N1327A
Registered owner: MSN 26328 LLC, NY (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
DURING TAXI, CREW RECEIVED R ENG BLEED OFF R PACK OFF NO R DUCT PRESSURE. CREW RETURNED TO THE GATE (BTB). MTX TROUBLE SHOT AND REMOVED AND REPLACED PRV CONTROLLER RH ENGINE IAW B767-300 AMM 36-11-19-004-001-002. OPS CHECK GOOD. PERFORMED RH ENG RUN PER AMM 71-00-00 OPS CHECK GOOD . AND RETURNED A/C TO SERVICE.
DURING CREW PREFLIGHT, LEFT UPPER STORAGE BIN DOOR HINGE ARM FAILED. DEFERRED LEFT OVERHEAD STORAGE BIN SHOCK BIN SHOCK STRUT IAW ABX MEL 25-28-1A. DUE TO OVERHEAD BIN STRUT DEFERRAL, PED FIRE BAG DEFERRED IAW ABX NEF 25-03-28. MBCB 5-26-26. PLACARD INSTALLED. A/C RETURNED TO SERVICE.
DURING DESCENT, LE SLAT DISAGREE LIGHT ILLUMINATED AFTER SELECTING FLAPS 25. CREW EXECUTED A MISSED APPROACH. FOLLOWED QRH PROCEDURES AND LANDED WITH FLAPS 20. MAINTENANCE PERFORMED FSEU READ-OUT FORM IAW AMM ALL SENSORS WITHIN LIMITS. FLAP SLAT SYS OPS NORMAL WITH NO FAULTS OK FOR SERVICE.
DURING TAXI OUT WHILE STARTING NR 1 ENGINE NO ROTATION ON NR 1, START VALVE STAYED OPEN , A/C RETURNED TO THE GATE (BTB) AND MTX GROUNDED A/C AND DEFERRED NR 1 START VALVE IAW MEL ABX-80-00-2-1 .A/C REMAINS ETOPS 180 . AND RETURNED ACFT TO SERVICE .
DURING TAXI, TE FLAP DISAGREE WHEN MOVING TO FLAPS 5 ON THE AFTER START CHECKLIST. CREW RETURNED TO BLOCK (BTB). MTC PERFORMED FIM 27-51 FT 811, RESET BY PASS LEVER. OPS CHECK GOOD. ACFT REMAINS ETOPS 180. ACFT RETURNED TO SERVICE.
PILOT REPORTED CARGO FIRE A 4 AMBER INDICATION. RESET ELECTRICAL CONNECTOR. ON BOX. ERROR CLEARED. OPS CHK GOOD. IAW B767 AMM 26-16-00. THIS CLEARS THE DI. PLACARDS REMOVED. NO MAINTENANCE ACTIONS REQUIRED. ACFT REMAINS ETOPS 180. AIRCRAFT RETURNED TO SERVICE.
DURING APPROACH INTO MIA, LANDING CONFIG WARNING LIGHT ILLUMINATED AT 3000 FT AGL. FLAPS WERE AT 15 AND GEAR LEVER IN OFF POSITION. CAPTAIN DID A GO AROUND AND CYCLED GEAR. SECOND APPROACH INTO MIA, LANDED WITH NO CONFIG WARNINGS. MAINTENANCE FOUND NO MSG AT THIS TIME, PERFORMED PSEU BITE TEST, NO FAULTS IAW FIM 32-09-00. AIRCRAFT RETURNED TO SERVICE.
DURING TAXI OUT AND AFTER START CHECKLIST, L PACK OFF EICAS DISPLAYED QRH PROCEDURE UNSUCCESSFUL. AIRCRAFT RETURNED TO BLOCKS (BTB). TRANSFERED LH PACK TO DI IAW ABX MEL 21-51-1-1. MX PROCEDURES ACCOMPLISHED PLACARD INSTALLED A/C RELEASED NO ETOPS PLACARD ROTATED MBCB: 02/16/2026. AIRCRAFT RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION, LT ENG OH LP1 EICAS MSG. PLACED ENG OH LP 1 ON DEFERRAL IAW MEL 26-11-2-1 MBCB 01/26/2026 AIRCRAFT ETOPS 120 PLACARD ROTATED. AIRCRAFT RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION, EICAS MSG AFT CARGO DET NR 1 ILLUMINATED. DEFERRED PER MEL 26-16-1-1-1. REMOVED AND REPLACED AFT CARGO SMOKE DETECTOR NR 1 PER AMM 26-16-01. CONFIG 1. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
DURING THE CURRENT C-6 HEAVY MAINTENANCE CHK, MAINT FOUND AT BS 871.5, RT FWD OVERWING EMERG EXIT DOOR HAD NICK DAMAGE ABOVE WINDOW-PLUG CUTOUT. FASTENERS REMOVED AT AFFECTED AREA IAW SRM 51-40-02 & DAMAGE BLENDED OUT IAW SRM 52-20-01 RESULTING IN THE FINAL BLEND SIZE OF 2.5-INCH-LONG X 0.75-IN-WIDE WITH MRT OF 0.056-IN CORRESPONDING TO ABOUT 21% MATERIAL LOSS. EXTERNAL & INTERNAL DVI ACCOMPLISHED INCLUDING WINDOW CUTOUT IAW SRM 51-10-08 & NO DAMAGE FOUND. SURFACE HFEC INSPECT ACCOMP AT DAMAGE BLEND-OUT IAW NDTM PART 6, 51-00-23 & NO DAMAGE FOUND. AN OPEN HOLE HFEC INSPECT ACCOMP AT DAMAGE LOCATION IAW NDTM PART 6, 51-00-16 & NO DAMAGE FOUND. ACCOMP REPAIR IAW EO 25129-1 REV. IR, & ABX-REA-5221-65284-00.
DURING THE C-6 MAINTENANCE VISIT AT HAECO GSO, CORROSION WAS FOUND ON THE LH HORIZONTAL STABILIZER LOWER BLADE SEAL SUPPORT FITTINGS. #2 FITTINGS TOTAL WERE FOUND TO HAVE CORROSION BETWEEN THE BLADE SEAL AND MATING FLANGE OF THE SUPPORT FITTINGS AND WITHIN THE SUPPORT ATTACHMENT HOLES. ALL CORROSION WAS REMOVED BY BLENDING OF THE FLANGE SURFACE AND DRILLING OF THE ATTACHMENT HOLES. THE 767-300 SRM DOES NOT PROVIDE ANY LIMITS OR REPAIRS FOR THESE SUPPORT FITTINGS, AND WE ARE CURRENTLY UNABLE TO OBTAIN REPLACEMENTS.REPAIRED LH IB SIDE HORIZONTAL STAB BLADE SEAL ATTACHMENT BRACKET #2 PER FVCI EO 25129-3 REV:IR THAT WAS ACCOMPLISHED ON NR 40760. ABX M-289 AND FAA FORM 337 ATTACHED.ABX-REA-5510-65830-00.
DURING THE C-6 MAINTENANCE VISIT AT HAECO GSO, CORROSION WAS FOUND ON THE LH HORIZONTAL STABILIZER LOWER BLADE SEAL SUPPORT FITTINGS. #3 FITTINGS TOTAL WERE FOUND TO HAVE CORROSION BETWEEN THE BLADE SEAL AND MATING FLANGE OF THE SUPPORT FITTINGS AND WITHIN THE SUPPORT ATTACHMENT HOLES. ALL CORROSION WAS REMOVED BY BLENDING OF THE FLANGE SURFACE AND DRILLING OF THE ATTACHMENT HOLES. THE 767-300 SRM DOES NOT PROVIDE ANY LIMITS OR REPAIRS FOR THESE SUPPORT FITTINGS, AND WE ARE CURRENTLY UNABLE TO OBTAIN REPLACEMENTS.REPAIRED LH IB SIDE HORIZONTAL STAB BLADE SEAL ATTACHMENT BRACKET #3 PER FVCI EO 25129-3 REV:IR THAT WAS ACCOMPLISHED ON NR 40760. ABX M-289 AND FAA FORM 337 ATTACHED.ABX-REA-5510-65830-00.
DURING THE C-6 MAINTENANCE VISIT AT HAECO GSO, CORROSION WAS FOUND ON THE LH HORIZONTAL STABILIZER LOWER BLADE SEAL SUPPORT FITTINGS. #4 FITTINGS TOTAL WERE FOUND TO HAVE CORROSION BETWEEN THE BLADE SEAL AND MATING FLANGE OF THE SUPPORT FITTINGS AND WITHIN THE SUPPORT ATTACHMENT HOLES. ALL CORROSION WAS REMOVED BY BLENDING OF THE FLANGE SURFACE AND DRILLING OF THE ATTACHMENT HOLES. THE 767-300 SRM DOES NOT PROVIDE ANY LIMITS OR REPAIRS FOR THESE SUPPORT FITTINGS, AND WE ARE CURRENTLY UNABLE TO OBTAIN REPLACEMENTS.REPAIRED LH IB SIDE HORIZONTAL STAB BLADE SEAL ATTACHMENT BRACKET #4 PER FVCI EO 25129-3 REV:IR THAT WAS ACCOMPLISHED ON NR 40760. ABX M-289 AND FAA FORM 337 ATTACHED.ABX-REA-5510-65830-00.
DURING THE C-6 MAINTENANCE VISIT AT HAECO GSO, CORROSION WAS FOUND ON THE LH HORIZONTAL STABILIZER LOWER BLADE SEAL SUPPORT FITTINGS. #5 FITTINGS TOTAL WERE FOUND TO HAVE CORROSION BETWEEN THE BLADE SEAL AND MATING FLANGE OF THE SUPPORT FITTINGS AND WITHIN THE SUPPORT ATTACHMENT HOLES. ALL CORROSION WAS REMOVED BY BLENDING OF THE FLANGE SURFACE AND DRILLING OF THE ATTACHMENT HOLES. THE 767-300 SRM DOES NOT PROVIDE ANY LIMITS OR REPAIRS FOR THESE SUPPORT FITTINGS, AND WE ARE CURRENTLY UNABLE TO OBTAIN REPLACEMENTS. REPAIRED LH IB SIDE STAB BLADE SEAL ATTACHMENT BRACKET #5 PER FVCI EO 25129-3 REV: IR THAT WAS ACCOMPLISHED ON NR 40760. ABX FORM M-289 AND FAA FORM 337 ATTACHED.ABX-REA-5510-65830-00.
DURING THE C-6 MAINTENANCE VISIT AT HAECO GSO, CORROSION WAS FOUND ON THE LH HORIZONTAL STABILIZER LOWER BLADE SEAL SUPPORT FITTINGS.# 6 FITTINGS TOTAL WERE FOUND TO HAVE CORROSION BETWEEN THE BLADE SEAL AND MATING FLANGE OF THE SUPPORT FITTINGS AND WITHIN THE SUPPORT ATTACHMENT HOLES. ALL CORROSION WAS REMOVED BY BLENDING OF THE FLANGE SURFACE AND DRILLING OF THE ATTACHMENT HOLES. THE 767-300 SRM DOES NOT PROVIDE ANY LIMITS OR REPAIRS FOR THESE SUPPORT FITTINGS, AND WE ARE CURRENTLY UNABLE TO OBTAIN REPLACEMENTS. REPAIRED #6 SUPPORT FITTING IAW ABX-REA-5510-65830/ FVCI EO 25129-3 REV IR.
DURING THE C-6 MAINT VISIT, CORROSION FOUND ON LT HORIZONTAL STAB LOWER BLADE SEAL SUPPORT FITTINGS. NR 7 FITTINGS TOTAL WERE FOUND TO HAVE CORROSION BETWEEN THE BLADE SEAL & MATING FLANGE OF SUPPORT FITTINGS & WITHIN THE SUPPORT ATTACHMENT HOLES. ALL CORROSION WAS REMOVED BY BLENDING OF THE FLANGE SURFACE AND DRILLING OF THE ATTACHMENT HOLES. THE 767-300 SRM DOES NOT PROVIDE ANY LIMITS OR REPAIRS FOR THESE SUPPORT FITTINGS, AND WE ARE CURRENTLY UNABLE TO OBTAIN REPLACEMENTS.REPAIRED IAW REPAIRED LH IB SIDE HORIZONTAL STAB SEAL ATTACHMENT BRACKET #7 PER FVCI EO 25129-3 REV:IR THAT WAS ACCOMPLISHED ON NR40760.ABX FORM M-289 AND FAA FORM 337 ATTACHED. REF.ABX-REA-5510-65830-00.
DURING C6 CHECK AT HACECO INSPECTION FOUND E&E DOOR CUTOUT FWD FRAME WEB STA303 HAS PUNCTURE REMOVED ANGLE SUPPORT RAIL IAW B767 SRM 51-40-02, REMOVED DAMAGE IAW B767 53-00-07 REPAIR 3. MATL ID FOR FILLER .032 7075 PO1060506.1 AND DOUBLER 7075 T6 .040 PO 983717.3 IAW B767 SRM 53-10-07. FABRICATED FILLER AND DOUBLER IAW B767 SRM 53-00-07 REPAIR 3. ALODINED AND PRIMED IAW B767 SRM 51-20-01 DOUBLER AND FILLER. INSTALLED DOUBLER FILLER AND ANGLE SUPPORT IAW B767 51-40-02. INSTALLED RAIL IAW B767 SRM 51-40-02.FORM M-287 AND FAA FORM 337 ATTACHED.
DURING THE C-6 MAINTENANCE CHECK, THE NR 2 ENGINE PYLON PANEL ASSEMBLY WAS FOUND TO BE DAMAGED BEYOND REPAIR. MAINTENANCE FABRICATED A NEW PANEL. ACCORDING TO BAC DWG 313T2381 REQUIREMENTS, THE PIECES MUST BE PHOSPHORIC ANODIZED (PAA) AND PRIMED WITH BMS5-137 TYP I ADHESIVE PRIMER BEFORE BONDING. HAECO GSO CANNOT PERFORM PAA, AND WE RECEIVED AUTHORIZATION FROM ABX TO USE THE ALTERNATE BMS5-162 TYPE 1 (AC-130 BOEGEL) PROCEDURE, IAW SRM 51-70-10, PARAGRAPH 11. FABRICATED NEW PANEL IAW FVCI EO# 25129-5 REV A AND ABX-REA-5450-65826-00.
DURING PUSHBACK GOT TCAS EICAS MSG. A/C RETURNED TO GATE (BTB) AND MTX GROUNDED A/C, MTX DEFERRED TCAS FOR DEPARTURE IAW MEL ABX-34-45-1A. AND RETURNED A/C TO SERVICE
ON TAXI OUT, AUTO THROTTLE DISC LIGHT & AUTO THROTTLE DISC EICAS MESSAGE ILLUMINATED. A/C RETURNED TO BLOCKS (BTB). DEFERRED AUTO THROTTLE IAW MEL ABX-22-30-1. A/C RETURNED TO SERVICE.
DURING TAXI R ISLN VALVE LIGHT ON, NO AIR FOR START AC RETURNED TO GATE AND MAITENANCE GROUNDED AC. MTX CYCLED RIGHT ISOLATION VALVE 3 TIMES SUCCESSFULLY PER AMM 36-11-04. AIRCRAFT REMAINS NO ETOPS. RETURNED AC TO SERVICE .
AT ROTATION ON TAKEOFF EICAS MSG C HYD SYS PRESS APPEARED AND AC PERFORMED ATB , AND AFTER LANDING MTX GROUNDED AC AND TROUBLE SHOT TO A CTR HYD PRESSURE SWITCH. AND REMOVED AND REPLACED CENTER HYDRALIC SYSTEM PRESSURE SWITCH IAW B767 AMM 29-11-09 OPS CHECK AND LEAK CHECK GOOD. MTX RETURNED AC TO SERVICE .
COCKPIT ELT TAPE DAMAGED. PER MCC REGISTERED WITH NOAA PER ENGINEERING DEPARTMENT IAW AMM 25-63-03. DMI 204893 CLOSED.
