N1489A

Part: SENSOR — FAULTED (RT ENGINE) · airframe 118,349 hrs · 24,984 cycles

RIGHT ENGINE CONTROL EICAS MESSAGE AFTER PUSHBACK FROM GATE AFTER ENGINE START, ACFT RETURNED TO GATE (BTB), AND MTX GROUNDED ACFT, MTX TROUBLESHOT & PERFORMED BIT PROCEDURE ON RH PIMU. FOUND SENSOR T25 FAULTING. R & R T25 CIT SENSOR ON RT ENGINE IAW FIM 73-21-00 & AMM 73-21-01 .OPS CHECKED GOOD PER TEST 11 OF AMM 71-00-00, ACFT RELEASED ETOPS 180, & RETURNED TO SERVICE.

Part: INDICATOR — UNRELIABLE (AIRSPEED) · airframe 117,280 hrs · 24,580 cycles

DURING CLIMB, AIRSPEED UNRELIABLE / STUCK AT 270 KTS INDICATION OF OVERSPEED WITH FLAPS & GEAR UP AT 270 KTS. EMERGENCY DECLARED, AIR TURN BACK. (ATB) . MAINTENANCE T/S - ALT VMO SWITCH SELECTED IAW CDL 32-12-1. AIRSPEED TAPE WILL SHOW 270 KTS. PERFORMED LANDING GEAR OPERATION ABOVE DESIGN SPEED CONDITIONAL INSPECTION IAW B767 AMM 05-51-07. NO DEFECTS NOTED. A/C REMAINS NO ETOPS. A/C RETURNED TO SERVICE.

Part: STARTER — MALFUNCTIONED (ZONE 500) · airframe 117,062 hrs · 24,506 cycles

DURING TAXI WHILE STARTING #2 ENGINE THE ENGINE FAILED TO START, A/C RETURNED TO GATE (BTB) AND MTX GROUNDED A/C. MTX TROUBLESHOT AND FOUND STARTER HAD FAILED INTERNALLY AND STARTVALVE WAS STICKING OPEN. MTX REMOVED AND REPLACED RH START VALVE IAW AMM 80-11-01. AND REPLACED #2 STARTER IAW AMM 80-11-02 . BOTH OPS CHECK GOOD . RETURNED A/C TO SERVICE START VALVE PN 3291172-2 SN 1191C TSN 1564 TSO 1564 TSO 1564

Part: VALVE — MALFUNCTIONED (ZONE 500) · airframe 116,893 hrs · 24,447 cycles

DURING TAXI WHILE DEICING A/C L ENGINE ANTI-ICE EICAS 5PSI L ENGINE PACK ILLUMINATED ON EICAS, A/C THEN RETURED TO THE GATE AND MTX GROUNDED A/C, MTX THEN TROUBLESHOT PER FIM 36-20 FT 804 FOUND PRSOV VALVE STUCK CLOSED WITH ZERO PSI.REPLACED LH PRSOV PER AMM 36-11-09 ANTI ICE TEST ACCOMPLISHED PER AMM 30-21-00 NO DEFECTS NOTED A/C REMAINS NO ETOPS.AND RETURNED AC TO SERVICE.

Part: RELAY — MALFUNCTIONED (PITOT HEAT) · airframe 116,825 hrs · 24,424 cycles

DURING TAXI CREW REPORTED AFTER STARTING L&R ENG. EEC MODE AND PROBE HEAT EICAS MESSAGE DISPLAYED , A/C RETERNED TO THE GATE (BTB) AND MTX GROUNDED A/C , FOUND RELAY K528 AND RELAY SOCKET MELTED, REPLACED K528 RELAY SOCKET AND RETERMINATED ASSOCIATED WIRING IAW B767 WDM 30-31-21C AND SWPM 20-81-12, ALSO REMOVED AND REPLACED K528 RELAY, OPS AND CONTINUITY CHECK GOOD, .OPS AND CONTINUITY CHECKS GOOD IAW AMM 30-31-00.AIRCRAFT REMAINS NO ETOPS. A/C RETURNED TO SERVICE.

Part: PROXIMITY SWITCH — MALFUNCTIONED (ZONE 100) · airframe 116,825 hrs · 24,424 cycles

"ATC DECARED EMERGENCY CREW REPORTS LND GEAR MONITOR, NOSE A/G DISAGREE, AIR/GROUND DISAGREE STATUS MESSAGES DISPLAYED IN FLIGHT UPON LANDING NO AUTOBRAKES, NO GROUND SPOILERS, NO THRUST REVERSERS AVAILABLE ON TAXI IN MN CARGO DOOR, + L REV ISLN VAL STATUS MESSAGE DISPLAYED ""UNABLE TO ARM AUTOBRAKES INFLIGHT""MTX GROUNDED A/C AND REPLACED PSEU IAW AMM 32-09-04 OPS CHECK GOOD NO FAULTS NOTED AT THIS TIME, INITIALLY FOUND AIR/GRND CIRCUIT BREAKER POPPED AND WOULD NOT RESET. AFTER REPLACING PSEU CIRCUIT BREAKER STAYS IN. NO MESSAGES. RETURNED AC TO SERVICE LP:39036-81/1-2"

Part: WARNING MESSAGE — FALSE ACTIVATION (ZONE 700) · airframe 116,564 hrs · 24,325 cycles

DURING TAXI, PARKING BRAKE EICAS MSG ILLUMINATED AND PARKING BRAKE ILLUMINATED AC RETURNED TO GATE (BTB) AND MTX GROUNDED AC . MTX PERFORMED OPS CHECK OF THE PARKING BRAKE SYSTEM ,UNABLE TO DUPLICATE .OPS CHECK GOOD IAW AMM 32-44-00. AND RETURNED AC TO SERVICE

Part: SHUTOFF VALVE — MALFUNCTIONED (ZONE 500) · airframe 116,484 hrs · 24,293 cycles

DURING DE-ICE BOTH L & R PACKS & L & R ENGINE BLEEDS OFF. L ENG BLEED DID NOT DISPLAY "OFF" NOR WAS A "L ENG BLEED OFF" EICAS MSG DISPLAYED .AC RETURNED TO THE GATE (BTB) AND MTX GROUNDED AC . TROUBLESHOT AND REMOVED AND REPLACED L/H ENG PRSOV IAW AMM 36-11-09. ALL OPS CHECKS NORMAL. ALL INDICATIONS NORMAL. NO LEAKS NOTED AT THIS TIME. A/C REMAINS NO ETOPS. AND AC WAS RETURNED TO SERVICE

Part: GENERATOR — WARNING LIGHT (ZONE 100) · airframe 116,334 hrs · 24,233 cycles

LH GEN DRIVE LIGHT ON PUSHBACK FOLLOWED QRH PROCRDURES AC RETURNED TO THE GATE AND MTX GROUNDED AC , MTX DEFERRED GEN FOR DEPARTURE AND RETURNED AC TO SERVICE .

Part: UNKNOWN — ODOR (CABIN) · airframe 116,116 hrs · 24,148 cycles

CREW REPORTS THERE WAS A STRONG BURNT RUBBER SMELL IN COCKPIT ON DECENT AND AFTER LANDING. MTX GROUNDED AC AND PERFORMED AR CONDITIONING SYSTEM OIL SMOKE /FUME PRACTICE IAW B767 AMM 21-00-21 . NO ODER PRESENT / NO OIL CONTAMINATION NOTED .OPERATIONAL TEST OF BOTH PACKS OKAY. MTX RETURNED AC TO SERVICE .

Part: DRIVE ASSY — MALFUNCTIONED (WEATHER RADAR) · airframe 116,028 hrs · 24,111 cycles

WXR RADAR FAIL MULTIPLE TIMES ON CLIMB OUT. WXR SYS STATUS MSG DISPLAYED. AC PERFORMED ATB AND LANDED MTX GOUNDED AC. REMOVED AND  REPLACED WXR DRIVE UNIT IAW B767 AMM 34-45-07. NO ADJUSTMENT REQ. DPS CHECK IAW B767 AMM 34-43-00. NO DEFECTS NOTED AT THIS TIME. RETURNED AC TO SERVICE

Part: PRESSURE SWITCH — MALFUNCTIONED (HYD SYSTEM) · airframe 115,805 hrs · 24,023 cycles

ON PUSH BACK C HYD PRES EICAS MSG AND CENTER HYD DISCRETE LIGHT ILLUMINATED AC RETURNED TO GATE AND MTX GROUNDED AC TROUBLE SHOT FOUND CENTER HYD PRESSURE SITCH FAULTY R/R CENTER HYD PRESS SWITCH S35 REF AMM 29-11-09. OPS CHECK LK CHECK OK. AND RETURNED AC TO SERVICE

Part: FRAME — CORRODED (BS 1562 S38-39R) · corrosion level 2 · airframe 115,305 hrs · 23,849 cycles

CORROSION ON FRAME WEB AT STA 1562 BETWEEN STGR 38RH AND STGR 39RH(<P>CORROSION ON FRAME WEB WAS REPAIRED PER CMA-TLS 24-0135-03B. NO FURTHER DEFECTS NOTED.</P>)

Part: PANEL — GOUGED (FWD CARGO) · airframe 115,305 hrs · 23,849 cycles

FUSELAGE, FWD CARGO HANDLING PANEL, LH SIDE OF CUTOUT, WITH GOUGES.(<P>GOUGE ON SECTION 43 FUSELAGE BEARSTRAP AT THE CUTOUT BETWEEN STA 453/478 AND STGR 23 RH WAS REPAIRED PER CMA-TLS 24-0155-03B. NO FURTHER DEFECTS NOTED.</P>)

Part: PANEL — CORRODED (AFT CARGO) · corrosion level 2 · airframe 115,305 hrs · 23,849 cycles

AFT FUSELAGE, AFT CARGO HANDLING PANEL, CUTOUT AT RH UPPER CORNER, WITH CORROSION(<P>CORROSION ON SECTION 46 FUSELAGE BEAR STRAP AT CUT OUT WAS REPAIRED PER CMS-TLS 24-0150-03B. NO FURTHER DEFECTS NOTED.&NBSP;</P>)

Part: TORQUE TUBE — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 115,305 hrs · 23,849 cycles

RH WING INB FLAP, INB RIB TORQUE TUBE SUPPORT UPPER ATTACHMENT BOLT HOLE WITH CORROSION.(<P>CORROSION ON RH WING INBOARD MAIN FLAP END RIB AT TORQUE TUBE SUPPORT HOLES (2 EA) WERE REPAIRED PER CMA-TLS 24-0152-02B. NO FURTHER DEFECTS NOTED.&NBSP;</P>)

Part: SUPPORT BEAM — CORRODED (RT WING) · corrosion level 2 · airframe 115,305 hrs · 23,849 cycles

RH WING, MAIN LANDING GEAR SUPPORT BEAM, BUSHING OUTER RACE CAVITY, WITH CORROSION.(<P>CORROSION ON RH MLG SUPPORT BEAM AT HOLE FOR AFT TRUNNION BUSHINGS WAS REMOVED AND REPAIRED PER CMM 57-54-13. NO FURTHER DEFECTS NOTED.</P>)

Part: SHEAR WEB — CORRODED (BS 267) · corrosion level 2 · airframe 115,305 hrs · 23,849 cycles

ELECTRONIC ELECTRIC COMPARTMENT, CORROSION ON THE BEAM AT STA 266.5, ON 40RBL(<P>SHEAR WEB WAS REPLACED PER DWG 141T5400. NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 115,305 hrs · 23,849 cycles

LH HORIZONTAL STABILIZER, LH ELEVATOR, DELAMINATION ON THE OUTBOARD LOWER SKIN BETWEEN OF ELEV STA 325.109 AND ELEV STA 251.665(<P>DELAMINATION ON LH ELEVATOR LOWER SKIN BETWEEN ELEV STA 325.109 AND ELEV STA 251.665 WAS REPAIRED PER SRM 55-20-01-2R-1. NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 115,305 hrs · 23,849 cycles

FOUR DENTS ON RH WING, INB AFT FLAP UPPER SKIN AT: 1) IFS 114.5 AND 7" FROM T/E 2) IFS 119.5 AND 5.5" FROM T/E 3) IFS 121.75 AND 3" FROM T/E 4) IFS 122.5 AND 5.8" FROM T/E(<P>DENTS (ITEM 2,3 AND 4) ON RH WING, INB AFT FLAP UPPER SKIN WERE REPAIRED PER SRM 57-53-01-2R-1. NO FURTHER DEFECTS NOTED.</P>)

Part: FLAP TRACK — DAMAGED (LT WING) · airframe 115,305 hrs · 23,849 cycles

LEFT WING TRAILING EDGE OUTBOARD FLAP, TRACK #2 ON INBOARD STAP AFT LOWER HOLE ELONGATED.(<P>FLAP TRACK #2 FITTING ASSY 1-3 WITH ELONGATED HOLES (2 EA) WERE REPAIRED PER CMA-TLS 24-0138-11B. NO FURTHER DEFECTS NOTED.</P>)

Part: SUPPORT BEAM — CORRODED (LT WING) · corrosion level 2 · airframe 115,305 hrs · 23,849 cycles

LH WING, MAIN LANDING GEAR SUPPORT BEAM, BUSHING OUTER RACE CAVITY, WITH CORROSION.(<P>CORROSION ON LH MLG SUPPORT BEAM AT HOLE FOR AFT TRUNNION BUSHINGS WAS REMOVED AND REPAIRED PER CMM 57-54-13. NO FURTHER DEFECTS NOTED.</P>)

Part: FLAP TRACK — DAMAGED (LT WING) · airframe 115,305 hrs · 23,849 cycles

LEFT WING TRAILING EDGE OUTBOARD FLAP, TRACK #1 ON INBOARD STAP AFT LOWER HOLE ELONGATED(<P>TWO (2 EA) ELONGATED HOLES ON LH WING FLAP TRACK #1 FITTING ASSY 1-3 WERE REPAIRED PER CMS-TLS 24-0139-17B. NO FURTHER DEFECTS NOTED.</P>)

Part: FLAP TRACK — DAMAGED (RT WING) · corrosion level 2 · airframe 115,305 hrs · 23,849 cycles

RIGHT WING TRAILING EDGE OUTBOARD FLAP, TRACK #8 ON INBOARD STRAP AFT LOWER HOLE ELONGATED.(<P>(3 EA) ELONGATED HOLES, HOLE WITH GOUGE AND HOLE WITH CORROSION ON RH WING FLAP TRACK #8 FITTING ASSY 1-3 WERE REPAIRED PER CMA-TLS 24-0137-11B. NO FURTHER DEFECTS NOTED.</P>)

Part: FLAP TRACK — CORRODED (RT WING) · corrosion level 2 · airframe 115,305 hrs · 23,849 cycles

RH WING INB FLAP, TRACK #6 ATTACHMENT BOLT HOLES WITH CORROSION.(<P>&NBSP;</P> / <P>CORROSION ON RH WING INB FLAP, TRACK #6 BOLT HOLES (2 EA) WERE REPAIRED PER CMA-TLS 24-0132-06B. NO FURTHER DEFECTS NOTED.</P> / <P>&NBSP;</P>)

Part: APU — LOW PRESSURE (ZONE 100) · airframe 116,409 hrs · 24,263 cycles

STARTED RIGHT ENGINE DURING TAXI . GOT 2 HUNG STARTS. N 2 MAX WAS 40. QRC DID NOT FIX IT(APU AIR DUCT PRESS LOW) AC RETURNED TO GATE (BTB) AND MTX GROUNDED AC .AND DEFERRED APU AIR FOR DEPARTURE IAW ABX-49-11-1-1 .AND RETURNED AC TO SERVICE.

