N643GT

Part: INDICATOR — NONE · airframe 22,519 hrs

LEFT HYDRAULIC SYSTEM PRESSURE LOSS AFTER TAKEOFF.(<P>T/S SYS. FOUND DIFFERENTIAL PRESS. POPOUT IND. AT LEFT EDP CASE DRAIN MODULE SHEARED OFF. REMOVED AND REPLACED DIFF. POPOUT INDICATOR IAW AMM 29-11-17. LEAK CHECKS OK.</P>)

Part: COUPLER — NONE · airframe 22,399 hrs · 5,767 cycles

LEFT HF INOP.(<P>T/S PER FIM 23-11-00. REMOVED/REPLACED LH HF COMM ANTENNA COUPLER AMM 23-11-01. MDDR 156972 CLEARED UP.</P>)

Part: NONE — NONE · airframe 22,399 hrs · 5,767 cycles

AUTO SPEEDBRAKES INOP .(<P>T/S FIM 27-62-F/T 808. ADJUSTED S371 AUTO S/B ARM SW PER AMM 27-62-06.</P> / <P>AUTO S/B OPERATIONAL TEST OK AMM 27-62-00. MDDR 157119 CLEARED UP.</P>)

Part: LATCH — NONE · airframe 22,399 hrs · 5,767 cycles

ENG #1 INB SIDE T/R CAM LATCH DAMAGED.(<P>ENG #1 INB SIDE T/R CAM LATCH WAS REMOVED AND REPLACED IN ACCORDANCE WITH AMM TASK 78-31-02-404-010-H00. OPS CHECK OK.</P>)

Part: LATCH — NONE · airframe 22,399 hrs · 5,767 cycles

ENGINE #2 INBD REVERSER CAM LATCH IS DAMAGED.(<P>REMOVED &AMP; REPLACED #2 ENGINE I/B T/R CAM LATCH PER AMM 20-11-00, 78-31-01. NO DEFECTS NOTED.</P>)

Part: NONE — NONE · airframe 22,315 hrs

INFO ONLY RT ENG OIL LEVEL 11 QTS @ FL370. ON GRD 16 QTS.(<P>INFO NOTED BY MX. LT &AMP; RT ENGS SVC'D WITH 3 QTS EACH AMM 12-13-01 REFS. NIL EXT LKS NOTED IAW AMM 79-00-00.&NBSP; BOTH OK FOR SVC.</P>)

Part: NONE — NONE

EVIDENCE OF BIRD STRIKE ON #1 ENGINE INLET(<P>CLEANED AND PERFORMED BIRD STRIKE INSP TO #1 ENG INLET &AMP; SURROUNDING IAW B767 AMM 05-51-18. NO DEFECTS NOTED AT THIS TIME.</P> / <P>DATED 10NOV21 - LOG PAGE 1396057 - ITEM 16: COMPLIED WITH BORESCOPE INSPECTION OF #1 ENGINE COMPRESSOR STAGES 1 AND 12 IAW B767 AMM 72-00-00-01 REF FIM TASK 71-05 FT 872 BLOCK 11. FOUND TO BE WITHIN LIMITS.</P>)

Part: NONE — NONE

FWD CARGO BACKUP EICAS ON FINAL APPROACH.(<P>PERFORMED T/S PER FIM 21-61 FAULT TREE 804 REV 134. MSG CLEARED. OPS CHECK NORMAL.</P>)

Part: NONE — NONE

LEFT ENG OIL PRESSURE INTERMITTENTLY FLUCTUATES BETWEEN 28 AND 165 PSI. ALL OTHER OIL INDICATIONS NORMAL.(<P>CLEANED AND RESEATED #1 ENG OIL PRESS XMITTER PER AMM 79-33-00 REV 133. RUN #1 ENG PER AMM 71-00-00, NIL DEFFECT NOTED. AIRCRAFT OK FOR SERVICE.</P>)

Part: LATCH — NONE · airframe 21,714 hrs · 5,671 cycles

ENG #1 O/B SIDE C/DUCT LATCH RING BENT(<P><SPAN>REMOVED AND&NBSP; REPLACED&NBSP; #1 ENG&NBSP; O/B UUPER CAM LATCH&NBSP; REF&NBSP; M/M&NBSP; &NBSP;70-50-00</SPAN></P>)

Part: NONE — NONE · airframe 21,714 hrs · 5,671 cycles

#1 ENG THRUST REVERSERS INOP(<P><SPAN>REMOVED&NBSP; AND REPLACED&NBSP; &NBSP;#1&NBSP; ENG&NBSP; &NBSP;VALVE&NBSP; &NBSP;THRUST&NBSP; REVERSER&NBSP; IAW&NBSP; AMM&NBSP; 78-34-05&NBSP;</SPAN></P> / <P><SPAN>OPS&NBSP; CHECK&NBSP; AND&NBSP; LEAK&NBSP; OK</SPAN></P>)

Part: MASK — NONE · airframe 21,714 hrs · 5,671 cycles

COCKPIT PORTABLE OXYGEN FULL FACE MASK DUE TIME CHANGE P/N 10800C15F S/N TLS24986 MF 31 AUG 18(<P><SPAN>REMOVED &AMP;&NBSP; REPLACED&NBSP; PORTABLE&NBSP; OXYGEN&NBSP; FULL FACE&NBSP; MASK IN&NBSP; COCKPIT&NBSP; &NBSP;AS PER&NBSP; &NBSP;B767-300 FAMM&NBSP; 35-31-00</SPAN></P>)

Part: HARNESS — NONE · airframe 21,714 hrs · 5,671 cycles

ENG #1, EGT HARNESS ( LOWER ) DAMAGED(<P><SPAN>REMOVED&NBSP; AND&NBSP; REPLACED&NBSP; #1&NBSP; ENG&NBSP; EGT&NBSP; LOWER&NBSP; HARNESS&NBSP; AS PER&NBSP; AMM&NBSP; 77-21-02</SPAN></P> / <P><SPAN>ENG #1&NBSP; RUN UP&NBSP; TEST&NBSP; OK</SPAN></P> / <P><SPAN>EGT&NBSP; IND.&NBSP; NORMAL&NBSP; PER&NBSP; AMM&NBSP; &NBSP;71-00-00/501&NBSP; &NBSP; REV&NBSP; 133 &AMP;&NBSP; AMM&NBSP; 77-21-00-501&NBSP; &NBSP;REV&NBSP; 133</SPAN></P>)

Part: LATCH — NONE · airframe 21,714 hrs · 5,671 cycles

#2 ENG INBOARD LATCH RING BENT(<P><SPAN>REMOVED &AMP;&NBSP; REPLACED&NBSP; 32&NBSP; ENG&NBSP; INBOARD&NBSP; LATCH&NBSP; RING&NBSP; IAW&NBSP; B767-300&NBSP; &NBSP;AMM&NBSP; 78-31-01&NBSP; OPS&NBSP; CK&NBSP; NORMAL</SPAN></P> / <P><SPAN>IAW&NBSP; B767-300&NBSP; &NBSP;AMM&NBSP; &NBSP;78-31-02</SPAN></P>)

Part: PLUG — NONE · airframe 21,714 hrs · 5,671 cycles

ENG #1, BORESCOPE PLUG B-31 DAMAGED(<P><SPAN>REMOVED &AMP;&NBSP; REPLACED&NBSP; ENG #1&NBSP; B3-1&NBSP; PER&NBSP; AMM&NBSP; 72-00-00&NBSP; &NBSP;&AMP;&NBSP; W/C #&NBSP; &NBSP;A-72-308-00-01</SPAN></P>)

Part: ANTENNA — NONE · airframe 21,714 hrs · 5,671 cycles

ATC ANTENNA WORN OUT(<P><SPAN>REMOVED / REPLACED&NBSP; ATC&NBSP; ANTENNA&NBSP; M259&NBSP; &AMP;&NBSP; OPS&NBSP; &NBSP;CHECK&NBSP; OK&NBSP; &NBSP;AMM&NBSP; &NBSP;34-53-03&NBSP; REV&NBSP; 133</SPAN></P>)

Part: HARNESS — NONE · airframe 21,714 hrs · 5,671 cycles

ENG #1 CONDUIT OF ALTERNATE GEN DAMAGED(<P><SPAN>REPAIRED HARNESS&NBSP; CONDUIT 31&NBSP; ENG&NBSP; PER&NBSP; SWPM&NBSP; 20-10-13&NBSP; REV&NBSP; 77;&NBSP; &NBSP; EEC&NBSP; GEN&NBSP; ALT&NBSP; &NBSP;T1519&NBSP; &NBSP;CONNECTORES</SPAN></P> / <P><SPAN>ENG #1&NBSP; RUN UP&NBSP; TEST&NBSP; OK&NBSP; &NBSP; AMM&NBSP; &NBSP;71-00-00/501&NBSP; &NBSP;REV&NBSP; 133</SPAN></P>)

Part: MASK — NONE · airframe 21,714 hrs · 5,671 cycles

SUPERNUMERARY PORTABLE OXYGEN FULL FACE MASK DUE TIIME CHANGE P/N 10800C15F S/N TLS24972 MF 31 JUL 18(<P><SPAN>REMOVED &AMP;&NBSP; REPLACED&NBSP; PORTABLE&NBSP; OXYGEN&NBSP; FULL FACE&NBSP; MASK&NBSP; AS&NBSP; PER&NBSP; B767-300&NBSP; &NBSP; FAMM&NBSP; 35-31-00</SPAN></P>)

Part: ANTENNA — NONE · airframe 21,714 hrs · 5,671 cycles

DME ANTENNA WORN OUT(<P><SPAN>REMOVED/REPLACED&NBSP; DME&NBSP; ANTENNA&NBSP; M263&NBSP; &NBSP;&AMP;&NBSP; OPS&NBSP; CHECK&NBSP; OK&NBSP; PER&NBSP; AMM&NBSP; 34-55-02&NBSP; &NBSP;REV&NBSP; 133</SPAN></P>)

Part: ROD — NONE · airframe 21,714 hrs · 5,671 cycles

ENG #2, INBD CORE COWL HAS HOLD OPEN ROD BROKEN(<P><SPAN>REMOVED AND&NBSP; REPLACED&NBSP; #2&NBSP; &NBSP;I/B&NBSP; &NBSP;CORE&NBSP; COWL&NBSP; &NBSP;ROD.&NBSP; M/M&NBSP; REF&NBSP; 70-50-00</SPAN></P>)

Part: NONE — NONE · airframe 21,714 hrs · 5,671 cycles

ENG #1 HYDRAULIC PUMP WITH EVIDENCE OF LEAK(<P><SPAN>CLEANED&NBSP; AREA&NBSP; AS&NBSP; REQUIRED,&NBSP; TIGHTENED&NBSP; CASE&NBSP; DRAIN&NBSP; HOSE,&NBSP; SUPPLY&NBSP; HOSE AND&NBSP; PRESSURE HOSE&NBSP; ON&NBSP; ENGINE HYD.&NBSP; DRIVEN&NBSP; PUMP&NBSP; IAW&NBSP; AMM&NBSP; 29-11-05.&NBSP; &NBSP;PENDING&NBSP; LEAK&NBSP; CHECK</SPAN></P> / <P><SPAN>OPS&NBSP; CHECK&NBSP; AND&NBSP; LEAK&NBSP; CHECK&NBSP; MTX&NBSP; PROCEDURES&NBSP; &NBSP;TRANSFERED&NBSP; TO&NBSP; FORM&NBSP; #&NBSP; 8007</SPAN></P>)

Part: DUCT — NONE · airframe 21,714 hrs · 5,671 cycles

#2 ENGINE IDG PRECOOLER INLET FLEXIBLE DUCT HAS DAMAGES(<P STYLE="TEXT-ALIGN: JUSTIFY;"><SPAN>REMOVED AND REPLACED&NBSP; #2&NBSP; INLET&NBSP; FLEX DUCT&NBSP; PER&NBSP; M/M&NBSP; 70-50-00</SPAN></P> / <P STYLE="TEXT-ALIGN: JUSTIFY;"><SPAN>PERFORMED&NBSP; LEAK&NBSP; CHECK,&NBSP; NO LEAKS&NBSP; CHECK&NBSP; NOTED.</SPAN></P>)

Part: BUCKLE — NONE · airframe 21,714 hrs · 5,671 cycles

COCKPIT 1ST SUPERNUMERARY SEAT BELT BUCKLE DAMAGE(<P><SPAN>REMOVED AND&NBSP; REPLACED&NBSP; COCKPIT&NBSP; 1ST&NBSP; SUPERNUMERARY&NBSP; SEAT&NBSP; BELT&NBSP; BUCK&NBSP; AS PER&NBSP; 767&NBSP; AMM&NBSP; 25-11-00</SPAN></P>)

Part: ELT — NONE · airframe 21,714 hrs · 5,671 cycles

COCKPIT SUPERNUMERARY ELT AUTO RELEASE SEAL DAMAGE(<P><SPAN>REMOVED AND&NBSP; REPLACED&NBSP; ELT&NBSP; IN&NBSP; COCKPIT&NBSP; SUPERNUMERARY&NBSP; POSITION&NBSP; AS&NBSP; PER&NBSP; &NBSP;B767-300F</SPAN></P> / <P><SPAN>AMM&NBSP; &NBSP;25-63-03</SPAN></P>)

Part: HEADSET — NONE · airframe 21,714 hrs · 5,671 cycles

COCKPIT REMOVE AND REPLACE ALL COCKPIT HEADSETS PER EO 6723A209. HEADSETS DO NOT CONFORM(<P><SPAN>REMOVED/REPLACED&NBSP; 3EA&NBSP; CREW&NBSP; HEADSET&NBSP; &AMP;&NBSP; OPS&NBSP; CHECK&NBSP; &NBSP;INTERPHONE&NBSP; / COMM&NBSP; &NBSP;OK PER&NBSP; AMM 23-51-00 REV 133</SPAN></P>)

Part: DUCT — NONE · airframe 21,714 hrs · 5,671 cycles

#2 ENGINE IDG PRECOOLER INLET FLEXIBLE DUCT HAS ONE CLAMP BROKEN(<P><SPAN>REMOVED AND&NBSP; REPLACED&NBSP; #2&NBSP; IDG&NBSP; AIR CLAMP DUCT&NBSP; REF&NBSP; M/M&NBSP; &NBSP;70-50-00</SPAN></P>)

Part: IGNITION UNIT — INOPERATIVE (APU)

APU FAILS TO START WITH NO IGNITION HEARD.(<P>APU ECU BITE C/OUT. LRU FAULTY-IGN UNIT FAULTED. T/SHOOTING C/OUT IAW FIM 49-11 FAULT TREE A10. APU IGNITION UNIT REQ'S REPLACEMENT. NIL SPARES AVAILABLE. OPERATE IAW MEL 49-11-01A. HMG TEST SATIS IAW AMM 24-25-00-715-001. MDDR 153466 CAT C EXPIRES 23SEP21. DISP: JZ @1814Z.</P> / <P>LP&NBSP;<SPAN>1310994: </SPAN><SPAN>APU IGNITION UNIT REPLACED IAW AMM 49-41-03/401 REV 132 22DEC20. APU NOW SERVICEABLE. DMI 153466 CLOSED. MCC: JOL TIME: 2216Z&NBSP;</SPAN></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT GENERATOR)

AFTER ENGINE START L GEN OFF CAUTION MESSAGE. RAN QRH, MESSAGE CLEARED(<P>PERFORMED BPCU BITE CHECK IAW 767 AMM 24-22-00. NO DEFECTS NOTED. PERFORMED ENGINE IDLE RUNS IAW B767 AMM 71-00-00 OPS CHECK GOOD</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT GENERATOR)

AFTER ENGINE START R GEN OFF CAUTION MESSAGE. RAN QRH, MESSAGE CLEARED(<P>PERFORMED ECU BITE CHECK IAW 767 24-22-00 NO DEFECTS NOTED. PERFORMED ENGINE IDLE RUN IAW AMM 71-00-00 OPS CHECKS GOOD.&NBSP;</P>)

Part: TERMINAL — BROKEN (LT FIRE LOOP)

L ENG. FIRE LP1 ON STS(<P>TRANS TO MDDR 152552 IAW MEL 26-11-01-01 CAT C DUE 06SEP21 PLACARD INSTALLED.</P> / <P>REF L/P 1394939&NBSP; PERFORMED BITE TEST IAW TASK26-11-00-815-804 FOUND WIRE TERMINAL BROKEN. REPLACED WIRE TERMINAL LOOP TEST PASS. AND MESSAGE CLEARED. THIS CLEARS MDDR 152552.</P>)

Part: SENSOR — FAULTED (LT A/C PACK) · airframe 21,543 hrs · 5,642 cycles

DURING CLIMB RT PACK TEMP AND RT PACK OFF EICAS WITH ASSOCIATED RT PACK INOP LIGHT. W/O NO 85408 CARRIED OUT. RIGHT PACK AUTO COMPRESSOR OUTLET SENSOR REPLACED IAW AMM 21-51-06/401, REV 123, 22 DEC 2020. SYS SERVICEABLE.

Part: CONTROL VALVE — FAULTED (APU) · airframe 21,491 hrs · 5,624 cycles

APU FAULT, LOSS OF POWER UNDER LOAD. TRANSFERRED TO DMI 152168 PER MEL 49-11-10A. REMOVED AND REPLACED SURGE CONTROL VALVE IAW AMM 49-53-01 OPS CHECKS GOOD. THIS CLEARS DMI 152168. MCC NOTIFIED. PLAC REMOVED.

Part: A/C PACK — MALFUNCTIONED (LEFT)

LEFT PACK DOES NOT OPERATE AND DOES NOT SHOW "INOP" LIGHT(<P>TRANSFERED TO DMI 152143 PER DDG 21-51-01-01 CAT C 26AUG21.</P> / <P>21AUG: CVG MX, LP 1469068, ITEM M5: PERFORMED BITE TEST OF PACK TEMPERATURE CONTROLLER. NO FAULTS NOTED IAW AMM 21-51-00. THIS CLOSES DMI # 152143. MCC NOTIFIED. PLACARD REMOVED. T: 0753Z, I: DT.</P>)

Part: SHUTOFF VALVE — FAULTED (APU) · 5,607 cycles

APU BLEED FUNCTION INOP(<P>FND APU DUCT PRESSURE DROP TO ZERO DURING L ENG START. PER AMM&NBSP; 71-00-00 PRFORM BOTH ENGINE DRY MOTORING, CONDITION NORMAL WITH GROUND PNEUMATIC SOURCE. TRANSFERRED TO MDDR 151273 IAW MEL 49-11-01-01 CAT C.</P> / <P>LP&NBSP;<SPAN>1483980: </SPAN><SPAN>REMOVED AND REPLACED APU SUPPLY SOV THEN OPER CHECK OK PER AMM 36-11-10/401. THIS CLEARS MDDR 151273.</SPAN></P>)

Part: GCU — FAULTED (APU) · airframe 21,473 hrs · 5,615 cycles

APU ELEC INOP(<P>TRANSFERRED TO DMI 151562 IAW MEL 49-11-01A&NBSP; CAT C.</P> / <P>LP<SPAN>1483980:</SPAN><SPAN> RERACKED APU GCU AND OPER CHECKED OK PER AMM 24-22-08/401 &AMP; 49-11-00/501. THIS CLEARS MDDR 151562.</SPAN></P>)

Part: INDICATOR — FAULTED (TEMP CONTROL)

THE TEMP CONTROL VALVE INDICATOR ON THE OVERHEAD PANEL WILL NOT MOVE POSITION EITHER IN AUTO CONTROL OR IN MAN CONTROL(<P>FOUND F/D TEMP VALVE WORKS OK ON ECS PAGE, BUT TEMP PANEL IND INOP. DEFERRED TO MEL 21-65-01 PER MDDR #151055, CAT "C". INSTALLED PLACARD. NOTIFIED TO MCC. NEED P/N 15420A T/I: JZ 0637Z</P> / <P>LP 1317792 ITEM 4: REMOVED AND REPLACED TEMP POSITION VALVE INDICATOR, THEN OPS CHECKED OK PER 21-64-01/401. THIS CLEARED MDDR 151055, NOTIFIED MCC.</P>)

Part: SKIN — CORRODED (LT WING) · airframe 21,298 hrs · 5,535 cycles

CORROSION ON PREVIOUS REWORKS IN LH WING UPPER SKIN AT / PANEL NO. 1 BETWEEN WS460.2 (RIB 11) / WS486.2 (RIB 12) AT STRINGER U-12.5. NOTE: INTERGRANULAR CORROSION WAS DETECTED(<P>TRIMOUT ON LH WING UPPER SKIN WAS DONE TO REMOVE THE INTERGRANULAR CORROSION</P> / <P>AND DOUBLER REPAIR WAS INSTALLED</P>)

Part: NONE — NONE

LIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN BETWEEN STA 1197 AND 1197+22 AND STRINGERS S-11L & S-13L. DOUBLER WAS INSTALLED

Part: WING — CORRODED · corrosion level 2 · airframe 21,298 hrs · 5,535 cycles

CORROSION ON PREVIOUS REWORKS IN LH WING UPPER SKIN AT PANEL NO. 1 BETWEEN WS616.2 (RIB 17) AT STRINGER U-12.5. NOTE: INTERGRANULAR CORROSION WAS DETECTED(<P>TRIMOUT ON LH WING UPPER SKIN WAS DONE TO REMOVE THE INTERGRANULAR CORROSION</P> / <P>AND DOUBLER REPAIR WAS INSTALLED</P>)

Part: SHUTOFF VALVE — INOPERATIVE (RT ENGINE) · airframe 21,298 hrs · 5,535 cycles

RIGHT ENGINE HPSOV INOP ( HIGH PRESSURE SHUTOFF VALVE(HPSOV) SYSTEMS CF6-80C2 . C CHECK, LP 1311040, ITEM M3: REMOVED AND REPLACED RIGHT ENGINE INTERMEDIATE PRESSURE CHECK VALVE IAW 36-11-06-404-009-001. HPSOV ACTIVATED IAW 36-11-07-424-016-001. OPS CHECKED GOOD DURING ENGINE RUN.

