N1399A

Part: FUEL CELL — LEAKING (ZONE 500) · airframe 101,694 hrs · 21,099 cycles

FUEL LEAK ON LEFT WING LWR SIDE OF BODY SPLICE PLATE AT STRINGER L-15 AND WBL 97.5 APROX.(<P>FUEL LEAK ON LEFT WING LWR SIDE OF BODY SPLICE PLATE AT STRINGER L- 15 AND WBL 97.5 APROX. SEALANT WAS REMOVED AND REPLACED. CLASS "A" AND CLASS "B" SEALANT WAS INSTALLED AND TEST FOR LEAK WAS PERFORMED AND WAS SATISFACTORY. REF AMM 28-11-00-308-013 REV 144.</P>)

Part: FUEL CELL — LEAKING (ZONE 500) · airframe 101,694 hrs · 21,099 cycles

FUEL LEAK ON LEFT WING LWR SIDE OF BODY SPLICE PLATE AT STRINGER L-6 AND WBL 97.5 APROX.(<P>FUEL LEAK ON LEFT WING LWR SIDE OF BODY SPLICE PLATE AT STRINGER L-6 AND WBL 97.5 APROX. THE AREA WAS VENTILATED, THE REMAINING FUEL WAS CLEANED, THE SEALANT IS REMOVED, THE AREA WAS CLEANED CORRECTLY, CLASS "A" AND CLASS "B" SEALANT WAS APPLIED CORRECTLY, THE FUEL LEAK TEST WAS PERFORMED SATISFACTORY IAW AMM 28-11-00-308-013.</P>)

Part: RETAINER — CORRODED (ZONE 800) · airframe 101,694 hrs · 21,099 cycles

MAIN LANDING GEAR DOOR RH, TRACK OF SEAL BULB AFT, WITH EVIDENCE WITH CORROSION.(<P>MAIN LANDING GEAR DOOR RH, TR ACK OF SEAL BULB AFT, WITH EVIDENCE WITH CORROSION, WAS REPLACED IAW SRM 51-10-02-0G-0 REV 127. NO FURTHER DEFECTS NOTED</P>)

Part: PCA — LEAKING (ZONE 500 AILERON) · airframe 101,694 hrs · 21,099 cycles

LH WING INBOARD AILERON INBOARD PCA WITH EVIDENCE HYDRAULIC LEAK.(<P>INBOARD PCA WAS REPLACED I.A.W. AMM 27- 11-48-422-040, REV. 144, DATE: DEC. 22, 2024. TORQUE APPLIED: ROD END: 1200 IN- LB, S/N: 0808504320. INBOARD AILERON ADJUSTMENT AND OPERATIONAL TEST WERE PERFORMED, I.A.W. AMM 27-11-48-244- 040, REV. 144, OPS CHECK GOOD.</P>)

Part: SKIN — DELAMINATED (ZONE 500 FLAP) · airframe 101,694 hrs · 21,099 cycles

LH WING, L/E OUTBD FLAP, FROM INBD EDGE TO 58 INCHES TO OUTSIDE WITH DELAMINATION.(<P>LH WING, L/E OUTBD FLAP, FROM INBD EDGE TO 58 INCHES WAS REPAIRED IAW SRM 57-53-01-2R-1 FIG 10 AND SRM 51-70-17-17-0G-0 PAR.4.A REV 127. NO FURTHER DEFECTS NOTED</P>)

Part: STRUCTURE — NONE (NLG WW) · airframe 101,694 hrs · 21,099 cycles

MISSING CIC ON SEVERAL AREAS OF NOSE LANDING GEAR WHEEL WELL.(<P>MISSING CIC ON SEVERAL AREAS OF NOSE LANDING GEAR WHEEL WELL. DAMAGED CIC WAS REMOVED AND AREA CLEANED FOR APPLICATION, CIC IS APPLIED CORRECTLY. AMM 51-24-09-377-008 REV 143 AND AMM 51-24-09-917-012 REV 143. NO FURTHER DEFECTS NOTED</P>)

Part: PCU — LEAKING (LT ELEVATOR) · airframe 101,694 hrs · 21,099 cycles

LH ELEVATOR, PCU'S LEAKING EVIDENCE.(<P>LH ELEVATOR, INBOARD, AND OUTBOARD PCA WERE REPLACED IAW AMM 29-31-05-424-027 REV144. TORQUE APPLIED: 200 LB-IN, 270 LB-IN S/N:040674400. ADJUSTMENT WAS PERFORMED. OPERATIONAL TEST WAS SATISFACTORY.</P>)

Part: FUEL TANK — LEAKING (MAIN) · airframe 101,694 hrs · 21,099 cycles

FUEL LEAK ON RIGHT WING LWR SIDE OF BODY SPLICE PLATE AT STRINGER L-15 AND WBL 97.5 APROX.(<P>THE SEALANT IS REMOVED, THE AREA IS CLEANED CORRECTLY, CLASS "A" AND CLASS "B" SEALANT IS APPLIED CORRECTLY AND THE FUEL LEAK TEST PERFORMED WAS SATISFACTORY. AMM 28-11-00-308-013 REV 143.</P>)

Part: LENS — BROKEN (ZONE 200) · airframe 101,694 hrs · 21,099 cycles

BROKEN EMERGENCY LIGHT ON FWD LH PASSENGER DOOR.(<P>LINING INSTL- FWD ENTRY DOOR, FWD SIDE DOORWAY LENS (EXIT) WAS INSTALLED IAW AMM 33-51-01-400-801-001. OPS CHK OK</P>)

Part: ACCESS PANEL — LOOSE (ZONE 400) · airframe 101,694 hrs · 21,099 cycles

ENG 1, INNER ACCESS PANEL 432 FL, PIPE "FIRE PROTECTION" WITH NUT LOOSE.(<P>ENG 1, INNER ACCESS PANEL 432 FL, PIPE "FIRE PROTECTION" NUT WAS TORQUED AND VERIFIED IAW AMM 20-11-00-910-801. NO FURTHER DEFECTS NOTED</P>)

Part: FRAME — CORRODED (ENG FAN COWL) · corrosion level 2 · airframe 101,694 hrs · 21,099 cycles

ENGINE 2 AIR INLET COWL, FAN FRAME, AROUND AT 7 TO 8 O CLOCK POSITION WITH CORROSION.(<P>&NBSP;ENG 2 INLET COWL WAS REPLACED IAW 71-11-01-404-005-H00 REV 144. NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — WORN (ZONE 600 SLAT) · airframe 101,694 hrs · 21,099 cycles

RH WING, SLAT # 7, WORN LOWER SKIN.(<P>RH WING, SLAT 7 LOWER SKIN WAS REPAIRED I.A.W SRM 57-43-02-2R-1 PG 1-3 FIG 201 AND SRM 51-70-10-2R-4 PG 1,15 FIG 202 SHEET 8 REV 127 15-DEC-24. NO FURTHER DEFECTS NOTED</P>)

Part: ORIFICE — OBSTRUCTED (ZONE 100) · airframe 101,694 hrs · 21,099 cycles

FWD CARGO COMPARTMENT CARGO SMOKE DET AIR SAMPLING INTAKE ORIFICES BLOCKED AND DIRTY.(<P>FWD CARGO COMPARTMENT CARGO SMOKE DET AIR SAMPLING INTAKE ORIFICES WERE CLEANED IAW AMM 26-05-03-202-001 REV 143. NO FURTHER DEFECTS NOTED</P>)

Part: SUPPORT ANGLE — CRACKED (ZONE 400) · airframe 101,694 hrs · 21,099 cycles

BROKEN ENG 2, ACCESS PANEL 447DB, ANGLE SUPPORT WITH CRACK.(<P>THE BROKEN SUPPORT ANGLE WAS REMOVED, THE AREA WAS CLEANED, THE NEW SUPPORT ANGLE WAS DRILLED AND INSTALLED CORRECTLY. THE SUPPORT ANGLE WAS REPLACED WITH A NEW ONE. DWG 313T3360 SRM 51-40-02-OG-O REV 127 15DEC-24 AND SRM 51-10-02-OG-O PAR 9 REV 127 15DEC24. NO FURTHER DEFECTS NOTED</P>)

Part: ACOUSTIC PANEL — CORRODED (ZONE 400) · corrosion level 2 · airframe 101,694 hrs · 21,099 cycles

ENGINE 2, AIR INLET COWL, ACOUSTICAL PANEL AT 7 TO 8 O'CLOCK POSITION WITH EVIDENCE OF CORROSION.(<P>ENGINE 2, AIR INLET COWL, ACOUSTICAL PANEL AT 7 TO 8 O'CLOCK POSITION WITH EVIDENCE OF LEVEL 2 CORROSION WAS REPLACED IAW AMM 71-11-01-404-005-H00 REV 144. NO FURTHER DEFECTS NOTED</P>)

Part: STRIP — CORRODED (ZONE 400) · airframe 101,694 hrs · 21,099 cycles

ENG 1, RH CORE COWL, UPPER STRIP WITH CORROSION. L: 2.500 IN, W: 1.000 IN.(<P>THE CORROSION METAL STRIP WAS REMOVED, THE NEW METAL STRIP WAS DRILLED AND WAS INSTALLED CORRECTLY. SRM 51-40-02-0G-0 REV 127 15DEC24 AND SRM 51-10-02-0G-0 PAR 9. LEVEL 1. NO FURTHER DEFECTS NOTED</P>)

Part: SERVO — LEAKING (ZONE 300) · airframe 101,694 hrs · 21,099 cycles

VERTICAL STABILIZER, REAR SPAR, YAW DAMPER SERVOS ASSY, LEAKING EVIDENCE.(<P>YAW DAMPER SERVOS LEFT AND RIGHT, WERE REPLACED, TEST WERE PERFORMED AND HYD LEAKAGE CHECK WAS PERFORMED AND TORQUE WAS APPLIED IAW AMM 22-21-02-414-016 REV 143. OPS CHECK GOOD.&NBSP;</P>)

Part: SKIN — CRACKED (ZONE 200) · airframe 101,694 hrs · 21,099 cycles

FORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER WITH TWO CRACK INDICATIONS AT HOLE 2 ON SKIN, POSITION 11 O´CLOCK AND 5 O'CLOCK, SEE N.D.T. INSPECTION REPORT.(<P>TWO CRACK INDICATIONS AT HOLE 2 ON SKIN, POSITION 11 O´CLOCK AND 5 O'CLOCK, WERE REPAIRED IAW SRM 53-10-01-2R-1 DETAIL II REV 127. CATEGORY REPAIR "B". NO FURTHER DEFECTS NOTED</P>)

Part: ORIFICE — OBSTRUCTED (SMOKE DETECTOR) · airframe 101,694 hrs · 21,099 cycles

AFT AND BULK CARGO COMPATMENT CARGO SMOKE DET AIR SAMPLING ORIFICES BLOCKED AND DIRTY.(<P>SMOKE DET AIR SAMPLING ORIFICES WERE CLEANED IAW 26-05-03-202-001 REV 143 22AUG24. NO FURTHER DEFECTS NOTED</P>)

