N1049A

Part: COVER — OUT OF POSITION (ZONE 200) · airframe 94,631 hrs · 15,843 cycles

EMERGENCY LIGHTS SWITCH COVER TURNS SWITCH OFF WHEN CLOSED. METAL BAR FOUND OUT OF POSITION AND WOULD FORCE SWITCH INTO OFF POSITION. ADJUSTED METAL BAR BACK INTO POSITION IN ACCORDANCE WITH BOEING 767 AIRCRAFT MAINTENANCE MANUAL 33-51-01. OPERATIONAL CHECK GOOD.

Part: DOOR — ERODED (ZONE 400) · airframe 94,425 hrs · 15,750 cycles

#2 ENG IB TR INSIDE LIP ON THE IDG DOOR HAS CHAFFING WEAR ON LANDING

Part: HINGE — ELONGATED (ZONE 400) · airframe 94,425 hrs · 15,750 cycles

#2 ENGINE PYLON HYD BAY ACCESS PANEL 447BR AFT HINGE HAS PLAY

Part: SKIN — DAMAGED (ZONE 300) · airframe 94,425 hrs · 15,750 cycles

RUDDER HAS SEVERAL LIGHTNING STRIKES AFT OF SMILE RT SIDE. HAECO WO 320013 NON ROUTINE 39028

Part: WEB — DAMAGED (ZONE 100) · airframe 94,425 hrs · 15,750 cycles

E&E DOOR UPPER AFT TRACK HAS DRILL START & GOUGE UNDER TRACK

Part: SKIN — GOUGED (ZONE 400) · airframe 94,425 hrs · 15,750 cycles

#1 OB CORE COWL EXTERNAL SKIN IS GOUGED AT AFT LOWER EDGE

Part: SKIN — DENTED (ZONE 500 FLAP) · airframe 94,425 hrs · 15,750 cycles

L/H WING INBD AFT FLAP LOWER SURFACE OF THE L/E PANEL IS DENTED APPROX 4" OTBD OF THE OTBD TRACK FAIRING

Part: STRUCTURE — CRACKED (ZONE 400) · airframe 94,425 hrs · 15,750 cycles

#2 ENGINE PYLON INTERNAL OF ZONE 442 INBD UPPER CHORD IS CRACKED AT APPROX NAC STA 221.5

Part: FAN COWL — DAMAGED (ZONE 400) · airframe 94,425 hrs · 15,750 cycles

#1 ENG O/B FAN COWL DOOR FWD EDGE LANDING SHOWING COMPOSITES MISSING PROTECTIVE FINISH

Part: FAN COWL — DAMAGED (ZONE 400) · airframe 94,425 hrs · 15,750 cycles

#2 ENG I/ FAN COWL DOOR FWD EDGE LANDING HAS COMPOSITES SHOWING PAINT MISSING AND WIRE MESH DAMAGE OUT OF LIMITS

Part: FAN COWL — ERODED (ZONE 400) · airframe 94,425 hrs · 15,750 cycles

#1 ENG I/B FAN COWL DOOR FWD EDGE LANDING SHOWING COMPOSITE EROSION DAMAGE

Part: STOP FITTING — GOUGED (ZONE 800) · airframe 94,425 hrs · 15,750 cycles

119AL E&E DOOR FWD LH STOP FITTING HAS A GOUGE

Part: STOP FITTING — GOUGED (ZONE 800) · airframe 94,425 hrs · 15,750 cycles

119AL E&E DOOR FWD RH STOP HAS GOUGE

Part: STIFFENER — CRACKED (ZONE 100) · airframe 94,425 hrs · 15,750 cycles

CRACK FOUND ON RIGHT HAND VERTICAL STIFFNER IN THE NOSE LANDING GEAR WHEEL WELL 10INCHES ABOVE ELECTRICAL PANEL BOX

Part: SKIN — DELAMINATED (ZONE 500 AILERON) · airframe 94,425 hrs · 15,750 cycles

L/W O/B AILERON UPPER SURFACE HAS DAMAGED COMPOSITES AT O/B TRAILING EDGE

Part: FRAME — GOUGED (ZONE 400) · airframe 94,425 hrs · 15,750 cycles

O/B CORE COWL #1 ENG 2ND FRAME SUPPORT STRUCTURE FROM FWD HAS GOUGE

Part: BRACKET — CRACKED (ZONE 400) · airframe 94,425 hrs · 15,750 cycles

#2 PYLON AFT FAIRING ASSY ATTACH ANGLE IS CRACKED ON O/B AFT UPPER CORNER STRUCTURE COMMON TO PANEL 447CR

Part: ATTACH ANGLE — DAMAGED (ZONE 200) · airframe 94,425 hrs · 15,750 cycles

MAIN CARGO DOOR CUTOUT - LOWER SEAL DEPRESSOR ATTACH ANGLE ELONGATED HOLES ON FWD AND AFT ENDS

Part: COWLING — CHAFED (THRUST REVERSER)

#2 ENG IB TR INSIDE LIP ON IDG DOOR HAS CHAFFING WEAR ON LANDING. HAECO WO 320013 NON ROUTINE 38713

Part: FITTING — CRACKED (ZONE 500) · airframe 94,425 hrs · 15,750 cycles

LH WING INBD FLAP HINGE ARM FOR THE AFT FLAP IS CRACKED AT THE ATTACH FLANGE COMMON TO THE LOWER SURFACE SKIN

Part: SKIN SPLICE — CRACKED (ZONE 600) · airframe 94,425 hrs · 15,750 cycles

RH WING FIXED LEADING EDGE SKIN PLATE IS CRACKED AT APPROX OFSS 505

Part: FORMER — CRACKED (ZONE 600) · airframe 94,425 hrs · 15,750 cycles

RH WING FIXED LEADING EDGE SKIN FORMER IS CRACKED AT APPROX OFSS 490

Part: RIB — WORN (ZONE 600) · airframe 94,425 hrs · 15,750 cycles

RIGHT WING #8 SLAT OUTBOARD SIDE EDGE IS WORN IN 2 PLACES. HAECO SERVICE ORDER 320013, NR 38540

Part: FORMER — CRACKED (ZONE 500) · airframe 94,425 hrs · 15,750 cycles

LEFT WING FIXED LEADING-EDGE FORMER CRACKED AT APPROX OSS 490. HAECO SERVICE ORDER 320013 AND NR 38512

Part: FORMER — CRACKED (ZONE 500) · airframe 94,425 hrs · 15,750 cycles

LEFT WING FIXED LEADING-EDGE FORMER IS CRACKED AT APPROX OSS 563. HAECO SERVICE ORDER 320013, NR 38499

Part: ATTACH BOLT — CRACKED (ZONE 500) · airframe 94,425 hrs · 15,750 cycles

LH WING #6 SLAT AT OUTBD CONTROL ROD LOWER ATTACH L BRACKET IS CRACKED

Part: SKIN — CRACKED (ZONE 200) · airframe 94,425 hrs · 15,750 cycles

R1 FWD SERVICE DOOR CUT OUT AFT LOWER CORNER FUSELAGE SKIN AND BEAR STRAP HAS CRACK EXTENDING FROM SECOND LOWER FASTENER HOLE AS MARKED

Part: SKIN — CRACKED (ZONE 200) · airframe 94,425 hrs · 15,750 cycles

CRACK INDICATION FOUND IN L1 FWD ENTRY DOOR CUTOUT LOWER AFT CORNER

Part: ACM — MALFUNCTIONED (ZONE 100) · airframe 93,790 hrs · 15,465 cycles

ENROUTE FROM KCVG TO KBDL CREW REPORTED FWD EQPT OVHT EICAS MESSAGE. CREW COMPLIED WITH ATI QRH; CABIN STARTED TO CLIMB. DIVERTED TO KBUF & AN EMERG DESCENT. LANDED WITHOUT INCIDENT. ACFT GROUNDED. DURING FAULT ISOLATION, LINE MX REPORTED WITH LT ENG ENGAED PER AMM 71-00-00 & OPS OF 1 PACK AT A TIME, PRESSURIZING ACFT IAW AMM 05-51-24, LT PACK UNABLE TO MAKE 1 PSI DIFF PRESSURE. RT PACK MADE DIFF PRESSURE. INSP OF LT ECS BAY SHOWED ACM INTAKE PLENUM COUPLING WAS NOT SECURED. IAW AMM 21-51-03. TROUBLESHOOTING IDENTIFIED LT PACK MAKING INSUFFICIENT AIR. LT PACK R & R IAW AMM 21-51-03. OPS & LEAK CHKD GOOD. NO FWD EQUIP COOLING OR OVERHEAT EICAS MESSAGES & LIGHTS DISPLAYED THROUGH THE COURSE OF FUNCTIONAL CHECKS.

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 93,128 hrs · 15,175 cycles

POST FLIGHT CREW REPORTED, WITH EMERGENCY LIGHTS IN ARMED POSITION EMERGENCY LIGHTS TURN ON AND OFF INTERMITTENTLY (SUPERNUMERY AREA). FAULT TRANSFERRED TO DEFERRAL MAINTENANCE ITEM 54717 PER ATI BOEING 767 MINIMUM EQUIPMENT LIST 33-51-01-01.CORRECTIVE ACTION DUE 29 DECEMBER 2024. PER BOEING 767-300 FAULT ISOLATION MANUAL 33-51-FIG 803, FORWARD AND AFT POWER SUPPLY BATTERIES REMOVED AND REPLACED IAW BOEING 767-300 AIRCRAFT MAINTENANCE MANUAL 33-51-07. SUPERNUMERARY LIGHTS OPERATIONAL CHECK SATISFACTORY PER BOEING 767-300 AIRCRAFT MAINTENANCE MANUAL 33-51-00. NO ADDITIONAL FAULTS NOTED. DEFERRAL MAINTENANCE ITEM 54717 CLEARED.

