N1327A

Part: SMOKE DETECTOR — DEFECTIVE (ZONE 100) · airframe 97,511 hrs · 16,873 cycles

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.

Part: SUPPORT FITTING — CORRODED (ZONE 300) · airframe 96,781 hrs · 16,602 cycles

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.

Part: SUPPORT FITTING — CORRODED (ZONE 300) · airframe 96,781 hrs · 16,602 cycles

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.

Part: SUPPORT FITTING — CORRODED (ZONE 300) · airframe 96,781 hrs · 16,602 cycles

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.

Part: SUPPORT FITTING — CORRODED (ZONE 300) · airframe 96,781 hrs · 16,602 cycles

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.

Part: SUPPORT FITTING — CORRODED (ZONE 300) · airframe 96,781 hrs · 16,602 cycles

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.

Part: SKIN — DAMAGED (ZONE 200) · airframe 96,781 hrs · 16,602 cycles

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.

Part: PANEL — DAMAGED (ZONE 400) · airframe 96,781 hrs · 16,602 cycles

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.

Part: DOOR FRAME — CORRODED (ZONE 100) · airframe 96,781 hrs · 16,602 cycles

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.

Part: SUPPORT FITTING — CORRODED (ZONE 300) · airframe 96,781 hrs · 16,602 cycles

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.

Part: TCAS SYSTEM — FAULTED · airframe 96,491 hrs · 16,491 cycles

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

Part: AUTOTHROTTLE SYS — WARNING MESSAGE (ZONE 100) · airframe 96,463 hrs · 16,478 cycles

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.

Part: ISOLATION VALVE — FAULTED (ZONE 600) · airframe 95,354 hrs · 16,057 cycles

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 .

Part: PRESSURE SWITCH — FAULTED (HYD SYSTEM) · airframe 95,189 hrs · 15,999 cycles

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 .

Part: TAPE — DAMAGED (ELT) · airframe 94,587 hrs · 15,764 cycles

COCKPIT ELT TAPE DAMAGED. PER MCC REGISTERED WITH NOAA PER ENGINEERING DEPARTMENT IAW AMM 25-63-03. DMI 204893 CLOSED.

Part: SIGN — DETACHED (CABIN) · airframe 94,591 hrs · 15,765 cycles

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>)

Part: ELT — UNKNOWN · airframe 94,587 hrs · 15,763 cycles

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>)

Part: GUARD — UNKNOWN (UNKNOWN) · airframe 94,114 hrs · 15,616 cycles

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>)

Part: FIRST AID KIT — UNKNOWN (UNKNOWN) · airframe 94,047 hrs · 15,593 cycles

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>)

Part: STIFFENER — UNKNOWN (UNKNOWN) · airframe 93,558 hrs · 15,432 cycles

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>)

Part: PCA — UNKNOWN (UNKNOWN) · airframe 93,558 hrs · 15,432 cycles

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 &AMP; 27-31-00-825-060 REV 139 22APR2023.</P> / <P>&NBSP;</P>)

Part: PIPE — UNKNOWN (UNKNOWN) · airframe 93,558 hrs · 15,432 cycles

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 &AMP; 26-11-02-424-033, REV140 22AUG2023.</P> / <P>&NBSP;</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,558 hrs · 15,432 cycles

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 &AMP; 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>)

Part: PCA — UNKNOWN (UNKNOWN) · airframe 93,558 hrs · 15,432 cycles

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 &AMP; 27-31-00-825-060 REV139 22APR2023</P> / <P>&NBSP;</P> / <P>&NBSP;</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,558 hrs · 15,432 cycles

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>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,558 hrs · 15,432 cycles

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>)

Part: HOSE — UNKNOWN (UNKNOWN) · airframe 93,558 hrs · 15,432 cycles

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>)

Part: HOSE — UNKNOWN (UNKNOWN) · airframe 93,558 hrs · 15,432 cycles

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>)

Part: ANGLE — UNKNOWN (UNKNOWN) · airframe 93,558 hrs · 15,432 cycles

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>)

Part: HOSE — UNKNOWN (UNKNOWN) · airframe 93,558 hrs · 15,432 cycles

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>)

Part: HOSE — UNKNOWN (UNKNOWN) · airframe 93,558 hrs · 15,432 cycles

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>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,558 hrs · 15,432 cycles

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>)

Part: ACTUATOR — UNKNOWN (UNKNOWN) · airframe 93,558 hrs · 15,432 cycles

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>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,558 hrs · 15,432 cycles

3 FAA  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>)

Part: PCA — UNKNOWN (UNKNOWN) · airframe 93,558 hrs · 15,432 cycles

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>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,558 hrs · 15,432 cycles

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>)

Part: SHEAR TIE — UNKNOWN (UNKNOWN) · airframe 93,558 hrs · 15,432 cycles

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>)

Part: SAFETY WIRE — UNKNOWN (UNKNOWN) · airframe 93,558 hrs · 15,432 cycles

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>)

Part: SUPPORT BEAM — UNKNOWN (UNKNOWN) · airframe 93,558 hrs · 15,432 cycles

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>)

Part: HOSE — UNKNOWN (UNKNOWN) · airframe 93,558 hrs · 15,432 cycles

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>)

Part: HOSE — UNKNOWN (UNKNOWN) · airframe 93,558 hrs · 15,432 cycles

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>)

Part: COMPUTER — UNKNOWN (ELEVATOR FEEL) · airframe 93,558 hrs · 15,432 cycles

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>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,558 hrs · 15,432 cycles

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>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,558 hrs · 15,432 cycles

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>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,558 hrs · 15,432 cycles

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>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,558 hrs · 15,432 cycles

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>)

Part: BONDING JUMPER — UNKNOWN (UNKNOWN) · airframe 93,558 hrs · 15,432 cycles

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>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,558 hrs · 15,432 cycles

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 &AMP; BAC MSG CMA TLS 23-0146</P>)

Part: O-RING — UNKNOWN (UNKNOWN) · airframe 93,558 hrs · 15,432 cycles

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>)

Part: FIRE LOOP — UNKNOWN (UNKNOWN) · airframe 93,558 hrs · 15,432 cycles

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>)

Part: BATTERY PACK — UNKNOWN (UNKNOWN) · airframe 93,349 hrs · 15,360 cycles

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.