CAPT REPORTED GALLEY ELT NOT TAPED CORRECTLY(<P>R/R GALLEY PORTABLE ELT IAW AMM 25-63-03 PART EFECTIVITY AIPC 25-63-52-97 ITEM 600. NO FURTHER DEFECTS NOTED. THIS CLEARS DMI 204877.&NBSP;</P>)
OBSERVED L1 EMERGENCY EXIT SIGN TO BE DISPLACED(<P>RE-SECURED EMERGENCY EXIT SIGN / LIGHT PER AMM 33-51-01. OPS CHCKS GOOD AT THIS TIME.&NBSP;</P>)
EMER LIGTHS GUARD SWITCH DOES NOT STAY CLOSED OR SNAPS CLOSED(<P>REMOVED AND REPLACED EMERGENCY LIGHTS GUARD PER AMM 20-11-00 AND 33-51-00-08-01B. OPS CHECKS GOOD. NO FURTHER DEFECTS NOTED&NBSP;</P>)
FOUND RED TAG MISSING ON FIRST AID KIT(<P>REMOVED AND REPLACED FIRST AID KIT IAW AMM 25-64-03. NO FURTHER DEFECTS NOTED</P>)
RH WING FUEL DUCT INSIDE CENTER AUX TANK BETWEEN RIB 2 & 3 WITH CLAMP LOOSE (FUEL TANK ACCESS PANEL 631BB)(<P>RH WING FUEL DUCT INSIDE CENTER AUX TANK BETWEEN RIB 2 & 3 WITH CLAMP INSTALLED CORRECTLY IAW AMM TASK 28-21-02-404-021 REV 139 22 APR2023 BONDING MEASUREMENT OF 1 MILLI OHM IAW AMM TASK 28-21-10-964-801 REV 139 22 APR2023.</P>)
3 FAAÃÂ AGING AIRCRAFT FINDINGS AFT CARGO FLOOR HAT CHANNEL DENTED B.S 1470, RBL14.(<P>3 FAA AGING AIRCRAFT FINDINGS AFT CARGO FLOOR HAT CHANNEL, B.S 1470, RBL14, WAS REPAIRED REF SRM 51-10-08-0G-0 REV 123 15AUG23, SRM 53-60-53-1A-2 REV 123 15AUG23 AND SRM 51-70-11-0G-0 REV 123 15AUG23. FOR TIMES AND REFERENCES SEE NON-ROUTINE SERIAL #00248.V 123 15AUG23.</P> / <P>&NBSP;</P>)
AFT CARGO COMPARTMENT, BEAM SUPPORT BROKEN BETWEEN STA.1395 AND 1417 RBL44.(<P>AFT CARGO COMPARTMENT, BEAM SUPPORT BETWEEN STA.1395 AND 1417 RBL44, WAS REPLACED REF SRM 51-10-02-0G-0 REV 123 15AUG23.</P> / <P>&NBSP;</P>)
RH WING FUEL TANK DUCT COOPLING WITH SAFETY WIRE LOOSE RIB 19(<P>RH WING FUEL TANK DUCT COOPLING SAFETY WIRE WAS REPLACED (RIB 19) IAW AMM 20-10-23-964-001 REV. 139 APR. 22-23.</P>)
LEFT WING TANK, FUEL DUCT WITH LEAD BONDING TORN LOCATED BETWEEN RIB 1 AND RIB 2. (ACCESS 531BB)(<P>N/R: 00299. LEFT WING TANK, FUEL DUCT, THE BONDING JUMPER WAS REPLACED, AND BONDING TEST IAW AMM 28-00-00-962-031, 28-22-07-404-008 REV 139 22APR-2023.</P> / <P>&NBSP;</P> / <P>&NBSP;</P>)
AFT CARGO COMPARTMENT, FLOOR LEVEL. FRAME WEB STIFFENER WITH CRACK AT STA 1087 RBL26.(<P>AFT CARGO COMPARTMENT, FLOOR LEVEL. FRAME WEB STIFFENER, AT STA 1087 RBL26 WAS REPLACED REF SRM 51-10-02-0G-0 REV 123 15AUG23.</P> / <P>&NBSP;</P>)
AFT CARGO COMPARTMENT, AT STA 1175, AND BTW S-29R ABD S-30R, SHEAR TIE WITH CRACK.(<P>AFT CARGO COMPARTMENT, AT STA 1175, AND BTW S-29R ABD S-30R, SHEAR TIE WAS REPLACED REF SRM 51-10-02-0G-0 PAR 9 REV 123 15AUG23.</P>)
DAMAGE FIRE DETECTION LOOP AT ENG 1.(<P>ENG 1 FIRE DETECTION LOOP WAS REPLACED AND TORQUED IAW AMM 26-11-02-424-033 REV140 22AUG2023.</P>)
FUEL LEAK ON NIPPLE AND PIPE OF FUEL FILTER SWITCH AT ENG 1.(<P>PIPE OF FUEL FILTER SWITCH AT ENG 1 WAS REPLACED AND LEAK CHECK WAS PERFORMED, NO LEAK FOUND IAW AMM 73-34-01-424-008-H00 REV. 140 AUG 22, 2023 & 26-11-02-424-033, REV140 22AUG2023.</P> / <P>&NBSP;</P>)
BULK CARGO COMPARTMENT, FLOOR LEVEL. FLOOR SUPPORT WITH CORROSION ON UPPER SURFACE AT STA 1480 LBL 8 AND LBL 14.(<P>BULK CARGO COMPARTMENT, FLOOR LEVEL. FLOOR SUPPORT, ON UPPER SURFACE AT STA 1480 LBL 8 AND LBL 14, WERE REPAIRED REF SRM 53-60-53-1A-2 REV 123 15AUG23, SRM 51-70-11-0G-0 REV 123 15AUG23 AND SRM 51-10-08-0G-0 REV 123 15AUG23.</P>)
BULK CARGO COMPARTMENT, FLOOR LEVEL. FLOOR SUPPORT WITH CORROSION BETWEEN B. STA 1480 AND 1502 LBL26.(<P>BULK CARGO COMPARTMENT, FLOOR LEVEL. FLOOR SUPPORT, BETWEEN B. STA 1480 AND 1502 LBL26. WAS REPAIRED REF SRM 51-10-08-0G-0 REV 123 15AUG23, SRM 53-60-53-1A-2 REV 123 15AUG23 AND SRM 51-70-11-0G-0 REV 123 15AUG23.</P>)
BULK CARGO COMPARTMENT, FLOOR LEVEL. FLOOR SUPPORT WITH CORROSION BETWEEN B. STA 1480 AND 1502 RBL8.(<P>BULK CARGO COMPARTMENT, FLOOR LEVEL. FLOOR SUPPORT BETWEEN B. STA 1480 AND 1502 RBL8, WAS REPAIRED REF SRM 51-10-08-0G-0 REV 123 15AUG23, SRM 53-60-53-A-2 REV 123 15AUG23 AND SRM 51-70-11-0G-0 REV 123 15AUG23</P> / <P>&NBSP;</P>)
BULK CARGO COMPARTMENT, FLOOR LEVEL. FLOOR SUPPORT WITH CORROSION BETWEEN B. STA 1439 AND 1461 LBL28.(<P>BULK CARGO COMPARTMENT, FLOOR LEVEL. FLOOR SUPPORT, BETWEEN B. STA 1439 AND 1461 LBL28 WAS REPAIRED REF SRM 51-10-08-0G-0 REV 123 15AUG23, SRM 53-60-53-1A-2 REV 123 15AUG23 AND SRM 51-70-11-0G-0 REV 123 15AUG23.</P>)
DELAMINATION ON PREVIOUS REPAIR AT RUD STA 106.142 RUDDER TRAILING EDGE RH.(<P>RUDDER TRAILING EDGE RH AT RUD STA 106.142 WAS REPAIRED IAW SRM 55-40-01-2R-1 FIG. 201 SHEET 2 PAGE 2-3 AND SRM 51-70-04-0G-0 PAR. 5G FIG. 9 SHEET 1 PAGE18,- 38,43 REV.123 AUG 15/2023</P>)
LIGHTNING STRIKE ON FASTENER HEAD AT STA 212.5 AND BELOW RBL 15, UPPER HALF FUSELAGE EXTERIOR.(<P>LIGHTNING STRIKE ON FASTENER HEAD AT STA 212.5 AND BELOW RBL 15, UPPER HALF FUSELAGE EXTERIOR WAS REPAIRED REF SRM 53-00-01-01A-1 AD1, SRM 53-00-01-2R-8 REV 123 15AUG23,&NBSP; EO TRE6753628 ISSUED DATE SEP19, 2023, FAA FORM 8100-9 DATE SEP28, 2023 REV. 123 AUG 15/2023 & BAC MSG CMA TLS 23-0146</P>)
LIGHTNING STRIKE ON FASTENER HEAD AT STA 287 AND 3" BELOW STGR 3 OF UPPER HALF OF FUSELAGE EXTERIOR.(<P>LIGHTNING STRIKE ON FASTENER HEAD AT STA 287 AND 3" BELOW STGR 3 OF UPPER HALF OF FUSELAGE EXTERIOR, WAS REPAIRED REF SRM 53-00-01-1A-1 AD1 FIG 101 TABLE I, III REV 123 15AUG23, SRM 53-00-01-2R-8 REV 123 15AUG23, TRE6753627 ISSUED DATE SEP16,2023, FVCI #23189-1 REV IR AND FAA FORM 8110-3.</P> / <P>&NBSP;</P>)
OUT OF LIMITS FREE PLAY ON OUTBOARD PCA OF RH ELEVATOR.(<P>OUTBOARD PCA OF RH ELEVATOR WAS REPLACED, ADJUSTED AND LEAK CHECK WAS SATISFACTORY IAW AMM 27-31-05-424-027 REV 139 22APR 2023</P>)
OUT OF LIMITS FREE PLAY ON OUTBOARD PCA OF LH ELEVATOR.(<P>N/R: 00028. OUTBOARD PCA OF LH ELEVATOR. WAS REPLACED, ADJUSTED AND TIGHTENED IAW AMM 27-31-05-424-027 & 27-31-00-825-060 REV139 22APR2023</P> / <P>&NBSP;</P> / <P>&NBSP;</P>)
OUT OF LIMITS FREE PLAY ON MIDDLE PCA OF LH ELEVATOR.(<P>MIDDLE PCA OF LH ELEVATOR WAS REPLACED, ADJUSTED AND TIGHTENED IAW AMM 27-31-05-424-027 & 27-31-00-825-060 REV 139 22APR2023.</P> / <P>&NBSP;</P>)
FUSELAGE SECTION 43, AREA ABOVE CEILING AT STA 544, SMOKE DETECTOR SYSTEM, ORANGE HOSE BROKEN (1EA)(<P>FUSELAGE SECTION 43, AREA ABOVE CEILING AT STA 544, SMOKE DETECTOR SYSTEM, ORANGE HOSE WAS REPLACED IAW AMM 25-59-01-400-804-001 REV. 139 APR22, 2023.</P>)
FUEL LEAK ON REAR SPAR SPLICE FITTING AND BBR 97.42 AT CENTER TANK.(<P>FUEL LEAK ON REAR SPAR SPLICE FITTING AND BBR 97.42 AT CENTER TANK WAS REPAIRED AND THE TEST WAS SATISFACTORY REF AMM 28-11-00-308-013 REV 140 22AUG23.</P> / <P>&NBSP;</P> / <P>&NBSP;</P>)
BULK CARGO COMPARTMENT, FLOOR LEVEL. LH SIDE ANGLE WITH CORROSION AT B.STA 1417 LBL41.(<P>&NBSP;</P> / <P>BULK CARGO COMPARTMENT, FLOOR LEVEL. LH SIDE ANGLE, AT B.STA 1417 LBL41 WAS REPLACED REF SRM 51-10-02-0G-0 PAR.9 REV123 15AUG23.</P> / <P>&NBSP;</P>)
BULK CARGO COMPARTMENT, FLOOR LEVEL. FLOOR SUPPORT WITH FASTENERS MISSING AT STA1461 LBL11.(<P>BULK CARGO COMPARTMENT, FLOOR LEVEL. FLOOR SUPPORT, AT STA1461 LBL- 11, FASTENERS WERE INSTALLED CORRECTLY REF SRM 51-40-02-0G-0 REV 123 15AUG23.</P>)
STABILIZER TORSION BOX. INTERNAL STRUCTURE, ELEVATOR FUEL COMPUTER BETWEEN STA 1702 AND STA 1725.5. WITH SEVERAL LINES WITH HYD LEAK.(<P>ELEVATOR FEEL COMPUTER WAS REPLACED, TORQUED, CHECKED FOR LEAK, NO LEAK FOUND AND OPERATIONAL TEST WAS SATISFACTORY REF IAW AMM 27-31-19-424-015 REV140 22AUG2023.</P> / <P>&NBSP;</P>)
STABILIZER TORSION BOX. INTERNAL STRUCTURE BETWEEN STA 1809.5 AND STA 1832, FEEL ACTUATOR WITH EVIDENCE LEAK.(<P>THE FEEL ACTUATOR WAS REPLACED, WAS TIGHTENED AND OPERATIONALTEST WAS SATISFACTORY IAW AMM 27-31-17-424-021 REV140 22AUG2023.</P>)
RH WING OVERWING PORT FUEL LEAK(<P>RH WING OVERWING PORT O-RINGS WERE REPLACED IAW AMM TASK 28-11-04-404-019 REV 140 DATE 22 AUG 23. LEAK TEST WAS PERFORMED, NO LEAKS WERE FOUND</P> / <P>&NBSP;</P>)
FUSELAGE SECTION 43, AREA ABOVE CEILING AT STA 610, SMOKE DETECTOR SYSTEM, ORANGE HOSE BROKEN (1EA)(<P>FUSELAGE SECTION 43, AREA ABOVE CEILING AT STA 610, SMOKE DETECTOR SYSTEM, ORANGE HOSE WAS REPLACED IAW AMM 25-59-01-400-804-001 REV 139 DATE 22 APR 23</P> / <P>&NBSP;</P>)
FUSELAGE SECTION 43, AREA ABOVE CEILING BTW STA 654+66 AND STA 654+88, SMOKE DETECTOR SYSTEM, ORANGE HOSE BROKEN (1EA)(<P>FUSELAGE SECTION 43, AREA ABOVE CEILING BTW STA 654:66 AND STA 654:88, SMOKE DETECTOR SYSTEM, ORANGE HOSE WAS REPLACED IAW AMM 25-59-01-400-804-001 REV 139 DATE 22 APR 23</P>)
FUSELAGE SECTION 46, AREA ABOVE CEILING BTW STA 1307 AND STA 1329, SMOKE DETECTOR SYSTEM, ORANGE HOSE BROKEN (1EA)(<P>FUSELAGE SECTION 46, AREA ABOVE CEILING BTW STA 1307 AND STA 1329, SMOKE DETECTOR SYSTEM, ORANGE HOSE WAS REPLACED IAW AMM 25-59-01-400-804-001 REV. 139 APR 22, 2023</P>)
FUSELAGE SECTION 46, AREA ABOVE CEILING BTW STA 1461 AND STA 1480, SMOKE DETECTOR SYSTEM, ORANGE HOSE BROKEN (1EA)(<P>FUSELAGE SECTION 46, AREA ABOVE CEILING BTW STA 1461 AND STA 1480, SMOKE DETECTOR SYSTEM, ORANGE HOSE WAS REPLACED IAW AMM 25-59-01-400-804-001 REV 139 DATE 22 APR 23</P>)
FUSELAGE SECTION 46, AREA ABOVE CEILING AT STA 1395, SMOKE DETECTOR SYSTEM, ORANGE HOSE BROKEN (1EA)(<P>FUSELAGE SECTION 46, AREA ABOVE CEILING AT STA 1395, SMOKE DETECTOR SYSTEM, ORANGE HOSE WAS REPLACED IAW AMM 25-59-01-400-804-001 REV 139 DATE 22 APR 239 APR 22, 2023</P>)
ON PREFLIGHT FOUND INTERIOR EMERGENCY EXIT LIGHTS INOP(<P>TRANSFER TO DMI 189699 PER MEL 33-51-01C. R/R BATTERY PACK M736 IAW AMM 33-51-07. OPS CHECK GOOD. PLACARD REMOVED AND NOTIFIED MCC.