Part: PCU — LEAKING (ELEVATORS) · airframe 101,694 hrs · 21,099 cycles

RH ELEVATOR PCU'S LEAKING EVIDENCE.(<P>RH ELEVATOR, INBOARD, AND OUTBOARD PCA WERE REPLACED IAW AMM 29-31-05-424-027 REV 144. TORQUE WAS APPLIED: 200 LB-IN, 270 LB-IN S/N: 0406744400. ADJUSTMENT WAS PERFORMED. OPERATIONAL TEST WAS SATISFACTORY.</P>)

Part: FRAME — CORRODED (ENG FAN CASE) · corrosion level 2 · airframe 101,694 hrs · 21,099 cycles

ENG 1, FAN FRAME, BTWN 4-8 O'CLOCK SURFACE WITH SEVERAL POINTS OF CORROSION.(<P>ENG 1, FLOWPATH EXTENSION BETWEEN 4 TO 8 O'CLOCK WERE REPLACED IAW AMM 72-33-00-308-104-H00 REV 144. NO FURTHER DEFECTS NOTED</P>)

Part: ACCESS PANEL — MISINSTALLED (ZONE 200) · airframe 101,694 hrs · 21,099 cycles

ACCESS PANEL OF MAIN DECK CARGO SMOKE DETECTOR WAS <SPAN STYLE="FONT-SIZE: 13.3333PX;">INSTALLED WRONG. </SPAN><SPAN STYLE="FONT-SIZE: 13.3333PX;"> </SPAN>(CCD ZONE 121)(<P>CARGO SMOKE DETECTOR ACCESS PANEL WAS INSTALLED CORRECTLY IAW AMM 23-16-01-400-801-061 STEP C. NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — DENTED (ZONE 600 SLAT) · airframe 101,694 hrs · 21,099 cycles

RH WING, SLAT #11 DENT ON UPPER SKIN.(<P>RH WING, SLAT 11 WAS REPAIRED IAW SRM 57-43-02-2R-1 REP 1 PAGE 2-3 FIG 201 AND SRM 51-70-1 OOR REP 4 PAGE 1-7 FIG 201 (SHEET 2) REV 127. 15-DEC-24. NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — CRACKED (ZONE 200) · airframe 101,694 hrs · 21,099 cycles

FUSELAGE - SECTION 41 - SERVICE DOOR CUTOUT AFT LOWER CORNER WITH A CRACK INDICATION AT HOLE 2 ON SKIN AND BEAR STRAP, POSITION 2 O´CLOCK, SEE N.D.T. INSPECTION REPORT.(<P>CRACK ON RH FUSELAGE, R1 DOOR CUTOUT, AFT LOWER CORNER ON SKIN WAS REPAIRED IAW SRM 53-10-01-2R-1 PAGE 1-17 REV 127. CATEGORY REPAIR "B". NO FURTHER DEFECTS NOTED.</P>)

Part: PCA — LEAKING (ZONE 600 AILERON) · airframe 101,694 hrs · 21,099 cycles

RIGHT WING INBOARD AILERON, PCA´S WITH LEAK EVIDENCE.(<P>RIGHT WING INBOARD AILERON, PCA´S LH, AND RH WERE REPLACED I.A.W AMM 27-11-48-022-003. NO FURTHER DEFECTS NOTED</P>)

Part: FUEL CELL — LEAKING (ZONE 500) · airframe 101,694 hrs · 21,099 cycles

FUEL LEAK EVIDENCE, LH WING LOWER SIDE AT BODY SPLICE AND STRINGER 10 AND 15.(<P>THE AREA WAS VENTILATED, THE REMAINING FUEL WAS CLEANED, THE SEALANT WAS REMOVED, THE AREA WAS CLEANED CORRECTLY, CLASS "A" AND CLASS "B" SEALANT WAS APPLIED CORRECTLY, THE FUEL LEAK TEST WAS PERFORMED AND WAS SATISFACTORY.</P>)

Part: LINE — LEAKING (ZONE 500) · airframe 101,694 hrs · 21,099 cycles

ENG 2 NACELLE STRUT LINE WITH LEAK.(<P>ENG 2 NACELLE STRUT LINE WITH LEAK, TORQUE WAS APPLIED 127 LB-IN SN:1017801833</P> / <P>DATE: 11-APR-25 IAW AMM: 71-00-02-404-049-H03 REV.144 DATE: 22-DEC-2024. LEAK CHECK WAS GOOD.</P>)

Part: STRUCTURE — NONE (NLG WW) · airframe 101,694 hrs · 21,099 cycles

CONTAMINATED EWIS WITH CIC OF NOSE LANDING GEAR WHEEL WELL.<BR>(<P>NOSE LANDING GEAR WHEEL WELL EWIS WAS CLEANED IAW SWPM 20-10-04 REV 87. NO FURTHER DEFECTS NOTED</P>)

Part: WARNING MESSAGE — FALSE INDICATION (HYD PUMP) · airframe 101,297 hrs · 20,926 cycles

ON APPROACH CENTER PRIMARY HYD PUMP #1 EICAS MSG(<P>PERFORMED TROUBLESHOOTING AND OPS CHECKS IAW FIM 29-11 FAULT TREE 810. OPS CHECK GOOD, NO C/B'S POPPED, COULD NOT DUPLICATE. NO FURTHER MX REQUIRED.</P>)

Part: BULB — INOPERATIVE (ZONE 200) · airframe 100,592 hrs · 20,644 cycles

BACKLIGHTING FOR EMERG LIGHT PAX OXY PANEL ONLY 1/2 ILLUMINATED. REPAIRED LIGHTPLATE & REPLACED BULBS PER SWPM 20-40-00. OPS CK OK PER 33-13-01.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 99,268 hrs · 20,157 cycles

LH WING, LOWER SURFACE, BBL 97.42 AND STRINGER 10 WITH FUEL LEAK(<P>LH WING, LOWER SURFACE, BBL 97.42 AND STRINGER 10 FUEL LEAK WAS REPAIRED AND TEST WAS SATISFACTORY IAW AMM 28-11-00-308-013 REV 140 22 AUG 23.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 99,268 hrs · 20,157 cycles

ENG 2, OUTBOARD THRUST REVERSER, MISSING ANTI-FIRE COVER AT INTERNAL PROTECTION(<P>&NBSP;ENG 2, OUTBOARD THRUST REVERSER, ANTI-FIRE COVER AT INTERNAL PROTECTION WAS REPAIRED AMM 78-31-00-308-072-H00 REV 140 22 AUG 23. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 99,268 hrs · 20,157 cycles

ENG 2, OUTBOARD THRUST REVERSER, DISBONDED ANTI-FIRE SEAL PROTECTION AT UPPER FWD CORNER(<P>&NBSP;</P> / <P>ENG 2, OUTBOARD THRUST REVERSER, ANTI-FIRE SEAL PROTECTION AT UPPER FWD CORNER WAS REPAIRED PER AMM 78-31-00-308-072-H00 REV 140 22 AUG 23</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 99,268 hrs · 20,157 cycles

RH WING FUEL LEAK STA 642.20 & 668.20(<P>FUEL LEAKS WERE CORRECTED IAW AMM 28-11-00-308-013. NO FURTHER DEFECTS NOTED</P>)

Part: MODULE — UNKNOWN (UNKNOWN) · airframe 99,268 hrs · 20,157 cycles

IN THE OPERATIONAL CHECK OF CARGO FIRE EXTINGUISHING BOTTLE, RELAYS THE AFT ARM SWITCH FOUND INOPERATIVE.(<P>TASK CARD A-26-016-00-01/002. CARGO FIRE EXT BOTTLE RELAY AFT CARGO WAS ACCOMPLISHED IAW TASK CARD A-26-016-00-01/001 (NR00509) AND MODULE ASSY MASTER WAS REPLACED IAW AMM 26-23-01-706-038 REV 140 DATE 22AUG2023. OPERATIONAL TEST WAS PERFORMED SATISFACTORY.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 99,268 hrs · 20,157 cycles

MAIN DECK CARGO DOOR, ZONE 838 WITH PRESSURIZATION LEAKS.(<P>PRESSURIZATION LEAKS WERE EVALUATED AND FOUND WITHIN THE ADL IAW AMM 05-51-24-782-001</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 99,268 hrs · 20,157 cycles

RH WING INBOARD MAIN FLAP L/E HOLE (FROM 26 IN RH EDGE)(<P>RH WING INBOARD MAIN FLAP, AFT FLAP WAS REPAIRED IAW SRM 57-53-01-2R-1 FIG 201 SHEET 5 PAGE 2-3, 6 AND SRM 51-70-17-0G-0 PAR 4 B FIG 24 PAGE 14, 55 REV.124 DEC 15/2023</P>)

Part: NUT — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 99,268 hrs · 20,157 cycles

MAIN EQUIPMENT CENTER BOX NLG UPPER SIDE BETWEEN STA 266/287 MECHANISM LOCK NLG ROD END WITH EVIDENCE OF CORROSION(<P>THE NUT ON ROD END WAS REPLACED. TORQUE 170 LB/IN WAS APPLIED. IAW AMM 32-21-06-404-023 REV:140 DATE: 22/AUG/23 TORQUE DATA: S/N: 05229028 EXP: 10/MAR/24</P>)

Part: STIFFENER — UNKNOWN (UNKNOWN) · airframe 99,268 hrs · 20,157 cycles

NACELLE STRUT #2 UPPER SPAR WEB CRACK IN LH STIFFENER NAC STA 196.86 (JUST BELOW UPPER LINK)(<P>R/R STIFFENER IAW BOEING DRAWING 311T1130. NO FURTHER DEFECTS NOTED.</P>)

Part: STRINGER SPLICE — UNKNOWN (UNKNOWN) · airframe 99,268 hrs · 20,157 cycles

MDC UPPEN MAIN - AUX SILLS SPLICE TO STRINGERS - BETWEEN STA 412 TO STA 434 ON STRINGER 17, CRACK INDICATION FOUND.(<P>STRINGER SPLICE WAS REPLACE IAW DRAWING 311T1130, FVCI #23238-1 REV A. NO FURTHER DEFECTS NOTED</P>)

Part: STRINGER SPLICE — UNKNOWN (UNKNOWN) · airframe 99,268 hrs · 20,157 cycles

MDC UPPEN MAIN - AUX SILLS SPLICE TO STRINGERS - BETWEEN STA 412 TO STA 434 ON STRINGER 13, CRACK INDICATION FOUND.(<P>STRINGER SPLICE WAS REPLACED IAW DRAWING 311T1130 &AMP; FVCI #23238-1 REV A. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 99,268 hrs · 20,157 cycles

KEEL BEAM LOWER SIDE LOWER FLANGE WITH EVIDENCE CORROSION(<P>KEEL BEAM LOWER SIDE LOWER FLANGE, AREA WAS REWORKED, INSPECTED, EVALUATED AND FOUND WITHIN LIMITS PER AMM 51-21-01-157-001 REV 140 - 22 AUG 23, AMM 51-21-10-377-003 REV 140 - 22 AUG 23 &AMP; SRM 53-50-12-1A-1 REV 124 - 15 DEC 23</P> / <P>&NBSP;</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 99,268 hrs · 20,157 cycles

