N1181A

Part: WARNING MESSAGE — FALSE ACTIVATION (TE FLAPS) · airframe 98,501 hrs · 25,612 cycles

ON APPROACH, SELECTED FLAPS TO 20. RECEIVED TE FLAP DISAGREE EICAS MESSAGE. DID GO AROUND, DECLARED EMERGENCY, AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED FIM PROCEDURE. NO DEFECTS NOTED.

Part: ESCAPE REEL — UNWANTED DEPLOY (ZONE 100) · airframe 97,063 hrs · 24,960 cycles

1 EA ESCAPE INERTIAL REEL DEVICE FULL OUT(<P>TRANSFER TO DMI 213408 PER MEL 25-61-01-01 CAT C DUE DATE 4AUG2024. PN 379103D-29</P> / <P>LP 1239968 ITEM 5 / ONT / 27JUL24: INSTALLED 1 EA INERTIA REEL IAW B767 AMM 25-61-01. NO FUTHER DEFECTS NOTED. THIS CLEARS MDDR 213408, PLACARD REMOVED.</P>)

Part: ESCAPE REEL — UNWANTED DEPLOY · airframe 96,352 hrs · 24,703 cycles

INERTIAL ESCAPE REEL DROPPED DURING DESCENT(<P>REVOVED AND REPLACED EMERGENCY DESCENT DEVICE IAW AMM 25-51-05. THIS CLEARS MDDR 205698. PLACARD REMOVED.</P>)

Part: ESCAPE REEL — UNWANTED DEPLOY · airframe 96,294 hrs · 24,687 cycles

INERTIAL REEL DEPLOYED ON TAKE-OFF ROLL(<P>R/R DEPLOYER DESCENT DEVICE IAW AMM 25-61-05. NO FURTHER DEFECTS NOTED</P>)

Part: TARGET — OUT OF ADJUST · airframe 96,266 hrs · 24,677 cycles

NOSE AIR/GRND STATUS MESSAGE(<P>INSTALLED TARGET AND ADJUSTMENT BRACKET INSTALLED IAW BOEING AMM 32-61-03 AND OPS CHECK CARRIED OUT IAW AMM 32-61-03, OPS CHECK GOOD.</P>)

Part: ESCAPE REEL — UNKNOWN (COCKPIT) · airframe 96,176 hrs · 24,644 cycles

ONE ESCAPE REEL REMOVED FROM AIRPLANE ( FLIGHT CREW/SUPERNUMERARY ESCAPE DEVICES {ALL CARGO CONFIGURATION} INERTIAL ESCAPE REELS )(<P>REMOVED AND REPLACED ESCAPE REEL IAW AMM 25-61-04. NO FURTHER DEFECTS NOTED. THIS CLEARS MDDR 203776. PLACARDS REMOVED. MCC NOTIFIED.</P>)

Part: ESCAPE REEL — UNKNOWN (UNKNOWN) · airframe 95,897 hrs · 24,560 cycles

ONE INERTIA DESCENT REEL FELL OUT OF HOLDER AND UNWOUND ON CLIMBOUT(<P>REPLACED THE SECOND AFT INERTIA DESCENT REEL DEVICE IAW AMM 25-61-05. THIS CLEARS MDDR 200637. MCC NOTIFIED.</P>)

Part: ESCAPE REEL — UNKNOWN (UNKNOWN) · airframe 95,764 hrs · 24,516 cycles

ESCAPE REELS REQUIRE INSPECT/STOWING MULTIPLE UNLOCKED DURING TAKEOFF(<P>R/R INERTIAL ESCAPE REEL IAW AMM 25-61-05. OPS CHECK GOOD. DMI 199173 CLOSED.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 94,582 hrs · 24,093 cycles

CORROSION ON INTERNAL FUSELAGE SKIN BETWEEN STA 1480 / DSTA 876.3 AND STRINGER S-9RH / S-10RH(<P>DOUBLER REPAIR WAS INSTALLED PER MXA EO TRE6753593 ISSUED ON MAY 05, 2023 (FVCI PROJECT NO. 23088-4). NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 94,582 hrs · 24,093 cycles

CORROSION ON INTERNAL FUSELAGE SKIN BETWEEN STA 1461 AND STRINGER S-14RH / S-15RH(<P>DOUBLER REPAIR WAS INSTALLED PER MXA EO TRE6753590 ISSUED ON MAY 04, 2023 (FVCI PROJECT NO. 23088-1). NO FURTHER DEFECTS NOTED</P>)

Part: BUSHING — UNKNOWN (UNKNOWN) · airframe 94,582 hrs · 24,093 cycles

CORROSION ON BUSHINGS FROM LH MAIN LANDING GEAR SUPPORT BEAM(<P>BUSHINGS WERE REPLACED PER SOPM 20-50-03 AND MXA EO TRE6757193 (CMM 57-54-13 REPAIR 2-1) MAJOR REPAIR. PN: 113T1108-17 AND 113T1108-23</P>)

Part: HINGE FITTING — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 94,582 hrs · 24,093 cycles

STABILIZERS - HORIZONTAL STABILIZER - RH HINGE FITTING BUSHING AND PIVOT BEARING CORROSION / SCRATCH DAMAGES(<P>THE HINGE FITTINGS WERE REPLACED / REPAIRED AND THE PIVOT FITTING WAS REWORKED WITH A SPECIAL TOOL PER MXA EO TRE6755055 REV 1. NO FURTHER DEFECTS NOTED. NOTE: AS ADDITIONAL INFORMATION THE BUSHINGS WERE REPLACED.</P>)

Part: BUSHING — UNKNOWN (UNKNOWN) · airframe 94,582 hrs · 24,093 cycles

CORROSION ON BUSHINGS FROM RH MAIN LANDING GEAR SUPPORT BEAM(<P>BUSHINGS WERE REPLACED PER SOPM 20-50-03 AND MXA EO TRE6757194 (CMM 57-54-13 REPAIR 2-1)</P> / <P>MAJOR REPAIR PN: 113T1108-17 AND 113T1108-23</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,582 hrs · 24,093 cycles

LIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 412 AND STRINGERS S-27LH / S-28LH(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,582 hrs · 24,093 cycles

LIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 654 AND STRINGER S-25LH.(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED</P>)

Part: PANEL — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 94,582 hrs · 24,093 cycles

CORROSION ON PANEL UNDER ROLLER TRAYS BETWEEN STA 564+66 AND STA 564+88 FROM FWD CARGO COMPARTMENT, FLOOR LEVEL.(<P>PANEL WAS REPLACED PER SRM 51-10-02-0G PAR.9. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,582 hrs · 24,093 cycles

LH INBD FLAP, SUPPORT RIB AT IFS 129 APPROX INNER SKIN WITH DENT(<P>AFFECTED AREA WAS REPAIRED PER SRM 51-70-10-2R-4. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,582 hrs · 24,093 cycles

FUEL LEAK AT BODY SPLICE OF STGR L-6 AND RBL 97.42, WING CENTER SECTION(<P>&NBSP;</P> / <P><SPAN>FUEL LEAK AT BODY SPLICE OF STRINGER&NBSP;</SPAN><SPAN>L-6 AND RBL 97.42 WING CENTER SECTION&NBSP;</SPAN><SPAN>WAS REPAIRED AND TEST WAS SATISFACTORY</SPAN></P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,582 hrs · 24,093 cycles

LIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 632 AND STRINGER S-25LH(<P>AFFECTED AREA WAS REPAIRED PER TRE6753601 (IAI CUSTOMER SERVICE #CS-26206-003). NO FURTHER DEFECTS NOTED.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,582 hrs · 24,093 cycles

LIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 500 AND STRINGERS S-27LH / S-28LH(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,582 hrs · 24,093 cycles

CORROSION ON INTERNAL FUSELAGE SKIN BETWEEN STA 1461 AND STRINGER S-8RH / S-10RH(<P>DOUBLER REPAIR WAS INSTALLED PER MXA EO TRE6753592 ISSUED ON MAY 05, 2023 (FVCI PROJECT NO. 23088-3). NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,582 hrs · 24,093 cycles

LIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 174.5 AND 5 INCH ABOVE OF STRINGER S-27LH(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,582 hrs · 24,093 cycles

LIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 325 AND STRINGERS S-28LH / S-29LH(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 94,582 hrs · 24,093 cycles

HORIZONTAL STABILIZER CENTER SECTION UPPER SKIN SURFACE WITH CORROSION DAMAGE BETWEEN RBL13.833 / RBL 32.67 AND STGR 3.(<P>DOUBLER REPAIR WAS INSTALLED PER MXA EO TRE6755054 (BOEING SR 3-5632149492). NO FURTHER DEFECTS NOTED.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 94,582 hrs · 24,093 cycles

FWD CARGO COMPARTMENT, FLOOR LEVEL, CORROSION ON FRAME WEB UPPER CHORD AT STA 654+44 LBL20(<P>AFFECTED ITEM WAS REPAIRED IAW B767 SRM 53-00-07-2R-4. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 94,582 hrs · 24,093 cycles

CORROSION ON INTERNAL FUSELAGE SKIN BETWEEN STA 1461 AND STRINGER S-12RH(<P>THE SURFACE PROTECTION WAS RESTORED ON THE REWORKED AREA PER MXA EO TRE6753591 (FVCI PROJECT NO. 23088-2). NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,582 hrs · 24,093 cycles

FUEL LEAK AT BODY SPLICE OF STGR L-10 AND LBL 97.42, WING CENTER SECTION(<P><SPAN>FUEL LEAK AT BODY SPLICE OF STRINGER&NBSP;</SPAN><SPAN>L-10 AND LBL 97.42, WING CENTER SECTION&NBSP;</SPAN><SPAN>WAS REPAIRED AND TEST WAS SATISFACTORY</SPAN></P> / <P>&NBSP;</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 94,582 hrs · 24,093 cycles

CORROSION ON INTERNAL FUSELAGE SKIN BETWEEN STA 1562 AND STRINGER S-9RH / S-10RH(<P>DOUBLER REPAIR WAS INSTALLED PER MXA EO TRE6753595 REV 1 ISSUED ON MAY 15, 2023 (FVCI PROJECT NO. 23088-6). NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 94,582 hrs · 24,093 cycles

CORROSION ON INTERNAL FUSELAGE SKIN BETWEEN STA 654+110 AND STRINGER S-9RH / S-10RH(<P>THE SURFACE PROTECTION WAS RESTORED ON THE REWORKED AREA PER MXA EO TRE6753589 (FVCI PROJECT NO. 23088-7). NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,582 hrs · 24,093 cycles

LIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 654+22 / STA 654+44 AND STRINGER S-25LH.(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 94,582 hrs · 24,093 cycles

CORROSION ON INTERNAL FUSELAGE BEARSTRAP BETWEEN STA 1540 AND STRINGER S-10RH / S-11RH(<P>DOUBLER REPAIR WAS INSTALLED PER MXA EO TRE6753594 ISSUED ON MAY 09, 2023 (FVCI PROJECT NO. 23088-5). NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,582 hrs · 24,093 cycles

LIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 368 AND STRINGERS S-28LH / S-29LH(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED.</P>)

Part: HINGE — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 94,582 hrs · 24,093 cycles

STABILIZERS - HORIZONTAL STABILIZER - LH HINGE FITTING BUSHING AND PIVOT BEARING CORROSION / SCRATCH DAMAGES(<P>THE HINGE FITTINGS WERE REPLACED / REPAIRED AND THE PIVOT FITTING WAS REWORKED WITH A SPECIAL TOOL PER MXA EO TRE6755056. NO FURTHER DEFECTS NOTED. NOTE: AS ADDITIONAL INFORMATION THE BUSHINGS WERE REPLACED.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,582 hrs · 24,093 cycles

LIGHTNING STRIKE DAMAGE ON FASTENER OF FUSELAGE EXTERNAL SKIN BETWEEN STA 566 AND STRINGERS S-27LH AND S-28LH.(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED</P>)

Part: PCA — UNKNOWN (UNKNOWN) · airframe 94,582 hrs · 24,093 cycles

RUDDER UPPER PCA WITH FREE PLAY OUT OF LIMITS(<P>RUDDER UPPER PCA WAS REPLACED PER AMM 27-21-02-422-038. OPS CHECK GOOD</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,582 hrs · 24,093 cycles

FUEL LEAK AT BODY SPLICE OF STGR L-6 AND LBL 97.42, WING CENTER SECTION(<P>FUEL LEAK AT BODY SPLICE OF STGR L-6 AND LBL 97.42, WING CENTER SECTION WAS REPAIRED AND TEST WAS SATISFACTORY.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,582 hrs · 24,093 cycles

VERTICAL STABILIZER, RH SURFACE, COMPOSITE PANEL DESBONDED BETWEEN AUXILIARY SPAR TO FRONT SPAR BETWEEN FSS 220.521 / FSS 321.046(<P>REPAIRED PER SRM 51-70-10-2R-4. NO FURTHER DEFECTS NOTED</P>)

Part: LINKAGE — UNKNOWN (UNKNOWN) · airframe 94,582 hrs · 24,093 cycles

VERTICAL STABILIZER REAR SPAR, UPPER PCA LINKAGE, RH HINGE WITH FREE PLAY(<P>UPPER PCA LINKAGE WAS REPLACED PER AMM 27-21-02-022-035 / -038. OPS CHECK GOOD</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,582 hrs · 24,093 cycles

LIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 654+44 / STA 654+66 AND STRINGER S-25LH.(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,582 hrs · 24,093 cycles

LIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 196.5 AND 8.5 INCH LOWER OF STRINGER S-21LH(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,582 hrs · 24,093 cycles

LIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 390 AND STRINGERS S-27LH / S-28LH(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED</P>)

Part: HPC — UNKNOWN (UNKNOWN) · airframe 94,488 hrs · 24,062 cycles

ON TAXI OUT R ENG BLEED LIGHT AND EICAS MESSAGE ON FOLLOWED STEP 3 OF APPLICABLE DDG 36-11-02 LIGHT AND DID NOT CLEAR PER MCC GUIDANCE RH ENGINE TO 70 PERCENT AND MESSAGE DID NOT CLEAR(<P>REMOVED AND REPLACED THE RH ENGINE HIGH PRESSURE CONTROLLER IAW B767 AMM 36-11-08/401. PERFORMED ENGINE RUN. NO ENG BLEED LIGHT OR EICAS MESSAGE. LEAK CHECK GOOD</P>)

Part: NONE — NONE · airframe 94,368 hrs · 24,022 cycles

ESCAPE REEL HANDLE FELL OUT AFTER LANDING(<P>R/R DESCENT DEVICE "B" IAW AMM 25-61-05. NO FURTHER DEFECTS NOTED</P>)

Part: NONE — NONE (NONE) · airframe 94,076 hrs · 23,934 cycles

DURING DEPARTURE IN CLIMB OUT, ACFT ENTERED AREA OF SEVERE TURBULENCE & W/S, ACFT INDICATED O/S OF 285, SPEED TAPE WITH NO ASSOCIATED OVERSPEED WARNINGS IAW 05-51-04, DATA FROM OUR ENGINEERING TEAM SHOWS AIRCRAFT DID NOT SHOW "G" LOADS OF SEVERE TURBULENCE. NO FURTHER INSPECTION REQUIRED. OPEN AND CLOSED PANELS 335CB, 335DB, 335AFB, 335GB, 335HB, 335JB, 335KB, NO DAMAGE NOTED.

Part: GUARD — DAMAGED (LIGHT SWITCH) · airframe 93,695 hrs · 23,829 cycles

EMERGENCY LIGHT GUARD INOP WITH GUARD CLOSED, EMER LIGHT REMAIN UNARMED. R/R EMERGENCY LIGHT GUARD IAW AMM 33-51-00. OPS CHECKED GOOD.

Part: NONE — NONE · airframe 93,444 hrs · 23,741 cycles

DESCENT DEVICE INOP(<P><SPAN>PER CREW, UPON OPENING STORAGE DEVICE. DESCENT REEL DROPPED DOWN. RESECURED DESCENT DEVICE IAW AMM 25-61-05. NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: NONE — NONE · airframe 92,212 hrs · 23,360 cycles

ENG #1 I/B T/R WITH SEAL DAMAGED LOCATED AT INTERNAL AREA .(<P>PREPARED, CLEANED, AND REPAIRED FIRE RETARDANT SEAL INNER AREA OF ENG. # 1 I/B T/R PER B767-300 AMM 78-31-00-308-072-H00 .</P>)

Part: NONE — NONE · airframe 92,212 hrs · 23,360 cycles

COCKPIT 1ST OBS SEAT BELTS MISSING COTTER PINS(<P>REMOVED AND REPLACED 1ST OBS COTTER PINS IAW B767-300 AMM 20-10-23</P>)

Part: SQUIB — NONE · airframe 92,212 hrs · 23,360 cycles

APU SQUIB P/N 30903856 S/N 01189 DUE FOR TIME CHANGE .(<P>REMOVED &AMP; REPLACED APU SQUIB PER B767-300 AMM 26-22-02.</P> / <P>SQUIB TEST PASSED . NEW&NBSP; DUE&NBSP; DATE&NBSP; &NBSP; &NBSP;31 OCT 29</P>)

Part: NONE — NONE · airframe 92,212 hrs · 23,360 cycles

LEFT INB AFT FLAP OB SIDE HAS SEAL MISSING .(<P><SPAN>REMOVED&NBSP; AND&NBSP; INSTALLED&NBSP; SEAL&NBSP; AT&NBSP; LEFT&NBSP; INB&NBSP; AFT&NBSP; FLAP&NBSP; O/B&NBSP; &NBSP;SIDE&NBSP; AS&NBSP; PER&NBSP; 767-300&NBSP; &NBSP;</SPAN></P> / <P><SPAN>AMM&NBSP; 20-10-23-964-001</SPAN></P>)

Part: NONE — NONE · airframe 92,212 hrs · 23,360 cycles

FWD CARGO CREW OXYGEN NEED SERVICE TO FULL .(<P>REMOVED, SERVICED &AMP; REINSTALLED FWD CARGO CREW O2 BOTTLE PER B767-300</P> / <P>AMM 12-15-08, 35-00-00, 35-11-00 &AMP; AC 43.13-1B PAR 9-46 THRU 9-51 PGS&NBSP; 9-448&NBSP; THRU 9-455.&NBSP;&NBSP;</P> / <P>NO LEAKS. P/N B42365-1. S/N R12-001419.</P>)

Part: POUCH — LOOSE · airframe 92,212 hrs · 23,360 cycles

COCKPIT F/O SEAT LIFE VEST POUCH VELCRO LOOSE .(<P>SECURED VELCRO AT COCKPIT F/O SEAT LIFE VEST AS PER 767-300 AMM 20-30-01-992-001</P>)

Part: ROD — NONE · airframe 92,212 hrs · 23,360 cycles

ENG. #1 O/B CORE COWL HOLD OPEN ROD DAMAGED(<P>REMOVED AND REPLACED #1 O/B CORE COWL HOLD OPEN ROD IAW&NBSP; B767-300 AMM 71-11-11</P> / <P>OPS&NBSP; CHECK&NBSP; GOOD</P>)

Part: NONE — NONE · airframe 92,212 hrs · 23,360 cycles

RH INB MID FLAP OB SIDE WITH AERODYNAMIC SEAL DAMAGED .(<P><SPAN>REMOVED&NBSP; AND&NBSP; INSTALLED&NBSP; AERODYNAMIC&NBSP; SEAL&NBSP; AT&NBSP; R/H&NBSP; INB&NBSP; MID&NBSP; FLAP&NBSP; O/B&NBSP; SIDE&NBSP; AS&NBSP; PER&NBSP; 767-300</SPAN></P> / <P><SPAN>AMM&NBSP; &NBSP;20-10-23-964-001</SPAN></P>)

Part: NONE — NONE · airframe 92,212 hrs · 23,360 cycles

COCKPIT LH STOWAGE LIFE RAFT P/N RO425A-107 S/N TAL6A072 DUE FOR SERVICE.(<P>REMOVED AND REPLACED COCKPIT LOWER LIFE RAFT AS PER&NBSP; B767-300&NBSP; AMM 25-62-00.</P>)

Part: NONE — NONE

EICAS: R GEN OFF AT ENG START, QRH 6.12 ACOMPLISHED + RESET OPS NORMAL(<P><SPAN>COMPLETED WITH OPS CHECK FOR RH GEN IN REF. AMM 71-00-00. ( ENT RUN ). OPS CHECK GOOD. NO FAULTS NOTED.&NBSP;</SPAN></P>)

Part: LIGHT — NONE · airframe 91,076 hrs · 23,012 cycles

FLIGHT DECK ENTRYWAY L/H SIDE AFT END OF SLIDE CONTAINER BOTTOM SIDE EMERGENCY EXIT LIGHT CRACKED AND DAMAGED. CAUTION: COULD BE HAZMAT HAZARD.(<P>REMOVED AND REPLACED FLIGHT DECK ENTRYWAY L/H SIDE AFT END OF SLIDE CONTAINER BOTTOM SIDE EMERGENCY EXIT LIGHT IAW B767 AMM 33-51-01.</P>)

Part: FLAP — NONE · airframe 91,076 hrs · 23,012 cycles

LH WING I/B FLAP LOWER SURFACE HAS BULGING AREA AT FASTENER ROW JUST I/B OF O/B TRACK.(<P>REMOVED CORROSION LH WING I/B FLAP LOWER SURFACE. ORIG. MAT. WAS .125" REMAINING MAT. IS .034" IS FOUND TO BE OUT OF LIMITS IAW B767 SRM 57-53-01. REMOVED AND REPLACED LH WING I/B FLAP UPON CUSTOMER REQ. IAW B767 AMM 27-51-06, 27-51-07</P>)

Part: NONE — NONE · airframe 91,076 hrs · 23,012 cycles

AREA OF CORROSION ON R/H HORIZ STAB UPPER SURFACE AT FRONT SPAR JUST O/B OF BANANA FAIRING.(<P>BLENDED THE AREA ON THE R/H HORIZONTAL STABILIZER UPPER SURFACE AT FRONT SPAR JUST O/B OF THE BANANA FAIRING IAW B767 SRM 51-10-02. UPON THE EVALUATION THE AREA WAS DEEMED IN LIMITS IAW FAS EA 21078 REV:IR</P>)

Part: NONE — NONE

F/O ESCAPE ROPE PANEL WILL NOT LATCH CLOSED.(<P>RE-SECURED FO ESCAPE ROPE PANEL IN REF AMM 25-61-05.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (AFT EQUIP FAN) · airframe 90,954 hrs · 22,975 cycles

STATUS MESSAGES AFT EQ FAN 1 &AMP; AFT EQ FAN 2(<P>FLIGHT CREW FOUND FWD &AMP; AFT CARGO FIRE ARM SWITCHES DEPRESSED. CYCLED SWITCHES. NO MESSAGES PRESENT AT THIS TIME, DONE IAW B767 AMM 26-19-00.</P>)

Part: ENGINE — WARNING MESSAGE · 22,963 cycles

UPON SHUTTING DOWN LEFT ENGINE L AC BUS MESSAGE DISPLAYED REMAINED ILLUMINATED UNTIL EXT POWER SELECTED.(<P>PERFORMED FIM TASK 24-32 FT803 BLOCKS 1 AND 2 FOLLOWED BY ENGINE RUN IAW AMM 71-00-00. OPS NORMAL AT THIS TIME. NO FURTHER DEFECTS NOTED. NUSSIANCE FAULT DUE TO IMPROPER ENGINE SHUTDOWN WITHOUT EXT POWER ON OR APU POWER ON.</P>)

Part: BLADE — NICKED (NR 18)

SMALL CHIP ON OUTER FAN BLADE # 18 OF RIGHT ENGINE(<P>NICK FOUND TO BE WITHIN REPAIRABLE LIMITS, BLENDED PER AMM 72-31-02. NO FURTHER DEFECTS NOTED. OK FOR SVC. TRANSFERRED TO NON MEL 152213 FOR DYE PENETRANT WITHIN 50FH 0R 10 FC,</P> / <P><SPAN>LP 1368567: PERFORMED FPI I/A/W 72-31-02; NO DEFECTS NOTED AT THE TIME OF INSPECTION. THIS CLOSES NON-MEL# 152213.</SPAN></P>)