OVERHEAD EMERGENCY LIGHT BY L1 DOOR INOP.(<P>RELAMPED LIGHT, OPS CHECKS GOOD IAW AMM 33-51-00</P>)
EMER DOORS LIGHT ON LEFT OVERHEAD PANEL COMING ON INTERMITTENTLY FOR LESS THAN A SECOND(<P><SPAN>R/R EMER DOOR LIGHT BULBS IAW AMM 33-11-00 OPS CHECK GOOD</SPAN></P>)
ON OVERHEAD PANEL EMER DOOR LIGHT FLICKERS(<P><SPAN>REMOVED AND REINSTALLED PSEU IAW B767 AMM 32-09-04, DOOR LIGHT OPS CHECKS GOOD&NBSP;</SPAN></P>)
EMER DOORS DISCRETE LIGHT ILLUMINATED INTERMITTENTLY IN FLIGHT(<P><SPAN>PERF PSEU TEST IAW AMM 52-71-00. NO FAULTS SHOW DURING TEST. PERF PESU TEST MULTIPLE TIMES WITH NO FAULTS SHOWING. EMER DOOR LIGHT NOT ILLUMINATED AT THIS TIME OR DURING THE PSEU TEST</SPAN></P>)
ONE INERTIAL ESCAPE REEL FELL FROM REEL CONTAINER.(<P>DEFERRED ONE INERTIAL ESCAPE REEL ON MDDR # 157585 PER MEL 25-61-01-01 EXPIRES ON 09DEC21. REEL REMOVED FROM AICRAFT.</P> / <P>29NOV, CVG MX: LP 1480402, ITEM M3: INSTALLED NEW INERTIAL REEL IAW B767 AMM 25-61-05. MCC NOTIFIED, PLACARDS REMOVED. DMI 157585 CLEARED.</P>)
R ENG HPSOV EICAS MSG INTERMITTENT DURING CLIMB OUT AND DESCENT(<P>TRANSFERRED TO MDDR # 156485 IAW MEL 36-11-02-02 DUE DATE 19 NOV 2021 CAT C PLACARD INSTALLED MX PROCEDURES MCC NOTIFIED.</P> / <P>&NBSP;</P> / <P>R AND R RH ENG HPSOV PER B767 AMM 36-11-07/401. LEAK CHECK GOOD. THIS CLEARS DMI. MCC NOTIFIED PLACARDS REMOVED.</P>)
R ENG HPSOV EICAS ADVISORY MSG INTERMITTENT FOR FIRST 2 HRS OF FLT. NO CHANGE IN DUCT PRESS WHEN MSG PRESENT. R ENG HPSOV STATUS MSG REMAINED.(<P>TRANSFERRED TO MDDR # 156439 PER MEL 36-11-02-02.</P> / <P>REF LOG 1373646 - REMOVED AND REPLACED RT ENG HPC IAW AMM 36-11-08. OPS CKS GOOD. THIS CLEARS MDDR 156439.</P>)
APU FAILED TO START ON GROUND ( APU TRU DEACTIVATED )(<P>TRANSFERRED TO MDDR 156465 PER MEL 24-32-01B CAT D DUE DATE 08FEB22 MX ACTION C/W.</P> / <P>&NBSP;</P> / <P>REMOVED AND REPLACED APU START TRU IAW AMM 24-32-04. OPS CHECK GOOD. THIS CLEARS DMI, MCC NOTIFIED. PLACARDS REMOVED.</P> / <P>&NBSP;</P> / <P>&NBSP;</P>)
R ENG HPSOV ADVISORY FLASHED ON SHORT FINAL BUT WENT AWAY. R ENG HPSOV STATUS MESSAGE REMAINING(<P>MESSAGE CLEARED PERFORMED AIR SUPPLY MODULE BITE TEST PER AMM 36-26-00. NO FAULTS NOTED</P>)
STATUS MESSAGE " R ENG HPSOV "(<P>TRANSFERRED TO MDDR 156260 PER MEL 36-11-02-02 CAT C DUE 15NOV21. GTC 0645Z.</P> / <P>07NOV21 - 1373638 - ITEM # 4 - AFW - REMOVED AND REPLACED #2 ENGINE HPSOV IAW B767 AMM 36-71-07. PERFORMED OPS AND LEAK CHECKS. NO DEFECTS NOTED. THIS CLEARS DMI 156260.</P>)
DURING PREFLIGHT FOUND L GEN FIELD LIGHT ON.(<P>PERFORMED BPCU BITE PER FIM 24-20 FT 801. FOUND LEFT GCU AT FAULT. REMOVED AND REPLACED GCU L/H IAW AMM 24-22-02. OPS CHECK GOOD. NO DEFECTS OR LIGHTS ONTED.</P>)
R FWD WINDOW HEAT EICAS.(<P>PER ATLAS REQUEST, REMOVED AND REPLACED CONTROLLER- WINDOW HEAT IAW AMM 30-41-01. OPS CHECK GOOD IAW AMM 30-41-02.</P>)
COCKPIT PORTABLE ELT AUTOMATIC RELEASE COVER TORN IN HALF.(<P>TRANSFERED TO MDDR # 154549 IAW MEL&NBSP; 25-63-10-01, CAT. D.</P> / <P>REMOVED AND REPLACED PORTABLE ELT IAW AMM 25-63-03. THIS CLEARS DMI 154549.</P>)
IN FLIGHT, "R GEN DRIVE" EICAS. COMPLIED WITH QRH AND CONTINUED W/MX AND DISPATCH CONCURRENCE(<P>REMOVED AND REPLACED RT ENG IDG PER AMM TASK 24-11-01-004-001-004. ENG RUN UP CKS NORMAL</P>)
WX RADAR STICKING @ 10 O'CLOCK POSITION. PERFORMED TS PER FIM 34-43- FT 805. OPS CHECK GOOD.</P>)
LEFT ENG ANTI-ICE MESSAGE, ONCE WE TURNED OFF ANTI-ICE IN DESCENT.(<P>ITEM PLACED ON DMI 153850 IAW MEL 30-21-01-04-02, LH ENG ANTI ICE VALVE LOCKED OPEN HPSOV LOCKED CLOSED. CAT C, DUE 01OCT21</P> / <P>21 SEP 21 - LP 1208271 ITEM 4 - CVG - REMOVED AND REPLACED LT ANTI-ICE VALVE. OPS AND LEAK CHECK GOOD IAW 30-21-03 THIS CLEARS MDDR 153850. MCC NOTIFIED AND PLACARD REMOVED.</P> / <P>&NBSP;</P>)
EICAS "L ENG ANTI ICE" VALVE NOT IN COMMANDED POSITION(<P>PERFORMED FIM 30-21 F/T 806. COULD NOT DUPLICATED FAULT. OPS CHECK GOOD. NO OTHER DEFECTS NOTED.</P>)
ELT PULL STRING SAFETY TAPE TORN / ( EMERGENCY LOCATOR TRANSMITTER (ELT), SURVIVAL TYPE ELTS )(<P>TRANSFERED TO MDDR 152702 PER MEL 25-63-10-01 CAT D...DUE DATE 28 DEC 21</P> / <P>ELT HAS BEEN ORDERED P/N:1151324-1 .</P> / <P>01SEP21 - 1395546 - ITEM# 2 - TPA - REMOVED AND REPLACED ELT AT L1 DOOR AMM 25-63-01. THIS CLEARS DMI #152702.</P>)
STATUS MESSAGE "R ENG HPSOV"(<P>TRANSFERRED TO MEL 36-11-02-02, CAT C, PLACARD INSTALLED. MDDR # 151181 DUE ON 12 AUG 21 C/W MX ACTION...</P> / <P>REF LOGPAGE 1390211 ITEM 6 . C/W AP20456 REMOVED AND REPLACED AIR SUPPLY MODULE IAW AMM 36-23-01. REACTIVATED HPSOV OPS CK GD..NO MSG. PERFORMED AIR SUPPLY BITE IAW AMM 36-23-00. NO ACTIVE&NBSP;</P> / <P>FAULTS.THIS CLEARS MDDR 151181, MCC NOTIFIED AND PLAC REMOVED.</P>)
LEFT CENTER FUEL PUMP INOP(<P>ITEM TRANSFERED TO MDDR 150554 PER MEL 28-22-02A&NBSP; &NBSP;CAT C ..DUE DATE 01AUG21, MX ACTION C/W CB PULLED AND COLLARED&NBSP;</P> / <P>&NBSP;</P> / <P>REF LOGPAGE&NBSP; 1399128ITEM 2: R/R LEST CENTER FUEL PUMP IAW 28-22-05 OPS CKS GOOD. THIS CLEARS DMI 10554. PLACRDS REMOVED MCC NOTIFIED ..DISPATCH BA @1326Z</P>)
AIR TURN BACK. ALT DISAGREE EICAS MESSAGE AT FL 390. CAPT ALT 39000 , FO ALT 39300 , STBY ALT 39600 PROGRESSIVELY GETTING WORST. PERFORMED TESTS OF THE AIR DATA COMPUTER SYS L AND R SUSPECT LEFT SYS AT FAULT , CHANGED LEFT AIR DATA COMPUTER IAW AMM 34-12-01 AND OPS CHECK 34-12-00 PITOT TEST 34-11-00 ALL CHECKS GOOD . CHECKED DRAINS AND QUICK CONNECTS FOR MOISTURE AND MISSING CAPS.
R HPSOV EICAS INFLIGHT TWICE BUT DISAPPEARED BOTH TIMES(<P><SPAN>REACTIVATED HPSOV IAW DDG 36-11-02-02 OPS CHECK GOOD</SPAN></P>)
R ENG HPSOV EICAS AND STATUS MESSAGES. REPEAT WRITE UP. TRANSFERED TO MDDR#150764 IAW MEL# 36-11-02-02, CAT C. MX ACTION COMPLIED WITH PLACARD INSTALLED. REMOVED AND REPLACED RIGHT HAND HPSOV CONTROLLER IAW AMM 36-11-08. PERFORMED LEAK CHECK ALL OPS AND LEAK ALL CHKS GOOD, ENGINE RUNS IAW 71-00-00, ALL CHKS GOOD. R/R HPC ON RH ENG OPS CHECK GOOD. PERF ENG RUN IAW AMM 71-00-00.ALL SYS PERF NORMAL
STATUS MSG: :R ENG HPSOV"(<P>PERFORMED @2 ENG RUN UP TO 80% N2 IAW AMM 72-00-00. NO MSGS RETURNED, PERFORMED BITE CHECK OF THE AIR SUPPLY BITE MODULE IAW B767 AMM 36-23-00. NO FAULTS FOUND AT THIS TIME.</P>)
ELT STRING/TETHER LOOSE AND UNRAVELING(<P><SPAN>REINSTALLED PORTABLE ELT TETHER PER AMM 25-63-03</SPAN></P>)
LEFT CTR FUEL PUMP INOP ( CENTER TANK FUEL PUMPS, ONE INOPERATIVE, CENTER TANK FUEL USED (NOTIFY DISPATCH) )(<P>ITEM TRANSFERED TO MDDR #150554 PER MEL 28-22-02A, CAT C. DUE DATE 01 AUG 21. MXACTION C/W. CB PULLED AND COLLARED.</P>)
STAUS MSG R ENG HPSOV STARTED ON APPROACH AS AN INTERMITTENT EICAS MESSAGE.(<P>PERFORMED AIR SUPPLY CTRL BITE TEST PER AMM 36-23-00. FOUND R HPSOV WIRE FAULT. PERF FIM 36-10 FT 833. DURING WIRE CHECKS FOUND CONNECTOR D4E10P LOOSE. RE-TIGHTENED CONNECTOR&NBSP; D4210P PER SWPM 20-60-06. OPS CKS GOOD. MESSAGE CLEARED . SEE LP #1461412 ITEM 4, PERFORMED ENGINE RUN IAW 71-00-00, NO DEFECTS NOTED @ THIS TIME.</P>)
APU WILL NOT START "GCU" SPARKS "IGN BOX" FAULT(<P>REMOVED AND INSTALLED SERVICEABLE IGNITION EXCITER IAW AMM 49-41-03. APU STARTS AND FUNCTIONS PROPERLY&NBSP;</P>)
EICAS MSG. IN CRUISE AFTER CYCLING THE ENG. ANTI-ICE OFF-ON-OFF R ENG. HPSOV RAN QRH. MSG BLANKED THEN REAPPEARED.(<P>TRANSFERRED TO MDDR 150273 PER 36-11-02-02, CAT C, DUE 26JUL21.</P> / <P>REF L/P 1399105: REMOVED AND REPLACED R ENG. HPSOV REF AMM 36-11-03. OPS AND LEAK CHECKS GOOD. MDDR 150273 CLOSED. PLACARDS REMOVED.</P>)
R ENG HPSOV EICAS DURING CRUISE. FOLLOWED QRH.(<P>PERFORMED BITE TEST, MESSAGE CLEARED. NO FURTHER FAULT NOTED. OPS CHECKS GOOD IAW FIM 36-10 FUNCTIONAL TEST 833.</P>)
STATUS MESSAGE R ENG HPSOV(<P>REMOVED AND REPLACED R ENG HPSOV PER AMM 36-11-07-424-016-001 AND 71-00-00</P>)
R ENG OIL PRESSURE INDICATION AMBER FLUCTUATION BETWEEN 1315 PSI TAXING IN TO PARKING. ALL OTHER INDICATIONS NORMAL ON R ENG.(<P>R/R RH ENG OIL PRESSURE TRANSMITTER IAW AMM 79-32-01. PERFORMED ENGINE IDLE RUN IAW AMM 71-00-00 OPS CHECK GOOD, LEAK CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS MOMENT.</P>)
IDLE DISAGREE EICAS MESSAGE X2 ON DECENT(<P>PERFORMED IDLE ENGINE RUN IAW AMM 71-00-00-862-144-H03. MX MSG L ENG EEC OBSERVED. TRANS TO MDDR 146550 PER MEL 73-21-01-03, CAT C, DUE 17 MAY21. CAT III RESTRICTED. COMPLIED WITH W/O # 80705 REMOVED AND REPLACED LT & RT ENG TAI RELAY K785, K786 IAW SWPM 20-81-22. AS PER ACTION PLAN AP-19951. NO OTHER DEFECTS NOTED.
INFO ONLY, DURING ENGINE START IN ILN, THE LEFT ENGINE HAD NO EGT RISE WHEN FUEL CONTROL SWITCH IN RUN. WHEN ENGINE START SELECTOR MOVED FROM SINGLE TO BOTH, LEFT ENGINE START NORMAL. PERFORMED IGNITION AUDIBLE CHECK OF LEFT ENGINE. OPS CHECK OKAY AT THIS TIME. REF AMM 74-00-00-705-104-H03.
THE WEATHER RADAR RETURNS LARGE VERTICLE STREAKS OF RED ON THE HSI(<P>PERFORMED BITE OF WEATHER RADAR SYSTEM IAW FIM TASK 34-43 FT 805, NO FAULTS FOUND. PERFORMED OPS CHECK OF WX SYSTEM IAW AMM 34-43-00. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.<BR /></P>)
DURING #1 ENG START ENG DID NOT LIGHT OFF. SUBSEQUENTLY SELECTED THE "ENG START" SELECTOR TO BOTH. ENG STARTED NORMALLY ON SEC ATTEMPT.(<P>PERFORMED IGNITION SYS AUDIBLE TEST IAW AMM 74-00-00.OPS CHK OK.RAN #1 ENG PER AMM 71-00-00. ENG START 1ST ATTEMPT.<BR /></P>)
"L ENG IGNITOR 2" STATUS MESSAGE IS DISPLAYED(<P>T/S PER FIM 71-01 FT 801.NO FAULTS NOTED AT THIS TIME. RAN #1 ENG PER AMM 71-00-00. STARTED 1ST ATTEMPT. NO MSG NOTED.<BR /></P>)
CARGO ARM AFT SWITCH "AFT" DOES DOES'T LIGHT UP DURING LAMP TEST OR CARGO FIRE/OVT TEST(<P>REMOVED AND REPLACED CARGO ARM SWITCH BACKSHELL "AFT" PER SWPM 20-84-00. OPS TEST GOOD IAW AMM 26-16-00.</P>)
AT FL360 RECEIVED EICAS&NBSP; "ALT DISAGREE" CAPT ALT READ 36000, FO 36250, STBY 36600 / REF LP 1247173 ITEM #1(<P>REMOVED AND REPLACED LH UPPER PITOT TUBE ASSY (CA'S PRIMARY) IAW AMM 34-11-01. OPS CHECKED IAW AMM 34-11-00, OPS CHECKS GOOD AT THIS TIME. MCC REQUEST REPLACEMENT OF RH LOWER PITOT TUBE ASSY. SEE LOG PAGE 1247174 ITEM M6 FOR CORRECTIVE ACTION FOR RH UNIT.</P><P><SPAN>LOG PAGE 1247174 ITEM M6:&NBSP;</SPAN>REMOVED AND REPLACED RH LOWER PITOT TUBE ASSY (CAPTS AUX) IAW AMM 34-11-01. OPS CHECKED GOOD AT THIS TIME. LEAK CHECKS GOOD AT THIS TIME (OFF PART: PN&NBSP;<SPAN>0856LU6, SN&NBSP;</SPAN><SPAN>164595).</SPAN></P>)
AFT CARGO DECK 2 STATUS MESSAGE. TRANSFERRED TO MDDR 141837 IAW MEL 26-16-01-01-01, CAT C.LP 1358580: R & R AFT CARGO SMOKE DETECTOR 2 IAW AMM 26-16-01. NO DEFECTS NOTED AT THIS TIME. THIS CLEARS MDDR 141837. MCC NOTIFIED. PLACARDS REMOVED.
