N1499A

Part: WARNING MESSAGE — ILLUMINATED (ZONE 300) · airframe 92,154 hrs · 21,856 cycles

DURING TAXI AFTER ENGINE START " RUDDER RATIO" EICAS MESSAGE DISPLAYED.A/C RETURNED TO GATE (BTB) AND MTX GROUNDED A/C MTX THEN COMPLIED WITH FIM-21-27 FT804, NO FAULTS NOTED AT THIS TIME, OPS TEST OF RUDDER AND RUDDER TRIM CONTROL SYSTEM GOOD IAW AMM.27-21-00 NO FAULTS NOTRD AT THIS TIME. MTX RETURNED A/C TO SERVICE

Part: WARNING MESSAGE — FALSE ACTIVATION (RUDDER) · airframe 92,154 hrs · 21,856 cycles

DURING TAXI OUT AND AFTER ENGINE START "RUDDER RATIO" EICAS MESSAGE DISPLAYED. AIRCRAFT RETURNED TO BLOCKS (BTB). C/W FIM 27-21 FT 804 NO FAULTS NOTED AT THIS TIME OPS TEST OF RUDDER AND RUDDER TRIM CONTROL SYS GOOD IAW AMM 27-21-00 NO FAULTS NOTED AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.

Part: BLEED VALVE — DEFECTIVE (ZONE 200) · airframe 92,148 hrs · 21,854 cycles

DURING TAXI OUT, LT BLEED ISLN VALVE NOT IN THE COMMANDED POSITION AFTER ENGINE START. A/C RETURNED TO BLOCKS. (BTB). REMOVED & REPLACED LEFT BLEED ISLN VALVE IAW AMM 36-11-04, OPS CHECK OK IAW AMM 36-11-04 AIRCRAFT REMAINS NO ETOPS. AIRCRAFT RETURNED TO SERVICE.

Part: ELEC CONNECTOR — DISCONNECTED (ZONE 100) · airframe 92,050 hrs · 21,816 cycles

DURING CREW PRE-FLIGHT CHECK, MAIN DECK CARGO LP 1 EICAS MESSAGE. DEFERRED MAIN DECK CARGO LOOP 1 IAW ABX MEL 26-16-2-1. WHILE TESTING TAIM LOOP 1, ZONE D AND E, FOUND CONNECTOR D31592 NOT SEATED PROPERLY. CLEANED CONNECTOR AND RE-INSTALLED IAW B767 SWM 20-10-13 AND 10-60-01. DI CLEARED. A/C REMAINS NO ETOPS. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (ZONE 200) · airframe 92,037 hrs · 21,811 cycles

ON DESCENT INTO BOG NEAR, BUT PRIOR TO FL250 CABIN ALT MASTER WARNING SIREN, LIGHT AND EICAS MESSAGE. EMERGENCY DECLARED. DONNED 02. AIRCRAFT. EICAS MESSAGE CLEARED NEAR TOUCHDOWN. LANDED WITHOUT FUTHER INCIDENT. BITE TEST PERFORMED ON CABIN CONTROLLERS, NO FAULTS FOUND, TEST OK IAW AMM 21-31-00, THE ACFT WAS PRESSURZIZED IAW AMM 21-31-00 TO VERFIY THAT SYSTEM WAS WORKING PROPERLY, NO DISCREPANCIES NOTED AT THIS TIME, AIRCRAFT REMAINS NO ETOPS. AFTER MAINTENANCE REVIEW, DEFERRED CABIN AUTO PRESS CONTROL 1 AS PRECAUTION, ON L/P 39250-16/3. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PUMP) · airframe 91,838 hrs · 21,739 cycles

DURING TAXI, CTR RIGHT FUEL PUMP EICAS ILLUMINATED. AIRCRAFT RETURNED TO BLOCKS (BTB). DEFERRED IAW ABX-28-22-2AT/S CTR R FUEL PUMP EICAS MESSAGE AND BLED PRESSURE SENSE LINE FOR R AUX OVERRIDE PUMP PER B767 FIM 28-22 FT 805. PERFORMED TEST OF OVERRIDE PUMPS AND PRESSURE SWITCHES IN AUX FUEL TANK PER B767 AMM 28-22-00. OPS CHK GOOD. DI CLEARED. REACTIVATION PROCEDURES APPLIED. PLACARDS REMOVED. A/C REMAINS NO ETOPS. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (APU) · airframe 90,920 hrs · 21,372 cycles

DURING TAXI OUT ALL THREE A/C TEMP CONTROLLERS INDICATED INOP, A/C RETURNED TO THE GATE (BTB) AND MTX GROUNDED A/C . AFTER TROUBLE SHOOTING FOUND APU CONTROL UNIT BAD, REPLACED APU CONTROL UNIT IAW AMM 49-61-05. OPS CHECK GOOD, A/C REMAINS NO ETOPS . A/C IS RETURNED TO SERVICE .

Part: AUTOTHROTTLE SYS — DEFECTIVE (ZONE 100) · airframe 90,880 hrs · 21,356 cycles

DURING TAKE OFF, AUTO THROTTLE FAILED TO ENGAGE. ABORTED TAKE OFF (ATO). T/S PER B767 FIM 22-02 TASK 801. FAULTING RH PIMU. REMOVED & REPLACED RH PIMU IAW B767 AMM 77-35-02. OPS CHECK GOOD. MCDP 30/40 TESTS. REF LP:39236-18/3 FOR RALM STATUS. A/C REMAINS NO ETOPS. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING MESSAGE — ILLUMINATED (CABIN TEMP) · airframe 90,699 hrs · 21,290 cycles

DURING TAXI OUT, AFT CABIN TEMP, FWD CABIN TEMP EICAS MESSAGE APPEARED, A/C RETURNED TO GATE (BTB) AND MXT GROUNDED A/C. PERFORMED T/S IAW FIM 21-61 FT 804. NO FAULTS OR DISCREPANCIES FOUND. MTX DEFERRED IAW MEL ABX-21-61-1-2 AND RETURNED A/C TO SERVICE.

Part: CONTROLLER — DEFECTIVE (ZONE 200) · airframe 90,689 hrs · 21,286 cycles

ON TAXI OUT, AFT, FWD, FLT DECK CABIN TEMP EICAS MSG ILLUMINATED. A/C RETURNED TO BLOCKS (BTB). MAINTENANCE REMOVED AND REPLACED TEMP CONTROL ASSY. IAW AMM 21-57-14. OPS CKECK GOOD IAW 21-51-00. NO FAULTS DEFECTS AT THIS TIME. A/C REMAINS NO ETOPS AND RETURNED TO SERVICE.

Part: FIRE WARNING — FALSE ACTIVATION (ZONE 100) · airframe 90,610 hrs · 21,256 cycles

FLT NR: ABX3116, AFTER TAKE OFF, FIRE LIGHT ILLUMINATED ON R CAPTS INST PANEL. EMERGENCY DECLARED AND AIR TURN BACK (ATB) TO AFW. REMOVED AND REPLACED FIRE / OVERHEAT CIRCUIT CARD M10274 IAW B767 AMM 26-10-01. NO DEFECTS NOTED. TESTED THE CARGO SMOKE DETECTION LOOPS IAW B767 AMM 26-19-00. OPS CHECKED GOOD. NO ETOPS. A/C RETURNED TO SERVICE.

Part: START VALVE — MALFUNCTIONED (NR 2 ENGINE) · airframe 90,439 hrs · 21,177 cycles

DURING TAXI WHILE STARTING #2 ENGINE START VALVE FAILED TO OPEN. A/C RETURNED TO THE GATE (BTB) AND MTX GROUNDED A/C. MTX FOUND START VALVE FROZEN, OPS CHECK START VALVE IAW AMM 80-11-02 OPS CHECK GOOD AT THIS TIME.

Part: SHUTOFF VALVE — FAULTED (RT ENGINE) · airframe 90,362 hrs · 21,141 cycles

AFTER PUSHBACK "R ENG HPSOV" EICAS MSG INFO:STATUS MSG R ENG HPSOV INFO: R ENG BLD DISCRETE LIGHT ILLUMINATED AC RETURNED TO GATE (BTB) AND MTX GROUNDED AC MTX DEFERRED RH HPSOV FOR DEPARTURE IAW MEL ABX-36-11- 2-2 AND RETURNED AC TO SERVICE.

Part: CIRCUIT CARD — MALFUNCTIONED (LT ENGINE) · airframe 90,362 hrs · 21,141 cycles

AFTER PUSHBACK, STATUS MSG L ENG SPEED CARD AC RETURNED TO GATE (BTB)AND MTX GROUNDED ACMTX PERFORMED STATUS MSG ERASE PROCEDURES IAW B767 AMM 31-41-00, NO MSG AT THIS TIME.MTX RETURNED AC TO SERVICE.

Part: FLAP SYSTEM — FAULTED · airframe 89,634 hrs · 20,796 cycles

AFTER CLEANUP ON CLIMB, GOT MASTER CAUTION CONFIG FLAPS AFTER CLEANUP. CONTINUED INTIL DIRTY AGAIN. TRIED GRND PRC FLAP OVERIDE DID NOT SILENCE WARNING & MASTER CAUTION RESET DID NOT SILENCE WARNING. AC RETURNED TO FIELD & MX GROUNDED AC . DURING TROUBLE SHOOTING .FOUND #4 FLAP TRANSMITTER OUT OF ADJUST, ADJUSTED IAW AMM 27-51-14. FSEU, PSEU, FSPM & T/O CONFIG TESTS SHOW NO FAULTS. FOUND NLG NOT COMPRESSED SENSORS S244 & S266 TARGETS DAMAGED & SENSORS DENTED. R & R S244 & S266 IAW WDM 32-09-11 AND 32-09-12. REPLACED & ADJUSTED TARGETS IAW AMM 32- 09-08. VERIFIED SENSORS USING LCR IAW AMM 32-09-13. ACCOMPLISHED TAKEOFF CONFIG TEST WITH TORSION LINK COMPRESSED & EXTENDED. OPS CHECK GOOD IAW AMM 31-51-00.

Part: CIRCUIT CARD — FAILED (ZONE 100) · airframe 89,634 hrs · 20,795 cycles

AFTER CLIMB ON CLEANUP FLAPS SLOW TO RETRACT. STARTED GETTING A CONSTANT "CONFIG" "FLAPS" WARNING. AC PERFORMED AIR T TURN BACK AND LANDED .MTX GROUNDED AC AND TROUBLESHOT . REMOVED AND REPLACED LANDING CONFIG WARNING AND MODULE TAKE OFF WARNING CARD MODULE IAW B767-300 AMM 31-51-04. PERFORMED OPERATIONAL TEST OF BOTH CARDS. OPS CHECK NORMAL. MTX RETURNED AC TO SERVICE .

Part: FIRE LOOP — FAULTED · airframe 89,551 hrs · 20,764 cycles

DURING TAXI MAI N DECK FIRE LOOP 2 STATIS MSG. APPEARED A/C RETURNED TO GATE AND MTX GROUNDED A/C. MTX DEFERRED THE FIRE LOOP IAW MEL ABX-26-16-2-1 . AND RETURNED AC TO SERVICE .

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 89,439 hrs · 20,724 cycles

LEFT WING INBOARD MAIN FLAP LEADING EDGE BROKEN(<P>CRACK ON LH WING INBD MAIN FLAP LEADING EDGE AT IFS 296.25 / 282.75 WAS REPAIRED PER SRM 57-53-01-2R-1. NO FURTHER DEFECTS NOTED.</P>)

Part: FLOOR SUPPORT — CORRODED (BS 1417 LBL29) · airframe 89,439 hrs · 20,724 cycles

BULK CARGO COMPARTMENT, FLOOR SUPPORT STRUCTURE, STA 1417, LBL29, AROUND NUTS, CORROSION.(<P>CORROSION ON BULK CARGO COMPARTMENT TRANSITION SUPPORT AT STA 1417 / 1439 AND LBL 29 WAS REPAIRED PER SRM 51-70-11-0G-0. NO FURTHER DEFECTS NOTED.</P>)

Part: FLOOR SUPPORT — CRACKED (BS 1461 BL0) · airframe 89,439 hrs · 20,724 cycles

AFT CARGO COMPARTMENT, AT STA 1461, BL (0.0), FLOOR SUPPORT STRUFTURE, WITH CRACK(<P>CRACK ON FUSELAGE SECTION 46 CARGO COMPARTMENT FLOOR SUPPORT STRUCTURE&NBSP; AT STA 1461 AND BL 0.0 WAS REPAIRED PER SRM 53-65-00. NO FURTHER DEFECTS NOTED.</P>)

Part: STRINGER — CRACKED (BS 1461-1483) · airframe 89,439 hrs · 20,724 cycles

MAIN DECK CARGO, BTW STA 1461 AND 1483, STRG 17L WITH CRACK.(<P>CRACK ON FUSELAGE SECTION 46 STRINGER FLANGE BETWEEN&NBSP; STA 1461 / 1480 AND STGR 17L WAS REPAIRED PER SRM 53-00-03-2R-1. NO FURTHER DEFECT NOTED.</P>)

Part: NOT REPORTED — CORRODED (BS 1329-1351) · airframe 89,439 hrs · 20,724 cycles

MAIN DECK CARGO, BTW STA 1329 AND 1351, STRG 19L WITH CORROSION(<P>CORROSION ON&NBSP;&NBSP;FUSELAGE SECTION 46 BETWEEN STA 1329 / 1351 AND STGR 19L WAS REPAIRED PER CMA-TLS 24-0166-02B. NO FURTHER DEFECT NOTED.</P>)

Part: FLOOR SUPPORT — CORRODED (BS 1417 RBL9) · corrosion level 2 · airframe 89,439 hrs · 20,724 cycles

BULK CARGO COMPARTMENT, FLOOR SUPPORT STRUCTURE, STA 1417+2, RBL9, AROUND NUTS, CORROSION.(<P>CORROSION ON BULK CARGO COMPARTMENT TRANSITION SUPPORT AT STA 1417 AND RBL 8.73 WAS REPAIRED PER SRM 51-70-11-0G-0. NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — DAMAGED (RT NR 11 SLAT) · airframe 89,439 hrs · 20,724 cycles

RH WING, SLAT 11 LEADING EDGE OSS BWT 910/984.73, SEVERAL BURN MARKS(<P>BURN MARKS ON RH WING ON SLAT NO.11 TRAILING EDGE WEDGE WERE REPAIRED PER SRM 57-43-02-2R-1. NO FURTHER DEFECTS NOTED.</P>)

Part: STRINGER — CORRODED (ZONE 100) · airframe 89,439 hrs · 20,724 cycles

MAIN DECK CARGO, BTW STA 1351 AND 1373, STRG 19R WITH CORROSION.(<P>CORROSION ON FUSELAGE SECTION 46 STRINGER FLANGE BETWEEN STA 1351 / 1373 AND STGR 19 RH WAS REMOVED, EVALUATED AND FOUND WITHIN ALLOWABLE DAMAGE LIMITS PER SRM 53-00-03-1A-1.</P>)

Part: SKIN — DAMAGED (BS 139 S21L) · airframe 89,439 hrs · 20,724 cycles

CREASE ON LH FUSELAGE SKIN AT STA.138.5 AND 21" ABOVE STRG 21.(<P>CREASE ON LH FUSELAGE SKIN AT STA.138.5 AND 21" ABOVE STRG 21 WAS REPAIRED PER SRM 53-00-01-2R-14. NO FURTHER DEFECT NOTED.</P>)

Part: TORQUE TUBE — CORRODED (RT WING) · corrosion level 2 · airframe 89,439 hrs · 20,724 cycles

RIGHT WING TORQUE TUBE WITH EVIDENCE OF CORROSION.(<P>TORQUE TUBE WAS REPLACED PER AMM 27-51-41-400-801. NO FURTHER DEFECTS NOTED.</P>)

Part: FLOOR SUPPORT — CORRODED (BS 1417-1439) · corrosion level 2 · airframe 89,439 hrs · 20,724 cycles

AFT CARGO COMPARTMENT, FLOOR SUPPORT STRUCTURE, BTW STA 1417 AND 1439, LBL22, AROUND NUTS, CORROSION(<P>CORROSION ON BULK CARGO COMPARTMENT FLOOR STRUCTURE TRANSITION SUPPORT AT STA 1417 AND LBL 22.33 WAS REPAIRED PER SRM 51-70-11-0G-0. NO FURTHER DEFECTS NOTED.</P>)

Part: WEDGE — DEBONDED (RT NR 8 SLAT) · airframe 89,439 hrs · 20,724 cycles

RH WING, SLAT NO. 8, TRAILING EDGE WEDGE, INBOARD EDGE DISBONDED.(<P>DISBOND ON RH WING INBOARD SLAT NO.8 TRAILING EDGE WEDGE WAS REPAIRED PER SRM 57-43-02-2R-1. NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — PUNCTURED (LT NR 5 SLAT) · airframe 89,439 hrs · 20,724 cycles

LEFT WING,SLAT NO 5,EXTERNAL SKIN,WITH PUNCTURE(<P>PUNCTURE ON LH WING SLAT NO. 5 TRAILING EDGE WEDGE UPPER SKIN AT OSS 389.71 WAS REPAIRED PER SRM 57-43-02-2R-1. NO FURTHER DEFECTS NOTED.</P>)

Part: COLLAR — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 89,439 hrs · 20,724 cycles

RIGHT WING INBD FLAP COLLAR FITTING WITH EVIDENCE OF CORROSION.(<P>COLLAR FITTING WAS REPLACED PER AMM TASK 27-51-41-400-801. NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — WORN (RT NR 8 SLAT) · airframe 89,439 hrs · 20,724 cycles

RH WING, SLAT 8, TRAILING EDGE WEDGE, INTERNAL SKIN, WITH WEAR AT 60" FROM INBOARD EDGE(<P>WEAR ON RH WING ON SLAT NO. 8 TRAILING EDGE WEDGE SKIN BETWEEN OSS 471.75 WAS REPAIRED PER SRM 57-43-02-2R-1. NO FURTHER DEFECTS NOTED.</P>)

Part: SHEAR TIE — CORRODED (BS 724 S36L&R) · corrosion level 2 · airframe 89,439 hrs · 20,724 cycles

FWD CARGO COMPARTMENT, STA 742, BTW STR 39L AND 39R, BRACKET WITH CORROSION.(<P>SHEAR TIE WAS REPLACED PER DWG 143T1214. NO FURTHER DEFECTS NOTED.</P>)

Part: FLOOR SUPPORT — CORRODED (BS 1439 LBL15) · corrosion level 2 · airframe 89,439 hrs · 20,724 cycles

BULK CARGO COMPARTMENT, STA 1439, LBL15, AROUND DRILL HOLES, CORROSION.(<P>CORROSION ON BULK CARGO COMPARTMENT FLOOR STRUCTURE TRANSITION SUPPORT AT STA 1439 AND LBL 15.48 REPAIRED PER SRM 51-70-11-0G-0. NO FURTHER DEFECTS NOTED.</P>)

Part: SEAT BELT — UNKNOWN (UNKNOWN) · airframe 88,228 hrs · 20,300 cycles

1ST SUPERNUMERARY SEAT BELT TSO TAG MARKING ILLEGIBLE.(<P>R/R 1ST SUPERNUMERARY SEAT BELT, INERTIA REEL &AMP; LAP BELT IAW AMM 25-11-03. OPS CHECK GOOD. THIS CLEARS DMI 195712. MCC NOTIFIED. PLACARDS REMOVED.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,228 hrs · 20,300 cycles

AFT NACELLE INBD SIDE REAR MODULE ( CASE DRAIN ) FILTER WITH EVIDENCE OF HYD LEAK.(<P>CLEANED AREA AT RH NACELLE, TIGHTENED CASE&NBSP; DRAIN FILTER PER&NBSP; 767-300 AMM 29-11-18. NO LEAKS NOTED&NBSP; DURING / AFTER SYSTEM OPERATION.</P>)

Part: CONTAINER — MISSING (OXYGEN MASK) · airframe 88,228 hrs · 20,300 cycles

M/D PORTABLE OXYGEN FULL FACE MASK BAG MISSING.(<P>INSTALLED PORTABLE OXYGEN FULL FACE MASK BAG AS REQUIRED PER AMM 35-31-01. OPS CHECK OK.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,228 hrs · 20,300 cycles

LH WING OUTBOARD FLAP - OUTBOARD AFT FAIRING HAS A LOOSE ATTACH BOLT .(<P>ATTACH&NBSP; BOLT&NBSP; AT&NBSP; AFT FAIRING OUTBOARD AREA BY LH WING OUTBOARD&NBSP; FLAP WAS&NBSP; REMOVED,&NBSP; CLEANED, LOCATED SECURED AND REINSTALLED PROPERLY. TORQUED&NBSP; AS PER BOEING 767-300 SRM 51-40-02-0G-0&NBSP; &AMP;&NBSP; AMM 20-11-00-910-802.</P>)

Part: BEARING — UNKNOWN (UNKNOWN) · airframe 88,228 hrs · 20,300 cycles

MAIN ENTRY DOOR L1 HAS A LOWER FWD BEARING ON SLIDER CHANNEL FLAT WORN OUT(<P>REMOVED AND REPLACED MAIN ENTRY DOOR&NBSP; L1&NBSP; FWD BEARING&NBSP; AS PER B767-300&NBSP; AMM 52-12-03. OPS CHECK NORMAL .</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,228 hrs · 20,300 cycles

MAIN DECK MAIN SIDE CARGO DOOR FUSELAGE FRAME SEAL DEPRESOR BENT AT LOWER AFT AND FWD CORNERS.(<P>REWORKED&NBSP; AREAS&NBSP; BACK&NBSP; TO ORIGINAL&NBSP; CONTOUR IAW B767&NBSP; SRM&NBSP; 51-10-02. PERFORMED&NBSP; FLOURESCENT&NBSP; PENETRANT&NBSP; INSPECTION,&NBSP; NO CRACK INDICATION&NBSP; NOTED AT THIS TIME REF SOPM 20-00-00</P>)

