N1409A

Part: TARGET — OUT OF POSITION (ZONE 500) · airframe 102,612 hrs · 21,501 cycles

AFTER LIFT OFF RECEIVED LE SLAT ASSYMETRY MESSAGE. RETURNED TO THE FIELD.

Part: SKIN — DENTED (ZONE 600 FLAP) · airframe 101,622 hrs · 21,021 cycles

INBOARD TRAILING EDGE FLAP RH WING , UPPER SIDE INNER CORNER WITH DENTS(<P>&NBSP;RH WING INBOARD AFT FLAP DENT 1 WAS EVALUATED AND FOUN WITHIN ALLOWABLE LIMITS IAW SRM 57-53-01-1A-1 TABLE I NOTE C DETAIL IV DOT 89020 WAS INSTALLED AS PER ATLAS AIR GMM 3.19.1.</P> / <P>&NBSP;</P> / <P>DENT 2 WAS REPAIRED IAW SRM 57-53-01-2R-1 FIG 201 SH EET 4 PAG 1-5 AND SRM 51-70-10-2R-4 FIG 201 SHEET 1 PAG 1,3 REV 50 15/AUG/24</P>)

Part: LIGHT — NO DISCREPANCY (EXTERIOR) · airframe 101,622 hrs · 21,021 cycles

EXTERIOR EMERGENCY LIGHTS INOP(<P>EXTERIOR EMERGENCY LIGHTS OPERATIONAL TEST WAS PERFORMED, TEST SATISFACTORY IAW AMM 33-51-00-715-001 REV 143 DATE 22-AUG-2024&NBSP;</P>)

Part: SKIN — CRACKED (RT ELEVATOR) · airframe 101,622 hrs · 21,021 cycles

RH OUTBOARD ELEVATOR, LEADING EDGE AREA, BETWEEN ELEV STA188.221 AND ELEV STA 261.665 WITH CRACK(<P>RH OUTBOARD ELEVATOR WAS EVALUATED AND REPAIRED IAW SRM 55-20- 02-2R-1 FIG. 201 AND SRM 51-70-04-0G-0 PAR. 5A. NO FURTHER DEFECTS NOTED</P>)

Part: HEATER — INOPERATIVE (ZONE 200) · airframe 101,622 hrs · 21,021 cycles

RIGHT SIDE WINDOW HEAT INOP FLIGHT DECK WINDOW HEAT SYSTEM, #2 SIDE WINDOWS(<P>RIGHT SIDE WINDOW HEAT INOP FLIGHT DECK WINDOW HEAT SYSTEM, #2 SIDE WINDOWS WAS REPLACED, ADJUSTED AND OPERATIONAL CHECK WAS PERFORMED IAW AMM 56-11-02-004-001 REV. 143 DATE: 22 AUG 24, AMM 30-41-00-715-001 REV 143 DATE: 22 AUG 24, AMM 56-11-02-715-145 REV. 143 DATE: 22 AUG 24 &AMP; AMM 56-11-02-404-026 REV. 143 DATE: 22 AUG 24. TORQUE APPLIED 40 LB IN AND 45 LB IN. S/N: 122912342 DATE: 16/JUL/25</P>)

Part: FITTING — CRACKED (ZONE 500) · airframe 101,622 hrs · 21,021 cycles

LH WING, INTERNAL FIXED LEADING EDGE, NEAR LES 281.82 WITH CRACK IN TORQUE TUBE GUIDE(<P>TORQUE TUBE GUIDE FITTING ASSY WAS REPLACED IAW SRM 51-10-02-0G-0, NO FURTHER DEFECTS NOTED</P>)

Part: FIRE SEAL — DEGRADED (THRUST REVERSER) · airframe 101,622 hrs · 21,021 cycles

ENGINE 2, LH THRUST REVERSER, IDG OIL SERVICE ACCESS DOOR, INNER AREA, DEGRADED FIRE SEAL.(<P>SEAL WAS REPAIRED IAW AMM 78-31-00-308-072-H00 REV 143 22-AUG-2024. NO FURTHER DEFECTS NOTED</P>)

Part: LINE — LEAKING (OXYGEN BOTTLE) · airframe 101,290 hrs · 20,880 cycles

CREW O2 PRESSURE 10PSI. FND 1ST OBS O2 BOX SUPPLY LINE LEAK. REPLACED LINE IAW AMM 35-00-00 &AMP; LEAK CHK OK. R/R CREW O2 BOTTLES IAW AMM 12-15-08 & LEAK CHECK GOOD. PART VERIFIED PER IPC 35-11-00 ITEM 1.

Part: CONNECTOR — FAULTED (AUTOTHROTTLE SYS) · airframe 100,840 hrs · 20,699 cycles

REJECTED TAKEOFF DUE TO NO AUTO THROTTLE AFT ENGAGING, EPR, AND V SPEEDS. DELETE TMC ANNC LIGHT(<P>REMOVED AND REPLACED CONNECTOR D4224P REF WDM 73-21-11. OPS CHECK GOOD AT THIS TIME.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 99,562 hrs · 20,246 cycles

FIRE EXTINGUISHER UNDER SIDE PANEL CANNOT BE PROPERLY SECURED. CLASP WILL NOT STAY LATCHED(<P>ADJUSTED FIRE EXTINGUISHER CLASP IAW AMM B676 AMM 51-40-02. OPS CHECKS GOOD AT THIS TIME. VERIFIED PROPERLY CLOSED IAW AMM 25-60-00</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 99,187 hrs · 20,128 cycles

RH VERTICAL STABILIZER EXTERIOR BTW FSS 220.521 TO FSS 270.784 WITH DELAMINATIONS.(<P>RH VERTICAL STABILIZER EXTERIOR BTW FSS 220.521 TO FSS 270.784 WAS REPAIRED IAW SRM 55-30-01-2R-1 REP 1 NOTE F FIG 201 PAGE 2 AND SRM 51-70-10-2R-4 REP 4 FIG 201 PAGE 1. REV 47 15 AUG 2023</P> / <P>&NBSP;</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 99,187 hrs · 20,128 cycles

LH VERTICAL STABILIZER EXTERIOR BTW FSS 220.521 TO FSS 270.784 WITH DELAMINATION.(<P>LH VERTICAL STABILIZER EXTERIOR BTW FSS 220.521 TO FSS 270.784 WAS REPAIRED IAW SRM 55-30-01-2R-1 REP 1 NOTE F FIG 201 PAGE 2 AND SRM 51-70-10-2R-4 REP 4 FIG 201 PAGE 1. REV 47 AUG 15/2023&NBSP;</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 99,187 hrs · 20,128 cycles

RH MAIN LANDING GEAR, AT AFT SIDE BRACE ON ATTACH WITH GOUGE.(<P>RH MAIN LANDING GEAR, AT AFT SIDE BRACE ON ATTACH GOUGE WAS REPAIRED IAW TRE6757208. APROV FAA FORM 8100-9, AUGUST 20, 2023</P> / <P>&NBSP;</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 99,187 hrs · 20,128 cycles

CENTER WING FRONT SPAR STA 785.9 AND LBL 97.95 FUEL LEAK(<P>CENTER WING FRONT SPAR STA 785.9 AND LBL 97.95 FUEL LEAK WAS REPAIRED AND THE TEST WAS SATISFACTORY PER AMM 28-11-00-308-013 REV 139 22APR-2023.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 99,187 hrs · 20,128 cycles

FAA AGING AIRCRAFT FINDINGS #1 T/R AFT FIRE BLANKET DAMAGED AFT SIDE(<P>ON #1 T/R AFT FIRE BLANKET AFT SIDE SEAL WAS APPLIED IAW AMM 78-31-00-308-072-H00 REV 139 22APR2023. NO FURTHER DEFECTS NOTED</P>)

Part: MODULE — UNKNOWN (UNKNOWN) · airframe 98,931 hrs · 20,028 cycles

AFTER V1, FIRE BELL HORN SOUNDED WITH NO EICAS MSG OR LIGHTS. UNABLE TO CANCEL THE HORN. RETURNED TO CVG. LANDING WIEGHT 308000.(<P>R/R MODULE ASSY-WARNING ELEC IAW B767 AMM 31-51-04. OPS CKKS GOOD AT THIS TIME. NO DEFEATS NOTED.</P>)

Part: FIRST AID KIT — OPEN · airframe 97,739 hrs

FIRST AID KIT SEAL BROKEN.(<P>REMOVED AND REPLACED FIRST AID KIT IAW B767 AMM 25-64-03.

Part: NONE — NONE · airframe 97,237 hrs · 19,466 cycles

ON WALK AROUND AFTER LANDING FOUND R/H MAIN LANDING GEAR SHOCK STRUT DOOR MISSING.(<P>PERFORMED DVI IAW AMM 05-51-59/201. TRANSFRRED TO CDL 168008, CDL 32-12-01, DUE 12 NOV 22 T &AMP; I BM 0040Z , PLACARDS INSTALLED</P>)

Part: HOSE — FRAYED · airframe 97,155 hrs · 19,436 cycles

COCKPIT CAPT OXYGEN MASK HOSE FRAYED. REMOVED & REPLACED CAPT O2 MASK PER B767-300 AMM 35-11-51. OPS CHECK GOOD NO LEAKS</P>)

Part: EVAS UNIT — LOOSE · airframe 97,155 hrs · 19,436 cycles

COCKPIT CAPT EVAS TOP COVER LOOSE READJUSTED CAPT EVAS COVER PER B767-300 AMM 25-60-99

Part: SEAL — DAMAGED · airframe 97,155 hrs · 19,436 cycles

R/W I/B AFT FLAP HAS DAMAGED SEAL AT O/B SIDE. REMOVED AND REPLACED DAMAGED SEAL AT RIGHT WING I/B AFT FLAP O/B SIDE AS PER 767-300 AMM 20-10-23-964-001</P>)

Part: DOOR TRACK — LACK OF LUBE · airframe 97,155 hrs · 19,436 cycles

FWD ENTRY DOOR (L1) TRACK REQUIRES CLEANING & LUBRICATION. CLEANED & LUBRICATED FWD ENTRY DOOR (L1) TRACKS PER; B767-300 AMM 12-21-108. OPS CHECK GOOD</P>)

Part: FASTENER — MISSING · airframe 97,155 hrs · 19,436 cycles

# 2 ENGINE INLET CASE CHAFING STRIP MISSING PLASTIC FASTENERS AT 5 AND 9 O'CLOCK POSITIONS. INSTALLED MISSING PLASTIC FASTENERS AT ENGINE INLET CASE CHAFING STRIP AS PER 767-300 SRM 51-40-02-0G-0

Part: RUB STRIP — WORN · airframe 97,155 hrs · 19,436 cycles

#1 ENGINE EXHAUST DUCT RUB PADS (ALL) LOOSE/WORN. REMOVED AND REPLACED WORN WEAR PADS AND SECURED LOOSE PADS AS PER 767-300 SRM 51-40-02-0G-0</P>)

Part: BONDING JUMPER — BROKEN · airframe 97,155 hrs · 19,436 cycles

#2 ENG R/H SIDE HAS 1EA BROKEN BONDING WIRE ( LOCATED ABOVE FUEL FILTER ) REMOVED & REPLACED #2 ENG R/H SIDE BONDING JUMPER TO THE HPSOV IAW B767 AMM 36-11-07</P>)

Part: BOLT — BROKEN · airframe 97,155 hrs · 19,436 cycles

BOLT IS BROKEN FOR CLAMP LOCATED ON #2 ENG R/H SIDE AFT OF HEAT EXCHANGER. INSTALLED BOLT AS PER B767-300 AMM 70-50-00. OPS CHECK GOOD</P>)

Part: FASTENER — MISSING · airframe 97,155 hrs · 19,436 cycles

#2 ENG AFT STRUT FAIRING MISSING 2EA FASTENERS ON R/H SIDE INSTALLED MISSING FASTENERS AT #2 ENGINE AFT STRUT FAIRING ON RH SIDE AS PER 767-300 SRM 51-40-02-0G-0</P>)

Part: NONE — NONE · 19,237 cycles

CRACK ON FWD UPPER CHORD AT STA 1809.5 BULKHEAD, STRINGER S-7LH.(<P ><SPAN>REPAIR WAS INSTALLED ON FWD UPPER CHORD AT STA 1809.5 AND STRINGERS S-6LH TO S-8LH PER 767 SRM 53-80-08 REPAIR 9</SPAN></P> / <P>&NBSP;</P>)

Part: SPLICE — NONE · corrosion level 2 · airframe 96,555 hrs

CORROSION ON SPLICE TEE P/N 145T8629-2 OF KEEL BEAM FAIRING PANEL AT STA 887 APPROXIMATELY(<P ><SPAN>AFFECTED SPLICE TEE P/N 145T8629-2 WAS REPLACED PER 767 SRM 51-10-02-0G-0 PAR. 9 &AMP; 767 IPC 53-52-54-01 ITEM 25</SPAN></P> / <P>&NBSP;</P>)

Part: NONE — NONE · corrosion level 2 · airframe 96,555 hrs

CORROSION ON THE UPPER SURFACE OF U-17 STRINGER OF RH WING SKIN PANEL 1 &AMP; 2 AND RIB 1 AND RIB 3(<P STYLE="MARGIN: 0IN; MARGIN-BOTTOM: .0001PT;"><SPAN>AFFECTED U-17 STRINGER SEGMENT WAS TRIMMED TO REMOVE ALL CORROSION.</SPAN></P> / <P STYLE="MARGIN: 0IN 0IN 0.0001PT;"><SPAN>NEW U-17 STRINGER SEGMENT WAS MANUFACTURED / INSTALLED AND SPLICE REPAIR STRAPS WERE INSTALLED PER BOEING SR 3-5250629088 AND SRM 57-00-03 REPAIR 2.</SPAN></P> / <P>&NBSP;</P> / <P>&NBSP;</P>)

Part: NONE — NONE · airframe 96,555 hrs

CUT OUT ON UPPER CHORD, RIB #2 BETWEEN U-16 STRINGER TO U-18 STRINGER. THIS WAS REQUIRED TO GET ACCESS DURING U-17 STRINGER REMOVAL(<P ><SPAN>UPPER CHORD, RIB #2 BETWEEN U-16 STRINGER TO U-18 STRINGER WAS REPAIRED PER 767 SRM 57-20-09 REPAIR 1</SPAN></P> / <P>&NBSP;</P>)

Part: NONE — NONE · airframe 96,555 hrs · 19,237 cycles

CRACK ON LH STRUT OUTBD SKIN PANEL P/N 311T2450-23 BETWEEN NAC STA 221.25 / NAC STA 237.5 (CUTOUT FOR ACCESS PANEL 432AL)(<P ><SPAN>LH STRUT OUTBD SKIN PANEL P/N 311T2450-23 WAS REPAIRED PER BOEING SR 4-5340563504</SPAN></P> / <P>&NBSP;</P>)

Part: NONE — NONE · airframe 96,256 hrs · 19,138 cycles

NO APU DUCT PRESS.(<P><SPAN>APU SHUTDOWN AND PERFORMED OPERATIONAL CYCLE CHECK IAW AMM 49-00-00 AND DUCT PRESSURE RESTORED.</SPAN></P>)

Part: NONE — NONE

HI FLOW INHIBIT STATUS MSG(<P><SPAN>PERFORMED T/S PER FIM21-51 F/T 854 , SYSTEM OPS CHECK NORMAL, MESSAGE CLEARED.</SPAN></P>)

Part: NONE — NONE · airframe 96,154 hrs · 19,102 cycles

RIGHT FWD FUEL PUMP EICAS ON DESCENT.(<P>PERF FIM 28-22 FT 819 AND RESET K10704 GFI RELAY, OPS CHECK NORMAL PER AMM 28-22-00, WIRING CHECK OK PER WDM 28-22-11.</P>)

Part: NONE — NONE · airframe 96,107 hrs · 19,090 cycles

DURING BEFORE START FLOW EICAS MESSAGE L AFT FUEL PUMP DISPLAYED EVEN WITH L AFT FUEL PUMP SWITCH ON, NOTICED L AFT FUEL BOOST PUMP CB POPPED(<P>CYCLED CB IAW AMM 20-60-01. OPS CHECK GOOD IAW AMM 28-21-00. NO FURTHER DEFECTS NOTED.</P>)

Part: MASK — NONE · 19,084 cycles

F/O O2 MASK HARD TP BREATHE.(<P>REMOVED AND REPLACED O2 MASK IAW AMM 35-11-51 OPS CHECK GOOD.</P>)

Part: NONE — NONE

L AFT FUEL PUMP "PRESS" LIGHT NOT ILLUMINATED WITH SWITCH OFF.(<P>TURNED APU POWER OFF AND PERFORMED FUEL BOOST PUMP PRESSURE SWITCH TEST IAW AMM 28-42-01. NO DEFECT NOTED, PRESS LIGHT &AMP; ASSOCIATED EICAS MSG'S APPEAR AS REQ'. OK FOR SERVICE.</P>)

Part: OXYGEN SYSTEM — MALFUNCTIONED (CREW)

CREW O2 INDICATION INOP.(<P>TRANSFERRED TO MDDR 153132 IAW MEL 35-11-02-01, CAT B.</P> / <P>REMOVED AND REPLACED AVERAGING UNIT IAW AMM 35-11-06. THIS CLEARS MDDR 153132.</P>)

Part: BLADE — NICKED (NR 1 ENG FAN)

DURING #1 ENGINE FAN BLADE INSPECTION FOUND NICK ON LEADING EDGE TIP OF #36 FAN BLADE(<P>REPAIRED LEFT ENGINE #36 FAN BLADE TIP DAMAGE IAW AMM 72-31-02. FLUORESENT PENETRANT TEST REQUIRED BEFORE RETURN TO SERVICE. COMPLETED FPI INPSECT NBR 1 ENG FAN BLADE NBR 36 PER AMM 71-11-06-232-001-H00. NO ITEMS FOUND.</P>)

Part: CONTROL PANEL — FAILED (TCAS SYSTEM)

TCAS/ ATC CONTROL PANEL FAILED, RELEASED SMOKE FROM DISPLAY. REF L/P 1390638/ M8 SMOKE OR FUMES IN THE CABIN, INSP. REQUIRED.(<P>REMOVED AND REPLACED TCAS/ATC CONTROL PANEL. OPS CHECK PASS. NO FAULTS AT THIS TIME IAW B767-300 AMM 34-53-02.</P> / <P>LP 1390638/M8: PERFORMED SMOKE/ FUMES IN CABIN INSP. PER AMM 05-51-56-206-001. NO DEFECTS NOTED OTHER THAN ATC CONTROL PANEL.</P>)

Part: DISPLAY — FAILED (EADI)

CAPTAINS ADI DISPLAY FLICKERED ON OFF. SMELL OF ELECTRIC BURNING. ALSO HEARD RELAY CLICKING NOISE. TURNED BRIGHTNESS DOWN, NO FURTHER PROBLEMS. PERFORMED SMOKE OR FUMES IN CABIN INSP. IAW AMM 05-51-56. NO SIGNS OF SMOKE OR OIL CONTAMINATION NOTED OPS NORMAL. REMOVED AND REPLACED CAPT'S EADI PER AMM 34-22-03 NO SIGNS OF ELECTRICAL ARCING OR BURNING SMELL NOTED.</P>)

Part: CIRCUIT BREAKER — TRIPPED (WX RADAR) · airframe 95,284 hrs · 18,828 cycles

PRIOR TO TAKE OFF WXRDR F23 AND F21 CIRCUIT BRAKERS POPPED. THUNDERSTORMS IN VICINITY AT DEPARTURE AIRPORT.(<P>PERFORMED OPS CK WXR RADAR PER AMM 34-43-00. OPS CHECK GOOD @ THIS TIME. NO DEFECTS NOTED.</P>)

Part: BATTERY — FAULTED (EMERGENCY LIGHTS) · airframe 95,172 hrs

EMERGENCY LIGHTS ILLUMINATE AND CYCLE IN FLIGHT(<P>REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AND CHARGER IAW B767 AMM 33-51-07. OPS CHECK GOOD AT THIS TIME.</P>)

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 95,150 hrs · 18,791 cycles

EXIT OVERHEAD &AMP; ENTRY LIGHTS BLINK INTERMITTENTLY AT LOWER ALTITUDES.(<P>ON CHECK FOUND EMERGENCY CEILING LIGHT BULB INOP. REMOVED AND REPLACED CELING EMERGENCY LIGHT BULB PER B767-300 AMM 33-51-11. OPS CHECK EMERGENCY LIGHTS PER B767-300 TASK 33-51-00-715-227. OPS CHECK GOOD.</P>)

Part: OXYGEN MASK — NO TEST (COCKPIT) · airframe 95,125 hrs

CAPTAIN 02 MASK HARNESS DOES NOT INFLATE DURING TEST(<P>REMOVED AND REPLACED CAPTAIN 02 MASK IAW AMM 35-11-51. OPS CHECK GOOD.</P>)

Part: WARNING MESSAGE — FALSE INDICATION · airframe 95,118 hrs · 18,781 cycles

EICAS MSG "FWD EQPT VAL" PRIOR TO BLOCK OUT(<P>EQUIP COOL AUTO MODE DEFERRED IAW MEL 21-51-01-01, MDDR # 148275, CAT C, EXP 19 JUN 21.</P><P>LOG PAGE 1453746: PERFORMED SYSTEM OPERATIONAL CHECK IAW 21-58-00, NO DEFECTS NOTED. THIS CLEARS MDDR 148275.<BR /></P>)

Part: CIRCUIT CARD — FAULTED (LT ENGINE) · airframe 95,066 hrs · 18,764 cycles

L ENG ANALOG N2 STATUS MESSAGE 2+10 IN FLIGHT(<P>PERFORMED FIM 73-21 FT901 RESISTANCE CHECK GOOD B/W PINS 3&AMP;4 ON N2 SPEED SENSOR.PERFORMED ENG RUN IAW AMM 71-00-00 MSG REMAINED.REMOVED AND REPLACED L ENG N2 SPEED CARD IAW WDM 77-12-12.AFTER MULTIPLE ENG RUNS STATUS MSG REAPPEARED ONLY WHEN L EICAS COMPUTER WAS SELECTED. REMOVED AND REPLACED L EICAS COMPLUTER IAW AMM 31-41-02.PERFORMED EICAS SOFTWARE LOAD IAW AMM 32-41-02, OPS CHECK GOOD. PERFORMED ENG RUN IAW AMM 71-00-00, OPS CHECK GOOD, NO STATUS MSG FOR L ENGINE ANALOG N2.<BR /></P>)

Part: CIRCUIT CARD — FAULTED (RT ENGINE) · airframe 95,066 hrs · 18,764 cycles

R ENG ANALOG N2 STATUS MESSAGE 0+30 IN FLIGHT(<P>PREFORMED FIM 73-21 FT 901 RESISTANCE BETWEEN PIN 3 AND 4 ON N2 SPEED SENSOR RESISTANCE CHECK GOOD, PERFORMED ENGINE RUN IAW AMM 71-00-00 STATUS MESSAGE REMAINED. REMOVED AD REPLACED RIGHT ENGINE N2 ENGINE SPEED CARD IAW WDM 77-12-12. PERFORMED ENGINE RUN. OPS CHECK GOOD "R ENG ANALOG N2" STATUS MESSAGE CLEARED.<BR /></P>)

Part: INDICATOR — LEAKING (NR 1 NACELLE) · airframe 94,728 hrs · 18,664 cycles

#1 PYLON DIFFERENTIAL PRESSURE INDICATOR LEAKING(<P>REMOVED AND REPLACED #1 PYLON DIFF PRESS IND PER AMM -29-11-17. NO LEAKS NOTED.</P>)

Part: UNKNOWN — LEAKING (THRUST REVERSER) · airframe 94,728 hrs · 18,664 cycles

#2 ENG THRUST REV OPEN/CLOSE ACTUATOR HAS EVIDENCE OF HYD LEAK(<P>CLEANED #2 ENG T/R ACTUATOR ON BOTH SIDES PENDING OPS CHECK. PERFORMED OPS CHECK PER AMM 78-31-00, NO LEAKS NOTED.&NBSP;<BR /></P>)

Part: DEPRESSOR — DENTED (DOOR SEAL) · airframe 94,728 hrs · 18,664 cycles

DENT FOUND ON FWD M/C DOOR DEPRESSOR SEAL AT STA 492 BTW S4L AND S13L DENT FOUND TO BE WITHIN LIMITS PER REF SRM 53-00-15-1A DETAIL 12(<P>REMOVED DAMAGED SEAL DEPRESSOR, LOCATED DRILLED AND INSTALLED NEW SEAL DEPRESSOR AT MAIN CARGO DOOR CUT OUT FWD SIDE PER B767-300 AMM 20-11-00-910-802.<BR /></P>)