BULGE ON RH WING SLAT# 9 T/E WEDGE LOWER SKIN AT OSS 603.74 AND 5" FROM T/E(<P>RH WING SLAT #9 T/E WEDGE LOWER SKIN WAS REPAIRED IAW SRM 57-43-02-2R-1 FIG 201 SHEET 2 PAGE1-3 AND SRM 51-70-10-2R-4 PAGE1-4 &AMP; 7 FIG 201 REV 124 DEC 15/2023</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 99,268 hrs · 20,157 cycles

LH WING, LOWER SURFACE, BETWEEN BBL 97.42 AND BBL 60.05, STRINGER 6 WITH FUEL LEAK(<P>LH WING, LOWER SURFACE, BETWEEN BBL 97.42 AND BBL 60.05, STRINGER 6 FUEL LEAK WAS REPAIRED AND TEST WAS SATISFACTORY AMM 28-11-00-308-013 REV 140 22 AUG 23</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 99,268 hrs · 20,157 cycles

LEFT WING, OUTBOARD TE FLAP, UPPER SURFACE, SEVERAL DENTS BTWN WS 616.2 AND WS 668.2 TO 31" TE.(<P>LEFT WING, OUTBOARD TE FLAP, ACCESS PANEL 566 KT, UPPER SURFACE WAS REPAIRED IAW SRM 57-53-01-2R-1 REP 1 FIG 201 SHEET 3 PAGE 1-7 AND SRM 51-70-10-2R-4 REP 4 FIG 201 SHEET 1 PAGE 1-3 REV 124 DEC 15/2023</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 99,268 hrs · 20,157 cycles

FWD SERVICE DOOR, ZONE 841 WITH PRESSURIZATION LEAKS.(<P>THE PRESSURIZATION LEAKS WERE EVALUATED AND FOUND WITHIN ADL IAW AMM 05-51-24-782-001</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 99,268 hrs · 20,157 cycles

AFT ENTRY DOOR, ZONE 833 WITH PRESSURIZATION LEAKS.(<P>FUEL LEAKS WERE EVALUATED AND FOUND WITHIN LIMITS IAW AMM 05-51-24-782-001 REV 140 DATE 22 AUG 23</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 99,268 hrs · 20,157 cycles

DENT ON LH WING INBD AFT UPPER SKIN AT 92" FROM INBD EDGE AND 4.5" FROM AFT EDGE(<P>PART WAS REPAIRED IAW OEM MANUAL SRM 57-53-01-2R-1. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 99,268 hrs · 20,157 cycles

TAT & AUTO BRAKE OVERHEAD ANNUNCIATER LIGHT STICK IN ANY ONLY ILLUMINATE INTERMITTENTLY(<P>ANNUNCIATER LIGHT STICK IN ANY ONLY ILLUMINATE INTERMITTENTLY WERE REPLACED IAW AMM 33-13-00-902-024. OPS CHECK GOOD</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 99,268 hrs · 20,157 cycles

FWD CARGO DOOR, ZONE 821 WITH PRESSURIZATION LEAKS(<P>LEAKS WERE EVALUATED AND FOUND WITHIN THE ALLOWABLE LIMITS IAW AMM 05-51-24-782-001</P>)

Part: RELAY — UNKNOWN (UNKNOWN) · airframe 99,268 hrs · 20,157 cycles

IN THE OPERATIONAL CHECK OF CARGO FIRE EXTINGUISHING BOTTLE RELAYS, THE RELAY K823 FOUND INOPERATIVE.(<P>THE RELAY K823 WAS REPLACED IAW SWPM 20-81-22 REV.84 DATE:15-OCT-23. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 99,268 hrs · 20,157 cycles

ENG 2, OUTBOARD THRUST REVERSER, MISSING ANTI-FIRE PROTECTION (RED SEALANT) ON INTERNAL FACE(<P>ENG 2, OUTBOARD THRUST REVERSER, ANTI-FIRE PROTECTION (RED SEALANT) ON INTERNAL FACE. WAS REPAIRED AMM 78-31-00-308-072-H00 REV 140 22 AUG 23. NO FURTHER DEFECTS NOTED</P> / <P>&NBSP;</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 99,268 hrs · 20,157 cycles

FWD ENTRY DOOR, ZONE 831 WITH PRESSURIZATION LEAKS(<P>SEAL WAS REPAIRED IAW AMM 05-51-24-782-001. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 99,268 hrs · 20,157 cycles

DENT ON RH WING SLAT# 7 T/E WEDGE UPPER SKIN AT ISS 152.38 AND 6.5" FROM T/ E(<P>RH WING SLAT #7 T/E WEDGE UPPER SKIN WAS REPAIRED IAW SRM 57-43-02-2R-1 FIG 201 SHEET 2 PAGE 2-3 AND SRM 51-70-10-2R-4 FIG 201 SHEET 1 PAGE 1-3 &AMP; 22 REV 124 DEC 15/2023</P> / <P>&NBSP;</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 99,268 hrs · 20,157 cycles

BULGE ON LH WING SLAT# 3 T/E WEDGE LOWER SKIN AT OSS 706.74 AND 5" FROM T/E(<P>LH WING SLAT# 3 T/E WEDGE LOWER SKIN WAS REPAIRED IAW SRM 57-43-02-2R-1 FIG.201 SHEET 1 PAGE 2-3 AND SRM 51-70-10-2R-4 FIG 201 SHEET 2 PAGE1, 3, 7 &AMP; 22 REV 124 DEC 15/2023</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 99,268 hrs · 20,157 cycles

DENT ON LH WING INBD AFT FLAP LOWER SKIN AT 11.50" FROM OUTBD EDGE AND 2.5" FROM AFT EDGE(<P>PART WAS REPAIRED IAW SRM 57-53-01-2R-1. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 99,268 hrs · 20,157 cycles

DENT ON LH WING INBD AFT UPPER SKIN AT 92" FROM INBD EDGE AND 4.5" FROM AFT EDGE(<P>PART WAS REPAIRED IAW OEM MANUAL SRM 57-53-01-2R-1. NO FURTHER DEFECTS NOTED.</P>)

Part: CAP — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 99,268 hrs · 20,157 cycles

ENG #2, PRSOV AIR FILTER CAPS WITH CORROSION 2EA (N/P 727576-1)(<P>ENG RH, THE CAPS OF PRSOV HAS BEEN REPLACED AND INSTALLED IAW AMM B767 36-11-09-402-114-001 REV 140 - 22 AUG 2023, THE CAPS HAS BEEN TIGHTENED TO 70 LB IN, TORQUE WRENCH: 0616601964, NEXT CALIBRATION DATA: 30-MAY-2024</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 99,268 hrs · 20,157 cycles

AFT SERVICE DOOR, ZONE 843 WITH PRESSURIZATION LEAKS(<P>LEAKS WERE EVALUATED AND FOUND WITHIN ADL IAW AMM 05-51-24-782-001</P>)

Part: RUB STRIP — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 99,268 hrs · 20,157 cycles

ENG 2, CORE COWL RH PANEL 428AR, WEAR STRIP UPPER WITH EVIDENCE OF CORROSION(<P>ENG 2, CORE COWL RH PANEL 428AR, WEAR STRIP UPPER WAS REPLACED PER SRM 51-10-02-0G-0 PARA 9 REV 124 15 DEC 23. NO FURTHER DEFECTS NOTED</P>)

Part: ACTUATOR — UNKNOWN (UNKNOWN) · airframe 99,268 hrs · 20,157 cycles

RH WING SPOILER #10 ACTUATOR INTERNAL LEAK(<P>RH WING SPOILER #10 ACTUATOR WAS REPLACED IAW AMM 27-61-02-424-023 REV 140 DATE 22 AUG 23, 1100 INLB, 140 INLB &AMP; 170 INLB WERE APPLIED WITH S/N 0119113493 DUE DATE 18 MAY 24, LEAK TEST WAS PERFORMED, NO LEAKS WERE FOUND</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · 20,157 cycles

MAIN DECK CARGO DOOR, ZONE 838 WITH PRESSURIZATION LEAKS.(<P>LEAKS WERE EVALUATED AND FOUND WITHIN ALLOWABLE LIMITS IAW AMM 05-51-24-782-001</P>)

Part: ACTUATOR — UNKNOWN (UNKNOWN) · airframe 99,268 hrs · 20,157 cycles

RH WING SPOILER #9 ACTUATOR INTERNAL LEAK(<P>RH WING SPOILER #9 ACTUATOR WAS REPLACED IAW AMM 27-61-02-424-023 REV 140 DATE 22 AUG 23, 1100 INLB, 140 INLB &AMP; 170 INLB WERE APPLIED WITH S/N 0119113493 DUE DATE 18 MAY 24 &AMP; S/N 422127196 DUE DATE 29 AUG 24, LEAK TEST WAS PERFORMED, NO LEAKS WERE FOUND</P> / <P>&NBSP;</P>)

Part: DRAIN MAST — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 99,268 hrs · 20,157 cycles

FUSELAGE WITH EVIDENCE OF CORROSION FWD DRAIN MASTIL AFT SIDE(<P>FWD DRAIN MASTIL WAS REPLACED IAW AMM 38-31-01-404-010 REV 140 DATE 22 AUG 23, 45INLB WAS APPLIED S/N 1222912269 DUE DATE 17 AUG 24, HEATING TEST OK, BONDING TEST OK 0.08 MILLIOHMS S/N 005293 DUE DATE 31 MAY 24</P>)

Part: TERMINAL — UNKNOWN (UNKNOWN) · airframe 98,594 hrs · 19,925 cycles

L ENG HPSOV IN FLIGHT BLEED LIGHT STAYS ILLUMINATED AFTER QRH PROCEDURE(<P>FOUND RING TERMINAL AT TERMINAL 2 ON LH HPSOV UN-SECURED. R/R RING TERMINAL IAW SWPM 20-30-11 AND WDM 36-11-61. NO FURTHER FAULTS NOTED</P>)

Part: ACTUATOR — UNKNOWN (UNKNOWN) · airframe 98,173 hrs · 19,784 cycles

UPON GEAR RETRACTION, GEAR DOOR AND GEAR DISAGREE EICAS MESSAGES. ALSO GEAR, AND LEFT MAIN DISCREET LIGHT ILLUMINATED(<P>REMOVED LH GEAR SIDE BRAKE ACTUATOR IAW AMM 32-32-02.&NBSP;</P> / <P>LP 1736216 M2: INSTALLED LH GEAR SIDE BRAKE ACTUATOR IAW AMM 32-32-02. OPS CHECK GOOD, NO LEAKS NOTED AT THIS TIME</P>)

Part: LIGHT — INOPERATIVE · 19,166 cycles

FOUND EMERGENCY LIGHT AT L I DOOR INOP.(<P><SPAN>RELAMPED LIGHT AT L I DOOR , OPS CHECK NORMAL IAW AMM 33-51-03.</SPAN></P>)

Part: BRAKE ASSY — NONE · airframe 95,935 hrs

HEAVY SMOKE EMITTING FROM BRAKE 1 &AMP; 4. TEMPS ARE 2 AND 2(<P><SPAN>REF LP 1543315 M 3 AND LP 1543316 ITEM M4 FOR CORRECTIVE ACTION.</SPAN></P> / <P><SPAN><SPAN>LOGPAGE 1543315: DURING INSPECTION FOUND HYD FLUID SEEPING FROM #1 BRAKE. REMOVED AND REPLACED #1 MLG BRAKE ASSY IAW AMM 32-41-08. LEAK &AMP; OPS CHECK GOOD. #1 MLG WHEEL ASS REQUIRE INSTALLATION REF M 6 LP #1543316. REINSTALLED #1 MLG WHEEL ASSY IAW AMM 32-45101. AIRCRAFT PERFORMED 1ST FLIGHT SINCE GEAR CHANGE. SUSPECT EXCESSIVE GREASE CAUSING SMOKE. PERFORMED BRAKE INSPECTION IAW 767 AMM 32-41-08. NO DEFECTS NOTED. PERFORMED MLG BRAKE OPC CHECK IAW 767 AMM 32-41-00. OPS CHECK GOOD. A/C OK FOR SERVICE.</SPAN></SPAN></P>)

Part: ACTUATOR — LEAKING · airframe 95,882 hrs · 19,098 cycles

NLG LOCK ACTUATOR WITH LEAK .(REMOVED& AND REPLACED NLG&UPLOCK ACTUATOR PER AMM 32-34-02.)