LEFT SPAR FUEL VALVE CB POPPED. TROUBLE SHOT IAW ACTION PLAN AP-18948, NO RESOLUTION, BROKE SYSTEM AT SP464 AND SP1754 AND RESPLICED, STILL BAD SHORT TO GROUND. REMOVED CLAMPS ON WIRE RUN FOUND WIRE CHAFED UNDER A CLAMP, SPLICED WIRE SHIELD WITH PN D-436-37 PER SWP 20, OPS CHECK GOOD IAW AMM 80-11-00.
WXR SYSTEM STATUS MESSAGE RIGHT SIDE INTERMITTENT. NO FAULTS NOTED. REMOVED AND REPLACED WXR ANTENNA DRIVE UNIT, IAW AMM 34-43-00. MCC NOTIFIED.
R WXR SYSTEM FAILURE WHILE AT CRUISE WXR FAIL ON HSI ASSOCIATED WXR SYS STATUS. OPERATIONS CHECK R WXR SYSTEM, IAW FIM 34-43 FT 805 SYSTEM OK. ENDED AT BLOCK 2 OPERATIONS CHECK NORMAL AT THIS TIME. REMOVED AND REPLACED RT WXR XCVR, PER AMM 34-43-01. OPERATIONS TEST NORMAL AT THIS TIME. NO FURTHER DEFECTS NOTED.
RT FWD WINDOW ELECTRICAL ARC W/DELAMINATION. REMOVED AND REPLACED RT FWD NR 1 WINDOW, IAW B767 AMM 56-11-01. OPERATIONS CHECK GOOD.
DUE TO RT FWD NR 1 WINDOW REPLACEMENT, REPLACED RT WINDOW HEAT CONTROL UNIT. REMOVED AND REPLACED RT WINDOW HEAT CONTROL UNIT, IAW B767 AMM 30-41-01. OPERATIONS CHECK GOOD. RIGHT WINDSHIELD D1670 J5 WINDOW HEAT LEAD INTERMITTANT BAD CONTACT. REMOVED AND REPLACED D1670 J5 CONNECTOR, PER WDM 30-41-12 & BUTTSPLICED WIRE SM14 PER SWPM 20-30-19. OPERATIONS CHECK, PER AMM 30-41-01, OPERATIONS CHECK IS NORMAL. S/N OFF NSN P/N OFF CWC01-1210.
LEFT SPAR VALVE CIRCUIT BREAKER WILL NOT RESET. TROUBLESHOT PER WDM 28-22-21 FOUND PIN 6 AT D1554 SHORT TO GROUND. CUT WIRE AT SPLICE SP464 ON W454-008-18, FOUND NO SHORT TO GROUND THRU CONNECTOR D1554. FOUND SHORT TO GROUND AT W458-001-18, REF WDM 28-22-21 CUT SPLICE AT SP1754 AT W264-001-18. RECHECK GROUND THRU W1264-001-18. REPLACED SPLICE SP1754 & SP464, PER SWPM 20-30-19, CHECK FOR GROUND AT D1554 AT PIN 6 FOUND NO GROUND. PERFORMED OPERATIONS CHECK ON LEFT SPAR VALVE, PER AMM 28-22-11. OPERATIONS CHECK IS NORMAL. BREAKER DOES NOT POP.
FWD EQUIPMENT EXHAUST FAN STATUS MESSAGE. FOUND EXHAUST FAN BLADE SEIZED. REMOVED AND REPLACED FAN, IAW AMM 21-58-06. OPERATIONS NORMAL.
RIGHT WX RADAR FAIL STATUS MESSAGE. PERFORMED GROUND TEST OF BOTH WEATHER RADAR TRANS SYSTEMS, REF AMM 34-43-00-715-001-001. BOTH OPERATIONS CHECK NORMAL.
WEATHER RADAR IS MAKING RANDOM SWIPES ON THE SCREEN CONSISTANTLY AT ALL ALTITUDES AND ALL TILT SETTINGS. PERFORMED OPERATIONAL TEST OF THE WEATHER RADAR SYSTEM, IAW AMM 34-43-00-715. NO FAULTS DURING THE SCANNING OF THE RADAR OPERATIONS CHECK. "WXR TEST" MESSAGE SHOWN ON BOTH EHSI'S, OPERATIONS CHECK NORMAL.
WX RADAR SYSTEM RIGHT FAIL NOTE LEFT SYSTEM OK. TRANSFERRED TO DMI 139400, CAT C, IAW MEL 34-43-01-02. PLACARD INSTALLED. MCC NOTIFIED WITH CHRIS REQUIRES RIGHT TRANSCEIVER P/N 622-5132-633. REMOVED AND REPLACED RT WXR TRANSCEIVER, IAW AMM 34-43-04. OPERATIONS NORMAL AT THIS TIME. THIS CLEARS DMI 139400. ALL PLACARDS REMOVED.
STATUS MESSAGE WXR SYSTEM. T/S IAW FIM 34-43 FAULT TREE 805. SYSTEM TEST GOOD, MESSAGE CLEARED.
"WXR FAIL" MESSAGE ON NAVIGATION DISPLAY, "WXR SYS" STATUS MESSAGE. PERFORMED OPERATIONAL TEST OF THE WEATHER RADAR SYSTEM, IAW AMM 34-43-00-715-011-001. OPERATIONS TEST GOOD, NO FAULTS NOTED.
AFT EQ EXHAUST FAN 1 EICAS MESSAGE EQUIPMENT LAV/GALLEY EXHAUST. REMOVED AND REPLACED AFT EQUIP COOLING FAN, IAW AMM 21-58-41. OPERATIONS CHECK GOOD.
RT WX RADAR FAIL. PERFORMED OPERATIONS CHECK OF RT WX RADAR. OPERATIONS CHECK GOOD, PER B767 AMM 34-43-00.
CA EMER FLASHLIGHT PLASTIC BAND LOOSE. TRANSFERRED TO MDDR 135777, IAW MEL 25-63-04B, DUE 110CT20, CAT C. DISP 02:30Z TS. REMOVED AND REPLACED CA FLASHLIGHT BRACKET, IAW AMM 25-11-00. OPS CHECK GOOD. THIS CLEARS DMI 135777. MCC NOTIFIED. PLACARDS REMOVED, IAW CMM 25-60-02.
RT ENG OIL PRESS LIGHT DID NOT ILLUMINATE WITH ENGINE SHUTDOWN. REMOVED AND REPLACED RT ENGINE LOW OIL PRESSURE WARNING SWITCH, IAW AMM 79-33-01/401. OPS CHECK NORMAL.
WHEN DESELECTING GROUND POWER APU FIRE LOOP 1 STATUS MSG. OPS TESTED APU FIRE SYSTEM, PER B767 FIM 26-22-00. OPS TEST GOOD. NO MESSAGE NOTED AT THIS TIME.
R SIDE WIDOW HEAT INOP LIGHT ILLUMINATED(<P>PERFORMED FIM 30-41 F/T 803 UP TO BLOCK 21.R/R WHCU, M191. OPS NORMAL, NO FURTHER DEFECTS NOTED.</P>)
FWD CARGO FIRE ANNUNCIATOR LIGHT INOP(<P>RELAMPED IAW AMM 33-13-00, NO HELP. PER WDM 33-16-18 FOUND 28VDC AT CON D864 PIN 3 &4. R/R KORRY SWITCH IAW SWPM 20-84-00. OPS GOOD, NO DEFECTS NOTED. LAMP P/N 387</P>)
STATUS MSG WXR SYSTEM AFTER SHUTDOWN.(<P>PERFORMED FIM 34-43 TASK 801, STATUS MSG CLEARS. OPS CHECK ON L AND R WXR SYSTEM, NO FAULTS.</P>)
RIGHT SIDE WINDOW HEAT INOP. CYCLED CIRCUIT BREAKER. OPS NORMAL AT THIS TIME IAW AMM 30-41-00.</P>)
RIGHT DOME LIGHT MOUNTED EMERGENCY LIGHT IS INOPERATIVE(<P>REMOVED AND REPLACED EMERGENCY LIGHT LAMP, OPS CHECKS GOOD IAW AMM 33-51-00.<BR /></P>)
R ENG ANTI-ICE MSG. QRH COMPLETE, MSG REMAINS. REMOVED AND REPLACED RT ENG ANTI-ICE VALVE REF: AMM 30-21-03. OPS CHECK REQUIRED. ENG RUN OPS CHECK NORMAL IAW AMM 30-21-03 AND 71-00-00
KEEL BEAM SPLICE TEE STA. 960 HAS CORROSION ON UPR SURFACE AT NUTPLATES REMOVED CORROSION AT SPLICE TEE IAW B767 SRM 51-10-02 100% MAT. LOSS OUT OF LIMITS IAW B767 SRM 51-10-02. REMOVED AND REPLACED SPLICE TEE AT STA. 960 IAW B767 SRM 51-40-02
RH IB FLAP REQUIRES REPLACEMENT DUE TO CORROSION FINDINGS ON REAR SPAR REMOVED AND REPLACED RH IB MAIN FLAP IAW B767 AMM 27-51-03. PERFORMED SATISFACTORY OPS CHECK IAW B767 AMM 27-51-00
R SIDE WINDOW HEAT "INOP" LIGHT ILLUMINATING W/ ADVISORY MESSAGE. TROUBLESHOT RT SIDE WINDOW HEAT IAW FIM TASK 30-41 TASK 801 AND 803, BITE RIGHT SIDE WINDOW HEAT CONTROL UNIT, TEST GOOD. PERFORMED WINDOW HEAT ELEMENT RESISTANCE TEST. TESTED WITHIN LIMITS. T
APU PNEUMATICS INOPERATIVE. PERFORMED TROUBLESHOOTING OF APU BLEED SYSTEM & NOTED A BAD APU BLEED AIR VALVE IAW AMM 49-11-00. REACTIVATED VALVE AND PERFORMED APU OPS CHECK IAW AMM 49-11-00 AND ECU BITE CHECK IAW FIM 49-11 F/T 987. APU BLEED SYSTEM OPERATES NORMALLY, NO DEFECTS NOTED AT THIS TIME.
LEFT WEATHER RADAR SPIKING IN CRUISE. REMOVED AND REPLACED WEATHER RADAR TRANSCEIVER IAW AMM 34-43-01, OPS CHECKED GOOD.
R WX SYSTEM INOPERATIVE. HS1 WXR FAIL MESSAGE AND WXR SYS STATUS MESSAGE. PERFORMED WXR BITE PROCEDURE IAW FIM 34-43 FAULT TREE 805, TEST PASSED, MESSAGE CLEARED.
WXR SYS STATUS MSG. PERFORMED WXR RADAR OPERATIONAL TEST REF AMM 34-43-00-715-001-001. OPS TEST GOOD. OK FOR RTS, MSG CLEARED.
AFTER ENGINE START R ENG BLEED OFF MSG ON EICAS REMOVED AND REPLACED PRV FOR RIGHT HAND ENGINE IAW AMM 36-11-18. LEAK AND OPS CHECK GOOD. MESSAGE CLEARED
NR 2 ELT EXPIRATION STICKER MISSING.(<P>TRANSFER TO MDDR 127939 IAW DDG 25-63-10-01, CAT 'D'.&NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; LP 1140476-8 (ONT) - 05MAY20 -&NBSP; REMOVED AND REPLACED PORTABLE ELT IAW AMM 25-63-03. OPS NORMAL AT THIS TIME. THIS CLEARS MDDR 127939.</P>)
FOUND MAIN DECK 3A SMOKE DETECTOR AMBER LIGHT ILLUMINATED.(<P>DEFERRED AND TRANSFERRED TO DMI 127478 IAW MEL 26-16-02-02, CAT "C", DUE DATE 04MAY2020.</P><P>LP&NBSP;1140586 ITEM M2: PERFORMED FIM TASK 26-19-00-815-803, NO DEFECTS NOTED AT THIS TIME. THIS CLEARS MDDR 127478.</P>)
ELT ANTENNA IS PULLED OUT AND MAY BE BENT.(<P>RESECURED ELT IAW AMM 25-63-03.</P>)
FWD LEFT FUEL PUMP SELECTED OFF REMAINS "ON".(<P>C/W TEST OF LH FWD FUEL PUMP IAW AMM 28-22-00-715-001. OPS CHECK GOOD.</P>)
LEFT AFT FUEL PUMP SWITCH STILL "ON" WITH PUMP SELECTED OFF.(<P>REMOVED AND REPLACED KORRY SWITCH FROM LEFT AFT PUMP SWITCH IAW B767 AMM 28-22-17-404-006. PERFORMED OPS CHECK, OPS CHECKS SATISFACTORY ALSO IAW B767 SPWD 20-84-30.</P>)
L ENG FUEL FILT EICAS MSG DISPLAY ON AND OFF(<P>REMOVED AND REPLACED L ENG FUEL FILT PER FIM 73-11 FAULT TREE 803 AND AMM 73-11-02/401. OPS AND LEAK CHECK GOOD.</P>)
RADAR SPIKES ON THE RH SYSTEM(<P>PERFORMED WEATHER RADAR SYSTEM OPERATIONAL TEST. NO FAULTS NOTED AT THIS TIME. LH & RH SYSTEM OPS CHECK GOOD AT THIS TIME IAW AMM 34-43-00.</P>)
RH ENG ANTI-ICE EICAS MESSAGE WHEN TURNING SWITCH OFF AFTER LANDING (REPEAT WRITE-UP).(<P>REMOVED AND REPLACED RH ENGINE ANTI-ICE VALVE IAW AMM 30-21-03. OPS CHECK GOOD. NO DEFECTS NOTED. RAN RH ENG IAW AMM 71-00-00. ENG RUN GOOD.</P>)
R ENG ANTI-ICE EICAS ADVISORY MESSAGE WITH VALVE LIGHT WHEN TURNING ANTI-ICE OFF ON GROUND AFTER LANDING.(<P>PERFORMED OPS CHECK OF RH ENG ANTI-ICE VALVE IAW AMM 30-21-00. OPS CHECKS NORMAL AT THIS TIME.</P>)
L GEN FIELD LIGHT ON.(<P>PERFORMED OPERATIONAL TEST FOR L GEN IAW AMM 24-11-00. LIGHT EXTINGUISHED. NO FAULTS NOTED, TEST NORMAL.<BR /></P>)
R GENERATOR DISCONNECT LIGHT INOP(<P>REMOVED AND REPLACED ELECTRICAL PANEL IAW B767-300 AMM 24-22-01. OPS CHECKED GOOD.</P>)
DURING LEFT ENGINE START, NO RISE IN EGT, NO LIGHT OFF, IGNITION SELECTED TO BOTH + NORMAL START. L ENG IGNITOR 2 STATUS MSG.(<P>PERFORMED FIM 74-00 FT 811, L PIMU FAULTED 351.21-A/B IGNITOR 2 FAIL IAW FIM 71-01-00 PIMU BITE, FOUND IGNITOR 2 DAMAGED, REMOVED AND REPLACED&NBSP;IGNITOR IAW AMM 74-21-02, PERFORMED SYS AUDIBLE TEST. TEST VERIFIED GOOD, PERFORMED ENG START IAW AMM 71-00-00. ENG START NORM, NO FAULTS NOTED.<BR /></P>)
RIGHT PACK TEMP AFTER LANDING.(<P>TRANSFER TO MDDR 124333 DDG 21-51-01-01, CAT 'C', DUE 15FEB2020.</P><P>LP 1187646: PERFORMED R TEMP CONT BITE IAW FIM 21-51 FT 803. FAULTED TEMP CONT VALVE, INSPECTED VALVE TEMP CONT, FOUND LOOSE CANNON PLUG. RE-SEATED PLUG IAW SWPM 20-61-19. PERFORMED R PACK TEST IAW AMM 21-61-00. TEST PASS. THIS CLEARS DMI 124333.<BR DATA-MCE-BOGUS="1" /></P>)
#1 ENG DID NOT LIGHT OFF (NO EGT) DURING START IN SCK WITH SINGLE IGN. PERFORMED NORMAL START USING BOTH POSITION ON IGNITION.(<P>PERFORMED AUDIBLE TEST FOR #1 ENG IAW AMM 74-00-00. TEST OK, PERFORMED 2 SUCCESSFUL STARTS IN SINGLE SOURCE IAW AMM 71-00-00. NO FAULTS NOTED.<BR /></P>)
UPON T/S OF LH ENG IGNITION, FOUND LH PIMU BAD.(<P>REMOVED AND REPLACED&NBSP;LH PIMU IAW AMM 77-35-02. OPS CHK GOOD.<BR /></P>)
RIGHT PACK OVER TEMP / RAN QRH.(<P>PERFORMED RIGHT TEMPERATURE CONTROLLER BITE TEST IAW FIM TASK 21-51 FAULT TREE 803, TEST PASS.</P>)
R ENGINE AI VALVE LIGHT ON.(<P>PERFORMED GROUND OPS CHECK IAW AMM 30-21-00. R ENGINE AI VALVE LIGHT OFF OPS CHECK GOOD.<BR /></P>)
LEFT ENGINE NO LIGHT OFF WITH IGNITER ON SINGLE. SWITCHED TO BOTH AND ENGINE LIT OFF.(<P>TRANSFERRED TO DMI 124233, LEFT ENGINE #1 IGNITION IAW MEL 74-00-01B, CAT "C", DUE 22FEB2020.</P><P>LP 1171918 - M7: PERFORMED FIM 74-00 FT 809 TO STEP 23. REMOVED AND REPLACED LH #1 EXCITER IAW AMM 74-11-01. PERFORMED 3 SUCCESSFUL ENGINE STARTS, OPS OK. THIS CLEARS DMI 124233.</P>)
R PACK TEMP ADVISORY MESSAGE. WENT OUT AFTER APROX. 1 MIN. PERFORMED BITE TEST PROCEDURE ON RIGHT PACK, IAW B767-300 FIM 21-51 FT 806. NO MESSAGE ON EICAS PRESENT AT THIS TIME.