Part: FASTENER — WORN (NR 1 NACELLE) · airframe 94,728 hrs · 18,664 cycles

#1 ENG PYLON HAS HYD RESERVOIR ACCESS PANELS WITH SMOKING RIVETS AT CLOSING LATCH POSITIONS ON I/B AND O/B SIDES (SAIL BOATS)(<DIV>REPLACED LOSSE FASTENERS AT #1 ENG PYLON BY ACCESS PANELS I/B AND O/B SIDE OF SAILBOATS PER B767-300 SRM 51-40-02-06-0.</DIV>)

Part: FILTER — NOT REPORTED (APU FUEL) · airframe 94,728 hrs · 18,664 cycles

PER MDDR 145973 REPLACE APU FUEL FILTER.(<P>REMOVED AND REPLACED APU FUEL FILTER ELEMENT IAW AMM 49-31-04, PENDING LEAK CHECK.&NBSP;</P><P>PERFORMED APU OPS. CHECK IAW AMM 49-11-00. NO LEAKS FOUND.</P>)

Part: SOLENOID — DAMAGED (HYD PUMP) · airframe 94,728 hrs · 18,664 cycles

#1 ENG HYD PUMP DEPRESSURIZATION SOLENOID IS DAMAGED(<P>REMOVED AND REPLACED #1 ENGINE HYD. PUMP DEPRESSURIZATION VALVE IAW AMM 29-11-05, PENDING LEAK AND OPS CHECK.&NBSP;</P><P>PERFORMED OPS CHECK AND LEAK CHECK PER AMM 71-00-00 AND AMM 29-11-05. OPS CHECK GOOD AND NO LEAKS.</P>)

Part: DEPRESSOR — DAMAGED (CARGO DOOR) · airframe 94,728 hrs · 18,664 cycles

MAIN CARGO DOOR AFT SEAL DEPRESSOR DAMAGED.(<P>REMOVED DAMAGED SEAL DEPRESSOR. LOCATED, DRILLED, DEBURRED, INSTALLED AND PAINTED NEW SEAL DEPRESSOR AT MAIN DECK CARGO DOOR CUT OUT AFT SIDE PER B767-300 AMM 20-11-0-910-802.<BR /></P>)

Part: SAFETY WIRE — MISSING (ECU MOUNT BOLT) · airframe 94,728 hrs · 18,664 cycles

#1 ENG (ECU) MOUNT BOLTS ARE NOT SAFETIED.(<P>VERIFIED #1 ENGINE ECU BOLTS TO FAN CASE TORQUE CHECK IAW AMM 73-21-15 AND SAFETIED BOLTS WITH LOCKWIRE IAW AMM 20-10-23.<BR /></P>)

Part: FASTENER — WORN (NR 2 NACELLE) · airframe 94,728 hrs · 18,664 cycles

#2 ENG I/B NACELLE STRUT ACCESS PANELS FOR HYD RESERVOIR (SAILBOATS) HAVE SMOKING RIVETS AT LATCH POSITIONS ON I/B SIDE.(<DIV>REMOVED AND REPLACED LOOSE FASTENERS AT #2 ENG I/B NACELLE STRUT ACCESS PANEL PER B767-300 SRM 51-40-02-06-0.</DIV>)

Part: BATTERY — NOT REPORTED (C/P FLASHLIGHT) · airframe 94,728 hrs · 18,664 cycles

COCKPIT FLASHLIGHT BATTERIES NEED TO BE REPLACED 2 EACH P/N P4-01-0021(<P>REMOVED AND REPLACED COCKPIT FLASHLIGHT BATTERIES 2 EA AS REQUIRED PER AMM 25-64-00. CK'D OK.<BR /></P>)

Part: WIRE — CHAFED (NR 1 FIRE LOOP) · airframe 94,728 hrs · 18,664 cycles

ENG 1 LOWER FIRE LOOP ELECTRICAL WIRE WITH CHAFFING LOCATED AT 6 O'CLOCK POSITION .(<P>REPAIRED ENG #1 FIRE LOOP WIRING INSULATION PER SWPM 20-10-13: ENG 1 FIRE DETECTION SYS TEST OK IAW AMM 26-11-00 REV132<BR /></P>)

Part: SEAL — DAMAGED (ELT) · airframe 94,728 hrs · 18,664 cycles

COCKPIT ELT AUTO RELEASE SEAL DAMAGE. PIN 1151324-1 S/N 1151324-07195(<DIV>REMOVED AND REPLACED COCKPIT ELT AS REQUIRED PER AMM 25-64-00 CK'D OK HEX CODE ADCC4060EC00161.</DIV>)

Part: WINDOW — LOOSE (LIFE RAFT BOX) · airframe 94,728 hrs · 18,664 cycles

COCKPIT LIFE RAFT COMPARTMENT VIEWING WINDOW LOOSE(<P>CLEANED AND RE-GLUE LOOSE WINDOW VIEWING AT COCKPIT LIFE RAFT COMPT PER B767-300 AMM 20-30-01-992-001.

Part: SENSOR — NO TEST (FUEL QTY) · airframe 94,728 hrs · 18,664 cycles

FUEL QUANTITY INDICATING SYSTEM "DRY CAPACITANCE TEST FOR THE RIGHT SURGE TANK FUEL LEVEL SENSOR FAIL TEST AT 4.8 PICOFARADS". NOTE: SENSOR TS196(<P>T/S F/M 28-21-F/T806; REMOVED &AMP; REPLACED TS196 RH SURGE TANK FUEL LEVEL SENSOR PER AMM 28-21-03. REV 132.

Part: SENSOR — NO TEST (SURGE TANK) · airframe 94,728 hrs · 18,664 cycles

FUEL TANK OPENING REQUIRED DUE TO THE RIGHT SURGE TANK FUEL LEVEL SENSOR FAIL TEST. NOTE: PANEL TO BE OPEN 642AB(<P>R/H SURGE TANK PLATE 642AB REMOVED FOR TANK ACCESS. REF M/M 28-11-03-004-001. APU BATTERY AND MAIN BATTERIES DISCONNECTED. OK TO REINSTALL R/H SURGE TANK PLATE. REINSTALLED R/H SURGE TANK PLATE 642AB PER AMM 28-11-03. NO LEAKS. RECONNECTED APU BATTERY PER AMM 24-31-04, OPS CHECK GOOD. RECONNECTED MAIN BATTERY PER AMM 24-31-01, OPS CHECK GOOD.&NBSP;<BR /></P>)

Part: SEAL — BROKEN (CONTAINMENT BAG) · airframe 94,728 hrs · 18,664 cycles

COCKPIT AVSAX CONTAINMENT BAG VACUUM SEAL IS BROKEN P/N AS-002-1(<P>REMOVED AND REPLACED COCKPIT AVSAX REF EO 6725A212<BR /></P>)

Part: FASTENER — WORN (NR 1 INLET) · airframe 94,728 hrs · 18,664 cycles

#1 ENG INLET CASE O/B ANTI - ICE PANELS HAS (2 EA) HOLES THAT FASTENERS HAS WORN THRU. REQUIRES DIMPLE WASHER ON FASTENERS.(<P>REMOVED AND REPLACED WORN FASTENERS AT #1 ENG BY INLET CASE O/B ANTI-ICE ACCESS PANEL PER B767-300 AMM 20-11-00-910-802.<BR /></P>)

Part: FILTER — FAILED (FUEL SYSTEM) · airframe 94,728 hrs · 18,664 cycles

"L ENG FUEL FILTER" EICAS MESSAGE, QRH COMPLETE, ENGINE INDICATIONS NORMAL(<P>PERF FUEL FILTER ELEMENT INSPECTION, FOUND PARTICULATE &LT; 0.25MM IN SIZE BOTH L AND R FUEL FILTERS. REPLACED BOTH FUEL FILTERS AMM TASK 73-11-02-216-001-H00. LEAK CHECKS GOOD. TRANSFERRED TO MDDR&NBSP;145973. REMOVED AND REPLACED #1 AND #2 ENGINE FILTERS AND PERFORMED MICROBIOLOGICAL GROWTH TEST WITH NO DEFECTS NOTED IAW AMM 28-10-00 AND AMM 73-11-02. MDDR CLEARED.&NBSP;</P>)

Part: OXYGEN MASK — INOPERATIVE · airframe 94,692 hrs · 18,654 cycles

#1 SUPERNUMERARY OXY MASK INOP ( SUPERNUMERARY SEAT / (ALL CARGO CONFIG) )(<P>ITEM TRANSFERED TO MDDR# 145648 PER MEL 25-25-03, CAT D, DUE DATE 19-AUG-21. SP@0116Z.</P><P>21APR21 - LP1188600 - M4 -ONT - PERFORMED OPS CHECK OF # 1 SUPERNUMERARY O2 MASK IAW AMM 35-11-00, OPS CHECK GOOD, NO DEFECTS NOTED, THIS CLEARS MDDR # 145648, PLACARD REMOVED</P><P>DISPATCH : JJT0857Z</P>)

Part: PRESSURE SWITCH — FAULTED (RT ENGINE) · airframe 94,225 hrs · 18,508 cycles

RIGHT ENG PRV STATUS MSG.(T/S IAW FIM 36-10 FAULT TREE 847. SUSPECT PRESSURE SWITCH TO BE AT FAULT. REMOVED AND REPLACED PRV PRESSURE SWITCH IAW AMM 36-21-03. REF LOG PAGE 1253834 ITEM NR 8 FOR OPS CK 14FEB21 LOG PG 1253834 ITM 8 CVG: PERFORMED LEAK CHECK OF RT ENG BLEED OVER PRESS SWITCH. NO LEAKS NOTED IAW AMM 36-21-03. PERFORMED PRECAUTIONARY ENGINE RUN OF LT AND RT ENGINES IAW AMM 71-00-00. NO DEFECTS NOTED.)

Part: VALVE — MALFUNCTIONED (APU AIR) · airframe 94,206 hrs · 18,499 cycles

APU WILL NOT DELIVER PNEUMATIC AIR VALVE APU VALVE CYCLED TWICE.(<P>PERFORMED OPS TEST OF PNEUMATIC SYSTEM, NO DEFECTS NOTED IAW AMM 36-00-00. SYSTEM OPS CHECK NORMAL.</P>)

Part: INDICATOR — FALSE INDICATION · airframe 94,183 hrs · 18,491 cycles

NO MANIFOLD DUCT PRESSURE WITH APU OPERATING &AMP; APU BLEED VALVE INDICATING.(<P>CYCLED BLEED SWITCH PER AMM 36-11-00. OPS CHK GOOD.<BR /></P>)

Part: RADAR — MALFUNCTIONED (WX SYSTEM) · airframe 94,172 hrs · 18,486 cycles

NO CONVECTIVE ACTIVITY AT&NBSP; FL320, GROUND RETURNS ON RADAR APPEAR WITH TILT SELECTED AT 0 DEGREES AND RANGE SELECTED TO 160 MILES, GAIN SELECTED TO AUTO AND WX OR WX/TURB SELECTED.(<P>PERFORMED SYSTEM TEST OF WXR IAW AMM 34-43-00-715-026. OPS CHECK GOD. NO FAULTS FOUND.&NBSP;</P>)

Part: ISOLATOR — WORN (APU) · airframe 94,088 hrs · 18,456 cycles

LEFT AFT APU VIBRATION ISOLATOR WORN TO LIMITS. REMOVED AND REPLACED LEFT AFT VIBRATION ISOLATOR, IAW AMM 49-13-01. OPERATIONS CHECK GOOD AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 94,044 hrs · 18,439 cycles

CABIN ALT AUTO 2 STATUS MESSAGE ILLUMINATED. PERFORMED BITE TEST ON NR 2 CABIN PRESSURE CONTROLLER. NO DEFECTS OR FAULTS NOTED. MESSAGE CLEARED, IAW AMM 21-31-00.

Part: FITTING — LEAKING (APU OIL SYSTEM) · airframe 94,033 hrs · 18,434 cycles

APU INOP(<P>FOUND BROKEN THREADED FITTING TO APU BEARING. OIL LEAKING. TRANSFERRED TO MDDR # 140687 IAW&NBSP; MEL 49-11-01A, CAT C, DUE 19 JAN 21. PLACARDS INSTALLED.</P><P>19JAN, CVG, LP 1239488, ITEM M5: REMOVED AND REPLACED APU IAW AMM 49-11-01. OPS CHECK OF APU GOOD AT THIS TIME. THIS CLEARS DMI # 140687. MCC NOTIFIED, PLACARDS REMOVED.

Part: RADAR — MALFUNCTIONED (LT WEATHER) · airframe 93,996 hrs · 18,423 cycles

LEFT WXR SYSTEM, WXR FAIL. PERFORMED GROUND TEST OF BOTH WEATHER RADAR SYSTEMS, REF AMM 34-43-00-715-001-001. BOTH OPERATIONS CHECK NORMAL.

Part: UNKNOWN — UNKNOWN (START VALVE) · airframe 93,903 hrs · 18,391 cycles

NUMBER 1 ENGINE START VALVE LIGHT FAILED TO ILLUMINATE, ENGINE START VALVE LIGHTS, -200/-300. TRANSFERRED TO MDDR 139877, IAW MEL 80-00-01-01, CAT C. PERFORMED ENGINE START 2X, START VALVE LIGHT ILLUMINATES & EXTINGUISHES AT START AND AT 50% N2 EACH ATTEMPT. OPERATES OK AT THIS TIME. THIS CLEARS MDDR 139877. MCC NOTIFIED. PLACARD REMOVED IAW AMM 71-00-00.

Part: WARNING LIGHT — FALSE ACTIVATION (APU) · airframe 93,893 hrs · 18,388 cycles

ITEM 3-APU FAULT ON LANDING/TAXI IN. RE-START OK. PERFORMED BITE CHECK OF THE APU ECU, IAW 49-61-05, NO FAULTS FOUND. OK FOR SERVICE.

Part: PANEL — OPEN · airframe 93,895 hrs · 18,389 cycles

ON POST FLIGHT INSPECTION, PANEL WAS FOUND OPEN. PERFORMED PNEUMATIC LEAK TEST, IAW BOEING 767 AMM 71-00-00. NO LEAK DETECTED. CLOSED PANEL, IAW BOEING 767 AMM 78-31-14.

Part: FAULT MESSAGE — FALSE ACTIVATION (APU) · airframe 93,761 hrs · 18,344 cycles

APU FAULT AFTER LANDING. REPEAT WRITE UP. PERFORMED BITE TEST OF APU ECU 49-11 FT 987, NO FAULTS NOTED. APU START TEST 49-11-00-201 NORMAL AT THIS TIME.

Part: INDICATION SYS — FAILED (FUEL QTY) · airframe 93,728 hrs · 18,328 cycles

ITEM 1-FUEL CONFIG EICAS. TOTALIZER VS. CALCULATED=3.1 THOUSAND POUNDS. TOTALIZER 3.1 THOUSAND LESS THAN CALCULATED INDICATION=SUSPECTED FUEL LEAK. PERFORMED BITE TEST ON FQIS, FOUND LM DENS CONTAM OR RESISTOR G AND LM COMPENSATOR CONTAMINATED G. STUCK LM AND RM TANK AND FOUND FUEL TOTAL QTY TO BE WITHIN 500 LBS OF INDICATOR AT THIS TIME. SUS FAULTY DENSIOMETER OR COMPENSATOR CONTINUED ON LP 1241030 AND 1241031. LP 1241030/ITEM M6/RIV-LT MAIN FUEL QTY INOPERABLE. TRANSFERRED TO MDDR 138163, CAT C DUE 30N0V20, IAW MEL 28-41-01-01. ETOPS RESTRICTED. TOTAL FUEL QUANITY INOPERABLE. TRANSFERRED TO MDDR 138164 CAT C DUE 30N0V20, IAW MEL 28-41-07A.

Part: FIRE DETECTOR — MALFUNCTIONED (RT ENGINE) · airframe 93,727 hrs · 18,327 cycles

ITEM 02-RT ENGINE FIRE LP 2 STATUS MESSAGE. R & R UPPER AFT ENGINE FIREWALL DETECTOR LOOP 2, IAW AMM 26-11-02. FAULT NO LONGER IN VIEW. PERFORMED ENGINE RUN RIGHT ENGINE, IAW AMM 72-00-00, NO DEFECTS NOTED.

Part: O-RING — LEAKING (FUEL FILTER) · airframe 93,705 hrs · 18,322 cycles

DUE TO SUSPECTED FUEL LEAK PERFORMED GVI OF WINGS AND LT & RT ENGINE. FOUND LEAK ON RT ENGINE FUEL FILTER DP SWITCH. REMOVED AND REPLACED FUEL FILTER DP SWITCH O-RING, IAW 73-34-01. PERFORMED DRY MOTOR, IAW AMM 71-00-00, NO LEAKS NOTED. OPERATIONS CHECK NORMAL AT THIS TIME.

Part: NONE — NONE (APU) · airframe 93,643 hrs · 18,305 cycles

INFO ONLY: RT ENGINE NO START FIRST ATTEMPT ON SINGLE IGNITOR. START OK ON BOTH. PERFORMED RT ENGINE IGNITION SYSTEM AUDIBLE TEST, IAW AMM 74-00-00. OPERATIONS CHECK GOOD, IGNITORS OPERATE NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (APU) · airframe 93,611 hrs · 18,297 cycles

"APU FAULT" EICAS UPON ATTEMPTING APU START ON GROUND. PERFORMED ECU BITE, IAW B767 FIM 49-11 FT 987. NO FAULTS THEN PERFORMED APU START, IAW B767 AMM 49-11-00, NO FAULTS. APU OPERATIONS NORMAL, APU STARTED FIRST ATTEMPT.

Part: APU — SPARKS · airframe 93,595 hrs · 18,291 cycles

DURING GROUND OPERATIONS MAINTENANCE WITNESSED SPARKS COMING OUT OF APU TAIL PIPE. MAINTENANCE SHUT DOWN APU AND PLACED ON DEFERRAL 49-11-01, MDDR 137202, CAT C. RAN APU IAW BITE TEST, PER FIM 49-11 FT 987, NO FAULTS NOTED. RAN BOTH PACKS, PER AMM 21-00-00. PERFORMED DRY MOTOR, IAW 71-00-00, NO FAULTS NOTED. INSPECTED APU, PER AMM 49-05-03, NO FAULTS NOTED. THIS CLEARS MDDR 137202. PLACARD REMOVED, MCC NOTIFIED ID 2314Z.

Part: ECU — MALFUNCTIONED (RT ENGINE) · airframe 93,533 hrs · 18,269 cycles

RT ENGINE CONTROL EICAS MESSAGE AFTER ENGINE START. REMOVED AND REPLACED ECU. OPERATIONS CHECKS NORMAL, IAW AMM 73-21-15. PERFORMED ENGINE RUN-UP, OPERATIONS CHECKS NORMAL. NO FAULTS NOTED, IAW AMM 71-00-00.

Part: BLEED VALVE — UNKNOWN (APU) · airframe 93,499 hrs · 18,252 cycles

DUCT PRESSURE 2500 PSI WITH APU ON AND APU BLEED VALVE OPEN. PERFORMED OPERATIONS CHECK OF PNEUMATIC SYSTEM, IAW AMM 36-00-00. OPERATIONS CHECKS GOOD, SYSTEM IS OK.

Part: GASKET — LEAKING (NR 2 ENGINE) · airframe 93,484 hrs · 18,246 cycles

NR 2 ENGINE SHOWS SIGN OF OIL LEAK. REMOVED AND REPLACED FUEL TO/OIL HEAT EXCHANGE TUBE GASKET, IAW B767 AMM 79-21-01.

Part: TRANSFORMER — SHORTED · airframe 93,428 hrs · 18,226 cycles

REPEAT WRITE-UP: DESCENDING THROUGH FL 180 AFTER TURNING WING AND LOGO LIGHTS ON, "RT AC BUS OFF" EICAS MESSAGE. RAN QRH, RT AC BUS RESTORED. ON FINAL APPROACH TURNED WING AND LOGO LIGHTS ON AGAIN ANOTHER RT AC BUS FAILURE. FOUND NUMEROUS WIRES CHAFED AT RT INBOARD, OUTBOARD, AND LT OUTBOARD LOGO LIGHT. REPAIRED WIRING, IAW SWPM CHP 20-10-13, FOUND RT INBOARD LOGO LIGHT TRANSFORMER SHORTED TO CASE GRND. REMOVED AND REPLACED RT INBOARD LOGO LIGHT, IAW AMM 33-45-00. PERFORMED OPS TEST, IAW AMM 33-45-00. PUT A/C IN AIR MODE, ISOLATED RT BUS, TURNED ALL LIGHT ON INCLUDING LOGO LIGHTS. NO BUS DEFECTS NOTED.

Part: BUSS — MALFUNCTIONED · airframe 93,428 hrs · 18,226 cycles

PASSING 18,000 AND AFTER SELECTING LANDING LIGHTS RECEIVED "RT AC BUS "OFF" EICAS. AFTER QRH, WE COULD NOT RESTORE RT AC BUS AND ACCEPTED LANDING CLEARANCE DUE TO LAND AT NEAREST SUITABLE AIRCRAFT CONFIGURED WITHOUT PROBLEM AND LANDING ROLLOUT AND TAXI UNEVENTFUL. RAN ENGINES TO TRY TO DUPLICATE THIS ISSUE. DURING ENGINE RUN, NO FAULTS WERE FOUND. PER FAULT TREE 24-20-801, WE DID A BITE TEST ON THE BPCU, NO FAULTS WERE FOUND. A/C SYSTEM IS OPERATING NORMALLY.

Part: APU — MALFUNCTIONED · airframe 93,417 hrs · 18,223 cycles

DURING TAXI-IN APU FAULT EICAS MESSAGE DURING APU START, SECOND START ATTEMPT WAS NORMAL START. OPERATIONS TESTED APU, REF 49-11-00, NO FAULTS NOTED AT THIS TIME. OK FOR CONTINUED SERVICE.

Part: BUSS — FAILED (RIGHT) · airframe 93,417 hrs · 18,223 cycles

RIGHT BUS FAILED, RESET VIA QRH, FAILED A SECOND TIME. PER CREW WHILE DESCENDING FROM 180 WHEN TURNING ON THE LANDING LIGHTS THE RT BUS FAILED. WHEN MX WENT TO DEBREIF THE CREW FOUND BOTH LT & RT BUSES OFF AND AC WAS ON STANDBY POWER, PER FIM 24-41 FT 805. RESET BOTH BUSES AND BITE THE BPCU, PER 24-20 FT 801, NO FAULTS NOTED. RAN BOTH ENGINES TO DO AN IDG LOAD TEST, PER AMM 71-00-00 AND AMM 24-11-00, NO FAULTS NOTED.

Part: FAULT MESSAGE — MALFUNCTIONED (APU) · airframe 93,391 hrs · 18,213 cycles

APU FAULT MSG. TRANSFERED TO MDDR 134960, CAT C, DUE 05AUG20 PER MEL 49-11-01A. RAN APU, PER AMM 49-00-00, NO FAULTS NOTED. BITE THE APU, PER FIM 49-11, NO FAULTS NOTED. RAN BOTH PACKS, PER AMM 21-00-00, NO FAULTS NOTED. RAN BOTH ENGINES, PER AMM 71-00-00, NO FAULTS NOTED. THIS CLEARS DMI 134960. MCC NOTIFIED. PLACARDS REMOVED.=

Part: GCU — MALFUNCTIONED (RT GENERATOR) · airframe 93,378 hrs · 18,208 cycles

RT AC BUS OFF EICAS MSG COM QRH AND MESSAGE WAS CLEARED. PERFORMED BPCU BIT, IAW 24-22-02. NO FAULTS FOUND. PERFORMED FIM 24-20 FT 801 THROUGH STEP 11. RT GEN CONTROL UNIT R & R, IAW 24-22-02 AND PERFORMED TEST OF GCU AND BPCU, IAW 24-22-02. OPS CHK GOOD. T/S ACCOMPLISHED, IAW 24-20 TASK 804 TABLE 102.

Part: GCU — MALFUNCTIONED (RT GENERATOR) · airframe 93,378 hrs · 18,208 cycles

RT GEN OFF EICAS MSG. RAN QRH AND MESSAGE DID NOT CLEAR. LANDED UNEVENTFULLY. PERFORMED FIM 24-20 FAULT TREE 801 THRU STEP 11. RT GEN CONTROL UNIT REMOVED & REPLACED, IAW 24-22-02. PERFORMED TEST OF GCU & BPCU, IAW 24-22-02. OPS CHECK GOOD AT THIS TIME. T/S ACCOMPLISHED, IAW 24-20 TASK 804 TABLE 102.