Part: SEAL — UNKNOWN (UNKNOWN) · airframe 88,228 hrs · 20,300 cycles

RIGHT INB AILERON WITH AERODYNAMIC SEAL DAMAGED .(<P>REMOVED DAMAGED AERODYNAMIC SEAL&NBSP; LOCATED AT RIGHT INBD&NBSP; AILERON. INSTALLED, CLEANED, SECURED &AMP; LOCATED AS PER BOEING 767-300 AMM 20-10-23-964-001.</P>)

Part: SUPPORT RING — UNKNOWN (UNKNOWN) · airframe 88,228 hrs · 20,300 cycles

LOWER CREW OXYGEN BOTTLE FWD RING IS DAMAGED.(<P>REMOVED &AMP; REPLACED LWR CREW OXYGEN BOTTLE FWD SUPPORT RING AS PER B767-300 AMM 35-11-00-206-233. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,228 hrs · 20,300 cycles

ENG #1 PYLON INBOARD SIDE HAS LOOSE SCREW AND A PANEL WITH ENLONGATED HOLE.(<P>REMOVED LOOSE SCREW AND ELONGATED WASHER LOCATED AT ENGINE #1 PYLON INBOARD SIDE. INSTALLED, CLEANED, SECURED AND TORQUED HARDWARE AT ENG #1 PYLON INBOARD SIDE AS PER BOEING 767-300 SRM 51-40-02-0G-0 &AMP; AMM 20-11-00-910-02</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,228 hrs · 20,300 cycles

RIGHT WING O/B FLAP I/B SIDE WITH SEAL DAMAGED(<P>REMOVED DAMAGED SEAL AT I/B&NBSP; AREA&NBSP; ON&NBSP; RIGHT WING&NBSP; O/B&NBSP; FLAP. LOCATED, CLEANED, SECURED &AMP; INSTALLED AS PER&NBSP; AMM&NBSP; 20-10-23-964-001. NO FURTHER DEFECTS NOTED.</P>)

Part: SEAL — UNKNOWN (UNKNOWN) · airframe 88,228 hrs · 20,300 cycles

RIGHT WING INBD AFT FLAP WITH SEAL DAMAGED.(<P>REMOVED DAMAGED SEAL LOCATED AT RIGHT WING INBD AFT FLAP. INSTALLED, CLEANED, LOCATED &AMP; SECURED NEW SEAL AS PER&NBSP; BOEING 767-300 AMM 20-10-23-964-001. NO FURTHER DEFECTS NOTED</P>)

Part: SEAL — UNKNOWN (UNKNOWN) · airframe 88,228 hrs · 20,300 cycles

R/W INBD AFT FLAP WITH SEAL DAMAGED.(<P>REMOVED DAMAGED SEAL AT R/W INBD AFT FLAP. INSTALLED, CLEANED, SECURED AND LOCATED NEW SEAL AS PER&NBSP; BOEING 767-300 AMM 20-10-23-964-001. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,228 hrs · 20,300 cycles

NLG LINES OF ACTUATOR CYLINDER WITH EVIDENCE OF HYD LEAK.(<P>CLEANED&NBSP; AREA AS REQUIRED AND TIGHTENED HYDRAULIC LINES ATTACHED TO NOSE LANDING GEAR RETRACT ACTUATOR IAW AMM 32-34-01. NO LEAKS FOUND.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,228 hrs · 20,300 cycles

FWD LOWER CARGO COMPARTMENT DOOR AFT LOWER DOOR HOOK ROLLER STOP/ BEARING DAMAGED ( ROLLER BEARING PARTING OUT )(<P>REPOSITIONED&NBSP; BEARING INSIDE HOUSING,&NBSP; TIGHTENED&NBSP; NUT IN&NBSP; BEARING PIN&NBSP; TO&NBSP; SPECIFIED&NBSP; TORQUE PER 767-300&NBSP; AMM 52-33-10.&NBSP; VERIFIED PULL IN&NBSP; PIN IS&NBSP; 2.50 IN FROM FRAME. OPERATIONAL CHECK IS NORMAL.</P>)

Part: ANTI-ICE VALVE — UNKNOWN (UNKNOWN) · airframe 88,110 hrs · 20,260 cycles

RH WING ANTI-ICE EICAS MSG(<P>T/S REF FIM 30-11 FT 803, R/R RELAY K414, NO HELP. R/R K1155 RELAY, NO HELP. R/R RH WING ANTI-ICE PRESSURE SWITCH REF AMM 30-11-04, NO HELP. RELAY R/R REF AMM 30-11-00. SEE ITEM 3 FOR WORK PERFORMED. LP 1627501 M3: PER MCC REQ, R/R RH WING WANTI-ICE VALVE. OPS TEST FAIL. REMOVED FOR BAD FROM STOCK VALVE REF AMM 30-11-02. SEE ITEM M4 FOR CORRECTIVE ACTION. LP 1627502 M4: INSTALLED RIGHT WING ANTI-ICE VALVE IAW B767 AMM 30-11-02. OPS CHECKS OK AT THIS TIME</P>)

Part: SPLICE PLATE — DAMAGED (FUSELAGE) · airframe 86,282 hrs · 19,638 cycles

LH CENTER WING AT SPLICE PLATE STGR L6 AND LBBL97.42 FUEL LEAK(<P>FUEL LEAK WAS REPAIRED IAW AMM 28-11-00-308-013 REV 137</P>)

Part: FUSE PIN — CRACKED (RT NACELLE) · airframe 86,282 hrs · 19,638 cycles

RH NACELLE PYLON ATTACH FUSE PIN UPPER LINK WITH CRACK INDICATION(<P>FUSE PIN OF UPPER LINK WAS REPLACED IAW AMM 54-51-03-404-030-002</P>)

Part: SPLICE PLATE — DAMAGED (FUSELAGE) · airframe 86,282 hrs · 19,638 cycles

RH CENTER WING, SPLICE PLATES AT ST GRL10 AND RBL97.42 FUEL LEAK(<P>LEAKS WERE REPAIRED IAW AMM 28-11-00-308-013</P>)

Part: SPLICE PLATE — DAMAGED (FUSELAGE) · airframe 86,282 hrs · 19,638 cycles

CENTER WING, RH SPLICE PLATE A ST GR 6 AND RBL97.42 FUEL LEAKS(<P>FUEL LEAKS WERE REPAIRED IAW AMM 28-11-00-308-013</P>)

Part: FAN — NONE · airframe 84,169 hrs

FWD EQUIPMENT SUPPLY FAN 1 INOP(<P>TRANS TO MDDR 156560 MEL 21-58-03-02-01 CAT C DUE DATE 20NOV21.</P> / <P>13NOV21 - 1395705 - ITEM #6 - AFW - REMOVED AND REPLACED FWD EQUIPMENT COOLING SUPPLY FAN 1 IAW AMM 21-58-06. OPS CHECKS GOOD. NO FURTHER DEFECTS NOTED. DMI CLEARED &AMP; MCC NOTIFIED. PLACARDS REMOVED.</P>)

Part: RELAY — NONE

"FWD EQ SUP FAN 1" DISPLAYED ON EICAS STATUS PAGE.(<P>PERFORMED FIM 21-58 FAULT TREE 991. REMOVED AND REPLACED RELAY. C/B RESET OPS CHECK GOOD IAW B767 FIM 21-58 AMM 21-58-00.</P>)

Part: NOSE COWL — NONE · airframe 84,122 hrs · 18,959 cycles

RH ENG NOSE COWL HAS A CRACK 5.325" LONG LE AT 11 O'CLOCK POSITION.(<P>REMOVED AND REPLACED NOSE COWL IAW AMM 71-1-01. OPS CK GOOD.</P>)

Part: FAN — NONE · airframe 84,115 hrs · 18,957 cycles

FWD EQ SUP FAN 1 STATUS MSGAFTER BLOCK IN.(<P>TRANSFERRED TO MDDR 156345 R/R FWD EQUIP SUP FAN 1 IAW B767 AMM 21-58-06 OPS CHECK GOOD.&NBSP;</P>)

Part: NONE — NONE

ON WALK AROUND DETECTED BIRD STRIKE #1 ENGINE(<P><SPAN>COMPLETED WITH INSPECTION FOR ENG #1 FOR BIRDSTRIKE. NO DAMAGE OR INGESTION FOR PRIMARY FLOW OR COMPRESSOR SECTION IN REF AMM 05-51-18, 72-00-00 AND FIM 71-05 F/T 872. NO DAMAGE NOTED AT THIS TIME</SPAN></P>)

Part: NONE — NONE · 18,936 cycles

AFT EQUIPMENT EXHAUST FAN 2 STATUS MESSAGE(<P>TRANSFER TO MDDR #156027 PER MEL 21-58-05, CAT C, DUE 11 NOV 21.</P> / <P>REF LOGPAGE 1391652 - PERFORMED FIM 21-26-FT806. OPS CKS GOOD. THIS CLEARS MDDR 156027.</P>)

Part: NONE — NONE

WHEN SET IN AUTO MODE UNABLE TO ADJUST FLIGHT DECK TEMPERATURE PROPERLY. GOES TO TOO COLD TO TOO HOT(<P>PERFORMED BITE TEST ON ZONE TEMPERATURE MODULE. ALL TEST HAVE PASSED IAW AMM 21-61-00.</P>)

Part: NONE — NONE

FWD EQUIPMENT OVERHEAT ADVISORY @ BLOCK-IN(<P>FOUND "EQUIP COOL FAN SUPPLY 1" CIRCUIT BREAKER ON P6 POPPED. RESET CIRCUIT BREAKER REF B767 AMM 21-58-00 AND EQUIPMENT COOING SYSTEM OPS CHECKS NORMAL AT THIS TIME. NO FAULTS/MESSAGES NOTED ATTHIS TIME. REF FIM 21-58 FT999.</P>)

Part: NONE — NONE

DURING PREFLIGHT, FOUND BOTH RIGHT ENGINE INLET SENSOR SEALS ARE PUSHED OUT SIGNIFICANTLY INTO THE AIRSTREAM POTENTIALLY BLOCKING THE SENSOR(<P>ADJUSTED BOTH R/H ENG INLET SENSOR SEALS IAW ATLAS AIR MX TIP B767 FAN AIR TEMP SENSOR VOL21 ISSUE 6.</P> / <P>OK FOR SERVICE.</P>)

Part: RELAY — NONE

REPEAT WRITE-UP. AUTOMATIC FLIGHT DECK TEMPERATURE CONTROL OPERATES NORMALLY ON THE GROUND BUT UNCONTROLLABLE IN FLIGHT, EVEN WITH TRIM VALVE SET MANUALLY TO FULL COLD. FLIGHT DECK STAYS VERY WARM.(<P>PERFORMED FIM 21-61 FT 917. FIM LEAD TO REPLACE RELAY K238 IN P37 PANEL IAW SWPM 20-81-22. OPS CHECK GOOD AT THIS TIME.</P>)

Part: NONE — NONE

COCKPIT TEMPERATURE CONTROL VALVE HEARD SQUEAKING FOLLOWED BY NO CONTROL OF TEMPERATURE TO COCKPIT.(<P><SPAN>PERFORMED OPS TEST ON A/C SYSTEM COOLING AND HEATING. HEARD NO NOISE, WORKS GOOD AT THIS TIME IAW AMM 21-48-00. COLD AND HOT SETTINGS OK.</SPAN></P>)

Part: NONE — NONE · airframe 83,931 hrs · 18,890 cycles

WITH THE FLT DECK TEMPERATURE CONTROL IN AUTO THE TEMPERATURE VARIES WILDLY WITH NO PILOT INPUT. TEMPERATURE OSCILLATES FROM APPROXIMATELLY 18-26 DEG.(<P>PERF OPS CHECK IAW AMM 21-51-00. OPS CHECK GOOD. NO FLUCTUATION NOTED ON AUTO OR MANUAL FUNCTIONS.</P>)

Part: FIRE LOOP — FAULTED (NR 1)

FIRE LOOP # 1 STATUS MSG WILL NOT CLEAR.(<P>TRANSFER MDDR 155166 PER MEL 26-11-01-01 CAT "C" DUE DATE 25OCT21</P> / <P>18OCT- AFW STA: R&AMP;R #1 ENG FIRE DETECTOR ASSY (LWR AFT) IAW AMM 26-11-01. THIS CLEARS DMI # 155166. PLACARD REMOVED. NO DETECTS NOTED AT THIS TIME.</P>)

Part: NONE — NONE · 18,885 cycles

OXYGEN PRESSURE INDICATING 40 PSI ON STATUS PAGE(<P>TRANSFERED TO DMI 155060 PER MEL 35-11-02-01.</P> / <P>REMOVED AND REPLACED VOLTAGE UNIT IAW AMM 35-11-06. OPS CHECK GOOD. THIS CLEARS MDDR 155060.</P>)

Part: NONE — NONE

STATUS MESSAGE: FWD EQ SUP FAN 1(<P>FOUND CB P6 "FWD EQ COOL SUPPLY FAN 1" POPPED. RESET CB IAW AMM 29060-01. PERFORMED OPS CHECK OF EQUIP COOLING IAW AMM 21-58-00/OPS CHECK GOOD. NO STATUS MSG PRESENT, NO (CB) BREAKERS POPPED.</P> / <P>LP 1313395: ITEM M5: TRANSFERRED TO MDDR # 155081 IAW MEL # 21-58-03-02-01, CAT C DUE DATE: 23OCT21, MX ACTION C/W. DISPATCHER: LC 1545Z.</P> / <P>16OCT- STL MX: LP 1313406, ITEM M3: R/R FWD EQP. SUPPLY FAN 1 C/B ON P-6 PANEL IAW B767 AMM 24-22-03. OPS CHECK GOOD. THIS CLEARS DMI 155081. ACL 0029Z</P>)

Part: NONE — NONE · 18,871 cycles

DURING CLIMB AFTER 10000' OUR AIRSPEED INDICATOR LIMIT VMO DID NOT GO ABOVE 265KTS. DX AND MX REQUESTED DIVERSION TO CVG(<P>FOUND VMO (5591) SWITCH IN MEC IN THE ALTERNATE POSITION, PLACED SWITCH BACK IN NORM POSITION IAW AMM 32-00-00.</P>)

Part: NONE — NONE · 18,863 cycles

AFTER SHUTDOWN WE RECEIVED AN EQUIPMENT OVHT LIGHT WITH FWD EQ SUP FAN 1 MSG(<P>PERFORMED OPERATIONAL TEST OF FWD RACK SUPPLY FAN. OPS CHECK GOOD, NO DEFECTS NOTED AT THIS TIME.</P>)

Part: IGNITER — WARNING MESSAGE · airframe 83,846 hrs

STATUS MESSAGE "R ENG INGITOR 2" STATUS MESSAGE "R ENG IGNITOR 2" CLEARED PER AMM 71-00-00, OPS CHECK GOOD.

Part: IGNITER — INOPERATIVE · airframe 83,836 hrs

STATUS MESSAGE "R ENG IGNITOR 1" DISPLAYED AFTER ENGINE START.TRANSFERRED TO MDDR 154325 PER MEL 74-00-01A CAT A DUE DATE: 30SEP21.LOG PAGE 1391753: R&R RH ENGINE #1 IGNITER IAW AMM 74-21-02. OPS CHECK GOOD. NO STATUS MSG AT THIS TIME, THIS CLEARS MDDR #154325.

Part: APU — INOPERATIVE

APU PNUMATICS INOP.(<P>TRANSFERRED TO MDDR 153880 IAW MEL 49-11-01-01, CAT C, DUE DATE 01OCT21.</P> / <P>23SEP, LP 1390926, ITEM M4: REF ITEM 3 OF LP 1390925. C/W ENGINE RUNS IAW AMM 71-00-00, NO FAULTS NOTED IN APU DUCT PRESSURE. APU DUCT PRESSURE NORMAL AT THIS TIME IAW 49-00-00. DMI 153880 CLEARED. PLACARDS REMOVED.</P>)

Part: IGNITER — INOPERATIVE

RIGHT ENGINE IGNITION 2 INOP(<P>REMOVED EXISTING FOR RH ENGINE AND INSTALLED NEW EXCITER IAW B767 AMM 74-11-01, NO HELP. ITEM PLACED ON DMI # 157527 PER MEL 74-00-01B, CAT C, DUE DATE: 25SEP21. DISPATCH: ACL @ 0150Z.</P> / <P>16SEP21 - 1395764 - ITEM # 3 - CVG - R/R #2 ENG #2 IGNITOR PLUG IAW AMM 74-21-02. OPS CHECK GOOD. NO EICAS MSG NOTED. THIS ACTION CLEARS DMI.</P>)

Part: RELAY — FAULTED (COOLING FAN)

EQUIPMENT COOLING OVHT LIGHT ON AUTO W/ FWD EQ SUP FAN 1 MSG. EQUIP COOLING STANDBY OPERATES NORMAL(<P>ITEM PLACED ON MDDR 153052 PER MEL 1-58-01-01, CAT C, DUE DATE 15 SEP 21. EQUIP COOLING SET TO STBY MODE.</P> / <P>CVG MX, 09SEP, LP 1430476, ITEM M4: REMOVED AND REPLACED RELAY K343 IAW FIM 21-58 FT 991 STEP 25. AND SWPM 20-81-22. OPS CHECK PERFORMED IAW AMM 21-58-00, OPS TEST OKAY. THIS CLEARS DMI # 153052. TIME/INIT: BM @ 1605Z</P>)

Part: TRANSCEIVER — FAULTED (WX RADAR SYS)

WXR SYS STATUS MESSAGE. INTERMITTENT WXR FAIL FLAG ON HSI WITH RIGHT WX RADAR SYS SELECTED(<P>TS PER FIM 34-43 FT 805 FAULTED RT WXR XCVR. REMOVED AND REPLACED RT WXR XCVR IAW AMM 34-43-01. OPS CHECKS OK, NO DEFECTS NOTED</P>)

Part: FAN — INOPERATIVE (FWD EQUIP BAY) · 18,772 cycles

FWD EQUIPMENT SUPPLY FAN 1 INOP. TROUBLESHOT FAULT TREE 991. REMOVED AND REPLACED FWD EQ SUPPLY FAN 1 B10. IAW AMM 21-58-06. NO FAULTS AT THIS TIME.

Part: GCU — FAULTED (RT GENERATOR) · airframe 83,554 hrs · 18,759 cycles

R GEN DRIVE EICAS MSG IN-FLIGHT. R GEN DRIVE DISCONNECTED AS PER QRH.(<P>REMOVED AND REPLACED R ENG GCU PER AMM 24-22-02. OPS CHECK GOOD. PERF R ENG IDLE RUN. NO MSG IN VIEW OR DEFECTS NOTED. INSPECTED &AMP; VERIFIED I.D.G AT PROPER LEVEL PER AMM 12-13-03. SYSTEM OK.</P>)

Part: LENS — BROKEN (SWITCH)

RIGHT AFT BOOST PUMP LENS BROKEN."PRESS" LIGHT INOP(<P>TRANSFERRED TO MDDR 151558 PER MEL 28-42-01-01, CAT C, 19AUG21. DISP DC 0611Z</P> / <P>LP 1440453 ITEM 1 - CVG - REMOVED AND REPLACED KORRY SWITCH LIGHT ASSY IAW AMM 33-13-00. OPS CHECK GOOD. THIS CLEARS DMI 151558. MCC NOTIFIED. PLACARDS REMOVED.</P>)

Part: RADAR — FAULTED (WX SYSTEM)

IN FLIGHT RECEIVED WX FAIL ON BOTH HSI AND STATUS MSG WXR SYS , USING RIGHT SYSTEM. WENT BACK TO RIGHT SYS LATER IN FLIGHT AND IT WORKED BUT DIDN'T PAINT GROUND RETURNS , LIKE LEFT SYS DOES.(<P>TRANSFER TO MDDR # 151474 IAW DDG 34-43-01 CAT D DUE DATE 05 DEC 21.</P> / <P>RIV MX, 08AUG, LP 895950, ITEM M4: PERFORMED FIM 34-43 F/T 805 UP TO BLOCK 3. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. THIS CLEARS THIS DMI 151434, PLACARDS REMOVED. DISP- SD @ 1831Z</P>)

Part: FAN — FAILED

FWD EQUIP SUP FAN EICAS MSG WHEN IN AUTO. PERFORMED FIM 21-58 FT 991. REMOVED AND REPLACED FWD RACK SUPPLY FAN #1 IAW 21-58-06 PER BLK 21. OPS CKS GOOD AT THE THIS TIME. NO MSG DISPLAYED.