Part: BOLT — MISSING (THRUST REVERSER) · airframe 21,068 hrs · 5,500 cycles

#1 ENGINE DURING T/R ELECTRO-MECH BRAKE TEST FOUND THE MANUAL DRIVE COVER ON CDU MANUAL PAD HELICOIL AND BOLT MISSING. FOUND JUST MISSING BOLT HELICOIL IS GOOD, INSTALLED NEW BOLT AT #1 ENG I/B T/REV PER AMM 20-11-00-910-802.

Part: WARNING MESSAGE — FALSE INDICATION · airframe 21,068 hrs · 5,500 cycles

FAULT: WARNING A LEFT (OR RIGHT) FAV CLOSED AND OPEN SWITCHES DISAGREE.(<P>PERFORMED TROUBLE SHOUTING IAW FIM 36-10. FAULT TREE 835. OP CHECK FOUND NORMAL.

Part: NONE — NONE · airframe 21,068 hrs · 5,500 cycles

COCKPIT PORTABLE OXYGEN FULL FACE MASK DUE TIME CHANGE MF JAN 12 P/N 10800C15F.(<P>REMOVED COCKPIT PORTABLE, OXYGEN FULL FACE MASK AS PER AMM 35-01-2-11. INSTALLED SERVICIABLE PORTABLE OXYGEN FULL FACE MASK AS PER AMM 35-01-2-11.

Part: OXYGEN MASK — MISSING (SPARE) · airframe 21,068 hrs · 5,500 cycles

LAV. SPARE OXYGEN MASK AND BAG MISSING MASK P/N 289-601-212 BAG P/N 801809-01.(<DIV>INSTALLED&NBSP; SPARE OXYGEN MASK&NBSP; AND&NBSP; BAG IN&NBSP; LAV&NBSP; AS PER&NBSP; &NBSP;B767-300&NBSP; &NBSP;AMM&NBSP; 35-01-211</DIV>)

Part: OXYGEN MASK — DAMAGED (CABIN) · airframe 21,068 hrs · 5,500 cycles

SUPERNUMERARY PORTABLE OXYGEN FULL FACE MASK LENS SCRATCHED VISION IMPAIRED.(<P><SPAN>REMOVED&NBSP; AND REPLACED SUPERNUMERARY&NBSP; PORTABLE OXYGEN&NBSP; FULL&NBSP; FACE MASK&NBSP; AS PER&NBSP; B767-300</SPAN></P><P><SPAN>AMM&NBSP; &NBSP;35-31-01</SPAN></P>)

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 21,068 hrs · 5,500 cycles

FAULT WARINING A LEFT (OR RIGHT) FAV VALVE CLOSED SIGNAL WAS NOT DETECTED.(<P>PERFORMED&NBSP; TROUBLESHOOTING&NBSP; IAW FIM&NBSP; 36-20&NBSP; &NBSP;FAULT LINE&NBSP; 8041. FOUND NORMAL AT THIS&NBSP; TIME</P>)

Part: SHUTOFF VALVE — FAULTED (LEFT) · airframe 21,068 hrs · 5,500 cycles

FAULT FAILURE LEFT (OR RIGHT) HPSOV CLOSED AND OPEN SWITCHES DISAGREE.(<P>PERFORMED&NBSP; FIM TASK&NBSP; 36-20&NBSP; &NBSP;TREE 804&NBSP; STEPS&NBSP; 1,2,3 AND&NBSP; 36.&NBSP; &NBSP;HPSOV&NBSP; FOUND&NBSP; FAULTING.</P><P><BR /></P><P>REMOVED&NBSP; AND&NBSP; REPLACED&NBSP; HPSOV&NBSP; IAW&NBSP; AMM&NBSP; 36-11-07,&NBSP; OPS&NBSP; CHECK&NBSP; OK</P>)

Part: NONE — NONE · airframe 21,068 hrs · 5,500 cycles

LAV PORTABLE OXYGEN MASK DUE TIME CHANGE MF JAN 13 P/N 289-601-212. REMOVED AND REPLACED LAV PORTABLE OXYGEN MASK AS PER AMM 35-31-01.

Part: OXYGEN MASK — MISSING (PORTABLE OXYGEN) · airframe 21,068 hrs · 5,500 cycles

SUPERNUMERARY PORTABLE OXYGEN FULL FACE MASK HOOD MISSING.(<P>INSTALLED&NBSP; MISSING&NBSP; FACE MASK HOOD&NBSP; AS PER&NBSP; &NBSP;B767-300&NBSP; &NBSP;AMM&NBSP; 35-31-01</P>)

Part: IDG — FAULTED (LT GENERATOR) · airframe 21,014 hrs · 5,492 cycles

L GEN EICAS ON T/O ROLL(<P>20 MAY 21 - LP 1311139 - ITEM # 1 - EMA - LEFT ENGINE IDG DISCONNECTED IAW DDG 24-00-01-01 CAT B. DMI # 147233.</P><P>20 MAY 21- LP 1325342 - ITEM # 7 - EMA - L GCU REPLACED BUT NO FZX. ORIGINAL UNIT REFITTED IAW AMM 24-22-02 REV 132. DMI 147233 REMAINS.</P><P>23MAY21 - LP 1325358 - ITEM # 2 - LEJ - REMOVED AND REPLACED LEFT IDG IAW AMM 24-11-01. PERFORMED ENG RUN IAW MM 71-00-00/201 FIG 3. LEFT IDG OPS AND LEAK CHKS OK. CLOSED MDDR# 147233. MCC NOTIFIED, PLACARD RMVD.</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (EQUIP EXHAUST) · airframe 20,967 hrs · 5,484 cycles

AFT EQUIPMENT EXHAUST FAN 2 STATUS MESSAGE.(<P>AFT EQUIP EXHAUST FAN 2 RESET IAW FIM 21-26 FAULT TREE 806, FOUND SERVICEABLE.</P>)

Part: CONTROLLER — FAULTED (SHUTOFF VALVE) · airframe 20,945 hrs · 5,481 cycles

EICAS MSG R ENG HPSOV IN FLIGHT, INVESTIGATION C/W IAW FIM 36-10 FAULT TREE 843, FAULT TRACED TO STICKY HPSOV, TRANSFER TO DMI 147169. HPSOV LOCKED OUT. MCC YC TIME 0123Z. FAULT TRACKED TO STICKY HPSOV. RT ENG HPSOV REPLACED IAW AMM 36-11-07-024-001 AND 36-11-07-024-016-001 (OFF PART: PN 802170-12, SN 200106160. AIR SUPPLY CONTROL SYS BITE TEST. FOUND SERVICABLE. NO FAULTS. LOG PAGE 1491387: R/H ENGINE HPSOV CONTROLLER REPLACED IAW AMM 36-11-08 PB 400. LEAK CHK C/O SATIS. AIR SUPPLY BITE SYSTEM TEST C/OUT IAW 36-23-00 PB 501, NIL FAULTS RECORDED.

Part: WARNING MESSAGE — FALSE INDICATION (BUSS) · airframe 20,712 hrs · 5,446 cycles

EICAS L AND R UTIL BUS OFF(<P>A/C ARRIVED WITH NO ISSUES. CREW RESET BOTH BUSES ON CLIMB SUCCESSFULLY. PERFORMED OPS CHECK OF BPCU IAW AMM 24-22-00. PS CHECK GOOD. NO MSG'S PRESENT.</P>)

Part: STATUS MESSAGE — FALSE INDICATION (PRV) · airframe 20,624 hrs · 5,432 cycles

R ENG. PRV STATUS MESSAGE(<P>ACCOMPLISHED GROUND TEST PER AMM 36-11-18. MSG CLEARED.<BR /></P>)

Part: GALLEY — ODOR (COCKPIT) · airframe 20,638 hrs · 5,434 cycles

FUMES IN COCKPIT COMING FROM GALLEY. RAN SMOKE, FIRE OR FUMES CHECKLIST. REMOVED POWER FROM GALLEY VIA PULLED C/B, FUMES/ SMOKE SMELL SLOWLY DISSIPATED (<P>UPON GALLEY INSPECTION, DISCOVERED CHARRED PAPER TOWEL CONTAINER(WRAPPED IN PAPER), LEANING AGAINST A GALLEY LIGHT(GALLEY LIGHT MISSING COVER). NO OTHER DEFECTS NOTED. IAW B767 AMM 05-51-56</P>).

Part: HOOK AND LOOP — PEELING (CAPTAIN'S EVAS) · airframe 20,638 hrs · 5,434 cycles

CAPT EVAS HOOK AND LOOP PEELING OFF(<P>REAPPLIED ADHESIVE IAW B767 AMM 20-30-01.</P>)

Part: CONTROL VALVE — FAULTED (LT A/C PACK) · airframe 20,491 hrs

EICAS MESSAGE L PACK OFF.(<P>REMOVED &AMP; REPLACED L/H PACK FLOW CONT REF AMM 21-61-01. OPS LEAK CK SAT.</P>)

Part: CONNECTOR — DIRTY (LT A/C PACK) · airframe 20,498 hrs

LEFT PACK REQUIRED PACK RESET TO ENERGIZE INITALLY(<P>RESET AND CLEANED PACK FLOW CONTROL CONNECTOR D00748. CLEANED L/H PACK FLOW CONTROL S/W. ALL CHECK NORMAL PER AMM 21-51-00</P>)

Part: CONTROLLER — FALSE ACTIVATION (RT A/C PACK TEMP) · airframe 20,456 hrs

R PACK TEMP EICAS MESSAGE IN FLIGHT(<P>PERFORMED FIM 21-51 TASK 876, FOUND RT TEMP CONTROLLER AT FAULT.&NBSP;<SPAN>REMOVED &AMP; REPLACED</SPAN><SPAN>&NBSP;RT TEMP CONTROLLER PER AMM 21-51-00-405-008-001. OPS CHK OK.</SPAN></P>)

Part: A/C PACK — MALFUNCTIONED (LEFT) · airframe 20,498 hrs

LEFT PACK OFF WOULD NOT RESET(<P>RESET LEFT PACK AND CYCLED APU BLEED SWITCH. OPS CHECK NORMAL IAW AMM21-51-00</P>)

Part: WARNING MESSAGE — FALSE INDICATION (RT A/C PACK TEMP) · airframe 20,456 hrs

R PACK TEMP EICAS(<P>RT TEMP. CONT FAIL LIGHT ON. RESET CONT &AMP; BITE TEST ACCOMPLISHED IAW AMM 21-51-11. RT PACK OPS CHECK NORMAL.<BR /></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (A/C PACK TEMP) · airframe 20,433 hrs · 5,401 cycles

RIGHT PACK TEMP EICAS(<P>RIGHT PACK TEMP CONTROLLER FAIL LIGHT ON. RESET CONT. &AMP; BITE TEST ACCOMP IAW AMM 21-51-14 - RT PACK OPS CHECK NORMAL.<BR /></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT A/C PACK TEMP) · airframe 20,433 hrs · 5,401 cycles

RIGHT TEMP PACK DURING TAXI(<P>RIGHT PACK TEMP CONTROLLER FAIL LT ON RESET C/OUT AND BITE TEST ACCOMPLISHED IAW AMM 21-51-14 OPERATIONAL TEST SATIS<BR /></P>)

Part: BLEED VALVE — FAULTED (APU) · airframe 20,383 hrs · 5,394 cycles

START VALVE LIGHT REMAINS ON BLEED AIR DROPS AND ENGINE N2 STOPS AT 14%.(<P>DEFERRED TO MEL 49-11-01A AND INSTALLED PLCD. CAT "C" PER DMI # 144280(M) PROCEDURE COMPLIED WITH. NOTIFIED TO MCC. T/I: JA 09:16Z.</P><P>ICN, 27MAR LP 1442679: T/S FOUND SURGE CONT VLV IS SOMETIMES INCORRECTLY OPEN &AMP; SURGE DUCT PUNCTURED, SO, REMOVED &AMP; REPLACED WITH SURGE CONT VLV &AMP; SURGE DUCT (P/N 23884292-2) THEN LEAK OPER &AMP; BITE CHK NORMAL IAW 49-53-01. CLEARED MDDR 144280, NOTIFIED MCC. T&AMP;I: DT 1017.</P>)

Part: WARNING MESSAGE — FALSE INDICATION (RT A/C PACK TEMP) · airframe 20,360 hrs · 5,389 cycles

EICAS MESSAGE R PACK TEMP(<P>PER AMM 21-51-00, PERFORMED R PACK TEMP CONTROLLER BITE TEST. PASSED. MSG GONE.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (A/C PACK TEMP) · airframe 20,342 hrs · 5,380 cycles

R PACK TEMP CAUTION APPEARED ON APPROACH WHEN PASSING THROUGH 10,000 / FEET. EMERGENCY PROCEDURE ACCOMPLISHED(<P>R PACK CONTROLLER BITE CHECKED "CONTROLLER FAULT" AND RECYCLED PACK TEMP&NBSP;CONT RELATED CBS THEN NO FAULT FOUND. R PACK SYS OPS NORMAL PER AMM&NBSP;21-51-00/501.</P>)

Part: TRANSMITTER — FLUCTUATES (NR 1 ENG) · airframe 20,298 hrs · 5,374 cycles

ENGINE OIL PRESSURE FLUCTUATION ON #1 ENGINE AFTER IDLE N2. AIRCRAFT RETURNED TO BAY. INVESTIGATION REVEALED #1 ENG OIL PRESSURE XMITTER ELEC CONNECTOR LOOSE. CONNECTOR REMOVED, CLEANED, INSPECTED &AMP; REINSTALLED IAW AMM 79-32-01. ENGINE RUN INDICATIONS READ NORMALLY (OPS CHECK GOOD).

Part: RADAR — FALSE INDICATION (WX SYSTEM) · airframe 20,241 hrs · 5,368 cycles

WX RADAR DISPLAYS PRECIPITATION THAT DOESNT EXIST, EVEN WITH TILT UP TO 8 DEG.(<P>RECYCLE L&R WX RADAR CB'S. WX RADAR STS TEST NORMAL PER AMM 34-43-00-735-033-002.

Part: CONNECTOR — DIRTY (VBV) · airframe 20,213 hrs · 5,361 cycles

DURING TOUCHDOWN, EICAS MESSAGE "R ENG CONTROL" DISPLAYED.(<P>R PIMU SHOWS "CH A/B SENS DISAGREE" R ENG VBV ACT ELEC CONN COND CHED OK, &AMP; CLEANED, NO EICAS MSG &AMP; STATUS MSG WITH R ENG RUN PER AMM 71-00-00.</P>)

Part: CONNECTOR — DIRTY (HMU) · airframe 20,222 hrs · 5,366 cycles

EICAS AND STATUS MSG: "R ENG CONTROL".(<P>R-PIMU SHOWED VBV OSI SNS DISAGREE. CLEAN UP VBV AND HMU ELEC CONECTOR, PERFORMED ENG RUN CK NORMAL, NO MSG AND NO FAULT IAW AMM 71-00-00</P>)

Part: CONNECTOR — DIRTY (HMU) · airframe 20,201 hrs · 5,355 cycles

"R ENG CONTROL" EICAS WHILE TAXIING TO PARKING"(<P>R PIMU SHOWED "VBV&NBSP;POSI SNS DISAGREE". CLEANED UP VBV AND HMU ELEC CONNECTOR. PERFORMED ENG RUN CK NORMAL. NO MSG NO FAULT STORED IAW AMM 71-00-00</P>)

Part: CONNECTOR — DIRTY (VBV) · airframe 20,201 hrs · 5,355 cycles

EICAS AND STATUS MSG: "R ENG CONTROL"(<P>R-PIMU SHOWED "VBV POSI SIG DISAGREE" SO VBV ELEC CONNECTOR CLEANED UP AND CHECKED OK, ALSO R ENG RUN UP THEN MSG DISAPEARED. R-PIMU NO FAULT STORED PER AMM 71-00-00-501</P>)

Part: BUSS — MALFUNCTIONED (UTILITY) · airframe 20,201 hrs · 5,355 cycles

DURING DESCENT, L UTIL BUS OFF AND R UTIL BUS OFF QRH PROCEDURE COMPLETED, POWER RESTORED TO BOTH BUSES. RESET L&R UTILITY BUS SWITCHES AND THEN OPER' CHKED OK AS PER AMM 24-22-00/501.

Part: CONTROLLER — MALFUNCTIONED (RT ENGINE) · airframe 20,146 hrs · 5,343 cycles

R ENG HPSOV MESSAGE ON APPROACH(<P>TEM TRANSFERRED TO MDDR # 143353. MEL 36-11-02-02, CAT C, DUE DATE 14MAR21. PERFORMED MAINTENANCE ACTION, CLOSED THE HPSOV. SHORTING PLUG NOT INSTALLED. ADVISED MCC. DISPATCH CC TIME 22:10Z.<BR /></P><P><SPAN>LOG 1324171 ITEM #2 REMOVED AND REPLACED RIGHT HIGH PRESSURE CONTROLLER AND THEN RIGHT HPSOV OPER CHECKED OK AS PER AMM 36-11-08/ 401 &AMP; AMM 71-00-00/ 501. CLEARED MDDR- RMVD PLAC, NOTIFIED MCC.</SPAN><BR DATA-MCE-BOGUS="1" /></P>)

Part: SHUTOFF VALVE — MALFUNCTIONED (RT ENGINE) · airframe 20,137 hrs · 5,342 cycles

RIGHT ENGINE HPSOV EICAS MESSAGE ON FINAL APPROACH. DEFERRED PER MDDR 143259 IAW MEL - 36-11-02-02, CAT C. LP 1195713: R ENG HPSOV REMOVED AND REPLACED IAW AMM 36-11-07 TESTED SERVICEABLE. MEL REVERSED. DMI 143259 CLEARED.

Part: BYPASS VALVE — LEAKING (OIL COOLER) · airframe 20,108 hrs · 5,339 cycles

APU OIL LEVEL EVIDENCE AT APU ACOC.(<P>REMOVED AND REPLACED PACKING AT OIL COOLER BYPASS VALVE,&NBSP;THEN OIL LEAK CHECK OK, NO LEAK IAW AMM 49-27-10 / 401.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENGINE) · airframe 20,108 hrs · 5,339 cycles

R.ENG HPSOV STATUS MSG (INTERMITTENT).(<P>NO STATUS MSG ON GRD, MANUALLY CHECKED R ENG HPSOV OPEN / CLOSE AND BLEED SYSTEM CHECKED NORMAL IAW AMM 36-11-07.&NBSP;<BR /></P>)

Part: RADAR — FALSE INDICATION (WX SYSTEM) · airframe 20,019 hrs · 5,317 cycles

WX RADAR SHOWS EXCESSIVE RETURNS ON GROUND AND CLIMB OUT WITH NO WEATHER. 0,5,7 AND GREATER DEGREES UP. WORKS FINE ABOVE FL 180. RECYCLE WX RADAR CB THEN WX RADAR OPERATION TEST OK PER AMM 34-43-00 PG 501.