Part: ECU — UNKNOWN (UNKNOWN) · airframe 114,053 hrs · 23,385 cycles

ENGINE FAILURE ( ROLLBACK) RIGHT SIDE.(<P>PERFORMED TROUBLESHOOTING OF #2 ENGINE FLAMEOUT IAW B767 FIM 71-05 FT 841 TO BLOCK 4 ITEM 23 SHEET 2.</P> / <P># 2 ENGINE REQUIRES REPLACEMENT OF WIRING FOR R/H RVDT FROM EEC TO RVDT. R/R WIRING FROM R/H RVDT TO EEC ON # 2 ENGINE T/R IAW B767 SWPM, OPS CHECKED GOOD. R/R RH ENGINE ECU IAW AMM 73-21-15, OPS CHECKS GOOD. NO DEFECTS NOTED. R/R L/H FEEDBACK RVDT&NBSP; S/N OFF MPP00671 P/N OFF 3M3-205A IAW AMM 78-36-03, CHECK GOOD.</P>)

Part: ECU — UNKNOWN (UNKNOWN) · airframe 114,051 hrs · 23,384 cycles

ENGINE FAILURE (ROLL BACK) RIGHT SIDE (IFSD)(<P>PERFORMED T/S OF #2 ENG FLAEMOUT IAW FIM 71-05 FT 841 TO BLOCK 4 ITEM 23 SHEET 2. #2 ENGINE REQ REPLACEMENT OF WIRING FOR RH RVDT FROM EEC TO RVDT. R/R WIRING FROM RH RVDT TO EEC ON #2 ENG T/R IAW SWPM, OPS CHECK GOOD. R/R RH ENG ECU IAW AMM 73-21-15, OPS CHECK GOOD. NO DEFECTS NOTED. R/R LH FEEDBACK RVDT SN OFF MPP00671 PN OFF 3M3-205A IAW AMM 78-36-03, OPS CHECK GOOD.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 113,511 hrs · 23,184 cycles

#2 ENG PNEU DUCT SUPPORT ROD BOLT MISSING 12 O'CLOCK POS FWD OF PRV .(<P>INSTALLED BOLT #2 ENG PNEU DUCT AT 12 O'CLOCK POS FWD OF PRV PER AMM 20-11-0</P>)

Part: LATCH — UNKNOWN (UNKNOWN) · airframe 113,511 hrs · 23,184 cycles

NACELLE STRUT #1 ACCESS DOOR AFT LATCH IS NOT PROPERLY SEATED(<P>REMOVED AND REPLACED 4EA LATCHES AT #1 ENG NACELLE STRUT ACCESS DOORS IAW B767 SRM 51-40-02. OPS CHECK GOOD.</P>)

Part: ELT — UNKNOWN (UNKNOWN) · airframe 113,511 hrs · 23,184 cycles

SUPERNUMERARY PORTABLE ELT AUTOMATIC RELEASE SEAL DAMAGE. P/N 1151324-1 S/N 1151324-05962 06 NOV 23(<P>REMOVED AND INSTALLED PORTABLE ELT AT SUPERNUMERARY POSITION AS PER B767-300F&NBSP;&NBSP;AMM 25-60-10. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 113,511 hrs · 23,184 cycles

NACELLE STRUT # 1 AFT FAIRING LOWER PANEL HAS ONE SCREW MISSING AT O/B SIDE .(<P>INSTALLED MISSING SCREW AT NACELLE STRUT #1 AFT FAIRING O/B SIDE IAW B767 SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)

Part: SURGE VALVE — UNKNOWN · airframe 113,511 hrs · 23,184 cycles

APU SURGE VALVE PNEUMATIC DUCT ASSY RUBBER COUPLING IS DAMAGED(<P>REMOVED AND REPLACED APU SURGE VALVE PNEUMATIC DUCT ASSY PER AMM 44-53-01-404-010. LEAK CHECK OK&NBSP;</P>)

Part: SNUBBER — UNKNOWN (UNKNOWN) · airframe 113,511 hrs · 23,184 cycles

NLG WHEEL WELL SNUBBERS BRAKE PADS WORN OUT.(<P>REMOVED&NBSP; WORN OUT&NBSP; SNUBBERS&NBSP; PADS&NBSP; LOCATED&NBSP; &NBSP;DRILLED&NBSP; &NBSP;AND&NBSP; INSTALLED&NBSP; NEW&NBSP; SNUBBERS&NBSP; &NBSP;PADS&NBSP; &NBSP;AT&NBSP; NOSE&NBSP; LANDING&NBSP; GEAR&NBSP; WHEEL&NBSP; WELL&NBSP; PER&NBSP; B767-300&NBSP; AMM 32-45-05-022-001 &AMP; AMM 32-45-05-422-007. NO FURTHER DEFECTS NOTED.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 113,511 hrs · 23,184 cycles

LEFT NACELLE STRUT # 1 AFT FAIRING O/B FWD INSPECTION PANEL HAS ONE SCREW LOOSE .(<P>SECURED SCREW AT L/H NACELLE STRUT #1 AFT FAIRING IAW B767 SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 113,511 hrs · 23,184 cycles

FWD E& E CREW OXYGEN NEED SERVICE TO FULL .(<P>SERVICED CREW OXYGEN CYLINDER @ LOWER&NBSP; E&AMP;E COMPARTMENT IAW 767-300 AMM 12-15-08, AMM 35-00-00, AMM&NBSP; 35-11-00 &AMP; AC.&NBSP; 43.13-1B PAR 9-46 THRU 9-51. NO LEAKS NOTED DURING NORMAL OPERATIONAL CHECK</P>)

Part: SEAL — UNKNOWN (UNKNOWN) · airframe 113,511 hrs · 23,184 cycles

LEFT WING O/B FLAP INBOARD EDGE HAS THE UPPER SEAL DAMAGED AT AFT END.(<P>REMOVED DAMAGED SEAL, CLEANED RETAINER LOCATED AND INSTALLED NEW SEAL AT L/H WING O/B FLAP I/B&NBSP; EDGE PER B767-300 AMM 20-10-23-963-001. NO FURTHER DEFECTS NOTED</P>)

Part: PROXIMITY SWITCH — FAULTED (LE SLAT SYS) · airframe 112,756 hrs · 22,939 cycles

LE FLAP ASSYMETRY EICAS MASSAGE WAS LE SLAT ASYM NOT FLAP. C/W FIM PROCEDURE 27-90-14 AND FOUND CODE 284 ON PSEU. REMOVED AND REPLACED LT INBD PROX SWITCH 284 IAW AMM 27-88-01, OPS CHECKED GOOD.

Part: WIRE — DAMAGED (SLAT SYSTEM) · airframe 112,720 hrs · 22,928 cycles

LE SLAT ASYM EICAS MESSAGE ON CLIMB OUT COMPLIED WITH QRH FLAPS STOPPED BETWEEN 1 AND UP(<P>REMOVED AND REPLLACED WIRES W480-05TB/R-20 AND W480-06TB/R-20 IAW WDM 27-88-22&NBSP; AND SWPM 20-00-13 OPS TEST GOOD NO FAULTS NOTED</P>)

Part: NONE — NONE · airframe 112,183 hrs · 22,763 cycles

APU COMP; CORROSION ON AND AROUND MULTIPLE FASTENERS COMMON TO SKIN AND DOOR HINGE ANGLE AT FWD END OF R/H APU DOOR(<P>REMOVED CORROSION FROM AROUND FASTENER COMMON TO DOOR UPPER LONGERON/SKIN. ORIGINAL MATERIAL .050" REMAINING MATERIAL .043". RESTORED PROPER FINISH. AREA WAS BLESSED AS IS IAW EA 22019 REV:IR</P>)

Part: NONE — NONE · airframe 112,183 hrs · 22,763 cycles

FWD CARGO DOOR INNER SKIN GOUGED FWD OF 5TH LATCH VIEWPORT(<P>REMOVED GOUGE FROM FWD CARGO DOOR INNER LOWER BEAM. ORIGINAL MATERIAL WAS .125" REMAINING MATERIAL IS .110". RESTORED PROPER FINISH. AREA WAS BLESSED AS IS IAW B767 EA 22020 REV:IR</P>)

Part: SUPPORT FITTING — NONE · airframe 112,183 hrs · 22,763 cycles

#2 PYLON FAN COWL SUPPORT MOUNT IS CRACKED ON I/B LOWER AFT RADIUS.(<P>REMOVED AND REPLACED #2 PYLON FAN COWL SUPPORT FITTING IAW B767 SRM 51-40-02</P>)

Part: NONE — NONE · corrosion level 2 · airframe 112,183 hrs · 22,763 cycles

LH WING INBD MAIN FLAP LOWER SURFACE HAS AREAS OF BULGING SKIN LOWER CHORD, APROX€™ 52€? FROM THE INBD END THRU THE INBD SIDE OF THE OUTBD FLAP TRACK.(<P>REMOVED THE CORROSION FROM THE AFT LOWER CHORD OF THE LH INBOARD FLAP IAW B767 SRM 51-10-02. ORIGINAL MATERIAL THICKNESS IS 0.150" AND THE REMAINING MATERIAL THICKNESS IS 0.065" AND IS OUT OF LIMITS IAW B767 SRM 57-53-02-1A-1. REMOVED AND REPLACED LH WING I/B MAIN FLAP IAW B767 AMM 27-51-03. (CORROSION LEVEL 2)</P>)

Part: TAPE — NONE · airframe 111,084 hrs

CA AND FO EVAS SECURITY TAPE BROKEN.(<P>REMOVED AND REPLACED EVAS SECURITY TAPE IAW AMM 25-60-99 FOR CA AND FO EVAS</P>)

Part: CONTROLLER — NONE · airframe 110,965 hrs · 22,371 cycles

LEFT PACK OFF REMAINED ILLUMINATED AFTER BOTH ENGINES STARTED(<P>R&AMP;R L PACK TEMP CONTROLLER PER AMM 21-51-14. CONTROLLER USED FROM AC N1373A OPS CHECK GOOD. NO DEFECTS NOTED</P>)

Part: WIRE HARNESS — INOPERATIVE (LT FIRE LOOP) · airframe 110,395 hrs · 22,185 cycles

LEFT ENGINE FIRE LOOP 1 INOP. ETOPS 120 RESTRICTED.(<P>TRANSFERRED TO DMI 154725 IAW MEL 26-11-01-01, CAT 'C'.</P> / <P>LP 1401394, ITEM M8: REMOVED AND REPLACED HARNESS TS682 ENG LWR AFT FIRE DET TO TS683 ENG LWR FWD FIRE DET. WIRE W5324-456R-16 IAW AMM 26-11-11 AND SWPM 20-30-00. OPS CHECK OK. THIS CLEAR DMI 154725. PLACARD REMOVED.</P>)

Part: TRANSCEIVER — NONE · airframe 110,384 hrs · 22,182 cycles

R WEATHER RADAR SYSTEM FAIL.(<P>TRANSFERRED TO MDDR # 154685 IAW MEL 34-43-01, CAT "C". DUE DATE: 03FEB2022. PLACARDS INSTALLED.</P> / <P>LP 1401393 ITEM 5: REMOVED AND REPLACED RH WX TRANSCEIVER IAW AMM 34-43-01. OPS CHECKS GOOD. THIS CLEARS MDDR 154685. MCC NOTIFIED. PLACARDS REMOVED. STR @ 0309Z&NBSP;</P>)

Part: NONE — NONE · airframe 110,382 hrs · 22,181 cycles

WEATHER SYS 2 FAIL "WXR SYS" STATUS.(<P>PERFORMED WX RADAR OPS TEST IAW AMM 34-43-00. OPS NORMAL.</P>)

Part: FIRE WARNING — FALSE ACTIVATION (LT ENGINE)

L ENG FIRE LP 1 STATUS MESSAGE. RAN FIM 26-11 F/T 804. STATUS MESSAGE CLEARED, ENDED AT BLOCK 110 "SYSTEM IS OK" OPS CHECK GOOD AT THIS TIME.

Part: FIRE LOOP — OUT OF POSITION (NR 1) · airframe 110,337 hrs · 22,170 cycles

AFTER ENG SHUTDOWN IN THE BLOCKS L ENG FIRE LP 1 STATUS MESSAGE DISPLAYED.(<P>PERFORMED L ENG FIRE LP 1 INSPECTION, FOUND CONTACT WITH THE LINE, ALIGNED IT IAW AMM 26-11-02. OPS CHECK GOOD.</P>)

Part: WARNING MESSAGE — ILLUMINATED (LT FIRE LOOP)

L ENGINE FIRE LOOP 1 STATUS MESSAGE AFTER ENGINE SHUTDOWN(<P>TRANSFERRED TO DDG IAW MEL 26-11-01-01, CAT C, MDDR 153959, DUE DATE 02OCT2021. PLACARDS INSTALLED.</P>)

Part: APU — OVERSERVICED · 22,150 cycles

APU AUTO SHUTDOWN AFTER PUSH BACK. RESTARTED APU AND RAN FOR 3 MIN THEN SHUT DOWN AGAIN. RETURN TO GATE.(<P>FOUND APU OIL OVER SVCD. PROPERLY SVCD APU IAW AMM 12-13-04. VERIFIED PROPER OIL SVC. PERFORMED FIM 49-11 FT 958. NO FAULTS NOTED. SYSTEM SATISFACTORY. OPS CHECK GOOD PER AMM49-11-00.</P>)

Part: SHUTOFF VALVE — BINDING

STATUS MESSAGE R ENG HPSOV(NOTICED IN FLIGHT) 2 INTERMITTENT EICAS R ENG HPSOV(<P>PERFORMED FIM TASK 36-10 FT 833 UP TO BLOCK 40. PERF AIR SUPPLY BITE PROCEDURE IAW AMM 36-20-00. R ENG HPSOV FAULTING ON BITE. PERFORMED LEAK TEST/OPS CHECK ON HPSOV HP CONTROLLER. NO LEAKS NOTED ON SENSE LINES. HPSOV FAILED LEAK TEST &AMP; TOOK LESS THAN 20 SECONDS TO CLOSE. FOUND HPSOV BINDING WHILE MANUALLY OPENING &AMP; CLOSING. REF LP 1391411(M7) FOR HPSOV R&AMP;R.</P> / <P>20SEP21/1391411/7/ONT REMOVED AND REPLACED R/H (#2) HPSOV IAW B767 AMM 36-11-07. OPERATIONAL CHECK SATISFACTORY. A/C OK FOR SERVICE.</P>)

Part: FIRE WARNING — FALSE ACTIVATION (NR 1) · 22,139 cycles

AFTER ENG SHUTDOWN AT THE BLOCKS L ENG FIRE LP 1 STATUS MESSAGE DISPLAYED. PERFORMED TS PER B767 FIM 26-11 FAULT TREE 804 BLOCK 1-110. STATUS MESSAGE CLEARED. DID NOT RETURN. SYSTEM OK AT THIS TIME. NO FURTHER MX REQ.

Part: CONTROLLER — WARNING MESSAGE

DURING TAKEOFF "R ENG HPSOV" ADVISORY MESSAGE DISPLAYED MOMENTARILY FOLLOWED BY R ENG HPSOV STATUS MSG(<P>TRANSFER TO MDDR 153644 IAW MEL 36-11-02-02 CAT C DUE DATE 26SEP21. MX ACTION C/W.</P> / <P>18SEP, AFW, LP 1391398, ITEM M12: T/S IAW B767 FIM 36-10 FT 843 TO BLOCK 5, NO DEFECTS FOUND. PER MCC REQUEST, REMOVED AND INSTALLED RT ENG HIGH PRESSURE CONTROLLER IAW B767 AMM 36-11-08, ALL CHECKS GOOD. THIS CLEARS MDDR # 153644, MCC NOTIFIED AND PLACARDS REMOVED. RKB @ 1201Z</P>)

Part: SHUTOFF VALVE — WARNING MESSAGE · airframe 110,278 hrs

R ENG HPSOV ADVISORY &AMP; STATUS MSG.(<P>PERFORMED AIR SUPPLY BITE PROCEDURE REF FIM 36-20-00. NO FAULTS NOTED.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENGINE) · airframe 110,252 hrs

L ENG FIRE LP1 STS MSG(<P>PERFORMED FIM TASK 26-11 FAULT TREE 804 ON L ENG FIRE LOOP 1 NO FAULTS FOUND.&NBSP;</P>)

Part: PUMP — INOPERATIVE (RT CENTER)

RIGHT CENTER FUEL PUMP INOP(<P>ITEM TRANSFERRED TO DMI 153192 PER MEL 28-22-02A CAT C DUE DATE 18SEP2021. MX ACTIONS C/W. DL @ 0541Z.</P> / <P>LOG PAGE 1391426: PERF FIM 28-31 F/T 809 GFI CONTINUED TO POP. REMOVED AND REPLACED RT CENTER TANK PUMP ASSY, IAW AMM 28-22-05, OPS NORMAL AT THIS TIME, THIS CLOSES MDDR 153192. PLACARDS REMOVED.</P>)

Part: APU — SHUTDOWN

APU SHUTDOWN BEFORE PUSH. RESTARTED WITH NO ISSUES(<P>PERFORMED OPS CHK OF APU START SYSTEM. OPS CHKS GOOD IAW AMM 49-41-00.</P>)

Part: STATUS MESSAGE — ILLUMINATED (APU DOORS) · 22,117 cycles

APU DOOR STATUS MESSAGE. APU DOOR ACTUATOR C/B RESET AND OPS TEST OK IAW AMM 49-11-00.

Part: CIRCUIT CARD — MALFUNCTIONED (LT ENG OVERHEAT)

L ENG OH LP 1 STATUS MESSAGE(<P>TRANSFERRED TO DMI #152929, CAT C, DUE DATE 12SEP21 IAW DDG 26-11-02-01.</P> / <P>03 SEP 21 - LP 1369067 ITEM 7 - CVG - T/S IAW FIM 26-11 FAULT TREE 804. FOUND L ENG OH LP CARD TO BE AT FAULT. REMOVED AND REPLACED L ENG OH LP1 CARD IAW AMM 26-10-01. OPS TEST GOOD. THIS CLEARS DMI #152929. MCC NOTIFIED. PLACARDS REMOVED</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT FIRE LOOP)

L ENG FIRE LP 1 STATUS MSG(<P>PERFORMED OPS CHK OF THE FIRE DETECTOR SYS. OPS CHECKS GOOD IAW AMM 26-11-00</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (NR 2 EXHAUST FAN)

AFT EXH FAN FAN #2 STATUS MSG(<P>REF FIM 21-51 FT A02. PERFORMED OPS CHECK OF AFT EXH FAN # 2 PER FIM OPS CHECK GOOD AT THIS TIME.&NBSP;</P>)

Part: STATUS MESSAGE — ILLUMINATED (LT FIRE LOOP)

L ENG FIRE LOOP 1 STATUS MESSAGE. REPLACED FIRE OVERHEAT CARD M10224 PER AMM 26-10-01.

Part: SENSOR — FAULTED (FLOW MODULE) · airframe 110,103 hrs · 22,085 cycles

APU INOPERATIVE. REMOVED AND REPLACED FLOW SENSOR ON FLOW SENSE MODULE IAW AMM 49-53-08. OPS CHECK AND SELF TEST DONE IAW AMM 49-11-00 & 49-61-05. BOTH TESTS GOOD AT THIS TIME. LEAK CHECK GOOD AT THIS TIME.