Part: FAULT LIGHT — FALSE ACTIVATION (APU) · airframe 93,364 hrs · 18,203 cycles

REPEAT WRITEUP APU FAULT ON 1 ATTEMPT, 2ND APU ATTEMPT SUCCESSFUL. PERFORMED APU CONTROL UNIT, IAW AMM 49-61-05. BITE TEST OPS CHECK AND TEST OK.

Part: RADAR — MALFUNCTIONED (WEATHER) · airframe 81,194 hrs · 18,062 cycles

WEATHER RADAR DOES NOT PAINT WEATHER VISUALLY, VERIFIED IN AUTO AND MANUAL VARIOUS. PERFORMED WEATHER SYSTEM TEST IAW AMM 34-43-00-735-033-002. WEATHER RADAR OPERATIONS CHECKS AND TEST GOOD, NO FAULTS.

Part: VALVE — MALFUNCTIONED (EQUP COOLING) · airframe 93,203 hrs · 18,146 cycles

EQUIP COOLING VALVE LIGHT ILLUMINATED. MOVED EQIP COOLING SWITCH FROM AUTO TO STBY VALVE ANNUNCIATOR LIGHT EXTINGUISES. THEN MOVE TO OVRD WITH PACK SWITCHES IN THE OFF POSITION.WARNING SOUNDS. RESET C/B THEN MOVED THE SWITCH BACK TO AUTO.NO VALVE LIGHT OR EICAS MESSAGE. MCC ADVISED.CONTINUED ON ITEM 2. PER FIM 21-58-FT 887.

Part: WARNING MESSAGE — FALSE ACTIVATION (APU) · airframe 93,193 hrs · 18,143 cycles

APU FAULT ADVISORY AFTER LANDING&NBSP;(<P>PERFORMED APU BITE IAW FIM 49-11 FR 805 FOUND LOW OIL PRESS ON ECU PER FIM 4911 FT 995 INSPECTED MAGNETIC CHIP DETECTOR FOUND NO DEBRIS&NBSP; CHECK APU OIL QUANTITYFOUND TO BE OVERSERVICES OPEN CAP AND LEFT OIL OVERFLOW UNTILL IT REACH FULL INDICATION&NBSP; APU OPERATED NORMAL&NBSP;</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (APU) · airframe 93,203 hrs · 18,146 cycles

APU FAULT AFTER LANDING. ONE START ATTEMPT MADE. PERFORMED APU ECU BITE AND APU OPS CHK REF AMM 49-61-05 AND AMM 49-11-00. APU OPS GOOD. MULTIPLE GOOD STARTS. NO FAULTS PRESENT.

Part: WARNING MESSAGE — FALSE ACTIVATION (APU) · airframe 93,142 hrs · 18,125 cycles

ON TAXI APU FAULT EICAS MSG ON FIRST APU START ATTEMPT. C/W QRH, SUCCESSFUL START ON SECOND ATTEMPT. PERFORMED APU START PROCEDURES IAW AMM 49-11-00. OPS TEST OK.

Part: LAMP — INOPERATIVE (LIGHT) · airframe 93,073 hrs · 18,099 cycles

R BLEED ISOL VALVE LIGHT INOP. RELAMPED R BLEED ISOLATION VALVE SWITCH IAW SWPM 20-84-13. OPS CHECK GOOD AT THIS TIME.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 93,082 hrs · 18,103 cycles

RIGHT DOME MOUNTED EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED LAMP, OPS CHECKS GOOD IAW AMM 33-51-11.

Part: GCU — FAULTED (RIGHT) · airframe 93,052 hrs · 18,092 cycles

R AC BUS OFF EICAS MSG AT TOUCHDOWN PERFORMED BPCU BITE TEST IAW FIM 24-20 FT 801. FOUND RH GCU AT FAULT, REPLACED GCU IAW AMM 24-22-02. BITE TEST NO FAULTS. ENG RUN CKS GOOD IAW AMM 71-00-00.

Part: STATUS MESSAGE — FALSE ACTIVATION (T/R UNIT) · airframe 93,052 hrs · 18,092 cycles

T-R UNIT EICAS STATUS MSG T/S IAW FIM 24-32 FT 803, NO FAULTS. MSG CLEARED, CKS OK.

Part: OIL SYSTEM — LOW (APU) · airframe 93,052 hrs · 18,092 cycles

APU FAULT ON START AFTER LANDING 2ND ATTEMPTS HUNG AT 20% RPM. SERVICED APU OIL. PERFORMED BITE TEST ON APU CONTROL. STARTED APU, START OK PER MM 49-41-00. OPS CHECK GOOD.<BR /></P>)

Part: PUMP — FAULTED (FUEL BOOST) · airframe 93,021 hrs · 18,082 cycles

LH AFT BOOST PUMP PRESS LIGHT INOP(<P>TRANSFER TO MDDR 132659 IAW DDG 24-42-01-01 CAT C, DUE DATE 20 AUG-20.</P><P><SPAN>LP #1296963 ITEM 1: REMOVED AND REPLACED THE LH AFT BOOST PUMP IAW AMM 28-22-03, OPS CHECK GOOD. THIS CLEARS MDDR #132659. MCC NOTIFIED. PLACARD REMOVED.</SPAN><BR DATA-MCE-BOGUS="1" /></P>)

Part: PUMP — FAULTED (FUEL BOOST) · airframe 93,023 hrs · 18,083 cycles

L AFT FUEL PUMP EICAS MSG IN CRUISE PRIOR TO ETOPS ENTRY. CIRCUIT BREAKER ALSO POPPED. AIR TURN BACK TO HNL(<P>REMOVED AND REPLACED L/H AFT BOOST PUMP IAW AMM 28-22-03 OPS CHECKS GOOD<BR /></P>)

Part: ADI — FAILED (CAPTAIN'S) · airframe 92,916 hrs · 18,050 cycles

AT CRUISE, FL 330, CAPTAIN`S ADI FLICKERED THEN FAILED. AFTER SCREEN FAILED A STRONG ODOR AND NOXIOUS FUMES BECAME APPARENT ON GROUND, SAW ADI CIRCUIT BREAKER TRIPPED. PERFORMED INSPECTION OF CAPTAIN'S ADI. DETERMINED FAILURE OF CRT. REMOVED AND REPLACED THE CAPTAIN'S ADI IAW AMM 34-22-03. OPS CHECKED GOOD. ACFT CLEARED FOR SERVICE.

Part: GCU — FAULTED (LEFT GENERATOR) · airframe 92,873 hrs · 18,039 cycles

LEFT GENERATOR OFF EICAS MESSAGE IN FLIGHT, RAN CHECKLIST, TURNED APU ON, MESSAGE REMAINED. REMOVED AND REPLACED THE LT GENERATOR CONTROL UNIT IAW AMM 24-22-02-004-001 AS PART OF T/S.

Part: WARNING SYSTEM — FALSE ACTIVATION (APU) · airframe 92,862 hrs · 18,036 cycles

APU FAULT MESSAGE ON FIRST START ATTEMPT AFTER LANDING, SECOND ATTEMPT STARTED NORMALLY. PERFORMED BITE CHECK OF APU ECU. NO FAULTS FOUND, REF AMM CHAP 49-00-00.

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 92,772 hrs · 18,010 cycles

APU "FAULT" AFTER 1ST AND 2ND START ATTEMPT. AFTER LANDING ACCOMPLISHED APU START WITH GOOD RESULTS. APU BITE CHECK DISPLAYED "START ABORT" W/ "SEE MY MANUAL" ON TWO PREVIOUS START ATTEMPTS REF FIM 49-11 FAULT TREE 989.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 92,772 hrs · 18,010 cycles

APU FAULT MSG. RECYCLED APU AND PERFORMED BITE TEST. NO FAULTS NOTED AT THIS TIME. EICAS SHOWS NO MESSAGES. APU AND OPERATIONAL IAW AMM 49-11-00 OK FOR SERVICE.

Part: OIL SYSTEM — LOW (APU) · airframe 92,712 hrs · 17,993 cycles

APU FAULT ON TAXI AFTER ATTEMPTED START, APU OIL QT ADD SHOWED ON STATUS. SERVICED APU OIL 2QTS IAW AMM 12-13-04. PERFORMED APU START; NO FAULTS, OK FOR SERVICES IAW 49-11-00.

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 92,683 hrs · 17,982 cycles

APU START ON 2ND ATTEMPT AFTER LANDING. FAULTED ON 1ST ATTEMPT.(<P>PERFORMED APU ECU BITE TEST REF AMM 49-61-05. NO FAULTS FOUND. TEST PASSED OK FOR RTS.<BR /></P>)

Part: OIL SYSTEM — LOW (APU) · airframe 92,674 hrs · 17,979 cycles

APU FAULT AFTER LANDING. 2 ATTEMPTS MADE.(<P>PERFORMED SUCCESSFUL STARTS IAW AMM 49-11-00. SERVICED .5&NBSP; QT OIL IAW AMM 12-13-04. BITE TEST ECU IAW AMM 49-61-05.</P>)

Part: BOOT — DAMAGED (APU) · airframe 92,675 hrs · 17,980 cycles

DAMAGE FOUND ON FLEX DOOR FOR APU DISCHARGE DUCT(<P>REMOVED AND REPLACED&NBSP;FLEX BOOT ON APU DISCHARGED DUCT IAW AMM 49-51-01.<BR /></P>)

Part: UNKNOWN — UNKNOWN (ELECTRICAL SYS) · airframe 92,669 hrs · 17,977 cycles

AFTER NOSE GEAR TOUCH DOWN THE BOTH UTILITY BUSES WERE OFF.(<P>PERFORMED BPCU BITE TEST ON AND CHECK BOTH&NBSP;UTILITY BUS IAW AMM 24-11-00. SYSTEM TEST OK.</P>)

Part: UNKNOWN — MALFUNCTIONED (ELECTRICAL SYS) · airframe 92,669 hrs · 17,977 cycles

RIGHT GEN OFF ON LANDING(<P>PERFORMED BPCU BITE TEST IAW AMM 24-22-00, PERFORMED ENGINE RUN UP IAW AMM 71-00-00. TEST OK.</P>)

Part: UNKNOWN — MALFUNCTIONED (ELECTRICAL SYS) · airframe 92,669 hrs · 17,977 cycles

STATUS: FWD EQ EXHAUST FAN T-R UNIT 1H FLOW INHIBITS.(<P>PERFORMED SYSTEM TEST FWD EQ EXH FAN, OK IAW AMM 21-58-00.</P><P><SPAN>LP 1141072: T/S T-R UNIT MASSAGE ON EICAS PER FIM 24-32-FT 803, SYS OK, NO MESSAGES PRESENT AT THIS TIME.</SPAN><BR DATA-MCE-BOGUS="1" /></P>)

Part: APU — INOPERATIVE (APU BAY) · airframe 92,673 hrs · 17,978 cycles

APU INOP(<P>TRANSFERRED TO MDDR 128526 IAW MEL 49-11-01A&NBSP;, CAT 'C'.</P><P>LP 1141077-7 - REMOVED AND REPLACED APU IAW WO #66347. OPS AND LEAK CHECK GOOD AT THIS TIME. THIS CLEARS DMI 128526, MCC NOTIFIED (AMM 49-11-01/401).</P><P>(NOTE: OPENED MDDDR 128588 - FOR APU COLD SOAK START VERIFICATION - DDG 25-AP-01)</P>)

Part: UNKNOWN — MALFUNCTIONED (GENERATOR SYS) · airframe 92,642 hrs · 17,968 cycles

RT GEN FAILED AFTER NOSE TOUCHED DOWN RECEIVED R AC BUS OFF MSG.(<P>PILOT STATED GOOD RESET ON R ENG GEN DURING TAXI. T/S PER FIM 24-20 FT 801 BPCU BITE. NO FAULTS NOTED, MCC ADVISED OK FOR SERVICE.<BR /></P>)

Part: SENSOR — MALFUNCTIONED (AOA) · airframe 92,627 hrs · 17,962 cycles

L AOA EICAS AFTER ENG START(<P>TRANSFERRED TO MDDR 128280 PER MEL 30-32-01, CAT 'C'.</P><P>LP 1131025: REMOVED AND REPLACED&NBSP; LEFT AOA&NBSP; SENSOR&NBSP; IAW AMM 34-12-03, OPS TEST OK. THIS CLEARS MDDR 128280.<BR /></P>)

Part: PRESSURE SWITCH — FAULTY (FUEL SYSTEM) · airframe 92,563 hrs · 17,936 cycles

L AFT FUEL PUMP LIGHT REMAINED ON AFTER SYS WAS ACTIVATED.(<P>PLACED ON MDDR 127937 PER MEL 28-22-01, CAT 'C'.</P><P>REF LP 1150108 - M2: REPLACED PRESSURE SW. S00071 IAW 28-42-01/401. OPS CHECKS GOOD. NO FURTHER DEFECTS NOTED. THIS CLEARS MDDR #127937. PLACARD REMOVED AND MCC NOTIFIED.</P>)

Part: OIL CAP — DEFECTIVE (APU) · airframe 92,543 hrs · 17,928 cycles

APU OIL QTY LOW(<P>TRANSFERRED TO MDDR 127826 PER MEL 49-11-01A, CAT 'C', DUE DATE 12MAY20, DISPATCH ACL 0459Z.<BR /></P><P>LP 1150085: REMOVED AND REPLACED APU OIL FILLER CAP IAW AMM 12-13-04 AND OPS CHECK IAW AMM 49-11-00. OPS CHECK GOOD. NO LEAKS NOTED. DMI #127826 CLOSED.</P>)

Part: O-RING — MISSING (APU OIL CAP) · airframe 92,551 hrs · 17,931 cycles

APU STATUS MESSAGE&NBSP; APU OIL QUANTITY&NBSP;(<P>FOUND APU OIL CAP MISSING O-RING, INSTALLED NEW O-RING IAW AMM 49-94-00 AND SERVICES IAW AMM 12-13-04, CHECK FOR LEAKS, GOOD. PERFORMED 3 STARTS WITH NO FAULTS.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 92,534 hrs · 17,925 cycles

L AFT FUEL PUMP EICAS AND PRESS LIGHT ILLUMINATED PRIOR TO ENGINE START. TURNING OFF THEN TURNING ON THE PUMP CLEARED THE MSG AND EXTINGUISHED THE LIGHT.(<P>PERFORMED OPS CHECK OF AFT FUEL PUMP PER AMM 28-22-00-501. OPS CHECK GOOD. NO FURTHER DEFECTS AT THIS TIME.</P>)

Part: BPCU — MALFUNCTIONED (ELECTRICAL SYS) · airframe 92,534 hrs · 17,925 cycles

UPON TOUCHDOWN R AC BUS DE-POWERED R GEN CONTROL SWITCH "OFF" LEGEND WAS ILLUMINATED. BPCU PER FIM 24-20 F/T 801, TEST OK. REMOVED AND REPLACED BUS POWER CONT UNIT, PERFORMED RT ENG GEN TEST IAW AMM 24-11-01 AND PERFORMED BPCU BITE TEST IAW AMM 24-22-00. OPS CHECKED GOOD. THIS CLEARS MDDR 127770.

Part: GCU — MALFUNCTIONED (RIGHT) · airframe 92,479 hrs · 17,907 cycles

R GEN TRIPPED OFF, RAN QRH, RECOVERED R GEN, BUT R UTILITY WOULD NOT COME ON LINE. POSITION 13000 FT MSL30 NM FROM ILN.(<P>ITEM PLACED ON MDDR 127461 IAW DDG 24-00-01-01, CAT 'B', DUE DATE 27AUG2020. AIRCRAFT REDUCED TO ER 120. MAINT. ACTIONS C/W. DISPATCH GTC 0238Z.</P><P>LP 1196493: REPLACED R/H GCU IAW AMM 24-22-02-004. OPS CHKS GOOD. CLOSED MDDR 127461.</P>)

Part: GCU — FAULTY (RIGHT) · airframe 92,481 hrs · 17,908 cycles

R AC BUS EICAS MSG DURING DESCENT&NBSP;(<P>REPLACED RH GEN GCU. IAW AMM 24-22-02. OPS CHKS GOOD.</P>)

Part: UNKNOWN — MALFUNCTIONED (ELECTRICAL SYS) · airframe 92,470 hrs · 17,905 cycles

R BUS FAILED DURING DESCENT.(<P>PERFORMED T/S PER FIM 24-20 FT 801 AND BITE CHK BPCU AND FOUND NO FAULTS, SYS CHKS OK.</P>)

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 92,416 hrs · 17,887 cycles

WX RADAR PAINT GROUND RETURN W/ 15 DEGREES TILT UP DURING CRUISE.(<P>PERFORMED OPERATIONAL TEST OF THE WEATHER&NBSP; RADAR SYSTEM, TEST OK IAW AMM 34-43-00.</P>)

Part: TRANSMITTER — FAULTY (RT ENGINE) · airframe 92,388 hrs · 17,877 cycles

R ENG FUEL FLOW .5 LOWER THAN L ENG FUEL FLOW REPEAT DISCREPANCY. R ENG FF SHOWED 0.0 IN IDLE DECENT. EVENT RECORDED.(<P>TRANSFERRED TO MDDR 126879 IAW MEL 73-31-01-02, CAT 'C', DUE DATE 20APR20. NO MX ACTION REQ. DISPATCH ACL 0619Z.</P><P>LP 1120337: REPLACED FUEL FLOW TRANSMITTER IAW AMM 73-31-01. OPS CKS GOOD. CLOSED MDDR 126879.</P>)

Part: PRESSURE SWITCH — FAULTY (ANTI-ICE SYSTEM) · airframe 92,376 hrs · 17,874 cycles

R ENG TAI VALVE MESSAGE ON SHUTDOWN.(<P>REPLACED R ENG INLET PRESS SWITCH IAW AMM 30-21-01. OPS CHKS NORMAL.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 92,215 hrs · 17,813 cycles

WX RADAR HSI MESSAGE AUTO TILT FAIL + 15 UP ON GROUND.(<P>PERFORMED WEATHER ANTENNA SYSTEM TEST IAW AMM 34-43-05. TEST PASS, NO MESSAGE.</P>)

Part: SENSE LINE — DAMAGED (RT ENGINE) · airframe 92,091 hrs · 17,772 cycles

RIGHT ENGINE PRV EICAS UPON CLIMB OUT WITH POWER AT CRUSE. EICAS WENT OUT, STATUS MESSAGE RIGHT ENGINE PRV REMAINS.(<P>TROUBLESHOT PER FIM 36-10 FT 847. FOUND RIGHT ENGINE PRV&NBSP;SENSE LINE DAMAGED. REPLACED DAMAGED PRV SENSE LINE. LEAK CHECK GOOD IAW B767 AMM 36-11-15. NO DEFECTS NOTED AT THIS TIME&NBSP;</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENG PRV) · airframe 92,088 hrs · 17,769 cycles

R ENGINE PRV STATUS MSG.(<P>PERFORMED FIM FOR R ENGINE PRV SHOWN AND R ENG BLEED LIGHT, FOUND NO FAULTS FROM AIR SUPPLY MODULE. RAN THE RIGHT ENGINE AND NO MSG SHOWN. EICAS&NBSP; MSG CLEARED. OPS CHECK NORMAL IAW FIM 36-10 FT 847 AND AMM 71-00-00.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENG PRV) · airframe 92,088 hrs · 17,769 cycles

R ENG PRV EICAS MSG.(<P>MSG CLEARED&NBSP;AND OPS CHECK NORMAL AT THIS TIME IAW FIM 36-10 FT 847 AND AMM 71-00-00.</P>)

Part: SEAL — MISSING (SHUTOFF VALVE) · airframe 92,090 hrs · 17,771 cycles

3RD TIME WRITE UP, "R ENG PRV" EICAS. ACCOMPLISHED QRH. R ENG PRV STATUS REMAIN.(<P>ON #2 ENG, SWAPPED PRV AND HPSOV PER MX CONT REQUEST IAW B767 AMM 36-11-18 AND 36-11-07. PERFORMED ENGINE RUN, OPS CHECK NORMAL.</P><P>LP 1086917 - ITEM M3:&NBSP;<SPAN>PER MAINTENANCE CONTROL REQUEST,&NBSP;</SPAN><SPAN>INSTALLED BLEED AIR CONTROL CARD FOR R ENG M860. FOUND TO BE BFS. REINSTALLED PREVIOUSLY REMOVED CARD. OPS CHECK NORMAL IAW B767 AMM 36-11-12. PART EFFECTIVITY VERIFIED.</SPAN></P><P>LP 1086918 - ITEM M5:&NBSP;<SPAN>WHILE REMOVING HPSOV FOUND E-SEAL MISSING ON #2 ENG.&NBSP;</SPAN><SPAN>INSTALLED NEW E-SEAL FOR HPSOV ON #2 ENG IAW B767 AMM 36-11-07. PART EFFECTIVITY VERIFIED. OPS CHECK NORMAL.</SPAN></P><P>LP 1086918 - ITEM M6: PERFORMED FIM 36-10 FAULT TREE 847. MESSAGE CLEARED.</P>)

Part: SHUTOFF VALVE — MALFUNCTIONED (LT A/C PACK) · airframe 91,961 hrs · 17,726 cycles

LEFT PACK OFF, WILL NOT RESET. PERFORMED A CHECK OF THE LEFT PACK FLOW CONTROL SHUTOFF VALVE IAW AMM 21-00-00. RESEATED CONNECTORS D2770 D1598, D746 AND D20316, LT PACK SHUTOFF VALVE. PERFORMED BITE TEST IAW AMM 21-51-01. NO FAULTS.

Part: DUCT — UNKNOWN (APU) · airframe 79,459 hrs · 10,923 cycles

APU PNEUMATIC INOPERATIVE. REMOVED AND REPLACED APU AIR SURGE DUCT IAW AMM 49-53-01. OPS AND LEAK CHECKED GOOD.

Part: GCU — FAILED (RT GENERATOR) · airframe 91,897 hrs · 17,709 cycles

R ENG GEN FIELD LIGHT AT P6 BPCU SHOWS OVER VOLT TRIP. REPLACED R GCU IAW AMM 24-22-02. OPS CHECK NORMAL.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 91,802 hrs · 17,679 cycles

FWD EQPT VALVE EICAS MESSAGE DISPLAYED. COMPLIED WITH QRH.(<P>ACCOMPLISHED AMM 21-58-00. ALL TESTS PASS. MSG CLEARED. A/C OK FOR SERVICE.<BR /></P>)

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 91,797 hrs · 17,678 cycles

MAIN CARGO FIRE MASTER WARNING WHILE AT GATE IN TPA.(<P>PERFORMED FIRE SMOKE DET FOR MAIN CARGO DECK IAW AMM 26-10-00. OPS CHK NORMAL.<BR /></P>)

Part: OIL SYSTEM — LOW (APU) · airframe 91,787 hrs · 17,673 cycles

APU FAULT AFTER LANDING. APU OIL INDICATES 0 (ADD).(<P>REPLENISHED OIL TO APU PER AMM 12-13-04. APU START NORMAL. NO FAULT MSG NOTED. OK FOR SERVICE. NO LEAKS NOTED.<BR /></P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (WEATHER RADAR) · airframe 91,741 hrs · 17,654 cycles

WEATHER RADAR SYSTEM STATUS MESSAGE. TROUBLESHOT IAW FIM 34-43 FT 805. NO FAULTS FOUND. SYSTEM OK.

Part: A/C PACK — UNKNOWN (LEFT) · airframe 91,741 hrs · 17,654 cycles

AFTER PUSHBACK LEFT PACK WILL NOT TURN ON. DUCT PSI OK. PERFORMED FIM 21-51 FT 803, NO FAULTS NOTED. OPS CHECKED GOOD. ALLOWED COOLING PERIOD OF PACKS. PERFORMED OPS CHECK AGAIN IAW FIM 21-51 FT 803. NO FAULTS NOTED IAW AMM 21-51-00.