Part: WARNING MESSAGE — FALSE ACTIVATION (FWD EQUIP)

AFTER LANDING FWD EQUIP OVERHEAT, WITH FWD EQ SUP FAN 1 STATUS MDG DISPLAYED(<P>PERFORMED TROUBLESHOOTING IAW B767 FIM 21-58 FAULT TREE 991 BLOCK 1. VERIFIED BOTH C/B'S IN. REMOVED ELECTRICAL POWER FROM A/C AND MOVED SWITCH IN AUTO. SUPPLIED ELECTRICAL POWER TO A/C. FWD EQ SUP FAN 1 WENT AWAY. VERIFIED IN STANDBY MODE MESSAGE NOT SHON. FAN 1 OPERATES AND C/B'S NOT POPPED. SYSTEM OPERATES NORMAL. A/C OK FOR CONTINUED SERVICE</P>)

Part: CONTAINER — INOPERATIVE (C/P OXYGEN MASK)

FIRST OBSERVERS EMERGENCY O2 MASK INOP(<P>FIRST OBSERVERS SEAT AND EMERGENCY EQUIPMENT TRANSFERED TO MDDR # 151177 PER B 767 MEL 25-11-02-01A&NBSP; CAT A DUE DATE 04 AUG 21</P> / <P>LP 895909 ITEM 5&NBSP; REINSTALLED FIRST OFFICERS O2 MASK MASK BOX IAW&NBSP; AMM 35-11-51-004-009. REMOVED AND REPLACED O2 MASK ASSY IAW 35-11-51-004-059 AND 35-11-51-404-060. OPS CK GOOD&NBSP; MDDR 151177 CLEARED.&NBSP; MCC NOTIFIED. PLACARD REMOVED&NBSP;</P>)

Part: RADAR — MALFUNCTIONED (WX SYSTEM)

LEFT WEATHER RADAR INOP CONSTANTLY PAINTS GROUND(<P>PERFORMED OPERATIONAL CHECK ON L AND R WEATHER IAW AMM 34-43-00, COULD NOT DUPLICATE ON GROUND. MCC NOTIFIED.</P>)

Part: A/C PACK — FAULTED (RIGHT)

RIGHT PACK UNABLE TO COOL FLIGHT DECK EVEN INFLIGHT(<P><SPAN>FOUND R/H PACK TEMP CONTROLLER FAULT. SWAPPED L/H PACK TEMP CONTROLLER (PN: 625946-9 SN: 088C-3294) WITH R/H PACK TEMP CONTROLLER (PN: 625946-9 SN: 041C-3656). R/H PACK OPS NORMAL OK FOR SERVICE.</SPAN></P>)

Part: CONTACTOR — FAULTED (APU STARTER) · airframe 83,280 hrs · 18,671 cycles

APU WOULD NOT START AT BLOCK IN. EICAS MESSAGE APU FAULT BOTH TIMES.(<P>PERFORMED APU BITE PROCEDURE REF B767 FIM 49-11 FT 987. FOUND MINIFLAG 34 AND "START ABORTED" MESSAGE. PERFORMED B767 FIM 49-11 FT 989 AND FOUND NO FURTHER DEFECTS. RESET ECU AND STARTED APU ON FIRST ATTEMPT SATISFACTORY. ALL APU PARAMETERS NORMAL. OK TO CONTINUE.</P> / <P>LP 1393836, ITEM M5: APU INOP PER ENGINEERING'S REQUEST. TRANSFERRED TO MDDR # 150135 PER MEL 49-11-01A, CAT "C". DUE: 23JUL21. PLACARDS INSTALLED. MCC ADVISED. DISPATCH: JT 21:22Z.</P> / <P>LOGPAGE 1343113 ITEM 5 AND LOGPAGE 1343114 ITEM 8: REMOVED AND REPLACED APU OIL TEMP SWITCH IAW AMM 49-27-14. LEAK CHECK GOOD. SEE LP 1343113 ITEM M7 FOR FURTHER WORK. REMOVED AND REPLACED APU CRANK CONTACTOR IAW AMM 49-41-05. OPS CHECK GOOD.

Part: HEAT EXCHANGER — FAULTED (LT A/C PACK) · airframe 83,265 hrs · 18,667 cycles

AFTER T/O LEFT PACK OFF & LEFT PACK TEMP EICAS MESSAGES. RAN QRH, CONTINUED FLT IN STANDBY MODE (N). FOUND CONNECTOR D2152 ON /H PACK TO BE FAULTY. REMOVED AND REPLACED LH PACK PRIMARY HEAT EXCHANGER IAW B767 AMM 21-51-02 OPS CHECK GOOD. P/N OFF: 194270-3, REMOVED AND REPLACED LH PACK SECONDARY HEAT EXCHANGER IAW AMM 21-51-02, OPS CHECKED GOOD. OPS CHECK, LEAK CHECK GOOD.

Part: APU — FAULTED

APU RELIABILITY COLD START ACCOMPLISHED ON FLT LEG ONT-CVG SAT -48°C FL 370 START UNSUCCESSFUL ON 3 ATTEMPTS. APU FAULT MESSAGE OCCURRED DURING APU RELIABILITY COLD START(<P>ITEM# 1 - ENG SNAPSHOT INFO NOTED BY MX. SEE NEXT DISC. ITEM FOR APU COLD SOAK FAIL..</P> / <P>ITEM# 2 - PERFORMED 3 SUCCESSFUL APU STARTS ON THE GROUND. APU REMAINS OPERATIONAL, NO DEFECTS FOUND REF AMM 49-11-00. APU COLD SOAK DMI 149804 REMAINS OPEN.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT A/C PACK)

L PACK OVHT WITH L PACK OFF(<P>PERFORMED BITE AND OPS CHECK ON L PACK SYSTEM, NO DEFECTS OR FAULTS NOTED, SYSTEM OPS CHECK NORMAL IAW AMM 21-51-00</P>)

Part: WARNING MESSAGE — FALSE INDICATION (LT PACK TEMP) · airframe 83,223 hrs · 18,656 cycles

L PACK TEMP EICAS AT FL410(<P>ITEM TRANSFERED TO DMI #149571 IAW MEL 21-51-03-01.</P> / <P>LP 1486008: PERFORMED FIM 21-51 FAULT TREE 844, NO FAULTS NOTED. PERFORMED BIT CK PACK #1 IAW AMM 21-51-14. ALL CKS GOOD, THIS CLEARS MDDR 149571.</P>)

Part: CONTROLLER — UNKNOWN (A/C PACK TEMP)

LEFT PACK TEMP INOP IN AUTO(<P>PEFORMED PACK TEMP CONTROLLER BITE PER AMM 21-51-00. OPS TEST GOOD AT THIS TIME.</P>)

Part: APU — UNKNOWN · airframe 83,192 hrs

APU FAULT(<P>PERFORMED APU BITE PROCEDURE ON APU CONTROL UNIT. NO FAULT MESSAGES NOTED IAW AMM 49-11-00-502-002. VERIFIED APU FAULT LIGHT DID NOT ILLUMINATE, NO DEFECTS NOTED AT THIS TIME. OPS CHECKED GOOD.&NBSP;&NBSP;</P>)

Part: FAN — FAILED (EQUIP BAY) · airframe 83,166 hrs · 18,638 cycles

FWD EQ SUP FAN 1(<P>FOUND FWD SUPPLY FAN BREAKER TRIPPED, RESET AND REPLACED FWD EQUIP SUPPLY FAN (B10) IAW AMM 21-58-06. OPS NORMAL</P>)

Part: A/C PACK — OVERTEMP (LEFT) · airframe 83,159 hrs

L PACK OFF/ L PACK TEMP EICAS F390, QRH LEAD TO PACK RESET AND STANDBY N POSITION, AFTER PACK RESET EICAS WENT AWAY.(<P>PLACED ON MEL 21-51-01-01 PER MDDR # 148879, CAT C, DUE: 29JUN21, MX ACTION C/W, PLACARD INSTALLED, MCC NOTIFIED. NO FAULTS ON BITE PER FIM 21-51 FT 855.</P>)

Part: APU — FAULTED · airframe 83,111 hrs · 18,618 cycles

APU FAULT 3 START ATTEMPTS(<P>PERFORMED APU ECU BITE CK PER AMM 49-61-05, NO FAULTS NOTED. ATTEMPTED APU START, SUCCESSFUL FIRST ATTEMPT. NO PRESENT OR PREVIOUS FAULTS NOTED. TRANSFERRED TO MDDR 148521 IAW DDG 25-AP-01, OPTION C, CAT N, DUE 14JUN22.</P> / <P>14JUNE21 - LP 1138016 - ITEM# 1 - ROC - APU COLD SOAK ACCOMPLISHED ON FLT. ONT-RFD SAT -48 FL370. START SUCCESSFUL ON FIRST ATTEMPT. THIS CLEARS MDDR 148521.</P>)

Part: NONE — NONE (WX RADAR) · airframe 83,051 hrs · 18,605 cycles

L WX RADAR TILT SEEMS OFF BY APPROX 2° VERSUS R. RIGHT SIDE SEEMS CORRECT(<P>PERFORMED WEATHER RADAR SYSTEM TEST IAW AMM 34-43-00. NO DEFECTS NOTED AT THIS TIME. SYSTEM TEST GOOD.</P>)

Part: SEAT TRACK — CORRODED (COCKPIT) · corrosion level 2 · airframe 83,024 hrs · 18,595 cycles

FLIGHT DECK CAPT SEAT R/H FWD SEAT TRACK CORRODED(<P>REMOVED AND REPLACED SEAT TRACK ON FLIGHT DECK CAPT SEAT R/H FWD IAW B767 SRM 51-40-02 AND B767 AMM 25-11-01-822-095-001 PN 1A098-0103 PO# 1499B-00026</P>)

Part: SKIN — DELAMINATED (RT NR 8 SLAT) · airframe 83,024 hrs · 18,595 cycles

RH WING #8 SLAT UPPER SURFACE OF TE WEDGE IS DELAMINATED AT IB UPPER CORNER OF SLAT. DOT 005(<P>REPAIRED UPR SURFACE OF #8 SLAT TE WEDGE IB UPR CORNER IAW B767 SRM 57-43-02-01-01, 51-70-10 REP.4</P>)

Part: SHEAR WEB — CORRODED (BS 1330) · corrosion level 2 · airframe 83,024 hrs · 18,595 cycles

AFT CARGO COMPARTMENT FLOOR SHEAR WEB HAS AREA OF CORROSION AT BONDING JUMPER ATTACH AREA BS 1330 RBL 40. DOT 016(<P>UPON EVAL. OF FLOOR SHEAR WEB STA. 1330 RBL 40. FOUND 100% OUT OF LIMITS IAW B767 SRM 51-70-13-0G-0.&NBSP; REMOVED AND REPLACED SHEAR WB IAW B767 SRM 53-60-53-01-1 LOCATED IN AFT PIT<BR /></P>)

Part: FLOORBEAM — CORRODED (BS 1345 RBL55) · corrosion level 2 · airframe 83,024 hrs · 18,595 cycles

AFT CARGO COMPARTMENT FLOOR PANEL ATTACH ANGLE IS CORRODED AT BS 1345 RBL 55. DOT 014(<P>UPON EVAL. FLOOR PNL ATTACH ANGLE AT STA. 1345 RBL 55 HAS 100% MAT. LOSS AND OUT OF LIMITS IAW B767 SRM 53-00-15-1A-1. REMOVED AND REPLACED ANGLE IAW BOEING DWG. 146T5001 REV. M,F</P>)

Part: SKIN — CORRODED (BS 1310 S34L) · corrosion level 2 · airframe 83,024 hrs · 18,595 cycles

BUBBLE PAINT EXTERIOR SKIN STA. 1310 STR. 34L SECTION 48. DOT 88-003(<P>UPON EVALUATION FUSELAGE SKIN AT STA. 1310 STR. 34L FOUND TO BE EXFOLIATED 100% MATERIAL LOSS. CUTOUT DAMAGE AND APPLIED A FILLER/DOUBLER REPAIR IAW B767 SRM 53-00-01-2R-1, 53-00-01, 51-10-02, 51-40-02, 51-21-00, 51-40-05, 51-40-08, AMM 51-21-10, SOPM 20-41-02</P>)

Part: DOOR SILL — GOUGED (BS 522) · airframe 83,024 hrs · 18,595 cycles

MAIN CARGO DOOR SILL GOUGED AT BS 522. DOT 99/035(<P>UPON EVALUATION OF DAMAGE AT MAIN CARGO LWR SILL STA. 522 FOUND OUT OF LIMITS IAW B767 SRM 53-00-15-1A-1.&NBSP; REPAIRED LWR SILL STA 522 IAW FAS EA 21051 REV. IR</P>)

Part: BEAR STRAP — CORRODED (BS 478-481) · corrosion level 2 · airframe 83,024 hrs · 18,595 cycles

C-1 DOOR CUT-OUT , UPPER FWD CORNER HAS EXFOLIATING CORROSION ON INNER SKIN.(<P>REMOVED CORROSION FROM C-1 DOOR CUT-OUT UPR BEAR STRAP FWD CORNER AND FOUND OUT OF LIMITS IAW B767 SRM 53-00-01-1A-1.&NBSP; REPAIRED UPR BEAR STRAP FWD CORNER IAW FAS EA 21050 REV. IR</P>)

Part: SEAT TRACK — CORRODED (COCKPIT) · corrosion level 2 · airframe 83,024 hrs · 18,595 cycles

FLIGHT DECK F/O SEAT L/H FWD SEAT TRACK CORRODED FWD R/H SIDE(<P>REMOVED AND REPLACED FO FWD IB SEAT TRACK PN 1A098-104 PO 1499B-00038 IAW B767 AMM 25-11-01-822-095-001.</P>)

Part: SPLICE ANGLE — CRACKED (BS 1577) · airframe 83,024 hrs · 18,595 cycles

AREA AFT OF BULK CARGO COMPT STA. 1577 RH OB SIDE WL 200 MAIN DECK FLOOR SUPT OB SPLICE ANGLE CRACKED 1IN IN LENGTH ON BOTTOM. DOT 127-013(<P>REMOVED CRACKED SPLICE ANGLE AT AFT OF BULK CARGO COMPT STA 1577 RH OB SIDE WL 200 MAIN DECK FLOOR SUPT OB SIDE IAW B767-300 SRM 51-40-02.&NBSP; FABRICATED NEW SPLICE ANGLE DIM 3"5" IAW B767-300 SRM 51-40-05 AND BOEING DWG 146T5651 REV.-. INSTALLED NEW SPLICE ANGLE IAW B767-300 SRM 51-40-02</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (EQUIP OVERHEAT) · airframe 82,977 hrs · 18,580 cycles

FWD EQPT OVHT UPON LANDING.(<P>TRANSFERRED TO DMI # 146288 MEL 21-58-03-02-01 CAT C DEFERRAL DUE DATE 12MAY21.</P><P>REF MDDR 146288 REF LOG PG # 1465089 ITEM M9 . TS PER FIM TASK 21-58 FT 991, NO FAULTS NOTED, UNABLE TO DUPLICATE FAULT. PERFORMED OPS CHECK OF FWD/AFT EQUIPMENT COOLING SYSTEM AMM 21-58-00.&NBSP; NO DEFECTS NOTED, THIS CLEARS MDDR 146288 PLACARDS REMOVED , MCC NOTIFIED.</P><P><BR DATA-MCE-BOGUS="1" /></P>)

Part: WARNING MESSAGE — FALSE INDICATION (EQUIP OVERHEAT) · airframe 82,981 hrs

FWD EQUIP OVHT UPON LANDING(<P>FWD EQUIP SUPPLY FAN TRANSFERRED TO MDDR 146288 IAW MEL 21-58-03-02-01.</P><P>2MAY2021 -&NBSP;1465089 ITEM #10 -&NBSP;TS PER FIM TASK 21-58 FT 991 NO FAULTS NOTED UNABLE TO DUPLICATE FAULT. PERF OPS CHECK OF FWD/AFT EQUIPMENT COOLING SYSTEM IAW AMM 21-58-00 NO DEFECTS NOTED. THIS CLEARS MDDR 146288 PLACARD REMOVED MCC NOTIFIED.</P>)

Part: CONNECTOR — DIRTY (EQUIP SUPPLY FAN) · airframe 82,820 hrs · 18,544 cycles

EICAS STATUS MSG. "FWD EQ SUP FAN 1". CB'S (2) COLLARED SYSTEM SWITCHED TO STBY DISPATCH JT @ 0421Z. LP 1066388: T/S PER FIM 21-58 FT 991 AND 21-58 FT 983. B767 AMM 21-58-10. CHECKED AIR INLET AIR GRILL, CLEANED CONNECTOR D446 AND OPS TESTED FWD EQUIPMENT COOLING SYS. NO FAULTS NOTED. THIS CLEARS DMI 145046. MCC NOTIFIED. PLACARDS REMOVED.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT A/C PACK TEMP) · 18,527 cycles

AT FL 400 L PACK TEMP EICAS MESSAGE FOLLOWED BY L PACK OFF.&NBSP; ACCOMPLISHED QRH AND RESET PACK. PACK LIGHTS EXTINGUISHED AND CONTINUED IN STBY.(<P>PERFORMED BITE TEST ON L PACK TEMP CONTROLLER BOX 1. NO FAULTS NOTED AND OPS CHECK OF L PACK GOOD IAW B767 AMM 21-51-14.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT A/C PACK) · airframe 82,755 hrs · 18,518 cycles

AT FL 400 L PACK TEMP EICAS MESSAGE FOLLOWED BY L PACK OFF. ACCOMPLISHED QRH AND RESET PCK. PACK LIGHTS EXTINGUISHED AND CONTINUED IN STBY N.(<P>PERFORMED BITE TEST ON L PACK TEMP CONTROLLER BOX, NO FAULTS NOTED. OPS CHECK OF L PACK GOOD. IAW B767 AMM 21-51-14.

Part: WARNING MESSAGE — FALSE ACTIVATION (A/C PACKS) · airframe 82,740 hrs · 18,510 cycles

L PACK INOP AND L PACK TEMP EICAS DISPLAYED ENROUTE AT CRUISE FL390, STANDBY "N" SELECTED PER QRH, PACK RESET SWITCH PUSHED AND EICAS REMAINED CLEARED WITH STANDBY *N* SELECTED.(<P>PERFORMED FIM TASK 21-51 FT 844. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.</P>)

Part: RADAR — MALFUNCTIONED (WX SYS) · airframe 82,686 hrs · 18,497 cycles

R WXR RADAR FAIL IN FLIGHT(<P>ACCOMPLISHED WXR OPERATIONAL TEST IAW ATLAS AMM TASK 34-43-00-715-026-002. OPS CHECK GOOD. NO FURTHER MX ACTION REQ.</P>)

Part: LINER — CRACKED (COMBUST CHMBR) · airframe 82,609 hrs · 18,474 cycles

ENGINE # 2 S/N 702954 COMBUSTION CHAMBER OUTER LINER BETWEEN 7 TO 8 O'CLOCK POSITION HAS A TWO PANEL CRACK BETWEEN PANEL # 1 AND PANEL #&NBSP; 2. REQUIRES RE-INSPECTION EVERY 200 CYCLES PER W/C # A-72-307-C1-2 TABLE 3(<P>TRANSFERRED ITEM TO MCI A-001</P>)

Part: FILTER ELEMENT — WARNING MESSAGE (LT ENGINE FUEL) · airframe 82,563 hrs · 18,456 cycles

ON CLIMB OUT RECEIVED "L ENG FUEL FILT" EICAS MSG. COMPLIED W/QRH PROC. ALL ENG. INDICATIONS NORMAL. ASSC. STATUS MSG. RECEIVED.(<P>REMOVED AND REPLACED L ENGINE FUEL FILTER ELEMENTS IAW FIM 73-11 FT 803 AND 73-11-02, NO FAULTS NOTED. LEAK CHECK GOOD.</P>)

Part: IDG — MALFUNCTIONED (RIGHT) · airframe 82,580 hrs · 18,463 cycles

"R GEN DRIVE" EICAS MANUALLY DISCONNECTED RIGHT GENERATOR DRIVE.(<P>PLACED ON&NBSP;MDDR 143574 IAW MEL 24-00-01-01, CAT B.</P><P>CVG MX, 10MAR21 LP 1345596, ITEM M2: REMOVED AND REPLACED R/H ENG IDG. REF B767 AMM 24-11-01. OPS CHECK IS SATISFACTORY. THIS CLEARS DMI 143574. W. O. 78194 C/W. PLACARDS REMOVED. DISPATCH DP @ 1750Z</P>)

Part: FILTER — WARNING MESSAGE (RT ENGINE FUEL) · airframe 82,580 hrs · 18,463 cycles

ON CLIMB OUT RECEIVED "R ENG FUEL FILT" EICAS MSG. COMPLIED W/ QRH. ALL ENGINE INDICATIONS NORMAL.(<P>REMOVED AND REPLACED&NBSP;RH ENG FUEL FILTER IAW AMM 73-11-02. PERFORMED IDLE RUN OF RH ENG IAW AMM 71-00-00. NO MESSAGES NOTED AT THIS TIME. NO LEAKS NOTED OPS CHECK GOOD.</P>)

Part: ECU — INOPERATIVE (APU) · airframe 82,521 hrs · 18,443 cycles

APU PNUEMATICS INOP(<P>TRANSFER TO MDDR #143232, CAT C, PER DDG 49-11-01-01. DUE 12 MAR21. PLACARDS INSTALLED, MX ACTION COMPLIED WITH.</P><P>LP 1254846: T/S PER FIM 49-11 FT A21 FIG 130. NO MINI FLAG. REMOVED AND REPLACED ECU. OPS CHECK GOOD IAW AMM 49-61-05. THIS CLEARS DMI 143232. PLACARDS REMOVED. MCC NOTIFIED.</P>)

Part: SENSOR — FAULTY (APU) · airframe 82,540 hrs · 18,449 cycles

APU INOP TRANSFERRED TO MDDR 143164 IAW MEL 49-11-01A, CAT C. PERFORMED APU BITE. IAW FIMM 49-11, FAULT 16, P2 SENSOR. REMOVED AND REPLACED P2 SENSOR. IAW AMM 49-61-04. DURING T/S FOUND APU OIL OVER SERVICED. SERVICED APU OIL TO PROPER LEVEL. IAW AMM 12-13-04. PERFORMED APU OPS CHECK GOOD MULTIPLE STARTS SUCCESSFUL. THIS CLEARS MDDR #143164. PLACARD REMOVED. MCC NOTIFIED.

Part: SEAL — NOT REPORTED (DUCT) · airframe 82,463 hrs · 18,427 cycles

PER MCC REQUESTED REPLACE LT DUCT INST BODY CROSSOVER AIR SUPPLY SYS(DUCT ONLY) SEALS PN 460-500 ON ASSY PN 14A640-101(<P>REMOVED AND REPLACED DUCT SEAL ON ASSY PN 14A640-101 ON LT DUCT BODY CROSSOVER AIR SUPPLY SYSTEM. IAW AMM 21-51-02 , SUB TASK 21-51-02-434-032. NO LEAKS NOTED AT THIS TIME.</P>)

Part: HEAT EXCHANGER — FAILED (LT A/C PACK) · airframe 82,452 hrs · 18,425 cycles

AFTER TAKE OFF, L PACK TEMP FOLLOWED BY L PACK OFF EICAS W/ ASSOCIATED OVHD PANEL LIGHTS IN AUTO (T/S IAW WITH FIM 21-51-848. L PACK TEMP CONTROLLER DID NOT PICK UP FAULT. LP 1480531 ITEM 4 -DURING SYS TEST/INSPECTION IAW 21-51-00 TEMP CONTROL VALVE INDICATION ON L PACK WOULD BLANK WHEN PLACED TO STANDBY W, REMOVED AND REPLACED TEMP CONTROL VALVE (OFF PART: PN HG1050AE15, SN 97021877) IAW 21-51-12, OPS CHECK GOOD. LP 1480533 - ITEM 8; REMOVED AND REPLACED L PACK TEMP PRIMARY HEAT HX CHANGER PRECAUTIONARY DUE TO HIGHER OUT TEMP THAN R PACK. IAW 21-51-02, OPS CHECK NORMAL. LP 1480534 ITEM 10; REMOVED AND REPLACED L PACK TEMP OVERHEAT SENSOR S48 IAW 21-51-12 OPS CHECK NORMAL. LP 1480534 ITEM 11- UPON OPS CHECK OF L PACK, FOUND SLIGHT DUCT LEAK POINTED DIRECTLY AT L PACK OUT SWITCH, REMOVED DUCT AND INSPECTED SEALS FOR DAMAGE, NO DAMAGE NOTED, CLAMP WAS IMPROPERLY INSTALLED, REINSTALLED CLAMPED IAW AMM SUBTASK 21-51-02-434-032. NO LEAKS NOTED, OPS NORMAL.)