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 93,128 hrs · 15,175 cycles

POST FLIGHT CREW REPORTED, WITH EMERGENCY LIGHTS IN ARMED POSITION EMERGENCY LIGHTS TURN ON AND OFF INTERMITTENTLY (SUPERNUMERY AREA). FAULT TRANSFERRED TO DEFERRAL MAINTENANCE ITEM 54717 PER ATI BOEING 767 MINIMUM EQUIPMENT LIST 33-51-01-01.CORRECTIVE ACTION DUE 29 DECEMBER 2024. PER BOEING 767-300 FAULT ISOLATION MANUAL 33-51-FIG 803, FORWARD AND AFT POWER SUPPLY BATTERIES REMOVED AND REPLACED IAW BOEING 767-300 AIRCRAFT MAINTENANCE MANUAL 33-51-07. SUPERNUMERARY LIGHTS OPERATIONAL CHECK SATISFACTORY PER BOEING 767-300 AIRCRAFT MAINTENANCE MANUAL 33-51-00. NO ADDITIONAL FAULTS NOTED. DEFERRAL MAINTENANCE ITEM 54717 CLEARED.

Part: SKIN — DAMAGED (ZONE 300) · airframe 92,994 hrs · 15,122 cycles

LH HORIZONTAL STAB UPPER BONDED PANEL JUST AFT OF L/E DAMAGED

Part: GENERATOR — FAULTED (RIGHT) · airframe 92,883 hrs · 15,071 cycles

ENROUTE FROM KCLT TO KSBD R GEN DRIVE MESSAGE DISPLAYED ON EICAS FL340. APU INOPERATIVE DUE TO SYSTEM ACTIVELY IN DEFERRED MAINTENANCE STATUS. PER ATI MINIMUM EQUIPMENT LIST 49-11-01-01 BOTH ENGINE GENERATORS MUST BE OPERATIVE IF APU IS INOPERATIVE FOR CURRENTLY SCHEDULED FLIGHT. CREW ELECTED DIVERSION TO KCVG. LANDING WAS WITHOUT INCIDENT AND NO ADDITIONAL PRECAUTIONARY ACTIONS NOTED. RIGHT ENGINE ELEC POWER IDG GENERATORY ASSEMBLY AND SHAFT SEAL REMOVED AND REPLACED PER BOEING 767-300 AIRCRAFT MAINTENANCE MANUAL 24-11-01. WITH RIGHT ENGINE ENGAGED IAW BOEING 767-300 AIRCRAFT MAINTENANCE MANUAL 71-00-00, OPERATIONAL AND LEAK CHECKS GOOD. NO ADDITIONAL SYSTEM FAULTS NOTED.

Part: BATTERY — NO TEST (FLASHLIGHT) · airframe 92,764 hrs · 15,021 cycles

FOLLOWING SCHEDULED CHECKS AND INSPECTIONS, LINE MAINTENANCE REPORTED BATHROOM WALL EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE ITEM-52497 PER ATI MINIMUM EQUIPMENT LIST 25-63-04-01. FLASHLIGHT CERTIFIED INOPERATIVE. EMERGENCY LIGHTING BATTERY REMOVED AND REPLACED PER B767 AMM 25-64-02. OPERATIONAL CHECK GOOD. DEFERRAL MAINTENANCE ITEM 52497 CLEARED.

Part: BATTERY — NO TEST (C/P FLASHLIGHT) · airframe 92,764 hrs · 15,021 cycles

FOLLOWING SCHEDULED CHECKS AND INSPECTIONS, LINE MAINTENANCE REPORTED CENTER PEDESTAL EMERGENCY FLASHLIGHT INOPERATIVE. CENTER PEDESTAL EMERGENCY FLASHLIGHT BATTERY REMOVED AND REPLACED PER BOEING 767-300 AIRCRAFT MAINTENANCE MANUAL 25-64-00. OPERATIONAL CHECK GOOD. NO ADDITIONAL SUBSYSTEM FAULTS NOTED.

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

RH FWD SERVICE DOOR CUTOUT AFT LWR CORNER CRACKED.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 90,169 hrs · 14,015 cycles

FIRST OFFICERS FORWARD O/B SEAT TRACK IS CRACKED.

Part: ROLLER TRAY — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,169 hrs · 14,015 cycles

ROLLER TRAY CORRODED

Part: PANEL — CRACKED (ZONE 500) · airframe 90,169 hrs · 14,015 cycles

PANEL 521BB CRACKED.

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,169 hrs · 14,015 cycles

FLOOR SUPPORT WEB CORRODED

Part: FAILSAFE — CRACKED (ZONE 100) · airframe 90,169 hrs · 14,015 cycles

LH STA. 955 FAIL SAFE STRAP CRACKED

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 90,169 hrs · 14,015 cycles

CAPTIANS FORWARD O/B SEAT TRACK CRACKED.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 90,169 hrs · 14,015 cycles

FIRST OFFICERS FORWARD O/B SEAT TRACK CRACKED

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 90,169 hrs · 14,015 cycles

CAPTAIN'S FORWARD IB SEAT TRACK IS CRACKED

Part: SEAT TRACK — WORN (ZONE 200) · airframe 90,169 hrs · 14,015 cycles

CAPTAINS I/B AFT SEAT TRACK HOLE ELONGATED AND WEAR ON TOP FLANGE.

Part: ROLLER TRAY — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,169 hrs · 14,015 cycles

ROLLER TRAY CORRODED

Part: SEAT TRACK — WORN (ZONE 200) · airframe 90,169 hrs · 14,015 cycles

FO AFT I/B SEAT TRACK HOLES ELONGATED AND WEAR ON TOP FLANGE

Part: FITTING — CRACKED (ZONE 100) · airframe 90,169 hrs · 14,015 cycles

CARGO HANDLING SUPPORT FITTING CRACKED

Part: ROLLER TRAY — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,169 hrs · 14,015 cycles

ROLLER TRAY CORRODED

Part: ROLLER TRAY — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,169 hrs · 14,015 cycles

ROLLER TRAY CORRODED

Part: ROLLER TRAY — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,169 hrs · 14,015 cycles

ROLLER TRAY CORRODED

Part: FITTING — LOOSE (ZONE 400) · airframe 90,169 hrs · 14,015 cycles

#1 PYLON OB SIDE LINK FITTING HAS LOOSE BUSHING

Part: SHROUD — CRACKED (ZONE 300) · airframe 90,169 hrs · 14,015 cycles

SHIELD FOR APU PNEUMATIC DUCK HAS A CRACK AT ATTACH POINT

Part: ROLLER — OUT OF ADJUST (SLIDING WINDOW) · airframe 89,486 hrs · 13,760 cycles

PRE-DEPARTURE CREW REPORTED COPILOT WINDOW WILL NOT LOCK CLOSED. CRANK ROLLER OF R2 WINDOW ADJUSTED IAW B767 AMM 56-11-02. OPERATIONAL CHECK GOOD. NO ADDITIONAL FAULTS WERE NOTED. AIRCRAFT RELEASED TO SERVICE.

Part: DISPLAY — FAILED (EICAS) · airframe 89,422 hrs · 13,735 cycles

LOWER EICAS DISPLAY WAS BLANK UPON ARRIVAL. AIRCRAFT GROUNDED FOR FAULT ISOLATION. REMOVED EICAS DISPLAY SWITCHING MODULES AND CHECKED WIRES FOR SHORT GROUNDS AND CONTINUITY. CLEANED AND ENSURED SECURITY OF CONNECTORS D5055, D5057, D5009, AND D5227. OPERATIONAL CHECK GOOD IAW B767 AMM 31-41-04, 31-41-01/02, WDM 31-41-21, AND 31-41-17. NO ADDITIONAL FAULTS FOUND. AIRCRAFT RELEASED TO SERVICE.

Part: BATTERY — INOPERATIVE · airframe 87,052 hrs · 12,956 cycles

DURING THE DAILY CHECK, MAINTENANCE TECH IDENTIFIED EMERGENCY FLASHLIGHT INOPERATIVE .REMOVED AND REPLACED #2 FLASHLIGHT BATTERY IAW B767AMM 25-64-00. OPERATIONAL CHECK GOOD. NO ADDITIONAL FAULTS NOTED.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 82,008 hrs · 11,372 cycles

RT ENG FIRE LOOP 1 STATUS MSG. PERFORMED FIRE DETECTION BITE PROCEDURE IAW FIM 26-11 FT 806 AND AMM 26-11-00 FIG 104, MESSAGE CLEARED. SYSTEM TEST OK AND NO FAULTS NOTED.

Part: FIRE LOOP — FAULTY (RT ENGINE) · airframe 82,009 hrs · 11,373 cycles

STATUS MESSAGE RIGHT ENGINE FIRE LOOP 1. TRANSFERRED TO MDDR 117181 AS PER DDG 26-11-01-01, CAT "C". LP 1091443 - M6: REMOVED AND REPLACED #2 ENGINE AFT LWR FIRE LOOP DETECTOR REF AMM 26-11-02. OPS CHECKED NORMAL. THIS CLEARS MDDR #117181. PLACARDS REMOVED AND MCC NOTIFIED.