Part: RADAR — MALFUNCTIONED (WEATHER) · airframe 91,710 hrs · 17,641 cycles

WX RADAR TILT (AUTO) TILT/DISH TO -1C AND PAINTS EXCESSIVE GROUND CLUTTER @ 37000.(<P>PERFORMED SYSTEM TEST AND OPERATIONAL TEST OF WEATHER RADAR SYSTEM, TESTED&NBSP;GOOD IAW B767 AMM 34-43-00-735-053-002 &AMP; 34-43-00-715-026-002. NO FURTHER DEFECTS NOTED AT THIS TIME.<BR /></P>)

Part: PUMP — INOPERATIVE (LT FUEL) · airframe 91,676 hrs · 17,630 cycles

L AFT FUEL PUMP INOP.(<P>TRANSFERRED TO MDDR 122287 IAW MEL 28-22-01, CAT 'C'.</P><P>LP 1232308: TROUBLESHOT&NBSP; PER&NBSP; FIM&NBSP; B767 28-22&NBSP; FAULT TREE&NBSP; 819. ALL&NBSP; SYSTEMS&NBSP; NORMAL.&NBSP; CLEANED&NBSP; &AMP; RESET&NBSP; CONNECTOR&NBSP; ON&NBSP; L&NBSP; AFT&NBSP; BOOST PUMP.&NBSP; NO&NBSP; DEFECTS&NBSP; NOTED AT&NBSP; THIS&NBSP; TIME. THIS&NBSP; CLEARS&NBSP; MDDR #122287. MCC NOTIFIED.&NBSP; ALL&NBSP; PLACARDS REMOVED.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (ENGINE) · airframe 91,710 hrs · 17,641 cycles

IDLE DISAGREE EICAS MESSAGE WHILE LANDING. ACCOMPLISHED FIM 32-09-03 FIG 103. NO PSEU FAULTS AT THIS TIME. CLEARED MSG, NO FURTHER FAULTS.

Part: START VALVE — MALFUNCTIONED (LEFT) · airframe 91,614 hrs · 17,605 cycles

ADVISORY: DURING LEFT ENG START, L ENG STARTER EICAS MSG APPEARED FOR 3 SECONDS, THEN DISAPPEARED. ENG THEN STARTED NORMALLY.(<P>T/S PER FIM 80-11 FT 803, PERFORMED BITE TEST ON L PIMU. FLAGGED "L SAV DISAGREE". REMOVED AND REPLACED START VALVE IAW AMM 80-11-02, OPS CKS GOOD.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (STARTER) · airframe 91,608 hrs · 17,602 cycles

ADVISORY: DURING LEFT ENGINE START, "L ENG STARTER" ILLUMINATED. PRIOR TO CREW BEGINNING CHECKLIST, EICAS MSG DISAPPEARED AND ENGINE STARTED NORMALLY.(<P>PREFORMED OPERATIONAL START OF L/H ENGINE IAW B767 AMM 80-11-00, NO DEFECTS NOTED. NO ENGINE STARTER MSG.<BR /></P>)

Part: PRESSURE SWITCH — FAILED (FUEL PUMP) · airframe 91,585 hrs · 17,592 cycles

LEFT FWD AND AFT FUEL PUMPS NOT DEPRESSURIZED. NO PRESS LIGHTS.(<P>TRANSFERRED TO MDDR 121445 AS PER MEL DDG 28-22-01-01. L AFT PUMP DE-ACTIVATED, C/B PULLED AND COLLARED, CAT 'C', DUE DATE 13-DEC-19. PLACARD INSTALLED.</P><P>LP 1232253 - M5: REMOVED AND REPLACED L/H AFT FUEL PUMP PRESSURE SWITCH IAW AMM 28-42-01. OPS CHECK GOOD, NO FAULTS NOTED. THIS CLEARS DMI 121445. PLACARD REMOVED AND MCC NOTIFIED.<BR /></P>)

Part: OIL SYSTEM — LOW (APU) · airframe 91,563 hrs · 17,583 cycles

APU OIL QUANTITY STATUS MESSAGE, APU DID NOT START. ONLY ONE ATTEMPT MADE.(<P>SERVICED APU OIL IAW AMM 12-13-04. RAN APU IAW AMM 49-11-00, OPS CHECK OK AT THIS TIME.</P>)

Part: REGULATOR — LEAKING (OXYGEN BOTTLE) · airframe 91,465 hrs · 17,550 cycles

CREW O2 BOTTLE 1 LEAKING AT&NBSP;COUPLING.(<P>REMOVED AND REPLACED CREW O2 BOTTLE 1 REGULATOR ASSY- TRANSDUCER IAW B767 AMM 35-11-04, NO LEAKS NOTED.<BR /></P>)

Part: PRESSURE SWITCH — MALFUNCTIONED (FUEL SYSTEM) · airframe 91,314 hrs · 17,491 cycles

AFT LEFT FUEL PUMP LOW PRESSURE LIGHT NOT ILLUMINATED WITH PUMPS SWITCH OFF. REPEAT WRITE-UP REF LOG PAGE 1086652 AND 1086631.(<P>TRANSFERRED TO MEL 28-22-01. MDDR 119492 ASSIGNED, CAT 'C', DUE DATE: 01-NOV-19. MAINT PROCEDURES C/W.</P><P><BR DATA-MCE-BOGUS="1" /></P><P><BR DATA-MCE-BOGUS="1" /></P><P>LP 1098183 - M2: REMOVED AND REPLACED L/H AFT FUEL PRESSURE SWITCH IAW AMM 28-42-01. THIS ACTION CLEARS DMI 119492. PLACARDS REMOVED AND MCC NOTIFIED.</P>)

Part: WARNING LIGHT — NO INDICATION (FUEL PUMP) · airframe 91,304 hrs · 17,487 cycles

AFTER SHUTTING DOWN BOTH ENGINES, WITH APU RUNNING AND TURNING ALL FUEL PUMPS OFF, THE LEFT AFT FUEL PUMP LOW PRESSURE LIGHT NOT ILLUMINATED.(<P>PERFORMED OPERATIONAL TEST OF THE LEFT AFT FUEL PUMP PER AMM 28-22-03, OPS CHECK NORMAL.</P>)

Part: KNOB — UNSECURE (APU SELECTOR) · airframe 91,271 hrs · 17,476 cycles

APU SELECTOR KNOB IS LOOSE. RE-SECURED APU SELECTOR KNOB REF AMM 49-41-81, OPS CHECK NORMAL AT THIS TIME.&NBSP;</P>)

Part: SEAL — DISLODGED (NR 2 ENG INLET) · airframe 91,264 hrs · 17,474 cycles

ORANGE SEAL APPEARS EXTRUDED OR DISLODGED ON SENSOR PROBES IN ENGINE INLET ON # 2 ENGINE.(<P>CORRECTED SEAL IAW AMM 72-32-00, NO FURTHER DEFECTS NOTED AT THIS TIME.&NBSP;</P>)

Part: SELECTOR — LOOSE (APU START) · airframe 91,258 hrs · 17,472 cycles

APU START SELECTOR IS LOOSE. ADJUSTED & TIGHTENED APU START SELECTOR IAW AMM 49-61-00. OP'S CHECK NORMAL AT THIS TIME.

Part: ENGINE — NOT REPORTED (NR 2) · airframe 91,170 hrs · 17,442 cycles

NR 2 ENG DISC RECORD COMPLIANCE ISSUE. REMOVED AND REPLACED THE NR 2 ENGINE IAW AMM 71-00-02.

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 91,111 hrs · 17,421 cycles

LEFT AFT FUEL PUMP WILL NOT TURNOFF WHEN DE-SELECTED, NO PRESSURE LIGHT OR ASSOCIATED EICAS MESSAGE. PERFORMED OPS TEST LEFT AFT FUEL PUMP IAW AMM 28-22-00-1. OPS CHECKED GOOD, PRESSURE LIGHT AND EICAS MESSAGE WHEN PUMP OFF.

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 91,046 hrs · 17,398 cycles

ITEM 1 - APU COLD SOAK START FL 360 -51 TEMP, 21:52Z; 3 ATTEMPTS UNSUCCESSFUL. ITEM 2 - APU FAULT EICAS. NOTED BY MX, DMI CONTINUES FOR APU COLD SOAK, MCC ADVISED. ITEM - 2: PERFORMED APU BITE PROCEDURE IAW FIM 49-11 FT 987. ECU LRU FAULTED, CLEARED FAULT, APU OPERATING NORMAL. LP 1051095 - ITEM 1: APU RELIABILITY COLD SOAK ACCOMPLISHED ON FLT LEG SCK - BWI SAT -54, FL 390; START SUCCESSFUL ON 1ST ATTEMPT.

Part: PRESSURE SWITCH — MALFUNCTIONED (LT FUEL PUMP) · airframe 90,917 hrs · 17,352 cycles

CTR LEFT FUEL PUMP INOP. PERFORMED FIM TASK 28-22 FT 805 UP TO AND INCLUDING SHEET 3 BLOCK 49/50. SYSTEM (PUMP) WORKED AS REQUIRED, PER FIM RECOMMEND PRESSURE SWITCH PN # 60B92400-7 (LOC:S423) REF WDM 28-22-12. REMOVED AND REPLACED CENTER (OVERRIDE) LT FUEL PUMP PRESSURE SWITCH IAW B767 AMM 28-42-01. OPS AND LEAK GOOD PER AMM 28-22-00.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 90,869 hrs · 17,336 cycles

LEFT ENG SPEED CARD STATUS MESSAGE DISPLAYED AT BLOCK-IN. TROUBLESHOT PER B767 FIM 73-21 FT 871, NO FAULTS NOTED AT THIS TIME.

Part: RELAY — UNKNOWN (FUEL PUMP) · airframe 90,821 hrs · 17,321 cycles

LEFT CENTER PUMP LOW PRESSURE LIGHT ILLUMINATED. TROUBLESHOT THE LEFT CENTER BOOST PUMP IAW FIM 28-22 FT 805, NO FAULTS NOTED. THE LEFT CENTER LIGHT STARTS FLASHING AROUND 1500 POUNDS, THIS IS NORMAL. RT CTR WILL PUMP TO .4 POUNDS. REOPENED ORIGINAL MDDR 116005. MX ACTION COMPLIED WITH NO FURTHER DEFECTS NOTED. PERFORMED A VISUAL INSPECTION, SHAKE DOWN OF LT AUX TANK BOOST PUMP WIRING IAW WDM 28-22-12, SHEET 1. FROM P6 PANEL CIRCUIT BREAKER C369 TO E/E P36 PANEL, PLUG D5894. NO WIRING DEFECTS NOTED. AS A PRECAUTION, R & R RELAY K633, LT PUMP OPS NORMAL, COULD NOT DUPLICATE FAILURE. RECOMMEND REPLACING RELAY K329, REMOVED AND REPLACED RELAY K329 IAW WD 28-22-12. OPS CHECKED NORMAL. REVERSED MAINTENANCE ACTION IAW DDG 28-22-02A. MONITORED LH FUEL PUMP FOR FUEL MIGRATION, NO MIGRATION NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PUMP) · airframe 90,788 hrs · 17,308 cycles

LEFT CENTER FUEL PUMP INOP ON TAXI OUT.(<P>TRANSFERRED TO MDDR 115786 IAW DDG 28-22-02A, CAT C. TROUBLESHOT L CTR FUEL PUMP IAW FIM 28-22 FAULT TREE 805. NO DEFECTS NOTED, OPS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 90,634 hrs · 17,252 cycles

RT GEN DRIVE REMAINED ON FOR 2 MINUTES AFTER START TNEN EXTINGUISHED(<P>PERFORMED IDG INSPECTION IAW AMM 24-11-01 NO DEFECTS NOTED</P>)

Part: PUMP — MALFUNCTIONED (FUEL SYSTEM) · airframe 90,624 hrs · 17,249 cycles

CENTER LEFT BOOS PUMP INOP&NBSP;(<P>TRANSFER TO MDDR # 114305 IAW DDG 28-22-02A&NBSP; CATC DUE DATE 16-JULY-2019</P><P>LP 1090219 -M4 RESET /B LEFT CENTER BOOST PUMP&NBSP; OPS CHECK OK IAW AMM 28-22-05&NBSP;</P>)

Part: INDICATION SYS — MALFUNCTIONED (FUEL SYSTEM) · airframe 90,624 hrs · 17,249 cycles

LEFT FUEL FLOW INDICATION INOP&NBSP;(<P>TRANSFER TO MDDR&NBSP; # 114307 IAW DDG 73-31-01-02 CAT C DUE DATE 16JULY-2019</P><P>LP 1090219-M5 INBOUND CREW REPORTED&NBSP; LEFT FUEL FLOW&NBSP; INIDICATION NORMAL RAN LEFT&NBSP; ENG AND OPS CHECK OK IAW AMM 71-00-00&NBSP;</P>)

Part: CONTROL PANEL — MALFUNCTIONED (WEATHER RADAR) · airframe 90,622 hrs · 17,248 cycles

L WXR SYS AUTO TILT MODE INOP&NBSP;(<P>TRANSFERRED TO MDDR # 114328 AS PER MEL 34-43-01-04 CAT C&NBSP;</P><P>LP 1090216-M3 REPLACED&NBSP; WXR CONTROL PANEL&NBSP; PERFORMED GROUND TEST&NBSP; SYSTEM OK&NBSP; &NBSP;IAW AMM 34-43-02 AND 34-43-00</P>)

Part: CONTROL VALVE — MALFUNCTIONED (AC BAY) · airframe 90,610 hrs · 17,244 cycles

LEFT PACK TEMP EICAS MSG AND AUTO SHUT DOWN(<P>REMOVED AND REPLACED LEFT PACK TEMPERATURE CONTROL VALVE IAW AMM 21-51-12 OPS CHECK GOOD&NBSP;</P>)

Part: CONTROL VALVE — MALFUNCTIONED (AC BAY) · airframe 90,610 hrs · 17,244 cycles

RIGHT PACK TEMP EICAS MESSAGE. &NBSP;(<P>C/W BITE CHECK ON TEMP CONTROL BOX IAW AMM 21-51-00. FOUND FAULT ON TEMP CONTROL VALVE, REPLACED RIGHT TEMP CONTROL VALVE AND OPS CHECKED IAW AMM 21-51-12-004-001/404-013. OPS CHECK GOOD, NO FAULTS NOTED.&NBSP;</P>)

Part: IDG — LOW (RT ENGINE) · airframe 90,610 hrs · 17,244 cycles

RIGHT GENERATOR DRIVE EICAS MESSAGE INTERMITTENT. &NBSP;(<P>SERVICED ENG # 2 IDG REF 12-13-03 AND PERFORMED ENGINE RUN REF AMM 71-00-00. IDG COMES ONLINE AS REQUIRED, PUT A LOAD, NO DEFECTS NOTED AT THIS TIME. A/C OK FOR SERVICE.&NBSP;</P>)

Part: CONTROL UNIT — MALFUNCTIONED (AC BAY) · airframe 90,600 hrs · 17,239 cycles

LEFT PACK TEMP EICAS MSG.(<P>PERFORMED BITE TEST ON LEFT PACK TEMP CONTROL UNIT IAW FIM 21-51-803. NO FAULTS NOTED AT THIS TIME, OPS TEST OK.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 90,600 hrs · 17,239 cycles

RT PACK TEMP EICAS MSG.(<P>PERFORMED BITE TEST CHECK ON TEMP CONTROLLER COMPT IAW FIM 21-51-803. NO FAULTS NOTED AT THIS TIME ON RIGHT HAND PACK.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 90,585 hrs · 17,231 cycles

R PACK TEMP EICAS MESSAGE ON GROUND. EICAS MESSAGE WENT AWAY AFTER A FEW MOMENTS. (<P>PERFORMED RT PACK OPS TEST AND BITE TEST OF RT PACK TEMP CONTROLLER IAW AMM 21-51-00. NO FAULTS NOTED AT THIS TIME.</P>)

Part: LANYARD — UNSECURE (PAX DOOR) · airframe 90,575 hrs · 17,227 cycles

MAIN ENTRY DOOR ESCAPE ROPE FELL OUT WHEN OPENING ENTRY DOOR. MISSING SNAP ON STORAGE BAG. SECURED SNAPS ON ESCAPE ROPE COVER IAW SRM 51-40-02, OPS NORMAL.

Part: BPCU — FAILED (NR 2 GENERATOR) · airframe 90,525 hrs · 17,208 cycles

AFTER START OR THE NR 2 ENGINE, GEN DRIVE LIGHT ILLUMINATED SELF EXTINGUISHED AFTER 1 MINUTE. SERVICED THE IDG IAW AMM 12-13-03. OPS CHECKED GOOD. BPCU SHOWS NO FAULTS. REMOVED AND REPLACED BPCU IAW AMM 24-41-03. OPS CHECKED GOOD.

Part: UNKNOWN — NOISE (COCKPIT) · airframe 90,525 hrs · 17,208 cycles

BLEED AIR NOISE IN COCKPIT REACHES 78.3 DB AT CLIMB POWER. COULD NOT DUPLICATE ON GROUND. OPS CHECK OF PACK SYSTEM GOOD IAW AMM 21-51-00. T/S FLIGHT DECK BLEED AIR NOISE IAW AMM 21-22-00. NO DEFECTS NOTED. RAN RH ENGINE TO TRY TO DUPLICATE THE NOISE IAW AMM 71-00-00. FLT DECK NOISE WITH PACKS ON WAS NORMAL.

Part: PRESSURE SWITCH — FAILED (FUEL PUMP) · airframe 90,525 hrs · 17,208 cycles

WITH FUEL IN CENTER TANK 1200LBS LEFT CENTER FUEL PUMP PRESSURE LIGHT ON WHEN OPERATING PUMP EICAS. REMOVED AND REPLACED LEFT CENTER PUMP PRESSURE SWITCH IAW AMM 28-42-01. PERFORMED TEST AND SYSTEM OK. RESET BREAKERS.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT A/C PACK) · airframe 90,516 hrs · 17,206 cycles

"RIGHT PACK TEMP" EICAS, RIGHT PACK OVERHEAT.(<P>PERFORMED PACK TEMPERATURE CONTROLLER BITE TEST REF AMM 21-51-14-705-035. COULD NOT DUPLICATE MESSAGE. OPS CHECK OK AT THIS TIME.</P>)

Part: PUMP — WARNING MESSAGE (LT FUEL) · airframe 90,480 hrs · 17,194 cycles

LEFT CTR FUEL PUMP PRESS LIGHT ILLUMINATED AND L CTR FUEL PUMP EICAS MSG (AMBER). REMOVED AND REPLACED LEFT CENTER OVERRIDE PUMP IAW AMM 28-22-05. LEAK CHECK GOOD, TRANSFERS GOOD, PRESS LIGHT GOOD.

Part: STATUS MESSAGE — FALSE ACTIVATION (LT SPEED CARD) · airframe 90,465 hrs · 17,190 cycles

STATUS MESSAGE, LEFT ENGINE SPEED CARD. PERFORMED OPS CHECK IAW PER B767 AMM 77-12-00. OPS CHECKED GOOD, NO STATUS MESSAGE DISPLAYED.

Part: PUMP — MALFUNCTIONED (LT CENTER) · airframe 90,465 hrs · 17,190 cycles

LEFT CENTER FUEL PUMP INOP. PERFORMED OPS CHECK OF PUMP PER AMM 28-22-01. OPS CHECK GOOD.

Part: IDG — MALFUNCTIONED (RIGHT) · airframe 90,453 hrs · 17,186 cycles

EICAS MSG "RT GEN OFF". TROUBLESHOT RT GEN OFF MSG. REMOVED AND REPLACED BUS POWER CONTROL UNIT IAW B767 AMM 24-41-03. BPCU TEST GOOD. OVER VOLTAGE TRIP FAULT WAS RECORDED ON LAST FLT WAS REASON. NO FAULTS PRESENT AT THIS TIME. REMOVED AND REPLACED RIGHT ENG GEN IDG IAW AMM 24-11-01. OPS CHECK GOOD AT THIS TIME.

Part: GCU — MALFUNCTIONED · airframe 90,441 hrs · 17,181 cycles

THRU 18,000 AFTER TURNING TAXI L&AMP;R TURNOFF LIGHTS &AMP; WING LANDING LIGHTS, ENTIRE 2 AC BUS FAILED. "R AC BUS ISLN" CAUTION MSG. RAN QRH &AMP; COMPLIED. A MAYDAY CALL WAS DECLARED. MULTIPLE SYSTEMS FAILURES OCCURRED DURING REST OF DESCENT.&NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; LP 1063372 - ITEM 5: ALL 3 HYD QTY INDICATOR READ RF AND DISPLAY 00.2, 00.3, 00.3 RESPECTFULLY. LP 1063372 -&NBSP; ITEM 6: AUTO BRAKES INOP ON DESCENT. LP 1063373 - ITEM 7: NO AUTOLAND ON ASA. LP 1063374 - ITEM 10: RIGHT IDG INOP.&NBSP;(<P>UPON T/S FOUND METAL IN PIN D13 OF CONNECTOR D256B CAUSING SHORT. REMOVED AND REPLACED RIGHT GEN CONTROL UNIT IAW 24-22-02. PERFORMED ENG RUN IAW 71-00-00 AND RIGHT IDG OPS TEST IAW 24-11-00. TEST NORMAL AT THIS TIME. NO FURTHER DEFECTS NOTED. DMI 112899 CLOSED.&NBSP;</P>)

Part: VALVE — MALFUNCTIONED (RT ENGINE) · airframe 90,434 hrs · 17,178 cycles

R/H ENG FAV CLOSED AND OPEN SWITCHES DISAGREE. REMOVED AND REPLACED THE R/H ENG FAV (SUPPLY PRE-COOLER VALVE) IAW B767 AMM 36-11-15. PERFORMED SATISFACTORY OPS CHECK IAW B767 AMM 36-11-15.</P>)

Part: WARNING MESSAGE — MISSING · airframe 90,434 hrs · 17,178 cycles

EICAS IS MISSING INDICATION ON RT "PRIM HX IN". PERFORMED BITE TEST FOR MR SUPPLY BITE MODULE IAW B767 AMM 36-11-16-745-135 BITE PASSED INDICATION PRESENT.

Part: CONNECTOR — NOT SEATED (A/C CONTROLLER) · airframe 90,434 hrs · 17,178 cycles

STANDBY PACK TEMP CONTROLLER FAILS BITE TEST "RIGHT COMP SENSOR" RESEATED CONNECTORS TO TS5134 AND TS5135 OPS CHECK GOOD IAW AMM 21-51-14-705-036, 21-51-06, SSM 21-50-06, 21-50-05, WDM 21-51-23, 21-51-13.

Part: SHUTOFF VALVE — MALFUNCTIONED (HYD SYSTEM) · airframe 90,434 hrs · 17,178 cycles

RH ENG HYD PRESSURE FROM PUMP WAS INOP. REMOVED AND REPLACED EDP. REMOVED AND REPLACED HYD SHUTOFF VALVE.

Part: UNKNOWN — DAMAGED (WINDOW HEAT) · airframe 90,434 hrs · 17,178 cycles

L/H SIDE WINDOW HEAT PB IS DAMAGED. REMOVED AND REPLACED L/H SIDE WINDOW HEAT PB IAW B767 AMM 30-41-02 AND SWPM 20-84-15. PERFORMED SAT OPS CHECK IAW AMM 30-41-02 AND 33-13-00. NO DEFECTS NOTED.

Part: UNKNOWN — DAMAGED (LT WINDOW HEAT) · airframe 90,434 hrs · 17,178 cycles

LH SIDE WINDOW HEAT P/B IS DAMAGED. REMOVED AND REPLACED LH SIDE WINDOW HEAT P/B IAW AMM 30-41-02 AND SWPM 20-84-15. PERFORMED OPS CHECK IAW B767 AMM 30-41-02 AND 33-13-00 NO FAULTS NOTED.

Part: PLUG — GOUGED (NR 2 ENGINE) · airframe 90,434 hrs · 17,178 cycles

NR 2 OB BORESCOPE PLUG B3-1 GOUGED. REMOVED AND REPLACED #2 ENG BORESCOPE PLUG B3-1 IAW AMM 72-00-00. LEAK CHECK ACCOMPLISHED ON TC T2031.

Part: SENSOR — FAULTED (DUCT TEMP) · airframe 90,434 hrs · 17,178 cycles

FLT DECK DUCT TEMP SENSOR FAULT ON ZONE TEMP CONTROLLER. REMOVED AND REPLACED FLT DECK DUCT TEMP SENSOR IAW AMM 21-61-02 PERFORMED GOOD OPS CHECK IAW B767 FSM 21-61FAULT TREE 912 NO DEFECTS NOTED.

Part: FILTER — TRIPPED (LT HYD SYSTEM) · airframe 90,434 hrs · 17,178 cycles

LEFT HYD BAY RETURN FILTER MODULE PRESSURE INDICATOR POPPED. REMOVED AND REPLACED LH HYD RETURN FILTER IN LH PYLON IAW B767 AMM 29-11-17. ACCOMPLISHED OPS CHECK IAW B767 AMM 29-11-00, 29-11-17 AND 71-00-00 NO DEFECTS NOTED.&NBSP;</P>)

Part: DOOR — EXCESS PLAY (NR 2 NACELLE) · airframe 90,434 hrs · 17,178 cycles

NR 2 ENG OB CORE COWL PRESSURE RELIEF DOOR HAS PLAY. REMOVED AND REPLACED NR 2 ENG OB CORE COWL PRESSURE RELIEF DOOR HINGE PINS AND RELATED HARDWARE IAW B767 AMM 71-11-09.

