N642GT

Part: STOWAGE BOX — NO TEST (OXYGEN MASK) · airframe 88,430 hrs · 25,625 cycles

DURING PREFLIGHT, FOUND OBS SEAT O2 MASK DOES NOT RESET DURING TEST. R & R OBSERVER'S O2 MASK ASSY IAW AMM 35-11-51 & IPC 35-11-51. OPS & LEAK CHECK GOOD AT THIS TIME.

Part: ELEC CONNECTOR — DAMAGED (ZONE 700) · airframe 88,312 hrs · 25,581 cycles

GEAR DISAGREE, GEAR DOORS EICAS MESSAGE AFTER GEAR UP SELECTION. PERFORMED PSEU LDG SYS 1 & 2. NO FAULT FOUND IAW AMM 32-09-04-204-013. PERFORMED PSEU LDG SYS 1 & 2, NO FAULTS FOUND IAW AMM 32-09-04-204-013. INSTALLED & REMOVED RT MAIN GEAR PIN ON SIDE BRACE NO PROBLEM. OPS IS NORMAL IAW 32-00-20-402-006. R & R RT MAIN SIDE BRACE LOCK ACTUATOR & PERFORMED OPS CHK NORMAL. NO LEAK IAW AMM 32-32-02-004-001 & IPC 32-32-02-01. ADDED SHIMS ON SENSOR 232 & 254 & CHECK WITHIN LIMIT. TESTED ON PSEU, NO FAULT ON SENSORS 232 & 254 IAW AMM 32-09-04-704-013, 32-61-03-822-022 & 32-61-03-722-043. R & R CONNECTORS D2220P & D1960P. OPS CHKD NORMAL IAW WDM 32-61-13, SWPM 2061-11 & AMM 32-61-03-722-043. R &R CONNECTORS D2206P & D1746P. OPS CHKD NORMAL IAW AMM 32-61-11, SWPM 20-61-11, & AMM 32-61-03-722-043. & R & R SIDE BRAKE LOCK ACTUATOR IAW AMM 32-32-02 & IPC 32-32-02-01. PERFORMED OPS TESTED MLG EXTENSION & RETRACTION SYS, OPS CHKD GOOD IAW AMM 32-32-00-705-001. R & R GEAR UP LINE FUSE RT MAIN & OPS CHKD NORMAL, NO LEAKS IAW AMM 32-32-104-007 & IPC 32-32-53-01.

Part: PSEU — FAULTED (ZONE 700) · airframe 88,311 hrs · 25,580 cycles

RH LANDING GEAR TOOK EXCESSIVELY LONG TO EXTEND AND / OR RH MAIN GEAR TO ILLUMINATE, LH AND NOSE GREEN LIGHTS WERE THE ONLY LIGHTS FOR 5-6 SECONDS. AT GEAR UP SELECTION, RECEIVED GEAR DISAGREE EICAS CAUTION MSG, GEAR DOORS EICAS ADVISORY MSG, AND A LDG GEAR MONITOR MSG W/ DU DEGRAGED STATUS MSG(<P><SPAN>R/R S240 SW &AMP; PSEU IAW AMM 32-09-04. OPS CHK OK. DMI 242595 CLOSED</SPAN></P>)

Part: HOOK AND LOOP — DAMAGED (EVAS UNIT) · airframe 87,860 hrs · 25,425 cycles

HOOK AND LOOP FOR EVAS ON CAPT SIDE NEEDS TO BE ATTACHED. EVAS IS SECURED WITH BOLTS. NO HOOK AND LOOP ON EVAS IAW AMM 25-60-99. NO FURTHER DEFECTS NOTED

Part: SKIN — DELAMINATED (ZONE 600 FLAP) · airframe 86,972 hrs · 25,154 cycles

RH WING, OUTBOARD FLAP, LOWER SURFACE, 9" TO 24" FROM INBOARD EDGE AND 23.5" TO 34" FROM LEADING EDGE, DELAMINATION.(<P>RH WING, OUTBOARD FLAP, LOWER SURFACE WAS REPAIRED I.A.W B767 SRM 57-53-01-2R-1 AND SRM 51-70-10-2R-4 PAG 1,4 FIG 201 SHEET 3 REV 127 15-DEC-24. NO FURTHER DEFECTS NOTED</P>)

Part: TRANSMITTER — FAULTED (FLAP SYS) · airframe 86,972 hrs · 25,154 cycles

TRANSMITER POSITION FLAPS M489 LOW INSULATION RESISTANCE.(<P>FLAP POSITION TRANSMITTER M489 WAS REPLACED IAW AMM 27-51-45-422-030 REV 144. FLAP POSITION TRANSMITTER M489 ADJUSTED AND TEST PERFORMED IAW AMM 27-51-45-822-161 REV 144. NO FURTHER DEFECTS NOTED.</P>)

Part: SIGN — LOOSE (ZONE 200) · airframe 86,972 hrs · 25,154 cycles

EMERGENCY LIGHT SIGN ENTERING THE CABIN, SCREWS LOOSE (2 EACH).(<P>TASK CARD A-06-040-01/004 EMERGENCY LIGHT SIGN ENTERING THE CABIN, SCREWS LOOSE. TWO SCREWS WERE INSTALLED CORRECTLY IAW AMM 33-51-01-412-003 REV 144 DATE 22DEC24. NO FURTHER DEFECTS NOTED.</P>)

Part: ANTI-SKID VALVE — NO TEST (ZONE 700) · airframe 86,972 hrs · 25,154 cycles

MLG, WHEEL #5, BRAKE UNIT, WHEN TEST WAS BEING PERFORMED, THE RECORDED PRESSURE WAS LOWER THAN PERMITTED.(<P>ANTISKID VALVE OF BRAKE #5 WAS REPLACED. IAW AMM 32-42-03-404-017. REV 144. DEC 22, 2024. TORQUE APPLIED: 105 LB IN. S/N: 0524121903. DATE: 15-MAY-25. ANTISKID/AUTOBRAKE CONTROL TEST WAS SATISFACTORY. PRESSURE ON BRAKE #5: 3000 PSI. S/N: 03220303188. DATE: 02-OCT-25. NO LEAKS WERE FOUND. BLEED THE WHEEL BRAKE SYSTEM WAS PERFORMED. IAW AMM 32-41-00- 682-001. REV 144. DEC 22, 2024. NO MORE ACTIONS REQUIRED.</P>)

Part: ACTUATOR — LEAKING (ZONE 600 SPOILER) · airframe 86,972 hrs · 25,154 cycles

RH WING SPOILER #12 WITH LEAK.(<P>POWER CONTROL ACTUATOR SPOILER #12 WAS REPLACED IAW AMM 27-61-02-424-023 REV 144. LEAK CHECK AND ADJUSTMENT WAS PERFORMED IAW AMM 27-60-00-825-072 REV 144. NO LEAK FOUND, SPOILER 12 IS GOOD FOR SEVICE.</P>)

Part: STRUCTURE — DAMAGED (ZONE 800) · airframe 86,972 hrs · 25,154 cycles

DAMAGE TO AFT LOWER CORNER OF FWD CARGO DOOR, CW SRM 5230011A1. PERMANENT REPAIR OF DOOR REQUIRED AT THE NEXT CHECK OR BEFORE 24 MONTHS.(<P>CRACK WAS REPAIRED IAW TRE6752055 &AMP; CMA-TLS-25-0009-05B. NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — DENTED (ZONE 600 FLAP) · airframe 86,972 hrs · 25,154 cycles

RH WING, INBOARD TRAILING EDGE FLAP, LOWER SECTION, OUTER SKIN WITH DENTS.(<P>RH WING, AFT FLAP - INBOARD TRAILING EDGE FLAP, LOWER SECTION, OUTER SKIN WAS REPAIRED IAW SRM 57-53-01-2R-1 FIG.201 SHEET 4 PAG.2,5 AND SRM 51-70-10- 2R-4 FIG.201 SHEET 1 PAG.1,3,7 REV.127 15 DEC-24. NO FURTHER DEFECTS NOTED.</P>)

Part: ACTUATOR — LEAKING (ZONE 500 SPOILER) · airframe 86,972 hrs · 25,154 cycles

LH WING SPOILER ACTUATOR #2, WITH LEAK EVIDENCE.(<P>POWER CONTROL ACTUATOR SPOILER #2 WAS REPLACED IAW AMM 27-61-02-424-023 REV 144. LEAK CHECK AND ADJUSTMENT WAS PERFORMED IAW AMM 27-61-00-825-072 REV 144. NO LEAK FOUND, SPOILER 2 IS GOOD FOR SERVICE.</P>)

Part: FUEL LINE — BENT · airframe 86,972 hrs · 25,154 cycles

ACCESS PANEL 197DL, FUEL LINE BENT.(<P>ACCESS PANEL 197DL, FUEL LINE WAS REPLACED. IAW AMM 28-13-06-404-005. REV 144. DEC 22, 2024. NO MORE ACTIONS REQUIRED. GOOD FOR SERVICE.</P>)

Part: ACTUATOR — OUT OF LIMITS (ZONE 300) · airframe 86,972 hrs · 25,154 cycles

DURING ELEVATOR SURFACE FREE PLAY FUNTIONAL CHECK, ELEVATOR RH, OUTBOARD POWER CONTROL ACTUATOR OUT OF LIMITS.(<P>POWER CONTROL ACTUATOR WAS REPLACED, TEST FOR LEAKS AND ADJUSTMENTS WAS PERFORMED IAW AMM 27-31-05-424-027 REV 144. OPS CHECK GOOD.</P>)

Part: SERVO — LEAKING (ZONE 300) · airframe 86,972 hrs · 25,154 cycles

VERTICAL STABILIZER WITH EVIDENCE OF HYDRAULIC LEAK IN BOTH YAW DAMPER SERVOS.(<P>YAW DAMPER SERVOS LH AND RH WERE REPLACED IAW AMM 22-21-02-414-016 REV 144. (OFF PART RH PN: 1540500-9 SN: 973BC, LH PN: 1536600-5 SN: 1856BA) INSTALLATION TEST WAS SATISFACTORY. NO LEAKS FOUND. GOOD FOR SERVICE.</P>)

Part: SKIN — CORRODED (ZONE 600 FLAP) · airframe 86,972 hrs · 25,154 cycles

RH WING INBOARD TE FLAP, CORROSION ON LOWER SKIN.(<P>RH WING INBOARD TE FLAP, LOWER SKIN WAS REPAIRED IAW TRE 6757282 RI ISSUED 13MAR25, AND FAA FORM 8100-9 (2-02) DATE 21MAR25. NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — CRACKED (ZONE 200) · airframe 86,972 hrs · 25,154 cycles

FWD ENTRY DOOR, AFT LOWER CORNER, HOLE 4 WITH CRACK INDICATION ON BEAR STRAP APPROX 10 O'CLOCK, AND HOLE 5 WITH CRACK INDICATION ON SKIN AND BEAR STRAP APPROX 10 O'CLOCK, 4 AND 11 O'CLOCK.(<P>CRACK WAS REPAIRED IAW 8017-0731_6753A-937_PART (1-2) REV 1 &AMP; SRM 51-40-02-0G-0 REV 127 &AMP;&NBSP;SRM 53-10-01-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED.</P>)

Part: ACTUATOR — LEAKING (ZONE 300) · airframe 86,972 hrs · 25,154 cycles

VERTICAL STABILIZER WITH EVIDENCE OF HYDRAULIC LEAK IN SERVO VALVE.(<P>RUDDER RATIO CHANGER ACTUATOR WAS REPLACED I.A.W AMM 27-21-15-422-024 OPERATONAL TEST WAS PERFORMED AND NO LEAKS FOUND, TORQUE APPLIED 280 LB-IN, 360 LB-IN S/N 0823114404 DATE 12DEC2026.</P>)

Part: FUEL LINE — DAMAGED (ZONE 100) · airframe 86,972 hrs · 25,154 cycles

CREASE ON APU FUEL SHROUD LINE AT STA 1646, LH SIDE.(<P>&NBSP;APU FUEL SHROUD LINE WAS REPLACED. IAW AMM 28-25-05-404-084 REV 144. DEC 22, 2024. TORQUE APPLIED ON CLAMPS: 24 LB IN. S/N: 0224110483. DATE: 11-MAY-25 BONDI NG TEST 0.5 MILLIHOMS SN: B0005830 DATE: 04-JUL-25 OPERATIONAL CHECK WAS PERFORMED. NO LEAKS FOUND. GOOD FOR SERVICE.</P>)

Part: FUEL TANK — LEAKING (ZONE 500) · airframe 86,972 hrs · 25,154 cycles

LH WING, LOWER EXTERNAL SURFACE, BTWN OUTB AND MAIN TANK, STRG 15, AT SPLICE, FUEL LEAK.(<P>MAIN TANK STRG 15 AT SPLICE LH SIDE SEALANT WAS REMOVED, AREA CLEANED AND SEALANT NSL 890A2, NSL 890B 1/2 APPLIED IAW 28-11-00-308-013 REV 144. FUEL LEAK TEST WAS SATISFACTORY.</P>)

Part: FUEL TANK — LEAKING (ZONE 500) · airframe 86,972 hrs · 25,154 cycles

LH WING, LOWER EXTERNAL SURFACE, BTW OUTB AND MAIN TANK, STRG 6, AT SPLICE, FUEL LEAK.(<P>MAIN TANK STRG 6 AT SPLICE LH SIDE SEALANT WAS REMOVED, AREA CLEANED AND SEALANT PS 890A2, NSL 890B 1/2 APPLIED IAW 28-11-00-308-013 REV 144. FUEL LEAK TEST WAS SATISFACTORY.</P>)

Part: SKIN — CORRODED (ZONE 600 FLAP) · corrosion level 2 · airframe 86,972 hrs · 25,154 cycles

RH WING INBOARD TE FLAP, CORROSION LOWER SKIN.(<P>RH WING INBOARD TE FLAP, LOWER SKIN WAS REPAIRED IAW TRE 6757282 R1 ISSUED 13MAR25, AND FAA FORM 8100-9 (2-02) DATE 21MAR25. NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — CORRODED (ZONE 300) · corrosion level 2 · airframe 86,972 hrs · 25,154 cycles

VERTICAL STABILIZER TIP REMOVABLE LEADING EDGE WITH CORROSION L= 4.0" W= 3.5 " (ACCESS PANEL 326A).<BR>(<P>VERTICAL STABILIZER TIP REMOVABLE LEADING EDGE WITH CORROSION L= 4.0" W= 3.5 " (ACCESS PANEL 326A) WAS REPLACED IAW SRM 51-10-02-0G-0 REV. 127 15-DEC-24. NO FURTHER DEFECTS NOTED</P>)

Part: FUEL LINE — DAMAGED (ZONE 100) · airframe 86,972 hrs · 25,154 cycles

CREASE ON APU FUEL SHROUD LINE AT STA 1720.5, LH SIDE.(<P>APU FUEL SHROUD LINE WAS REPL ACED. IAW AMM 28-25-05-404-084 REV 144. DEC 22, 2024. TORQUE APPLIED ON CLAMPS: 24 LB IN. S/N: 0224110483. DATE: 11-MAY-25 BONDING TEST 0.5 MILLIHOMS SN B0005830 DATE: 04-JUL-25 OPERATIONAL CHECK WAS PERFORMED. NO LEAKS FOUND. GOOD FOR SERVICE.</P>)

Part: FEEL UNIT — LEAKING (ZONE 300) · airframe 86,972 hrs · 25,154 cycles

LEAKAGE AT ELEVATOR FEEL UNIT IN HORIZONTAL STABILIZER TORSION BOX COMPARTMENT, LH SIDE.(<P>LEAKAGE AT ELEVATOR FEEL UNIT IN HORIZONTAL STABILIZER TORSION BOX COMPARTMENT, LH SIDE. ELEVATOR FEEL UNIT WAS REPLACED AND TEST WAS PERFORMED IAW AMM 27-31-19-424-015 REV 144. NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 86,972 hrs · 25,154 cycles

UPPER FUSELAGE SURFACE WITH CORROSION AT THE BASE OF THE TOP TCAS ANNTENA.(<P>UPPER FUSELAGE SURFACE CORROSION AT THE BASE OF THE TOP TCAS ANNTENA. REPAIR WAS PERFORMED IN ACCORDANCE WITH TRE6753716 FEB 24, 2025. FVC TITLE REPAIR- FUSELAGE SKIN- CROWN AREA-CORROSION DAMAGE ON DOUBLER BETWEEN STA 368-STA 390 AND STR S-1L/S-1R B767, CONTROL #25036-1 REV IR DATE 2/19/2025. SRM 51-10-02-OG-O REV 127 15DEC24 AND SRM 51-40-02-OG-O REV 127 15DEC24. CORROSION LEVEL 2. NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — CORRODED (ZONE 300) · corrosion level 2 · airframe 86,972 hrs · 25,154 cycles

VERTICAL STABILIZER TIP LEADING EDGE WITH CORROSION L=5.0" W=4.00".(<P>VERTICAL STABILIZER TIP LEADING EDGE WITH CORROSION L=5.0" W=4.00".THE VERTICAL STABILIZER LEADING EDGE TIP HAS BEEN REPLACED. NO FURTHER DEFECTS NOTED</P>)

Part: FUEL TANK — LEAKING (ZONE 500) · airframe 86,972 hrs · 25,154 cycles

LH WING, LOWER EXTERNAL SURFACE, BTWN OUTB AND MAIN TANK, STRG 10, AT SPLICE, FUEL LEAK.(<P>MAIN TANK STRG 10 AT SPLICE LH SIDE SEALANT WAS REMOVED, AREA CLEANED AND SEALANT NSL 890A2, NSL 890B 1/2 APPLIED IAW 28-11-00-308-013 REV 144. FUEL LEAK TEST WAS SATISFACTORY.</P>)

Part: SKIN — CRACKED (ZONE 200) · airframe 86,972 hrs · 25,154 cycles

SERVICE DOOR, AFT LOWER CORNER, HOLE 5 WITH CRACK INDICATION ON SKIN AND BEAR STRAP APPROX 2 AND 8 O'CLOCK.(<P>CRACK WAS REPAIRED IAW 8017-0731_6753A-937_PART (1-2) REV 1 &AMP; SRM 51-40-02-0G-0 REV 127. NO FURTHER DEFECTS NOTED.</P>)

Part: ACTUATOR — OUT OF LIMITS (ZONE 300) · airframe 86,972 hrs · 25,154 cycles

DURING ELEVATOR SURFACE FREE PLAY FUNTIONAL CHECK, ELEVATOR LH, OUTBOARD POWER CONTROL ACTUATOR OUT OF LIMITS.(<P>POWER CONTROL ACTUATOR WAS REPLACED, TEST FOR LEAKS AND ADJUSTMENT WAS PERFORMED IAW AMM 27-31-05-424-027 REV 144. OPS CHECK GOOD.</P>)

Part: STOWAGE BOX — NO TEST (ZONE 200) · airframe 86,972 hrs · 25,154 cycles

DMI 225437 PASSENGER #3 OXIGEN MASK REST SWITCH DOESN'T TEST. SEAT NOT ALLOWED TO BE OCCUPIED.(<P>STOWAGE BOX WAS REPLACED IAW AMM 35-11-51-400-803-001 REV 144, 22DEC2024 AND TEST WAS SATISFACTORY. NO FOUND LEAKS.</P>)

Part: SKIN — DENTED (ZONE 100) · airframe 86,972 hrs · 25,154 cycles

LOWER HALF OF FUSELAGE, BTW STA 654+44 AND 654+66, BTW STR 34L AND 33L, DENT ON SKIN.(<P>THE DENT WAS EVALUATED AND FOUND OUT OF LIMIT. IT WAS REPAIRED IAW SRM 53-00-01-2R-29 REPAIR 29. NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — DENTED (ZONE 600 FLAP) · airframe 86,972 hrs · 25,154 cycles

RIGHT WING INBD FLAP UPPER AND LOWER SKIN WITH SEVERAL DENTS.(<P>RH WING, AFT FLAP - INBOARD TRAILING EDGE FLAP, LOWER SECTION, OUTER SKIN WAS REPAIRED IAW SRM 57-53-01-2R-1 FIG.201 SHEET 4 PAG.2,5 AND SRM 51-70-10- 2R-4 FIG.201 SHEET 1 PAG.1,3,7 REV.127 15 DEC-24 FOR TIMES AND REFERENCES SEE : 00098 TASK CARD: A-57-580-00-02/001. NO FURTHER DEFECTS NOTED.</P>)

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 86,972 hrs · 25,154 cycles

EMERGENCY LIGHTS OF THE CABIN LH INOP.(<P>TASK CARD A-06-040-01/002 EMERGENCY LIGHTS OF THE CABIN LH, LAMPS WERE REPLACED IAW AMM 33-22-01 DATE. 10MAY10. TEST WAS PERFORMED SATISFACTORY.</P>)

Part: OXYGEN MASK — INOPERATIVE (ZONE 200) · airframe 86,972 hrs · 25,154 cycles

PASSENGER #3 OXYGEN MASK INOP.(<P>TRANSFER TO DMI 225437 PER MEL 35-11-03-02A CAT C DUE DATE 15FEB25</P> / <P>LP 1810355 ITEM M10, 21MAR25: STOWAGE BOX WAS REPLACED IAW AMM 35-11-51-400-803-001. TEST SATISFACTORY, NO FOUND LEAKS. IPC 35-11-52-15 REV 76 22FEB25 WAS VERIFIED. THIS CLEARS MDDR 225437.

Part: SEAL — DAMAGED (ZONE 600 FLAP) · airframe 86,492 hrs · 25,042 cycles

RIGHT O/B T/E FLAP WITH SEAL DAMAGED AT INBOARD SIDE.(<P>REMOVED DAMAGED SEAL AT R/H O/B T/E FLAP, I/B SIDE AREA, LOCATED, CLEANED, PREPARED, SECURED AND INSTALLED NEW SEAL AS REQUIRED AT R/H O/B T/E FLAP, I/B SIDE AREA PER BOEING 767-300 AMM 57-25-01-05 &AMP; AMM 20-10-23-964-001. NO FURTHER DEFECTS NOTED</P>)

Part: LATCH — BROKEN (ZONE 400) · airframe 86,492 hrs · 25,042 cycles

ENG #2 NACELLE STRUT, INBOARD ACCESS PANEL WITH LATCH BROKEN.(<P>REMOVED DAMAGED LATCH AT ENG #2, NACELLE STRUT INBOARD ACCESS PANEL AREA, LOCATED, CLEANED, TRIMMED, SECURED, ADJUSTED, SAFETY WIRE, INSTALLED NEW LATCH AS REQUIRED AT ENG #2 NACELLE STRUT, INBOARD ACCESS PANEL AREA PER BOEING 767-300 SRM 51-40-02-0G-0. NO FURTHER DEFECTS NOTED</P>)

Part: SHUTOFF VALVE — FAULTED (THRUST REVERSERS) · airframe 86,492 hrs · 25,042 cycles

LEFT TR INOP(<P>REMOVED DEFECTIVE REVERSER PRSOV REF 767-300 M/M 78-34-05-004-001-H00. OK TO INSTALL SERVICEABLE UNIT.</P> / <P>INSTALLED SERVICEABLE PRSOV REF 767-300 M/M 78-34-05-404-009-H00. INDICATOR AND OPERATION GOOD WITHOUT ENGINE OPERATING REF 767-300 M/M 78-33-00-725-005-H00. CHECK REVERSER OPS DURING ENGINE RUN-UP. ACCOMPLISHED #1 ENG RUN IAW AMM 71-00-00. T/R OPS CHECK OK&NBSP;</P>)

Part: SHUTOFF VALVE — FAULTED (CABIN PRESSURE) · airframe 86,485 hrs · 25,039 cycles

DURING CRUISE, RECEIVED A MASTER WARNING "CABIN ALT". COMPLIED W/ QRH. FL380. CABIN ALT 11,000' DPSI 7.0. USED MANUAL PRESSURIZATION MODE TO CONTROL &AMP; STABILIZED CABIN ALT. "CABIN AUTO INOP" CAUTION MSG. COMPLIED W/ QRH PROC. "CABIN ALT AUTO 1" AND "CABIN ALT AUTO 2" STATUS MSG'S.(<P>T/S PER FIM 21-31 FT 803. LOW FLOW INDICATED ON BITE TEST ASU, PER FIM, FOUND LH ENG PRSOV. R/R LH ENG PRSOV, LEAK &AMP; OPS CHK OK PER AMM 36-11-09. AS A PRECUATION, R/R CABIN PRESSURE CONTROL PANEL, DUE TO LANDING ACT SET KNOB SLIPS. OPS CHECK NORMAL IAW AMM 21-31-01.</P>)

Part: FUSE PIN — CRACKED (TE FLAP) · airframe 86,118 hrs · 24,924 cycles

SUPPORT #3 INBOARD FLAP - FUSE PIN - UNDERWING FITTING TO FOWARD TO TENSION LINK, WITH CRACK INDICATION FOUND AND CORROSION.(<P>FUSE PIN WAS REPLACED AND TORQUE WAS APPLIED IAW AMM 27-51-02-004-001. NO FURTHER DEFECTS NOTED</P>)

Part: PIVOT ASSY — CORRODED (ZONE 300) · corrosion level 2 · airframe 86,118 hrs · 24,924 cycles

HORIZONTAL STABILIZER - PIVOT FITTING - UPPER ATTACHMENT - MOST OUTBOARD REAR BOLT HOLE WITH INDICATION OF CORROSION(<P>TRE6755057 WAS PERFORMED AND NIL DAMAGE FOUND, TRE6755057 WAS BASED ON OEM MESSAGES CMA-PAO-24-0103</P>)

Part: PACKING — LEAKING (BOOST PUMP) · airframe 86,118 hrs · 24,924 cycles

FUEL LEAK IN MAIN FUEL BOOST PUMP WING RH(<P>THE PACKING AT THE MAIN FUEL BOOST PUMP WING RH WAS REPLACED. NO LEAKS WERE FOUND IAW AMM 24-22-03-004-001 AND 28-22-03-404-027 REV. 143 DATE: 22 AUG 24. TORQUE APPLIED: 55 LB-IN AND 35 LB-IN. S/N: 0821902601 DATE: 04-APR-25</P>)

Part: FUSE PIN — CRACKED (TE FLAP) · airframe 86,118 hrs · 24,924 cycles

SUPPORT #6 INBOARD FLAP - FUSE PIN - UNDERWING FITTING TO FOWARD TO TENSION LINK, WITH CRACK INDICATION FOUND AND CORROSION.(<P>FUSE PIN WAS REPLACED AND TORQUE WAS APPLIED IAW AMM 27-51-02-004-001. NO FURTHER DEFECTS NOTED</P>)

Part: ATTACH FITTING — CORRODED (ZONE 300) · corrosion level 2 · airframe 86,118 hrs · 24,924 cycles

LH UPPER HORIZONTAL STABILIZER PIVOT FITTING ATTACHMENT WITH CORROSION(<P><SPAN DATA-OLK-COPY-SOURCE="MESSAGEBODY">REMOVE FASTENERS FROM ALTERNATE ROWS, REAM THE AFFECTED HOLES THRU THE ENTIRE STACK-UP IN 1/64 INCH INCREMENTS UNTIL FASTENER HOLE IS CLEAN, ROUND AND DAMAGE FREE. PERFORM AN OPEN-HOLE HFEC INSTALL FASTENERS. THE REPAIR WAS DONE IAW CMA</SPAN>-PAO-24-0103.</P>)

Part: PIN — CORRODED (ZONE 500 FLAP) · airframe 86,118 hrs · 24,924 cycles

LEFT 6-6 PIN FLAP SUPPORT #4 WITH CORROSION(<P>PIN WAS REPLACED AND TORQUE WAS APPLIED IAW AMM 27-51-04-402-135. NO FURTHER DEFECTS NOTED</P>)

Part: TRANSMITTER — FAILED (ZONE 500 FLAP) · airframe 86,118 hrs · 24,924 cycles

LEFT WING TRANSMITTER FLAP POSITION #1 WITH FAIL(<P>LEFT WING TRANSMITTER FLAP POSITION #1 WAS REPLACED AND TESTED IAW AMM TASK 27-51-45-422-030 REV 143 DATE 22 AUG 24, TEST OK, 50 IN LB WERE APPLIED. S/N 0818911494 DUE DATE 04 APR 25</P>)

Part: PANEL — DAMAGED (ZONE 300) · airframe 86,118 hrs · 24,924 cycles

EVALUATE AND REPAIR AS REQUIRED, INDUCED DAMAGE TO RH HORIZONTAL STABILIZER T/E PANEL(<P>RH HORIZONTAL STABILIZER T/E PANEL WAS REPAIRED IAW SRM 55-10-01-2R-1 FIG 201 SHEET 4 PAGE 1-5 AND SRM 51-70-07- 0G-0 PAR 5.D FIG 11 PAG 16,37 REV 126 15/AUG/24</P>)

Part: UNION — LEAKING (FUEL SYSTEM) · airframe 86,118 hrs · 24,924 cycles

FUEL LEAK IN THE DENSITOMETER CONNECTOR PUMP QTY WING LH(<P>FUEL LEAK IN THE DENSITOMETER CONNECTOR PUMP QTY WING LH WAS R/R &AMP; NO LEAKS WERE FOUND IN IAW AMM 28-41-09-004-001-002 AND 28-41-09-404-028-002 REV. 143 DATE: 22 AUG 24. TORQUE APPLIED: 240 LB-IN S/N: 0823114442 DATE: 15/NOV/24</P>)

Part: SUPPORT FITTING — WORN (TE FLAPS) · corrosion level 2 · airframe 86,118 hrs · 24,924 cycles

FLAP SUPPORT #1 FITTING OUTBOARD ACTUATOR SPAR FITTING WEAR FOUND 3 HOLES WITH CORROSION INDICATION (LOCATED 12:00, 08:00 AND 10:00 O´CLOCK)(<P>CORROSION WAS REMOVED, REAMING THE AFFECTED HOLES AND FREEZE PLUGS WERE INSTALLED. THIS REPAIR WAS BASED ON CMA-PAO-24-0102 MESSAGES &AMP; TRE6757269</P>)

Part: STARTER — FAILED (APU) · airframe 87,743 hrs · 25,395 cycles

JUST BEFORE ENGINE START, A VERY STRONG ELECTRICAL SMELL OVERWHELMED THE FLIGHT DECK. SMELL GOES AWAY AFTER PACKS ARE SHUT OFF(<P>APU STARTER WAS BURNT AND WAS DETERMINED TO BE THE CAUSE OF THE SMOKE SMELL. R/R APU STARTER PER AMM 49-41-01. OPS CHK OK. NO DEFECTS NOTED. NO SMOKE SMELL NOTED. REF IPC 49-41-01-01 ITEM 50. R/R APU CONTROL UNIT PER AMM 49-61-05. OPS CHK OK. NO DEFECTS NOTED. REF IPC 49-61-05-01 FIG 5. SMOKE SMELL ADDRESSED PER CH 5 INSPECTION. NO MORE DEFECTS PER AMM 5-51-56.</P>)

Part: WARNING LIGHT — FALSE ACTIVATION (ZONE 800) · airframe 87,743 hrs · 25,395 cycles

MAIN CARGO DOOR DISCRETE LIGHT ON AFTER 2ND ENGINE START(<P>MDC CHECKED IAW AMM 52-31-00. OPENED &AMP; INSPECTION CHECKED GOOD. THIS CLOSES MDDR 236249&NBSP;</P>)

Part: CONTROL PANEL — FAULTED (VOR) · airframe 85,547 hrs · 24,738 cycles

FO SIDA UNABLE TO TURN VOR EMERGENCYIN MANUAL MODE(<P>REMOVED AND REPLACED VOR CONTROL PANEL IAW AMM 34-51-02. NO DEFECTS NOTED AT THIS TIME. VERIFIED PART EFFECTIVITY IAW IPC 31-11-11-17</P>)

Part: STOWAGE BOX — UNKNOWN (OXYGEN MASK) · airframe 85,537 hrs · 24,734 cycles

/FO OXYGEN STOWAGE BOX REQ REPLACEMENT(<P>R/R F/O'S OXYGEN STOWAGE BOX REF 35-11-51 LEAK CHECK GOOD OPS CHECK GOOD. PART EFFECTIVITY VERIFIED IAW AIPC 35-11-52-15</P>)

Part: STOWAGE BOX — NO TEST (OXYGEN MASK) · airframe 85,537 hrs · 24,734 cycles

FIRST OBSERVERS OXYGEN MASK NOT TESTING(<P>SUSPECT FO'S OXYGEN STORAGE BOX AND MASK WITH FIRST OBSERVERS SEAT PER AMM 35-11-51. DEFERRING FIRST OBSERVERS SEAT TO DMI 210052 PER MEL 25-11-02-01 CAT A DUE DATE 06JUN24. PLACARDS INSTALLED. LEAK&NBSP; CHECKS OK. REMOVED AND REPLACED FIRST OBSERVERS STORAGE BOX &AMP; LEAK CHECKS OK IAW AMM 35-11-51. DMI 210052 CLOSED.</P>)

Part: DISC — MISSING (BLOWOUT) · airframe 85,183 hrs · 24,607 cycles

ON PREFLIGHT A CHUNK OF THE O2 BLOWOUT DISC WAS DISCOVERED MISSING. REMOVED AND REPLACED O2 BLOWOUT DISK IAW AMM 20-10-23 AND AIPC 35-11-09-01.