Part: CIRCUIT CARD — MALFUNCTIONED (FIRE DETECTION) · airframe 81,956 hrs · 11,354 cycles

STATUS MESSAGE: RIGHT ENGINE FIRE LOOP 1. PER FIM 26-11 FT 804, FOUND R ENG FIRE LOOP 1 AFOLTS CARD NEEDED TO BE REPLACED. REMOVED AND REPLACED AFOLTS CARD (M683) IAW AMM 26-10-01. OPS CHECK GOOD, NO FAULTS NOTED, MSG CLEARED.

Part: STATUS MESSAGE — FALSE INDICATION (RT FIRE LOOP) · airframe 81,954 hrs · 11,353 cycles

R ENG FIRE LOOP NR 1 STATUS MESSAGE. PERFORMED FIRE DETECTION BITE PROCEDURE PER AMM FIM TASK 26-11 FT 806 AND FIM 26-11-00/101, FIG 104. MSG CLEARED, SYSTEM TEST OK, AND NO FAULTS NOTED.

Part: SMOKE DETECTOR — MALFUNCTIONED (MAIN DECK) · airframe 81,920 hrs · 11,339 cycles

MAIN DECK SMOKE DETECTOR LED LOOP 1A AMBER ILLUMINATED.&NBSP;(<P>REMOVED AND REPLACED LOOP A # 1 DETECTOR IAW AMM 26-19-01. NO FURTHER DEFECTS NOTED AT THIS TIME.&NBSP;</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT A/C PACK) · airframe 81,846 hrs · 11,319 cycles

EICAS MESSAGE: LEFT PACK TEMP. PERFORMED FIM 21-51 FT 806. FOUND NO DEFECTS, PACK OPERATES NORMALLY. PERFORMED BITE PER FIM 21-51 FT 803 AND FOUND NO ACTIVE OR PREVIOUS FAULTS. OPS CHECK GOOD, NO FURTHER DEFECTS NOTED.

Part: RADAR — MALFUNCTIONED (WX SYSTEM) · airframe 81,828 hrs · 11,311 cycles

RADAR DOES NOT PAINT ACTIVE THUNDERSTORMS OR ANY PRECIP ENROUTE. IT ALSO SHOWS AN ARC OF GREEN IN FRONT THE AIRCRAFT IN CLEAR CONDITIONS.&NBSP;(<P>WEATHER RADAR OPS TEST GOOD IAW AMM 34-43-00. NO FAULTS FOUND AT THIS TIME AS PER B767 FIM 34-43 FT 805.

Part: BATTERY — DEFECTIVE (APU) · airframe 81,708 hrs · 11,269 cycles

APU BATTERY DOES NOT APPEAR TO LOAD PROPERLY. (<P>REMOVED AND REPLACED APU BATTERY CHARGER. OPS CHECK NORMAL PER AMM 24-31-05. STANDBY POWER CHECK OK PER AMM 24-33-00. &NBSP; OFF PART (PN:&NBSP;<SPAN>S282T003-3, SN: C551)</SPAN></P><P>LP 1063288 - M9: REMOVED AND REPLACED APU BATTERY. OPS CHECK NORMAL PER AMM 24-31-04. STANDBY POWER CHECKS OK PER AMM 24-33-00.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 81,666 hrs · 11,255 cycles

L ENGINE BLEED OFF EICAS MESSAGE. CREW COMPLETED NON-NORMAL CHECKLIST.(<P>PERFORMED BITE CHECK ON AIR SUPPLY BITE MODULE. NO FAULTS RECORDED, REF 36-10 FT 836. OK FOR SERVICE.<BR /></P>)

Part: STATOR — LOOSE · airframe 81,620 hrs · 11,238 cycles

FOUND CONNECTOR LOSE ON STATOR AND LEAK AROUND STATOR HOUSING(<P><SPAN>R/R / OF THE LT STATOR ASSEMBLY IAW AMM 73-21-08. OPS CHECK GOOD. NO DEFECTS NOTED / AT THIS TIME</SPAN><BR /></P>)

Part: PRESSURE VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 81,599 hrs · 11,229 cycles

UPPER OVER PRESSURIZATION VALVE DOOR NOT FLUSH.(<P>RESET OVER PRESSURIZATION VALVE IAW 21-31-01.</P>)

Part: IDG — NOT REPORTED · airframe 81,532 hrs · 11,209 cycles

INSTALL IDG ON APU. REMOVED IDG FROM APU AND INSTALLED. OPS CHECKED GOOD IAW AMM 24-21-01.

Part: CIRCUIT CARD — MALFUNCTIONED (FIRE DETECTION) · airframe 81,517 hrs · 11,204 cycles

STATUS MESSAGE "R ENG FIRE LP 1".(<P>REMOVED AND REPLACED R ENG FIRE WARNING CARD IAW AMM 26-10-01. FIRE WARNING TEST NORMAL.</P>)

Part: FIRE LOOP — INOPERATIVE (NR 1) · airframe 81,517 hrs · 11,204 cycles

RIGHT ENGINE FIRE LOOP 1 INOPERATIVE. T/S IAW FIM 26-11 TREE 804 SWITCHED CARDS M681 AND M683. PROBLEM FOLLOWED. T/S R ENG LOOP 1 IAW FIM 26-11 F/T 804 FOUND CORROSION ON CERAMIC INSULATOR. CLEANED INSULATOR ON AFT LOWER LOOP PER BLOCK 103. OPS CHECK GOOD. REMOVED AND REPLACED RH ENGINE FIRE LOOP LOWER FWD IAW AMM 26-11-02. OPS CHECK GOOD AT THIS TIME.

Part: STATUS MESSAGE — FALSE ACTIVATION (FIRE LOOP 1) · airframe 81,505 hrs · 11,200 cycles

STATUS MESSAGE R ENG FIRE LOOP 1. PERFORMED FIM 26-11 FT 804, NO FAULTS FOUND.

Part: RADAR — INOPERATIVE (WX SYSTEM) · airframe 81,484 hrs · 11,191 cycles

AUTO TILT FUNCTION OF THE WX RADAR DOES NOT WORK ON THE LEFT RADAR SYSTEM. PERFORMED OPERATIONAL TEST IAW AMM 34-43-00. NO FAULTS NOTED AT THIS TIME.

Part: FAULT CODE — FALSE ACTIVATION (BPCU) · airframe 81,464 hrs · 11,186 cycles

UNABLE TO TRANSFER ELECTRICAL POWER FROM EXTERNAL TO APU GENERATOR. BITE CHECK BPCU. CLEARED FAULT. OPS CHECK GOOD AT THIS TIME IAW AMM 24-11-00.

Part: SHUTOFF VALVE — MALFUNCTIONED (FUEL SYSTEM) · airframe 81,163 hrs · 11,089 cycles

EVIDENCE OF FUEL LEAK LEFT WING INBOARD OF LT MLG AT REAR SPAR AREA.(<P>CYCLED APU FUEL SHUT OFF VALVE.&NBSP; NO LEAKS NOTED AT THIS TIME.&NBSP; (SEE L/P 1024264 FOR DEFERRAL)&NBSP; REF AMM 28-25-02.<BR /></P>)

Part: ACTUATOR — MALFUNCTIONED (FUEL SYSTEM) · airframe 81,156 hrs · 11,086 cycles

APU INOP.(<P>APU PLACED ON MEL PER MEL 49-11-01A</P><P>LOG PAGE 1024271 REMOVED AND REPLACED APU SHUTOFF VALVE ASSY IAW AMM 28-25-02 (P/N OFF 1257706-1 S/N T43464). ALSO REMOVED AND REPLACED APU SHUTOFF VALVE ASSY ACTUATOR IAW AMM 28-25-02 OPS CHECK OK. MDDR # 110923 CLOSED.&NBSP;</P>)

Part: SHUTOFF VALVE — FAILED (RT BLEED) · airframe 80,960 hrs · 11,029 cycles

AFTER BOTH ENG START, RIGHT ENG EICAS MSG & RIGHT PACK OFF AS RIGHT ENG BLEED OFF COULD NOT ESTABLISH DUCT PRESSURE TO THE RIGHT DUCT. AFTER DEFERING HPSOV, RIGHT ENG HAS NO BLEED AIR. REMOVED RH ENG PRSOV IAW AMM JC-11-09. R/H ENG HPSOV R/H T/R REMAINS ACTIVATED, REMOVED AND REPLACED THE RH ENG AIR SUPPLY CONTROL CARD. DIDN'T FIX THE FAULT. REMOVED AND REPLACED PRSOV ON # 2 ENG I.A.W AMM 36-11-09. LEAK CHECK AND OPS CHECK GOOD AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 80,959 hrs · 11,028 cycles

TERR SYS STATUS MSG ON ARRIVAL.(<P>PERFORMED SYSTEM TEST PER B767 AMM 34-43-00. SYSTEM TEST NORMAL, NO STATUS MESSAGE ON EICAS.<BR /></P>)

Part: INDICATION SYS — MALFUNCTIONED (FUEL FLOW) · airframe 80,890 hrs · 11,005 cycles

