PACK, OPERATED NORMALLY REMAINDER OF FLIGHT. FOUND RT PACK COMPRESSOR OUTLET TEMPERATURE ELECTRICAL CONNECTOR DISCONNECTED. CONNECTED THE CONNECTOR. RIGHT PACK TEMP OPS CHECKS NORMAL IAW AMM 21-61-00.

Part: TRANSMITTER — FROZEN (LT ENGINE) · airframe 74,924 hrs · 9,448 cycles

LEFT ENGINE FUEL FLOW INDICATOR FROZEN ON DESCENT, FL360, FL315, FROZEN AT 3.9 FROZEN WITH THROTTLE MOVEMENT. REMOVED AND REPLACED LEFT ENG FUEL FLOW TRANSMITTER IAW AMM 73-31-01, OPS AND LEAK CHECKED NORMAL.

Part: PUMP — FAILED (LT BOOST) · airframe 75,036 hrs · 9,481 cycles

LEFT PUMP INOPERATIVE EICAS MESSAGE. REMOVED AND REPLACED THE LEFT AFT FUEL PUMP IAW AMM 28-22-03. OPS AND LEAK CHECKED OK.

Part: CONNECTOR — DIRTY (FUEL INDICATOR) · airframe 74,914 hrs · 9,446 cycles

LEFT ENGINE FUEL FLOW INDICATOR FROZEN ON DESCENT, FL 390 DOWN TO 340, INDICATOR FROZEN AT 4.4, FL 180 ON DOWN. CLEANED AND SEATED THE FUEL FLOW CONNECTOR. OPS CHECKED NORMAL IAW AMM 73-31-01.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENG IGNITER) · airframe 74,775 hrs · 9,409 cycles

STATUS MESSAGE FOR THE RT ENG IGNITER NR 1. AN AUDIBLE TEST OF IGNITION SYSTEM CARRIED OUT IAW AMM 74-00-00-705, TEST PASSED. ENGINE RUN PERFORMED IAW 71-00-00. ALL INDICATIONS SATISFACTORY.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENG IGNITER) · airframe 74,775 hrs · 9,409 cycles

STATUS MESSAGE FOR THE LT ENGINE IGNITER NR 1. AUDIBLE TEST OF IGNITION SYSTEM CARRIED OUT IAW AMM 74-00-00-705, TEST PASSED, ENG RUN PERFORMED IAW AMM 71-00-00, ALL INDICATIONS SATISFACTORY.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENG IGNITER) · airframe 74,775 hrs · 9,409 cycles

STATUS MESSAGE FOR THE LT ENGINE IGNITER NR 2. AN AUDIBLE TEST OF IGNITION SYSTEM WAS CARRIED OUT IAW AMM 74-00-00-705, TEST PASSED. ENGINE RUN PERFORMED IAW AMM 71-00-00 . ALL INDICATIONS SATISFACTORY.

Part: STRINGER — CRACKED (BS 588) · airframe 74,761 hrs · 9,406 cycles

FWD CARGO BS 588, STRINGER 26L. STRINGER FOUND CRACKED. REMOVED DAMAGED STRINGER SECTION AND AREA REINFORCED WITH HAT SECTION AND FILLER.

Part: STRINGER — CRACKED (BS 368) · airframe 74,761 hrs · 9,406 cycles

MAIN DECK, BS 368, STRINGER 10L FOUND CRACKED. REPAIRED THE STRINGER IAW SRM 51-10-02, AND SRM 53-00-03, FIG 201, REPAIR 1.

Part: STRINGER — CRACKED (BS 522-544) · airframe 74,761 hrs · 9,406 cycles

FWD CARGO BETWEEN BS 522 - 544, STRINGER 26L FOUND CRACKED. REMOVED AND REPLACED THE STRINGER SECTION AND REINFORCED AREA WITH HAT SECTION AND FILLER IAW SRM 53-00-03 FIG 201 REPAIR 2, AND INSTALLED IAW SRM 51-40-02..

Part: STRINGER — CRACKED (BS 478-500) · airframe 74,761 hrs · 74,761 cycles

FWD CARGO, BETWEEN BS 478 - 500, STRINGER 26L FOUND CRACKED. REMOVED THE STRINGER SECTION AND REINFORCED AREA WITH HAT SECTION AND FILLER IAW SRM 53-00-03, FIG 201, REPAIR 2, AND SRM 51-40-02.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 74,761 hrs · 9,406 cycles

FWD CARGO B/T STA 478-500 STR 26L. STRINGER FOUND CRACKED. REMOVED DAMAGED STR SECTION AND REINFORCED AREA WITH HAT SECTION AND FILLER P/N N633GT. FABRICATED PER SRM 53-00-03 FIG 201 REPAIR-2 INSTALLED PER SRM 51-40-02.

Part: STRINGER — CRACKED (BS 478-500) · airframe 74,761 hrs · 9,406 cycles

FWD CARGO BAY, BS 478 - 500, STRINGER 26L FOUND CRACKED. REMOVED THE DAMAGED STRINGER SECTION AND FABRICATED A REPAIR IAW SRM 53-00-03, FIG 201, REPAIR 2. INSTALLED IAW SRM 51-40-02.

Part: STRINGER — CRACKED (BS 522-544) · airframe 74,761 hrs · 9,406 cycles

FWD CARGO BAY, BS 522 - 544, STRINGER 26L FOUND CRACKED. REMOVED THE STRINGER SECTION AND FABRICATED A REPAIR IAW SRM 53-00-03, FIG 201, REPAIR 2, AND INSTALLED IAW SRM 51-40-02.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 74,761 hrs · 9,406 cycles

FWD CARGO B/T STA 522-544 STR 26L STRINGER FOUND CRACKED. REMOVED DAMAGED STR SECTION AND REINFORCED AREA WITH HAT SECTION AND PILLER P/N: N633GT. FABRICATED PER SRM 53-00-03 FIG 201 REPAIR-2 INSTALLED PER SRM 51-40-02.

Part: STRINGER — CRACKED (BS 368) · airframe 74,761 hrs · 9,406 cycles

MAIN DECK BS 368, STRINGER 10L FOUND CRACKED. TRIMMED DAMAGE STRINGER SEGMENT IAW SRM 51-10-02. A REPAIR WAS FABRICATED IAW SRM 53-00-03, FIG 201, REPAIR 1.

Part: STRINGER — CRACKED (BS 588) · airframe 74,761 hrs · 9,406 cycles

FWD CARGO BS 588, STRINGER 26L FOUND CRACKED. REMOVED DAMAGED STRINGER SECTION AND A REPAIR WAS FABRICATED IAW SRM 53-00-03, FIG 201, REPAIR 2.