Part: WINDOW — INOPERATIVE (CAPTS SIDE HEAT) · airframe 19,711 hrs · 5,285 cycles

LEFT SIDE WINDOW EICAS MESSAGE. FOUND CAPTS NR 2 SIDE WINDOW HEAT INOP. ITEM DEFERRED TO DDG 30-41-01-02, CAT C, MDDR 141701. FOLLOWED M PROCEDURE. INSTALLED PLACARD. TIME AND INITIALS CC @ 23:38Z. NOTIFIED MCC. DATE 01 FEB 21 LP 1324715 ITEM 8 & NRT. R & R CAPT'S NR 2 WINDOW PANE IAW AMM 56-11-02 407. NOTIFIED MCC. THIS MDDR 141701 IS CLOSED.

Part: FILTER — DIRTY (AIR CONT SYS) · airframe 19,711 hrs · 5,285 cycles

RIGHT ENGINE FAN AIR CONTROL SYSTEM INOP. TRANSFERRED TO MDDR 141660 AS PER MEL 36-12-02-01, ACCOMPLISHED M PROCEDURE DATE 31JAN21 LP 1324714 ITEM 5 NRT. PERFORMED FAMV MAN OPE TEST AND SENSING LINE LEAK CK OK BTWN FAMV & FATS. FOUND FAMV AIR FILTER VERY DIRTY. ALSO FATS AIR FILTER DIRTY, SO CLEANED UP AIR FILTER THEN R-ENG FAN AIR CONT SYS OPE TEST NORMAL, NO EICAS MSG FOUND BY ENG RUN UP,& ALSO BITE TEST PASSED PER AMM 36-11-16 36-11-17 36-11-00. THIS CLEARS MDDR 141660.

Part: VOLT REGULATOR — FAILED (OXY PRESS IND) · airframe 19,695 hrs · 5,277 cycles

CREW OXY PRESS IND CORRUPT (IND: 1100 PSI, ACTUAL: 1650). REPLACED VOLTAGE AVERAGING UNIT AND OPERATIONS CHECK NORMAL, PER AMM 35-11-06.

Part: SENSE LINE — LOOSE (PRIORITY VALVE) · airframe 19,549 hrs · 5,250 cycles

RT ENGINE PRV STATUS UPON ARRIVAL AT ICN. TROUBLESHOT AND FOUND RT ENGINE PRVC PNEUMATIC SENSE LINE WAS LOOSENED. RETIGHTENED SENSE LINE AND CHECKED OK, PER AMM 36-11-10/401 & 71-00-00/501.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENG PRV) · airframe 19,489 hrs · 5,236 cycles

RT ENGINE PRV STATUS MESSAGE. ASBM BITE SHOWS "R PRV" THEN VERIFY TEST PASSED AND NO MESSAGE, PER AMM 36-23-00-715-001. ALSO RT ENGINE RUN UP AND NO MESSAGE SHOWED, PER AMM 80-11-00-705-003-H00.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 19,448 hrs · 5,231 cycles

L1 DOOR EXIT SIGN BROKEN. RE-INSTALLED EXIT SIGN AND OPERATIONS CHECK OK, IAW AMM 33-51-09-201.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT PACK TEMP) · airframe 19,412 hrs · 5,221 cycles

LT PACK TEMP ILLUMINATED IN CRUISE. PERFORM L PACK TEMPERATURE CONTROLLER BITE TEST AND TEST NORMAL, AS PER AMM 21-51-14. PERFORMED LT & RT PACK OPERATION CHECK AND AIR COND CHECK NORMAL, AS PER AMM 21-00-00/ 21-51-00.

Part: A/C PACK — MALFUNCTIONED (LEFT) · airframe 19,397 hrs · 5,214 cycles

LEFT PACK INOPERABLE. PACK TEMP CONTL SHOWS "CONTROLLER FAULT". RECYCLED CB AND VERIFY TEST PASSED, IAW AMM 21-51-04. ALSO PACK OPERATION NORMAL.

Part: SWITCH — ODOR (LIGHT) · airframe 19,260 hrs · 5,191 cycles

BURNING RUBBER SMELL BELIEVED TO BE ASSOCIATED WITH RUNWAY TURN OFF LIGHT ACTIVATION, PER AMM 05-51-56. PERFORM SMOKE & FUMES IN CABIN CONDITION INSPECTION SATISFACTORY, PER MEL 33-42-03. RELEASE A/C CAT C, NOTIFIED MCC, MDDR NR 139747, T/I 20:18 YC. PLACARD INSTALLED. LT RUNWAY TURNOFF LT SW BURNING SMELL. REMOVED AND REPLACED LT RUNWAY TURN-OFF LIGHT, IAW SSM 33-42-02. OPERATIONS CHECK REFERENCE IS AMM 33-42-03/201. OPERATIONS CHECKS GOOD.

Part: LANDING LIGHT — INOPERATIVE (LT WING) · airframe 19,258 hrs · 5,190 cycles

ITEM 1: LEFT WING LANDING LIGHT INOPERABLE, SMELL OF BURNING RUBBER WHEN SELECTING WING LANDING LIGHTS ON. ITEM 2: SMELL REPORTED IN DISCREPANCY NR 01 SEEMS TO HAPPEN WHEN TAXI/RUNWAY TURNOFF LIGHTS SELECTED ON (NOT WING LANDING LIGHTS). INSPECTED LANDING LIGHT CONTROL PANEL, P11 CIRCUIT BREAKER PANELS AND COCKPIT PANELS, NO BURNING EVIDENCE FOUND. PERFORMED LIGHTS TEST, OK PER AMM 33-42-00/501 AND AMM 05-51-00. A/C OK FOR SERVICE. MCC NOTIFIED.

Part: SENSOR — FAILED (AIR TEMP) · airframe 19,253 hrs · 5,188 cycles

"RT ENGINE HPSOV" EICAS ON CLIMB OUT. RAN QRH. REMOVED AND REPLACED RIGHT BLEED AIR CONTROL CARD (OFF PART: PN 285T1115-15, SN V02252) AND RIGHT FAN AIR TEMPERATURE SENSOR AND THEN RIGHT ENGINE HPSOV SYSTEM OPER CHECKED OK, PER AMM 36-11-12/401.

Part: SHUTOFF VALVE — NOT REPORTED (RT ENGINE) · airframe 19,251 hrs · 5,187 cycles

RT ENGINE HPSOV. REMOVED AND REPLACED RT ENGINE HPSOV THEN OPER CHECKED OK, PER AMM 36-11-07/401.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENG SOV) · airframe 19,247 hrs · 5,185 cycles

RT ENGINE HPSOV EICAS AT TOP OF CLIMB, QRH PROCEDURE COMPLETED. PERFORMED ASBM BITE TEST RT HPSOV, SHOW PERFORM VERIFY CHECK, NO FAULT FOUND. COND CHECK NORMAL, IAW AMM 36-11-07. AIR SUPPLY SYSTEM BITE CHECK OK, IAW AMM 36-23-00.

Part: SHUTOFF VALVE — FAULTED (RT ENGINE) · airframe 19,249 hrs · 5,186 cycles

RT ENGINE HPSOV EICAS. ASBM SHOWED HPC AND BITE SOV FAULT. REPLACED RT HPSOV, IAW AMM 36-11-07. OPERATIONS CHECK GOOD.

Part: HPC — MALFUNCTIONED (RT ENGINE) · airframe 19,247 hrs · 5,185 cycles

RT ENGINE HPSOV EICAS ON CLIMB OUT RAN QRH. REMOVED AND REPLACED RT ENGINE HPC THEN OPER CHECKED OK, PER AMM 36-11-08/401.

Part: CONNECTOR — DIRTY (SHUTOFF VALVE) · airframe 19,247 hrs · 5,185 cycles

RT ENGINE HPSOV EICAS ON CLIMB OUT RAN QRH. ASBM BITE SHOWED RT HPSOV SO CLEANED UP ELEC CONNECTOR ON HPSOV AND HPSOV CONTROLLER. ALSO RT ENGINE RUN UP, NO MESSAGE SHOWED, PER AMM 36-11-07-401 AND 80-11-00-705-003-H00.

Part: LINE — LOOSE (SHUTOFF VALVE) · airframe 19,241 hrs · 5,182 cycles

RT ENGINE HPSOV ENROUTE EICAS. APPLIED QRH, TIGHTENED SENSING LINE AND EXERCISED VALVE. 2 ENGINE RUN 2 TIMES, NO MESSAGE SHOWED. AIR SUPPLY SYSTEM BITE TEST CHECKED OK. NOTIFIED MCC, AS PER AMM 80-11-00-705-003-H00 & AMM 36-11-07/401.

Part: TRANSDUCER — MALFUNCTIONED (VOLTAGE) · airframe 19,067 hrs · 5,141 cycles

FOUND CREW OXY PRESSURE INDICATION ABNORMAL. TRANSFERRED TO MDDR 138395, IAW MEL 35-11-02-01, CAT B. REMOVED AND REPLACED AVERAGING VOLTAGE UNIT & REGULATOR TRANSDUCER ON CREW OXY. THEN OPERATIONS CHECK OK, IAW AMM 35-11-04/401 & AMM 35-11-06/401. CLEARED MDDR NR 138395, REMOVED PLACARD, NOTIFIED TO MCC. T/I: DT 0548Z.

Part: INDICATOR — INOPERATIVE (OXYGEN PRESSURE) · airframe 19,065 hrs · 5,140 cycles

OXYGEN PRESSURE INDICATION IS INOPERABLE, CREW OXYGEN SYSTEM, PRESSURE INDICATION (EICAS). CLEANED AND SECURED ELECTRICAL CANNON PLUG FOR VOLTAGE AVERAGING UNIT AND PRESSURE TRANSDUCER. OPERATIONS GOOD, IAW AMM 35-11-06.

Part: CONTROL VALVE — MALFUNCTIONED (LT A/C PACK) · airframe 18,993 hrs · 5,127 cycles

L PACK OFF EICAS MESSAGE PACK OFF LIGHT. PERFORMED LT PACK BITE THEN NO FAULT FOUND. L FCV WIRING CHECK OK, IAW FIM 21-51 FAULT TREE 852. REMOVED AND REPLACED L-PACK FLOW CONTROL VALVE AND L-PACK OPERATIONS NORMAL, PER AMM 21-51-01 ALSO L PACK OPERATION CHECK OK WITH BOTH ENGINE RUN.

Part: SWITCH — MALFUNCTIONED (LT A/C PACK) · airframe 18,974 hrs · 5,125 cycles

LT PACK NO START, AFTER FEW SECONDS. "LT PACK OFF" EICAS MESSAGE AT LT PACK SW AUTO. RE-RACKED LT PTC & RE-CONNECT COMPRESSOR OUTLET OVERHEAT SW THEN OPERATIONS NORMAL. ALSO SW WIRING CHECKED OK AND REMOVE/REPLACED SW THEN OPERATIONS CHECK OK, PER FIM 21-51 TASK 876, WPM 21-51-11, AMM 21-51-19/201 & AMM 21-51-14/401.

Part: CONTROLLER — INOPERATIVE (LT A/C PACK) · airframe 18,907 hrs · 5,118 cycles

LT PACK TEMP INOPERABLE. ENTERED INTO DMI 137689, MEL 21-51-03-01, CAT C. REMOVED AND REPLACED LT PACK CONTROLLER ASSEMBLY, IAW AMM 21-51-14-401. USED LOAN PARTS FROM UPS. THEN LT PACK OPERATION CHECK OK. CLOSED DMI 137689. T&I CC 0137Z.

Part: SHUTOFF VALVE — INOPERATIVE (RT ENGINE) · airframe 18,907 hrs · 5,118 cycles

RT ENGINE HPSOV INOPERABLE. ENTERED INTO DMI 137663, IAW MEL 36-11-02-02, CAT C. 14NOV20 LP 114468 ITM 10 NRT. RT ENGINE PNEU LEAK CHECK AT HPSOV DOWN STREAM. REPLACED T-SEAL AND PNEU LEAK CHECK OK, IAW AMM 36-11-07/401. REACTIVATE RT ENGINE HPSOV, IAW MEL 36-11-02-02. DT 0712Z. THIS CLEARS DMI 137663.

Part: STATUS MESSAGE — FALSE ACTIVATION · airframe 18,860 hrs · 5,113 cycles

STATUS MESSAGE "RT ENGINE PRV" AIR SUPPLY BITE MODULE SHOWS NO FAULT. AIR SUPPLY BITE TEST NORMAL, PER AMM 36-23-00-071J-001.

Part: CONTROL UNIT — MALFUNCTIONED (APU) · airframe 18,860 hrs · 5,113 cycles

APU AUTO SHUT DOWN WHEN GPU POWER TRANSFER, IAW AMM 49-61-05. REPLACED APCU AND APCU BITE TEST AND SELF TEST OK AND APU OPERATION CHECK NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT HPSOV) · airframe 18,842 hrs · 5,104 cycles

DURING CRUISE EICAS MESSAGE "RT HPSOV", AFTER ONE MINUTE MESSAGE CLEARED, PER FIM 36-20-00 CARRIED OUT AIR SUPPLY BITE PROCEDURE AND NO FAULT FOUND - 2. PER AMM 36-23-00 AIR SUPPLY SYSTEM BITE TEST NORMAL.

Part: APU — FAULTED · airframe 18,676 hrs · 5,066 cycles

APU SHUTDOWN WHILE ON GROUND ACCOMPANIED BY "APU FAULT" EICAS, PER AMM 49-61-05 FIM APU CONTROL UNIT BITE TEST OK. RESTART APU CONTROL NORMAL.

Part: RETAINER — BROKEN (RT A/C PACK) · airframe 18,593 hrs · 5,055 cycles

RT PACK INOPERABLE LT APPEARED. ARM OUTLET DISCHARGE DUCT JOINT SLEEVE DETACHED. FOUND BROKEN RESTRAINT FLEXIBLE WIRE (1 EA). REPLACED RESTRAINT FLEXIBLE WIRE CABLE 2 EA ON THE ACM OUTLET DISCHARGE DUCT AREA AND SEAL. REALIGNED THE ACM OUTLET DUCT. OPERATIONS CHECK OK, PER AMM 21-5100. PERFORMED RESET AND BITE TEST VERIFY CHECK OK RT PACK. RT PACK OPERATIONS CHECKED OK, PER AMM 21-51-00.

Part: CONTROLLER — INTERMITTENT (HPSOV) · airframe 18,538 hrs · 5,042 cycles

RT ENGINE HPSOV EICAS STATUS MESSAGE ON CLIMBOUT, INTERMITTENT. 4TH WRITE UP. REMOVED & REPLACED WITH NEW HP BLEED CONTROLLER, IAW AMM 36-11-08 AND BLEED SYSTEM OPERATIONAL CHECKS OK.

Part: SHUTOFF VALVE — FAULTED (RT ENGINE) · airframe 18,534 hrs · 5,040 cycles

RT ENGINE HPSOV EICAS AND STATUS MESSAGE IN CRUISE, 3RD WRITE UP. ASBM SHOWS HPSOV FAULT. PERFORMED RT ENGINE RUN UP THEN RT ENGINE HPSOV NORMAL OPT AND NO MESSAGE. ALSO, ASBM NO FAULT AND VERIFY TEST PASSED, IAW AMM TASK 36-23-00-715-001.

Part: LINE — LOOSE (PNEUMATIC SENSE) · airframe 18,532 hrs · 5,039 cycles

RT ENGINE HPSOV EICAS AND STATUS MESSAGE. 2ND WRITE UP ON CLIMB OUT. CHECKED AND FOUND PNEUMATIC SENSE LINE WAS LOOSENING. RE-TIGHTENED AND RT ENGINE OPEN CHECKED OK, PER AMM 36-11-08/401.

Part: WARNING MESSAGE — FALSE ACTIVATION (HPSOV) · airframe 18,522 hrs · 5,034 cycles

RT ENGINE HPSOV EICAS MESSAGE AND STATUS MESSAGE. ASBM SHOWS "HPSOV" FAULT. PERFORMED RT ENGINE RUN UP THEN RT ENGINE HPSOV NORMAL OPT AND NO MESSAGE. ALSO ASBM NO FAULT AND VERIFY TEST PASSED, IAW AMM TASK 36-23-00-715-001.

Part: WARNING SYSTEM — FALSE INDICATION (NR 1 ENG EGT) · airframe 18,476 hrs · 5,011 cycles

UPON START NR 1 ENGINE (LEFT SIDE) THE EGT INITIALLY ACCELERATED ABNORMALLY QUICKLY AND STABILIZED AROUND 430 F EGT. INSPECTED NR 1 ENG'S INLET & EXHAUST AREA AND NO TROUBLE FOUND. NO EGT EXCEEDANCE MSG FOUND ON ENG EXCD PAGE. PERFORMED PIMU BITE PROCEDURE AND NO FAULT FOUND, PER FIM 71-01-00/101. PERFORMED NR 1 & NR 2 ENG'S RUN UP CHECK AND THEN BOTH EGT SYSTEMS CHECKED OK, SAME CONDITION PER AMM.

Part: CONTROLLER — FAULTED (RT A/C PACK) · airframe 18,425 hrs · 4,993 cycles

RIGHT PACK TEMP EICAS IN FLIGHT. PERFORMED PTC BITE TEST, FOUND CONTROLLER FAULT. REMOVED AND REPLACED CONTROLLER, IAW AMM 21-51-4.

Part: CONTROLLER — MALFUNCTIONED (PACK TEMP) · airframe 18,413 hrs · 4,987 cycles

RIGHT PACK TEMP EICAS AFTER TAKEOFF, LEFT PACK DEFERRED. RETURN TO ICN. FOLLOWED FIM TASK 21-51 FAULT TREE 844 PERFORMED T/S, FOUND RT STANDBY CONTROLLER FAULT. REMOVED AND REPLACED RT STANDBY CONTROLLER AND CHECKED OK, NO FAULT FOUND PER AMM 21-51-14/401. PERFORMED BITE TEST OF RT PACK TEMP CONTROLLER, FOUND PACK TEMP CONTROLLER FAULT, RAM INLET ACT FAULT, LT CHECKED OK. REMOVED & REPLACED RT PACK TEMP CONTROLLER (SOS PART) AND RT PACK CHECKED OK, PER AMM 21-51-14/401. NO FAULT MSG FOUND PER AMM 21-53-03/401.

Part: DUCT — CRACKED (RT A/C PACK) · airframe 18,412 hrs · 4,986 cycles

UPON ARRIVAL INTO THE COCKPIT THE TEMPERATURE WAS 29. T/S AND FOUND RT PACK COMPRESSOR OUTLET DUCT CRACKED. SWAPPED DUCT WITH LT PACK THEN RT PACK OPS CHKS NORMAL, AS PER AMM 21-51-03. APPROVED BY MCC. LT PACK IS ALREADY DEFERRED.

Part: CONTROLLER — MALFUNCTIONED (LT A/C PACK TEMP) · airframe 18,413 hrs · 4,987 cycles

LT PACK INOP, COCKPIT WOULD NOT COOL DOWN, REMAINED OVER 33'C AT FL 340 ENTIRE FLIGHT. TRANSFERRED TO MDDR 134263 IAW MEL 21-51-01-01, CAT C. REMOVED AND REPLACED LT PACK TEMP CONTROLLER AND OPER CHECKED OK, NO FAULT FOUND, PER AMM 21-51-14/401. A/C OK FOR SERVICE. CLEARRED MDDR 134263. NOTIFIED MCC DISPATCH ZS 0639Z.

Part: CONTROL UNIT — MALFUNCTIONED (AUTOBRAKES) · airframe 18,385 hrs · 4,972 cycles

AUTOBRAKES DISARM PRIOR TO LANDING. T/S AND FOUND SUSPECT ANTISKID/AUTOBRAKE CONT UNIT DEFECTIVE, PER WDM 32-42-03 P/N: S003T001-07. ITEM TRANSFERRED TO MDDR NR 134057, AS PER MEL 32-42-04-01A CAT C, CAT III RECTRICTED. INSTALLED PLACARD. REMOVED AND REPLACED AUTOBRAKE/ANTISKID CONTROL UNIT, IAW AMM 32-42-01. OPS CHK GOOD, THIS CLEARS MDDR 134057.

Part: CONTROLLER — MALFUNCTIONED (LT A/C PACK) · airframe 18,369 hrs · 4,968 cycles

LT PACK TEMP EICAS INDICATION ON DEPARTURE. RAN QRH TEMP EICAS AND INOP MSG EXTINGUISHED. BIT ON LPTC SHOWS CONT FAULT + RAI ACTUATOR, RESET + VERIFIED C/O IAW AMM 21-51-00. DEFECT CLEARED SUBS PACK OPS DURING TRANSIT SATIS. DUE HISTORY APPLIED MEL 21-51-03-01, CAT C, MDDR 133970. REMOVED & REPLACED LT PACK TEMP CONTROLLER AS PER AMM 21-51-04, OPS NORMAL. THIS CLEARS MDDR 133970.