Part: PUMP — DAMAGED (NR 2) · airframe 90,434 hrs · 17,178 cycles

#2 ENG EDP FOUND DAMAGED DEPRESS VALVE. REMOVED AND REPLACED NR 2 EDP DEPRESS VALVE IAW B767 AMM 29-11-05 ACCOMPLISHED OPS CHK. IAW AMM 29-11-00, 29-11-05 AND 71-00-00 NO DEFECTS NOTED.

Part: CONNECTOR — CORRODED (IGNITION BOX) · airframe 90,434 hrs · 17,178 cycles

NR 1 ENG IGNITION BOXES HAVE CORROSION ON CANNON PLUG CONNECTION RECEPTACLES. REMOVED AND REPLACED BOTH IGNITION EXCITER BOXES AND PERFORMED SATISFACTORY OPS TESTS #1 ENG IAW AMM 74-11-01 AND AMM 74-00-00.

Part: WIRE — BROKEN (A/C CONTROLLER) · airframe 90,434 hrs · 17,178 cycles

RIGHT PACK CONTROLLER BITE FAILS MX MAN SENSOR. FOUND AND RETERMINATED BROKEN WIRES AT CONNECTOR D2826 IAW B767 WDM 21-51-22 PERFORMED SATISFACTORY OPS CHECK IAW B767 AMM 21-51-14. NO DEFECTS NOTED. FAULT CLEARED.

Part: UNKNOWN — MALFUNCTIONED (IGNITION SYS) · airframe 90,412 hrs · 17,168 cycles

NO LIGHT ON FIRST START ATTEMPT USING SINGLE IGNITION. USED BOTH FOR SECOND ATTEMPT, SUCCESSFUL START. RIGHT ENGINE(<P>PERFORMED IGNITION AUDIBLE TEST IAW AMM 74-00-00 NO FAULTS NOTED. OPS CHECK NORMAL AT THIS TIME.</P>)

Part: IGNITER — FAULTY (RT ENGINE) · airframe 90,400 hrs · 17,164 cycles

RIGHT ENGINE IGNITER 2 STATUS MESSAGE&NBSP;(<P>REMOVED AND REPLACED THE RIGHT ENGINE NR 2 IGNITER PLUG. OPS CHECK GOOD ON AUDIO CHECK IAW AMM 74-21-00 AND 74-00-00-705-015.&NBSP;</P>)

Part: UNKNOWN — MALFUNCTIONED (NR 2 ENGINE) · airframe 90,400 hrs · 17,164 cycles

NR 2 ENGINE NO EGT RISE ON FIRST START&NBSP;(<P>SEE ITEM 3 ON LOG PAGE&NBSP;1078399. ACCOMPLISHED RIGHT ENGINE START OPS CHECK NORMAL IN BOTH, SINGLE AND DUAL IGNITION. OPERATION IAW AMM 74-00-00 AND 72-00-00</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 90,387 hrs · 17,159 cycles

RIGHT ENG IGNITION 2 STATUS MSG ON RIGHT ENG START&NBSP;(<P><SPAN>PERFORMED RT ENG IGNITION SYS AUDIBLE TEST IAW AMM 74-00-00. OPS CHECK GOOD. PERFORMED PIMU (RT) BITE PROCEDURE IAW FIM 71-01 FAULT TREE 810 AND PERFORMED 2 ENGINE RUNS OF RT ENGINE IAW AMM 71-00-0. ALL OPS CHECK GOOD.</SPAN></P>)

Part: OXYGEN MASK — DAMAGED (COCKPIT) · airframe 90,369 hrs · 17,152 cycles

CAPT O2 MASK RATTLES WHEN BREATHING IN.(<P>SWAPPED CAPTS O2 MASK P/N MC10-08-109 SN SE72273 WITH THE RIGHT SUPERNUMERARY SEAT PN MC 10-08-109 SN B124047. IAW AMM 35-11-51. OPS CHECK NORMAL. REF ITEM 3 THIS PAGE FOR RIGHT SUPERNUMERARY SEAT DEFERRAL.</P>)

Part: OXYGEN MASK — INOPERATIVE · airframe 90,369 hrs · 17,152 cycles

RIGHT SUPERNUMERARY SEAT OXYGEN MASK INOP.(<P>TRANSFERRED TO DMI 110647.</P><P>LOG PAGE 1078435: REF DMI 110647, REMOVED AND REPLACED RH SUPERNUMERARY O2 MASK IAW AMM 35-11-51. OPS CHECKS GOOD. THIS CLEARS DMI 110647. MCC NOTIFIED AND PLACARDS REMOVED.</P>)

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 90,300 hrs · 17,128 cycles

R ENGINE NO LIGHT OFF WITH SINGLE IGNITER, SWITCHED TO BOTH IGNITERS.(<P>PERFORMED ENGINE START / RUN W. SINGLE IGNITER SELECTED. ENGINE START UP NORMAL THROUGH ALL PARAMETERS. ALSO PERFORMED IGNITER CHECK PRIOR TO START. NO FAULTS NOTED IAW AMM 74-00-00 &AMP; 80-11-00.<BR /></P>)

Part: MONOPOLE — LOOSE (NR 2) · airframe 90,300 hrs · 17,128 cycles

APU INOP. PERFORMED APU CONTROL UNIT BITE TEST IAW AMM 49-61-05. FOUND SPEED SENSOR #1 & 2 FAULTED ON ECU PREVIOUS 3RD &AMP; 4TH STARTS. PER MCC PERFORMED OPS CHECK OF APU . OPS NORMAL. NO DEFECTS NOTED. COMPLIED WITH WDM 49-16-11, & CONTINUITY GOOD BOTH MONOPOLES WITH THE ECU. FOUND MONOPOLE 2 TO BE LOOSE. REMOVED AND REPLACED MONOPOLE 2 WITH NEW IAW AMM 49-61-02. PERFORMED ECU BITE PER AMM 49-61-05. NO FAULTS FOUND.

Part: PUMP — INOPERATIVE (FUEL BOOST) · airframe 90,289 hrs · 17,124 cycles

LH FWD FUEL BOOST PUMP INOP&NBSP;(<P>TRANSFERRED TO MDDR 110289.</P><P>LP 1061087 - PERFORMED TS IAW FIM 28-25 FT 807 AND RESET GFI RELAY K10701. PERFORMED OPS CHECK IAW AMM 28-22-03. ALL CHECKS NORMAL. THIS CLEARS MDDR 110289. PLACARD REMOVED AND MCC ADVISED.&NBSP;MCC RA @ 0300Z/16.</P>)

Part: APU — MALFUNCTIONED · airframe 90,284 hrs · 17,123 cycles

APU FAULT ON 1ST ATTEMPT AFTER LANDING. SUCCESSFUL START ON 2ND ATTEMPT. PERFORMED BITE TEST PER AMM 49-81-02. OPS CHECK GOOD PER AMM 49-11-00. NO DEFECTS NOTED AT THIS TIME

Part: WARNING MESSAGE — FALSE ACTIVATION (ENG ANTI-ICE) · airframe 90,177 hrs · 17,094 cycles

LEFT ENGINE ANTI ICE(<P>PERFORMED FIM 30-21 F.T. 806 ON LEFT ENG ANTI ICE. NO DEFECT NOTED AT THIS TIME. OPS CHECK NORMAL AT THIS TIME. CONTINUITY CHECKS CHECKED GOOD.</P>)

Part: OIL SYSTEM — LOW (APU) · airframe 90,167 hrs · 17,090 cycles

APU FAULT ON TAXI IN(<P>PERFORMED TEST OF APU ECU ONLY FAULT NOTED WAS LOW OIL IAS AMM 49-61-01 SERVICED OIL IAS AMM 12-13-04 NO FURTHER FAULT NOTED OK AT THIS TIME</P>)

Part: CONNECTOR — DIRTY (FUEL TRANSMITTER) · airframe 90,095 hrs · 17,067 cycles

LEFT ENGINE FUEL FLOW 300 - 400 PPH HIGHER THAN RIGHT, WITH NO FUEL IMBALANCE. &NBSP;(<P>PER FIM 73-31 FT 806, NO LEAKS NOTED. CLEANED CONNECTOR AT FF TRANSMITTER AND RAN ENGINE MIN IDLE, HAD 200 LBS SPLIT. OK TO CONTINUE SERVICE.&NBSP;</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 90,041 hrs · 17,048 cycles

DURING ENG START MOMENTARY OVERSPEED WARNING MSG(<DIV>PERFORMED FIM TASK 71-01-00 PIMU BITE CHECK NO FAULT FOUND AT THIS TIME. STARTED ENGINE MULTIPLE TIMES IAW 71-00-00, ALL ENGINE STARTS NORMAL AT THIS TIME.&NBSP;</DIV>)

Part: GUARD — DEFECTIVE (EMERGENCY LIGHTS) · airframe 90,014 hrs · 17,040 cycles

GUARD FOR EMERGENCY LIGHT SWITCH OVERHEAD P5 PANEL INOP&NBSP;&NBSP;(<P>TRANSFERRED TO MDDR 108362 AS PER DDG 25-20-01 NEF FLIGHT DECK (NEW NEF).&NBSP;&NBSP;</P><P>LP 1051442-M3: REMOVED AND REPLACED EMERGENCY LIGHTS GUARD SWITCH ASSEMBLY IAW AMM 33-51-08. THIS CLEARS MDDR 108362, STICKER REMOVED AND MCC NOTIFIED.&NBSP;</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 90,004 hrs · 17,037 cycles

INFO ONLY: "APU FAULT" EICAS MESSAGE. APU STARTED CORRECTLY ON THE SECOND ATTEMPT.&NBSP;(<P>PERFORMED OPS TEST OF APU, OPS CHECK OK IAW AMM 49-11-00.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (APU OIL) · airframe 89,929 hrs · 17,016 cycles

APU OIL LEVEL LOW. PERFORMED VISUAL INSPECTION OF APU OIL LEVEL . FOUND TO BE WITHIN OIL LEVEL SPECS IAW AMM 49-27-00, NO FURTHER DEFECTS NOTED.

Part: TEST SWITCH — DAMAGED (OXYGEN BOX) · airframe 89,868 hrs · 16,998 cycles

FIRST OBSERVER OXYGEN MASK STOWAGE BOX TEST SW DAMAGED.(<P>TRANSFER TO MDDR # 107395 IAW DDG 25-11-02-01A&NBSP;&NBSP;</P><P>LP 706777: R&AMP;R O2 BOX, LEAK CHECK OK. THIS CLEARS DMI 107395.&NBSP;</P><P><BR DATA-TEMP="1" /></P>)

Part: LAMP — INOPERATIVE (PRESSURE LIGHT) · airframe 89,800 hrs · 16,974 cycles

L FWD FUEL PUMP PRESSURE LIGHT&NBSP; INOP(<P>TRANSFER TO MDDR #107152 IAW DDG 28-42-01-01 CAT C DUE DATE 20-FEB-19 PLACARD INSTALLED.&NBSP;</P><P>LEFT FWD FUEL PUMP PRESS LIGHT RELAMPED IAW AMM 33-13-00 AS PER MX CONTROL. OPS CHECK GOOD. THIS ACTION CLEARS DMI #107152, TIME &AMP; INITIALS CW/1520<BR /></P>)

Part: INDICATOR — DEFECTIVE (E&E BAY) · airframe 89,747 hrs · 16,955 cycles

E&E COOLING LOW FLOW MONITOR IRU-C, IRU-L, AND E5, FLOW BALLS STUCK IN UP POSITION. REMOVED AND REPLACED E&E COOLING MONITOR INDICATOR. OPS TESTED OK PER AMM 21-58-00-715-244-008.

Part: INDICATOR — INOPERATIVE (FUEL SYSTEM) · airframe 89,747 hrs · 16,955 cycles

FUELING STA FUEL SELECT INDICATOR BACK LIGHT INOP. R&R FUELING & RIGHT & FUEL TANK LOAD SELECT INDICATOR IAW AMM 28-41-06. INDICATION TESTS GOOD.

Part: INDICATOR — INOPERATIVE (FUEL SYSTEM) · airframe 89,747 hrs · 16,955 cycles

FUELING STA LT FUEL SELECT INDICATOR, INDICATOR BACK LIGHT INOP. R&R FUELING STA LT FUEL SELECT/QTY INDICATOR. OPS CHECK OK PER AMM 28-41-06.

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 89,729 hrs · 16,946 cycles

AFTER LANDING, APU FAILED TO START FIRST ATTEMPT APU RPM 30% HANGING, THEN APU FAULT EICAS MSG , SUCCESSFUL START ON SECOND ATTEMPT&NBSP;(<P>PERFORMED BITE OF PAU ECU NO FAULTS NOTED , APU STARTED NORMALLY BITE IAW AMM 49-61-05</P>)

Part: INDICATOR — DEFECTIVE (OUTFLOW VALVE) · airframe 89,611 hrs · 16,902 cycles

OUTFLOW VALVE POSITION INDICATOR VARIES ERRACTICALLY . INDICATES FULLY CLOSED IN CRUISE(<DIV>RR CABIN PRESSURE INDICATOR IAW AMM 21-33-01. OPS CHECK IS NORMAL AT THIS TIME. NO DEFECTS NOTED&NBSP; &NBSP;PN 130502-7&NBSP; SN OFF 105-70416&NBSP; &NBSP;SN ON 113-372&NBSP;</DIV>)

Part: CONNECTOR — DISCONNECTED (OXYGEN MASK) · airframe 89,606 hrs · 16,900 cycles

FIRST OFFICERS OXYGEN MASK MICROPHONE DOES NOT TEST SUCCESSFULLY.(<P>FOUND MASK MIC FO SIDE CONNECTOR DISCONNECTED - RE-SECURED AS REQUIRED - OPS TEST GOOD IAW 35-11-51.<BR /></P>)

Part: CONTROL VALVE — MALFUNCTIONED (AC BAY) · airframe 89,566 hrs · 16,885 cycles

RT PACK TEMP EICAS MSG RAN QRH PROCEDURE WHICH PLACED PACK CONTROL SELECTOR TO STBY R PACK TEMP LIGHT EXTINGUISHED , CHECK LIST COMPLTED&NBSP;&NBSP;(<P>REMOVED AND REPLACED&NBSP;RT TEMP CONTROL VALVE IAW AMM REF 21-51-12 OPS CKS GOOD ON GROUND&NBSP;</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 89,581 hrs · 16,892 cycles

RT PACK TEMP EICAS MESSAGE. PERFORMED BITE CHECK OF THE RIGHT PACK TEMP CONTROL IAW FIM 21-51 FAULT TREE 844. BITE TEST NORMAL, OPS CHECK OF RIGHT PACK GOOD AT THIS TIME PER AMM 21-51-00.

Part: UNKNOWN — FAULT MESSAGE (APU) · airframe 89,562 hrs · 16,884 cycles

APU FAULT ON START UP AFTER LANDING STARTED SECOND ATTEMPT(<P>PERFORMED APU &AMP; &AMP; ECU BITE TEST IAW FIM 49-11 FT 987 &AMP; AMM 49-11-00 / 501 NO FAULT NOTED AT THIS TIME PERFORMED 03 NORMAL APU START TO TEST;&NBSP; OPS CHECK NORMAL.</P>)

Part: HEATER — MALFUNCTIONED (PITOT PROBE) · airframe 89,562 hrs · 16,884 cycles

EICAS PROBE HEAT AFTER ENGINE START(<P><SPAN>FOUND / PITOT HEAT C/B POPPED. RESET BREAKERS. SYSTEM OPS OK. (AMM 30-31-00)</SPAN></P>)

Part: CONNECTOR — DIRTY (RT PACK TEMP) · airframe 89,541 hrs · 16,878 cycles

RIGHT PACK TEMP EICAS CAUTION MSG, RAN QRH, MSG DISAPPEARED.&NBSP;(<P>FOUND TCV FAULT ON RT PACK CONTROLLER BITE , CLEANED AND RE-SECURED CANNON PLUG ON TCV, RIGHT PACK OPS TEST GOOD I.A.W AMM 21-51-00 FAULT CLEARED AND NO EICAS MSG DISPLAYED&NBSP;</P>)

Part: HOSE — DEFECTIVE (LT A/C PACK) · airframe 89,521 hrs · 16,871 cycles

LEFT PACK INOPERATIVE. REMOVED AND REPLACED DEFECTIVE HOSE FOUND IN L/H PACK BAY IAW B767 AMM 20-11-00 THIS CLEARS DMI 104991&NBSP;</P>)

Part: ENGINE — VIBRATION (LEFT) · airframe 89,498 hrs · 16,863 cycles

ENGINE CHANGE REQUIRED DUE TO HIGH VIBRATION&NBSP;(<P>REMOVED AND REPLACED LH ENGINE I.A.W AMM 71-00-00 OPS CHECK NORMAL, NO LEAKS NOTED&NBSP;</P>)

Part: UNKNOWN — VIBRATION (RT ENGINE) · airframe 89,497 hrs · 16,861 cycles

DURING TO AND CLIMB THE RIGHT ENG FAN VIB WAS AT 4.1-4.4 WITH A NOTICABLE AIRFRAME VIBRATION. DURING CRUISE VIB WENT DOWN TO 1.6. PERFORMED VISUAL INSPECTION OF RT ENGINE FAN BLADE, SPINNER AND TURBINE BLADES IAW FIM 71-05 FT 853. FIM C/W NO DEFECTS.

Part: UNKNOWN — VIBRATION (LT ENGINE) · airframe 89,492 hrs · 16,858 cycles

DURING CLIMB OUT THE LEFT FAN ENGINE VIBE WENT UP TO 4.3 ON THE SCALE ON THE LOWER EICAS, ONCE LEVEL AT 16000 WITH CRUISE THRUST THE FAN VIBE WAS 1.1. PERFORMED VISUAL INSPECTION OF THE LT ENG FAN BLADE, SPINNER AND TURBINE BLADES IAW FIM 71-05 FT 853, NO DEFECTS NOTED.

Part: ENGINE — VIBRATION (RIGHT) · airframe 89,497 hrs · 16,862 cycles

DURING CLIMB OUT RT ENGINE VIB 3.6 IN CRUISE 2.1 2.3. PERFORMED TRIM BALANCES PROCEDURRES IAW AMM 72-31-00 WITHIN SERVICEABLE LIMITS.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 89,490 hrs · 16,857 cycles

APU FAULT CAUTION MSG. PERFORMED BITE CHECK OF APU ECU IAW AMM 49-61-05, NO FAULTS FOUND. PERFORMED OPS CHECK OF APU 4 TIMES IAW AMM 49-11-00. OPS CHECK GOOD.

Part: ANTI-ICE VALVE — FAILED (RT ENGINE) · airframe 89,354 hrs · 16,811 cycles

RIGHT ENGINE ANTI ICE VALVE STATUS MESSAGE ON ARRIVAL(<P>REMOVED AND REPLACED RH ENGINE ANTI-ICE VALVE I.A.W AMM 30-21-03 OPS CHECK GOOD&NBSP;</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI-ICE VALVE) · airframe 89,341 hrs · 16,805 cycles

RIGHT ENGINE ANTI ICE VALVE STATUS MESSAGE ON ARRIVAL&NBSP;(<P>RIGHT ENGINE ANTI ICE VALVE STATUS MESSAGE ERASED IAW FIM 30-21 FT 805. PERFORMED ENGINE RUN OF RIGHT ENGINE IAW FIM 30-21 FT 805 BLOCK 2 WITH NO FAULT FOUND. SYSTEM OPS CHECK OK&NBSP;</P>)

Part: ANTI-ICE VALVE — MALFUNCTIONED (RT ENGINE) · airframe 89,346 hrs · 16,807 cycles

RIGHT ENGINE TAI VALVE STATUS MSG AFTER LANDING(<P>REMOVED AND REPLACED TAI IAW AMM 30-21-03 ALSO R&AMP;R #2 ENGINE PRESSURE SWITCH IAW 30-21-01 OPS CHECK GOOD&NBSP;</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI-ICE VAVLE) · airframe 89,346 hrs · 16,807 cycles

RIGHT ENGINE TAI VALVE STATUS MSG&NBSP;(<P>RIGHT ENGINE TAI VALVE EICAS MESSAGE ERASED PER FIM 30-21 FT 805 RAN ENG OPERATED RIGHT ENG TAI PRESS MAINTAINED 38 PSI WITH TAI ON OPS CKS OK PER FIM 30-21-FT 805&NBSP;</P>)

Part: ANTI-ICE VALVE — FAILED (RT ENGINE) · airframe 89,291 hrs · 16,789 cycles

AFTER SHUTDOWN RIGHT ENGINE ANTI ICE VALVE LIGHT ILLUMINATED ON OVERHEAD PANEL(<DIV>REMOVED AND REPLACED&NBSP; VALVE COWL ANTI ICE IAW AMM 30-21-00 OPS CHECK GOOD&NBSP;</DIV>)

Part: SENSOR — MALFUNCTIONED (APU SPEED) · airframe 89,556 hrs · 16,883 cycles

APU DID NOT START ON&NBSP; FIRST ATTEMPT&NBSP;(<P>PERFORMED BITE TEST OF APU AT ECU PREVIOUS START STOPPED ABORTED START FOR SPED SENSOR / # 2 SPEED SENSOR MEMORY CLEARED ECU BITE TEST NORMAL IAW FIM 49-11 FT 987 NORMAL&NBSP;2 OPERATIONAL TEST NORMAL IAW 49-11-00/501&NBSP;</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENGINE) · airframe 89,174 hrs · 16,750 cycles

LEFT ENGINE VALVE LIGHT AND LEFT VALVE EICAS MESSAGE ILLUMINATED. CYCLED THE CIRCUIT BREAKER IAW AMM 26-60-01. NO DEFECT NOTED. OPS CHECKED GOOD.

Part: CLAMP — MISSING (NR 1 ENGINE) · airframe 89,115 hrs · 16,730 cycles

ENGINE VIBE ON LEFT FAN EXCEEDED 4.0 DURING CLIMB. ACCOMPLISHED FIM 71-05 FT 852 - CREW REPORTED ENGINE VIBE WAS NORMAL AT CRUISE. FIM TASK NOTED B - LEVEL SHOULD BE CONSIDERED AT STABLE CONDITION. FOUND WIRE BUNDLE NR 1 ENG FAN ACCELEROMETER LOOSE AND MISSING CLAMP. REPLACED CLAMP IAW 20-11-00 ENG RUN NORMAL IAW 71-00-00.

Part: FILTER — CLOGGED (TEMP SENSOR) · airframe 89,102 hrs · 16,724 cycles

FLT DECK AUTO TEMP CONTROLLER ERRATIC AND UNABLE TO MAINTAIN TEMPERATURE. FOUND FLIGHT COMPARTMENT ZONE TEMP SENSOR FILTER CLOGGED. CLEANED FILTER AND OPS CHECK GOOD IAW AMM 21-61-08-004-003.

Part: CHIP DETECTOR — MISSING (APU) · airframe 89,098 hrs · 16,723 cycles

APU MAGNETIC CHIP DETECTOR MISSING. R&R MAGNETIC CHIP DETECTOR IAW AMM 49-27-04. OPS CHECK GOOD, NO DEFECTS NOTED AT THIS TIME.

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 89,098 hrs · 16,723 cycles

WHILE PARKED AT THE GATE AND CARGO LOADING, RECIEVED MASTER WARNING "MAIN CARGO FIRE LOOP 1 MESSAGE, ALERTED MX. WARNING CLEARED AFTER TWO MINUTES, NO INDICATION, VISUAL OR SMELL. PERFORMED FIRE TEST OF MD CARGO LOOP 1 AFTER CB RECYCLED, NO FAULTS FOUND, MESSAGE CLEARED, NO SMOKE OR FIRE DETECTED IN MD CARGO.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 89,077 hrs · 16,716 cycles

APU FAULT. PERFORMED BITE TEST PROCEDURE OF THE ECU & CLEARED MSG. RESET ECU PERFORMED OPERATIONS TEST OF APU FOUND NO FAULTS IAW AMM 49-61-05-201. OPS CKD GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 89,063 hrs · 16,711 cycles

APU FAULT ON COLD START ATTEMPT. PERFORMED ECU BITE IAW FIM 49-11FT 987, NO FAULT. APU OPS NORMAL.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 89,055 hrs · 16,708 cycles

APU FAULT ON COLD START ATTEMPT. PERFORMED ECU BITE IAW FIM 49-11 FT 987 NO FAULTS, APU OPERATION NORMAL.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 89,039 hrs · 16,702 cycles

APU FAULT TWICE ON TAXI IN STARTED AND STAYED RUNNING ON THIRD ATTEMPT. PERFORMED BITE CHECK NO CURRENT FAULTS NOTED REF AMM 49-11-00, OPS NORMAL.