Part: INDICATOR — FAULTED (AIRSPEED) · airframe 110,067 hrs · 22,076 cycles

DURING T/O ROLL AIRSPEED WOULD STAGNATE AT CONSISTENT 20 KTS INTERVALS FOR +/- 2 SECONDS. T/O REJECTED AT 120 KTS.(<P>PERF L&AMP;R ADC BITE PER AMM 34-12-00. SYSTEM TEST GOOD. PER AMM 34-11-00. LEAK &AMP; OPS CHECK PASSED. INSPECTED PITOT TUBES &AMP; DRAIN, NO DESCREPANCIES NOTED.</P>)

Part: ECU — FAULTED (APU)

10 SECONDS AFTER SELECTING AU HYD PUMPS ON DURING BEFORE START APU COMPLETELY SHUT DOWN ALARM SOUNDED.(<P>TRANSFERRED TO MDDR 151805 PER MEL 49-11-01-01. APU PNEUMATICS INOP, CAT C, DUE DATE 23AUG21. DDG 36-11-04 COMPLIED WITH.</P> / <P>LP 1370461 - 14AUG21 - ITEM 4 - ONT - C/W WITH ECM 2021P-274 AND REMOVED AND REPLACED ECU IAW AMM 49-61-05. OPS CHECK GOOD. THIS CLEARS DMI 151805. PLACARDS REMOVED. MCC NOTIFIED.&NBSP;</P> / <P>LP 1370462 - 14AUG21 - ITEM 9 - ONT - C/W ECM 2021P-274, REMOVED AND REPLACED APU CONTROLLER, REF MDDR 151805 FOR R/R. OPS CHECK GOOD.</P>)

Part: VALVE — FAILED (APU PNEUMATIC SY) · airframe 110,019 hrs · 22,065 cycles

APU PNEUMATICS INOP(<P>ITEM TRANSFERRED TO MDDR 151753 PER MEL 49-11-01-01, CAT C. DUE DATE 22-AUG21.</P> / <P>LOGPAGE 1402488 ITEM 4: PERFORMED FIM 49-11 F/T 958, FOUND REVERSE FLOW FAULT DISPLAYED. REMOVED AND REPLACED SURGE CONTROL VALVE. OPS CKS GOOD. THIS CLEARS DMI 151753, PLAC REMOVED.</P>)

Part: CLAMP — LOOSE (APU BLEED) · airframe 109,940 hrs · 22,040 cycles

APU BLEED INOP(<P>TRANSFERRED TO MDDR 151192 IAW MEL 49-11-01A , CAT C.</P> / <P>CVG&NBSP; 08 AUG 21 LP# 1370355 ITEM# M6&NBSP; INSTALLED CLAMP ON PNEUMATIC DUCT TO APU SOV IAW B 767 AMM 36-11-01. LEAK CHECK GOOD.&NBSP; OPS CHECK GOOD.&NBSP; THIS CLEARS DMI 151192, MCC NOTIFIED , PLACARDS REMOVED.&NBSP;</P>)

Part: RADAR — FAULTED (WX SYSTEM)

WX RADAR NOT PAINTING CORRECT W/ TILT(<P>PERFORMED WX RADAR OPS TEST IAW 34-43-00. OPS NORMAL AT THIS TIME. NO DEFECTS NOTED, COULD NOT DUPLICATE ON GROUND.</P>)

Part: OIL SYSTEM — LEAKING (NR 2 ENGINE)

ENG #2 HAS OIL LEAK INSIDE THE FAN SPINNER AREA OF #1 BEARING MANIFOLD(<P>REMOVED AND REPLACED #2 ENG&NBSP; #1 BEARING MANIFOLD IAW AMM 72-31-03</P> / <P>SEE LOGPAGE 1188466 ITEM 15...REPLACED #2 ENG IAW AMM 72-00-00.</P> / <P>&NBSP;</P>)

Part: START VALVE — INOPERATIVE (NR 2 ENGINE) · airframe 109,650 hrs

EICAS MSG: R ENG STARTER(<P>REPLACED #2 ENG STARTER VALVE REF B767 AMM 80-11-02-404-012-H00. PERFORMED START VALVE TEST. OPS CHECK GOOD. NO LEAKS NOTED. REF B767 AMM 71-00-00-995-229-H03.&NBSP;</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (WX RADAR SYS) · airframe 109,417 hrs · 21,882 cycles

'WXR SYS" STATUS MESSAGE(<P>PERFORMED OPERATIONAL TEST OF BOTH WEATHER RADAR SYSTEM IAW AMM 34-43-00. NO FAULTS FOUND AT THIS TIME. NO CURRENT STATUS MESSAGE.</P>)

Part: WARNING MESSAGE — FALSE INDICATION (WX RADAR SYS) · 21,849 cycles

RIGHT RADAR SYSTEM INOP "WXR FAIL" ON MFD(<P>PERFORMED THE WEATHER RADAR SYSTEM OPERATIONAL TEST IAW AMM 34-43-00. NO FAULTS FOUND, OK TO CONTINUE<BR /></P>)

Part: MODULATING VALVE — NOT REPORTED · airframe 109,297 hrs

REF A/P-19857(<P>PER MCC REQUEST R&AMP;R FAN AIR MODULATING VALVE.TEST FAILED AND REINSTALLED ORIGINAL FAMV PER B 767 AMM 36-11-16-404-015-006. TRANSFERRED TO MDDR # 146267 IAW 36-12-02-01. COMPLIED WITH MX PROCEDURES PER DDG. CAT C DUE DATE 12-MAY-21 MCC NOTIFIED. PLACARDS INSTALLED.</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (FIRE LOOP) · airframe 109,297 hrs

STATUS " L ENG FIRE LP 2"(<P>TRANSFERRED TO MDDR 146126 IAW MEL 26-11-01-01 CAT C&NBSP;</P><P>2MAY2021 - 1485163 ITEM #1 - PERFORMED FIM 26-11 FAULT TREE 805, LOOP RESISTANCE CHECKS ACCOMPLISHED. NO DEFECTS NOTED. MDDR CLEARED.</P>)

Part: FITTING — CORRODED (FWD CARGO) · corrosion level 2 · airframe 109,229 hrs · 21,828 cycles

FWD CARGO COMPT. I/B OF LOWER SILL BEAM CARGO HANDLING FITTING HAS EXFOLIATED CORROSION AT FWD O/B MOUNT AT STA 526 RBL 35"(<P>REMOVED CORRODED MOUNT PAD AT FWD CARGO I/B OF LOWER SILL BEAM CARGO HANDLING FITTING FWD O/B MOUNT STA 526 RBL 35". UPON FURTHER EVALUATION FOUND TO BE OUT OF LIMITS 100% MATERIAL LOSS. INSTALLED NEW PAD P/N:451T2505013 PO:1489C-00036 IAW B767 SRM 53-00-15,51-40-02.

Part: SKIN — CRACKED (LT WING) · airframe 109,229 hrs · 21,828 cycles

CRACK NOTED ON THE LH LOWER WING SKIN MOST INBOARD FASTENER COMMON TO STR. L6.5. CRACK LENGTH APPROX .25", MARKED ON AIRCRAFT(<P>REPAIRED LH LOWER WING SKIN MOST IB FASTENER HOLE AT STR. L-6.5 AND REPLACED STR.-6.5 IN COMPLIANCE WITH EO: 6757A140 PART 3, FAS EA 21031 REV. IR, B767 SRM 51-40-02, 51-20-01</P>)

Part: SUPPORT ANGLE — CORRODED (FWD CARGO) · corrosion level 2 · airframe 109,229 hrs · 21,828 cycles

FWD CARGO COMT. LOWER SILL BEAM ANGLE SUPPORT FOR CARGO HANDLING HAS EXFOLIATED CORROSION STA 538(<P>REMOVED DAMAGE ON ANGLE SUPPORT AND IT WAS FOUND TO BE OUT OF LIMITS IAW B767 SRM 53-00-15. REPLACED ANGLE SUPPORT IAW B767 SRM 51-40-02. THE MATERIAL LOOSE ON ORIGINAL PART WAS GREATER THAN 10% THAT IS ALLOWED&NBSP;</P>)

Part: SPAR — GOUGED (LT WING) · airframe 109,229 hrs · 21,828 cycles

LH WING SLAT #2 I/B AUX TRACK, WING FRONT SPAR GOUGE(<P>REWORKED GOUGE LH WING SLAT #2 I/B AUX TRACK L/E FRONT SPAR IN COMPLIANCE WITH FAS EA 21036 REV:IR, B767 SRM 51-10-02, 57-20-10, AMM 51-24-21</P>)

Part: SLAT TRACK — DENTED (LT WING SLAT) · airframe 109,229 hrs · 21,828 cycles

LH WING #1 SLAT O/B AUX TRACK WING L/E HAS 2EA DENTS. REWORKED AREA LT WING NR 1 SLAT O/B AUX TRACK L/E SPAR IN COMPLIANCE WITH FAS EA 21035 REV:IR, SRM 57-20-10, AMM 51-54-21.

Part: STIFFENER — CORRODED (BS 500-588) · corrosion level 2 · airframe 109,229 hrs · 21,828 cycles

FWD CARGO COMPT. DOOR CUTOUT LOWER SILL BEAM UPPER SURFACE ANGLE ATTACHED TO SILL BEAM HAS 4EA SPOTS OF CORROSION BETWEEN STA 500 AND 588(<P>REMOVED AND REPLACED 4EA STIFFENERS ON FWD CARGO DOOR CUTOUT LOWER SILL BEAM IAW B767 SRM 51-40-02 DUE TO ORIGINAL EVALUATION THERE ARE NO PERMITTED LIMITS AVAILABLE IAW B767 SRM 53-00-51-1A-1</P>)

Part: FLOORBEAM — CORRODED (BS 560) · corrosion level 2 · airframe 109,229 hrs · 21,828 cycles

FWD CARGO STA 560 RBL44 APPROX FLOOR BEAM T-CHORD CORRODED. REMOVED CORROSION AT FWD CARGO STA 560 RBL44 FLOOR BEAM T-CHORD. ORIG. MAT. WAS .100 REAINING MAT. IS .050 FOUND TO BE OUT OF LIMITS. REMOVED,FABRICATED, AND INSTALLED NEW T-CHORD PN:BAC1506-3123 7075T-T6511 IAW B767 SRM 51-40-02,51-40-05,53-00-15,51-20-01,AMM 51-24-22,DWG:D141005320</DIV>)

Part: SLAT TRACK — GOUGED (LT WING SLAT) · airframe 109,229 hrs · 21,828 cycles

LH WING SLAT #2 O/B AUX TRACK, WING FRONT SPAR GOUGED(<P>REWORKED AREA LH WING SLAT #2 O/B AUX TRACK L/E FRONT SPAR IN COMPLIANCE WITH FAS EA 21037 REV:IR, B767 SRM 51-10-02, 57-20-10, AMM 51-24-21, 27-81-02</P>)

Part: FLOORBEAM — CORRODED (FWD CARGO) · corrosion level 2 · airframe 109,229 hrs · 21,828 cycles

FWD CARGO LOWER DOOR CUTOUT FLOOR BEAM T-CHORD CORROSION AT STA 560+17(<P>REMOVED CORROSION AT FWD CARGO FLOOR BEAM T-CHORD STA 560+17. ORIG. MAT. .100 REMAINING MAT. .060 FOUND TO BE OUT OF LIMITS. REMOVED,LOCATED,DRILLED, AND INSTALLED NEW FLOOR BEAM T-CHORD P/N:143T8236-17 PO:FS2103420 IAW B767 SRM 51-40-02,51-40-05,53-00-15,51-20-07, AMM 51-20-01</P>)

Part: SUPPORT — CORRODED (BS 820 BL0) · corrosion level 2 · airframe 109,229 hrs · 21,828 cycles

KEEL BEAM STA 820 BL0 APPROX PANEL SUPPORT CORRODED(<P>REMOVED CORROSION FROM KEEL BEAM PANEL SUPPORT AT STA 820. ORIG. MAT. WAS .100 REMAINING MAT. IS .056 FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED PANEL SUPPORT PN:145T8629-2 PO:FS2103139 IAW B767 SRM 51-40-02,53-30-12,51-40-05,51-20-01</P>)

Part: DOOR SILL — CORRODED (BS 560 RBL44) · corrosion level 2 · airframe 109,229 hrs · 21,828 cycles

FWD CARGO STA 560 RBL 44 APPROX DOOR SILL CORRODED(<P>REMOVED CORROSION ON FWD CARGO DOOR SILL STA 560 RBL 44. REWORKED AREA IN COMPLIANCE WITH EA:21033 REV:IR, B767 SRM 51-40-02,51-10-02,53-00-15,51-20-01,AMM 51-24-22</P>)

Part: BEAM — CORRODED (BS 610) · corrosion level 2 · airframe 109,229 hrs · 21,828 cycles

FWD CARGO COMPT. DOOR CUTOUT LOWER SILL BEAM FLOOR SUPPORT ATTACH TO SILL BEAM HAS CORROSION ON UPPER SURFACE AT STA 610(<P>REMOVED CORROSION AT LOWER SILL BEAM STA 610. ORIG. MAT. WAS .100 REMAINING MAT. IS .074 FOUND TO BE OUT OF LIMITS. REMOVE, FABRICATED, AND INSTALLED NEW FLOOR BEAM T-CHORD MAT ID BAC1506-3123 PO: FS2007624 IAW B767 SRM 51-40-02, 51-10-02,51-40-05, AMM 51-54-22.51-24-21</P>)

Part: PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 109,229 hrs · 21,828 cycles

LH WING #1 SLAT LOWER COVE PANEL HAS AREA OF CORROSION JUST I/B OF O/B AUX TRACK(<P>REMOVED CORROSION ON LH WING #1 SLAT LOWER COVE PANEL JUST I/B OF O/B AUX TRACK. ORIG. MAT. WAS .050 REMAINING MAT. IS .031 IS OUT OF LIMITS IAW B767 SRM 57-43-01-1A-01. FABRICATED AND INSTALLED NEW COVE PANEL 526DB IAW B767 SRM 51-40-05,57-43-01,51-40-02,51-20-01</P>)

Part: FLOORBEAM — CORRODED (BS 560) · corrosion level 2 · airframe 109,229 hrs · 21,828 cycles

FWD CARGO LOWER DOOR CUTOUT FLOOR BEAM T-CHORD CORROSION AT STA 560+10(<DIV>REMOVED CORROSION AT FWD CARGO STA 560+10 FLOOR BEAM T-CHORD. ORIG. MAT. WAS .100 REMAINING MAT. IS .055 FOUND TO BE OUT OF LIMITS. REMOVED,LOCATED,DRILLED,AND INSTALLED NEW T-CHORD PN:143T8236-8 PO:FS2103388 IAW B767 SRM 51-40-02,51-40-05,51-10-02,AMM 51-24-21,51-24-22,DWG143T8201</DIV>)

Part: SUPPORT — CORRODED (BS 852 BL0) · corrosion level 2 · airframe 109,229 hrs · 21,828 cycles

KEEL BEAM STA 852 BL0 APPROX PANEL SUPPORT CORRODED(<P>REMOVED CORROSION FROM KEEL BEAM PANEL SUPPORT AT STA 852. FOUND 100% MAT. LOSS IS OUT OF LIMITS. REMOVED AND REPLACED PANEL SUPPORT PN:145T8629-2 PO:FS2103139 IAW B767 SRM 51-40-02,53-30-12,51-40-05,51-20-01</P>)

Part: FLOORBEAM — CORRODED (BS 580) · corrosion level 2 · airframe 109,229 hrs · 21,828 cycles

FWD CARGO LOWER DOOR CUTOUT FLOOR BEAM T-CHORD CORROSION AT STA 580. REMOVED CORROSION ON THE FWD CARGO FLOOR BEAM T-CHORD AT STA 580 ORIG. MAT. WAS .100 REMAINING MAT. IS .070 FOUND TO BE OUT OF LIMITS AFTER DAMAGE REMOVAL IAW B767 SRM 53-00-15 ASSET #00226622. FABRICATED NEW T-CHORD FLOOR BEAM IAW B767 DWG:D141005320 AND INSTALLED IAW B767 SRM 51-40-02.>)

Part: SEAL — LEAKING (STARTER DRAIN) · airframe 109,228 hrs · 21,827 cycles

NBR 1 ENG STARTER DRAIN SHOWS LEAK EVIDENCE - DRAIN LINE CAPPED IAW ECM 2021P-087 SEAL REPLACEMENT DUE WITHIN 10 FLIGHT CYCLES(<P>TRANSFERRED TO&NBSP;NON-MEL 144108</P>)

Part: APU — UNKNOWN · airframe 109,219 hrs · 21,823 cycles

APU FAIL TO START(<P>ECU BITE CHECK IAW AMM 49-61-05. NO FAULTS NOTED. APU OPS TEST NORMAL.<BR /></P>)

Part: APU — MALFUNCTIONED · airframe 109,152 hrs · 21,803 cycles

"APU FAULT" APU FAILED TO START AFTER 3 ATTEMPTS(<P>PERFORMED APU CONTROL UNIT BITE TEST REF AMM 49-61-05. TESTED NORMAL, STARTED APU NORMAL</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (APU) · airframe 109,053 hrs · 21,761 cycles

APU FAULT EICAS (NO FAULT FOUND, APU STARTED PER AMM 49-11-00, START OK.)

Part: STATUS MESSAGE — FALSE ACTIVATION (WX RADAR SYSTEM) · airframe 109,000 hrs · 21,745 cycles

WXR STATUS MESSAGE ON LOWER EICAS ACCOMPANIED BY WXR FAIL ON LOWER ND'S WHEN RIGHT SYSTEM IS SELECTED. OPERATES NORMALLY ON LEFT SYSTEM. PERFORMED WEATHER RADAR SYSTEM TEST IAW AMM 34-43-00. OPS CHECK GOOD.

Part: STATUS MESSAGE — FALSE ACTIVATION (EXHAUST FAN) · airframe 109,000 hrs · 21,745 cycles

AFT EQ EXH FAN 2 STATUS MSG(<P>CLEARED MSG PER FIM 31-41-00, OPS CHECKED PER AMM 21-58-05. OPS NORMAL.<BR /></P>)

Part: CONNECTOR — DAMAGED (APU) · airframe 108,937 hrs · 21,718 cycles

APU INOPERATIVE/(AUXILIARY POWER UNIT (APU), ER OPERATIONS NOT ALLOWED (NOTIFY DISPATCH) R60. TRANSFERRED TO DMI 141801, IAW MEL 49-11-01A, CAT C. REPLACED PIN NR 33 AT CONNECTOR D4111, PER B767 WDM 49-14-11 AND SWPM 20-61-11. OPERATIONS CHECK GOOD, PER B767 AMM 49-11-00. PANELS CLOSED.

Part: AVRANGING UNIT — FAILED (OXYGEN IND) · airframe 108,920 hrs · 21,712 cycles

OXYGEN INDICATION DIFFERENT FROM BOTTLE GAUGE READING. REMOVED AND REPLACED VOLTAGE AVERAGING UNIT, IAW AMM 35-11-06. OPERATIONS CHECK GOOD.

Part: TAIL CONE — OIL CONSUMPTION (NR 2 ENG OIL SY) · airframe 108,935 hrs · 21,717 cycles

REF 74069-NR-0023 RIGHT NR 2 ENG HAS OIL IN TAIL CONE. AFTER FURTHER EVALUATION AND BORESCOPE OF NR 2 ENG CRF IAW B767 AMM 72-00-00-206-175-H00 FOUND OIL WETTING ON SUMP SCAVENGE TUBE AND AT JOINT BETWEEN THE SUMP OUTER WALL AND THE CRF, 6 O'CLOCK POS, WITH THE CURRENT OIL CONSUMPTION AT .12 QTS/HR WHICH IS IN LIMITS. THIS LEAKAGE IS ACCEPTABLE IAW B767 AMM SUBTASK 72-00-00-216-181-H00 PARAGRAPH (7) INSTRUCTIONS. ENG CAN BE PUT BACK IN SERVICE AND OIL USAGE WILL BE CONTINUOUSLY MONITORED.