Part: NONE — NONE · airframe 91,769 hrs · 14,827 cycles

OVERHEAD EMERGENCY LIGHT BY L1 DOOR INOP.(<P>RELAMPED LIGHT, OPS CHECKS GOOD IAW AMM 33-51-00</P>)

Part: LIGHT — INOPERATIVE · airframe 91,423 hrs

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>)

Part: LIGHT — INOPERATIVE · airframe 90,802 hrs · 14,511 cycles

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>)

Part: NONE — NONE · airframe 90,635 hrs · 14,461 cycles

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>)

Part: NONE — NONE · airframe 89,911 hrs · 14,228 cycles

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>)

Part: VALVE — NONE · airframe 89,822 hrs

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>)

Part: TRU — NONE · airframe 89,824 hrs

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>)

Part: HPC — NONE

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>)

Part: NONE — NONE

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>)

Part: VALVE — NONE · airframe 89,781 hrs · 14,180 cycles

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>)

Part: GCU — NONE · 14,129 cycles

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>)

Part: ELT — NONE · 14,107 cycles

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>)

Part: NONE — NONE

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>)

Part: CONTROLLER — NONE

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>)

Part: DISPLAY — STICKING · airframe 89,509 hrs · 14,095 cycles

WX RADAR STICKING @ 10 O'CLOCK POSITION. PERFORMED TS PER FIM 34-43- FT 805. OPS CHECK GOOD.</P>)

Part: VALVE — LOCKED

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>)

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI-ICE VALVE) · airframe 89,302 hrs · 14,021 cycles

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>)

Part: STRING — TORN (ELT)

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>)

Part: MODULE — MALFUNCTIONED (RT ENGINE) · airframe 89,081 hrs

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>)

Part: ADC — FAULTED

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.

Part: PUMP — INOPERATIVE (CENTER FUEL) · airframe 89,046 hrs · 13,952 cycles

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>)

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 89,046 hrs

R HPSOV EICAS INFLIGHT TWICE BUT DISAPPEARED BOTH TIMES(<P><SPAN>REACTIVATED HPSOV IAW DDG 36-11-02-02 OPS CHECK GOOD</SPAN></P>)

Part: CONTROLLER — MALFUNCTIONED (RT ENGINE)

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

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 89,041 hrs

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>)

Part: PUMP — INOPERATIVE (LT CNTR FUEL) · airframe 88,986 hrs · 13,938 cycles

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>)

Part: TETHER — UNSECURE (ELT)

ELT STRING/TETHER LOOSE AND UNRAVELING(<P><SPAN>REINSTALLED PORTABLE ELT TETHER PER AMM 25-63-03</SPAN></P>)

Part: WIRE — FAULTED (SHUTOFF VALVE)

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>)

Part: EXCITER — FAULTED (APU)

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>)

Part: SHUTOFF VALVE — MALFUNCTIONED

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>)

Part: WARNING MESSAGE — FALSE ACTIVATION (SHUTOFF VALVE)

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>)

Part: SHUTOFF VALVE — FAULTED (RT ENGINE) · airframe 88,750 hrs · 13,869 cycles

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>)

Part: TRANSMITTER — MALFUNCTIONED (RT OIL PRESSURE) · airframe 88,577 hrs · 13,817 cycles

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>)

Part: RELAY — FAULTED (RT ENGINE) · airframe 88,470 hrs · 13,789 cycles

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 &AMP; RT ENG TAI RELAY K785, K786 IAW SWPM 20-81-22. AS PER ACTION PLAN AP-19951. NO OTHER DEFECTS NOTED.

Part: ENGINE — UNKNOWN (LEFT) · airframe 88,271 hrs · 13,728 cycles

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.

Part: RADAR — MALFUNCTIONED (WX SYSTEM) · airframe 88,240 hrs

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>)

Part: WARNING MESSAGE — FALSE ACTIVATION (NR 2 IGNITER) · airframe 88,214 hrs · 13,709 cycles

"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>)

Part: ENGINE — UNKNOWN (NR 1) · airframe 88,214 hrs · 13,709 cycles

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>)

Part: SWITCH — INOPERATIVE (CARGO BAY) · airframe 88,093 hrs · 13,669 cycles

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>)

Part: PITOT TUBE — MALFUNCTIONED (CAPTAIN'S) · airframe 87,858 hrs · 13,597 cycles

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>)

Part: DETECTOR — FAULT MESSAGE (AFT CARGO BAY) · airframe 87,806 hrs · 13,577 cycles

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.

Part: CIRCUIT BREAKER — POPPED (LT SPAR FUEL VAL) · airframe 87,803 hrs · 13,576 cycles

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.

Part: DRIVE UNIT — MALFUNCTIONED (WX RADAR ANTENNA) · airframe 87,756 hrs · 13,564 cycles

WXR SYSTEM STATUS MESSAGE RIGHT SIDE INTERMITTENT. NO FAULTS NOTED. REMOVED AND REPLACED WXR ANTENNA DRIVE UNIT, IAW AMM 34-43-00. MCC NOTIFIED.

Part: TRANSCEIVER — FAILED (WX RADAR) · airframe 87,740 hrs · 13,561 cycles

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.

Part: CONTROL UNIT — MALFUNCTIONED (WINDSHEILD HEAT) · airframe 87,740 hrs · 13,561 cycles

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.

Part: WINDOW — ARCED (RT FWD WINDOW) · airframe 87,740 hrs · 13,561 cycles

RT FWD WINDOW ELECTRICAL ARC W/DELAMINATION. REMOVED AND REPLACED RT FWD NR 1 WINDOW, IAW B767 AMM 56-11-01. OPERATIONS CHECK GOOD.

Part: WIRE — CUT (SPAR VALVE) · airframe 87,668 hrs · 13,543 cycles

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.