Part: ACTUATOR — MALFUNCTIONED (LT A/C PACK) · airframe 18,302 hrs · 4,961 cycles

ON CLIMB OUT RECEIVED "L PACK TEMP" EICAS MESSAGE. COMPLIED WITH QRH.(<P>PACK TEMP CONT "AUTO" INOP. ITEM DEFERRED PER MEL 21-51-03-01, MDDR #133749, CAT 'C'.</P><P>LP 1153914 ITEM 7: PTC BITE SHOWS "RAM INLET ACTR" FAULT, SO REMOVED &AMP; REPLACED L PACK RAM AIR INLET ACTUATOR ASSY PER AMM 21-53-03-401, CONFIRMED PTC BITE NO FAULT&NBSP;REPORTED PER AMM 21-51-00-501, THEN L PACK OPERATION CHECK OK, CLOSED DMI # 133749, MCC NOTIFIED.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (FWD CARGO) · airframe 18,264 hrs · 4,957 cycles

FWD CARGO BACKUP EICAS MSG(PERFORMED OPERATIONAL TEST IAW AMM 21-43-00 SYSTEM OK).

Part: OVERHEAT SYS — MALFUNCTIONED (LT ENGINE) · airframe 18,250 hrs · 4,950 cycles

RIGHT ENGINE OH LP1; LEFT ENGINE OH LP2 STS MESSAGE DISPLAYED(PERFORMED CONVERSION FIRE DETECTION SYSTEM PER EO 6726A005 THEN FIRE/OVERHEAT SYSTEM OPERATIONS CHECKED NML AS PER AMM 26-10-01 WDM 26-11-22).

Part: START VALVE — MALFUNCTIONED (RT ENGINE) · airframe 18,121 hrs · 4,927 cycles

RIGHT ENGINE START VALVE INOPERABLE (APPLIED MEL 80-00-02-01 WITH MDDR 132891, CAT 'C'. C/W MAINT PROCEDURE, MCC MIZ TIME 007. LP 1131722 ITEM 4: REMOVE AND REPLACED RIGHT ENGINE STARTER VALVE OPS NORMAL PER AMM 80-11-02/401. ITEM CLOSED DMI # 132891, NOTIFIED MCC, TI 23:17 J.A).

Part: VALVE — MALFUNCTIONED (APU) · airframe 18,045 hrs · 4,919 cycles

APU PNEUMATIC FUNCTION INOP (AUXILIARY POWER UNIT, PNEUMATIC FUNCTION)(<P>TRANSFERRED TO MEL 49-11-01-01, MDDR 132671 RAISED, CAT 'C'.<BR /></P><P>LP 1131759 ITEM 7: IAW AMM 49-53-01/401 REMOVED &AMP; REPLACED SURGE CONTROL VALVE AND APU BLEED SYSTEM NORMAL WITH ENGINE MOTORING (N2 2906, DUCT PRESSURE 35PSI), ITEM CLOSED DMI #132671.<BR /></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 17,994 hrs · 4,904 cycles

HI FLOW INHIBIT STATUS MSG PRIOR TO BLOCK OUT FOLLOWED FIM 21-51 TASK 875, CYCLED PACKS AND OPS CHECK GOOD, MSG CLEARED.

Part: IGNITION UNIT — FAILED (APU) · airframe 17,979 hrs · 4,897 cycles

APU COLD SOAK START UNSUCCESSFUL AFTER 3 ATTEMPTS AT FL 320, OAT -39C. APCU BITE SHOWS FAULT REASON NO LIGHT OFF, FAULT LRU IGNITION UNIT. REMOVED AND REPLACED APU IGNITER PLUG. . REMOVED AND REPLACED APU IGNITION UNIT IAW AMM 49-41-03-401. CHECKED GOOD.

Part: APU — FAULTED · airframe 17,969 hrs · 4,896 cycles

APU FAULT, APU BITE CARRIED OUT, NO LIGHT OFF, MINI FLAG CODE IGNITION UNIT. APU START ATTEMPT CARRIED OUT NORMAL. APU RESET IAW AMM 49-61-00.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 17,876 hrs · 4,886 cycles

FOUND WHEN #2 PACK ON, ODOR SMELL IN COCKPIT.(<P>PER AMM TASK 21-51-21-004-001/404-015 REV. INSP PACK WATER SEPARATOR AND NO CONTAMINATION FOUND. AFT APU CHANGED PER AMM TASK 21-00-21-102-030 REV 130, CHECK NO ODOR SMELL WHEN OPERATING PACK 2.</P>)

Part: PLUG — NO TEST (STARTER) · airframe 17,876 hrs · 4,886 cycles

FOUND #2 ENG STARTER DRAIN PLUG CHECK VALVE FUNCTION FAIL AND OIL LEAK.(<P>PER AMM TASK 12-22-02-603-054-001 REV 130 REPLACED #2 ENG STARTER DRAIN PLUG AND SERVICE STARTER OIL WITH MOBIL JET -11 AND OVERFLOW, CONDITION CHECK NO LEAK FOUND. JOB COMPLETED AND CONDITION CHK SATISFACTORY.</P>)

Part: PLUG — LEAKING (STARTER) · airframe 17,876 hrs · 4,886 cycles

FOUND #1 ENG STARTER DRAIN PLUG CHECK VALVE FUNCTION FAIL AND OIL LEAK(<P>PER AMM TASK 12-22-02-603-054-001 REV 130 REPLACE #1 ENG STARTER DRAIN PLUG AND SERVICE STARTER OIL WITH MOBILE JET -11 AND OVERFLOW, CONDITION CHK NO LEAK FOUND AND CONDITION SATISFACTORY.</P>)

Part: CONTROL VALVE — FAULTED (RT A/C PACK) · airframe 17,834 hrs · 4,868 cycles

RIGHT PACK INOPERATIVE. PERFORMED APU PNEUMATIC FUNCTION SYSTEM, CHECKED OK, REPLACED FLOW CONTROL VALVE IAW AMM 21-51-00. PERFORMED SYSTEM TEST, CHECKED OK.

Part: LATCH — INOPERATIVE (ESCAPE ROPE DOOR) · airframe 17,683 hrs · 4,814 cycles

EMERGENCY ESCAPE ROPE DOOR ABOVE CO-PILOT SEAT DOES NOT PROPERLY LATCH.(<P>ADJUSTED LATCH, OPERATIONAL CHECK NORMAL IAW AMM 25-61-00.</P>)

Part: ANTI-ICE SYSTEM — UNKNOWN (ENGINE) · airframe 17,617 hrs · 4,807 cycles

ENGINE ANT-ICE IN AUTO REMAINED ON FOR THE LAST 13 MIN OF FLIGHT WITH CLEAR SKIES. 48 C. LT & RT ENG THERMAL NACELLE ANTI-ICE VALVES OPERATION CHECK COMPLETED IAW AMM 30-21-03-714. ALL OPS & INDICATIONS NORMAL.

Part: CONTROLLER — FAULTED (A/C PACK TEMP) · airframe 17,541 hrs · 4,772 cycles

LEFT A/C PACK WAS INOPERATIVE. PTC BITE SHOWS A CONTROLLER FAULT. PERFORMED LT PTC VERIFICATION, TESTED OK IAW AMM 21-51-14. REMOVED AND REPLACED THE PACK, TEMP CONTROLLER IAW AMM 21-51-14/401. BITE TESTED NORMAL.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 17,536 hrs · 4,769 cycles

LT PACK TEMP EICAS OBSERVED ON CLIMB OUT. PERFORMED QRH; PROC. DID NOT RESET. CONTINUED FLIGHT W/ LEFT PACK OFF IAW QRH. IAW FIM 21-51 TASK 877, LT PTC BITE CONTROLLER AND INLET DOOR ACTR FAULT LIGHT ON. PFM VERIFY. RESET, BOTH LIGHT GONE. PERFORMED LT PACK CHK CONDITION NORMAL IAW AMM 21-51-00.

Part: GUIDE VANE — DAMAGED (RT ENGINE) · airframe 17,484 hrs · 4,747 cycles

FIVEOF OGV'S ON RT ENGINE FOUND DELAMINATED AT 9 O`CLOCK LOOKING FROM AFT. PERFORMED TEMPORARY REPAIR IAW EO 1972A783, REMOVED AND REPLACED THE NR 2 ENGINE FAN CASES OGV'S IAW AMM 72-33-04.

Part: GUIDE VANE — DELAMINATED (RT ENGINE) · airframe 17,484 hrs · 4,747 cycles

FIVE OF OGV'S ON RT ENGINE FOUND DELAMINATED AT 9 O CLOCK LOOKING FROM AFT. PERFORMED TEMPORARY REPAIR AS PER EO 1972A783. REPEAT INSPECTION EVERY 3 FLT CYCLES FOR THE INTEGRITY. PERMANENT REPAIR NEED BEFORE 25 FLT CYCLES. RAISED NON-MEL #129103.

Part: VALVE — INOPERATIVE (AC BAY) · airframe 17,279 hrs · 4,710 cycles

FOUND OVERRIDE VALVE INOP WHEN PERFORMING EO6721A012.(<P>PER AMM 21-58-20-024-035/21-58-20-424-033 REV 130 REPLACED OVERRIDE VALVE. TESTED NORMAL AND CONDITION CHECK NORMAL.</P>)

Part: STARTER — INOPERATIVE (APU) · airframe 16,878 hrs · 4,633 cycles

APU INOP (AUXILIARY POWER UNIT (APU), ER OPERATIONS NOT ALLOWED (NOTIFY DISPATCH) R60)(<P>TRANSFER TO MDDR 126307 IAW MEL&NBSP;49-11-01A, CAT 'C'.</P><P>LP 1205568: T/S TO STARTER MOTOR. REMOVED AND REPLACED STARTER MOTOR ASSY IAW AMM 49-41-01. OPS CHK GOOD. THIS CLEARS MDDR 126307.&NBSP;</P><P><BR /></P>)

Part: DIODE — UNKNOWN (FIRE ARM LIGHT) · airframe 16,651 hrs · 4,586 cycles

AFT CARGO FIRE ARM LIGHT INOP.(<P>DEFERRED PER MEL 26-23-01, CAT C, MDDR 125081. </P><P>LP 1218496: REINSTALLED LWR AFT CARGO FIRE EXTINGUISHING ARM SWITCH FUSE/DIODE IAW AMM 33-13-00 AND LIGHT TESTS SATISFACTORY IAW AMM AMM 26-23-01. PERFORMED LOWER AFT CARGO FIRE EXTINGUISHING ARMED SWITCH ACTIVATION CHECK, SATISFACTORY. DMI 125081 CLOSED. PLACARD REMOVED.</P>)

Part: START VALVE — FAILED (NR 1 ENGINE) · airframe 16,612 hrs · 4,574 cycles

FOUND NO. 1 ENG START VALVE FUNCTION FAIL.(<P>IAW AMM 80-11-02-004-001 REV. 129 AND AMM 80-11-02-404-017 REV. 129 REPLACED NO. 1 ENG START VALVE WITH NEW PARTS. IAW AMM 80-11-02-404-017 REV. 129 STEP H PERFORMED START VALVE INSTALLATION TEST. TEST RESULT SATISFIED. CONDITION CHECK NORMAL, AND&NBSP;THE JOB IS COMPLETE.&NBSP;</P>)

Part: RUB STRIP — CORRODED (RT NACELLE) · corrosion level 2 · airframe 16,612 hrs · 4,574 cycles

CORROSION - WEAR STRIP, NO. 1 ENG R/H CORE COWL L/E OUTER SIDE, NEAR 2:00.(<P>REMOVE DAMAGED PARTS IAW SRM 51-40-02 REV. 76. INSTALL NEW PARTS IAW SRM 51-40-02 REV. 76 AND GOODRICH CMM 71-13-24 FIG 1 SH 1 OF 22 REV. 44. JOB COMPLETED AND CONDITION CHECK SATISFIED.&NBSP;</P>)

Part: RUB STRIP — CORRODED (RT NACELLE) · corrosion level 2 · airframe 16,612 hrs · 4,574 cycles

CORROSION - SURFACE, NO. 2 ENG R/H CORE COWL EXTERIOR FWD L/E WEAR STRIP. TOTAL 4EA.(<P>REMOVE DAMAGED PARTS IAW SRM 51-40-02 REV. 76 (OFF PARTS: PN 224-2301-71 &AMP; 224-2301-146). INSTALL NEW PARTS IAW SRM 51-40-02 REV. 76 AND GOODRICH CMM 71-13-24 REV. 44. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: PACKING — LEAKING (NR 2 PRVC) · airframe 16,612 hrs · 4,574 cycles

LEAK - FWD NO. 2 ENG PRVC SENSING TUBE JOINT LEAKAGE.(<P>IAW AMM 36-11-19-004-001 REV. 129 AND AMM 36-11-19-404-014 REV. 129 REPLACED THE PACKING WITH SERVICEABLE PARTS AT NO. 2 ENG PRVC SENSING TUBE, IAW AMM 36-11-19-404-012 REV. 129 PERFORMED INSTALLATION TEST, RESULT WAS&NBSP;NO LEAK FOUND AND CONDITION CHECK NORMAL.</P>)

Part: MODULE — NOT REPORTED (AIR SUPPLY) · airframe 16,612 hrs · 4,574 cycles

REMOVE AND REPLACE FAULTY AIR SUPPLY BITE MODULE.(<P>IAW AMM 36-23-01-004-001, 36-23-01-404-005 REV. 129 REPLACED THE AIR SUPPLY BITE MODULE. IAW AMM 36-23-00-715-001 REV. 129 PERFORMED THE AIR SUPPLY CONTROL SYSTEM BITE TEST. THE RESULT WAS SATISFACTORY.</P>)

Part: SKIN — CORRODED (LT WING TE FLAP) · airframe 16,612 hrs · 4,574 cycles

CORROSION - SKIN, L/H WING INBD AFT FLAP T/E UPPER SURFACE WBL 278.(<P>REMOVE THE DAMAGED MATERIAL AND CLEAN AND MEASURE THE DAMAGED AREA (L = 2.4", W = 0.75", D = 0.012", 8.25" FROM OUTBD EDGE, AT PNL T/E) BOND REPAIR DOUBLER (L = 6.9", W = 2.25", D = 0.025") AND REPAIR FILLER (L = 2.4", W = 0.75", D = 0.012") WITH FILM ADHESIVE. CURE AT 250 DEGREES (F) FOR MINIMUM 90 MINUTES. MAINTAIN A MINIMUM VACUUM PRESSURE 20 IN/HG IAW B767-300F SRM 57-53-01-2R-1, REFER TO SRM 51-70-10-2R-0 AND SRM 51-70-10-2R-4 REV. 76. CONDITION CHECK IS SATISFACTORY.</P>)

Part: RUB STRIP — CORRODED (THRUST REVERSER) · corrosion level 2 · airframe 16,612 hrs · 4,574 cycles

CORROSION - INNER SURFACE, NO. 2 ENG R/H T/R INTERIOR REAR UPPER WEAR STRIP. TOTAL = 4EA.(<P>REMOVE DAMAGED PARTS IAW SRM 51-40-02 REV. 76. INSTALL NEW PARTS IAW SRM 51-40-02 REV. 76 AND MRAS IPC 78-32-22 FIG. 7 SH6 REV. 83. JOB COMPLETED AND CONDITION CHECK SATISFIED.&NBSP;</P>)

Part: VALVE — MALFUNCTIONED (NR 2 ENGINE) · airframe 16,612 hrs · 4,574 cycles

FUNCTION FAIL - PRVC, FOUND NO. 2 ENG PRVC REFERENCE PRESSURE LESS THAN 12 PSI WHEN SUPPLY PRESSURE IS 20 PSI.&NBSP;(<P>IAW AMM 36-11-19-004-001-002 REV. 129 &AMP; AMM 36-11-19-404-014-002 REV. 129 REPLACED NO. 2 ENG PRVC WITH SERVICEABLE PARTS. IAW AMM 36-11-19-404-014-002 REV. 129 PERFORM NO. 2 ENG PRVC INSTALLATION TEST AND LEAK CHECK. RESULT NO LEAK FOUND AND CONDITION CHECK NORMAL.</P>)

Part: COMPRESSOR — FAILED (HP) · airframe 16,612 hrs · 4,574 cycles

FUNCTION FAIL - HPC, FOUND NO. 2 ENG HPC BIT 18 CAN'T CHANGE FROM 1 TO 0 WHEN SUPPLY PRESSURE IS 10-18 PSI.(<P>IAW AMM 36-11-08-004-006-007 REV. 129 &AMP; AMM 36-11-08-404-014-007 REV. 129.&NBSP; REPLACED NO. 2 ENG HPC WITH SERVICEABLE PARTS. IAW AMM 36-11-08-404-014-007 REV. 129 PERFORM NO. 2 ENG HPC LEAK CHECK AND BITE TEST RESULT NO LEAK FOUND AND CONDITION CHECK NORMAL.</P>)

Part: RETAINER — CORRODED (RT MLG DOOR) · corrosion level 2 · airframe 16,612 hrs · 4,574 cycles

CORROSION - RETAINER, R/H MLG DOOR INBD SIDE SEAL RETAINER.(<P>DRILLED SCREW HOLES ON NEW RETAINER IAW SRM 51-40-02 AND SRM 51-40-05 REV. 76 AND DWG NO. 149T6906 SH01 REV. E SH02 REV. H SH03 REV. A. JOB COMPLETED AND CONDITION CHECK NORMAL. REMOVE/INSTALL REF JOB ATTACHING SHEET 0207476, 0207477.</P>)

Part: PACKING — DAMAGED (FUEL SYSTEM) · airframe 16,519 hrs · 4,550 cycles

FUEL MINOR SEEPING FROM ENG 2 FUEL FILTER DIFF PRESSURE SWITCH JAM NUT.(<P>REMOVED AND REPLACED JAM NUT PACKING. OPS TEST GOOD AND NO LEAK FOUND IAW AMM 73-34-01.</P>)

Part: TRU — FAILED (APU) · airframe 16,526 hrs · 4,553 cycles

APU FAULTED AFTER THREE ATTEMPTS. IAW FIM 49-11 FT 987, 988, PERFORMED APU BITE TEST. FOUND BATTERY START APU OK, BUT APU TRU INOPERATIVE. APU START TRU REPLACED AND TESTED SERVICEABLE IAW AMM 24-32-04.

Part: CONTROLLER — MALFUNCTIONED (LT A/C PACK) · airframe 16,463 hrs · 4,536 cycles

LEFT PACK RAM AIR INLET DOOR SECURED OPEN. L PACK TEMP, L PACK RESET SW INOP.(<P>TRANSFER TO MDDR 122670 IAW DDG 21-53-01A, CAT 'C', REMOVED AND REPLACED LEFT PACK INLET DOOR ACTUATOR PER AMM 21-53-03 AND PACK TEMP CONTROLLER PER AMM 21-51-14 LEFT PACK OPS CHECKED NORMAL. ACTIVATED RAM AIR INLET AND EXHAUST DOOR AND DOOR OPEN CHECK NORMAL PER AMM 21-00-00.

Part: CONTROLLER — FAILED (LT A/C PACK TEMP) · airframe 16,417 hrs · 4,530 cycles

LEFT PACK TEMP APPEARED. FOUND LT PACK TEMP CONTROLLER DEFECTIVE BY SWAP CHECK, REMOVED AND REPLACED PACK TEMP CONTROLLER IAW AMM 21-51-14 AND OPS CHECKED NORMAL. NO MESSAGES.

Part: PACKING — LEAKING (FUEL SYSTEM) · airframe 16,323 hrs · 4,505 cycles

FOUND FUEL SEEPING FROM ENG #2 FUEL FILTER DIFFERENTIAL SWITCH JAM NUT.(<P>REPLACED PACKING OF THE FUEL FILTER DIFFERENTIAL PX SW ON ENG 2, AND CHECKED NO LEAK FOUND IAW AMM 73-34-01.</P>)

Part: PITOT TUBE — WARNING MESSAGE (FIRST OFFICER'S) · airframe 16,267 hrs · 4,493 cycles

F/O PITOT EICAS UPON RIGHT ENGINE START.(<P>SERVICEABLE R/H UPPER PITOT/STATIC PROBE FITTED IAW AMM 34-11-01-409-017 REV 128. SUBSEQUENT PITOT/STATIC LEAK TEST C/W ON FO'S SYSTEM IAW AMM 34-11-00-862-045 REV 128, ALL OPS NOW NORMAL.<BR /></P>)

Part: INLET — CRACKED (NR 1 ENGINE) · airframe 16,255 hrs · 4,490 cycles

FOUND ENG 1 INNER INLET COWL RIVET AREA CRACK (0.5" X 0.5") AT SIX O'CLOCK POSITION;REMOVED AND REPLACED L ENG INLET COWL IAW AMM 71-11-01. TAI DUCT LEAK CHECK SATISFACTORY.