Part: MODULE — NOT SEATED (PIMU) · airframe 108,910 hrs · 21,709 cycles

IDLE DISAGREE EICAS MESSAGE ON LT ENGINE AFTER START. RE-RACKED THE PIMU MODULE. RAN LT ENG AT IDLE PER 71-01-02. OPERATIONS CHECK GOOD. NO EICAS MESSAGES AT THIS TIME. PIMU RE-RAKED, IAW AMM 77-35-02, MESSAGE CLEARED, PER AMM 31-41-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (EQUIP FAN) · airframe 108,860 hrs · 21,693 cycles

AFT EQ EXH FAN 2 STATUS. PERFORMED FIM PROCEDURE 31-41-00/101 MESSAGE CLEARED, NO FAULTS NOTED.

Part: MODULE — SHORTED (APU) · airframe 108,871 hrs · 21,696 cycles

APU INOPERABLE. TRANSFERRED TO MDDR 141057 PER MEL 49-11-01A CAT "C". FOUND SPLICE MODULE SM1, 3M2, SM16, SM17 SHORTED TO SHIELD. REPAIRED SPLICES, IAW SWPM 20-10-11 & WDM 49-14-11. OPERATIONS CHECK OF APU GOOD AT THIS TIME. THIS CLEARS DMI 1411057, ECM 2021P-013 C/W.

Part: SWITCH — DAMAGED (WINDOW HEAT C/P) · airframe 108,851 hrs · 21,690 cycles

WINDOW HEAT CONTROL PANEL DAMAGED SWITCH. REMOVED AND REPLACED WINDOW HEAT CONTROL PANEL ON P11, IAW B767 AMM 30-41-02. OPERATIONS CHECK GOOD.

Part: IDG — MALFUNCTIONED (LT GENERATOR) · airframe 108,871 hrs · 21,696 cycles

AT CRUISE FL350, L GEN DRIVE EICAS. REMOVED & REPLACED NR 1 IDG, IAW AMM 24-11-01. LEAK & OPERATIONS CHECK GOOD.

Part: UNKNOWN — UNKNOWN (APU) · airframe 108,871 hrs · 21,696 cycles

APU INOPERABLE. TRANSFERRED TO MDDR 141057. C/W STEP 1 OF ECM. NO DEFECTS NOTED BETWEEN D4088 (J10) AND M893, YBMM3 (CONN P11 PIN1) AND CONN P25. PINS D408B (E4) & (E5) SHOWS 187 M OHM, POSSIBLE INSULATION DEGRADATION. PINS (E5) & (J10) 5M OHM. PIN (E5) TO GRD 3M OHM, REF WDM 49-14-11 WAITING ON POWERPLANT EVALUATION FOR NEXT COURSE OF ACTION BASED ON ECM FINDINGS.

Part: OIL SYSTEM — LOW (APU) · airframe 108,830 hrs · 21,684 cycles

APU WOULD NOT START AFTER LANDING. PERFORMED FIM TASK 49-11 FAULT TREE 958, NO DEFECTS NOTED. SERVICED APU OIL, IAW AMM 12-13-01. TO FULL W/ .5 QUART. PERFORMED GBVI OF EWIS, IAW AMM 20-60-04-102-001. PERFORMED OPERATIONS CHECK, IAW AMM 49-11-00. 3 GOOD STARTS AND NO DEFECTS NOTED. ALSO USE A WIDE PNEUMATIC & ELECTRICAL LOAD ON APU.

Part: WARNING MESSAGE — FALSE ACTIVATION (WX RADAR SYS) · airframe 108,736 hrs · 21,650 cycles

WXR SYSTEM STATUS MESSAGE DISPLAYED. "WXR FAIL" MESSAGE DISPLAYED ON HSI DISPLAY. FOUND ENROUTE CB WX RADAR F2 F23 OPEN, CLOSED CB OPERATIONS NORMAL. PERFORMED FIM TASK 34-43 FAULT TREE 805 "WXR BITE", FOUND THE WEATHER SYSTEM OPERATES NORMALLY. NO DEFECTS AT THIS TIME.

Part: VALVE — MALFUNCTIONED (PNEUMATIC SYS) · airframe 108,702 hrs · 21,634 cycles

APU PNEUMATICS SURGING. TRANSFERRED TO MEL 49-11-01-01. MDDR NR 139876 CAT "C" DUE DATE 31DEC20. MCC NOTIFIED. "M" FUNCTION C/W. REMOVED AND REPLACED APU SURGE VALVE, IAW AMM 49-53-01. OPERATIONS CHECK GOOD. THIS CLEARS MDDR NR 139876.

Part: STATUS MESSAGE — FALSE ACTIVATION (EXHAUST FAN) · airframe 108,629 hrs · 21,615 cycles

AFT EQUIPMENT EXHAUST FAN 2 STATUS PRIOR TO DEPARTURE. PERFORMED TASK, PER FIM 21-36 FAULT TREE 806. FAULT NO LONGER REMAINS PRESENT. OPERATIONS CHECKS GOOD.

Part: BLEED AIR SYS — MALFUNCTIONED (APU) · airframe 108,622 hrs · 21,613 cycles

NO DUCT PRESSURE AFTER BLOCK OUT. PERFORMED RESTART ON APU, IAW 49-00-00. DUCT PRESSURE NORMAL AFTER RESTART. APU OPERATIONS NORMAL.

Part: WIRE — UNSECURE (EQUIP VALVE) · airframe 108,524 hrs · 21,585 cycles

FWD EQUIPMENT VALVE EICAS MESSAGE ON PRE-FLIGHT. UPDATED DEFERRAL 138653 TO DDG 21-58-07-02-01. INSTALLED AND SECURED JUMPER WIRES BETWEEN PINS 1 AND 2 AND 5 AND 6, IAW DDG 21-58-07-02-01 PROCEDURE 1, AMM 21-00-00-049-047 AND WDM 21-58-13 UPDATED DMI PLACARD. REMOVED AND REPLACED OVERBOARD EXHUAST VALVE, IAW 21-58-05. OPERATIONS CHECKS GOOD. THIS CLEARS MDDR 138653. DP 1822Z.

Part: SHUTOFF VALVE — INTERMITTENT (RT ENGINE) · airframe 108,520 hrs · 21,583 cycles

RT ENGINE BLEED OFF LIGHT ILLUMINATED INTERMITTENT. TRANSFERRED TO MDDR 138500, IAW MEL 36-11-01-02B, CAT C. REMOVED AND REPLACED RT ENGINE PRSOV, IAW AMM 36-11-09. OPERATIONS NORMAL, THIS CLEARS MDDR 138500.

Part: BLEED VALVE — STICKING (RT ENGINE) · airframe 108,485 hrs · 21,572 cycles

RT ENGINE BLEED VALVE STICKS CLOSED AFTER START AND REQUIRES HIGH PRESSURE/POWER TO OPEN (HIGHER THAN IDLE). PERFORMED ENGINE RUN AND FOUND BOTH ENGINES TO OPERATE NORMAL AT THIS TIME. ALSO PERFORMED BITE MODULE TEST, SYSTEM OPERATES NORMAL AT THIS TIME, REF AMM 71-00-00.

Part: EGT INDICATION — READS HIGH (APU) · airframe 108,473 hrs · 21,569 cycles

INFO ONLY, APU FAILED TO START FIRST ATTEMPT. EGT RAPIDLY REACHED 775 AT 30% RPM & STOPPED ACCELERATING APU. APU FAULT EICAS MESSAGE, NOTED BY MX. APU OPERATIONS CHECK GOOD, IAW AMM 49-11-00.

Part: SOLENOID — FAILED (APU) · airframe 108,421 hrs · 21,554 cycles

APU INOPERABLE ER OPERATIONS NOT ALLOWED. TRANSFERED TO MDDR: 138036, MEL: 49-11-01A CAT C DUE 28NOV20. DISPATCH: DL 0902Z. REMOVED AND REPLACED APU DE-OIL SOLENOID VALVE, IAW AMM 49-27-08. OPERATIONS TEST GOOD. APU COLD SOAK START REQUIRED, REF DMI 138063. THIS CLEARS MDDR 138036, PLACARD REMOVED, MCC NOTIFIED.

Part: APU — MALFUNCTIONED · airframe 108,406 hrs · 21,549 cycles

AFTER LANDING APU FAULT AFTER 3 ATTEMPTS. PERFORMED OPERATIONS TEST OF APU, IAW AMM 49-11-00, APU STARTED AND STOPPED NORMALLY 3 TIMES ON GROUND. PERFORM APU ECU BITE, IAW FIM 49-11 F/T 958 FOUND NO FAULTS ON ECU. OPERATIONS NORMAL AT THIS TIME.

Part: CONNECTOR — CONTAMINATED (LT START VALVE) · airframe 108,216 hrs · 21,488 cycles

LT START VALVE LIGHT DID NOT ILLUMINATE DURING START, TESTED NORMAL WITH LIGHT TEST, STARTER OPERATES NORMAL. FOUND CONTAMINATION & LOOSE CANNON PLUG D10970 ON LT STARTER VALVE. RESECURED, PER WDM 80-11-11 AND CLEANED PLUG, PER AMM 20-60-00. OPERATIONS CHECK OK.

Part: PACKING — LEAKING (IDG OIL LINE) · airframe 108,205 hrs · 21,485 cycles

LT IDG LEAKING FROM FUEL/OIL HEAT EXCHANGER SUPPLY LINE. REMOVED AND REPLACED LT IDG OIL SUPPLY LINE PACKING, IAW 24-11-01. RAN LT ENGINE, IAW 71-00-00. LEAK CHECK GOOD. NO FURTHER DEFECTS NOTED.

Part: WARNING LIGHT — NO INDICATION (START VALVE) · airframe 108,205 hrs · 21,485 cycles

LT ENGINE START VALVE LIGHT DID NOT ILLUMINATE. TRANSFERRED TO MDDR 136201, PER DDG 80-00-01-01, CAT C DUE DATE: 26OCT20. TI: AA @ 1300Z RIV MX, 18OCT. RAN LT ENGINE, IAW 71-00-00, START VALVE OPERATIONS NORMAL. LIGHT ILLUMINATED AND EXTINGUISHED 2 TIMES, THIS CLEARS DMI 136201. BA 1753Z.

Part: UNKNOWN — UNKNOWN · airframe 108,181 hrs · 21,479 cycles

UPON CONNECTING EXTERNAL POWER RIGHT ENGINE SPOOLED TO FLIGHT IDLE FOR FIVE SECONDS BEFORE SPOOLING BACK DOWN TO GROUND IDLE BEFORE SHUTDOWN. PERFORMED ENGINE 2 IDLE RUN. NO DEFECTS NOTED AFTER SHUTDOWN WHEN TRANSFERRING POWER, REF B767 AMM 71-00-00. OPERATIONS CHECK GOOD AT THIS TIME.

Part: APU — INOPERATIVE (APU BAY) · airframe 108,125 hrs · 21,459 cycles

APU INOPERABLE. TRANSFERRED TO MDDR 135790, IAW MEL 49-11-01A, CAT C, EXP 19OCT20 DISP INITIALS ZH 1547Z. REMOVED AND REPLACED APU, IAW AMM 49-11-01. OPERATIONS TEST AND LEAK CHECK GOOD. DMI 135790 CLEARED. PLACARDS REMOVED. TI-1145Z AA.

Part: FAULT LIGHT — FALSE ACTIVATION (APU) · airframe 108,115 hrs · 21,457 cycles

APU FAULT EICAS MESSAGE ON START. PERFORMED BITE OF ECU, IAW FIM 49-11 FT 958. LAST 2 RUNS START ABORTED MINI FLAG TEST SHOWS OK. PERFORMED OPERATIONS CHECK OF APU, IAW AMM 49-11-00. APU STARTED ON FIRST ATTEMPT. ALL OPERATIONS NORMAL, NO DEFECTS NOTED AT THIS TIME.

Part: HEATER — FAILED (PITOT HEAD) · airframe 108,085 hrs · 21,447 cycles

"L AUX PITOT" EICAS MESSAGE ILLUMINATED. PERFORMED FIM TASK 30-31 FT 804. FOUND BAD AUX PITOT. REMOVED AND REPLACED AUX PITOT, IAW AMM 34-11-01. OPERATIONS CHECK GOOD. PERFORM LOW RANGE LEAK AUX LEAK TEST, IAW 34-11-00 AUX 1 AND AUX 2 LEAK CHECK GOOD AT THIS TIME.

Part: CONTROLLER — MALFUNCTIONED (RT ENGINE) · airframe 108,031 hrs · 21,431 cycles

RT ENG HPSOV. TRANSFERRED TO MDDR 135110, PER DDG 36-11-02-02, CAT C. MX ACTION C/W. HPSOV LOCKED CLOSED. DUE 8 OCT 20. REMOVED AND REPLACED HPSOV, IAW AMM 36-11-01 LEAK CHECK PENDING. NO LEAKS NOTED, OPS CHECK NORMAL, IAW AMM 36-11-07. THIS CLEARS MDDR 135110. PLACARDS REMOVED. SP 2035Z S/N OFF: 9805135 P/N OFF 802170-12. REMOVED AND REPLACED HPSOV CONTROLLER ASSY, NO LEAKS NOTED. OPS CHECK NORMAL, IAW AMM 36-11-08.

Part: STATUS MESSAGE — FALSE ACTIVATION (T/R UNIT) · airframe 108,031 hrs · 21,431 cycles

STS MSG T-R UNIT. PERFORMED T/S PER FIM 24-32-F/T 803. NO FAULTS NOTED. SYSTEM OPS CHECK NORMAL.

Part: CONTACTOR — FAILED (GENERATOR) · airframe 108,026 hrs · 21,429 cycles

ON TRANSFER RIGHT GEN WILL NOT POWER LEFT A/C. REMOVED AND REPLACED BTB, IAW AMM 24-22-03. OPS CHECK NO HELP S/N OFF: CL17588, P/N OFF: B430-1. REPLACED LEFT TRANSFORMER RECTIFIER TRU, REFER TO ITEM 1. NO HELP S/N OFF: 2550, P/N OFF: 4-273-03. REPLACED LEFT GCB C901, NO HELP, REF AMM 24-23-01. S/N OFF: CL 17588, P/N OFF: B-430-1. ITEM M3: DURING T/S FOUND NO CONTINUITY ON PINS 17-18, K114, PER SSM 24-20-02. R & R K114, IAW AMM 24-41-01, PERFORMED CONTACTOR INSTALLATION TEST, IAW AMM 24-41-01, NO DEFECT NOTED. S/N OFF: CL-16925, P/N OFF: B429-1.

Part: ECU — MALFUNCTIONED (APU) · airframe 108,024 hrs · 21,428 cycles

NO DUCT PRESSURE FROM APU. TRANSFERED TO MDDR 134869, DDG 49-11-01-01, CAT C. PERFORM FIM TASK 49-11 FT 981 UP TO BLOCK 26, NO DUCT LEAK NOTED AND NO DEFECTS NOTED. STANDBY C-72L/11R DYBY W 10L/9R DUCT PRESSURE WITHIN 2 PSI. REMOVED AND REPLACED APU CONTROL UNIT (ECU), IAW AMM 49-61-05. REACTIVATED APU SHUT OFF VALVE. PERFORMED ENGINE RUN. OPS CHECK DUCT PRESS WITH BOTH PACS ON, IAW AMM 49-11-00, OPS CHECK IS NORMAL AT THIS TIME. ENG RUN PER AMM 71-00-00. PLACARDS REMOVED. THIS CLOSES DMI 134869.

Part: PNEUMATIC SYSTEM — MALFUNCTIONED (APU) · airframe 107,982 hrs · 21,415 cycles

APU AIR PNEUMATIC FUNCTION INOP AUXILIARY POWER UNIT, PNEUMATIC FUNCTION. DEFERRED IAW DDG 49-11-01-01 MDDR 134624, CAT C, DISPATCH 0712Z JJT. PERFORMED OPS CHECK OF APU PNEUMATICS, IAW AMM 49-11-00, OPS CHECK GOOD. PERFORMED BITE OF ECU, NO PREVIOUS FAULTS FOUND. ALL OPS NORMAL. THIS CLEARS DMI 134624, MCC NOTIFIED, PLACARDS REMOVED. PERFORMED BITE OF ECU, IAW FIM 49-11 FT 958 DISPATCH-JL @ 1449Z.

Part: SWITCH — MALFUNCTIONED (ISOLATION VALVE) · airframe 107,925 hrs · 21,397 cycles

LT ISOLATION VALVE INDICATION LIGHT INOP. TRANSFERRED TO MDDR 134049 IAW MEL 36-22-04-01, CAT C. REMOVED AND REPLACED KORRY SWITCH, OPS GOOD. THIS CLEARS DMI #134049, IAW AMM 33-13-00. TIME INITIAL-DC 1135Z.

Part: RELIEF VALVE — INOPERATIVE (RT ENGINE) · airframe 107,871 hrs · 21,381 cycles

RT ENGINE PRV STATUS MESSAGE, INOPERABLE OPEN, APU AIR SOURCE DOR ADP. RT THRUST REVERSOR LOCKED OUT, REF MDDR 133767. RT PRV FAULTS ON AIR SUP BITE AT BLOCK 42 AT FIM 36-10 FT 847. TRANSFERRED TO MDDR NR 133767, PER MEL 36-11-08-01-01A, CAT C, DUE 12 SEP 2020. FAN AIR MOD VALVE LOCKED IN INTERMEDIATE POSITION. DISPATCH NOTIFIED, BR DATA-MCE-BOGUS="1". REMOVED AND REPLACED RT ENGINE PRV VALVE. FAULT CLEARED, LEAK CHECK GOOD, REF AMM 36-11-18/401, MEL 36-11-08-01-01A PROCEDURES REVERSED. PLACARDS REMOVED. THIS CLEARS DMI 133767.