RT PACK TEMP LIGHT CAME ON AND WENT OUT TWICE ON FINAL DESCENT. PERFORMED PACK TEMP CONTROLLER BITE IAW AMM 21-51-00. FOUND TEMP CONT VALVE FAULT, RESET PTC, OPS TESTED IAW AMM 21-51-00. OPS TEST GOOD, NO NEW FAULT.
EICAS MSG "R ENG FUEL FILT". MSG BLANKED ASCENDING FL210. STATUS MSG "R ENG FUEL FILT" REMAINS.(<P>REMOVED AND REPLACED R ENG FUEL FILTER IAW AMM 73-11-02. PERFORMED LEAK CHECK. NO LEAKS NOTED. MSG EXTINGUISHED AND DID NOT RETURN DURING OPS CHECK. REF B767 AMM 71-00-00-712-168. OPS CHECK SATISFACTORY.</P>)
AFT CABIN TEMP EICAS CAUTION MSG IN FLIGHT.(<P>PERFORMED BITE CHECK ON THE ZONE TEMP CONTROL UNIT. NO CURRENT FAULT, NO MESSAGES PRESENT. REF AMM 21-61-00.</P>)
EICAS MSG: AFT CABIN TEMP.(<P><SPAN>REMOVED AND REPLACED AFT TRIM AIR VALVE RELAY IAW SWPM 20-81-00. PREVIOUSLY AFT TRIM AIR VALVE WAS REPLACED PER FIM 21-60-FT 804. REPLACE K240 RELAY IF PROBLEM CONTINUES. OPS CHECK NORMAL IAW AMM 21-61-00.</SPAN><BR /></P>)
R ENGINE OIL PRESSURE LIGHT NOT ILLUMINATED(<P>REMOVED AND REPLACED OIL PRESSURE SWITCH IAW AMM 79-32-00. OPS CHK&NBSP; GOOD.</P>)
AFT CABIN TEMP EICAS MESSAGE ON THE GROUND. REMOVED AND REPLACED AFT TRIM MODULATING VALVE IAW AMM 21-61-02-004-006, AND 21-61-02-404-041. OPS CHECKED GOOD.
EICAS MSG AFT CABIN TEMP(<P>PERFORMED ZONE TEMP CONTROLLER BITE IAW FIM 21-60 F/T 804. FOUND AFT ZONE TRIM MODULATING VALVE FAULT. REMOVED AND REPLACED AFT ZONE TRIM MODULATING VALVE IAW AMM 21-61-07. OPS CHECK GOOD. NO DEFECTS NOTED.<BR /></P>)
RIGHT ENGINE OIL LOW PRESSURE LIGHT INOPERATIVE. INBOUND FLIGHT CREW REPORTED NO OTHER FAULTS. OPS CHECKED THE LIGHT IAW FIM 79-33 FT 803, OPS CHECKED GOOD.
L FWD FUEL PUMP EICAS AT APPROXIMATELY 13K FEET.(<P>TRANSFERRED TO MDDR 122041 IAW DDG 28-22-01, CAT "C", DUE DATE 24-DEC-19. PLACARD INSTALLED. MCC NOTIFIED. </P><P>LP 1221107 - M3: REMOVED AND REPLACED LEFT FWD FUEL PUMP AS PER AMM 28-22-02 (OFF PART: PN&NBSP;<SPAN>5006003D, SN</SPAN><SPAN>&NBSP;</SPAN><SPAN>2365)</SPAN><SPAN>. NO HELP. DMI 122041 REMAINS OPEN.</SPAN></P><P>LP 1221110 - M5: REMOVED AND REPLACED L FWD FUEL PUMP GFI RELAY PER AMM 28-22-18. OPS CHECK NORMAL. THIS CLEARS DMI 122041 MEL 28-22-01. PLACARD REMOVED.</P>)
AFT CABIN ZONE TEMP INOP, LIGHT ILLUMINATES INTERMITTENTLY. REMOVED AND REPLACED CABIN AIR SENSOR IAW AMM 21-61-01. OPS CHECKED GOOD.
CTR RT FUEL PUMP EICAS MSG AND CTR R FUEL PUMP PRESSURE LIGHT. REMOVED AND REPLACED RIGHT FUEL BOOST PUMP UFI RELAY IAW WDM 28-22-12 AND UFI FIM 28-20-00. OPS CHECK GOOD AT THIS TIME.
AFT CABIN TEMP EICAS MESSAGE DISPLAYED ON DESCENT.(<P>PERFORMED BITE ON ZONE CONTROL UNIT REF FIM 21-61 FT 803, OPS CHECK NORMAL.&NBSP;</P>)
EICAS MSG AFT CABIN TEMP ON CLIMBOUT.(<P>PERFORMED BITE TEST ON ZONE CONTROL BOX REF FIM 21-60 FT 804, OPS CHECK NORMAL.</P>)
AFT CABIN TEMP ADVISORY MESSAGE.&NBSP;(<P>T/S PER FIM 21-60-806&NBSP; AND FOUND TEMP CONTROL FAULT LIGHT FOR AFT ON. TRANSFERRED TO MDDR #121719 IAW MEL 21-61-01-02, CAT 'C', DUE DATE: 17-DEC-2019.&NBSP;</P><P>LP&NBSP;1075672 - M3: PERFORMED FIM 21-61 FT 804, AFT ZONE TRIM AIR VALVE FAULTED. REMOVED AND REPLACED AFT ZONE TRIM AIR VALVE (V3) IAW AMM 21-61-07, OPS CHECK NORMAL. NO EICAS MSG PRESENT. THIS ACTION CLEARS DMI 121719, PLACARDS REMOVED AND MCC NOTIFIED.</P>)
EXTRA FIRST AID KIT HAS SEAL MISSING.(<P>RE-SEALED EXTRA FIRST AID KIT IAW GMM 3-28-1.<BR /></P>)
FIRST AID KIT BY L1 DOOR HAS BROKEN SEAL.(<P>FIRST AID KIT WAS INVENTORIED, CONTENT AMOUNTS VERIFIED, AND RESEALED IAW GMM 3.28.1. MCC NOTIFIED.</P>)
CARGO DET AIR ON EICAS DISPLAY.(<P>TRANSFERRED TO MDDR 120587 IAW MEL 26-14-01, CAT 'C', DUE DATE 24-NOV-19.</P><P>LP 1107211 - M8: REMOVED AND REPLACED PRESSURE SWITCH S454 IAW AMM 26-16-03, NO HELP.&NBSP;OFF PART (PN:&NBSP;32V92, SN: 3051) PER FIM 26-16 FT 814, SUSPECT FORWARD SMOKE DET BLOWERS 1 & 2. PLACED PART ON ORDER WITH MCC, P/N 033638. DMI 120587 REMAINS OPEN.</P><P>LP&NBSP;1107215&NBSP;- M3: PERFORMED OPERATIONAL TEST OF THE CARGO COMPARTMENT SMOKE DETECTION SYSTEM IAW AMM 26-19-00. WITH THE APU ON AND SUPPLIED PNEUMATIC PRESSURE, THE MESSAGE "CARGO DET AIR" GOES AWAY ON EICAS. OPS CHECK NORMAL, DMI 120587 REMAINS OPEN.&NBSP;</P><P>LP&NBSP;1107217 - ITEM 1: PERFORMED FIM TASK 26-16 FAULT TREE 814, SYSTEM NORMAL. THIS CLEARS MEL 26-14-01, DMI #120587. PLACARD REMOVED AND MCC NOTIFIED.&NBSP;</P>)
CAPT REPORTED FWD EQPT VAL MSG APPEARED AFTER START UP AND WENT AWAY AFTER RE-START. REMOVED AND REPLACED 3 WAY SHUTOFF VALVE IAW AMM 21-58-01, OPS CHECK GOOD.
L1 DOOR FLASHLIGHT INOPERATIVE/SEAL BROKEN.&NBSP;(<P>TRANSFERRED TO MDDR 120100 PER NEF 25-20-01, CAT 'E', DUE DATE: 02-MAR-2020. FLT DECK ITEM 41.</P><P>LP 1109386 -&NBSP;ITEM M5: INSTALLED NEW SEAL AS REQUIRED IAW AMM 25-10-00, FLASHLIGHT OPERATES NORMAL AT THIS TIME. THIS CLEARS DMI #120100. PLACARDS REMOVED.<BR /></P>)
ITEM 1: "L ENG STARTER" EICAS MSG, L ENGINE STARTER INOP. ITEM 2: LEFT ENGINE, NO MANUAL START. 1-3 ATTEMPTS, NO AIR PRESSURE DROP OR N2 ROTATION. ON 4TH ATTEMPT, N2 ROTATION TO MAX MOTORING THEN HUNG AT 29%. N2 THEN FLUCTUATES BETWEEN 29-25%, THEN 19-22%, START ABORTED.(<P>TRANSFERRED TO MDDR 119339 IAW MEL 80-00-02-01, CAT 'C'.</P><P>LP 1109324 - M3: REMOVED AND REPLACED L ENG STARTER ASSY IAW AMM 80-11-01. OPS CHECK NORMAL AT THIS TIME, NO EICAS MSG NOTED. THIS CLEARS DMI #119339. PLACARDS REMOVED AND MCC NOTIFIED.</P><P>LP 1109324 - ITEM 2: REF ITEM M3 FOR LEFT ENG STARTER CHANGE. RAN LEFT ENGINE TWICE USING 1 & 2 IGNITION, AND A & B EEC CHANNELS PER AMM 71-00-00. OPS CHECK GOOD WITH NORMAL PARAMETERS.&NBSP;</P>)
"FWD EQPT VAL" EICAS AFTER LEFT ENGINE START. QRH FOLLOWED, "VALVE" LIGHT ON EQUIP COOLING PANEL FAILED TO EXTINGUISH.(<P>PERFORMED FIM TASK 21-58 FT 899, SUSPECT BAD MANIFOLD INTERCONNECT VALVE. REMOVED AND REPLACED MANIFOLD INTERCONNECT VALVE IAW AMM 21-58-01, NO FAULTS NOTED.<BR /></P><P>LP 1109323 - ITEM 1: SWAPPED K488 RELAY, P/N: BACR13CF2AB WITH K2193 RELAY, P/N: BACR13CF2AB IAW SWPM 20-81-22. OPS CHECK GOOD, NO FAULTS NOTED IAW AMM 21-58-01.</P>)
"AFT CABIN TEMP" EICAS NOTED DURING PRE-FLIGHT.(<P>TRANSFERRED TO MDDR #119271 IAW MEL 21-61-04-02, CAT 'C', DUE DATE: 27-OCT-19.&NBSP;MX ACTION C/W.&NBSP;</P><P>LP 1109319 - M3: PERFORMED FIM 21-60 FT 806, AFT ZONE TRIM AIR VALVE FAULT. REMOVED AND REPLACED AFT TRIM AIR MODULATING VALVE IAW AMM 21-61-07. OPS CHECK GOOD, NO MSG PRESENT. THIS CLEARS MDDR #119271.&NBSP;<BR /></P>)
AFTER ENGINE START, EICAS MESSAGE "FWD EQUIPMENT VALVE". QRH FOLLOWED, DID NOT CLEAR. RECYCLED EQUIPMENT COOLING SWITCH FROM AUTO TO STANDBY, OPERATION NORMAL AT THIS TIME PER AMM 21-58-00.
LEFT RADAR DISPLAYED INTERMITTENT SPIKES AFTER ABOUT AN HOUR AND HALF INTO THE FLIGHT. C/W OPERATIONAL TEST OF LEFT WEATHER RADAR SYSTEM IAW B767-300 AMM 34-43-00, OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME. ALSO PERFORMED WEATHER BITE PROCEDURES PER FIM 34-43 FT 805, SYSTEM TEST OK.
CENTER RIGHT FUEL PUMP EICAS MESSAGE, AFTER START. INSPECTED WIRING AT THE PUMP PER SWPM 20-10-06, NO DEFECTS NOTED. RT CENTER FUEL PUMP OPS CHECK GOOD IAW AMM 28-22-00. TRANSFERRED 10,000 LBS INTO CENTER TANK AND BACK IAW AMM 28-26-00, OPS CHECKED GOOD.
FORWARD EQUIPMENT VALVE EICAS MESSAGE AFTER ENGINE START. PERFORMED FIM 21-58 FT 898 FOR FWD EQPT VALVE MSG AND SUSPECT MANIFOLD INTERCONNECT VALVE TO BE THE ISSUE DUE TO POSITION NOT CHANGING. REMOVED AND REPLACED MANIFOLD INTERCONNECT VALVE IAW AMM 21-58-01. OPS CHECK GOOD, NO FAULTS NOTED.A/C OK FOR SERVICE.
"ENG VALVE" DISCRETE LIGHT ILLUMINATED BRIEFLY ON DESCENT.&NBSP;(<P>PERFORMED OPS CHECK OF L & R ENG VALVE IAW AMM 71-00-00, TEST 4. OPS CHECK GOOD AT THIS TIME.&NBSP;</P>)
L RADAR SPIKED INTERMITTENTLY, APPROX LAST HALF OF FLIGHT. PERFORMED WEATHER RADAR SYSTEM OPERATIONAL TEST, COULD NOT DUPLICATE FAULT. NO FAULTS NOTED ON (L) SYSTEM AT THIS TIME. MCC NOTIFIED.
OXYGEN LEAK. PERFORMED LEAKS CHECK OF CREW O2 SYSTEM LINES IAW AMM 35-11-00. CHECKED AND TIGHTENED LINES IAW AMM 20-11-00. CHECKED CAPTAINS, F/O, AND OBSERVER MASKS FOR LEAKS, AND PROPER STORAGE IAW AMM 35-11-51. NO LEAKS NOTED, SYSTEM OPS NORMAL AT THIS TIME. LP 1088963 - M4: REMOVED AND REPLACED CREW O2 BOTTLE IAW AMM 35-11-00, AMM 12-15-08, AND GMM 3.25.3. LEAK CHECK GOOD, OPS NORMAL AT THIS TIME.