Part: SENSOR — MALFUNCTIONED (LT ENGINE) · airframe 16,041 hrs · 4,427 cycles

FOUND L/H ENG T25 SENSOR, CHANNEL A BLANK DURING ENGINE RUN.(<P>REMOVED AND REPLACED SENSOR IAW AMM 73-21-02-024-010 AND AMM 73-21-02-424-009 REV. 128. PERFORMED TEST NO.11 (EEC) STATIC TEST AND RESULT WAS SATISFACTORY IAW AMM 71-00-00-725-268 REV. 128.&NBSP;</P>)

Part: SKIN — CRACKED (RWS 995) · airframe 16,041 hrs · 4,427 cycles

CRACK - PFM SB AP 767-57-010 R12, FOUND RH WING LOWER SKIN HAD CRACK, NEAR WS 995, STR L - 9.5.(<P>ACCOMPLISHED J/C NO. 6757A088 PART 1-2, AND PART 4 REV.1. JOB COMPLETED AND CONDITION CHECKS NORMAL.&NBSP;</P><P><BR DATA-MCE-BOGUS="1" /></P><P>NOTE: CRACK LENGTH: 1.16", 1.02"</P>)

Part: CONTROLLER — MALFUNCTIONED (LT A/C PACK) · airframe 15,902 hrs · 4,410 cycles

LEFT PACK OFF LIGHT OCCURRED DURING T/O ROLL UNTIL 80 KNOTS AND DURING DESCENT BELOW 8000 FEET. REMOVED AND REPLACED LEFT PACK TEMP CONTROLLER AND BITE TEST OK PER AMM 21-51-14/401. LEFT PACK OPERATION NORMAL. REMOVED AND REPLACED LEFT PACK FLOW CONTROL AND SHUTOFF VALVE. OPS CHECK NORMAL WITH ENGINE HIGH POWER RUN (N1 95%) IAW AMM 21-51-00/401. CHECKED L-PTC BITE AND NO FAULTS FOUND. PRIMARY AND SECONDARY HEAT EXCHANGER CLEAN AND NO DAMAGE FOUND IAW FIM 21-51 FT 845, CHECKED WIRING, FLOW CONTROL VALVE, AND FLOW CONTROL CIRCUIT. NO DEFECTS FOUND. LEFT FLOW CONTROL VALVE WAS REMOVED AND REPLACED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 15,892 hrs · 4,409 cycles

L PACK TRIPPED WITH L PACK OFF EICAS MSG. PACK RESET ITSELF BEFORE QRH PROCEDURES WAS ADDRESSED.(<P>ACCOMPLISHED OPS CHECK AND FOUND L PACK WORKS NORMAL IAW&NBSP;AMM 21-00-00.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 15,882 hrs · 4,408 cycles

L PACK TRIP AND EICAS MSG. RESET PACK AND IT TRIPPED AGAIN, OPS OK IN STBY.(<P>L AND R PACK TEMP CONTROLLERS INTERROGATED, NO FAULTS EVIDENT, TESTED OK PER AMM 21-62-00. NO FAULTS EVIDENT WITH ZONE TEMP CONTROLLER, TESTED OK PER AMM 21-61-00.</P>)

Part: BOOT — LEAKING (DUCT) · airframe 15,542 hrs · 4,367 cycles

DUCT BOOTS HAS AIR LEAK FROM APU SURGE BLEED VLV EXH SIDE.(<P>REMOVED AND REPLACED DUCT BOOTS AT APU SURGE BLEED VLV EXH SIDE AND LEAK CK OK IAW AMM 49-11-00-201.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (UTILITY BUSS) · airframe 15,501 hrs · 4,362 cycles

ENROUTE: L & R UTIL BUS EICAS MESSAGE. CLEARED AFTER QRH PROCEDURE. ACCOMPLISHED BPCU BITE TEST PER AMM 24-21-00-501. FOUND NO FAULTS.

Part: CONTROLLER — MALFUNCTIONED (BLEED AIR SYS) · airframe 15,352 hrs · 4,342 cycles

DURING CLIMB, "R ENG HPSOV" CAUTION MESSAGE INDICATED, COMPLIED WITH QRH. &NBSP;(<P>ITEM DEFERRED TO MEL 36-11-02-02. MAINT PROCEDURE COMPLIED WITH. NOTIFIED MCC, PLACARDS INSTALLED, MDDR 115328.</P><P>LP 924200 - M4: PERFORMED AIR SUPPLY BITE TEST. REMOVED AND REPLACED RT ENGINE HPC PER AMM 36-11-08. ENGINE RUN OK PER AMM 71-00-00. MDDR 115328 CLOSED, PLACARD REMOVED AND MCC NOTIFIED.&NBSP;<BR /></P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 15,290 hrs · 4,311 cycles

R ENG FIRE LP 1 STATUS MSG. (<P>PLACED OM MDDR 114591 PER MEL 26-11-01-01.</P><P>LP 924163 - M11: PFM ENG FIRE DETECTION SYSTEM OPERATIONAL TEST AND FOUND CONDITION SATISFACTORY IAW AMM 26-11-00-715-001 REV. 127. &NBSP;CLOSED&NBSP;MDDR 114591 AND MCC NOTIFIED.</P>)

Part: WIRE HARNESS — DEFECTIVE (FUEL SYSTEM) · airframe 15,246 hrs · 4,300 cycles

IN CLIMB OUT, CTR L PUMP EICAS MSG, COMPLIED W/ QRH.(<P>DUE TIME MEL 28-22-02A CAT 'C' APPLIED, DMI 114158 RAISED. MAINT PROC CARRIED OUT.</P><P>LOG PAGE 624156:PER WDM 28-22-12 &AMP; SWPM 20-10-15/ 20-30-12 RPL WIRE BUNDLE W 444-402B/R/Y/G-14. PER WDM 28-22-12 PFM WIRING CHK FROM D17302P TO D2802 &AMP; PER MM 20-10-21 BOUNDING CHK NML. PER MM 28-31-00 CTR LEFT FUEL PUMP OPERATIONAL TEST NML &AMP; MDDR # 114158 CLZ, PLACARD RMV. MP REVERSED&NBSP;</P><P>MZ @ 13:08Z</P>)

Part: OXYGEN MASK — MALFUNCTIONED (CAPTAIN'S) · airframe 15,156 hrs · 4,290 cycles

CAPTAIN`S OXYGEN MASK DOES NOT WORK PROPERLY. WHEN INHALING, OXYGEN COMES OUT IN SHORT BURSTS, NOT A STEADY FLOW. REMOVED AND REPLACED OXYGEN MASK IAW AMM 35-11-51, AND CHECKED OK.

Part: GUIDE VANE — MALFUNCTIONED (APU) · airframe 15,033 hrs · 4,274 cycles

APU BLEED VALVE EICAS MESSAGE. REMOVED AND REPLACED APU INLET GUIDE VANE, ACTUATOR BLEED SYSTEM OPS CHECK NORMAL PER AMM 49-52-02.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 14,974 hrs · 4,244 cycles

STATUS MSG "R ENG HPSOV". (<P>UNABLE TO DUPLICATE. R ENG HPSOV SYSTEM GND CHECKED OK IAW AMM 36-11-00.</P><P>LP 954853 - M3: BITE AIR SUPPLY MODULE IAW FIM 36-10 FT 843, FOUND NO FAULTS. INSPECTION AND MANUAL CRANKING R ENGINE HPSOV FOUND SATISFACTORY IAW AMM 36-11-07. INSPECTION OF R ENG AIR SUPPLY CONTROL CARD ASSY NORMAL IAW AMM 36-11-12. AIR SUPPLY MODULE BITE, NO FAULT AFTER POWER UP CHECK. A/C OK FOR SERVICE.&NBSP;</P><P>LP 954857 - M2: BITE AIR SUPPLY MODULE IAW FIM 36-10 FT 833, NO FAULT.&NBSP; WIRING CHECK HPSOV IAW WDM 36-11-62 AND 36-23-21. HPC POS SW NML, HPSOV V347 TO PC CARD AND BITE MODULE, HPC M7191 TO PC CARD AND BITE MODULE, WIRING CHECK NORMAL IAW AMM 36-11-12 AND 36-23-01. PERFORMED ENGINE RUN UP CHECK, HPSOV FUNCTION NORMAL IAW AMM 71-00-00.</P>)

Part: CONTROLLER — MALFUNCTIONED (BLEED AIR SYS) · airframe 14,953 hrs · 4,234 cycles

R ENG HPSOV STATUS MESSAGE.(<P>TRANSFER TO MDDR #112094 AS PER MEL 36-11-02-02. DEACTIVATED R ENG HPSOV AND MAINT ACTION COMPLIED.</P><P>LOG PAGE 917090: IAW FIM 36-10 FT 833 HPSOV THUMB TEST IS 46 SEC TO CLOSE. REACTIVE HPSOV, PERFORM WIRING CHECK HPSOV PIN 2 HPC PIN 6 TO E3-1 GND OK. REMOVED AND REPLACED HPC &AMP;&NBSP;PERFORM ENG RUN UP, COND NML IAW AMM 36-11-08 AND 71-00-00.&NBSP; MDDR 112094 CLOSED.&NBSP;</P>)

Part: CONNECTOR — DIRTY (RT ENGINE) · airframe 14,902 hrs · 4,228 cycles

R ENG CONTROL STATUS MSG(<P>R PIMU SHOW T25 SENSOR DISAGREE MSG&NBSP; 352-15A/B ,155-15 A/B CLEANED UP CONNECTOR OF T25 A/B THEN T25 INIDCATION CHECK PER AMM 73-21-02 -401 IAW AMM 71-00-00-501 R ENG IDLE RUN CHECK OK FOUND NO MSG</P>)

Part: SHUTOFF VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 14,883 hrs · 4,226 cycles

R HPSOV EICAS DURING LEVEL OFF. COMPLIED WITH QRH.&NBSP; R HPSOV STATUS ON FOR DURATION OF FLIGHT.(<P>BLEED MONITOR SHOW HPSOV WIRE FAULT ITEM DEFER PER MEL 36-11-02-02 CAT C. MDDR 111712.</P><P>REF LOG PAGE 917070 ITEM 4; RIGHT HPSOV REPLACED, LEAK CHECK AND FUNCTIONAL CHECK C/OUT IAW AMM 36-11-07-024-001-001 AND AMM 36-11-07-424-016-001. NIL DEFECTS DMI CLEARED&NBSP;</P><P>REF LOG PAGE 917070 ITEM M5; RIGHT ENGINE HPSOV ELECTRICALLY RE CONNECTED, BONDING CHECK C/OUT, RIGHT ENGINE HPC RE CONNECTED AND AIR SUPPLY MODULE BITE C/OUT PER AMM 36-11-07-024-001-001. ALL OPS SYSTEM INDICATION NORMAL.&NBSP;</P>)

Part: CONNECTOR — DIRTY (BLEED AIR SYS) · airframe 14,833 hrs · 4,220 cycles

APU BLEED VAL EICAS MSG.(<P>APU BLEED VLV ELEC CONNECTOR CLEANED &AMP; VLV CYCLED IAW AMM 36-11-10, OPS CHECK NORMAL.</P>)

Part: CDU — INOPERATIVE (THRUST REVERSER) · airframe 14,697 hrs · 4,163 cycles

FOUND #1 ENG R/H SIDE T/R CDU INOP.(<P>REMOVED #1 ENGINE R/H SIDE T/R CDU IAW AMM 78-31-21-004-001-H00 REV: 126. SWAPPED #1 ENG R/H SIDE T/R POSITION FEEDBACK TRANSDUCER IAW AMM 78-36-03-004-001-H00/404-008-H00 REV: 126. INSTALLED #1 ENG R/H SIDE T/R CDU IAW 78-31-21-404-035-H00 REV: 126. C/W THE T/R CDU OPERATIONAL TEST AND CONDITION CHECKS NORMAL IAW AMM 71-00-00-995-229-H03 REV: 126.&NBSP;<BR /></P>)

Part: RELAY — MALFUNCTIONED (STARTER) · airframe 14,235 hrs · 4,047 cycles

RH STARTER CUTOUT AND RH ENG STARTER TURN ON IN FLIGHT(<DIV>1-IAW AMM 12-22-00&AMP;80-11-21 CHG RH ENG STARTER AND STARTER IND. ALL COND CHK NML&NBSP; 2- REF WDM 80-11-21 PG 4 &AMP; 31-31-22- PG 6 CHK CONTINUITY &AMP; INSULATION BETWEEN RELAY K666 SOCKET C3/D3 &AMP; CONNECTOR D10970 ON RH ENG START VLV SOCKET 4 AND RELAY K666 SOCKET C1 &AMP; D10940 SOCKET 1, ALL CHK NML.&NBSP; 3- RPL RELAY K666 AND PERFORMED RH ENG IDLE RUN TWICE FOR BOTH CHANNELS A&AMP;B RESULT NML&NBSP; (NOTE: ECM 2019P-781 ACCOMPLISHED)</DIV>)

Part: RELAY — MALFUNCTIONED (START CONTROL) · airframe 14,207 hrs · 4,044 cycles

RH ENG STARTER EICAS MSG DUR LAST HR OF FLT - SELECTOR IN AUTO(<P>R/H ENG START CONTROL RELAY K666 REPLACED AND TESTED&NBSP; SYSTEM TEST OK&NBSP; IAW AMM 80-11-01</P>)

Part: PROBE — FAILED (LEFT) · airframe 14,186 hrs · 4,041 cycles

" LEFT AUX PROBE " EICAS ON ENG START(<P>REMOVED AND REPLACED&NBSP; IAW AMM 34-11-01 PROBE HEAT TEST PASS&NBSP;</P>)

Part: WARNING LIGHT — FALSE ACTIVATION (PITOT HEAT) · airframe 14,186 hrs · 4,041 cycles

L AUX PITOT EICAS TAXIING IN(<P>OPERATIONAL TEST C/OUT WITH NO FAULT PER AMM 30-31-00-715-008<BR /></P>)

Part: START VALVE — MALFUNCTIONED (RT ENGINE) · airframe 14,084 hrs · 4,010 cycles

AFTER NORMAL ENGINE START ON RIGHT ENGINE AND DURING LEFT ENGINE START MASTER CAUTION AND EICAS R STARTER CUTOUT RECEIVED, QRH PROCEDURE COMPLIED WITH AND MESSAGE WENT AWAY, ON TAKEOFF SAME CAUTION MESSAGE, REJECTED TAKEOFF&NBSP;(<P>PERFORMED FIM FAULT CODE 80-90 05 02, REMOVED AND REPLACED RT ENGINE START VALVE IAW AMM 80-11-02 PERFORMED ENGINE RUN CHECK, SATISFACTORY NO MESSAGE&NBSP;</P>)

Part: CIRCUIT CARD — LOOSE (FIRE WARNING) · airframe 14,084 hrs · 4,010 cycles

R ENGINE FIRE LP1&NBSP; STATUS MSG APPEAR ON GROUND.&NBSP;(<P>TRANSFER TO MDDR # 106044 PER MEL 26-11-01-01 CAT C.&NBSP;PERFORMED FIM 26-11 F/T 804 FOUND AVOLS CARD M683 LOOSE MAKE SURE RESISTANCE BETWEEN PIN / 20 AND 21 0N M68 IS 11.7 OHM INSULATION BETWEEN PIN 18 AND 21 IS 2.47 OHM AND PIN 18 AND 20 2.64 / OHM WITHIN TABLE B LIMITATION REINSTALL FIRE DETECTION CARD M683 FIRE TEST NORMAL IAW AMM / 26-11-01-01 MDDR CLOSED PLACARD REMOVED.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 14,075 hrs · 4,009 cycles

CARGO TRIM AIR STATUS MESSAGE APPEARED DURING FLT.(<P>RESET CB AND MESSAGE CLEARED IAW FIM 21-28 TASK 801.<BR /></P>)

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 13,989 hrs · 3,985 cycles

R ENG FIRE LP 1 STATUS MSG. PERFORMED ENG FIRE DET SYS OPS TEST AND PASSED . MSG CLEARED IAW AMM 26-11-00.

Part: WARNING LIGHT — FALSE ACTIVATION (STARTER) · airframe 13,840 hrs · 3,952 cycles

" R STARTER CUTOUT" EICAS MSG DISPLAYED NUMBER OF TIMES INFLIGHT. ENG START SUCCESSFUL I AUTO, VALVE LIGHT NEVER ILLUMINATED(<P>PER FIM FAULT CODE 80 90 05 52, RIGHT ENGINE START VALVE REPLACED AND TESTED IAW AMM 80-11-02<BR /></P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (RT ENG FIRE LOOP) · airframe 13,590 hrs · 3,896 cycles

R ENG FIRE LP 1 STATUS MESSAGE DISPLAYED&NBSP;(<P>ENG FIRE / OVHT SYSTEM PASS &AMP; MSG ERASED PER AMM 26-11-00</P>)

Part: CONTROL PANEL — DEFECTIVE (COCKPIT) · airframe 13,395 hrs · 3,827 cycles

OUTFLOW VALVE INDICATION INOP. R&R PRESS SEL PANEL, OPS CHECK OK IAW AMM 21-31-01.

Part: WARNING MESSAGE — ILLUMINATED (CARGO FIRE DET) · airframe 13,315 hrs · 3,787 cycles

DURING PRE FLIGHT CHECK STATUS MSG MN CARGO LOOP 2(<P>IAW MEL 26-16-02-01 CAT C TRANSFERRED TO MDDR 100167 ,, BEFORE DEPARTURE TO VERIFY REMAINING DETECTORS OPERATE NORMAL ..OPS CHECK NORMAL.</P>)

Part: CONNECTOR — DIRTY (APU) · airframe 13,280 hrs · 3,769 cycles

STATUS MESSAGE, APU OIL QTY. CLEANED & SECURED OIL TXMTR PLUG AND APU OPERATIONAL CHKS OK IAW AMM 49-74-00.

Part: PUMP — FAILED (CENTER FUEL CELL) · airframe 13,031 hrs · 3,703 cycles

AT TOP OF CLIMB, RECEIVED A LT CTR FUEL PUMP ADVISORY MESSAGE. COMPLIED WITH QRH. REMOVED AND REPLACED FUEL PUMP, AND OPS CHECKED OK IAW AMM 28-22-05-401.

Part: SENSOR — FAULTY (NR 1 ENGINE) · airframe 12,914 hrs · 3,678 cycles

ENG FUEL SUCTION FEED TEST, ECS MSG SHOW" L ENG EEC C2". IAW FIM 71-01 FAULT TREE810 REV124 FIM 71-01 TASK 143 REV124 AND WDM 71-51-51 REV16 PERFORM FIMU BITE PROCEDURE AND WIRING CONTINUITY CHECK 2. IAW 73-21-02-024-010 REV124 AND AMM 73-01-02-424-099 REV124 RPL CJT SENSOR. 3IAW AMM 71-00-00-725-268 REV124 PERFORM EEC STATIC TEST. RESULT NORMAL.

Part: FUEL LINE — DAMAGED (NR 1 ENGINE) · airframe 12,914 hrs · 3,678 cycles

FOUND NR 1 ENG UPPER NR 1 FUEL LINE DAMAGE. IAW AMM 28-22-07-004-017 AND AMM 28-22-07-404-008 REV 126 RPL NR 1 ENG UPPER NR 1 FUEL LINE IAW 28-22-07-796-001 REV 1 24. PFM NR 1 ZNG FUEL LINE CHECK RESULT, ALL CHK NML AND JOB COMPLETED.

Part: NOSE COWL — CORRODED (NR 1 ENGINE) · airframe 12,917 hrs · 3,680 cycles

CORROSION EXTERNAL SURFACE NR 1 ENG NOSE COWL INNER BARREL FACE TO ENG VIEW NEAR 7 O'CLOCK. IAW AMM 71-11-004-002 AND AMM 71-11-01-404-005 REV124 REPLACE NR 1 ENG INLET COWL.

Part: RIVET — LOOSE (NR 1 COWLING) · airframe 12,917 hrs · 3,680 cycles

LOOSEN RIVET NR 2 ENG INLET COWL AFT BULKHEAD 6'OCLOCK POSITION TO PLATE. REMOVE DAMAGE RIVETS IAW SRM 51-40-02 REV 71. INSTALL NEW PARTS IAW SRM 51-40-02 REV 71 CMM IPC 71-11-16 REV 45. JOB COMPLETED AND COND CHK NML.