Part: START VALVE — FAULTED (RIGHT) · airframe 90,655 hrs · 22,889 cycles

R STARTER CUTOUT EICAS MESSAGE ILLUMINATED MOMENTARILLY. WHILE AT CRUISE. REPEATED SEVERAL TIMES BUT ONLY FOR A SECOND AT A TIME.(<P>R/R RIGHT ENG STARTER VALVE PER AMM 80-11-02. PERF ENG RUN IAW AMM 71-00-00. OPS TEST NORMAL, NO DEFECTS NOTED, ITEM 2 IS RELATED TO STARTER VALVE MALFUNCTION AND ITEM IS CLEARED ON ITEM 1.</P>)

Part: FAULT LIGHT — FALSE ACTIVATION (APU)

APU FAULT EICAS DURING TAXI IN.(<P>PERFORMED APU BITE TEST PER FIM 45-11 FT 958. NO FAULTS FOUND. NO MINI FLAGS APU OIL LEVEL GOOD. OPS TESTED APU NORMAL PER AMM 49-11-00&NBSP;</P>)

Part: WARNING LIGHT — FALSE ACTIVATION (EQUIP COOL VLV)

EQUIPMENT COOLING "VALVE "LIGHT ILLUMINATED.(<P>CYCLED EQUIPMENT COOLING SELECTOR SWITCH FROM "AUTO" TO "STBY" REF B767 AMM 21-58-00 VALVE CLEARD ONCE SWITCH WAS TAKEN BACK TO AUTO. NO FURTHER EFFECTS NOTED.</P>)

Part: PNEUMATIC SYSTEM — UNKNOWN (APU) · 22,867 cycles

APU PNEUMATICS INOP. T/S IAW FIM 49-11 FAULT TREE. NO FAULTS FOUND. PERFORMED VISUAL INSPECTION ON APU BLEED AIR DUCT IAW AMM 36-11-02. NO DEFECTS FOUND. PERFORMED ENGINE RUN IAW AMM 72-00-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (EXHAUST FAN)

STATUS 'AFT EQ EXH FAN 2'(<P>PERFORMED FIM TASK 21-26 FAULT TREE 808. NO FAULTS FOUND. COULD NOT DUPLICATE. OPS CHECKS GOOD.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENG STARTER) · airframe 90,553 hrs · 22,850 cycles

R ENG STARTER EICAS MSG DURING ENG START. 2ND. ATTEMPT OK.(<P>PERFORMED R/H ENG STARTER VALVE OPS CHECK IAW B767 AMM 71-00-00. NO DEFECTS NOTED AT THIS TIME. A/C OK FOR SERVICE.</P>)

Part: WARNING MESSAGE — FALSE INDICATION

AFTER SHUTDOWN TR UNIT STATUS MESSAGE DISPLAYED(<P><SPAN>PERFORMED T/S PER FIM 24-32 F/T 803, NO DEFECTS NOTED, SYSTEM OPS CHECK NORMAL.</SPAN></P>)

Part: SWITCH — FAULTED (APU)

APU DEFERRED PER MCC (INOP)(<P>TRANSFER TO MDDR DMI #150314 IAW B767 DDG MEL 49-11-01A, CAT C, DUE 27JUL21 "M" PROC C/W.&NBSP;</P> / <P>C/W WITH ECM #2021P-233 REF. LOGPAGE 1369494 ITEM 8...REPLACED DE-OIL SOLENOID VALVE.. P/N 3876166-1..S/N 1102&NBSP; ON APU IAW AMM49-27-08 OPS CKS GOOD...</P> / <P>REFERENCE ITEM 9 THIS LOG PAGE..REPLACED APU OIL TEMP SWITCH IAW AMM 49-27-14 LEAK CKS GOOD. THIS CLEARS MDDR 150314.</P>)

Part: UNKNOWN — LEAKING (LT ENGINE) · airframe 90,467 hrs · 22,822 cycles

EXCESSIVE OIL FOUND ON INBOARD SURFACE OF LEFT ENGINE EXHAUST COWL (6 O'CLOCK POSITION).(<P>OPENED AND INSPECTED LEFT ENGINE EXHAUST COWL FOR OIL LEAKS, NO LEAKS NOTED.</P>)

Part: CIRCUIT CARD — FAULTED (STARTER)

EICAS MSG "R STARTER CUTOUT" INTERMITTENTLY DISPLAYED IN CRUISE FOR ABOUT 3-5 SECONDS.(<P>RIGHT STARTER VALVE PREV REPLACED ON 03APR21. PERFORMED OPS CHECK IAW AMM 71-00-00. OPS CHECK OK. DUE TO HISTORY REPLACED N2 SPEED CARD (M1092) IAW AMM 73-21-54. REMOVED AND REPLACED START 1 RELAY K666 ON P6 PER SWPM 20-81-20 &AMP; WDM 80-11-21. RAN ENGINE # 2. OPS CHECK GOOD. RELAY PN: BACR13CG2A</P>)

Part: WARNING LIGHT — FALSE ACTIVATION (ANTI-ICE SYS)

DURING CLIMB WHEN SELECTING L ENG ANTI-ICE FROM ON TO OFF THE L ENG ANTI ICE EICAS MESSAGE DISPLAYED FOR APPROX 3-5 SECONDS, WENT AWAY(<P>PER AMM 30-21-00 SYSTEM OPERATES NORMAL. NO FURTHER DEFECTS NOTED AT THIS TIME.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENGINE)

WHEN SHUTTING DOWN LEFT ENGINE IN THE BLOCKS, THE L AC BUS FAILED.(<P>T/S PER FIM 24-32 FT 803, SYSTEM TEST OK, T/S PER FIM 24-20 FT 801. NO FURTHER DEFECTS NOTED AT THIS TIME, A/C IS OKAY FOR FURTHER SERVICE.</P>)

Part: STARTER — MALFUNCTIONED (RT ENGINE)

BAD POWER TRANSFER STARTING RT ENGINE. RETURN TO BLOCK TO POWER RESTART.(<P>PERFORMED RESET IAW AMM 24-22-00 RT GEN PER RH ENG RUN IAW 71-00-00 POWER TRANSFER SUCCESSFUL. NO FUTHER DEFECTS NOTED.</P>)

Part: TRANSCEIVER — FAULTED (WX RADAR) · airframe 90,294 hrs · 22,772 cycles

L WX RADAR FAILED TWICE IN FLIGHT, SWITCHED TO R WX RADAR AND THE SYSTEM WORKED NORMALLY.(<P>TRANSFERRED TO DMI # 148947, CAT D, DUE DATE 18OCT21 IAW DDG 34-43-01 T.I. LUC 2223Z.</P> / <P>CVG MX, 21JUN21, LP 1444308, ITEM M7: REMOVED AND REPLACED WX RADAR TRANSCEIVER IAW AMM 34-43-01. OPS CHECK GOOD AT THIS TIME. MEL 148947 CLOSED, MCC NOTIFIED. PLACARD REMOVED. DISP: DSP: JL TIME : 17:30Z.</P> / <P>&NBSP;</P>)

Part: MODULATING VALVE — FAILED (CABIN TEMP) · airframe 90,294 hrs · 22,772 cycles

FWD CABIN INOP(<P>PERFORMED FIM 21-60 FT 804 ZONE TEMPERATURE BITE PROCEDURE FAULT LIGHT FOR FWD ZONE TRIM VALVE: ILLUMINATED &AMP; PERFORMED FIM 21-60 FT 811 HAD FWD TEMP MSG &AMP; FWD CAB INOP LIGHT. REMOVED AND REPLACED FWD TRIM AIR MODULATING VALVE IAW AMM 21-61-07, OPS CHK GOOD &AMP; LEAK CHK GOOD. BITE CHK PASSED, NO ACTIVE FAULTS, NO EICAS MSG &AMP; NO FWD CAB INOP LIGHT.</P>)

Part: ANTI-ICE VALVE — FAULTED (LT ENGINE) · airframe 90,257 hrs · 22,760 cycles

LEFT ENG ANTI ICE VALVE DID NOT CLOSE WHEN SWITCH OFF(<P>PERF OPS CHECK OF L ENG TAI VALVE, OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. REF: 30-21-03-404-022</P>)

Part: TRANSCEIVER — FAILED (WX RADAR SYS) · airframe 90,246 hrs · 22,757 cycles

L RADAR "WXR FAIL" DURING CLIMB. WHEN IT WAS OPERATIONAL, IT APPEARED TO BE TILTED LOWER THAN SELECTED TILT.(<P>REMOVED AND REPLACED L/H R/T TRANCEIVER IAW B767 AMM 34-43-01. OPS CHECK GOOD AT THIS TIME.</P>)

Part: FIRE LOOP — MALFUNCTIONED (NR 1) · airframe 90,236 hrs · 22,752 cycles

RT FIRE LOOP1, RT FIRE LOOP 2(<P>REMOVED AND REPLACED RT ENG FIRE LOOP 1 AMM 26-11-02. REMOVED AND REPLACED RT ENG FIRE LOOP 2 DET ELEMENT. OPS NORMAL IAW AMM 26-11-02.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN TEMP) · airframe 90,234 hrs · 22,751 cycles

FWD CABIN TEMP EICAS MESSAGE.(<P>PERFORMED BITE ON ZONE TEMP CONTROLLER. PER 21-60-99 MSG CLEARED, OPS CK NORMAL, NO FAULTS NOTED.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN TEMP) · airframe 90,220 hrs · 22,746 cycles

FWD CABIN TEMP EICAS MSG PRIOR TO BLOCK OUT(<P>DEFER PER MEL 21-61-01-02 CAT C DUE 13JUN21 REF MDDR 147976 CW AT 22:41Z.</P><P>LOG 1343041 ITEM #4&NBSP;TROUBLE SHOOT PER FIM 21-60 FAULT TREE 806. MESSAGE NOT DISPLAYED. OPS NORMAL. THIS CLEARS MDDR #147976. ID@0118Z</P>)

Part: TRU — FAULTED (APU) · airframe 90,207 hrs · 22,741 cycles

APU FAULT ON FIRST ATTEMPT START OK(<P>TRANSFERRED TO DMI # 147866 CAT C DUE DATE 11 JUN 21 IAW DDG 49-11-01A&NBSP;</P><P>CVG MX, 01JUN21 LP 1306574, ITEM M8: PERFORMED FIM 49-11 TREE 959 &AMP; FIM 49-11 963, FIM LEAD TO APU TRU. REMOVED &AMP; REPLACED APU TRU IAW 767 AMM 24-32-01, APU OPS CHECK GOOD(3X). MCC NOTIFIED, PLACARDS REMOVED. DMI 147866 CLEARED. TIME/INITIALS: GTC 0317Z.</P>)

Part: START VALVE — FAULTED (RT ENGINE) · airframe 90,033 hrs

R ENG STR CUTOUT EICAS ON SHORT FINAL WENT AWAY TWICE. AFTER LOADING EICAS CAME BACK AND STAYED. RAN QRH CHECK LIST ITEMS.(<P>REMOVED AND REPLACED START VALVE IAW AMM 80-11-02. OPS CHECKS NORM AT THIS TIME. LEAK CHECK GOOD AT THIS TIME.<BR /></P>)

Part: IGNITER — FAILED (RT ENGINE) · airframe 90,033 hrs

STATUS MSG R ENG IGNITOR 2(<P>REMOVED AND REPLACED RT ENG IGNITOR 2 IAW AMM 74-21-02. OPS CHECK GOOD NO FURTHER DEFECTS NOTED. STATUS MSG CLEARED.<BR /></P>)

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 89,955 hrs · 22,665 cycles

RT E/I VALVE DISAGREE LIGHT ILLUMINATED PRIOR TO ENG START. VALVE OPERATED NORMALLY(BUT SLOW) POST START. START CONDUCTED W/ MX &AMP; DISP. CONCURRENCE.(<P>C/W ENGINE INLET TAI VALVE OPS CHECK, CHECKS GOOD, PER AMM 30-21-03-404-022 SUBTASK 30-21-03-714-062</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI-ICE VALVE) · airframe 89,991 hrs · 22,675 cycles

RT E/I VALVE DISAGREE LIGHT ILLUMINATED PRIOR TO ENG START. VALVE OPERATED NORMALLY BUT SLOW POST START. START CONDUCTED W/ MX AND DISPATCH CONCURRENCE.(<P>C/W ENGINE INLET TAI VALVE OPS CHECK, CHECKS GOOD PER AMM 30-21-03-404-022 SUBTASK 30-21-03-714-062.</P>)

Part: INERTIA REEL — DETACHED · airframe 89,934 hrs · 22,659 cycles

ONE ESCAPE INERTIAL REEL FELL OUT OF HOLDER ON TAKE OFF. 6 EACH SERVICEABLE. COMPLIED WITH REEL REMOVAL FROM PLANE SPACER REINSTALLED BACK IN POSITION.</P><P>INSTALLED ESCAPE REEL IAW AMM 25-61-02. THIS CLEARS MDDR 146036. PLACARD REMOVED, MCC NOTIFIED</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN TEMP) · airframe 89,850 hrs · 22,635 cycles

FWD CABIN TEMP EICAS MSG.(<P>TRANSFERRED TO MDDR # 145639 OAW MEL 21-61-01-02 DUE DATE: 30APR21 CAT "C". C/W MX PROCEDURE. SP 2315Z</P><P>21APR, ONT MX LP 695222, ITEM M3: PERF OPS CHECK OF ZONE TEMP CONTROL SYSTEM IAW AMM 21-61-00. OPS CHECK GOOD, NO PREVIOUS OR CURRENT FAULTS. THIS CLEARS DMI #145639. MCC NOTIFIED, PLACARD REMOVED. RS @ 1316Z</P>)

Part: ESCAPE REEL — UNWANTED DEPLOY · airframe 89,844 hrs · 22,633 cycles

DURING TRANSIT CHECK FOUND DESCENT DEVICE DEPLOYED. P/N 379103D-29, SERIAL NO. 20985(<P>TRANSFER TO MDDR 145610 PER MEL 25-61-01-01, CAT C. DUE 30APT21. PLACARDS INSTALLED. DEVICE REMOVED PER MEL. DF 09:58Z</P><P>ONT MX, 21APR21, LP 695223, ITEM M6: INSTALLED NEW EMERGENCY DESCENT DEVICE #2 IAW AMM 25-61-02. NO DEFECTS NOTED. THIS CLEARS MDDR # 145610. PLACARD REMOVED. RS @ 1411Z</P>)

Part: GCU — MALFUNCTIONED (RT ENGINE) · airframe 89,861 hrs · 22,637 cycles

AFTER R ENG START, R GEN WAS INOP(<P>REMOVED AND REPLACED&NBSP;RIGHT ENG GCU PER AMM 24-22-01. OPS TEST GOOD, NO DEFECTS NOTED. ENG RUN PER AMM 71-00-00, OPS GOOD. PLACED .62 ELEC LOAD TO ISOLATE RT GEN APPROX. 5 MINS, NO FAULTS NOTED.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (OVERSPEED) · airframe 89,768 hrs · 22,611 cycles

"OVERSPEED" MSTR WARNING EICAS FLASHED BRIEFLY DURING #2 ENG. START.(<P>A/C ON GROUND DURING "OVERSPEED" INDICATION. C/W FIM FT 34-90-49-00. ADC OPS TEST GOOD PER AMM 34-12-00-715-001. ACCOMPLISHED #2 ENG RUN PER 71-00-00-862-053-H03, FAULT NOT REPRODUCED. NO FAULTS NOTED.</P>)

Part: START VALVE — FAULTED (RT ENGINE) · airframe 89,710 hrs

R STARTER CUTOUT EICAS MESSAGE IN FLIGHT(<P>TRANSFERRED TO&NBSP;MDDR 144761 MEL&NBSP;80-00-02-01 CAT C. 4 APR 2021</P><P>3 APR 2021-LOG PAGE 1465749 M7: REMOVED AND REPLACED #2 ENG START VALVE, IAW AMM 80-11-02, OPS CHECK GOOD. THIS CLEARS DMI 144761, PLACARDS REMOVED.</P>)

Part: CONNECTOR — DAMAGED (FUEL TRANSMITTER) · airframe 89,656 hrs · 22,578 cycles

#2 ENG FUEL TRANSMIITTER (PRESS) CONNECTOR IS DAMAGED(<P>REPLACED #2 ENG FUEL PRESS TY CONNECTOR&NBSP; D10998 PER SWPM 20-63-00 &AMP; W/D 73-33-11</P><P>ENG #2 RUN UP; L&NBSP; PRESS IND.&NBSP; NORMAL PER AMM&NBSP; 73-33-00</P>)

Part: OXYGEN MASK — NOT REPORTED (LAVATORY) · airframe 89,656 hrs · 22,578 cycles

LAV PORTABLE OXYGEN MASKS DUE FOR SHOP VISIT P/N 289-601-212(<P>REMOVED AND REPLACED LV PORTABLE OXYGEN MASK AS PER&NBSP; B767-300&NBSP; AMM&NBSP; 35-31-00</P>)

Part: PNEUMATIC SYSTEM — LEAKING (NR 1 ENGINE) · airframe 89,656 hrs · 22,578 cycles

ENGINE #1 HAS PNEUMATIC LEAK @ LOCATION "K"; AS PER EO #1936A088. SEE 8017- TALLY 140 PRV; REPLACEMENT FOR CORRECTION ACTION.

Part: DEPRESSOR — DAMAGED (CARGO DOOR) · airframe 89,656 hrs · 22,578 cycles

MAIN CARGO DOOR FWD SEAL&NBSP; DEPRESSOR DAMAGED(<P>REMOVED &AMP; REPLACED DAMAGED SEAL DEPRESSOR BY MAIN CARGO FWD SIDE OF CUT OUT PER&NBSP; B767-300 SRM 51-40-02-0G-0.</P>)

Part: BATTERY — NOT REPORTED (FLASHLIGHT) · airframe 89,656 hrs · 22,578 cycles

COCKPIT FLASHLIGHT BATTERY DUE FOR SHOP VISIT 2 EACH P/N P4-01-0021. REMOVED AND REPLACED FLASHLIGHT BATTERY AS PER AMM 25-64-00/001. OPS CK OK.

Part: SEAL — BROKEN (CONTAINMENT BAG) · airframe 89,656 hrs · 22,578 cycles

COCKPIT AVSAX CONTAINMENT BAG VACUUM SEAL BROKEN PN&NBSP; AS-002-1(<P>REMOVED AND REPLACED AVSAX CONTAINMENT BAG AS PER&NBSP; B767-300&NBSP; AMM&NBSP; 25-60-00</P>)

Part: HANDLE — MALFUNCTIONED (THRUST REVERSER) · airframe 89,690 hrs · 22,587 cycles

#1 ENG T/R LEFT HAND ELECTROMECHANICAL BRAKE DISENGAGE HANDLE WILL NOT LOCK IIN THE UP POSITION(<P>REMOVED &AMP; REPLACED #1 L/H T/R ELECTRO-MECHANICAL BRAKE PER 78-34-07-404-005-J00. OPS CHECKED GOOD.

Part: FIRST AID KIT — NOT REPORTED (COCKPIT) · airframe 89,656 hrs · 22,578 cycles

COCKPIT FIRST AID KIT DUE FOR SHOP VISIT. P/N&NBSP; 56-01-0005-306(<P>REMOVED AND REPLACED FIRST AID KIT IN COCKPIT&NBSP; AS PER&NBSP; B767-300&NBSP; AMM 25-60-00</P>)

Part: OXYGEN BOTTLE — LOW PRESSURE (CREW) · airframe 89,656 hrs · 22,578 cycles

FWD CARGO R/H SIDE COMPARTMENT SERVICE OXYGEN CYLINDER TO FULL(<P>SERVICED FWD CARGO R/H SIDE COMPARTMENT OXYGEN CYLINDER&NBSP; IAW&NBSP; B767-300&NBSP; AMM&NBSP; 12-15-08-603-001&NBSP; AMM&NBSP; 35-00-00-912-005,&NBSP; AMM&NBSP; 35-11-00-206-228,&NBSP; AMM&NBSP; 35-11-00-206-233&NBSP; AC&NBSP; 43.13-1B&NBSP; PAR&NBSP; 9-46 THRU 9-51 PGS&NBSP; 9-448&NBSP; THRU 9-455. NO LEAK NOTED. O2 BOTTLE&NBSP; PN&NBSP; 801307-00&NBSP; SN&NBSP; ST326329</P>)

Part: COVER — WRONG PART (F/O SEAT) · airframe 89,656 hrs · 22,578 cycles

COCKPIT F/O SEAT LAP BELT BUCKLE STORAGE POUCH ON WRONG SIDE OF SEAT COVER(<P>REMOVED &AMP; REPLACED SEAT COVER AT F/O SEAT IAW&NBSP; B767-3&NBSP; AMM&NBSP; 20-30-01</P>)

Part: SHUTOFF VALVE — INTERMITTENT (NR 1) · airframe 89,656 hrs · 22,578 cycles

#1 HPSOV ONLY OPERATES PARTIALLY(<P>REMOVED AND REPLACED #1 ENG HPSOV PER M/M 36-11-05-400-802-001. LEAK &AMP; FUNCT CHECK GOOD REQUIRES&NBSP; RUN-UP&NBSP; OPS&NBSP; CHECK.</P><P>PERFORMED POST INSTALLED CHECK IAW AMM 36-11-05 OP CHECK FOUND NORMAL NO LEAKS NOTED.</P>)

Part: POUCH — LOOSE (LIFE VEST) · airframe 89,656 hrs · 22,578 cycles

COCKPIT CAPT SEAT LIFE VEST POUCH LOOSE VELCRO(<P>SECURED LIFE VEST POUCH AT COCKPIT CAPT SEAT IAW&NBSP; B767 AMM 20-30-01</P>)

Part: MONITOR — INOPERATIVE (ENGINE VIBRATION) · airframe 89,628 hrs · 22,569 cycles

NO VIB INDICATION FOR L AND R ENGINE(<P>REPLACED ENG VIB MONITOR UNIT IAW AMM 77-31-03, OPS CHECK GOOD.</P>)

Part: ESCAPE REEL — DETACHED (COCKPIT) · airframe 89,627 hrs · 22,568 cycles

1 INERTIAL ESCAPE REEL CAME UNATTACHED(<P>TRANSFERED TO DMI# 143989 PER MEL 25-61-01-01, MX ACTION C/W. CAT C, DUE DATE 28MAR21.</P><P>LP 1254740: INSTALLED DESCENT DEVICE IAW B767 AMM 25-61-05. THIS CLEARS DMI 143989. PLACARD REMOVED, MCC NOTIFIED.</P>)

Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 89,627 hrs · 22,568 cycles

LH ENG ANTI ICE LIGHT ON OVERHEAD PANEL STAYS ON WHEN SELECTED.(<P>ITEM TRANSFERRED TO MDDR # 143929 IAW DDG MEL 30-21-02-01A CAT C. DD 26MAR21 MCC NOTIFIED, PLACARD INSTALLED. LH ENG TAI VERIFIED OPERABLE. T&AMP;I: SD 1844.</P><P>17MAR21 - LP1254729 - ITEM# 2 - CVG -&NBSP;REMOVED AND REPLACED ANTI ICE PANEL IAW AMM 30-11-01. THIS CLEARS MDDR 143929.</P>)

Part: BUSS — DISCONNECTED (RT AC SYSTEM) · airframe 89,606 hrs · 22,560 cycles

&NBSP;RIGHT AC BUS OFF AFTER RIGHT ENGINE START FOLLOWED BY NUMEROUS EICAS MSG(<P>PERFORMED BPCU BITE PROCEDURE IAW FIM 24-20-43-801, OPS CHECK GOOD. PERFORMED ENGINE RUN IAW AMM 71-00-00</P>)

Part: ENGINE — VIBRATION (LEFT) · airframe 89,586 hrs · 22,550 cycles

LE N2 VIB 3.5 IN DESCEND. EVENT RECORDED(<P>PERFORMED T/S IAW FIM 71-05 FAULT TREE 858, COULD NOT DUPLICATE, FOUND TO BE WITHIN LIMITS. OK FOR SERVICE.</P>)

Part: SWITCH — MALFUNCTIONED (CABIN PRESSURE) · airframe 89,546 hrs · 22,532 cycles

AFTER LANDING INSPECTION FOUND OUTFLOW VALVE FULLY CLOSED. TRANSFER TO MDDR 143233 IAW DDG 21-31-01A, CAT C, DUE 12MAR21.LP 1145720: REMOVED AND REPLACED;MICRO SW PACK; PER AMM 22-32-04-402-069 DUE TO MICROSWITCH DAMAGE. FOUND PRESS SYS 1 &AMP; 2 OPT NORMAL. REF BITE TEST 21-31-00-705-001 NO FAULTS. ACCOMPLISHED MICRO SW ADJUSTMENT PROCEDURE REF AMM 22-32-04-402-065-G AND OPT REF AMM 22-32-04-402-069-H. NO FAULTS DETECTED. OPT NORMAL. OPT NORMAL REF AMM 21-31-00-705-001. NO FAULTS PRESENT. THIS CLEARS DMI # 143233.