Part: IGNITER — FAILED (APU) · airframe 82,447 hrs · 18,423 cycles

APU NO LIGHT OFF. REMOVED AND REPLACED APU IGNITER PLUG IAW AMM 49-41-02. OPS CHECK GOOD AT THIS TIME.

Part: PACKING — LEAKING (SENSE LINE) · airframe 82,406 hrs · 18,409 cycles

NUMBER 1 ENG PRVC SENSE LINE LOC C FITTING HAS A LEAK. REMOVED AND REPLACED PACKING AT LOC E AS PER EO NR 1936A088. NO LEAKS NOTED.

Part: CLAMP — BROKEN (HEAT EXCHANGER) · airframe 82,406 hrs · 18,409 cycles

ONE EA BROKEN CLAMP AT NR 1 ENG I/B SIDE AFT OF HEAT EXCHANGER (PNEUMATIC LINE FOR HPSOV ) (REMOVED AND REPLACED CLAMP AT NR 1 ENG I/B PNEUMATIC LINE FOR HPSOV AS PER B767-300 AMM 70-50-01.)

Part: IRS — FAILED (LEFT) · airframe 82,406 hrs · 18,409 cycles

LEFT IRS FAIL ON TAKE - OFF. PERFORMED L IRS NNC. REPLACED TROLH M159 AND OPS TEST OK AMM 34-21-01.

Part: PACKING — LEAKING (NR 1 ENGINE) · airframe 82,406 hrs · 18,409 cycles

NUMBER 1 ENG LEAK AT PRVC ACTUATOR PRESSURE TUBE LOC K. REMOVED AND REPLACED PACKING AT LOCK AS PER EO NR 1936A088. NO LEAKS NOTED.

Part: SERVO — INOPERATIVE (LT AUTOPILOT) · airframe 82,406 hrs · 18,409 cycles

LT AUTO PILOT INOPERATIVE. AUTO PILOT SYSTEMS, ONE INOPERATIVE. NOTIFY DISPATCH. A/C CAT III REST. PERFORMED FAULT TREE 22-03 MCDP G/T 08 SERVO ELEV. FAIL L ELEV. AP SERVO M271; SERVO ELEV LT M271 ON ORDER. REMOVED AND REPLACED ELEV & LT AUTO PILOT SERVO PER MM 22-12-01.424-019. PENDING CHK; PERFORMED LT SERVO INSTALLATION &TEST OK PER AMM 22-12-1. PERFORMED GND TEST 40; AUTO LAND PASS PER AMM FIM 22-03 TASK 820 MDDR NR 142044 CLEARED UP PLACARD REMOVED.

Part: PACKING — LEAKING (NR 2 ENGINE) · airframe 82,406 hrs · 18,409 cycles

NUMBER 2 ENG LEAK AT PRVC ACTUATOR PRESSURE TUBE LOC K. REMOVED AND REPLACED PACKING PER ENGINEERING ORDER NR 1936A088 AT PRVC ACTUATOR PRESSURE TUBE LOCK.

Part: PRESSURE SENSOR — FAULTED (APU BLEED SYSTEM) · airframe 82,406 hrs · 18,409 cycles

APU BLEED SYSTEM INOPERATIVE. REMOVED AND REPLACED APU COMP INLET PRESS SENSOR IAW 767 AMM 49-61-04. OPS CHK GOOD.

Part: SEAL — BROKEN (CONTAMINATE BAG) · airframe 82,406 hrs · 18,409 cycles

COCKPIT AVSAX CONTAINMENT BAG VACUUM SEAL IS BROKEN PN AS-002-1. REMOVED AND REPLACED AVSAX CONTAINMENT BAG AS REQUIRED PER AMM 25-13-00 CK'D OK.

Part: SEAL DEPRESSOR — DAMAGED (MD CARGO DOOR) · airframe 82,406 hrs · 18,409 cycles

MAIN DECK CARGO DOOR. LOWER LEFT SIDE CORNER DEPRESSOR SEAL DAMAGED. REMOVED DAMAGED LOWER CORNER SEAL DEPRESSOR. DRILLED DEBURRED & INSTALLED NEW SEAL DEPRESSOR AT M/D DOOR CUTOUT PER B767-300 SRM 51-40-02-0G-0 AND AMM 20-11-00-910-802.

Part: PACKING — LEAKING (NR 2 ENGINE) · airframe 82,406 hrs · 18,409 cycles

NUMBER 2 ENG LEAK AT HPC SIGNAL PRESSURE TUBE LOC N. REMOVED AND REPLACED PACKING PER ENGINEERING ORDER NR 1936A088 AT HPC SIGNAL PRESSURE TUBE LOC N.

Part: DEPRESSOR — DAMAGED (CARGO DOOR SEAL) · airframe 82,406 hrs · 18,409 cycles

MAIN CARGO DECK SEAL DEPRESSOR DAMAGED AFT MIDDLE. FOUND TO BE WITHIN LIMITS PER SRM 53-06-15-1A-1. REMOVED AND REPLACED DAMAGED SEAL DEPRESSOR AT M/D CARGO DOOR CUT OUT DRILLED DEBURRED; INSTALLED NEW SEAL DEPRESSOR AND PAINTED PER B767-300; SRM 51-40-02-0G-0 AND AMM 20-11-00-910-802.

Part: AUTOBRAKE SYS — MALFUNCTIONED · airframe 82,406 hrs · 18,409 cycles

AUTO BRAKES INOPERATIVE. PERFORMED AUTO BRAKE INOPERATIVE NNC. AFTER ACCOMPLISHED CORRECTIVE ACTION NR-15 "LEFT IRS FAIL ON T/O" PERFORMED AUTO BRAKE & SYSTEM TEST OK PER AMM 32-42-00/705.

Part: PACKING — LEAKING (NR 1 ENGINE) · airframe 82,406 hrs · 18,409 cycles

NUMBER 1 ENGINE LEAK AT HPC SIGNAL PRESSURE TUBE LOC N. REMOVED AND REPLACED PACKING AS PER EO NR 1936A088. NO LEAKS NOTED.

Part: APU — MALFUNCTIONED · airframe 82,404 hrs · 18,408 cycles

APU FAULT. 3 START ATTEMPTS(<P>PERFORMED FIM TASK 49-11 FAULT TREE 988. APU START SATISFACTORY ON 1ST ATTEMPT. NO FURTHER DEFECTS<BR /></P>)

Part: RADAR — INOPERATIVE (NOSE) · airframe 82,360 hrs · 18,397 cycles

RIGHT RADAR INOPERATIVE, GIVING A FAINT GREEN BAND RETURN REGARDLESS OF TILT OR WX. PERFORMED WEATHER RADAR OPS CHECK RT SIDE. IAW AMM 34-43-00, SWEEP PATTERN CHECKS OK. NO FAULTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT A/C PACK) · airframe 82,181 hrs · 18,353 cycles

EICAS LT PACK TEMP. PERFORMED OPERATIONS CHECK, IAW AMM 21-51-00/501. NO FAULTS NOTED.

Part: ACTUATOR — MALFUNCTIONED (APU) · airframe 82,170 hrs · 18,350 cycles

APU COLD SOAK START -62 DEGREES SAT FL390 ATTEMPTS 3 UNSUCCESSFUL. APU DOOR STATUS MESSAGE AFTER EACH ATTEMPT(<P>TRANSFERRED TO DMI# 140868 IAW MEL 49-15-01-01A CAT C DUE DATE 23JAN2021. M PROCEEDURES C/W - APU DOOR DEACTIVATED OPEN.</P><P>18JAN21 - LP 1253321 ITEM 5 - ONT:&NBSP;REMOVED AND REPLACED APU AIR INTAKE DOOR ACTUATOR IAW AMM 49-15-06. OPS CHECK GOOD. PERFORMED APU BITE IAW AMM 49-61-05. NO MESSAGES DISPLAYED.

Part: PRESSURE SWITCH — LEAKING (APU OIL SYSTEM) · airframe 82,006 hrs · 18,307 cycles

APU LOW OIL PRESS SWITCH LEAKING OIL. REMOVED AND REPLACED LOW OIL PRESS SWITCH, IAW AMM 49-94-02. OPERATIONS NORMAL, NO DEFECTS NOTED.

Part: APU — FAULTED · airframe 81,930 hrs · 18,291 cycles

AFTER LANDING EICAS "APU FAULT" 3 START ATTEMPTS. PER FIM 49-11 F/T 987 AND FIM 49-11 F/T 988 UP TO BLOCK 30. APU START SUCCESSFUL ON FIRST ATTEMPT, PER AMM 49-11-00. PERFORMED 3 SUCCESSFUL STARTS WITH NO FAULTS.

Part: DUCT — DAMAGED (APU) · airframe 81,761 hrs · 18,239 cycles

APU FAULT ON TAXI IN. FOUND HOLE IN APU EXHAUST DUCT. REMOVED AND REPLACED DUCT, IAW 49-52-00.

Part: ANTENNA — FAILED (WX RADAR SYS) · airframe 81,685 hrs · 18,216 cycles

WXR FAIL FLAG AT CRUISE AND WXR SYSTEM STATUS MESSAGE AT SHUTDOWN. REMOVED AND REPLACED WEATHER RADAR ANTANNAE, REF AMM 34-43-05. OPERATIONS CHECKS GOOD.

Part: RELAY — MALFUNCTIONED (ISOLATION VALVE) · airframe 81,675 hrs · 18,212 cycles

RT BLEED AIR ISOLATION VALVE FAULT ON OVHD PANEL. TRANSFERRED TO MDDR 137572, IAW MEL 36-11-06. FOUND RT ISOLATION VALVE LIGHT STAYING ON WHEN SWITCH IS IN OPEN POSITION. OPERATIONS CHECKS NORMAL IN CLOSED POSITION. REMOVED AND REPLACED K18 RELAY VALVE OPEN RELAY, PER SWPM 20-81-18, NO HELP. SLAVED IN RT ISOLATION VALVE ON LEFT SYSTEM, PROBLEM FOLLOWED. REMOVED AND REPLACED RT ISOLATION VALVE, PER AMM 36-11-04. PRESSURIZED PNEUMATICS, PER AMM 36-00-00 AND RAN RT ENGINE, PER AMM 71-00-00. OPERATIONS AND LEAK CHECK GOOD. THIS CLEARS MDDR 137572, PLACARD REMOVED, MCC NOTIFIED.

Part: CONTROL VALVE — MALFUNCTIONED (LT TEMP) · airframe 81,681 hrs · 18,214 cycles

LEFT PACK BITE ON MX PAGE. LEFT PACK SURGING, T/S BITE INDICATES TEMP CONTROL VALVE & TRANSFERRED TO MDDR 137549, PER DDG 21-51-01-01, CAT C. PERFORMED BITE TEST OF LT CONTROLLER, PER FIM TASK 21-51 FT 844, "TEMP CONT VALVE" FAULT LIGHT ON PANEL. REMOVED AND REPLACED LT TEMP CONT VALVE, IAW B767 AMM 21-51-12. OPERATIONS CHECK GOOD. THIS ACTION CLEARS DMI NR 137549. RE-ACTIVATED FLOW CONTROL VALVE. MXC NOTIFIED, PLACARD REMOVED DISP: DP 1622Z.

Part: MODULATING VALVE — FAILED (CABIN TEMP) · airframe 81,578 hrs · 18,179 cycles

EICAS MESSAGE "FWD CABIN TEMP" WHILE AT PARKING SPOT. TRANSFERRED TO MDDR NR 136755, PER DDG 21-61-01-02, CAT C. DUE 05NOV20. T/I ACL 0428. REMOVED AND REPLACED FWD TRIM AIR MODULATING VALVE, IAW AMM 21-61-07. OPERATIONS CHECK GOOD, MESSAGE CLEARED. THIS CLEARS DMI 136755. PLACARD REMOVED, MCC NOTIFIED.

Part: VALVE — MALFUNCTIONED (CABIN TEMP) · airframe 81,524 hrs · 18,165 cycles

FWD CABIN TEMP INOPERABLE (CABIN COMPT TEMP CONTROL SYSTEM ALL CARGO CONFIGURATION). TRANSFERRED TO MDDR MEL 21-61-02, FWD CABIN TEMP INOPERABLE CAT "C" MEL. COMPLIED WITH MAINTENANCE PROCEDURE. 22 OCT 2020-1241771-M6-RIV. REMOVED AND REPLACED FWD TRIM VALVE, IAW AMM 21-61-07. OPERATIONS CHECK IS NORMAL AT THIS TIME. THIS CLOSES DMI 136434. PLACARDS REMOVED-DP 1805Z.

Part: BLADE — DISTORTED (NR 1 ENGINE) · airframe 81,358 hrs · 18,117 cycles

ENGINE NR 1 BLADE NR 11 HAS DISTORTION. PERFORMED INSPECTION OF THE FAN BLADE, IAW B767 AMM 72-31-02-226-012-H00. DIMENSIONS FOUND TO BE AT 0.15 INCHES AT THIS TIME, WITHIN LIMITS AT THIS TIME. OPENED NON-MEL FOR TRACING: MDDR 135354.

Part: CONNECTOR — NOT SEATED (CABIN TEMP) · airframe 81,183 hrs · 18,059 cycles

FWD CABIN ZONE TEMP INOPERABLE. PERFORMED FIM TASK 21-61 FT915. PREVIOUS FLT FAULT FWD TRIM AIR VALVE, PERFORMED DVI OF FWD TRIM VALVE. NO DEFECTS NOTED. RESEATED CONNECTOR PLUG IAW AMM 21-61-07. PERFORMED OPERATIONS CHECK IAW AMM 21-61-00. OPERATIONS CHECKED GOOD, VALVE OPENS AND CLOSES.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT A/C PACK) · airframe 81,058 hrs · 18,022 cycles

L PACK TEMP EICAS MESSAGE DISPLAYED DURING CLIMB L PACK OFF ALSO DISPLAYED PERFORMED LH PACK TEMP CONTROLLER BITE PROCEDURE PER B 767 AMM 21-51-00. NO CURRENT FAULTS PRESENT. NO PREVIOUS FAULTS LOGGED ON CONTROLLER. BOTH PACKS OPERATING SATISFACTORY AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT A/C PACK) · airframe 81,010 hrs · 18,009 cycles

EICAS L PACK TEMP(<P>PERFORMED FIM 21-51 FT 844 PACK TEMP CONTROLLER BITE. NO FAULTS ON BIT OR PREVIOUS F/L.&NBSP; VERIFY WAS A GO. FOLLOWED FIM UP TO #8. SYSTEM IS OK FOR SERVICE. RAN PACK FOR 1 HOUR IAW AMM 21-51-00 NO FAULTS NOTED.

Part: HSI — SMOKE (COCKPIT) · airframe 81,005 hrs · 18,008 cycles

CA HSI/MFD SHORTED OUT INFLIGHT. CAPT REPORTED SMOKE IN THE COCKPIT AND FUMES WHICH CEASED ON THE WAY BACK TO HNL. REF ITEM 1 PER MCC REQUEST ADDITIONAL CHECKS TO INSURE COOLING SYS OPERATION NORMAL. REMOVED AND REPLACED CAPT HSI/MFD IAW B767 AMM 34-22-04 OPS CHECK GOOD. PERFORMED INSPECTION FOR SOURCE OR OTHER SOURCES, FOUND CAPT HSI/MFD SHORTED. NO FURTHER DISCREPANCIES FOUND PER B767 AMM 05-51-55. SEE ITEM ONE. PERFORMED INSPECTIONS OF COOLING SYSTEM PER B767 AMM REF 21-58-00 21-58-22 21-53-05. NO DISCREPANCIES FOUND. OPS CHECK GOOD.

Part: APU — MALFUNCTIONED · airframe 80,962 hrs · 17,996 cycles

3 ATTEMPTS TO START APU AFTER LANDING, UNSUCCESSFUL.(<P>PERFORMED BITE CHECK ON APU ECU. "ABORT START" MESSAGE NOTED AND CLEARED. APU STARTED FIRST ATTEMPT. OPS NORMAL. NO FAULTS NOTED IAW AMM 49-11-00.<BR /></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (APU) · airframe 81,010 hrs · 18,009 cycles

APU FAULT EICAS MESSAGE AFTER 2 START ATTEMPTS. PERFORMED BITE CHECK ON APU ECU, NO FAULTS NOTED. MAINT STARTED APU FIRST ATTEMPT, NO FAULTS, REF: AMM 49-61-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (EXHAUST FAN) · airframe 80,542 hrs · 17,868 cycles

AFT EQ EXH FAN 2 AFTER START. T/S IAW FIM 21-58, FAULT TREE A02, SYSTEM TESTS NORMAL, NO OTHER FAULTS NOTED.

Part: WIRE HARNESS — FAILED (APU) · airframe 80,471 hrs · 17,842 cycles

APU BLEED INOPERATIVE. REMOVED AND REPLACED APU WIRE HARNESS IAW SWPM 20-10-04. CHECK OF APU PNEU GOOD IAW AMM 49-52-00.

Part: ECU — FAILED (APU) · airframe 80,456 hrs · 17,835 cycles

APU DUCT PRESSURE SURGING EXCESSIVELY. REMOVED AND REPLACED APU ECU, IAW AMM / 49-61-05, OPS CHECKED GOOD.

Part: VALVE — FAILED (APU BLEED AIR) · airframe 80,442 hrs · 17,830 cycles

NO APU BLEED AIR. REMOVED AND REPLACED VALVE APU BLEED AIR IAW AMM 49-52-00. OPS AND LEAK CHECKED OK.

Part: FILTER — DIRTY (COCKPIT TEMP) · airframe 80,442 hrs · 17,830 cycles

RIGHT PACK ALONE IS UNABLE TO ADEQUATELY COOL THE COCKPIT DURING FLIGHT. HIGHEST RECORDED COCKPIT TEMP WAS 36 DEG C. CLEARED COCKPIT TEMP SENSOR FILTER IAW AMM 21-61-09. OPS CHECK NORMAL.

Part: MODULE — FAULTY (APU) · airframe 80,431 hrs · 17,825 cycles

APU LOSS OF BLEED AIR PRESSURE. REMOVED AND REPLACED APU FLOW SENSING MODULE IAW AMM 49-53-08. TEST OK. THIS CLEARS MDDR 129149.

Part: HOSE — BROKEN (LT A/C PACK) · airframe 80,427 hrs · 17,823 cycles

LH PACK INOPERATIVE. REMOVED AND REPLACED A BROKEN HOSE IAW AMM IAW 21-51-03 AND REACTIVATED PACK. OPS CHECKED GOOD.

Part: SURGE VALVE — FAULTY (APU) · airframe 80,427 hrs · 17,823 cycles

APU PNEUMATIC FUNCTION INOP ( AUXILIARY POWER UNIT, PNEUMATIC FUNCTION )TRANSFERRED TO MDDR 129107 PER MEL 49-11-01-0,1 CAT "C", DUE 11JUN20 0710Z. CL PLACARDS INSTALLED. REMOVED AND REPLACED APU SURGE VALVE IAW AMM 49-53-01. THIS CLEARS MDDR 129107.