Part: RIVET — WORN (NR 1 COWLING) · airframe 12,914 hrs · 3,678 cycles

WORN RIVET, NR 1 ENG RT CORE COWL AFT UPPER SIDE WEAR STRIP. RMV DAMAGE PART IAW SRM 51-40-02 REV 71. INSTALL NEW PART IAW SRM 51-40-02 REV 71 AND CMM 71-13-24 REV 43. JOB COMPLETED AND COND CHK NML.

Part: RIVET — LOOSE (NR 2 COWLING) · airframe 12,917 hrs · 3,680 cycles

LOOSEN RIVET NR 2 ENG LT CORE COWL INNER SURFACE T/E UPPER SIDE WEAR STRIP. REMOVE LOOSEN RIVET IAW SRM 51-40-02 REV 71. INSTALL RIVET IAW SRM 51-40-02 REV71 AND CMM IPC 71-13-23 REV 40. JOB COMPLETED AND COND CHK NML.

Part: ADAPTER — WORN (NR 1 COWLING) · airframe 12,917 hrs · 3,680 cycles

WORN ADAPTER AND BRACKET NR 1 ENG RT CORE COWL HOLD-OPEN ROD SUPPORT. REMOVED DAMAGE PARTS IAW SRM 51-40-02 REV 71. INSTALL NEW PARTS IAW SRM 51-40-02 REV 71 AND CMM IPC 71-13-24 REV 43. JOB COMPLETED AND COND CHK NML.

Part: COWLING — ERODED (NR 1 ENGINE) · airframe 12,914 hrs · 3,678 cycles

EROSION, LE, NR 1 ENG LT FAN COWL. REPAIR DAMAGE AREA IAW CMM 21-13-21 REPAIR NR 9 REV 42. CHECK CONDITION WAS SATISFACTION.

Part: SPINNER — DAMAGED (NR 2 ENGINE) · airframe 12,917 hrs · 3,680 cycles

PEEL OFF-PAINTING NR 2 ENGINE SPINNER CORE EXTERNAL SURFACE. CLEAN UP SURFACE AND APPLY THE COATING IAW ESM 72-21-10 REPAIR006 REV 87. COND CHK RESULT SATISFY.

Part: BRACKET — WORN (LT COWLING) · airframe 12,911 hrs · 3,677 cycles

WORN BRACKET, NR 2 ENG LT CORE COWL HOLD OPEN ROD SUPPORT. RMV DAMAGE PARTS IAW SRM 51-40-02 REV71. INSTALL NEW PARTS IAW SRM 51-40-02 REV 71 CMM IPC 71-13-23 REV 40. JOB COMPLETED AMD COND CHK NML.

Part: TRANSMITTER — DEFECTIVE (FUEL SYSTEM) · airframe 12,917 hrs · 3,680 cycles

RT ENG FUEL PRESSURE INDICATOR ALWAYS SHOWS 200. IAW AMM73-33-01-002-001 AND AMM 73-33-01-402-007 REV124 PRL ENG NR 2 FUEL PRESSURE TRANSMITTER IAW AMM 71-00-00795-228 REV124. PFM TEST AND ALL CHK NML.

Part: LINER — DEBONDED (NR 2 ENGINE) · airframe 12,917 hrs · 3,680 cycles

DISBOND LINER SEGMENT NR 2 ENG FAN CASE FWD OUTER LINER SEGMENT AT 8 O'CLOCK POSITION 1. REPAIR THE BACKSHEET DISBOND AREA AND CURED THE ADHESIVE IAW EM72-22-02 REPAIR 004 REV 87. REPLACED THE BUMPER AND CURE THE ADHESIVE IAW EM 72-22-02 REPAIR 001 REV 87. FINAL INSPECTION RESULT SATISFACTORY.

Part: PRECOOLER — DAMAGED (BLEED AIR SYS) · airframe 12,917 hrs · 3,680 cycles

FOUND NR 1 ENG PRECOOLER OUTLET PORT F2N C FLAKE AWAY. IAW AMM 36-11-15-004-003 AND AMM 36-11-15-404-020 REV 124 REPLACE NR 1 ENGINE PRECOOLER IAW AMM 36-11-15-404-020 REV 124. PFM PRECOOLER TEST AND ALL CHK NML.

Part: BRACKET — CHAFED (NR 1 COWLING) · airframe 12,917 hrs · 3,680 cycles

CHAFING BRACKET NR 1 ENG LT CORE COWL HOLD OPEN ROD FORWARD SIDE. REMOVE DAMAGE PARTS IAW SRM 51-40-02 REV 71. INSTALL NEW PARTS IAW SRM 51-40-02 REV 71 AND CMM IPC 71-13-23 REV 40. JOB COMPLETED AND COND CHK NML.

Part: COWLING — ERODED (NR 2 ENGINE) · airframe 12,914 hrs · 3,678 cycles

EROSION SURFACE. NR 2 ENG RT FAN COWL L/E. REPAIR DAMAGE AREA IAW CMM 71-12-22 REPAIR NR 8 REV 43 2. CHECK CONDITION WAS SATISFACTION.

Part: RESTRAINT — BROKEN (AC BAY) · airframe 12,916 hrs · 3,677 cycles

BROKEN FLEXIBLE RESTRAINT AT BOTH AIR CONDITIONING PACK HEATER EXCHANGER DUCT COUPLING TOTAL 3EA. IAW AMM 21-51-02-404-019 REV 1 24 AND J/C A-21-017-01 INSTALL HEAT EXCHANGER AND RPL CABLE TOTAL 3 EA. CONDITION CHECK NORMAL AND JOB COMPLETED.

Part: RUB STRIP — WORN (NR 1 COWLING) · airframe 12,911 hrs · 3,677 cycles

WORN WEAR STRIP, NR 1 ENG LT CORE COWL UPPER AFT SIDE. RMV DAMAGE PART IAW SRM 51-20-02 REV 71. INSTALL NEW PART IAW SRM 51-40-02 REV 71 AND CMM 71-13-23 REV 40. JOB COMPLETED AND COND CHK NML.

Part: BOLT — DAMAGED (OUTFLOW VALVE) · airframe 12,911 hrs · 3,677 cycles

FOUND CABIN PRESSURE OUTFLOW VALVE CONNECTING ROD BOLT AND NUT DAMAGE AT BULK CARGO. IAW AMM 21-31-03-002-066 REV1 24 RPL THE BOLT AND NUT. CONDITION CHECK NORMAL AND JOB COMPLETED.

Part: PLATE — WORN (NR 1 COWLING) · airframe 12,917 hrs · 3,680 cycles

WORN PLATE NR 1 ENG LT CORE COWL AFT LOWER CORNER BRACKET. REMOVE DAMAGE PART IAW SRM 51-40-02 REV 71. INSTALL NEW PART IAW SRM 51-40-02 REV71 AND CMM 71-13-23 REV 40. JOB COMPLETED AND COND CHK NML.

Part: COWLING — BULGED (NR 2 ENGINE) · airframe 12,911 hrs · 3,677 cycles

BULGE SURFACE NR 2 ENG INLET COWL INNER BARREL T/E FACE TO ENG VIEW AT 8 O'CLOCK POSITION. IAW AMM 71-11-01-004-002 AND AMM 71-11-01-404-005 REV 124 RPL NR 2 ENG INLET COWL.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 12,878 hrs · 3,660 cycles

EICAS MSG MAIN CARGO DECK LOOP NR 2. BITE PROC FOR CARGO COMPT SMOKE DETECTIONS SYSTEM, TEST OK. PFM TEST OF THE TEST ALARM INTERFACE MODULE, ALL COND CHECK NML. NO FAULT FOUND IAW AMM 26-14-00.

Part: APU — MALFUNCTIONED · airframe 12,516 hrs · 3,497 cycles

APU INOPERATIVE. BITE TESTED THE APUC, NO FAULT FOUND IAW AMM 49-61-05. OPS TESTED THE PACKS IAW FIM 49-11 FT A08, CHECKED SURGE VALVE, FUNCTIONED NORMAL. DUCT PRESSURE NORMAL, PERFORMED ENGINE DRY MOTORING, CHECKED DUCT PRESSURE, FOUND NORMAL IAW AMM 71-00-00.

Part: START VALVE — MALFUNCTIONED (RT ENGINE) · airframe 12,448 hrs · 3,463 cycles

RT ENGINE STARTER EICAS DISPLAYED DURING ENGINE START. ENGINE STARTED NORMAL. REMOVED AND REPLACED THE RT ENGINE START VALVE AND PERFORMED AN ENGINE RUN-UP, OPS NORMAL IAW AMM 80-11-02, AND AMM 71-00-00.

Part: STARTER — FAILED (RT ENGINE) · airframe 12,432 hrs · 3,455 cycles

DURING RIGHT ENGINE START, RT ENGINE STARTER EICAS MESSAGE ILLUMINATED, THEN OFF. R & R THE RT ENGINE STARTER & PERFORMED AN ENGINE RUN, TEST CHECKED OK IAW AMM 80-11-01.

Part: CONNECTOR — DIRTY (STARTER) · airframe 12,423 hrs · 3,450 cycles

DURING RIGHT ENGINE START, A RT ENGINE STARTER EICAS MESSAGE ILLUMINATED, THEN EXTINGUISHED. CLEARED & SECURED THE ELECTRICAL CONNECTOR TO THE RT ENGINE START VALVE. STARTING OPERATIONAL TESTED OK.

Part: ANTI-ICE SYSTEM — MALFUNCTIONED (ENGINE) · airframe 12,404 hrs · 3,445 cycles

ENGINE ANTI-ICE TURNS ON IN AUTO MODE EVEN WHEN THERE IS NO VISUAL INDICATION OF ICE, NOR SAY ICING CONDITION. SUSPECTED ICE DETECTION SYSTEM INTERMITTENTLY AT FAULT. DDG 30-80-01-02 PO APPLY FOR ICE DETECTION SYSTEM PRIMARY INOPERATIVE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 12,372 hrs · 3,440 cycles

ENGINE ANTI-ICE CAME ON AT FL130 CLEAR SKY TAT18 SWITCH POSITION IN AUTO. PERFORM ICE DETECTION SYSTEM OPERATIONAL TEST CONDITION NORMAL, PERFORM ENGINE TAI VALVE INSTALL TEST CONDITION CHECK NORMAL IAW AMM30-81-00 AND 30-21-03.

Part: IDG — LEAKING (RIGHT) · airframe 11,977 hrs · 3,338 cycles

RIGHT GENERATOR DRIVE LIGHT. REMOVED AND REPLACED THE IDG, IDG OIL LEVEL CHECK AND SERVICE CONDITION NORMAL. OIL SYSTEM CHECK, NO LEAKS FOUND. PERFORMED RT ENGINE POWER PLANT TEST, FOUND NORMAL IAW AMM 24-11-01, AMM 71-00-00, 71-71-00, 12-13-03, AND AMM 24-11-00.

Part: VALVE — MALFUNCTIONED (LT A/C PACK) · airframe 11,434 hrs · 3,200 cycles

LEFT PACK INOPERATIVE REMOVED AND REPLACED THE LT PACK FLOW CONTROL AND SHUT OFF VALVES. LEFT PACK OPS CHECKED NORMAL IAW AMM 21-51-01/401.

Part: VALVE — FAILED (LT A/C PACK) · airframe 11,430 hrs · 3,198 cycles

AS THE LEFT PACK WAS ON, DUCT PRESSURE DROPPED TO 10 PSI, RT BLEED SWITCHED OFF. REMOVED AND REPLACED THE LT PACK FLOW CONTROL AND SHUTOFF VALVES, LT PACK OPS CHECKED NORMAL, PTC BITE CHECKED OK IAW AMM 21-51-1/401.

Part: DETECTOR — INOPERATIVE (MAIN CARGO) · airframe 11,023 hrs · 3,057 cycles

MAIN DECK CARGO FIRE LOOP 2 INOPERATIVE IAW FIM 26-14 BITE PROCEDURE CARGO SMOKE DETECTION SYS. REPLACED MAIN DECK CARGO LOOP 2 DETECTOR AND OPERATIONAL CHECK NO FAULTS FOUND.

Part: CIRCUIT CARD — MALFUNCTIONED (CARGO LOOP) · airframe 10,956 hrs · 3,023 cycles

STATUS MESSAGE FOR MN CARGO LOOP 2. PEFORMED AN ENGINE, APU, AND CARGO FIRE, OVERHEAT TEST. NO OTHER MESSAGES APPEARED. R & R THE AFLOTS CARD IAW AMM 26-14-00, OPERATIONAL TEST, MAIN DECK CARGO BAY SMOKE DETECTION SYS TEST PASSED. NO FAULT FOUND.

Part: APU — FAULTED · airframe 10,905 hrs · 3,013 cycles

APU FAULT ON LANDING. DID NOT ATTEMPT SECOND START. ACCOMPLISHED ECU BITE TEST & SELF TESTED OK. PERFORMED ACTUAL CHECK NORMAL, APU START NORMAL IAW AMM 49-61-05-742-045.

Part: SMOKE DETECTOR — MALFUNCTIONED (MAIN CARGO) · airframe 10,886 hrs · 3,011 cycles

STATUS MESSAGE FOR THE MAIN CARGO LOOP 2. PERFORMED ENGINE, APU, AND A CARGO FIRE-OVERHEAT TEST. NO OTHER MESSAGE APPEARED. REPLACED WITH NEW MAIN DECK CARGO ZONE 2A SMOKE DETECTOR THEN GROUND OPS CHECKED OK IAW AMM 26-14-01/401.

Part: EADI — FAILED (CAPTAIN'S) · airframe 10,811 hrs · 2,973 cycles

DURING CRUISE, CAPTAIN`S ADI WENT BLANK, STRONG ODOR. ADI CIRCUIT BREAKER TRIPPED. ODOR WENT AWAY. IAW AMM TASK 05-51-06 PERFORMED VISUAL CHECK ELECT WIRE AND NO TROUBLE FOUND. REMOVED AND REPLACED EADI ON CAPTAIN`S SIDE THEN OPS CHECKED OK IAW AMM 34-22-01/401.

Part: JUMPER — BROKEN (NR 1 ENGINE) · airframe 10,782 hrs · 2,958 cycles

FOUND GROUND JUMPER AND RETAINING CABLE BROKEN ON NR 1 ENGINE HPSOV IAW AMM TASK 70-50-00-912-001-H00, REV 12. REPLACED THE GROUND JUMPER AND RETAINING CABLE AND CONDITION CHECKED NORMAL.

Part: APU — SHUTDOWN · airframe 10,653 hrs · 2,929 cycles

WHILE SITTING AT THE GATE, THE APU FAILED. PERFORMED FIM 49-11-0-815, APU BITE CHECKED OUT, NO FAULTS FOUND. SUCCESSFULL START IAW AMM 49-11-00-802.

Part: PITOT TUBE — MALFUNCTIONED (FIRST OFFICER'S) · airframe 10,554 hrs · 2,890 cycles

F/O PITOT EICAS STATUS MESSAGE, AFTER PUSH BACK. REMOVED AND REPLACED THE F/O PITOT PROBE AND OPS CHECKED OK, COULD NOT DUPLICATED FAULT IAW AMM 34-11-01/401.

Part: WARNING MESSAGE — FALSE ACTIVATION (BUSS) · airframe 10,412 hrs · 2,865 cycles

AT FL 180 DURING DECENT, BOTH UTILITY BUSS EICAS MESSAGES CAME ON. BOTH GENERATORS NORMAL. RESET BOTH BUSSES IAW QRH, ALL RETURNED NORMAL IAW FIM 24-FAULT CODE 72, FIGURE 712. FUNCTION NORMAL IAW AMM 24-51-05, UTILITY BUSS TEST & FUNCTION NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENGINE EEC) · airframe 10,384 hrs · 2,851 cycles

LEFT ENGINE EEC, C1 EICAS MESSAGE. CHECKED THE PIMU 353, 14A FMV FEEDBACK ,353 16A, VBV F/B,353 18A, VSV F/B, 354 15A CROSS LINK , THEN LEFT ENGINE ACTUATOR TEST PASSED IAW AMM 71-00-00-501 NO MESSAGE FOUND.

Part: WARNING LIGHT — FALSE ACTIVATION (UTILITY BUSSES) · airframe 10,369 hrs · 2,843 cycles

ON APPROACH AT 1500 FT, BOTH UTILITY BUSSES OFF. AFTER LANDING, STARTED APU AND PERFORMED NON-NORMAL PROCEDURE. BOTH UTILITY BUSSES RESET. BPCU SHOWED NO FAULTS, CHECKED IDG, BOTH OIL QTY CHECKED OK IAW AMM 24-22-00.

Part: CONTROL VALVE — FAILED (A/C PACK) · airframe 10,196 hrs · 2,780 cycles

LOW DUCT PRESSURE NOTED WITH BOTH PACKS RUNNING, PACK OUTPUT PRESSURE LOW AND COCKPIT TEMP HIGH&NBSP;(<P>MEL 36-11-04 RAISED & DDG COMPLIED WITH. REACTIVATED APU AIR SUPPLY SHUTOFF VALVE TO OPEN. PFM APU STARTING & OPS FOR TROUBLESHOOTING AND APU SURGE CONTROL VALVE STUCK IN OPEN POS. REPLACED THE SURGE CONTROL VALVE. PEFORMED APU START, OPS CHECKED PACK DUCT PRESSURE, ALL NORMAL. PFM APU CONTROL UNIT BITE TESTED OK IAW AMM 49-61-05, 49-11-00 &49-61-05. 3.

Part: APU — SHUTDOWN (APU BAY) · airframe 9,917 hrs · 2,685 cycles

APU AUTOSHUTDOWN. RPL APU PER CONTROL 7018, JC71071 AND AMM 49-11-01. OPERATION CHECK OK & NO LEAK.

Part: WARNING MESSAGE — FALSE ACTIVATION (WINDOW) · airframe 9,649 hrs · 2,617 cycles

EICAS MESSAGE FOR THE RT WINDOW. CAPTAIN, STATED MESSAGE WAS GONE AFTER RT WINDOW HEAT SWITCH CYCLED. BITE LT & RT WHCU, NO FAULTS & CHECKED WINDOWS, CONDITION NORMAL IAW AMM 56-11-00. FIM TASK 30-41 TASK 801. CHECK CONDITION SATISFACTORY.

Part: SKIN — DENTED (NR 2) · airframe 9,632 hrs · 2,609 cycles

NR 2 ENG NOSE COWL INNER BARREL LOWER SIDE IS DENTED. CUT OUT THE DENT SKIN DIA: 0.5" AT 5 O' CLOCK POS OF LOWER ACOUSTIC PANEL AND CLEAN INSTALLED THE SPACER INTO THE HOLE CURED AT 250 FAHRENHEIT FOR 2 HOURS. FILLED THE HOLE WITH ADHESIVE CURED AT 200 FAHRENHEIT FOR ONE HOUR IAW SRM 54-15-01-2R-3 REPAIR 3 REV 67. CHECK CONDITION WAS SATISFACTORY.

Part: GASKET — LEAKING (HEAT EXTCHANGER) · airframe 9,632 hrs · 2,609 cycles

FOUND THE NR 1 ENGINE FUEL / OIL HEAT EXCHANGER GASKET FUEL SEEPING. REPLACED THE NR 1 ENGINE FUEL / OIL HEAT EXCHANGER GASKET IAW AMM 79-21-01-024-065 REV 120 & AMM 79-21-01-424-066 REV 120. PERFORM IDLE LEAK CHECK, NO LEAKS FOUND IAW AMM 71-00-00-795-034 REV 120.

Part: STRIP — CHAFED (NR 2 COWLING) · airframe 9,632 hrs · 2,609 cycles

CHAFING NR 2 ENG RT CORE COWL INNER AFT WEAR STRIP CHAFING. REMOVED DAMAGED STRIP IAW SRM 51-40-02-0G-0 REV 67. INSTALLED NEW STRIP IAW SRM 51-40-02-0G-0 REV 67 AND CMM 71-13-24 REV43. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: ROD END — WORN (NR 2 ENGINE) · airframe 9,632 hrs · 2,609 cycles

FOUND NR 2 ENG RT 14TH STG PNEUMATIC DUCT SUPPORT LINK ROD END WORN AT BOTH SIDES. IAW AMM 70-50-00-912-001 REV 120 RPL THE NR 2 ENG RT 14TH STG PNEUMATIC DUCT SUPPORT LINK ROD END WITH SERVICEABLE PARTS AND COND CHK NORMAL.

Part: RIVET — WORN (NR 1 NACELLE) · airframe 9,632 hrs · 2,609 cycles

WORN RIVETS NR 1 NACELLE. REMOVED DAMAGED RIVETS IAW SRM 51-40-02-0G-0 REV 67. INSTALLED NEW RIVETS IAW SRM 51-40-02-0G-0 REV 67 AND CMM 71-13-24 REV 43.