Part: BULB — NONE · airframe 95,079 hrs

LEFT LANDING GEAR DID NOT INDICATE DOWN AND LOCKED. RAN QRH PROCEDURES(<P>PERFORMED BITE TEST OF PSEU NO FAULTS .CKD LT MLG DOWN INDICATOR FOUND BOTH BULBS BURNT OUT. RELAMPED OPS CKS GOOD&NBSP;</P>)

Part: NONE — NONE · airframe 94,928 hrs · 18,786 cycles

PORTABLE ELT ACROSS L1 DOOR, NYLON STRING BROKEN.(<P>TRANSFERRED TO MDDR # 158785 PER MEL 25-63-10-01, CAT C. DUE DATE 20APR22. MCC NOTIFIED. PLACARD INSTALLED. DIS- ID @ 1926Z.</P> / <P>ONT MX- 22DEC: LP 1383733, ITEM M4: R&AMP;R L1 DOOR PORTABLE ELT IAW AMM 25-63-03, THIS CLEARS DMI # 158785. PLACARD REMOVED. DISP: YK @ 1426Z</P>)

Part: INDICATOR — NONE · 18,763 cycles

RTO AT 80 KNOTS DUE TO NO INDICATION ON STANDBY AIRSPEED, AIRSPEED REACHED ABOUT 110 KNOTS BUT STANDYBY STUCK AT 12(<P>FOUND DAMAGED QUICK DISCONNECT FITTING ON FLEX LINE CONNECTING TO STANDBY AIRSPEED INDICATOR. REMOVED AND REPLACED FITTING IAW AMM 20-11-00. STANDBY AIRPSEED INDICATOR LEAK AND OPS CHECKS GOOD IAW AMM 34-11-00.</P> / <P>LP 1424598: REMOVED AND REPLACED STANDBY AIRSPEED INDICATOR IAW AMM 34-13-05. PERFORMED AUX PITOT SYSTEM LEAK TEST IAW AMM 34-11-00. NO DEFECTS NOTED AT THIS TIME.</P>)

Part: CONTROLLER — NONE · airframe 94,715 hrs · 18,720 cycles

L ENG HPSOV STATUS MESSAGE(<P>TRANSFERRED TO MDDR 156648 PER MEL 36-11-02-02, CAT C, DUE 22NOV21</P> / <P>14NOV21 - LP 1371819 - ITEM #5 - AFW - REMOVED AND REPLACED HPSOV IAW AMM 36-11-07. ALL CHECKS GOOD. S/N OFF - 2003091257. P/N OFF - 802170-12.</P> / <P>14NOV21 - LP 1371819 - ITEM #6 - AFW - REMOVED AND REPLACED HP CONTROLLER IAW AMM 36-11-08. ALL CHECKS GOOD. THIS CLEARS MDDR 156648. PLACARD REMOVED.</P>)

Part: NONE — NONE · 18,707 cycles

"APU OIL QTY" STATUS, APU OIL QTY "ADD"(<P>SERVICED APU OIL IAW AMM 12-13-04. CAP INSTALLED AND VERIFIED SHUT.</P>)

Part: VALVE — NONE · airframe 94,549 hrs

RIGHT PACK INOP AUTO MODE.(<P>TRANSFERRED TO MDDR 155078 PER MEL 21-51-03-01, CAT C.</P> / <P>REMOVED AND REPLACED RH PACK FLOW CONTROL AND SHUTOFF VALVE IAW AMM 21-51-01. OPS CHECK GOOD. NO DEFECTS NOTED.</P> / <P>19OCT- CVG MX, REMOVED AND REPLACED ACM TEMP CONTROL VALVE R/H IAW B767-300 AMM 21-51-12, OPS CHECK GOOD. NO FAULTS FOUND, THIS ACTION CLEARS DMI # 155078. MCC NOTIFIED. ALL PLACARDS REMOVED. PERFORMED AIR SUPPLY BITE MODULE. BITE CHECK GOOD, NO FLAGS FAULTED. P/N OFF: 398750-5, S/N OFF: 2929P.</P>)

Part: SWITCH — NONE

R PACK OFF EICAS MESSAGE AT TOP OF DESCENT.(<P>TRANSFERRED TO MDDR # 154863 PER MEL 21-51-01-01, CAT 'C', DUE DATE: 19OCT. DISP: DP @ 1503Z.</P> / <P>12OCT21 - LP 1313338 - ITEM # 4 - CVG - REMOVED AND REPLACED R/H PACK OVERHEAT SWITCH "S99" IAW B767 AMM 21-51-18. OPS CHECK GOOD AT THIS TIME. THIS CLEARS DMI 154863. PLACARDS REMOVED. MCC NOTIFIED.</P>)

Part: SENSOR — NONE

R PACK OFF EICAS ON DESCENT. REPEAT WRITE UP.(<P>TRANSFER TO MDDR 154664 IAW MEL 21-51-01-01 CAT "C", DUE DATE 16OCT21. MCC NOTIFIED. TJ @ 1434Z</P> / <P>REF LOG 1480837:&NBSP; PERF R PACK BITE PER FIM 21-51 FT 803. VERIFY FAULTED R PACK COMP OUTLET SENSOR T542. ERASED FAULT, OPERATED R PACK MULTIPLE ATTEMPTS &AMP; R OUTLET TEMP COMP WAS HIGHER THAN L PACK NORMAL. PLACARD T542 P/N 6259282 ON ORDER WITH MCC. DMI REMAINS OPEN.</P> / <P>REF LOG 1480841, ITEM 5: PERF R PACK TEMP BITE REF FIM 21-58 FT 803. FOUND RH COMPR OUTLET SENSOR FAULT, REMOVED AND REPLACED RH PACK COMP OUT SENSOR IAW AMM 21-51-06. OPS CHECK NORMAL AT THIS TIME, NO FAULTS NOTED. THIS CLEARS MDDR 154664, PLACARDS REMOVED.</P>)

Part: NONE — NONE

RT PACK SHUTDOWN IN FLIGHT "RT PACK OFF" MESSAGE.(<P>PERFORMED BITE TEST PER AMM 21-48-10 AND RESTARTED APU, OPS CHECK GOOD.</P>)

Part: VALVE — NONE

AFTER TWO ENGINES STARTED "RT PACK OFF" EICAS MSG.(<P>TRANSFER TO MDDR 154592 IAW MEL 21-51-01-01.</P> / <P>05OCT21 - LP 1480825 - ITEM# 10 - CVG - REMOVED AND REPLACED RT ENG HPSOV IAW AMM 36-11-07-024-001 AND LEAK CHECK CARRIED OUT. THIS CLEARS MDDR 154592.</P>)

Part: NONE — NONE

R PACK OFF EICAS W/ TWO ENG'S RUNNING. PACK OFF (RH) DISCREET LIGHT ILLUMINATED.(<P>TRANSFERRED TO MDDR 154525 IAW MEL 21-51-01-01. DUE DATE 13OCT21. PLACARDS INSTALLED.</P> / <P>CVG MX, 04OCT, LP 1391234, ITEM M4: REMOVED AND REPLACED R/H PACK FLOW CONTROL PC CARD M864, REF B767 AMM 21-51-09. PERFORMED NO.1 &AMP; NO.2 ENGINE RUNS. REF 71-00-00 &AMP; 21-51-09, OPS CK GOOD. THIS CLEARS DMI 154525. MCC NOTIFIED, PLACARDS REMOVED. DSPCH: DP 1518</P>)

Part: SHUTOFF VALVE — FALSE INDICATION

L ENG HPSOV PERFORMED AIR SUPPLY CONT SYTEM BITE TEST. NO FAULTS NOTED. MESSAGE CLEARED I/A/W AMM 36-23-00.

Part: A/C PACK — WARNING MESSAGE · airframe 94,440 hrs · 18,615 cycles

DURING DESCENT PASSING FL330 R PACK OFF EICAS MESSAGE DISPLAYED.INSPECTED R AIR PACK PER AMM TASK 21-51-00-216-001. NO FAULTS FOUND. OPS CHECK NORMAL.

Part: OXYGEN MASK — FAILED (CAPTAIN'S)

CAPT O2 MASK 100% SWITCH STICKING. MASK EXTREMELY HARD TO BREATH THROUGH. NEEDS TO BE REPLACED.(<P>REMOVED AND REPLACED CAPT O2 MASK IAW AMM 35-11-51. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.</P>)

Part: ISOLATION VALVE — FAULTED

DURING UNLOADING LOST APU DUCT PRESSURE(<P>TRANS TO MDDR 152610 CAT C IAW DDG 49-11-01-01.</P> / <P>REF LOGPAGE 1395659 ITEM 5: FOUND ISO VALVES IN OFF POSITION, PUSHED ISO SWITCH IN, OPS CHECK GOOD. THIS CLEARS MDDR #152610 IAW B767 AMM 49-11-00.</P>)

Part: TRANSCEIVER — FAULTED (WX RADAR SYS) · airframe 94,247 hrs · 18,559 cycles

NO RETURNS ON RIGHT WX RADAR(<P>TRANSFER TO MDDR 152553 CAT D DUE 25DEC21 IAW DDG 34-43-.01. R/R RT WEATHER TRANSCEIVER&NBSP; IAW AMM 34-43-01 OPS CHECK GOOD. DISPATCHER JT 0126Z&NBSP;</P> / <P>REFERENCE LOG 1395661 ITEM 3 ..CVG... REMOVED AND REPLACED WEATHER RADAR TRANSCEIVER ON R/H IAW BOEING AMM 34-43-01 OPS TEST GOOD. THIS CLEARS DMI 152553 AND CLOSES W/O 85285 REV 0.. ALL PLACARDS REMOVED.