Part: UNKNOWN — LEAKING · airframe 107,779 hrs · 21,353 cycles

FLUID LEAKING FROM TAIL SECTION AROUND APU VISUAL INSPECTION CLEANED THE APU AREA IAW MM 49-05-03. NO LEAKS NOTED AT THIS TIME.

Part: EEC — INOPERATIVE (LT ENGINE) · airframe 107,743 hrs · 21,340 cycles

LEFT ENGINE EEC C1 INOP (ELECTRONIC ENGINE CONTROL (EEC) SYSTEMS, EEC C1 FAULTS (CF6 FADEC))(<P>DEFERRED TO DMI 132560 IAW MEL 73-21-01-05, CAT "A" DUE 300HRS, NO PROCEDURES REQ'D, PLACARDS APPLIED. MX CTRL EDGAR DISPATCH TS 2018.</P><P>LP 1296659:&NBSP;ACCOMPLISHED FIM, FOUND P71 CONNECTOR ON HMU LOOSE. REMOVED AND CLEANED AND RESECURED, ACCOMPLISHED WIRING CHECKS AND OPERATIONAL CHECKS IAW AMM&NBSP;<SPAN>73-21-23</SPAN><SPAN>. NO MESSAGE. OPS CHECKS GOOD. THIS CLEARS MDDR 132560. PLACARD REMOVED.</SPAN></P>)

Part: BLEED VALVE — MALFUNCTIONED (APU) · airframe 107,700 hrs · 21,327 cycles

AFTER ENG START, EICAS MESSAGE APU BLEED VALVE AND VALVE LIGHT ILLUMINATED IN APU SWITCH. MX ACTION C/W. APU SHUTOFF VALVE LOCKED OUT.

Part: SHUTOFF VALVE — FAULTED (APU) · airframe 107,700 hrs · 21,327 cycles

AFTER ENG START EICAS MSG APU BLEED VAL AND VALVE LT ILLUMINATED IN APU SWITCH. APU SHUTOFF VALVE LOCKED OUT. REMOVED AND REPLACED APU AIR SUPPLY SHUT OFF VALVE, IAW AMM 36-11-10, LEAK CHK OK AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 107,667 hrs · 21,318 cycles

T/R UNIT STATUS MSG PERFORMED TS PER FIM 24-32 FT 803, SYSTEM OPS CHECK NORMAL. MESSAGE CLEARED.

Part: UNKNOWN — UNKNOWN (LT BUSS) · airframe 107,667 hrs · 21,318 cycles

LEFT BUSS OFF DURING ENG SHUTDOWN. PERFORMED TROUBLESHOOTING IAW FIM 24-20 FT 801. SYSTEM OPS CHECKED NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 107,700 hrs · 21,327 cycles

LEFT BUSS OFF DURING ENG SHUTDOWN. T/S PER FIM 24-2C BREAKER C901 IAW AMM 24-22-03. RAN ENGINE PER 71-00-00. OPS CHECKED OK.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 107,700 hrs · 21,327 cycles

TR UNIT STATUS MSG(<P>T/S PER FIM 24-32 FAULT TREE 803. OPENED CONT C/D THEN CLOSED. NO MSG SHOWN. SYSTEM OK.<BR /></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 107,667 hrs · 21,318 cycles

STATUS T-R UNIT ON EICAS. PERFORMED FIM TASK 24-32 FAULT TREE 803. STATUS MESSAGE CLEARED PER PROCEDURE 31-41-00.<BR /></P>)

Part: ADC — MALFUNCTIONED (LT & RT) · airframe 107,632 hrs · 21,305 cycles

AIRSPEED DISAGREE, ALTITUDE DISAGREE, AILERON LOCK OUT, RUDDER RATIO EICAS MESSAGE. REMOVED AND REPLACED THE AIR DATA COMPUTER, LEFT AND RIGHT SIDE IAW AMM 34-12-01. OPS CHECKED GOOD. PERFORMED A TEST OF PITOT STATIC SYS IAW AMM 34-11-00, SYSTEM FOUND TO BE WITHIN LIMITS.

Part: WARNING MESSAGE — FALSE ACTIVATION (PITOT SYSTEM) · airframe 107,630 hrs · 21,304 cycles

EICAS MSG CAPT PITOT.(<P>REMOVED AND REPLACED CAPT PITOT LH UPPER PER B767 AMM 34-11-01. PERFORMED LEAK CHECK PER B767 AMM 34-11-00-730-811. NO FAULTS NOTED. SYSTEM WITHIN LIMITS. TEST ON PITOT PER AMM 30-31-00, OPS CHECK NORMAL.</P>)

Part: ECU — MALFUNCTIONED (APU) · airframe 107,545 hrs · 21,278 cycles

APU WILL NOT START. REMOVED AND REPLACED ECU IAW AMM 49-61-05, RUNS OK.

Part: GCU — FAILED (LEFT) · airframe 107,549 hrs · 21,279 cycles

LT AC BUS FAILED DURING POWER TRANSFER WHILE SHUTTING OFF ENGINES PERFORMED BITE TEST OF BPCU. LT GCU FAIL AND BTB SW/WIRWEI GCU MESSAGES. REMOVED AND REPLACED LT GCU PER AMM 24-22-02. OPS CHECK GOOD. FOUND LOOSE CONNECTOR J4 AT ELEC SYS CONTROL PANEL. RECONNECTED CONNECTOR. NO FURTHER DEFECTS NOTED.

Part: UNKNOWN — MALFUNCTIONED (ELECTRICAL SYS) · airframe 107,544 hrs · 21,278 cycles

L AC BUS OFF AFTER ENG SHUTDOWN. PERFORMED BPCU BITE IAW FIM 24-20 TASK 801. NO FAULTS.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 107,538 hrs · 21,275 cycles

T-R UNIT STATUS MESSAGE. PERFORMED FIM 24-32 F/T 803 BOX 1, RESET "DC BUS TIE CONTROL" C/B, MSG CLEARED, PER FIM SYSTEM OK. OPS NORMAL AT THIS TIME.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 107,531 hrs · 21,272 cycles

CABIN ALT AUTO 2 EICAS MESSAGE. REMOVED AND REPLACED AUTO CABIN PRESSURE CTRL SYS IAW AMM 21-31-02. OPS CHECKED OK.

Part: BLADE — NICKED (RT ENGINE) · airframe 107,344 hrs · 21,212 cycles

RH ENG BLADE NR 33 SMALL NICK WITHIN LIMITS IAW AMM 72-31-02-2226-012-H00. BLADE BLEND OUT REPAIR ACCOMPLISHED. PERFORMED A FLUORESCENT PENETRANT INSPECTION IAW AMM 70-11-06-232-001-H00. NO DEFECTS NOTED.

Part: CONTROL PANEL — FAULTY (FUEL SYSTEM) · airframe 107,344 hrs · 21,212 cycles

CTR L FUEL PUMP FLOW BAR NOT ILLUMINATED. REMOVED AND REPLACED FUEL MGMT PANEL IAW AMM 28-22-17.

Part: ECU — INOPERATIVE (APU) · airframe 107,283 hrs · 21,190 cycles

APU PNEUMATIC INOP(<P>TRANSFER TO MDDR 128583 IAW DDG 49-11-01-01, CAT 'C', DUE DATE 30 MAY 20.</P><P>LP&NBSP;<SPAN>1166935:&NBSP;</SPAN><SPAN>REMOVED AND REPLACED APU ECU PER FIM 49-11 FAULT TREE 958 IAW AMM 49-61-05. APU PNEUMATICS OPS CHECKS NORMAL. THIS CLEARS MDDR 128583. ACL @ 04:53</SPAN></P>)

Part: INDICATOR — BROKEN (COCKPIT) · airframe 107,283 hrs · 21,190 cycles

STANBY ENGINE INDICATOR TEST SWITCH BROKEN(<P>REMOVED AND REPLACED STANDBY ENGINE INDICATOR IAW B767 AMM 77-41-01/401. OPS CHECK GOOD.<BR /></P>)

Part: BLEED VALVE — INOPERATIVE (APU) · airframe 107,160 hrs · 21,146 cycles

APU PNEUMATIC INOP.(<P>TRANSFERRED TO MDDR 127865 IAW DDG 49-11-01A, CAT 'C', DUE 13MAY20.</P><P>LOG PAGE 1150403: REMOVED AND REPLACED APU BLEED VALVE IAW 767 AMM 36-11-1 AND OPS CHECK IS GOOD AT THIS TIME. THIS CLEARS DMI #127865.</P>)

Part: PNEUMATIC SYSTEM — INOPERATIVE (APU) · airframe 107,160 hrs · 21,146 cycles

APU PNEUMATIC INOP.(<P>TRANSFERRED TO MDDR 127865 IAW DDG 49-11-01A, CAT 'C', DUE 13MAY20.</P>)

Part: CONTROLLER — MALFUNCTIONED (BLEED AIR SYS) · airframe 107,029 hrs · 21,104 cycles

"R ENG HPSOV" STATUS ON TAXI OUT(<P>PERFORMED AIR SUPPLY BITE CHECK IAW AMM 36-23-00. FOUND RH HPC FLAGGING. REMOVED &AMP; REPLACED RH ENGINE HPC IAW AMM 36-11-08. OPS CHECK GOOD. NO FURTHER FAULTS NOTED.</P>)

Part: MODULATING VALVE — MALFUNCTIONED (CABIN TEMP) · airframe 106,993 hrs · 21,091 cycles

AFT TRIM VALVE INOP(<P>TRANSFERRED TO DMI #126981 IAW MEL 21-61-04-02 , CAT 'C'.<BR DATA-MCE-BOGUS="1" /></P><P>LP&NBSP;<SPAN>822015:&NBSP;</SPAN><SPAN>BIT ZONE TEMP CONTROLLER AND RECEIVED AFT ZONE TRIM VALVE FAULT. CHECKED CONTINUITY FROM D7702 C13 AND C15 TO DXO PIN 1&AMP;2. CONTINUITY CHECK GOOD. PER FIM 21-61 FT 912 , REMOVED AND REPLACED TRIM AIR MODULATING VALVE IAW AMM 21-61-07. OPS CHECK GOOD. DMI 126981 CLOSED.</SPAN></P>)

Part: OXYGEN MASK — BROKEN (COCKPIT) · airframe 106,974 hrs · 21,086 cycles

#3 SUPERNUMERARY SEAT O2 MASK BROKEN(<P>TRANSFERRED TO MDDR 126960 PER MEL 25-25-03, CAT 'D'.</P><P>LOG PAGE 822013:&NBSP;REMOVED AND REPLACED #3 SUP NUM SEAT O2 MASK IAW AMM REF 35-11-51-004-059 AND 35-11-404-060, MCC NOTIFIED AND THIS CLEARS MDDR 126960.</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 106,993 hrs · 21,091 cycles

"CABIN ALT AUTO 2" STATUS.(<P>PERFORMED BITE CHECK PER FIM 21-31 FAULT TREE 810. NO FAULTS NOTED.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 106,958 hrs · 21,080 cycles

CAPT PITOT ON EICAS AFTER TAKEOFF(<P>PERFORMED CAPT PITOT PROBE TEST REF AMM 34-11-01. OPS CHECKED NORMAL. PERFORMED ENG RUNS PERFORMED TEST, ALSO NO FAULTS NOTED. CREW SATISFIED WITH ACFT.</P>)

Part: CONTROLLER — MALFUNCTIONED (CABIN TEMP) · airframe 106,929 hrs · 21,069 cycles

AFT CABIN TEMP EICAS MESSAGE(<P>TRANSFER TO MDDR 126634 IAW DDG 51-61-04-02, CAT C, DUE DATE 13-APR-2020.</P><P>LOG PAGE 822006: REPLACED CONTROLLER CABIN ZONE TEMPERATURE MODULE, PROBLEM RESOLVED, OPS CHECK GOOD AS PER AMM 21-61-03. THIS CLEARS MDDR 126634.</P>)

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 106,937 hrs · 21,072 cycles

WEATHER RADAR SYS LEFT AND RIGHT ERRONEOUS RETURNS, MAGENTA RETURNS WITH LIGHT PRECIPITATION AND LIGHT TURB. GAIN ADJUSTMENT INEFFECTIVE, TILT ADJUSTMENT INEFFECTIVE.(<P>WXR RADAR OPERATIONAL TEST PERFORMED ON GROUND, TEST PASSED ON GROUND. OK FOR RTS. REF AMM 34-43-00-715-001-001. WRX RADAR SYSTEM TEST ALSO PERFORMED REF AMM 34-43-00-735-001, TEST PASS. OK FOR RTS.</P>)

Part: BRACKET — NOT REPORTED (COCKPIT) · airframe 106,849 hrs · 21,045 cycles

CAPTS AND FO'S EVAS SYSTEM INOP ( COCKPIT SMOKE VISION SYSTEM ( CSVS) (STC ST00731LA) )(<P>TRANSFERRED TO MDDR&NBSP;126058 IAW MEL 25-63-06, CAT 'D'.</P><P>LP 1208559: C/W EO 6725A222 EPT &AMP; FURNISHINGS - INSTALLATION NEW BRACKETS - EVAS SYSTEM CAPT AND FO OPS CHECK OK . THIS CLOSES MDDR 126058 - PLACARDS REMOVED. MCC ADVISED.<BR /></P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 106,711 hrs · 20,999 cycles

CABIN AFT ZONE TEMP MSG(<P>TRANSFERRED TO MDDR 125575 IAW DDG 21-61-04-02, CAT 'C', DUE 19MAR20. VERIFIED AFT ZONE TRIM VALVE CLOSED. DISCONNECTED AND STOWED. </P><P>LP 822586: PERFORMED OPS CHECK OF AFT CABIN ZONE TEMP SYSTEM IAW FIM 26-61 FAULT TREE. OPS CHECKED GOOD. NO FAULTS NOTED. THIS CLEARS MDDR 125575. PLACARDS REMOVED.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 106,651 hrs · 20,979 cycles

CABIN ALT AUTO 2 STATUS MSG.(<P>C/W FIM 21-31 FT 810. NO DEFECTS NOTED AT THIS TIME.<BR /></P>)

Part: RADAR — MALFUNCTIONED (WEATHER) · airframe 106,629 hrs · 20,972 cycles

RADIAL SPIKING ON BOTH EHSI RADAR DISPLAYS. ONLY ON L SYS, DID NOT TEST R SYS.(<P>PERFORMED OPS CHK ON LEFT AND RIGHT WXR, TEST PASS. UNABLE TO DUPLICATE FAULT IAW AMM 34-43-00.<BR /></P>)

Part: WARNING LIGHT — NO INDICATION (SPAR VALVE) · airframe 106,621 hrs · 20,970 cycles

LEFT ENGINE SPAR VALVE DID NOT ILLUMINATE ON START.(<P>RECYCLED L ENGINE SPAR VALVES CB AND ATTEMPT ENGINE START SUCCESSFUL AT THIS TIME PER FIM 28-22 FAULT TREE 804.<BR /></P>)

Part: CONTROL UNIT — FAILED (CREW OXYGEN) · airframe 106,539 hrs · 20,942 cycles

CREW O2 EICAS PRESSURE INDICATION INOP (CREW OXYGEN SYSTEM, PRESSURE INDICATION (EICAS))(<P>TRANSFERRED TO MDDR #124460 IAW 35-11-02-01, CAT 'B', DUE 12FEB20, OXYGEN PRESSURE CB COLLARED&NBSP; ST 1837.</P><P>LP 1181412 - M2: REMOVED AND REPLACED VOLTAGE AVERAGING UNIT IAW AMM 35-11-06. OPS NORMAL AT THIS TIME. THIS CLEARS MDDR #124460. PLACARDS REMOVED. MCC NOTIFIED.</P>)

Part: ENGINE — FAILED (LEFT) · airframe 106,492 hrs · 20,928 cycles

LEFT ENGINE VIB INDICATED 4.0 TO 5.0 IN FLIGHT.(<P>FOUND THE #1 ENGINE HAD FAILED. REMOVED AND REPLACED THE #1 ENGINE IAW 71-00-00-401 AND W/C A71-899-04-02. RAN ENGINE FOR LEAKS. NONE FOUND.</P>)

Part: LINE — LEAKING (OIL COOLER BYPAS) · airframe 106,490 hrs · 20,927 cycles

FOUND EVIDENCE OF OIL LEAK FROM #1 ENG.(<P>UPON TROUBLESHOOTING FOUND FUEL/ OIL COOLER OIL BYPASS LINE LEAKING.&NBSP;TIGHTENED LINE, REF AMM 30-11-00.&NBSP;REF M6 FOR IDLE RUN LEAK CHECK.&NBSP;PERFORMED ENG IDLE RUN LEAK CHECK PER AMM 71-00-00. #1 ENG NO LEAKS NOTED AT THIS TIME.<BR /></P>)

Part: GASKET — LEAKING (FUEL HEATER) · airframe 106,500 hrs · 20,931 cycles

AFTER IDLE ENGINE RUN, FOUND FUEL HEATER GASKET LEAKING.(<P>REMOVED AND REPLACED FUEL HEAT EXCHANGER GASKET IAW AMM 79-21-01-424-066-400. NO&NBSP; LEAKS&NBSP; NOTED.<BR /></P>)

Part: ACTUATOR — MALFUNCTIONED (APU INTAKE) · airframe 106,345 hrs · 20,883 cycles

APU WOULD NOT START AFTER TWO ATTEMPTS.(<P>PERFORMED ECU BITE TEST IAW FIM 49-11 FT 859, FAULTED APU DOOR. REMOVED AND REPLACED INTAKE DOOR ACTUATOR IAW AMM 45-15-06. OPS TEST OK .</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 106,295 hrs · 20,870 cycles

R FWD FUEL PUMP EICAS CAUTION ILLUMINATED WHEN FUEL PUMPS WERE TURNED ON FOR ENG START.(<P>CYCLED R FWD FUEL PUMP SW, LIGHT WENT OUT AND STAYED OUT IAW MM CH 28-42-01. NO OTHER ISSUE NOTED IAW MM CH 28-22-00.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 106,244 hrs · 20,853 cycles

STATUS MESSAGE FOR CABIN ALT AUTO 1. PERFORMED FIM 21-31 FT 809. MESSAGE CLEARED. ACFT OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 106,236 hrs · 20,850 cycles

SLIGHT PACK ODOR DURING DESCENT. WET SMELL COMING FROM AIR VENTS. MUSTY TYPE ODOR.(<P>PERFORMED OPS CHECK OF BOTH LEFT AND RIGHT PACK SYSTEMS, NO ODOR PRESENT AT THIS TIME PER AMM 21-63-00.</P>)

Part: UNKNOWN — ODOR (CABIN) · airframe 106,240 hrs · 20,851 cycles

FAINT DIRTY SOCK ODOR DETECTED CLIMBING THROUGH 15000-20000. PERFORMED OPS CHECK OF BOTH LEFT AND RIGHT PACK SYSTEM IAW AMM 21-51-00. NO DETECTED ODOR AT THIS TIME, OK FOR FURTHER SERVICE.