Part: FAN — SEIZED (EQUIP EXHAUST) · airframe 87,657 hrs · 13,539 cycles

FWD EQUIPMENT EXHAUST FAN STATUS MESSAGE. FOUND EXHAUST FAN BLADE SEIZED. REMOVED AND REPLACED FAN, IAW AMM 21-58-06. OPERATIONS NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (WX RADAR SYS) · airframe 87,631 hrs · 13,532 cycles

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.

Part: RADAR — UNKNOWN (WX SYSTEM) · airframe 87,545 hrs · 13,503 cycles

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.

Part: TRANSCEIVER — FAILED (RT WX RADAR) · airframe 87,490 hrs · 13,486 cycles

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.

Part: STATUS MESSAGE — FALSE ACTIVATION (WX RADAR SYS) · airframe 87,465 hrs · 13,479 cycles

STATUS MESSAGE WXR SYSTEM. T/S IAW FIM 34-43 FAULT TREE 805. SYSTEM TEST GOOD, MESSAGE CLEARED.

Part: WARNING MESSAGE — FALSE ACTIVATION (WX RADAR SYS) · airframe 87,450 hrs · 13,474 cycles

"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.

Part: FAN — FAILED (GALLEY) · airframe 87,410 hrs · 13,462 cycles

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.

Part: RADAR — MALFUNCTIONED (RT WX SYSTEM) · airframe 87,349 hrs · 13,445 cycles

RT WX RADAR FAIL. PERFORMED OPERATIONS CHECK OF RT WX RADAR. OPERATIONS CHECK GOOD, PER B767 AMM 34-43-00.

Part: BRACKET — BROKEN (FLASHLIGHT) · airframe 86,992 hrs · 13,325 cycles

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.

Part: SWITCH — FAILED (RT ENG OIL) · airframe 86,891 hrs · 13,298 cycles

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.

Part: STATUS MESSAGE — FALSE INDICATION (NR 1 FIRE LOOP) · airframe 86,855 hrs · 13,287 cycles

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.

Part: CONTROL UNIT — MALFUNCTIONED (WINDOW HEAT) · airframe 86,689 hrs · 13,237 cycles

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>)

Part: SWITCH — FAILED (FIRE DETECTION) · airframe 86,689 hrs · 13,237 cycles

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 &AMP;4. R/R KORRY SWITCH IAW SWPM 20-84-00. OPS GOOD, NO DEFECTS NOTED. LAMP P/N 387</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (WX RADAR SYS) · airframe 86,673 hrs · 13,233 cycles

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>)

Part: HEATER — MALFUNCTIONED (WINDOW HEAT) · airframe 86,678 hrs · 13,234 cycles

RIGHT SIDE WINDOW HEAT INOP. CYCLED CIRCUIT BREAKER. OPS NORMAL AT THIS TIME IAW AMM 30-41-00.</P>)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 86,684 hrs · 13,236 cycles

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>)

Part: ANTI-ICE VALVE — FAILED (RT ENGINE) · airframe 86,663 hrs · 13,231 cycles

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

Part: KEELBEAM — CORRODED (BS 960) · airframe 86,656 hrs · 13,227 cycles

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

Part: SPAR — CORRODED (RT WING TE FLAP) · airframe 86,656 hrs · 13,227 cycles

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

Part: WARNING MESSAGE — FALSE ACTIVATION (WINDOW HEAT) · airframe 86,638 hrs · 13,221 cycles

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

Part: BLEED VALVE — UNKNOWN (APU) · airframe 86,608 hrs · 13,210 cycles

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.

Part: TRANSCEIVER — MALFUNCTIONED (WEATHER RADAR) · airframe 86,499 hrs · 13,173 cycles

LEFT WEATHER RADAR SPIKING IN CRUISE. REMOVED AND REPLACED WEATHER RADAR TRANSCEIVER IAW AMM 34-43-01, OPS CHECKED GOOD.

Part: STATUS MESSAGE — FALSE ACTIVATION (WX RADAR SYS) · airframe 86,326 hrs · 13,114 cycles

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.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 86,317 hrs · 13,111 cycles

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.

Part: PRIORITY VALVE — MALFUNCTIONED (RT ENGINE) · airframe 86,217 hrs · 13,080 cycles

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

Part: ELT — UNSERVICEABLE (NR 2) · airframe 86,102 hrs · 13,044 cycles

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>)

Part: SMOKE DETECTOR — FALSE ACTIVATION (MAIN DECK) · airframe 86,031 hrs · 13,017 cycles

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>)

Part: ANTENNA — PULLED (ELT) · airframe 86,033 hrs · 13,018 cycles

ELT ANTENNA IS PULLED OUT AND MAY BE BENT.(<P>RESECURED ELT IAW AMM 25-63-03.</P>)

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 86,006 hrs · 13,009 cycles

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>)

Part: SWITCH — FAULTY (FUEL SYSTEM) · airframe 86,004 hrs · 13,008 cycles

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>)

Part: FUEL FILTER — FAULTY (LT ENGINE) · airframe 85,954 hrs · 12,987 cycles

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>)

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 85,861 hrs · 12,955 cycles

RADAR SPIKES ON THE RH SYSTEM(<P>PERFORMED WEATHER RADAR SYSTEM OPERATIONAL TEST. NO FAULTS NOTED AT THIS TIME. LH &AMP; RH SYSTEM OPS CHECK GOOD AT THIS TIME IAW AMM 34-43-00.</P>)

Part: ANTI-ICE VALVE — MALFUNCTIONED (RT ENGINE) · airframe 85,745 hrs · 12,918 cycles

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>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 85,737 hrs · 12,916 cycles

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>)

Part: WARNING LIGHT — FALSE ACTIVATION (COCKPIT) · airframe 85,714 hrs · 12,909 cycles

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>)

Part: CONTROL PANEL — INOPERATIVE (RT GENERATOR) · airframe 85,552 hrs · 12,851 cycles

R GENERATOR DISCONNECT LIGHT INOP(<P>REMOVED AND REPLACED ELECTRICAL PANEL IAW B767-300 AMM 24-22-01. OPS CHECKED GOOD.</P>)

Part: IGNITER — INOPERATIVE (LT ENGINE) · airframe 85,480 hrs · 12,827 cycles

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>)

Part: CONTROL VALVE — FAULTED (RT A/C PACK) · airframe 85,479 hrs · 12,826 cycles