Part: WARNING LIGHT — FALSE ACTIVATION (ANTI-ICE VALVE) · airframe 89,451 hrs · 22,503 cycles

RIGHT ENGINE ANTI ICE SWITCH VALVE LIGHT IS ILLUMINATED(<P>PERFORMED OPS TEST OF RT ENG ANTI ICE VALVE AND FOUND VALVE TO OPERATE NORMALLY IAW AMM 30-21-03.</P>)

Part: MONITOR — MALFUNCTIONED (ENGINE VIBRATION) · airframe 89,438 hrs · 22,498 cycles

LEFT ENGINE PEAK FAN VIB 5.0(<P>ITEM TRANSFERRED TO MDDR 142204 PER MEL 22-31-01-01, CAT C, DUE 19FEB21.</P><P>DATE 14 FEB 21 - LP 1253285 - ITEM 7 - RIV -&NBSP;REMOVED AND REPLACE ENGINE VIBE MONITOR IAW AMM 77-31-03-401. THIS CLEARS MDDR 142204.</P>)

Part: CONTROLLER — FAILED (DUCT PRESSURE) · airframe 89,438 hrs · 22,498 cycles

L DUCT PRESSURE AFTER ENGINE START @10 PSI AND L END R SLOW TO DEPLOY AND RETRACT(<P>ITEM TRANSFERRED TO MDDR 142202 PER MEL 36-11-02-02, CAT C, DUE 19 FEB21.</P><P>11FEB21 - LG PG 1251312 ITEM 4 TPA - REMOVED AND REPLACED PRESSURE REGULATING VALVE CONTROLLER IAW AMM 36-11-19. OPS AND LEAK CHECK GOOD, THIS CLEARS MEL 142202.</P>)

Part: ESCAPE REEL — MISSING (CABIN) · airframe 89,408 hrs · 22,491 cycles

1 EACH INERTIAL ESCAPE REEL MISSING(<P>TRANSFERRED TO MDDR 142038 PER MEL 25-61-01-01, CAT C, DUE DATE: 16FEB21. DISPATCHER:&NBSP;ZH @ 16:49Z</P><P>LP 1274014: INSTALLED #2 DESCENT DEVICE IAW AMM 25-61-05. NO DEFECTS NOTED. THIS CLEARS DMI 142038.</P>)

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 89,397 hrs · 22,488 cycles

CABIN ALT AUTO 1(<P>ITEM PLACED ON MEL 21-31-01A. MDDR 141968. EXP 17FEB21. JJT- 0850Z</P><P>05FEB, RIV, LP 1274000, ITEM M4: PERF FIM 21-31 F/T 803. UP TO BLOCK 6. BIT AUTO 1 CONTROLLER AND FOUND NO FAULTS, SYS OK. THIS CLEARS DMI 141968. ALL PLACARDS REMOVED. TJ 18:35Z.</P>)

Part: RADAR — INOPERATIVE (WX RADAR SYS) · airframe 89,365 hrs · 22,477 cycles

WEATHER RADAR TILT NEEDED OVER +2 IN CLIMB AND OVER +1 IN CRUISE TO NOT PICK UP GROUND RETURN. PERFORMED OPERATIONAL TEST OF WX RADAR SYS IAW AMM 34-43-00. OPS NORMAL AT THIS TIME NO DEFECTS NOTED AT THIS TIME.

Part: APU — FAULTED (APU BAY) · airframe 89,312 hrs · 22,462 cycles

APU FAULT ON START AFTER LANDING. PERFORMED APU OPERATIONS TEST, TEST NORMAL, IAW AMM 49-11-00.

Part: MODULATING VALVE — FAULT MESSAGE (AFT CABIN) · airframe 89,317 hrs · 22,465 cycles

AFT CABIN TEMP EICAS MESSAGE. TRANSFERRED TO MDDR 141430, IAW MEL 21-61-04-02, CAT C. REMOVED AND REPLACED CABIN TRIM AIR MODULATING VALVE, IAW AMM 21-61-07. OPERATIONS AND LEAK CHECKS NORMAL. THIS CLEARS MDDR 141430.

Part: SWITCH — FAILED (ENGINE N1 GAUGE) · airframe 89,304 hrs · 22,458 cycles

REV DISPLAYED ABOVE LEFT ENGINE N1 GAUGE NORMAL REVERSE WORKED ON LANDING. TRANSFERED TO MDDR 141401, IAW MEL 78-31-01 CAT C, DUE 04FEB21 PLACARD INSTALLED MX PROCEDURE C/W. REMOVED NR 1 TR OUTBOARD SWITCH, PER B767 AMM 78-36-01 AND REPLACED W/78-36-01. OPERATIONS CHECK GOOD. THIS CLEARS DMI 141481.

Part: VALVE — INOPERATIVE (PASS CABIN) · airframe 89,304 hrs · 22,459 cycles

AFT ZONE TEMP EICAS MESSAGE. TRANSFERRED TO MDDR 141343, IAW MEL 21-61-01-02, CAT C. PERFORMED BITE TEST, IAW FIM 21-60-60 FAULT TREE 806 FOUND TRIM VALVE TO BE AT FAULT. ALSO OPC AFT TRIM VALVE MODULE, IAW AMM 21-61-07 CONFIRMED VALVE INOPERABLE. WHILE PERFORMING GVI FOUND AFT TRIM VLV, CONNECTOR NOT SECURED. SECURED CONNECTOR, OPERATIONS CHECK GOOD, IAW B767 21-64-01. THIS CLEARS DMI 141343.

Part: FAN — FAILED (EQUIPMENT BAY) · airframe 89,278 hrs · 22,448 cycles

EICAS MESSAGE "FWD EQPT OVHT" SHOW AND OVHT LIGHT IS ON, ON THE P5 PANEL. OVERHEAT LIGHT GOES OFF AFTER SELECTING THE EQUIP COOLING SELECTOR TO THE STANDBY POSITION. TRANSFERRED TO MDDR 141061, PER MEL 21-58-01-01 CAT "C" DUE 27 JAN 21. REMOVED AND REPLACED FWD EQP SUPPLY FAN, IAW AMM 21-58-06, OLD UNIT FOUND TO HAVE BROKEN FAN ROTOR BLADES. PERFORMED CLEANING OF SUPPLY FAN SCREEN, IAW AMM 21-58-30. OPERATIONS TEST GOOD. THIS CLEARS DMI 141061.

Part: WARNING MESSAGE — FALSE ACTIVATION (AFT CABIN TEMP) · airframe 89,278 hrs · 22,448 cycles

AFT CABIN TEMP CONTROL EICAS MESSAGE DISPLAYED. TRANSFERRED TO MDDR 141028, PER MEL 21-61-01-02 CAT "C". RAN FIM 21-60 FT 804. CLEANED RHEOSTAT, IAW AMM 12-25-00. OPERATIONS CHECKS, IAW AMM 21-61-00. CLEARED DMI 141028. PLACARD REMOVED.

Part: CIRCUIT CARD — MALFUNCTIONED (BLEED CONTROL) · airframe 89,268 hrs · 22,445 cycles

DURING PERFORMING T/S FOR LT ENGINE BLEED SYSTEM FOUND BLEED AIR CONTROL PC ASSEMBLY CARD BROKEN (M859). ALSO FOUND LT ENGINE BLEED CONT C/B OPEN. REMOVED AND REPLACED L BLEED AIR CONTROL PC ASSEMBLY CARD, IAW B767 AMM 36-11-12. OPERATIONS CHECK GOOD, NO DEFECTS NOTED AT THIS TIME. REMOVED AND REPLACED (2 BLEED AIR ENG N2 RELAY(K00777), IAW WDM 36-11-51. OPERATIONS CHECK GOOD OK FOR SERVICE.

Part: STARTER — FAULTED (APU) · airframe 89,234 hrs · 22,437 cycles

APU FAULT, FAILED TO START ON 2 ATTEMPTS. REMOVED AND REPLACED & APU STARTER, IAW AMM 49-41-01. OPERATIONS CHECK GOOD AT THIS TIME. REMOVED AND REPLACED ECU, IAW AMM 49-61-05. OPERATIONS CHECK GOOD AT THIS TIME. (SN: PN: 2117342-20). TIGHTENED APU VENT LINE AND APU PNEUMATIC SHUTOFF VALVE LINE, IAW AMM 20-11-00.

Part: RELAY — MALFUNCTIONED (EQUIP FAN) · airframe 89,226 hrs · 22,435 cycles

FWD EQ SUP FAN STATUS MSG(<P>PLACED ON MEL 21-58-04-02-01 CAT "C" DUE DATE 23JAN21. TRANSFERRED TO MDDR# 140831.</P><P>13JAN21 / 1259294 / ITEM 4 / ONT -&NBSP;PERF FIM 21-58 F/T 904 FWD EQP SUP FAN, SWAPPED ECS CONTROL CARD M861 WITH ECS CONTROL CARD M862. STATUS MSG DOES NOT REMAIN. SWAPPED ORG CARDS BACK. PLACED P/N 285T0078-15 ON ORDER.&NBSP; M861 CARD ECS FAN DMI REMAINS OPEN.</P><P>1/17/2021 - LP 1311970 ITEM 5 - BWI:&NBSP;REMOVED AND REPLACED RELAY K343 WDM 21-58-14.OPS TEST GOOD. THIS CLEARS MDDR 140831. PLACARD REMOVED.</P><P><BR /></P>)

Part: FAULT MESSAGE — FALSE ACTIVATION (APU) · airframe 89,208 hrs · 22,429 cycles

APU FAULT WHEN STARTING AFTER LANDING. PERFORMED TEST ON GROUND, IAW AMM 49-41-01. OPERATIONS CHECK TEST OK.

Part: FAN — FAILED (EQUIPMENT COOL) · airframe 89,155 hrs · 22,413 cycles

AFT EQ EXHAUST FAN NR 1. REMOVED AND REPLACED NR 1 AFT EQUIPMENT EXHAUST FAN, IAW AMM 21-58-41. OPERATIONS CHECKED GOOD.

Part: SEAL — UNKNOWN (L1 DOOR) · airframe 89,166 hrs · 22,415 cycles

L1 DOOR SEAL SHOWING LIGHT. PRESSURIZED IAW AMM 21-31-00. L1 DOOR SEAL OPERATIONS CHECK NORMAL AT THIS TIME.

Part: TRANSCEIVER — MALFUNCTIONED (WX RADAR SYSTEM) · airframe 89,070 hrs · 22,387 cycles

L RADAR SYSTEM SHOWS INCORRECT/BAD DATA. T/S PER FIM 34-43 FT 812. REMOVED AND REPLACED LT WEATHER TCVR, IAW AMM 34-43-01. OPERATIONS CHECK GOOD. NO DEFECTS NOTED.

Part: SWITCH — OUT OF LIMITS (GENERATOR FIELD) · airframe 89,045 hrs · 22,378 cycles

LEFT GENERATOR FIELD LIGHT ILLUMINATED. RESET LT GENERATOR FIELD SWITCH, IAW AMM 24-11-01. ALL OPERATIONS NORMAL.

Part: GENERATOR — TRIPPED (LEFT) · airframe 89,030 hrs · 22,371 cycles

LEFT GEN TRIPPED, RAN QRH, RESET NORMAL. PERFORMED BPCU BITE, IAW B767 FIM 24-20 FT 801. NO FAULTS. THEN PERFORMED ENGINE RUN OF THE ENGINE NR 1. NO FAULTS. GEN OPERATES NORMAL.

Part: SEAL DEPRESSOR — DAMAGED (PAX DOOR) · airframe 88,960 hrs · 22,346 cycles

DAMAGE FOUND ON AFT EDGE OF MCD DOOR SEAL DEPRESSOR. DAMAGE AT AFT EDGE OF MCD AT STATION 632 BETWEEN S-4L & S-13L, EXCEEDS SRM LIMITS. C/W PART 1 OF EO 6753A891 (TIME LIMITED REPAIR) APPLIED SPEED TAPE AT STA 632 MCD SEAL DEPRESSOR. PART 2 (DVI) INSPECTION EVERY 1 FLIGHT CYCLE. PART 3 (PERMANENT REPAIR) ON OR BEFORE 30 FLIGHT CYCLES. TRANSFERED TO NON-MEL MDDR NR 138029.

Part: CONTROLLER — MALFUNCTIONED (PRV) · airframe 88,927 hrs · 22,337 cycles

BTB LEFT ENGINE BLEED OFF EICAS ON CLIMBOUT, WOULD NOT RESET. PER FIM 36-20 F T 804 UP TO BLOCK 36. PERFORMED THUMB TEST, PER AMM 36-11-18. FOUND PRV LOCKOUT PIN LOOSE ALLOWING AIR TO ESCAPE. TIGHTENED LOCKOUT PIN, PER AMM 36-11-18-404-818-001. PERFORMED ENGINE RUN, PER AMM 71-00-00-00. OPERATIONS CHECKED GOOD. LEFT ENGINE SUPPLIED GOOD PRESSURE. PER FIM 36-20 FT 804 AND FIM 36-10 FT 832 BLOCK 21. REMOVED AND REPLACED PRESSURE REGULATING VALVE CONTROLLER, PER AMM 36-11-19. PERFORMED ENGINE RUN, PER AMM 71-00-00. NO HELP, REF LOG PG 1240981 ITEM 1 FOR CORRECTIVE ACTION.

Part: RADAR — MALFUNCTIONED (WEATHER SYS) · airframe 88,915 hrs · 22,333 cycles

AT FL360 LEFT RADAR SYSTEM AT 0 DEG TILT RETURNS SOLID RED BEYOND 80 NM. RIGHT RADAR SYSTEM RETURNS "NORMAL" GROUND CLUTTER AT SAME SETTING. SUSPECT LEFT RADAR TILT IS OUT OF CALIBRATION. PERFORMED WXR BITE, IAW FIM 34-43 FT 805, NO FAULTS NOTED. OPERATIONS CHECK GOOD. PERFORMED WXR OPERATIONS TEST, IAW AMM 34-43-00. OPERATIONS TEST GOOD.

Part: NONE — NONE (ENGINE) · airframe 88,862 hrs · 22,319 cycles

LEFT ENGINE APPEARS TO BE STRUCK BY BIRD. DUE TO BIRD STRIKE ON NR 1 ENGINE CONDITIONAL INSPECTION REQUIRED. INSPECTED NR 1 ESN 702640 FOR BIRD STRIKE, IAW B767 AMM 72-00-00. FOUND NO DAMAGE BY BIRDSTRIKE WITHIN THE LPC OR HPC. C/W CONDITIONAL BIRD STRIKE INSPECTION, IAW 05-51-18. NO EVIDENCE OF DAMAGE NOTED. BIRD INGESTED INTO CORE OF NR 1 ENGINE ONLY.

Part: RADAR — MALFUNCTIONED (LT WX SYSTEM) · airframe 88,732 hrs · 22,281 cycles

LEFT RADAR TILT APPEARS TO BE OUT OF CALIBRATION. EXCESSIVE GROUND CLUTTER IN CRUISE AT NORMAL TILT SETTINGS. RADAR TILT APPEARS TO BE LOWER THAN INDICATED. PERFORMED LT WX RADAR SYSTEM, REF FIM 34-43 FT 805. OPERATIONS CHECK NORMAL. COULD NOT DUPLICATE ON GROUND.

Part: CONTROLLER — WARNING MESSAGE (COCKPIT TEMP) · airframe 88,732 hrs · 22,281 cycles

FLIGHT DECK TEMP EICAS IN CRUISE. COMPLETED QRH PROCEDURE. PERFORMED BITE CHECK ON ZONE TEMP CONTROLLER, REF FIM 21-60 FT 805. NO FAULTS NOTED. MESSAGE CLEARED, OPERATIONAL CHECK NORMAL AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT GENERATOR) · airframe 88,705 hrs · 22,271 cycles

LT GEN OFF UPON LEFT ENGINE START. QRH COMPLETE. MAINTENANCE & DISPATCH NOTIFIED. PLACED ON MEL 136542, IAW AMM/DDG 24-00-01-01. CAT D, DUE 24OCT20. PERFORMED OPERATIONS CHECK OF LEFT ENGINE IDG, IAW AMM 24-11-00. OPERATIONS TEST GOOD. THIS CLEARS MDDR 136542. PLACARD REMOVED. MCC NOTIFIED.

Part: WARNING LIGHT — FALSE ACTIVATION (RT ENG ANTICE V) · airframe 88,683 hrs · 22,263 cycles

RT ENGINE ANTI ICE VALVE LIGHT ON SHUT DOWN. C/W OPERATIONS CHECK OF RT ENGINE ANTI ICE SYSTEM, IAW AMM 30-21-00. OPERATIONS CHECK GOOD, NO FAULTS NOTED. OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE INDICATION · airframe 88,646 hrs · 22,252 cycles

"FWD EQ EXHAUST FAN" STATUS MESSAGE, INTERMITTENT "OVERHEAT" ANNUNCIATOR ON EQUIPMENT COOLING PANEL. CYCLED EQ COOLING TO STANDBY AND BACK TO AUTO. PERFORMED OPERATIONS TEST, IAW AMM 21-50-00. SYSTEM TEST OK, NO FAULTS FOUND.

Part: PUMP — FAILED (FUEL BOOST) · airframe 88,608 hrs · 22,240 cycles

RIGHT AFT FUEL PUMP PRESSURE EICAS AND LIGHT. TRANSFERRED TO MDDR NR 135738 MEL 28-22-01, CAT C D. I CW 2103Z 10OCT20, BWI MX. REMOVED AND REPLACED RIGHT AFT FUEL PUMP, AS PER B767-30-0 AMM 28-22-03/401 AND PERFORMED OPERATIONS CHECK, PER AMM 28-22-00/501 FOUND GOOD. THIS CLEARS DMI NR 135738. DISP DM 1246Z.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 88,606 hrs · 22,239 cycles

LT GEN OFF EICAS MESSAGE AFTER START, RAN QRH, EICAS CLEARED. STARTED ENGINES, IAW MM 71-00-00. LT GEN CHECK OK MM 24-11-00. IDG OIL OK, PER MM 12-13-03. OK TO CONTINUE.

Part: TRU — MALFUNCTIONED (APU) · airframe 88,596 hrs · 22,235 cycles

APU FAULT ON FIRST ATTEMPT. TRANSFERRED TO MDDR 135610, PER DDG 49-11-01A. REMOVED AND REPLACED APU TRANSFORMER RECTIFIER UNIT, AS PER AMM 24-32-04 AND APU FAULT ANN SWITCH ASSEMBLY, AS PER AMM 33-16-02. OPERATIONAL CHECKS FOUND OK. THIS WILL CLEAR MDDR 135610.

Part: SENSOR — FLUCTUATES (ENG OIL TEMP) · airframe 88,606 hrs · 22,239 cycles

RT ENG OIL TEMP FLUCTUATING IN FLIGHT TO 0 DEG C, ALWAYS SHOWED LESS THAN LT ENGINE ON START. RT ENGINE OIL TEMP FLUCTUATING UP TO -17 DEG C. REMOVED AND REPLACED RIGHT ENGINE OIL TEMP SENSOR. OPS CHECKS GOOD, IAW AMM 79-34-01.

Part: CONTROL UNIT — FAILED (APU) · airframe 88,596 hrs · 22,235 cycles

APU FAULT ON FIRST ATTEMPT. REMOVED AND REPLACED APU CONTROL UNIT. OPERATIONS CHECKS NORMAL, IAW AMM 49-61-05.

Part: CONNECTOR — DIRTY (FUEL BOOST PUMP) · airframe 88,567 hrs · 22,225 cycles

RT AFT FUEL PUMP EICAS MESSAGE AND PRESS LT IN SWITCH ILLUMINATED AFTER PRESSURIZING AND TURNING FUEL PUMPS ON. TRANSFER TO MDDR 135436, IAW DDG 28-22-01, CAT "C", 13OCT20. DPI: EH 1720Z. PERFORMED CANNON PLUG CLEANING ON RT AFT FUEL BOOST PUMP, IAW AMM SWPM 20-60-01. RESET AND PERFORMED GFI FUNCTIONAL TEST, IAW AMM 28-22-00. OPERATIONS CHECKS NORMAL. NO EICAS MESSAGE NOTED. THIS CLEARS DMI 135436. MCC NOTIFIED. PLACARD REMOVED.

Part: WARNING MESSAGE — FALSE ACTIVATION (APU) · airframe 88,544 hrs · 22,218 cycles

APU FAULT, NO FAULTS FOUND, COULD NOT DUPLICATE. APU STARTED ON GROUND. NO FAULTS FOUND. OPS CHECK, REF AMM 49-00-00.

Part: UNKNOWN — FAULTED (APU) · airframe 88,531 hrs · 22,214 cycles

APU FAILED TO START FIRST ATTEMPT AFTER LANDING. 785 EGT 29% RPM THEN SHUTDOWN AND "APU FAULT" MESSAGE. SUCCESSFUL SECOND START ATTEMPT. PERFORMED APU START PROCEDURE, OPS CHECK NORMAL, IAW AMM 49-11-00.

Part: TRU — MALFUNCTIONED (APU) · airframe 88,523 hrs · 22,211 cycles

APU FAULT, CHRONIC APU STARTING ISSUES AFTER LANDING. PERFORMED APU BITE, IAW FIM 49-11 FT 958, NO FAULTS NOTED ON APU ECU AND NO FAULTS NOTED ON ECU SELF TEST. PERFORMED THREE SUCCESSFUL STARTS, IAW 49-11-00. OPERATIONS CHECKS NORMAL. DUE TO CHRONIC APU FIRST TIME STARTING ISSUE. TRANSFERED TO MDDR 135006, IAW MEL 49-11-01A, CAT C, DUE DATE 06OCT20. REMOVED AND REPLACED APU TRU, IAW AMM 24-32-04-404-003. OPERATIONS GOOD. THIS CLEARS MDDR 135006. PLACARD REMOVED.

Part: UNKNOWN — FAULTED (APU) · airframe 88,511 hrs · 22,207 cycles

APU FAULT WHEN STARTING UPON LANDING. PERFORMED APU BITE, IAW FIM 49-11 FT 958, NO MSGS NOTED OR FAULTS NOTED ON APU BOX. PERFORMED APU EXTERIOR INSPECTIONS, IAW AMM 49-21-00. NO LEAKS, CRACKS, TEARS, OR LOOSE CANNON PLUGS FOUND. PERFORMED 4 SUCCESSFUL STARTS, IAW AMM 49-61-05. WITH NO FAULTS FOUND.

Part: ANTENNA — FAILED (WX RADAR SYSTEM) · airframe 88,494 hrs · 22,201 cycles

WXR FAIL BOTH L/R SYS. REPLACED WXR RADAR ANTENNAE ASSY, PER AMM 34-43-05. OPS CHECK L/R WXR, SYSTEM CHECK GOOD.