RT SIDE WINDOW HEAT INOP. TRANSFERRED TO MDDR #117150 IAW DDG 30-41-01-02, CAT C, DUE DATE 10-SEP-19. MX ACTIONS C/W. LP 1082311 - M2: RECYCLED RT WINDOW HEAT C/B'S, OPS CHECK DONE IAW AMM 30-41-00. OPS CHECKS GOOD AT THIS TIME. DMI #117150 CLEARED. PLACARDS REMOVED.
RIGHT CENTER FUEL PUMP INOP. TRANSFERRED TO MDDR 117130 IAW DDG 28-22-02A, CAT 'C'. LP 1101270 - M2 PERFORMED FIM 28-22 F/T 805 UP TO STEP 22 SHEET 2. COULD NOT GET POWER TO K330 OVERRIDE PUMP RELAY PIN X1. SUSPECT RIGHT FUEL OVERRIDE PUMP CONTROL SWITCH LIGHT ON FUEL MANAGEMENT PANEL. REQUIRES FURTHER T/S, DMI 117130 REMAINS OPEN. LP 1082335 - M2; REMOVED AND REPLACED THE FUELING CONTROL PANEL IAW AMM 28-21-13-004-001. OPS TEST GOOD. THIS CLEARS MDDR 117130. PLACARDS REMOVED AND MCC NOTIFIED.
R WXR SYS FAIL, WXR STATUS MESSAGE. FOUND PUSHED PIN ON RELAY K9201. RESET AND LOCKED THE PIN BACK ON THE RELAY 9201 IAW SWPM 20-80-00. PERFORMED OPS CHECK OF THE FO'S WEATHER RADAR SIDE SYSTEM IAW AMM34-43-00. ALL SYSTEM TEST PASSED, NO FAULTS NOTED.
STATUS AFT EQ EXH FAN 2. (<P>PERFORMED FIM 21-26 FT 808 BLOCKS 1, 40. FAULT CLEARED, OK FOR SERVICE.</P>)
R ENG BLD EICAS MSG INTERMITTENT THROUGH FLT. (<P>TRANSFERRED TO MEL 36-12-02-01 MDDR 115218, CAT C, DUE DATE: 02-AUG-19. PERFORMED BITE ON AIR SUPPLY MODULE FAV LIGHT SHOWN FIM 36-11-16.</P><P>LP 1090086 - M5:&NBSP;PERFORMED BITE TEST ON AIR SUPPLY BITE MODULE FOR FAULTS FROM LAST FLIGHTS. FOUND FAMV FAULT (DEFERRED). PERFORMED ENGINE RUN ON RT ENG IAW AMM 71-00-00 AFTER REACTIVATING FAMV (UNLOCKED). USE RT ENG BLEED. NO DEFECTS NOTED. RE DEFERRED (LOCKED) FAMV PER MEL 36-12-02-06. ITEM REMAINS OPEN. MCC NOTIFIED. &NBSP;</P><P>LP 1090091 - M5:&NBSP;REMOVED AND REPLACED FAN AIR VALVE ASSY ON RIGHT ENGINE IAW AMM 36-11-16. OPS CHECKS GOOD. THIS CLEARS MDDR 115218. MX ACTIONS REVERSED. MCC NOTIFIED AND PLACARDS REMOVED.&NBSP;</P>)
APU REAR BEARING PRESSURE LINE BOSS CRACKED. (<P>TRANSFERRED TO MDDR 115247 AS PER MEL 49-11-01A, CAT "C", DUE: 02-AUG-19.</P><P>LP&NBSP;1090090 - M2:&NBSP;W/O 54440 ISSUED FOR REPLACEMENT OF THE APU. REMOVED AND REPLACED APU IAW W/O # 54440 AND AMM 49-11-01. OPS CHECKED GOOD IAW 49-11-00. THIS CLEARS MDDR 115247. MCC NOTIFIED AND PLACARD REMOVED.</P>)
MDDR 113328 - ICE DETECTION SYSTEM INOP. (<P>REMOVED AND REPLACED ANTI-ICE PANEL IAW AMM 30-11-01 AND OPS CHECK IS GOOD AT THIS TIME. THIS CLEARS DMI # 113328. MCC NOTIFIED AND STICKERS REMOVED. WO # 53560 COMPLIED WITH.<BR /></P>)
CARGO FIRE CONTROL PANEL A-3 LIGHT IS ILLUMINATED AMBER, ALL OTHER LIGHTS NORMAL.(<P>T/S IAW FIM 26-19 F/T 803. FOUND SMOKE DETECTOR TO BE INOP. REMOVED AND REPLACED A3 SMOKE DETECTOR IAW AMM 26-19-01. OPS CHECK GOOD.</P>)
LEFT ENGINE ANTI ICE VALVE LIGHT STAYS ILLUMINATED. (<P>TRANSFERRED TO MDDR 113946 IAW MEL 30-21-02-01A, CAT C, DUE DATE: 09-JUL-19.</P><P>LP 1050844 - M3: PERFORMED 767 FIM 30-21 FAULT TREE 806. RAN LEFT ENGINE, CYCLED ANTI-ICE SEVERAL TIMES, LIGHT EXTINGUISHED EACH TIME. THIS ACTION CLEARS DMI #113946. MCC NOTIFIED AND PLACARDS REMOVED.&NBSP;</P>)
STANDBY ENG INDICATOR WILL NOT PERFORM BITE FUNCTION. REMOVED AND REPLACED THE STANDBY ENG INDICATOR IAW AMM 77-41-01, OPERATIONAL TESTED NORMAL.
DURING LEFT ENGINE START, NO LIGHT OFF. PERFORMED CORRECTIVE PROCEDURE AND SNGINE START WAS SUCCESSFUL ON SECOND ATTEMPT,(<P>PERFORMED AUDIBLE IGNITION TEST ON LEFT ENGINE, COULD NOT HEAR #2 SYSTEM (TOP) IGNITER. REMOVED AND REPLACED #2 IGNITOR WITH NEW. OPS CHECK IS GOOD. REF 767 AMM 74-21-02</P>)
R AFT FUEL PUMP ILLUMINATED INFLIGHT. QRH COMPLETED. TROUBLESHOOT IAW FIM 28-22 FT 819 FOUND R AFT FUEL PRESSURE SWITCH REQUIRES REPLACEMENT. T/S PER FIM 28-22 FT 819 BOOST PUMP LOW PRESSURE LIGHT ON EICAS. PER STEP 48 REPLACE APPLICABLE PRESSURE SWITCH. MCC NOTIFIED. REMOVED AND REPLACED RIGHT AFT FUEL PUMP PRESSURE SWITCH IAW AMM 28-42-01. DID NOT FIX THE PROBLEM. CONTINUE T/S IAW FIM 28-22 FT 819 STEP 49. FOUND CORROSION ON D1532. REMOVED, CLEANED FROM CONNECTOR PLUG.AND SW. CHECKED FOR CONT. ALL OK. OPS CKD PRESS SW IAW 28-42-01, STILL FAILED. REMOVED AND REPLACED RH AFT BOOST PUMP IAW B767 AMM 28-22-03. OPS CHECK GOOD.
WHEN DOING THE APU SHUFFLE AND APU BLEED VALVE SELECTED TO OFF, THE APU SHUTDOWN WITH A FAULT LIGHT. (<P>TRANSFERRED TO MDDR 112283 IAW DDG 49-11-01A CAT 'C'.&NBSP;</P><P>LP 1073282 - M3:&NBSP;T/S APU PER FIN 49-11-FT987. ECU CODE SHOWED FILTER SW (GEN), MCC NOTIFIED. PART ORDERED. DMI 112283 CONTINUES.</P><P>LP 1073286 - M2:&NBSP;REMOVED AND REPLACED APU GEN OIL FILTER DIFFERENTIAL PRESSURE SWITCH IAW AMM 49-27-15. OPS CHECK OF APU GOOD AT THIS TIME. MCC NOTIFIED. THIS CLEARS DMI #112283. PLACARDS REMOVED.</P>)
WHEN APU IS GIVEN FULL LOAD IT SHUT DOWN. ONCE IN BLOCKS IN TPA, RESTART NORMAL, AFTER #2 ENGINE STARTED, APU DIED AGAIN.(<P>PERFORMED OPS CHECK OF APU IAW AMM 49-11-00, NO FAULTS FOUND.</P>)
RIGHT ENGINE B3-1 BORESCOPE PLUG WORN. (<P>REMOVED AND REPLACED RT ENG B3-1 BORESCOPE PLUG PER AMM 72-00-00.</P>)
RIGHT FORWARD FUEL BOOST PUMP GFI RELAY K190 FAILED TEST. (<P>REMOVED AND REPLACED GFI RELAY K190 RT FWD FUEL BOOST PUMP IAW SWPM 20-81-14. OPS CHECK NORMAL IAW AMM 28-22-00.&NBSP;</P>)
O2 PRESSURE BLEED DOWN INFLIGHT AFTER BEING SERVICED @ SCK.(<P>PERFORMED O2 LEAK TEST IAW AMM 35-11-00. LEAK TEST CHECK GOOD. NO DEFECTS NOTED.</P>)
EICAS MSG FWD CABIN TEMP PRIOR TO BLOCK.(<P>TRANSFER TO MDDR # 111449 IAW DDG 21-61-06-02 CAT C DUE DATE 20-MAY-19.</P><P>LP 1063384-M5: REMOVED AND REPLACED FWD CABIN TEMP VALVE IAW AMM 21-61-07. OPS CHECK NORMAL. THIS CLEARS DMI 111449.</P>)
STATUS MSG R ENG SPEED CARD.(<P>PERFORMED CARD TEST IAW FIM 73-21 F/T 871 MSG CLEARED SYSTEM TEST OK.</P>)
APU INOP(<P>ITEM TRANSFER TO MDDR 110915 IAW DDG 49-11-01A CAT C DUE DATE 05-MAY-19.</P><P>LP 1033505 - M5:&NBSP;PERFORMED FIM 49-11 FAULT TREE 987 WMES WITH FAULT 16. CLEARED ECU AND CLEANED P2 SENSOR CONNECTOR AND CHECKED ALL LINES PER B767 AMM 49-61-04 NO FAULTS NOTED. APU RUN PERFORMED PER B767 AMM 49-05-00 FAULTS ECU WITH CODE 16. FOUND EXHAUST DUCT DAMAGED/TORN MCC NOTIFIED.&NBSP;</P><P>LP 1033507 - M3:&NBSP;R AND R SURGE CONTROL VALVE DUCT IAW AMM 49-53-01 APU STARTED NORMAL AND SHOWED GOOD DUCT PRESSURE WITH A LOAD. PREFORMED ENGINE RUN IAW 71-00-00 FOUND NO DEFECTS AND HAD GOOD ENGINE START. THIS CLEARS DMI 11915 ALL PLACARDS REMOVED.&NBSP;</P><P>RE-OPENED MDDR 110915</P><P>LP 1035513 - M4:&NBSP;R & R ECU WITH NEW ECU IAW AMM 49-61-05 NO HELP. PROBLEM CONTINUES, REPLACE OLD ECU IAW AMM 49-61-05. DMI 110915 REMAINS OPEN</P><P>LP 1033516 - M7:&NBSP;T/S APU BLEED USING FIM 36-10-00-815-839. REMOVED AND REPLACED APU CHECK VALVE. NO HELP IAW AMM 36-11-11. DMI 110915 REMAINS OPEN.</P><P>LP 1033526 - M5:&NBSP;REMOVED & REPLACED APU COMPRESSOR INLET TEMP SENSOR. NO HELP. DMI 110915 REMAINS OPEN.</P><P>LP 1033528 - M5:&NBSP;T/S AS FOLLOWS: CHECKED ECU FOR FAULTS. P2 SENSOR LRU IN WINDOW, CLEARED ECU MEMORY. CK'DP2 SENSOR INLET TUBE AND CLEANED. RAN APU AFTER SHUTDOWN NO FAULTS OR LRU'S ON ECU. RAN ENGINES 1 & 2 WITH GOOD PRESS, APROX 31 PSI. AFTER ENGINES SHUTDOWN LOSS OF APU PRESS TO 5 PSI. CHECKED ECU FOR FAULTS, P2 SENSOR IN WINDOW AGAIN. FIM REF 49-11 FT A21 STEP 1. REPLACE P2 SENSOR..PN# 3876035-5..REF IPC 49-61-00-01N ITEM 110. DMI REMAINS OPEN.</P><P>LP 1033529 - M6:&NBSP;CHECKED ECU FOR FAULTS. P2 SENSOR IN WINDOW AGAIN. FIM REF 49-11 FT A21 STEP 1 REPLACE P2 SENSOR .PN# 3876035-5. REF IPC 49-61-00-01 ITEM 110.</P><P>LP 1033530 - M3:&NBSP;REMOVED AND REPLACED INLET TEMP SENSOR GASKET IAW AMM 49-61-03 APU TO REMAIN ON DMI 110915 REMAINS OPEN AT THIS TIME.</P><P>LP 1078213 - M4: REMOVED & REPLACED INLET PRESSURE (P2) SENSOR IAW AMM 49-61-04. OPS CHK GOOD. THIS CLEARS DMI # 110915. MCC NOTIFIED & PLACARDS REMOVED.</P>)
APU INOP.(<P>TRANSFERRED TO MDDR 110852.</P><P>LP 1018850 - M3: PERFORMED APU BITE IAW FIM 49-11 F/T 987. NO FAULTS NOTED. PERFORMED OPS CHECK OF APU PER AMM 49-11-00. OPS CHECK NORMAL. THIS CLEARS DMI 110852. PLACARDS REMOVED. MCC NOTIFIED. DISPATCH - AA @ 0517.</P><P><BR DATA-MCE-BOGUS="1" /></P><P>NOTE: APU COLD SOAK VERIFICATION WAS OPEN ON LP 1018851 - MDDR 110901.</P>)
R PIMU EICAS MESSAGE(<P>REMOVED, CLEANED, AND REINSTALLED NR 2 ENGINE T-12 SENSOR IAW AMM 73-21-06.<BR /></P>)
APU AUTOMATIC SHUTDOWN (NOTE: ON DEPARTURE/ENG START).&NBSP;(<P>PERFORMED OPERATIONAL CHECK OF APU PER AMM 49-11-01. OPS CHECK GOOD.&NBSP;</P>)
AFTER POWER TRANSFER FROM GPU TO AIRCRAFT POWER, APU SHUT DOWN.(<P>RESET ECU FOR APU AMM 49-11-00. OPS CHECK GOOD.</P>)
WHEN CAPTAIN SELECTS WX RADAR IT CAUSED F/O TERRAIN DISPLAY TO BECAME INOPERATIVE. PERFORMED OPS CHECK PER AMM 34-43-00-701-001-001. CREW REPORTED THE RT WX RADAR OPERATED NORMALLY DURING FLIGHT. PERFORMED WXR BITE PROCEDURE IAW FIM TASK 34-43 FAULT TREE 805 SYSTEM CHECKED OK. SUSPECT RELAY WAS INOP. WEATHER RADAR TESTED IAW AMM 34-43-00/501 COULD NOT DUPLICATE TERRAIN FLICKER ON F/O DISPLAY UNIT. REMOVED AND REPLACED WXR CONTORL PANEL IAW AMM 34-43-02. OPS CHECKED GOOD. CARRIED OUT CONTINUITY CHECKS FOR SHORTS IN THE CIRCUITRY, RELAY K9201 & CONNECTOR PLUG WIRING IAW WD 34-46-17. NO FAULTS FOUND. RELAY WAS RESET TO SIT MORE SECURELY. T/S IAW WDM 34-43-21-1. SWAPPED WRCP, SWAPPED WAVEGUIDE SWITCH, SWAPPED LT TO RT IRU'S, NO HELP. SYS FUNCTIONS NORMALLY IN LH POS ON WRCP. IN RT POS. LT EHSI FUNCTIONS NORMALLY IN WX TEST BUT RT EHSI SHOWS WX FAIL. ACCOMPLISHED AP 15379. OPS CHECKED GOOD IAW AMM 34-43-00-5.
LEFT FWD FUEL PUMP EICAS. REMOVED AND REPLACED FUEL BOOST PUMP IAW AMM 28-22-03-404- OPS CHECK AND LEAK CHECK GOOD.