Part: RECTIFIER — FAILED (APU) · airframe 9,632 hrs · 2,609 cycles

FOUND APU TRU FUNCTION FAILED. REPLACED APU START TRANSFORMER RECTIFIER UNIT IAW AMM 24-32-04-004-012, 24-32-04-404-003 REV.120. & PERFORMED TEST OF THE APU START TRU INSTALLATION, RESULT WAS SATISFACTORY IAW AMM 24-32-04-404-003 REV.120 .

Part: LINK ROD — WORN · airframe 9,632 hrs · 2,609 cycles

FOUND NR 1 ENGINE START DUCT SUPPORT LINK ROD END BEARING WORN AT 1 O'CLOCK. IAW AMM 70-50-00-912-001 REV 120 REPLACED THE NR 1 ENG START DUCT SUPPORT LINK ROD END WITH SERVICEABLE PART AND ALL CONDITION CHECK NORMAL.</P>)

Part: SUPPORT — WORN (NR 1 ENGINE) · airframe 9,632 hrs · 2,609 cycles

FOUND NR 1 ENGINE LT LPTACC MANIFOLD DUCT SUPPORT LINK WORN AT 9 O'CLOCK. IAW AMM 70-50-00-912-001 REV 120 REPLACED THE SUPPORT LINK.

Part: CLAMP — CRACKED (OIL SUMP) · airframe 9,632 hrs · 2,609 cycles

FOUND NR 1 ENGINE D SUMP OIL SUPPLY TUBE CLAMP CRACK. IAW AMM 70-50-00-912-001 REV 120 REPLACED THE ENGINE SUMP OIL SUPPLY TUBE CLAMP WITH SERVICEABLE PARTS AND ALL CONDITION CHECK NORMAL.

Part: CLAMP — DAMAGED (BLEED AIR SYS) · airframe 9,632 hrs · 2,609 cycles

FOUND ENG 2 RT HPSOV MUSCLE AIR TUBE SUPPORT CLAMP DAMAGE. IAW AMM 70-50-00-912-001 REV120 RPL ENG 2 RT HPSOV MUSCLE AIR TUBE SUPPORT CLAMP WITH SERVICEABLE PARTS AND COND CHK NML.

Part: BRACKET — CHAFED (NR 2 COWLING) · airframe 9,632 hrs · 2,609 cycles

NR 2 ENG LT AND RT CORE COWL INNER FWD SUPPORT ROD BRACKET CHAFING. REMOVED DAMAGE BRACKET SRM 51-40-02-0G-0 REV 67. INSTALL NEW BRACKET IAW SRM 51-40-02-0G-0 REV 67 AND CMM 71-13-23 REV 40 AND CMM 71-13-24 REV 43. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: CLAMP — BROKEN (A/C BAY) · airframe 9,632 hrs · 2,609 cycles

CLAMP RUBBER CUSHION ON RT AIR CONDITION BAY PNEUMATIC TUBE AREA BROKEN. REPLACED THE CLAMP IAW AMM 20-11-00-910-802 REV 120.

Part: RIVET — WORN (NR 2 NACELLE) · airframe 9,632 hrs · 2,609 cycles

NR 2 NACELLE HAS A WEAR STRIP RIVET WORN. REMOVED DAMAGE RIVET IAW SRM 51-40-02-0G-0 REV.67. INSTALLED NEW RIVET IAW SRM 51-40-02-0G-0 REV.67 AND CMM 71-13-23 REV 40.

Part: LINK — WORN (NR 2 ENGINE) · airframe 9,632 hrs · 2,609 cycles

FOUND NR 2 ENG LEFT LPT ACC DUCT SUPPORT LINK AT FWD AND AFT FLANGE UPPER SIDE WORN OUT. REPLACED IAW AMM 70-50-00-912-001 REV 120 AND ALL CONDITION CHECKED NORMAL.

Part: FILTER — DIRTY (COCKPIT TEMP) · airframe 9,495 hrs · 2,569 cycles

FLT DECK TEMP CONTROL INOPERTIVE IN MANUAL OR AUTO. CLEANED THE FLT DECK TEMP SENSOR AIR FILTER, OPS NORMAL IAW AMM 21-61-00.

Part: CONTROLLER — FAILED (PRV) · airframe 9,488 hrs · 2,566 cycles

RIGHT ENGINE BLEED OFF EICAS AFTER ENGINE START. MAINTENANCE PROCEDURES COMPLETED. REPLACED THE PRV CONTROLLER, CHECKED GOOD IAW AMM 36-11-19.

Part: VALVE — FAILED · airframe 9,396 hrs · 2,541 cycles

RIGHT ENGINE BLEED OFF CAUTION MESSAGE. NO DUCT PRESSURE ON THE RIGHT SIDE. PERFORMED TROUBLESHOOTING AND FOUND THE PRV AIR LEAK. INTERCHANGE WITH HPSOV, LOCK OUT VALVE. REMOVED AND REPLACED PRV, OPS CHECK NORMAL. REACTIVATED RT THRUST REVERSER.

Part: PRESSURE SWITCH — NOT REPORTED (CABIN PRESSURE) · airframe 9,326 hrs · 2,520 cycles

EQUIPMENT COOLING FLOW LOW. FOUND, ALTITUDE PRESSURE SWITCH. R & R IAW AMM 31-41-08, PERFORM ALTN STATIC SYST LOW RANGE LK TEST. CHECKED NORMAL IAW AMM 34-11-00.

Part: SWITCH — MALFUNCTIONED (E/E COOLING) · airframe 9,179 hrs · 2,488 cycles

E/E COOLING TEST, LEFT 5 INDICATORS DO NOT TEST. EQUIPMENT COOLING SWITCH CYCLED AND FURTHER TESTS CARRIED OUT AND PASSED IAW AMM 21-58-34.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 9,022 hrs · 2,459 cycles

CABIN ALTITUDE AUTO 2 STATUS MESSAGE. REMOVED AND REPLACED THE NRE 2 AUTO PRESSURE CONTROLLER IAW AMM 21-31-02. BITE CHECKED AND OPS CHECKED OK.

Part: CABIN PRESSURE — INOPERATIVE · airframe 9,006 hrs · 2,451 cycles

CABIN ALT AUTO 2 ADVISORY EICAS MSG. CABIN PRESS CONT 2 BIT VERIFY TEST OK PER AMM 21-31-00-705-001.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 8,958 hrs · 2,427 cycles

STATUS MSG, CABIN ALT AUTO 1. IAW AMM 21-31-02, REPLACED AUTOMATIC PRESSURE CONTROLLER 2. BITE TEST NO FAULTS FOUND.

Part: BEARING — BROKEN (LE SLAT) · airframe 8,944 hrs · 2,420,270 cycles

FOUND NR 9 SLAT TRACK BEARING BROKEN. REPLACED NR 9 SLAT TRACK BEARING AND CONDITION CHECK NORMAL IAW AMM TASK 27-81-02-024-001/424-099, REV.

Part: PILOT VALVE — FAULTY (THRUST REVERSER) · airframe 8,499 hrs · 2,420 cycles

FOUND NR 1 ENGINE T/R STATUS MESSAGE IAW AMM TASK 78-34-01-004-003-H00/404-014-H00, REV 119. REPLACED NR 1 ENGINE DIRECTIONAL PILOT VALVE AND CONDITION CK NORMAL. NR 1 ENGINE T/R SYS TEST C/W IAW AMM TASK 71-00-00-700-807-H03, REV 119.

Part: SCREW — LOOSE (NR 2 ENGINE) · airframe 8,499 hrs · 2,420 cycles

FOUND NR 2 ENGINE ACOUSTICAL LINER SEGMENT SCREW LOOSENED. RETORQUED NR 2 ENGINE ACOUSTICAL LINER SEGMENT SCREW AND CONDITION CHECK NORMAL IAW AMM 72-33-01-404-011-H00, REV 119.

Part: COMPRESSOR BLADE — DAMAGED (RT ENGINE) · airframe 8,944 hrs · 2,420 cycles

RIGHT ENGINE FAN BLADE TIP NR 34 HAS CURL. RT ENGINE FAN BLADE NR 34 TIP NO CURL, FOUND NR 33 HAS CURL, REPLACED NR 33 IAW AMM 72-31-02. OPS IAW AMM 71-00-00, VIB SURVEY CHECKED WITH IN LIMITS.

Part: SCREW — LOOSE (NR 1 ENGINE) · airframe 8,944 hrs · 2,420 cycles

FOUND NR 1 ENG ACOUSTICAL LINER SEGMENT SCREW LSN. RETORQUED NR 1 ENGINE ACOUSTICAL LINER SEGMENT SCREW AND CONDITION CHECK NORMAL IAW AMM 72-33-01-404-011-H00, REV 119.

Part: HMU — MALFUNCTIONED (RT ENGINE) · airframe 8,944 hrs · 2,420 cycles

RIGHT ENGINE CONTROL, EICAS MSG IAW AMM 73-21-14 REPLACE RT ENGINE HMU IAW AMM 71-00-00-401, CONFIGURATION 3. PFM RT ENGINE DRY MOTOR AND ECU GROUND ACTUATOR TEST AND ALL CONDITIONS SATISFACTORY, NO MSG SHOWS.

Part: EEC — MALFUNCTIONED (LT ENGINE) · airframe 8,944 hrs · 2,420 cycles

RIGHT ENGINE CONTROL, EICAS, MESSAGE DURING TAXI OUT. CHECK RT ENGINE CHANNEL B SAME DATA MISSING IN EPCS PAGE 2. REPLACED RT ENGINE, ELECTRONIC ENGINE CONTROL IAW AMM 73-21-15. PERFORMED POWER PLANT TEST NR 11 ELECTRONIC ENGINE CONTROL STATIC TEST AND NR 12. ELECTRONIC ENGINE CONTROL ACTUATOR SATISFACTORY PIMU BITE TEST, OK. PERFORMED ENGINE RUN TEST IAW AMM 71-00-00, OK.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 8,944 hrs · 2,420 cycles

REF EO 6753A341, MAIN DECK FLOOR POS, BS 620, LBL 33 SEAT TRACK CROWN LIPS DAMAGED IAW CONTROL 8017-2, EO 6753A361. REPAIR DAMAGE FLOOR TRACK STA 620 MAIN DECK, CONDITION CK SATISFACTORY IAW AMM 25-58-21.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 8,909 hrs · 2,407 cycles

STATUS MSG: WEATHER SYS STATUS MESSAGE ERASED, WEATHER SYS OPS CHECK OK IAW 34-43-00.

Part: DISPLAY — FAILED (COCKPIT) · airframe 8,713 hrs · 2,373 cycles

CAPTAIN`S CDU WENT BLANK WITH A BURNING ODOR AND SMOKE. CIRCUIT BREAKER DID NOT OPEN.

Part: IDG — MALFUNCTIONED (RT ENGINE) · airframe 8,604 hrs · 2,341 cycles

RIGHT IDG OUT TEMP AUTO EVENT AND CHECK RISING TEMP 29C. FLUSH RT IDG OIL SYS IAW 12-13-07, OIL LEAK CK NORMAL NEED FURTHER MONITOR.

Part: FILTER — DIRTY (COCKPIT TEMP) · airframe 8,576 hrs · 2,327 cycles

FLIGHT DECK TEMP CONTROL SENSOR FILTER DIRTY. IAW AMM 21-61-09, CLEANED THE SENSOR FILTER. CONDITION CHECKED SATISFACTORY.

Part: SWITCH — DEFECTIVE (AC BAY) · airframe 8,481 hrs · 2,310 cycles

LT PACK INOPERATIVE LIGHT NOT ON AT TEST. RELAMPED BUT SAME ITEM DEFERED IAW MEL 21-52-01, CAT C, MDDR 68395. R & R SW IAW AMM 33-51-00. OPS CHECK NORMAL. REPLACED LT PACK SW ASSY AND OPS CHECKED OK IAW AMM 21-51-00 INOPERATIVE LIGHT AND PACK CK NORMAL CLEARED MDDR 68395.

Part: STRUT — INOPERATIVE (RT COWLING) · airframe 8,413 hrs · 2,290 cycles

RIGHT ENGINE, LEFT FAN COWLING FWD STRUT ASSY INOPERATIVE IAW IPC 71-11-11-51, ITEM 595. REPLACED RT ENGINE, LT FAN COWLING FWD STRUT ASSY AND CHECK NORMAL IAW AMM 71-11-11-212-001.

Part: BONDING WIRE — BROKEN (NR 2 ENGINE) · airframe 8,247 hrs · 2,253 cycles

FOUND NR 2 ENGINE HPSOV JUMPER WIRE BROKEN. REPLACED JUMPER WIRE IAW AMM 70-50-00-912-001-H00, REV 118.

Part: CLAMP — BROKEN (NR 1 ENGINE) · airframe 8,247 hrs · 2,253 cycles

FOUND NR 1 ENG HPSOV SENSING TUBE SUPPORT CLAMP BROKEN. REPLACED CLAMP IAW AMM 70-50-00-912-001-H00, REV 118.

Part: STRUT — BROKEN (NACELLE DOOR) · airframe 8,247 hrs · 2,253 cycles

FOUND NR 2 LT CORE COWL HOLD OPEN ROD BROKEN. REPLACED HOLD OPEN ROD IAW AMM 70-50-00-912-001-H00, REV 118.

Part: FAN — WARNING MESSAGE (EXHAUST) · airframe 7,912 hrs · 2,199 cycles

STATUS MESSAGE FWD EQUIPMENT EXHAUST FAN. R & R FWD EQUIPMENT EXHAUST FAN IAW AMM 21-58-06-401.M OPS CHECK OK. MESSAGE DISAPPEARD.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 7,885 hrs · 2,194 cycles

SMOKE DETECTOR IN LAV ACTIVATED ON GROUND. R & R LAV SMOKE DETECTOR IAW AMM 26-13-00-904-001, OPS CHECK OK.

Part: SYMBOL GENERATOR — MALFUNCTIONED · airframe 70,830 hrs · 21,086 cycles

F/O SYMBOL GENERATOR IS NOT DISPLAYING THE "A" FOR THE WEATHER RADAR DEFECT CONFIRMED FOUND RT SYMBOL GENERATOR HAS -021. OPS SOFTWARE INSTALLED CORRECT -012 OPS SOFTWARE INSTALLED IAW AMM 34-22-00, SYMBOL GENERATOR TEST C/O IAW AMM 34-22-01. OPS SOFTWARE CHECKS OK.

Part: PROBE — SHORTED (PITOT) · airframe 7,708 hrs · 2,170 cycles

AFTER BOTH ENGINES STARTED, EICAS MESSAGE, F/O PITOT-CONFIRMED F/O PITOT COLD BY TOUCH. ALSO, CHECK USING P61 FAILED, PITOT PROBE HEAT MSG AND LIGHT, OVERHEAD PANEL ON. REMOVED PITOT PROBE AND CONFIRMED HIGH RESISTANCE. R & R F/O PITOT PROBE PERFORMED HEATER TEST AND LEAK TEST OK, IAW AMM 30-31-00 AND 34-11-00.

Part: TRANSMITTER — INOPERATIVE (APU OIL QTY) · airframe 7,574 hrs · 2,136 cycles

APU OIL QTY INOPERATIVE. REPLACED TRANSMITTER IAW AMM 49-94-04, OPS NORMAL.

Part: VALVE — MALFUNCTIONED (LT ENGINE) · airframe 7,661 hrs · 1,802 cycles

LEFT ENGINE PREVIOUS STATUS MESSAGE. LEFT ENGINE PRESSURE REGULATOR VALVE REPLACED IAW AMM 36-11-18.

Part: WARNING LIGHT — FALSE ACTIVATION (FAN) · airframe 7,106 hrs · 2,014 cycles

AFT EQ EXHAUST FAN 2 STATUS MSG. REF FIM 21-26, FAULT TREE 806. PFM AFT EQ EXHAUST FAN TEST NORMAL IAW AMM 21-26-01, CHECK AFT EQ EXHAUST FAN 1; 2 CONNECTORS AND WIRING NORMAL SSM 21-58-09, PG 101. IAW AMM 21-58-00, PFM AFT EQ EXHAUST FAN OPERATION TEST FUNCTION NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (FAN) · airframe 7,101 hrs · 2,012 cycles

AFT EQUIPMENT EXHAUST FAN 1 STATUS MSG, FOLLOWED FIM 21-26 FAULT TREE 803 ERASED MSG SYSTEM TEST OK IAW FIM 21-26-00/101 105.

Part: WARNING MESSAGE — FALSE ACTIVATION (EXHAUST FAN) · airframe 7,097 hrs · 2,010 cycles

STATUS MSG AFT EQUIPMENT EXHAUST FAN 2. RECYCLED AFT EQUIPMENT EXHAUST FAN 2 CCB, THEN EXHAUST FAN 2, CHECKED OK. ERASED STS MSG IAW AMM 21-58-00-705-123-008.

Part: TRU — SHORTED (APU) · airframe 7,095 hrs · 2,009 cycles

APU FAILED TO START, 3 ATTEMPTS. FOUND APU T/R CIRCUIT BREAKER TRIPPED. FOUND TRU SHORT TO GROUND. R & R APU TRU, PERFORMED APU OPS CHECK, CONDITION OK IAW AMM 24-32-04. AMM 49-11-00.

Part: CONNECTOR — LOOSE (PRV) · airframe 6,795 hrs · 1,921 cycles

STATUS MESSAGE FOR LT ENGINE, AIR SUPPLY BITE MODULE CHECKED IAW MM 36-23-00 WITH NO FAULTS, FOUND PRV PLUG LOOSE, RETIGHTENED IAW AMM 36-11-19, PRV OPS CHECKED IAW MM 36-11-18, PRV ACTUATOR LEAK TEST IAW MM 36-11-18, ALL OPS OK.

Part: VALVE — MALFUNCTIONED (FUEL SYS) · airframe 6,754 hrs · 1,908 cycles

DURING RT ENGINE START, ENGINE FLAMED OUT AND MSG "RT FUEL SPAR VALVE" EICAS MSG. GATE RETURNED. FOUND RT -SPAR VALVE CB'S POPPED OUT SO RESET CB'S THEN RT-SPAR VALVE OPERATION CK OK IAW AMM 28-22-01. RT ENGINE FUEL SHUTOFF VALVE ACTUATOR ASSY. REPLACE REQUESTED. R & R WITH NEW RT ENG FUEL SHUTOFF VALVE ACTUATOR ASSY AND GROUND OPS CHECKED OK IAW AMM 28-22-11/401.

Part: BLADE — DAMAGED (NR 2 ENGINE FAN) · airframe 6,568 hrs · 1,848 cycles

BIRD STRIKE DURING CLIMBOUT, FOUND NR 2 ENGINE FAN BLADE NR 33 DISTORTION. LENGTH 2.5 CORD WIDTH 1.125 DISTORTION .5, 4" FROM TIP OF BLADE. PERFORMED BLEND OUT IAW AMM 72-31-02-226-012-400. AFTER BLEND OUT DIMENSION LENGTH 3.5, CHORD .55, WIDTH .25 DISTORTION. BIRD STRIKE COND INSPECTED OK IAW AMM 05-18-221-001.

Part: APU — FAILED · airframe 6,509 hrs · 1,818 cycles

APU AUTO SHUTDOWN WHEN GROUND POWER SELECTED. REPLACED APU ASSY IAW AMM 49-11-00, OPS FUNCTION NORMAL, APU OIL SERVICE TO FULL, BUT STILL SHOW ADD, REPLACED APU OIL QTY TRANSMITTER & CHECKED NORMAL IAW AMM 49-94-04. PERFORMED APU GENERATOR RETENTION NUTS RE-TORQUE, CONDITION SATISFACTORY IAW AMM 24-21-01.

Part: FILTER — CLOGGED (APU OIL) · airframe 6,435 hrs · 1,781 cycles

APU FAULT EICAS; LIGHT AT 95 PERCENT RPM DURING APU START, FOLLOWED FIM 49-11, FT995, FOUND LUBE FILTER DPI POPPED OUT IAW AMM 49-27-03, R & R LUG; GEN SCAVENGE FILTER ELEMENTS IAW AMM 49-11-00, OPS CHECKED NORMAL, OIL LEVEL NORMAL AMM 12-13-04.

Part: WARNING LIGHT — FALSE ACTIVATION (APU OIL) · airframe 6,432 hrs · 1,779 cycles

APU FAULT LIGHT AT APROXIMATELY 95 PERCENT AFTER LANDING, START ATTEMPT, 2 START ATTEMPTS UNSUCCESSFUL. APU SHOWED LOW OIL PRESSURE PERFORMED APU BITE THEN TEST RESULT NO FAULTS. ERASED FAULT MEMORY. RESTARTED APU THEN OPS CHECK OK. OIL LEVEL OK BY SIGHT GAGE. FULL IAW AMM 49-11-00/201.