Part: ELT — UNKNOWN (UNKNOWN) · airframe 84,696 hrs · 24,389 cycles

BOTH ELT ANTENNA CABLES TANGLED AND NOT WRAPPED APPROPRIATELY. REMOVED AND REPLACED L1 DOOR SIDE ELT PER AMM 25-63-03/401. OPS CHK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,947 hrs · 24,027 cycles

DURING TASK 52-32-00-705-041, FOLLOWINGS STEPS ARE NOT SATISFACTORY: -STEP(K)(3)(D)4 S9024 SWITCH. "DOOR NOT CLOSED" LIGHT IS ON (INSTEAD OF OFF). -STEP(K)(3)(H)2 S9024 SWITCH. "DOOR NOT LATCHED" LIGHT IS O  (INSTEAD OF ON). STEP(K)(3)(I)2 S9020 SWITCH. "DOOR NOT CLOSED" LIGHT IS OFF (INSTEAD OF ON). -STEP(K)(3)(Q)3 . "DOOR NOT LOCKED" LIGHT IS ON (INSTEAD OF OFF).(<P><SPAN LANG="EN-US">CONTINUITY TEST WAS PERFORMED IN THE DOOR CLOSED, LATCHED AND LOCKED SYSTEM, NOT DAMAGE FOUND. THE WRONG IDENTIFY WAS FOUND BETWEEN TWO SWITCHES (S9024 AND S9020), DUE THE WRONG IDENTIFY OF SWITCHES S9024 AND S9020 THE LIGHTS DON'T BE OPERATING IN ACCORDANCE WHIT TASK 52-32-00-705-041. THE PLACARDS OF THE SWITCHES S9024 AND S9020 WERE REINSTALLED CORRECTLY. I.A.W AMM 20-10-13-401 REV.139 DATE:22/APR/2023 AND AMM SUPPLEMENT MANUAL 52-71-09-REV.35 DATE 01/JUL/2018. THE STEP (K)(3)(D)4 HAVE A DISCREPANCY FOR WRONG WRITING IN TASK 52-32-00-705-401, THE SWITCH S9024 MUST BE WRITTEN AS S9022. THE LIGHT IN THE STEP (K)(3)(Q)3 MUST BE ON IN ACCORDANCE WHIT THE NOTE IN STEP (K)(3)(A) BY THE RELAY K9850 INSTALLED ON THE AIRCRAFT. DOOR CLOSED, LATCHED AND LOCKED INDICATION TEST WAS PERFORMED. TEST WAS SUCCESSFUL.</SPAN></P> / <P>&NBSP;</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,947 hrs · 24,027 cycles

MAIN DECK FLOOR STRUCTURE STA 654+88 LBL 5 SEAT TRACK WITH CRACK(<P>MAIN DECK FLOOR STRUCTURE AT STA 654+88 AND AT RBL 11 SEAT TRACK WAS REPAIRED PER SUPPLEMENT SRM 53-00-52 REPAIR 2 REV.4 30 SEP 2017</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,947 hrs · 24,027 cycles

MAIN DECK FLOOR STRUCTURE STA 654+88 LBL 54 SEAT TRACK WITH CRACK(<P>SUMMARY: MAIN DECK FLOOR STRUCTURE STA 654+88 LBL 54 SEAT TRACK WAS REPAIRED IAW IAI SUPLEMENT SRM 53-00-52 REPAIR 2 REV.4 30 SEP 2017</P> / <P>&NBSP;</P>)

Part: DRAIN VALVE — UNKNOWN (UNKNOWN) · airframe 83,947 hrs · 24,027 cycles

LEFT WING, INSPAR LOWER SURFACE EXTERIOR, SUMP DRAIN MAIN TANK, WITH FUEL LEAK(<P>MAIN TANK SUMP DRAIN VALVE WAS REPLACED IAW AMM 28-11-05-404</P> / <P>CHECK FOR LEAKS WAS&NBSP;PERFORMED AND NO FOUND LEAKS</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,947 hrs · 24,027 cycles

LIGHTING STRIKE ON UPPER FUSELAGE OUTER SKIN AT STA.396.75 AND 5" BELOW STGR 3RH(<P>LIGHTNING STRIKE WAS REPAIRED ON UPPER FUSELAGE OUTER SKIN AT STA 396 AND 5" BELOW STR 2 RH&NBSP;</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,947 hrs · 24,027 cycles

LEFT WING, OUTBOARD FLAP, LOWER SURFACE, WS 764.2, WITH PERFORATION(<P>LEFT WING, OUTBOARD FLAP, LOWER SURFACE WAS REPAIRED IAW 57-00-00.</P>)

Part: BOTTLE — UNKNOWN (UNKNOWN) · airframe 83,949 hrs · 24,028 cycles

CARGO 1 BTL EICAS MSG(<P>REMOVED AND REPLACED #1 CARGO BTL IAW AMM 26-23-02. OPS CHK GOOD.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,947 hrs · 24,027 cycles

CRACK ON PYLON #1 FWD UPPER SPAR WEB BETWEEN NAC STA 221.25 - 237.5, POWER FEEDER CABLE CUTOUT(<P>REPAIR WAS ACCOMPLISHED BY MXA EO TRE6754178 (SR ID 4-5858404778) <SPAN>AND BOEING SB 767-54-0090</SPAN></P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,947 hrs · 24,027 cycles

AFT CARGO DOOR, AFT AND UPPER OUTER SKIN WITH GOUGE(<P>&NBSP;AFT CARGO DOOR, AFT AND UPPER OUTER SKIN WAS REPAIRED. PER SRM 52-30-01-2R- 6 REV 122.&NBSP;</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,668 hrs · 23,894 cycles

3 EA INERTIAL ESCAPE REELS FELL OUT(<P>TRANSFER TO DMI 184857 PER MEL 25-61-01-01 CAT C, DUE DATE 11MAY2023.</P> / <P>LP 1749741 M2: INSTALL DESCENT DEVICE 3 EACH PER REELS AMM 25-61-05/401. SN: 30767, 30764 &AMP; 30768</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,604 hrs · 23,863 cycles

2 EA ESCAPE REELS INOP. 2 ESCAPE REELS NEED TO BE RE-STOWED ( FLIGHT CREW/SUPERNUMERARY ESCAPE DEVICES {ALL CARGO CONFIGURATION} INERTIAL ESCAPE REELS ) TRANSFER TO DMI 184127 PER MEL 25-61-01-01 CAT C, DUE 29APR23. MX PROCEDURE C/W. INSTALLED 2 EACH DEVICE PER AMM 25-61-05/401 & CHECKED OK. CLEARED DMI 184127. MCC NOTIFIED. PLACARD REMOVED.

Part: ESCAPE REEL — INOPERATIVE · airframe 82,859 hrs · 23,485 cycles

4 ESCAPE REELS INOP.(<P>REMOVED AND REPLACED DESCENT REELS IAW AMM 25-61-05. OPS CHECK GOOD</P>)

Part: NONE — NONE · airframe 82,767 hrs

ITEM #1 FLAP/SLAT ELEC STATUS MSG. ITEM #2 CENTER HYDRAULIC QTY AND PRESSURE LOST DURING FLIGHT COMPLIED WITH QRH NORMAL LANDING.(<P>UPON FURTHER INSPECTION FOUND LEAK AND BLOWN SEAL FROM HYD FLAP/SLAT SHUTOFF VALVE MODULE . REMOVED AND REPLACED FLAP/SLAT SHUTOFF VALVE MODULE IAW AMM 27-51-48. OPS CHECK AND LEAK CHECK. NO DEFECTS NOTED. LOST CENTER HYD QTY DUE TO LEAK AND BLOWN SEAL FROM THE FLAP/SLAT SHUTOFF VALVE MODULE (SEE LP 1556875 ITEM #1) SERVICED CENTER HYD SYSTEM IAW AMM 12-12-01. ADDED 28 QTS CENTER SYSTEM OPS CHECK AND LEAK CHECK GOOD. NO DEFECTS NOTED.</P>)

Part: LIGHT — INOPERATIVE · airframe 82,683 hrs

EMER LIGHTS LIGHT "DISARMED" NEED RELAMP(<P><SPAN>RELAMPED EMER LIGHTS SWITCH IAW B767 AMM 33-13-00.&NBSP; OPS CHECK GOOD.</SPAN></P>)

Part: ACTUATOR — OUT OF LIMITS · airframe 82,368 hrs · 23,260 cycles

LH ELEVATOR INNER ACTUATOR OUT OF LIMITS IAW TASK THE ELEVATOR SURFACE FREEPLAY(REMOVED AND REPLACED ACTUATOR PER AMM 27-31-05-424-027)

Part: VALVE — FAULTY · airframe 82,368 hrs · 23,260 cycles

ENG-1 PRV, VALVE CLOSE IN LESS THAN 20 SEC. IT IS NECESSARY TO REPLACE OF THE VALVE(VALVE WAS REPLACED PER AMM)

Part: SKIN — GOUGED · airframe 82,379 hrs

GOUGE DAMAGE ON IAI MAIN DECK CARGO DOOR SURROUND LOWER SKIN BETWEEN STA 500 AND STRINGER S-26LH (LAP JOINT AREA)(IT WAS REPAIRED BY MXA EO NO. TRE6753493)

Part: VALVE — FAULTY · airframe 82,368 hrs · 23,260 cycles

ENG #1 HPSOV FULLY CLOSED DO NOT CHANGE BIT 15 TO 0(VALVE WAS REPLACED PER AMM)

Part: FAILSAFE — CRACKED · airframe 82,368 hrs

CRACK ON FAIL SAFE STRAP P/N 145T2524-24 AT STA 955 / WL 93.5 REAR SPAR BULKHEAD SIDE FITTING - RH SIDE.(FAIL SAFE STRAP P/N 145T2524-24 WAS REPAIRED / MODIFIED PER SB767-53A0100 R3)

Part: FITTING — CRACKED · airframe 82,379 hrs

CRACK ON FASTENER HOLE OF LOWER HORIZONTAL TANG, OUTBD MIDSPAR FITTING OF RH STRUT BETWEEN NAC STA 285.45 / NAC STA 295.09 AND NAC RBL 11.0 / NAC RBL 12.0 (AFFECTED PART WAS REPLACED PER A PART OF THE SIP SERVICE BULLETIN 767-54-0081 R2 (THIS IS IN ACCORDANCE WITH SERVICE REQUEST #3-5264783404; BOEING MESSAGE NO. CMA-PAO-22-0001-27B))

Part: ACTUATOR — OUT OF LIMITS · airframe 82,368 hrs · 23,260 cycles

RH ELEVATOR, MIDDLE ACTUATOR OUT LIMITS IAW TASK ELEVATOR SURFACE FREEPLAY.(REMOVED AND REPLACED ACTUATOR PER AMM 27-81-05-424-027)

Part: FAILSAFE — CRACKED · airframe 82,368 hrs

CRACK ON FAIL SAFE STRAP P/N 145T2524-23 AT STA 955 / WL 93.5 REAR SPAR BULKHEAD SIDE FITTING - LH SIDE. NOTE: ADDITIONALLY IT WAS FOUND CORROSION DAMAGE OUT OF LIMITS PER SB767-53A0100 R3(FAIL SAFE STRAP P/N 145T2524-23 WAS REPAIRED / MODIFIED PER SB767-53A0100 R3 AND THE CORROSION OUT OF LIMITS WAS ATTENDED PER BOEING SR# 3-5286232348.)

Part: FITTING — CRACKED · airframe 82,379 hrs

CRACK ON BACKUP FITTING P/N 311T2568U8 LOCATED IN THE OUTBD AFT SIDE OF RH STRUT BETWEEN NACSTA 273.5 / NAC 285.45 AND NACWL 132.38 / NACWL 140.00(IT WAS REPLACED PER BOEING DRAWING AND B767 SRM 51-10-02 GRAL, PARAGRAPH 9)

Part: ACTUATOR — LEAKING · airframe 82,368 hrs · 23,260 cycles

RH WING, INBOARD AILERON OUTBOARD ACTUATOR WITH LEAK.(REMOVED AND REPLACED ACTUATOR PER AMM)

Part: PUMP — OUT OF LIMITS · airframe 82,368 hrs · 23,260 cycles

OUT OF LIMITS THE ELECTRICAL PARAMETERS ON RIGHT WING, FWD BOOST PUMP(REMOVED AND REPLACED FWD BOOST PUMP PER AMM 28-2-03-404-074)

Part: SKIN PANEL — CRACKED · airframe 82,379 hrs

CRACK ON RH WING UPPER SKIN PANEL 2 AT FRONT SPAR PITCH LOAD FITTING BETWEEN WSTA 375.8 / WSTA 404.4.(IT WAS REPAIRED IN ACCORDANCE WITH TLS EO NO. 6757A024)

Part: PUMP — OUT OF LIMITS · airframe 82,368 hrs · 23,260 cycles

OUT OF LIMITS THE ELECTRICAL PARAMETERS ON RIGHT WING, AFT BOOST PUMP(REMOVED AND REPLACED AFT BOOST PUMP PER AMM 28-22-03-404-074)

Part: STRUCTURE — CORRODED · corrosion level 2 · airframe 82,379 hrs

CORROSION ON INNER CHORD OF LOWER FRAME SEGMENT AT STA 1219 BETWEEN LBL 42 / RBL 39 AND WL 124.43 (AFT CARGO COMPT. FLOOR STRUCTURE)(IT WAS REPLACED THE AFFECTED PART)

Part: PUMP — OUT OF LIMITS · airframe 82,368 hrs · 23,260 cycles

OUT OF LIMITS THE ELECTRICAL PARAMETERS ON LEFT WING, FWD BOOST PUMP(REMOVED AND REPLACED FWD BOOST PUMP PER AMM 28-22-03-404-074)

Part: STRUCTURE — CRACKED · airframe 82,379 hrs

CRACK ON NOSE WHEEL WELL BULKHEAD VERTICAL CHORD (TEE P/N 141T2938-16) AT STA 287, LBL 25 (IT WAS REPAIRED PER SRM 51-70-12-0G-0)

Part: ACTUATOR — OUT OF LIMITS · airframe 82,368 hrs · 23,260 cycles

LH ELEVATOR OUTBOARD ACTUATOR OUT OF LIMITS IN ACCORDANCE WITH TASK THE ELEVATOR SURFACE FREE PLAY(LH ELEVATOR OUTBD ACTUATOR WAS REPLACED PER AMM)

Part: ACTUATOR — LEAKING · airframe 82,368 hrs · 23,260 cycles

LH WING, INBOARD AILERON BOTH ACTUATOR WITH LEAK(REMOVED AND REPLACED ACTUATOR PER AMM)

Part: FLANGE — CORRODED · airframe 82,368 hrs · 23,260 cycles

CORROSION ON LOWER SURFACE OF KEEL BEAM LOWER CHORD FLANGE P/N 145T8611-15 FROM STA 785.9 TO STA 1081 AT LBL 9.5 / LBL 10 (IT WAS REPAIRED PER SRM)

Part: STRUCTURE — CRACKED · airframe 82,368 hrs

CRACK ON NOSE WHEEL WELL BULKHEAD VERTICAL CHORD (TEE P/N 141T2938-15) AT STA 287, RBL 25(IT WAS REPAIRED PER SRM 51-70-12-0G-0)

Part: PUMP — OUT OF LIMITS · airframe 82,368 hrs · 23,260 cycles

OUT OF LIMITS THE ELECTRICAL PARAMETERS ON LEFT WING, AFT BOOST PUMP(REMOVED AND REPLACED AFT BOOST PUMP PER AMM 28-22-03-404-074)

Part: ESCAPE REEL — WRONG PART · airframe 82,434 hrs

ONE EMERGENCY ESCAPE REEL REMOVED / ( FLIGHT CREW/SUPERNUMERARY ESCAPE DEVICES {ALL CARGO CONFIGURATION} INERTIAL ESCAPE REELS )(TRANS TO MDDR 167030 IAW DDG 25-61-01-01 CAT C EXP 24 JUN 22 MX ACTION C/W AND REMVOVED FROM AIRCRAFT)

Part: NONE — NONE

CABIN ALT AUTO 2 STATUS MSG(<P>TRANSFERRED TO DMI # 156576 MEL 21-31-01A DUE 21 NOV 21 CAT C</P> / <P>11NOV21 - LOG PAGE 1424620 - ITEM 4: PERFORMED RESET TO AUTO 2 CABIN PRESS CONTROL UNIT. OPS CHECK GOOD. NO FAULTS FOUND IAW AMM 21-31-00. MESSAGE CLEARED. THIS CLEARS DMI # 156576, PLACARDS REMOVED.</P>)

Part: NONE — NONE

ON WALKAROUND FOUND BIRD STRIKE TO # ENGINE.(<P>PERFORMED BIRD STRIKE INSPECTION PER AMM 05-51-18. REF LP 1372482 ITEM M9 FOR BOROSCOPE INSP. NO OTHER DEFECTS NOTED. CLEANED AND REMOVED BIRD REMAINS.</P> / <P>LOG PAGE 1372482: COMPLETED NBR 1 ENG BORESCOPE OF HPC STAGE 1 THRU 14 PER B767 AMM 72-00-00-206-146-H00. NO ITEMS FOUND.</P>)

Part: NONE — NONE

L FWD FUEL PUMP EICAS MESSAGE PASSING APPROXIMATELY 37000, 12 MINUTES INTO FLIGHT. DISPLAYED FOR APPROXIMATELY 1 MINUTE, EXTINGUISHED BEFORE DIRECTED TO FUEL PUMP OFF BY QRH.(<P><SPAN>FOUND CONNECTOR ON L FWD FUEL PUMP PRESSURE SWITCH LOOSE AND DIRTY, CLEANED AND SECURED CONNECTOR, OPS CHECK NORMAL I/A/W AMM 20-30-07 AND 28-42-00</SPAN></P>)

Part: NONE — NONE · airframe 81,933 hrs · 22,937 cycles

AFTER FIRST ENGINE START (RIGHT) RED EICAS "OVERSPEED" WARNING FLASHED MOMENTARILY(<P>PERFORMED FIM 73-21 FAULT TREE 871. R ENG SPEED CARD TEST OPS NORMAL, NO CURRENT FAULTS.</P>)

Part: NONE — NONE

INTERMITTENT LT FWD FUEL PUMP EICAS MSG DURING CLIMB OUT(<P>PERFORMED OPERATIONAL CHECK REF AMM 28-22-00. OPS CHECKS GOOD AT THIS TIME. NO EICAS MESSAGE PRESENT AT THIS TIME</P>)

Part: VALVE — NONE

AFTER TAKEOFF RIGHT DUCT PRESS FLUCUATED RAPIDLY AND CONTINUOUSLY BETWEEN 20-40 PSI.(<P>ITEM TRANSFERRED TO MDDR 154728 IAW MEL 36-11-00-02.</P> / <P>09OCT21 - LP 784412 - ITEM# 3 - ATL - REACTIVATED HPSOV PER AMM TASK 36-00-00-440-801. C/W EO 1936A079. REMOVED AND REPLACED RH ENG PRSOV IAW AMM 36-11-09/401. LEAK CHECK GOOD. THIS CLEARS DMI 154728.</P>)

Part: VALVE — NONE · airframe 81,882 hrs

DURING T/S OF RH DUCT SURGE FOUND LEFT PACK TEMPERATURE CONTROLLER FAULTY(<P>TRANSFERRED TO MDDR 154731 IAW MEL 21-51-01-01, CAT C.</P> / <P>PER MCC REQUEST, SWAPPED LH PACK TEMPERATURE CONTROLLER P/N 1151864-1 S/N 1170-0354 WITH RH PACK TEMPERATURE CONTROLLER P/N 625946-10 S/N 060C-3515 IAW AMM 21-51-14. LEFT PACK OPERATES NML..</P> / <P>LP 784401 - ITEM 3: REMOVED AND REPLACED RIGHT HAND TEMP CONTROLLER (PN&NBSP;<SPAN>1151864-1, SN&NBSP;</SPAN><SPAN>1170-0354)</SPAN><SPAN>&NBSP;IAW AMM 767 21-51-14. OPS CHK GOOD.</SPAN></P> / <P>LP 784412 - ITEM 2 - ATL - REF LOG 784412 ITEM# 3 FOR PRSOV REPLACEMENT. REACTIVATED PACK AFTER VLV REPLACEMENT, OPS CHECK OK. THIS CLEARS MDDR 154731.</P>)

Part: NONE — NONE · airframe 81,854 hrs · 22,871 cycles

AFTER FLYING LEVEL AT 6000 MSL, WE INITIATED A CLIMB. WHEN CLIMB THRUST WAS SET THE RIGHT DUCT PRESSURE BEGAN SURGING BETWEEN 15-40 PSI APPROX ONCE PER SECOND. THE CONDITION PERSISTED UNTIL REACHING APROX 16000 MSL. AT THIS POINT THE CABIN DIFFERENTIAL PRESSURE WAS 6 PSI. BOTH LEFT AND RIGHT DUCT PRESSURE STABILIZED AT 36 PSI. REPEAT WRITE UP. REF LOG PAGE # 1435214 AND # 1461261.(<P>INSPECTION OF HPSOV IN R/H ENGINE PYLON IAW AMM 36-11-07. ALL FITTINGS &AMP; PLUGS ARE SECURE. NO DAMAGE OR LEAKS NOTED. C/W BITE TEST OF PRSOV IAW FIM 36-20 FT 804. NO FAULTS DETECTED. SYSTEM OP CHECK NORMAL.</P>)

Part: CONTROLLER — NONE

RT HPSOV INOP ( HIGH PRESSURE SHUTOFF VALVE(HPSOV) SYSTEMS CF6-80C2 )(<P>TRANSFERED TO MDDR 154269 PER MEL 36-11-02-02 CAT C</P> / <P>REF LOGPAGE 1461270 ITEM 5 CVG 29 SEP21&NBSP; REMOVED AND REPLACED RIGHT HAND ENGINE HIGH PRESSURE CONTROLLER ASSY. IAW AMM 36-11-08. OPS CHECK GOOD. THIS CLEARS MDDR #154269. PLACARDS REMOVED.</P>)

Part: NONE — NONE

PACKS SURGE ON TAKE OFF SUBSIDES AFTER LIFTOFF. NO EICAS OR STATUS MESSAGES.(<P><SPAN>C/W BITE TEST FOR PACK TEMP CONTROLLER AND STANDBY CONTROLLER IAW AMM 21-51-14. C/W COOLING PACK INSPECTION CHECK IAW AMM 21-50-00. NO DEFECTS NOTED AT THIS TIME. A/C OK FOR SERVICE.&NBSP;</SPAN></P>)

Part: SELECTOR — NONE

SIGNIFICANT PACK SURGE ON TAKEOFF AND INITIAL CLIMB THROUGH 10,000 FT(<P>PER MCC REQUEST REMOVED AND REPLACED CABIN PRESSURE SELECTOR &AMP; PERFORMED OPS TEST IAW B767 AMM 21-31-01. OPS TEST NML. PERFORMED CABIN PRESSURE TEST IAW B767 AMM 05-51-24. NO DEFECTS NOTED.</P>)

Part: NONE — NONE

AFTER START EICAS R ENG BLEED OFF REMAINED ILLUMINATED. QRH READ, DDG CONSULTED, NOT FC DEFERRABLE(<P>REMOVED AND REPLACED #2 ENG PRSOV IAW B767 AMM 36-11-09. PERFORMED ENGINE IDLE RUN IAW B767 AMM 71-00-00. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.&NBSP;</P>)

Part: FIRST AID KIT — NONE · airframe 81,816 hrs · 22,841 cycles

MEDICAL KIT IN CABINET ABOVE JUMPSEAT IS MISSING SEAL/TIE. EXAMINATION GLOVE BOX MISSING PLASTIC WRAP. ALL OTHER ITEMS IN KIT ARE ACCOUNTED FOR - SEALED.(<P>TRANSFERRED TO MDDR 153707</P> / <P>CVG - 18 SEP - LP 1372525 ITEM 3 -&NBSP; REMOVED AND REPLACED OVERHEAD BIN FIRST AID KIT IAW 25-64-03. THIS CLOSES MDDR 153707.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT GENERATOR)

"R GEN DRIVE" EICAS MESSAGE APPEARED MOMENTARILY DURING TAKEOFF ROLL AND THEN EXTINGUISHED.(<P>SERVICED #2 ENG IDG IAW B767AMM 12-13-03-613-027. PERFORMED ENGINE RUN AT IDLE IAW B767AMM 71-00-00-862-053-H03. OPS NORMAL.</P>)

Part: RELAY — INOPERATIVE (FUEL PUMPS) · airframe 81,740 hrs · 22,784 cycles

BOTH LEFT AND RIGHT CENTER FUEL PUMPS INOP.(<P>REMOVED AND REPLACED K633 IAW SWPM 20-81-11. SEE LOG PAGE 1435172 ITEM M19 FOR FURTHER ACTIONS. REMOVED AND REPLACED K357 AND K179 IAW SWPM 20-81-11. OPS CHECK GOOD NO DEFECTS NOTED AT THIS TIME.</P>)

Part: SEALANT — DAMAGED (INLET PROBE)

ORANGE SEALS STICKING OUT OF ENGINE INLET PROBES OF R ENGINE(<P>PERFORMED GVI INSPECTION OF POWERPLANT IAW AMM 71-00-00. FOUND RTV INTACT PROBES OF R ENG. NO DEFECT NOTED.</P>)

Part: SWITCH — BROKEN (LT IDG)

LEFT IDG INOP (PUSH BUTTON KORRY SWITCH BROKEN).(<P>TRANSFERRED TO MDDR 149822 IAW MEL 24-00-01-01, CAT B.</P> / <P>REMOVED AND REPLACED L GEN CONTROL SWITCH IAW SWPM 20-24-15. OPS CHECK GOOD. VERIFIED IDG OPERATIONAL IAW AMM 71-00-00. THIS CLEARS DMI 149822. MCC NOTIFIED. PLACARDS REMOVED TI 0720Z DT.</P>)

Part: SENSE LINE — LOOSE (RT ENGINE) · airframe 81,485 hrs · 22,626 cycles

RIGHT FIRE LOOP 1 IS DISPLAYED(<P>LP 1299616, ITEM M22: FOR TROUBLESHOOTING SWAPPED LEFT FIRE DETECTOR LOOP 1 CIRCUIT CARD M681 WITH RIGHT FIRE DETECTOR LOOP; 1 CIRCUIT CARD M683, EICAS MSG DID NOT FOLLOW TO LEFT FIRE DETECT LOOP 1. SWAPPED BACK TO ORIGINAL POSITIONS FOR THE L/H AND R/H FIRE DETECT LOOP 1 CIRCUIT CARDS IAW AMM 26-10-01. RIGHT FIRELOOP 1 IS DISPLAYED ON EICAS.</P> / <P>ITEM M23: SLAVED IN LOOP 1 FROM REMOVED ENG. NO FIX. RETURNED BACK TO ORIGINAL CONFIGURATION AND PARTS IAW AMM 26-11-02.</P> / <P>ITEM M24: FOUND SENSE LINE ON RIGHT ENGINE UPPER AFT FIRE LOOP BROKEN, REMOVED AND REPLACED RIGHT UPPER LOOP IAW 26-11-02. OPS CHECK GOOD.</P>)

Part: BLADE — DAMAGED (NR 2 ENG HPT) · airframe 81,485 hrs · 22,626 cycles

ENGINE #2 HAS UNSERVICEABLE DAMAGE OF HPT 1 BLADE AND VANES, FOUND DURING BORESCOPE INSPECTION.(<P>PER WO# 82193, REMOVED AND REPLACED #2 ENGINE IAW WORK CARD A-71-999-04-02, AND OPS CHECK IS GOOD AT THIS TIME.</P>)

Part: ESCAPE REEL — DISCONNECTED · airframe 81,413 hrs · 22,583 cycles

ESCAPE REELS NOT CONNECTED(<P>TRANSFER TO DMI # 147153 IAW MEL 25-61-01-01. CAT C DUE DATE 28MAY21. REEL REMOVED FROM #3 POSITION. PLACARD INSTALLED. T/I: MZ 11:02Z.</P><P>19MAY21, CVG MX, LP 1478527, ITEM M4: C/W W/O # 81091 REV O. INSTALLED #3 DESCENT DEVICE IAW AMM 25-61-05. THIS CLEARS DMI # 147153. MCC NOTIFIED. PLACARDS REMOVED. DT AT 0623Z</P>)

Part: ECU — FAULTED (APU) · airframe 81,370 hrs · 22,557 cycles

APU HAS NO DUCT PRESSURE.(<P>REMOVED AND REPLACED APU CONTROL UNIT ECU IAW AMM 49-61-05. OPS CHECKS GOOD AT THIS TIME.</P>)

Part: BOTTLE — DISCHARGED (CARGO BAY) · airframe 81,377 hrs · 22,561 cycles

CARGO BOTTLE 2 DISCHARGE, REMOVED AND REPLACED CARGO BOTTLE 2A. OPS CHECKED GOOD, WORK PERFORMED IAW AMM 26-23-02.