Part: STATUS MESSAGE — FALSE ACTIVATION (APU DOOR) · airframe 106,163 hrs · 20,829 cycles

APU WILL NOT START, 2 ATTEMPTS. APU DOOR STATUS MESSAGE.(<P>PERFORMED FIM 49-11 FT 959, PERFORMED BITE OF APU / SELF TEST, NO FAULTS NOTED, NO MINI FLAGS NOTED. APU STARTED SUCCESSFULLY 4 TIMES, OPS CHK NORMAL AT THIS TIME.&NBSP;</P>)

Part: DUCT — CRACKED (PNEUMATIC SYS) · airframe 106,140 hrs · 20,825 cycles

CRACK FOUND IN PNEUMATIC DUCT IN LEFT WHEEL WELL.(<P>CREW NOTIFIED MAINTENANCE OF SUSPICIOUS AND UNUSUAL NOISE FROM LEFT WHEEL WELL. FOUND DUCTING BELOW CENTER ISOLATION VALVE V46 CRACKED AT FLANGE. REMOVED AND REPLACED DUCT IAW AMM 36-11-01. NO LEAKS FOUND, NO FURTHER DEFECTS NOTED.</P>)

Part: START VALVE — MALFUNCTIONED (RT ENGINE) · airframe 106,118 hrs · 20,814 cycles

RIGHT START VALVE STAYED ILLUMINATED WITH ASSOCIATED EICAS MESSAGE FOR 2 START ATTEMPTS. 3RD START ATTEMPT SUCCESSFUL. MAINTENANCE EXERCISED VALVE MANUALLY PRIOR TO 3RD ATTEMPT. REPLACED THE RT ENG START VALVE IAW AMM 80-11-02, OPS CHECKED GOOD.

Part: START VALVE — NONE · airframe 106,110 hrs · 20,810 cycles

RIGHT START VALVE VERY SLOW TO OPEN.(<P>PERFORMED OPERATIONAL STARTING TEST OF R/H ENGINE IAW AMM 80-11-00, NO DEFECTS NOTED. NO ENG STARTER MSG.</P>)

Part: STARTER — SLOW (RT ENGINE) · airframe 106,112 hrs · 20,811 cycles

R/H ENGINE STARTER SLOW TO ENGAGE, REQUIRED 2 ATTEMPTS TO BE SUCCESSFUL.(<P>PERFORMED OPERATIONAL START OF R/H ENGINE IAW B767 AMM 80-11-00, NO DEFECTS NOTED. NO ENGINE START MSG.<BR /></P>)

Part: DOOR — FROZEN (APU) · airframe 106,022 hrs · 20,786 cycles

MX FOUND ICE ON APU DOOR.&NBSP;(<P>PERFORMED FIM 49-11 FT 959, UP TO BLOCK 36. REMOVED ICE FROM DOOR. PERFORMED OPS TEST OF APU IAW AMM 49-11-00, OPS CHECK NORMAL. REFER TO ITEM 2 FOR COLD SOAK DMI.&NBSP;</P><P>LP 1224934 - ITEM M2: TRANSFERRED TO MDDR 121372 IAW DDG 25-AP-01, CAT 'N', DUE DATE: 30-NOV-20.&NBSP;</P><P>LP 1224938 - ITEM 1: ACCOMPLISHED APU COLD SOAK START SATISFACTORY INTO ONT. THIS CLEARS DMI 121372. PLACARD REMOVED AND MCC NOTIFIED.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENG STARTER) · airframe 106,006 hrs · 20,782 cycles

RIGHT ENGINE STARTER EICAS ON START. RAN QRH, MSG CLEARED. ENGINE STARTED 2ND ATTEMPT.(<P>PERFORMED ENGINE DRY MOTOR&NBSP; IAW AMM 71-00-00. OBSERVED NO FAULTS OR DELAYS AT THIS TIME, OPS CHECK GOOD.</P>)

Part: APU — MALFUNCTIONED · airframe 105,942 hrs · 20,759 cycles

2 FAILED START ATTEMPTS ON THE GROUND; APU.(<P>PERFORMED BITE CHECK OF APU ECM IAW AMM 49-61-05 AND SELF TEST, NO FAULT FOUND. APU STARTED THIRD ATTEMPT, OPS CHECK GOOD AND NO FAULTS NOTED.</P>)

Part: APU — MALFUNCTIONED · airframe 105,904 hrs · 20,746 cycles

APU WOULD NOT START DURING TAXI IN, WORKED FINE AT DEPARTURE STATION.(<P>PERFORMED APU BITE IAW AMM 49-61-05, NO FAULTS NOTED AT THIS TIME. OPS CHECKED APU IAW AMM 49-11-00, OPS CHECK GOOD AT THIS TIME.</P>)

Part: APU — MALFUNCTIONED · airframe 105,907 hrs · 20,747 cycles

APU RELIABILITY COLD SOAK START ACCOMPLISHED ON FLT RFD TO SCK. SAT -66*C, FL 400, START UNSUCCESSFUL, 3 ATTEMPTS.(<P>PERFORMED ECU BITE IAW FIM 49-11 FT 958 LEG 4. REASON SHUTDOWN OCCURRED, REFERENCES DOOR SYSTEM. NO FLAGS. CLEARED ECU. OPS CHECK NORMAL IAW AMM 49-11-00. DMI #120541 REMAINS OPEN FOR COLD SOAK. MCC ADVISED.&NBSP;</P><P><BR /></P><P>NOTE: LP 1216646 - ITEM 3: APU COLD SOAK START ACCOMPLISHED, FIRST ATTEMPT SUCCESSFUL. NOTED BY MX, THIS CLEARS DMI #120541. PLACARDS REMOVED AND MCC NOTIFIED.</P>)

Part: STRUCTURE — UNKNOWN (LT NACELLE) · airframe 86,262 hrs · 17,542 cycles

FAA FINDING ON LH ENG FAN COWLING FAIRINGS.(<P>INSPECTED + MEASURED LH&NBSP; ENG FAN&NBSP; COWL&NBSP; IAW&NBSP; AMM 71-11-00-822-001.&NBSP; FOUND&NBSP; WITHIN&NBSP; ACCEPTABLE&NBSP; LIMITS&NBSP; AT&NBSP; THIS&NBSP; TIME.&NBSP; NO&NBSP; OTHER&NBSP; DEFECTS&NBSP; NOTED.<BR /></P>)

Part: EXHAUST VALVE — MALFUNCTIONED (AC BAY) · airframe 105,821 hrs · 20,721 cycles

AFTER LANDING, FWD EQUIPMENT VALVE DISPLAYED.(<P>TRANSFERRED TO MDDR 120092 IAW MEL 21-58-01-01, CAT 'C', DUE DATE: 13-NOV-19. PLACARDS INSTALLED.&NBSP;</P><P>LP 1116521 - M3: T/S PER B767 FIM 21-58 FT 985. STOPPED @ STEP 4 FOR REPLACEMENT OF EQUIPMENT COOLING INDICATION CARD, M867 IN THE P50 PANEL. P/N 285T0095-8 ON ORDER. MCC NOTIFIED AND DMI REMAINS OPEN.</P><P>LP 1116523 - M2: REMOVED AND REPLACED PRINTED CIRCUIT CARD #M867 IAW AMM 21-58-00, P50 CARD&NBSP; FILE, NO HELP. DMI 120092 REMAINS OPEN. OFF PART (P/N:&NBSP;285T0095-8, S/N: D00575).</P><P>LP 1216648 - M9: REMOVED AND REPLACED FORWARD EXHAUST VALVE (V12) IAW B767 AMM 21-58-05, OPS CHECK GOOD. FORWARD EQUIPMENT COOLING AUTO SYSTEM OPS CHECK GOOD. THIS CLEARS MDDR 120092. PLACARDS REMOVED AND MCC NOTIFIED.</P>)

Part: UNKNOWN — MALFUNCTIONED (LT AC BUSS) · airframe 105,785 hrs · 20,711 cycles

UPON LEFT ENGINE SHUTDOWN DURING TAXI IN, LOST L AC BUS, DIDN'T TRANSFER.(<P>AFTER TURNING A/C DARK, TRANSFERRED POWER FROM GPU TO APU AND APU TO GPU, COULD NOT DUPLICATE FAULT PER AMM 24-51-00.&NBSP;</P><P>LP 1097272 - M7: PER MCC REQUEST, RAN ENGINE IAW AMM 71-00-00 TO PERFORM POWER DISTRIBUTION CHECK PER AMM 24-51-00, OPS CHECK NORMAL AT THIS TIME.</P>)

Part: RELAY — INOPERATIVE (FUEL PUMP) · airframe 105,767 hrs · 20,707 cycles

R CENTER TANK PUMP INOP(<P>TRANSFERRED TO MDDR 119560 PER MEL 28-22-02B, CAT C, PLACARD INSTALLED.</P><P>LP 1097265 - M8: PER MCC REQUEST, REMOVED AND REPLACED RIGHT CENTER PUMP GFI RELAY IAW AMM 28-22-18. R CTR BOOST PUMP OPERATIONAL CHECK NORMAL AT THIS TIME. THIS CLEARS DMI 119560.&NBSP;CIRCUIT COLLARS&NBSP;REMOVED.</P>)

Part: MODULE — MALFUNCTIONED (FLOW SENSING) · airframe 105,745 hrs · 20,696 cycles

WITH APU ON, PAX AIR FLUCTUATION; WITH L/H, R/H OR BOTH PAX SELECTED (APU PNEUMATIC FUNCTION INOP).(<P>TRANSFERRED TO MDDR #119418 IAW DDG 49-11-01-01A, CAT 'C', DUE DATE 30-OCT-2019. MAINT ACTION C/W.&NBSP;</P><P>LP 1097264 - M5: T/S APU BLEED IAW FIM 49-11 FT 958, NO FAULTS NOTED ON SYSTEM TEST OR LRU. MINI FLAG 15 SHOWN.&NBSP;REMOVED AND REPLACED&NBSP;FLOW SENSING MODULE AS PRECAUTIONARY IAW 49-53-08. OPS CHECK GOOD, NO FLUCTUATIONS NOTED AT THIS TIME. RAN ENGINES IAW 71-00-00, NO DEFECTS NOTED BEFORE OR AFTER ENGINE RUN, APU DID NOT FLUCTUATE. OPS CHECK NORMAL AT THIS TIME. MDDR 119418 CLEARED. PLACARDS REMOVED AND MCC NOTIFIED.</P>)

Part: CONTROLLER — MALFUNCTIONED (WINDOW HEAT) · airframe 105,687 hrs · 20,675 cycles

CAPTAIN'S FWD WINDOW ARCED, THEN SHATTERED.&NBSP;(<P>REMOVED AND REPLACED CAPT FWD L1 WINDOW IAW AMM 56-11-01, OPS CHECK NORMAL. OFF PART (PN: 141T4800-13, SN: H2566). REF LP 1097302 - M8 FOR WINDOW HEAT CONTROLLER REPLACEMENT AND LP 1097303 - M10 &AMP; M11 FOR NON-MEL, TORQUE AND SEALANT.&NBSP;&NBSP;</P><P>LP 1097302 - M8:&NBSP;REMOVED AND REPLACED L/H FWD WINDOW HEAT CONTROLLER IAW AMM 30-41-01. LEFT FWD WINDOW HAS HEAT, OPS CHECK GOOD NO DEFECTS AT THIS TIME.&NBSP;</P>)

Part: FAN — FAILED (FWD EQUIPMENT) · airframe 105,665 hrs · 20,668 cycles

FWD EQ SUP FAN 1 STATUS MESSAGE. REMOVED AND REPLACED FWD EQUIPMENT SUPPLY FAN 1 IAW AMM 21-58-06, OPS CHECKED GOOD.

Part: BATTERY — FAULTY (APU) · airframe 105,657 hrs · 20,662 cycles

APU FAULT DURING START, AFTER LANDING. REMOVED AND REPLACED APU BATTERY, REFERENCE AMM 24-31-04. APU STARTS NORMAL AT THIS TIME.

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 105,615 hrs · 20,650 cycles

APU COLD SOAK START FAILED THREE ATTEMPTS FL 410 -55 SAT. PERFORMED APU ECU BITE TEST IAW AMM 49-61-05. NO FAULTS NOTED AT THIS TIME. VF OPENED DMI# 117364. APU COLDSOAK START ATTEMPT SUCCESSFUL ON FIRST ATTEMPT, DMI CLOSED. ECM 2019P-392 TO ISSUED BY PP ENGINEERING.

Part: OIL SYSTEM — LOW (APU) · airframe 105,583 hrs · 20,639 cycles

AFTER LANDING, COULDN'T START THE APU. APU FAULT LIGHT SHOWN. FLT CREW NOTIFIED MX THAT APU WOULD NOT START, 2 ATTEMPTS. BIT ECU IAW 49-11-00, LAST 2 CYCLES "SEE MAINT MAN" AFTER AUTO SHUTDOWN. FOUND APU OIL LOW AND SERVICED IAW AMM 12-13-04, APU START SUCCESSFUL ON 3RD ATTEMPT. NO DEFECTS NOTED ON SUCCESSFUL RUN. ECU SELF TEST GOOD, MINI FLAG #15 ON LAMP CHECK. INFO ONLY: ECU LOCATED IN AFT CARGO AREA, MOISTURE NOTED. OPERATIONAL CHECK GOOD AT THIS TIME.

Part: ECU — MALFUNCTIONED (APU) · airframe 105,534 hrs · 20,623 cycles

APU RELIABILITY COLD START, 3 ATTEMPTS UNSUCCESSFUL. PERFORMED APU ECU BITE CHECK, FAULTED ECU. REMOVED AND REPLACED APU ECU WITH NEW. OPS CHECKED GOOD, PERFORMED 3 SUCCESSFUL STARTS. NO DEFECTS NOTED AT THIS TIME IAW AMM 49-61-05 AND AMM 49-11-00.

Part: APU — MALFUNCTIONED · airframe 105,508 hrs · 20,615 cycles

APU INOPERATIVE. CREW STARTED APU ON SECOND ATTEMPT. PERFORMED START-UP PROCEDURES FOR APU REF AMM 49-11-00. NO FAULTS NOTED AT THIS TIME. APU OPERATION NORMAL, MX STARTED ON FIRST ATTEMPT.

Part: WARNING LIGHT — FALSE ACTIVATION (CABIN TEMP) · airframe 105,489 hrs · 20,609 cycles

ON PREFLIGHT, FOUND AFT CAB TEMP CONT INOP LIGHT ON. PERFORMED BITE CHECK ON TEMP CONTROLLERS AND PACK CONTROLLERS. CLEARED FAULTS AND PERFORMED CONTROLLER FAULT VERIFICATION. NO FAULTS NOTED AT THIS TIME AND OPS CHECK GOOD IAW AMM 21-51-00.

Part: REHEATER — CRACKED (RT A/C PACK) · airframe 105,425 hrs · 20,586 cycles

RIGHT BLEED DUCT LEAK WHILE SITTING AT THE GATE WITH APU ON AND BOTH PACKS RUNNING. COMPLIED WITH QRH. FOUND CRACK IN R PACK REHEATER. REMOVED AND REPLACED THE RT PACK REHEATER IAW AMM 21-51-07. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 105,420 hrs · 20,585 cycles

CABIN ALT AUTO 1 STATUS MESSAGE. C/W BITE TEST OF NR 1 CABIN PRESSURE CONTROLLER IAW AMM 21-31-00, NO DEFECTS NOTED.

Part: FUEL FILTER — FAULTED (LT ENGINE) · airframe 105,391 hrs · 20,573 cycles

ITEM 1 - L ENG FUEL FILTER EICAS MESSAGE AFTER TAKE OFF. ITEM 2 - STATUS MESSAGE, L ENG FUEL FILTER.&NBSP;(<P>REMOVED AND REPLACED LEFT ENGINE FUEL FILTER IAW AMM 73-11-02, LEAK CHECK GOOD.&NBSP;</P>)

Part: TRANSCEIVER — MALFUNCTIONED (WEATHER RADAR) · airframe 105,358 hrs · 20,565 cycles

LEFT WEATHER RADAR PAINTING TARGETS THAT ARE NOT THERE. (<P>RE-RACKED WX RADAR TRANSCEIVER AND PERFORMED OPERATIONAL CHECK IAW AMM 34-43-00-715-026-002. OPS CK NORMAL AT THIS TIME, NO DEFECTS NOTED.<BR /></P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 105,337 hrs · 20,558 cycles

AFT CABIN TEMP EICAS MESSAGE. (<P>DURING POWER TRANSFER FROM APU TO GPU, MESSAGE CLEARED. PERFORMED FIM 21-61 FT 915, NO FAULTS NOTED.</P>)

Part: UNKNOWN — MALFUNCTIONED (CABIN TEMP IND) · airframe 105,318 hrs · 20,550 cycles

"AFT CARGO TEMP LIGHT INOP ( COMPT TEMP INOP LIGHTS / ALL CARGO CONFIGURATION )(<P>PERFORMED BITE TEST OF ZONE TEMP CONTROL UNIT IAW AMM 21-61-03. &NBSP;C/W ADJUSTMENT TEST PER AMM 21-61-03</P>)

Part: IGNITION LEAD — ARCED (NR 1 ENGINE) · airframe 105,247 hrs · 20,527 cycles

ENGINE NR1 IGNITION LEAD (B) SHOWS SIGNS OF ARCING AT THE IGNITER PLUG END OF THE LEAD. (<P>REMOVED AND REPLACED ENG 1 IGNITION LEAD 1 IAW AMM 74-21-01. OPS CHECK GOOD.&NBSP;</P>)

Part: ESCAPE REEL — MISSING (CABIN) · airframe 105,247 hrs · 20,527 cycles

DESCENT DEVICE POSITION "A" MISSING. (<P>INSTALLED DESCENT DEVICE POSITION "A" IAW AMM 25-61-03. NO DEFECTS NOTED AT THIS TIME.</P>)

Part: TRANSCEIVER — MALFUNCTIONED (WEATHER RADAR) · airframe 89,020 hrs · 22,934 cycles

CAPTAIN SIDE WEATHER RADAR FAIL. RIGHT SYSTEM FAILED. REMOVED AND REPLACED R/H WXR TRANSCEIVER IAW B767 AMM 34-43-01. OPS CHECKED GOOD.