Part: NOT REPORTED — MALFUNCTIONED (WEATHER RADAR) · airframe 89,033 hrs · 16,700 cycles

WX RADAR PAINTS GROUND AT ANY SELECTED TILT ANGLE INCLUDING 15 DEGREES UP. TI DOES THIS IN EITHER LT OR RT SYS. OPENED RADOME AND VERIFIED UP & DOWN TILT OPERATES NORMAL. BOTH CAPT & FO WX RADAR DISPLAY CHANGES & PAINTS DIFFERENT IMAGES NOT THE GROUND. REF AMM 34-43-00-115-026-002 & REF AMM 34-43-00-735-033-002. ALL OPS CHECKS OF WX RADAR SYSTEM NORMAL.

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 89,007 hrs · 16,690 cycles

RADAR AUTO TILT FUNCTION PAINTS AT ALL PHASES OF FLIGHT WITH NO ACTUAL WEATHER. PERFORMED A SYSTEM TEST ON THE WEATHER RADAR SYSTEM IAW AMM 34-53-00-735-033-002. NO DEFECTS NOTED AT THIS TIME. OPS TEST GOOD.

Part: SENSOR — MALFUNCTIONED (FUEL FILL VALVE) · airframe 89,124 hrs · 16,734 cycles

WHILE PERFORMING AN OPS CHECK OF THE OVERFILL RESET SWITCH, FOUND THE SWITCH HAD TO BE HELD IN ORDER TO OPEN THE FUEL FILL VALVES. REMOVED AND REPLACED THE RT FUEL LEVEL SENSOR IAW AMM 28-21-03, OPS CHECKED GOOD.

Part: SWITCH — BINDING (COCKPIT) · airframe 89,124 hrs · 16,734 cycles

RIGHT FUEL PUMP SWITCH STUCK IN THE OVERHEAD PANEL. R & R THE FUEL PUMP SWITCH. OPS CHECKED NORMAL IAW AMM 28-22-00.

Part: SWITCH — MALFUNCTIONED (FUELING PANEL) · airframe 89,124 hrs · 16,734 cycles

RESET SWITCH BROKEN ON THE REFUELING PANEL. R & R OVER FILL RESET SWITCH. OPS CHECKED NORMAL IAW AMM 28-21-13.

Part: LAMP — INOPERATIVE (PUMP SWITCH) · airframe 89,124 hrs · 16,734 cycles

RIGHT AFT FUEL PUMP SWITCH PRESS LIGHT INOPERATIVE. REPLACED THE LAMP. OPS CHECKED NORMAL IAW AMM 33-13-00.

Part: CONTROL PANEL — DEFECTIVE (COCKPIT) · airframe 88,943 hrs · 16,666 cycles

LEFT WING ANTI ICE VALVE WILL NOT OPEN WITH WING A/I SELECTOR IN ON POSITION. REMOVED AND REPLACED WING /ENGINE ANTI-ICE PANEL IAW AMM 30-11-01. OPS CHECK GOOD IAW AMM 30-81-00.

Part: OIL SYSTEM — LOW (APU) · airframe 88,943 hrs · 16,666 cycles

APU FAULT EICAS MESSAGE. APU WOULD NOT START ON GROUND AFTER LANDING, 2 ATTEMPTS MADE. UPON INSPECTION FOUND APU OIL QTY MESSAGE ON EICAS. SERVICED APU OIL IAW AMM 12-13-04. OPS CHECK GOOD IAW AMM 49-11-00.

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 88,923 hrs · 16,659 cycles

WX RADAR AUTO TILT GOES TO AND REMAINS AT -1 IN BOTH LEFT AND RT SYSTEM. PERFORMED FIM 34-43 F/T 805 LEFT AND RIGHT SYSTEM TEST OK, NO DEFECTS NOTED.

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 88,943 hrs · 16,666 cycles

REPEAT WRITEUP, AUTOTILT ON RADAR UNUSABLE. RADAR PAINTS GROUND AT FL370. AUTOTILT IS -1 TOO LOW. WHEN ON APPROACH AND IN MANUAL TILT +15° RADAR RETURNS MAGENTA. OPS CHECK GOOD IAW AMM 34-43-00. NO DEFECTS NOTED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,886 hrs · 16,645 cycles

APU BATT CHARGE STATUS MESSAGE. MX PROCEDURE C/W. PERFORMED SYSTEM OPERATIONAL TEST OK IAW AMM 49-11-00.

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 88,881 hrs · 16,644 cycles

RADAR AUTO TILT PAINTS RADAR TOO LOW, PAINTING THE GROUND MID-SCREEN. PERFORMED FIM 34-43 FAULT TREE 811 & 812. OPS CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 88,849 hrs · 16,630 cycles

UNABLE TO START APU EICAS "APU FAULT". SUSPECTED BAD STARTER MOTOR ON APU DUE TO RATTLING SOUND COMING FROM APU STARTER. R&R APU STARTER IAW AMM 49-41-01. NO HELP, APU STILL AUTO SHUTDOWNS DURING START.

Part: TRU — FAULTY (APU) · airframe 88,830 hrs · 16,623 cycles

UNABLE TO START APU EICAS APU FAULT. REMOVED AND REPLACED APU TRU IAW AMM 24-32-04 OPS CHECK GOOD.

Part: CONTROL VALVE — FAULTY (AC BAY) · airframe 88,761 hrs · 16,599 cycles

LT PACK TEMP EICAS. R&R ACM TEMP CONTROL VALVE IAW AMM 21-51-12. UNCOLLARED AND RESET C/B'S - P-11, PNL,B-2, N-10,00-24. OPS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,724 hrs · 16,584 cycles

AFTER LANDING, RIGHT FWD WINDOW EICAS MSG COMPLIED WITH QRH. MSG CLEARED. OPS CHECK IAW AMM 30-41-00. NO DEFECTS NOTED AT THIS TIME.

Part: CONNECTOR — LOOSE (WINDOW HEAT) · airframe 88,713 hrs · 16,581 cycles

REPEAT WRITE UP (04TH TIME) REFERENCE AIRCRAFT LOG DATES 22AUG18, 25AUG18, 25AUG18, EICAS MSG RT FWD WINDOW. PERFORMED INSPECTION OF WINDOW HEAT WIRING, FOUND LOOSE CONNECTIONS AT CB C392 WITH CARBON BUILDUP. CLEANED AND TIGHTENED CONNECTION ALL WORK PERFORMED IAW FIM 30-41-FT 803. OPS CHECK NORMAL.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,705 hrs · 16,577 cycles

AFTER LANDING RIGHT FWD WINDOW EICAS MESSAGE. PERFORMED OPS CHECK IAW AMM 30-41-00. NO FAULT NOTED AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,703 hrs · 16,576 cycles

AFTER LANDING RECEIVED RIGHT FWD WINDOW ADVISORY MSG, COMPLIED WITH QRH, MSG CLEARED. OPS CHECK IAW AMM 30-40-01, NO DEFECTS NOTED AT THIS TIME.

Part: APU — SHUTDOWN (APU BAY) · airframe 88,693 hrs · 16,572 cycles

APU FAULT FIRST ATTEMPT AUTO SHUTDOWN, SECOND ATTEMPT SUCCESSFUL. PERFORMED APU BITE CHECK IAW FIM 49-11 FT 988, PERFORMED OPERATIONALTEST IAW AMM 49-11-00, OPS NORMAL.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,674 hrs · 16,566 cycles

RIGHT FORWARD WINDOW EICAS ON TAXI IN. PERFORMED WINDOW HEAT OPS CHECK IAW AMM 30-41-00, NO FAULTS NOTED AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,703 hrs · 16,576 cycles

APU FAULT ON FIRST START, SECOND ATTEMPT SUCCESSFUL. PERFORMED APU STARTING AND OPERATION PROCEDURE, NO DEFECTS NOTED AT THIS TIME PER AMM 49-11-00-802-002.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,657 hrs · 16,561 cycles

RT FWD WINDOW HEAT. ACCOMPLISHED OPS CK OF WINDOW HEAT SYSTEM IAW 30-11-00, OPS CK GD, NO DEFECTS NOTED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,641 hrs · 16,557 cycles

RIGHT FWD WINDOW EICAS MESSAGE RECEIVED AFTER LANDING. PERFORMED OPS CHECK OF FLIGHT COMPARTMENT WINDOW ANTI ICING SYSTEM GOOD IAW AMM 30-41-00, NO DEFECT NOTED AT THIS TIME.

Part: SWITCH — MALFUNCTIONED (WINDOW HEAT) · airframe 88,639 hrs · 16,556 cycles

RT FWD WINDOW HEAT EICAS AFTER LANDING. RESET R FWD WINDOW SWITCH IAW AMM 30-41-00 OPS CHECKS GOOD ON GROUND.

Part: SWITCH — MALFUNCTIONED (WINDOW HEAT) · airframe 88,645 hrs · 16,558 cycles

RT FWD WINDOW HEAT EICAS AFTER LANDING. RESET R FWD WINDOW SWITCH IAW 30-41-00/501. OPS CHECK GOOD, NO EICAS MESSAGE.

Part: SWITCH — MALFUNCTIONED (WINDOW HEAT) · airframe 88,630 hrs · 16,553 cycles

RT FWD WINDOW HEAT EICAS AFTER LANDING. RESET RFWD WINDOW SWITCH IAW AMM 30-41-00. OPS CHECK GOOD, NO EICAS MSG.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,591 hrs · 16,538 cycles

RT FWD WINDOW EICAS MESSAGE ON AFTER LANDING REPEAT WRITE UP. PERFORMED OP/BITE TEST IAW AMM 30-44-00, TEST PASSED. OPS GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,586 hrs · 16,537 cycles

RT FWD WINDSHIELD EICAS MSG WITH RT FWD W/S HEAT INOP LIGHT. PERFORMED BIT TEST OF WINDOW HEAT CONTROLLER IAW AMM 30-41-00, NO FAULTS NOTED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,586 hrs · 16,537 cycles

ON LANDING RT FWD WINDOW HEAT MSG AND INOP LIGHT ILLUMINATED. PERFORMED OPS /BIT TEST IAW AMM 30-41-00. NO FAULTS, OPS GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,553 hrs · 16,524 cycles

RIGHT FWD WINDOW EICAS. PERFORMED BITE TEST IAW 34-41-00, NO FAULTS FOUND OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,557 hrs · 16,525 cycles

RIGHT FWD WINDOW EICAS MSG ON TOUCHDOWN. ACCOMPLISHED FIM 30-41 TASK 802 STEP A, NO DEFECTS FOUND OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,549 hrs · 16,523 cycles

RT FORWARD WINDOW HEAT EICAS AFTER LANDING. PERFORMED BITE TEST IAW 30-41-00, NO FAULTS FOUND OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,553 hrs · 16,524 cycles

RT FWD WINDOW EICAS MSG. PERFORMED RT FWD WINDOW ANTI-ICE OPERATIONAL TEST IAW AMM 30-41-00. OPS CHECK GOOD, MESSAGE ERASED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,534 hrs · 16,517 cycles

RT FWD WINDOW EICAS MSG. PERFORMED RT FWD WINDOW ANTI-ICE OPERATIONAL TEST IAW 30-41-00. OPS CHECK GOOD. MESSAGE ERASED.

Part: CONTROL UNIT — FAULTY (COCKPIT) · airframe 88,517 hrs · 16,509 cycles

RIGHT FWD WINDOW HEAT MESSAGE DISPLAY. FOUND WIRING TO BE ROUTED INCORRECTLY AROUND R1 WINDOW, PERFORMED CHECK OF WIRE ROUTING ALL THE WAY RT WINDOW WINDOW HEAT CONTROL UNIT IAW WPM 30-41-12. FOUND LOOSE AND CONTAMINATED CONNECTOR D4294P CLEANED AND RE-SECURED IAW SWPM 20-60-02. PERFORMED TORQUE OF SENSOR BOLTS PER MCC REQUEST REF AMM 51-11-01 BOLTS WERE CORRECTLY INSTALLED AND TORQUED. FOUND POWER DELIVERY FROM WINDOW HEAT CONTROL UNIT TO THE R1 WINDOW HEAT SENSOR TO BE UNDER SPEC FROM D2898A PINS 19 AND 20 TO D1912 CONTACTS. REMOVED AND REPLACED WINDOW HEAT CONTROL UNIT IAW AMM 30-41-01. OPS CHECK GOOD. VOLTAGE CHECK AND RESISTANCE. CHECKS GOOD PER FIM 30-41 F/T 802 NO FURTHER DEFECTS NOTED.

Part: NOT REPORTED — MALFUNCTIONED (WINDOW HEAT) · airframe 88,517 hrs · 16,509 cycles

RIGHT FWD WINDOW. PERFORMED WINDOW HEAT BITE TEST AS PER AMM 30-41-00. NO FAULTS NOTED AT THIS TIME.

Part: CONTROLLER — FAULTY (BLEED AIR SYS) · airframe 88,512 hrs · 16,506 cycles

STATUS PAGE RT ENG HPSOV. RT ENG HPC FAULT ON AIR SUPPLY BITE MODULE. REMOVED AND REPLACED RT ENGINE HP CONTROLLER IAW AMM 36-11-08. LEAK AND OPS CHECK OK.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,679 hrs · 16,567 cycles

RT FWD WINDOW EICAS MSG ON TAXI IN. PERFORMED WINDOW HEAT OPS CHECK IAW AMM 30-41-00, NO FAULTS NOTED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,508 hrs · 16,505 cycles

RT FWD WINDOW EICAS MSG ON LANDING. PERFORMED OPS FOR WINDOW HEAT IAW AMM 30-41-00. OPS GOOD AT THIS TIME.

Part: CLAMP — NOT SEATED (BLEED AIR SYS) · airframe 88,496 hrs · 16,501 cycles

PNEUMATIC CLAMP NOT SEATED PROPERLY. RE-SEATED CLAMP, FUNCTION CHECK PASSED.

Part: IGNITION LEAD — CUT (NR 1 ENGINE) · airframe 88,496 hrs · 16,501 cycles

NR 1 ENGINE INBD SIDE (BRACKET) CUT THROUGH UPPER IGNITER LEAD. REMOVED AND REPLACED LEAD, OPS CHECK GOOD.

Part: SHUTOFF VALVE — FAULTY (BLEED AIR SYS) · airframe 88,491 hrs · 16,498 cycles

RT ENG HPSOV STATUS. DEFERRED RT ENG HPSOV IAW DDG 36-11-02-02, REF M5 FOR TR DEACTIVATION REQUIRED BY DDG 36-11-02-02.

Part: UNKNOWN — MALFUNCTIONED (WINDOW HEAT) · airframe 88,491 hrs · 16,498 cycles

RT FWD WINDOW HEAT. PERFORMED OPS CHECK OF WINDOW HEAT/FLT. COMPARTMENT ANTI-ICE SYSTEM IAW AMM 30-41-00-715-001. OPS CHECK GOOD AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,482 hrs · 16,495 cycles

RT FWD WINDOW EICAS AFTER LANDING. PERFORMED FLIGHT COMPARTMENT WINDOW ANTI-ICE SYSTEM OPERATIONAL TEST, OPS CHECK GOOD PER AMM 30-41-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,482 hrs · 16,495 cycles

RT FWD WINDOW EICAS AFTER LANDING REPEAT WRITE UP. PERFORMED FLIGHT COMPARTMENT WINDOW ANTI-ICE SYSTEM OPERATIONAL TEST, OPS CHECK GOOD AS PER AMM 30-41-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,468 hrs · 16,490 cycles

RT FWD WINDOW EICAS DURING TAXI AFTER LANDING. PERFORMED FLIGHT COMPARTMENT WINDOW ANTI-ICE SYSTEM OPERATIONAL TEST, OPS CHECK GOOD PER AMM 30-41-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,481 hrs · 16,494 cycles

REPEAT WRITE UP - RT FWD WINDOW HEAT EICAS MESSAGE. PERFORMED OPS CHECK IAW AMM 30-41-00 OPS CHECK GOOD NO DEFECTS NOTED, CHECK MAIN PINS FOR SPARES FA195, FC 192 CHECKED GOOD, CHECK WIRE CONNECTORS D2898A, AFT PIN 19 WIRE CHECK GOOD, CHECKED WIRE D2998B PIN 5 CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,459 hrs · 16,486 cycles

ON LANDING RIGHT FWD WINDOW EICAS. PERFORMED FLIGHT COMPARTMENT OPS TEST. OPS CHECK GOOD PER AMM 30-41-00-715-001.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,463 hrs · 16,488 cycles

RT FWD WINDOW HEAT EICAS MESSAGE CAME ON AFTER LANDING. COULD NOT DUPLICATE AT THIS TIME. INTERCHANGED LEFT AND RIGHT WINDOW HEAT CONTROLLERS REF AMM 30-41-01, BOTH SYSTEMS CHECK NORMAL AT THIS TIME. P/N OFF 624066-5, S/N OFF 030C-4104 POS RT.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,453 hrs · 16,483 cycles

TR FWD WINDOW HEAT EICAS ON LANDING. PERFORMED FLIGHT COMPARTMENT WINDOW ANTI-ICING SYSTEM OPERATIONAL TEST, OPS CHECKED GOOD PER AMM 30-41-00-715.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,459 hrs · 16,486 cycles

RIGHT FWD WINDOW EICAS ON TAXI IN. PERFORMED FLIGHT COMPARTMENT WINDOW ANTI ICING SYSTEM OPERATIONAL TEST, OPS CHECK GOOD PER AMM 30-41-00-715-001.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,455 hrs · 16,484 cycles

RT FWD WDW EICAS MESSAGE ON TAXI IN. CHECKED WIRE 713-24 AS PER WIRING DIAGRAM 30-41-12. OPS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,455 hrs · 16,484 cycles

RT ENG HPSOV STATUS MESSAGE UPON SHUTDOWN. INSPECTED,TORQUE AND PERFORMED. OPS TEST OF HPSOV IAW AMM 36-11-07, MSG CLEARED NO FURTHER FAULTS NOTED AT THIS TIME. OPS TEST SATISFACTORY.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,448 hrs · 16,482 cycles

RT FWD WINDOW MSG AFTER LANDING MULTIPLE REPEAT WRITE UP. PERFORMED BITE PROCEDURES FOR RT FWD WINDOW HEAT IAW FIM 30-41 FT 804. NO DEFECTS NOTED, OPS CHECK GOOD AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,440 hrs · 16,479 cycles

AFTER LANDING RECEIVED EICAS RT FWD WINDOW. PERFORMED BITE PROCEDURE FOR RT FWD WINDOW HEAT AS PER FIM 30-41 FT 804. NO DEFECTS NOTED AT THIS TIME.

Part: WIRE — NOT SEATED (COCKPIT) · airframe 88,437 hrs · 16,478 cycles

RT FWD WINDOW EICAS AFTER LANDING. PERFORMED BITE CHECK ON WINDOW HEAT CONTROLLER IAW AMM 30-41-00. CLEANED & RESEATED WINDOW HEAT WIRING AS PER AMM 56-11-01, OPS CHECK OK.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,418 hrs · 16,472 cycles

RT FWD WINDOW EICAS MESSAGE CAME ON DURING DESCENT. PERFORMED BITE PROCEDURE FOR RT FWD WINDOW HEAT MSG IAW FIM 30-41 FT 803, NO MESSAGE DISPLAYED AT THIS TIME, OPS CHECK GOOD AT THIS TIME.

Part: CIRCUIT CARD — LOOSE (FIRE WARNING) · airframe 88,418 hrs · 16,472 cycles

MAIN CARGO FIRE WARNING MESSAGE CAME ON AFTER LANDING. PERFORMED FIM TASK 26-14 FT 809, FOUND LOOSE AFOLTS CARD AT P54 PANEL, RE-RACKED CARD, PERFORMED BITE TEST OPS CHECK GOOD AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,412 hrs · 16,469 cycles

RIGHT FWD WINSHIELD EICAS MSG AFTER LANDING. RECYCLE SWITCH PER QRH. PERFORMED FIM TASK 30-31-FAULT TREE 804, NO FAULT FOUND THIS TIME OPS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,408 hrs · 16,467 cycles

RT FWD WINDOW HEAT EICAS ON TAXI. PERFORMED FIM TASK 30-31 FT 804 NO FAULTS NOTED AT THIS TIME, CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,413 hrs · 16,470 cycles

EICAS MSG "R FWD WINDOW" DISPLAYED AFTER LANDING. PERFORMED WINDOW HEAT BIT / VERIFY OPS CHECK IAW AMM 30-41-00, OPS CKD GOOD.

Part: CONNECTOR — DIRTY (AC BAY) · airframe 88,407 hrs · 16,466 cycles

LEFT PACK INOP IN AUTO. PERFORMED BITE TEST, FOUND COMPRESSOR SENSOR FAULTY. CLEANED AND SECURED CONNECTORS PER SP 20-60-00. PERFORMED TEST IAW AMM 21-51-03.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,407 hrs · 16,466 cycles

APU FAULT AFTER SUCCESSFUL START UPON LANDING. T/S APU START NO FAULTS, T/S APU ECU BITE CODES 34 & 23 DISPLAYS SHUT DOWN 2 & 3 STARTS ABORTED FROM "A/C STRT CIRCUIT" LRU. SUMMARY CALLS OUT "ECS CTRL" & "A/C STRT CIRUIT" 1529 UTC PERFORMED FIM 49-11 FT 987. NO FAULTS NOTED AT THIS TIME. APU OPS CHECK GOOD.

Part: TERMINAL BLOCK — DEFECTIVE (COCKPIT) · airframe 88,407 hrs · 16,466 cycles

TROUBLESHOOT DUE TO HISTORY OF R1 WINDOW FAULTS. REMOVED AND REPLACED TERMINAL BLOCKS 324-1+2, REMOVED AND REPLACED PINS AT TB 324 FOR WIRES W624-204, W624-205, AND 216 DUE TO CORROSION, WORK PERFORMED IAW SWPM CHP 20, OPS CHECK GOOD IAW AMM 30-41-00 PER 124.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,390 hrs · 16,461 cycles

RT FWD WINDOW EICAS MESSAGE. PERFORMED BITE TEST OF WINDOW HEAT LRU FOR R1 WINDSHIELD IAW AMM 30-41-00 AND FOLLOWED FIM 30-41 F/T 806 NO DEFECTS NOTED AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,385 hrs · 16,458 cycles

R FWD WINDOW HEAT EICAS MESSAGE ON LANDING. PERFORMED BITE CHECK ON RIGHT WINDOW PER FIM TASK 30-41, OPS CHECK GOOD AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,388 hrs · 16,459 cycles

AFTER LANDING RH FWD WINDOW HEAT EICAS AND INOP LIGHT. RAN QRH AND RESET. RECURRING ITEM. PERFORMED BITE CHECK NO FAULTS FOUND. OK FOR SERVICE IAW AMM 30-41-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,385 hrs · 16,457 cycles

RIGHT FWD WINDOW EICAS MSG AFTER LANDING. PERFORMED WINDOW HEAT BITE TEST IAW AMM 30-41-00. NO FAULTS FOUND AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,377 hrs · 16,455 cycles

REPEAT WRITE UP, EICAS MESSAGE R FWD WINDOW ON LANDING. REFERENCE LOG PAGES: 985051, 985056, 985058, 985061, 985062, 985065, 985074, 985078. PERFORMED WINDOW HEAT BITE TEST IAW AMM 34-41-00. NO FAULTS FOUND AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,360 hrs · 16,450 cycles

"APU FAULT" EICAS WHEN STARTING APU AFTER LANDING. PERFORMED APU OPERATIONAL CHECK IAW AMM 49-11-00. NO DEFECTS FOUND AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,360 hrs · 16,450 cycles

AFTER LANDING "R FWD WINDOW" EICAS. PERFORMED BITE TEST ON WINDOW HEAT CONTROLLER IAW AMM 30-41-00. NO FAULTS FOUND. EICAS "R FWD WINDOW" MESSAGE NOT FOUND.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,340 hrs · 16,444 cycles

RT FWD WINDOW EICAS MESSAGE AFTER LANDING INOP LIGHT ILLUMINATED - REPEAT WRITE-UP. PERFORMED BITE TEST ON WINDOW CONTROLLER NO DEFECTS NOTED IAW AMM - 30-41-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,338 hrs · 16,443 cycles

REPEAT AFTER LANDING "R FWD WINDOW" INOP LIGHT ILLUMINATED. PERFORMED BITE TEST AND OPS CHECK FOUND NO DEFECTS ON HEAT CONTROL IAW AMM 30-41-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,338 hrs · 16,443 cycles

RIGHT FWD EICAS WINDOW MESSAGE. PERFORMED OPERATION TEST AT FLIGHT DECK WINDOW A/I NO DEFECTS NOTED. WINDOW HEAT OPERATION NORMAL AMM 30-41-00.