Part: WARNING MESSAGE — FALSE INDICATION (RT EEC) · airframe 81,360 hrs · 22,551 cycles

R ENG EEC C1 STATUS MESSAGE DISPLAYED ON SHUTDOWN. RT ENG EEC C1 MSG PLACED ON DEFERRAL MEL 73-21-01-05 CAT A, DMI 146620, DUE @AC HOURS 81662.09. PERFORMED PIMU GROUND TEST AND BITE. IAW FIM 71-01 FT 810. NO FAULTS NOTED, NO MESSAGE ON BLOCK IN. THIS CLEARS MDDR #146620. MCC NOTIFIED AND PLACARDS REMOVED.</SPAN></P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (RT ENG EEC) · airframe 81,347 hrs · 22,544 cycles

R ENG EEC C1 STATUS MSG.(<P>PERFORMED PIMU BITE TEST IAW AMM 71-00-00 MSG CLEARED.</P>)

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 81,276 hrs · 22,506 cycles

"STATUS MSG" CABIN ALT AUTO 2.(<P>TRANSFERRED TO MDDR 145043, MEL 21-31-01A , DUE 19APR21, CAT "C".</P><P>10APR21 - LP1453888 - M11 - CVG - REMOVED AND REPLACED #2 PRESSURIZATION CONTROLLER IAW B767 AMM 21-31-02 STEP E. OPERATION CHECK GOOD AT THIS TIME. THIS CLEARS MDDR #145043. NOTIFIED MCC. REMOVED PLACARDS. TI: YM 1208Z</P>)

Part: PRESSURE SWITCH — MALFUNCTIONED (FIRE BOTTLE) · airframe 81,262 hrs · 22,498 cycles

" CARGO BTL 2" EICAS MSG(<P>TRANSFER TO MDDR 144785 IAW MEL 26-23-01-01 CAT "C" DUE DATE 13 APR 21</P><P>04 APR 21-LP 1329329 ITEM 10-CVG-&NBSP;PERFORMED FIM 26-23 FAULT TREE 813 BLOCK 1. NO DEFECTS NOTED. PERFORMED OPS CHECK OF THE #2 BTL PRESSURE SWITCH IAW AMM 26-23-00. OPS CHECK GOOD. DMI #144785 REMAINS.</P><P>04 APR 21 - LP 1329330 - ITEM 13 CVG -&NBSP;REMOVED AND REINSTALLED CARGO FIRE EXT BOTTLES 2 AND 2A IAW AMM 26-23-02 IN ORDER TO PERFORM WEIGHT CHECK OF BOTH BOTTLES IAW AMM 26-23-02. BOTH BOTTLES WEIGHT CHECKS OK. ALSO PERFORM CARGO 2 AND 2A BOTTLES PRESS SW CHECK IAW AMM 26-23-00. CHECKS OK. NO FAULTS PRESENT AT THIS TIME. DMI 144785 OK TO CLEAR MEL AND PLACARDS REMOVED.&NBSP;</P>)

Part: ESCAPE REEL — DETACHED · airframe 81,182 hrs · 22,453 cycles

ESCAPE REELS FELL OUT. REMOVED AND REPLACED DESCENT DEVICE IAW AMM 25-61-03.

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI-ICE VALVE) · airframe 81,141 hrs · 22,429 cycles

AFTER LANDING ON GROUND L ENG TAI VALVE STAUS MESSAGE WHEN L ENG ANTI ICE VALVE TURNED OFF(<P>PERFORMED ENG RUN, ANTI ICE VALVE OPERATES NORMAL IAW AMM 30-20-00 &AMP; 71-60-00<BR /></P>)

Part: SWITCH — MALFUNCTIONED (ANTI ICE) · airframe 81,141 hrs · 22,429 cycles

ON DEPARTURE CLIMB WHEN LEFT ENGINE ANTI ICE SWITCH TURNED OFF VALVE LIGHT STAYED ON WITH L ENG ANTI-ICE EICAS MESSAGE. QRH ACCOMPLISHED W/ L ENG ANTI ICE SWITCH REMAINS OPEN.(<P>PERFORMED L ENG RUN, ANTI-ICE VALVE OPERATIONAL NORMAL IAW AMM 30-20-00-71-00-00.

Part: NONE — NONE · airframe 81,118 hrs · 22,417 cycles

BIRD STRIKE ON NR 1 ENGINE RT INLET SIDE(CLEANED AND INSPECTED BIRD STRIKE ON RT SIDE OF NR 1 ENGINE INLET IAW AMM 05-51-18. NO DEFECTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (FIRE BOTTLE) · airframe 81,115 hrs · 22,416 cycles

CARGO BTL EICAS MESSAGE (TRANSFERRED TO MDDR NR 142785, DDG 26-23-01-01, CAT C, DUE 03 MAR 21. UPON ARRIVAL NO FAULTS NOTED OR PRESENT ON CARGO EXT BTC NR 2. PERFORMED CARGO BOTTLE OPS TEST IAW B767-300 AMM 26-23-00. CARGO BOTTLE NR 2. OPS CHECK NORMAL. BOTTLE WEIGHT WITHIN LIMITS. THIS CLEARS MDDR 142785. MEL AND PLACARD REMOVED.)

Part: BLOWER — FAILED (SMOKE DETECTOR) · airframe 81,095 hrs · 22,407 cycles

CARGO DET AIR STATUS MESSAGE DISPLAYED. (TRANSFERRED TO MDDR 142678 IAW MEL;26-16-01-01-01, CAT C. LP 1491984: REMOVED AND REPLACED NR 1 AND NR 2 SMOKE DET BLOWERS IAW AMM 26-16-02. THIS CLEARS MDDR;142678. OFF PART: PN; 033638, SN DX0821.)

Part: WARNING MESSAGE — FALSE INDICATION (ANTI-ICE VALVE) · airframe 81,092 hrs · 22,405 cycles

STATUS L ENG ANTI ICE VALVE. PERFORMED SYSTEM OPS CHECK IAW 767 AMM 30-21-00. OPS CHECK GOOD AT THIS TIME.

Part: STATUS MESSAGE — FALSE INDICATION (LT ANTI-ICE VALV) · airframe 81,092 hrs · 24,405 cycles

L ENG TAI VALVE STATUS MSG. PERFORMED L ENG TAI VALVE SYSTEM TEST IAW B767 AMM 30-21-00, OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.

Part: SMOKE DETECTOR — INOPERATIVE (FWD CARGO) · airframe 81,092 hrs · 22,405 cycles

FORWARD CARGO SMOKE DET 2 INOPERATIVE. DEFERRED PER 26-16-01-01-01, MDDR 142550, CAT C, DUE 27FEB21 19FEB21 - LOG PG 1482029 ITM 4 - CVG. REMOVED AND REPLACED FWD CARGO DETECTOR 2 IAW AMM 26-16-01. OPS CHECK GOOD AT THIS TIME. THIS CLEARS DMI 142550.

Part: CIRCUIT BREAKER — TRIPPED (APU DOOR) · airframe 81,076 hrs · 22,393 cycles

APU DOOR STATUS MESSAGE(<P>TRANSFERRED TO MDDR# 142450 IAW DDG 49-15-01-01B. CAT C DUE 25FEB21.</P><P>LP 1362482: FOUND APU INLET DOOR CB POPPED. RESET CB AND PERFORMED OPS CHECK OF APU IAW AMM 49-11-00. OPS CHECK GOOD. MCC NOTIFIED. THIS CLEARS DMI 148450. PLACARDS REMOVED.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT OIL FILTER) · airframe 81,057 hrs · 22,383 cycles

R OIL FILTER STATUS MESSAGE DISPLAYED(<P>PERFORMED R ENG OIL FILTER BYPASS WARNING TEST IAW B767 AMM 79-35-00.OPS CHECK GOOD.NO DEFECTS NOTED AT THIS TIME. PERFORMED VISAUL INSPECTION ON R ENG OIL FILTER. NO DEFECTS NOTED AT THIS TIME.<BR /></P>)

Part: VALVE — WARNING MESSAGE (ENG ANTI-ICE SYS) · airframe 81,037 hrs · 22,372 cycles

STATUS MSG LT ENG TAI VALVE. PERFORMED OPS TEST OF LT ENGINE TAI VALVE IAW B767 AMM 30-21-03. OPS CHECK GOOD. VALVE OPENS & CLOSES. NO FAULTS NOTED.

Part: MASK — BROKEN (FIRST OBSERVER) · airframe 81,031 hrs · 22,368 cycles

FIRST OBSERVERS SMOKE GOGGLES BROKEN. OBSERVER SEATS, FIRST OBSERVER SEAT INCLUDING ASSOCIATED EQUIPMENT. TRANSFER TO DMI 141598 MEL 25-11-02-01. DUE 31JAN21. CAT A 247490 ITEM 1 CVG. R & R FO SMOKE GOGGLES IAW AIRCRAFT CHECKLIST T2112. THIS CLOSES MDDR 141598.

Part: WARNING MESSAGE — FALSE ACTIVATION (ENG ANTI ICE VLV) · airframe 81,005 hrs · 22,353 cycles

LEFT ENGINE TAI VALVE STATUS MESSAGE. PERFORMED OPERATIONAL TEST OF LT ENGINE TAI VALVE, IAW FIM 30-21 FAULT TREE 805. OPERATIONS CHECK GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENG A/I VALVE) · airframe 80,990 hrs · 22,345 cycles

LT ENGINE TAI VALVE STATUS MESSAGE DISPLAYED. ACCOMPLISHED RESET OF LT ENGINE TAI VALVE, IAW AMM 30-21-00. MESSAGE CLEARED.

Part: CHARGER — INOPERATIVE (APU) · airframe 80,980 hrs · 22,338 cycles

APU INOPERABLE DUE TO APU BATTERY CHARGER EICAS MESSAGE. TRANSFERRED TO MDDR 140940, IAW MEL 49-11-01A, CAT "C". REMOVED AND REPLACED APU BATTERY CHARGER, IAW AMM 24-31-05. OPERATIONS CHECK GOOD AT THIS TIME. THIS CLEARS DMI NR 140940.

Part: STATUS MESSAGE — FALSE ACTIVATION (LT TAI VALVE) · airframe 80,941 hrs · 22,315 cycles

LT ENGINE TAI VALVE STATUS MESSAGE. PERFORMED FIM 30-21 FAULT TREE 805. LT ENGINE TAI OPERATIONS CHECK GOOD. OK FOR SERVICE AT THIS TIME.

Part: IDG — FAULTED (RT GENERATOR) · airframe 80,940 hrs · 22,314 cycles

RT GEN DRIVE EICAS. FAULT CONFIRMED. TRANSFERRED TO MDDR NR 140354, MEL 24-00-01-01 CAT "B" DUE DATE 05JAN21. MCC NOTIFIED AND PLACARD INSTALLED. T/I MZ/1636Z. REMOVED AND REPLACED RT IDG, IAW AMM 24-11-01. OPERATIONS AND LEAK CHECK GOOD. THIS CLEARS MDDR NR 140354. PLACARD REMOVED.

Part: WARNING MESSAGE — FALSE ACTIVATION (FIRE LOOP) · airframe 80,946 hrs · 22,318 cycles

LT ENGINE FIRE LP 1 STATUS MESSAGE. TRANSFERED TO MDDR NR 140312, PER MEL 26-11-01-01. MCC NOTIFIED. PLACARDS INSTALLED. 01JAN21/LP 1246000/I M5/CVG. PERFORMED ENGINE FIRE LOOP OPERATIONS TEST, IAW B767 AMM 26-11-00. OPERATIONS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME. COULD NOT DUPLICATE PROBLEM. THIS CLEARS DMI 140312, PLACARDS REMOVED, MCC NOTIFIED.

Part: WARNING MESSAGE — FALSE ACTIVATION (FIRE BOTTLE) · airframe 80,914 hrs · 22,299 cycles

EICAS STATUS MESSAGE "DISCHARGE CARGO BOTTLE 2" CAME UP. PERFORMED FIRE/OVHT SYSTEM TEST, IAW AMM 26-23-00, TEST PASSED. STATUS MESSAGE "DISCHARGE CARGO BOTTLE 2" WENT AWAY.

Part: WARNING MESSAGE — FALSE ACTIVATION (ENG OIL FILTER) · airframe 80,914 hrs · 22,299 cycles

EICAS STARUS MESSAGE "RT OIL FILTER", OIL PRESSURE NORMAL, IAW AMM 71-00-00-862-0120-H03 POWERPLANT OPERATING LIMITATIONS. THIS MESSAGE "RT OIL FILTER" DISPLAYED BRIEFLY WITH OIL PRESSURE WITHIN NORMAL RANGE IS NORMAL. OK TO CONTINUE.

Part: ESCAPE REEL — DETACHED · airframe 80,877 hrs · 22,278 cycles

1 EA EMERGENCY DESCENT DEVICE FELL AND UN-REELED DURING TAKEOFF ROLL. TRANSFERRED TO MDDR NR 139638 USED MEL NR 25-61-01-01 CAT C DUE DATE 25DEC2020. REMOVED UNSERVICEABLE DESCENT DEVICE AND ROUTED TO IAH STORES. INSTALLED NEW DECENT DEVICE IN GALLEY, IAW IAI AMM 25-61-03. OKAY FOR SERVICE. THIS CLEARS MDDR NR 139638. MCC NOTIFIED.

Part: ESCAPE REEL — DETACHED · airframe 80,866 hrs · 22,272 cycles

DESCENT DEVICE FELL FROM DESCENT DEVICE CONTAINER. ITEM 7-REMOVED AND REPLACED DESCENT DEVICE, IAW AMM 25-61-05. P/N-379103D-29 S/N OFF-21201. ITEM 8-REMOVED AND REPLACED DESCENT DEVICE, IAW AMM 25-61-05. P/N-379103D-29 S/N OFF-20985. ITEM 9-REMOVED AND REPLACED DESCENT DEVICE, IAW AMM 25-61-05.

Part: FIRE LOOP — FALSE ACTIVATION (APU BAY) · airframe 80,817 hrs · 22,244 cycles

APU FIRE LOOP 2 DISPLAY. TRANSFERRED TO MDDR NR 138809, IAW MEL 26-15-01A. PERFORMED FIRE/OVERHEAT TEST, IAW AMM 26-11-00. TEST SUCCESSFUL, NO EICAS MESSAGE DISPLAYED. NO DEFECTS NOTED, THIS CLEARS DMI 138809.

Part: CONNECTOR — SHORTED (APU) · airframe 80,793 hrs · 22,230 cycles

APU NO DUCT PSI. TROUBLESHOT WIRING FROM PLUG D4100J PINS 10, 11 TO PLUG D4098P PINS 4, 5. FOUND SHORT TO SHIELD. SPLICED NEW SHIELDS AT PLUGS D 4100J PINS 11 AND PLUG D4098 PINS 5, IAW WDM DRAWING NR 47094MM801 AND SWPM 20-25-11. ALL OPERATIONS CHECKS GOOD AT THIS TIME. THIS CLEARS DMI 138481. PLACARD REMOVED. MCC NOTIFIED.

Part: FIRE LOOP — BROKEN (NR 2) · airframe 80,676 hrs · 22,162 cycles

INTERMITTENT RT ENGINE NR 2 FIRE LOOP STATUS MESSAGE. FOUND BROKEN/DAMAGED TERMINAL STUD. REMOVED & REPLACED LOWER AFT FIRE DETECTOR ASSEMBLY OF LOOP NR 2(B), IAW AMM 26-11-02/401. OPERATIONS TEST GOOD.

Part: STATUS MESSAGE — FALSE ACTIVATION (RT ENG FIRE LOOP) · airframe 80,662 hrs · 22,155 cycles

RIGHT ENGINE FIRE LOOP STATUS MESSAGE. PERFORMED ENGINE/APU FIRE DETECTION TEST, IAW 767 AMM 26-11-00. MESSAGE CLEARED, OPERATIONS TEST GOOD AT THIS TIME.

Part: LOGIC CARD — MALFUNCTIONED (LT ENG SPEED) · airframe 80,648 hrs · 22,147 cycles

"LT ENGINE SPEED CARD" STATUS MESSAGE DISPLAYED. REMOVED AND REPLACED LT ENGINE N2 SPEED CARD, IAW AMM 73-21-54. STATUS MESSAGE CLEARED. OPERATIONS CHECK GOOD.

Part: STATUS MESSAGE — FALSE ACTIVATION (RT ENG FIRE LOOP) · airframe 80,648 hrs · 22,147 cycles

RT ENG FIRE LP 2 STATUS CAME ON AFTER TAKE OFF THEN WENT OUT. TROUBLESHOT IAW B767 FIM TASK 26-10. NO FAULTS FOUND. A/C OK TO CONTINUE SERVICE AT THIS TIME.

Part: OXYGEN BOTTLE — LEAKING (NR 2) · airframe 80,597 hrs · 22,119 cycles

NR 2 O2 BOTTLE LEAKING, INSPECTED NR 2 O2 BOTTLE AAND FITTINGS AND FOUND MAIN B NUT FITTING NOT SEATED PROPERLY. LOOSENED AND RESEATED MAIN B NUT, IAW AMM 35-11-00. OPS AND LEAK CHECK GOOD AT THIS TIME, IAW B767 AMM 12-15-08. LEAK CHECK NR 2 O2 REGULATOR AND ASSOC TUBING IN 35-11-53-05E, NO LEAKS NOTED. PERFORMED AMM TASK 35-11-00 CREW O2 STORAGE BOX TEST, TEST CHECK GOOD.

Part: FIRE LOOP — INOPERATIVE (LT ENGINE) · airframe 80,584 hrs · 22,112 cycles

LEFT ENG LP 1 FIRE LOOP INOP. TRANSFERRED TO MEL NR 26-11-01-01, MDDR NR 134556, CAT C, DUE DATE 27 SEP 20. T/S PER FIM 26-11 FAULT TREE 805, FOUND RESISTANCE ON LOOP AS FOLLOWS: F I D LOWER 4119/4-494K. DMI REMAINS AFT LOWER 4.487/4.492K OPEN. T/S PER FIM 26-11 FT 805 - NO MORE FAULTS FOUND AND PERFORMED OPERATIONAL TEST, PER AMM 26-11-00-705-001, ALL TESTS OK. THIS CLEARS MDDR 134556, PLACARDS REMOVED, MCC ADVISED.

Part: STATUS MESSAGE — FALSE ACTIVATION (LT ENG FIRE LOOP) · airframe 80,577 hrs · 22,108 cycles

STATUS MESSAGE: LT ENG FIRE LOOP 1. PERFORMED ENGINE FIRE LOOP TEST, IAW AMM 26-11-00. OPS CHECK GOOD. NO DEFECTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENG FIRE LOOP) · airframe 80,570 hrs · 22,104 cycles

INFO ONLY LT ENG FIRE LP 1 STATUS MESSAGE APPEARED AFTER LIFTOFF. MESSAGE CLEARED UPON REACHING FL330, NOTED BY MX. PERFORMED ENG FIRE LOOP TEST IAW AMM 26-11-00. OPS CHECKS GOOD AT THIS TIME.

Part: OXYGEN MASK — DAMAGED (CAPTAIN'S) · airframe 80,575 hrs · 22,107 cycles

CAPTAINS O2 MASK REMAINING P/N APPEARS TO BE STUCK IN AND WILL NOT HOLD THE O2 MASK IN PLACE. FOUND DAMAGED DURING PRE FLIGHT. RE-SEATED PIN, IAW AMM 35-11-51. NO DEFECTS NOTED.

Part: DRIVE UNIT — FAILED (WX RADAR SYS) · airframe 80,566 hrs · 22,102 cycles

WX RADAR FAIL. REMOVED AND REPLACED WEATHER RADAR DRIVE UNIT, IAW AMM 34-43-05. OPS CHECKS GOOD. NO DEFECTS NOTED AT THIS TIME.

Part: FILL PORT — CORRODED (LT WING) · corrosion level 2 · airframe 80,565 hrs · 22,101 cycles

LT OVERWING FUEL PORT HAS CORROSION ON MATING SURFACE FOR FUEL CAP HOUSING. REPAIRED LT OVERWING FUEL PORT, IAW FAS EA 20021 REV. IR.

Part: SIGN — LOOSE (CABIN) · airframe 80,565 hrs · 22,101 cycles

L-1 ENTRY DOOR AREA FWD JAMB INTERIOR EXIT LIGHT COVER FITS LOOSE. REMOVED AND REPLACED EXIT SIGN LENS AND HOUSING, IAW B767 AMM 33-51-01. PERFORMED SATISFACTORY OPS CHECK OF NEW EXIT SIGN, IAW B767 AMM 35-51-01-400-801-001.

Part: IGNITER — INOPERATIVE (RT ENGINE) · airframe 80,565 hrs · 22,101 cycles

RH ENGINE IGNITION 1 INOPERATIVE. EXCEPT ER OPERATIONS. PERFORMED AUDIBLE TEST OF THE RH ENGINE IAW AMM 71-00-00, NR 1 IGNITER INOPERATIVE, NR 2 IGNITER OPERATIONAL IAW AMM LIMITS.

Part: IGNITER — UNKNOWN (RT ENGINE) · airframe 80,556 hrs · 22,096 cycles

RT ENGINE NR 1 IGNITER INOPERATIVE (IGNITION SYSTEMS, EXCEPT ER OPERATIONS. ACCOMPLISHED NR 2 ENGINE IDLE RUN ON SINGLE IGNITION SYSTEM 1 & 2 IAW AMM 71-00-00, STARTED NORMAL.

Part: ESCAPE REEL — INOPERATIVE (NR 3) · airframe 80,507 hrs · 22,063 cycles

ONE DESCENT DEVICE INOPERATIVE. REMOVED THE NR 3 DESCENT DEVICE FROM AIRCRAFT AND INSTALLED A NEW DECENT DEVICE IN THE NR 3 SPOT IAW AMM 25-61-05.

Part: WATER SEPARATOR — INOPERATIVE (LT A/C PACK) · airframe 80,458 hrs · 22,022 cycles

LEFT PACK INOPERATIVE. REMOVED AND REPLACED THE WATER EXTRACTOR IAW AMM 21-51-04. LEAK CHECK OK.

Part: VALVE — MALFUNCTIONED · airframe 80,438 hrs · 22,006 cycles

FWD EQUIP VAL EICAS MESSAGE AFTER ENGINE START. REPEAT WRITE-UP. SEE LOGBOOK PAGE 1279386. REMOVED AND REPLACED THE MANIFOLD INTERCONNECT VALVE V90 IAW AMM 21-58-01. OPS CHECKS GOOD. PERFORMED ENGINE RUNS IAW AMM 71-00-00. OPS CHECKS GOOD. NO DEFECTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 80,451 hrs · 22,016 cycles

FWD EQPT VALVE EICAS DISPLAYED AFTER ENGINE START. PERFORMED FIM 21-58 TREE 805, NO DEFECTS NOTED. PERFORMED FWD EQUIPMENT OPS CHECK IAW AMM 21-58-00, OPS CKS GOOD.

Part: RELAY — FAILED (EXHAUST FAN) · airframe 80,399 hrs · 21,974 cycles

AFT EXHAUST FAN 2 STATUS MESSAGE. REMOVED AND REPLACED K886 AFT EXHAUST FAN SHUT OFF RELAY 2 IAW WDM 21-26-16 AND K347 AFT / EQUIP LAV GALLEY VENT FAN 2 RELAY IAW WDM 21-26-11. OPS CHECK GOOD IAW AMM 21-26-01.

Part: APU — SHUTDOWN · airframe 80,385 hrs · 21,964 cycles

APU SHUTDOWN. REMOVED AND REPLACED APU IAW AMM 49-11-01. OPS TEST GOOD AT THIS TIME. NO DEFECTS NOTED ON ECU AT THIS TIME, REF AMM 49-61-05. NO DEFECTS DETECTED.

Part: APU — INOPERATIVE · airframe 80,383 hrs · 21,963 cycles

APU INOPERATIVE. SERVICED APU IAW AMM 12-13-04 AND PERFORMED AN OPS CHECK IAW AMM 49-11-00. OPS CHECKED GOOD.

Part: APU — SMOKE · airframe 80,378 hrs · 21,960 cycles

DURING POST FLIGHT NOTICED APU WAS EXHAUSTING SMOKE. APU SHUT DOWN, NO APU FIRE INDICATION. ACCOMPLISHED VISUAL INSPECTION OF APU TAIL PIPE AND EXTERIOR OF APU, NO DISCREPANCIES NOTED. ACCOMPLISHED FIM TASK 49-11-00-815, NO FAULTS. ACCOMPLISHED APU ECU BITE LAST LEG NORMAL STOP RAN APU SEVERAL TIMES WITH NO FAULTS. OK FOR SERVICE.

Part: CIRCUIT BREAKER — TRIPPED (WEATHER RADAR) · airframe 80,374 hrs · 21,958 cycles

LEFT WX RADAR FAIL. FOUND LEFT CIRCUIT BREAKER NR 2 OUT, RESET PER MM 20-90-01, ACCOMPLISHED WXR SYSTEM TEST PER MM 34-43-00/001 CONFIG 2. NO DEFECTS NOTED AND NO PREVIOUS C/B DISCREPANCIES.

Part: WARNING MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 80,373 hrs · 21,957 cycles

L GEN OFF MSG ON DEPARTURE. RAN QRH TO CLEAR. PERFORMED L IDG OPERATIONAL TEST IAW AMM 24-11-00. OPS CHECK GOOD. NO FAULTS NOTED. SERVICED LEFT IDG IAW AMM 12-13-03.

Part: STOWAGE BOX — FAULTY (COCKPIT) · airframe 80,359 hrs · 21,947 cycles

FO OXY MASK DOES NOT TEST PROPERLY. M2: FIRST OBS SEAT INOP DUE TO OXYGEN MASK INOP. SWAPPED MASK WITH FIRST OBS POSITION IAW AMM 35-11-04, OPS CHECK OK. NOW FIRST OBS SEAT INOP DUE TO OXYGEN MASK INOP. REMOVED AND REPLACED FIRST OBSERVERS OXYGEN MASK STORAGE BOX PER AMM 35-11-51, OPS CHECK GOOD. THIS CLEARS MDDR 129580.

Part: ESCAPE REEL — DEPLOYED (CABIN) · airframe 80,346 hrs · 21,938 cycles

DURING WALKAROUND FOUND NUMBER 3 EMERGENCY DESCENT DEVICE DEPLOYED. REMOVED AND REPLACED NUMBER THREE EMERGENCY DESCENT DEVICE IAW AMM 25-61-00. OPS CHECKS NORMAL.

Part: ESCAPE REEL — DEPLOYED (CABIN) · airframe 80,318 hrs · 21,920 cycles

1X DESCENT DEVICE DEPLOYED DURING LANDING. REMOVED AND REPLACED DESCENT DEVICE IAW AMM 25-61-05. CHECKED INTEGRITY OF RETAINER DOOR LATCH IAW AMM 25-61-05. NO DEFECTS NOTED AT THIS TIME.

Part: CONNECTOR — DIRTY (START VALVE) · airframe 80,276 hrs · 21,895 cycles

RIGHT ENGINE START VALVE LIGHT INOP(<P>TRANSFER TO MDDR 128306 IAW DDG 80-00-01-01, CAT 'C' DUE DATE MAY 23-20.</P><P>LP 1147450: VERIFIED START VALVE CANNON PLUG, CLEANED AND SECURED. ACCOMPLISHED STARTER MM 71-00-00. ACCOMPLISHED #2 ENG START VALVE LIGHT OPERATION CHECK PER MM 80-11-00. ALL CHECKS NORMAL. THIS CLEARS MDDR 128306.<BR /></P>)

Part: PANEL — MALFUNCTIONED (COCKPIT) · airframe 80,275 hrs · 21,894 cycles

RT FO'S WX SWX BULB BURNT OUT.(<P>REMOVED AND REPLACED ANNUNCIATION&NBSP; ASSY IAW SPM 20-61-00. OPS CHECK GOOD IAW AMM 34-43-00.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 80,237 hrs · 21,861 cycles

STATUS RIGHT ENG TAI VALVE.(<P>PERFORMED OPERATIONAL CHECK OF ENGINE # 2 TAI VALVE WITH ENGINE PNEUMATICS REF AMM 30-21-00. COULD NOT DUPLICATE FAULT AT THIS TIME, OPERATIONAL CHECK GOOD.</P>)

Part: CONTROL UNIT — MALFUNCTIONED (WINDOW HEAT) · airframe 80,222 hrs · 21,843 cycles

L SIDE WINDOW HEAT INOP(<P>REMOVED AND REPLACED L SIDE/RFWB WINDOW HEAT CONTROL UNIT IAW AMM 30-41-01. OPS CHECKS GOOD.<BR /></P>)

Part: START VALVE — FAILED (LT ENGINE) · airframe 80,209 hrs · 21,832 cycles

LEFT ENG START VALVE FAILED(<P>TRANSFERRED TO MDDR 126765, MEL 80-00-02-01, CAT C, DUE DATE 17APR20.</P><P>LP&NBSP;1232027 ITEM 2: REMOVED AND REPLACED LEFT ENG START VALVE IAW AMM 80-11-02. OPS CHECK GOOD. THIS CLEARS MDDR 126765. PLACARD REMOVED.</P>)

Part: A/C PACK — ODOR (AC BAY) · airframe 80,207 hrs · 21,830 cycles

STRONG MUSTY SMELL FROM LEFT PACK.(<P>PERFORMED LEFT/RIGHT PACK CLEAN OUT IAW AMM 21-00-21.<BR /></P>)

Part: STARTER — FAILED (LT ENGINE) · airframe 80,199 hrs · 21,822 cycles

LEFT STARTER FAILURE DURING ENGINE START AFTER PUSH BACK.(<P>REMOVED AND REPLACED AND SECURED LEFT ENGINE STARTER IAW B767 AMM 80-11-01. OPS CHECK GOOD.</P>)

Part: CONTROL VALVE — FAULTY (APU) · airframe 80,198 hrs · 21,820 cycles

APU DOES NOT INCREASE PNEUMATIC PRESSURE ON ENGINE START.(<P>TRANSFERRED APU PNEUMATIC FUNCTION TO DMI 126477 PER B767 DDG 49-11-01-01, CAT "C" DUE 10APR2020.</P><P>REF LOG PAGE 1232005 ITEM M4: REMOVED AND REPLACED SURGE CONTROL VALVE IAW AMM 49-53-01. OPS TEST NORMAL, ALL INDICATIONS NORMAL. PERFORMED DRY MOTOR OF ENGINE 1 IAW AMM 71-00-00, DUCT PRESSURE @ 37 PSI. THIS ACTION CLEARS DMI 126477.&NBSP;</P>)

Part: PANEL — INOPERATIVE (ANTI-ICE SYSTEM) · airframe 80,195 hrs · 21,816 cycles

FOUND RIGHT WING ANTI-ICE VALVE LIGHT INOP.(<P>TRANSFERRED TO MDDR #126326 I.A.W MEL 30-11-02C, CAT C.</P><P>LOGPAGE 1231999:&NBSP;REMOVED AND REPLACED PANEL ASSY IAW B767 AMM 30-11-01. OPS TEST GOOD. THIS CLEARS DMI #126326.</P>)

Part: BUTTON — BROKEN (COCKPIT) · airframe 80,195 hrs · 21,816 cycles

LEFT ENGINE ANTI-ICE FLOW BAR BUTTON IS BROKEN.(<P>TRANSFERRED TO MDDR #126325 I.A.W MEL 30-21-02-01-04, CAT C.</P><P>LOG PAGE 1231999: REMOVED AND REPLACED&NBSP;PANEL ASSEMBLY IAW B767 AMM 30-11-01. OPS TEST GOOD. THIS CLEARS MDDR&NBSP; 126325.</P>)

Part: APU — MALFUNCTIONED (APU BAY) · airframe 80,177 hrs · 21,797 cycles

APU FAILS TO START.(<P>TRANSFERRED TO MDDR 125888 PER B767 DDG 49-11-01A, CAT 'C', DUE 27MAR20. PROCEDURES C/W. PLACARDS INSTALLED.</P><P>LOGPAGE 1231997: TROUBLESHOT RELAY K197 PER B767 FIM 49-11 TREE 959, FOUND HIGH RESISTANCE BETWEEN X1 AND X2 PINS. REPLACED RELAY IAW SWPM 20-81-22. NO HELP. REMOVED AND REPLACED APU ECU IAW AMM 49-61-05.&NBSP;APU ECU P/N OFF 2117342-20, S/N OFF 727711. OPS CHECK GOOD.THIS CLEARS DMI 125888.</P><P>LOG PAGE 123997 ITEM M6. REMOVED AND REPLACED APU IAW B767 AMM 49-11-01 AND W/O A49.999-00-01. OPS CHECK GOOD .&NBSP;</P>)

Part: BLADE — DENTED (LT ENGINE) · airframe 80,171 hrs · 21,789 cycles

DURING WALK AROUND FOUND DENT ON LEADING EDGE OF #15 FAN BLADE.(<P>BLENDED AND DAMAGE REMOVED ON FAN BLADE #15 AROUND THE EDGE PER AMM 72-31-02. ON THE LEADING EDGE.</P><P><SPAN>(NOTE: OPENED MDDR 125624 FOR LEFT ENGINE FAN BLADE #15 BLENDED (REPAIR ACCOMPLISHED),&NBSP; PENDING FLUORESCENT PENETRANT TEST BEFORE OR AT 50 FLIGHT HOURS OR 10 FLIGHT CYCLES.)</SPAN><BR DATA-MCE-BOGUS="1" /></P>)

Part: ROTOR — DEFECTIVE (RT ENGINE) · airframe 80,168 hrs · 21,786 cycles

RIGHT ENGINE CONTROL EICAS MESSAGE.(<P>T/S PER FIM 73-21 FT 878 BLOCK 1, RIGHT PIMU DISPLAYED 353-29A PMA POWER AND 353-29B PMA POWER. FOUND RIGHT STATOR / ROTOR AT FAULT. REMOVED AND REPLACED STATOR / ROTOR IAW B767 AMM 73-21-08. OPS CHECK GOOD IAW AMM 71-00-00. REF LOG PAGE 1174248 FOR STATOR PART INFO.</P><P>STATOR P/N OFF: 87006-9, S/N OFF: HTL1487.</P>)

Part: ROTOR — DEFECTIVE (RT ENGINE) · airframe 80,168 hrs · 21,786 cycles

RIGHT ENGINE EEC C1 - STATUS MESSAGE AFTER START.(<P>FOUND MESSAGE OF PMA POWER ON RIGHT PIMU, MESSAGE CLEARED. RAN ENGINE TO VERIFIED RIGHT ENGINE EEC C1 RETURNS. TRANSFERRED TO DMI 125533 IAW POLAR MEL 73-21-01-05, 300 HOURS TIME DUE 10 APR 2020.</P><P>REF LOG PAGE 1174247 - M1: T/S PER FIM 73-21 FT 878 BLOCK 1, RIGHT PIMU DISPLAYED 353-29A PMA POWER AND 353-29B PMA POWER. FOUND RIGHT STATOR / ROTOR AT FAULT. REMOVED AND REPLACED THE RIGHT ENGINE PMA STATOR AND ROTOR GENERATOR AC IAW B767 AMM 73-21-08. PERFORMED ENGINE RUN IAW B767 AMM 71-00-00. ALL OPS CHECK GOOD AT THIS TIME AND NO FAULTS. THIS CLEARS MDDR 125533. REF LOG PAGE 1174248 FOR STATOR PART INFO. STATOR P/N OFF: 87006-9, S/N OFF: HTL1487.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 80,164 hrs · 21,784 cycles

STATUS MESSAGE RIGHT ENGINE EEC C1.(<P>PIMU FAULT EEC / PIMU CODE DISAGREE. PERFORMED GROUND TEST FOR PIMU IAW AMM 77-35-00. TEST GOOD, MESSAGE CLEARED.</P>)

Part: FIRE DETECTOR — FAULTY (RT ENGINE) · airframe 80,149 hrs · 21,766 cycles

R ENG FIRE LP 1 STATUS MSG.(<P>TRANSFERRED TO MDDR #125120 I.A.W MEL 26-11-01-01, CAT 'C'.</P><P><SPAN>LP&NBSP;</SPAN><SPAN>1191502:&NBSP;</SPAN><SPAN>REMOVED AND REPLACED UPPER AFT FIRE DETECTOR ASSY IAW B767 AMM 26-11-02. PERFORMED FIRE TEST IAW AMM 26-11-01. OPS CHECK GOOD AT THIS TIME. MCC NOTIFIED. PLACARDS REMOVED. THIS CLEARS MDDR 125120.</SPAN></P>)

Part: BATTERY — DISCHARGED (MASTER) · airframe 80,102 hrs · 21,715 cycles

FOUND MAIN BATTERY LOW. SWAPPED SERVICEABLE APU BATTERY WITH MAIN BATTERY IAW AMM 24-31-01 AND 24-31-04. MAIN BATTERY OPS CHECKED GOOD IAW AMM 24-31-01. APU INOPERATIVE DUE TO APU BATTERY DISCHARGED (DDG 49-11-01A). APU BATTERY DISCHARGED (DDG 24-331-01-02). REMOVED AND REPLACED APU BATTERY IAW AMM 24-31-04. OPS CHECKED GOOD.