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 104,782 hrs · 20,391 cycles

DURING PRE-FLIGHT CHECKS, THE CREW EXPERIENCED SEVERAL INTERMITTENT CARGO FIRE ALERTS.(<P><SPAN>PERFORMED OPS CHECK IAW AMM 26-14-00. NO DEFECTS NOTED AT THIS TIME.</SPAN><BR /></P>)

Part: CONTROL PANEL — MALFUNCTIONED (WEATHER RADAR) · airframe 104,794 hrs · 20,397 cycles

FO'S WX/TERR SELECT BACKLIGHT PARTIALLY INOP(<P>TRANSFERRED TO MDDR 110834.</P><P>LOGPAGE 1050461 - M2: REMOVED AND REPLACED WX RADAR PANEL IAW AMM 34-43-02. OPS CHECK IS GOOD AT THIS TIME. MCC NOTIFIED AND STICKER REMOVED. THIS CLEARS DMI 110834. YK 1346Z</P>)

Part: CONTROL UNIT — FAILED (WINDOW HEAT) · airframe 104,754 hrs · 20,383 cycles

R FWD WINDOW EICAS IN FLIGHT. 1 RESET PER QRH. MSG REAPPEARED, R FWD WINDOW HEAT SWITCH WAS TURNED OFF.(<P>R FWD &AMP; L SIDE WINDOW HEAT CONTROL UNIT FAILED ON BITE PROCEDURE R/R CONTROL UBIT IAW AMM 30-41-01. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.</P>)

Part: SENSOR — MALFUNCTIONED (CIT) · airframe 104,718 hrs · 20,375 cycles

LEFT ENGINE OIL TEMP IS 5 HIGHER THAN THE RIGHT ENGINE. FUEL FLOW FLUCTUATION ON LEFT ENG UP TO 700 LBS. NO ENGINE PARAMETERS WERE EXCEEDED DURING FLIGHT.&NBSP; &NBSP;(<P>LEFT CIT SENSOR REMOVED &AMP; REPLACED. PLEASE SEE ITEM 2 ON LOG PAGE 1032748.</P>)

Part: DISPLAY — MALFUNCTIONED (WX RADAR SYS) · airframe 104,704 hrs · 20,369 cycles

R WXR SYS DISPLAYS "WXR WEAK".(<P>GROUND TEST "WXR SYS". SYSTEM TESTS NORMAL IAW AMM 34-43-00.</P>)

Part: SENSOR — FALSE ACTIVATION (LT ENGINE N1) · airframe 104,704 hrs · 20,369 cycles

LEFT ENGINE N1 UP TO 10% FLUCTUATION ON BELOW THE RIGHT ENGINE, N2 READS 5 % HIGHER THAN THE RIGHT ENGINE. LEFT EGT BLINKS OFF &AMP; ON DURING DESCENT. STATUS MSG L ENG EEC C2. STATUS MESSAGE L PIMU.(<P>L PIMU FAULTED T25 SENSOR CHANNEL A, READING 0 CHANNEL B, READING 92 C.&NBSP; REPLACED T25 SENSOR ON LEFT ENGINE IAW AMM 73-21-02. OPS CHECK NORMAL IAW AMM 71-00-00 TEST 11. ENG RUN &AMP; INDICATION ON N1 &AMP; N2 NORMAL IAW 71-00-00. RESET CONNECTORS ON EGT JUNCTION BOX ON LEFT ENGINE. EGT OPS CHECK NORMAL.&NBSP;</P>)

Part: TRANSCEIVER — INTERMITTENT (WEATHER RADAR) · airframe 104,709 hrs · 20,371 cycles

RH WXR SYS DISPLAYS "WXR WEAK" INTERMITTENTLY.(<P>REMOVED AND REPLACED RH WXR TRANSCEIVER IAW AMM 34-43-02 &AMP; CLEANED CONNECTOR D489 @ M269 WXR FLAT PLATE ANTENNA. OPS CHECKED WXR SYSTEM IAW AMM 34-43-00 &AMP; OPS CHECK NORMAL. NO DEFECTS NOTED AT THIS TIME.</P>)

Part: CIRCUIT CARD — FAILED (SMOKE DETECTION) · airframe 104,684 hrs · 20,364 cycles

MAIN DECK CARGO COMPARTMENT SMOKE DETECTION SYSTEM LOOP #2 INOP.(<P>TRANSFERRED TO MDDR 110407.<BR /></P><P>LP 1032737 - M1:&NBSP;PERFORMED OPS CHECK OF MAIN DECK CARGO FIRE DETECTION PER DDG 26-16-02-10 AND CHECKED FAILED. T/S PER FIM 26-14 TREE 809 AND FOUND PRINTED CIRCUIT FIRE CARD M2026 TO BE BAD. REPLACED AND OPS CHECK IS GOOD. REINSPECT IS GOOD. DMI 110407 REMAINS OPEN.</P><P>LP 1032739 - M5:&NBSP;T/S DISCREPANCY AND RAN FIM 26-14 TREE 809. FOUND NO FAULTS, DMI 110407 REMAINS OPEN PER MCC.</P><P>LP 1032740 - P1:&NBSP;PERFORMED T/S OF MAIN CARGO LOOP 2 SYSTEM IAW AMM 26-14-00 AND FIM 26-14-00 FT 809 OPS TEST NORMAL AT THIS TIME. DMI 110407 REMAINS OPEN AT THIS TIME. FOR FURTHER MONITORING PEP MCC.</P><P>LP 1056815 - M7:&NBSP;PERFORMED FIM 26-14 FT 809, NO FAULTS NOTED, PERFORMED FIN 26-10 FT 803, AFOLTS CARD BITE, NO FAULTS NOTED, PUT MAIN CARGO AFOLTS CARD ON ORDER WITH MCC P/N 285N0028-136 EQUIP # M2026. DMI 110407 REMAINS OPEN.</P><P>LP 1056817 - M1:&NBSP;<SPAN>REMOVED AND REPLACED MAIN CARGO FIRE/OVHT PRINTED CIRCUIT CARD M2026 IAW AMM 26-10-01.&NBSP; OPS CHECK GOOD,

Part: HMU — MALFUNCTIONED (LT ENGINE) · airframe 104,605 hrs · 20,337 cycles

DURING A SHALLOW ENROUTE DESCENT, THE STATUS MSG "L ENG CONTROL" APPEARED. AFTER LANDING "L ENG CONTROL" EICAS APPEARED. REPEAT WRITE UP.(<P>REMOVED AND REPLACED HMU IAW AMM 73-21-14. OPS AND LEAK CHECK GOOD AT THIS TIME. EICAS MESSAGE CLEARED.<BR /></P>)

Part: SOCKET — FAILED (SWITCH LIGHT) · airframe 104,596 hrs · 20,334 cycles

DURING #1 ENG START, ENG VALVE INDICATION LIGHT DID NOT CYCLE ON THEN OFF. #1 ENG WAS SHUT DOWN AND ENG VALVE LIGHT DID NOT CYCLE.(<P>DEFERRED #1 ENG VALVE INDICATION PER MEL 73-21-03-01, MDDR 109604 CAT C DDG PROCEDURE C/W.<BR /></P><P>LP 1050175 - REMOVED AND REPLACED LH ENG VALVE KORRY SW LIGHT BASE ASSY. OPS CK GOOD IAW SWPM 20-84-18. THIS ACTION CLEARS DMI 109604. MCC NOTIFIED AND 2 PLACARDS REMOVED.<BR /></P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (ENGINE CONTROL) · airframe 104,596 hrs · 20,334 cycles

DURING DESCENT 'L ENG CONTROL' STATUS MSG APPEARED.&NBSP; AFTER LANDING 'L ENG CONTROL' EICAS MSG APPEARED.(<P>PERFORMED FIM TASK 73-21 FT 878 AND PERFORMED ENGINE RUN REF AMM 71-00-00 FOR FAULT 155 23-A. NO CURRENT FAULTS NOTED @ THIS TIME, OK FOR SERVICE.<BR /></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (ENGINE CONTROL) · airframe 104,596 hrs · 20,334 cycles

DURING LANDING L ENG CONTROL EICAS. DURING FLIGHT L ENGINE CONTROL STATUS MSG.(<P>ACCOMPLISHED (L) PIMU BITE IAW AMM 77-35-02-714-011-H00. NO FAULTS NOTED. PERFORMED (L) ENG IDLE RUN IAW AMM 71-00-00/201, NO MESSAGES OR FAULTS NOTED.<BR /></P>)

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 104,554 hrs · 20,318 cycles

WEATHER RADAR DOES NOT REPORT WEATHER ON TURB. ON EITHER LEFT/RIGHT SYSTEM. OR IN EITHER WEATHER OR WEATHER/TURB. ONLY DISPLAYS GROUND RETURNS&NBSP;(<P>PERFORMED OPS CHECK OF LEFT /RIGHT WEATHER RADAR SYSTEM IAW AMM 34-43-00/501 SYSTEM OPS CHECK NORMAL AT THIS TIME. OK TO CONTINUE&NBSP;</P>)

Part: CHARGER — INOPERATIVE (APU) · airframe 104,523 hrs · 20,310 cycles

APU BAT CHARGER STATUS MSG(<P>R&AMP;R BATT CHARGER APU AMM 24-31-05<BR /></P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 104,449 hrs · 20,287 cycles

MULTIPLE CARGO FIRE WARNINGS ON GROUND&NBSP;(<P>PERFORMED OPS CHECK IAW AMM 26-14-00. NO DEFECTS NOTED AT THIS TIME.&NBSP;</P>)

Part: TRANSCEIVER — MALFUNCTIONED (WEATHER RADAR) · airframe 104,391 hrs · 20,270 cycles

RADAR ONLY DISPLAY GROUND CLUTTER&NBSP; DOES NOT DISPLAY&NBSP; WEATHER IN EITHER L/R&NBSP;(<P>REMOVED AND REPLACED WEATHER RADAR TRANSCEIVER IAW AMM 34-43-01 OPS CHECK GOOD</P>)

Part: APU — SHUTDOWN (APU BAY) · airframe 104,323 hrs · 20,253 cycles

JUST PRIOR TO PUSHBACK APU AUTOSHUTDOWN(<P>PERFORMED NORMAL 1 X APU START, NO ABNORMAL INDICATIONS PRESENT. SYSTEM TEST GOOD AT THIS TIME IAW 49-05-00.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 104,314 hrs · 20,251 cycles

L IDG VALVE STATUS MSG(<P>CHECK IDG VALVE PER AMM 24-11-00. NO STATUS MESSAGE DISPLAYED AT THIS TIME, OPS CHECK GOOD</P>)

Part: TRANSCEIVER — MALFUNCTIONED (WEATHER RADAR) · airframe 104,303 hrs · 20,249 cycles

RIGHT WEATHER RADAR FAIL.&NBSP;(<P>REMOVED AND REPLACED RIGHT WEATHER RADAR TRANSCEIVER IAW AMM 34-43-01, OPS CHECK IAW AMM 34-43-00 OPS CHECK GOOD.&NBSP;&NBSP;</P>)

Part: RADAR — MALFUNCTIONED (WX SYSTERM) · airframe 104,244 hrs · 20,231 cycles

WEATHER RADAR SYSTEM STATUS MESSAGE, RIGHT WEATHER RADAR FAILED IN FLIGHT. PERFORMED AN OPS TEST OF THE WEATHER RADAR SYSTEM IAW AMM 34-43-00. OPS CHECKED NORMAL.

Part: EEC — MALFUNCTIONED (LT ENGINE) · airframe 104,220 hrs · 20,225 cycles

LEFT ENGINE CONTROL STATUS MESSAGE(<P>REMOVED AND REPLACED LEFT ENGINE EEC IAW AMM 73-21-15. OPS CHECK NORMAL, ALL OPS TEST NORMAL<BR /></P>)

Part: ANTI-ICE VALVE — FAILED (LT ENGINE) · airframe 104,220 hrs · 20,225 cycles

LEFT ENGINE TAI VALVE STATUS MESSAGE(<P>REMOVED AND REPLACED TAI VALVE IAW B767 AMM 30-21-03<BR /></P>)

Part: SENSOR — NO TEST (CIT) · airframe 104,239 hrs · 20,229 cycles

CIT SENSOR NEEDS R&AMP;R AS PER BITE TEST.(<P>R&AMP;R CIT SENSOR IAW B767 AMM 73-21-00.&NBSP; L ENG SENSOR.<BR /></P>)

Part: CONNECTOR — UNSECURE (ANTI-ICE VALVE) · airframe 104,207 hrs · 20,219 cycles

STATUS MESSAGE: L ENG TAI VALVE(<P>RESET CONNECTOR ON L ENG TAI VALVE OPS CHECK NORMAL IAW B767 AMM 30-21-03</P>)

Part: WARNING MESSAGE — FALSE INDICATION (WEATHER RADAR) · airframe 104,151 hrs · 20,206 cycles

WXR FAIL MESSAGE.(<P>PERFORMED WXR OPERATIONAL TEST IAW AMM 34-43-00-715-026-002. OPS TEST NORMAL. NO FAULTS FOR LEFT AND RIGHT SYS NOTED. GOOD FOR CONTINUEDSERVICE.&NBSP;<BR /></P>)

Part: ANTI-ICE VALVE — MALFUNCTIONED (LT ENGINE) · airframe 104,032 hrs · 20,169 cycles

LEFT ENGINE INLET THERMAL ANTI - ICE VALVE STATUS MESSAGE&NBSP;(<P>RESET IN REF TO AMM 30-21-00-201-001, OPS CHECK NORMAL&NBSP;</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 103,973 hrs · 20,148 cycles

STATUS MESSAGE LEFT ENGINE TAI VALVE&NBSP;(<P>PERFORMED FIM 30-21 FT 805 THEN PERFORMED FIM 31-41 FT 812. PERFORMED ENGINE RUN PER STEP 2. NO EICAS MESSAGE NOTED. OK FOR SERVICE. ENGINE RUN PERFORMED PER AMM 72-00-00</P>)

Part: UNKNOWN — MALFUNCTIONED (TEMP SYSTEM) · airframe 103,919 hrs · 20,128 cycles

TRIM AIR SYSTEM, STILL HAVING DIFFICULTY MAINTAINING A NORMAL TEMPERATURE&NBSP;(<P>PERFORMED FIM 21-61 FT 912 ZONE TEMP CONTROLLER BITE PROCEDURES, NO FAULTS NOTED, PERFORMED VISUAL ON FLIGHT DECK TRIM AIR VALVE NO FAULT NOTED, PERFORMED OPS CHECK OF FLIGHT DECK ZONE TEMP CONTROL SYSTEM, OPS CHECK GOOD&NBSP;</P>)

Part: VALVE — FAULTY (TEMP SYSTEM) · airframe 103,916 hrs · 20,127 cycles

FLT DECK TEMP ADVISORY EICAS MSG REPEAT WRITE UP(<P>REMOVED AND REPLACED FLT DECK TRIM AIR VALVE&NBSP; OPS CHECK&NBSP; GOOD IAW AMM 21-61-01</P>)

Part: UNKNOWN — MALFUNCTIONED (COCKPIT TEMP) · airframe 103,912 hrs · 20,125 cycles

FLT DECK&NBSP; EICAS&NBSP; WOULD NOT COOL IN MANUAL SHUT OFF TRIM AIR (REPEAT WRITEUP) SET BOTH PACKS TO NORMAL CONTROL TEMP(<P>PERFORMED&NBSP; ZONE TEMP CONTROL&NBSP; AIR TEST IAW AMM 21-61-03 OPS CHECK ON NOT FAULTS OR MSG</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 103,925 hrs · 20,130 cycles

FLT DECK TEMP CAUTION MSG(<P>PERFORMED ZONE TEMP CTL BITE TEST IAW AMM 21-61-03 OPS CK OK.<BR /></P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 103,925 hrs · 20,130 cycles

WXR SYS STATUS MSG.(<P>PERFORMED WEATHER RADAR SYSTEM TEST IAW AMM 34-43-00 OPS TEST OK.<BR /></P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 103,863 hrs · 20,106 cycles

30 MINUTES INTO FLIGHT, EICAS MSG "FLT DECK TEMP", AFTER 1 HOUR IN MANUAL MODE TEMP ZONES 29/18/21 FLT DECK CONTROL IS INOP IN AUTO AND MANUAL MODES. (<P>PERFORMED BITE TEST IAW FIM 21-61 FAULT TREE 914. CLEARED MESSAGE AND PERFORMED OPS CHECK IAW AMM 21-61-07. OPS CHECK GOOD, NO FAULTS AT THIS TIME.</P>)

Part: EEC — MALFUNCTIONED (LT ENGINE) · airframe 103,862 hrs · 20,105 cycles

L ENG CONTROL AMBER EICAS MSG QRH COMPLIED WITH(<P>REMOVED AND REPLACED #1 ENG ELECTRONIC CONTROL UNIT IAW AMM 73-21-15 OPS CHECKED GOOD.</P>)

Part: FILTER — DIRTY (TEMP SENSOR) · airframe 103,876 hrs · 20,110 cycles

FLT DECK TEMP EICAS MSG IN FLT(<P>CLEANED CKPT TEMP SENSOR FILTER, HAVE FULL CTL OF TEMP ADJ. BIT TEMP CTRL PER FIM 21-61 F/T914&NBSP; RAN PACKS ON GRND CHKS GOOD PER AMM 21-61-01&NBSP;&NBSP;</P>).