Part: ANTI-ICE SYSTEM — MALFUNCTIONED (WINDOW HEAT) · airframe 88,338 hrs · 16,443 cycles

AFTER LANDING RECEIVED EICAS "R FWD WINDOW". RESET RT WINDOW HEAT PREFORMED BITE CHECK ON HEAT CONTROLLER NO DEFECT NOTED IAW AMM 30-41-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,323 hrs · 16,437 cycles

R FWD WINDOW EICAS AFTER LANDING. PERFORMED GROUND TEST OF THE WINDOW SYSTEM, NO DEFECTS NOTED. NO EICAS MSG SHOWING IAW AMM 30-41-00. ACFT OK FOR SERVICES.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,321 hrs · 16,436 cycles

R FWD WINDOW EICAS MESSAGE AFTER LANDING. PERFORMED OPS CHECK OF WINDOW HEAT SYSTEM IAW AMM 30-41-00. NO FAULTS NOTED AT THIS TIME.

Part: FIRE WARNING — FALSE ACTIVATION (MAIN DECK) · airframe 88,307 hrs · 16,428 cycles

DURING LOADING, RECEIVED MULTIPLE MAIN DECK FIRE ALERTS WITH NO EVIDENCE OF ACTUAL FIRE. ACCOMPLISHED FIM 26-14 FT 809, NO FAULTS FOUND, NO EICAS MESSAGES SHOWING , AIRCRAFT OK FOR SERVICE.

Part: UNKNOWN — MALFUNCTIONED (WINDOW HEAT) · airframe 88,317 hrs · 16,433 cycles

RT FWD WINDOW HEAT INOP. PERFORMED WINDOW HEAT CONTROL UNIT BITE TEST AND OPS TEST GOOD IAW AMM 30-41-00. CHECKED POWER AT THE TERMINALS OF THE WINDOW FOUND 115V. R1 WINDOW WORKS GOOD AT THIS TIME.

Part: HEATER — MALFUNCTIONED (RT WINDOW) · airframe 88,307 hrs · 16,428 cycles

RIGHT FWD WINDOW HEAT BECAME INOPERATIVE ON LANDING. PERFORMED A GROUND TEST OF THE WINDOW HEAT SYSTEM, NO DEFECTS NOTED , NO EICAS MESSAGE SHOWING IAW AMM 30-41-00, ACFT OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT WINDOW) · airframe 88,296 hrs · 16,422 cycles

RIGHT FWD WINDOW EICAS MESSAGE ON LANDING, DID NOT RESET. OPS CHECKED IAW AMM 30-41-00. NO DEFECTS NOTED. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (WINDOW HEAT) · airframe 88,296 hrs · 16,422 cycles

RIGHT FWD WINDOW HEAT EICAS DURING TAXI IN. PERFORMED A BITE TEST. NO FAULTS FOUND. PERFORMED AN OPS CHECK IAW AMM 30-41-00, OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (WINDOW HEAT) · airframe 88,290 hrs · 16,418 cycles

RIGHT FWD WINDOW EICAS MESSAGE AFTER TOUCHDOWN. PERFORMED AN OPS TEST OF COCKPIT WINDOW ANTI-ICING SYSTEM IAW AMM 30-41-00, OPS CHECKED GOOD , NO DEFECTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (WINDOW HEAT) · airframe 88,290 hrs · 16,418 cycles

RIGHT FWD WINDOW EICAS MESSAGE AFTER LANDING. CREW ALREADY HAD SWITCHED TO THE OFF POSITION, RESET THE WINDOW HEAT PUSH BUTTON, PERFORMED A BITE TEST IAW FIM 30-41 F/T 804, OPS CHECKED NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (WINDOW HEAT) · airframe 88,284 hrs · 16,416 cycles

RIGHT FWD WINDOW HEAT INOPERATIVE DURING TAXI IN. COMPLIED WITH FIM 30-41 FT 804, NO FAULTS FOUND , OPS NORMAL.

Part: WARNING MESSAGE — FALSE INDICATION (WINDOW HEAT) · airframe 88,272 hrs · 16,410 cycles

RIGHT FWD WINDOW HEAT INOPERATIVE. PERFORMED AN OPS CHECK OF THE RT FWD WINDOW HEAT SYSTEM IAW 30-41-00. NO FAULTS.

Part: HEATER — MALFUNCTIONED (RT WINDOW) · airframe 88,265 hrs · 16,407 cycles

RIGHT FWD WINDOW HEAT INOPERATIVE. INSPECTED RH BTB C904, TB102 ON P61 AND TB324 ON E & E, NO DEFECTS NOTED. , PERFORMED AN OPERATIONAL CHECK IAW AMM 30-41-00, NO FAULTS NOTED.

Part: WINDOW — NOT REPORTED (RIGHT FWD) · airframe 88,269 hrs · 16,408 cycles

RIGHT FWD WINDOW COMPLIED WITH IAW FIM 30-41. BITE CHECK LRU. NO FAULTS FOUND AT THIS TIME. OPS CHECKED GOOD IAWAMM 30-41-00.

Part: HEATER — INOPERATIVE (WINDOW) · airframe 88,269 hrs · 16,408 cycles

RIGHT FWD WINDOW HEAT INOPERATIVE. INSPECTED THE RT BUSS TIE CIRCUIT BREAKER C904, TB102 AND TB 304. ALL CHECKED GOOD IAW AMM 36-41-00

Part: WARNING MESSAGE — FALSE ACTIVATION (WINDOW) · airframe 88,269 hrs · 16,408 cycles

RIGHT FWD WINDOW EICAS DURING TAXI IN. PERFORMED AN OPS CHECK . CHECKED GOOD IAWAMM 30-61-00</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,256 hrs · 16,403 cycles

ON TOUCHDOWN, R FWD WINDOW EICAS MESSAGE. REMOVED R1 WINDOW HEAT CONTROLLER. INSPECTED CONNECTOR NO FAULTS NOTED. REINSTALLED WINDOW HEAT CONTROLLER IAW AMM 30-41-01. PERFORMED FIM BITE TEST IAW AMM 30-41-00 NO FAULT NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT WINDOW) · airframe 88,256 hrs · 16,403 cycles

RIGHT FWD WINDOW EICAS AT TOUCHDOWN. PERFORMED A BITE TEST CHECK RESET, RT FWD WINDOW HEAT OPS CHECKED GOOD IAW AMM 30-41-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (COCKPIT WINDOW) · airframe 88,257 hrs · 16,404 cycles

RIGHT FWD WINDOW EICAS AFTER LANDING. COMPLIED WITH FIM 30-41 BITE CHECK , NO FAULTS, CHECKED GOOD IAW AMM 30-41-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT WINDOW) · airframe 88,250 hrs · 16,400 cycles

RIGHT FORWARD WINDOW HEAT WARNING AFTER LANDING. COMPLIED WITH FIM 30-41, WINDOW ANTI ICE BITE PROCEDURE. FOUND NO DEFECTS AT THIS TIME.

Part: TERMINAL — LOOSE (WINDOW HEAT) · airframe 88,256 hrs · 16,403 cycles

EICAS CAUTION RT FWD WINDOW ON LANDING. RESET THE WINDOW HEAT. PERFORMED FIM 30-41-803. BITE CHECK FOR THE CONTROLLER. NO FAULTS FOUND. CHECKED OK. TIGHTENED THE CONNECTIONS ON TERMINAL END WIRES IAW AMM 56-11-01. PERFORMED AN OPS TEST IAW AMM 30-41-00. TESTED GOOD.

Part: HEATER — MALFUNCTIONED (RT WINDSHIELD) · airframe 88,250 hrs · 16,400 cycles

RIGHT FWD WINDSHIELD HEAT CYCLED OFF BEFORE TAKEOFF AND AFTER LANDING. PERFORMED A WINDOW HEAT OPS CHECK IAW AMM 30-41-00 FOR 15 MINUTES , NO DEFECTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (WINDOW HEAT) · airframe 88,224 hrs · 16,392 cycles

WHILE APU WAS STARTING, THE RT FED WINDOW HEAT CAUTION MESSAGE APPEARED. COMPLIED WITH FIM 30-41 FAULT TREE 804, NO FAULTS FOUND, OPS NORMAL.

Part: GENERATOR — MALFUNCTIONED (RIGHT) · airframe 88,227 hrs · 16,393 cycles

DESENDING THROUGH 18000 FEET, LOST RIGHT GENERATOR, RAN QRH FOR RT AC BUSS OFF, RESET GEN & ISOLATION BUSS TIE, NO ANOMOLIES AFTER RESET. SERVICED THE RT IDG IAW AMM 12-13-03 , PERFORMED BPCU BITE PROCEDURE, NO FAULTS NOTED IAW FIM 24-20 FT 801 IAW MX OPERATED NR 2 ENGINE, VERIFIED PROPER OPERATION OF IDG AT IDLE ENGINE RUN IAW AMM 71-00-00, OPS CHECKED OK.

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 88,184 hrs · 16,377 cycles

MAIN DECK CARGO FIRE LIGHT REPEATEDLY COMES ON DURING PREFLIGHT. PERFORMED BITE PROCEDURE FOR THE CARGO COMPARTMENT SMOKE DETECTION SYSTEM, NO FAULTS NOTED, NO WARNING MESSAGES NOTED AS PER FIM 26-14 FT 809.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,180 hrs · 16,376 cycles

RIGHT FDW WINDOW EICAS MSG. OPS CHECK GOOD IAW AMM 30-41-00, NO DEFECTS AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION (WINDOW HEAT) · airframe 88,157 hrs · 16,365 cycles

RIGHT FORWARD WINDOW HEAT INOPERATIVE 25 SECONDS AFTER TOUCHDOWN. PERFORMED AN OPS CHECK OF THE R1 WINDOW HEAT IAW AMM 30-41-00, NO FAULTS FOUND.

Part: PUMP — UNKNOWN (FUEL BOOST) · airframe 88,159 hrs · 16,366 cycles

LEFT AFT BOOST PUMP INOPERATIVE. TROUBLESHOT IAW FIM 28-22 TREE 819. CHECKED WIRING IAW FIM 28-22- TREE 819, NO FAULTS FOUND.

Part: WARNING MESSAGE — FALSE ACTIVATION (WINDOW HEAT) · airframe 88,150 hrs · 16,362 cycles

RIGHT FWD WINDOW HEAT INOPERATIVE. PERFORMED FIM 30-41 FT 804, NO FAULTS FOUND , ACFT OK FOR SERVICE.

Part: CONTROL PANEL — MALFUNCTIONED (WINDOW HEAT) · airframe 88,146 hrs · 16,361 cycles

ON TOUCHDOWN, THE RT WINDOW HEAT EICAS MESSAGE ILLUMINATED. RAN QRH AND EICAS MESSAGE CLEARED. TROUBLESHOT & FOUND BROKEN INSULATION AT TR324. REPAIRED THE INSULATION IAW SWPM 20-10-13. R & R THE WINDOW ANTI ICE CONTROL PANEL IAW AMM 30-41-00, OPS CHECKS GOOD.

Part: CONTROL VALVE — FAULTED (LT A/C PACK) · airframe 88,146 hrs · 16,361 cycles

LEFT PACK TEMP ILLUMINATED ON SHORT FINAL AND AGAIN DURING TAXI IN. TROUBLESHOT THE LEFT PACK TEMP MESSAGE IAW FIM 21-51 FT 848, FOUND PACK TEMP CONTROL VALVE TO BE AT FAULT, REMOVED AND REPLACED THE PACK TEMP CONTROL VALVE IAW AMM 21-51-12. INSTALLATION TEST GOOD IAW AMM 21-51-12.

Part: WINDOW — INOPERATIVE (COCKPIT) · airframe 88,145 hrs · 16,360 cycles

RIGHT FWD WINDOW HEAT INOPERATIVE DURING TAXI. R & R THE WINDOW IAW AMM 56-11-01. OPS CHECKED NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (WINDOW HEAT) · airframe 88,145 hrs · 16,360 cycles

RIGHT FWD WINDOW HEAT CAUTION MESSAGE DURING LANDING. PERFORMED AN OPS CHECK OF THE RIGHT FWD WINDOW HEAT. OPS CHECKED GOOD , NO FAULTS NOTED IAW AMM 30-41-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT WINDOW HEAT) · airframe 88,140 hrs · 16,357 cycles

RIGHT FWD WINDOW MESSAGE. PERFORMED A WINDOW HEAT OPS CHECK IAW AMM 30-41-00, OPS CHECKED GOOD.

Part: SENSOR — LOOSE (WINDOW HEAT) · airframe 88,133 hrs · 16,355 cycles

RIGHT FWD WINDOW HEAT EICAS MESSAGE. TROUBLESHOT IAW W/D 30-41-12, AND FIM 30-41 F/T 802 . CONNECTOR D2898B, PINS 1 AND 2 115 VAC. VERIFY INTEGRITY S1 SWITCH AT PIN 6 D2898A. RESISTANCE CHECK OF WINDOW WITHIN LIMITS. INSPECTED WINDOW SENSOR 1 AND FOUND LOOSE.. SECURED THE SENSOR AND PERFORMED WINDOW HEAT OPS CHECK IAW AMM 30-41-01. WINDOW HEAT SYSTEM CHECKED NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT WINDOW HEAT) · airframe 88,140 hrs · 16,357 cycles

RIGHT WINDOW HEAT CAUTION MESSAGE AFTER LANDING. TROUBLESHOT IAW FIM 30-41 FT 804, DISCONNECTED THE WIRES FROM THE WHCU TO MAIN SENSOR AND CONNECTED TO THE SPARE SENSOR , PERFORMED WINDOW ANTI-ICING SYSTEM OPS CHECK IAW AMM 30-41-00, OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (WINDOW ANTI-ICE) · airframe 88,126 hrs · 16,353 cycles

RIGHT FWD WINDOW EICAS MESSAGE. WINDOW ANTI-ICE SYSTEM OPS CHECKED IAW AMM 30-41-00. NO FAULS NOTED. OPS CHECKED OK.

Part: CONTROL UNIT — MALFUNCTIONED (WINDOW HEAT) · airframe 88,136 hrs · 16,356 cycles

EICAS MESSAGE AFTER LANDING, FOR THE RT FWD WINDOW. REMOVED AND REPLACED THE RIGHT FWD WINDOW HEAT CONTROL UNIT. OPS CHECKED GOOD IAW 30-41-01.

Part: CONTROL UNIT — MALFUNCTIONED (WINDOW HEAT) · airframe 88,113 hrs · 16,348 cycles

AFTER LANDING, AN EICAS MESSAGE FOR THE RT FWD WINDOW. REMOVED AND REPLACED THE WINDOW HEAT CONTROL UNIT IAW AMM 30-41-01-004-001, AND 30-41-01-404-007. OPS CHECKED GOOD, NO FAULTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (WINDOW HEAT) · airframe 88,112 hrs · 16,347 cycles

RIGHT FWD WINDOW HEAT ADVISORY MESSAGE, AFTER LANDING. PERFORMED A SYSTEM CHECK OF THE RT FWD WINDOW HEAT IAW AMM 30-41-00. NO DEFECT NOTED.

Part: GCU — FAILED (RIGHT) · airframe 88,122 hrs · 16,352 cycles

RIGHT AC BUSS FAILED DURING DESCENT, QRH PROCEDURE RESTORED POWER WITH RT ISL ILLUMINATED. PERFORMED BITE CHECK ON THE BPCU, FOUND DP TRIPPED, MAIN BUSS, OVERLAP ZONE MESSAGE , REMOVED AND REPLACED THE RIGHT GCU, OPS CHECKED GOOD IAW AMM 24-22-02.

Part: GCU — MALFUNCTIONED · airframe 88,108 hrs · 16,345 cycles

R AC BUS FAILURE IN DESCENT, QRH PROC RESTORED PWR W/R ISL ILLUMINATED. PERFORMED BIT CHECK ON BPCU, FOUND DP TRIP/MAIN BUS/OVERLAP ZONE MESSAGE. REMOVED AND REPLACED RT GCU, OPERATIONAL CHECK GOOD IAW AMM 24-22-02.

Part: IDG — INOPERATIVE (RIGHT) · airframe 88,108 hrs · 16,345 cycles

RIGHT IDG INOPERATIVE. REMOVED AND REPLACED THE RT IDG IAW AMM 24-11-01, OPS CHECKED GOOD.

Part: BUSS — MALFUNCTIONED (AC) · airframe 88,095 hrs · 16,338 cycles

RIGHT AC BUSS OFF EICAS MESSAGE DURING DECENT, QRH COMPLIED WITH. FIM 24-20 F/T 801. OBSERVED FAULT, IDG HIGH RISE TEMP COMPLETED, IDG SERVICING ON RT IAW MCC REQUEST IAW AMM 12-13-03. NO CURRENT BUSS ISSUES NOTED.

Part: GCU — MALFUNCTIONED (NR 2) · airframe 88,093 hrs · 16,337 cycles

DURING DESCENT, WHEN TURNING LANDING LIGHTS ON, THE RT AC BUSS OFF EICAS ILLUMINATED. RT GENERATOR CONTROL, RT BUSS TIE, QRH COMLETED. RESET THE RT GENERATOR CONTROL AND RT BUSS TIE PREVIOUS FLT HAD SAME RESULT. ISOLATION AND BOTH UTILITY BUSS SHED. REMOVED AND REPLACED THE NR 2 GCU, OPS CHECKED GOOD IAW AMM 24-22-02.

Part: CONTROLLER — MALFUNCTIONED (WINDOW HEAT) · airframe 88,097 hrs · 16,339 cycles

RT FWD WINDOW HEAT EICAS MESSAGE ON LANDING. RERACKED THE WINDOW HEAT CONTROLLER AND PERFORMED TEST. OPS CHECKED GOOD IAW AMM 30-41-00.

Part: HEATER — FAULTED (WINDOW) · airframe 88,087 hrs · 16,334 cycles

RIGHT FWD WINDOW HEAT FAULTED. PERFORMED AN OPS CHECK OF THE RT FWD WINDOW HEAT. OPS CHECKED GOOD IAW AMM 30-41-00.

Part: TRANSFORMER — MALFUNCTIONED · airframe 88,082 hrs · 16,332 cycles

TR UNIT STATUS MESSAGE. PERFORMED A BITE TEST ON THE TR UNIT, NO FAULTS FOUND , RESET UNIT, SYSTEM OK IAW FIM 24-32 FT 803.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 88,082 hrs · 16,332 cycles

CABIN ALT AUTO 2 STATUS MESSAGE. PERFORMED A BITE TEST OF PRESSURE CONTROLLER , NO FAULTS FOUND, RESET THE UNIT IAW FIM 21-31 FT 803.

Part: BPCU — FAILED (AC SYSTEM) · airframe 88,082 hrs · 16,332 cycles

RIGHT AC BUSS FAIL INDICATED , RECYCLING RT GENERATOR RESTORED POWER TO RIGHT AC BUSS , RESSETING RT BUSS ISOLATION SWITCH UNSUCCESFUL , OCCURED DESCENDING THROUGH 18000 FT. PERFORMED AN OPS CHECK OF BPCU, OPS CHECK FAILED, REMOVED AND REPLACED BPCU IAW AMM 24-41-03. ALSO SERVICED THE RT IDG IAW AMM 12-13-03, OPS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,065 hrs · 16,327 cycles

ON APPROACH RT FWD WINDOW HEAT FAILED. OPS CHECKED RT FWD WINDOW HEAT NO FAULT FOUND IAW AMM 30-40-00.

Part: CONNECTOR — DIRTY (HEAT CONTROLLER) · airframe 88,058 hrs · 16,324 cycles

RIGHT FWD WINDOW HEAT INOPERATIVE. PERFORMED WINDOW HEAT GROUND TEST IAW AMM 30-41-00, NO DEFECTS NOTED, CLEANED & SECURED THE CONNECTOR ON THE WINDOW HEAT CONTROL PANEL ( P5 ) IAW SWPM 20-60-01, CHECKED CONTINUITY FROM PIN 9 TO PIN 8 ON CONTROLLER, NO DEFECTS NOTED , SYSTEM OPS CHECKED GOOD IAW AMM 30-41-00. ACFT OK FOR SERVICE.

Part: HMU — MALFUNCTIONED (RT ENGINE) · airframe 88,053 hrs · 16,323 cycles

RIGHT ENGINE APPROACH IDLE INOPERATIVE. ONCE RIGHT ENGINE STARTED, ENGINE WENT TO APPROACH IDLE RANGE OF 44% N1 AND 77% N2, REMOVED & REPLACED THE RT ENGINE EEC IAW AMM 73-21-15. OPS CHECKED NORMAL. REMOVED & REPLACED THE RT HMU IAW AMM 73-21-14, OPS CHECKED NORMAL

Part: EEC — MALFUNCTIONED (RT ENGINE) · airframe 88,061 hrs · 16,325 cycles

ONCE THE RIGHT ENG STARTED, THE ENGINE WENT TO APPROACH IDLE RANGE OF 44% N1 & 77% N2. REMOVED & REPLACED THE RIGHT ENGINE EEC IAW AMM 73-21-15, OPS CHECKED NORMAL.

Part: HEATER — MALFUNCTIONED (WINDOW) · airframe 88,043 hrs · 16,320 cycles

RT FORWARD WINDOW HEAT INOPERATIVE, TROUBLESHOT THE RIGHT FORWARD WINDOW HEAT IAW FIM 30-41-01, FAULT TREE 802 AND 804. CHECKED WITHIN LIMITS.

Part: IDG — FAILED (RIGHT) · airframe 88,045 hrs · 16,321 cycles

RIGHT GENERATOR FAILED ON ARRIVAL WITH RIGHT AC BUSS FAILURE WHEN LOGO LIGHTS SELECTED ON. REPLACED THE RIGHT IDG IAW AMM 24-11-01, NO FAILURES NOTED. FUNCTIONAL CHECKED IAW AMM 74-11-00-75. FUNCTIONAL CHECKED GOOD IAW AMM 24-11-00-75.

Part: CONTROL UNIT — FAILED (RT GENERATOR) · airframe 88,040 hrs · 16,319 cycles

RIGHT GENERATOR TRIPPED IN FLIGHT, RESET THE GEN CIRCUIT BRAKER & RT BUS TIE CIRCUIT BREAKER. REMOVED AND REPLACED THE RT GENERATOR CONTROL UNIT IAW AMM 24-22-02. OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (EXHAUST FAN) · airframe 88,040 hrs · 16,319 cycles

FWD EQ EXHAUST FAN STATUS MESSAGE. PERFORMED AN OPS CHECK ON THE FWD EQ FAN IAW AMM 21-25-01. OPS CHECKED GOOD. MESSAGE CLEARED.

Part: WARNING MESSAGE — FALSE ACTIVATION (WINDOW HEAT) · airframe 88,045 hrs · 16,321 cycles

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

Part: APU — FAULTED · airframe 88,021 hrs · 16,312 cycles

APU FAULTED ON FIRST START ATTEMPT. OPS CHECKED GOOD IAW FIM 49-11, TASK 958.

Part: LEAD — DIRTY (WINDOW HEAT) · airframe 88,026 hrs · 16,313 cycles

FO FWD SIDE WINDOW EICAS MESSAGE. INOPERATIVE LIGHT REMAINED ILLUMINATED. CLEANED WINDOW LEADS, OPS CHECKED WINDOW HEAT FOR 1/2 HOUR, NO FAULTS NOTED, OPS NORMAL IAW SWPM 20-10-04 & AMM 30-41-00.

Part: ANTI-ICE SYSTEM — MALFUNCTIONED (ENGINE) · airframe 88,021 hrs · 16,312 cycles

DURING CRUISE, AT FL 380, IN CLEAR WEATHER. BOTH ENGINE ANTI-ICE CAME ON WITH SELECTOR IN AUTO. TURNED THE ANTI-ICE OFF AND ICING ENGINE EICAS MESSAGE CAME ON. NORMAL OPERATION IAW FIM 30-90-20-00. PERFORMED OPS CHECK IAW AMM 30-81-01, NO DEFECTS NOTED, OPS CHECKED GOOD.