Part: SIGN — UNSECURE (CABIN) · airframe 80,055 hrs · 21,672 cycles

EXIT SIGN FELL OFF NEAR L1 DOOR.(<P>RESECURED EXIT SIGN NEAR L1 DOOR IAW AMM 33-51-01.<BR /></P>)

Part: RADAR — MALFUNCTIONED (TERRAIN) · airframe 80,032 hrs · 21,658 cycles

TERRAIN INOPERATIVE IN FLIGHT. PERFORMED FIM 34-43 FT 805. NO FAULTS ON WEATHER BITE. RAN AN ADJUSTMENT TEST OF THE WEATHER / TERRAIN IAW AMM 34-43-00. NO FAULTS, SYS TESTS GOOD.

Part: RADAR — MALFUNCTIONED · airframe 80,029 hrs · 21,657 cycles

TERRAIN INOP. PERFORMED FIM 34-43 FT 505. NO FAULTS ON WX BITE. RAN ADJ/TEST ON WX/TERRAIN IAW 34-43-00. NO FAULTS NOTED, SYS TEST NORMAL.

Part: TRANSCEIVER — FAILED (LT RADAR) · airframe 80,021 hrs · 21,653 cycles

LEFT RADAR SYS TILTS DOWN UNCOMMANDED IN FLT. TILT DEGREE ON HSI SHOWS COMMANDED TILT, BUT THE RADAR POINTS DOWN AND PAINTS GROUND CLUTTER. L SYS IS UNRESPONSIVE TO TILT INPUTS. 2ND WRITE UP ON CONSECUTIVE FLIGHTS. REMOVED AND REPLACED THE LT RADAR TRANSCEIVER IAW AMM 34-43-01. BITE CHECKED GOOD. CLEAR TO RETURN TO SERVICE.

Part: APU — FAULTED · airframe 80,019 hrs · 21,652 cycles

APU FAULT WHEN WE ATTEMPTED TO START IT DURING TAXI.ACCOMPLISHED 2 SUCCESSFUL APU STARTS PER AMM 49-41-00. ACCOMPLISHED APU ECU BITE PER AMM 49-61-05. NO STORED FAULTS. OK FOR SERVICE.

Part: TRANSCEIVER — FAILED · airframe 80,019 hrs · 21,652 cycles

RADAR LEFT SYSTEM TILTS ITSELF DOWN AND IS UNRESPONSIVE TO POSITION OF TILT SETTING. SWITCHED TO RIGHT SYSTEM, THEN BACK TO LEFT AND SYSTEM APPEARED TO RESET ITSELF AND WORKED OKAY FOR A MINUTE, THEN TILTED DOWN AGAIN. RIGHT SYSTEM WORK FINE. ACCOMPLISHED TASK 34-43 FIG 806 AND FIG 811 BITE PROCEDURES FOR EXTERNAL FAULTS AND WORK TILT CODE FAULTS. NO STORED FAULTS. ACCOMPLISHED OPERATIONAL TEST OF BOTH LEFT AND RIGHT WEATHER RADAR SYSTEM PER AMM 34-43-00-715-026-002. ALL TESTS OK.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 79,921 hrs · 21,602 cycles

MAIN CABIN DOOR EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE WITH EMERGENCY LIGHT TEST SWITCH OR FLIGHT DECK EMER LIGHT SWITCH ON.(<P>REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PER IAI AMM 33-51-00. OPS TEST GOOD PER IAI AMM 33-51-00, NO FURTHER DEFECTS NOTED AT THIS TIME.&NBSP;</P>)

Part: IDG — MALFUNCTIONED (LT GENERATOR) · airframe 79,902 hrs · 21,593 cycles

LEFT GEN CONT CAUTION LIGHT AT APPROX 50 KTS ON TAKEOFF ROLL, L GEN OFF.(<P>TRANSFERRED TO MDDR 121311 IAW DDG 24-00-01-01, CAT 'B', DUE DATE: 03-DEC-2019. MCC NOTIFIED.</P><P>LP 1112612 - ITEM 2: INSPECTED A/C FOR HIGH ENERGY STOP INSPECTION IAW AMM 05-51-14.</P><P>LP 1112615 - ITEM 3: REMOVED AND REPLACED LEFT ENGINE IDG IAW B767 AMM 24-11-01. OPS CHECK GOOD AT THIS TIME AND NO LEAKS NOTED. THIS ACTION CLEARS MDDR 121311. PLACARDS REMOVED AND MCC NOTIFIED.</P>)

Part: STATUS MESSAGE — ILLUMINATED (LT ENGINE) · airframe 79,901 hrs · 21,592 cycles

LEFT ENGINE CONTROL STATUS MESSAGE.&NBSP;(<P>PERFORMED FIM TASK 71-01-00/201, FOUND 354-27A/B ON PIMU. PERFORMED FIM 71-01-00-810-A88-801, MESSAGE CLEARED. AIRCRAFT FLOWN&NBSP;THRU WEATHER, NO FAULTS NOTED AT THIS TIME.&NBSP;&NBSP;</P>)

Part: IDG — LOW · airframe 79,887 hrs · 21,586 cycles

GEN DRIVE DISC SWITCH FLASHING.(<P>SERVICED IDG OIL TO FULL IAW AMM 12-13-613-027. RAN ENGINE (L/H) PER AMM 71-00-00. IDG OPS CHECKED GOOD PER AMM 24-11-00-715-005. A/C OK FOR CONTINUED SERVICES. MCC NOTIFIED.</P>)

Part: IDG — UNDERSERVICED (LEFT) · airframe 79,878 hrs · 21,580 cycles

L GEN CONT TRIPPED, RESET WAS SUCCESSFUL. FOLLOWED BY SEVERAL FLASHES OF GEN DRIVE LIGHT.(<P>RAN BITE ON BPCU, FAULTS LT IDG LOW OIL PRESSURE. SERVICED IDG IAW AMM 12-13-03, RAN ENG IAW AMM 71-00-00. IDG OPS CHECKS GOOD, NO LEAKS. RE-RAN BPCU BITE, NO FAULTS.</P>)

Part: ANNUNCIATOR — MALFUNCTIONED (RADAR SYS) · airframe 79,847 hrs · 21,564 cycles

WXR/TERR SWITCH BACK LIGHT (REF MDDR #120330).(<P>REMOVED AND REPLACED CAPTAIN'S SIDE WXR/TERRAIN ANNUNCIATOR PANEL IAW B767 AMM 34-46-01, OPS CHECK GOOD. THIS CLEARS DMI 120330.&NBSP;MCC NOTIFIED AND PLACARDS REMOVED.<BR /></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (OIL FILTER) · airframe 79,813 hrs · 21,547 cycles

STATUS MESSAGE: L OIL FILTER.(<P>PERFORMED IDLE ENGINE RUN OF L/H ENG IAW AMM 71-00-00. MESSAGE IS CLEARED WITH NO DEFECTS NOTED AT THIS TIME.&NBSP; &NBSP;</P><P>LP 1089201 - M5: PER MCC REQUEST, REMOVED AND REPLACED #1 ENG&NBSP;SCAVENGE OIL FILTER ELEMENT IAW B767 AMM 79-21-04. PERFORMED ENGINE RUN IAW B767 AMM 71-00-00, NO DEFECTS OR LEAKS NOTED AT THIS TIME.</P><P>LP 1089201 - M6: PERFORMED FIM 79-21 FT 803 TO SHEET 1, FIG 103, ITEM 12. AIRCRAFT REQUIRES CHIP DETECTOR &AMP; SCAVENGE FILTER INSPECTION ON NEXT 5 FLT CYCLES. ITEM TRANSFERRED TO NON-MEL MDDR 120526 FOR TRACKING.</P>)

Part: TRU — MALFUNCTIONED (APU) · airframe 79,715 hrs · 21,492 cycles

APU WON'T START.&NBSP;(<P>TRANSFERRED TO MDDR #119510 IAW DDG 49-11-01A, CAT 'C', DUE DATE: 01-NOV-19. PLACARD INSTALLED. DISPATCH NOTIFIED YM @ 1443Z.</P><P>LP 1101236 - M2: T/S PER FIM 49-11. NEEDS APU TRU, P/N 60B40104-2. DMI #119510 REMAINS OPEN.&NBSP;</P><P>REF LOG PAGE 1057561 ITEM M2; REMOVED AND REPLACED APU TRU OPS CHECK GOOD IAW AMM 24-32-04. THIS CLEARS MDDR 119510.&NBSP;</P>)

Part: EEC — MALFUNCTIONED (LT ENGINE) · airframe 79,614 hrs · 21,435 cycles

LEFT ENGINE EEC C1 STATUS. PERFORMED BITE ON L ENG PIMU, FOUND EEC-CPU FAIL FAULT. PERFORMED FIM 71-01 FT A81 TO ITEM B1. REMOVED AND REPLACED THE STATOR AC GENERATOR IAW AMM 73-21-02. MESSAGE WAS STILL DISPLAYED. REMOVED AND REPLACED THE LT AC GENERATOR ROTOR IAW AMM 73-21-02 AND STATUS MESSAGE DID NOT GO AWAY. T/S DOWN TO LT ENGINE EEC UNIT IAW FIM 71-01 FT 810. REMOVED AND REPLACED THE LEFT ENGINE EEC IAW AMM 73-21-15. OPS CHECKED GOOD IAW AMM 71-00-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 79,600 hrs · 21,418 cycles

RECEIVED "LT ENG STARTER" ALERT ON ALL 3 ENGINE START ATTEMPTS. PERFORMED ENGINE START IAW AMM 71-00-00. ENG STARTED NORMAL, NO MSG PRESENT. OK FOR SERVICE.

Part: BLEED VALVE — FAULTY (APU) · airframe 79,600 hrs · 21,418 cycles

RECEIVED "APU BLEED VALVE" ALERT ON ENGINE START. APU INOP. TRANSFERRED TO MDDR #117950 IAW MEL 49-11-01A, CAT 'C', DUE DATE: 29-SEP-19 LP 1107630 - M3: REMOVED AND REPLACED VALVE APU BLEED IAW AMM 36-11-10, OPS CHECK GOOD. APU BLEED WORKS NORMAL AT THE MOMENT. THIS CLEARS MDDR #117950. MCC NOTIFIED AND PLACARDS REMOVED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 79,600 hrs · 21,418 cycles

RECEIVED "ENG VALVE" ALERT ON MANUAL ENGINE START VALVE ATTEMPT. PERFORMED ENG START IAW AMM 71-00-00. ENGINE STARTED NORMAL, NO MSG PRESENT. OK FOR SERVICE.

Part: GPU — FAILED · airframe 79,523 hrs · 21,336 cycles

AFTER BLOCK IN AT CVG, A BAD DHL GPU CAUSED "APU FIRE LP 2" STATUS MSG.(<P>PERFORMED FIRE TEST OF APU IAW AMM 26-15-00. STATUS MESSAGE CLEARED, NO DEFECTS NOTED AT THIS TIME.&NBSP;</P>)

Part: COVER — CUT (NR 1 ENGINE) · airframe 79,488 hrs · 21,303 cycles

DURING #1 ENG. CHANGE, DISCOVERED 2 INCH CUT IN CONTAINMENT RING OUTER COVER, 5 O'CLOCK POSITION.(<P>PERFORMED REPAIR OF CONTAINMENT RING OUTER COVER IAW AMM 72-32-00, CURE TIME IS 8 HOURS. REF LP 1049527 ITEM M34 FOR REMOVAL OF FILM.&NBSP;</P><P>LP 1049527 - M34: POLYETHYLENE COVER REMOVED FROM REPAIR. NO FURTHER DEFECTS NOTED AT THIS TIME IAW AMM 72-32-00.</P>)

Part: ENGINE — VIBRATION (LEFT) · airframe 79,475 hrs · 21,289 cycles

LEFT ENGINE NIB (N2) REACHED 5.0 AFTER THRUST REDUCED TO IDLE AT TOP OF DESCENT.(<P>C/W FIM TASK 71-05 F/T 852. DEFERRED LEFT ENGINE VIB INDICATION PER DDG 77-31-01 CAT C DMI 114191.</P><P>LP 1049522 - M19: LEFT ENGINE BORESCOPE NOT SUFFICIENT, ENGINE CHANGE CALLED.&NBSP;</P><P>LP 1049522 - M21: REMOVED AND REPLACED LT ENG IAW ATLAS WC A-71-999-04-02. OPS CHECK NORMAL.</P><P>LP 1049525 - M29: REFERENCE LOGPAGE 1049522 ITEM M21, LT ENG REMOVED AND REPLACED. THIS CLEARS DMI 114191. MCC NOTIFIED AND PLACARD REMOVED.&NBSP;</P>)

Part: MONITOR — MALFUNCTIONED (LT ENG VIBRATION) · airframe 79,466 hrs · 21,277 cycles

LEFT ENGINE VIBRATION, 5.0 AT IDLE DESCENT. REMOVED AND REPLACED AVM IAW AMM 77-31-03 CONDITIONER SELF TESTED GOOD. PERFORMED ENGINE VIBRATION SURVEY TEST 6 IAW AMM 71-00-00 (AFTER EVM REPLACEMENT). OPS CHECKED GOOD. FAN 0.8 - LPT - 0.1 - N2 - 1.08. ALL WITHIN LIMITS IAW AMM.

Part: SENSOR — MALFUNCTIONED (ENG VIBRATION) · airframe 79,452 hrs · 21,262 cycles

LEFT ENGINE VIBRATION MONITORING INOPERATIVE. REMOVED AND REPLACED ACCELEROMETER INDICATION, INCORRECT, SPORADIC, AND FLUTTERING. REMOVED AND REPLACED L/H ENG VIBRATION SENSOR IAW AMM 77-31-00. REMOVED AND REPLACED WIRE HARNESS FROM D4214P-J4214P IAW WDM 77-31-11 AND SWPM 20-10-11, VIBRATION STILL HIGH. CHECKED WIRES W355-01TR-20 TO 232R-22 AND W356-01TW-20 TO 232B-22 WITH ACCEPTABLE RESULTS IAW WDM 77-31-11. REACTIVATED ENG 1 ACCELEROMETER IAW AMM 77-31-01 PUTTING SYSTEM BACK IN SERVICE.

Part: ROD — UNSECURE (THRUST REVERSER) · airframe 79,452 hrs · 21,261 cycles

LEFT ENGINE HIGH VIBRATIONS 5.0 N2, WHEN IN IDLE DESCENT CONSISTENTLY.(<P>C/W FIM 77-31 FT 808. INSPECTED ACCESSORIES, ALL SECURED. INSPECTED DUCTS, ALL SECURED. INSPECTED CHIP DETECTOR, FOUND CLEAN. FOUND T/R HOLD OPEN ROD NOT STOWED. STOWED AND SECURED. RAN ENG. PER AMM 71-00-00-862-020-H03. N2 HIGHEST READING WAS 2.7. ACFT OK FOR CONTINUED SERVICE. MCC NOTIFIED.</P>)

Part: CONTROL PANEL — INOPERATIVE (WX RADAR SYS) · airframe 79,448 hrs · 21,257 cycles

LEFT RADAR INOP(<P>REMOVED AND REPLACED WEATHER RADAR CONTROL PANEL ASSY. I,A,W AMM 34-43-02 OPS CHECK GOOD.

Part: SWITCH — FAILED (BLEED AIR SYS) · airframe 79,391 hrs · 21,193 cycles

PRIOR TO DEPARTURE, CENTER BLEED ISOLATION VALVE SWITCH INOP.&NBSP;(<P>SWAPPED APU ISOLATION VALVE SWITCH WITH CENTER BLEED IAW SWPM FOR&NBSP;T/S PER AMM 33-13-00.&NBSP; CENTER ISOLATION SWITCH GOOD.&NBSP;&NBSP;</P>)

Part: CONTROL PANEL — FAULTY (BLEED AIR SYS) · airframe 79,391 hrs · 21,193 cycles

APU BLEED ISOLATION VALVE SWITCH INOP.&NBSP;(<P>DEFERRED APU PER MEL 49-11-01A CAT "C", REF DMI 111285.</P><P>LOG PAGE 1061227 - M2: REMOVED AND REPLACED BLEED CONTROL PANEL IAW AMM 36-11-26. OPS CHECK NORMAL. THIS CLEARS DMI 111285. PLACARD REMOVED AND MCC NOTIFIED.<BR DATA-MCE-BOGUS="1" /></P>)

Part: STARTER — MALFUNCTIONED (LT ENGINE) · airframe 79,363 hrs · 21,159 cycles

DURING LEFT ENGINE START, ENGINE STARTER DISENGAGED AT 5% N2. NO EXCEEDANCES WERE OBSERVED AND THE 2ND ATTEMPT WAS SUCCESSFUL.(<P>PERFORMED GROUND START #1 ENGINE IAW AMM 71-00-00. TEST OK, NO DEFECTS NOTED.</P>)

Part: BLEED VALVE — SLOW (APU) · airframe 79,363 hrs · 21,159 cycles

APU BLEED VALVE CYCLES ABNORMALLY SLOW.(<P>PERFORMED APU BLEED VALVE OPS TEST IAW AMM 36-00-00. OPS CHECK GOOD AT THIS TIME.</P>)

Part: DISPLAY — MALFUNCTIONED (WX RADAR SYSTEM) · airframe 79,340 hrs · 21,135 cycles

WX FAIL DISPLAY ON ND.(<P>PERFORMED LOPERATIONAL TEST OF R/L WX SYS REF AMM 34-43-00 SYS PASSED NO ISSUE. PERFORMED FIM 34-43-TREE 805. R/L WX BIT TEST PASSED.<BR /></P>)

Part: ESCAPE REEL — UNSECURE · airframe 79,335 hrs · 21,128 cycles

ON LANDING REEL CASE OPENED AND ESCAPE REEL FELL. (<P>R&AMP;R DECENT DEVICE "C" IAW AMM 20-11-00 OK FOR SERVICE.<BR /></P>)

Part: SHUTOFF VALVE — ABNORMAL (BLEED AIR SYS) · airframe 79,320 hrs · 21,109 cycles

APU BLEED VALVE LIGHT INOP.(<P>TRANSFER TO MDDR 108320 IAW DDG 36-22-06 CAT C.</P><P>LOG PAGE 893259: REMOVED AND REPLACED APU ISOLATION VALVE IAW AMM 36-11-04 VALVE OPERATIONALLY CHECKED &AMP; LEAK CHECK OK. (P/N 2780539-103, S/N 0701)&NBSP;</P><P>LOG PAGE 893260 REMOVED AND REPLACED APU AIR SUPPLY S/O VALVE IAW AMM 36-11-10 LEAK CHECK AND OPS CHECK OK. PERFORMED T/S PER WDM 36-11-41 PAGE 5 SHEET 3, INSPECTED WIRE W1256-024-22 AND FOUND PIN 7 LOOSE IN CONNECTOR D5874J, SECURED PIN IN PLUG PER SWPM, MDDR # 108320 CLOSED.&NBSP;</P>)

Part: CONNECTOR — NOT SEATED (FIRE BOTTLE) · airframe 79,315 hrs · 21,102 cycles

CARGO BOTTLE 2 AFT SQUIB FAILED SQUIB CONNECTION TEST.(<P>RESEATED CARGO BOTTLE 2 AFT SQUIB CONNECTOR, IAW SWPM 20-60-06,OPS CHECK GOOD IAW AMM 26-23-02-404-106 SEC G.</P>)

Part: SMOKE DETECTOR — DIRTY (CARGO BAY) · airframe 79,315 hrs · 21,102 cycles

AFT CARGO SMOKE DETECTOR FAILED SMOKE TEST.(<P>CLEANED SENSING PORT OF AFT CARGO SMOKE DETECTOR IAW AMM 26-16-00,OPS CHECK GOOD.</P>)

Part: WIRE — DAMAGED (CONTROL PANEL) · airframe 79,315 hrs · 21,102 cycles

EXT POWER " ON" INOP NEEDS RELAMP&NBSP;(<P>FOUND DAMAGED WIRES ON ELECTRICAL POWER CONTROL PANEL, REMOVED AND REPLACED POWER CONTROL PANEL IAW AMM 24-22-01 OPS CHECK GOOD&NBSP;</P>)

Part: SMOKE DETECTOR — DIRTY (CARGO BAY) · airframe 79,315 hrs · 21,102 cycles

FOWARD CARGO SMOKE DETECTORS FAILED SMOKE TEST.(<P>CLEANED SENSING PORT OF FWD CARGO SMOKE DETECTOR IAW AMM 26-16-00,OPS CHECK GOOD.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 79,284 hrs · 21,072 cycles

LT FWD WINDOW ILLUMINATED DURING FLIGHT QRH PROCEDURES OPERATED NORMAL REST OF FLIGHT&NBSP;(<P>ACCOMPLISHED FIM 30-41 FT 803 SYSTEM TEST NORMAL AT THIS TIME VERIFIED LT FWD WINDOW IS HEATING SYS NORMAL&NBSP;</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 79,268 hrs · 21,057 cycles

RT FWD WINDOW HEAT EICAS MESSAGE. FOLLOWED QRH .(<P>PERFORMED OPS CHECK AT RT FWD WINDOW HEAT IAW AMM 30-40-00 NO DEFECTS NOTED AT THIS TIME.</P>)

Part: ANTI-ICE VALVE — MALFUNCTIONED (LT ENGINE) · airframe 79,268 hrs · 21,057 cycles

REPEAT ITEM - LT ENG ANTI-ICE VALVE EICAS MESSAGE FOLLOWED QRH. HAPPENED AFTER TURNING ANTI-ICE OFF LEVELED OFF&NBSP;(<P>REMOVED AND REPLACED LT ENG ANTI-ICE VALVE IAW AMM 30-21-03. INSTALLATION CHECKS OK&NBSP;</P>)

Part: ANTI-ICE VALVE — FAULTY (LT ENGINE) · airframe 79,267 hrs · 21,056 cycles

L ENG ANTI ICE VALVE&NBSP; EICAS MESSAGE FOLLOWED QRH&NBSP; HAPPENED AFER TURNING&NBSP; ANTI ICE OFF&NBSP;(<P>REMOVED AND REPLACED L ENGINE ANTI ICE VALVE IAW AMM 30-21-03 INSTALLATION CHECK OK&NBSP;</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 79,266 hrs · 21,055 cycles

L ENGINE ANTI ICE VALVE&NBSP; EICAS MESSAGE DURING&NBSP; DESCENT AFTER TURNING ENGINE ANTI ICE OFF FOLOWED QRH(<P>PERFORMED L ENGINE&NBSP; TAI TEST&NBSP; IAW AMM 30-21-03 TEST PASSED NO FAULTS NOTED&NBSP;</P>)

Part: BATTERY — FAULTY (MAIN) · airframe 79,257 hrs · 21,044 cycles

MAIN BATTERY CHARGER STATUS MSG. R&R MAIN BATTERY ASSY PER AMM 24-21-01 OPS CHECKS GOOD, STATUS MSG CLEARED OK FOR SERVICE. R&R MAIN BATTERY ASSY PER AMM 24-21-01 OPS CHECKS GOOD, STATUS MSG CLEARED OK FOR SERVICE.

Part: NOT REPORTED — MALFUNCTIONED (FUEL SYSTEM) · airframe 79,260 hrs · 21,047 cycles

ON GND (TAXI) CENTER FUEL TANK QUANTITY INCREASES SLOWLY 0 TO 12. C/W FQIS BITE IAW AMM 28-41-00. NO DEFECTS NOTED PER MCC REQUEST VERIFIED OP0S OF REFUEL AND DEFUEL VALVES VERIFIED FUEL IS IN FACT MIGRATING INTO CENTER TANK FROM WING TANKS FURTHER T/S REQUIRED.