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>)

Part: ENGINE — UNKNOWN (NR 1) · airframe 85,473 hrs · 12,825 cycles

#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>)

Part: PIMU — FAILED (LEFT) · airframe 85,480 hrs · 12,827 cycles

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>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT A/C PACK) · airframe 85,456 hrs · 12,819 cycles

RIGHT PACK OVER TEMP / RAN QRH.(<P>PERFORMED RIGHT TEMPERATURE CONTROLLER BITE TEST IAW FIM TASK 21-51 FAULT TREE 803, TEST PASS.</P>)

Part: EXCITER — MALFUNCTIONED (LT NR 1) · airframe 85,450 hrs · 12,817 cycles

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>)

Part: WARNING LIGHT — FALSE ACTIVATION (RT ENG ANTI-ICE) · airframe 85,462 hrs · 12,822 cycles

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>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT A/C PACK) · airframe 85,356 hrs · 12,782 cycles

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.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 85,332 hrs · 12,771 cycles

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.

Part: FUEL FILTER — FAULTED (RT ENGINE) · airframe 85,270 hrs · 12,746 cycles

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>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 85,251 hrs · 12,740 cycles

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>)

Part: RELAY — FAILED (CABIN TEMP) · airframe 85,251 hrs · 12,740 cycles

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>)

Part: PRESSURE SWITCH — FAULTY (RT ENGINE) · airframe 85,240 hrs · 12,737 cycles

R ENGINE OIL PRESSURE LIGHT NOT ILLUMINATED(<P>REMOVED AND REPLACED OIL PRESSURE SWITCH IAW AMM 79-32-00. OPS CHK&NBSP; GOOD.</P>)

Part: MODULATING VALVE — MALFUNCTIONED (CABIN TEMP) · airframe 85,233 hrs · 12,734 cycles

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.

Part: MODULATING VALVE — FAULTY (CABIN TEMP) · airframe 85,218 hrs · 12,730 cycles

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>)

Part: WARNING LIGHT — FALSE ACTIVATION (ENG OIL PRESSURE) · airframe 85,192 hrs · 12,723 cycles

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.

Part: RELAY — FAILED (FUEL PUMP) · airframe 85,108 hrs · 12,691 cycles

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>)

Part: SENSOR — MALFUNCTIONED (CABIN TEMP) · airframe 85,087 hrs · 12,685 cycles

AFT CABIN ZONE TEMP INOP, LIGHT ILLUMINATES INTERMITTENTLY. REMOVED AND REPLACED CABIN AIR SENSOR IAW AMM 21-61-01. OPS CHECKED GOOD.

Part: RELAY — FAILED (FUEL PUMP) · airframe 85,073 hrs · 12,682 cycles

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.

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN TEMP) · airframe 85,066 hrs · 12,680 cycles

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>)

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN TEMP) · airframe 85,048 hrs · 12,674 cycles

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>)

Part: VALVE — MALFUNCTIONED (AIR TRIM) · airframe 85,051 hrs · 12,675 cycles

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>)

Part: SEAL — MISSING · airframe 84,981 hrs · 12,652 cycles

EXTRA FIRST AID KIT HAS SEAL MISSING.(<P>RE-SEALED EXTRA FIRST AID KIT IAW GMM 3-28-1.<BR /></P>)

Part: SEAL — BROKEN (FIRST AID KIT) · airframe 84,919 hrs · 12,630 cycles

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>)

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 84,856 hrs · 12,607 cycles

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 &AMP; 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>)

Part: SHUTOFF VALVE — MALFUNCTIONED (FWD E/E BAY) · airframe 84,803 hrs · 12,589 cycles

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.

Part: SEAL — BROKEN (FLASHLIGHT) · airframe 84,801 hrs · 12,588 cycles

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>)

Part: STARTER — INOPERATIVE (LT ENGINE) · airframe 84,699 hrs · 12,548 cycles

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 &AMP; 2 IGNITION, AND A &AMP; B EEC CHANNELS PER AMM 71-00-00. OPS CHECK GOOD WITH NORMAL PARAMETERS.&NBSP;</P>)

Part: VALVE — FAILED (MANIFOLD) · airframe 84,699 hrs · 12,548 cycles

"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>)

Part: MODULATING VALVE — MALFUNCTIONED (TRIM AIR) · airframe 84,691 hrs · 12,545 cycles

"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>)

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 84,684 hrs · 12,543 cycles

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.

Part: RADAR — MALFUNCTIONED (WX SYSTEM) · airframe 84,684 hrs · 12,543 cycles

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.

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PUMP) · airframe 84,558 hrs · 12,502 cycles

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.

Part: SHUTOFF VALVE — MALFUNCTIONED (E/E BAY) · airframe 84,541 hrs · 12,495 cycles

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.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 84,526 hrs · 12,489 cycles

"ENG VALVE" DISCRETE LIGHT ILLUMINATED BRIEFLY ON DESCENT.&NBSP;(<P>PERFORMED OPS CHECK OF L &AMP; R ENG VALVE IAW AMM 71-00-00, TEST 4. OPS CHECK GOOD AT THIS TIME.&NBSP;</P>)

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 84,459 hrs · 12,467 cycles

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.

Part: LINE — LOOSE (OXYGEN SYS) · airframe 84,398 hrs · 12,447 cycles

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.

Part: UNKNOWN — MALFUNCTIONED (WINDOW HEAT) · airframe 84,293 hrs · 12,417 cycles

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.

Part: CONTROL PANEL — MALFUNCTIONED (FUEL SYSTEM) · airframe 84,290 hrs · 12,416 cycles

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.