Part: CONTROL PANEL — MALFUNCTIONED (ELECTRICAL) · airframe 88,482 hrs · 22,197 cycles

APU GENERATOR NOT GOING OFF WHEN COMMANDED. REMOVED AND REPLACED APU GEN POWER BREAKER, IAW B767 AMM 24-22-03. OPS CHECK FAILED. FURTHER T/S REQUIRED. REMOVED AND REPLACED ELEC SYS CONTROL PANEL, IAW AMM 24-22-01. NO DEFECTS NOTED.

Part: APU — INOPERATIVE (APU BAY) · airframe 88,449 hrs · 22,183 cycles

APU INOPERABLE, TRANSFERRED TO MEL 49-11-01A, MDDR #133991, CAT C. REMOVED AND REPLACED APU, IAW WORK CARD A-49-999-00-01. REVERSE FLOW MESSAGE ON ECU CLEARED. THIS CLEARS MDDR 133991, MCC NOTIFIED. PLACARD REMOVED.

Part: SENSOR — LOOSE (HYD PUMP) · airframe 88,427 hrs · 22,176 cycles

APU SHUTDOWN TWICE PRIOR TO START, AFTER HYDRAULIC FUEL PUMPS TURNED ON. TURNED PACK OFF PRIOR TO THIRD HYD POWER UP, NORMAL START. PERFORMED APU BITE PER FIM 49-11 FT 958 "REVERSE FLOW" AS REASON FOR SHUTDOWNS. TIGHTENED INLET TEMP SENSOR FOR LCIT IAW FIM 49-11 FIG. 103, TABLE A AND AMM 49-61-03 OPERATIONAL TEST OF APU PASSED.

Part: SMOKE DETECTOR — MALFUNCTIONED (NR 4) · airframe 88,413 hrs · 22,172 cycles

#4 SMOKE DETECTOR AMBER LIGHT ILLUM ON CARGO FIRE PANEL. CYCLED BREAKERS AND PERFORMED BYTE CHECK ON CARGO COMP SMOKE DETECTOR SYSTEM AS PER FIM TASK 26-19-00-815-803. OPS CHECK NORMAL AT THIS TIME.

Part: FILTER — WARNING MESSAGE (SCAVANGE) · airframe 88,341 hrs · 22,145 cycles

APU INOP DUE (AUXILIARY POWER UNIT (APU),ER OPERATIONS NOT ALLOWED. REMOVED AND REPLACED APU GENETATOR SCAVENGE FILTER ELEMENT IAW TASK 49-27-03-004-001. REMOVED AND REPLACED APU SURGE VALVE FILTER IAW TASK 49-53-06-402-009. CHECKED OPS GOOD.

Part: UNKNOWN — UNKNOWN (APU) · airframe 88,329 hrs · 22,141 cycles

AFTER LOAD APPLIED TO HYD SYSTEM, APU AUTO FAULTED AND SHUT DOWN. PERFORMED APU BITE TEST IAW AMM 49-61-05. NO FAULTS NOTED, APU STARTED AND OPERATING NORMAL.

Part: BPCU — FAILED (LT GENERATOR) · airframe 88,323 hrs · 22,139 cycles

L FIELD GEN FLASHING DURING BITE CODE 44 BPCU FAULT FOUND. REMOVED AND REPLACED BPCU IAW 24-41-03. NO FURTHER DEFECTS NOTED AT THIS TIME

Part: APU — MALFUNCTIONED · airframe 88,313 hrs · 22,135 cycles

APU FAULT & SHUTDOWN PRIOR TO BLOCK OUT. C/W APU START AND RUN PROCEDURE, SYSTEM CHECKED GOOD AT THIS TIME IAW MM CH 49-11-00.

Part: WARNING LIGHT — FALSE ACTIVATION (LT BLEED) · airframe 88,279 hrs · 22,123 cycles

LEFT ENG BLEED AIR SWITCH OFF LIGHT REMAINS ILLUMINATED EVEN AFTER COMPLIANCE WITH DDG 30-21-P1-04-02 PROCEDURES. PERFORMED ENG RUN IAW AMM 71-00-00-862 .OPS CK GOOD. NO DEFECT NOTED. ALL PNEUMATIC CKS GOOD. A/C OK FOR SVC.

Part: ANTI-ICE VALVE — MALFUNCTIONED (LT ENGINE) · airframe 88,253 hrs · 22,114 cycles

EICAS L ENG ANTI ICE AFTER ATTEMPTING TO TURN OFF. PERFORMED QRH IN FLIGHT. REMOVED AND REPLACED L/H ENGINE ANTI-ICE VALVE IAW AMM 30-21-03. OPS CK GOOD.

Part: APU — SHUTDOWN · airframe 88,087 hrs · 22,063 cycles

WHEN GPU POWER REMOVED, APU SHUT DOWN. RESTARTED NORMALLY. C/W APU OPS CHECK IAW AMM 49-00-00. OPS CHECK GOOD.

Part: APU — MALFUNCTIONED · airframe 88,052 hrs · 22,054 cycles

APU SHUTDOWN DURING PUSHBACK. PERFORMED A BITE ON THE APU ECU, NO CURRENT FAULTS, NORMAL STOP SIGNAL, APU STARTED SECOND ATTEMPT, NO FAULTS IAW AMM 49-61-00.

Part: CONTROL VALVE — MALFUNCTIONED (APU) · airframe 87,885 hrs · 22,003 cycles

APU PNEUMATIC INOP (AUXILIARY POWER UNIT, PNEUMATIC FUNCTION). PERFORMED BITE CHECK OF SYSTEM PER AMM 49-61-05. NO FAULTS NOTED. APU START 1ST ATTEMPT. CB BREAKER S-23 C VALVE VERIFIED IN OFF POSITIONS PER 36-11-04. REMOVED AND REPLACED SURGE CONTROL VALVE IAW AMM 49-53-01. OPS CHECK NORMAL. NO AUTO SHUTDOWN. PERFORMED APU BITE IAW AMM 49-61-05. NO FAULTS NOTED. THIS CLEARS DMI 130515. PLACARDS REMOVED. MCC NOTIFIED.

Part: INDICATOR — NO TEST (COOLING SYS) · airframe 87,788 hrs · 21,975 cycles

INSTRUMENT COOLING SYSTEM, E1-E2 BALL NOT TESTING. REMOVED AND REPLACED THE E/E MONITOR INDICATOR IAW AMM 21-58-34. OPS TESTED OK.

Part: RADAR — FAILED (WEATHER) · airframe 87,756 hrs · 21,964 cycles

WEATHER RADAR SYS LEFT AND RIGHT FAIL INDICATIONS. RESET WX RADAR C/B LT & RT. PERFORMED OPS CHECK IAW AMM 34-43-00. ALL CHECKS GOOD.

Part: ATTACH FITTING — BROKEN (FLAP TRACK) · airframe 87,754 hrs · 21,963 cycles

LT WING OB FLAP OB TRACK, LWR TRAILING EDGE ATTACH FITTING AT WBL 710 BROKEN. REMOVED AND REPLACED THE ATTACH FITTING ON THE LT WING OB FLAP TRACK TRAILING EDGE AT WBL 710 IAW SRM 51-40-02.

Part: ADAPTER — CORRODED (LT WING) · airframe 87,754 hrs · 21,963 cycles

LEFT WING UPPER SURFACE OVERWING FILL PORT ADAPTER FLANGE HAS CORROSION. REMOVED CORROSION FROM LT WING UPPER FILL PORT ADAPTER FLANGE AND WAS FOUND OUT OF LIMITS IAW SRM 57-20--01-1A-1. REPAIRED OVERWING FILL PORT ADAPTER FLANGE IAW FAS EA 20017 REV IR.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 87,756 hrs · 21,962 cycles

AFTER TAKEOFF HAD SMOKE/FUMES IN COCKPIT(<P>PERFORMED SMOKE OR FUMES IN CABIN CONDITIONAL INSPECTION REF AMM 05-51-56. REMOVED OIL CONTAMINATION FROM THE AIR CONDITIONING AND PNEUMATIC SYSTEM REF AMM 21-00-21-102.</P><P>LP 1130723 - M6: REMOVED AND REPLACED LEFT ENGINE REF AMM 71-00-02. ENGINE RUN SATISFACTORY. NO LEAKS NOTED.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 87,746 hrs · 21,958 cycles

ON CLIMB OUT RECEIVED R FWD FUEL PUMP MESSAGE WITH PRESS LIGHT&NBSP;(<P>T/S IAW FIM 28-22 FAULT TREE 819 PUMP OPERATES NORMAL. ALSO T/S IAW FIM 28-41-FAULT TREE 854. NO FAULTS FOUND.</P>)

Part: UNKNOWN — ODOR · airframe 87,728 hrs · 21,951 cycles

STRONG STINK ODOR FROM PACKS BELOW 10K FEET.(<P>TRANSFERRED TO MDDR 128086 IAW DDG 21-51-01-01, CAT 'C', DUE DATE 18MAY20, MAINT ACTIONS C/W. NOTE: MX VERIFIED SMELL STRONG FROM LEFT PACK, DEFERRAL IS FROM LEFT PACK ONLY. T&AMP;I JT0142Z.</P><P>LP&NBSP;1130707: PERFORMED INSPECTION OF L COOLING PACK IAW AMM 21-51-00, HEAT EXCHANGER &AMP; CONDENSERS, DUCTS ARE CLEAR OF FOD. NO SIGN OF FOUL SMELL. CLEANED OUT WATER FROM WATER SEPARATOR DRAIN IAW 21-51-21. SUPPLIED CONDITION AIR IAW AMM 21-00-00. NO FOUL SMELL. THIS CLEARS DMI 128086.<BR /></P>)

Part: CONTROL MODULE — FAULTY (ECS FAN) · airframe 87,725 hrs · 21,950 cycles

AFT EQ EXH FAN 2 EICAS MSG.(<P>TRANSFERRED TO MDDR 128074 PER MEL 21-58-05, CAT 'C', DUE DATE: 17MAY20. DISPATCHER: JT @18:24Z.</P><P>LP 1130713: REPLACED ECS FAN CONTROL MODULE M861 IAW AMM 21-58-24. CHKS GOOD. CLOSED MDDR 128074.</P>)

Part: UNKNOWN — ODOR · airframe 87,705 hrs · 21,944 cycles

PACKS HAVE A VERY DIRTY SMELL ON TAKEOFF &AMP; APPROACH.(<P>ACCOMPLISHED OPS TEST OF COOLING SYSTEM THRU FULL TEMP RANGE IAW AMM 21-51-00. COULD NOT REPRODUCE SMELL ON GROUND.</P>)

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 87,705 hrs · 21,944 cycles

APU FAILED AND SHUTDOWN BEFORE ENG START(<P>PLACED ON MDDR 127985 PER MEL 49-11-01A, CAT 'C'.</P><P>08MAY20, BWI LP 1150050, ITEM M5: PERF APU BITE IAW FIM 49-11 FT 958. FOUND NO FAULTS. APU OPERATING NORMAL AND STARTING PARAMETERS SHOW NO SIGNS OF A BAD START. THIS CLEARS DMI 127985. DP @ 16:05Z.</P>)

Part: AIR DUCT — CONTAMINATED (AC BAY) · airframe 87,712 hrs · 21,946 cycles

BURNT OIL SMELL FROM AIR CONDITIONING SYSTEM WHEN THROTTLES ADVANCED FOR DEPARTURE AND ON DESCENT DURING 16K.(<P>PER CUSTOMER REQUEST, PERFORMED REMOVAL OF OIL CONTAMINATION PER B767 AMM 21-00-201 FROM THE AIR CONDITIONING AND PNEUMATIC SYSTEMS, VISUALLY INSPECTED RAM AIR INLETS AND L &AMP; R PACK BAYS AFTERWARDS IAW AMM 21-00-00. NO BURNT OIL SMELLS NOTED AND NO DISCREPANCIES FOUND. MCC NOTIFIED.</P>)

Part: SHUTOFF VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 87,612 hrs · 21,911 cycles

L ENG BLEED OFF AFTER BOTH ENG STARTED. COMPLETE SHUTDOWN OF L ENG &AMP; RE-START BUT DID NOT CLEAR, RTB PARKING.(<P>REMOVED AND REPLACED L PRSOV VALVE I.A.W AMM 36-11-09. OPS CHECK GOOD.</P>)

Part: PRESSURE SWITCH — DISCONNECTED (RT ENGINE) · airframe 87,566 hrs · 21,896 cycles

R ENG NOSE COWL THERMAL ANTI ICE PRESSURE SWITCH IS DISCONNECTED AND HEAVILY CORRODED INSIDE CONNECTOR P/N 215N41-84.(<P>REMOVED AND REPLACED THERMAL ANTI ICE PRESSURE SWITCH IAW AMM 30-21-01/401 REV 129. OPS CHECK GOOD.</P>)

Part: UNKNOWN — MALFUNCTIONED (WARNING SYSTEM) · airframe 87,552 hrs · 21,890 cycles

B LOOP ON CARGO DETECT INOP&NBSP;(<P>TRANSFERRED TO MDDR #126848 I.A.W MEL 26-16-02-01, CAT C.</P><P>LOG PAGE 1189953: PERFORMED BITE PROCEDURE ON MAIN DECK CARGO REF FIM 26-19 FT 803. NO MESSAGE NOTED. TEST PASS, MDDR #126848 CLOSED.</P>)

Part: EEC — MALFUNCTIONED (APU) · airframe 87,543 hrs · 21,887 cycles

PRIOR TO ENGINE START, WITH SELECTION OF HYDRAULIC DEMAND PUMPS, APU AUTO SHUT DOWN DUE TO RIGHT EEC CB CHANNEL A.(<P>RESET CB, REF FIM 73-21 FT 885, NO FAULTS NOTED.</P><P>ITEM 2: APU STARTED FIRST ATTEMPT, NO APU WORK DONE, NO FAULTS NOTED. NO COLD SOAK REQUIRE. REF AMM 49-11-01.<BR DATA-MCE-BOGUS="1" /></P>)

Part: EXCITER — FAULTY (APU) · airframe 87,508 hrs · 21,877 cycles

APU FAULT ON START ATTEMPT. ATTEMPTED TWICE. 20 MAX RPM W/ NO EGT RISE.(<P>TRANSFERRED TO MDDR 126631 PER MEL 49-11-01A, CAT C, DUE DATE 13APR20. DI: JT @ 20:37Z.</P><P>BWI, 04APR, LP 1071367, ITEM M2: REMOVED AND REPLACED APU IGNITION EXCITER IAW AMM 49-41-03. REMOVED AND REPLACED APU ELEC IGNITOR LEAD (OFF P/N 3888076-2, NSN)&NBSP;IAW AMM 49-41-02, OPS CHECKED GOOD. THIS CLEARS MDDR 126631. PLACARD REMOVED, MX NOTIFIED.</P>)

Part: BULB — BROKEN (AC PACK) · airframe 87,479 hrs · 21,867 cycles

ON WALK AROUND FOUND #1 PACK TEMP BULB BROKEN OFF DUCT #1 PACK INOP.(<P>TRANSFERRED TO MDDR #126206 I.A.W MEL 21-51-01-01, CAT 'C'.</P><P>LOG PAGE 1185224: INSTALLED NEW PRIM HX INLET TEMP BULB I.A.W AMM 21-52-08. OPS CHECK AND LEAK CHECK GOOD, MDDR #126206 CLOSED.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 87,475 hrs · 21,865 cycles

WX FAIL MESSAGE ON EHSI WITH LEFT WX RADAR SYSTEM SELECTED.(<P>PERFORMED WEATHER RADAR SYSTEM OPERATIONAL TEST, NO FOUL AT THIS TIME. L &AMP; R SYSTEM OPS CHECK GOOD AT THIS TIME.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 87,455 hrs · 21,859 cycles

ON DEPARTURE CLIMBING THRU 4000' +/- THE RIGHT FWD FUEL PUMP PRESS LIGHT ILLUMINATED, LIGHT EXTINGUISHED.(<P>PERFORMED FIM TASK 28-22 FAULT TREE 819, OPS CHECK GOOD AT THIS TIME.</P>)

Part: SELECTOR KNOB — LOOSE (COCKPIT) · airframe 87,419 hrs · 21,847 cycles

RIGHT ENGINE STARTER SELECTOR LOOSE AND SLIDES OFF SHAFT.(<P>FOUND SELECTOR KNOB LOOSE. TIGHTENED LOCK SCREWS IAW AMM 20-11-00. SELECTOR SECURE, OPS GOOD.<BR /></P>)

Part: PRESSURE SWITCH — MALFUNCTIONED (RT FUEL PUMP) · airframe 87,321 hrs · 21,810 cycles

"R FWD FUEL PUMP" EICAS MESSAGE SHORTLY AFTER LIFTOFF. FUEL IN TANK WAS APPROX 14.5.(<P>REMOVED AND REPLACED&NBSP;R FWD FUEL PUMP PRESSURE SWITCH IAW AMM 28-42-01. FUEL PUMP OPERATES NORMAL, NO FAULTS NOTED AT THIS TIME.</P>)

Part: SMOKE DETECTOR — INOPERATIVE (MAIN CARGO) · airframe 87,177 hrs · 21,767 cycles

MAIN CARGO #2A SMOKE DETECTOR INOP.(<P>TRANSFERRED TO MDDR #124487 IAW MEL 26-16-02-02, CAT 'C', DUE 20FEB20.</P><P>LP 1188760, ITEM M2: REMOVED AND REPLACED #2A SMOKE DETECTOR IAW 26-19-01. OPS CHECK NORMAL, NO FAULTS NOTED. THIS CLEARS MDDR 124487.</P>)

Part: ACTUATOR — MALFUNCTIONED (RAM AIR DOOR) · airframe 87,120 hrs · 21,745 cycles

RIGHT PACK INOP / (AIR CONDITIONING PACKS, -200/-300 (NOTIFY DISPATCH) (ER RESTICTIED R-60))(<P>TRANSFERRED TO MDDR #124209 PER DDG 21-51-01-01, CAT "C",&NBSP; DUE 12FEB20. MX PROCEDURE COMPLIED WITH.</P><P>LP 929492: REMOVED AND REPLACED RIGHT RAM AIR INLET DOOR ACTUATOR IAW AMM 21-53-03, OPS CHECK OK. THIS CLEARS MDDR 124209.</P>)

Part: ECU — MALFUNCTIONED (APU) · airframe 87,061 hrs · 21,724 cycles

NO APU PNEUMATIC PRESSURE FROM APU, PERFORMED AIR STARTS, APU IS GOOD. PERFORMED APU BITE TEST IAW FIM 49-11 FT 958. FAULTED P2 SENSOR. REPLACED THE SENSOR IAW AMM 49-61-04. NO HELP. REPLACED ECU IAW AMM 49-61-05. OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (FAN) · airframe 87,035 hrs · 21,716 cycles

AFT EQUIPMENT EXHAUST FAN 2 STATUS MSG.(<P>RESET AFT EQUIPMENT EXHAUST FAN 2 C.B. AND PERFORMED OPS TEST. OPS CHECK GOOD. MSG REMAINS EXTINGUISHED, REF B767 AMM 21-58-41-710-002-002. NO FURTHER DEFECTS NOTED.</P>)

Part: SHUTOFF VALVE — INOPERATIVE (APU) · airframe 87,008 hrs · 21,708 cycles

NO PNEUMATIC WITH APU RUNNING. REMOVED AND REPLACED APU BLEED AIR SHUTOFF VALVE IAW AMM 36-11-10. OPS CHECK GOOD.

Part: ECU — FAULTY (APU) · airframe 86,961 hrs · 21,695 cycles

APU FAILED TO START. TROUBLE SHOT IAW FIM 49-11, REMOVED AND REPLACED ECU IAW AMM 49-61-03. OPS CHECK GOOD AT THIS TIME. (NOTE: OPENED A DMI 123422 IAW DDG 25-AP-01, OPTION C - FOR APU COLD SOAK START VERIFICATION)

Part: AIR DUCT — CRACKED (APU) · airframe 86,961 hrs · 21,695 cycles

NOTED EXTERIOR BLEED AIR NOISE COMING FROM LEFT MAIN GEAR DOOR AREA. FOUND CRACK AT FLANGE IN APU BLEED AIR DUCT. REMOVED AND REPLACED APU BLEED AIR DUCT ELBOW FWD OF APU SOV (CTR ISOL VLV), CHECKED FOR AIR LEAKS. NO AIR LEAK NOTED. REF AMM 20-11-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 86,950 hrs · 21,692 cycles

AFTER TAKEOFF - RT FWD FUEL PUMP EICAS MESSAGE & ASSOCIATED LOW PRESS LIGHT ILLUMINATED MOMENTARILY. PERFORMED OPS CHECK ON ALL FUEL PUMPS IAW AMM 28-22-00. OPS CHECK GOOD.

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 86,929 hrs · 21,681 cycles

APU FAILED TO START ON 2 ATTEMPTS AFTER LANDING.(<P>PERFORMED ECU BITE CHECK I.A.W AMM 49-61-05. NO LIGHT OFF FAULT, PERFORMED APU OPERATIONAL TEST I.A.W AMM 49-11-00. NO DEFECTS NOTED.</P>)

Part: CONTROL VALVE — MALFUNCTIONED (APU) · airframe 86,883 hrs · 21,665 cycles

APU INOP ( AUXILIARY POWER UNIT (APU), ER OPERATIONS NOT ALLOWED (NOTIFY DISPATCH) R60 )(<P>TRANSFERRED TO MDDR 122826, MEL 49-11-01A, CAT 'C', DUE 10JAN20.</P><P><SPAN>LP 1205918: REMOVED AND REPLACED APU FUEL VALVE CONTROL ASSY IAW AMM 49-31-01. OPS CHECK GOOD. NO LEAKS NOTED. THIS CLEARS MDDR 122826. PLACARD REMOVED.</SPAN><BR /></P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 86,883 hrs · 21,665 cycles

MAIN CARGO FIRE SMOKE DETECTOR A2 STATUS LIGHT ILLUMINATED AMBER.(<P>T/S PER FIM 29-16 FT 803, FAULTS CLEARED, SYS TESTS OK AT THIS TIME&NBSP;IAW&NBSP;<SPAN>AMM 26-16-00.</SPAN><BR /></P>)

Part: INERTIA REEL — INOPERATIVE · airframe 86,729 hrs · 21,605 cycles

INERTIAL REEL POSITION B UNSERVICABLE. REMOVED AND REPLACED DESCENT DEVICE INERTIAL REEL B IAW AMM 25-61-05, NO DEFECTS NOTED.