Part: CIRCUIT CARD — FAULTED (LT ENG FIRE LOOP)

STATUS MSGS: L ENG FIRE LP 1 AND L ENG OH LP 1.(<P>ITEM 1 - OPENED LEFT ENGINE AND FOUND CANNON PLUG DISCONNECTED. CLEANED CANNON PLUG AND RESECURED. PERFORMED OPS CHECK OF FIRE DETECTION SYSTEM IAW AMM 26-11-00. NO FURTHER DEFECTS NOTED AT THIS TIME.</P> / <P>ITEM 2 - REMOVED AND REPLACED L ENG LOOP 1 FIRE DETECT CARD M681 IAW AMM 26-10-01. NO FIX. S/N OFF - 12698. P/N OFF - 6445-01.</P> / <P>ITEM 3 -&NBSP;&NBSP;REMOVED AND REPLACED L ENG LOOP 1 FIIRE OVHT CARD M687 IAW AMM 26-10-01. NO FIX. S/N OFF - 29960. P/N OFF - 6445-01.</P> / <P>LOG 1462911 - ITEM 4 - REMOVED AND REPLACED FIRE/OVHT LOGIC TEST CARD M10224 IAW AMM 26-10-01. NO FIX.</P>)

Part: WIRE — DAMAGED (FIRE LOOP)

L ENG FIRE LP 1 STATUS MSG, REPEAT WRITEUP(<P>ITEM#3 - TRANSFER TO MDDR 151625 CAT C DUE 20AUG21 PER MEL 26-11-01-01. ETOPS RESTRICTED TO 120.</P> / <P>10AUG21 - 1391250 - ITEM# 6 - PDX - DURING TROUBLESHOOTING FOUND CHAFFING WIRE RESTING ON IGNITOR CABLE L/H SIDE OF ENGINE. REPOSITIONED WIRE AND PERFORMED STANDARD WIRE REPAIR IAW B767 SWPM 20-10-15. PERFORMED OPERATIONAL TEST IAW B767 AMM 26-11-*00-715-075-003. OPS CHECK GOOD. NO DEFECTS NOTED.</P> / <P>10AUG21 - 1391251 - ITEM# 7 PDX - FOUND CHAFFING WIRE RESTING ON IGNITOR CABLE L/H SIDE OF ENGINE. REPOSITIONED WIRE AND PERFORMED STANDARD WIRE REPAIR IAW B767 SWPM 20-10-15. PERFORMED OPERATIONAL TEST IAW B767 AMM 26-11-00-715-075-003. OPS CHECK GOOD. NO DEFECTS NOTED. THIS CLOSES MDDR 151625. PLACARD REMOVED.</P>)

Part: CIRCUIT CARD — FAULTED (LT ENG FIRE LOOP) · airframe 94,144 hrs

L ENG FIRE LP 1 STATUS MSG(<P>REMOVED AND REPLACED LH ENGINE FIRE LOOP 1 CONTROL CARD FIRE &AMP; OVERHEAT (M681) PER AMM 26-10-01, OPS CHECK GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT FIRE LOOP) · airframe 94,141 hrs · 18,526 cycles

L ENG FIRE LP 1 STATUS MESSAGE.(<P>RE-RACKED CARD M681- L ENG FIRE LP 1 IAW AMM 26-10-01. MESSAGE CLEARED, OPS CHECK GOOD.</P>)

Part: FIRE LOOP — MALFUNCTIONED (LT ENGINE) · airframe 94,144 hrs

L ENG FIRE LP 1 STATUS MESSAGE.(<P>R&AMP;R LH ENGINE UPPER AFT FIRE LOOP IAW AMM 26-11-02, OPS CHECK GOOD.</P>)

Part: FIRE LOOP — FALSE ACTIVATION (LT ENGINE) · 18,528 cycles

L ENG FIRE LP 1 STATUS MESSAGE. PERFORMED FIM TASK 26-11 FAULT TREE 804. NO FAULTS FOUND. COULD NOT DUPLICATE.

Part: WARNING MESSAGE — FALSE ACTIVATION (CARGO TEMP) · 18,512 cycles

AFTER T/O EICAS "FWD CGO BACKUP" ACCOMPLISHED QRH AND EICAS BLANKED AFTER 15 MIN OF FLIGHT. NORMAL OPS. NO MESSAGES ON ARRIVAL IN HNL. BTE CK'D AUX ZONE AND PACK TEMP CONTROLLER PER FIM 21-61 TASK 803. NO FAULTS NOTED. OK TO CONTINUE.

Part: CIRCUIT CARD — NOT SEATED (RT ENG SPEED) · airframe 94,065 hrs

R ENG SPEED CARD STATUS(<P>RERACKED N2 SPEED CARD IAW 73-21-54, MSG CLEARED. PERFORMED FIM TASK 73-21 FT 871 UP TO BLOCK 44. OPS CHECK NORMAL.</P>)

Part: CLAMP — UNSECURE (BLEED DUCT)

L BLD DUCT LEAK EICAS PRIOR TO START UP(<P>FOUND 3 LEAKS.&NBSP; ADJUSTED CLAMPS AND RE-TIGHTENED.&NBSP; NO FAULTS FOUND AT THIS TIME. IAW B767 AMM 20-11-00.&NBSP; LEAK CHECK GOOD</P>)

Part: RADAR — MALFUNCTIONED (WX SYSTEM)

R RADAR DOES NOT PAINT GROUND OR WEATHER RETURNS(<P>PERFORMED WEATHER RADAR SYSTEM OPERATIONAL TEST IAW B767 AMM 34-43-00-715-001-001. OPS CHECK NORMAL AT THIS TIME.&NBSP;</P>)

Part: OXYGEN BOTTLE — LEAKING (PAX) · airframe 93,968 hrs

PAX O2 REGULATOR LEAKING(<P><SPAN>REMOVED O2 BOTTLE AND INSTALLED OVERHAULED UNIT IAW AMM 35-11-03. LEAK CHECK PER AMM 35-11-00</SPAN></P>)

Part: START VALVE — FAULTED (NR 1 ENGINE) · airframe 93,847 hrs · 18,439 cycles

EICAS MESSAGE L START VALVE CUTOUT(<P>REMOVED AND REPLACED ENGINE #1 START VALVE IAW B767 AMM 80-11-02. OPS CHECK NORMAL AT THIS TIME. NO MESSAGES PRESENT AT THIS TIME.&NBSP;</P>)

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT SYSTEM) · airframe 93,852 hrs

AUTOPILOT (C) FAILED AT FL380. UNABLE TO RE-ENGAGE THE C OR R AUTOPILOT FROM FL 370 AND THE HALFWAY POINT OF THE FLIGHT UNTIL LANDING. HAND FLEW THE REMAINDER OF THE FLIGHT AT 280. RVSM RESTRICTED(<P><SPAN>PERFORMED TEST 40 AND FOUND NO INFO CENTER C-CH DETENT R IN PER FIM 22 05 FT 847 REMOVED AND REPLACED CENTER FCC. PERFORMED TEST 40, OPS CHECK GOOD AND CENTER AND RIGHT FCC TEST OPS CHECK GOOD, REF AMM 22-11-01. A/C OK TO CONTINUE</SPAN></P>)

Part: RELAY — FAULTED (START VALVE) · airframe 93,824 hrs · 18,431 cycles

ENG #1 START VALVE INOP(<P>TRANSFERRED TO FLIGHT CREW DEFERRAL MEL # 148762, DDG 80-00-02-01 CAT "C", 27JUN21 TJ 1801Z. REMOVED AND REPLACED ENG START RELAY K1173 PER WDM 80-11-11. PERF ENG RUN PER AMM 71-00-00 FOR L ENG. START STAYS ON GND AND 50% CLICKS BACK TO AUTO. OPS CHECK SUCCESSFUL.

Part: RELAY — FAULTED (NR 1 ENGINE STAR) · airframe 93,824 hrs · 18,431 cycles

ENG #1 START SELECTOR WILL NOT STAY IN GND DURING ENGINE START.(<P>TRANSFERRED TO FLIGHT CREW DEFERRAL MEL #148761, DDG 80-11-02, CAT "C", 27JUN21 TJ M1755Z.</P> / <P>ONT - 23JUN21- LP 1478315 ITEM 10 - REF LP 1478314 ITEM M9, RELAY (K1173) REMOVED AND REPLACED. ENG L RUN PER 71-00-00, NO CUTOUT MSG AND VALVE LIGHT EXTINGUSHED. OPS CHECK GOOD. THIS CLEARS DMI 148761.

Part: IGNITER — FAULTED (RT ENGINE) · airframe 93,820 hrs

RT ENG IGNITOR 2 EICAS MSG ( IGNITION SYSTEMS, ER OPERATIONS ALLOWED )(<P><SPAN>TRANSFERRED TO MEL 74-00-01A, MDDR 148600.</SPAN></P> / <P>ONT-15 JUN - LP 1386635 - ITEM 6 - REMOVED AND REPLACED RIGHT HAND ENGINE IGNITOR PLUG IAW AMM 74-21-02. OPS CHECKS GOOD. NO FURTHER DEFECTS NOTED. PLACARD REMOVED. MCC NOTIFIED. THIS CLEARS MDDR 148600.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT SPEED CARD) · airframe 93,820 hrs

STATUS MSG R ENG SPEED CARD(<P>PERF FIM 73-21 FT 871. CLEARED MSG. TEST CHANNEL 1 AND 2. MSG DISPLAYS. SYSTEM TEST OK</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 93,820 hrs · 18,430 cycles

IN DESCENT THROUGH FL350 STATUS MSG: R ENG SPEED CARD. PERFORMED T/S IAW FIM 73-21 FAULT TREE 871 AND FIM 31-41-00/101. NO FAULTS NOTED, SYSTEM IS OK.

Part: WARNING MESSAGE — FALSE ACTIVATION (EXHAUST FAN) · airframe 93,788 hrs · 18,420 cycles

STATUS MSG AFT EQ EXH FAN 2(<P>PERFORMED OPS CHECK IAW AMM 21-58-00, OPS CHECK GOOD. FIM TASK 21-58 TASK 805 STATES SHORT TEMPORARY INTERRUPTIONS LIKE THE ONE THAT OCCUR DURING A POWER TRANSFER (GROUND-APU-ENGINE APU-GROUND) CAN CAUSE THE EICAS MESSAGE.</P>)

Part: CONNECTOR — DAMAGED (APU) · airframe 93,806 hrs · 18,426 cycles

APU AUTO SHUTDOWN APPROX 30 MIN AFTER START, APU FAULT MESSAGE. TROUBLESHOT PER B767 FIM 49-11 TREE 909 GEN FILTER MSG ON ECU - APU INOP - ITEM PLACED ON DMI 148253 IAW MEL 49-11-01A, CAT C, DUE 19 JUN21. C/W AP-20109, PERFORMED AMM 49-20-00 GVI TASK NO FAULTS/BLOCKAGES. PERFORMED FIM 49-11 FT 987, NO FAULTS FOUND, WHILE PERFORMING FIM 49-11 FT 998, FOUND PIN 2 PUSHED AT P20 PLUG REF WDM 49-14-11 ALSO FOUND DIFFERENTIAL PRESSURE SWITCH TO BE FAULTY, PLUG P20 AND DIFFERENTIAL PRESSURE SWITCH ON ORDER, DMI REMAINS OPEN.</P><P>LP 1306177, ITEM M14: REMOVED AND REPLACED P20 PLUG AT GENERATOR OIL FILTER-DIFFERENTIAL SWITCH PER WDM 49-14-11, SWPM 20-74-20, AND AMM 49-27-15 FOR OPS CHECK.</P><P>LP 1306177, ITEM M15: REMOVED AND REPLACED GENERATOR OIL FILTER-DIFFERENTIAL SWITCH IAW B767-300 AMM 49-27-15 (<SPAN>S/N OFF: 90-50625-637, P/N OFF: 3876048-3</SPAN><SPAN>), OPS CHECK, NO FAULTS AT THIS TIME. THIS CLEARS DMI # 148253. MCC NOTIFIED. ALL PLACARDS REMOVED.</SPAN></P>)