Part: WINDSHIELD — ARCED (L1) · airframe 79,237 hrs · 21,029 cycles

CAPTAINS LOWER WINDOW INTERMITTENTLY ARCING/SPARKING IN FLIGHT. APPEARS TO BE COMING FROM&NBSP; ELECTRICAL STRIP IN WINDOW BURN MARKS PRESENT.(<P>REMOVED AND REPLACED 1L WINDOW IAW B767 AMM 56-11-01-004-039 AND B767&NBSP; AMM 56-11-01-404-017. OPS CHECK GOOD.&NBSP; WINDOW PN OFF 141T4800-13&NBSP; SN OFF H4405&NBSP; &NBSP;PN ON 141T4801-49 SN 3118716</P><P>NOTE- PER MCC REQUEST ALSO REPLACED L1 WINDOW HEAT CONTROL UNIT OPS CHECK OK (PN 624066-5&NBSP; SN OFF 0190-1295 SN ON 083C-450)</P>)

Part: CONNECTOR — LOOSE (ANTI ICE SYSTEM) · airframe 79,220 hrs · 21,017 cycles

DURING DESCENT EICAS MSG "LH ENG ANTI-ICE WHEN SELECTED OFF"&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; NOTE: LP 1024911 - (LAX) PER ATLAS REQUESWT DO INTEGRITY TEST OF PNEUMATIC AND L ENG ANTI-ICE VALVE(<P>MSG CLEARED AND VERIFIED NOT PRESENT. TS THROUGH B767 FIM 30-21 FT 803 PERFORMED BITE TEST OF THE AIR SUPPLY CONTROL UNIT&NBSP; MODULE IAW B 767 AMM 36-23-02-715-001 OPS CHECK GOOD. MSG CLEARED. OK FOR SERVICE&NBSP;</P><P>NOTE: LP 1024911 - (LAX) -&NBSP;CHECKED LH ANTI-ICE SYSTEM PER FIM 30-21 FT 803, FOUND CONNECTOR LOOSE AT ANTI-ICE VALVE. RESECURED SAME. LEAK TEST OF PNEUMATIC SYSTEM REF AMM 71-00-00-795-002-H03 FOUND NO LEAKS AT THIS TIME.&NBSP;</P>)

Part: SHUTOFF VALVE — MALFUNCTIONED (LEFT) · airframe 79,218 hrs · 21,015 cycles

DURING DESCENT EICAS MSG " LH ENG ANTI-ICE" ASSOCIATED VALVE LIGHT ON LH ENG ANTI-ICE AFTER TURNING IT OFF(<P>ASSOCIATED WITH PRSOV EICAS MSG ENG INLET TAI SYS TEST IAW B767 30-21-00-735-001 OPS CHK NORMAL</P><P>(NOTE: SEE ITEM LP 1024907 - 1 - LH BLEED OFF MESSAGE - LH PRSOV REPLACED)</P>)

Part: SHUTOFF VALVE — MALFUNCTIONED (LT ENG BLEED) · airframe 79,218 hrs · 21,015 cycles

EICAS MSG " LH ENG BLEED OFF" &AMP; " LH PACK OFF" APPEARED TWICE DURING CLIMB @ APROX 11,000 FT(<DIV>R&AMP;R PRSOV IAW B767 AMM 36-11-09-002-133-008 LH ENG #1, RAN ENG OPS CHECK NORMAL.</DIV>)

Part: CONTROLLER — MALFUNCTIONED (LT ENG PRV) · airframe 79,217 hrs · 21,014 cycles

"LEFT ENGINE BLEED OFF"," LEFT PACK OFF" CAUTION MESSAGES APPEARED TWICE AT APPROX, 10,000' ON CLIMB OUT. REPEAT WRITE-UP.(<P>T/S PER FIM 36-10 FT 837 REMOVED AND REPLACED LT ENG PRV CONTROLLER PER AMM 36-11-19-004-001-002 RAN ENG AND OPS CHECKS OK FOR SERVICE.</P>)

Part: DUCT — LOW PRESSURE · airframe 79,213 hrs · 21,010 cycles

DURING CRUISE WITH ANTI-ICE ON L DUCT PRESS DROPS TO 5 PSI WITH INTERMITTENT L BLEED OFF EICAS.(<P>T/S PER FIM 36-10 F/T 837. CKD ALL LINES FOR PROPER CONDITION RE-TORQUE ALL B NUTS CKD WIRING CLEANED CONNECTOR RAN ENG NO FAULTS, A/C OK FOR SERVICE.</P>)

Part: DUCT — LOW PRESSURE (PNUMATIC SYS) · airframe 79,212 hrs · 21,009 cycles

W/ ENGINE ANTI-ICE ON LEFT DUCT PRESSURE DROPS TO 7 PSI AND MOMENTARILY L ENG BLEED OFF EICAS(<DIV>NO FAULT SHOWN IN STATUS PG. BITE CHK IN THE AIR SUPPLY BITE MODULE, NO FAULT IAW AMM 36-23-00-715. ITEM CLOSED, OKAY TO CONTINUE.</DIV>)

Part: WARNING MESSAGE — FALSE ACTIVATION (WINDOW) · airframe 79,197 hrs · 21,002 cycles

RIGHT FWD WINDOW EICAS DURING CRUISE AT FL 350. HAPPENED&NBSP; DURING APU COLD START VERIFICATION&NBSP;(<P>PERFORMED PIT CHECK ON RIGHT FWD CONTROLLER FOR WINDOW HEAT IAW AMM 30-41-00. BIT CHECK GOOD AT THIS TIME&NBSP;</P>)

Part: VALVE — MAKING METAL (LT ENGINE) · airframe 79,188 hrs · 20,995 cycles

LH ENG BLEED OFF MESSAGE INTERMITTENT ON TAKEOFF AND CLIMBOUT(<P>TRANSFERRED TO MEL 36-11-08-01-01A, MDDR # 103939 CAT C DUE 15DEC18</P><P>(NOTE:&NBSP; PRV INOP IN OPEN POSITION, HPSOV BLOCKED CLOSED AND FAN AIR VALVE BLOCKED IN THE INTERMEDIATE POSITION PER DDG PROCEDURES) REMOVED AND REPLACED LH PRSOV IAW AMM 36-11-09. OPS CHECK GOOD. THIS CLEARS DMI # 103939 / MCC NOTIFIED. PLACARDS REMOVED AND HPSOV REACTIVATED.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (WINDOW HEAT) · airframe 79,178 hrs · 20,987 cycles

AFTER LANDING: R FWD WINDOW MSG(<P>PERFORMED OPS CHECK R FWD WINDOW HEAT IAW B767 AMM 30-41-00 OPS CHECK GOOD COULD NOT DUPLICATE AT THIS TIME.</P>)

Part: ELT — UNSECURE · airframe 79,171 hrs · 20,978 cycles

PORTABLE ELT TETHER IS NO LONGER SECURED TO THE&NBSP;(<P>REMOVED AND REPLACED ELT IAW AMM AMM 25-63-00</P>)

Part: CONNECTOR — LOOSE (WINDOW HEAT) · airframe 79,147 hrs · 20,955 cycles

RIGHT FWD WINDOW EICAS MESSAGE&NBSP;(<P>NOTED BY MAINTENANCE</P><P>REF LOG PAGE 1024717 ITEM M8; TROUBLESHOT RIGHT WINDOW HEAT FAULT IAW WDM 30-41-12. FOUND CONNECTOR D1668 ON WINDOW LOOSE. RE SECURED CONNECTOR AND OPS CHECK RIGHT WINDOW HEAT IAW AMM 30-41-00. OPS CHECK NORMAL&NBSP;&NBSP;</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (WINDOW HEAT) · airframe 79,123 hrs · 20,939 cycles

R FWD WINDOW EICAS MSG ON LANDING(<P>RESET AND ACCOMPLISHED R WINDOW HEAT BITE IAW AMM 30-40-00 OPS CHECKED&NBSP; NORMAL AT THIS TIME</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT EEC) · airframe 79,114 hrs · 20,933 cycles

LEFT ENGINE EEC C1 STATUS MESSAGE. PERFORMED A PIMU BITE IAW FIM 71-01-00/101. BITE TESTED GOOD. MESSAGE CLEARED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 79,104 hrs · 20,925 cycles

PER FLIGHT CREW DEBRIEF, LT ENG EEC C1 SHOWN IN STATUS PAGE. NO OTHER INDICATIONS CAME WITH IT. LT PIMU & RT PIMU MSG SHOWN IN MX PG. ACCOMPLISHED EICAS RESET IAW AMM 31-41-00-752 FAULT CLEARED. CHKD LRU NO FAULT LOGGED IN MEMORY . ACFT OK TO CONTINUE.

Part: CIRCUIT BREAKER — TRIPPED (COCKPIT) · airframe 79,098 hrs · 20,922 cycles

LT ENG IGNITOR 1 STATUS MESSAGE(<P>FOUND CIRCUIT BREAKER M1 ON P11 PANEL OUT. RESET BREAKER AND PERFORMED ENGINE IDLE RUN IAW AMM 71-00-00 OPS CHECKS GOOD.</P>)

Part: CIRCUIT BREAKER — TRIPPED (COCKPIT) · airframe 79,098 hrs · 20,922 cycles

RT ENGINE IGNITER 1 STATUS MESSAGE(<P>FOUND C/B&NBSP; M2 ON P11 PANEL LEFT OUT. RESET CIRCUIT BREAKER AND PERFORMED ENGINE IDLE RUN IAW AMM 71-00-00 OPS CHECKS OK&NBSP;</P>)

Part: PUMP — MALFUNCTIONED (FUEL SYSTEM) · airframe 79,110 hrs · 20,931 cycles

FUEL MIGRATION TO CENTER TANK FROM UNKNOWN ORIGIN, WHEN CENTER PUMPS WERE TURNED ON, THE CTR LT AND CTR RT FUEL PUMP EICAS MESSAGE DISPLAYED, ORH DIRECTS TO TURN OFF THE PUMPS, NOT ALLOWING FULL USE OF FUEL MIGRATING TO CENTER TANK. OK FOR SERVICE IAW SERVICE LETTER 767-SL-28-035-A.

Part: NOT REPORTED — DAMAGED (LT ENGINE) · airframe 79,072 hrs · 20,912 cycles

L ENG BYPASS EPOXY CHIPPING(<P>TRANSFERRED TO NON MEL 101238.<BR /></P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 79,072 hrs · 20,912 cycles

FWD R WINDOW HEAT EICAS MSG AFTER LANDING(<P>RESET ACCOMPLISHED R WINDOW HEAT BITE TEST IAW AM 30-40-00 OPS NORMAL NO FAULT<BR /></P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 79,065 hrs · 20,904 cycles

RIGHT WINDOW EICAS MESSAGE. PERFORMED TEST AMM 30-41-06-715-001 AND AMM 30-41-765-046. OPS CHECK GOOD AT THIS TIME OK FOR SERVICE.

Part: CONNECTOR — DEFECTIVE (WINDOW HEAT) · airframe 79,064 hrs · 20,903 cycles

RT FWD WINDOW EICAS MESSAGE AFTER LANDING(<P>REPLACED CONNECTOR 28998B IAW AMM 30-41-12SHEET 2 AND SWPM 20-71-11 OPS CHECK NORMAL FOR CONTINUED FOR SERVICE<BR /></P>)

Part: CONNECTOR — NOT REPORTED (COCKPIT) · airframe 79,067 hrs · 20,907 cycles

R FWD WINDOW EICAS AFTER LANDING. REPLACED CONNECTOR 2898B IAW WDM 30-41-12 SHEET 2 AND SWPM 20-71-11. OPS CHECK NORMAL. OK FOR CONTINUED SERVICE.

Part: ANTI-ICE SYSTEM — MALFUNCTIONED (WINDOW HEAT) · airframe 79,059 hrs · 20,898 cycles

R FWD WINDOW INOP. RESET AND ACCOMPLISHED R WINDOW HEAT BITE IAW AMM 30-40-00 OPS NORMAL.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 79,049 hrs · 20,887 cycles

EICAS : R FWD WINDOW MSG(<P>MX TROUBLE SHOOTING IN WORK @ SFO<BR /></P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 79,049 hrs · 20,887 cycles

EICAS RT FWD WINDOW(<P>&NBSP;PERFORMED WINDOW HEAT BITE IAW AMM 30-41-00 TEST PASSED OPS CK GOOD<BR /></P>)

Part: CONNECTOR — DEFECTIVE (WINDOW HEAT) · airframe 79,045 hrs · 20,883 cycles

REPEAT WRITE UP - ON TAXI IN RT FWD WINDOW EICAS . CW WITH QRH AND MSG CLEARED(<DIV>LOG PAGES 0965135-3, LOG PAGE 0965137-07 AND -08 : TS PER WDM 30-41-012 CW CONTINUITY&NBSP; CHECKS FROM R1 WINDOW J1,J5,D1914,D1912 TO WINDOW HEAT CONTROLLER AND FROM CONT PANEL TO R1 WINDOW ALL WIRES CHECKED OK SEE LOG PAGE 0965137-7 FOR CORRECTIVE ACTION - REMOVED AND REPLACED CONN D1914 AND D1912 PER WDM 30-41-12 SHT 2 RT FWD WINDOW HEAT OPS CHECKS OK PER AMM 30-41-00. ALSO, REMOVED AND REPLACED CONNECTOR D2898A PER WDM 30-41-12 SHT 2 WINDOW HEAT OPS CHECKS OK PER AMM 30-41-00 (PN DPX2DA-26575-33B-1401)&NBSP;</DIV>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 79,045 hrs · 20,883 cycles

R FWD WINDOW EICAS(<P>RESET R FWD WINDOW HEAT AND ACCOMPLISHED WINDOW HEAT BITE IAW AMM 30-41-00&NBSP; OPS NORMAL<BR /></P>)

Part: TERMINAL — LOOSE (WINDOW HEAT) · airframe 79,045 hrs · 20,883 cycles

ON TAXI IN RECEIVED R FWD WINDOW EICAS. COMPLIED WITH QRH, MESSAGE CLEARED(<P>T/S PER FIM 30-41 F/T 804. FOUND POWER J1 TERMINALS LOOSE. TIGHTENED TO AMM VALUE 25 IN/LB. ALL OPS CHECKED. OK FOR SERVICE<BR /></P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 79,034 hrs · 20,871 cycles

RT FWD WINDOW EICAS MSG RECEIVED ON TAXI IN. COMPLIED WITH QRH. MSG CLEARED. PERFORMED WINDOW HEAT BITE IAW AMM 30-41-00, NO FAULTS PRESENT.

Part: CONTROLLER — MALFUNCTIONED (COCKPIT) · airframe 79,028 hrs · 20,865 cycles

RT FWD WINDOW EICAS AFTER LANDING, RESET WITH SWITCH. REMOVED AND REPLACED WINDOW HEAT CONTROLLER IAW AMM 30-41-01 OPS CHECKED GOOD.

Part: SHUTOFF VALVE — FAULTY (LT IDG) · airframe 79,016 hrs · 20,852 cycles

LT IDG VALVE STATUS CAME ON IN CRUISE. LT IDG AIR S/O VALVE T/S PER FIM 24-00 FT 802, ALL WIRING CHECK OK. REMOVED AND REPLACED LT IDG AIR S/O VALVE IAW 24-11-01/201. OPS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 79,013 hrs · 20,849 cycles

DURING TAXI IN RT FWD WINDOW HEAT EICAS MESSAGE, COMPLIED WITH QRH AND EICAS MESSAGE CLEARED. ACCOMPLISHED WINDOW HEAT BITE TEST IAW AMM 30-40-00, OPS GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (WINDOW) · airframe 78,972 hrs · 20,805 cycles

RIGHT FWD WINDOW EICAS MESSAGE. RESET THE RT FWD WINDOW, OPS CHECKED NORMAL IAW AMM 30-41-01. SYSTEM OK.

Part: CONTROLLER — MALFUNCTIONED (WINDOW HEAT) · airframe 78,969 hrs · 20,804 cycles

RIGHT FWD WINDOW WARNING ILLUMINATED AFTER LANDING. COMPLIED WITH AP-14378, CHECKED RESISTANCE AT D2898B PINS 4 AND 5. 10.5 OHMS. CHECKED RESISTANCE AT D2898A PINS 19 AND 20. 318 OHMS AT 80 DEG F. REPLACED THE WINDOW CONTROLLER M192 IAW AMM 30-41-01. OPS CHECKED GOOD IAW AMM 30-41-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 78,964 hrs · 20,798 cycles

EICAS MSG "RT FWD WINDOW". CYCLED CIRCUIT BRAKER IAW AMM 20-60-01, C/W BITE CHECK IAW AMM 30-41-01. NO FAULTS NOTED. OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 78,952 hrs · 20,786 cycles

EICAS RT FWD WINDOW. OPERATIONAL TEST IAW AMM 30-41-00, OPS CHECK NORMAL.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 78,945 hrs · 20,780 cycles

RT WINDOW(HEAT) AMBER CAUTION MESSAGE AFTER LANDING. PERFORMED OPS CHECKS ON WINDOW HEAT SYSTEM IAW AMM 30-41-00 OPS CHECK GOOD AT THIS TIME. A/C OK FOR SERVICE.

Part: UNKNOWN — MALFUNCTIONED (WINDOW HEAT) · airframe 78,939 hrs · 20,772 cycles

RT FWD WINDOW HEAT INOP ON TAXI IN. PERFORMED OPS CK ON WINDOW HEAT SYS IAW AMM 30-41-00, OPS CKD GOOD.

Part: UNKNOWN — MALFUNCTIONED (WINDOW HEAT) · airframe 78,937 hrs · 20,769 cycles

RT FWD WINDOW HEAT INOP ON TAXI IN. PREFORMED OPS CHECK ON WINDOW HEAT SYSTEM IAW AMM 30-41-00. OPS CHECK GOOD AT THIS TIME OK FOR SERVICE.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 78,936 hrs · 20,768 cycles

STATUS MESSAGE AFT EQUIPMENT EXHAUST FAN. T/S IAW FIM 21-26 FT 805, OPS CHECK NORMAL NO FAULTS FOUND.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 78,913 hrs · 20,735 cycles

APU FAULT DURING PUSHBACK/ENGINE START. INSTALLED AND TESTED SERVICEABLE APU IAW AMM REV 124 49-11-01 AND WORK CARD A-49-999-00-01. OPS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 78,904 hrs · 20,722 cycles

"RT FWD WINDOW" EICAS MESSAGE. CYCLED RT FWD WINDOW HEAT SWITCH AND PERFORMED WINDOW HEAT TEST IAW AMM 30-41-00. NO FAULTS NOTED AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 78,898 hrs · 20,714 cycles

RT FWD WINDOW EICAS MESSAGE DURING LANDING. CYCLED RT FWD WINDOW HEAT SWITCH, OPS CHECK GOOD IAW AMM 30-41-00 NO FAULTS NOTED AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 78,894 hrs · 20,708 cycles

RT FWD WINDOW HEAT ILLUMINATED AFTER LANDING. PERFORMED BITE TEST R1 AND L1 WHCU NO FAULTS FOUND. CHECKED CONTINUITY AND SHORTED TO GROUND FROM R1 WINDOW TO WHCU VISUALLY INSPECTED THE WIRE BUNDLE AT RACK 4 E 2-1 AND T8 124. NO DEFECTS NOTED OPS CHECKED GOOD IAW AMM 30-41-00 AND WDM 30-41-12.

Part: CONTROLLER — FAULTY (WINDOW HEAT) · airframe 78,893 hrs · 20,706 cycles

RT FWD WINDOW HEAT INOP LIGHT ILLUMINATED UPON LANDING. REMOVED AND REPLACED WINDOW HEAT CONTROLLER FOR RT FWD AND LEFT SIDE PER AMM 30-40-01. OPS CHECKS GOOD.

Part: DETECTOR LOOP — DEFECTIVE (CARGO BAY) · airframe 78,877 hrs · 20,683 cycles

FWD CARGO DET 2 STATUS MSG DISPLAYED. REMOVED AND REPLACED NR 2 BLOWER IAW AMM 26-16-02. REMOVED AND REPLACED FWD CARGO DETECTOR LOOP 2 IAW AMM 26-16-01. OPS CK NORMAL.

Part: PAD — LOOSE (RT ENGINE) · airframe 78,847 hrs · 20,652 cycles

RIGHT ENGINE ISOLATION PAD LOOSE. RE INSTALLED ATTACHED ENGINE ISOLATION PAD PER SP. OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (WINDOW) · airframe 78,832 hrs · 20,637 cycles

RIGHT FWD WINDOW EICAS AFTER LANDING. INSPECTED THE WINDOW IAW AMM 56-11-01. FOUND NO ABNORMALITY. OPS CHECKED NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (CHARGER) · airframe 78,774 hrs · 20,577 cycles

BATTERY CHARGER STATUS INDICATED. COMPLETED FIM 24-31 FT 003 SYSTEM TEST. TESTED OK.

Part: SEAL DEPRESSOR — DAMAGED (FUSELAGE) · airframe 78,733 hrs · 20,536 cycles

RAMP CREW REPORTED MAIN CARGO DECK LWR FWD AFT SEAL DEPRESSOR PUSHED IN. REWORKED MAIN CARGO DOOR LWR FWD AND LWR AFT SEAL DEPRESSOR AS REQUIRED PER SRM 53-00-15-1A.

Part: WARNING MESSAGE — INTERMITTENT (RT EEC) · airframe 78,709 hrs · 20,511 cycles

RIGHT ENGINE EEC C1 MESSAGE. PERFORMED EICAS SYSTEM BITE CHECK AND CIRCUIT BREAKER RESET FOR THE RT ENG EEC C1 MESSAGE. NO MESSAGE FOUND AND PERFORMED ENGINE RUN IAW 71-00-00, ALL SYSTEM OPS CHECKED NORMAL.

Part: PIMU — INOPERATIVE (LEFT) · airframe 78,708 hrs · 20,510 cycles

POST FLIGHT FOUND THE LT PIMU M1413 INOPERATIVE. REMOVED AND REPLACED THE PIMU IAW 77-35-02-404-006-H00. OPS CHECKED GOOD.

Part: ACOUSTIC LINER — DAMAGED (NR 1 ENGINE) · airframe 78,623 hrs · 20,442 cycles

NR 1 ENGINE, BETWEEN THE 9 & 12 O'CLOCK ACOUSTICAL PANEL HAS A 3 INCH DIAMETER HOLE. REMOVED AND REPLACED THE ACOUSTICAL LINER SEGMENT IAW AMM 72-33-01.

Part: BLEED AIR SYS — INOPERATIVE (APU) · airframe 78,598 hrs · 20,422 cycles

APU AIR INOPERATIVE. COMPLIED WITH MAINTENANCE PROCEDURE 36-11-04, APU BLEED VALVE SECURED.

Part: BLEED AIR SYS — INOPERATIVE (APU) · airframe 78,596 hrs · 20,420 cycles

NO DUCT PRESSURE AVAILABLE ON APU FOR ENGINE START. RESTARTED APU AND OPS CHECKED OK. GOOD FOR SERVICE IAW AMM 49-10-00.

Part: APU — MALFUNCTIONED · airframe 78,596 hrs · 20,420 cycles

RETURNED DUE TO NO APU AIR FOR START. STARTED APU & VERIFIED APU DUCT PRESSURE SUFFICIENT IAW AMM 49-10-00, OPS NORMAL.

Part: ENGINE — FOD (NR 1) · airframe 78,444 hrs · 20,292 cycles

FOD IN THE LEFT ENGINE DURING POST FLIGHT WALK AROUND. INSPECTED THE NR 1 ENGINE IAW AMM 71-00-00-216. FOUND AND REMOVED PLASTIC FROM COLD SECTION OF ENG.

Part: PACKING — LEAKING (APU FUEL FILTER) · airframe 78,416 hrs · 20,271 cycles

ON ARRIVAL, FOUND THE APU FUEL FILTER HOUSING LEAKING. REPLACED THE PACKING ON THE HOUSING, IAW AMM 49-31-04-004-001, AND 49-31-04-404-006. LEAK CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 78,381 hrs · 20,241 cycles

EICAS MESSAGE FOR CABIN ALTITUDE AUTO 1. PERFORMED A BITE TEST IAW FIM 21-31 FT 809, MESSAGE CLEARED , AIRCRAFT OK FOR SERVICE.

Part: APU — MALFUNCTIONED · airframe 78,369 hrs · 20,229 cycles

ON ENGINE SHUTDOWN, APU FAILED. GPU WOULDN`T HANDLE A/C ELECTRICAL LOAD. ACCOMPLISHED APU ECU BITE CHECK, NO FAULTS FOUND, RAN APU UNDER LOAD AND CHECKED ECU, NO FAULTS FOUND. OPS CHECKED GOOD IAW FIM 49-11 F/T 958</DIV>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT WINDOW HEAT) · airframe 78,368 hrs · 20,228 cycles

RIGHT FWD WINDOW MESSAGES. PERFORMED WINDOW HEAT TEST IAW AMM 30-41-00 & 501. SYSTEM OPS CHECKED GOOD, WINDOW HEAT NORMAL.

Part: CONTROLLER — MALFUNCTIONED (CABIN TEMP) · airframe 78,295 hrs · 20,175 cycles

EICAS MESSAGE AFT CABIN TEMP. REMOVED AND REPLACED CABIN ZONE TEMP CONTROLLER IAW AMM 21-61-03. OPS CHECKED GOOD.

Part: CONTROLLER — MALFUNCTIONED (NR 1 ENGINE) · airframe 78,292 hrs · 20,172 cycles

NR 1 ENGINE HIGH PRESSURE CONTROLLER FAILED PART 2 ITEM 6H OF EO6736A005_CS. REMOVED AND REPLACED THE PRESSURE CONTROLLER IAW AMM36-11-08-404-014-007.

Part: CONTROLLER — MALFUNCTIONED (NR 1 ENGINE) · airframe 78,292 hrs · 20,172 cycles

NR 1 ENGINE PRESSURE REGULATING VALVE CONTROLLER FAILED PART 3 ITEM 7 OF EO 6736A005_CS. REMOVED AND REPLACED THE NR 1 ENGINE PRESSURE REGULATING VALVE CONTROLLER IAW AMM 36-11-08-004-006-007, LEAK CHECKED GOOD.

Part: HEATER — NO TEST (CARGO BAY) · airframe 78,292 hrs · 20,172 cycles

UNABLE TO GET EICAS MESSAGE, AFT CARGO HEAT DURING TEST. FOUND RELAY CABLES K229 AND K790 SWAPPED, CHECKED WIRING AND PIN ON CONNECTOR DB0694 RELAY K229 IAW WDM 21-44-11, PG 2. OPS CHECKED GOOD.

Part: CONNECTOR — DAMAGED (INTERCONNECTOR) · airframe 78,292 hrs · 20,172 cycles

FAIL, MANIFOLD INTERCONNECT VALVE IS NOT OPENING. TROUBLESHOT AND INSPECTED CONNECTORS D3058, D20360, FOUND PIN 4 OF D3058 RECESSED, SECURED PIN 4 IAW SRM 21-58-02, OPS CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (BS 1420-1540) · corrosion level 2 · airframe 78,292 hrs · 20,172 cycles

BULK CARGO FLOOR SUPPORT LT SIDE BS 1421, LBL 34 HAS CORROSION. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-40-05-0G-0.

Part: SENSOR — MALFUNCTIONED (LT A/C PACK) · airframe 78,292 hrs · 20,172 cycles

LEFT PACK PRIMARY HEAT EXCHANGER IN TEMP INDICATION IS MISSING FROM EICAS SCREEN. REMOVED AND REPLACED AIR TEMP BULB SENSOR TS433 IAW WOM 21-57-31. OPS CHECKED GOOD.

Part: WIRE — DAMAGED (FUSELAGE) · airframe 78,292 hrs · 20,172 cycles

WIRE DAMAGED AT BS 632 LEFT SIDE WALL. REMOVED THE DAMAGED WIRES W1274-120-20 IAW SWPM 20-30-12.

Part: REGULATOR — FAILED (NR 2 ENGINE) · airframe 78,292 hrs · 20,172 cycles

NR 2 ENGINE PRESSURE REGULATING VALVE CONTROLLER FAILED PART3 ITEM 7 OF EO6736A005-CS. REMOVED AND REPLACED THE NR 2 ENGINE PRESSURE REGULATING VALVE IAW AMM 36-11-19-004-001-002, OPS CHECKED GOOD.

Part: MOUNT — GOUGED (AFT CARGO DOOR) · airframe 78,292 hrs · 20,172 cycles

LOWER AFT PORTION OF AFT CARGO DOOR HAS A GOUGE ON THE DOOR MOUNT. REPAIRED IAW EA 767-5360-28-A6909, REV 2.

Part: FITTING — LEAKING (EXTINGUISHER SYS) · airframe 78,292 hrs · 20,172 cycles

FWD AND AFT FIRE EXTINGUISHER METERED DISCHARGE LINE LEAKING IAW WORK CARD A-26-017-55 STEPS 17C, AND 21C. TORQUED TWO FITTINGS IAW WORK CARD A-26-017-55 STEPS 17C AND 21C, NO LEAKS NOTED.

Part: CONTROLLER — NO TEST (CABIN TEMP) · airframe 78,292 hrs · 20,172 cycles

A-21-025-00-01 STEP 13D,E OF WORK CARD FAILED TRIM VALVE AT FLIGHT DECK IS NOT OPENING. REMOVED AND REPLACED ZONE TEMP CONTROLLER IAW AMM 21-61-03-404-016, OPS CHECKED GOOD.

Part: CHECK VALVE — GOUGED (LT CABIN) · airframe 78,292 hrs · 20,172 cycles

LEFT CABIN AIR SUPPLY CHECK VALVE FLAPPER HAS DEEP GOUGE. REMOVED AND REPLACED LT CABIN AIR SUPPLY CHECK VALVE IAW AMM 21-51-15-404-148.

Part: HEAT SHIELD — CRACKED (PYLON) · airframe 78,292 hrs · 20,172 cycles

PANEL 446BL HEAT SHIELD IS CRACKED. REPAIRED IAW EA 767-5450-28A6911, REV 1, OPTION 1.

Part: EXCHANGER — LEAKING (FUEL/OIL) · airframe 78,292 hrs · 20,172 cycles

NR 1 ENGINE JUST BEHIND AGB 6 O'CLOCK POSITION, HEAT EXCHANGER OIL/FUEL IS LEAKING THROUGH METAL GASKETS. REMOVED AND REPLACED 2EA GASKETS ON FUEL/OIL HEAT EXCHANGER #1 ENGINE PER B767 AMM 79-21-01-024-065 LEAK CHECK GOOD.

Part: WARNING SYSTEM — ILLUMINATED (NR 1 OIL SYSTEM) · airframe 78,292 hrs · 20,172 cycles

OIL FILTER BYPASS WARNING SYSTEM FOR THE NR 1 ENGINE. COMPLIED WITH WORK CARD A-79-310-01-1.

Part: HEAT SHIELD — CRACKED (PYLON) · airframe 78,292 hrs · 2,172 cycles

PANEL 446BL HEAT SHIELD IS CRACKED. REPAIRED IAW EA 767-5450-28A6911, REV 1 OPTION 1.

Part: CIRCUIT CARD — UNSECURE (FIRE LOOP) · airframe 78,292 hrs · 20,172 cycles

EICAS SCREEN SHOWS APU FIRE LOOP 2 MESSAGE. FOUND FIRE LOOP 2 CARD UNSECURE. REMOVED AND REINSTALLED THE APU NR 2 FIRE LOOP. OPS CHECKED GOOD IAW FIM TASK 26-15, AND WDM 26-15-11.

Part: PRECOOLER — CORRODED (NR 2 ENGINE) · airframe 78,292 hrs · 20,172 cycles

NR 2 ENGINE PRE-COOLER EXHAUST SIDE COOLING FINS CORRODED AND MISSING(<P>REMOVED AND REPLACED #2 ENGINE BLEED PRE-COOLER PER B767 AMM 36-11-15-404-117-004</P>)

Part: FRAME — CORRODED (BS 1407) · corrosion level 2 · airframe 78,292 hrs · 20,172 cycles

BULK CARGO DOOR SILL FWD FRAME LOWER END HAS CORROSION AT BS 1407. REMOVED, FABRICATED, AND INSTALLED EDGE MEMBER ON BULK CARGO DOOR SILL IAW SRM 51-40-05-0G-0 PG3.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 78,292 hrs · 20,172 cycles

NR 1 ENGINE HYDRAULIC PUMP (EDP) LEAKING THROUGH ITS BODY. CLEANED THE NR 1 ENGINE EDP IAW AMM 12-25-01-001. RAN THE NR 1 ENGINE WITH NO LEAKS.

Part: SENSOR — MALFUNCTIONED (LT A/C PACK) · airframe 78,292 hrs · 20,172 cycles

LEFT PACK PRIMARY HEAT EXCHANGER IN TEMP INDICATION IS MISSING FROM EICAS SCREEN. REMOVED AND REPLACED AIR TEMP BULB SENSOR TS433 IAW WDM 21-52-31, OPS CHECKED GOOD.

Part: SPRING — FAILED (FLAPPER VALVE) · airframe 78,292 hrs · 20,172 cycles

LEFT ISOLATION BYPASS VALVE FLAPPER SPRING IS BROKEN. REMOVED AND REPLACED LT ISOLATION BYPASS VALVE IAW AMM 36-11-05-404-009</P>)

Part: SENSOR — FAILED (PACK TEMP) · airframe 78,280 hrs · 20,165 cycles

RIGHT PACK TEMP EICAS. THE TEMP CONTROLLER FAULTED MIX MANIFOLD SENSOR, REMOVED AND REPLACED MIX MANIFOLD SENSOR IAW AMM 21-61-02, OPS CHECKED GOOD.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 78,258 hrs · 20,144 cycles

CABIN ALTITUDE AUTO 2 EICAS MESSAGE. REMOVED AND REPLACED AUTO PRESSURE CONTROLLER IAW AMM 21-31-02. OPS CHECKED NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENG EEC) · airframe 78,236 hrs · 20,115 cycles

STATUS MESSAGE FOR THE LT ENGINE EEC. TROUBLESHOT LEFT ENGINE EEC IAW FIM 73-21 FT 885, CLEARED BITE PIMU, COMPLIED WITH ENGINE RUNS IAW AMM 71-00-00. OPS CHECKED GOOD & NO DEFECTS NOTED.

Part: WARNING MESSAGE — INTERMITTENT (SPAR VALVE) · airframe 78,201 hrs · 20,073 cycles

NR 1 ENGINE SPAR VALVE INDICATION INTERMITTENT.

Part: LAMP — INOPERATIVE (SPAR VALVE) · airframe 78,185 hrs · 20,053 cycles

LEFT ENGINE SPAR VALVE FAILED OPERARTIONAL CHECK. THE ENG SPAR VALVE LAMP WAS REPLACED. OPS CHECHED OK IAW AMM 28-22-00, NO FAULTS FOUND.

Part: WARNING MESSAGE — FALSE ACTIVATION (EXHAUST FAN) · airframe 78,180 hrs · 20,047 cycles

STATUS MESSAGE FOR THE FWD EQUIPMENT EXHAUST FAN. PERFORMED FIM 21-58-FT905. EQUIPMENT COOLING CONTROL SWITCH CYCLED & FWD EQUIPMENT EXHAUST FAN FUNCTIONED SERVICEABLE.