Part: ESCAPE REEL — UNWANTED DEPLOY · airframe 86,653 hrs · 21,578 cycles

ONE DESCENT DEVICE DEPLOYED AND REMOVED.(<P>TRANSFERRED TO MDDR #120939 IAW MEL 25-61-01-01, CAT 'C', DUE DATE: 01-DEC-2019.&NBSP; PLACARD INSTALLED AND MX DDG PROCEDURE C/W.&NBSP;</P><P>LP&NBSP;1097349 - M4; INSTALLED NEW DESCENT DEVICE 1 EA IAW AMM 25-61-05. THIS CLEARS MDDR 120939. PLACARDS REMOVED AND MCC NOTIFIED.</P>)

Part: ESCAPE REEL — UNWANTED DEPLOY · airframe 86,606 hrs · 21,561 cycles

EMERGENCY DECENT DEVICE EXTENDED ON LANDING.&NBSP;(<P>TRANSFERRED TO MDDR 120649 PER MEL 25-61-01-01, CAT 'C', C/W DDP. REMOVED AFFECTED ESCAPE DEVICE.</P><P>LP 1223283 - M4: INSTALLED&NBSP;EMERGENCY DESCENT DEVICE IAW B767 AMM 25-61-05, NO FURTHER DEFECTS NOTED. THIS CLEARS DMI #120649. MCC NOTIFIED AND PLACARD REMOVED.</P>)

Part: ACTUATOR — LOW TORQUE (APU) · airframe 86,604 hrs · 21,560 cycles

APU INOP DUE TO NUMEROUS ECU FAULTS PER POWERPLANT ENGINEERING.(<P>TRANSFERRED TO&NBSP;MDDR 120639 PER MEL 49-11-01A, CAT 'C'.<BR /></P><P>LP 1223288 - M5: REMOVED AND REPLACED INLET GUIDE VANE ACTUATOR REF B767 AMM 49-52-02, OPS CHECK GOOD. THIS CLEARS DMI 120639. PLACARD REMOVED AND MCC NOTIFIED.</P>)

Part: APU — MALFUNCTIONED · airframe 86,582 hrs · 21,552 cycles

AFTER LANDING; APU START EICAS MSG, APU FAULT.(<P>PERFORMED VISUAL CHECK OF THE APU OIL NOT VISIBLE IN SIGHT GLASS. SERVICED APU IAW AMM 12-13-04 AND PERFORMED APU OPERATIONAL CHECK; OPS CHECK GOOD AT THIS TIME. VERIFIED OIL CAP IS INSTALLED. NO LEAKS NOTED.</P><P>NOTE: LP 1111482 - M5: APU COLD SOAK START VERIFICATION MDDR 120552 OPENED DUE TO ITEM ABOVE.</P><P>LP 1111484 - ITEM 2: APU COLD SOAK START ATTEMPTED FL 360, SAT -58 C, 0853Z, START SUCCESSFUL ON FIRST ATTEMPT. THIS CLEARS MDDR 120552. PLACARD REMOVED AND MCC NOTIFIED.&NBSP;</P>)

Part: TRANSCEIVER — INOPERATIVE (WX RADAR SYS) · airframe 86,578 hrs · 21,550 cycles

LH WEATHER RADAR SYSTEM INOP(<P>PERFORMED WX BITE TEST, SYSTEM FAILED. ITEM TRANSFERRED TO MDDR 120536 AS PER ATLAS DDG 34-43-01, CAT 'D'.</P><P>LP 1111492 - M5: REMOVED AND REPLACED LT WX TRANSCEIVER&NBSP;IAW B767-300 AMM 34-43-01. OPS CHECKED NORMAL IAW 34-43-00. THIS CLEARS&NBSP; MDDR 120536, PLACARD REMOVED.</P>)

Part: ESCAPE REEL — DISLODGED (CABIN) · airframe 86,576 hrs · 21,549 cycles

ESCAPE REEL DISLODGED ON LANDING.(<P>TRANSFERRED TO DMI #120498 IAW MEL 25-61-01-01, CAT 'C', DUE 22-NOV-19.&NBSP;</P><P>LP 1111478 - M5: INSTALLED DESCENT DEVICE POSITION "B" IAW AMM 25-61-03. THIS ACTION CLEARS DMI #120498.&NBSP;PLACARD REMOVED.</P>)

Part: ESCAPE REEL — DISLODGED (NR 3) · airframe 86,561 hrs · 21,544 cycles

DESCENT REEL C FELL OUT OF ITS CONTAINER.(<P>REMOVED AND REPLACED #3 DESCENT DEVICE REEL IAW B767 AMM 25-60-05.</P>)

Part: RADAR — MALFUNCTIONED (WX SYSTEM) · airframe 86,489 hrs · 21,514 cycles

RADAR WAS FLASHING.(<P>COMPLETED FUNCTION TEST IAW AMM 34-43-00, OPS CHECK GOOD AND NO FAULTS FOUND.&NBSP;</P>)

Part: SWITCH — INOPERATIVE · airframe 86,435 hrs · 21,493 cycles

LEFT ENGINE BLEED OFF LIGHT INOP.&NBSP;(<P>TRANSFERRED TO MDDR #119157 IAW MEL 36-21-02, CAT 'C'.&NBSP;</P><P>LP 1098127 - M3: REMOVED AND REPLACED L ENG BLEED KORRY LIGHT SWITCH IAW AMM 33-16-02. THIS CLEARS MDDR #119157. MCC NOTIFIED.&NBSP;</P>)

Part: NOZZLE — OBSTRUCTED (EXTINGUISHER) · airframe 86,352 hrs · 21,466 cycles

AFT CARGO STATION 1150, FIRE EXTINGUISHER NOZZLE BLOCKED. REMOVED OBSTRUCTION FROM NOZZLE AS PER AMM 26-23-00, ALL OTHER NOZZLES OK.

Part: CONTROL PANEL — FAILED (STARTING) · airframe 86,315 hrs · 21,453 cycles

AFTER ENGINE START, RT ENGINE IGNITION SWITCH REMAINED IN GND POSITION. NO VALVE LIGHT ILLUMINATED, NO EICAS MESSAGE ILLUMINATED. REMOVED AND REPLACED ENGINE IGNITION AND STARTING PANEL IAW AMM 80-11-51. OPS CHECK SUCCESSFUL, NO DEFECTS NOTED.

Part: ECU — MALFUNCTIONED (APU) · airframe 86,299 hrs · 21,447 cycles

APU INOPERATIVE. PERFORMED APU BITE PER FIM 49-11 FT 958, FOUND NO FAULTS. APU STARTED AND OPERATED NORMAL IAW AMM 49-11-00-802-002. REMOVED AND REPLACED APU CONTROL UNIT (ECU) IAW AMM 49-61-05. OPS AND BITE CHECK GOOD AT THIS TIME.

Part: PANEL — FAULTY (COCKPIT) · airframe 86,297 hrs · 21,446 cycles

FOUND STBY POWER BATTERY TEST LIGHT NOT ILLUMINATED.(<P>REMOVED AND REPLACED STBY POWER BATTERY PANEL IAW AMM 24-33-04, OPS TEST OK.&NBSP;</P>)

Part: SHUTOFF VALVE — INOPERATIVE (E/E BAY) · airframe 86,295 hrs · 21,445 cycles

FORWARD EQUIPMENT VALVE EICAS MESSAGE DISPLAYED. T/S SYSTEM, FOUND SHUT-OFF 3 WAY VALVE INOPERATIVE. REMOVED AND REPLACED SHUT-OFF 3 WAY VALVE IAW AMM 21-58-01. OPS AND LEAK CHECKS GOOD.

Part: OIL SYSTEM — LOW (APU) · airframe 86,269 hrs · 21,435 cycles

APU WOULD NOT START AFTER LANDING. 2 ATTEMPTS, APU FAULT BOTH TIMES.(<P>PERFORMED BITE TEST OF APU ECU. LAST RUN, LOW OIL PRESS MESSAGE. CHECKED APU OIL LEVEL, FOUND TO BE LOW. SERVICED OIL IAW AMM 12-13-04 TO FULL. ECU BITE TEST IAW AMM 49-61-05. RAN APU, EXTERNAL LEAK CHECK OK, AND SUBSEQUENT BITE TEST OK.</P>)

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 86,260 hrs · 21,433 cycles

REF MEL 25-AP-01 APU COLD SOAK START UNSUCCESSFUL - 2 ATTEMPTS, FL 410, SAT -59°C, (APU STARTED - RUN MOMENTARILY THEN "APU FAULT" EICAS &AMP; SHUTDOWN).&NBSP;(<P>LP 1223468 - M6:&NBSP;WIND MILLED #1 ENG, PUT APU IN MES MODE AND CHECKED SURGE VALVE POSITION. IT WAS NEAR CLOSED BUT NOT FULLY CLOSED. PERFORMED BITE CHECK AND GOT A LOW OIL PRESSURE BITE. DMI 118222 REMAINS OPEN. REF FIM 49-11 FAULT TREE 966.</P><P>LP 1223470 - ITEM 1:&NBSP;APU RELIABILITY COLD START ACCOMPLISHED ON FLIGHT LEG CVG-ONT SAT 49 C FL 360 ,START SUCCESSFUL ON 2ND ATTEMPT.&NBSP;NOTED BY MX. THIS CLEARS DMI 118222. PLACARDS REMOVED. PERFORM APU BITE PROCEDURE IAW FIM 49-11 FT 958. NO FAULTS NOTED. MCC NOTIFIED.&NBSP;</P>)

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 86,256 hrs · 21,432 cycles

APU FAILED DURING START AND APU FAULT EICAS MESSAGE OCCURRED.&NBSP;(<P>PERFORMED BITE TEST ON APU CONTROLLER, NO FAULTS NOTED. STARTED APU ON FIRST ATTEMPT, NO EICAS MESSAGE PER AMM 49-11-00.</P>)

Part: PRESSURE SWITCH — FAULTY (FUEL SYSTEM) · airframe 86,246 hrs · 21,429 cycles

R FWD FUEL PUMP EICAS MESSAGE AFTER ROTATION. MESSAGE EXTINGUISHED AT APPROX 3,500 FEET. T/S RIGHT FWD FUEL PUMP EICAS MESSAGE IAW FIM 28-22 FT 819. REMOVED AND REPLACED RIGHT FWD FUEL PUMP PRESSURE SWITCH IAW AMM 28-42-01. OPS CHECK NORMAL, NO EICAS MESSAGE AT THIS TIME.

Part: PUMP — FAULTY (FUEL SYSTEM) · airframe 86,246 hrs · 21,429 cycles

FUEL CONFIG EICAS MSG AS A RESULT OF WRITE UP #1. AFTER ROTATION, APPROX 1, 800 LBS IMBALANCE. FUEL BALANCED WHEN PUMP TURNED BACK ON. DUE TO HISTORY, REMOVED AND REPLACED R FWD BOOST PUMP IAW AMM 28-22-03. OPS CHECK NORMAL AT THIS TIME, NO LEAKS NOTED.

Part: PRESSURE SWITCH — MALFUNCTIONED (FUEL SYSTEM) · airframe 86,180 hrs · 21,404 cycles

R FWD FUEL EICAS DURING DURING CLIMB. FUEL MIGRATION FROM R TO L FUEL TANK OF 3000 LBS. T/S EICAS R FWD FUEL PUMP MESSAGE PER FIM TASK 28-22 FT 819, SHEET 3, BOX #4. DEFERRED R FWD BOOST PUMP PER MEL 28-22-01. THIS OPENS MDDR 117781. MCC BOB NOTIFIED, ALL PLACARDS INSTALLED. LP 1076167 - M3: T/S IAW FIM 28-22 FT 819. REMOVED RT FWD FUEL PUMP PRESSURE SWITCH TO BLEED PRESSURE SENSE LINE PER FIM IAW AMM 28-42-01. REINSTALLED RT FWD FUEL PUMP PRESSURE SWITCH AND OPS CHECK GOOD. NO DEFECTS NOTED, MDDR 117781 CLOSED. PLACARDS REMOVED AND MCC NOTIFIED.`

Part: PIN — BACKED OUT (LIGHT CONNECTOR) · airframe 86,131 hrs · 21,386 cycles

EXTERIOR LOWER FUSELAGE EMERGENCY LIGHT INOP DURING TEST. FOUND PIN 1 PUSHED BACK AT CONNECTOR D6330P. RE-SECURED PER SWPM 20-60-06. OPS CHECK GOOD PER AMM 33-51-00.

Part: FITTING — LEAKING (NR 2 IDG) · airframe 86,131 hrs · 21,386 cycles

#2 ENGINE IDG SERVICING FITTING LEAKING. REMOVED AND REPLACED #2 ENGINE IDG SERVICING FITTING IAW AMM 24-11-00. LEAK CHECK GOOD.

Part: CONTROL PANEL — DEFECTIVE (COCKPIT) · airframe 86,131 hrs · 21,386 cycles

ON THE FIRE PNL HANDLE, FOUR SW LIGHTS: L ENG OVHT, ENG BTL 1 DISCH, ENG BOTTLE B DISCH, AND R ENG OVHT ASSY ARE NOT WORKING PROPERLY, STUCK AND STICKING. REMOVED AND REPLACED FIRE/OVERHEAT TEST PANEL IAW AMM 26-11-01, OPS CHECK NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PUMP) · airframe 86,010 hrs · 21,350 cycles

AFTER DEPARTURE, RECEIVED R FWD FUEL PUMP & FUEL IMBALANCE EICAS MSG. LEFT WING HAD 3,000 LBS LESS THEN RIGHT TANK, WE WERE GOING TO RUN QRH PROCEDURES THEN FUEL BALANCED OUT AND EICAS MESSAGES WENT AWAY. MONITORED FUEL IN BOTH MAIN TANKS FOR 4 HRS, NO UNWANTED FUEL TRANSFER NOTED. COMPLIED WITH FQI BITE PER FIM 28-41 FT 882, NO FAULTS NOTED. ACCOMPLISHED FUEL CONFIG MSG FIM 28-41 FT 884, NO FAULTS NOTED. ALL BOOST PUMPS OPS CHECK NORMAL PER AMM 28-22-00.

Part: RADAR — MALFUNCTIONED (WX SYSTEM) · airframe 85,928 hrs · 21,321 cycles

RIGHT WXR RADAR FAIL. OPS TEST GOOD IAW AMM 34-43-00. NO FAULTS FOUND AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PUMP) · airframe 85,884 hrs · 21,306 cycles

R FWD FUEL PUMP AND FUEL CONFIG LIGHT EICAS CAME ON DURING CLIMB OUT. LEFT FUEL QUANTITY INDICATION ROSE APPROXIMATELY 3000 LBS FOR 2-3 MIN, THEN RETURNED TO NORMAL PERFORMED FQIS BITE PROCEDURE, NO PRESENT LEG FAULTS. FUEL QTY INDICATING SYSTEM OPS CK NORMAL. OK FOR SERVICE IAW B767 FIM 28-41-00.

Part: SOFTWARE — DEFECTIVE (COCKPIT) · airframe 85,783 hrs · 21,269 cycles

FO SIDE TERRAIN INOP. FO SIDE WX RADAR ALSO REQUIRES WX RADAR TO BE PUSHED MULTIPLE TIMES.&NBSP;&NBSP;(<P>TRANSFERRED TO MDDR 114890 PER MEL 34-22-05B.</P><P>LP 1053563 - ITEM 1:&NBSP;VERIFIED SYMBOL GENERATOR ISOLATION IAW AMM 34-22-05B VERIFY EACH FLIGHT DAY. DMI 114890 REMAINS OPEN FOR FO'S TERRAIN: WEATHER SWITCHES.</P><P>LP 1086165 - ITEM 1:&NBSP;PERFORMED SYS GEN SOFTWARE UPDATE IAW AMM 34-22-00. OPS CHECK GOOD. WX RADAR TERRAIN ON F.O.'S SIDE OPS CHECK GOOD. THIS CLEARS DMI 114890. PLACARD REMOVED AND MCC NOTIFIED.&NBSP;</P>)

Part: ECU — MALFUNCTIONED (APU) · airframe 85,783 hrs · 21,269 cycles

APU SLOW TO START AND FAILED TO START. (<P>REMOVED AND REPLACED APU ECU WITH NEW. OPS CHECK GOOD. REF AMM 49-61-05<BR /></P>)

Part: WARNING SWITCH — FAULTY (MASTER CAUTION) · airframe 85,744 hrs · 21,253 cycles

NO AURAL WARNING BELL AND MASTER CAUTION LIGHT WHEN DOING WHEEL WELL ENG APU CARGO FIRE OVHT TESTS(<P><SPAN>REPLACED / CA MASTER CATION WARNING SWITCH IAW SWPM 20-84-18 PERFORMED FIRE OVHT TEST IAW AMM 26-17-00 PS TEST GOOD</SPAN><BR /></P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 85,744 hrs · 21,253 cycles

ON DEPARTURE AMBER EICAS RT FWD FUEL PUMP&NBSP;(<P>PERFORMED OPS CHECK OF RT FWD FUEL PUMP&NBSP; IAW AMM 28-22-00 OPS CHECK GOOD NO DEFECT NOTED</P>)

Part: CONTROL PANEL — FAILED (WX RADAR SYS) · airframe 85,626 hrs · 21,210 cycles

WX FAILED HSI MESSAGE, USING RT WX SYSTEM. REMOVED AND REPLACED WX CTRL PANEL IAW AMM 34-43-02, OPS CHECK GOOD.

Part: TRANSCEIVER — INOPERATIVE (WEATHER SYS) · airframe 85,539 hrs · 21,188 cycles

RIGHT WEATHER RADAR INOP LEFT RADAR OPERATES NORMAL(<P>TROUBLESHOT PER FIM 34-43 FT 805. SUSPECT FAULTY RH TRANSCEIVER. NO PARTS AVAILABLE. DEFERRED IAW MEL 34-43-01, CAT 'D', DUE 05OCT19, DMI #112842. MCC AND DISPATCH NOTIFIED. REMOVED AND REPLACED RIGHT WEATHER RADAR TRANSCEIVER IAW B767 AMM 34-43-01. OPS CHECK OK AT THIS TIME. MCC NOTIFIED.

Part: INDICATOR — UNKNOWN (ENG STANDBY) · airframe 85,505 hrs · 21,176 cycles

STDBY ENGINE INDICATOR BACKGROUND LIGHT INOP. REMOVED AND REPLACED STANDBY ENGINE INDICATOR IAW B767 AMM 77-41-01. OPS CHECKED GOOD.

Part: APU — MALFUNCTIONED · airframe 85,462 hrs · 21,161 cycles

APU TOOK 3 ATTEMPTS TO START. PERFORMED AUX POWER CONTROL UNIT BITE TEST. TEST PASS, NO FAULTS SHOWN. OPS NORMAL AS PER AMM 49-11-00.

Part: ACM — UNSERVICEABLE (AC BAY) · airframe 85,460 hrs · 21,160 cycles

LEFT PACK AIR CYCLE MACHINE WITH AIR LEAK AND HARDWARE MISSING. (<P>REMOVED AND REPLACED LEFT PACK AIR CYCLE MACHINE IAW AMM 21-51-03. OPS CHECK GOOD. NO LEAKS NOTED AT THIS TIME. </P><P><BR DATA-MCE-BOGUS="1" /></P><P>PACKING P/N: S9028T906</P><P>SEAL P/N: 460-400</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 85,428 hrs · 21,149 cycles

MAIN BATTERY CHARGER STATUS MESSAGE.(<P>T/S PER FIM 24-31 FT 804. NO FURTHER FAULTS NOTED AT THIS TIME.</P>)

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 85,411 hrs · 21,143 cycles

RIGHT RADAR UNABLE TO CONTROL PITCH ON THE GROUND. (<P>PERFORMED OPS CHECK OF RT WX RADAR SYSTEM IAW AMM 34-43-00. OPS CHECK NORMAL AT THIS TIME.</P>)

Part: PUMP — MALFUNCTIONED (FUEL SYSTEM) · airframe 85,367 hrs · 21,129 cycles

AFTER T/O AMBER ADVISORY MESSAGE, R FWD FUEL PUMP MESSAGE (CLEARED PASSING 7000). LP 1033533-3: AFTER T/O &AMP; AFTER RT FWD FUEL PUMP LOW PRESS, FUEL CONFIG WARNING, LEFT FUEL TANK INDICATED A 3000+ LB IMBALANCE. LP 1033534 - 3: 3000 LB IMBALANCE WITH L TANK SHOWING 9000 LB + RT TANK SHOWING 12.4, MADE LEFT TURN AND IMBALANCED DISAPPEARED AND FUEL CONFIG MSG CLEARED.&NBSP;(<P>REMOVED AND REPLACED RH FWD BOOST PUMP PER AMM 28-22-03. OPS CHECK GOOD AND LEAK CHECK GOOD.</P>)

Part: SMOKE DETECTOR — FAILED (MAIN DECK) · airframe 85,301 hrs · 21,110 cycles

NR 2 MAIN DECK SMOKE DETECTOR "A" FAILED ( AMBER LIGHT)&NBSP;(<P>TRANSFERRED TO MDDR 111153 CAT "C" AS PER MEL 26-16-02-01.&NBSP;</P><P>REF LOG PAGE 1065595 ITEM M4; REMOVED AND&NBSP;REPLACED THE NR 2 MAIN DECK DETECTOR IAW AMM 26-19-01. PERFORMED OPS CHECK GOOD AMBER LIGHT EXTINGUISHED, THIS CLEARS MDDR 111153&NBSP;</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 85,275 hrs · 21,102 cycles

R ENG ANTI-ICE VALVE LIGHT ON AFTER ENG SHUTDOWN WITH SWITCH OFF(<P>C/W OPS TEST IAW AMM 30-21-03. OPS TESTS GOOD</P>)

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 85,254 hrs · 21,095 cycles

R ENG FIRE LP 2 STATUS MSG.(<P>T/S PER AMM 26-11-00, NO FAULTS&NBSP; NOTED. NO MESSAGES AT THIS TIME C/W DVI, NO FAULTS DETECTED.&NBSP; DUE TO HISTORY, TRANSFERRED TO MDRR # 110870.&NBSP; PLACARD INSTALLED.&NBSP;</P><P>LP 1065574 - 5:&NBSP;INSPECTED FIRE LOOP, ENG NR 2 HARNESS AND CLAMPS FOR SHOT WIRES PER SWPM 20-10-06. NO DEFECTS NOTED. NR 2 ENG FIRE TEST GOOD PER FIM 26-11-00 TASK 804. MDDR 110870 STILL VALID.</P><P>LP 1065582 - M5:&NBSP;PERFORMED SWAP OF RT ENG FIRE LOOP CARDS M683 AND M684 PER WDM 26-11-21 SHEET 2. NO STS MSGS WERE ON THE EICAS. OPS CHECK OF THE FIRE LOOP SYSTEM TESTED OK. REF USED 26-21-00-705-001 MDDR OPEN FOR FURTHER TROUBLESHOOTING.</P><P>LP 1065583 - M2:&NBSP;PILOTS NOTED NO MSG'S DURING FLT. NO MSG'S CURRENTLY NOTED, DMI REMAINS OPEN.</P><P>LP 1065588 - M3:&NBSP;CREW REPORTS NO FURTHER MESSAGE FOR R ENG LP 2. THIS CLEARS DMI # 110870. DISPATCH AND MCC NOTIFIED.&NBSP;</P>)

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 85,259 hrs · 21,097 cycles

"R ENG FIRE LP 2" STATUS MESSAGE SHORTLY AFTER TAKEOFF. (<P><SPAN>PERFORMED VISUAL INSPECTION OF R ENG LP 2. NO DAMAGE NOTED IAW FIM 26-11 FAULT TREE 804 BLOCK 3.</SPAN><BR /></P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (NR 2 FIRE LOOP) · airframe 85,259 hrs · 21,097 cycles

STATUS R ENG FIRE LOOP 2 PERFORMED FIM 26-11 FT 804 PER BLOCK 103. C/W VISUAL INSPECTION OF ENG LOOP 2 AND BLEED DUCTS, NO LOOSE CONNECTIONS AND NO DAMAGE NOTED. OPS CHECK, NO FURTHER DEFECTS NOTED.

Part: STRUT — SEIZED (NR 2 ENGINE) · airframe 85,237 hrs · 21,089 cycles

FWD R/H COWLING FAN STRUT SEIZED ENG #2.(<P>REMOVED AND REPLACED FWD RH FAN COWLING STRUT PER AMM 71-11-11 CHECK NORMAL.</P>)

Part: BLOWER — INOPERATIVE (SMOKE DETECTION) · airframe 85,201 hrs · 21,077 cycles

LOWER FWD CARGO SMOKE DETECTION SYS INOPERATIVE. PERFORMED FIM 26-16 FAULT TREE 814. FOUND BLOWER 2 INOP. T/S PER FIM 26-16 FT 814 EICAS MSG CARGO DET AIR. REMOVED AND REPLACED AFT CARGO AIR DETECT PRESSURE SWITCH IAW AMM 26-16-03, OPS CHECK GOOD FOR SWITCH BUT SUSPECT FWD NR 1 BLOWER IS INOPERATIVE. TS PER SRM 26-16-01, VERIFIED FWD 1 BLOWER MOTOR IS SETTING POWER AND MOTOR DOES NOT RUN. REMOVED AND REPLACED AFT SMOKE DETECTOR BLOWER 1 IAW AMM 26-16-02. NO HELP. REMOVED AND REPLACED AFT SMOKE DETECTOR PLENUM PRESSURE SWITCH S4-55 IAW AMM 26-16-03. NO HELP. R & R BLOWER 1 FOR CARGO DET AIR IAW AMM 26-16-02.