Part: ECU — FAILED (APU) · airframe 88,005 hrs · 16,307 cycles

APU NOT SUPPLYING AIR PRESSURE. REMOVED AND REPLACED APU ECU IAW 49-61-05, OPS CHECKED GOOD.

Part: CONNECTOR — DIRTY (ENGINE ANTI ICE) · airframe 87,996 hrs · 16,301 cycles

LT ENGINE ANTI ICE EICAS ILLUMINATED DURING ENGINE RUN. REMOVED AND CLEANED THE ANTI ICE CONNECTOR, CHECKED PINS J1,J2 & J3 IAW FIM 30-21 TR 803, RAN ENGINE OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (APU) · airframe 87,975 hrs · 16,294 cycles

DURING APPROACH WITH APU RUNNING, AT 1000 AGL, AN EICAS APU GENERATOR OFF AND THEN AN APU FAULT DISPLAYED. PERFORMED A BITE CHECK ON ECU, NO DEFECTS NOTED. UNABLE TO DUPLICATE ISSUES. PERFORMED OPS CHECK IAW AMM 49-01-00.

Part: PUMP — INOPERATIVE (FUEL BOOST) · airframe 87,957 hrs · 16,287 cycles

LEFT WING AFT FUEL PUMP INOPERATIVE. TROUBLESHOT IAW FIM 28-22- FT 820, WIRING CHECKED GOOD. REMOVED AND REPLACED THE BOOST PUMP, OPS CHECKED GOOD IAW AMM 28-22-03. NO LEAKS NOTED.

Part: CIRCUIT BREAKER — TRIPPED (FUEL PUMP) · airframe 87,949 hrs · 16,282 cycles

FOUND THE LT AFT FUEL PUMP CIRCUIT BREAKER TRIPPED. PERFORMED CIRCUIT BREAKER RESET AND PERFORMED OPS CHECK IAW AMM 28-22-00, OPS CHECKED GOOD.

Part: APU — SHUTDOWN · airframe 87,906 hrs · 16,267 cycles

APU AUTO SHUTDOWN, WILL NOT RESTART. REMOVED AND REPLACED THE APU IAW AMM 49-11-01 OPS AND LEAK CHECKED.

Part: SWITCH — BROKEN (WX RADAR PANEL) · airframe 87,904 hrs · 16,266 cycles

WEATHER RADAR PANEL HAS A BROKEN SWITCH. REPLACED WEATHER RADAR PANEL IAW AMM 34-43-02. OPS CHECKED GOOD.

Part: TRANSCEIVER — FAILED (WX RADAR) · airframe 87,877 hrs · 16,259 cycles

WITH TILT IN AUTO, RIGHT WEATHER RADAR SHOWS 16 DOWN MANUAL TILT (-16M). REMOVED AND REPLACED RT WEATHER RADAR TRANSCEIVER IAW AMM 34-43-01, OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PUMP) · airframe 87,877 hrs · 16,259 cycles

LEFT AFT FUEL PUMP MESSAGE AND CIRCUIT BREAKER AFT FUEL BOOST PUMP OUT. QRH PROCEDURE COMPLIED WITH. PERFORMED FIM 28-22, 812 AND OPS CHECKED IAW AMM 28-22-00. NO FURTHER DEFECTS NOTED.

Part: ANTI-ICE VALVE — NOT REPORTED (LT ENGINE) · airframe 87,875 hrs · 16,258 cycles

LEFT ENGINE ANTI-ICE NEEDS TO BE REPLACED PER MAINTENANCE CONTROL. REMOVED AND REPLACED THE LEFT ENGINE ANTI-ICE VALVE IAW AMM 30-21-03-404-022.

Part: INDICATOR — FAILED (CABIN PRESSURE) · airframe 87,889 hrs · 16,262 cycles

PRESSURE RATE NEEDLE SPINS IN ALL DIRECTION AT LEVEL FLT. DIFF & ALT OK READINGS. REMOVED AND REPLACED THE CABIN PRESSURE INDICATOR. OPERATED IAW AMM 21-31-00.

Part: WARNING LIGHT — ILLUMINATED · airframe 87,872 hrs · 16,256 cycles

LEFT ENGINE ANTI-ICE VALVE INDICATES OPEN AT GATE. RESET THE ANTI-ICE VALVE TO THE OFF POSITION, OPS CHECKED NORMAL IAW AMM 30-21-00.

Part: CONNECTOR — DIRTY (ANTI ICE VALVE) · airframe 87,872 hrs · 16,256 cycles

AFTER TAKE OFF, HAD A LEFT ENGINE ANTI-ICE EICAS MESSAGE & LT ENG ANTI-ICE VALVE STATUS MESSAGE. CLEANED AND SECURED THE LT ENGINE ANTI-ICE VALVE CONNECTOR, SYSTEM CHECKED GOOD IAW MM 30-21-00.

Part: ANTI-ICE VALVE — OUT OF ADJUST (LT ENGINE) · airframe 87,830 hrs · 16,243 cycles

LEFT ENGINE ANTI-ICE EICAS WHILE ON DESCENT IN ICING CONDITIONS. PERFORMED ADJUSTMENT AND TEST OF THE LEFT ENGINE ANTI-ICE VALVE IAW AMM 30-21-00. PERFORMED ENGINE RUNS AND CYCLED THE ANTI-ICE VALVE, NO DEFECTS NOTED IAW AMM 31-00-00.

Part: INDICATOR — MALFUNCTIONED (CABIN PRESSURE) · airframe 87,816 hrs · 16,238 cycles

AT FL 400, CABIN ALTITUDE INDICATOR FLUCTUATED BETWEEN 20,000- 10,000 FT. NO CABIN ALTITUDE EICAS CAUTION MESSAGE OR MASTER CAUTIONS ILLUMINATED. DESCENDED TO FL 340 AND HAD NORMAL INDICATION. CABIN DIFFERENTIAL PRESSURE NEVER WENT INTO THE AMBER BAND. REMOVED AND REPLACED THE CABIN PRESSURE GAUGE PANEL ASSY IAW AMM 21-33-01. OPS CHECKED GOOD.

Part: PUMP — MALFUNCTIONED (FUEL BOOST) · airframe 87,816 hrs · 16,238 cycles

LEFT AFT FUEL PUMP CAUTION MESSAGE CAME ON AFTER ENGINE START. RAN QRH AND RETURNED TO GATE. REMOVED AND REPLACED LEFT FUEL BOOST PUMP IAW AMM 28-22-03. OPS CHECKED GOOD .

Part: DOUBLER — WORN (NR 2 NACELLE) · airframe 87,789 hrs · 16,233 cycles

NR 2 ENGINE RT CORE COWL PRECOOLER EXIT DUCT FOUND WORN. THE DUCT DOUBLER WAS REPAIRED IAW SB TBC - 80C2-NAC-71-032. REV 2.

Part: BRACKET — WORN (NR 2 NACELLE) · airframe 87,789 hrs · 16,233 cycles

ATA 71-13 #2 ENGINE L/H CORE COWL HOLD OPEN ROD STOW PIN SUPPORT BRACKET ADAPTER FOUND WORN AS MARKED. NR 2 ENGINE - L/H CORE COWL HOLD OPEN ROD STOW PIN SUPPORT WORN BRACKET AND ADAPTER REMOVED AND REPLACED AS PER B767-300 SRM 51-40-02 , REV. 105.

Part: SEAL — TORN (NR 2 COWLING) · airframe 87,789 hrs · 16,233 cycles

NR 2 ENGINE RT FAN COWL LOWER AREA 02 EACH SEALS FOUND TORN. NR 2 ENGINE RT FAN COWL LOWER AREA 02 EACH SEALS REMOVED AND REPLACED IAW AMM 20-11-00 REV 122.

Part: SUPPORT PLATE — WORN (LT NACELLE) · airframe 87,789 hrs · 16,233 cycles

NR 1 ENGINE LT CORE COWL INTERIOR SURFACE MID SECTION SUPPORT PLATE FOUND WORN. THE SUPPORT PLATE WAS REMOVED AND REPLACED IAW SRM 51-40-02 REV. 105.

Part: RUB STRIP — WORN (NR 1 NACELLE) · airframe 87,789 hrs · 16,233 cycles

NR 1 ENGINE L/H CORE COWL INTERIOR SURFACE UPPER AFT SECTION RUB STRIP FOUND WORN. THE RUB STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02 REV 105.

Part: FRAME — WORN (LT NACELLE) · airframe 87,789 hrs · 16,233 cycles

NR 2 ENGINE LT CORE COWL 2ND ZEE FRAME FROM FWD EXISTING REPAIR DOUBLER AND FILLER FOUND WORN. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02 REV 105.

Part: BRACKET — WORN (NR 1 NACELLE) · airframe 87,789 hrs · 16,233 cycles

NR 1 ENGINE RT CORE COWL HOLD OPEN ROD STOW PIN SUPPORT BRACKET & ADAPTER FOUND WORN THE BRACKETS AND ADAPTER WERE REMOVED AND REPLACED IAW SRM 51-40-02. REV 105.

Part: RUB STRIP — WORN (NR 1 NACELLE) · airframe 87,789 hrs · 16,233 cycles

NR 1 ENGINE, NOSE COWL EXTERIOR SURFACE AFT EDGE HAD THREE RUB STRIPS FOUND WORN LOCATED 7 TO 11 O'CLOCK POSITION AND 1 TO 3 O'CLOCK POSITION. THE RUB STRIPS WERE REMOVED AND REPLACED IAW SRM 51-40-02. REV. 105.

Part: FAIRING — WORN (NR 2 NACELLE) · airframe 87,789 hrs · 16,233 cycles

NR 2 ENGINE LT CORE COWL FAIRING SKIN INTERIOR SURFACE UPPER AFT CUT-OUT SECTION FOUND WORN. THE FAIRING SKIN WAS REPAIRED IAW SRM 54-42-01. REV.105.

Part: FIRESHIELD — TORN (NR 2 NACELLE) · airframe 87,789 hrs · 16,233 cycles

NR 2 ENGINE LT CORE COWL INTERIOR SURFACE SEVERAL FIRESHEILD FOUND TORN. THE FIRESHIELD WAS REPAIRED IAW SRM 54-42-01-2R-6, REPAIR 6, REV 105.

Part: RUB STRIP — WORN (NR 1 NACELLE) · airframe 87,789 hrs · 16,233 cycles

NR 1 ENGINE LT CORE COWL FAIRING ASSY INTERIOR SURFACE AFT UPPER SECTION RUBSTRIP FOUND WORN. THE RUB STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02 REV 105.

Part: SEAL — WORN (NR 1 NACELLE) · airframe 87,789 hrs · 16,233 cycles

NR 1 ENGINE LT CORE COWL FAIRING ASSY INTERIOR SURFACE UPPER FWD EDGE SEAL FOUND WORN. THE SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02. REV 105.

Part: BRACKET — WORN (NR 2 NACELLE) · airframe 87,789 hrs · 16,233 cycles

NR 2 ENGINE RT CORE COWL HOLD OPEN ROD STOW PIN SUPPORT BRACKET ADAPTER FOUND WORN. REMOVED AND REPLACED AS PER B767-300 SRM 51-40-02 , REV. 105.

Part: BOLT — WORN (NR 1 NACELLE) · airframe 87,789 hrs · 16,233 cycles

NR 1 ENGINE O/B CORE COWL MOUNTING BOLT FOUND WORN. THE BOLT WAS REMOVED AND REPLACED IAW AMM 71-11-06 , REV. 122.

Part: LONGERON — WORN (NR 2 NACELLE) · airframe 87,789 hrs · 16,233 cycles

NR 2 ENGINE R/H CORE COWL AFT LOWER EDGE LONGERON FOUND WORN. LONGERON REMOVED AND REPLACED IAW SRM 51-40-02 , REV. 105.

Part: RUB STRIP — WORN (NR 2 NACELLE) · airframe 87,789 hrs · 16,233 cycles

NR 2 ENGINE NOSE COWL EXTERIOR SURFACE AFT EDGE RUB STRIP FOUND WORN. THE RUB STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02. REV. 105.

Part: SWITCH — MALFUNCTIONED (APU) · airframe 87,789 hrs · 16,233 cycles

WHEN APU DC PUMP RUNNING, EICAS MSG 'DC FUEL PUMP ON' DOES NOT SHOW. APU DC FUEL PUMP PRESSURE SWITCH REMOVED, REPLACED AND TESTED IAW AMM 28-25-03 REV 122, FOUND SATISFACTORY.

Part: FRAME — WORN (NR 1 ENGINE) · airframe 87,789 hrs · 16,233 cycles

NR 1 ENGINE LT CORE COWL AFT HAT FRAME REPAIR DOUBLERS FOUND WORN. NR 1 ENGINE LH CORE COWL AFT WORN HAT FRAME REMOVED AND REPLACED AS PER B767-300 SRM 51-40-02 REV 105</P>)

Part: RIVET — SHEARED (NR 1 COWLING) · airframe 87,789 hrs · 16,233 cycles

NR 1 ENGINE LT CORE COWL INTERIOR SURFACE DATA SUPPORT PLATE ATTACH RIVETS FOUND SHEARED. NR 1 ENGINE LT CORE COWL INTERIOR SURFACE DATA SUPPORT PLATE ATTACH SHEARED RIVETS REMOVED AND REPLACED AS PER SRM 51-40-02 REV 105.

Part: BRACKET — WORN (NR 2 COWLING) · airframe 87,789 hrs · 16,233 cycles

NR 2 ENGINE RT CORE COWL HOLD OPEN ROD. ROD END BEARING AND WEL BRACKET FOUND WORN. NR 2 ENGINE RT CORE COWL HOLD OPEN ROD, ROD END BEARING AND WEL BRACKET REMOVED AND REPLACED IAW AMM 70-50-00 REV 122.

Part: RIVET — SHEARED (NR 2 COWLING) · airframe 87,789 hrs · 16,233 cycles

NR 2 ENGINE LT CORE COWL INTERIOR SURFACE DATA SUPPORT PLATE ATTACH RIVETS FOUND SHEARED. NR 2 ENGINE LT CORE COWL INTERIOR SURFACE DATA SUPPORT PLATE ATTACH SHEARED RIVETS REMOVED AND REPLACED AS PER SRM 51-40-02 REV 105.

Part: RUB STRIP — WORN (NR 2 NACELLE) · airframe 87,789 hrs · 16,233 cycles

NR 2 ENGINE LT CORE COWL FAIRING ASSY INTERIOR SURFACE AFT UPPER SECTION RUBSTRIP FOUND WORN. THE RUBSTRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02 REV 105.

Part: DOOR — DAMAGED (NR 2 COWLING) · airframe 87,789 hrs · 16,233 cycles

NR 2 ENGINE LT CORE COWL FAIRING ASSY FLIPPER DOOR ASSY. FOUND DAMAGED. NR 2 ENGINE LT CORE COWL FAIRING ASSY DAMAGED FLIPPER DOOR ASSY REMOVED AND REPLACED AS PER SRM 51-40-02. REV 105.

Part: RETAINER — WORN (NR 1 NACELLE) · airframe 87,789 hrs · 16,233 cycles

NR 1 ENGINE RT CORE COWL PRESSURE RELIEF DOOR CUT-OUT UPPER RETAINER FOUND WORN. THE RETAINER WAS REMOVED AND REPLACED IAW SRM 51-40-02. REV. 105.

Part: CONNECTOR — DAMAGED · airframe 87,789 hrs · 16,233 cycles

P37 PANEL ELECTRICAL CONNECTOR (D05052P) FOUND TERM 8 PIN LOCK BROKEN. REMOVED AND REPLACED IAW SWPM 20-61-11 REV 66 FOUND SATISFACTORY.

Part: BRACKET — WORN (NR 1 COWLING) · airframe 87,789 hrs · 16,233 cycles

NR 1 ENGINE LT CORE COWL HOLD OPEN ROD, ROD END BEARING AND WEL BRACKET FOUND WORN. NR 1 ENGINE LT CORE HOLD OPEN ROD, ROD END BEARING AND WELL BRACKET REMOVED AND REPLACED IAW AMM 70-50-00 REV 122.

Part: RIVET — SHEARED (NR 2 COWLING) · airframe 87,789 hrs · 16,233 cycles

NR 2 ENGINE LT CORE COWL EXTERIOR SURFACE FWD LOWER SECTION RIVETS FOUND SHEARED. NR 2 ENG LT CORE COWL EXTERIOR SURFACE FWD LOWER SECTION SHEARED RIVETS REMOVED AND REPLACED AS PER SRM 51-40-02, REV 105.

Part: SEAL — WORN (NR 2 NACELLE) · airframe 87,789 hrs · 16,233 cycles

NR 2 ENGINE, LT CORE COWL FAIRING ASSY UPPER AFT AFT AND FWD EDGE STRIP SEAL FOUND WORN. THE SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02. REV.105.

Part: RUB STRIP — WORN (NR 2 NACELLE) · airframe 87,789 hrs · 16,233 cycles

NR 2 ENGINE RT CORE COWL FAIRING ASSY INTERIOR SURFACE AFT UPPER SECTION RUBSTRIP FOUND WORN. THE RUBSTRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02 REV 105.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 87,789 hrs · 16,233 cycles

DENT AND BUCKLE ON AN EXTERNAL DOUBLER REPAIR OF THE BULK CARGO DOOR BS 1417 TO 1425. STRINGERS 31L TO 32L. REPAIRED IAW SRM 52-30-01-2R-6. REPAIR 6. REV. 105.

Part: FRAME — WORN (NR 2 NACELLE) · airframe 87,789 hrs · 16,233 cycles

NR 2 ENGINE LT CORE COWL AFT HAT FRAME REPAIR DOUBLERS FOUND WORN. NR 2 ENGINE LH CORE COWL AFT SECTION WORN HAT FRAME REMOVED AND REPLACED IAW SRM 51-40-02 REV 105.

Part: DUCT — WORN (NR 1 NACELLE) · airframe 87,789 hrs · 16,233 cycles

NR 1 ENGINE RT CORE COWL PRECOOLER EXIT DUCT FOUND WORN. THE DUCT WAS REPAIRED IAW SB TBC - 80C2-NAC-71-032. REV. 2.

Part: RUB STRIP — CRACKED (NR 2 NACELLE) · airframe 87,789 hrs · 16,233 cycles

NR 2 ENGINE RT CORE COWL EXTERIOR SURFACE FWD UPPER SECTION RUB STRIP FOUND CRACKED. THE RUB STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02 REV 105.

Part: PRIORITY VALVE — NO TEST (NR 2 ENGINE) · airframe 87,789 hrs · 16,233 cycles

NR 2 ENGINE PRV FAILED THUMB CHECK. NR 2 ENGINE PRV REMOVED AND REPLACED IAW AMM 36-11-18 REV 122.

Part: FAIRING — WORN (NR 1 NACELLE) · airframe 87,789 hrs · 16,233 cycles

NR 1 ENGINE LT CORE COWL FAIRING SKIN INTERIOR SURFACE UPPER AFT CUT-OUT SECTION FOUND WORN. REPAIRED IAW SRM 54-42-01, REPAIR 5. REV 105.

Part: BRACKET — WORN (NR 1 COWLING) · airframe 87,789 hrs · 16,233 cycles

NR 1 ENGINE RT CORE COWL HOLD OPEN ROD, ROD END BEARING AND WEL BRACKET FOUND WORN. NR 1 ENGINE RT CORE COWL HOLD OPEN ROD, ROD END & BEARING AND WEL BRACKET REMOVED AND REPLACED IAW AMM 70-50-00 REV 122.

Part: CONNECTOR — CRACKED (SHUTOFF VALVE) · airframe 87,789 hrs · 16,233 cycles

LT REAR SPAR FOUND APU FUEL SOV ELECTRICAL CONNECTOR CRACKED. CONNECTOR REMOVED AND REPLACED IAW WDM 28-25-21 REV 13 AND SWPM 20-61-00 REV 65. OPS TESTED GOOD IAW AMM 28-25-00 REV 122.

Part: RETAINER — WORN (NR 2 NACELLE) · airframe 87,789 hrs · 16,233 cycles

NR 2 ENGINE RT CORE COWL PRESSURE RELIEF DOOR CUT-OUT UPPER RETAINER FOUND WORN. THE RETAINER WAS REMOVED AND REPLACED IAW SRM 51-40-02. REV. 105.

Part: SKIN — WORN (NR 1 NACELLE) · airframe 87,789 hrs · 16,233 cycles

NR 1 ENGINE LT CORE COWL SKIN FOUND WORN, UPPER AFT EDGE. REPAIRED IAW EO 1971A157. REV. 0.

Part: CONNECTOR — DAMAGED · airframe 87,789 hrs · 16,233 cycles

FOUND CONNECTOR D5656P PIN 38 UNABLE TO LOCK., REMOVED AND REPLACED IAW SWPM 20-61-11 REV 66 FOUND SATISFACTORY.

Part: SEAL — WORN (NR 1 NACELLE) · airframe 87,789 hrs · 16,233 cycles

NR 1 ENGINE L/H CORE COWL FAIRING ASSY UPPER AFT EDGE STRIP SEAL FOUND WORN.. THE SEAL WS REMOVED AND REPLACED IAW SRM 51-40-02 REV.105.

Part: SKIN — CRACKED (NR 2 NACELLE) · airframe 87,789 hrs · 16,233 cycles

NR 2 ENGINE LT CORE COWL SKIN UPPER AFT CUT-OUT SECTION FOUND CRACKED. SKIN REPAIRED IAW SRM 54-42-01-2R-4 , REPAIR 4 , REV. 105.

Part: SEAL — WORN (NR 2 NACELLE) · airframe 87,789 hrs · 16,233 cycles

NR 2 ENGINE LT CORE COWL FAIRING ASSY INTERIOR SURFACE UPPER FWD EDGE SEAL FOUND WORN. THE SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02. REV. 105.

Part: STRIKER — WORN (NR 2 NACELLE) · airframe 87,789 hrs · 16,233 cycles

NR 2 ENGINE RT CORE COWL INTERIOR SURFACE PRESSURE RELIEF DOOR CUT-OUT LOWER STRIKER PLATE FOUND WORN. THE STRIKER PLATE WAS REMOVED AND REPLACED IAW SRM 51-40-02 REV 105.

Part: STRUCTURE — DAMAGED (NR 2 NACELLE) · airframe 87,789 hrs · 16,233 cycles

DENT AND BUCKLE AND EXISTING REPAIR ON #2 ENGINE INBOARD T/R INNER SURFACE SIDE AT 8 O'CLOCK POSITION. NR 2 ENGINE L/H TRANSLATING COWL REMOVED AND REPLACED I.A.W B767-300 AMM 78-31-10 , REV. 122. FOR THRUST REVERSER OPERATIONAL TEST REFER TO W/C # A-78-333-01-2. FOR WORK DETAILS.

Part: LONGERON — WORN (LT NACELLE) · airframe 87,789 hrs · 16,233 cycles

NR 2 ENGINE L/H CORE COWL AFT LOWER EDGE LONGERON FOUND WORN. NR 2 ENGINE - L/H CORE COWL AFT LOWER EDGE LONGERON REMOVED AND REPLACED IAW SRM 51-40-02 , REV. 105.</P>)

Part: RUB STRIP — WORN (NR 2 NACELLE) · airframe 87,789 hrs · 16,233 cycles

NR 2 ENGINE RT CORE COWL INTERIOR SURFACE UPPER AFT SECTION RUB STRIP FOUND WORN. THE RUB STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02 REV 105.

Part: BOLT — WORN (NR 2 NACELLE) · airframe 87,789 hrs · 16,233 cycles

NR 2 ENGINE O/B AND I/B CORE COWL TWO MOUNTING BOLTS FOUND WORN. THE BOLTS WERE REMOVED AND REPLACED IAW AMM 71-11-06 , REV. 122.

Part: CONTROL UNIT — FAILED (HEATER) · airframe 87,789 hrs · 16,233 cycles

NR 2 ENGINE HEATER CONTROL UNIT FOUND WORN DURING RECEIVING INSPECTION. NR 2 HEATER CONTROL UNIT REMOVED AND REPLACED IAW AMM 73-21-22 REV 122 AND ECU STATIC TEST CARRIED OUT IAW AMM 71-00-00-725-268-H03 REV 122 FOUND SATISFACTORY.

Part: CHECK VALVE — CHAFED (RT A/C BAY) · airframe 87,789 hrs · 16,233 cycles

A/C BAY, RT ISOLATION BYPASS CHECK VALVE FOUND THE HOUSING CHAFDED. THE RT ISOLATION BYPASS VALVE WAS REMOVED, REPLACED, AND LEAK CHECKED IAW AMM 21-51-15, AND 36-11-00, REV 122. FOUND SATISFACTORY.