Part: COOLING FAN — MALFUNCTIONED (E&E BAY) · airframe 78,170 hrs · 20,037 cycles

AFT EQ EXH FAN 1 STATUS MSG. REMOVED AND REPLACED NR 2 AFT EQ COOLING FAN IAW SUPP 21-51-41. OPS CK GOOD AT THIS TIME MDDR IS CLOSED.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 78,164 hrs · 20,030 cycles

STATUS MESSAGE FOR THE FWD EQUIPMENT EXHAUST FAN FIM 21-58, FAULT TREE 905, EQUIPMENT COOLING CONTROL SWITCH CYCLED AND OPS TESTED SERVICEABLE.

Part: DRIVE UNIT — MALFUNCTIONED (WEATHER RADAR) · airframe 78,133 hrs · 20,000 cycles

RIGHT WEATHER FAIL ANNUNCIATED IN FLIGHT. REMOVED AND REPLACED RT SIDE WEATHER RADAR TRANCEIVER, OPS CHECKED GOOD IAW 34-43-01, REMOVED AND REPLACED WEATHER RADAR ANTENNA DRIVE UNIT, OPS CHECKED GOOD IAW AMM 34-43-05.

Part: RADAR — MALFUNCTIONED (WEATHER RADAR) · airframe 78,128 hrs · 19,995 cycles

WITH WX RADAR SYS R SELECTED, WXR R FAIL. PERFORMED GROUND OPERATIONAL CHECK & RT WX SYSTEM TEST OK IAW AMM 34-43-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 78,100 hrs · 19,966 cycles

WXR FAIL ON BOTH ND AND ON SYSTEM L AND R. BOTH WXR TESTED IAW AMM 34-43-00/501, NO FAULTS FOUND, CHECKS SERVICEABLE.

Part: OXYGEN MASK — LEAKING (CABIN) · airframe 78,077 hrs · 19,945 cycles

OXYGEN MASK FOR SUPERNUMERARY POSITION NR 1 HAS LEAK TO HEAD HARNESS. REPLACED OXYGEN MASK ASSY IAW AMM 35-11-08 OPS AND LEAK CHECKED OK.

Part: BLADE — NICKED (NR 2 ENGINE) · airframe 78,042 hrs · 19,930 cycles

NICK FOUND IN FAN BLADE IN NR 2 ENGINE. BLADE 1/16" NICK 5.5" FROM TIP. BLADE BLENDED & FOUND WITHIN LIMITS IAW AMM 72-31-02.

Part: ACTUATOR — INOPERATIVE (SHUTOFF VALVE) · airframe 78,012 hrs · 19,922 cycles

SPAR VALVE DID NOT CYCLE DURING LEFT ENGINE START. REPLACED THE LT ENGINE FUEL SHUTOFF VALVE ACTUATOR IAW AMM 28-22-11. OPS CHECKED NORMAL.

Part: UNKNOWN — LEAKING (UNKNOWN) · airframe 78,012 hrs · 19,922 cycles

DURING WALK AROUND INSPECTION, FIRST OFFICER NOTED OIL LEAKING FROM LEFT ENGINE. PERFORMED INSPECTION OF EXTERNAL & INTERNAL ON LEFT ENGINE, NO OIL LEAK EVIDENCE FOUND AMM 79-00-00/601. ACFT OK TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (CABIN TEMP) · airframe 77,988 hrs · 19,917 cycles

UNABLE TO CONTROL FWD AND AFT CABIN TEMPERATURE CONTROLLERS, TEMP WAS 27* ON FULL COLD. BOTH PACK OPERATION CHECKED NORMAL IAW AMM 21-51-00 / 001.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENGINE BLEED) · airframe 77,939 hrs · 19,899 cycles

LEFT ENGINE BLEED OFF, ADVISORY MESSAGE DISPLAYED DURING DESCENT ON SEVERAL OCCASIONS. PERFORMED FIM 36-10 FAULT TREE 838. HPSOV AND PRV PFM THUMB TEST. TESTED OK. CHECKED LINE AND FITTINGS, NONE LOOSE OR DAMAGED. PFM ENGINE RUN CHECKED. NO FAULTS FOUND.

Part: CONTROL PANEL — INOPERATIVE (WX RADAR SYS) · airframe 77,686 hrs · 19,667 cycles

FIRST OFFICER WEATHER RADAR INOPERATIVE. REMOVED AND REPLACE EFIS CONTROL PANEL. OPS TESTED OK IAW AMM 34-22-02 AND AMM 34-43-00.

Part: SWITCH — DISLODGED (WX RADAR SYS) · airframe 77,691 hrs · 19,671 cycles

F/O WEATHER RADAR SELECT SWITCH DISLODGED. RESEATED THE SWITCH, SYSTEM TESTED NORMAL AMM 34-43-00.

Part: APU — INOPERATIVE (APU BAY) · airframe 77,677 hrs · 19,656 cycles

REF MDDR 68830, APU INOPERATIVE PERFORMED BITE TEST ON BPCU IAW AMM 24-20-001. OPS CHECK GOOD. CLEARED MDDR 68830 PLACARD. REMOVED APU OPS CHECK OK IAW AMM 49-00-00.

Part: BUTTON — STUCK (WX TRANSCEIVER) · airframe 77,672 hrs · 19,652 cycles

F/O'S WXR/TERR PUSH BUTTON IS STUCK. WEATHER RADAR TRANSCEIVER PUSH BUTTON REMOVED AND SET PROPERLY AND IS OK FOR SERVICE, GROUND TESTED OK. RETURNED TO SERVICE IAW AMM 34-43-00.

Part: LATCH — UNSECURE (RT NACELLE) · airframe 77,657 hrs · 19,633 cycles

RIGHT PYLON LATCH OPENED IN FLIGHT. SECURED THE NR 2 PYLON LATCH IAW AMM 70-00-00. NO DEFECTS NOTED WITH LATCH, OK TO CONT SERVICE.

Part: TRANSMITTER — OUT OF ADJUST (LE SLAT) · airframe 77,624 hrs · 19,599 cycles

L/E SLAT DISAGREE ON FINAL AT APPROXIMATELY 180 KNOTS EICAS LIGHT OUT UPON GO AROUND TO FLAPS 20. CHECKED ALL TRANSMITTERS IAW AMM 27-51-45 TRANSMITTERS 1 AND 8 FOUND OUT OF RANGE, ADJUSTED NR 1 AND NR 8 TRANSMITTERS IAW AMM 27-51-45. OPS CHECK GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (EQUIP COOLING) · airframe 77,546 hrs · 19,514 cycles

"FWD EQUIPMENT COOLING" AND OVERHEAT LIGHT ON 3 MINUTES AFTER TAKEOFF. TROUBLESHOT FWD EQUIPMENT COOLING OVERHEAT LIGHT, CHECKED BOTH FANS CHECK GOOD IAW AMM 21-58-02. CHECKED ALL VALVES, ALL VALVES CHECK GOOD IAW AMM 21-58-4, 21-58-05, 21-58-07, 21-58-08. CHECK ALL DUCTS FOR LEAK NO LEAKS NOTED IAW AMM 21-20-11. NR 10 - FOUND RESTRICTOR PLATE INSTALLED AFTER HEAT EXCHANGER SHUTOFF VALVE BEFORE THE SKIN HEAT EXCHANGER, CHECKED IPC AND IAI MOD, FOUND NO REF TO BE INSTALLED, REMOVED AND OPS CHECKED GOOD IAW AMM 21-58-00. REMOVED PN 214T3436-714.

Part: CIRCUIT CARD — MALFUNCTIONED · airframe 77,544 hrs · 19,511 cycles

FWD EQUIPMENT COOLING EICAS MESSAGE CAME ON AT TOP OF CLIMB, WITH OVERHEAT LIGHT. R & R COOLING INDICATION CONTROL CARD IAW AMM 21-58-24-404-010 PERFORMED INSTALLATION TEST. CHECKS GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (EQUIP COOLING) · airframe 77,543 hrs · 19,509 cycles

FORWARD EQUIPMENT COOLING, EICAS MESSAGE ON 2 MIN BEFORE LANDING. DIFFERENTIAL PRESSURE SWITCH IAW AMM 21-52-29, EQUIPMENT COOLING TEST PASSED, NO DEFECTS NOTED AT THIS TIME.

Part: RELAY — MALFUNCTIONED (EQUIP COOLING) · airframe 77,544 hrs · 19,511 cycles

1 MINUTE BEFORE LANDING, FWD EQUIPMENT COOLING, EICAS MSG ON. REPLACED TIME DELAY RELAY K698 ON P36 PANEL REF WDM 21-58-02. OPS CHECK NORMAL AT THIS TIME MCC INFORMED.

Part: SHUTOFF VALVE — MALFUNCTIONED · airframe 77,542 hrs · 19,507 cycles

FWD EQUIPMENT COOLING EICAS MSG ON RT AFTER TAKEOFF. R & R 3-WAY SHUTOFF VALVE IAW AMM 21-58-01/401. PERFORMED OPS TEST EQUIPMENT COOLING SYS IAW AMM 21-58-00, TEST GOOD ON GROUND.

Part: COOLING FAN — FAILED · airframe 77,540 hrs · 19,506 cycles

FWD EQUIPMENT COOLING EICAS MESSAGE CAME ON SHORTLY AFTER TAKEOFF, STBY MODE SELECTED, MESSAGE EXTINGUISHED AND CAME BACK ON IN 5 MINUTES. OVERRIDE MODE SELECTED. MESSAGE WENT OUT UNTIL JUST BEFORE LANDING. R & R EXHAUST FAN B-12 IAW FIM 21-58, FT 902, BLOCK 50 AND AMM 21-58-06. PERFOMED OPS CHECK NORMAL ON GROUND AT THIS TIME. LP 800759-5 - ADDITIONAL TS PERFORMED IAW SSM 21-58-00 CONFIRMED COMPONENT CONDITION FOR EQUIPMENT COOLING SYSTEM FOR ACFT ON GROUND TEMP GREATER THAN 45 DEG F. OPS IN AUTO/STBY AND OVRIDE MODE. OPS CHECKS OF MANIFOLD/OVERRIDE VALVE, SUPPLY, EXHAUST FANS/ALL VALVES OPERATION NORMAL ON GROUND IAW AMM 21-58-00, CONFIG 6, PAGE 514.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 77,536 hrs · 19,501 cycles

DURING CLIMB EICAS MSG EQUIPMENT OVERHEAT FOLLOWED PROCEDURE FIM 21- 58 FAULT TREE 902 COULD NOT DUPLICATE ON GROUND. OPS CHECK GOOD AT THIS TIME.

Part: CIRCUIT CARD — INOPERATIVE (OVERHEAT DETECT) · airframe 77,526 hrs · 19,491 cycles

FWD EQUIPMENT OVERHEAT EICAS ; COMPLIED WITH QRH PROCEDURE. MSG EXTINGUISHED AFTER SELECTING OVERHEAD AUTO AFTER 30 MINUTES. R & R IN EC5 CONTROL CARD IAW AMM 21-58-42.

Part: WARNING MESSAGE — FALSE ACTIVATION (EQUIPMENT COOL) · airframe 77,523 hrs · 19,488 cycles

FWD EQUIPMENT COOL, EICAS, OPERATED IN OVERHEAD. CW FIM 21-58, FT 902 COULD NOT DUPLICATE ON GROUND OPS CHECK GOOD AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION (APU GEN) · airframe 77,515 hrs · 19,480 cycles

APU GENERATOR FELL OFF LINE TWICE WHEN PRESSURIZING SYS. PERFORMED APU OPS CHECK IAW AMM 49-11-00. OPS CHECKED GOOD AT THIS TIME, LP 800458-3. CW APU ECU SELF AND BITE TEST IAW AMM 49-61-05, NO FAULTS NOTED. CW BPCU BITE TEST IAW AMM 24-22-00 NO FAULTS NOTED. PERFORMED OPS CHECK OF APU GENERATOR, NO FAULTS NOTED IAW AMM 24-21-00. ACFT OK FOR CONTINUED ETOPS SERVICE.

Part: LIGHT — INOPERATIVE (PRESSURE GAUGE) · airframe 77,464 hrs · 19,417 cycles

DUCT PRESSURE GAUGE BACK LIGHT INOPERATIVE. R & R DUCT PRESSURE GAUGE IAW AMM 36-21-02, OPS CK GOOD.

Part: CLUTCH — FAILED (APU STARTER) · airframe 77,458 hrs · 19,408 cycles

APU WILL NOT START. R & R STARTER CLUTCH IAW 49-41-06, OPS NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT FIRE LOOP) · airframe 77,458 hrs · 19,408 cycles

STATUS MESSAGE, RT ENGINE FIRE LP1, PERFORMED FIM 26-11 TR 804/805, ALL PASSED GROUND CKS.

Part: CONTROLLER — MALFUNCTIONED (LT ENGINE) · airframe 77,458 hrs · 19,408 cycles

STATUS MSG, LT ENGINE PRV PERFORMED FIM 36-10, TK847, PRV OPS CK ON GROUND NORMAL. CVG: R & R LT ENGINE PRV CONTROLLER IAW AMM 36-11-18, OPS AND LEAK CHECK GOOD, NO DEFECTS NOTED. SN 981007, PN 792755-15. LP 739567, ORD: R & R NR 1 ENGINE PRV IAW AMM TASK 36-11-18-404-018-001, OPS CHECKED OK AT THIS TIME.

Part: FIRE LOOP — FALSE ACTIVATION (RT NACELLE) · airframe 77,458 hrs · 19,408 cycles

RIGHT ENGINE FIRE LP 1, STATUS MESSAGE. REPLACED UPPER FIRE LOOP, LOWER FWD FIRE LOOP, LOWER AFT FIRE LOOP. R & R WIRES ON RT ENGINE LOOP 1 AND PERFORMED CHECK OF RT ENGINE FIRE DETECTION SYS IAW AMM 26-11-00. CHECKED GOOD.

Part: WINDOW — CRAZED (COCKPIT) · airframe 77,441 hrs · 19,403 cycles

COCKPIT NR 1 RT WINDOW ANTI-ICING WINDSHIELD TOP AND MID SUSPECT SIGNS OF HEATING AND AT RT SIDE OF THE WINDOW MID AREA FOUND SIGNS OF CRAZING. REPLACED RT NR 1 WINDOW IAW AMM 56-11-01, REV 116 CHECKED IAW AMM 30-41-00, REV 116.

Part: TRANSMITTER — NO TEST (FUEL SYSTEM) · airframe 77,441 hrs · 19,403 cycles

ENGINE NR 2 FUEL TRANSMITTER FAILED IN TEST. REPLACED FUEL TRANSMITTER IAW AMM 73-31-01, REV 116.

Part: BRACKET — BROKEN (FIRE LOOP) · airframe 77,440 hrs · 19,403 cycles

AFT STABILIZER COMPARTMENT BS 1809-1829, LT FOUND FIRE LOOP DETECT BRACKET SUPPORT LOOSE, NRC MO446. INSTALL NEW FASTENER IAW SRM 51-40-02, FASTENER CODE MS20470AD4-5.

Part: CIRCUIT CARD — UNKNOWN · airframe 77,444 hrs · 1,940,426 cycles

STATUS MESSAGE RT ENGINE FAIL LOOP 1. REPLACED THE CARD ASSY FIRE OVERHEAT IAW AMM 26-10-01.

Part: DETECTOR — NO TEST (LOW FLOW) · airframe 77,440 hrs · 19,403 cycles

FLIGHT DECK LOW FLOW DETECTOR, TS163 FAIL IN TEST, NRCMO397. REPLACED AND TESTED F/D LOW FLOW DETECTOR, TS163 IAW AMM 21-58-17.

Part: VALVE — NOT REPORTED · airframe 77,444 hrs · 19,404 cycles

IAW CUSTOMER REQUEST NEED TO REPLACE APU SURGE CONTROL VALVE AFTER T/S. REPLACED APU SURGE CONTROL VALVE, PERFORMED OPS TEST OF APU WITH LOAD. LT AND RT PACK FOR 60 MIN. NO PRESSURE DROP APPEARED IAW AMM 49-53-01.

Part: ACTUATOR — FAILED (OUTFLOW VALVE) · airframe 77,441 hrs · 19,403 cycles

DURING OPERATION TEST, OUTFLOW VALVE ACTUATOR FAILED. REPLACED OUTFLOW VALVE ACTUATOR IAW AMM 21-31-04, TEST IAW AMM 21-31-00/501.

Part: STRINGER — DAMAGED (BS 89-111) · airframe 77,440 hrs · 19,403 cycles

STRINGER DAMAGED AT BS 89 - 111, STRINGERS 2R. REPAIRED IAW REA MB01083R0025, REV NEW AND SRM 53-00-03, REPAIR 1.

Part: BULB — BROKEN (OUTLET TEMP) · airframe 77,440 hrs · 19,403 cycles

THE RT PACK OUTLET TEMP BULB IS BROKEN, NRC-C0008. REPLACED THE RT PACK OUTLET TEMP BULB, TS40 AND TESTED IAW AMM 21-52-06.

Part: BULB — BROKEN (TEMP) · airframe 77,440 hrs · 19,403 cycles

THE LT PACK OUTLET TEMP BULB IS BROKEN. REPLACED THE LT PACK OUTLET TEMP BULB, TS39 AND TESTED IAW AMM 21-52-06.

Part: PCB — DAMAGED (SMOKE DETECTION) · airframe 77,440 hrs · 19,403 cycles

LOWER SMOKE DETECTOR TEST STATUS MESSAGE ON EICAS DISPLAY, FWD. DET 1 FWD DET 2, NRC MO404. REPLACED LOGIC/TEST FIRE OVERHEAT. PRINTED CIRCUI ASSY, M10427 AT P-54 PANEL AND TESTED IAW AMM 26-16-00.

Part: HOSE — TORN (E/E BAY) · airframe 77,441 hrs · 19,403 cycles

FWD CARGO E/E COMP AIR EXHAUST NOSE, PN AS1544-6A0071, TORN. REPLACED HOSE IAW AMM 21-58-00, REV 116.

Part: CONTROLLER — FAILED (NR 2 ENGINE) · airframe 77,441 hrs · 19,403 cycles

ENGINE NR 2 HIGH PRESSURE CONTROLLER TEST FAILED IN RUN-UP. REPLACED HIGH PRESSURE CONTROLLER IAW AMM 36-11-08, TESTED DURING RUN-UP, FOUND OK IAW AMM 71-00-00-201.

Part: SHUTOFF VALVE — FAILED (NR 2 ENGINE) · airframe 77,441 hrs · 19,403 cycles

ENGINE NR 2 PRSOV TEST FAILED. REPLACED PRSOV IAW AMM 36-11-09, TESTED IAW AMM 36-23-00/501.

Part: TUBE — DAMAGED (EXTINGUISHER) · airframe 77,441 hrs · 19,403 cycles

AFT CARGO FOUND FIRE EXT. TUBES PN 453T2620-273 AND PN 453T2620-135 DAMAGED. REPLACED TUBES IAW AMM 26-23-11, REV 116 AND CONV J/C 371-26-20-C1361-001.

Part: BULKHEAD WEB — DAMAGED (BS 1582) · airframe 77,440 hrs · 19,403 cycles

AFT PRESSURE BULKHEAD WEB DAMAGED AT BS 1582, APPROXIMATELY RBL 80, WL 270. REPAIRED IAW IAW REA MF01083R0211, REV C.

Part: CLAMP — LOOSE (FIRE LOOP) · airframe 77,457 hrs · 19,406 cycles

STATUS MESSAGE RT ENGINE FIRE LP1. FOUND CLAMPS LOOSE ON FIRE LOOP. TIGHTENED IAW AMM 26-41-00. CKS GOOD.

Part: TUBE — DAMAGED (EXTINGUISHER) · airframe 77,441 hrs · 19,403 cycles

AFT CARGO LT AT BS 1197+66, FOUND FIRE EXT TUBE, DAMAGED. REPLACED TUBE IAW AMM 26-23-11, REV 116.

Part: SKIN — DENTED (BS 412) · airframe 77,440 hrs · 1,940,353 cycles

DENT ON EXTERIOR SKIN BS 412, STRINGERS 29 - 30R. REPAIRED IAW REA MB 01083R0051, REV NEW AND DWG 371-38-32-C1924-003, REV C.

Part: LENS — BROKEN (CABIN) · airframe 76,900 hrs · 19,293 cycles

EMERGENCY LIGHT LENS COVERS ROWS 1R & 1L AFT BROKEN. PLACED ON MDDR 57997 IAW MEL 33-51-03-01.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 76,813 hrs · 19,276 cycles

APU FAULT EICAS MSG ON GND ON FIRST START ATTEMPT AFTER LANDING. PERFORMED APU BITE CHECK & STARTED APU, NO FAULTS FOUND IAW MM 49-61-05-742.

Part: RADAR — FAILED · airframe 76,666 hrs · 19,243 cycles

RIGHT RADAR FAILED IN FLIGHT. REMOVED & REINSTALLED RT WX RECVR IAW AMM 34-43-01401. CONNECTOR OK, COOLING OK, TESTED RT WX OK IAW AMM 34-43-00. OPERATIONS & SYS, NO FAULTS.

Part: PACKING — DAMAGED (NR 1 ENGINE) · airframe 76,537 hrs · 19,217 cycles

NUMBER 1 ENG, NR 1 BEARING MANIFOLD LEAKING OIL. R & R 1 BEARING MANIFOLD PACKING SEAL IAW AMM 72-31-00. NO LEAKS NOTED.

Part: LIGHT — DISCHARGED (CABIN) · airframe 75,537 hrs · 19,217 cycles

AFT GALLEY EMER FLOOR PATH LIGHTS, THREE EACH INOPERABLE. DURING TROUBLESHOOTING FOUND THE LIGHT ASSEMBLY PIN END DISCONNECTED, RECONNECTED THE PIN END TO THE LIGHT ASSEMBLY SOCKET IAW 33-51-05. OPERATIONS CHECKED GOOD.

Part: WINDOW — DELAMINATED (COCKPIT) · airframe 76,537 hrs · 19,217 cycles

CAPTAINS L2 WINDOW DELAMINATED. REMOVED L2 OPERABLE WINDOW IAW AMM 56-11-02. R & R L2 OPERABLE WINDOW ASSEMBLY IAW CMM 56-11-12 REPAIR 3 - 3. INSTALLED L2 OPERABLE WINDOW IAW AMM 56-11-02. SYS OPERATIONS CHECKED NORMAL.

Part: DEFIBRILLATOR — INOPERATIVE (CABIN) · airframe 75,967 hrs · 19,098 cycles

AUTOMATIC EXTERNAL DEFIBRILLATOR IN AFT OVERHEAD INOPERATIVE. EMER MEDICAL EQUIP, AED & OR ASSOCIATED EQUIP, NOT REQUIRED BY FAR. PLACED ON MDDR 55015 IAW MEL 25-64-01-03B.

Part: BATTERY — DEFECTIVE (APU) · airframe 75,838 hrs · 19,069 cycles

APU BATTERY CHARGER STATUS MSG. REPLACED APU BATTERY. OPERATIONS CHECKED OK.

Part: SMOKE DETECTOR — INOPERATIVE (LAVATORY) · airframe 75,838 hrs · 19,069 cycles

LAVATORY F SMOKE DETECTOR INOPERATIVE. REPLACED SMOKE DETECTOR, CHECKED GOOD.

Part: HINGE — BENT (GALLEY) · airframe 75,812 hrs · 19,061 cycles

AFT GALLEY LT WASTE BIN DOOR HAS BENT HINGE & FWD EDGE REQUIRES TRIM TO FIT. REMOVED WASTE BIN DOOR CLEANED DEBRIS FROM HINGE & REINSTALLED WASTE BIN DOOR IAW AMM 25-00-00-117-045.

Part: BOOT — TORN (AC BAY) · airframe 75,812 hrs · 19,061 cycles

LEFT AIR CONDITIONING PACK PLENUM EXHAUST BOOT IS TORN. REPLACED IAW AMM 21-51-02 401.

Part: FIRE LOOP — FAILED (NR 2 ENGINE) · airframe 75,812 hrs · 19,061 cycles

ENGINE 2 UPPER FWD FIRE LOOP FAILS OPERATIONS CHECK IAW EO 6726A006. INSTALLED NEW NR 2 ENG UPPER FWD FIRE LOOP DETECTOR IAW AMM 26-11-02. OPERATIONS CHECKED GOOD.

Part: FILTER — DAMAGED (FUEL SYSTEM) · airframe 75,812 hrs · 19,061 cycles

NUMBER 1 ENG MAIN FUEL FILTER HOUSING & FILTER HEAD THREADS ARE DAMAGED. R & R IAW AMM 73-11-08. LEAK CHECK ACCOMPLISHED ON TASK CARD 8007 ITEM 14.

Part: SLIDE — DEFECTIVE (L4 DOOR) · airframe 75,812 hrs · 19,061 cycles

L4 DOOR SLIDE APPEARS TO BE COMING APART. REMOVED L4 DOOR SLIDE & INSTALLED SERVICEABLE ONE IAW AMM 25-66-01.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 75,812 hrs · 19,061 cycles

SMOKE DETECTOR IN LAVATORY MS-11 IS FAULTY. GOING OFF FALSELY, RED LIGHT & AURAL WARNING. REPLACED SMOKE DETECTOR IAW AMM 26-13-00.

Part: TUBE — LEAKING (AC BAY) · airframe 75,812 hrs · 19,061 cycles

LOWER END OF HOT AIR SUPPLY TUBE IS LEAKING. RESTORED & LEAK CHECKED NR 2 PACK HOT AIR SUPPLY TUBE IAW AMM 21-51-07.

Part: FILTER — DIRTY (NR 2 ENGINE) · airframe 75,812 hrs · 19,061 cycles

DURING REPLACEMENT OF OIL SCAVENGE FILTER NR 2 ENG FOUND METALLIC & NON-METALLIC PARTICLES IN FILTER BOWL. CHECKED FILTER & BOWL ON NR 2 ENG OIL SCAVENGE FILTER AFTER ENG RUN FILTER & BOWL CLEAN REINSTALLED IAW AMM 79-21-04.

Part: SLEEVE — DAMAGED (APU) · airframe 75,812 hrs · 19,061 cycles

APU OIL COOLER OUTLET DUCT RUBBER SLEEVE IS DRIED & CRACKED. R & R APU OIL COOLER OUTLET DUCT RUBBER SLEEVE IAW AMM 49-51-01.

Part: SHUTOFF VALVE — DAMAGED (IDG) · airframe 75,812 hrs · 19,061 cycles

NUMBER 1 ENG IDG HEAT EXCHANGER SOV HAS DAMAGED THREADS IN FILTER BOSS. R & R IAW AMM 24-11-07.

Part: DOOR — LACK OF LUBE (LAVATORY) · airframe 75,812 hrs · 19,061 cycles

LAVATORY H WASTE BIN DOOR DOES NOT CLOSE CORRECTLY. LUBRICATED LAVATORY H WASTE BIN DOOR IAW AMM 12-21-00.

Part: CLAMP — MISSING (OIL SYSTEM) · airframe 75,812 hrs · 19,061 cycles

ENGINE 1 INBD REAR OIL SUM LINE MISSING CLAMP LOCATED JUST ABOVE FIRE LOOP AFT SECTION. INSTALLED NEW CLAMP IAW AMM 20-10-11.

Part: BONDING WIRE — FRAYED (AC BAY) · airframe 75,812 hrs · 19,061 cycles

RIGHT PACK HEAT EXCHANGER OUTLET BOND WIRE FRAYED. REPLACED BOND WIRE IAW SWPM 20-20-10. RESISTANCE CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,812 hrs · 19,061 cycles

FLOOR EMER LIGHT STRIPS AT MID CABIN GALLEY HAVE BURNT OUT BULBS. REPLACED MID CABIN GALLEY RT SIDE EMER ESCAPE PATH ELECTROLUMINESCENT LIGHT ASSEMBLY IAW AMM 33-51-10. OPERATIONS CHECKED GOOD.

Part: BONDING WIRE — FRAYED (AC BAY) · airframe 75,812 hrs · 19,061 cycles

RIGHT PACK BONDING WIRE FRAYED AT COMPRESSOR OUTLET. REPLACED IAW SWPM 20-20-10. RESISTANCE CHECKED GOOD.

Part: STAND OFF — DEBONDED (AC BAY) · airframe 75,812 hrs · 19,061 cycles

RIGHT PACK WIRE STANDOFF DISBONDED FROM RAM AIR INLET DUCT. SECURED DISBONDED RT PACK WIRE STANDOFF ON RAM AIR INLET DUCT IAW SOPM 20-50-12.

Part: CABLE — LOOSE (AC BAY) · airframe 75,812 hrs · 10,961 cycles

SEVERAL DUCT RESTRAINT CABLES IN RT PACK BAY ARE LOOSE. TIGHTENED CABLES IAW AMM 21-51-02 IN RT PACK BAY.

Part: SMOKE DETECTOR — DIRTY (LAVATORY) · airframe 75,812 hrs · 19,061 cycles

SMOKE DETECTOR IN LAVATORY MS 12 KEEPS GOING OFF INTERMITTENTLY. CLEANED LAVATORY MS 12 SMOKE DETECTOR IAW AMM 26-13-01. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 75,812 hrs · 19,061 cycles

EXIT SIGN NEAR FLOOR AT DOOR L2 SEVERAL BULBS INOPERATIVE. REPLACED BULBS IN EXIT SIGN NEAR FLOOR AT L2 DOOR IAW AMM 33-51-09. LIGHT OPERATIONS CHECKED GOOD.

Part: O-RING — LEAKING (AC BAY) · airframe 75,812 hrs · 19,061 cycles

COUPLING UPSTREAM OF LOW LIMIT CONTROL VLV ON NR 1 PACK IS LEAKING. R & R O RINGS IN COUPLING UPSTREAM OF LOW LIMIT CONTROL VLV ON NR 1 PACK IAW AMM 21-51-11. NO LEAKS NOTED.

Part: SCREW — LOOSE (ANTI-ICE EXHAUST) · airframe 75,812 hrs · 19,061 cycles

NUMBER 1 ENG NOSE COWL LOWER ANTI-ICE EXHAUST OUTLET HAS LOOSE HARDWARE. R & R 1 EACH SCREW IAW SRM 51-40-04.

Part: BONDING WIRE — FRAYED (AC BAY) · airframe 75,812 hrs · 19,061 cycles

LEFT PACK HEAT EXCHANGER OUTLET BONDING WIRE FRAYED. R & R IAW SWMP 20-20-10. RESISTANCE CHECKED GOOD.

Part: FILTER — DIRTY (NR 1 ENGINE) · airframe 75,812 hrs · 19,061 cycles

DURING REPLACEMENT OF OIL SCAVENGE FILTER NR 1 ENG FOUND METALLIC & NON-METALLIC PARTICLES IN FILTER BOWL. CHECKED FILTER & BOWL ON NR 1 ENG OIL SCAVENGE FILTER, AFTER ENG RUN FILTER & BOWL CLEAN. REINSTALLED IAW AMM 79-21-04.

Part: BONDING WIRE — FRAYED (AC BAY) · airframe 75,812 hrs · 19,061 cycles

RIGHT PACK TEMP CONTROL VLV BOND WIRE FRAYED. R & R BONDING WIRE. BOND RESISTANCE TEST PASSED IAW SWPM 20-20-10.

Part: DOOR — DAMAGED (LAVATORY) · airframe 75,812 hrs · 19,061 cycles

LAVATORY G WASTE BIN DOOR HAS EDGE DAMAGE & LOWER CORNER IS CRACKED. REPAIRED & PAINTED LAVATORY G WASTE BIN DOOR IAW AMM 25-00-00.