Part: FIRE DETECTOR — FALSE INDICATION (RT ENGINE) · airframe 85,191 hrs · 21,073 cycles

RH ENG FIRE LOOP 1 STATUS MSG. REMOVED AND REPLACED LOWER AFT FIRE EDT ELEMENT ON # 2 ENG IAW AMM 26-11-02. OPS CHECK GOOD. R ENG FIRE LP 1 STS MSG, T/S PER AMM 26-11-00. NO FAULTS FOUND AT THIS TIME. C/W DVI, NO FAULT FOUND AT THIS TIME. PER NOTED HISTORY, SWAPPED AFOLTS CARDS M681. STATUS MESSAGE SWAPPED TO NR 1 ENG BUT NR 2 EMGINE MESSAGE STILL DISPLAYED. RETURNED CARDS TO ORIGINAL POSITIONS. R & R R ENG UPPER AFT FIRE DETECTOR LOOP IAW AMM 26-11-02. FIRE WARN TESTS OK, NO MSG.

Part: WINDOW — FAILED (COCKPIT) · airframe 85,197 hrs · 21,075 cycles

L FRONT WINDOW PANE SHATTERED IN FLIGHT.(<P>REMOVED AND REPLACED L1 WINDOW IAW AMM 56-11-01 STEPS 1 THRU 18 B. SEE LOG PAGE 1024159 ITEMS M7 AND M8&NBSP; FOR FINAL STEPS. </P><P>LP 1024159 - M7:&NBSP;PERFORMED SECOND TORQUE OF THE L1 WINDOW IAW AMM 56-11-01.&NBSP;SEE LOGPAGE 1024159 ITEM M8 FOR FINAL TORQUE. </P><P>LP 1024159 - M9:&NBSP;PERFORMED STEPS 23-39.&NBSP; INSTALLATION OF L1 WINDOW IS COMPLETE.&NBSP; OPS CHECK OF WINDOW HEAT ARE GOOD. REF 767 AMM 56-11-01.</P>)

Part: ESCAPE REEL — INOPERATIVE · airframe 85,180 hrs · 21,070 cycles

01 INERTIAL ESCAPE REELS INOP ( 6 OPERATIONAL).(<P>PLACED ON MDDR 110082 PER MEL 25-61-01-01.&NBSP;</P><P>LP 1024155 - M5:&NBSP;INSTALLED DESCENT DEVICE IAW AMM 25-61-05. NO FURTHER DEFECTS NOTED AT THIS TIME. THIS CLEARS DMI 110082 PLACARDS REMOVED.</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (RT ENG FIRE LOOP) · airframe 85,176 hrs · 21,068 cycles

R ENG FIRE LP 1 STATUS MSG.(<P>PERFORMED OPS CK OF RIGHT ENG FIRE LP 1 PER FIM TASK 26-11 FT 804. UNABLE TO DUPLICATE, NO FAULTS FOUND.<BR /></P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 85,010 hrs · 21,014 cycles

RIGHT FWD FUEL PRESS ADVISORY DURING INITIAL CLIMB.(<P><SPAN>PERFORMED OPS CHECK OF RT FWD FUEL PUMP IAW AMM 28-22-00. OPS CHECK GOOD AT THIS TIME.</SPAN></P>)

Part: PIN — NOT REPORTED (ACCELEROMETER) · airframe 84,998 hrs · 21,007 cycles

NR 2 ENGINE VIBE INDICATION INOP(<P>TRANSFER TO MDDR # 108505 IAW DDG 77-31-01-01 CAT C DUE DATE 21 MAR-19</P><P>LP 1015904-4: REPLACED N2 ACCELEROMETER CONNECTOR 3 PINS. OPS CHECK GOOD&NBSP;IAW SWDM 20-36-03.&NBSP;THIS ACTION CLOSES MDDR 108505, MCC NOTIFIED AND STICKERS REMOVED.<BR /></P>)

Part: STARTER — FAULTED (APU) · airframe 84,963 hrs · 20,993 cycles

APU FAULT AFTER LANDING AND ATTEMPTING TO START APU .(<P>TRANSFERRED TO MDDR # 108134 AS PER MEL 49-11-01A CAT C. REMOVED AND REPLACED STARTER MOTOR IAW AMM 49-41-01 OPS CKS NORMAL.</P>)

Part: COVER — UNSECURE (ESCAPE ROPE) · airframe 84,917 hrs · 20,982 cycles

F/O EMERGENCY ESCAPE ROPECOVER DOOR WILL NOT REMAIN CLOSED.(<P>RE-STOWED EMERGENCY ESCAPE ROPE IAW 25-60-00 DOOR NOW REMAINS CLOSED.<BR /></P>)

Part: PRESSURE SWITCH — DAMAGED (BOOST PUMP) · airframe 84,890 hrs · 20,975 cycles

RIGHT FWD BOOST PUMP PRESSURE SWITCH S72 AND CONNECTOR D01532 ARE SEIZED TOGETHER. REMOVED AND REPLACED THE BOOST PUMP PRESSURE SWITCH S72 AND CONNECTOR D01532 IAW WDM 28-42-1, AND AMM 28-42-01. PERFORMED SATISFACTORY OPS CHECK.

Part: BLADE — NICKED (NR 2 COMPRESSOR) · airframe 84,890 hrs · 20,975 cycles

NR 2 ENGINE LP COMPRESSOR ROTOR BLADE NR 20 HAS A NICK AT L/E CONTOUR. BLENDED THE NICK AND RAISED MATERIAL ON THE NR 2 FAN BLADE 20, MATERIAL LOSS AFTER REPAIR .028,MAX ALLOW .060, VERFIED CONDITION OF BLADE VIA NDT, BLADE FOUND TO BE SERVICEABLE, NO FURTHER ACTION REQUIRED IAW AMM 72-31-02.

Part: BLADE — NICKED (NR 2 ENGINE LPC) · airframe 84,890 hrs · 20,975 cycles

NR 2 ENGINE LP COMPRESSOR ROTOR BLADE NR 1 HAS A NICK AT L/E CONTOUR. INSPECTED AND FOUND TO BE .0003" IN DEPTH, MAX ALLOWABLE .060". NR 1 FAN BLADE FOUND TO BE IN LIMITS AND SERVICEABLE IAW AMM 72-31-02-226-019.

Part: ACTUATOR — MALFUNCTIONED (FUEL JETTISON) · airframe 84,890 hrs · 20,975 cycles

WHILE PERFORMING BOOST OVERRIDE ON A JETTISON PUMP TASK CARD, CHECK FAILED AT STEP C.3, LEFT JETTISON NOZZLE OPENED DURING CHECK. RESEATED THE LEFT JETTISON NOZZLE ACTUATOR IAW AMM 28-31-05, PEFORMED A GOOD OPS CHECK IAW AMM 28-31-00.)

Part: FUSE — FAILED (EXTERNAL POWER) · airframe 84,892 hrs · 20,976 cycles

EXTERNAL POWER INOPERATIVE. REMOVED AND REPLACED THE INTERLOCK FUSES AND PERFORMED AN OPS CHECK IAW AMM 24-41-00. THIS CLEARS MDDR #107609 PLACARD REMOVED,<BR /></P>)

Part: UNKNOWN — MALFUNCTIONED (ENGINE) · airframe 84,846 hrs · 20,956 cycles

STBY ENG INST. INOP(<P>PERFORMED BITE TEST.OPS TEST NORMAL IAW B767 AMM 77-41-00. PERFORMED ENGINE RUNS IAW B767 AMM 71-41-00-00, OPS CHECKS NORMAL IAW B767 AMM 71-41-00. DESCRIPTION AND OPERATION WHEN IN "ON" POSITION POWER IS SUPPLIED THRU ENGINES RUNNING OR EEC MAINT SWITCH "TEST".</P>)

Part: FAN — MALFUNCTIONED (E&E BAY) · airframe 84,785 hrs · 20,934 cycles

STATUS MESSAGE, "FWD EQ EXH FAN". REMOVED AND REPLACED FWD EQ EXH FAN IAW AMM 21-58-06. FAN OPS CHECK NORMAL.

Part: ESCAPE REEL — UNWANTED DEPLOY · airframe 84,780 hrs · 20,932 cycles

TWO ESCAPE REELS DEPLOY.(<P>INSTALLED 2EA DESCENT DEVICES IAW AMM 25-61-01 THIS ACTION CLEARS MDDR 106844 PLACARD REMOVED. INSTALLED SN 11554, 26272 PN 379103D-29<BR /></P>)

Part: ESCAPE REEL — INOPERATIVE · airframe 84,758 hrs · 20,924 cycles

ONE EACH INERTIAL ESCAPE REEL INOP. TRANSFERRED TO MDDR 106759.&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>REPLACED REEL DECENT DEVICE. THIS ACTION CLOSES MDDR 106759.</DIV>)

Part: IDG — FAILED (RT ENGINE) · airframe 84,728 hrs · 20,913 cycles

RIGHT IDG INOP.&NBSP;(<P>TRANSFER TO MDDR # 106390 IAW DDG 24-00-01-01- CAT B DUE DATE&NBSP; 28-JAN-19</P><P>LP 1040367-M3 REMOVED AND REPLACED RT IDG IAW AMM 24-11-01 PERFORMED OPS CHECK IAW AMM 24-11-00 OPS CHECK GOOD THIS CLEARED MDDR 106390.</P>)

Part: BUSS — MALFUNCTIONED (ELECTRICAL SYS) · airframe 84,718 hrs · 20,909 cycles

RIGHT A/C BUS FAILED INFLT DESCENDING BELOW 240&NBSP;(<P>PERFORMED OPS CHECK IAW AMM 24-22-00 OPS CHECK NORMAL AT THIS TIME NO FURTHER DEFECTS NOTED&NBSP;</P>)

Part: ESCAPE REEL — UNSECURE · airframe 84,722 hrs · 20,910 cycles

ESCAPE REEL FELL FROM HOUSING.(<P>TRANSFER TO DMI 106237 PER MEL 25-610-01-01. <BR /></P><P>INSTALLED NEW ESCAPE REEL IN POSITION B IAW AMM 25-61-00 THIS CLOSES DMI 106237<BR /></P><P>REMOVED PART WAS REMOVED AT THE TIME OF OCCURRENCE. THERE IS NO OFF UNIT RECORDED.<BR /></P>)

Part: FAN — MALFUNCTIONED (E&E BAY) · airframe 84,650 hrs · 20,880 cycles

FWD EQ EXH FAN STATUS MESSAGE AFTER LANDING&NBSP;(<P>TRANSFERRED TO MDDR # 105939 AS PER MEL 21-58-04-02-01 CAT C&NBSP;</P><P>LP 1032286-M3: R/R FORWARD EQUIP EXHAUST FAN ASSEMBLY. OPS CHECK GOOD. STATUS MESSAGE EXTINGUISHED IAW AMM 21-58-06. THIS CLEARS DMI #105939.</P>)

Part: ESCAPE REEL — UNSECURE (CABIN) · airframe 84,621 hrs · 20,870 cycles

EMERGENCY ESCAPE DEVICE FELL FROM CEILING COMPARTMENT&NBSP;(<P>TRANSFERRED TO MDDR # 105800 AS PER MEL 25-61-01-01 CAT C.</P><P>LP 1047509-M3: INSTALLED&NBSP;NEW EMERGENCY&NBSP;DECENT DEVICE IAW AMM 25-61-05.&NBSP;THIS ACTION CLOSES DMI 105800, MCC NOTIFIED &AMP; PLACARDS REMOVED.</P>)

Part: ESCAPE REEL — UNWANTED DEPLOY · airframe 84,556 hrs · 20,849 cycles

INERTIA REEL DEPLOYED DURING TAKEOFF ROLL.(<P>REMOVED AND REPLACED INERTIA REEL AT POSITION B IAW AMM 25-61-01.</P>).

Part: ESCAPE REEL — UNWANTED DEPLOY (COCKPIT) · airframe 84,559 hrs · 20,850 cycles

01 EA INERTIAL ESCAPE REEL DEPLOYED IN THE COCKPIT - 06 REELS STILL AVAILABLE FOR USAGE(<P>TRANSFER TO DMI 105285 PER MEL 25-61-01-01 CAT C MBCB 10JAN19 MPCW PLACARD INSTALLED. </P><P>REMOVE AND REPLACED DESCENT DEVICE IAW AMM 25-61-00 THIS CLEARS MDDR 105285 PLACARD REMOVED.<BR DATA-MCE-BOGUS="1" /></P>).

Part: IGNITER — FAILED (APU) · airframe 84,498 hrs · 20,830 cycles

APU FAILED TO START&NBSP;(<P>REMOVED AND REPLACED APU EXCITER IAW 49-41-03 OPS CKD OK REMOVED AND REPLACED IGNITOR IAW AMM 49-41-02 OPS GOOD</P>)

Part: UNKNOWN — MALFUNCTIONED (SMOKE DETECTION) · airframe 84,437 hrs · 20,806 cycles

MAIN DECK SMOKE DET LOOP A INOP. PERFORMED TEST OF DETECTION SYSTEM IAW AMM 26-14-00, NO FURTHER DEFECTS NOTED.

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 84,402 hrs · 20,794 cycles

APU WILL NOT START. PERFORMED APU BITE PROCEDURE IAW AMM 49-11-00 F/T 815, NO FAULTS AT THIS TIME. APU OPS CHECK NORMAL IAW AMM 49-11-00.

Part: RELAY — MALFUNCTIONED · airframe 84,394 hrs · 20,792 cycles

FWD EQUIP EXHAUST FAN STATUS MESSAGE. REMOVED AND REPLACED CURRENT SENSOR RELAY IAW SWPM 20-81-00. OPS CHECK GOOD IAW FIM 21-58 FT 905, NO DEFECTS NOTED AT THIS TIME.

Part: UNKNOWN — MALFUNCTIONED (MAIN BATTERY) · airframe 84,394 hrs · 20,792 cycles

ON BATTERY PWR STBY PWR DID NOT WORK. PERFORMED STANDBY OPERATIONAL TEST IAW AMM 24-33-00 TEST OK AT THIS TIME.

Part: OIL SYSTEM — LOW (APU) · airframe 84,358 hrs · 20,785 cycles

APU WILL NOT START NO LIGHT OFF&NBSP;(<P>TRANSFERRED TO MDDR # 103645 AS PER MEL 49-11-01A CAT C&NBSP;</P><P>LOG PAGE 1016942 SERVICED APU OIL WITH 01 QT I.A.W AMM 12-13-04 , APU OPERATES NORMALLY AT THIS TIME AS PER AMM 49-11-00.

Part: SYMBOL GENERATOR — MALFUNCTIONED (RADAR SYSTEM) · airframe 84,330 hrs · 20,775 cycles

FOR WXR ON TERRAIN MUST BE SELECTED ON AND OFF SEVERAL TIMES BEFORE E(<P>LOADED NEW EFIS SYMBOL GENERATOR IAW AMM 34-22-00 OPS CKS GOOD&NBSP;</P>)

Part: RADAR — MALFUNCTIONED · airframe 84,330 hrs · 20,775 cycles

WX RADAR OR TERRAIN MUST BE SELECTED ON AND OFF SEVERAL TIMES BEFORE ENGAGING&NBSP;(<P>ACCOMPLISHED OPERATION CHECK OF WXR AND TERR IAW AMM 34-43-00 AND AMM 34-46-01 OPS CHECK NORMAL&NBSP;</P>)

Part: ESCAPE ROPE — UNWANTED DEPLOY (NOT REPORTED) · airframe 84,308 hrs · 20,768 cycles

DESCENT DEVICE DEPLOYED ON LANDING(<P><SPAN>REMOVED / AND REPLACED DESCENT DEVICE IAW SPECIAL FREIGHTER MAINT MANUAL 25-61-03</SPAN></P>)

Part: CASE — CORRODED (NR 1 ENGINE FAN) · airframe 84,273 hrs · 20,757 cycles

CORROSION AROUND 3EA FASTENERS HOLES ON #1 ENG FAN CASE EXTERNAL SURFACE, LOCATED APPROX BETWEEN 7 AND 8 O CLOCK POSITION AND JUST BELOW THE ECU(<P>REMOVED CORROSION, EVALUATED AREA AND FOUND WITHIN LIMITS IAW GE CF6-80C2 ENGINE MANUAL 72-22-01. TREATED AND PRIMED.</P>)

Part: CONTROL VALVE — UNKNOWN · airframe 84,273 hrs · 20,757 cycles

REMOVE SURGE CONTROL VALVE AND INSTALL TROUBLESHOOTING SURGE CONTROL VALVE FOR TROUBLESHOOTING PURPOSES.(<P>REMOVED AND REPLACED APU SURGE CONTROL VALVE IAW B767 AMM 49-53-01. PERFORMED SATISFACTORY OPS AND LEAK CHECK, NO DEFECTS NOTED.</P>)

Part: STRAP — CORRODED (BS 1175) · airframe 84,273 hrs · 20,757 cycles

LH AFT WTB FAIRING STRUCTURE TO FUSELAGE STRAP BS 1175 CORRODED(<P>REMOVED CORROSION AT LH AFT WTB FAIRING STRUCTURE TO FUSELAGE STRAP BS 1175 FOUND WITHIN LIMITS IAW B767 SRM 53-00-71</P>)

Part: DOUBLER — CORRODED (FAN CASE) · airframe 84,273 hrs · 20,757 cycles

CORROSION AROUND DOUBLER AT 5 O'CLOCK POSITION IN FAN CASE ENG #1(<P>ACCOMPLISHED REPAIR ON ENG #1 FAN CASE AT 5 O'CLOCK POSITION IAW GE CF6-80C2 ENGINE MANUAL 72-22-01</P>)

Part: FAN — DAMAGED (E.E BAY) · airframe 84,273 hrs · 20,757 cycles

EQUIPMENT COOLING FAN SATURATED WITH OIL AND NICKS ON FAN BLADES(<P>REMOVED AND REPLACED EQUIPMENT COOLING FAN IAW AMM 2-58-06</P>)

Part: SEAL — LEAKING (DUCT COUPLING) · airframe 842,273 hrs · 20,757 cycles

LH AC PACK GROUND AIR SUPLLY&NBSP;DUCT COUPLING LEAKING AIR(<P>REMOVED AND REPLACED PERI SEALS AT LH FD CROSSOVER DUCT AND PERFORMED GOOD LEAK TEST IAW AMM 36-11-01</P>)

Part: DOUBLER — CORRODED (FAN CASE) · airframe 84,273 hrs · 20,757 cycles

CORROSION AROUND DOUBLER AT 7 O' CLOCK POSITION IN FAN CASE ENGINE #1(<P>ACCOMPLISHED REPAIR IN ENG #1 FAN CASE AT 7 O'CLOCK POSITION IAW GE CF6-80C2 ENGINE MANUAL 72-22-01.</P><P><BR DATA-MCE-BOGUS="1" /></P>)

Part: SMOKE DETECTOR — CLOGGED (FWD CARGO) · airframe 84,273 hrs · 20,757 cycles

FWD CARGO COMPARTMENT CEILING HAS CLOGGED SMOKE DETECTION AT BS 502 LBL 5(<P>CLEANED AND UNBLOCKED SMOKE DETECTI TUBE IAW BOEING SOPM 20-30-03</P>)

Part: HEAT SHIELD — TORN (NR 1 ENGINE) · airframe 84,273 hrs · 20,757 cycles

#1 ENG COOLING DUCT HEAT SHIELD SECTION IS TORN, APPROX 3 O CLOCK POSITION JUST AFT OF THE UPPER IGNITER PLUG.(<P>REMOVED AND REPLACED HEAT SHIELD INSULATION BLANKET ON #1 ENGINE DUCT AT 3 O' CLOCK POSITION IAW GE CF680C2 ESM 72-00-0</P>)

Part: SEAL — LEAKING (CROSSOVER DUCT) · airframe 84,273 hrs · 20,757 cycles

RH ECS BAY AFT LWR CROSSOVER DUCT O/B OF VALVE IS LEAKING(<P>REMOVED AND REPLACED RH ECS BAY AFT LOWER CROSSOVER DUCT SEALS IAW AMM 36-11-01, NO LEAK DETECTED.</P>)

Part: DOUBLER — CORRODED (FAN CASE) · airframe 84,273 hrs · 20,757 cycles

CORROSION AROUND DOUBLER AT 6 O' CLOCK PSOTION&NBSP;IN FAN CASE #1 ENGINE(<P>ACCOMPLISHED REPEAIR&NBSP;ON ENGINE #1 FAN CASE AT 6 O' CLOCK POSITION IAW GE CF6-80C2 ENGINE MANUAL 72-22-01.</P>)

Part: SUPPORT BRACKET — CORRODED (RT WING) · airframe 84,273 hrs · 20,757 cycles

RH WING T/E SUPPORT BRACKET I/B OF #9 SPOILER HAS EXFOLIATING CORROSION(<P>UPON EVALUATION FOUND SUPPORT BRACKET OUT OF LIMITS DUE TO 100% MATERIAL LOSS, REPAIRED BRACKET IAW B767 SRM 51-70-12 DETAIL III</P>)

Part: STRAP — CORRODED (BS 1109) · airframe 84,273 hrs · 20,757 cycles

RT AFT WTB STRUCTURE FUSELAGE STRAP BS 1109 CORRODED 111-40(<P>REMOVED CORROSION AT RT AFT WTB STRUCTURE FUSELAGE STRAP BS 1109 FOUND WITHIN LIMITS IAW B767 SRM 53-0-71 AND SRM 51-10-02, TREATED, PRIMED, AND TOP COATED AREA IAW B767 SRM 51-20-01</P>)

Part: SENSE LINE — CHAFED (BLEED AIR DUCT) · airframe 84,273 hrs · 20,757 cycles

LH WING TO BODY AREA, BLEED AIR DUCT SENSE LINE RUBBING AGAINST AROUND STUD INSIDE ACCESS PANEL #193KL(<P>REMOVED AND REPLACED BLEED AIR SENSE LINE IAW AMM 20-10-09. PERFORMED LEAK CHECK, NO LEAKS NOTED IAW B767 AMM 36-11-00.</P>)

Part: STRAP — CORRODED (BS 1109) · airframe 84,273 hrs · 20,757 cycles

LH AFT WTB STRUCTURE FUSELAGE STRAP BS 1109 CORRODED.(<P>REMOVED CORROSION AT LH AFT WTB STRUCTURE FUSELAGE STRAP BS 1109 FOUND WITHIN LIMITS IAW B767 SRM 53-00-71</P>)

Part: NONE — NONE (NONE) · airframe 84,273 hrs · 20,757 cycles

EVIDENCE OF BIRD INGESTION ON ENG #1 INLET COWL AT 1230 POSITION (FACING ENG) AND OUTLET GUIDE VANE AT 1130 POSITION(<P>COMPLETED GVI #1 ENGINE NOSE COWL AND ENGINE INTAKE AND FOUND EVIDENCE OF BIRD STRIKE AT 1230 POSITION ON INLET COWL IAW B767 AMM 05-51-18. COMPLETED VISUAL CONDITION INSPECTION AND COMPLETED VISUAL INSPECTION ENGINE INTAKE AND EXHAUST AREAS FOUND NO DEFECTS IAW B767 AMM 72-00-00-206. NO EVIDENCE OF INGESTION TO THE CORE OF THE ENGINE NOTED.</P>)

Part: BLEED AIR SYS — FLUCTUATES (APU) · airframe 84,272 hrs · 20,756 cycles

LT ENG START DUCT PRESS FLUCTUATED 10-20 PSI MAX N2 OF 14, DISCONTINUED. START CROSSBLEED START ACCOMPLISHED NORMALLY. PERFORMED APU OPS TEST IAW AMM-49-11-00, NO FAULTS NOTED. OPS CHECK GOOD. UNABLE TO DUPLICATED CONDITION.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 84,272 hrs · 20,756 cycles

APU INOP. TRANSFER TO MDDR 101463 IAW MEL 49-11-01A CAT C DUE DATE 30-OCT-18.

Part: BLEED AIR SYS — LOW PRESSURE (APU) · airframe 84,272 hrs · 20,756 cycles

LOW APU BLEED PRESSURE DURING LEFT ENGINE START DISCONTINED START AND PERFORM A X BLEED START. UNABLE TO DUPLICATE CONDITION PERFORMED APU OPS TEST IAW AMM 49-11-00 OPS CHECK OK.