REF LP&NBSP; 880766-01 FUEL FLOW ALSO INDICATED 300-400 PPH HIGHER THAN RT NR 2 ENGINE(<P>PERFORMED NR 1 AND NR 2 ENG RUN&NBSP; IAW AMM 72-10-00 FF&NBSP; INDICATION&NBSP; NORMAL&NBSP; NO FF IMBALANCE NOTED ALL ENG PARAMETER NORMAL OK FOR SERVICES&NBSP; AT TIME&NBSP;</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 80,893 hrs · 11,006 cycles

R PACK OFF MSG CAME ON DURING DESCENT(<P>PERFORMED BITE IAW FIM 21-51-809 NO FAULTS</P>)

Part: UNKNOWN — MALFUNCTIONED (RT ENGINE) · airframe 80,893 hrs · 11,006 cycles

RIGHT ENG FAN VIBRATION UP TO 4.0 IN CLIMB, CRUISE AND DESCENT(<P>PERFORMED GVI INSP OF RT ENG PER AMM 71-00-001 501 NO DEFECTS NOTED. PERFORMED AVM TEST IAW AMM 77-31-00 . NO DEFECTS NOTED</P>)

Part: IGNITER — NOT REPORTED (APU) · airframe 80,854 hrs · 10,993 cycles

REPLACE APU IGNITER PLUGS AS PER WORK CARD. (<P>REMOVED AND REPLACED APU IGNITER PLUGS. PER AMM 49-41-02. OPS CHECK SATISFACTORY REF: AMM 49-11-00.</P>)

Part: STARTER — DEFECTIVE (NR 2 ENGINE) · airframe 80,854 hrs · 10,993 cycles

NR 2 ENGINE OIL QTY. DRAINED IS LESS THAN 17 FL OZ. (REQUIRES REPLACEMENT). (<P>REMOVED AND REPLACED NR 2 ENGINE STARTER IAW 80-11-01. OPS AND LEAK CHECK NORMAL NO LEAKS.</P>)

Part: STARTER — DEFECTIVE (NR 1 ENGINE) · airframe 80,854 hrs · 10,993 cycles

ENGINE NR 1 STARTER OIL DRAINED LESS THAN 17 FLUID OZ. REPLACE STARTER. (<P>REMOVED AND REPLACED NR 1 ENGINE STARTER PER AMM 80-11-01 OPS AND LEAK CHECK NORMAL NO LEAKS.&NBSP;</P>)

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 80,852 hrs · 10,992 cycles

WX RADAR ONLY DEPICTS GROUND RETURNS DOES NOT SHOW EX OR TURBULENCE (<DIV>PERFORMED OPS CHECK OF WX RADAR IAW AMM 34-43-00. OPS CHECK GOOD AT THIS TIME.</DIV>)

Part: RELIEF VALVE — OBSTRUCTED (CABIN PRESSURE) · airframe 80,804 hrs · 10,974 cycles

ON POSTFLIGHT, FOUND OVER-PRESSURE RELIEF VALVE NOT FLUSH WITH FUSELAGE(<P>FOUND PIECE OF DEBRIS BETWEEN UPPER POSITIVE PRESSURE RELIEF VALVE FLANGE DOOR AND ACFT SKIN. REMOVED DEBRIS AND FLAPPER DOOR OPERATES NORMALLY PER AMM 21-32-00 NO DEFECTS NOTED.</P>)

Part: GENERATOR — MALFUNCTIONED (APU) · airframe 80,709 hrs · 10,940 cycles

APU WILL NOT PICK UP LOAD WHEN TRANSFERRING FROM EXT POWER.(<P>RESET APU POWER SYSTEM REF AMM 49-11-00. OPS CHECK GOOD POWER TRANSFER SATISFACTORY NO FURTHER DEFECTS NOTED.<BR /></P>)

Part: CONTROLLER — MALFUNCTIONED (COCKPIT TEMP) · airframe 80,695 hrs · 10,935 cycles

UNABLE TO MAINTAIN CONSTANT COCKPIT TEMPERATURE, EITHER HOT OR COLD. PERFORMED FIM 21-61 F/T 803, AND 822. NO FAULTS FOUND. RACKED THE ZONE TEMP CONTROLLER. OPS TESTED THE CONTROLLER. OPS TESTED GOOD 21-30-17.

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PUMP) · airframe 80,680 hrs · 10,929 cycles

CENTER RT FUEL PUMP EICAS MESSAGE PRIOR TO TAKEOFF. PERFORMED FIM TASK 28-22 FT 805, COULD NO DUPLICATE FAULT. PERFORMED AN OPS CHECK OF THE ENGINE FUEL FEED SYSTEM IAW AMM 28-22-00. OPS CHECKED NORMAL, NO FAULTS FOUND.

Part: PRESSURE SWITCH — INOPERATIVE (FUEL SYSTEM) · airframe 80,642 hrs · 10,920 cycles

LEFT AFT FUEL PUMP PRESSURE LIGHT DOES NOT ILLUMINATE. PERFORMED FIM 28-22 FT 828, BLOCK 23. FOUND THE LEFT AFT PRESSURE SWITCH INOPERATIVE. REMOVED AND REPLACED L AFT AFT FUEL PUMP PRESSURE SWITCH IAW AMM 28-42-01, OPS CHECKED GOOD, NO FUTHER DEFECTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT PACK TEMP) · airframe 80,642 hrs · 10,920 cycles

LEFT PACK TEMP EICAS. COMPLIED WITH QRH PROCEDURE WITH CLEARED EICAS&NBSP;(<P>PERFORMED FIM TASK 21-31 FT 803 ACCOMPLISHED. OPS CHECK NORMAL AT THIS TIME.&NBSP;</P>)

Part: APU — FAULTED · airframe 80,571 hrs · 10,897 cycles

APU FAULT WHEN ATTEMPTING TO START&NBSP;(<P>TROUBLESHOOT PER FIM 49-65-06 CLEARED FAULT ON ECU&NBSP; STARTED SEVERAL TIMES NO DEFECTS NOTED&NBSP;&NBSP;</P>)

Part: FAN — MALFUNCTIONED (E&E BAY) · airframe 80,552 hrs · 10,889 cycles

AFT EQUIPMENT FAN NR 2 INOP. REMOVED AND REPLACED NR 2 FAN IAW AMM 21-58-41. OPS CHECK GOOD.

Part: BLOWER — WARNING MESSAGE (CARGO BAY) · airframe 80,522 hrs · 10,877 cycles

CARGO DET AIR MESSAGE. PLACED ON MDDR 106775. REPLACED NR 1 AND NR 2 AFT BLOWERS. CHECKS GOOD, PER AMM 26-16-02. CLOSED MDDR. REPLACED NR 1 AND NR 2 AFT BLOWERS. CHECKS GOOD, PER AMM 26-16-02. CLOSED MDDR.

Part: STARTER — INOPERATIVE (APU) · airframe 80,508 hrs · 10,872 cycles

APU WONT START.&NBSP;(<P>TRANSFERRED TO MDDR 106752 IAW DDG 49-11-01A CAT "C"&NBSP;</P><P>LP 1031066 -M2 REMOVED AND REPLACED STARTER ASSY MOTOR IAW AMM 49-41-01 OPS CHECK GOOD

Part: FAN — FAILED (EQUIP BAY) · airframe 80,525 hrs · 10,879 cycles

STATUS CARGO DET&NBSP; AIR(<P>TRANSFER TO MDDR 3 106776 CAT C DUE DATE 11FEB-19 PLACARD INSTALLED&NBSP;</P><P>LP 1031066-M3 REMOVED AND REPLACED&NBSP; AFT EQUIP COOLING FAN IAW AMM 21-58-11 OPS TEST OK CLEARED MDDR 106776</P>)

Part: CONTROLLER — MALFUNCTIONED (RT ENGINE PRV) · airframe 80,533 hrs · 10,882 cycles

R/H ENGINE PRV STATUS MSG.(<P>R&AMP;R PRV CONTROLLER IAW AMM 36-11-19. OPS CHECK GOOD @ THIS TIME. NO STATUS MSG PRESENT.<BR /></P>)

Part: RELAY — MALFUNCTIONED (APU) · airframe 80,492 hrs · 10,865 cycles

APU FAULT FAILED TO START(<P>TRANSFER TO MDDR 106611 IAW MEL 49-11-01A.</P><P>ACCOMPLISHED OPERATIONAL TEST OF THE APU. WHEN TRU BREAKER IS PULLED, APU STARTS NORMALLY. SUSPECT TRU MIGHT BE FAILING IAW&NBSP;B767 AMM 49-40-00 AND 49-61-00. REPLACED K615 APU START RELAY IAW SWPM 20-81-14 OPS CHECK GOOD. THIS CLEARS MDDR 106611</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENGINE BLEED) · airframe 80,504 hrs · 10,871 cycles

ON INITIAL &AMP; DURING DESENT L ENG BLEED OFF EICAS MESSAGE AND OFF LT ON LEFT BLEED SWITCH WOULD COME ON AND THEN GO OUT WHEN POWER CAME BACK UP OR PACK TURNED OFF.(<P>PERFORMED ENGINE RUNS IAW MM 71-00-20 OPS CK GOOD NO DEFECTS NOTED PERFORMED AIR SUPPLY BITE MODULE TEST IAW 767 AMM 36-11-00, OPS GOOD NO DEFECT FOUND AT THIS TIME.<BR /></P>)

Part: GCU — INOPERATIVE (APU) · airframe 80,290 hrs · 10,791 cycles

APU GEN INOP&NBSP;(<P>DEFERRED APU GEN IAW DDG 24-00-02A MDDR 105274&NBSP;</P><P><BR /></P><P>REMOVED &AMP; REPLACED APU GCU IAW AMM 24-22-02, OPS CKD NML</P>)

Part: ACTUATOR — LEAKING (RT SPAR VALVE) · airframe 80,239 hrs · 10,775 cycles

RIGHT ENGINE SPAR VALVE LEAKING(<P><SPAN>REMOVED AND REPLACED RIGHT ENG SPAR VALVE ACTUATOR IAW MM 28-22-11 LEAK CH GOOD AND OPS / CH GOOD&NBSP;</SPAN></P>)

Part: SWITCH — OBSTRUCTED (COCKPIT) · airframe 80,231 hrs · 10,770 cycles

LEFT FUEL CONTROL SWITCH DOES NOT SNAP INTO CUTOFF POSITION, MAKING IT EASY TO ACCIDENTALLY LEAVE IT IN "RUN" INADVERTANTLY. CLEANED DEBRIS FROM LT FUEL CONTROL SWITCH DETENT, OPS TEST GOOD IAW AMM 76-11-00.