Part: APU — MALFUNCTIONED · airframe 103,826 hrs · 20,090 cycles

AFTER ENGINE START ISOL VALVE SELECTED APU FAULTS AND SHUTS DOWN(<P>PERFORMED ECU BITE CHK PER FIM 49-11 FAULT TREE 958 CHECKED APU WITH AND WITHOUT ENGINES RUNNING PER AMM 49-11-00 AND AMM 72-00-00 NO FAULTS NOTED APU OPS CKS NORMAL&NBSP;</P>)

Part: TRANSCEIVER — INOPERATIVE (WX RADAR SYS) · airframe 103,812 hrs · 20,085 cycles

RH WX RADAR INOP(<P>REMOVED &AMP; REPLACED RT WX RADAR TRANX IAW AMM 34-43-01, OPS CKD GOOD</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (A/C PACK) · airframe 103,799 hrs · 20,080 cycles

HI FLOW INHIBIT STATUS MESSAGE&NBSP;(<P>PERFORMED FIM 21-51 FT 854 NO FAULTS AT THIS TIME OPS CHECK&NBSP; GOOD</P>)

Part: CIRCUIT CARD — FALSE INDICATION (WW FIRE) · airframe 103,799 hrs · 20,080 cycles

AFTER 20 MINUTES AT CRUISE THE&NBSP; L STRUT&NBSP; LEAK&NBSP; EICAS&NBSP; MSG AND&NBSP; DUCT LEAK&NBSP; WARN LIGHT CAME&NBSP; ON&NBSP; STAYED ON FOR REMAINDER ON FLIGHT AND AFTER ENGINE SHUTDOWN&NBSP;(<P>TROUBLE SHOOTING IAW FIM 26-18-FT 804 REPLACED WHEEL WELL FIRE CARD&NBSP; M691 IAW AMM 26-10-01 OPS CHECK NORMAL NO FAULTS AT THIS TIME RAN ENGINES FOR&NBSP; 6 MINUTES NO FAULTS&NBSP;</P>)

Part: CIRCUIT CARD — MALFUNCTIONED (BLEED AIR) · airframe 103,799 hrs · 20,080 cycles

REF ITEM # 1 SWAPPED M859 AND M 860 FOR TROUBLE SHOOTING LEFT DUCT LEAK EICAS MSG(<P>SWAPPED BLEED AIR CONTROL CARD M859 WITH M860 IAW AMM 36-11-12 OPS CHECK NORMAL&NBSP;</P>)

Part: TRANSCEIVER — INOPERATIVE (WX RADAR SYSTEM) · airframe 103,812 hrs · 20,085 cycles

RH WX RADAR INOP(<P>TRANSFER TO MDDR&NBSP; 104898 IAW DDG&NBSP; 34-43-01 PLACARD INSTALLED&NBSP;</P><P>LP 1044329-M5 REMOVED AND REPLACED RT WEATHER RADAR TRANSCEIVER&NBSP; IAW AMM 34-43-01 OPS CHECK GOOD&NBSP; THIS CLEAR MDDR PLACARD REMOVED&NBSP;</P>)

Part: CIRCUIT CARD — MALFUNCTIONED (BLEED CONTROL) · airframe 103,799 hrs · 20,080 cycles

AFTER&NBSP; LEVEL OFF L STRUT DUCT LEAK EICAS MSG APROX 20MN MSG EXTINGUISHED&NBSP; BUT DUCT WARN LIGHT REMAINED ON FOR LT ENG STRUT LIGHT WENT OUT W/ BLEED AIR SW OFF(<P>SWAPPED BLEED AIR CONTROL CARD&NBSP; M859 -M860 FOR TROUBLE SHOOTING&NBSP; IAW AMM 36-11-12 OPS CHECK NORMAL SEE ITEM 2 FOR REPAIR ,SEE ITEM 4 FOR M 860 CARD&NBSP;</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (EQ FAN) · airframe 103,799 hrs · 20,080 cycles

AFT EQ FAN 1 STATUS MSG AFTER SHUTDOWN(<P>PERFORMED FIM 21-26 FT 803 STEP 2-20 AND 41 OPS CHECK NORMAL AT THIS TIME&NBSP;</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 103,770 hrs · 20,072 cycles

STATUS MSG CABIN ALT AUTO 1&NBSP;(<P>PERFORMED CABIN PRESSURE CONTROLLER BITE TEST NO FAULT NOTED I.A.W FIM 21-31 FT 809 CABIN PRESSURE SYSTEM 1 WORKS GOOD&NBSP;</P>)

Part: CONTROL PANEL — DEFECTIVE (COCKPIT) · airframe 103,747 hrs · 20,063 cycles

BATTERY ON LIGHT INOP. REMOVED AND REPLACED BATTERY STANDBY PWR CONTROL PANEL IAW AMM 24-33-04. OPS CHECK GOOD.

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 103,733 hrs · 20,059 cycles

APU RELIABILITY COLD START, AOT -63C FLT 40,000 3 ATTEMPTS UNSUCCESSFUL. PERFORMED BITE TEST ECU IAW AMM 49-61-05, NO DEFECTS OR FAULTS NOTED. APU START FIRST ATTEMPT AND OPS CHECK NORMAL IAW AMM 49-11-00.

Part: FUEL FILTER — WARNING MESSAGE (RT ENGINE) · airframe 103,513 hrs · 19,994 cycles

RIGHT ENGINE FUEL FILTER EICAS STATUS MESSAGE&NBSP;(<P>T/S PER FIM REMOVED AND REPLACED RIGHT ENGINE FUEL FILTER LEAK AND OPS CK NO MSG ON EICAS&NBSP;</P>)

Part: CIRCUIT CARD — MALFUNCTIONED (LT ENGINE) · airframe 103,475 hrs · 19,979 cycles

DURING CLIMB, THE LEFT DUCT WENT TO ZERO, NO EICAS OR BLEED LIGHTS ILLUMNATED. REMOVED AND REPLACED PRINTER CIRCUIT CARD, LEFT BLEED AIR CONTROL IAW AMM 36-11-12 AND AMM 20-10-01. OPS CHECKED GOOD, ENGINE RUN PERFORMED IAW AMM 71-00-00, OPS CHECKED GOOD, BLEED AIR OPERATES NORMALLY.

Part: UNKNOWN — MALFUNCTIONED (LT A/C PACK) · airframe 103,480 hrs · 19,980 cycles

LEFT PACK OFF EICAS MESSAGE. QRH COMPLIED WITH. NO BLEED AIR SUPPLIED TO LEFT PACK , PERFORMED AN OPS CHECK OF THE LEFT PACK IAW AMM 21-51-00, NO FAULTS NOTED. OPS CHECKED GOOD.

Part: CIRCUIT BREAKER — TRIPPED · airframe 103,379 hrs · 19,946 cycles

ON LANDING ROLLOUT AND DISENGAGEMENT OF THE AUTOBRAKE, EICAS MESSAGES APEARED FOR, APU BLEED VALVE, RT AFT FWP PUMP, RT YAW DAMPER, C HYD PRIM 2, AND RT UTILITY BUSS. FOUND A HOT BATTERY BUSS CIRCUIT BREAKER SECT 2 OUT. RESET THE CIRCUIT BREAKER ON THE P6-2 PANEL IAW SWP 20-60-00. ALL MESSAGES CLEARED, NO FURTHER FAULTS NOTED.

Part: IRS — MALFUNCTIONED (COCKPIT) · airframe 103,325 hrs · 19,926 cycles

NO 1 FMC EICAS MSG ENROUTE, SCRATCH PAD MSG SHOWED SPLIT IRS. R&R LEFT AND CENTER IRS IAW AMM 34-21-01, OPS CHECK NORMAL.

Part: SLEEVE — DETERIORATED (LT IDG) · airframe 103,325 hrs · 19,926 cycles

LEFT IDG POWER FEEDER WIRE COLD SHRINK SLEEVE DETERIORATED. INSTALLED NEW COLD SHRINK SLEEVE PER EO 6724A012.

Part: FILTER — DIRTY (LT ENGINE) · airframe 103,263 hrs · 19,903 cycles

LT ENGINE FUEL FILTER BY PASS EICAS/STATUS. R&R NR 1 ENG FUEL FILTER IAW AMM 73-11-03.

Part: VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 103,180 hrs · 19,874 cycles

RT ENG BLEED OFF EICAS MSG. REMOVED AND REPLACED FAMV IAW AMM 36-11-16. OPS CHECK GOOD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 103,118 hrs · 19,852 cycles

RT ENG BLEED OFF EICAS MSG AFTER TAKEOFF APPROX FL180. OCCURRED SHORTLY AFTER ENGAGING ENG ANTI-ICE. LOST RT DUCT PRESS ASSOCIATED RT PACK OFF EICAS MSG. DEFERRED PER MEL 36-12-02-01 MDDR 100118. CAT C DUE 04 OCT 2018 FAMV LOCKED IN INTERMEDIATE POSITION.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 103,118 hrs · 19,852 cycles

AFTER SELECTING ENGINE NAI WE GOT RIGHT ENG BLEED OFF EICAS MESSAGE FOLLOWED BY RIGHT PACK OFF EICAS MESSAGE. RAN QRH PROC, RT ENG BLEED OFF DURING QRH PROCEDURE. MESSAGE WAS INTERMITENTLY COMING BACK AND FINALLY CLEARED ON ITS OWN. PERFORMED AIR SUPPLY BTIE TEST IAW AMM SUBTASK 36-11-00-745-007 AND FIM 36-20 FAULT TREE 804. NO FAULTS NOTED AT THIS TIME. OK FOR SERVICE.

Part: CONTROL BOX — MALFUNCTIONED (BLEED AIR SYS) · airframe 103,076 hrs · 19,837 cycles

TURNING ON WING ANTI-ICE RIGHT BLEED FAILED AND PACK OFF LIGHT ILLUMINATED. PERFORMED IDLE ENGINE RUN AFTER RESETTING BLEED CONTROL BOX RT BLEED WORKING OK AS PER AMM 71-00-00.

Part: INDICATION SYS — FAULTY (COCKPIT) · airframe 103,071 hrs · 19,836 cycles

DESENDING THRU FL200 WE SAW THE CABIN ALT INDICATOR INDICATED 0, DIFF PREESSURE AND RATE APPEARED NORMAL. PERFORMED OPS CHECK ON CABIN ALT PRESS SYSTEM IAW AMM 21-31-00. OPS CHECK GOOD AT THIS TIME.

Part: SELECTOR — FAULTY (CABIN PRESSURE) · airframe 103,086 hrs · 19,841 cycles

CABIN ALTITUDE VALVE INDICATOR, DOES NOT LINE UP WITH FULL OPEN INDEX WITH VALVE FULL OPEN. REMOVED AND REPLACED CABIN PRESSURE SELECTOR ASSY IAW AMM AMM 21-31-01. OPERATIONAL CHECK IAW AMM 21-31-01-704-014 PERFORMED. OPS CHECK GOOD.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 103,017 hrs · 19,814 cycles

EICAS WARNING CABIN ALTITUDE AT FL 380. FOLLOWED QRH AND EMERGENCY DESCENT PROCEDURES. AUTO 1 AND AUTO 2 BOTH DID NOT STABLE CABIN ALTITUDE, SWITCHED TO MAIN MODE AND WAS ABLE TO STABILIZE CABIN. REPEAT WRITE UP.-AUTO 2 CABIN ALTITUDE STILL INOP. PERFORMED BITE CHECK ON SYS1 AND SYS2. NO FAULTS SYS2, SYS1 FAULTED AC MOTOR. RANG OUT WIRES ON SYS1 PER WDM 21-31-11, SYS2 PER WDM 21-31-21, FOUND NO CONTINUITY BETWEEN PIN 22, CONNECTOR B24(SELECTOR) AND PIN C1 CONNECTOR D2712/ EQUIP RACK. VERIFIED CONTINUITY AS PER WIRING SCHEMATIC/WDM 21-31-21. CABIN PRESS SYS AUTO2 AND PER STD WIRING PRACTICES. REPLACED CABIN OUTFLOW VALVE ASSY IAW AMM 21-31-03: P/N OFF: 606832-18, S/N:13-1761. REMOVED AND REPLACED CABIN PRESSURE SELECTOR, OPS CHECK GOOD PER AMM 21-31-01: P/N OFF: 130502-6, S/N 113-372. REMOVED AND REPLACED NR 1 CABIN PRESSURE CONTROLLER, OPS CHECK GOOD PER AMM 21-31-02.

Part: MOTOR — FAULTY (NR 1) · airframe 103,015 hrs · 19,813 cycles

RECEIVED CABIN ALTITUDE WARNING AT FL390. FOLLOWED QRH ABLE TO MAINTAIN CABIN ALTITUDE IN MANUAL MODE ONLY. AFTER TROUBLESHOOTING FOUND NR 1 AC MOTOR FAULTY. REMOVED AND REPLACED AC MOTOR OPS CHECK GOOD IAW AMM 21-31-05.

Part: CONTROLLER — FAULTY (AC PACK) · airframe 103,011 hrs · 19,811 cycles

LT PACK TEMP EICAS MESSAGE PERFORMED QRH ITEMS. OPERATED PACK IN STBY LT PACK TEMP CONTROLLER BITE SHOWS CONTROLLER FAULT. R&R LT PACK TEMP CONTROLLER, OPS CHECK OK AMM 21-51-14.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 103,013 hrs · 19,812 cycles

CABIN AUTO INOP EICAS MESSAGE. CHECKLIST COMPLETED, CABIN PRESSURE NORMAL IN MANUAL MODE. PERFORMED BITE TEST PER AMM 21-31-00-705-001, NO FAULTS INDICATED, NO EICAS MESSAGE. OK FOR SERVICE.

Part: CONTROL VALVE — FAULTY (AC BAY) · airframe 102,976 hrs · 19,799 cycles

"LT PACK TEMP" EICAS AFTER LEVEL OFF AT FL 360. ACCOMPLISHED QRH, PACK SELECTED TO STBY N AND EICAS PACK INOP LIGHT EXTINGUISHED. REMOVED AND REPLACED LT PACK TEMP CONTROL VALVE IAW AMM 21-51-12. OPS CHECK GOOD. A/C OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 102,957 hrs · 19,792 cycles

LEFT PACK TEMP EICAS MESSAGE CAME ON CLIMBING THROUGH FL 300. PERFORMED OPERATIONAL CHECK OF COOLING PACK SYSTEM OPS NORMAL NO MESSAGE. PERFORMED BITE IAW 21-51- FT 804 CLEARED FAULTS, NO FAULT RETURN OPS CHECK IAW AMM 21-51-00. NO FAULT NOTED.

Part: RELAY — FAILED (START SYSTEM) · airframe 102,920 hrs · 19,779 cycles

NR 2 ENGINE START VALVE WOULD NOT OPEN VALVE, LIGHT STAYED ON BUT NO N2 ROTATION. PERFORMED FIM TASK 80-11 FT 803 FOUND RELAY K1174 DEFECTIVE. REPLACED RELAY K1174 IAW SWPM 20-80-22. OPS CHECK NORMAL AT THIS TIME.

Part: CLAMP — LOOSE (AC BAY) · airframe 102,920 hrs · 19,779 cycles

LEFT PACK TEMP LIGHT ILLUMINATED AFTER DEPARTURE. PERFORMED FIM 21-51-FT 844 COULD NOT DUPLICATE LEFT PACK TEMP FAULT. FOUND TWO CLAMPS LEAKING AROUND ACM TORQUED CLAMP. OPS CHECK NORMAL.

Part: START VALVE — MALFUNCTIONED (NR 2 ENGINE) · airframe 102,914 hrs · 19,777 cycles

AFTER PUSH IN BWI NR 2 ENGINE START VALVE WOULD NOT OPEN. VALVE LIGHT STAYED ON BUT NO N2 ROTATION. ENGINE STARTED BY MANUALLY OPENING START VALVE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 102,855 hrs · 19,758 cycles

LEFT PACK TEMP EICAS MESSAGE FOLLOWED QRH PROCEDURE AND MESSAGE WENT AWAY. PERFORMED FIM TASK 21-51 FT 803. NO ISSUES NOTED. COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 102,793 hrs · 19,733 cycles

LEFT PACK TEMPERATURE EICAS MESSAGE. PERFORMED FIM 21-51 F/T 803 BITE OF LEFT PACK TEMPERATURE CONTROLLER. OK, NO DISCREPANCIES NOTED. A/C OK FOR SERVICE.

Part: CONTROLLER — FAULTY (WINDOW HEAT) · airframe 102,759 hrs · 19,720 cycles

L1 WINDOW ARCING. REMOVED AND REPLACED L1 WINDOW CONTROLLER IAW AMM 30-41-01. OPS CHECK GOOD.

Part: ANTI-ICE VALVE — FAULTY (LT WING) · airframe 102,748 hrs · 19,714 cycles

LT WING ANTI-ICE EICAS AT HIGH THRUST SETTING. REMOVED AND REPLACED LT ANTI-ICE VALVE IAW AMM 30-11-02, OPS CHECK OK.

Part: PRESSURE SWITCH — FAULTY (ANIT-ICE SYS) · airframe 102,744 hrs · 19,713 cycles

LEFT WING ANTI-ICE EICAS ADVISORY AT 500FEET AFTER TAKEOFF. PERFORMED FIM TASK 30-11-02FT 803. TEST OK REF LOG PAGE 953927 ITEM M6; PERFORMED T/S OF LEFT WING ANTI-ICE IN REF TO WD 30-11-11. CHECKED OPEN/GROUND AT PINS 4/5 AT D1594. CHECKED GOOD. CHECKED WING ANTI-ICE VALVE COIL AT PIN 1/2 D1594, GOT 352.7 OMH. CHECKED 5398 AT PINS 1/2 D2384, CHECKED GOOD. SWAPPED THERMAL PRESSURE SWITCH ON WING VALVE. 8G1270/2780537-104 P/N REF LOG PAGE 953928 ITEN M7. REMOVED AND REPLACED WING THERMAL ANTI ICE (LEFT) PRESSURE SWITCH IAW AMM 30-11-02, OPS CHECK GOOD. NO FAULTS NOTED AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 102,725 hrs · 19,710 cycles

LT WING ANTI-ICE EICAS. PERFORMED FIM 30-11 FT 803 SYSTEM TEST. OK AS PER FIM 30-11 803 BLOCK 2 NO DEFECTS NOTED.