Part: NOT REPORTED — MALFUNCTIONED (WEATHER RADAR) · airframe 84,196 hrs · 20,729 cycles

FO RADAR DISPLAY TURNS OFF THE RADAR. PERFORMED WX RADAR OPERATIONAL TEST IAW AMM 34-43-00 & SYSTEM TEST IAW AMM 34-43-00. OPS CHECKED GOOD. NO DEFECTS NOTED AT THIS TIME.

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 84,172 hrs · 20,721 cycles

F/O MFD DOES NOT DEPICT WEATHER WHEN SELECTED NOR TERRAIN WHEN SELECTED. PERFORMED OPERATION TEST ON F/O WEATHER RADAR IAW AMM 34-43-00. OPS CHECK NORMAL, NO DEFECTS AT THIS TIME.

Part: IRU — OUT OF ALIGNMENT (COCKPIT) · airframe 84,178 hrs · 20,723 cycles

FO'S WXR AND TERR SELECT SWITCHES INTERMITTENLY DONT FUNCTION WHEN NEEDED. ALIGNED IRU'S AND CYCLED THROUGH CAPT AND FO'S WX AND TERR SWITCHED SEVERAL TIMES IN BOTH TEST AND WX POSITION. OPS CHECKED OK IAW AMM 34-43-00.

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 84,164 hrs · 20,718 cycles

APU INOP. PERFORMED APU RUN THREE TIMES AND PUT LOAD ON IAW AMM 49-11-01, DUCT PRESSURE 30 PSI PERFORMED BITE IAW FIM 49-11 F/T 958. NO DEFECTS NOTED AT THIS TIME.

Part: ECU — MALFUNCTIONED (APU) · airframe 84,196 hrs · 20,729 cycles

APU INOP. REPLACED ECU PER AMM 49-61-05 OPS CHECKS GOOD. TESTED APU, CYCLED APU BLEED VALVE 4 TIMES, OPS CHECKED GOOD.

Part: CONNECTOR — CONTAMINATED (FUEL PUMP) · airframe 84,150 hrs · 20,714 cycles

CTR L FUEL PUMP MSG DISPLAYED AFTER ENG START, LEFT C PUMP DISPLAYED PRESSURE LIGHT. PERFORMED VOLTAGE CHECK AT LT CENTER FUEL PUMP AT PINS 2,4,6, 115VOLTS AC PERFORMED VOLTAGE CHECK AT LT FUEL OVRD PUMP CONT RELAY AT PINS A2,B,C2 115 VOLTS AC NOTED, THEN ALSO CHECKED VOLTAGE AT PINS X1 AND X2 28 VOLTS NOTED. THEN CHECKED VOLTAGE COMING OUT AT PINS A1,B1,C1 115 VOLTS AC NOTED. FOUND CONNECTOR ON LT CENTER FUEL PUMP CONTAMINATED. CLEANED CONNECTOR IAW SWPM 20-60-01 PERFORMED OPS CHECK OF LT CENTER FUEL PUMP IAW AMM 28-31-0, OPS CHECK GOOD. VOLTAGE CHECK IAW WDM 28-22-12 SHEET 1.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 84,135 hrs · 20,708 cycles

STATUS MSG AFT EQ EXH FAN 2. COMPLIED WITH SYSTEM TEST IAW AMM 21-58-41 CHECKS GOOD, ERASED STATUS MSG PER AMM 31-41-00.

Part: CLAMP — OUT OF POSITION (APU) · airframe 84,140 hrs · 20,711 cycles

APU BLEED PRESS LOW. TROUBLE SHOOT PER FIM 49-11 FT 979, FOUND EXCESSIVE AMOUNT OF BLEED AIR LEAKING FROM SURGE VALVE. REPOSITIONED AND SECURED CLAMPS, OPS CHECK GOOD.

Part: O-RING — DAMAGED (APU) · airframe 84,097 hrs · 20,695 cycles

APU OIL QTY TRANSMITTER LEAKING. REMOVED AND REPLACED OIL QTY TRANSMITTER O RING, NO LEAKS NOTED IAW AMM 49-94-04.

Part: PRESSURE SWITCH — LEAKING (FUEL SYSTEM) · airframe 84,097 hrs · 20,695 cycles

FUEL LEAK BY PRESSURE SWITCH LEFT FWD FUEL PUMP. REMOVED AND REPLACED LEFT PRESSURE SWITCH ON FWD FUEL PUMP IAW AMM 28-43-01.

Part: SENSOR — DIRTY (APU) · airframe 84,086 hrs · 20,690 cycles

APU INOP. CLEANED SENSOR IAW AMM 49-53-08. PERFORMED SUPPLY PRESSURE INDICATING SYSTEM. OPERATIONAL CHECK GOOD AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 83,995 hrs · 20,653 cycles

STATUS MSG AFT EQ EXH FAN 2. MSG CLEARED AND AFT EQ EXH FANS TEST OK PER AMM 21-26-01.

Part: MODULE — MALFUNCTIONED (APU) · airframe 83,955 hrs · 20,640 cycles

APU AUTO SHUT DOWN. REMOVED AND REPLACED FLOW SENSING MODULE IAW AMM 49-33-03. OPS CHECK GOOD.

Part: MODULE — FAULTY (APU) · airframe 83,944 hrs · 20,637 cycles

APU NO DUCT PRESSURE. PERFORMED BITE CHECK IAW FIM 49-11 FT 975. FAULTY PT SENSOR, REMOVED AND REPLACED FLOW SENSING MODULE IAW AMM 49-53-00. OPS CHECK GOOD, NO FAULTS NOTED.

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 83,850 hrs · 20,602 cycles

ON DEPARTURE WX TERR WOULD NOT DISPLAY EITHER SIDE BOTH CAPT AND F/O RECYCLED AISLE STAND AND FWD PANEL SWITCHES APPROX 6 TIMES EACH ,THEN WX TERR AND TERR WAS DISPLAYED. PERFORMED WXR BITE PROCEDURES IAW FIM 34-43-FT 805. OPS CHECK NORMAL WXR SWITCH ON THE LEFT AND RIGHT EFIS CONTROL PANEL ON ON PAINTING IS DOUBLE PUSH TO SELECT.

Part: WINDOW — SPARKS (COCKPIT) · airframe 83,822 hrs · 20,591 cycles

DURING FLIGHT ENCOUNTERED ST ELMOS STATIC SPARKS ON FO WINDOW. WINDOW INSP AND OPS CK GOOD PER AMM 56-11-02.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 83,796 hrs · 20,582 cycles

LEFT BLEED OFF EICAS MESSAGE ON DESCENT. C/W TASK 36-10 FAULT TREE 836 BLEED AIR VALVE OFF LIGHT ILLUMINATED WITH SWITCH ON DUCT PRESSURE NORMAL. OPS CHECK GOOD.

Part: SENSOR — FAULTED (APU) · airframe 83,841 hrs · 20,598 cycles

AFTER APU START NO DUCT PRESS. CONFIRMED APU ISO VALVE OPEN AND PNEU ISO VALVE OPEN, PERFORMED BITE TEST ON APU ECU, FOUND P/T SENSOR FAULT ON LAST RUN, CLEARED. RESTART APU PNEUMATICS, OPS TEST NORMAL AS PER AMM 49-11-01.

Part: INDICATION SYS — MALFUNCTIONED (FUEL SYSTEM) · airframe 83,785 hrs · 20,579 cycles

EICAS MSG RT FWD FUEL PUMP WITH LEFT FUEL QTY INDICATING 2500 LOW ERRORS SELF CORRECTED AFTER 2 MINUTES. PERFORMED OPS CHECK OF FUEL BOOST PUMP IAW AMM 28-22-03. OPS CK NORMAL. PERFORMED BITE AND OPS CHECK OF FUEL QTY INDICATING SYSTEM NO FAULTS.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 83,771 hrs · 20,572 cycles

ON DEPARTURE FO WX RADAR INDICATED FAIL USING L SYSTEM, AFTER CYCLING WX SELECTOR, WX RADAR WORKED WITH NO FURTHER ISSUES. PERFORMED WXR BITE TEST IAW AMM 34-43-00.

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 83,771 hrs · 20,572 cycles

LEFT FWD FUEL PUMP AUTO FUNCTION INOP. PERFORMED OPS CHECK FUNCTION IAW AMM 28-25-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 83,760 hrs · 20,568 cycles

STATUS MESSAGE CABIN ALT AUTO 2 AND CABIN ALT AUTO 1 AFTER LANDING. PERFORMED FIM TASK 21-31 FAULT TREE 803, NO DEFECTS. OPS CK GOOD.

Part: MODULE — FAULTY (APU) · airframe 83,700 hrs · 20,547 cycles

APU AUTO SHUTDOWN AFTER BLOCKOUT. REMOVED AND REPLACED FLOW SENSING MODULE IAW AMM 49-53-08. PERFORMED OPS CHECK OF APU AND RAN NR 1 ENGINE IAW AMM 71-00-00. NO DEFECTS NOTED. ENGINE RUN PERFORMED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 83,569 hrs · 20,500 cycles

RT FWD FUEL PUMP EICAS MESSAGE DISPLAYED FOR APPROX 60 SECONDS DURING INITIAL CLIMB. OPS CK FUEL SYSTEM IAW AMM 28-21-00. OPS GOOD.

Part: MODULE — MALFUNCTIONED (APU) · airframe 83,560 hrs · 20,497 cycles

APU AUTO SHUTDOWN AFTER BLOCK OUT. REMOVED AND REPLACED FLOW SENSING MODULE IAW AMM 49-53-08. PERFORMED OPS CHECK OF APU AND RAN NR 1 ENGINE IAW AMM 71-00-00. NO DEFECTS NOTED. ENGINE RUN PERFORMED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 83,528 hrs · 20,485 cycles

RT FWD FUEL PUMP EICAS MSG FOR SEVERAL MINUTES AFTER TAKE OFF. PERFORMED OPS CHECK ON RIGHT FWD FUEL BOOST PUMP PER FIM 28-22, FAULT TREE 820. NO FAULTS FOUND AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 83,557 hrs · 20,494 cycles

RT FWD FUEL PUMP EICAS FOR SEVERAL MINUTES AFTER TAKE OFF. PERFORMED OPS CHECK ON RIGHT FWD FUEL BOOST PUMP IAW FIM 28-22 FT 820, NO FAULT FOUND AT THIS TIME.

Part: UNKNOWN — MALFUNCTIONED (APU BLEED AIR) · airframe 83,512 hrs · 20,480 cycles

ON ARRIVAL, APU BLEED AIR VALVE WOULD NOT OPEN- NO DUCT PRESSURE. RECYCLED APU SWITCHES, DUCT PRESSURE NORMAL, NO DEFECTS NOTED AT THIS TIME IAW AMM 49-11-00.

Part: FILTER — CLOGGED (APU) · airframe 83,504 hrs · 20,478 cycles

APU INOP. (DUE PNEUMATIC PRESS LOW). PERFORMED FIM 49-11 FT 979, FOUND DEBRIS IN LINE AND FILTER CLOGGED. R&R SURGE FILTER IAW AMM 49-53-06 OPS CHECK NORMAL.

Part: ECU — MALFUNCTIONED (APU) · airframe 83,460 hrs · 20,461 cycles

APU INOP. R&R APU ECU, PERFORMED APU BITE, NO DEFECTS NOTED AT THIS TIME AS PER AMM 49-61-05.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT A/C PACK) · airframe 83,352 hrs · 20,422 cycles

RIGHT A/C PACK TEMP MESSAGE AT FL 390, LIGHT EXTINGUISHES WITH SWITCH IN THE STBY N POSITION. OPS CHECKED THE RT PACK TEMP IAW AMM 21-60-00, NO DEFECTS NOTED. OPS CHECKED GOOD.

Part: CONTROL PANEL — MALFUNCTIONED (WX RADAR SYSTEM) · airframe 83,352 hrs · 20,422 cycles

WEATHER RADAR ON BOTH THE CAPTAIN`S, AND FIRST OFFICER`S SIDES MUST BE CYCLED ON AND OFF SEVERAL TIMES BEFORE IT TURNS ON. REMOVED AND REPLACED THE WEATHER RADAR CONTROL PANEL IAW AMM 34-43-02, OPS CHECKED GOOD.

Part: APU — UNKNOWN · airframe 83,332 hrs · 20,414 cycles

APU WILL NOT START. PERFORMED TWO APU STARTS IAW AMM 49-11-00, BOTH STARTS SUCCESSFUL ,

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 83,295 hrs · 20,403 cycles

WEATHER RADAR DOES NOT DISPLAY ON CAPTAINS MFD. PERFORMED OPERATIONAL CHECK ON WEATHER RADAR SYSTEM IAW AMM 34-43-00. OPS CHECK GOOD AT THIS TIME.

Part: FIRE DETECTOR — INOPERATIVE (MAIN CARGO) · airframe 83,251 hrs · 20,389 cycles

MAIN CARGO FIRE LOOP A DECTECTOR NR 4 INOPERATIVE. REPLACED THE FIRE DETECTOR IAW AMM 26-19-01. CHECKED GOOD.

Part: FIRE DETECTOR — FALSE ACTIVATION (MAIN CARGO) · airframe 83,208 hrs · 20,373 cycles

MAIN DECK FIRE DETECTOR LOOP A STATION 2 IS AMBER. PERFORMED AN OPS CHECK OF THE MAIN CARGO FIRE DETECT IAW AMM 26-11-01, NO ISSUES NOTED. OPS CHECKED GOOD,

Part: CONTROL PANEL — MALFUNCTIONED (FIRE TEST) · airframe 83,207 hrs · 20,372 cycles

DURING A TRANSIT CHECK, FOUND THE ENG/APU, CARGO TEST FIRE SWITCH STICKING, MASTER WARNING, CAUTION LIGHTS NOT WORKING. REMOVED & REPLACED THE FIRE - OVERHEAT TEST PANEL & THE FIRST OFFICER`S MASTER CAUTION WARNING SWITCH ASSY IAW SWPM 20-84-15, AMM 31-51-00, & AMM 26-11-01. OPS CHECKED GOOD.

Part: DISPLAY — MALFUNCTIONED (WEATHER RADAR) · airframe 83,039 hrs · 20,314 cycles

WEATHER RADAR DISPLAY HAS TENDENCY TO SPOKE AT ABOUT 3O DEGREES RIGHT IN BOTH LT & RT SYSTEMS. OPS CHECKED THE WEATHER RADAR DISPLAY IAW AMM 34-43-00 , UNABLE TO DUPLICATE SPOKE ISSUE , FUNCTIONAL TESTED OK.

Part: RADAR — MALFUNCTIONED (LT WX SYS) · airframe 83,021 hrs · 20,304 cycles

LEFT RADAR DOES NOT PAINT WEATHER. PERFORMED AN OPS CHECK IAW AMM 34-43-00.

Part: RADAR — MALFUNCTIONED (WX SYSTEM) · airframe 82,966 hrs · 20,284 cycles

FIRST OFFICER`S WEATHER RADAR WOULD NOT DISPLAY ON HSI. PERFORMED AN OPS TEST OF THE WEATHER RADAR SYSTEM , OPS CHECKED GOOD IAW AMM 34-43-00.

Part: CIRCUIT CARD — MALFUNCTIONED (EXHAUST FAN) · airframe 82,938 hrs · 20,274 cycles

AFT EQUIPMENT EXHAUST FAN NR 2 MESSAGE. RACKED THE NR 2 AFT EQUIPMENT EXHAUST FAN CONTROL CARD IAW FIM 21-26-808, OPS CHECKED GOOD. MESSAGE CLEARED.

Part: CIRCUIT CARD — FAILED (EXHAUST FAN) · airframe 82,943 hrs · 20,276 cycles

FWD EQUIPMENT EXHAUST FAN NR 2 STATUS MESSAGE. R & R THE EXHAUST FAN CIRCUIT CARD IAW AMM 20-10-01, OPS CHECKED GOOD.

Part: PUMP — FAILED (FUEL BOOST) · airframe 82,925 hrs · 20,270 cycles

EICAS RT AFT FUEL PUMP MESSAGE. REMOVED AND REPLACED RIGHT AFT BOOST PUMP ASSY IAW AMM 28-22-03. OPS CHECKED NORMAL IAW AMM 28-22-00.

Part: PRESSURE SWITCH — FAILED (FUEL SYSTEM) · airframe 82,929 hrs · 20,271 cycles

LEFT FWD FUEL PUMP EICAS MESSAGE. REMOVED AND REPLACED THE LT FWD PRESSURE SWITCH IAW AMM 28-42-01, LEAK AND OPS CHECKED GOOD.

Part: FAN — INOPERATIVE (E/E BAY) · airframe 82,919 hrs · 20,268 cycles

AFT EQUIPTMENT COOLING FAN INOPERATIVE IN AUTO. REMOVED AND REPLACED AFT EQUIPMENT COOLING FAN IAW AMM 21-26-01. OPS CHECKED GOOD.

Part: CIRCUIT BREAKER — TRIPPED (FUEL BOOST PUMP) · airframe 82,867 hrs · 20,249 cycles

THREE HOURS INTO FLIGHT, WITH 30K LBS OF FUEL IN THE RIGHT TANK, RT TANK AFT RIGHT FUEL PUMP CIRCUIT BREAKER TRIPPED. IAW FIM 28-22 F/T 820, NO SIGNS OF FUEL LEAKAGE OR ANY ELECTRICAL DAMAGED NOTED. IAW FIM 28-22 F/T 820, BLOCK 5, SHEET 3. PERFORMED A BOOST PUMP OPS CHECK. OPS CHECKED GOOD.

Part: WINDOW — DEFECTIVE (COCKPIT) · airframe 82,842 hrs · 20,237 cycles

NR 1 WINDOW F/O SIDE HAS MOISTURE AND ARCING. REMOVED AND REPLACED THE NR 1 WINDOW IAW AMM 56-11-01.

Part: AIR DUCT — TORN (APU) · airframe 82,842 hrs · 20,237 cycles

APU BLEED, SURGE AIR DUCT TORN. REMOVED AND REPLACED APU BLEED SURGE AIR DUCT IAW AMM 20-11-00.

Part: SENSOR — FAULTY (LT ENGINE) · airframe 82,842 hrs · 20,237 cycles

LEFT ENGINE FATS FAILED ASM CHECK. REMOVED AND REPLACED FAN AIR TEMP SENSOR. OPS CHECK AND LEAK CHECK NORMAL IAW 36-23-00, 36-11-17.

Part: WINDOW — DEFECTIVE (COCKPIT) · airframe 82,842 hrs · 20,237 cycles

NR 2 WINDOW LT SIDE HAS SIGNS OF MOISTURE ON BUS BAR. REMOVED AND REPLACED NR 2 WINDOW LT SIDE IAW AMM 56-11-02.

Part: SWITCH — CRACKED (WINDOW HEAT) · airframe 82,842 hrs · 20,237 cycles

WINDOW HEAT SW FACE CRACK LEFT SIDE AND FWD. REMOVED AND REPLACED LEFT SIDE WINDOW KORRY SWITCHES IAW AMM 30-40-00.

Part: UNKNOWN — DEFECTIVE (CABIN) · airframe 82,842 hrs · 20,237 cycles

DESCENT DEVICE EXTENDED. REMOVED AND REPLACED DESCENT DEVICE IAW AMM 25-61-03.

Part: UNKNOWN — DEFECTIVE (CABIN) · airframe 82,842 hrs · 20,237 cycles

DESCENT DEVICE EXTENDED. REMOVED AND REPLACED DESCENT DEVICE IAW AMM 25-61-03.

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PUMP) · airframe 82,808 hrs · 20,224 cycles

AT ROTATION & DURING INITIAL CLIMB THROUGH 10.000 FT, RT FWD FUEL PUMP EICAS MESSAGE, MESSAGE EXTINGUISHED AS QRH WAS STARTED, DID NOT PRESSURE INDICATION ON PUMP, AFTER ROTATION & DURING CLIMB, FUEL CONFIGURATION MESSAGE , LEFT TANK INDICATED 3000 LBS LESS THAN RIGHT , MESSAGE EXTINGUISHED AT SAME TIME RT FWD FUEL PUMP MESSAGE DID. PERFORMED FIM TASK 28-41 FT 854, FQIS BITE TESTED GOOD. NO FAULTS NOTED, PERFORMED OPERATIONAL TEST OF FWD RIGHT BOOST PUMP IAWAMM 28-22-00, NO FAULTS NOTED, NO CIRCUIT BREAKER TRIPPED.

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PUMP) · airframe 82,799 hrs · 20,221 cycles

RT FWD FUEL PUMP EICAS MESSAGE, OPS CHECKED AW AMM 28-42-0314-039. CHECKS GOOD</P>)

Part: MONITOR — MALFUNCTIONED (ENGINE) · airframe 82,774 hrs · 20,210 cycles

ENGINE VIBRATION INDICATING SYSTEM HAS FLUCTUATIONS FOR THE RT ENGINE. REMOVED AND REPLACED THE ENGINE VIBRATION MONITOR IAW AMM 77-31-03.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT AFT FUEL PUMP) · airframe 82,768 hrs · 20,208 cycles

RIGHT AFT FUEL PUMP EICAS MESSAGE, QRH PROCEDURE COMPLIED WITH. COMPLIED WITH FIM 28-22, FAULT TREE 819 NO DEFECTS NOTED. OK FOR SERVICE.

Part: TERMINAL — DAMAGED (BUSS TIE) · airframe 82,762 hrs · 20,206 cycles

RIGHT BUSS TIE CIRCUIT BREAKER DAMAGED. REMOVED & REPLACED THE CIRCUIT BREAKER. REMOVED & REPLACED THE L3 TERMINAL AT C904BTB IAW SWPM 20-30-11 & WDM 24-21-51. OPS CHECKED OK IAW AMM 24-22-03.

Part: SWITCH — MALFUNCTIONED (START VALVE) · airframe 82,612 hrs · 20,134 cycles

AFTER ENGINE SHUTDOWN, THE NR 2 ENGINE WAS STILL AT MOTORING SPEED. NOTICED START VALVE WAS STILL IN GROUND. NEVER GOT ANY INDICATION BY EICAS OR VALVE LIGHT ON BY START SWITCH. REMOVED AND REPLACED THE NR 2 ENGINE START SWITCH IAW AMM 80-11-51. PERFORMED A NR 2 ENGINE START PROCEDURES IAW AMM 80-11-00. NO FAULTS NOTED.

Part: HEATER — MALFUNCTIONED (R2 WINDOW) · airframe 82,604 hrs · 20,130 cycles

DURING THE FIRST OFFICER`S PRE-FLIGHT, THE R2 WINDOW HEAT WAS NOT WORKING, R2 WINDOW HEAT INOPERATIVE. IAW FIM 30-41-TR 801, OPS CHECKED IAW AMM 30-41-00.

Part: SIGN — DISLODGED (EMERGENCY LIGHTS) · airframe 82,567 hrs · 20,112 cycles

EMERGENCY EXIT SIGN AT L1 DOOR FELL DOWN OFF LINER.(<DIV>FOUND EXIT SIGN ATTACH BRACKET DISCONNECTED. RE-ATTACHED MOUNT BRACKET ON INSTALLED LIGHT ASSY AS PER AMM 33-51-01. OPS CHK OK</DIV>)

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PUMP) · airframe 82,537 hrs · 20,098 cycles

IN CRUISE RIGHT AFT FUEL PUMP EICAS MESSAGE DISPLAYED. RAN QRM AND SELECTED PUMP OFF. ALSO FOUND ITS CIRCUIT BRAKER POPPED&NBSP;(<P>RESETC/B AND RESET FUEL FLEC PANEL IAW B767 FIM 28-22-43 -828. NO DEFECTS NOTED. OPS CHECK GOOD&NBSP;</P>)

Part: LIGHT — DETACHED (L1 DOOR) · airframe 82,514 hrs · 20,088 cycles

L1 DOOR EMERGENCY EXIT LIGHT ASSEMBLY DETACHED&NBSP;FROM SIDE WALL&NBSP;(<P>RE-SECURED&NBSP; LIGHT ASSY AT C1 DOOR EMERGENCY EXIT OK FOR SERVICE&NBSP;</P>)

Part: DRIVE UNIT — FAILED (WX RADAR SYS) · airframe 82,498 hrs · 20,080 cycles

WX RADAR FAILED IN FLIGHT&NBSP;(<P>TRANSFERRRED TO MDDR 86734 PER MEL 34-43-01-02</P><P>LOGPAGE 924927 ITEM #6: REMOVED AND REPLACED DRIVE UNIT IAW 767 AMM 34-43-05 OPS CHECKS GOOD&NBSP; THIS CLEARS MDDR86734</P>)

Part: RELAY — INOPERATIVE (ENGINE VALVE) · airframe 82,430 hrs · 20,047 cycles

RIGHT ENGINE VALVE LIGHT FAILED TO ILLUMINATE WHEN RIGHT FUEL CONTROL SWITCH WAS SELECTED TO RUN. REPLACED THE RELAY K1252. OPS CHECKED GOOD.