Part: SHUTOFF VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 80,319 hrs · 17,785 cycles

L ENG BLEED OFF EICAS(<P>REMOVED AND REPLACED&NBSP;PRSOV IAW 36-11-09. OPS CHECK NORMAL, LEFT ENG BLEED PRESSURE NORMAL.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 80,310 hrs · 17,781 cycles

L ENG HPSOV MESSAGE ON APPROACH(<P>CLEARED MSG PER AMM 36-11-00, NO FURTHER FAULTS NOTED AT THIS TIME.</P>)

Part: SHUTOFF VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 80,314 hrs · 17,783 cycles

L ENG HPSOV EICAS L ENG PRV EICAS/STATUS. RAN QRH PROC.(<P>REMOVED AND REPLACED LH ENG HPSOV PER AMM 36-11-07, OPS CHECKED WITH NO FAULTS FOUND PER AMM 71-00-00.</P>)

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 80,310 hrs · 17,781 cycles

CABIN ALTITUDE #2 INOP(<P>TRANSFERRED TO MDDR 128073 PER MEL 21-31-01A, CAT 'C', DUE DATE 17MAY20. DISPATCH DP @ 18:04Z. LP LP 1130644: C/W CABIN PRESS SELECTOR TEST IAW B767 AMM 21-31-01-704-014. THEN PERFORMED FIM 21-31 FAULT TREE 803. CABIN PRESS BITE. NO FAULTS AT THIS TIME. (REPLACED THE CABIN PRESSURE CONTROLLER). THIS CLEARS MDDR 128073.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 80,220 hrs · 17,756 cycles

APU BLEED VALVE MESSAGE DISPLAYED.(<P>PERFORMED PNEUMATIC SYSTEM TEST IAW AMM 49-11-00. SYSTEM TEST OK.</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 80,150 hrs · 17,733 cycles

STATUS MSG R ENG EEC C1 AFTER ENG START.(<P>COMPLIED WITH R PIMU BITE CK. SYSTEM PASS, OK FOR CONTINUED SERVICE AT THIS TIME, FIM 73-21-885-00, MSG CLEARED.</P>)

Part: EEC — FAILED (RT ENGINE) · airframe 80,167 hrs · 17,739 cycles

RH ENG EEC C1 STATUS MESSAGE. REMOVED AND REPLACED THE RT EEC IAW AMM 73-21-15. PERFORMED TEST 12 GROUND TEST EEC IAW AMM 71-00-00. PERFORMED ENGINE RUN IAW AMM 71-00-00. OPS CHECK GOOD.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 80,148 hrs · 17,732 cycles

R ENG EEC C1 STATUS MESSAGE.(<P>PERFORMED BITE PROCEDURE ON R PIMU IAW AMM/FIM 71-01-FT-810. MSG CLEARED, MCC NOTIFIED.</P>)

Part: ANTI-ICE VALVE — MALFUNCTIONED (RT WING) · airframe 80,064 hrs · 17,702 cycles

RIGHT WING ANTI-ICE EICAS MESSAGE AND RIGHT WING ANTI-ICE VALVE LIGHT BOTH COME ON INTERMITTENTLY.(<P>REMOVED AND REPLACED RIGHT WING ANTI ICE VALVE IAW AMM 30-11-02. OPS TEST OK AND LEAK CHECK OK.</P>)

Part: NUT — LOOSE (OVERHEAT LOOP) · airframe 79,923 hrs · 17,656 cycles

STATUS MESSAGE LEFT ENGINE OVERHEAT LOOP 1.(<P>T/S LEFT ENGINE OVERHEAT LOOP 1 MESSAGE IAW FIM 26-11 FT 807. FOUND NUT LOOSE IN #1 ENGINE OVERHEAT LOOP. SECURED NUT IAW AMM 26-11-02. NO FAULTS AT THIS TIME.</P>)

Part: CIRCUIT CARD — FAULTY (FIRE WARNING) · airframe 79,894 hrs · 17,644 cycles

STATUS MSG "L ENG OH LP 1".(<P>TRANSFERRED TO MDDR 125773 PER MEL 26-11-02-01, CAT 'C', DUE DATE: 24MAR20. DISP: SD @ 13:48Z.</P><P>LP 1071255: REMOVED AND REPLACED LT ENG FIRE LOGIC TEST CARD M10224 IAW AMM 26-10-01. OPS CKD GOOD. THIS CLEARS MDDR 125773.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 79,894 hrs · 17,644 cycles

STATUS MSG L ENG OH LP1.(<P>PERFORMED FIM TASK 26-11 FT 807, T/S MSG USING FIM TASK 26-11 FT 804. NO DEFECTS NOTED AT THIS TIME, PERFORMED ENGINE FIRE DETECTION SYSTEM OPERATIONAL CHECK I.A.W AMM 26-11-03. OPS CHECK GOOD, NO FURTHER DEFECTS NOTED , A/C OK FOR SERVICE.</P>)

Part: CIRCUIT CARD — NOT SEATED (OVERHEAT SYS) · airframe 79,847 hrs · 17,627 cycles

STATUS MESSAGE LEFT ENGINE OH LP1 INTERMITTENT.(<P>RE-RACKED THE LEFT ENG OVHT LP 1 AND AFOLTS CARD, AND PER FIM 26-11 FT 804 NO DEFECT NOTED AT THIS TIME. LEFT ENG OVHT DETECTION SYSTEM WORKS GOOD.</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 79,847 hrs · 17,627 cycles

L ENG OH LP 1 STATUS MSG.(<P>TRANSFERRED TO MDDR #125372 I.A.W MEL 26-11-02-01, CAT C.</P><P>LP 1208441: PERFORMED FIM TASK 26-11 FAULT TREE 804 FOR ENGINE FIRE DETECTION SYSTEM BITE PROCEDURES, COULD NOT DUPLICATE THE L ENG ON LP 1 STATUS MSG. OPS CHECKS NORMAL AT THIS TIME. C/W WO # 63683 WITH ACCOMPLISHMENT OF TROUBLESHOOTING. DMI REMAINS OPEN FOR FURTHER TROUBLESHOOTING.</P><P>LP 1208451: PERF. DVI AND CLEANING OF ALL FIRE DET. ELEMENTS. NO DEFECTS NOTED. PER AMM 26-11-02/701. RERACKED ENG #1 LOOP 1 AFOLTS CARDS PER AMM 26-11-02. PERF ENG. FIRE 1 OVERHEAT TEST IAW AMM 26-11-01. TEST OK. PERF ENGINE RUN IAW AMM 71-00-00, COULD NOT DUPLICATE. NO MSG NOTED.</P><P>LP 1208456: OBSERVED NO EICAS MSG PER MCC, THIS CLEARS DMI 125372, PLACARD REMOVED.</P><P><BR /></P>)

Part: CIRCUIT CARD — DEFECTIVE (FIRE WARNING) · airframe 79,843 hrs · 17,626 cycles

L ENG FIRE LP 2 STATUS MESSAGE APPEARED AFTER TAKEOFF AND EXTINGUISHED AFTER LANDING.(<P>TRANSFERRED TO MDDR 125274, MEL 26-11-01-01, CAT C, DUE 12MAR20. DOWNGRADED ETOPS TO 120. PLACARDS INSTALLED.</P><P>LP 1112130 - M4: TROUBLESHOT PER FIM 26-11 FT 804, FOUND BAD L ENG FIRE LOOP CARD. REMOVED AND REPLACED FIRE CARD 682 IAW AMM 26-10-01. OPS CHECKED GOOD. THIS CLEARS MDDR 125274. PLACARD REMOVED.</P>)

Part: BUTTON — INOPERATIVE (WEATHER RADAR) · airframe 79,836 hrs · 17,624 cycles

FO WX RADAR SELECT BUTTON INOP.(<P>RE-INSTALLED WX RADAR BUTTON PER AMM 34-22-02. OPS CHK OK AT THIS TIME.</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 79,830 hrs · 17,621 cycles

STATUS MSG L ENG FIRE LP 2 IN FLIGHT. CLEARED AFTER ENGINE SHUTDOWN.(<P>PERFORMED AFOLTS SYSTEM CHECK PER AMM 26-10-00. NO FAULTS NOTED. NO STATUS MSG REMAINS.</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 79,843 hrs · 17,626 cycles

L ENG FIRE LOOP 2 STATUS MSG.(<P>PERFORMED FIM TASK 26-11 FT 804 UP TO AND INCLUDING SHEET 5 BLOCK 110. COULDN'T DUPLICATE DISCREPANCY. NO FURTHER DEFECTS NOTED.<BR /></P>)

Part: LINE — LEAKING (OIL COOLER) · airframe 79,814 hrs · 17,618 cycles

DURING WALK AROUND FOUND LEAK NEAR # 1 ENG IDG.(<P>FOUND LEAK AT UNION ON TUBE BETWEEN OIL COOLER &AMP; IDG PRESSURE RELIEF VALVE, REMOVED AND REPLACED OIL COOLER TUBE I.A.W AMM 24-11-18, PERFORMED ENGINE RUN I.A.W AMM 71-00-00. OPS CHECK GOOD, NO LEAKS NOTED.</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (LT ENG FIRE) · airframe 79,783 hrs · 17,606 cycles

DURING CRUISE FLIGHT L ENG FIRE LOOP 2 STATUS MESSAGE DISPLAYED.(<P>DEFERRED PER MEL 26-11-01-01, MDDR 125021, CAT C.</P><P>REF LOG PAGE 1187722 ITEM M3: COMPLIED WITH FIM TASK 26-11 FAULT TREE 805. NO MESSAGE SHOWN ON EICAS. PERFORMED OPERATIONAL TEST OF ENGINE FIRE DETECTION SYSTEM IAW AMM 26-11-80, NO DEFECTS NOTED. THIS CLEARS DMI 125021. PLACARDS REMOVED.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (HYD GEN VALVE) · airframe 79,770 hrs · 17,600 cycles

EICAS MSG "HYD GEN VALVE", PERFORMED FIM 24-25 FAULT TREE 804. HYD GEN VALVE MESSAGE CLEARED. THEN PERFORMED HYD MOTOR GEN OPS CHECK IAW AMM 24-25-00-715-001. MESSAGE DOES NOT COME BACK. OPS CHECKED OK.

Part: WARNING LIGHT — FALSE ACTIVATION (LT GENERATOR) · airframe 79,758 hrs · 17,595 cycles

GEN FIELD MAIN RESET (L) FIELD OFF LIGHT ILLUMINATED. RESET L GEN CONTROL SWITCH, THEN RESET FIELD OFF (GEN FIELD) SWITCH. FIELD OFF LIGHT EXTINGUISHED. PERFORMED L GEN FIELD OPS CHECK IAW AMM SUBTASK 24-22-04-714-015. OPS CHECKED OK.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 79,709 hrs · 17,573 cycles

L ENG HPSOV CAUTION MSG ON APPROACH. PERFORMED AIR SUPPLY BITE PROCEDURE IAW B767 FIM 36-20 FAULT TREE 804. NO FAULTS FOUND AT THIS TIME. BITE CHK GOOD.

Part: CONNECTOR — DIRTY (GENERATOR) · airframe 79,647 hrs · 17,556 cycles

LT GEN DRIVE EICAS. ITEM TRANSFERRED TO MDDR 123413 IAW MEL 24-01-01, CAT 'B', DUE DATE 17JAN20. PERFORMED FIM 24-20 FT 801 BPCU PROCEDURE. FAULT IDG/PRESS SW WIRING. PERFORMED FIM 24-20 FT 804 TABLE 102. CHECKED CONTINUITY ON CONNECTOR P10964 PINS 9&10, NO FAULTS NOTED. CLEANED CONNECTOR, ALSO SERVICED IDG TO FULL IAW AMM 12-13-03, NO LEAKS NOTED. PERFORMED LT ENGINE RUN, PLACED LOAD ON ENGINE, NO FAULTS/MSGS NOTED. PERFORMED BITE OF BPCU IAW AMM 24-11-00. NO FAULTS NOTED, OPS NORMAL AT THIS TIME. THIS CLEARS DMI 123413. PLACARDS REMOVED. MCC NOTIFIED.

Part: HINGE — BROKEN (OXYGEN BOX) · airframe 79,532 hrs · 17,516 cycles

CAPTAIN'S OXYGEN MASK HAS COMPTARTMENT DOOR HINGE BROKEN, UNABLE TO SECURE MASK PROPERLY. SWAPPED WITH FIRST OBSERVER'S OXYGEN BOX, REMOVED AND REPLACED THE OXYGEN MASK BOX AT OBSERVER PANEL IAW MM 35-11-51. TEST OK.

Part: CONTROL SYSTEM — MALFUNCTIONED (TEMP CONTROL) · airframe 79,516 hrs · 17,511 cycles

AUTO FUNCTION FOR AFT AND FWD TEMP CONTROL INOPERATIVE. PERFORMED FIM 21-61 FT 915, ALL TESTS PASSED.

Part: WARNING MESSAGE — FALSE ACTIVATION (CARGO FIRE) · airframe 79,491 hrs · 17,500 cycles

MAIN DECK CARGO FIRE EICAS MSG DISPLAYED ON GROUND, THEN EXTINGUISHED.(<P>PERFORMED OPERATIONAL TEST AND SYSTEM TEST IAW B767 AMM 26-14-00. OPS CHECKED GOOD, SYSTEM CHECKS GOOD AT THIS TIME.</P>)

Part: APU — INOPERATIVE · airframe 79,491 hrs · 17,500 cycles

APU INOP. RESECURED LINES, CLAMPS AND AND CONNECTOR PLUG IAW AMM 49-53-01. BITE CHECKED ECU IAW FIM 49-11 FT 987. REAPPLIED FIM 49-11 FT A05, NO SURGING, APU RUNS STRONG.

Part: APU — FAULTED · airframe 79,424 hrs · 17,483 cycles

APU FAULT 2 ATTEMPTS&NBSP;(<P>PERFORMED BITE TEST ON ECU, NO FAULTS FOUND. APU STARTED ON 3RD ATTEMPT, OPS CHECK GOOD, REF AMM 49-11-00.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 79,414 hrs · 17,480 cycles

STATUS MSG: CABIN ALT AUTO 2.(<P>PERFORMED CABIN PRESSURE BITE PROCEDURE IAW FIM 21-31 FT 809, MESSAGE CLEARED. OPS CHECK GOOD IAW AMM 21-31-00.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 79,408 hrs · 17,477 cycles

ITEM 5: CABIN AUTO INOP EICAS MESSAGE IN DESCENT, COMPLETED QRH PROCEDURE. ITEM 6: CABIN ALT AUTO 2 STATUS MESSAGE. CABIN ALT AUTO 1 STATUS MESSAGE.(<P>PERFORMED BITE PROCEDURE, CABIN PRESSURE CONTROLLER IAW FIM 21-31. FAULT TREE FOUND AC FAULT. FAULT ERASED AND MESSAGE CLEARED FROM EICAS.</P>)

Part: MODULATING VALVE — MALFUNCTIONED (COCKPIT AIR) · airframe 79,408 hrs · 17,477 cycles

COCKPIT TEMP REGULATION IS ERRATIC, VALVE CYCLES FROM WARM TO COLD (FULL DEFLECTION). COCKPIT TEMP VARIES CONSTANTLY, UNABLE TO COOL COCKPIT BELOW 21C.&NBSP;(<P>TRANSFERRED TO DMI 121748 PER MEL 21-61-04-02. PLACARDS INSTALLED AND MCC NOTIFIED.</P><P>LP&NBSP;1224647 - M11: REMOVED AND REPLACED&NBSP;FLIGHT DECK TRIM AIR MODULATING VALVE IAW AMM 21-61-02, OPS CHECK GOOD. THIS CLEARS MDDR 121748.&NBSP;MCC NOTIFIED AND PLACARD REMOVED.</P><P><BR /></P>)

Part: FILTER — DIRTY (TEMP SENSOR) · airframe 79,397 hrs · 17,474 cycles

UNABLE TO REGULATE FLIGHT DECK TEMP IN AUTO MODE. WITH DECK RHEOSTAT SELECTED TO WARM AND TRIM VALVE POINTER ON "W", COLD AIR STILL COMES OUT OF THE GASPERS. AIR EVENTUALLY BECOMES TOO WARM, BUT THEN CYCLES TOO COLD.(<P>CLEANED FLIGHT DECK ZONE TEMP SENSOR FILTER IAW AMM TASK 21-61-00-107-027. SUCCESSFUL BITE TEST OF ZONE TEMP CONTROLLER PERFORMED IAW AMM TASK 21-61-03-715-022.</P>)

Part: CONNECTOR — DIRTY (LT A/C PACK) · airframe 79,375 hrs · 17,466 cycles

LEFT PACK OFF LOCAL LIGHT WILL NOT ILLUMINATE. LEFT PACK OFF EICAS MESSAGE DOES NOT ILLUMINATE EITHER.(<P>REMOVED AND CLEANED CONNECTOR TO LEFT PACK FLOW CONTROL VALVE, OPS CHECK NORMAL IAW AMM 21-51-01.</P>)

Part: RELAY — FAILED (COCKPIT TEMP) · airframe 79,370 hrs · 17,462 cycles

FLT DECK TEMP EICAS MSG AND INOP LIGHT.(<P>ITEM TRANSFERRED TO MDDR 121537 IAW MEL 21-61-02-03, CAT 'C', DUE DATE 14DEC19.</P><P>LP 1224631 - ITEM 1: REMOVED AND REPLACED RELAY K238&NBSP;<SPAN>IAW WDM 21-61-11 PAGE 14.1. OPS CHECK OKAY IAW AMM 21-61-00. </SPAN></P><P><SPAN>ITEM 3: REF ITEM 1, THIS ACTION ALSO CLEARS MDDR 121537.&NBSP; FLT DECK TEMP CHECK OK IN AUTO AND MAN MODES.</SPAN><BR /></P>)

Part: CONNECTOR — DIRTY (COCKPIT TEMP) · airframe 79,366 hrs · 17,460 cycles

FLT DECK TEMP MANUAL MODE ON FULL WARM,&NBSP; TEMP REACHED 35C. HAD TO SHUT TRIM AIR OFF TO STOP TEMP FROM RISING.(<P>REMOVED CANNON&NBSP; PLUG, SPRAYED VALVE &AMP; CANNON&NBSP; PLUG WITH CONTACT CLEANER. REINSTALLED&NBSP; CANNON PLUG, VALVE OPS CHECK OK IN MANUAL MODE PER&NBSP; AMM 21-61-00 (FLT DECK TRIM AIR VALVE).<BR /></P>)

Part: MODULATING VALVE — FAILED (COCKPIT TEMP) · airframe 79,365 hrs · 17,458 cycles

FLIGHT DECK CONT (TEMP) INOP IN AUTO MODE. REMOVED AND REPLACED FLT DECK TEMP VALVE IAW AMM 21-61-01, OPS CHECK NORMAL.

Part: CONTROL PANEL — MALFUNCTIONED (ANTI-ICE SYSTEM) · airframe 79,282 hrs · 17,434 cycles

ANTI-ICE WING LIGHT IN SWITCH IS INOP.&NBSP;(<P>RELAMPED, NO HELP. PLACED WING ANTI-ICE SWITCH LIGHT ON DEFERRAL; TRANSFERRED TO MDDR #120986 IAW MEL 30-11-02A, CAT 'C'.&NBSP;</P><P>LP&NBSP;1073500 - M3: REMOVED AND REPLACED WING &AMP; ENGINE ANTI ICE PANEL ASSY IAW B767 AMM 30-11-01. OPS CHECK GOOD AT THIS TIME. THIS CLEARS DMI 120986.&NBSP;</P>)

Part: SEAL — MISSING (FIRST AID KIT) · airframe 79,275 hrs · 17,431 cycles

DURING PRE-FLIGHT INSPECTION, DISCOVERED FIRST AID KIT BY LAVATORY MISSING TAMPER SEAL.(<P>TRANSFERRED TO&NBSP;MDDR 120960 PER MEL CH 25-64-01-01B, CAT 'D', DUE 20MAR20.</P><P>LP&NBSP;1073500 - ITEM M2: INSPECTED AND SECURED FIRST AID KIT IAW B767 AMM 25-34-03. THIS CLEARS DMI 120960.&NBSP;</P>)

Part: CONTAINMENT BAG — MISSING (CABIN) · airframe 79,192 hrs · 17,402 cycles

FOUND PED FIRE CONTAINMENT BAG MISSING.(<P>TRANSFERRED TO MDDR 120293 IAW MEL 25-20-01, CAT 'E', NEW NEF ITEM.</P><P>LP 1075529 - M3 INSTALLED NEW PED FIRE CONTAINMENT BAG IAW B767 AMM 25-60-99. THIS CLEARS DMI 120293. PLACARDS REMOVED.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (APU) · airframe 79,125 hrs · 17,379 cycles

APU FAULT EICAS MESSAGE, 2 START ATTEMPTS.(<P>PERFORMED APU ECU BITE CHECK, NO CURRENT FAULTS FOUND REF AMM 49-61-05. APU OPS CHECK GOOD, NO FAULTS NOTED REF AMM 49-11-00.</P><P><BR DATA-MCE-BOGUS="1" /></P><P>NOTE: APU COLD SOAK MDDR 119880 WAS OPENED IAW DDG 25-AP-01, OPTION C (FLT LEG HNL-ONT).&NBSP;</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (WEATHER RADAR) · airframe 79,101 hrs · 17,371 cycles

WXR SYS STATUS MSG IN CRUISE.(<P>PERFORMED FIM 34-43 FT 803 WXR SYS, NO FAULTS FOUND. OPS CHECK NORMAL AT THIS TIME.</P>)

Part: FUEL FILTER — WARNING MESSAGE (RT ENGINE) · airframe 79,109 hrs · 17,373 cycles

R ENGINE FUEL FILTER EICAS ON DEPARTURE.(<P>REMOVED AND REPLACED FUEL FILTER PER B767 AMM 73-11-02-004-001-H00 &AMP; 73-11-02-404-008-H00, NO LEAKS NOTED.</P>)

Part: IDG — FAILED (RT GENERATOR) · airframe 79,080 hrs · 17,367 cycles

RIGHT GEN OFF ON TAKEOFF.&NBSP;(<P>REMOVED AND REPLACED RIGHT ENGINE IDG IAW AMM 24-11-01, LEAK AND OPS CHECK GOOD AT THIS TIME.&NBSP;</P>)

Part: INDICATOR — INOPERATIVE (OUTFLOW VALVE) · airframe 79,048 hrs · 17,353 cycles

OVERHEAD PANEL; OUTFLOW VALVE POSITION INDICATOR INOPERATIVE, INDICATES FULL OPEN AT ALL TIMES. PRESSURIZATION NORMAL IN FLIGHT.&NBSP;(<P>TRANSFERRED TO MDDR #119464 IAW&NBSP;21-33-04, CAT 'C', DUE DATE: 31-OCT-19. PLACED P/N 130502-7 ON ORDER W/ MCC.</P><P>LP 1048322 - M4:&NBSP;PERFORMED OPS CHECK OF THE OUTFLOW VALVE ALL MANUAL MODE. OUTFLOW VALVE OPERATES CORRECTLY BUT NO INDICATIONS IAW AMM 21-31-03. THEN, CHECKED CONTINUITY BETWEEN CABIN PRESS CONTROL UNIT AND CABIN SELECTOR PANEL PINS 1 &AMP; 8, 2 &AMP; 20, 8 &AMP; 30, NO FAULTS.&NBSP;</P><P>LP 1048322 - M6: PER WDM 21-31-11 SH1 &AMP; SH2, CLEANED VALVE POSITION SWITCHES. OBSERVED SLIGHT&NBSP; DEFLECTIONS, ALL IN THE CABIN PRESSURE CONTROL UNIT. MDDR 119464 REMAINS OPEN AT THIS TIME.</P><P>LP 1091202 - M4: REMOVED AND REPLACED CABIN PRESSURE SELECT PANEL IAW AMM 21-31-01, OPS CHECK GOOD. THIS CLEARS DMI 119464. MCC NOTIFIED AND PLACARD REMOVED.&NBSP;</P>)

Part: APU — MALFUNCTIONED · airframe 79,052 hrs · 17,354 cycles

APU COLD SOAK START UNSUCCESSFUL, 3 ATTEMPTS @ FL 390, SAT -38 DEG.(<P>COMPLIED WITH&NBSP;OPS CHECK OF THE APU. START SUCCESSFUL 2 TIMES ON GROUND IAW AMM 49-11-00, OPS GOOD. REQUESTED COLD SOAK ON NEXT FLT.&NBSP; NOTE: MDDR 119439, 25-AP-01, PREVIOUSLY OPENED IS STILL APPLIED.&NBSP;</P><P>LP 1048321 - ITEM 1: APU INFLIGHT START SUCCESSFUL ON 2ND TRY @ FL 310, -40 SAT. NOTED BY MX, THIS CLEARS DMI 119439. MCC NOTIFIED.&NBSP;</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT EEC) · airframe 79,052 hrs · 17,354 cycles

L ENGINE CONTROL EICAS AFTER ENGINE START.(<P>C/W FIM 73-21 FT 878 (PIMU BITE), NO MESSAGES PRESENT ON PIMU. RAN LEFT ENGINE WITH NO ISSUES NOTED. COULD NOT DUPLICATE IAW AMM 71-00-00.&NBSP;</P>)

Part: APU — MALFUNCTIONED · airframe 79,043 hrs · 17,352 cycles

APU FAULT ON TWO START ATTEMPTS.(<P>PERFORMED BITE CHECK OF APU ECU IAW B767 AMM 49-61-05, OPS CHECK NORMAL. APU STARTED ON 3 ATTEMPT. OPS CHECK NORMAL, NO FAULTS FOUND.</P><P>NOTE: LP 1213015 - M4: AIRCRAFT RELEASED TO&NBSP;ETOPS SERVICE FOR APU COLD SOAK START VERIFICATION.&NBSP;OPENED MDDR 119439 PER DDG 25-AP-01 OPTION C, CAT 'N',&NBSP; FLT LEG HNL-ONT.&NBSP;</P>)

Part: APU — MALFUNCTIONED · airframe 79,009 hrs · 17,340 cycles

APU FAULT, ATTEMPTED 3 STARTS WITH NO SUCCESS. APU DOOR STATUS MESSAGE APPEARED MOMENTARILY. PERFORMED APU OPERATIONAL TEST, OPS CHECK GOOD PER AMM 49-11-00. ALSO PERFORMED APU CONTROL UNIT BITE TEST, NO FAULTS NOTED AT THIS TIME.