Part: DOOR — UNSECURE (ESCAPE ROPE) · airframe 6,429 hrs · 1,778 cycles

F/O ESCAPE ROPE HATCH FALLS OPEN IAW AMM 25-61-02 PERFORMED LATCH OPS. REINSTALLED PANEL; CONDITION CHECKED NORMAL.

Part: COVER — UNSECURE (ESCAPE ROPE) · airframe 6,405 hrs · 1,765 cycles

F/O EMERGENCY ESCAPE, ROPE COVER OPENS IN FLIGHT WITHOUT ACTIVATION OR TURBULANCE. ADJUST LATCH AND REINSTALL COVER, CONDITION CHK SATISFACTORY IAW AMM 25-61-02.

Part: DOOR — WEAK (ESCAPE ROPE) · airframe 6,429 hrs · 1,778 cycles

EMERGENCY ESCAPE ROPE DOOR ON F/O'S SIDE WILL NOT STAY CLOSED. REINSTALL PANEL AND CHK BACK TO NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (IDG) · airframe 6,368 hrs · 1,746 cycles

STATUS MESSAGE "IDG OUT TEMP" PERFORMED, FIM 24-20, CHECKED CONDITION NORMAL.

Part: ESCAPE ROPE — MALFUNCTIONED (FIRST OFFICER'S) · airframe 6,331 hrs · 1,728 cycles

F/O'S EMERGENCY ESCAPE ROPE PANEL UNLOCKS DURING TAXI AND LIGHT TURBULANCE, ADJUSTED F/O SIDE EMERGENCY ESCAPE ROPE PANEL AND CONDITION CHECK NORMAL IAW AMM 25-61-02.

Part: EXCITER — MALFUNCTIONED (LT ENGINE) · airframe 6,306 hrs · 1,715 cycles

LT ENGINE IGNITER 1, ERASED STATUS MESSAGE, LT ENGINE IGNITER 1 AUDIBLE CHECK. REPLACED LT ENGINE IGNITOR 1 EXCITER. IAW AMM 74-00-00, PERFORMED LT ENGINE IGNITOR SYS AUDIBLE TEST, CONDITION SATISFACTORY.

Part: CONTROLLER — MALFUNCTIONED (NR 1 ENGINE) · airframe 6,282 hrs · 1,701 cycles

FOUND NR 1 ENGINE FAILED HEALTH CHECK TEST IAW AMM 36-11-08-004-006 AND AMM 36-11-08-404-014. REPLACED NR1 ENGINE HPC IAW AMM 36-11-08-404-014, REV 112. TEST RESULT PASS.

Part: SENSOR — FAILED (RT A/C PACK) · airframe 6,282 hrs · 1,701 cycles

THE RT PACK STANDBY TEMP SENSOR TEST FAILED IAW AMM 21-51-08-004-026 AND AMM 21-51-08-404 R & R RT PACK STANDBY TEMP SENSOR.

Part: SEAL — LEAKING (PNEUMATIC SYS) · airframe 6,282 hrs · 1,701 cycles

THE PNEUMATIC DUCT LEAK AT BODY CROSSOVER AIR SUPPLY SYS IAW AMM 36-11-01-004-131-001 REV 112 AND AMM 36-11-01-404-142-001. REPLACED SEAL AT BODY CROSSOVER DUCT OPS CK NORMAL

Part: ACTUATOR — LEAKING (HPSOV) · airframe 6,282 hrs · 1,701 cycles

FOUND NR 2 HPSOV ACTUATOR LEAKAGE THUMB TEST FAIL IAW AMM 36-11-07-024-001 AND AMM 36-11-07-424-016. REPLACED NR 2 ENGINE HPSOV IAW AMM 36-11-27-424-016, TEST CK NORMAL.

Part: WIRE — CHAFED (SHUTOFF VALVE) · airframe 6,282 hrs · 1,703 cycles

FOUND EDP S/O VALVE FUNCTIONAL FAIL DURING FIRE HANDLE OPERATION IAW SWPM 20-10-13, REV 60. REPAIRED THE CHAFING WIRE NEAR CONNECTOR AND CONDITION CHECK NORMAL IAW SWPM 20-61-19, REV 60, WDM 29-11-21, REV 9. REPLACED ENGINE NR 2 EDP S/O VALVE CONNECTOR D10980P AND PERFORMED CONTINUITY CHECK AND THE RESULT WAS SATISFACTORY IAW AMM 29-11-06-004-001, 29-11-06-404-016, REV 112. REPLACED EDP S/O VALVE AND CONDITION CHECK NORMAL IAW AMM 29-11-06-404-016, REV 112. PERFORMED TEST AND RESULT WAS SATISFACTORY.

Part: RELAY — NOT REPORTED (APU STARTER) · airframe 6,282 hrs · 1,703 cycles

PERFORM E/O NR: 6749A003, STEP 5.F REPLACED APU START RELAY K197 IAW SWPM 20-81-22 REV 60 AND WDM 49-41-11, REV 9. REPLACED RELAY K197 IAW AMM 49-11-00-802-002, REV 112. PERFORMED APU STARTING AND OPS TEST AND THE RESULT WAS SATISFACTORY.

Part: ELT — FAILED · airframe 6,282 hrs · 1,703 cycles

THE ELT GAVE A FAULT CODE SIGNAL DURING AN ELT SELF TEST IAW AMM 23-24-01-002-085, 23-24-01-402-086, REV 112. REPLACED ELT NAV INTERFACE UNIT IAW AMM 23-24-00-715-030, REV 112 PERFORMED ELT OPS TEST AND THE RESULT WAS SATISFACTORY.

Part: WARNING MESSAGE — FALSE ACTIVATION (EQUIP COOLING) · airframe 6,252 hrs · 1,687 cycles

EICAS MESSAGE FOR THE FWD EQUIPMENT VALVE. EQUIPMENT VALVE CIRCUIT BREAKER RESET IAW FIM 21-58, FAULT TREE 985. PFM FWD EQUIPMENT COOLING TEST CHECKED NORMAL, VALVES OPS TESTED FIVE TIMES, CHECKED OK IAW AMM 21-58-00.

Part: FMC — ODOR · airframe 6,252 hrs · 1,687 cycles

LEFT FMC CIRCUIT BREAKER TRIPPED. FMC WENT BLANK. ELECTRICAL ODOR WAS PRESENT, VISUALLY INSPECTED IAW AMM 05-51-56, NO DEFECTS NOTED. DEFFERED CDU IAW MEL 34-61-01-01A, MDDR 58839.

Part: STARTER — FAILED (APU) · airframe 5,930 hrs · 1,595 cycles

APU CANT START, ZERO RPM, BITE-STARTER MESSAGE. R & R APU STARTER MOTOR, C/W BITE TEST IAW AMM 49-61-05, TEST OK, C/W APU STARING TEST MM 49-11-00, OPS CHECKED NORMAL.

Part: DUCT — LEAKING (RT A/C PACK) · airframe 5,702 hrs · 1,550 cycles

EICAS MESSAGE "PACK TEMP". EICAS MESSAGE "R PACK OFF" ACCOMPLISHED PACK TEMP PROCEDURE, STBY AND WORKED FINE, RT PACK RESET. PNEUMATIC AIR LEAKED FROM RT PACK COMPRESSOR OUTLET DUCT, REINSTALLED RT PACK COMPRESSOR OUTLET DUCT AND LEAKS OK IAW AMM 21-51-23/401. CLEANED AND REINSTALLED LT OUTLET TEMP SENSOR AND THEN CHECKED OK IAW AMM 21-52-06/401.

Part: CONTROLLER — FAULTED (LT ENGINE) · airframe 5,649 hrs · 1,543 cycles

LEFT ENGINE PRV STATUS MESSAGE. FIM PROCEDURE 36-10, FAULT TREE 847, CARRIED OUT. LEFT ENGINE PRV CONTROLLER REPLACED & AMP; TESTED IAW AMM 36-11-19 P 401, LEFT BLEED SYSTEM SERVICEABLE.

Part: SENSOR — MALFUNCTIONED (SLAT SYS) · airframe 4,730 hrs · 1,280 cycles

ON DEPARTURE, DURING FLAP RETRACTION FROM 1 TO 0, GOT EICAS L/E SLAT ASYM. PERFORMED QRH PROCEDURE AND RETURNED TO DEPARTURE. ACCOMPLISHED FIM TASK 27-81, FT 809. FOUND NR 11 SLAT INBD SENSOR FAIL. REPLACED NR 11 INBD SLAT SENSOR IAW AMM 27-88-01-902-001. ALL OPS AND INDICATIONS NOW GOOD.

Part: PROXIMITY SWITCH — MALFUNCTIONED (SLATS) · airframe 4,681 hrs · 1,272 cycles

ON DEPARTURE, DURING FLAP RETRACTION FROM 1 TO 0, GOT EICAS MSG; L/E SLAT ASYM. PERFORMED QRH PROCEDURE AND RETURNED TO DEPARTURE, FSEU BITE MEMORY SHOWED L/E OTBD ASYM, CHECKED PSEU BITE MEMORY TARGET, 278, 279, 280, 284, 296, 298,301 FAULT IAW FIM 27-81-809. PERFORMED ALL L/E PROXIMITY SENSOR AND WIRING RESISTANCE, INDUCTANCE, INSULATION CHECKS AND FOUND ALL SATISFACTORY, PERFORMED VISUAL CHECK ON L/E PROXIMITY SENSORS & AMP; TARGETS FROM IN & AMP; INTERMEDIATE POSITION, FOUND ALL SATISFACTORY, R & AMP; R PSEU IAW AMM 32-09-04. TESTED SATISFACTORY, EICAS MSG, NO LONGER ACTIVE, CYCLED FLAPS SEVERAL TIMES SATISFACTORY IAW AMM 27-81-00.

Part: EXCITER — MALFUNCTIONED (NR 2) · airframe 4,659 hrs · 1,260 cycles

STATUS MESSAGE, LT ENGINE IGNITOR 2" IAW AMM 74-21-02, REPLACED LT ENGINE IGNITOR 2 PLUG IAW AMM 74-11-01. REPLACED NR 2 EXCITER IAW AMM 74-00-00 PRM SUITABLE TEST, FUNCTION NORMAL. NO MORE MSG SHOWING.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 3,837 hrs · 865 cycles

LEFT ENG PRV STATUS. THIS MSG IS LATCHED, STATUS MSG. RESET DISAPPEARED, ALSO AIR SUPPLY BITE MODULE VERIFY CHECKED OK IAW AMM 36-23-00-501.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 74,087 hrs · 15,609 cycles

LT ENG PRV STATUS MSG. LATCHED STATUS MSG, RESET & DISAPPEARED, ALSO AIR SUPPLY BITE MODULE VERIFY CHECKED OK IAW AMM 36-23-02.

Part: RIVET — DAMAGED (FUSELAGE) · airframe 342 hrs · 697 cycles

FOUND ONE FASTENER HEAD LIGHTING STRIKE. REPLACED DAMAGED RIVETS WITH NEW RIVETS IAW SRM 53-00-01. REPAIR 8 REV 57 & CONDITION BACK TO NORMAL NRC=001.

Part: SENSE LINE — NOT SEATED (BLEED AIR SYS) · airframe 3,188 hrs · 688 cycles

STATUS MSG, LT ENG PRV. FIM PROCEDURE 36-10 TREE 847 CARRIED OUT, BLEED AIR BITE SYS CO MSG CLEARED, PRV SENSE LINE RE-SEATED.

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 3,055 hrs · 662 cycles

WEATHER RADAR SYSTEM FAIL DURING DESCENT. RECYCLED CB & NBSP. WXR OPERATIONS CHECKED, CONDITION BACK TO NORMAL IAW AMM 34-43-00.

Part: CONTROL UNIT — MALFUNCTIONED (APU) · airframe 3,014 hrs · 649 cycles

APU BLEED FUNCTION INOPERATIVE, AFT APU START. R&R APU CONTROL UNIT & IGV ACTUATOR IAW AMM 49-61-05 & 49-52-02. PERFORMED PNEUMATICS FUNCTIONAL CHECK IAW AMM 49-11-00, OPERATIONS CHECKED NORMAL. APU CONTROL UNIT OFF PN 2117342, SN 82-C0082, EGV ACTUATOR PN OFF 3886167-4 & SN 3631.

Part: BLEED AIR SYS — MALFUNCTIONED (APU) · airframe 2,963 hrs · 638 cycles

NO BLEED AIR FOR ENG START, RETURNED TO GATE FOR APU RE-START. AFTER APU RE-START, BLEED AIR PRESS OK IAW MM 36-11-00.

Part: INDICATOR — FAULTY (COCKPIT) · airframe 2,933 hrs · 630 cycles

FUEL TEMP & TOTAL FUEL ON OVERHEAD PANEL ARE HARD TO READ DUE TO MULTIPLE SEGMENTS OF DIGITS BEING ILLUMINATED SIMULTANEOUSLY. R & R WITH NEW FUEL QTY INDICATOR MODULE. PERFORMED OPERATIONS TEST OF FUEL QTY. INDICATING SYS IAW AMM 28-41-00-715-001-002, CHECKED NORMAL.

Part: WINDSHIELD WIPER — OUT OF ADJUST (COCKPIT) · airframe 2,840 hrs · 605 cycles

IAW MDDR 44825 LT WINDSHIELD WIPER DEPLOYED HALFWAY OF WINDOW WITH SWITCH IN OFF POSITION. IAW AMM 30-42-00-825-013 ADJUSTMENT ON THE WINDSHIELD WIPER SYS & ADJUSTED SWITCH COND BACK TO NORMAL, MDDR CLEARED.

Part: UNKNOWN — MALFUNCTIONED (WINDSHIELD WIPER) · airframe 2,832 hrs · 601 cycles

DURING CRUISE THE LT WINDSHIELD WIPER DEPLOYED HALFWAY UP WINDOW WITH THE SWITCH IN OFF POSITION. PLACED ON DEFERRAL.

Part: FILTER — WARNING MESSAGE (RT ENGINE) · airframe 2,585 hrs · 539 cycles

EICAS MESSAGE RT ENGINE FUEL FILTER MESSAGE FOR 2 SECONDS THEN AUTOMATIC TRANSFERRED TO STATUS MESSAGE. R & R FUEL FILTER IAW MM 73-11-02, LEAK CHECKED OK.

Part: FILTER — FAILED · airframe 2,561 hrs · 530 cycles

FOUND NR 1 ENG EDP CASE DRAIN FILTER DPI POP OUT. REPLACED NR 1 ENG EDP CASE DRAIN FILTER LEAK CHECK CONDITION NORMAL.

Part: IGNITER — WARNING MESSAGE (RT ENGINE) · airframe 2,490 hrs · 494 cycles

STATUS MESSAGE FOR RT ENGINE IGNITER 2. R & R RT ENGINE SYS 2 IGNITER PLUG IAW AMM 74-21-02, PERFORMED ENG 2 IGNITION SYS AUDIBLE TEST NORMAL IAW AMM 74-00-00. PERFORMED RIGHT ENGINE IDLE RUN IAW AMM 71-00-00, OPS CHECKED NORMAL.

Part: RELAY — LOOSE (LT ENGINE) · airframe 2,299 hrs · 443 cycles

IDLE DISAGREE EICAS MESSAGE. LEFT ENGINE IDLE AROUND 10 PERCENT HIGHER THAN NORMAL, IN FLIGHT AND GROUND IDLE. IAW FIM 71-05-00 CHECK, FOUND K 434 RELAY LOOSEN. REINSTALL AND OPS CHECKED, BACK TO NORMAL IAW AMM 71-00-00.

Part: RELAY — LOOSE (BOOST PUMP) · airframe 2,109 hrs · 392 cycles

EICAS MESSAGE " RT FWD FUEL PUMP" ON CLIMB OUT, QRH PROCEDURE COMPLIED WITH TROUBLESHOOT IAW FIM 28-22-03 FAULT CODE, FAULT ISOLATION REF 28-22 FAULT TREE 819, CB 6G18 NOT OPEN. FOUND BOOST PUMP CONTROL RELAY K190 LOOSE. REMOVED AND REINSTALLED RELAY & AMP; TESTED PUMP OK IAW AMM 28-22-00/501, TASK 28-22-00-715-001,2.F. TESTED GFI IAW 28-22-00/542, PASS.

Part: COWLING — DAMAGED (NR 2 INLET) · airframe 1,927 hrs · 369 cycles

FOUND LIGHTING STRIKE ON NR 2 ENGINE INLET COWL AREA IAW AMM 05-51-19 INSPECTION. REPAIR AS REF SRM 54-15-01-2R-9.

Part: FUEL CONTROL — INOPERATIVE (APU) · airframe 1,793 hrs · 323 cycles

APU AUTO SHUTDOWN. R & R APU FUEL CONTROL UNIT IAW AMM 49-11-01. OPS & LEAK CHECKED GOOD.

Part: MODULE — INOPERATIVE (WARNING SYS) · airframe 1,769 hrs · 311 cycles

COCKPIT AURAL WARNINGS GO OFF ON THEIR OWN, UNCOMMANDED. R & R BELL CHIME MODULE ASSY. OPS CHECK OK IAW AMM 31-51-04.

Part: CONNECTOR — DIRTY (APU) · airframe 1,769 hrs · 311 cycles

APU AUTO SHUTDOWN TWICE DURING PUSHBACK. REMOVED AND CLEANED OIL PRESSURE SWITCH CONNECTOR, OPERATED APU IN FULL LOAD AND UNLOADED CONDITIONS, ALL OPS NORMAL.

Part: APU — MALFUNCTIONED · airframe 1,768 hrs · 310 cycles

APU AUTO SHUTDOWN TWICE DURING PUSH BACK. PERFORMED BITE TEST CHECK ON APU CONTROLLER, INDICATES LOW OIL PRESSURE, CHECKED OIL QTY, CHECKS FULL.

Part: GCU — INOPERATIVE (APU GENERATOR) · airframe 1,205 hrs · 194 cycles

APU GENERATOR INOPERATIVE. REPLACED GENERATOR CONTROL UNIT, IAW 24-00-02 AMM, ALL OPS CHECKS NORMAL.

Part: FILTER — FAILED (LEFT IDG) · airframe 1,124 hrs · 184 cycles

LEFT IDG VALVE EICAS MESSAGE. R & R IDG PNEUMATIC SHUTOFF VALVE FILTER IAW AMM 24-11-07, OPS CHECKED GOOD.

Part: IDG — WARNING MESSAGE (LEFT) · airframe 1,116 hrs · 183 cycles

LEFT IDG VALVE STATUS MESSAGE.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT IDG) · airframe 1,067 hrs · 177 cycles

LEFT IDG VALVE STATUS MESSAGE. ACCOMPLISHED FIM TASK 24-20 FAULT TREE 802 FOR LT IDG VALVE. NO FAULTS . ACCOMPLISHED IDLE POWER RUN LT ENGINE. ALL OPS INDICATIONS NORMAL ALL SYSTEMS.

Part: BLEED AIR SYS — INOPERATIVE (APU) · airframe 741 hrs · 137 cycles

APU BLEED AIR INOPERATIVE. RESTARTED APU, BLEED AIR OPS CHECK OK IAW AMM 49-11-00.

Part: ENGINE — MAKING METAL (NR 1) · airframe 602 hrs · 120 cycles

FOUND METAL CHIPS IN TAIL PIPE OF NR 1 ENGINE. R & R NR 1 ENGINE IAW AMM 71-00-00 ENG RUN & LEAK CHECKS SATISFACTORY.

Part: INDICATOR — INTERMITTENT · airframe 389 hrs · 94 cycles

STANBY ENGINE INDICATION INTERMITTENT. REMOVED AND INSTALLED STANBY ENGINE INDICATOR IAW AMM 77-41-01, OPS CHECKED GOOD.

Part: INDICATOR — FALSE INDICATION (OIL QTY) · airframe 355 hrs · 90 cycles

LEFT ENGINE OIL QTY DROPPED TO 7 AT 4+30 IN FLT, RECOVERED TO 10 OVER NEXT 2 HRS AC BLOCK IN 20 AT FLT TERMINATION. EICAS INDICATION AT BLOCK IN READS 19QTS CAP CHECK OIL INDICATION SHOWS FULL ADDED 1QT, IAW AMM 79-31-00 C/W ENGINE, INSPECTION FOR OIL LEAKAGE IAW AMM TASK 79-00-206-004, NO OIL LEAKAGE NOTED MCC NOTIFIED.