Part: PIN — DAMAGED (WX RADAR) · airframe 84,236 hrs · 12,396 cycles

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.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 84,077 hrs · 12,335 cycles

STATUS AFT EQ EXH FAN 2. (<P>PERFORMED FIM 21-26 FT 808 BLOCKS 1, 40. FAULT CLEARED, OK FOR SERVICE.</P>)

Part: VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 84,069 hrs · 12,331 cycles

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>)

Part: BOSS — CRACKED (APU) · airframe 84,073 hrs · 12,333 cycles

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>)

Part: CONTROL PANEL — MALFUNCTIONED (ANTI-ICE SYS) · airframe 83,926 hrs · 12,285 cycles

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>)

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY) · airframe 83,898 hrs · 12,276 cycles

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>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 83,898 hrs · 12,276 cycles

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>)

Part: INDICATOR — NO TEST (STANDBY) · airframe 83,838 hrs · 12,255 cycles

STANDBY ENG INDICATOR WILL NOT PERFORM BITE FUNCTION. REMOVED AND REPLACED THE STANDBY ENG INDICATOR IAW AMM 77-41-01, OPERATIONAL TESTED NORMAL.

Part: IGNITER — INOPERATIVE (LT ENGINE) · airframe 83,780 hrs · 12,237 cycles

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>)

Part: PUMP — FAILED (AFT FUEL BOOST) · airframe 83,672 hrs · 12,202 cycles

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.

Part: PRESSURE SWITCH — FAULTY (APU) · airframe 83,630 hrs · 12,192 cycles

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>)

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 83,596 hrs · 12,179 cycles

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>)

Part: PLUG — WORN (RT ENGINE) · airframe 83,573 hrs · 12,169 cycles

RIGHT ENGINE B3-1 BORESCOPE PLUG WORN. (<P>REMOVED AND REPLACED RT ENG B3-1 BORESCOPE PLUG PER AMM 72-00-00.</P>)

Part: RELAY — FAILED (FUEL SYSTEM) · airframe 83,573 hrs · 12,169 cycles

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>)

Part: UNKNOWN — MALFUNCTIONED (O2 SSYTEM) · airframe 83,573 hrs · 12,169 cycles

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>)

Part: VALVE — MALFUNCTIONED (CABN TEMP) · airframe 83,543 hrs · 12,158 cycles

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>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 83,507 hrs · 12,145 cycles

STATUS MSG R ENG SPEED CARD.(<P>PERFORMED CARD TEST IAW FIM 73-21 F/T 871 MSG CLEARED SYSTEM TEST OK.</P>)

Part: PRESSURE SENSOR — MALFUNCTIONED (APU) · airframe 83,454 hrs · 12,126 cycles

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 &AMP; 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 &AMP; 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 &AMP; 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 &AMP; REPLACED INLET PRESSURE (P2) SENSOR IAW AMM 49-61-04. OPS CHK GOOD. THIS CLEARS DMI # 110915. MCC NOTIFIED &AMP; PLACARDS REMOVED.</P>)

Part: SENSOR — DIRTY (NR 2 ENGINE) · airframe 83,457 hrs · 12,127 cycles

R PIMU EICAS MESSAGE(<P>REMOVED, CLEANED, AND REINSTALLED NR 2 ENGINE T-12 SENSOR IAW AMM 73-21-06.<BR /></P>)

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 83,446 hrs · 12,123 cycles

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>)

Part: APU — MALFUNCTIONED · airframe 83,402 hrs · 12,110 cycles

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>)

Part: ECU — TRIPPED (APU) · airframe 83,430 hrs · 12,119 cycles

AFTER POWER TRANSFER FROM GPU TO AIRCRAFT POWER, APU SHUT DOWN.(<P>RESET ECU FOR APU AMM 49-11-00. OPS CHECK GOOD.</P>)

Part: DISPLAY — ABNORMAL (WX RADAR SYS) · airframe 83,235 hrs · 12,056 cycles

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.

Part: PUMP — WARNING MESSAGE (FUEL BOOST) · airframe 83,217 hrs · 12,051 cycles

LEFT FWD FUEL PUMP EICAS. REMOVED AND REPLACED FUEL BOOST PUMP IAW AMM 28-22-03-404- OPS CHECK AND LEAK CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (APU) · airframe 83,215 hrs · 12,050 cycles

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>)

Part: STARTER — MALFUNCTIONED (APU) · airframe 83,199 hrs · 12,046 cycles

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>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 83,187 hrs · 12,043 cycles

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>)

Part: CONNECTOR — DIRTY (ANTI-ICE SYSTEM) · airframe 83,174 hrs · 12,039 cycles

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>)

Part: UNKNOWN — MALFUNCTIONED (ANTI-ICE SYSTEM) · airframe 83,154 hrs · 12,034 cycles

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>)

Part: UNKNOWN — MALFUNCTIONED (AC BAY) · airframe 83,071 hrs · 12,006 cycles

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>)

Part: SWITCH — FAULTY (ANTI-ICE SYS) · airframe 83,030 hrs · 11,993 cycles

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>)

Part: CIRCUIT BREAKER — TRIPPED (FUEL PUMP) · airframe 82,990 hrs · 11,983 cycles

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>)

Part: CONNECTOR — DIRTY (ANTI-ICE VALVE) · airframe 82,990 hrs · 11,983 cycles

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.

Part: CONNECTOR — DIRTY (FUEL PUMP) · airframe 82,990 hrs · 11,983 cycles

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.

Part: SYMBOL GENERATOR — MALFUNCTIONED (WEATHER RADAR) · airframe 82,975 hrs · 11,977 cycles

WXR DSPY FAULT ILLUMINATED, ON THE FIRST OFFICER`S HISTORY WHEN WEATHER RADAR POWER WAS SELECTED. TROUBLESHOT TO THE RT EFIS SYMBOL GENERATOR.