APU INOP.(<P>APU DEFERRED PER MDDR #109271.<BR /></P><P>REMOVED AND REPLACED APU STARTER IAW AMM 49-41-01 JL @ 16:07Z</P>)
APU INLET DOOR ACTUATOR INOP (ON SYSTEM DOOR CLOSED). (<P>REACTIVATED APU INLET DOOR OPS CHECK OF DOOR SATISFACTORY REF DDG 49-15-01.<BR /></P>)
APU FAULT IN FLIGHT&NBSP;(<P>T/S PER FIM 49-11 FT 987 LAST START NO FAULTS. 2ND START - NO START. NO MINI FLAGS. OPS CHECK NO FAULTS CLEARED FOR SERVICE.&NBSP; ////&NBSP; ON LP 1054810 - OPENED MDDR 109251 (MEL 25-AP-01) - APU COLD SOAK START VERIFICATION REQUIRED</P>)
RT ENG ANTI-ICE EICAS MSG WHEN TRYING TO DESELECT RIGHT ENGINE ANTI-ICE(<P>PERFORMED D.V.I., CLEANED AND RE-SECURED C/P ON RT ENGINE ANTI-ICE VALVE. PERFORMED OPS TEST OF RT ENG ANTI-ICE VALVE IAW AMM 30-21-00 OPS CHECK GOOD. NO EICAS MSG OR VALVE LIGHT&NBSP;</P>)
L ENG ANTI ICE FAILED UPON LANDING. (<P>OPS CHECKED L. ENG ANTI ICE VALVE IAW AMM 30-21-03. OPS CHECK GOOD AT THIS TIME<BR /></P>)
R PACK TEMP(<P>PFORMED PACK TEMP CONTROLLER BITE&NBSP; PROCEDURE IAW FIM 21-51 FT 803 RESET BITE BOX NO FAULTS FOUND&NBSP; SYSTEM OPS CHECK GOOD&NBSP;</P>)
L/H ENGINE ANTI ICE VALVE ILLUMINATED.(<P>TRANSFERRED TO MDDR 108063 IAW MEL 30-21-02-01A CAT C DUE DATE: 14 MAR 19, MX ACTION C/W. REMOVED AND REPLACED SWITCH IAW AMM 33-13-00 OPS TEST OK IAW AMM 30-21-03.<BR /></P>)
LEFT FWD FUEL PUMP LIGHT REMAINS ON WITH SWITCH SELECTED ON(<P>TRANSFERED TO MDDR 107785 PEER DDG 28-22-01 CAT C DUE 06MAR19 DISP T/I S.D. 0846Z LOG PAGE&NBSP;1058447, FOUND C/B GFI OPEN AT K188 RESET AND PERFORMED OPS CHECK OF SYSTEM IAW AMM 28-22-01, MDDR CLEARED. DISPATCH @ ST0854 PLACARD REMOVED.</P>)
RT ENGINE ANTI-ICE ILLUMINATED AFTER SHUT DOWN. VERIFIED RT ENGINE ANTI-ICE VALVE CLOSED. CLEANED THE ELECTRICAL CONNECTOR AND INSTALLED IAW AMM 30-21-00, AND 30-21-02-01. GROUND OPS CHECKED NORMAL.
LEFT FWD FUEL PUMP PRESSURE LIGHT ILLUMINATED DURING FLIGHT. CLEANED THE CONNECTOR ON THE FUEL PUMP, NO EICAS MESSAGE, OPS CHECKED NORMAL IAWAMM 28-22-00.
"WXR DSPY" FAULT ON FO HIST WHEN WXR PWR SELECTED.(<P>T/S TO R EFIS SYM GENERATOR. TRANSFER TO MDDR 107661 MEL 34-22-05B. CAT "C" MX ACTION C/W. MCC NOTIFIED. PLACARD INSTALLED. DISP BA @ 1744Z.</P><P>&NBSP;<BR /></P><P><BR /></P><P>LOG PAGE 1032655: T/S PER WDM 34-22-34. FOUND WIRES CROSSED AT TB119 H61,H63. CORRECTED WIRES PER WDM 34-22-00. OPS CHECKS OK PER AMM 34-22-00. MDDR # 107661 CLOSED AND PLACARD REMOVED.<BR /></P>)
WXR DSPY FAULT ILLUMINATED, ON THE FIRST OFFICER`S HISTORY WHEN WEATHER RADAR POWER WAS SELECTED. TROUBLESHOT TO THE RT EFIS SYMBOL GENERATOR.
#1 ENGINE #20 FAN BLADE HAS NICK(<P>ACCOMPLISHED BLEND OF #1 ENGINE #20 FAN BLADE IAW B767 AMM 72-31-02 ACCOMPLISHED FPT IAW B767 AMM 72-31-12 AND 70-11-06 NO DEFECTS NOTED.</P>)
#2 ENGINE FAN BLADE #2 NICKED(<P>ACCOMPLISHED BLEND OF #2 ENGINE #2 FAN BLADE IAW B767 AMM 72-31-02 ACCOMPLISHED FPT IAW B767 AMM 72-31-02 AND 70-11-06 NO DEFECTS NOTED.</P>)
#1 ENGINE #2 FAN BLADE HAS NICK(<P>ACCOMPLISHED BLED OF #1 ENGINE #2 FAN BLADE IAW B767 AMM 72-31-02 ACCOMPLISHED FPT IAW B767 AMM 72-31-02 AND 70-11-06 NO DEFECTS NOTED</P>)
#1 ENGINE IDG HEAT EXCHANGER S/O VALVE FILTER HOUSING FILTER STRIP THREADS(<P>REMOVED AND REPLACED #1 ENGINE IDG HEAT EXCHANGER S/O VALVE IAW B767 AMM 24-11-07</P>)
LEFT CENTER FUEL BOOST PUMP PRESSURE LIGHT NOT ON WHEN SWITCH IS CLOSED AND FUEL PANEL IS CLOSED WHEN SWITCH CYCLED NO PRESSURE LIGHT AT ALL(<P>PERFORMED T/S AND FOUND LOOSE CONNECTOR, RE-SECURED LOOSE CONNECTOR D5558P IAW 767 WDM 28-22-12. PERFORMED OPS CHECK TO THE LH CENTER FUEL BOOST PUMP IAW B767 AMM 28-22-00.</P>)
APU BLEED VALVE WILL NOT OPEN(<P>PERFORMED T/S FOUND SWAPPED WIRE AT CONNECTOR D4100J PIN 9,10,11. CORRECTED AND PERFORMED SATISFACTORY OPS TEST OF APU BLEED VALVE IAW B767 WDM 49-14-11 AND AMM 49-00-00</P>)
FUEL JETTISON FAULT LIGHT IS ON AT ALL TIMES - EICAS SHOWS MESSAGE "RH XFR JETTISON VLV"(<P>UPON INITIAL INSPECTION FOUND CONNECTOR D12182 OB V160 THE RIGHT JETTISON TRANSFER VALVE ACTUATOR LOOSE. TIGHTENED LOOSE CONNECTOR AND OPS CHECK GOOD IAW B767 WDM 28-31-11 AND B767 AMM 28-31-00</P>)
#1 ENGINE INLET SPINNER WHITE STRIPE REQUIRES PAINT TOUCH UP(<P>PREPPED, PRIMED, AND TOP COATED #1 ENGINE SPINNER IAW GE ESM 72-21-10.</P>)
#1 ENGINE #30 FAN BLADE SLIDER DOVETAIL SEAL TORN(<P>REPAIRED #1 ENGINE #30 FAN BLADE DOVE TAIL SEAL IAW B767 AMM 72-31-02</P>)
R/H PRSOV DOESNT OPEN OR REGULATED LOW MESSAGE AFTER ASM TEST ENGINE RUN(<P>REMOVED AND REPLACED R/H ENGINE PRSOV IAW B767 AMM 36-11-09 OPS CHECK GOOD IAW EO 6736A013 PAR 1</P>)
#2 ENGINE R/H CORE COWL LWR EXT SIDE AT MID LATCH SKIN HAS A 0.8 INCH LENGTH CRACK(<P>REMOVED AND REPLACED #2 ENGINE O/B CORE COWL IAW B767 AMM 71-11-06</P>)
#1 ENGINE #2 FAN BLADE HAS NICK(<P>ACCOMPLISHED BLEND REPAIR OF #1 ENGINE #2 FAN BLADE IAW B767 AMM 72-31-02 AND ACCOMPLISHED FPI TEST IAW B767 AMM 72-31-02 AND 70-11-06 NO DEFECTS NOTED.</P>)
R/H AC PACK 1EA BOOT AFT OF LARGE PLENUM ASSY TORN 1 INCH ON BOTTOM(<P>REMOVED AND REPLACED PLENUM ASSY FLEX DUCT ON R/H SIDE IAW B767 AMM 21-51-02, COMPLETED AND GOOD LEAK CHECK, NO LEAKS NOTED.</P>)
#1 ENGINE OUTBOARD SIDE ON FAN CASE HAS EVIDENCE OF LEAK (HYD/OIL)(<P>CLEANED AND PERFORMED LEAK CHECK ON #1 ENGINE O/B HYDRAULIC HOSES IAW B767 71-00-00 NO LEAKS FOUND.</P>)
CARGO DET AIR MSG ON EICAS(<P>PERFORMED GOOD OPS CHECK OF CARGO SMOKE DETECTION SYSTEM IAW AMM 26-14-00 NO FAULTS NOTED.</P>)
LEFT ENGINE BLEED WILL NOT OPEN WITH ENGINE RUNNING(<P>REMOVED AND REPLACED LH PRSOV IAW B767 AMM 36-11-09 OPS CHECK GOOD IAW B767 AMM 71-00-00, RESECURED PNEUMATIC SENSE LINE IAW B767 AMM 36-11-18, SYSTEM CHECKS GOOD IAW B767 AMM 71-00-00</P>)
FWD EQPT VALVE EICAS AFTER 2ND ENG START. ACCOMPLISHED QRH NO SUCCESS RETURNED TO GATE(<P>TRANSFER TO MDDR 106038 IAW MEL 21-58-07-02-01, MX PROCEDURE 2 FOLLOWED.&NBSP;</P><P>REMOVED AND REPLACED FWD EQUIPMENT EXHAUST VALVE IAW AMM 21-58-02 OPS CHECK GOOD , MDDR 106038 CLOSED&NBSP;</P>)
CARGO DET AIR DISPLAYED W/ APU IN OPERATION(<P>C/W FIM 26-16 FT 814 UP TO STEP 10, NO HELP. DEFERRED PER MEL 26-14-01 CAT C DUE 22JAN19, MX ACTIONS ACCOMPLISHED THIS BECOMES MDDR 105810.</P><P>LP 1034460-2:R/R AFT CARGO DETECTOR NR 1 BLOWER IAW AMM 26-16-02. THIS ACTION&NBSP;CLEARS DMI 105810, MCC NOTIFIED AND PLACARDS REMOVED.&NBSP;</P>)
CABIN AUTO INOP EICAS MESSAGE ILLUMINATED DURING CRUISE, FOLLOWED QRH PROCEDURE. ACCOMPLISHED CABIN PRESS CONTROLLER BITE TEST PROCEDURE FIM 21-31 FT 803, MSG CLEARED. OPS CHECK NORMAL.
APU INOP. REMOVED AND REPLACED FLOW SENSING MODULE IAW AMM 49-53-08. NO HELP. MINI FLAG TROUBLE CODES ON ECU: 14,15,16,120 PN OFF 3614400-7 S/N 492126. PERFORMED APU ECU BITE TEST IAW AMM 49-61-05. PERFORMED OPERATIONAL TEST OK.
ON BEFORE START FLOW. SWITCHED ON RT AFT FUEL PUMP PRESSURE LIGHT ILLUMINATED RT AFT FUEL PUMP EICAS MESSAGE. RESET C/B RT AFT FUEL PUMP OPS CHECKED GOOD IAW AMM 28-22-03.
AIRCRAFT DISCONNECTED/DROPPED GROUND POWER 03 TIMES BEFORE ACCEPTING IT AND HOLDING POWER. PERFORMED BPCU BITE PROCEDURES IAW FIM 24-20 FT 801. NO FAULTS NOTED. OK TO CONTINUE.
MAIN CARGO DECK FIRE DETECTOR NR 3 AMBER INDICATION ON PREFLIGHT. REPLACED CARGO DECK SMOKE DETECTOR IAW 26-14-01.
WHEEL WELL FIRE DETECTION SYSTEM INOP. REPLACED WW SWITCH IAW AMM 33-13-00.
APU TRU INOP. REPLACED TRU IAW AMM 24-32-04 OPS CHECKS GOOD.
RT ENG ANTI-ICE VALVE LIGHT ON. PERFORMED / OPS CHECK OF SWITCH FOR RT ENG ANTI-ICE VALVE IAW FIM 30-21 FAULT TREE NO / DEFECTS NOTED AT THIS TIME.
AT 03:54Z RIGHT SIDE WEATHER RADAR ELEVATION INDICATIONS FLICKERING ON SCREEN, SWITCH EFI SWITCH WITH NO CHANGE&NBSP;(<P>PERFORMED OPS CHECK I.A.W AMM 34-43-00 OPS CHECK GOOD&NBSP;</P>)
WHEN CA SWITCHES FROM TERRAIN DISPLAY TO WXR WITH FO SIDE SELECTED TERRAIN FO SIDE LOSES HSI TERRAIN DISPLAY. NO INDICATION OTHER THAN RADAR TILT FLICKERS.(<P><SPAN>PERFORMED / OPERATIONAL TEST OF WX RADAR SYSTEM IAW AMM 34-43-00 AND FOUND SYSTEM TO / OPERATE NORMAL AT THIS TIME.&NBSP;</SPAN></P>)
RIGHT ENGINE ANTI-ICE VALVE LIGHT STAY ILLUMINATED AFTER SHUTDOWN , RIGHT ENGINE ANTI-ICE EICAS MSG(<P>PERFORMED SYSTEM TEST I.A.W AMM 30-21-00 SYSTEM CHECKS GOOD AT THIS TIME COULD NOT DUPLICATE <BR /></P>)
DURING ENGINE START, APU AUTOSHUT DOWN AS ENG ACCELERATED THROUGH 35% N2. INTERROGATED THE ECU, NO FAULTS NOTED, TESTED OK IAW AMM 49-11-00.
RIGHT ENGINE ANTI-ICE VALVE INDICATION LIGHT INOP. COULD NOT DUPLICATE ON GROUND, RAN ENG 5 MINUTES IAW 30-00-00/901, OPS NML.
LT ENG ANTI ICE BUTTOM ON DISPLAY INTERMITTENT. PERFORMED OPS CHECK OF LT ENG ICE SWITCH STEM IAW AMM 30-21-00 THE ON SYSTEM LIGHT CAME ON STAY ON NO DEFECTS NOTED AT THIS TIME.
CAPT QTY MASK WONT TEST. R&R CAPT OXY MASK IAW AMM 35-11-51. OPS GOOD.
FO WXR/TERR MODES ONLY WORK WHEN MATCHING CA WXR/TERR SELECTION. PERFORMED WX RADAR SYSTEM TEST IAW AMM 34-43-00, ALL CHECKS GOOD AT THIS TIME.
FO'S TERRAIN AND WX SWITCHES SHOW FLASHING TILT W/ CAPT ON SW ON AND WILL NOT DISPLAY TERRAIN UNLESS CAPT SW IN TERRAIN AND WX OFF. PERFORMED FIM 34-43-FT 805 WXR BITE PROCEDURE NO FAULTS NOTED AT THIS TIME. PERFORMED OPS CHECK IAW AMM 34-43-00. OPS CHECK GOOD AT THIS TIME.
"LT ENG STARTER" AND VALVE LIGHT ON START UP OF LEFT ENGINE. REQUIRED MANUAL VALVE OPENING LT ENG START PROCEDURE. REMOVED AND REPLACED START VALVE IAW MM 80-11-01 OPT CK GOOD.
APU FAULT EICAS MESSAGE. PERFORMED FIM TASK 49-11 FT 987 BITE PROCEDURE FAULTED " REVERSE FLOW" ALSO PERFORMED FIM TASK 49-11 FT 994, TS TO COMPRESSOR INLET TEMP SENSOR PN 3876072-1. REMOVED AND REPLACED APU SURGE CONTROL VALVE IAW AMM 49-53-01. OPS CHECK GOOD.