Part: PIN — RECESSED (APU CONNECTOR) · airframe 93,781 hrs · 18,417 cycles

APU AUTO SHUT DOWN.(<P>PERFORMED APU CONTROL UNIT BITE TEST., FAULT CODE GEN FILTER ON BITE, REQUIRES FURTHER T/S. LOG 1485729 ITEM #9: FOUND CONNECTOR P20 PIN 2 RECESSED, PERFORMED FIM 49-11 F/T 998 FOR APU AUTO SHUT DOWN, FOUND RECESSED PIN ON CONNECTOR P20 PIN 2, REPAIRED PIN IAW SWPM 20-63-00.</P>)

Part: APU — FAULTED · airframe 93,672 hrs · 18,386 cycles

APU PNEUMATIC FUNCTION INOP ( AUXILIARY POWER UNIT, PNEUMATIC FUNCTION )(<P>TRANSFERED TO MDDR 147249 IAW MEL 49-11-01-01, CAT C, DUE 30MAY21.</P><P>LOG PAGE 1341621: REMOVED AND REPLACED APU IAW WORK CARD A-49-999-00-01. THIS CLEARS MDDR 147249.</P><P><BR /></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (CARGO TEMP) · airframe 93,639 hrs · 18,374 cycles

STATUS MESSSAGE - CARGO A/C TEMP.(<P>PERFORM SYSTEM BITE CHECK OF THE AIR SUPPLY CONTROL SYSTEM IAW AMM 26-23-00. OPS CHECK GOOD, NO FURTHER DEFECTS NOTED BY MX. STATUS MSG NO LONGER APPEARS.</P>)

Part: FIRE LOOP — FAULTED (LT ENGINE) · airframe 93,613 hrs · 18,366 cycles

LH ENG FIRE LOOP 1 STATUS MESSAGE(<P>TRANSFERRED TO MDDR #146764 IAW MEL 26-11-01-01 CAT-C, DUE-20MAY21</P><P>13MAY21 - LP 1341607 - ITEM# 25 - CVG -&NBSP;REMOVED AND REPLACED LWR AFT FIRE DECTOR ASSY ON #1 ENG IAW AMM 26-11-02. MCC NOTIFIED. PLACARDS REMOVED. THIS CLEARS DMI 146764.</P>)

Part: FIRE DETECTOR — FAULTED (RT ENGINE) · airframe 93,613 hrs · 18,366 cycles

R ENG FIRE LOOP 1 STATUS MESSAGE(<P>TRANSFERRED TO MDDR# 146763 IAW MEL 26-11-01-01 CAT-C DUE-20MAY21</P><P>14MAY21 - LP 1341609 - ITEM# 26 - CVG -&NBSP;REMOVED AND REPLACED LWR AFT FIRE DETECTOR ASSY IAW AMM 26-11-02.OPS CHECK GOOD. THIS CLEARS DMI 146763. MCC NOTIFIED.</P>)

Part: CIRCUIT CARD — FAILED (LT FIRE LOOP) · airframe 93,594 hrs · 18,360 cycles

LEFT ENGINE FIRE LOOP 1 STATUS MESSAGE(<P>PERFORMED GVI OF FIRE LOOP 1 SYSTEM, NO DEFECTS NOTED. PERFORMED FIM 26-11 FT804 ENG FIRE DETECT BITE, TO SHEET 3 BLOCK 4. SUSPECT BAD LEFT ENG CONTROL CARD M681 FIRE LOOP 1. REMOVED AND REPLACED M681 FIRE LOOP 1 IAW AMM 26-10-01. OPS CHECKED PER AMM 26-11-00. NO FAULTS NOTED</P>)

Part: SEALANT — MISSING (NR 1 NACELLE) · airframe 93,518 hrs · 18,340 cycles

#1 ENG INLET COWL ACOUSTICAL PANEL @ 6 O'CLOCK POSITION MISSING SEALANT.(<P>APPLIED SEALANT AROUND THE ACOUSTICAL LINER SEGMENT @ 6 O'CLOCK POSITION IAW 72-33-01.</P>)

Part: STUD — BROKEN (RT FIRE LOOP) · airframe 93,521 hrs · 18,341 cycles

STATUS MESSAGE R ENG FIRE LOOP 1(<P>TRANSFERRED TO MDDR 145950 IAW MEL 26-11-01-01, CAT C.</P><P>LOG PAGE&NBSP;1465432: REMOVED AND REPLACED UPPER AFT FIRE LOOP DETECTOR PER B767 AMM 26-11-02 DURING REMOVAL OF UPPER AFT FIRE LOOP FOUND BROKEN STUD ALSO TERNIBAL WIRE PASTIALLY BROKEN , DMI# 145950 REMIANS OPEN, MCC NOTIFIED.</P><P>LOG PAGE 1465441: RETERMINATED AND SHRINK WRAPPED ENG #2 FIRE LP1 LEAD IAW B767 SWPM 20-30-00-&AMP; 20-10-14. OPS CHECKED IAW B767 AMM TASK 26-11-00-715-075-003. NO DEFECTS NOTED.

Part: CONNECTOR — DIRTY (FIRE LOOP) · airframe 93,487 hrs · 18,331 cycles

R ENGINE FIRE LP 1 MESSAGE(<P>FORWARD TO MDDR 145720 IAW MEL 26-11-01-01, CAT C, DUE 2 MAY 21.</P><P>MIA MX, 23APR, LP 1355451, ITEM M10: ENSURED SECURITY OF TERMNALS ON RT ENG. LOOP 1 RESPONDERS, LOOP RESISTANCE WITHIN LIMITS, NO SHOTS TO GROUND OR INTERMITTENT, DH MIC READINGS, CLEANED CONNECTORS IAW AMM 26-11-02 AND WDM CH 26-11-21. SYSTEM TEST PASS IAW SUBTASK 26-11-02 AND TASK 31-41-00. CLEARED MDDR 145720 PER MCC.&NBSP;</P>)

Part: FIRE LOOP — FALSE ACTIVATION (RT ENGINE) · airframe 93,472 hrs · 18,323 cycles

R ENG FIRE LP 1 STATUS MESSAGE(<P>PERFORMED FIM 26-11 FT 806 UP TO FIG 106 BLOCK 3. MSG CLEARED . NO FAULTS NOTED AT THIS TIME.<BR /></P>)

Part: WARNING LIGHT — INTERMITTENT (FUEL PUMP) · airframe 93,397 hrs · 18,300 cycles

AFTER CENTER FUEL TANK IND 0 BOTH C PUMP PRESS LIGHTS FLICKERED BUT NEVER BECAME SOLID. DID NOT GET EICAS MSG EITHER OF C TANK LOW PRESS.(<P>C/W OPS CHECK OF CENTER FUEL PUMPS AUTOMATIC SHUTOFF FUNCTION IAW 28-22-00. CHECK GOOD AT THIS TIME.</P>)

Part: ANTENNA — FAULTED (WX RADAR) · airframe 93,397 hrs · 18,300 cycles

WXR PREDICT EICAS MSG(<P>RAN FIM FT 805, RECEIVED ANTENNA FAULT ON BOTH L & R TRANSCIEVER, CHECKED SWITCH S269 ON ANT MOUNT AND NOTED ANTENNA MOUNTING UNCOMMANDED SUSPECTED INTERNAL SHORT ON MOUNT TERMINAL. REMOVED AND REPLACED ANTENNA MOUNT IAW 34-43-05-024. REMOVED AND REPLACED ANTENNA PLANER ARRAY IAW 34-43-05-425. OPS CHECK IAW 34-43-05 GOOD SYS L AND R.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (CARGO TEMP) · airframe 93,371 hrs · 18,291 cycles

STATUS MSG CARGO A/C TEMP(<P>PERFORMED BITE CHECK OF ZONE TEMP CONT, NO FAULTS FOUND, OLD FAULT ON EICAS CLEARED PER AMM TASK 21-61-03-715-022.</P>)

Part: WINDSHEAR SYS — MALFUNCTIONED · airframe 93,397 hrs · 18,300 cycles

DURING CLIMB OUT WINDSHEAR SYSTEM EICAS MESSAGE AND FO WX FAIL FLAG ON EHSI. BOTH BLANKED AFTER SWITCHING WX RADAR TO L SYSTEM. WX FAIL FLAG REAPPEARED SHORTLY AFTER. INSPECTED L WAVE GUIDE, NO DAMAGE NOTED IAW AMM 34-43-04 & 1261164 ITEM 4. SWAPPED LEFT CENTER SYMBOL GENERATOR FOR EFIS FROM T/S. LEFT SYM GEN P/N 66-9456-101 S/N 2597 IN CENTER POS AND CENTER SYM GEN P/N 622-9456-101 S/N 113771 IN LEFT POS AFTER CHECK IAW AMM 34-12-010 AND GMM 3.27.10.

Part: CONNECTOR — DISCONNECTED (WX RADAR SYS) · airframe 93,338 hrs

WX RADAR FAILED(<P>PERFORMED WXR BITE IAW FIM 34-43 FT 805. FOUND CONNECTOR D395 DISCONNECTED. RECONNECTED CANNON PLUG IAW AMM 34-43-02. PERF OPS CHECK OF WXR. OPS TEST GOOD. NO OTHER DEFECTS NOTED. AMM 34-43-00</P>)

Part: SENSOR — FAULTED (CARGO DUCT) · airframe 93,319 hrs · 18,275 cycles

FWD CGO BACKUP EICAS MSG DISPLAYED AFTER LANDING.(<P>PERFORMED TASK 21-28 FAULT TREE 809, FAULTED FWD CARGO DUCT SENSOR. REMOVED AND REPLACED SENSOR AMM 21-61-01.</P>)

Part: SENSOR — FAULTED (MANIFOLD TEMP) · airframe 93,319 hrs

L PACK TEMP EICAS MSG DISPLAYED AFTER LANDING(<P>PERFORMED FIM 21-51 FAULT TREE 804. IDENTIFIED L MANIFOLD TEMP SENSOR FAULTY. P/N 624016-2 ON ORDER. REMOVED AND REPLACED L MANIFOLD TEMP SENSOR, OPS TEST GOOD.<BR /></P><P>07 APR 21 - LP 1145835 ITEM 6 - TPA -&NBSP;REMOVED AND REPLACED LF ACM IAW AMM 21-51-03. OPS CHECK GOOD.</P>)

Part: CONTROL PANEL — MALFUNCTIONED (WX RADAR SYS) · airframe 93,319 hrs · 18,275 cycles

LEFT SYSTEM WXR FAIL(<P>DEFERRED TO DMI 144835 MEL 34-43-01 CAT D DUE DATE 2 AUG 21 PLACARD INSTALLED&NBSP;</P><P>04 APR 21-LP 1145832 ITEM 8 - CVG - REMOVED AND REPLACED WX PANEL IAW B767 AMM 34-43-02. OPS CHECK IAW 34-43-00. NO DEFECTS NOTED AT THIS TIME THIS CLEARS DMI 144835 MCC NOTIFIED PLACARDS REMOVED</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (WINDSHEAR SYS) · airframe 93,319 hrs