Part: WIRE — CROSSED · airframe 82,975 hrs · 11,977 cycles

"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>)

Part: BLADE — NICKED (NR 1 ENGINE FAN) · airframe 82,979 hrs · 11,978 cycles

#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>)

Part: SHUTOFF VALVE — INOPERATIVE (LT ENGINE BLEED) · airframe 82,981 hrs · 11,979 cycles

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>)

Part: SHUTOFF VALVE — FAILED (RT ENGINE) · airframe 82,981 hrs · 11,979 cycles

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>)

Part: BLADE — NICKED (NR 2 ENGINE FAN) · airframe 82,979 hrs · 11,978 cycles

#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>)

Part: SEAL — TORN (BLADE DOVETAIL) · airframe 82,979 hrs · 11,978 cycles

#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>)

Part: CONNECTOR — LOOSE (BOOST PUMP) · airframe 82,979 hrs · 11,978 cycles

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>)

Part: BLADE — NICKED (NR 1 ENGINE FAN) · airframe 82,979 hrs · 11,978 cycles

#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>)

Part: SMOKE WARNING — FALSE INDICATION (CARGO BAY) · airframe 82,981 hrs · 11,979 cycles

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>)

Part: CASE — STAINED (NR 1 ENGINE FAN) · airframe 82,981 hrs · 11,979 cycles

#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>)

Part: CONNECTOR — LOOSE (JETTISON VALVE) · airframe 82,979 hrs · 11,978 cycles

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>)

Part: SKIN — CRACKED (NR 2 NACELLE) · airframe 82,981 hrs · 11,979 cycles

#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>)

Part: SHUTOFF VALVE — DAMAGED (HEAT EXCHANGER) · airframe 82,979 hrs · 11,978 cycles

#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>)

Part: PLENUM — TORN (RT A/C PACK) · airframe 82,981 hrs · 11,979 cycles

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>)

Part: SPINNER — WORN (NR 1 ENGINE) · airframe 82,979 hrs · 11,978 cycles

#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>)

Part: BLADE — NICKED (NR 1 ENGINE FAN) · airframe 82,981 hrs · 11,979 cycles

#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>)

Part: WIRE — OUT OF POSITION (APU BLEED VALVE) · airframe 82,979 hrs · 11,978 cycles

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>)

Part: EXHAUST VALVE — FAULTY (E&E BAY) · airframe 82,894 hrs · 11,949 cycles

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>)

Part: BLOWER — MALFUNCTIONED (CARGO BAY) · airframe 82,890 hrs · 11,948 cycles

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>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 82,743 hrs · 11,893 cycles

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.

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 82,743 hrs · 11,893 cycles

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.

Part: UNKNOWN — MALFUNCTIONED (EXTERNAL POWER) · airframe 82,628 hrs · 11,852 cycles

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.

Part: CIRCUIT BREAKER — TRIPPED (COCKPIT) · airframe 82,628 hrs · 11,852 cycles

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.

Part: SMOKE DETECTOR — FAULTY (MAIN CARGO BAY) · airframe 82,631 hrs · 11,853 cycles

MAIN CARGO DECK FIRE DETECTOR NR 3 AMBER INDICATION ON PREFLIGHT. REPLACED CARGO DECK SMOKE DETECTOR IAW 26-14-01.

Part: SWITCH — FAULTY (FIRE DETECTION) · airframe 82,642 hrs · 11,856 cycles

WHEEL WELL FIRE DETECTION SYSTEM INOP. REPLACED WW SWITCH IAW AMM 33-13-00.

Part: TRU — INOPERATIVE (APU) · airframe 82,642 hrs · 11,856 cycles

APU TRU INOP. REPLACED TRU IAW AMM 24-32-04 OPS CHECKS GOOD.

Part: RADAR — MALFUNCTIONED (WX SYSTEM) · airframe 82,598 hrs · 11,842 cycles

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>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 82,642 hrs · 11,856 cycles

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.

Part: RADAR — MALFUNCTIONED · airframe 82,579 hrs · 11,835 cycles

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>)

Part: WARNING LIGHT — FALSE ACTIVATION (ANTI-ICE VALVE) · airframe 82,538 hrs · 11,819 cycles

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>)

Part: APU — SHUTDOWN · airframe 82,509 hrs · 11,810 cycles

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.

Part: LIGHT — MALFUNCTIONED (ANTI-ICE SYSTEM) · airframe 82,509 hrs · 11,810 cycles

RIGHT ENGINE ANTI-ICE VALVE INDICATION LIGHT INOP. COULD NOT DUPLICATE ON GROUND, RAN ENG 5 MINUTES IAW 30-00-00/901, OPS NML.

Part: BUTTON — INTERMITTENT (COCKPIT) · airframe 82,393 hrs · 11,770 cycles

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.

Part: OXYGEN MASK — INOPERATIVE (COCKPIT) · airframe 82,377 hrs · 11,764 cycles

CAPT QTY MASK WONT TEST. R&R CAPT OXY MASK IAW AMM 35-11-51. OPS GOOD.

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 82,288 hrs · 11,727 cycles

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.

Part: NOT REPORTED — MALFUNCTIONED (COCKPIT) · airframe 82,103 hrs · 11,661 cycles

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.

Part: START VALVE — FAULTY (LT ENGINE) · airframe 82,070 hrs · 11,651 cycles

"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.

Part: CONTROL VALVE — MALFUNCTIONED (APU) · airframe 81,934 hrs · 11,598 cycles

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.

Part: RELAY — MALFUNCTIONED (FUEL SYSTEM) · airframe 81,851 hrs · 11,566 cycles

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.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 81,851 hrs · 11,566 cycles

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.

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 81,766 hrs · 11,536 cycles

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.

Part: IGNITER — MALFUNCTIONED (RT ENGINE) · airframe 81,734 hrs · 11,523 cycles

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.

Part: IGNITER — MALFUNCTIONED (LT ENGINE) · airframe 81,734 hrs · 11,523 cycles

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.

Part: PUMP — FAILED (FUEL SYSTEM) · airframe 81,708 hrs · 11,514 cycles

EICAS - L AFT FUEL PUMP. R&R PUMP IAW AMM 28-22-03.

Part: WARNING MESSAGE — INTERMITTENT (COCKPIT) · airframe 81,708 hrs · 11,514 cycles

RT WING ANTI-ICE MSG INTERMITTENTLY. ITEM PLACED ON MEL 30-11-02A MDDR 96104 CAT C DUE 15 JUL 18.

Part: RELAY — FAULTY (ANIT-ICE SYS) · airframe 81,708 hrs · 11,514 cycles

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.

Part: ANTI-ICE VALVE — DEFECTIVE (RT WING) · airframe 81,700 hrs · 11,512 cycles

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.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 81,666 hrs · 11,497 cycles

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.