Part: SOLENOID VALVE — FAILED (APU DEOILER) · airframe 78,976 hrs · 17,329 cycles

APU RELIABILITY COLD SOAK -55C FL 390. 3 ATTEMPTS/UNSUCCESSFUL. PERFORMED APU HEALTH CHECK IAW EO 6749A003, NO DEFECTS NOTED. REMOVED AND REPLACED DE-OIL SOLENOID VALVE IAW AMM 49-27-08. LEAK CHECK GOOD. SUCCESSFUL APU COLD SOAK START C/W INTO CVG.&NBSP;</P>)

Part: SELECTOR — MALFUNCTIONED (CABIN PRESSURE) · airframe 78,963 hrs · 17,326 cycles

OUTFLOW VALVE POSITION INDICATOR SHOWS FULL OPEN INFLIGHT. CABIN IS PRESSURIZED. NO FURTHER DEFECTS NOTED. PLACED P/N 130502-7 ON ORDER WITH MCC. REMOVED AND REPLACED CABIN PRESSURE SELECTOR IAW AMM 21-31-01. OPS CHECK GOOD AT THIS TIME.

Part: APU — MALFUNCTIONED · airframe 78,968 hrs · 17,327 cycles

APU WOULD NOT START X3 ATTEMPTS. PERFORMED APU ECU BITE TEST, NO FAULTS NOTED. OPS CHECK OK IAW AMM 49-11-00. APU COLD SOAK REQUIRED DUE TO WORK ON APU.

Part: IDG — MALFUNCTIONED (LT ENGINE) · airframe 78,846 hrs · 17,286 cycles

AFTER ENGINE START, "L GEN DRIVE" EICAS MSG. LASTED FOR ABOUT 1 MIN THEN WENT AWAY. REMOVED AND REPLACED L ENG IDG IAW AMM 24-11-01. PERFORMED OPS CHECK AND ENGINE RUN IAW AMM 71-00-00. NO FAULTS NOTED, NO MESSAGE PRESENT AT THIS TIME.

Part: B-NUT — LOOSE (LT IDG) · airframe 78,831 hrs · 17,282 cycles

PER CUSTOMER REQUEST, PERFORM VISUAL INSPECTION OF LT ENGINE IDG FOR OIL LEAKS AND SERVICE IDG OIL. PERFORMED VISUAL INSPECTION ON LH ENGINE IDG, FOUND ONE OF THE B-NUTS LEAKING OIL. TIGHTENED THE B-NUT TO THE STANDARD TORQUE VALUE IAW AMM 20-11-00. SERVICED IDG IAW AMM 24-11-01, LEAK CHECK GOOD.

Part: IDG — LOW (LT ENGINE) · airframe 78,825 hrs · 17,279 cycles

L GEN DRIVE (WITH OVERHEAD DRIVE LIGHT) ON FOR 30 SECONDS AFTER START, THEN WENT OUT. SERVICED L IDG IAW AMM 12-13-03. PERFORMED OPS CHECK IAW AMM 71-00-00, OPS CHECK GOOD AT THIS TIME.

Part: ACTUATOR — MALFUNCTIONED (APU) · airframe 78,823 hrs · 17,278 cycles

APU NO START AFTER LANDING. TROUBLESHOT APU IAW FIM TASK 49-11 FT 988. SUSPECT APU INLET DOOR IS BAD. APU TRANSFERRED TO DMI #117979 IAW MEL 49-11-01A, CAT 'C', DUE 29-SEP-19. NO MX ACTION REQUIRED. LP 1055715 - M4: REMOVED AND REPLACED AIR INTAKE ACTUATOR ASSY (APU) IAW AMM 49-15-06. OPS CHECK GOOD AT THIS TIME. THIS CLEARS DMI #117979. PLACARD REMOVED AND MCC NOTIFIED.

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 78,814 hrs · 17,276 cycles

APU FAULT EICAS MESSAGE. APU WOULD NOT START AFTER LANDING, MOMENTARY APU DOOR STATUS MESSAGE APPEARED. 2 START ATTEMPTS. PERFORMED BITE TEST OF THE APU ECU, NO FAULTS FOUND. OPS CHECK OK, APU STARTED ON FIRST ATTEMPT BY MX. OPS CHECK OK AS PER AMM 49-41-00 AND 49-61-05.

Part: IDG — LOW (NR 1 ENGINE) · airframe 78,777 hrs · 17,264 cycles

AFTER L ENG START, L GEN DRIVE EICAS MESSAGE DISPLAYED. EICAS MESSAGE STAYED ILLUMINATED FOR APPROX 20 SECONDS THEN WENT AWAY. SAFETY WIRE BROKEN FOR L ENG DRIVE DISK, SWITCH NOT PUSHED. FOUND IDG ON ENG 1 LOW. SERVICED IDG IAW AMM 12-13-03, LEAK CHECK GOOD. NO FAULTS AT THIS TIME.

Part: IDG — LOW (LT ENGINE) · airframe 78,705 hrs · 17,239 cycles

LEFT GEN DRIVE EICAS ON AFTER START FOR APPROX 4 MINUTES, AND THEN OUT. SERVICED LH IDG PER PER AMM 12-13-03. OPS CHECK PER AMM 24-11-00, OPS CHECK OK AT THIS TIME. A/C OK FOR SERVICE.

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 78,682 hrs · 17,232 cycles

APU FAULT X3. PERFORMED APU/ECU BITE CHECK PER FIM 49-11-00. NO FAULTS FOUND AT THIS TIME.

Part: WARNING LIGHT — FALSE ACTIVATION (START VALVE) · airframe 78,602 hrs · 17,208 cycles

LEFT ENGINE START VALVE. PERFORMED ENGINE RUN ON NR 1 ENG. OPS CHECK GOOD GOOD AT THIS TIME, WORK ACCOMPLISHED IAW B767 AMM 71-00-00.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (EXHAUST FAN) · airframe 78,600 hrs · 17,207 cycles

"AFT EQPT EXH FAN 2" STATUS MSG. RESET EICAS AUTO EVENT PER AMM 31-41-00. AFT EQUIP COOLING FAN CHECK OK AS PER AMM 21-58-41.

Part: LINE — LEAKING (IDG OIL) · airframe 78,600 hrs · 17,207 cycles

L/H ENGINE IDG OIL LINE LEAKING DURING ENGINE RUN AT RATE OF 11 DROPS PER MINUTE.&NBSP;(<P>READJUSTED OIL LINE ( OIL COOLER ) AND TORQUED FITTING. RAN ENGINE AND FOUND NO FURTHER LEAKS PER AMM 24-11-00. NO LEAKS OR DEFECTS NOTED, OK FOR CONTINUE SERVICE.</P>)

Part: IDG — DISCONNECTED (LT GENERATOR) · airframe 78,580 hrs · 17,199 cycles

LT GEN DRIVE EICAS MSG - DRIVE DISCONNECTED. REMOVED AND REPLACED #1 ENG IDG IAW AMM 24-11-01. PERFORMED OPS/LEAK CHECK OF IDG IAW AMM 24-11-00, OPS CHECK GOOD, NO LEAKS NOTED.

Part: IDG — FAILED (LEFT) · airframe 78,556 hrs · 17,188 cycles

LEFT GEN DRIVE AND LT GEN OFF MESSAGE AFTER ENGINE START. RECONNECTED IDG IAW AMM 24-11-01. RAN ENGINE IAW AMM 71-00-00. LT GENERATOR STILL INOPERATIVE, IDG LOW PRESSURE LIGHT NEVER WENT OUT. AFTER ENGINE START, DISCONNECTED IDG. REMOVED AND REPLACED LT ENGINE IDG IAW AMM 24-11-01. OPS CHECKED GOOD.

Part: APU — SURGES (APU BAY) · airframe 78,556 hrs · 17,188 cycles

APU SURGES BETWEEN 30 AND 15 PSI DURING ENGINE START. REMOVED AND REPLACED APU IAW AMM 49-11-01. OPS CHECKED APU WAS GOOD.

Part: APU — MALFUNCTIONED · airframe 78,542 hrs · 17,184 cycles

APU FAILED TO START ON TAXI IN. PERFORMED MULTIPLE OPS CHECKS ON APU START AND CHECKED OUT OPERATIONAL EVERY TIME. NO DEFECTS NOTED IAW AMM 49-11-00.</P>)

Part: BUSS — DEACTIVATED (LT & RT) · airframe 78,538 hrs · 17,183 cycles

LEFT AND RIGHT UTILITY BUS BOTH DE-ENERGIZED IN CRUISE. LT & RT UTILITY MESSAGES APPEARED, RAN QRH AND BUS RESET, GALLEY OVEN WAS ON AT THE TIME. PERFORMED BPCU BITE PROCEDURES AND NO FAULTS NOTED REF FIM 24-20 FAULT TREE 801.

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 78,475 hrs · 17,161 cycles

AFTER LANDING, "APU FAULT" EICAS MSG. APU FAILED TO START WITH X3 ATTEMPTS. (<P>STARTED APU IAW AMM 49-05-00, STARTED FIRST ATTEMPT. OPS CHECK TESTED OK. BLEED AIR PRESSURE NORMAL. PERFORMED ECU BITE PER FIM 49-11 FAULT TREE 987. NO FAULTS, OK FOR SERVICE.</P>)

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 78,438 hrs · 17,146 cycles

APU FAULT AFTER LANDING, 2 STARTS ATTEMPTS UNSUCCESSFUL. (<P>OPS CHECKED PER B767 AMM 49-21-00, NO FAULTS NOTED. STARTED FIRST ATTEMPT.&NBSP;</P>)

Part: LOOP — UNKNOWN (CARGO BAY) · airframe 78,421 hrs · 17,140 cycles

MAIN CARGO LOOP 1. (<P>PERFORMED FIRE/OVRHT OPS CHECK, NO DEFECTS NOTED. MSG CLEARED. OPS CHECK GOOD REF AMM 26-11-01.<BR /></P>)

Part: CONTROL VALVE — MALFUNCTIONED (APU) · airframe 78,386 hrs · 17,124 cycles

DURING APU START ON TAXI IN, "APU FAULT" ON 2 START ATTEMPTS. (<P>APU INOP, TRANSFERRED TO MDDR # 114864 IAW DDG 49-11-01A, CAT 'C', DUE 26-JUL-19.</P><P>LOG PAGE 1080692- M6: REMOVED AND REPLACED SURGE CONTROL VALVE IAW AMM 49-53-01, OPS CHECK NORMAL AT THIS TIME. PERFORMED APU SELF TEST AS PER AMM 49-61-05, NO FAULTS NOTED. THIS CLEARS DMI #114864. PLACARD REMOVED AND MCC NOTIFIED.</P>)

Part: RELAY — FAULTY (APU) · airframe 78,328 hrs · 17,106 cycles

APU WILL NOT START ON GROUND(<P><SPAN>REMOVED / AND REPLACED RELAY K176 AND K547 IAW WDM 49-15-11 AND B767 FIM TASK 49-11 / FT 988. OPS CHECK GOOD</SPAN><BR /></P>)

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 78,280 hrs · 17,093 cycles

APU FAULT.(<P>PERFORM BITE CHECK OF ECU, ABORTED START FAULT, NO FURTHER INFORMATION PER AMM 49-61-05. START SUCCESSFUL 1ST ATTEMPT, OPS CHECK GOOD.</P><P><BR /></P><P>NOTE: LP 1066170 - M3: OPENED AN APU COLD SOAK START DEFERRAL (OPTION C) - MDDR NR 113975 (DDG 25-AP-01).</P><P>LP 1091223: APU COLD START ACCOMPLISHED. THIS CLEARS MDDR 113975. PLACARD REMOVED.</P>)

Part: ROD — DAMAGED (NACELLE DOOR) · airframe 78,246 hrs · 17,082 cycles

NR 2 ENGINE OUTBD CORE COWL OPEN HOLD ROD FOUND DAMAGED. REMOVED AND REPLACED OUTBD CORE COWL HOLD OPEN ROD PER AMM 70-11-00.

Part: THRUST REVERSER — DAMAGED (LT ENGINE) · airframe 78,246 hrs · 17,082 cycles

INBOARD LT ENGINE THRUST REVERSER CORE COWL AT THE 2 O'CLOCK POSITION, SHOWING WIRE MESH. PREPARED, CLEANED, AND REPAIRED DAMAGED WIRE MESH AT INBD L/H ENGINE THRUST REVERSER IAW AMM 78-31-00-00-308-074-H00, AND EO 6778A019, PART 3, REV 3.

Part: ROD — DAMAGED (NACELLE DOOR) · airframe 78,246 hrs · 17,082 cycles

NR 1 ENGINE INBD CORE COWL OPEN HOLD ROD LOCK DAMAGED. REMOVED AND REPLACED ENGINE INBD CORE COWL OPEN HOLD ROD PER AMM 20-11-00.

Part: TRANSCEIVER — INOPERATIVE (WX RADAR) · airframe 78,172 hrs · 17,057 cycles

RIGHT SIDE WXR INOPERATIVE. REMOVED AND REPLACED RIGHT RADAR TRANCEIVER IAW AMM&NBSP; 34-43-01 TEST OK.

Part: CHARGER — MALFUNCTIONED (APU) · airframe 78,069 hrs · 17,028 cycles

APU INOP. APU AUTO SHUTSDOWN AFTER REACHING 36% RPM.(<P>PERFORMED ECU BITE PROCEDURE PER B767 FIM 49-11 FAULT TREE 987. NO MINI FLAGS. PERFORMED BITE PROCEDURE OF APU ECU IAW B767 FIM 49-11 PT 987, NO FAULTS FOUND. WHEN STARTING APU BATT VOLTAGE STAYS ABNORMALLY LOW DURING ENTIRE START. SUSPECT BATTERY CHARGER AND/OR BATTERY. REMOVED AND REPLACED APU BATTERY CHARGER IAW AMM 24-31-05. OPS CHECK GOOD. REMOVED AND REPLACED THE APU BATTERY IAW AMM 24-31-04. OPS CHECKED GOOD.

Part: RELAY — FAULTY (APU) · airframe 78,047 hrs · 17,020 cycles

APU FAILED TO START. (<P>T/S&NBSP;PER FIM 49-11 FT 991, FOUND FAULTY START RELAY. &NBSP; REMOVED AND REPLACED RELAY K197 WITH NEW. 3 SUCCESSFUL STARTS ACCOMPLISHED&NBSP;REF AMM 49-41-11. NO DEFECTS NOTED AT THIS TIME.</P>)

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 78,017 hrs · 17,011 cycles

APU FAILED TO START ON TAXI IN. 2 ATTEMPTS. (<P>PERFORMED APU CONTROL UNIT BITE TEST. NO FAULTS FOUND AT THIS TIME. APU OPS TEST GOOD IAW AMM 49-61-05-742.</P>)

Part: ECU — MALFUNCTIONED (APU) · airframe 78,001 hrs · 17,006 cycles

AFTER LANDING "APU FAULT" EICAS. APU FAILED TO START ON 2 ATTEMPT (EGT RISE BUT RPM HUNG).(<P>BIT APU BOX FOUND NO FAULTS. RE-RACKED APU ECU AND OPS CHECK OF APU IS GOOD AT THIS TIME IAW AMM 49-11-00.&NBSP;&NBSP;</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 77,971 hrs · 16,997 cycles

STATUS MSG " WXR SYS".(<P>PERFORMED FIM 34-43 FT 805. NO DEFECTS NOTED, MSG ERASED. OPS CHECKED WEATHER RADAR IAW AMM 34-43-00. OPS CHECK GOOD AT THIS TIME OF LH &AMP; RH SYSTEMS.&NBSP;</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 77,971 hrs · 16,997 cycles

"APU FAULT" WHEN STARTING APU AFTER LANDING.&NBSP;(<P>PERFORMED FIM. 49-11 FT 989. NO DEFECTS FOUND, APU STARTED NORMALLY.</P>)

Part: OIL SYSTEM — LOW (APU) · airframe 77,981 hrs · 17,002 cycles

APU FAULT DURING START. (<P>VISUALLY INSPECTED APU, FOUND APU OIL TO BE LOW. SERVICED APU OIL IAW AMM 12-13-04-613-001. NO FAULT LIGHTS, APU STARTS NORMAL.&NBSP;<BR /></P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 77,956 hrs · 16,993 cycles

STATUS MSG: AFT EQ EXH FAN 2 AFTER START.(<P>RAN FIM 21-58 A02 TO STEP 22, FOUND SYSTEM OK. ERASED MSG DID NOT RETURN. NO FURTHER DEFECTS NOTED AT THIS TIME.&NBSP;</P>)

Part: OIL SYSTEM — LOW (APU) · airframe 77,934 hrs · 16,986 cycles

APU FAULT.(<P>FOUND APU OIL LEVEL LOW. SERVICED APU OIL LEVEL TO FULL. REF LOG PG 1079140 ITEM M4. PERFORMED APU START PER AMM 49-40-00. OPS TEST NORMAL.</P>)

Part: PACKING — DAMAGED (APU) · airframe 77,934 hrs · 16,986 cycles

APU FAULT AFTER LANDING.(<P>APU CAP IS DAMAGED, PLACED APU ON MDDR 111689 IAW B767 AMM 49-11-01A&NBSP; CAT 'C' DUE 5-25-2019. MCC NOTIFIED AND STICKERS INSTALLED.&NBSP;</P><P>LP 1079143 - 3: APU OIL STS MSG.&NBSP;NO OIL REQUIRED DUE TO DMI# 111689. MCC NOTIFIED. DMI REMAINS OPEN.</P><P>LP 1079153 - M4:&NBSP;REMOVED AND REPLACED OIL FILLER CAP PACKING IAW AMM 49-27-00. NO LEAKS NOTED. THIS CLEARS DMI 111689. MCC NOTIFIED.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 77,863 hrs · 16,962 cycles

APU FAULT(<P>PERFORMED APU VISUAL CHECK AND MAGNETIC CHIP DETECTOR. NO DEFECTS NOTED. PERFORMED ECU BITE TEST PER AMM 49-11-00. APU STARTS NORMAL.<BR /></P>)

Part: TRANSCEIVER — FAILED (WEATHER RADAR) · airframe 77,788 hrs · 16,938 cycles

LEFT WEATHER RADAR CONSTANTLY DISPLAYS GREEN BAND FROM 0 TO 40 MILES, NO MATTER WHAT TILT.&NBSP;&NBSP;(<P>REMOVED AND REPLACED LEFT WEATHER RADAR RECEIVER TRANSMITTER PER MAINTENANCE MANUAL.34-43-01.</P>)

Part: TRANSCEIVER — MALFUNCTIONED (WEATHER RADAR) · airframe 77,794 hrs · 16,940 cycles

L SYSTEM BACKGROUND WX RDR PAINTS RED(<P>REMOVED &AMP; REPLACED WEATHER RADAR TRANSCEIVER IAW AMM 34-43-01. NO DEFECTS NOTED, OPS CKD GOOD.</P>)

Part: SWITCH — NOT REPORTED (CABIN TEMP) · airframe 77,777 hrs · 16,934 cycles

REMOVE AND REPLACE SKIN TEMPERATURE SWITCH PER MCC REQUEST.&NBSP;(<P>REMOVED AND REPLACED EQUIPMENT COOLING SKIN TEMPERATURE SWITCH&NBSP; IAW AMM 21-58-21. OPS CHECK GOOD.<BR /></P>)

Part: ECU — DIRTY (APU) · airframe 77,769 hrs · 16,932 cycles

APU WILL NOT START. STARTED APU 4 TIMES AND CLEARED APU ECU IAW AMM 49-00-00. OPS CHECKS GOOD AT THIS TIME, NO FAULTS.<BR /></P>)

Part: GROUND WIRE — FAILED · airframe 77,742 hrs · 16,922 cycles

FWD EQPT VAL EICAS MSG ON DESCENT. PERFORMED FIM FAULT TREE 985 AND FOUND RELAY K1206 TO BE FAULTY. REMOVED AND REPLACED K1206 RELAY.&NBSP; FOUND FAULTY CONTROL SWITCH SENSOR ASSY- COULDNT R & R BECAUSE LOWER CARGO WAS LOADED. REMOVED AND REPLACED RELAY K1008 PER FIM FAULT TREE 985 IN PANEL 136 IAW AMM WDM 21-58-16. OPS CHECK GOOD ON GROUND. PERFORMED TROUBLE SHOOTING PER WDM 21-58-13. FOUND BAD GROUND AT GD1208-DC. WIRE W986-008-20. TERMINATED WIRE AT GD1208-DC IAW SWPM 20-30-00. SYSTEM OPS CHECKED GOOD AT THIS TIME IAW AMM 21-58-00.