Part: TUBE — DAMAGED (START VALVE) · airframe 75,812 hrs · 19,061 cycles

ENGINE 1 START VLV FILTER TUBE NUT, STRIPED AT FILTER END DOT 20. R & R START VLV FILTER TUBE ON ENG 1 IAW TASK 80-304-01-1 & AMM 80-11-04.

Part: SMOKE DETECTOR — DIRTY (LAVATORY) · airframe 75,812 hrs · 19,061 cycles

SMOKE DETECTOR IN LAVATORY A 3 KEEPS GOING OFF INTERMITTENTLY. CLEANED SMOKE DETECTOR IN LAVATORY A 3 IAW AMM 26-13-01. OPERATIONS CHECKED GOOD.

Part: RESTRAINT — DAMAGED (AC BAY) · airframe 75,812 hrs · 19,061 cycles

LEFT LOWER INBD PRIMARY HEAT EXCHANGER DUCT RESTRAINT CABLE THREADS ARE DAMAGED. REPLACED CABLE & HARDWARE ON LT LOWER INBD PRIMARY HEAT EXCHANGER DUCT. TO BE CONNECTED AT HEAT EXCHANGER INSTALL IAW AMM 21-51-02.

Part: RIVET — LOOSE (GALLEY) · airframe 75,812 hrs · 19,061 cycles

AFT GALLEY RT WASTE BIN DOOR HINGE IS LOOSE. R & R RIVETS IN DOOR HINGE OF AFT GALLEY RT WASTE BIN DOOR IAW AMM 51-40-02.

Part: BONDING WIRE — BROKEN (AC BAY) · airframe 75,812 hrs · 19,061 cycles

LEFT PACK FLOW SENSOR BONDING WIRE BROKEN. REPLACED LT PACK FLOW SENSOR BONDING WIRE IAW AMM 20-20-10. RESISTANCE CHECKED GOOD.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,812 hrs · 19,061 cycles

FUSELAGE STATION 786 FWD SUPPORT FOR PANEL 139AO HAS CORROSION AROUND FASTENER HOLES. UPPER & LOWER SURFACES DI 34 DOT 51, REMOVED CORRODED PLATE, FABRICATED NEW & INSTALLED IAW AMM 51-40-05.

Part: SIDEWALL PANEL — BOWED (LAVATORY) · corrosion level 2 · airframe 75,812 hrs · 19,061 cycles

LAVATORY AC 3 HAS A BOWED OUT SIDEWALL, INBD, AFT LOWER. R & R, REINSTALLED LAVATORY AC 3 IAW AMM 25-41-04.

Part: BONDING WIRE — FRAYED (AC BAY) · airframe 75,812 hrs · 19,061 cycles

RIGHT PACK REHEATER INLET DUCT BOND WIRE FRAYED. REPLACED IAW SWMP 20-20-10. RESISTANCE CHECKED GOOD.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,812 hrs · 19,061 cycles

FUSELAGE STATION 830 AFT SUPPORT FOR KEEL BEAM PANEL 139AO HAS CORROSION AROUND FASTENER HOLES. R & R AFT SUPPORT TEE BRACKET IAW AMM 51-40-05.

Part: CONNECTOR — LOOSE (AC BAY) · airframe 75,812 hrs · 19,061 cycles

LEFT PACK COMPRESSOR OUTLET TEMP BULB CONNECTOR & SENSOR LOOSE. SECURED LT PACK COMPRESSOR OUTLET TEMP BULB, BULB CONNECTOR & SENSOR IAW AMM 21-51-06.

Part: MOUNT — CORRODED (LAVATORY) · corrosion level 2 · airframe 75,812 hrs · 19,061 cycles

LAVATORY AC 4 HAS AFT MOUNT CORRODED. REMOVED & REINSTALLED AFT LAVATORY AC-4 IAW AMM 25-41-04. REPLACED LAVATORY AC-4 MOUNTS.

Part: SEAL — LEAKING (BLEED AIR SYS) · airframe 75,812 hrs · 19,061 cycles

BLEED AIR DUCT LEAKING, LT WING LE INBD OF NR 1 PYLON. REMOVED & REINSTALLED NR 1 PYLON BLEED AIR DUCT INBD LT IAW AMM 36-11-01. LEAK CHECKED, NO LEAKS NOTED.

Part: UNKNOWN — MALFUNCTIONED (FIRE DETECTION) · airframe 75,812 hrs · 19,061 cycles

FIRE DETECTION SYS FAIL LIGHT CHECK. FAILED STEP 3 FOR CARDS M683 & M684. FAIL LIGHT DID NOT ILLUMINATE. TROUBLE SHOT FIRE DETECTION SYS FAIL LIGHT CHECK IAW AMM TASK CARD 26-020-01. OPERATIONS CHECKED GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 75,812 hrs · 19,061 cycles

EMERGENCY TRACK LIGHTING WIRES AT SEAT ROW 18KH & 20CA ARE BROKEN. RECONNECTED ELEC CONNECTORS BETWEEN SEAT ROW 18KH & 20CA IAW AMM 33-51-10-962-063.

Part: RESTRAINT — DAMAGED (AC BAY) · airframe 75,812 hrs · 19,061 cycles

LEFT LOWER INBD PRIMARY HEAT EXCHANGER DUCT RESTRAINT CABLE THREADS ARE DAMAGED. REPLACED CABLE & HARDWARE ON LT INBD PRIMARY HEAT EXCHANGER DUCT & CONNECTED AT HEAT EXCHANGER INSTALLATION IAW AMM 21-51-02.

Part: LATCH — LACK OF LUBE (LAVATORY) · airframe 75,812 hrs · 19,061 cycles

LAVATORY C WASTE BIN DOOR DOES NOT CLOSE CORRECTLY. LUBRICATED LAVATORY C WASTE BIN DOOR LATCH & HINGES IAW AMM 12-21-00.

Part: LANYARD — WORN (AC BAY) · airframe 75,812 hrs · 19,061 cycles

COUPLING UPSTREAM OF LOW LIMIT CONTROL VLV IS LEAKING & HAS WORN LANYARDS ON NR 2 PACK. R & R O RINGS IN COUPLING OF LOW LIMIT CONTROL VLV. REPLACED WORN LANYARD ON COUPLING IAW AMM 21-51-11. NO LEAKS NOTED.

Part: SKIN — GOUGED (FUSELAGE) · airframe 75,812 hrs · 19,061 cycles

EXTERIOR FUSELAGE LT SIDE STATION 1473.5 GOUGE IN SKIN ADJACENT TO RIVET. CTR RIVET AT LAP SEAM, STATION 17L JUST FWD OF L4 DOOR DI34, DOT 43. ACCOMPLISHED REWORK HFEC, SURFACE SCAN, GENERATED SR 3-3086487519 FOR EVALUATION OF REWORK, RESTORED FINISH & RECEIVED FORM 8100-9 FOR CATEGORY AN APPROVAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 75,812 hrs · 19,061 cycles

EMERGENCY EXIT SIGNS ABOVE DOORS 833C & 843R ARE INOPERATIVE. REPLACED EMER LIGHTS POWER SUPPLY M1210 IAW AMM 33-51-07. OPERATIONS CHECKED GOOD.

Part: SHUTOFF VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 75,773 hrs · 19,050 cycles

RIGHT ENG BLEED SWITCH LIGHT OFF, LIGHT FAILS TO ILLUMINATE ON SHUTDOWN. LIGHT IS OK, MULTIPLE OCCASIONS. R & R PRSOV. RUN OPERATIONS CHECKED GOOD IAW AMM 36-11-09.

Part: CONTROL VALVE — MALFUNCTIONED (AC BAY) · airframe 75,773 hrs · 19,050 cycles

LEFT PACK LIGHT NOT ILLUMINATED WITH PACK OFF. REPLACED LT PACK FLOW CONTROL VLV IAW AMM 21-51-01 401. TESTED OK.

Part: CONNECTOR — DIRTY (AC BAY) · airframe 75,768 hrs · 19,047 cycles

LEFT PACK CTL VLV REMAINS OPEN WITH SWITCH OFF. PACK CONTINUES TO RUN, HAS OCCURRED ON NUMEROUS STARTS. VERIFIED THAT VLV MOVES TO COMMANDED POSITION. REMOVED, CLEANED & RECONNECTED CLOSED POSITION SWITCH ASSEMBLY ELEC CONNECTOR. TESTED IAW AMM 21-51-01 401. OPERATIONS CHECKED OK.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 75,773 hrs · 19,050 cycles

ON PREFLIGHT, STATUS MSG, AFT EQ EXH FAN 1. ACCOMPLISHED EQUIP COOLING SYS ADJUSTMENT & TEST ISW AMM 21-58-00 501. PLACARD REMOVED, NO STATUS MSG. ACFT RESTORED TO NORMAL CONFIG. OPERATIONS CHECKED NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 75,678 hrs · 19,023 cycles

EMERGENCY LIGHT EXIT SIGN L306 RT SIDE OF CABIN AFT BEFORE R3 DOOR DOESN’T TEST. R & R BATTERY CHARGER IAW AMM 33-51-07. OPERATIONS CHECKED GOOD.

Part: COVER — CRACKED (CABIN) · airframe 75,612 hrs · 19,008 cycles

EMERGENCY FLOOR LIGHT TRACK COVER CRACKED ON RT SIDE CABIN AT SEATS 5K & H & 6K & H. R & R FLOOR LIGHT TRACK COVER IAW AMM 33-51-10-002-112.

Part: LIGHT — BROKEN (CABIN) · airframe 75,612 hrs · 19,008 cycles

EMERGENCY FLOOR LIGHT AT LT CABIN POSITION SEAT 4C & A BROKEN. R & R BROKEN FLOOR LIGHT IAW AMM 33-51-10-962-063.

Part: FUEL FILTER — DEFECTIVE (LT ENGINE) · airframe 75,569 hrs · 18,997 cycles

LEFT ENG FUEL FILTER STATUS MSG. ACCOMPLISHED FIM 73-11 FT 803, NO CONTAMINATION. REPLACED FUEL FILTER IAW AMM 73-11-02 401. COMPLIED WITH POWER PLANT TEST 71-00-00 501 TEST 2, NO LEAKS.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 75,545 hrs · 18,991 cycles

STATUS MSG ON DESCENT CABIN ALT AUTO 2. ACCOMPLISHED FIM 21-31 FT 803. TESTED OK NO FAULTS.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 75,511 hrs · 76,008 cycles

ON CLIMB EICAS ADVISORY LT ENG PRV STATUS MSG. CLEARED STATUS & OPERATIONS CHECKED IAW AMM 36-11-18 413-415. OPERATIONS CHECKED OK.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 75,480 hrs · 18,976 cycles

RIGHT ENG PRV STATUS MSG ON ENG START. DURING DDG DEACTIVATION PROCEDURE, MSG EXTINGUISHED, REACTIVATED PRV & ACCOMPLISHED OPERATIONS. CHECKED IAW AMM 36-11-18 413 F - G PASS, MSG DID NOT RECUR.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 75,371 hrs · 18,951 cycles

IDG OUT TEMP MX MSG. IN WORK ACFT IS IN A CHECK.

Part: CLAMP — LOOSE (APU) · airframe 75,319 hrs · 18,939 cycles

APU BLEED AIR LOW 15 PSI. TIGHTENED CLAMP ON SURGE VLV.

Part: TRU — FAULTY (APU) · airframe 75,324 hrs · 18,940 cycles

APU FAULT ON START AFTER LANDING. APU TRU DEACTIVATED. REPLACED APU STARTING TRU. TESTED IAW AMM 24-32-04 401. TESTED OK, ACFT RESTORED TO NORMAL CONFIGURATION.

Part: CONTROL VALVE — MALFUNCTIONED (AC BAY) · airframe 75,308 hrs · 18,937 cycles

RIGHT PACK INOPERATIVE LIGHT. REPLACED PACK TEMP CONTROL VLV.

Part: FUEL FILTER — FAULTED (RT ENGINE) · airframe 75,271 hrs · 18,927 cycles

STATUS MSG DISPLAY RT ENG FUEL FILTER. R & R RT ENG FUEL FILTER IAW MM 73-11-02 601. OPERATIONS CHECKED NORMAL.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 72,535 hrs · 18,919 cycles

RIGHT EMER LIGHTS FROM K5 TO K10 NOT ILLUMINATING DURING TEST. REPOSITIONED K10 LIGHT ASSEMBLY IAW 33-51-16. OPERATIONS CHECKED NORMAL.

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 75,210 hrs · 18,914 cycles

APU FIRE LP1 MSG CAME ON. PERFORMED OPERATIONS CHECK IAW AMM 26-15-00, NO FURTHER MSGS.

Part: FIRE LOOP — FAULTY (APU) · airframe 75,217 hrs · 18,915 cycles

APU FIRE LP 1 EICAS STATUS MSG NOTED UPON LANDING. R & R APU UPPER FIRE LOOP IAW MM 26-15-02. OPERATIONS CHECKED OK.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 75,188 hrs · 18,909 cycles

RIGHT ENG CONTROL STATUS MSG. PERFORMED FIM 73-21 FT 878, BITE PIMU IAW 71-01 FT 810. MSG CLEARED. PERFORMED OHMS CHECK OF ECU P 7 & 8, CHECKED WITHIN LIMITS. PERFORMED GND TEST & ENG RUN, NO FAULT NOTED.

Part: WINDOW — CRACKED (COCKPIT) · airframe 75,008 hrs · 18,870 cycles

CAPTAINS FWD WINDOW SHATTERED & CRACKED DURING CRUISE. R & R CABIN L1 WINDOW IAW AMM 56-11-01 & 30-41-00. OPERATIONS CHECKED NORMAL.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 75,054 hrs · 18,881 cycles

STATUS MSG R ENG PRV. ACCOMPLISHED ENG RUN ERASED STATUS MSG. PNEUMATICS TESTED OK IAW AMM 36-11-00/501, NO MSGS GENERATED. ACCOMPLISHED FIM 36-20 FT 804 FIG 104. VERIFY TEST, NO FAULTS PRESENT.

Part: CIRCUIT CARD — FAULTY (FIRE WARNING) · airframe 74,740 hrs · 18,810 cycles

APU FIRE LP 1. R & R APU FIRE WARNING CONTROL CARD IAW AMM 26-15-00. OPERATIONS CHECKS COMPLIED WITH.

Part: GASKET — UNKNOWN (APU) · airframe 74,646 hrs · 18,788 cycles

APU IGNITER PLUG REQUIRES NEW GASKET. REPLACED APU IGNITER PLUG GASKET WITH NEW GASKET IAW AMM 49-41-02.

Part: LIGHT — INOPERATIVE · airframe 74,646 hrs · 18,788 cycles

LEFT MID SLIDE LIGHT INOPERATIVE. REPLACED LT MID SLIDE BULB IAW AMM 33-51-06-902-082. OPERATIONS CHECKED GOOD IAW AMM 33-51-06-862-083.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,646 hrs · 18,788 cycles

FLOOR LIGHTS BETWEEN DOOR L1 & SEAT 2AC INOPERATIVE. EMER PATHWAY LIGHTING. REPAIRED IAW AMM 33-51-10-93.

Part: WIRE — BROKEN (CABIN) · airframe 74,646 hrs · 18,778 cycles

FLOOR EMER LIGHT BETWEEN DOORS L1 & R1 INOPERATIVE. REPAIRED BROKEN WIRES IAW AMM 33-51-10.

Part: IDG — INOPERATIVE (RT ENGINE) · airframe 74,577 hrs · 18,776 cycles

RIGHT GEN INOPERATIVE. TRANSFERRED TO DMI 49937. R & R RT IDG IAW AMM 24-11-01. OPERATIONS CHECKED & LEAK CHECKED IAW AMM 24-11-00, MEL CLEARED.

Part: GCU — FAILED (RT GENERATOR) · airframe 74,550 hrs · 18,771 cycles

RIGHT GENERATOR DRIVE EICAS MESSAGE. ACCOMPLISHED RT GENERATOR DRIVE QRH PROCEDURE. RAN RT ENGINE IDG FREQS ARE 392 GEN CONTINUED TO DISCONNECT. REMOVED AND REPLACED GENERATOR CONTROL UNIT IAW AMM 24-22-02, OPS CHECKED OK.

Part: HEATER — CRACKED (RT A/C PACK) · airframe 74,465 hrs · 18,753 cycles

RIGHT PACK OVERHEAT, REHEATER CRACKED. R & R PACK REHEATER IAW MM 21-51-07, OPS CHECKED OK.

Part: WARNING SYSTEM — FALSE ACTIVATION (BLEED AIR SYS) · airframe 74,377 hrs · 18,733 cycles

RIGHT BLD DUCT LEAK, EICAS MSG. PERFORMED OPERATIONAL CHECK OF WING & BODY DUCT LEAK DETECTION IAW MM 26-18-00, OPERATES NORMAL, NO DEFECTS NOTED.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 74,346 hrs · 18,725 cycles

SMOKE DETECTOR ON LAVATORY A3 ACROSS FROM THE L4 JUMP SEAT ACTIVATES INTERMITTENT IN FLIGHT. R & R SMOKE DETECTOR IAW MM 26-13-01, OPS NORMAL.

Part: ECU — FAILED (APU) · airframe 74,315 hrs · 18,718 cycles

APU BLEED INOPERATIVE. R & R APU ECU IAW MM 49-61-05. OPS CHECKED NORMAL.

Part: DOOR — DAMAGED (A/C BAY) · airframe 74,257 hrs · 18,705 cycles

VIBRATION & RT PACK OVERHEAT EICAS MESSAGE. PASSING 10,000 FT & ACCELERATING. DIVERTED AND LANDED. INSPECTED ACFT & FOUND DUE TO IMPROPER DOOR PROCEDURES, BOTH PACK BAY ACCESS DOORS DAMAGED WITH ASSOCIATED HARDWARE & WIRING DAMAGED. PERFORMED REPAIR OF WIRING, SUPPORTS, R & R BOTH ACCESS DOORS ALONG WITH ASSOCIATED HARDWARE. PERFORMED OPS CHECK OF BOTH PACKS WITH ALL NORMAL & VERIFIED DOOR OPERATION NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,598 hrs · 18,646 cycles

FLOOR EMERGENCY LIGHTS INOPERATIVE RT SIDE ROWS 26 - 30. REPLACED FLOOR EMERGENCY PATH LIGHTS AT ROWS 26 - 30 IAW AMM 33-51-10, OPERATIONS CHECKED SATISFACTORY.

Part: SLIDE — LOW PRESSURE (L4 DOOR) · airframe 73,958 hrs · 18,646 cycles

L4 DOOR SLIDE REQUIRES REPLACEMENT FOR LOW PRESS. R & R ENTRY SERVICE DOOR ESCAPE SLIDE PACK IAW AMM 25-66-01 AT L4 DOOR POSITION.

Part: ELT — DAMAGED (CABIN) · airframe 73,958 hrs · 18,646 cycles

ELT BEHIND SEAT 37CA ANTENNA STRING IS BROKEN & UNRAVELED. INSTALLED NEW ELT BEHIND SEAT 37CA IAW AMM 25-63-00, 25-05-03.

Part: WINDOW — DAMAGED (COCKPIT) · airframe 73,962 hrs · 18,647 cycles

FL 41 BIRD STRIKE L1 OUTER PANE. R & R L1 WINDOW IAW AMM 56-11-01.

Part: PLENUM — DELAMINATED (AC BAY) · airframe 73,958 hrs · 18,646 cycles

LEFT PACK RAM AIR EXIT HAS DELAMINATION IN DUCT. REMOVED & REINSTALLED LT PACK EXHAUST PLENUM IAW AMM 21-51-03. REPAIRED PLENUM IAW SRM 51-70-06, LEAK CHECKED GOOD.

Part: CLAMP — BROKEN (NR 2 ENGINE) · airframe 73,598 hrs · 18,646 cycles

ENG 2 D SUMP RETURN OIL LINE CLAMP IS BROKEN AT APPROX 7 O`CLOCK POSITION ABOVE THE LOWER RECOUP DUCT. R & R CLAMP AT 7 O`CLOCK POSITION ON D SUMP RETURN OIL LINE IAW AMM 20-11-00.

Part: CARBON SEAL — LEAKING (RT ENGINE) · airframe 73,598 hrs · 18,646 cycles

RIGHT ENG CONSUMES MORE OIL THAN LT ENG. D SUMP AREA SUSPECTED TO BE AT FAULT. R & R SEALS AT D SUMP & STARTED CARBON SEALS. NO LEAKS NOTED AFTER ENG RUN IAW AMM 71-00-00.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 73,958 hrs · 18,646 cycles

R1 DOOR SLIDE REQUIRES REPLACEMENT FOR LOW PRESS. R & R ENTRY SERVICE DOOR ESCAPE SLIDE PACK AT R1 DOOR IAW AMM 25-66-01.

Part: CONNECTOR — DIRTY (APU) · airframe 73,958 hrs · 18,646 cycles

STATUS MSG APU LP 1 DISPLAYS INTERMITTENTLY. PERFORMED TROUBLESHOOTING. CLEANED & INSPECTED CONNECTORS, RECONNECTED IAW AMM 26-15-02, FIM 26-15-00, FAULT TREE 803 & SWPM 20-60-01. NO FAULTS PRESENT AT THIS TIME.

Part: SEAL — DAMAGED (RT ENGINE) · airframe 73,958 hrs · 18,646 cycles

RIGHT ENG CONSUMES MORE OIL THAN LT ENG & D SUMP AREA SUSPECTED TO BE AT FAULT. R & R D SUMP SEAL. R & R STARTER CARBON SEAL IAW AMM & EO 2016 2, NO LEAKS NOTED AFTER GND TEST IDLE.

Part: BLEED AIR SYS — INOPERATIVE (APU) · airframe 73,942 hrs · 18,642 cycles

APU BLEED INOPERATIVE.

Part: RELAY — DEFECTIVE (APU) · airframe 73,942 hrs · 18,642 cycles

APU BLEED INOPERATIVE. TRANSFERRED TO MDDR 48227, DEFERRED IAW DDPG 49-11-01-01 CAT C PLACARD. R & R RELAY K23 AT PANEL P49 IAW SWPM 20-81-22. OPERATIONS CHECKED OF APU SOV GOOD IAW AMM 36-11-10. THIS CLEARS MDDR 48227, MCC NOTIFIED & PLACARD REMOVED.

Part: UNKNOWN — MALFUNCTIONED (COCKPIT) · airframe 73,918 hrs · 18,636 cycles

TERR MODE NOT DISPLAY CORRECT INFORMATION IN FLT. ACCOMPLISHED WEATHER RADAR OPERATIONS CHECK IAW AMM 34-43-00-215-026-002 & OPERATIONS CHECK OF EGPWS IAW AMM 34-46-00, ALL INDICATION NORMAL.

Part: VALVE — MALFUNCTIONED (APU) · airframe 73,828 hrs · 18,613 cycles

APU AIR INOPERATIVE. R & R APU SHUTOFF VLV IAW AMM 36-11-10, VLV CHECKED GOOD. FOUND LEAKING AIR DUCT IAW AMM 36-11-02. APU DUCT OPERATIONS CHECKED GOOD.

Part: STATUS MESSAGE — INTERMITTENT (COCKPIT) · airframe 73,824 hrs · 18,612 cycles

INTERMITTENT STATUS MSG, APU FIRE LOOP 1, IN FLIGHT. OPERATIONS CHECKED IAW MM 26-15-00, NO DEFECTS NOTED AT THIS TIME.

Part: SWITCH — FAULTY (FUEL SYSTEM) · airframe 73,775 hrs · 18,600 cycles

LEFT AFT FUEL PUMP WON’T TURN OFF. REPLACED BOOST PUMP LT AFT SWITCH, IAW SWPM 20-84-14. OPERATIONS CHECKED IAW AMM 28-22-03, MDDR CLEARED.

Part: BATTERY — FAULTY (APU) · airframe 72,509 hrs · 216,676 cycles

STATUS MSG APU BATTERY CHARGER. PERFORMED TROUBLESHOOTING IAW FIM 24-31-805. FOUND APU BATTERY FAULTY, REPLACED IAW AMM 24-31-04. SYS OPERATIONS & GND CHECKED GOOD.

Part: FIRE LOOP — FALSE ACTIVATION (APU) · airframe 73,655 hrs · 18,572 cycles

APU FIRE LOOP ONE STATUS MSG. PERFORMED FIM PROCEDURE 26-15-FAULT TREE 804 & ALL INDICATIONS NORMAL.

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 73,608 hrs · 18,561 cycles

STATUS MESSAGE, APU FIRE LP 1. PERFORM FIM PROCEDURE 26-15 FAULT TREE 804, ALL INDICATIONS NORMAL.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 73,528 hrs · 18,544 cycles

RUDDER RATIO EICAS MSG, RUDDER RATIO LIGHT ON TAXI OUT. RE RACKED LT & RT RUDDER RATIO BOX, CHECKED TEST SWITCH POSITION, SYS OPERATIONS CHECKED NORMAL IAW FIM 27-21, FAULT TREE 804 & 27-09-00 101, CAT II/III.

Part: UNKNOWN — MALFUNCTIONED (AUTOPILOT SYS) · airframe 73,493 hrs · 18,535 cycles

NON-COMMANDED AILERON INPUT, NON-COMMANDED RT AUTOPILOT ENGAGEMENT, NON-COMMANDED VS ENGAGEMENT, NON-COMMANDED HEADING HOLD & NON-COMMANDED STAB TRIM RUNAWAY FULL NOSE UP. FOUND FAULT INDICATION ON RT AILERON STAB TRIM MOSUDE, RESET & ALL INDICATIONS RETURNED TO NORMAL. PERFORMED AL TEST 40 ON MCDP IAW AMM 22-41-00, ALL INDICATIONS NORMAL.

Part: FIRE LOOP — FAULTY (RT ENGINE) · airframe 73,493 hrs · 18,535 cycles

RT ENG FIRE LOOP 1 DISPLAYED ON STATUS PAGE. R & R LOOP 1 DETECTOR ELEMENT, OPERATIONS CHECKED OK.

Part: ACM — SEIZED (AC BAY) · airframe 73,474 hrs · 18,533 cycles

LEFT PACK AUTO MODE INOPERATIVE. TROUBLE SHOT IAW FIM, FOUND ACM TURBINE SHAFT SEIZED. REPLACED ACM WITH REPAIRED UNIT IAW AMM 21-51-03. LEAK & GND OPERATIONS CHECKED GOOD, PLACARD REMOVED.

Part: CONTROLLER — FAILED (WINDOW HEAT) · airframe 73,469 hrs · 18,531 cycles

RIGHT SIDE WINDOW EICAS MESSAGE. PERFORMED FIM 30-41-801803 WINDOW RESISTANCE 10.3 OHMS, WITHIN LIMITS. REPLACED CONTROLLER IAW AMM 30-41-01, BITE CHECKED GOOD, PLACARD REMOVED.

Part: PRESSURE SWITCH — MALFUNCTIONED (FUEL SYSTEM) · airframe 73,469 hrs · 18,531 cycles

CENTER LT OVRD PUMP PRESS LIGHT ILLUMINATED. TABLE STYLE WIDTH 113PT, BORDER COLLAPSE, COLLAPSE ID 92A3531D-4E0B-4D55-B76A-01D9F2525878. BORDER "0" CELLS PACING "0" CELL PADDING "0" WIDTH "150" "WIDTH, 13PT, WIDTH SOURCE USER SET, WIDTH-ALT 5485, WIDTH "150". HEIGHT, 67.5PT, HEIGHT "90"!--START FRAGMENT WIDTH, 113PT; HEIGHT 67.5PT, DIR. LET CLASS X L63, HEIGHT 90 WIDTH 150. INSTALLED LET PRESS SWITCH YAW FIRM 28-22, FAULT TREE 805, OPERATIONS CHECKED NORMAL YAW AM 28-22-00. !

Part: CLAMP — UNSECURE (AC BAY) · airframe 73,469 hrs · 18,531 cycles

LEFT PACK OVERTEMP DURING GND OPERATION IN AUTO & STANDBY. ACCOMPLISHED FIM PROCEDURE 21 - 51 FAUL TREE 804, FOUND LOW LIMIT CONTROL VLV LEAKING, SECURED CLAMPS, MDDR 46801CLOSED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 73,460 hrs · 18,530 cycles

EICAS MESSAGE, RT SIDE WINDOW, ILLUMINATED IN FLIGHT. PERFORMED OPERATIONAL TEST IAW AMM TASK 30-41-00-715-001, ALL INDICATIONS NORMAL.

Part: SWITCH — INOPERATIVE (CARGO BAY) · airframe 73,342 hrs · 18,504 cycles

FORWARD CARGO COMPARTMENT FIRE, ARMED SWITCH, LIGHT INOPERATIVE. R & R FWD CARGO COMPARTMENT FIRE ARMING SWITCH IAW AMM 26-23-01, OPERATIONS CHECKED AMM 26-23-00.

Part: LIGHT — INOPERATIVE (FIRE DETECTION) · airframe 72,253 hrs · 21,610 cycles

FORWARD CARGO COMPARTMENT FIRE DETECTIVE SYS WARNING LIGHT INOPERATIVE. RE-LAMPED FWD CARGO LIGHT CAPSULE & OPERATIONS CHECKED OKAY IAW AMM 26-20-08.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,314 hrs · 18,499 cycles

L1 MAIN ENTRY DOOR EMERGENCY DOORWAY LIGHT INOPERATIVE WHEN TESTED. REPLACED L1 MAIN ENTRY DOOR EMERGENCY DOORWAY LIGHT BULB IAW AMM 33-51-03, OPERATIONS CHECKED GOOD.

Part: IGNITER — ERODED (APU) · airframe 73,314 hrs · 18,499 cycles

APU IGNITER PLUG ERODED BEYOND LIMITS. R & R APU IGNITER PLUG IAW AMM 49-41-02. OPERATIONS CHECKED NORMAL.

Part: RELAY — FAILED (APU) · airframe 73,314 hrs · 18,499 cycles

APU HEALTH CHECK FAILS STEP 5 D OF EO 6749A003, NO 28V DC AT TERMINAL X1. R & R APU START RELAY K197 IAW EO 6749A003 & AMM 49-41-11.

Part: SLIDE — UNSERVICEABLE (L4 DOOR) · airframe 73,314 hrs · 18,499 cycles

L4 DOOR SLIDE LANYARD HAS COME LOOSE FROM THE FIRING MECHANISM AT THE CORNER OF THE DOOR. R & R L4 DOOR ESCAPE SLIDE & RAFT ASSEMBLY IAW AMM 25-66-01.

Part: SWITCH — DEFECTIVE (COCKPIT) · airframe 73,222 hrs · 18,479 cycles

RIGHT GENERATOR SWITCH COVER WILL NOT STAY LATCHED. REPLACED GEN CONTL SWITCH LIGHT ASSEMBLY.

Part: APU — SHUTDOWN (APU BAY) · airframe 73,176 hrs · 18,469 cycles

PRIOR TO DEPARTURE, APU AUTO SHUTDOWN, APU MDDR 45788. R & R APU IAW AMM 49-11-01, WORK ORDER 6972 TASK CARD T1071.

Part: GAUGE — FAULTY (FUEL SYSTEM) · airframe 73,176 hrs · 18,469 cycles

FUEL QTY CBE4 ON P6 1 PANEL TRIPPED. TROUBLESHOT IAW FIM 28-41. REPLACED LT TANK QTY LOAD SELECTOR GAUGE IAW AMM 28-41-16, ALL CHECKED GOOD.