Part: PACKING — DAMAGED (AC BAY) · airframe 80,199 hrs · 10,756 cycles

RT PACK LEAKING DUCT 90 DEGREE FITTING. REMOVED AND REPLACED PACKING TO RT COMPRESSOR OUTLET DUCT AT 90 DEGREE ELBOW FITTING REF AMM 21-51-13. ACCOMPLISHED OPS AND LEAK CHECK. OPS REF AMM 21-51-00/601.

Part: CLAMP — MISSING (THRUST REVERSER) · airframe 80,199 hrs · 10,756 cycles

ENGINE NR 1 I/B THRUST REVERSER UPPER FLEX SHAFT BRAID BROKEN MISSING CLAMP. REMOVED AND REPLACED ENG NR 1 I/B THRUST REVERSER UPPER FLEX SHAFT IAW AMM 78-31-18. REINSTALLED CLAMP. OPS CHECK GOOD PER AMM 78-31-00.

Part: GENERATOR — INOPERATIVE (LT ENGINE) · airframe 80,197 hrs · 10,755 cycles

LEFT HMG INOPERATIVE. ACCOMPLISHED MAINTENANCE PROCEDURE. PLACARD INSTALLED. R&R LEFT HYDRAULIC MOTOR GENERATOR IAW AMM 24-25-01.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 80,189 hrs · 10,751 cycles

STATUS MESSAGE RIGHT ENGINE PRV. CREW FEED BACK, REPORTED NO PRESSURE FLUCTUATIONS, ALL NORMAL TEMPERATURE CONDITIONS, NO BLEED PRESSURE LIGHT INDICATION. COMPLIED WITH AIR SUPPLY CONTROL SYSTEM TEST. BITE PASS IAW AMM CH 36-23-00, MESSAGE ERASED IAW AMM CH 31-41-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 80,189 hrs · 10,751 cycles

APU FAULT TWICE WHEN TRYING TO START AFTER LANDING. TROUBLESHOT THE ECU. NO FAULTS NOTED AT THIS TIME.

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 80,153 hrs · 10,736 cycles

APU WOULD NOT START 2 ATTEMPTS. PERFORMED APU START OF APU, NO FAULTS DETECTED AT THIS TIME AMM 49-40-00.

Part: VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 80,149 hrs · 10,735 cycles

STATUS MESSAGE R ENG PRV. PERFORMED BITE PROCEDURE IAW FIM TASK 36-10 FT 847 PRV FAULT DISPLAYED. REMOVED AND REPLACED PRV V352 IAW AMM 36-11-18. OPERATIONAL CHECK IS NORMAL.

Part: CONTROLLER — NOT REPORTED (LT PACK TEMP) · airframe 80,118 hrs · 10,721 cycles

LEFT PACK TEMP(<P>LEFT PACK TRANSFERRED TO MDDR 103467 MEL 21-51-01-01 CAT C DUE 06DEC18, REMOVED AND REPLACED PACK CONTROLLER IAW 21-61-03 OPS CKS NORMAL DEFERALL CLEARED.</P>)

Part: APU — UNKNOWN · airframe 80,076 hrs · 10,708 cycles

APU FAILED TO START. 2 ATTEMPTS IN THE AIR AND 1 ATTEMPT ON THE GROUND AFTER LANDING.(<P><SPAN>BIT / THE APU BOX IAW FIM 49-11-00-815-987. OPS CHECK GOOD. RAN APU MULTIPLE TIMES / COULD NOT DUPICATE FAULT</SPAN></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (PR VALVE) · airframe 80,076 hrs · 10,708 cycles

STATUS MESSAGE: R ENG PRV.(<P><SPAN>PERFORMED / BITE CHECK IAW AMM 36-23-00. NO FAULTS NOTED AT THIS TIME.</SPAN></P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (RT ENGINE) · airframe 80,022 hrs · 10,689 cycles

RIGHT ENGINE PRV STATUS MESSAGE&NBSP;(<P>CLEARED MESSAGE, BITE CHECK OF AIR SUPPLY INDICATION SYSTEM PASSED. NO OTHER FAULTS NOTED IAW AMM 36-10-00</P>)

Part: BULB — INOPERATIVE (CONTROL PANEL) · airframe 80,022 hrs · 10,689 cycles

F/O EFIS CONTROL PANEL WEATHER RADAR LIGHT INOP&NBSP;(<P>NO BULBS REQUIRED ON WEATHER RADAR SWITCH. SELECT SWITCH ON EFIS CONTROL PANEL REF. WIRING DIAGRAM MANUAL 34-43-22-3 AND 34-43-12 SYSTEM TEST GOOD IAW AMM 34-43-00</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENG PRV) · airframe 80,014 hrs · 10,685 cycles

AFTER THE RT ENGINE START, HAD A RIGHT ENGINE PRV STATUS MESSAGE. TROUBLESHOT IAW FIM 36-20-00, AND AMM 36-23-00. NO FAULTS NOTED.

Part: SEAL — LEAKING (STARTER) · airframe 79,918 hrs · 10,651 cycles

CAPPED THE NR 1 ENGINE DRAIN LINES, STARTER, IDG, FUEL PUMP, HMU, AND HYDRAULIC PUMP IAW AMM 71-71-00, AND ECM 2018P-694, DUE TO HIGH OIL CONSUMPTION. REMOVED AND REPLACED THE NR 1 ENGINE STARTER ACCESSORY GEARBOX SEAL IAW AMM 80-11-01, AND 72-64-02. OPS AND LEAK CHECKED GOOD.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 79,870 hrs · 10,635 cycles

STATUS MSG ENGINE VIB BITE. PERFORMED ENGINE VIB BITE PROCEDURE IAW AMM 34-41-00, 77-31-00 AND FIM 77-31. FOUND NO FAULT AND ERASED MESSAGE.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 89,115 hrs · 16,730 cycles

HI FLOW INHIBIT STATUS MESSAGE. PERFORMED FIM 21-51 FT 854 AND NO FAULTS FOUND.

Part: A/C PACK — FAULTY (APU) · airframe 79,849 hrs · 10,626 cycles

APU SHUTDOWN ON PUSH BACK. PERFORMED FIM 49-11FT 994. REMOVED AND REPLACED SURGE VALVE IAW AMM 49-53-01.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 79,830 hrs · 10,619 cycles

RT ENG PRV STATUS MSG. PERFORMED AIR SUPPLY BITE PROCEDURE IAW FIM TASK 36-20-FT 805, MSG CLEARED. PERFORMED BITE PROCEDURES NOT FAULTS NOTED.

Part: UNKNOWN — MALFUNCTIONED (AUTOTHROTTLE SYS) · airframe 79,581 hrs · 10,533 cycles

ON INITIAL DESCENT FROM FL390 TO FL 370. THROTTLE DEVELOPED A SIGNIFICANT SPLIT, RT ENGINE WOULD THEN NOT ACCELERATE ABOVE 87.7 N1 REGARDLESS OF AUTOTHROTTLE ENGAGEMENT. PERFORM PER ACCORDANCE TEST IAW AMM 71-00-00. ALL ENG PARAMETERS NORMAL, NO THROTTLE SPLIT. ACCOMPLISHED THRUST MANAGEMENT SYSTEM OPERATIONAL TEST IAW AMM 22-32-00, SYSTEM OPS TEST NORMAL.

Part: MONITOR — MALFUNCTIONED (ENGINE) · airframe 79,551 hrs · 10,523 cycles

EICAS MSG ENGINE VIBRATION. REMOVED AND REPLACED THE ENGINE VIBRATION MONITOR UNIT IAW AMM 77-31-03. OPS CHECK NORMAL.

Part: CIRCUIT BREAKER — FAULTY (COCKPIT) · airframe 79,551 hrs · 10,523 cycles

CIRCUIT BREAKER C830 HYD GEN 28 VDC. POWER WILL NOT RESET. REPLACED CIRCUIT BREAKER IAW AMM TASK 24-25-00-715-00 AND WDM 24-31-11.

Part: FAN — MALFUNCTIONED (E&E BAY) · airframe 79,544 hrs · 10,520 cycles

FWD EQ SUP FAN 1 MESSAGE. REMOVED AND REPLACED FORWARD SUPPLY FAN IAW AMM 21--58-06. OPS CHECK GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 79,325 hrs · 10,440 cycles

EMERGENCY LIGHT "UNARMED" LIGHT HALF ILLUMINATED. RELAMPED LIGHT IAW AMM 33-13-00, OPS CKECK GOOD.