Part: FILTER — NOT REPORTED (APU) · airframe 81,589 hrs · 11,472 cycles

APU AUTOSHUTDOWN MESSAGE GEN FILTER. REMOVED AND REPLACED APU GEN FILTER IAW AMM REF 49-27-03 & OPS CHECK NORMAL.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 81,555 hrs · 11,459 cycles

EICAS MSG APU FAULT DURING NR 2 ENGINE START. RESET FAULT STARTED APU NO FAULTS AT THIS TIME IAW AMM 49-00-00.

Part: PRESSURE SWITCH — INTERMITTENT (FUEL PUMP) · airframe 81,492 hrs · 11,435 cycles

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.

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PUMP) · airframe 81,492 hrs · 11,435 cycles

AFTER ENGINE START, THE RIGHT FWD FUEL PUMP EICAS MESSAGE DISPLAYED. OPS CHECK OK, IAW AMM 28-22-00.

Part: CONTROL PANEL — MALFUNCTIONED (WX RADAR SYSTEM) · airframe 81,449 hrs · 11,421 cycles

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.

Part: CONTROL PANEL — INTERMITTENT (WX RADAR SYSTEM) · airframe 81,449 hrs · 11,421 cycles

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.

Part: PUMP — MALFUNCTIONED (CENTER FUEL CELL) · airframe 81,398 hrs · 11,402 cycles

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.

Part: WARNING LIGHT — ILLUMINATED (FUEL PUMP) · airframe 81,266 hrs · 11,357 cycles

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.

Part: LIGHT — INOPERATIVE (GAUGE) · airframe 81,226 hrs · 11,340 cycles

DUCT PRESSURE GAUGE BACKGROUND LIGHT INOPERATIVE. REPLACED THE PRESSURE GAUGE IAW AMM 36-21-00.

Part: PUMP — MALFUNCTIONED (FUEL BOOST) · airframe 81,207 hrs · 11,335 cycles

LEFT CENTER TANK PUMP INOPERATIVE. PERFORMED AN OPERATIONAL TEST AND FOUND THE PUMP TO BE NORMAL IAW AMM 28-12-01.

Part: RELAY — FAILED (FUEL PUMP) · airframe 76,591 hrs · 15,977 cycles

RIGHT AFT FUEL PUMP AFT RELAY K 189 FAILED. REPLACED THE RELAY IAW AMM 28-22-00.

Part: CLAMP — DAMAGED (APU DUCT) · airframe 81,215 hrs · 11,337 cycles

APU PNEUMATIC DUCT LEAKING AROUND CLAMPS. REMOVED AND REPLACED THE APU PNEUMATIC DUCT CLAMP IAW AMM 49-53-01. OPS CHECKED NORMAL.

Part: PRESSURE SWITCH — FAILED (CENTER LEFT) · airframe 80,922 hrs · 11,225 cycles

CENTER LEFT FUEL PUMP INOPERATIVE. REMOVED AND REPLACED THE FUEL PRESSURE SWITCH IAW AMM 28-42-01. OPS AND LEAK CHECKED NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (APU FIRE LOOP) · airframe 80,855 hrs · 11,199 cycles

APU FIRE LOOP 1 STATUS MESSAGE. CYCLED POWER AND PERFORMED AFOLT TEST IAW AMM 26-15-00, OPS CHECKED GOOD, NO STATUS MESSAGE.

Part: PUMP — INOPERATIVE (FUEL BOOST) · airframe 80,827 hrs · 11,188 cycles

LEFT CENTER BOOST PUMP INOPERATIVE. REMOVED AND REPLACED THE BOOST PUMP, OPS CHECKED GOOD IAW AMM 28-22-05.

Part: APU — SHUTDOWN · airframe 80,796 hrs · 11,177 cycles

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.

Part: WARNING MESSAGE — ILLUMINATED (FUEL PUMP) · airframe 80,779 hrs · 11,171 cycles

CENTER FUEL PUMP EICAS.

Part: CONTROLLER — BINDING (AUTO PRESSURE) · airframe 80,695 hrs · 11,140 cycles

DURING CREW CHECKLIST, AUTO PRESSURE CONTROLLER LDG ALT JAMMED. REMOVED AND REPLACED CABIN ALT CONTROLLER IAW MM 21-31-01, TESTS OK.

Part: CIRCUIT CARD — FAILED (NR 2 N2 SPEED) · airframe 80,694 hrs · 11,139 cycles

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.

Part: CONNECTOR — DIRTY (RT A/C PACK) · airframe 80,668 hrs · 11,129 cycles

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.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT A/C PACK) · airframe 80,662 hrs · 11,127 cycles

RIGHT PACK TEMP CAUTION. PERFORMED AN OPS AND BITE CHECKS ON RT PACK TEMP CONTROLLER IAW AMM 21-51-14. NO FAULTS NOTED.

Part: OIL CAP — DAMAGED (APU) · airframe 80,634 hrs · 11,115 cycles

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.

Part: CAP — LEAKING (APU OIL) · airframe 80,617 hrs · 1,107 cycles

STATUS MESSAGE FOR APU OIL QTY AFTER LANDING. REMOVED AND REPLACED THE OIL CAP IAW AMM 49-27-00.

Part: DUCT — TORN (APU SURGE VALVE) · airframe 80,608 hrs · 11,102 cycles

APU SURGE VALVE DUCT TORN. REMOVED AND REPLACED THE DUCT, APU OPS CHECKED GOOD IAW AMM 49-53-01. NO LEAKS DETECTED.

Part: FIRE LOOP — MALFUNCTIONED (CARGO BAY) · airframe 80,617 hrs · 11,106 cycles

CARGO FIRE LOOP B INOPERATIVE. COMPLIED WITH FIM 26-16 FT 832, NO FAULTS NOTED.

Part: ENGINE — VIBRATION (NR 1) · airframe 80,612 hrs · 11,104 cycles

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.

Part: CLAMP — BROKEN (NACELLE) · airframe 80,608 hrs · 11,102 cycles

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.

Part: VALVE — FAILED (THRUST REVERSER) · airframe 80,606 hrs · 11,101 cycles

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.

Part: UNKNOWN — VIBRATION (NR 1 ENGINE) · airframe 80,593 hrs · 11,094 cycles

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.