EICAS MESSAGE: WINDSHEAR SYS(<P>ITEM PLACED ON MEL 34-43-01-01A DUE DATE 07APR21 CONTINGENCY LOG 142608 MCC NOTIFIED - PLACARD INSTALLED (MDDR 144833)</P><P>DATE 04 APR 21 - LP 1145830 ITEM 4 - CVG -&NBSP;COMPLIED WITH AP 19531 NO DEFECTS NOTED - OPS CHECKS GOOD - THIS CLEARS DMI 144833 PLACARDS REMOVED</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (CARGO TEMP) · airframe 93,250 hrs · 18,256 cycles

CARGO A/C TEMP STATUS MESSAGE.(<P>PERFORMED BITE OF LEFT PACK CONTROLLER RIGHT PACK CONTROLLER AND AUX ZONE, TEMP CONTROLLER. NO FAULTS FOUND AT THIS TIME. REF AMM 21-61-00/001 AND FIM 21-61/101</P>)

Part: TRANSCEIVER — FAILED (WX RADAR SYS) · airframe 93,222 hrs · 18,248 cycles

LEFT WX RADAR FAILED(<P>TRANSFERRED TO MDDR # 144409 IAW MEL 34-43-01, CAT D, PLACARDS INSTALLED. DUE 24JUL21 JT @ 2112Z</P><P>LP 1456726: PERFORMED FIM 34-43 FAULT TREE 805. NO FAULTS FOUND. PERFORMED WEATHER TEST 34-33-00-735-033-002, NO FAULTS FOUND. REMOVED AND REPLACED LT TRANSCEIVER IAW 34-33-01. MDDR 144409 CLEARED PLAC RMVD. MCC NOTIFIED.&NBSP;</P>)

Part: RADAR — MALFUNCTIONED (WX SYSTEM) · airframe 93,211 hrs · 18,244 cycles

LEFT WEATHER RADAR FAIL(<P>PERFORMED WEATHER RADAR SYSTEM OPERATIONAL TEST REF B767 AMM 34-43-00-715-026-002. OPERATIONAL TEST PASSED/NORMAL AT THIS TIME.</P>)

Part: RADAR — INTERMITTENT (WX SYSTEM) · airframe 93,143 hrs · 18,226 cycles

WXR FAIL MESSAGE ON HSI FOR L+R WXR SYS. R SIDE SEEMS INTERMITTENT. WXR SYS STATUS MESSAGE DISPLAYED BOTH PILOTS IN TERRAIN ON CLIMB, MSG RECEIVED ON CLIMBOUT.(<P>PERFORMED L+R OPERATIONAL CHECK OF WEATHER RADAR SYSTEM PER AMM 34-43-00. OPS CHECK OKAY AT THIS TIME. NO FAULTS FOUND.<BR /></P>)

Part: WARNING FLAG — FALSE ACTIVATION (WX RADAR SYSTEM) · airframe 93,143 hrs · 18,226 cycles

WXR SYS STATUS MSG AND WX FAIL FLAG ON EHSI(<P>RAN FIM 34-43 TASK 801, CLEARED EICAS MSG. ALSO RAN 34-22-FAULT TREE 808. NO DEFECTS NOTED.&NBSP;<BR /></P>)

Part: PRIORITY VALVE — FAULTED (RT ENGINE) · airframe 92,955 hrs · 18,163 cycles

STATUS MSG "R ENG PRV"(IAW FIM 36-10-00. FOUND THE PRV TO BE AT FAULT. REMOVED AND REPLACED RT ENGINE PRV IAW AMM 36-11-18. OPS TEST GOOD. STATUS MESSAGE CLEARED.)

Part: CONTROLLER — FAULTED (CARGO TEMP) · airframe 92,975 hrs · 18,169 cycles

STATUS MSG "CARGO A/C TEMP"(TS IAW FIM 21-28 FAULT TREE 809. FOUND PACK FLOW CONTROLLER TO BE AT FAULT. REMOVED AND REPLACED PACK FLOW CONTROLLER IAW AMM 21-51-24. OPS GOOD.)

Part: LIGHT — NO INDICATION (PUMP) · airframe 92,975 hrs · 18,169 cycles

AFTER ENGINE SHUTDOWN PRESS LIGHT WOULD NOT ILLUMINATE IN R AFT FUEL PUMP SWITCH WITH SWITCH OFF. LIGHTS TEST GOOD. CYCLED AFT FUEL PUMP SWITCH, OPS CHKS GOOD PER AMM 28-40-00.

Part: STATUS MESSAGE — FALSE ACTIVATION (CARGO TEMP) · airframe 92,955 hrs · 18,163 cycles

CARGO A/C TEMP STATUS MESSAGE DISPLAYED AFTER TAKEOFF. (T/S IAW FIM 21-61-00, NO FAULTS FOUND. OPS GOOD. MSG CLEARED AT THIS TIME.)

Part: STATUS MESSAGE — FALSE INDICATION (CARGO TEMP) · airframe 92,934 hrs · 18,157 cycles

STATUS MSG "CARGO A/C TEMP". PERFORMED BITE CHECK ON ZONE TEMP CONTROLLER. NO FAULTS FOUND, OPS CHECK GOOD REF FIM 21-61-00.

Part: STATUS MESSAGE — FALSE ACTIVATION (CARGO TEMP) · airframe 92,917 hrs · 18,149 cycles

STATUS MSG / CARGO A/C TEMP(<P>FAULT CLEARED PRIOR TO ARRIVAL, ACCOMPLISHED ZONE TEMP CONT OPS TEST W/APU. BITE PASSED W/NO FAULTS, TEMP CONTROL VALVES CYC NORMALLY.<BR /></P>)

Part: SEAT BELT — DAMAGED (CAPT SEAT) · airframe 92,877 hrs · 18,138 cycles

COCKPIT CAPT. R/H SEAT BELT TSO TAG DAMAGE(<P>REMOVED &AMP; REPLACED CAPT LAP BELT IAW 767&NBSP; AMM&NBSP; 25-11-01. OP CHECK NORMAL</P>)

Part: ACTUATOR — INOPERATIVE (THRUST REVERSER) · airframe 92,877 hrs · 18,138 cycles

RIGHT ENGINE THRUST REVERSER INOP(<P>REMOVED &AMP; REPLACED #2 ENG&NBSP; I/B T/REV ACTUATOR PER B767 AMM 78-31-21. LEAK &AMP; OPS CHECKED,&NBSP;</P><P>NO DEFECTS NOTED</P>)

Part: ACOUSTIC LINER — CRACKED (NR 2 ENGINE) · airframe 92,877 hrs · 18,138 cycles

#2 ENGINE AT 6 O'CLOCK POSITION APROX MID ACUSTIC PANEL FOUND CRACKED(<P>REMOVED &AMP; REPLACED DAMAGED ACOUSTIC LINER SEGMENT AT #2 ENG 6 O'CLOCK POSITION PER&NBSP; B767-300 AMM 72-33-01-004-001-H00, AMM 72-33-01-404-011-H00.</P>)

Part: SEAL DEPRESSOR — DENTED (MDC DOOR) · airframe 92,877 hrs · 18,138 cycles

MAIN DECK CARGO FWD LOWER SEAL DEPRESSOR HAS 1 EA&NBSP; DENT FOUND TO BE WITHIN&NBSP; LIMITS&NBSP; IAW&NBSP; SRM&NBSP; 53-00-15-1A-1. NO CRACKS FOUND&NBSP;(<P>REMOVED DAMAGED SEAL DEPRESSOR LOCATED DRILLED DEBURRED AND INSTALLED NEW SEAL DEPRESSOR AT MAIN DECK FWD LOWER CORNER MAIN CARGO DOOR CUT OUT PER&NBSP; B767-300&NBSP;&NBSP;</P><P>SRM 51-40-02-0G-0</P>)

Part: HOOK AND LOOP — UNSECURE (C/P LIFE VEST) · airframe 92,877 hrs · 18,138 cycles

COCKPIT CAPT SEAT LIFE VEST POUCH VELCRO LOOSE(<P>REMOVED AND REPLACED LOOSE VELCRO&NBSP; AT&NBSP; CKPIT&NBSP; CAPT SEAT LIFE VEST POUCH&NBSP; PER&NBSP; B767-300</P><P>AMM&NBSP; 20-30-01-992-001</P>)

Part: FLEX LINE — LEAKING (HEAT EXCHANGER) · airframe 92,877 hrs · 18,138 cycles

#1 ENG PNEUMATIC LINE @ HEAT EXCHANGER LOCATION "E" AS PER&NBSP; EO1936A088 IS LEAKING(<P>REMOVED &AMP; REPLACED PNEU. FLEX LINE AT&NBSP; LOCATION "E"&NBSP; PER&NBSP; M/M&NBSP; 20-11-00. LEAK CK GOOD, REF EO 1936A088</P>)

Part: PRIORITY VALVE — LEAKING (NR 2 ENGINE) · airframe 92,877 hrs · 18,138 cycles

#2 ENGINE PR VALVE HAS PENUMATIC LEAK AS PER&NBSP; EO # 1936A088(<P>REMOVED AND REPLACED #2 ENG PRV AS PER 36-11-18&NBSP; LEAK CHECK GOOD. REQUIRES&NBSP; RUN UP. OPS&NBSP; CHECK. NO LEAKS NOTICED&NBSP; POST ENG RUN UP. OP CHECK NORMAL.</P>)

Part: PACKING — LEAKING (DRAIN LINE) · airframe 92,877 hrs · 18,138 cycles

ENG #1 PRESSURE CASE DRAIN FILTER MODULE FWD RIGID LINE LEAKING AT "B"&NBSP; NUT(<P>REMOVED AND REPLACED PACKING ON L ENGINE PRESS MODULE RETURN LINE&NBSP; UNION. RE INSTALLED&NBSP; UNION&NBSP; &AMP; RETURN LINE PER&NBSP; M/M 29-11-17-404-028. REQUIRES&NBSP; ENGINE&NBSP; RUN UP, LEAK CHECK.</P><P>NO LEAKS NOTICED POST ENG RUN UP.</P>)

Part: ENGINE — VIBRATION (NR 2) · airframe 92,877 hrs · 18,138 cycles

#2 ENG VIBRATION @ RUN UP REQUIRES REMOVAL CLEAN INSPECTION LUBE REINSTALLATION OF 1ST STAGE BLADES(<P>PERFORMED REMOVED, RELUBE &AMP; RE INSTALLATION OF FAN BLADES @ #2 ENG IAW 767 AMM 72-31-02.</P><P>PERFORMED VIB&NBSP; SURVEY IAW&NBSP; 71-00-00&NBSP; TEST # 6&NBSP; VIB @ .9 UNITS, FOUND WITHIN LIMITS</P>)

Part: RADAR — FAULT MESSAGE (WX RADAR SYS) · airframe 92,844 hrs · 18,128 cycles

WEATHER RADAR FAILED ON LT AND RT AUTO AND MANUAL MODES. WX FAIL MESSAGE ON BOTH NAV DISPLAYS. PERFORMED WX RADAR OPS TEST LT & RT PER AMM TASK 34-43-00-715-001-001. OPS CHECK GOOD AT THIS TIME. 29JAN21 LOG PG 1272422 ITM 3 PDX. PERFORMED WX RADAR OPS TEST LT & RT PER AMM TASK 34-43-00-715-001-001. FAULTS CLEARED AND OPS TEST WAS GOOD AT THIS TIME. 29JAN21 LOG PG 1272423 ITM 2 PDX. PERFORMED WIND SHEAR SYS TEST WITH WX RADAR LT & RT TEST AS IN WRITE UPPER AMM 34-43-00-701-001-001. FAULTS CLEARED. OPS & CHECK WAS GOOD AT THIS TIME.