Part: ECU — FAILED (APU) · airframe 82,401 hrs · 20,033 cycles

APU INOPERATIVE. REMOVED AND REPLACED APU ECU IAW AMM 49-11-01A. OPS CHECKED GOOD.

Part: SWITCH — FAILED (FUEL VALVE) · airframe 82,366 hrs · 20,016 cycles

RIGHT ENGINE FUEL VALVE LIGHT FAILED TO ILLUMINATE WHEN RIGHT FUEL CONTROL SWITCH WAS SELECTED TO RUN. RIGHT ENGINE FUEL VALVE INDICATION INOPERATIVE. REPLACED THE LAMP & INDICATING SWITCH. PERFORMED AN INDICATOR LIGHT TEST, OPS CHECKED GOOD IAW AMM 33-13-00.

Part: CONTROL PANEL — INOPERATIVE (FIRE DETECTION) · airframe 82,360 hrs · 20,013 cycles

FIRE DETECTION CONTROL PANEL BACKGROUND LIGHTING INOPERATIVE. REMOVED AND REPLACED FIRE OVERHEAT TEST PANEL IAW AMM 26-11-01. OPS CHECKED NORMAL.

Part: WARNING LIGHT — FALSE ACTIVATION (BOOST PUMP) · airframe 82,329 hrs · 20,001 cycles

ON DEPARTURE, RT FUEL BOOST PUMP LOW PRESSURE LIGHT ILLUMINATED. EICAS MESSAGE CAME ON. EXTINGUISH AFTER APPROX 2 MINUTES. PERFORMED EICAS BITE IAW FIM 31-41-00/101, SYSTEM OK.

Part: CONTROL VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 82,270 hrs · 19,978 cycles

PRVC LT ENGINE INOP. REMOVED AND REPLACED LT ENGINE PRVC VALVE PER AMM 36-11-18.

Part: WIRE — BURNED · airframe 82,270 hrs · 19,978 cycles

WIRE W1050-99-22 BURN FROM K547, PIN 8 TO DC396J PIN 8 FOUND DURING APU INLET DOOR MOD. REPAIRED WIRE W1050-99-22 IAW SWPM 20-10-13.

Part: SEAL — DAMAGED (AC PACK) · airframe 82,270 hrs · 19,978 cycles

RT PACK HAS A WATER LEAK AT THE ACM OUTLET COUPLING. REMOVED AND REPLACED SEALS AT THE ACM OUTLET COUPLING IAW AMM 21-51-03. OPS CHECK NO LEAK FOUND.

Part: LIGHT — INOPERATIVE · airframe 82,270 hrs · 19,979 cycles

FUSELAGE EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED FUSELAGE EMERGENCY LIGHT IAW AMM 33-51-00.

Part: SENSOR — MALFUNCTIONED (CABIN TEMP) · airframe 82,241 hrs · 19,966 cycles

DURING PREFLIGHT, FOUND A FLIGHT DECK CAUTION MESSAGE ON EICAS. REMOVED & REPLACED THE DUCT AIR TEMP SENSOR IAW AMM 21-61-02, OPS NORMAL.

Part: SWITCH — DIRTY (WX RADAR SYS) · airframe 82,175 hrs · 19,947 cycles

CAPTAIN`S WEATHER RADAR SWITCH INTERMITTENT, TAKES MORE THAN ONE ATTEMPT TO TURN WEATHER RADAR ON. CLEANED THE WEATHER RADAR SWITCH IAW AMM 34-43-05, OPS CHECKED NORMAL.

Part: BLOWER — INOPERATIVE (SMOKE DETECTOR) · airframe 82,135 hrs · 19,935 cycles

MAINT MESSAGE AFT DETECTOR FAN. FOUND THE NR 1 AFT DETECTOR FAN INOPERATIVE. REMOVED & REPLACED THE SMOKE DETECTOR BLOWER IAW AMM 26-16-02. OPS CHECKED GOOD.

Part: SHUTOFF VALVE — INOPERATIVE (RT ENGINE) · airframe 82,098 hrs · 19,923 cycles

RIGHT ENGINE BLEED AIR OFF LIGHT INOPERATIVE. REMOVED AND REPLACED RIGHT ENGINE PRSOV IAW AMM 36-11-09, OPS AND LEAK CHECKED OK.

Part: MODULATING VALVE — MALFUNCTIONED (CABIN AIR) · airframe 82,094 hrs · 19,922 cycles

AFT CABIN TEMP MESSAGE. REMOVED AND REPLACED AFT TRIM AIR MODULATING VALVE IAW AMM 21-61-07 LEAK AND OPS CHECKED GOOD.

Part: BLOWER — FAILED (SMOKE DETECTOR) · airframe 82,077 hrs · 19,916 cycles

MAINTENANCE MESSAGE AFT DETECTOR FAN. REMOVED AND REPLACED THE NR 1 SYSTEM AFT CARGO SMOKE DETECTOR BLOWER IAW AMM 26-16-02, OPS CHECKED GOOD.

Part: CONTROL VALVE — FAILED (RT A/C PACK) · airframe 82,060 hrs · 19,910 cycles

DURING DESCENT AT ABOUT 13000 FT, AN EICAS FOR THE RT PACK TEMP, FOLLOWED QRH, AND MESSAGE WENT AWAY. CONTROLLER SELECTED TO N. REMOVED AND REPLACED THE RIGHT TEMP PACK CONTROL VALVE IAW AMM 21-51-12. OP CHECKED GOOD.

Part: SENSOR — FAILED (COCKPIT TEMP) · airframe 82,060 hrs · 19,910 cycles

FLT DECK TEMP CONTROLLER INOPERATIVE. BITE CHECKED AUTO CONTROLLER, FAILED FLT DECK TEMP SENSOR TS175, REMOVED AND REPLACED THE SENSOR IAW AMM 21-61-02, OPS CHECKED GOOD .

Part: ACM — MALFUNCTIONED (RIGHT) · airframe 82,044 hrs · 19,905 cycles

AFTER ENGINE START BUT BEFORE TAKEOFF, A RIGHT PACK TEMP EICAS ILLUMINATED. REMOVED AND REPLACED THE ACM IAW 21-51-03, OP CHECKED NORMAL.

Part: START VALVE — UNKNOWN (RT ENGINE) · airframe 81,911 hrs · 19,867 cycles

RIGHT ENGINE VALVE LIGHT DID NOT ILLUMINATED UPON ENGINE START.

Part: CIRCUIT BREAKER — TRIPPED (RT SPAR VALVE) · airframe 81,903 hrs · 19,865 cycles

RT ENGINE SPAR VALVE LIGHT STUCK ON. FOUND THE RT ENGINE FUEL VALVE BREAKER OUT, RESET, AND VALVE OPERATION NORMAL IAW AMM 28-22-11.

Part: SENSOR — FAULTY (AC BAY) · airframe 81,868 hrs · 19,856 cycles

RIGHT PACK TEMPERATURE EICAS MESSAGE WITH ASSOCIATED INOP LIGHT. PERFORMED PACK TEMP QRH PROCEDURE SELECTED STANDBY NORMAL. DEFERING RT PACK IAW DDG 21-51-01-01 MDDR 81837 PLACARD INSTALLED. REPLACED MIX MANIFOLD SENSOR OPS CKS GOOD IAW AMM 21-61-02. CLEARED MDDR.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 81,864 hrs · 19,855 cycles

HI FLOW INHIBIT STATUS MESSAGE. COMPLIED WITH FIM 21-51 FT 813, NO FAULTS ON PREVIOUS FLIGHT IAW FLIGHT CREW,

Part: CIRCUIT CARD — FAULTED (LT ENGINE SPEED) · airframe 81,836 hrs · 19,843 cycles

LEFT ENGINE SPEED CARD FAULTED. REMOVED AND REPLACED THE SPEED CARD IAW AMM 73-21-54. OPS CHECKED GOOD.

Part: WARNING LIGHT — ILLUMINATED · airframe 81,831 hrs · 19,841 cycles

AT 11,000 FT ,A3.0 PSI MAIN CARGO DOOR LIGHT & C/W QRH 1.17 AT 1,500 ON LANDING 0.4 PSI.

Part: RADAR — MALFUNCTIONED (WX SYSTEM) · airframe 81,836 hrs · 19,843 cycles

WEATHER RADAR TILT SEEMS OFF, HAD TO TILT OVER 5 DEGREES DOWN JUST TO GET GROUND. PERFORMED AN OPS CHECK, NO DEFECTS NOTED AT THIS TIME IAW AMM 34-43-00.

Part: SKIN — DENTED (NR 2 INLET) · airframe 81,847 hrs · 19,849 cycles

DENT FOUND ON NR 2 ENGINE. INLET COWL INNER SKIN AT THE 5 O'CLOCK POSITION. ACCOMPLISHED PART ONE, IAW EO 1971A149. REMOVED AND REPLACED THE NR 2 ENGINE INLET COWL IAW AMM 71-11-01.

Part: INDICATOR — INOPERATIVE (R2 WINDOW HEAT) · airframe 81,783 hrs · 19,823 cycles

R2 WINDOW HEAT SIDE SWITCH LIGHT INOPERATIVE IN THE ON POSITION.

Part: WARNING LIGHT — FALSE ACTIVATION (MAIN CARGO DOOR) · airframe 81,773 hrs · 19,818 cycles

AFTER TAKE OFF, PASSING 4000 FT, MAIN CARGO DOOR WARNING LIGHT ILLUMINATED. VERIFIED THE CARGO DOOR WAS CLOSED AND LOCKED IAW AMM.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 81,774 hrs · 19,819 cycles

AFT EQUIPMENT EXHAUST FAN NR 2 STATUS MESSAGE. TROUBLESHOT IAW FIM 21-26, FAULT TREE 808. MESSAGE CLEARED, OPS CHECKED OK.

Part: STARTER — INOPERATIVE (APU) · airframe 81,778 hrs · 19,821 cycles

APU WILL NOT START AFTER FLIGHT. REMOVED AND REPLACED THE APU STARTER IAW AMM 49-00-00.

Part: SKIN — DAMAGED (BS 137) · airframe 81,773 hrs · 19,818 cycles

FUSELAGE SKIN DAMAGED BOTTOM SIDE BS 137 AND RBL 10.5. ACCOMPLISHED A REPAIR IAW EO 6753A513, REV O, PART 1. NO CRACK INDICATIONS NOTED AT THIS TIME IAW NDT M PART 6-51-00-01.

Part: VALVE — UNSECURE (ENGINE) · airframe 81,774 hrs · 19,818 cycles

AFTER TAKE OFF, RECEIVED SIMUTIANOUS LT ENG OVERHEAT AND ENGINE FIRE, BOTH ON EICAS WITH MASTER WARNING AND AURAL WARNING. PERFORMED INSPECTION OF THE NR 1 ENGINE IAW MM 72-00-00. FOUND PLUG ON TCC VALVE LOOSE AND LEAKING OUT ONTO FIRE LOOP. SECURED THE LEAK AND CHECKED TCC VALVE, NO LEAKS NOTED IAW AMM 71-00-00. REPLACED THE LT OVERHEAT DETECTION WIRES IAW WD 26-11-12, & SWPM 20-10-11. PERFORMED LT ENGINE FIRE DETECTION OVERHEAT SYS TEST, TESTED OK IAW AMM 26-11-00.

Part: WARNING MESSAGE — ILLUMINATED (CARGO DOOR) · airframe 81,770 hrs · 19,815 cycles

MAIN CARGO DOOR MESSAGE CLIMBING THROUGH 14000'FT, ATB.

Part: VALVE — UNKNOWN · airframe 81,752 hrs · 19,810 cycles

COCKPIT TRIM VALVE INDICATION, BOTH DIGITAL IN ECS MAINTENANCES PAGE & MANUAL ON OVERHEAD PANEL. WHEN EVER IT CASSES THE 70 TOOLEDDS THE FULL CLOSE POS . IN START TO FLUCTUTE FROM CLOSE TO 0.70 WORKS OK. TEST FLIGHT(<DIV>COCKPIT TRIM AIR &NBSP;VALVE REPLACED &NBSP;IAW AMM 21-61-07 CHECKED &NBSP;FOR OPERATION FOUND OK</DIV>)

Part: WARNING LIGHT — FALSE ACTIVATION (FUEL SYSTEM) · airframe 81,752 hrs · 19,810 cycles

AFTER 30 MINUTES OF FLIGHT, THE RT FWD FUEL PRESSURE MESSAGE ILLUMINATED AND THE PRESSURE LIGHT IN BOTTON. TEST FLIGHT. PERFORMED TROUBLESHOOTING IAW FIM 28-22, FT819 FOUND K107 , AND THE RT FWD RELAY OPEN AND PERFORMED A RESET. PERFORMED FIM FIG 119 FT 831 SHEET 3 P-AGE 174 AND THE FAULT WAS NO PRESSENT.

Part: TUBE — DENTED (COOLING) · airframe 81,752 hrs · 19,810 cycles

FWD CARGO, LEFT SIDE EQUIPMENT COOLING TUBE DENTED. THE COOLING TUBE WAS REPLACED IAW MM 21-58-00.

Part: SEAL — TORN (NR 2 NACELLE) · airframe 81,752 hrs · 19,810 cycles

NR 2 ENGINE, RT FAN COWL HAS A TORN SEAL. THE FAN COWL ASSY WAS REPLACED IAW MM 71-11-04.

Part: SKIN — DENTED (NR 2 NACELLE) · airframe 81,752 hrs · 19,810 cycles

NR 2 ENGINE FAN COWLS HAVE DENTS IN SOME PLACES. DENTS FILLED WITH COMPOUND IAW MM 54-21-01 & REPAINTED IAW MM 51-21-10.

Part: RESTRAINT — DAMAGED (LT A/C PACK) · airframe 81,752 hrs · 19,810 cycles

LEFT PACK FLEXIBLE TIE RESTRAINT IS DAMAGED. LT PACK RESTRAINT TIE REPLACED IAW MM 21-51-00.

Part: BRACKET — LOOSE (NR 2 NACELLE) · airframe 81,752 hrs · 19,810 cycles

NR 2 ENGINE, CORE COWL AFTER LOWER TRIANGULAR BRACKET HAD FASTENERS LOOSE OR MISSING. BRACKET FASTENERS REPLACED IAW SRM 51-40-02.

Part: STRUCTURE — DELAMINATED (NR 2 NACELLE) · airframe 81,752 hrs · 19,810 cycles

NR 2 ENGINE, FAN COWL INNER SIDE IS DELAMINATED. REPLACED IAW MM 71-11-04.

Part: TUBE — CORRODED (APU DRAIN) · airframe 81,752 hrs · 19,810 cycles

APU DRAIN MAST TUBE CORRODED. THE DRAIN MAST TUBE WAS REPLACED IAW MM 49-16-00.

Part: GUARD — BROKEN (SWITCH) · airframe 81,752 hrs · 19,810 cycles

LEFT IDG DISCONNECT SWITCH GUARD BROKEN. THE SWITCH GUARD WAS REPLACED IAW SWPM 20-84-00.

Part: SUPPORT — CHAFED (NR 2 NACELLE) · airframe 81,752 hrs · 19,810 cycles

NR 2 ENGINE, LT FAN COWL AFT OPEN ROD SUPPORT CHAFED. THE SUPPORT WAS REPLACED IAW MM 71-11-11-201.

Part: BONDING — FAILED (CROSSFEED) · airframe 81,752 hrs · 19,810 cycles

FWD AND AFT ENGINE FUEL CROSSFEED HINGE BONDING RESISTANCE. FUEL CROSSFEED BONDING CLEANED, REINSTALLED CHECKED FOR OPERATION &AMP; FOUND OK PER MM 20-41-00</P>)

Part: BOLT — MISSING (NACELLES) · airframe 81,752 hrs · 19,810 cycles

NR 2 AND 1 ENGINES FAN COWLS SLING BOLTS MISSING. FAN COWLS MISSING SLING BOLTS REPLACED IAW MM 20-11-00.

Part: SKIN — SCRATCHED (NR 2 NACELLE) · airframe 81,752 hrs · 19,810 cycles

NR 2 ENGINE CORE COWLS SCRATCHED IN SOME PLACES. SCRATCHES SMOOTHED IAW MM 51-10-02, NDT CHECKED IAW D634T301, PART 651-00-10, FOUND WITHIN LIMITS PER SRM 54-42-01.</P>)

Part: SHUTOFF VALVE — NO TEST (NR 1 ENGINE) · airframe 81,752 hrs · 19,810 cycles

NR 1 ENGINE PRSOV FAILED TEST. THE PRSOV WAS REPLACED IAW MM 36-11-09.

Part: COUPLING — DAMAGED (FUEL LINES) · airframe 81,752 hrs · 19,810 cycles

FWD CARGO AT MIX BAY, FOUR COUPLING TUBES DAMAGED. THE COUPLING TUBES WERE REPLACED IAW MM 21-21-52.

Part: STRIP — BROKEN (NR 1 NACELLE) · airframe 81,752 hrs · 19,810 cycles

NR 1 ENGINE, INLET COWL AFT BULKHEAD WEARSTRIP BROKEN AT 6 O'CLOCK , AND 9 O'CLOCK POSITIONS. THE WEARSTRIP WAS REPLACED IAW MM 71-11-04.

Part: BONDING — DIRTY (JETTISON PUMP) · airframe 81,752 hrs · 19,810 cycles

OVERRIDE, JETTISON PUMPS AT RT WING TANK HAS RESISTANCE AT BONDINGS. THE BONDING WAS CLEANED AND REINSTALLED. CHECKED FOR OPERATION AND FOUND OK IAW MM 20-41-00.

Part: BOLT — CORRODED (ISOLATOR) · airframe 81,752 hrs · 19,810 cycles

APU ISOLATOR VIBRATION BOLTS CORRODED. VIBRATION BOLTS REPLACED IAW MM 49-11-01.

Part: SLEEVE — CORRODED (BOOST PUMP) · airframe 81,752 hrs · 19,810 cycles

RT AND LT BOOST PUMP SLEEVES ARE CORRODED. SLEEVES REPLACED IAW MM 28-22-05.

Part: KEELBEAM — CORRODED · airframe 81,752 hrs · 19,810 cycles

FUSELAGE KEEL BEAM LBL 9.50 AND RBL 9.50, FROM BS 676 TO 1307 AT ANCHOR NUTS ARE CORRODED.

Part: PDU — INOPERATIVE (AFT CARGO) · airframe 81,752 hrs · 19,810 cycles

AFT CARGO NR 6R PDU IS INOPERATIVE. THE PDU REPLACED IAW MM 25-53-01 CHECKED FOR OPERATION AND FOUND OK.

Part: BONDING — DIRTY · airframe 81,752 hrs · 19,810 cycles

ENGINE FUEL SHUTOFF VALVE ACTUATOR AT LT WING TANK, BONDING HIGH RESISTANCE. THE BONDING WAS REMOVED CLEANED REINSTALLED CHECKED AND FOUND OK IAW MM 20-41-00

Part: SEAL — TORN (NR 2 NACELLE) · airframe 81,752 hrs · 19,810 cycles

NR 2 ENGINE RT FAN COWL HAD A TORN SEAL. THE SEAL REPLACED IAW MM 71-11-04.

Part: SKIN — DENTED (NR 1 NACELLE) · airframe 81,752 hrs · 19,810 cycles

NR 1 ENGINE FAN COWLS HAVE DENTS IN SOME PLACES. THE DENTS WERE FILLED WITH COMPOUND IAW MM 54-21-01 & REPAINTED IAW MM 51-21-10.

Part: GASKET — MISSING (COOLING SYS) · airframe 81,752 hrs · 19,810 cycles

FWD CARGO BAY EQUIPMENT COOLING SYSTEM, 5 GASKETS ARE MISSING. NEW GASKETS INSTALLED IAW MM 21-58-00.

Part: BRACKET — LOOSE (NR 1 NACELLE) · airframe 81,752 hrs · 19,810 cycles

NR 1 ENGINE, LT CORE COWL HOLD OPEN BRACKET WORN. BRACKET FASTENERS REPLACED IAW MM 26-23-02.

Part: BUSHING — WORN (NR 2 NACELLE) · airframe 81,752 hrs · 19,810 cycles

NR 2 ENGINE, LT CORE COWL SUPPORT BOLT HAVE PLAY. THE BRACKET BUSHING & BOLTS REPLACED IAW AMM 71-11-11.

Part: CLAMP — CORRODED (APU BLEED DUCT) · airframe 81,752 hrs · 19,810 cycles

APU LT AIR SURGE BLEED DUCT CLAMPS ARE CORRODED. APU SURGE BLEED DUCT CLAMP REPLACED IAW MM 49-53-01.

Part: LATCH — CORRODED (NACELLE DOOR) · airframe 81,752 hrs · 19,810 cycles

NR 2 ENGINE, FAN COWL LATCHES CORRODED. THE LATCHES WERE CLEANED IAW MM 20-30-03.

Part: PACKING — TORN (A/C PACKS) · airframe 81,752 hrs · 19,810 cycles

LEFT AND RIGHT PACKS, FOUR PACKINGS ARE TORN THE PACKINGS WERE REPLACED IAW MM 21-51-08.

Part: FIRE LOOP — DAMAGED (NR 2) · airframe 81,752 hrs · 19,810 cycles

NR 2 ENGINE EICAS MESSAGE FOR THE NR 2 FIRE LOOP. THE FIRE LOOP WAS REPLACED IAW MM 26-11-01.

Part: RUB STRIP — LOOSE (NR 2 NACELLE) · airframe 81,752 hrs · 19,810 cycles

NR 2 ENGINE INLET COWL AFT BULKHEAD RUBSTRIP HAS RIVETS MISSING AT 6 O'CLOCK POSITION. REPLACED THE RIVETS IAW MM 71-11-04.

Part: DISPLAY — INOPERATIVE (A/C PACK) · airframe 81,752 hrs · 19,810 cycles

AIR CONDITIONING PANEL DISPLAY NOT READING. TEMP COMPARTMENT INDICATOR WAS REPLACED IAW MM 21-65-01-401-014.

Part: SKIN — SCRATCHED (NR 2 NACELLE) · airframe 81,752 hrs · 19,810 cycles

NR 2 ENGINE, RT CORE COWL SCRATCHED IN THE MIDDLE. SCRATCH SMOOTHED IAW SRM 51-10-02, NDT CHECKED IAW D634T301, PART 6 51-00-19, NO CRACKS FOUND. THICKNESS MEASURED IAW D 634T301, PART 4 51-00-10, & FOUND WITH IN LIMITS IAW SRM 54-42-01.

Part: BRACKET — CRACKED (NR 2 HPT) · airframe 81,752 hrs · 19,810 cycles

NR 2 ENGINE HPT COOLING TUBE AT 3 O'CLOCK POSITION ATTACHING BRACKET IS CRACKED. REPLACED THE BRACKET.

Part: BONDING — DIRTY · airframe 81,752 hrs · 19,810 cycles

OVERRIDE, JETTISON PUMP AT LT WING HIGH BONDING RESISTANCE. BONDING CLEANED &TREATED, CHECKED AND FOUND OK IAW MM 20-41-00.