LT FWD FUEL PUMP EICAS MSG DURING DESCENT. FOUND LT FWD GFI RELAY (K188) BOOST PUMP OPEN. ACCOMPLISHED FIM 28-22 FT 831 (RELAY RESET). NO DISCREPANCY FOUND. OPS CHECK GOOD.
ON FINAL APPROACH, RT WING ANTI ICE EICAS. QRH PROCEDURE COMPLIED WITH, EXERCISED RT WING ANTI-ICE VALVE AND TESTED IAW AMM 30-11-00/501. OPS CHECK GOOD.
RADAR SENSITIVITY IN "CALIBRATED" MODE PAINTS UNUSABLE AND WEAK RETURNS AND REQUIRES USE OF MANUAL GAIN ONE UNIT LESS THAN "MAX" FOR RELIABLE DISPLAY. BOTH LT AND RT SYSTEMS. PERFORMED WEATHER RADAR SYSTEM BITE CHECK IAW FIM 34-43 FT 805 NO FAULTS - RADAR OPS OK.
RT ENG IGNITOR 2 STATUS MSG. RESET RT ENG IGNITOR 2 AND PERFORMED OPS CHECK OF ENGINE IGNITION IAW AMM 74-11-00. NO FURTHER DEFECTS NOTED AT THIS TIME.
LT ENG IGNITOR 2 STATUS MSG. RESET LT ENG IGNITOR 2 AND PERFORMED OPS CHECK OF ENGINE IGNITION IAW AMM 74-11-00. NO FURTHER DEFECTS NOTED AT THIS TIME.
EICAS - L AFT FUEL PUMP. R&R PUMP IAW AMM 28-22-03.
RT WING ANTI-ICE MSG CYCLES INTERMITTENTLY. REPLACED WING TAI CONTROL RELAY AS PER FIM TASK 30-11 FT 803. TEST GOOD ON GROUND RELAY K414.
RT WING ANTI-ICE MSG INTERMITTENTLY. ITEM PLACED ON MEL 30-11-02A MDDR 96104 CAT C DUE 15 JUL 18.
RT WING ANTI-ICE VALVE LIGHT INTERMITTENT. MX ACTION VERIFIED RT ANTIICE VALVE OPERATED AS COMMANDED C/W. REMOVED AND REPLACED RT WING THERMAL ANTI ICE VALVE IAW AMM 30-11-02.
WX FAIL ON BOTH HSI WITH WX SYS SELECTED IN R OR L WX SYS REMAINS WX FAIL STATUS MESSAGE ON WX SYS. PERFORMED RADAR BITE PROCEDURE IAW FIM 34-43 FT 805 COULD NOT DUPLICATE SYSTEM TESTED GOOD AT THIS TIME.
APU AUTOSHUTDOWN MESSAGE GEN FILTER. REMOVED AND REPLACED APU GEN FILTER IAW AMM REF 49-27-03 & OPS CHECK NORMAL.
EICAS MSG APU FAULT DURING NR 2 ENGINE START. RESET FAULT STARTED APU NO FAULTS AT THIS TIME IAW AMM 49-00-00.
LEFT AFT FUEL PUMP INTERMITTENT ON GROUND. CYCLED THE PUMP, MESSAGE STILL PRESENT. REPLACED THE PRESSURE SWITCH IAW AMM 28-42-01. OPS CHECKED NORMAL.
AFTER ENGINE START, THE RIGHT FWD FUEL PUMP EICAS MESSAGE DISPLAYED. OPS CHECK OK, IAW AMM 28-22-00.
FIRST OFFICER`S EHSI FLICKERED AND ATTEMPTED TO DISPLAY TERRAIN AND WEATHER MODE AT THE SAME TIME WHEN WX/TER WAS PRESSED, EVEN IF THE MODE IS RELEASE. PERFORMED A FIRST OFFIER`S EHSI FILTER FOR COOLING CHECK AND EQUIPMENT COOLING CHECK IAW AMM 21-58-00, NO DEFECTS NOTED. REMOVED AND REPLACED THE WEATHER RADAR CONTROL PANEL IAW AMM 34-43-02 SYSTEM OPS TEST OK.
SIDE EHSI FLICKERED AND INTERMITTENLY LOST ALL COLOR. GOES BLACK AND WHITE , WHILE IN WEATHER MODE. REMOVED AND REPLACED THE WEATHER RADAR CONTROL PANEL IAW AMM 34-43-02, AND OPS TESTED OK. PERFORMED AN A/C EQUIPMENT COOLING CHECK, FOUND OK IAW AMM 21-58-00.
CENTER RIGHT FUEL PUMP INOPERATIVE. RT CENTER PUMP OPS CHECKED GOOD IAW AMM 28-22-00, ACCOMPLISHED FIM 28-22 FT 812, NO FAULTS NOTED.
LEFT CENTER TANK FUEL PUMP PRESSURE LIGHT ILLUMINATED WITH CTR L FUEL PUMP EICAS MESSEGE IAW DDG 28-22-02A, CAT C. RESET THE LEFT UFI, COMPLIED WITH AP-14062 , ALL POWER CHECKS WERE NORMAL , REPLACED THE RELAY K329 AS A PRECAUTION IAW WDM 20-81-11, LEFT CENTER OVERRIDE PUMP TESTED NORMAL IAW AMM 28-22-00.
DUCT PRESSURE GAUGE BACKGROUND LIGHT INOPERATIVE. REPLACED THE PRESSURE GAUGE IAW AMM 36-21-00.
LEFT CENTER TANK PUMP INOPERATIVE. PERFORMED AN OPERATIONAL TEST AND FOUND THE PUMP TO BE NORMAL IAW AMM 28-12-01.
RIGHT AFT FUEL PUMP AFT RELAY K 189 FAILED. REPLACED THE RELAY IAW AMM 28-22-00.
APU PNEUMATIC DUCT LEAKING AROUND CLAMPS. REMOVED AND REPLACED THE APU PNEUMATIC DUCT CLAMP IAW AMM 49-53-01. OPS CHECKED NORMAL.
CENTER LEFT FUEL PUMP INOPERATIVE. REMOVED AND REPLACED THE FUEL PRESSURE SWITCH IAW AMM 28-42-01. OPS AND LEAK CHECKED NORMAL.
APU FIRE LOOP 1 STATUS MESSAGE. CYCLED POWER AND PERFORMED AFOLT TEST IAW AMM 26-15-00, OPS CHECKED GOOD, NO STATUS MESSAGE.
LEFT CENTER BOOST PUMP INOPERATIVE. REMOVED AND REPLACED THE BOOST PUMP, OPS CHECKED GOOD IAW AMM 28-22-05.
APU SHUT DOWN WHEN APU GENERATOR WAS PUT ON LINE. PERFORMED A BITE CHECK OF APU ECU LAST 2 SHUTDOWNS WERE REVERSE FLOW. PERFORMED FIM 49-11 FT 994 SYSTEM OK, OPERATED APU UNDER ELECTRICAL & PNEUMATIC LOAD IAW AMM 49-11-00, NO FAULTS NOTED, PERFORMED A BITE CHECK IAW FIM 49-11 FT 958, NO FAULTS NOTED.
CENTER FUEL PUMP EICAS.
DURING CREW CHECKLIST, AUTO PRESSURE CONTROLLER LDG ALT JAMMED. REMOVED AND REPLACED CABIN ALT CONTROLLER IAW MM 21-31-01, TESTS OK.
CENTER LT FUEL PUMP EICAS MESSAGE AFTER START. RESET THE FAULT ON UFI CONTROL BOX , OPS TESTED THE FUEL PUMP, CHECKED OK IAW AMM 28-22-05. REMOVED AND REPLACED THE LEFT N2 SPEED CARD IAW AMM 73-21-54. OPS CHECKED GOOD. TRANSFERED THE FUEL FROM CENTER TO WINGS, OPS CHECKED GOOD.
RIGHT A/C PACK INOPERATIVE. REMOVED, CLEANED, REINSTALLED RAM INLET DOOR ACTUATOR,ELECTRICAL CONNECTOR IAW SWPM 20-60-01. BITE CHECKED THE RT PACK TEMP CONTROLLER IAW AMM 21-51-14, NO FAULTS NOTED. OPS CHECKED GOOD.
RIGHT PACK TEMP CAUTION. PERFORMED AN OPS AND BITE CHECKS ON RT PACK TEMP CONTROLLER IAW AMM 21-51-14. NO FAULTS NOTED.
APU INOPERATIVE. REMOVED AND REPLACED THE OIL CAP IAW AMM 49-27-00. SERVICED APU IAW AMM 12-13-04. OPS CHECKED GOOD, LEAK CHECKED GOOD.
STATUS MESSAGE FOR APU OIL QTY AFTER LANDING. REMOVED AND REPLACED THE OIL CAP IAW AMM 49-27-00.
CARGO FIRE LOOP B INOPERATIVE. COMPLIED WITH FIM 26-16 FT 832, NO FAULTS NOTED.
APU SURGE VALVE DUCT TORN. REMOVED AND REPLACED THE DUCT, APU OPS CHECKED GOOD IAW AMM 49-53-01. NO LEAKS DETECTED.
VIBRATION MONITOR FOR THE LEFT LOW PRESSURE TURBINE, MAXED OUT AT 5.0 DURING CLIMB OUT WITH ASSOCIATED ENGINE HUM. DURING CRUISE FLIGHT 4.4 AND VIBRATION INDICATED. DURING DESCENT NOTICEABLE VIBRATION FELT AND HEARD ASSOCIATED WITH LEFT LPT HIGH VIBRATION INDICATION. REMOVED AND REPLACED THE NR 1 ENGINE ASSY IAW E1029.
VIBRATION MONITOR INDICATED BETWEEN 4.6 AND 5.0 LPT AT CRUISE. VIBRATION NOTICABLE ON CLIMBOUT. PERFORMED INLET AND EXHAUST OF LT ENGINE GENERAL INSPECTION IAW AMM 05-51-38 REF TO 938543 M3, A BROKEN COWL ROD CLAMP FOUND.
LEFT ENGINE BLEED OFF MESSAGE, DESCENDING THROUGH 14000 FT. TURNED EAI ON AND PACK OFF. NO REVERSER FOR LEFT ENGINE ON LANDING AND LEFT THRUST REVERSER ISOLATION VALVE STATUS MESSAGE. REMOVED AND REPLACED THE LT ENGINE PRV IAW AMM 36-11-18. OPS CHECKED GOOD.
NR 1 ENGINE VIBRATION DURING FLIGHT. PERFORMED A HEAVY INSPECTION OF INLET , FAN EXHAUST DUCT & LPT, NO DISCREPANCIES NOTED , PERFORMED PIMU BITE CHECK ON THE NR 1 ENGINE VIBRATION BOX, NO FAULTS NOTED IAW FIM 71-05 FT 854. OK FOR SERVICE.
ON LEFT ENGINE START, AN EICAS MESSAGE FOR THE LT ENG BLEED OFF. RETURN TO BLOCKS. REMOVED AND REPLACED THE LEFT ENGINE PRVC IAW AMM 36-11-09, PERFORMED A LEAK CHECK IAW AMM 36-11-09 AND ENGINE RUNS IAW AMM 71-00-00. OPS AND LEAK CHECKED OK.
RT SIDE WINDOW, EICAS MESSAGE.
RIGHT ENGINE HAS A FUEL LEAK AT THE FUEL FLOW TRANSMITTER FEED LINE TO FITTING CAP. TIGHTENED THE CAP ON THE TEE FITTING IAW AMM 73-31-01 , WET MOTORED ENGINE IAW AMM 71-00-00, LEAK CHECKED OK.
RT ENGINE FUEL FILTER STATUS MESSAGE. R & R THE FUEL DIFFERENTIAL PRESSUR SWITCH IAW AMM 73-34-01. PERFORMED DRY MOTORING AND LEAK TEST IAW AMM 71-00. OPS CHECKED GOOD.
DURING CLIMB OUT IN ICING CONDITIONS, AN EICAS MESSAGE FOR THE RT ENGINE FUEL FILTER. RAN QR4 PROCEDURES, RT ENG FUEL FILTER REPLACED IAW AMM 78-11-03. LEAK AND OPS CHECKED GOOD.
WEATHER RADAR DOES NOT PAINT ANY WEATHER AT ANY RANGE. R & R THE WAVE GUIDE SWT, OPS CHECKED NORMAL IAW AMM 34-43-04.
APU AUTO SHUTDOWN.
RIGHT FWD WINDOW HEAT EICAS MESSAGE AND RT FWD WINDOW HEAT INOPERATIVE LIGHT. REMOVED AND REPLACED THE WINDOW HEAT CONTROLLER IAW AMM 30-41-01.
RIGHT FWD WINDOW EICAS AND RT FWD WINDOW INOPERATIVE LIGHT AFTER LANDING. RESET THE SWITCH, PERFORMED A BITE CHECK IAW AMM 30-41-00, NO FAULTS NOTED AT THIS TIME.
LEFT AFT FUEL PUMP FAILED IN FLIGHT , CIRCUIT BREAKER TRIPPED. CLEANED AND CHECKED THECONNECTOR FOR LT AFT BOOST PUMP, RESET THE CIRCUIT BREAKER FOR THE PUMP AND OPS NORMAL FOR SEVERAL HOURS AND PUMPED 35000 LBS FROM TANK TO TANK. OK FOR SERVICE IAW AMM 28-22-00.
RT AFT FUEL PUMP FAILED IN FLIGHT , CIRCUIT BREAKER TRIPPED. REMOVED AND REPLACED THE FUEL PUMP IAW AMM 28-22-05. OPS NORMAL.
R1 WINDOW OUTER PANE SHATTERED, ARCING OBSERVED BRIEFLY PRIOR TO GLASS SHATTERING. REMOVED AND REPLACED THE R1 WINDOW IAW AMM 56-11-01.
AFT SMOKE DETECTOR M718 IN THE AFT CARGO BAY FAILED. REPLACED THE BLOWER SMOKE DETECTOR.
RIGHT ENGINE STATUS MESSAGE, ENG TAI VALVE DOES NOT SHOW DURING RUNUP WHEN ANTI-ICE SWITCH IN ON POSITION. FOUND A WIRE DISCONNECTED W066-56W-24 OF PLUG D5406P. THE WIRE WAS RECONNECTED IAW W/D 30-12-11.
LEFT GENERATOR FAILED TO CONNECT TO THE BUSS DURING RUNUP. FOUND A DISCONNECTED WIRE W412-301Y. THE WIRE WAS CONNECTED.
NR 1 MID PYLON, IN AIR PRESSURE SWITCH PLUG CORRODED. THE PRESSURE SWITCH WAS REPLACED.
RIGHT WING OVERWING FUEL FILLING PORT WING CUTOUT FOUND CORRODED. THE CORROSION WAS REMOVED.
CENTER AUTOPILOT RUDDER SERVO M278 FAIL DURING TEST. THE SERVO WAS REPLACED.
RIGHT AUTOPILOT RUDDER SERVO M279 FAIL DURING TEST. THE SERVO WAS REPLACED.
LEFT ENGINE IDG DISCONNECT LIGHT FAILED TO ILLUMINATE WHEN ENGINE IS NOT RUNNING. IDG REPLACED.
LEFT HPC FAIL DURING AIR SUPPLY BITE TEST. HPC REPLACED.
E/E COOLING SUPPLY FAN DIRTY. THE FAN WAS REPLACED.
LEFT PACK TEMP CONTROLLER M126 FAILED. REPLACED THE TEMP CONTROLLER.
K105 RELAY, AC STANBY POWER AT P6 UNSERVICABLE. REPLACED THE RELAY.
RIGHT GENERATOR FAILED TO CONNECT TO THE BUS DURING RUNUP. FOUND DISCONNECTED WIRE W222-301B-18. WIRE RECONNECTED.
RIGHT WEATHER RADAR WEAK. REMOVED AND REPLACED RIGHT WEATHER RADAR TRANSCEIVER.
NR 2 ENGINE IDLE SPEED HIGH, EICAS MESSAGE IDLE DISAGREE DISPLAYED AND AIRPLANE NOT IN APPROACH IDLE CONFIGURATION. PERFORMED TROUBLESHOOTING IAW FIM 71-05, FAULT TREE 844 AND FOUND EEC DISCRETE CARD.
TEMP PNL M14 FLT DECK TRIM IN DOES NOT RESPOND WHEN SELECTING TEMPERATURE. REPLACED TEMP CONT PNL (M14).