Part: VALVE — FAILED · airframe 77,719 hrs · 16,913 cycles

FWD EQPT VALVE EICAS PRIOR TO TAXI. REMOVED RELAY K1005 AND CHECKED CONNECTOR D11538 PIN 4 FOR PRESSURE OF GROUND. FOUND GOOD GROUND THROUGH CONNECTOR AT PIN 4. ALL WORK PERFORMED IAW B767 WDM 21-58-12 & AMM 20-11-00. REINSTALLED K1005 RELAY INTO P136 PANEL B767 SWPM. REMOVED AND REPLACED OVBD EXH VALVE V12 IAW AMM 21-58-05. OPS CHECK OK AND DMI 109830 CLOSED.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (BATTERY) · airframe 77,692 hrs · 16,903 cycles

DURING PRE-FLIGHT, WITH BATT SW SELECTED ON, BATT OFF LIGHT ILLUMINATED AND DISCHARGE LIGHT ILLUMINATED.(<P>POWERED DOWN &AMP; REBOOT ACFT REF. AMM 24-31-01 &AMP; 34-31-02. NO MSGS, AIRCRAFT OK FOR SERVICE.</P>)

Part: APU — MALFUNCTIONED · airframe 77,692 hrs · 16,903 cycles

APU WOULD NOT START AFTER LANDING(<DIV>PERFORMED APU BITE PROC. IAW AMM 49-11-03-958 FIM. PERFORMED MINI-FLAG INTERROGATION PROC. REF. HONEYWELL AMM 31-15671 NO DEFECT NOTED. NO MINI-FLAGS RECORDED. STARTED APU 4 TIMES SUCCESSFULLY, OPS CHECK OK.&NBSP;</DIV>)

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 77,684 hrs · 16,900 cycles

FOUND OUTFLOW VALVE ASSY ACTUATOR BROKEN.(<P>REMOVED AND REPLACED E&AMP;E COOLING OUTFLOW VALVE IAW B767 AMM 21-58-05, GPS CHECK GOOD NO DEFECT NOTED AT THIS TIME. VERIFIED THE DUCT CLOSED IAW DDG 21-58-07-02-01 MCDOWELL 17109<BR /></P>)

Part: VALVE — MALFUNCTIONED · airframe 77,654 hrs · 16,886 cycles

AFTER BOTH ENGINES STARTED EICAS FWD EQPT VAL ACCOMPLISHED QRH AND RETURNED TO GATE(<P>TRANSFERED TO MDDR 109287 IAW ATLAS MEL 21-58-07-02-01 CAT C EXPIRES 05APR19 M PROCEDURES #2 APPLIED.&NBSP;</P><P>LP 880552 - M1:&NBSP;R&AMP;R FWD EQPT COOLING DUCT ASSY IAW AMM 21-58-02. T/S EQUIPT COOLING VALVE LIGHT AND EICAS MSG, NO FIX. FURTHER TROUBLESHOOTING REQUIRED FWD EQUIPT VALVE DEACTIVATED AND CONFIRMED CLOSED IAW DDG 21-58-07-02-01. DMI REMAINS OPEN AT THIS TIME.&NBSP;</P><P>LP 880557 - M2:&NBSP;REPLACED K1206 REPLAY IAW WDM 21-58-11, OPS CHECK GOOD ON THE GROUND DMI 109287 REMAINS OPEN TO CONTINUE TROUBLESHOOTING.&NBSP;</P><P>LP 880562 - M1:&NBSP;PERFORMED TS OF FWD EQUIP VALVE IAW FIM 21-58 TASK 805. NO FAULTS FOUND, PER ATLAS REQUEST REMOVE AND REPLACE OVERRIDE VALVE IAW AMM 21-58-20. OPS CHECK GOOD, NO DEFECTS NOTED AT THIS TIME. THIS CLEARS DMI 109287. MCC NOTIFIED AND&NBSP; PLACARD REMOVED</P>)

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 77,636 hrs · 16,880 cycles

LEFT WX SYS PAINTS ARCS AT 20 AND 40 MILES INTERMITTENT&NBSP;(<P>COMPLIED WITH OPERATIONAL TEST OF LT WX RADAR SYSTEM WITH NO FAULTS NOTED AT THIS TIME IAW AMM 34-43-00</P>)

Part: RELAY — FAILED · airframe 77,618 hrs · 16,872 cycles

FWD EQPT VALVE EICAS MSG AFTER BOTH ENGINE STARTED C/W QRH AND VALVE LIGHT REMAINED ILLUMINATED&NBSP;(<P>RE-OPENED MDDR # 108533 IAW DDG 21-58-06 CAT D DUE DATE 09-JUL-19</P><P>LP 880616-&NBSP;ACCOMPLISHED FIM TASK 21-58-00 FIG 104A - NO FAULTS NOTED. ACCOMPLISHED EQPT COOLING SYSTEM VALVE HEALTH CHECK PER AMM 21-58-00-700-805. VALVES CHECKS OK. MDDR CONTINUES (WAITING TD RELAY PN TDH1852-3002</P><P>LP 880617 -&NBSP;REMOVED AND REPLACED 30 SEC TIME DELAY RELAY K1206 PER WDM 21-58-11 OPS CHECKS OK PER AMM 21-58-00. MDDR 108533 CLEARED PLACARD REMOVED&NBSP;</P>)

Part: TUBE — LEAKING (NR 1 IDG) · airframe 77,615 hrs · 16,871 cycles

NR 1 ENGINE HAS EVIDENCE OF AN OIL LEAK LEFT SIDE.WHEN T/R WAS OPENED. (<P>REMOVED AND REPLACED #1 ENGINE INTERGRATED DRIVE UNIT GENERATOR TUBE OIL COOLING PER AMM 24-11-01. ACCOMPLISHED LEAK CHECK. NO LEAKS NOTED AT THIS TIME. PER AMM 71-71-00-601.</P>)

Part: UNKNOWN — MALFUNCTIONED (AC BAY) · airframe 77,615 hrs · 16,871 cycles

UNABLE TO MODULATE FLT DECK TEMP IN AUTO POSITION. VARIES FROM VERY HOT TO VERY COLD TEMPS. (<DIV>PERFORMED BITE TEST OF PACK TEMP CONTROLLERS IAW AMM 21-51-00. PERFORMED OPS TEST OF FLOW CONTROL SHUT OFF VALVE IAW AMM 21-51-01. PERFORMED OPS CHECK OF CABIN ZONE TEMP CONTROL PANEL 21-61-04. ALL OPS CHECK GOOD.&NBSP;</DIV>)

Part: DUCT — DAMAGED (E&E BAY) · airframe 77,609 hrs · 16,868 cycles

CABIN ALTITUDE MSG&NBSP;(<P>REF LOG PAGE 1040415 ITEMS M4 &AMP; M5, DAMAGED EXHAUST DUCTS REPLACED, PRESSURIZATION CONTROL SYSTEM TEST OK IAW AMM 21-31-00. REMOVED AND REPLACED FWD EQUIPMENT DUCTS IAW AMM 21-58-00 OPS AND LEAK CHECK GOOD.</P><P>2ND PART OFF: (P/N 217T1144-1, NSN)&NBSP;<BR /></P>)

Part: RELAY — FAILED (AC SYSTEM) · airframe 77,600 hrs · 16,865 cycles

AFTER ENGINE START&NBSP; FWD EQPT VALVE EICAS AND ASSOCIATED VALVE OVERHEAD LIGHT ILLUMINATED&NBSP;(<P>TRANSFER TO MDDR 108533 IAW DDG 21-58-06 CAT D&NBSP;</P><P>LP 1014012:PERFORMED THE FIM 21-58 FAULT TREE 986, FOUND FAULTY RELAY IN P-36 PANEL (FIM CALLS FOR REPLACEMENT ON INBOARD SUPPLY VALVE IND RELAY - K1007). COULDN'T FIND RELAY AS A/C HAS UNDERGONE CONVERSION.</P><P>LP 1040414:&NBSP;REMOVED AND REPLACED EQUIP COOLING CARD IAW AMM 21-58-24 (P/N:&NBSP;285T0095-8, S/N:&NBSP;D00628). NO HELP, MDDR # 108533 REMAINS OPEN.&NBSP;</P><P>DURING A-CHECK, REF NR 00002 &AMP; LP 1040426;&NBSP;<SPAN>REPLACED K1007 AND K1008 RELAYS. GROUND TEST FAILED. REPLACED K1006 AND K1011 ON P136 PER&NBSP;</SPAN>WD 21-58-12 AND 21-58-11.&NBSP; OPS CHECKED&NBSP; V90,V178,V178, AND V12. GROUND TEST EQUIP COOLING OK PER AMM 21-58-00. </P><P>MDRR 108533 CLEARED AND PLACARD REMOVED.&NBSP;</P>)

Part: IGNITER — FAULTY (LT ENGINE) · airframe 77,574 hrs · 16,853 cycles

LEFT ENGINE FAILED TO START ON FIRST ATTEMPT WITH IGNITOR ON SINGLE , FOLLOWED FROM GUIDANCE FOR NO EGT RISE , SECOND START ATTEMPT WITH IGNITORS SELECTED TO BOTH WAS SUCCESSFUL(<P>TRANSFERRED TO MDDR # 108301 AS PER MEL 74-00-01B CAT C.</P><P>LP 1047021: REMOVED AND REPLACED LEFT ENG IGNITER PLUG IAW 74-21-02-004-005-1100. OPS CHECK GOOD. DISPATCH UP @0811Z. THIS CLOSES MDDR 108301.</P>)

Part: UNKNOWN — MALFUNCTIONED (IGNITION SYS) · airframe 77,574 hrs · 16,853 cycles

NO LIGHT OFF DURING LEFT ENGINE START IGNITION, BOTH SELECTED NORMAL START.&NBSP;(<P>T/S I.A.W AMM 74-00-00 BOTH IGNITION SYSTEMS CHECK OK. STARTED LT ENG WITH EACH IGN SYS, BOTH CHECKED GOOD. A/C OK FOR SERVICE.&NBSP;</P>)

Part: UNKNOWN — MALFUNCTIONED (IGNITION SYS) · airframe 77,569 hrs · 16,850 cycles

NO LIGHT OFF DURING START OF LEFT ENGINE IGNITION LEFT ING BOTH FOR&NBSP; REMAINDER OF THE FLIGHT&NBSP;(<P>T/SHOOTING IAW FIM 71-01 FT 810 NO ADDITIONAL FAULTS FOUND IGNITION FAULT CLEARED PERFORMED&NBSP; TWO SUCCESSFUL STARTS OF THE LEFT ENGINE IN SINGLE SOURCE IGNITION OPS CHECK GOOD NO FUTHER DEFECTS NOTES A THIS TIME&NBSP;</P>)

Part: BOOT — DAMAGED (APU) · airframe 77,560 hrs · 16,845 cycles

APU DID NOT START AFTER LANDING THREE ATTEMPTS.&NBSP;(<P>FOUND SURGE VALVE BOOT DAMAGED, REPLACED BOOT IAW AMM 49-53-01. OPS CHECK GOOD AND APU STARTED ON FIRST ATTEMPT.&NBSP;</P>)

Part: TRANSCEIVER — MALFUNCTIONED (WEATHER RADAR) · airframe 77,560 hrs · 16,845 cycles

LEFT WEATHER RADAR FAIL, WXR SYS STATUS MESSAGE&NBSP;(<P>TRANSFERRED TO MDDR # 107994 AS PER MEL 34-43-01 CAT D.&NBSP;</P><P>LOG PAGE 1045256: COMPLIED WITH AP 15077, REMOVED AND REPLACED LT WX RADAR TRANSCEIVER &AMP; OPS CHECK LT WX RADAR SYSTEM TEST NORMAL IAW AMM 34-43-01. MDDR #107994 CLOSED&NBSP;</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT A/C PACK) · airframe 77,555 hrs · 16,844 cycles

LH PACK TEMP EICAS AFTER LANDING.(<DIV>RAN SYSTEM BITE TEST ON LH. PACK TEMP CONTROLLER IAW B767 AMM 21-51-14-705. NO FAULTS NOTED OPS CHECK LH. PACK NO STATUS&NBSP; OR MAINT MSGS AT THIS TIME.</DIV>)

Part: ECU — MALFUNCTIONED (RT ENGINE) · airframe 77,549 hrs · 16,843 cycles

IDLE DISAGREE @ 7000FT N1 LEFT 41.0 RIGHT 31.0(<P>TRANSFER TO MDDR 107888 IAW DDG 73-21-08-02&NBSP;</P><P>REF LOG PAGE 1047007 ITEM M6; REMOVED AND REPLACED THE RIGHT ENGINE ECU IAW AMM 73-21-15-404-068-H00 AND 71-00-00/501. OPS CHECK GOOD, THIS CLEARS MDDR 107888</P>)

Part: APU — UNKNOWN · airframe 77,545 hrs · 16,841 cycles

APU WOULD NOT START 2 ATTEMPTS. PERFORMED AN OPS CHECK OF THE APU STARTER, NO FAULTS NOTED IAW AMM 49-11-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (TE FLAPS) · airframe 77,538 hrs · 16,839 cycles

TE FLAP DISAGREE DURING APPROACH. PERFORMED FSEU BITE TEST IAW FIM 24-51 FT 809, FOUND NO FAULTS, PERFORMED OPS TEST OF FLAP / SLAT SYSTEM IAW AMM 27-51-00. NO DEFETS NOTED. REMOVED AND REPLACED INBOARD SLAT NR 6 OUTBOARD PROXIMATELY SWITCH IAW AMM 27-88-01, OPS CHECK TESTED GOOD, NO FUTHER DEFECTS NOTED SWITCH TARGET TEST SUCCESFUL, INSPECTED FSEU SENSOR VALUES IAW AMM 27-51-45 AND 27-51-26 AND 27-81-11 NO DEFECTS NOTED.

Part: ACTUATOR — MALFUNCTIONED (SLATS) · airframe 77,510 hrs · 16,830 cycles

LE SLAT ASYM EICAS. COMPLIED WITH QRH, SLATS WOULD NOT RETRACT, THEN SLAT/FLAP WOULD NOT DEPLOY IN NORMAL OPS, ALT FLAP SLAT EXTENSION&NBSP;(<P>T/S PER FIM 27-81 F.T.809 L/E FLAP ASYM MSG IAW FIM 27-51 F.T. 809 AND TASK 803 FSEU SHOWS LOAD RELIEF ACT MSG 2751200. REPLACED LOAD RELIEF ACTUATOR IAW AMM 27-51-30/401 AND 27-51-00 OPS NORMAL NO FAULTS AT THIS TIME FSEU REPLACED AS PRECAUTION FSEU P/N 285T0049-63&NBSP; &NBSP;S/N OFF FO1736</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (APU BLEED VALVE) · airframe 77,510 hrs · 16,830 cycles

APU BLEED VALVE ADVISORY MSG. COMPLIED WITH QRH.(<P>OPERATED APU SEVERAL TIMES AND APU BLEED AIR SYSTEM. OPS CHECKS GOOD PER AMM 49-11-00. NO MSG.<BR /></P>)

Part: CONTROL PANEL — MALFUNCTIONED (WEATHER RADAR) · airframe 77,502 hrs · 16,826 cycles

WXR SYS STATUS MSG&NBSP;(<P>REMOVED AND REPLACED WX RADAR CONTROL PANEL I.A.W AMM 34-43-02 LH &AMP; RH TEST GOOD&NBSP;</P>)

Part: OIL CAP — UNSECURE (APU) · airframe 77,444 hrs · 16,808 cycles

"APU OIL QTY" STATUS MESSAGE. APU OIL QTY SHOWED "FULL" ON GROUND. SERVICED PER AMM 12-13-04. SECURED OIL FILLER CAP. PERFORMED LEAK CHECK. NO LEAKS NOTED AT THIS TIME.

Part: RADAR — INTERMITTENT (WEATHER RADAR) · airframe 77,442 hrs · 16,807 cycles

LT & RT WX RADAR WORK INTERMITTENTLY & WXR SYS STATUS MSG. PERFORMED OPS TEST OF BOTH LT AND RT WX SYSTEM IAW AMM 34-43-00 NO FAULTS NOTED AT THIS TIME. LT WX RADAR SYSTEM REMAINS ON DEFERRAL.

Part: DRIVE UNIT — MALFUNCTIONED (WEATHER RADAR) · airframe 77,425 hrs · 16,802 cycles

LEFT WX RADAR INOP. REPLACED WEATHER RADAR DRIVE UNIT IAW AMM 34-43-05. OPS CHECK OK.

Part: WARNING MESSAGE — FALSE ACTIVATION (WEATHER RADAR) · airframe 77,425 hrs · 16,802 cycles

"WXR SYS" STATUS MSG AFTER SHUTDOWN(<P>PERFORMED OPS TEST ON WEATHER SYSTEM OPS CHECK OK AT THIS TIME IAW B767 AMM 34-43-00-715-026-002</P>)

Part: RADAR — FAILED (WEATHER SYS) · airframe 77,408 hrs · 16,796 cycles

LEFT WX RADAR FAIL(<P>PERFORMED OPERATIONAL TEST OF THE WX SYSTEM IAW B767 AMM 34-43-00. WXR OPS TEST SATISFACTORY. COULD NOT DUPLICATE DISCREPANCY. A/C OK FOR SERVICE.</P>)

Part: APU — FAULTED · airframe 77,403 hrs · 16,795 cycles

APU FAULT&NBSP;(<P>PERFORMED ECU BITE CHECK PER AMM 49-61-05, FAULT START ABORTED AC START CIRCUIT NOTED. SYSTEM RESET. START NORMAL, NO NEW FAULTS NOTED AND OPS CHECK GOOD.</P>)

Part: TRANSCEIVER — MALFUNCTIONED (WEATHER RADAR) · airframe 77,378 hrs · 16,789 cycles

WEATHER RADAR EHSI MESSAGE AND WEATHER RADAR STATUS MESSAGE. REMOVED AND REPLACED WEATHER RADAR TRANSCEIVER IAW AMM 34-43-01, OPERATION CHECK NORMAL.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 77,378 hrs · 16,789 cycles

APU FAULT. PERFORMED APU ECU BITE IAW AMM 49-61-05, SYS CHECK NORMAL OPS CHECK GOOD. APU START NORMAL.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 77,378 hrs · 16,789 cycles

STATUS MESSAGE WXR SYSTEM. PERFORMED WXR SYSTEM TEST IAW AMM 34-43-00, OPS CHECK GOOD MESSAGE CLEARED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 77,358 hrs · 16,785 cycles

APU FAULT(<P>PERFORMED APU BITE IAW FIM 49-11-00 FT 987. NO DEFECTS NOTED. PERFORMED APU START. OPS NORMAL.&NBSP;</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 77,352 hrs · 16,783 cycles

STATUS MSG SYS(<DIV>PERFORMED WXR SYSTEM TEST&NBSP; IAW AMM 34-43-00 TEST PASSED&NBSP; MSG CLEARED</DIV>)

Part: GENERATOR — LOW (LT ENGINE) · airframe 77,352 hrs · 16,783 cycles

LT GEN DRIVE&NBSP;(<P>INSPECTED AND FOUND LT GEN DRIVE /GENERATOR OIL LEVEL LOW SERVICED NR 1 ENG GENERATOR&NBSP; AS REQUIRED PER AMM 24-00-00</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 77,334 hrs · 16,778 cycles

WXR SYS STATUS MSG&NBSP;(<P>PERFORMED RESET WX RADAR SYSTEM ( LEFT AND RIGHT ) OPS CHECK GOOD IAW AMM 34-43-00 STATUS MSG CLEARED&NBSP;</P>)

Part: OIL SYSTEM — LOW (APU) · airframe 77,330 hrs · 16,777 cycles

APU FAULT WOULD NOT START(<P>SERVICED APU OIL IAW AMM 12-13-04 OPS CHECK NORMAL AT THIS TIME&NBSP;</P>)

Part: VALVE — FAULTY (E&E BAY) · airframe 77,300 hrs · 16,767 cycles

" FWD EQUIP VALVE " EICAS MESSAGE(<P>DEFREED IAW DDG 21-58-06 MAINT PROCEDURE&NBSP; 2 C/W. DDG #106211.<BR /></P><P>LOG PAGE 1032265: TROUBLESHOT PER FIM 21-58 FAULT TREE 986, FOUND FWD V900 VALVE BAD, R&AMP;R V900 VALVE IAW 21-58-00 AMM, OPS CHECK GOOD, THIS CLEARS DMI #106212. PLACARDS REMOVED&NBSP;<BR DATA-MCE-BOGUS="1" /></P>)

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 77,237 hrs · 16,749 cycles

WEATHER RADAR WX FAIL ON EHSI DURING APPROACH AND LANDING(<P>PERFORMED OPERATIONAL TEST OF WEATHER RADAR SYSTEM IAW AMM 34-43-00 FOUND NO FAULTS ISSUE WITH SYSTEM OPS CHECK GOOD AT THIS TIME&NBSP;</P>)