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 79,301 hrs · 10,431 cycles

WEATHER RADAR TILT FUNCTION INOP. WEATHER RADAR AUTO TILT, MANUAL TILT OPS CHECK GOOD IAW AMM 34-43-00. NO DEFECTS NOTED AT THIS TIME.

Part: FASTENER — LOOSE (APU) · airframe 79,284 hrs · 10,425 cycles

APU FAULTY CAUTION MSG ON START AFTER LANDING. APU ECU BITE FOUND MSG START ABORTED, PERFORMED TROUBLE SHOOTING IAW FIM 49-11, FT 989. FOUND IGV ACTUATOR MOUNTING HARDWERE LOOSE, SECURED HARDWARE IAW AMM 49-52-02. PERFORMED 3 SUCCESFUL STARTS, NO DEFECT NOTED A THIS TIME.

Part: OIL SYSTEM — LOW (APU) · airframe 79,254 hrs · 10,416 cycles

APU FAULT. SVCD APU OIL IAW AMM 12-13-04. ALSO CHECKED FOR FAULTS ON ECU WITH NONE NOTED. APU RUNS CHECKS OK, (ADDED 01 QT).

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 79,243 hrs · 10,411 cycles

ATTEMPTED APU START AFTER LANDING, EICAS APU FAULT WITH FAULT LT. RAN QRH, ATTEMPTED SECOND START WITH SAME RESULT. CONDUCTED APU START 6 TIMES IAW AMM 49-11-00. APU STARTED EVERYTIME ON THE FIRST ATTEMPT. NO FAULT CODES WERE NOTED ON THE ECU AT THIS TIME. OK FOR SERVICE. AN APU COLD SOAK START VERIFICATION DMI WAS OPENED.96929)</P>)

Part: NOT REPORTED — MALFUNCTIONED (APU) · airframe 79,076 hrs · 10,351 cycles

APU INOP. PERFORMED BITE PROCEDURES IAW AMM 49-11 FT 958, OPS CHECK GOOD AND NO FAULTS NOTED. DUCT PRESSURE NORMAL AND APU PNEUMATIC LOAD DEMAND GOOD. ENGINE RUNS SUCCESSFUL.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 79,013 hrs · 10,330 cycles

RT ENGINE FIRE LP1 STATUS MESSAGE. NOTED BY PILOT, NO STATUS MSG DISPLAYED AT THIS TIME.

Part: MONITOR — MALFUNCTIONED (COCKPIT) · airframe 78,982 hrs · 10,320 cycles

ENG VIBE INDICATIONS WENT BLANK NO READOUT OR POINTERS. REMOVED AND REPLACED AIRBORNE VIBRATION MONITORING UNIT PER AMM 70-10-01. OPS CHECK GOOD AT THIS TIME IAW AMM 77-31-00.

Part: RELAY — FAILED (LE FLAP) · airframe 78,969 hrs · 10,314 cycles

LE FLAP ASYM WHEN RETRACTING FLAPS AFTER T/O FLAP INDICATION NEEDLES STOPPED BETWEEN UP AND 1. REPLACED FLAPS INTERNAL/RETRACT MH REF RELAY K353IAW SWPM 20-81-22, REPLACED LEN08 PROX SENSOR S304 IAW AMM 27-08-00. PERFORMED INDUCTANCE AND RESISTANCE CK OF OF THE S304 IAW AMM SERVICE LETTER 767-SL- 27-103C WITH TARGET NEAR 5.9MH 5.9MH TARGET FAR 4.8 RESISTANCE 20.0 HM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 78,969 hrs · 10,314 cycles

EXTERNAL EMERGENCY EXIT LIGHT INOP. RELAMPED L388 EXTERNAL EMERG EXIT LIGHT IAW AMM 33-51-17 OPS CHECKED GOOD.

Part: CONNECTOR — DISCONNECTED (AC BAY) · airframe 78,968 hrs · 10,312 cycles

LT PACK TEMP CONTROLLER FAILS BITE FOR CONTROLLER FAULT. RECONECTED PLUG TO T5178 IAW AMM 21-65-03 PERFORMED SATISFACORY LT PACK TEMP CONTROLLER BITE IAW AMM 21-51-14.

Part: VALVE — DAMAGED (IDG) · airframe 78,969 hrs · 10,314 cycles

NR 1 ENG IDG HEAT EXCHANER AIR/SHUT OFF VALVE WAS FOUND TO HAVE DAMAGED THREADS IN THE FILTER PORT. R&R NR 1 ENG IDG HEAT EXCHANGERS AIR/SHUTOFF VALVE AMM 24-11-07 OP/LK CHECK SATISFACTORY IAW AMM 71-00-00/NO DEFECT NOTED.

Part: INSULATION — DAMAGED (IDG) · airframe 78,969 hrs · 10,314 cycles

ENG NR 1 IDG POWER CABLE HAS DAMAGED COLD SHRINK INSULATION AT T3 LEAD. NR 1 ENG IDG POWER CABLE COLD SHRINK INSULATION AT T3 LEAD IAW AMM 24-11-01 & SWPM 20-30-14. PERFORMED SATISFACTORY OPS CHECK IAW 15767 AMM 71-00-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 76,502 hrs · 16,476 cycles

LE SLAT ASYM WHEN TRIMING TO RETRACT FLAPS AFTER T/O. PERFORMED FIM 27-81 FAULT TREE 809 NO FAULTS NOTED, OPERATED SLAT AND FLAP NUMEROUS TIME NO FAULTS NOTED.

Part: INSULATION — DAMAGED (IDG) · airframe 78,968 hrs · 10,312 cycles

ENG NR 2 IDG POWER FEEDER CABLE HAS DAMAGED COLD SHRINK INSULATION SLEEVE ATT2 LEAD. R&R NR 2 ENG IDG COLD SHRINK ATT2 LEAD IAW AMM 24-11-01 SWPM 20-30-14. ACCOMPLISHED TEST OF THE IDG SHOWN IN THE POWER PLANT TEST REF TABLE 71-00-00/201 CONFIG3 TEST GOOD.

Part: RELAY — DEFECTIVE (FIRE SUPPRESSION) · airframe 78,969 hrs · 10,314 cycles

28VDC STILL PRESENT ON CARGO FIRE BOTTLE SQUIBS WHEN DISCHARGE SWITCH SWITCH IS RELEASED UNTIL SYSTEM IS DISARMED. T/S CARGO FIRE BOTTLE SQUIBS IAW R767 SSM 26-23-01 FOUND X2 RECESSED PINS ON RELAY K822. RECESSED PIN X2 IAW SWPM 20-15-46 & 26-23-12 OPS GOOD IAW AMM 26-23-01.

Part: WARNING MESSAGE — FALSE ACTIVATION (FIRE LOOP) · airframe 78,955 hrs · 10,305 cycles

RIGHT ENGINE FIRE LOOP 1 STATUS MESSAGE. PERFORMED AN OPS CHECK IAW AMM 26-10-00. NO DEFECTS NOTED. PERFORMED FIM 26-11 TREE 806, SYSTEM CHECKED OK.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT A/C PACK) · airframe 78,838 hrs · 10,266 cycles

DURING DESCENT, RIGHT PACK OFF EICAS MESSAGE ILLUMINATED FOR MOMENT. RESET THE RIGHT PACK CONTROLLER, AND BITE CHECKED, NO FAULTS NOTED. OPS CHECKED NORMAL IAW AMM 21-50-00, AND 21-51-00.

Part: CONTROLLER — FAILED (WINDOW HEAT) · airframe 78,723 hrs · 10,224 cycles

AFTER LANDING, RT FWD WINDOW EICAS MESSAGE. REPLACED THE WINDOW HEAT CONTROLLER, TESTED NORMAL IAW AMM 30-41-07.

Part: IGNITION LEAD — FAILED (APU) · airframe 78,695 hrs · 10,215 cycles

APU INOPERATIVE, DID NOT START. REMOVED AND REPLACED IGNITION LEAD IAW AMM 49-41-04, OPS CHECKED GOOD IAW 49-11-00.

Part: IGNITER — MALFUNCTIONED (RT ENGINE) · airframe 78,560 hrs · 10,167 cycles

RIGHT ENGINE IGNITOR 2 STATUS MESSAGE. REMOVED AND REPLACED THE IGNITER IAW AMM 74-21-02, OPS CHECKED NORMAL , NO MESSAGE PRESENT,

Part: PRIORITY VALVE — FAILED (LT ENGINE) · airframe 78,461 hrs · 10,130 cycles

LEFT PRV VALVE POSITION INDICATION ON AIR SUPPLY MONITOR SHOWS ERROR. REMOVED AND REPLACED NR 1 ENGINE PRV VALVE IAW AMM 36-11-18.

Part: SENSOR — FAULTED (DUCT PRESSURE) · airframe 78,461 hrs · 10,130 cycles

DUCT PRESSURE SENSOR M1843 FAULTY. REMOVED AND REPLACED THE DUCT PRESSURE SENSOR IAW AMM 36-21-08. OPS CHECKED NORMAL.

Part: ACCELEROMETER — FLUCTUATES (RT ENGINE) · airframe 78,461 hrs · 10,130 cycles

RT ENGINE INDICATION FLUCTUATES BETWEEN 0 - 5 WITH ON AND OFF. REMOVED AND REPLACED THE RT ACCELEROMETER IAW AMM 77-31-02. OPS CHECKED NORMAL.