Part: ISOLATION VALVE — FAULTY (BLEED AIR SYS) · airframe 13,154 hrs · 2,434 cycles

LEFT BLEED ISOL VLV EICAS INTERMITTENT ON LANDING. REPLACED LT BLEED ISOL VLV WITH REPAIRED UNIT IAW AMM 36-11-04. LEAK & OPERATIONS CHECKED GOOD & NBSP.

Part: COOLING FAN — INOPERATIVE (E&E BAY) · airframe 73,099 hrs · 18,453 cycles

AFT EQUIP COOLING FAN INOPERATIVE. R & R EQUIP FAN IAW AMM 21- 26-01, OPERATIONS SATISFACTORY.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 71,917 hrs · 21,528 cycles

AFTER SHUT DOWN NR 2 CABIN CONTROLLER STATUS MESSAGE. R & R NR 2 CABIN PRESS CONTROLLER IAW MM 21-31-02 401, OPERATIONS CHECKED OK.

Part: APU — SHUTDOWN (APU BAY) · airframe 72,975 hrs · 18,418 cycles

APU AUTO SHUTDOWN ON THE GROUND. R & R APU. APU OPERATIONS & LEAK CHECKED GOOD.

Part: GROUND WIRE — FAILED (FIRE EXTINGUISHE) · airframe 72,734 hrs · 18,367 cycles

CARGO FIRE EXT FWD BOTTLE ARM SWITCH "ARM" LIGHT WILL NOT ILLUMINATE, FOUND SWITCH, LIGHT PANEL ASSY FOUND BAD GROUND IN PANEL REPAIRED OPS CHECKED GOOD IAW 33-13-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 72,702 hrs · 18,361 cycles

L-2 EXTERIOR EMERGENCY EXIT FLOOD LIGHT INOPERATIVE. REPLACED LAMP, OPS CHECKED OK IAW MM 33-51-06.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 72,702 hrs · 18,361 cycles

MOST FWD STEWARDESS CENTER EMERGENCY LIGHT SEGMENT INOPERATIVE. REPLACED LAMP IAW AMM 33-51-10.

Part: SHUTOFF VALVE — INOPERATIVE (RT ENGINE BLEED) · airframe 72,603 hrs · 18,340 cycles

RIGHT ENGINE BLEED DID NOT OPEN AFTER START. R & R NR 2 ENGINE PRSOV, IAW AMM 36-11-07, OPS CHECKED GOOD.

Part: BLEED AIR SYS — MALFUNCTIONED (RT ENGINE) · airframe 72,603 hrs · 18,340 cycles

RT ENGINE BLEED DID NOT OPEN AFTER START. OPEN

Part: WARNING LIGHT — FALSE ACTIVATION (LT A/C PACK) · airframe 72,549 hrs · 18,329 cycles

LEFT PACK OVERTEMP ON CLIMBOUT. PERFORMED BITE IAW FIM 21-51, FT 803, TEST PASSED, OPS CHECKED NORMAL.

Part: ANTI-SKID VALVE — FAULTED · airframe 72,534 hrs · 18,325 cycles

ANTI-SKID STATUS MESSAGE DISPLAYED, NORMAL ANTI-SKID ALSO DISPLAYED, BITE CHECK SHOWS VALVE FAULT, REPLACED NR 2 ANTI-SKID VALVE IAW AMM 32-42-03, LEAK AND OPS CHECKED GOOD.

Part: OXYGEN BOTTLE — EMPTY (CABIN) · airframe 72,246 hrs · 18,263 cycles

TWO PORTABLE OXYGEN CYLINDERS DEPLEATED. SERVICED OXYGEN CYLINDERS IAW GMM 3-28-3.

Part: TRANSDUCER — FAILED (APU BLEED) · airframe 72,118 hrs · 18,234 cycles

APU SURGE BLEED DUCT BLOWN, AND APU BLEED AIR INOPERATIVE. R & R PT TRANSDUCER IAW AMM 49-53-02, OPS CHECKED GOOD. R & R APU SURGE BLEED DUCT IAW AMM 49-53-01. OPS CHECKED. LEAK CHECKED GOOD.

Part: BLEED AIR SYS — INOPERATIVE (APU) · airframe 72,108 hrs · 18,233 cycles

APU BLEED AIR FUNCTION INOPERATIVE.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 72,017 hrs · 18,212 cycles

AFT GALLEY EMERGENCY LIGHT INOPERATIVE. SEATED CONNECTOR IAW AMM 33-51-05, OPS CHECKED GOOD.

Part: STIFFENER — CRACKED (NR 2) · airframe 71,989 hrs · 18,027 cycles

ENG 2, RT SIDE LOW PRESSURE TURBINE COOLING TUBE MANIFOLD STIFFENER CRACKED AT 5 O'CLOCK POSITION. R & R NR 2 ENGINE RT SIDE LOW PRESSURE TURBINE COOLING MANIFOLD IAW AMM 75-24-03.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 71,989 hrs · 18,207 cycles

EMERGENCY LIGHT AFT OF LAV F IS BURNED OUT. R & R EMERGENCY FLOOR TRACK LAMP IAW AMM 33-51-10-962-077.

Part: LENS — WRONG PART (EMERGENCY LIGHT) · airframe 71,989 hrs · 18,207 cycles

FWD CABIN EMERGENCY PATH LIGHTING LENS COLORED WITH RED MARKER. REPLACED FWD CABIN EMERGENCY PATH LIGHTING LENS IAW AMM 33-51-10.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,989 hrs · 18,207 cycles

L2 EXIT EMERGENCY LIGHT IS INOPERATIVE. R & R BULB AT L2 EMERGENCY EXIT LIGHT IAW AMM 33-51-06 OPS CHECKED GOOD.

Part: LINE — DENTED (ENGINE FUEL) · airframe 71,989 hrs · 18,207 cycles

RT PYLON, TOPSIDE FUEL LINE HAS SHALLOW DENT (DENT MEASURES 0.027" DEEP FOUND TO BE WITHIN LIMITS IAW AMM 28-22-07).

Part: CASE — CRACKED (PRECOOLER) · airframe 71,989 hrs · 18,207 cycles

NR 2 ENGINE PRECOOLER CASE IS CRACKED AT LOWER SIDE AT OUTLET WELDED AREA. REPLACED NR 2; ENGINE PRECOOLER TO BE INSTALLED IAW AMM 36-11-15.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 71,989 hrs · 18,207 cycles

R1 DOOR EXIT SIGN HAS BURNED OUT LIGHT BULB. REPLACED BULB IAW AMM 33-51-03, OPS CHECKED GOOD.

Part: CLAMP — BROKEN (APU DUCT) · airframe 71,989 hrs · 18,207 cycles

APU OIL COOLING FAN INLET DUCT CLAMP BROKEN. INSTALLED NEW FAN INLET DUCT CLAMP AT APU OIL COOLING FAN IAW AMM 49-51-02.

Part: LIGHT — MALFUNCTIONED (COCKPIT) · airframe 71,989 hrs · 18,207 cycles

COCKPIT EMERGENCY LIGHT ABOVE DOOR WHEN EXITING STAYS ON. R & R COCKPIT EMERGENCY LIGHT IAW AMM 33-51-01. OPS CHECKED GOOD.

Part: PACKING — DEFECTIVE (APU) · airframe 71,989 hrs · 18,207 cycles

APU BLEED DUCT IS LEAKING AT LOWER SIDE OF APU COMPRESSOR AT FLANGE ATTACH POINT. REPLACED DEFECTIVE PACKING WITH A SERVICABLE PACKING IN PNEUMATIC DUCT AT LOWER SIDE OF APU COMPRESSOR AT FLANGE ATTACH POINT. LEAK CHECKED GOOD IAW AMM 49-53-05.

Part: EXHAUST DUCT — DAMAGED (LT A/C PACK) · airframe 71,989 hrs · 18,207 cycles

LEFT PACK EXHAUST DUCT HAS FIBERGLASS LINING COMING LOOSE INSIDE DUCT. REPAIRED LT PACK EXHAUST DUCT IAW AMM 21-51-23.

Part: INDICATOR — MISSING · airframe 71,989 hrs · 18,207 cycles

LAV H MISSING TEMPERATURE INDICATOR ON WASTE DISPOSAL CHUTE (OUTSIDE). INSTALLED NEW TEMPERATURE INDICATOR ON WASTE DISPOSAL CHUTE (OUTSIDE) ON LAV H IAW AMM 11-35-02.

Part: CONNECTOR — DAMAGED (MODULE) · airframe 71,989 hrs · 18,207 cycles

RT PRV WIRE FAULT DISPLAYED ON AIR SUPPLY BITE MODULE DURING TEST. R & R AIR SUPPLY BITE MODULE IAW 36-20-01. DID NOT FIX PROBLEM. FOUND PUSHED PIN AT D2378A. PIN B8 RESEATED PIN IAW 20-71-13.

Part: MAGNETIC PLUG — BROKEN (STARTER) · airframe 71,989 hrs · 18,207 cycles

NR 1 ENGINE STARTER MAGNETIC DRAIN PLUG ASSY BROKEN DURING REMOVAL. R & R NR 1 ENGINE STARTER MAGNETIC DRAIN PLUG ASSY W/REF AMM 12-22-02-603-054.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 71,989 hrs · 18,207 cycles

RT ENGINE HYD PRIMARY PUMP HAS NO PRESSURE INDICATION. PERFORMED A TEST OF THE RT RESERVOIR PRESSURIZATION SYSTEM. OPS CHECKED GOOD IAW AMM 29-12-00.

Part: SEAL — LEAKING (AIR DUCT) · airframe 71,989 hrs · 18,207 cycles

RT A/C PACK HAS TWO AIR LEAKS AT THE HEAT EXCHANGER DUCTS. REPOSITIONED CLAMP AND TORQUED AT UPPER INBD HEAT EXCHANGER POSITION AND REPLACED SEAL AT INBD CONDENSOR TO HEAT EXCHANGER DUCT, LEAK CHECKED GOOD IAW AMM 21-51-10.

Part: PANEL — LOOSE (LAVATORY) · airframe 71,989 hrs · 18,207 cycles

LAV F, INOPERATIVE 02 PANEL IN CEILING HELD IN PLACE WITH CARGO TAPE. CORNER FOUND TO HAVE LOOSE ATTACHING HARDWARE-TIGHTENDED HARDWARE IAW AMM 20-11-00.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 71,989 hrs · 18,207 cycles

EMERGENCY FLOOR PATH LIGHTING HAS MANY SECTIONS NOT WORKING. REPLACED LAMP AND RESCURED FLOOR PATH LIGHTING IAW AMM 33-51-10. OPS CHECKED OK.

Part: COUPLING — MISINSTALLED (APU) · airframe 71,989 hrs · 18,207 cycles

APU LT; LWR DUCT COUPLINGS INSTALLED INCORRECTLY AFT OF SURGE CONTROL VALVE. ADJUSTED APU LT; LWR DUCT COUPLINGS IAW AMM 49-53-01.

Part: ATTACH BRACKET — CRACKED (STARTER) · airframe 71,989 hrs · 18,207 cycles

NR 2 ENGINE STARTER DUCT ROD ATTACH BRACKET CRACKED (LOWER ROD AT ENGINE ATTACH). R & R CRACKED BRACKET WITH NEW SERVICABLE BRACKET ON NR 2 ENG STARTER DUCT ATTACHING ROD IAW AMM 70-50-00 AND AMM 49-53-01.

Part: CONTROLLER — INOPERATIVE (A/C PACK) · airframe 71,892 hrs · 18,186 cycles

LEFT PACK BITE STATUS MESSAGE. R & R LT PACK CONTROLLER, OPS CHECK & BITE CHECK C/W. MESSAGE DID NOT REPEAT, OK FOR SERVICE. REF MM 21-51-00/601.

Part: FILTER — CLOGGED (HSI) · airframe 71,777 hrs · 18,160 cycles

CAPTAIN'S HSI WEATHER RADAR DISPLAY FAULT MESSAGE INTERMITTENT. PERFORMED SYS INSPECTION AND TEST IAW FIM 34-43-805 & AMP; 34-22-00 FIG103, FOUND CAPTAIN'S HSI INLET COOLING FILTER CLOGGED. ELEMENT SYS, SYSTEM OPS & GROUND TEST GOOD.

Part: IGNITION UNIT — FAULTY (APU) · airframe 71,671 hrs · 18,139 cycles

APU DID NOT START - FAULT LIGHT ON. (R & R APU IGNITION UNIT IAW AMM 49-41-03. OPS CHECKS GOOD.)

Part: WASTEGATE VALVE — STICKING (LAVATORY) · airframe 71,579 hrs · 18,123 cycles

LAV D WASTE FLAP STICKING AND WILL NOT RETURN TOP CLOSED POSITION. WASTE COMP. DOOR LATCH NOT WORKING AND LOOSE HARDWARE. CLEANED LAV D WASTE FLAP HINGE- OPS CHECK GOOD. REPLACED MISSING SCREWS IN TRASH DOOR AT LAV D AS NEEDED - DOOR OPS CHECK GOOD REF 25-00-00 AND 20-11-00 IAW AMM.

Part: COVER — DAMAGED (EMERGENCY LIGHTS) · airframe 71,579 hrs · 18,123 cycles

EMERGENCY FLOOR PATH LIGHTING CONDUIT COVER DAMAGED. R & R EMERGENCY FLOOR PATH LIGHTING CONDUIT COVER AS REQUIRED - OPS CHECK GOOD, AMM 33-51-10.

Part: RESERVOIR — OVERSERVICED (HYD SYSTEM) · airframe 71,579 hrs · 18,123 cycles

EICAS MX MESSAGE "RT HYD QTY O/FULL". REMOVED EXCESS HYD FLUID FROM RT HYD SYS RESERVOIR, OPS CHECKED GOOD AMM 12-12-01.

Part: ANTI-SKID VALVE — INOPERATIVE (NR 8) · airframe 71,579 hrs · 18,123 cycles

NR 8 BRAKE DEACTIVATED DUE TO ANTI-SKID EICAS MESSAGE IN FLIGHT MI 39201. R & R ANTI SKID VALVE IAW AMM 32-42-03.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,579 hrs · 18,123 cycles

EXTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE AT L1 AND R3 DOORS. R & R LAMPS AT L1 AND R3 EXTERIOR EMERGENCY LIGHTS. OPS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 71,579 hrs · 18,123 cycles

FLASHLIGHT LOCATED AT PILOTS SEAT INOPERATIVE. R & R EMERGENCY FLASHLIGHT BATTERY LOCATED AT PILOTS SEAT, CHECKED LIGHT AND RED FLASHING INDICATOR, OPS CHECKED GOOD AMM 25-64-00.

Part: BRACKET — LOOSE (LAVATORY) · airframe 71,579 hrs · 18,123 cycles

LAVATORY E WASTE COMP DOOR CABLE BRACKET RIVETS LOOSE AND PULLED THROUGH. R & R 2 LOOSE RIVETS SECURING BRACKET IN PLACE REF SRM 51-40-02.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 71,579 hrs · 18,123 cycles

FORWARD GALLEY CROSS AISLE FLOOR TRACK LIGHTS INOPERATIVE. FOUND BROKEN PIN ON FLOOR TRACK LIGHT ASSEMBLY AT FWD GALLEY. REPLACED PIN IAW SWPM 20-60-02, OPS CHECK GOOD.

Part: PANEL — DAMAGED (WASTE CONTAINER) · airframe 71,579 hrs · 18,123 cycles

LAVATORY C, F, & H WASTE CONTAINER UPPER SEAL PANEL MISSING HARDWARE. REPLACED HARDWARE ON LAV. C, F, & H WASTE CONTAINER UPPER SEAL PANEL IAW CMM 25-40-64.

Part: GASKET — TORN (FUEL LINE) · airframe 71,514 hrs · 18,111 cycles

FUEL LEAK AT NR 1 ENGINE. FOUND FUEL LINE BETWEEN HMU & TRANSMITTER GASKET TORN, R & R GASKET ON HMU TRANSMITTER LINE, LEAK CHECKED GOOD. REF AMM 73-33-00/001.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,442 hrs · 18,100 cycles

EMERGENCY LIGHT AT R2 DOOR INOPERATIVE. REPLACED LAMP, OPS CHECKED GOOD IAW AMM 33-51-00.

Part: SUMP — LEAKING (LT FUEL TANK) · airframe 71,454 hrs · 18,101 cycles

LT MAIN TANK FWD FUEL SUMP LEAKING. RESEATED LT MAIN SUMP IAW MM 12-11-03 NO LEAK NOTED.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 71,442 hrs · 18,100 cycles

TWO BULBS BURNED OUT AT R3 EMERGENCY EXIT SIGN. REPLACED LAMPS IAW 33-51-00. OPS CHECKED OK.

Part: WIRE — DISCONNECTED (EMERGENCYLIGHT) · airframe 71,348 hrs · 18,081 cycles

UPON ARRIVAL, MX INSPECTOR FOUND MID CABIN LT SIDE WHOLE ROW OF FLOOR EMERGENCY LIGHTS INOPERATIVE. FOUND WIRE DISCONNECTED FROM LIGHT MODULE, RE-INSTALLED WIRE, OPS CHECKED GOOD IAW MM 33-50-01.

Part: WARNING LIGHT — FALSE ACTIVATION (RUDDER) · airframe 71,344 hrs · 18,080 cycles

AFTER ENGINE START, EICAS MESSAGE " RUDDER RATIO", BLOCK TURN-BACK. PERFORMED RUDDER RATIO OPS CHECK IAW AMM 27-21-00, SUB TASK 27-21-00-215, OPS CHECKED GOOD. NO DEFECTS NOTED AT THIS TIME.

Part: APU — MALFUNCTIONED · airframe 71,311 hrs · 18,071 cycles

APU FAULT ON START ATTEMPT AFTER LANDING. OPEN

Part: VALVE — INOPERATIVE · airframe 71,160 hrs · 18,028 cycles

HMG VALVE INOPERATIVE. R & R HMG VALVE IAW AMM 24-25-03,, GROUND OPS CHECKED GOOD.

Part: PRESSURE SWITCH — MALFUNCTIONED (ANTI ICE SYS) · airframe 71,086 hrs · 18,014 cycles

STATUS MESSAGE "NR 1 ANTI-ICE VALVE" DISPLAYED. R & R NR 1 ANTI ICE VALVE SWITCH, IAW AMM 30-21-01, OPS CHECKS GOOD, ENGINE RUN OPS CHECKS GOO, IAW AMM 72-00-00.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 71,086 hrs · 18,014 cycles

F/O OXYGEN MASK LEAKING. R & R OXYGEN MASK, LEAK CHECKED GOOD, REF AMM 35-11-54.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 71,086 hrs · 18,014 cycles

RT FORWARD EMERGENCY PATH LIGHTS HAS SECTION INOPERATIVE. CONNECTED EMERGENCY PATH LIGHT, OPS CHECKED GOOD IAW AMM 33-51-10-402-113.

Part: WARNING MESSAGE — ILLUMINATED (LT ENGINE) · airframe 71,080 hrs · 18,012 cycles

AT 5+30 HRS INTO FLT STATUS MESSAGE LT ENG TAI VALVE. PERFORMED FIM 30-21 FAULT TREE 805 PROCEDURES, ENGINE TAI OPS CHECK NORMAL.

Part: WIRE — EXPOSED (EMERGENCY LIGHT) · airframe 71,050 hrs · 18,007 cycles

EMERGENCY TRACK LIGHT WIRE EXPOSED AT SEAT 4H. REPOSITIONED FLOOR TRACK IAW AMM 33-51-10, OPS CHECK GOOD.

Part: WIRE — EXPOSED (EMERGENCY LIGHT) · airframe 71,050 hrs · 18,007 cycles

EMERGENCY TRACK LIGHTING WIRE EXPOSED AT R2 DOOR. REINSTALLED LENS CAP IAW AMM 33-51-10, OPS CHECK GOOD.

Part: WIRE — EXPOSED (EMERGENCY LIGHT) · airframe 71,050 hrs · 18,007 cycles

EMERGENCY TRACK LIGHT WIRE EXPOSED AT SEAT 4H. REPOSITIONED FLOOR TRACK IAW AMM 33-51-10, OPS CHECK GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 71,050 hrs · 18,007 cycles

EMERGENCY TRACK LIGHT WIRE EXPOSED AT R2 DOOR. REINSTALLED LENS COVER IAW AMM 33-51-10, OPS CHECKED GOOD.

Part: WIRE — EXPOSED (EMERGENCY LIGHT) · airframe 71,050 hrs · 18,007 cycles

EMERGENCY TRACK LIGHT EXPOSED AT SEAT 43H. REPOSITIONED FLOOR TRACK COVER IAW AMM 25-27-01 OPS CHECK GOOD.

Part: BLADE — NICKED (ENGINE FAN) · airframe 71,050 hrs · 18,007 cycles

FAN BLADE NICKED NR 1 ENGINE. BLENDED AREA WITHIN LIMITS IAW AMM 72-31-02, FLORESCENT PARTICLE INSPECTION WITH NO ITEMS INDICATED.

Part: SHUTOFF VALVE — INTERMITTENT (BLEED AIR SYS) · airframe 70,887 hrs · 17,974 cycles

LEFT ENGINE HPSOV ILLUMINATED INTERMITTENTLY DURING ALL PHASES OF FLIGHT. R & R LT ENGINE HPSOV IAW AMM 36-11-07, SYS BITE, LEAK CHECKED GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 70,873 hrs · 17,970 cycles

EMERGENCY LIGHT LENS MISSING AT THE FOLLOWING POSITIONS; 25 A, 43A AND 43F.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 70,832 hrs · 17,957 cycles

R2 DOOR FLASHLIGHT INOPERATIVE. R & R BATTERY IAW MM 25-64-00. OPS NORMAL.

Part: CONTROL VALVE — MALFUNCTIONED (RT A/C PACK) · airframe 70,763 hrs · 17,935 cycles

RT PACK TEMP CONTROL VALVE TRIPS ALERT DURING BITE TEST. REPLACED THE RT PACK TEMP CONTROL VALVE, IAW AMM 21-51-11. OPS CHECKED GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 70,763 hrs · 17,935 cycles

BEFORE DEPARTURE, FLIGHT CREW REPORTED EICAS MESSAGE " RT PACK TEMP" APPEAR. SYS OPS CHECKS GOOD IN STANDBY AND MANUAL.

Part: HOSE — LEAKING (OXYGEN MASK) · airframe 70,679 hrs · 17,909 cycles

FIRST OFFICER`S O2 MASK STARTED LEAKING OXYGEN. REPLACED FLEXIABLE HOSE BELOW O2 MASK. OPS AND LEAK CHECKED GOOD. INSTALLED IAW AMM 20-10-10.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 70,662 hrs · 17,905 cycles

EMERGENCY LIGHT, ROW 4 BEHIND SEAT H, COVER BROKEN. RECONNECTED EMERGENCY LIGHT COVER, OPS CHECK GOOD, REF AMM 33-51-10.

Part: FILTER — WARNING LIGHT (FUEL SYSTEM) · airframe 70,630 hrs · 17,898 cycles

LT ENG FUEL FILT STATUS MESSAGE. R & R LT ENGINE FUEL FILTER, LEAK CHECK, OPS CHECKED GOOD, STATUS MESSAGE CLEARED. REF AMM 73-11-02-004-001-H00, ENG 71-00-00.

Part: REGULATOR — LEAKING (CREW OXYGEN) · airframe 70,473 hrs · 17,864 cycles

WHILE LEAK CHECKING CREW OXYGEN CYLINDER REPLACEMENT, FOUND LEAK AT OXYGEN REGULATOR. R & R CREW O2 REGULATOR, TRANSDUCER ASSY IAW AMM 35-11-03, OPS ; LEAK CHECK GOOD.

Part: FILTER ELEMENT — FAILED (RT ENGINE) · airframe 70,468 hrs · 17,861 cycles

RT ENGINE FUEL FILTER MESSAGE, REPLACED RT ENGINE FUEL FILTER ELEMENT IAW AMM 73-11-02/401. DRY MOTORED AND WET MOTORED IAW AMM 71-00-00, OPS CHECKED GOOD.

Part: ACTUATOR — FAILED (FUEL VALVE) · airframe 70,464 hrs · 17,860 cycles

APU WOULD NOT START AT GATE "APU FUEL VALVE" EICAS MESSAGE. R & R APU FUEL VALVE ACTUATOR. LEAK & OPS CHECKED. REF AMM 28-25-02/401.

Part: SEAL — BROKEN (PBE) · airframe 70,447 hrs · 17,858 cycles

PBE AT L1 DOOR CLOSET HAS A BROKEN SEAL. R & R PBE IAW AMM 35-31-02.

Part: SHUTOFF VALVE — MALFUNCTIONED (HYD SYSTEM) · airframe 70,437 hrs · 17,854 cycles

AIR DRIVEN PUMP IS BYPASSING AIR WHEN ADP IS TURNED OFF. REPLACED ADP PRSOV IAW AMM 29-11-30, OPS CHECKS GOOD. THIS IS AN ETOPS SIGNIFICANT SYS.

Part: MOTOR — FAILED (LE FLAPS) · airframe 70,438 hrs · 17,855 cycles

ON FLAP EXTENSION, "L/E FLAP DISAGREE MSG" ILLUMINATED- NO ROLL TENDENCY, QRH PROCEDURE FOLLOWED. RETURNED FLAPS TO NORMAL CONFIG. ON SUBSEQUENT EXTENSION FLAPS, EXTENDED NORMALLY. GAGE INDICATOR APPEARS TO JUMP BETWEEN FLAPS 1 AND FLAPS UP. (ACCOMPLISHED FLAP/SLAT PRIMARY AND ALTERNATE SYS CHECK IAW AMM 27-81-00. PRIMARY CHECKS OK. ALTERNATE CHECK FAILED,VERY SLOW TO EXTEND INBD SLATS. REPLACED ELECTRIC MOTOR, FOR INBD POSITION, IAW AMM 27-81-11. ACCOMPLISHED ALTERNATE SYS CHECK, ALL CHECKS GOOD, NO FAULTS. INSTALLATION REQUIRED USING ADAPTER PLATE IAW AMM 27-81-11)

Part: WARNING LIGHT — FALSE ACTIVATION (BLEED SYSTEM) · airframe 70,431 hrs · 17,853 cycles

APPROXIMATELY 1 HOUR 10 MINUTES INTO THE FLIGHT, ENCOUNTERED A "LT BLEED DUCT LEAK" EICAS MESSAGE, ALONG WITH "DUCT LEAK" CAUTION LIGHT AND MASTER CAUTION LIGHTS. THE LIGHTS AND EICAS MESSAGE INITIALLY CAME ON THEN WENT OFF AND CAME BACK ON STEADY. ACCOMPLISHED THE BLEED DUCT LEAK NON-NORMAL CHECKLIST AND ALL CAUTION AND EICAS MESSAGES WENT OUT. AIR TURNBACK ACCOMPLISHED; BACK TO DEPARTURE. DISPATCH. BEING WORKED.

Part: SWITCH — INOPERATIVE (BOOST PUMP) · airframe 70,387 hrs · 17,845 cycles

LEFT AFT BOOST PUMP SWITCH INOPERATIVE. REPLACED PUSH SWITCH ASSY IAW AMM 33-13-00, OPS CHECKED GOOD.

Part: ANTENNA — MISMANUFACTURED (ELT) · airframe 70,340 hrs · 17,838 cycles

DURING PREFLIGHT INSPECTION, F/A FOUND ELT'S ANTENNA CABLE (PORTABLE) TO BE IMPROPERLY WOUND. R & R ELT UNIT IAW CMM 25-60-10, PG 18- 25. RESOLVED THE FORWARD ELT. SECOND ELT (AFT) TRANSFERRED TO MEL 25-63-10-01, CAT. D, MDDR 34976, MCC AND DISPATH NOTIFIED.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 70,319 hrs · 17,834 cycles

LEFT BLEED DUCT LEAK DISPLAYED APPROX 1 HR AFTER TAKE OFF. DUCT LEAK LT ON OVERHEAD PANEL ILLUMINATED. QRH NON-NORMAL PROC ACCOMPLISHED. ABLE TO ESTABLISH NORMAL OPS, AND NORMAL OPS REMAINDER OF FLIGHT. TROUBLESHOT IAW FIM PROCEDURE 26-18-00 PG 105, NO FAULTS NOTED.

Part: CIRCUIT CARD — FAILED (FAN CONTROL) · airframe 70,064 hrs · 17,793 cycles

DURING CLIMBOUT EICAS MESSAGE FWD EQUIPMENT OVERHEAT DISPLAYED ALONG WITH OVERHEAT LIGHT ON OVERHEAD. FOLLOWED QRH PROCEDURE. LIGHTS REMAINED EXTINGUISHED. REPLACED M990 ECS FAN CONTROL CARD IAW AMM 21-26-05. OPS CHECKS GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,606 hrs · 17,716 cycles

CEILING LIGHT BETWEEN ROW 39 AND 39 EMERGENCY LIGHT INOPERATIVE. RELAMPED IAW AMM 33-51-00.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,606 hrs · 17,716 cycles

R3 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED IAW AMM 33-51-00.

Part: BLADE — DAMAGED (NR 1 FAN) · airframe 69,606 hrs · 17,716 cycles

NR 1 ENGINE FIRST STAGE FAN L/E HAS FOD IN AREA "B". REPAIRED BLENDED IAW AMM 72-31-02.

Part: PUMP — INOPERATIVE (HYD SYSTEM) · airframe 69,606 hrs · 17,716 cycles

NR 2 PYLON HYD CASE DRAIN FILTER MODULE DPI BUTTON DEPLOYED. REPLACED ENGINE DRIVEN PUMP AND FILTER IAW AMM 29-11-00.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,606 hrs · 17,716 cycles

L2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED IAW AMM 33-51-00.

Part: WARNING LIGHT — FALSE ACTIVATION (RT A/C PACK) · airframe 69,542 hrs · 17,704 cycles

EICAS MESSAGE "RT PACK OFF" DURING FLT. PERFORMED OPS TEST AND RESET OF BOTH PACKS IAW FIM 21-51-00, FIG 109A SHEET 1. NO FAULTS FOUND. OK FOR SERVICE. BITE CHECK OF PACK TEMP CONTROL SHOWS NO FAULTS BEFORE OR AFTER SYS CHECK.

Part: DOOR — BENT (LT MLG) · airframe 69,185 hrs · 17,637 cycles

LEFT MLG TRUNNION DOOR BENT T/E AFT CORNER. ACCOMPLISHED EO 6752A005, REF ITEM PART 1.

Part: BLEED VALVE — FAILED (APU ENGINE) · airframe 69,105 hrs · 17,623 cycles

APU FAULT MESSAGE ON EICAS. APU FAILED AT ENGINE START WHEN APU BLEED SELECTED. R & R APU SURGE BLEED VALVE, OPS CHECKED SATISFACTORY IAW AMM 49-53-01.

Part: SWITCH — FAILED (FUEL BOOST PUMP) · airframe 68,987 hrs · 17,600 cycles

LEFT FWD BOOST PUMP CANNOT BE SELECTED ON WIGH SWITCH. PUMP OPS NORMAL. REMOVED & REPLACED FUEL PUMP SWITCH ASSY, OPS CHECKED GOOD IAW AMM 33-13-00 902-024, 28-22-00.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 68,984 hrs · 17,599 cycles

NO RED LENS ON EMERGENCY PATH LIGHTING. INSTALLED RED LENS COVERS ON EMERGENCY PATH LIGHTING.

Part: DRIVE ASSY — INOPERATIVE (WEATHER RADAR) · airframe 68,977 hrs · 17,597 cycles

LEFT & RIGHT WEATHER RADAR INOPERATIVE. R & R RADAR ANTENNA DRIVE AND ANTENNA SENSOR IAW MM 34-43-05/ 34-43-07, SYS OPS CHECKED GOOD IAW MM 34-43-00/501.