Part: BEARING — DAMAGED (MLG) · airframe 77,205 hrs · 16,735 cycles

NR 6 BRAKE ON LEFT GEAR DRAGGING - REACHED 3 ON DEPARTURE AND 7 ON LANDING WITH OTHERS ALL 0 AND 1 - BRAKE TEMP LIGHT ON TAXI IN&NBSP;(<P>FOUND NR 6 BRAKE BEARING DAMAGE CAUSING HEAT DAMAGE TO THE NR 6 AXLE&NBSP; - REMOVED AND REPLACED NR 6 BRAKE PN 2612412-1 SN 0255 / REPLACED NR 6 MWA PN 2608811-5 SN OFF 6774/8130&NBSP; REPLACED NR 6 MWA ANTISKID TRANSDUCER DUE DAMAGED / ALSO DUE AXLE DAMAGED, REMOVED AND REPLACED REAR AXLE BUILDUP ASSY MLG ASSY IAW CMM 32-11-20 AND 32-11-50&NBSP; OK&NBSP; ALSO COMPLIED WITH INSPECTION IAW AMM 05-51-17-212-001 (WHEEL BEARING FAILURE INSPECTION) AND ALSO COMPLIED WITH INSPECTION IAW AMM 05-51-17-212-036&NBSP; (HEAT DAMAGE INSPECTION) ALL OK&NBSP;</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 77,205 hrs · 16,735 cycles

STATUS WXR SYS.(<P>PERFORMED OPS CHECK OF WXR SYS OPS CHECK GOOD NO MSG REMAINING IAW AMM 34-43-00.<BR /></P>)

Part: FILTER — NOT REPORTED (LT ENGINE) · airframe 77,180 hrs · 16,725 cycles

L ENG FUEL FILTER(<P>REMOVED AND REPLACED L ENG FUEL FILTER PER AMM 73-11-02-004-001-H00 AND 73-11-02-704-008-H00 FLIGHT CREW RAN ENGINES, NO LEAKS NOTED&NBSP;</P>)

Part: RADAR — FALSE INDICATION (WEATHER SYSTEM) · airframe 77,167 hrs · 16,721 cycles

WX RADAR FAIL MESSAGE ON LEFT SIDE(<P>OPS CHECKED OK IAW AMM 34-43-00 NO FAULTS NOTED</P>)

Part: OIL SYSTEM — LOW (LT IDG) · airframe 77,165 hrs · 16,720 cycles

ON T/O ROLL " LH GEN DRIVE" "LH GEN OFF" "LH UTILITY BUS OFF" RT UTILITY BUS OFF" ON CLIMB "L GEN DRIVE" CLEARED. COMPLIED WITH QRH FOR "GEN OFF" ALL MESSAGES CLEARED(<P>FOUND LH IDG LOW, SERVICED 1.5 QT IAW 12-13-03 OPS CHECKED L IDG IAW AMM 24-11-00 OPS CHECK GOOD. PERFORMED ALSO BPCU BITE TEST OK IAW 24-20-FT 801 .</P>)

Part: GENERATOR — MALFUNCTIONED (LEFT) · airframe 77,164 hrs · 16,719 cycles

L GEN OFF ON CLIMB OUT RESET L GEN CONT AS PER CHECK LIST L GEN FUNCTIONAL NORMALLY(<P>NOTE BY MX COULD NOT DUPLICATED ON GROUND RUN IAW AMM 71-00-00</P>)

Part: DETECTOR — FAULTY (CARGO BAY) · airframe 77,144 hrs · 16,713 cycles

MAIN CARGO LOOP 1 STATUS MSG. (<P>TRANSFERRED TO MDDR 105113 AS PER MEL 26-16-02-01 CAT C. PERFORMED FIM 26-10 FT 803 ALFOLTS CARD M10226, M10276, M10400 AND M10427 NO LIGHTS SYSTEM OK PER FIM 26-14 FT 803 BITE TEST FOR SMOKE DETECTOR SYS, NO FAULTS NOTED. PERFORMED AND RESET CBS 1, 2, 3, 4 FIRE DETECT MAIN CARGO PER WDM 26-16-31, NO FAULTS NOTED. THIS CLEARS MDDR 105113. TS PER FIM 26-14 FT 809 FOUND DETECTOR M12213 AT FAULT REMOVED AND REPLACED DET M12213 PER AMM 26-14-01/401 OPS CHECKS OK MDDR CLEARED, PLACARD REMOVED &NBSP; (DETECTOR SN 31459B&NBSP; PN 2156-55)</P><P><BR DATA-MCE-BOGUS="1" /></P><P>1/3/2019 - RE-OPENED MDDR 105133 - PER LOGPAGE 1042248 REMOVED AND REPLACED DETECTOR SN &NBSP;<SPAN>32028B PN&NBSP;</SPAN><SPAN>2156-55; MDDR 105113 CLOSED AS OG 1/12/2019</SPAN></P>).

Part: STATUS MESSAGE — FALSE ACTIVATION (CRG FIRE DETECT) · airframe 77,167 hrs · 16,721 cycles

MAIN CARGO LOOP 2 STATUS MSG DISPLAYED INTERMITTENTLY THROUGH OUT FLIGHT(<P>PERFORMED BITE TEST OF THE CARGO COMPARTMENT SMOKE DETECTION SYSTEM PER TASK 26-14 FT 809 NO MESSAGES NOTED AT THIS TIME</P>)

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 77,089 hrs · 16,693 cycles

PFD UNIT ON LEFT SIDE STARTED SMOKING, COMPLIED WITH QRH. R&R LEFT EADI PER AMM 34-22-03 OPS CKD GOOD, ALSO NO FUMES OR SIGNS OF ANY FURTHER SOURCE OF FUMES PER AMM 05-51-56, OPS CHECKS & NO FUMES PRESENT. GOOD AT THIS TIME, AIRCRAFT OK FOR SERVICE.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 77,084 hrs · 16,692 cycles

INTERMITTENT MAIN CARGO LOOP 1 STATUS MESSAGES. PERFORMED OPS TEST OF MAIN DECK CARGO SMOKE DETECTION SYSTEM IAW AMM 26-00-00 OPS TEST GOOD. NO FAULTS NOTED AT THIS TIME. AT TIME OF VISITING ACFT STATS MSGS WERE NOT PRESENT. PERFORMED FIM 26-14 FT 809 FOUND FAULT WHEN PRESSING ENG/APU/CARGO SWITCH AND MN CARGTO LOOP 1 AND MAIN CARGO LOOP 2 DID NOT APPEAR ON THE "ECS/MSG". NEEDS FURTHER TROUBLESHOOTING. T/S IAW FIM 26-14 FT 809, OPS CHECKED IAW AMM 26-14-00. SYSTEM CKS NORMAL, NO DEFECTS NOTED.

Part: MODULATING VALVE — FAULTY (AC SYSTEM) · airframe 77,084 hrs · 16,692 cycles

FWD EQUIP VALVE ADVISORY MESSAGE. REACTIVATED EQUIP COOLING SYSTEM AND FOUND NO FAULTS. ATTEMPED POWER TRANSFER GND TO APU AND APU TO GND AND COULD NOT RE-CREATE FAULT. ALSO OBSERVED VALVE LIGHT ANNUNCIATE AND EXTINGUISH WHEN TOGGLING COOLING SELECTOR FROM AUTO STBY. NEEDS FURTHER TROUBLE SHOOTING AND DEACTIVATED COOLING VALVES PER DDG 21-58-06 PROCEDURE 2. REPLACED EQUIP COOLING MODULATING VLV IAW AMM REF 21-61-06, OPS CKS GOOD.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 77,106 hrs · 16,700 cycles

STATUS MSSG: MN CARGO LOOP 1. UPON INSPECTION OF STATUS PAGE, FOUND NO NO STATUS MESSAGE FOR MAIN CARGO LOOP 1. PERFORMED BITE CHECK OF CARGO COMPARTMENT SMOKE DETECTOR SYSTEM SYSTEM IAW FIM 26-14 FAULT TREE 809. BITE CHECK GOOD. COULD NOT REPRODUCE PROBLEM AT THIS TIME.

Part: RELAY — FAILED (AC SYSTEM) · airframe 77,065 hrs · 16,685 cycles

FWD EQUIPMENT VALVE EICAS MESSAGE LIGHT ILLUMINATED. REACTIVATED EQUIPMENT OVERBOARD VALVE PER AMM 21-00-00 PROCEDURE 2. REMOVED AND REPLACED RELAY K200 PER SWPM 20-81-22. OPS CHECKED EQUIPMENT COOLING PER AMM 21-58-00, NO FAULTS NOTED. OPS CHECK NORMAL.

Part: VALVE — MALFUNCTIONED (E&E BAY) · airframe 77,057 hrs · 16,682 cycles

FWD EQ COOLING VALVE INOP. PERFORMED FIM TEST 985 FWD EX VALVE CLEARED.

Part: AUTOPILOT SYS — MALFUNCTIONED (COCKPIT) · airframe 77,042 hrs · 16,678 cycles

CENTER AUTOPILOT INOP, CATIII NOT ALLOWED, REF DMI 103447. PERFORMED MCDP TEST 40 & 30 TEST PASSED, NO FAULT NOTE AT THIS TIME IAW AMM 22-00-02.

Part: SENSOR — DIRTY (NLG) · airframe 77,042 hrs · 16,678 cycles

ON PREFLIGHT FOUND FWD EQUIP COOLING VALVE ADVISORY MESSAGE AND VALVE LIGHT. T/S FOUND EXCESSIVE GREASE ON NOSE GEAR AIR/GND SENSOR, CLEANED SENSOR. CYCLED A/G SYS ALT, SYS 1 AND POS 1 & 2 C/B, VALVE LIGHT EXTINGUISHED, MESSAGE CLEARED PER AMM 21-58-00.

Part: INDICATOR — DAMAGED (E&E BAY) · airframe 77,042 hrs · 16,678 cycles

COOLING MONITOR INDICATOR IS DAMAGED. REMOVED AND REPLACED E&E COOLING AIR MONITOR INDICATOR PER AMM 21-58-34, INDICATOR OPS CHECK GOOD.

Part: ANTI-ICE VALVE — MALFUNCTIONED (LT ENGINE) · airframe 77,040 hrs · 16,677 cycles

LT ENG ANTI ICE VALVE WONT CLOSE AFTER SHUTDOWN.(<P>R+R LH ENGINE ANTI ICE VALVE IAW AMM 30-21-00 OPS GOOD.</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (FIRE LOOP) · airframe 77,015 hrs · 16,667 cycles

INTERMITTENT CARGO LOOP 2 STATUS MESSAGE&NBSP;(<P>NO DEFECTS NOTED DURING OPS CHECK PER B767 AMM 26-00-00</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI-ICE VALVE) · airframe 77,021 hrs · 16,670 cycles

L ENG ANTI- ICE VALVE LIGHT ON AFTER TURNING ENG ANTI ICE SWITCH OFF AT BLOCK IN(<DIV>PERFORMED FIM TASK 30-21 FAULT TREE 803.&NBSP; CHECKED CONNECTIONS ON ANTI ICE CONTROL PANEL.&NBSP; NO FAULTS NOTED&NBSP;</DIV>)

Part: STATUS MESSAGE — INTERMITTENT (FIRE DETECTOR) · airframe 77,010 hrs · 16,664 cycles

MAIN CARGO LOOP 1 AND MAIN CARGO LOOP 2 STATUS MESSAGE ON INTERMITTENTLY DURING FLIGHT&NBSP;(<P>PERFORMED MAIN CARGO COMPARTMENT SMOKE DETECTOR TEST PER FIM 26-14 FT 809, ALL LED GREEN FOR ZONE A,B,C,D, LOOP 1 AND LOOP 2 - NO EICAS MESSAGE DISPLAYED&NBSP;</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 77,017 hrs · 16,668 cycles

MAIN CARGO LOOP 1 MESSAGE DURING FLIGHT. PERFORMED OPS CHECK MAIN DECK COMPARTMENT SMOKE DETECTOR SYSTEM PER AMM 26-14-00. SYSTEM OPERATED GOOD, NO FAULTS.

Part: IDG — MALFUNCTIONED (LT ENGINE) · airframe 77,026 hrs · 16,673 cycles

LEFT IDG & DRIVE LIGHT OFF WITH ENGINE OFF, WILL TEST. REMOVED AND REPLACED LEFT ENGINE IDG IAW AMM 24-11-01. OPS CHECK NORMAL NO LEAKS NOTED.

Part: CIRCUIT CARD — FAILED (FIRE DETECTION) · airframe 76,985 hrs · 16,654 cycles

MAIN CARGO LOOP 1 STATUS MESSAGE&NBSP;(<P>TRANSFERRED TO MEL 26-16-01-02&NBSP; MDDR 102882</P><P>REF LOGPAGE 1009581 - REMOVED AND REPLACED FIRE PRINTED CIRCUIT CARD PER AMM 26-17-01; MDDR 102882 CLEARED AT THIS TIME.</P>)

Part: RADAR — UNKNOWN (LEFT) · airframe 76,985 hrs · 16,654 cycles

LEFT RADAR FAILED&NBSP;(<P>PERFORMED GROUND TEST OF LEFT RADAR SYSTEM IAW AMM 34-43-00 PASSED EICAS MSG CLEARED&NBSP;</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (FIRE DETECTOR) · airframe 76,954 hrs · 16,639 cycles

STATUS MSG MD CARGO LOOP 1(<P>PERFORMED FIRE WARNING TEST IN REF TO AMM 26-00-01 OPS NORMAL AT THIS TIME <BR /></P>)

Part: OIL SYSTEM — LOW (APU) · airframe 76,954 hrs · 16,639 cycles

APU FAILED TO START DURING START OF APU OIL QTY DROPPED TO .25(<P>SERVICED APU OIL IN REF TO AMM 12-10-00 OPS CHECK OK <BR /></P>)

Part: FILTER — WARNING MESSAGE (RT ENGINE) · airframe 76,951 hrs · 16,638 cycles

RIGHT ENGINE FUEL FILTER EICAS MESSAGE. THE FUEL FILTER WAS REPLACED IAW AMM 73-34-00, STATUS MESSAGE CLEARED.

Part: WARNING MESSAGE — FALSE ACTIVATION (WX RADAR SYS) · airframe 76,908 hrs · 16,625 cycles

LEFT WEATHER RADAR SYSTEM FAILED IN FLIGHT WITH A STATUS MESSAGE , RIGHT WX RADAR SYSTEM OPERATES NORMALLY. RESET WX RADAR CONTROL BOX AND PERFORMED OPS CHECK ON LEFT & RIGHT WX RADAR SYSTEM IAW AMM 34-43-00 OPS CHECK GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (CARGO FIRE DETEC) · airframe 76,908 hrs · 16,625 cycles

MAIN CARGO LOOP 1 AND 2 STATUS MESSAGES(<P>MAIN CARGO LOOP 1 AND 2 MSG LOOP 2 CLEARED AFTER OPS CHECK LOOP 1 MSG REMAINED , TRANSFERRED TO MDDR # 102367 AS PER DDG 26-16-02-01 CAT C <BR /></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (WX RADAR) · airframe 76,908 hrs · 16,625 cycles

STATUS WEATHER RADAR FAILED MESSAGE DISPLAYED WHEN THE LEFT WEATHER RADAR WAS SELECTED. RESET THE WEATHER RADAR CONTROL BOX AND PERFORMED OPS CHECK ON LEFT AND RIGHT WX RADAR SYSTEM IAW AMM 34-43-00, OPS CHECKED GOOD. NO FAULTS FOUND

Part: UNKNOWN — UNKNOWN · airframe 76,908 hrs · 16,625 cycles

AFTER DESELECTING THE LEFT ENGINE ANTI-ICE VALVE, THE INDICATOR LIGHT REMAINED ILLUMINATED. RAN ENGINES IAW AMM 71-00-00, SELECTED ENGINE ANTI-ICE VALVES, THEN TURNED OFF PRIOR TO SHUT DOWN , OPS CHECKED NORMAL.

Part: ECU — FAILED (APU) · airframe 76,883 hrs · 16,614 cycles

APU FAULT DURING START, FAULTED ON SECOND START. REMOVED AND REPLACED APU ECU IAW AMM 49-61-00 OPS CHECKED NORMAL.

Part: VALVE — MALFUNCTIONED (APU) · airframe 76,883 hrs · 16,614 cycles

APU INOPERATIVE. REMOVED AND REPLACED THE SURGE VALVE IAW AMM 49-53-01, OPS CHECKED OK.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 76,827 hrs · 16,594 cycles

MAIN CARGO LOOP 1 STATUS MSG. C/W MAIN DECK CARGO LOOP CHECK OPS NORMAL IAW FIM 26-14 FT 809.

Part: APU — FAULTED (APU BAY) · airframe 76,827 hrs · 16,594 cycles

APU FAULT. FOUND SLOW TO START ON APU ECU, RESET MEMORY AND PERFORMED BITE TEST NO FAULTS NOTED AT THIS TIME THIRD ATTEMPT SUCCESSFUL AS PER AMM 49-61-05.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 76,795 hrs · 16,581 cycles

IN FLIGHT, MN CARGO LOOP 1 STATUS MSG. UPON INSPECTION STATUS MSG DID NOT LATCH. CYCLED ASSOCIATED BREAKERS & PERFORMED OPERATIONAL TEST IAW AMM 26-14-00. OPS CHECK NORMAL. NO MSG ON EICAS.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 76,796 hrs · 16,582 cycles

MN CARGO LOOP 1 MSG IN FLIGHT. STATUS MSG DID NOT LATCH, CYCLED ASSOCIATED CB'S PERFORMED OPS TEST IAW AMM 26-14-00. OPS CHECKED GOOD, NO MSG ON EICAS.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 76,752 hrs · 16,567 cycles

APU FAULT WHEN STARTING APU ON TAXI IN, 3RD ATTEMPT SUCCESSFUL. PERFORMED FIM 49-11 FT 987 BITE TEST ECU LAST 2 RUNS SLOW START. NO OTHER FAULTS NOTED, OPS CHECKED APU GOOD.

Part: UNKNOWN — MALFUNCTIONED (GENERATOR SYS) · airframe 76,730 hrs · 16,559 cycles

LEFT GEN DRIVE LIGHT EXTINGUISHED WITH ENGINES NOT RUNNING. PERFORMED 5 MIN IDLE RUN ON LT ENG IDG PER 24-11-00-715-005 & 71-00-00/201. IDG DRIVE LIGHT OPERATES NORMAL AT THIS TIME.

Part: OIL SYSTEM — LOW (APU) · airframe 76,705 hrs · 16,548 cycles

2 APU FAULT ON ATTEMPT TO START AFTER LANDING. START RPM STAGNATED BETWEEN 30%-40%. FOUND OIL LEVEL AT 50%, SERVICES OIL IAW AMM 12-13-04. OPS CHECK GOOD AT THIS TIME.

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 76,671 hrs · 16,536 cycles

APU FAULT 2 ATTEMPTS NO START. PERFORMED 3 SUCCESSFUL APU STARTS WITH NO DEFECTS NOTED IN REF TO AMM 49-11-00, PERFORMED BITE TEST PER FIM 49-11 FT 987, NO FAULTS NOTED AT THIS TIME.

Part: TRANSCEIVER — FAILED (WEATHER RADAR) · airframe 76,632 hrs · 16,521 cycles

LEFT WEATHER RADAR FAIL. R&R WXR RADAR TRANSCEIVER IAW AMM 34-43-01. OPS GOOD.

Part: FUSE — DEFECTIVE (APU) · airframe 76,621 hrs · 16,518 cycles

APU INOP. AFTER APU START UP, ENGINE SHUTDOWN NO APU BLEED PRESSURE. REMOVED AND REPLACED GROUND INTERLOCK FUSES IAW SWPM 20-84-18, APU/FUNCTION NORMALLY AT THIS TIME.

Part: LIGHT — INOPERATIVE (CONTROL PANEL) · airframe 76,633 hrs · 16,522 cycles

LEFT ENGINE BLEED AIR SWITCH LIGHT BURNT OUT (FLOW BAR SIDE). REMOVED AND REPLACED BLEED AIR SUPPLY CONTROL PANEL IAW AMM 36-11-26. REMOVED & REINSTALLED ON NEW PANEL DUCT PRESSURE INDICATOR IAW AMM 36-21-02. OPS CHECK GOOD AT THIS TIME. LT ENG BLEED FLOW BAR ILLUMINATED AT THIS TIME.

Part: CONTROL PANEL — INOPERATIVE (EXTERNAL POWER) · airframe 76,617 hrs · 16,516 cycles

EXT PWP FOUND TO BE INOP. R&R P5 ELEC PANEL IAW AMM 24-22-01. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. THIS INSTALLED PART IS A CONFIRMED GOOD PART.

Part: CONTROL SWITCH — FAULTY (WINDOW HEAT) · airframe 76,611 hrs · 16,514 cycles

FWD LEFT WINDOW HEAT LIGHT INOP. REPLACED FWD CONTROL SW AS PER 30-40-01-00. OPS CHECKS GOOD.

Part: CLAMP — BROKEN (APU) · airframe 96,582 hrs · 16,504 cycles

FOUND BROKEN CLAMP ON APU SURGE VALVE DUCT. REMOVED AND REPLACED APU CLAMP AT SURGE VALVE IAW AMM 49-53-01 OPS CHECK NORMAL.

Part: DUCT — UNSECURE (COCKPIT) · airframe 76,579 hrs · 16,502 cycles

LARGE VOLUME AIR COMING OUT F/O LEFT FOOT WELL. RESECURED DUCT REF AMM 21-58-10.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 76,560 hrs · 16,495 cycles

R ENG BLEED OFF EICAS MSG AFTER STARTING R ENG. COMPLIED WITH FIM 26-18 FAULT TREE 804. OPS CHECK OK.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 76,560 hrs · 16,495 cycles

BEFORE BLOCK OUT R STRUT DUCT LEAK EICAS CAUTION, COUPLED WITH R DUCT LEAK LIGHT ON OVERHEAD. COMPLIED WITH FIM 26-18 FAULT TREE 804, OPS CHECK NORMAL.

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 103,030 hrs · 19,820 cycles

LEFT WEATHER RADAR FAIL. PERFORMED WX RADAR SYSTEM TEST IAW AMM 34-43-TASK 805, NO FAULTS FOUND AT THIS TIME.

Part: TRANSCEIVER — MALFUNCTIONED (WEATHER RADAR) · airframe 76,525 hrs · 16,484 cycles

WX RADAR INTERMITTENT FAIL STATUS WXR SYS. REMOVED AND REPLACED LT WXR TRANSCEIVER IAW AMM 34-43-01. PERFORMED OPS, GOOD AT THIS TIME.