Part: IGNITION LEAD — BROKEN (APU) · airframe 78,461 hrs · 10,130 cycles

APU IGNITER LEAD TIP BROKEN. REMOVED AND REPLACED IGNITION LEAD IAW AMM 49-41-04.

Part: SENSOR — FAULTED (FAN AIR TEMP) · airframe 78,461 hrs · 10,130 cycles

FAN AIR TEMP RT SENSOR FAULTY DURING OP CHECK. REMOVED AND REPLACED THE FAN AIR TEMP SENSOR IAW AMM 36-11-17.

Part: TERMINAL — DIRTY (PRI VALVE) · airframe 78,461 hrs · 10,130 cycles

PRV INDICATION VALVE POSITION FAULTY DURING OPS CHECK. CLEANED THE TERMINAL AT THE PRV D4156P CONNECTOR IAW AMM 36-00-30, INDICATIONS NORMAL.

Part: PRIORITY VALVE — FAILED (RT ENGINE) · airframe 78,461 hrs · 10,130 cycles

RIGHT PRV STUCK IN PARTIAL POSITION DURING ASM ENGINE RUN. REMOVED AND REPLACED THE PRV IAW AMM 36-11-18.

Part: WARNING MESSAGE — FALSE ACTIVATION (PRV) · airframe 78,446 hrs · 10,121 cycles

RIGHT ENGINE PRV STATUS MESSAGE AFTER BLOCK OUT. RT BLEED SYSTEM CHECKED GOOD IAW FIM 36-10 TREE 848. AIRCRAFT OK FOR CONTINUED SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (RT PRV) · airframe 78,452 hrs · 10,125 cycles

STATUS MESSAGE FOR THE RIGHT ENGINE PRV. RT ENG PRV CHECKED GOOD IAW FIM 36-20-00-21, OK FOR SERVICE.

Part: APU — SHUTDOWN · airframe 78,444 hrs · 10,120 cycles

APU SHUTDOWN ON RAMP. PERFORMED AN OPS CHECK OF APU, ALL CHECKED NORMAL. RAN APU ONE HOUR, NO PROBLEMS OR SHUTDOWNS IAW AMM 49-00-00.

Part: RADAR — MALFUNCTIONED (WX SYSTEM) · airframe 78,431 hrs · 10,115 cycles

WEATHER RADAR FAILED WITH LEFT WEATHER SYS SELECTED. CIRCUIT BREAKER F2 TRIPPED. WEATHER RADAR SYS STATUS MESSAGE. RESET THE CIRCUIT BREAKER. WEATHER RADAR GROUND TESTED OK IAW AMM 34-43-00.

Part: DUCT — UNSECURE (ANTI-ICE) · airframe 78,389 hrs · 10,095 cycles

ON ARRIVAL, PERFORMED WALK AROUND AND FOUND THE RT LE ANTI-ICE DUCT BLOWOUT PANEL BLOWN OUT ON OUTBOARD SIDE OF RT ENGINE. EVALUATED LE ANTI-ICE DUCT AND FOUND RT LE DUCT UNSECURE. SECURED TH ERH LE ANTI-ICE DUCT IAW AMM 30-11-06. LEAK CHECKED GOOD.

Part: CONTROL VALVE — FAILED (APU) · airframe 78,355 hrs · 10,079 cycles

APU DUCT PRESSURE DROPPED TO 15 PSI DURING START. REMOVED AND REPLACED SURGE CONTROL VALVE IAW AMM 49-53-01, OPS CHECKED GOOD.

Part: APU — LOW PRESSURE · airframe 78,321 hrs · 10,063 cycles

APU NOT PRODUCING ENOUGH PRESSURE 15 PSI&NBSP;(<P>RESET APU AND PERFORMED BITE CHECK IAW AMM 49-40-01 OPS CHECK OK&NBSP;</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (EXHAUST FAN) · airframe 78,291 hrs · 10,050 cycles

AFT EQ EXH FAN 2 STATUS MSG(<P>CLEARED MSG. OPS TEST IAW 21-58-00. CKS GOOD</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (FAN) · airframe 78,277 hrs · 10,043 cycles

STATUS MSG AFT EQ EXH FAN 2.(<P>PERFORMED OPS CHECK, IAW AMM 21-58-00, NO DEFECTS NOTED. OPS CHECK GOOD.</P>)

Part: BLEED AIR SYS — INOPERATIVE (APU) · airframe 78,247 hrs · 10,029 cycles

APU INOP WILL NOT SUPPLY BLEED PRESSURE(<P>REOPENED MDDR 86667 MEL 49-11-01A&NBSP; CAT C DUE 10DEC17</P>)

Part: ACTUATOR — MALFUNCTIONED (APU IGV) · airframe 78,229 hrs · 10,020 cycles

DURING ENG START DUCT PRESS DROPPED BELOW 10PSI AND N2 ROTATION STAGNATED AT 14.9%. REMOVED AND REPLACED IGV ACTUATOR I.A.W AMM 49-52-02 OPS CHECK C/W , APU OPERATES NORMAL.

Part: STARTER — MALFUNCTIONED (RT ENGINE) · airframe 78,219 hrs · 10,015 cycles

RIGHT ENGINE WOULD NOT START, TWO ATTEMPTS WITHOUT START. OPS CHECKED GOOD IAW MM 71-00-00.

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 78,134 hrs · 9,972 cycles

CARGO FIRE LOOP A NR 4 INDICATOR LIT. PLACARD INSTALLED, MCC NOTIFIED. TESTED PER AMM OPS CKS NORMAL.

Part: SMOKE DETECTOR — INOPERATIVE (MAIN CARGO) · airframe 78,069 hrs · 9,940 cycles

MAIN CARGO SMOKE DETECTOR A4 INOPERATIVE. R & R THE SMOKE DETECTOR, OPS CHECKED OK IAW AMM 26-14-00.

Part: FAULT LIGHT — FALSE ACTIVATION (APU) · airframe 78,061 hrs · 9,936 cycles

APU FAULT AFTER START. PERFORMED APU ECU BITE IAW AMM 49-61-05. NO FAULTS NOTED PERFORMED OPERATIONAL CHECK IAW AMM 49-11-00, OPS CHECKED GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (APU) · airframe 78,061 hrs · 9,936 cycles

DURING PREDEPARTURE, APU FAULTED AFTER RUNNING FOR 22 MINUTES. PACK OFF, APU BLEED VALVE OPEN. PERFORMED A BITE TEST, NO FAULTS FOUND IAW 49-05-00.

Part: FILL PORT — MISSING (STARTER) · airframe 77,951 hrs · 9,897 cycles

LEFT ENGINE STARTER FILL PORT MISSING. INSTALLED THE FILL PORT IAW AMM 80-11-01.

Part: RELAY — FAILED (RT AOA HEAT) · airframe 77,949 hrs · 9,896 cycles

RIGHT AOA HEAT DISCRETE LIGHT INOPERATIVE. REMOVED AND REPLACED THE K401 RELAY. OPS CHECKED NORMAL IAW AMM 30-33-00.

Part: WINDOW — MALFUNCTIONED (L1) · airframe 77,951 hrs · 9,897 cycles

L1 COCKPIT WINDOW HAS SPARE SENSOR INOPERATIVE. REMOVED AND REPLACED THE WINDOW IAW AMM 56-11-01. OPS CHECKED NORMAL.

Part: ROD — BROKEN (NR 1 NACELLE) · airframe 77,934 hrs · 9,887 cycles

NR 1 ENGINE OUTBOARD SIDE FWD HOLD OPEN ROD BROKEN. REMOVED AND REPLACED THE HOLD OPEN ROD IAW AMM 71-11-10 AND 20-11-00.

Part: CONNECTOR — DAMAGED (PRESSURE SWITCH) · airframe 77,934 hrs · 9,887 cycles

FOUND THE NR 2 ENGINE SCAVENGE OIL PRESSURE SWITCH BACKSHELL CONNECTOR BROKEN ON SWITCH SIDE. REPLACED PRESSURE SWITCH IAW AMM 79-33-01, OPS AND LEAK CHECKED GOOD.

Part: STARTER — MALFUNCTIONED (RT ENGINE) · airframe 77,921 hrs · 9,883 cycles

BTB EICAS MESSAGE FOR RT ENGINE STARTER, ABORTED START, DUCT PRESSURE AT START 9 PSI MAX, ACCOMPLISHED APU ECU BITE CHECK IAW AMM 49-61-05, OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (FUEL PUMP SWITCH) · airframe 77,904 hrs · 9,878 cycles

RIGHT FWD FUEL PUMP INOPERATIVE. REMOVED AND REPLACED THE FUEL PUMP SWITCH LIGHT ASSY IAW AMM 33-13-00, OPS CHECKED GOOD.

Part: PCA — LEAKING (LT ELEVATOR) · airframe 77,796 hrs · 9,841 cycles

C HYD QTY EICAS MESSAGE DISPLAYED DURING CRUISE. COMPLIED WITH QRH PROCEDURE, C HYD QTY CONTINUED TO DECREASE, CONSULTED WITH MCC ENROUTE, MONITORED HYD QTY SAW A SLOW BUT STEADY DECREASE DURING DESCENT. COMPLETED QRH PROCEDURE. DURING ALTERNATE FLAP EXENSION, T/E FLAP DISAGREE EICAS MESSAGE DISPLAYED AT FLAPS 5. COMPLETED QRH PROCEDURE RESULTED IN A FLAPS 5 LANDING. REMOVED AND REPLACED LEFT ELEVATOR CENTER PCA IAW AMM 27-31-05. OPS AND LEAK CHECKED NORMAL.