Part: CONTROLLER — FAILED (LT ENGINE) · airframe 80,600 hrs · 11,097 cycles

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.

Part: WARNING MESSAGE — ILLUMINATED (RT WINDOW) · airframe 80,557 hrs · 11,075 cycles

RT SIDE WINDOW, EICAS MESSAGE.

Part: TEE FITTING — LEAKING (FUEL SYSTEM) · airframe 80,521 hrs · 11,058 cycles

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.

Part: PRESSURE SWITCH — MALFUNCTIONED (RT FUEL FILTER) · airframe 80,441 hrs · 11,019 cycles

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.

Part: FILTER — WARNING MESSAGE (FUEL SYSTEM) · airframe 80,339 hrs · 10,967 cycles

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.

Part: WAVE GUIDE — MALFUNCTIONED (WX RADAR) · airframe 80,303 hrs · 10,949 cycles

WEATHER RADAR DOES NOT PAINT ANY WEATHER AT ANY RANGE. R & R THE WAVE GUIDE SWT, OPS CHECKED NORMAL IAW AMM 34-43-04.

Part: APU — SHUTDOWN · airframe 80,278 hrs · 10,938 cycles

APU AUTO SHUTDOWN.

Part: CONTROLLER — MALFUNCTIONED (WINDOW HEAT) · airframe 80,179 hrs · 10,898 cycles

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.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 80,122 hrs · 10,877 cycles

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.

Part: PUMP — FAILED (FUEL BOOST) · airframe 80,094 hrs · 10,868 cycles

RT AFT FUEL PUMP FAILED IN FLIGHT , CIRCUIT BREAKER TRIPPED. REMOVED AND REPLACED THE FUEL PUMP IAW AMM 28-22-05. OPS NORMAL.

Part: CIRCUIT BREAKER — TRIPPED (FUEL PUMP) · airframe 80,094 hrs · 10,868 cycles

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.

Part: WINDOW — FAILED (R1) · airframe 80,094 hrs · 10,868 cycles

R1 WINDOW OUTER PANE SHATTERED, ARCING OBSERVED BRIEFLY PRIOR TO GLASS SHATTERING. REMOVED AND REPLACED THE R1 WINDOW IAW AMM 56-11-01.

Part: WIRE — DISCONNECTED (LT GENERATOR) · airframe 80,088 hrs · 10,867 cycles

LEFT GENERATOR FAILED TO CONNECT TO THE BUSS DURING RUNUP. FOUND A DISCONNECTED WIRE W412-301Y. THE WIRE WAS CONNECTED.

Part: COMPRESSOR — NO TEST (LEFT) · airframe 80,088 hrs · 10,867 cycles

LEFT HPC FAIL DURING AIR SUPPLY BITE TEST. HPC REPLACED.

Part: TRANSCEIVER — WEAK (WEATHER RADAR) · airframe 80,088 hrs · 10,867 cycles

RIGHT WEATHER RADAR WEAK. REMOVED AND REPLACED RIGHT WEATHER RADAR TRANSCEIVER.

Part: CONTROLLER — FAILED (LT A/C PACK) · airframe 80,088 hrs · 10,867 cycles

LEFT PACK TEMP CONTROLLER M126 FAILED. REPLACED THE TEMP CONTROLLER.

Part: CONTROL PANEL — INOPERATIVE (COCKPIT) · airframe 80,088 hrs · 10,867 cycles

TEMP PNL M14 FLT DECK TRIM IN DOES NOT RESPOND WHEN SELECTING TEMPERATURE. REPLACED TEMP CONT PNL (M14).

Part: CIRCUIT CARD — FAULTY (EEC) · airframe 80,088 hrs · 10,867 cycles

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.

Part: SERVO — NO TEST (AUTOPILOT) · airframe 80,088 hrs · 10,867 cycles

CENTER AUTOPILOT RUDDER SERVO M278 FAIL DURING TEST. THE SERVO WAS REPLACED.

Part: RELAY — INOPERATIVE · airframe 80,088 hrs · 10,867 cycles

K105 RELAY, AC STANBY POWER AT P6 UNSERVICABLE. REPLACED THE RELAY.

Part: SMOKE DETECTOR — FAILED (AFT CARGO BAY) · airframe 80,088 hrs · 10,867 cycles

AFT SMOKE DETECTOR M718 IN THE AFT CARGO BAY FAILED. REPLACED THE BLOWER SMOKE DETECTOR.

Part: FAN — DIRTY (E/E BAY) · airframe 80,088 hrs · 10,867 cycles

E/E COOLING SUPPLY FAN DIRTY. THE FAN WAS REPLACED.

Part: IDG — INOPERATIVE (LEFT ENGINE) · airframe 80,088 hrs · 10,867 cycles

LEFT ENGINE IDG DISCONNECT LIGHT FAILED TO ILLUMINATE WHEN ENGINE IS NOT RUNNING. IDG REPLACED.

Part: PRESSURE SWITCH — CORRODED (NR 1 PYLON) · airframe 80,088 hrs · 10,867 cycles

NR 1 MID PYLON, IN AIR PRESSURE SWITCH PLUG CORRODED. THE PRESSURE SWITCH WAS REPLACED.

Part: FILL PORT — CORRODED (RT WING) · airframe 80,088 hrs · 10,867 cycles

RIGHT WING OVERWING FUEL FILLING PORT WING CUTOUT FOUND CORRODED. THE CORROSION WAS REMOVED.

Part: WIRE — DISCONNECTED (ANTI ICE VALVE) · airframe 80,088 hrs · 10,867 cycles

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.

Part: WIRE — DISCONNECTED (RT GENERATOR) · airframe 80,088 hrs · 10,867 cycles

RIGHT GENERATOR FAILED TO CONNECT TO THE BUS DURING RUNUP. FOUND DISCONNECTED WIRE W222-301B-18. WIRE RECONNECTED.

Part: SERVO — FAILED (RUDDER) · airframe 80,088 hrs · 10,867 cycles

RIGHT AUTOPILOT RUDDER SERVO M279 FAIL DURING TEST. THE SERVO WAS REPLACED.