Part: RELAY — FAILED (AOA) · airframe 77,330 hrs · 9,690 cycles

RIGHT ANGLE OF ATTACK CIRCUIT BREAKER TRIPPED. REMOVED AND REPLACED RELAY K646. OPS CHECKED GOOD IAW AMM 30-22-21.

Part: BLEED VALVE — DAMAGED (APU) · airframe 77,260 hrs · 9,665 cycles

APU SURGE VALVE FILTER ASSY MISSING A SPRING. REMOVED AND REPLACED APU SURGE BLEED VALVE IAW AMM 49-53-01. OPS CHECKED GOOD.

Part: MONITOR — MALFUNCTIONED (VIBRATION) · airframe 77,022 hrs · 9,592 cycles

RT ENGINE VIBRATION INDICATION, LPT 5.0 AND FAN 5.0 INTERMITTENTLY, ALL OTHER PARAMETERS NORMAL. REMOVED AND REPLACED AVM UNIT IAW AMM 77-31-03. PERFORMED AVM OPERATIONAL CHECK IAW AMM 77-31-00, NO FAULTS NOTED, OPS CHECKED NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (ENGINE VIBRATION) · airframe 77,003 hrs · 9,587 cycles

RIGHT ENGINE VIBRATION INDICATED 5.0 LPT INTERMITTENTLY, ENGINE OPS NORMAL, BB INDICATION. HARDWARE, AND ELEC CONNECTORS , WIRING, AND MOUNTS INSPECTED FOR CONDITION IAW FIM 77-31-808, NO DEFECTS NOTED.

Part: WARNING LIGHT — FALSE ACTIVATION (ENGINE VIBRATION) · airframe 77,003 hrs · 9,587 cycles

RIGHT ENGINE VIBRATION LIGHT, CHECKED MOUNTING HARDWARE, ELEC CONNECTORS, AND WIRING FOR PROPER MOUNTING AND CONDITION CHECKED FOR BENT AND BROKEN PINS AND WIRES IAW FIM FAULT TREE 77-31-808, NO PROBLEMS FOUND AT THIS TIME NO FURTHER ACTION REQUIRED AT THIS TIME.

Part: INDICATOR — MALFUNCTIONED (VIBRATION) · airframe 76,961 hrs · 9,575 cycles

RIGHT ENGINE VIBRATION NEEDLE INTERMITTANTLY PEGS HIGH, ENGINE OPS NORMAL. REMOVED, INSPECTED, AND CLEANED THE CONNECTORS. TIGHTENED THE ACCELEROMETERS, INSTALLED CONNECTORS IAW 77-31-05. CONDUCTED BITE TEST IAW 77-31-00. OPS CHECKED NORMAL.

Part: ECU — MALFUNCTIONED (APU CONTROL) · airframe 76,949 hrs · 9,572 cycles

UNABLE TO START APU, PERFORMED FIM 49-11 TREE 958 NO FAULTS NOTED. RE RACK APU ECU IAW AMM 49-61-05. APU OPS CKS NORMAL. APU START SUCCESSFULLY.

Part: BATTERY — INOPERATIVE (MASTER) · airframe 76,929 hrs · 9,567 cycles

MAIN BATTERY INOPERATIVE AND NOT CHARGING. REMOVED AND REPLACED THE MAIN BATTERY IAW AMM 24-31-02. CHECKED NORMAL.

Part: CONTROL VALVE — MALFUNCTIONED (RT A/C PACK) · airframe 76,921 hrs · 9,563 cycles

RIGHT PACK EXTREMELY LOUD ON FINAL. REMOVED AND REPLACED THE FLOW CONTROL VALVE IAW AMM 21-51-01.

Part: CONTROL CARD — MALFUNCTIONED (RT A/C PACK) · airframe 76,891 hrs · 9,554 cycles

RT A/C PACK EXCESSIVELY LOUD ON TAXI, CLIMB, & CRUISE. REMOVED AND REPLACED THE RIGHT PACK FLOW CONTROL CARD IAW AMM 21-51-09. OPS CHECKED NORMAL AT THIS TIME.

Part: A/C PACK — MALFUNCTIONED (RIGHT) · airframe 82,494 hrs · 17,482 cycles

RT PACK OPERATING IN HIGH FLOW DURING ENTIRE FLIGHT. EXCESSIVE AIR NOISE. MAKING COMMUNICATION HARD. PERFORMED FIM TASK 21-51-813 AND OPS TEST OF PACK HIGH FLOW INHIBIT IAW AMM 21-51-00/705.

Part: A/C PACK — MALFUNCTIONED (RIGHT) · airframe 76,851 hrs · 9,541 cycles

RT PACK OPERATING IN HIGH FLOW AT ALL TIMES. EXCESSIVE AIR NOISE. OUTFLOW VALVE 70% OPEN WITH RT PACK ON. PERFORMED BITE TEST ON RT CONTROLLER, NO FAULTS NOTED. PERFORMED OPS CHECK OF RT PACK IAW AMM 21-51-00. SYSTEM CHECKED NORMAL. NO LOUD NOISE HEARD. OK FOR SERVICE.

Part: SENSOR — FAILED (N1) · airframe 76,817 hrs · 9,531 cycles

ENGINE VIBRATION BITE MAINTENANCE MESSAGE, PERFORMED FIM 77-31, FT 808, 77-31, FT 812. LEAD TO RT ENGINE N1 SENSOR SIGNAL CUT OUT. REMOVED AND REPLACED THE RT ENGINE N1 SENSOR IAW 77-12-01. OPS CHECKED GOOD.

Part: INDICATION SYS — MALFUNCTIONED (RT ENGINE) · airframe 76,736 hrs · 9,507 cycles

AT RT ENGINE START, THE N1 INDICATION WAS ZERO UNTIL FUEL CONTROL WAS IN RUN, FAN ROTATION VERIFIED BY GROUND CREW WHEN N1 SHOWED ZERO. PERFORMED PIMU BITE, NO FAULTS NOTED IAW FIM 71-01-00/101. PERFORMED OPS TEST IAW AMM 77-12-00. NO FAULTS NOTED, OPS NORMAL.

Part: CIRCUIT CARD — MALFUNCTIONED (OVERHEAT DETECT) · airframe 76,736 hrs · 9,507 cycles

RIGHT ENGINE OVERHEAT LOOP 1 ILLUMINATED. REMOVED AND REPLACED ALFOLTS CARD IAW FIM 26-11 TASK 804 AND SWPM 20-82-13. OPS CHECKED NORMAL.

Part: DETECTOR — MALFUNCTIONED (ENGINE OVERHEAT) · airframe 76,747 hrs · 9,510 cycles

STATUS MESSAGE FOR THE RT ENGINE OVERHEAT LOOP 1. REMOVED AND REPLACED THE RT ENGINE UPPER FWD OVERHEAT DETECTOR IAW AMM 26-11-02. OPS CHECKED NORMAL

Part: CIRCUIT CARD — FAILED (OVERHEAT LOOP) · airframe 76,704 hrs · 9,496 cycles

RT ENGINE OVERHEAT LOOP 1 STATUS MESSAGE DURING FLIGHT. REMOVED AND REPLACED THE RT OVERHEAT LOOP 1 DETECTOR CARD M689 IAW AMM 26-10-01 , OPS CHECKED OK.

Part: CIRCUIT CARD — NOT SEATED (FIRE LOOP) · airframe 76,704 hrs · 949,626 cycles

INTERMITTENT RT ENGINE OH LP 1 STATUS MESSAGE DURING CRUISE. PERFORMED ENGINE FIRE DETECTION SYSTEM BITE IAW FIM 26-11 TASK 804, SEATED THE CIRCUIT CARD M689 IAW AMM 26-10-01/401 FAULT CLEARED.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT A/C PACK) · airframe 76,685 hrs · 9,489 cycles

LEFT PACK BITE MAINTENANCE, FOUND A LOW LIMIT VALVE WARNING MESSAGE. CLEARED FAULT, PREFORMED BITE IAW FIM 21-51 FT 803, NO FAULTS. WIRING CHECKED BETWEEN D1590 - D9588 IAW WDM 21-51-12, NO FAULTS NOTED.

Part: RELAY — FAILED (LT A/C PACK) · airframe 76,685 hrs · 9,489 cycles

LEFT PACK BITE MAINTENANCE, PREFORMED FIM 21-51 FT 803. R & R RELAY K10317 IAW WDM 21-51-12 OPS NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI ICE VALVE) · airframe 76,655 hrs · 9,480 cycles

RT ENGINE TAI VALVE STATUS MESSAGE. PERFORMED FIM TASK 31-21-805 RESET MESSAGE. IAW FIM TASK 31-41-00. PERFORMED OPS CHECK NORMAL NO FAULTS NOTED.

Part: VALVE — FAULTED (LT A/C PACK) · airframe 76,588 hrs · 9,459 cycles

LEFT PACK BITE MAINTENANCE MESSAGE, FAULTS LEFT PACK LOW LIMIT VALVE. PERFORMED FIM TASK 803 & 21-51 REV 1. LT PACK CONTROLLER IAW FIM TASK REMOVED AND REPLACED LOW LIMIT VALVE IAW AMM 21-51-11. NO FAULTS FOUND.