Part: CONTROL PANEL — INOPERATIVE (WEATHER RADAR) · airframe 92,800 hrs · 18,112 cycles

WX RADAR AUTO TILT INOPERABLE. TRANSFERRED TO MDDR 34-43-01-04, CAT "C". DUE DATE: 04FEB21 DMI 141412. REMOVED AND REPLACED WEATHER RADAR CONTROL PANEL. PERFORMED WEATHER RADAR SYSTEM TEST, OPERATIONS CHECK GOOD. THIS CLEARS DMI 141412, REF MM 34-43-02 RKB 17:21Z.

Part: WARNING MESSAGE — FALSE INDICATION (CARGO BAY) · airframe 92,800 hrs · 18,111 cycles

CARGO A/C TEMP STATUS MESSAGE. PERFORMED OPERATIONS TEST ON ZONE TEMP CONT SYSTEM. NO DEFECTS OR FAULTS NOTED, IAW AMM 21-61-00, MESSAGE CLEARED.

Part: A/C PACK — UNKNOWN (CABIN TEMP) · airframe 92,778 hrs · 18,103 cycles

COMPARTMENT TEMP INDICATED 12 DEG C IN THE FWD CABIN AND 18 DEG C IN THE AFT CABIN WITH TEMP SELECTED TO FULL WARM. FLT DECK WAS DIFFICULT TO WARM UP. PERFORMED OPERATIONS TEST OF ZONE TEMP CONTROL SYSTEM, TEST NORMAL IAW AMM 21-61-00.

Part: IGNITER — WORN (NR 2 ENGINE) · airframe 92,724 hrs · 18,084 cycles

DURING BORO INSPECTION FOUND NR 2 ENGINE UPPER IGNITER WITH EXCESSIVE TIP WEAR. REMOVED AND REPLACED NR 2 ENGINE UPPER IGNITER PLUG, IAW AMM 74-11-01.

Part: TRANSMITTER — INOPERATIVE (ELT) · airframe 92,614 hrs · 18,049 cycles

PORTABLE EMERGENCY LOCATOR TRANSMITTER INOPERABLE 1 SERV ON BOARD, SURVIVAL TYPE ELTS. TRANSFERRED TO MDDR 139848, IAW MEL 25-63-10-01, CAT D. REMOVED AND REPLACED PORTABLE ELT, IAW AMM 25-63-03. THIS CLEARS MDDR 139848, PLACARD REMOVED, MCC NOTIFIED.

Part: STATUS MESSAGE — FALSE ACTIVATION (CARGO TEMP) · airframe 92,606 hrs · 18,047 cycles

CARGO A/C TEMP STATUS MESSAGE. PERFORMED AUX ZONE TEMP CNT BITE, NO FAULT FOUND. CLEARED STATUS MESSAGE IAW 21-61-12.

Part: STATUS MESSAGE — FALSE ACTIVATION (CARGO TEMP) · airframe 92,569 hrs · 18,035 cycles

CARGO A/C TEMP STATUS. PERFORMED OPERATIONS CHECK, PER AMM 26-23-00. OPERATIONS CHECK GOOD.

Part: STATUS MESSAGE — FALSE ACTIVATION (WX RADAR SYSTEM) · airframe 92,468 hrs · 18,007 cycles

WXR STATUS MESSAGE. PERFORMED BITE, IAW FIM 34-43 SHEET 1 BLOCK 2. NO FAULTS NOTED.

Part: ENGINE — POWER LOSS (LEFT) · airframe 92,395 hrs · 17,990 cycles

BELOW 5000 ON ARRIVAL AMBER IDLE DISAGREE MESSAGE DISRUPTED LT ENGINE WAS 28% WHEN RT ENGINE WAS 40%. PERFORMED LT & RT ENGINE PIMU BITE PROCEDURE 71-01-01 FT 810. NO FAULTS ON EITHER PIMU BITE. NO IDLE DISAGREE MESSAGE DISPLAYED NO FAULTS AT THIS TIME.

Part: CONTROLLER — MALFUNCTIONED (A/C SYSTEM) · airframe 92,316 hrs · 17,965 cycles

CARGO A/C CONT EICAS MSG ON FINAL. COMPLIED WITH QRH. REMOVED AND REPLACED PACK FLOW AND CARGO A/C CONTROLLER, IAW AMM 21-51-24. OPERATIONS CHECK GOOD. NO FAULTS AT THIS TIME.

Part: STOWAGE BOX — INOPERATIVE (OXYGEN MASK) · airframe 92,305 hrs · 17,962 cycles

1ST OBS SEAT MASK O2 INOPERABLE. TRANSFERRED TO MDDR 137721, PER MEL 25-11-02-01C CAT A, DUE 14 NOV 20. REMOVED AND REPLACED STOWAGE, PER AMM35-11-51. OPERATIONS CHECK GOOD. NO LEAKS NOTED THIS CLEARS MDDR 137721. PLACARD REMOVED.

Part: SKIN — CRACKED (BS 654-720) · airframe 92,191 hrs · 17,923 cycles

UPPER FUSELAGE AT APPROXIMATELY STA 654 TO STA 720 STR 10R TO 10L HAS EVIDENCE OF MULTIPLE SMOKED RIVETS. UPON REMOVAL OF 130 EA FASTENERS FOUND 2 EA. FASENTER HOLES CRACKED AT CROWN STA 654+22 STR 1L AND STR 1R. REAMED 2 EA CRACKED HOLES TO .214 WITH NDT VERIFICATION NO DEFECTS NOTED. RE-INSTALLED 130 EA FASTNERS, IAW B767 SRM 51-40-0251-40-05.

Part: OXYGEN BOTTLE — CORRODED (LAVATORY) · airframe 92,191 hrs · 17,923 cycles

LAVATORY OXYGEN BOTTLE IS CORRODED. REMOVED AND REPLACED LAV OXYGEN BOTTLE, IAW B767 AMM 35-31-01-400-801-001.

Part: LANYARD — DETACHED (ELT) · airframe 92,157 hrs · 17,911 cycles

PORTABLE ELT SAFETY CORD DAMAGED. RE-ATACHED LANYARD AS NECESSARY, IAW AMM 25-63-03.

Part: OXYGEN MASK — INOPERATIVE (FIRST OFFICER'S) · airframe 92,148 hrs · 17,908 cycles

F/O O2 MASK INOPERABLE. RESECURED F/O O2 MASK, IAW AMM 35-11-51. OPERATIONS CHECK GOOD.

Part: STATUS MESSAGE — FALSE ACTIVATION (HI FLOW INHIBIT) · airframe 92,152 hrs · 17,910 cycles

HI FLOW INHIBIT STATUS MESSAGE. TRANSFERRED TO MDDR 135222 DDG 21-51-02-02 CP-22:01Z 29SEP, BWI MX. PERFORMED T/S, PER FIM 21-51 FAULT TREE 813, THE MESSAGE ERASED AND SYSTEM OPS NORMAL. THIS CLEARS THE DMI NR 135222. MCC NOTIFIED AND PLACARD REMOVED. DIS SL @ 07:57Z.

Part: STATUS MESSAGE — FALSE ACTIVATION (HI FLOW INHIBIT) · airframe 92,164 hrs · 17,913 cycles

DURING FLIGHT STATUS MESSAGE "HI FLOW INHIBIT". PERFORMED PACK HI FLOW INHIBIT OPERATIONAL TEST, AS PER AMM 21-51-700 AND NO FAULT FOUND AT THIS TIME.

Part: STATUS MESSAGE — FALSE ACTIVATION (HI FLOW INHIBIT) · airframe 92,116 hrs · 17,898 cycles

HI FLOW INHIBIT STATUS MESSAGE IN FLIGHT. PERFORMED T/S, PER FIM 21-51 F/T 854. NO FAULTS NOTED, SYSTEM CHECK NORMAL.

Part: STATUS MESSAGE — FALSE ACTIVATION (HI FLOW INHIBIT) · airframe 92,084 hrs · 17,888 cycles

HI FLOW INHIBIT STATUS MSG. PERFORMED CHECK, IAW FIM 21-51 FT 813. NO DEFECT, SYSTEM OPERATED NORMAL.

Part: ACOUSTIC LINER — DAMAGED (RT ENGINE) · airframe 92,097 hrs · 17,892 cycles

RIGHT ENGINE ACOUSTIC LINER DAMAGED AFT OF FAN BLADES 6 O'CLOCK POSITION. OK TO CONTINUE, IAW AMM 72-00-00-206-167-H00 FOR UP TO 10 FLIGHT CYCLES OR 100 FLIGHT HOURS, WHICHEVER COMES FIRST. TRANSFERRED TO MDDR 134661 NON MEL, IAW AMM 72-00-00-206-167-H0. REMOVED AND REPLACED LINER, IAW AMM 72-33-01 SYSTEM OK. THIS CLEARS MDDR 134661.

Part: GENERATOR — MALFUNCTIONED (APU) · airframe 92,038 hrs · 17,874 cycles

TRU STATUS MSG DISPLAYED. TRANSFERRED TO MDDR 134008, IAW MEL 24-00-02B, CAT B. REMOVED AND REPLACED APU GENERATOR, IAW AMM 24-21-01. OPS CHECK NORMAL AT THIS TIME, STATUS MSG NOT PRESENT. THIS CLEARS MDDR 134008. MCC NOTIFIED. PLACARD REMOVED.

Part: WARNING MESSAGE — FALSE ACTIVATION (HI FLOW INHIBIT) · airframe 92,038 hrs · 17,874 cycles

HI FLOW INHIBIT STATUS MESSAGE. PERFORMED FIIM 21-51 FT 813 UP TO STEP 21, MESSAGE CLEARED. NO FURTHER DEFECTS NOTED. OPERATED LT & RT PACK FOR 1 HR IAW 21-51-00, MESSAGE DID NOT APPEAR. OPERATIONS CHECK NORMAL.

Part: START VALVE — MALFUNCTIONED (RT ENGINE) · airframe 91,949 hrs · 17,846 cycles

RIGHT STARTER CUTOUT AND RT ENG STARTER EICAS CAUTION INTERMITTENT INFLIGHT. FL 350. PREVIOUS WRITE UP PAGE 1160322. REMOVED AND REPLACED RH ENG. START VALVE IAW AMM 80-11-02 OPS CHECK GOOD</P>)

Part: COMPUTER — FAULTED (EICAS) · airframe 91,930 hrs · 17,842 cycles

RT STARTER CUT OUT MSG CAUTION INTERMITTENT AT 31,000 FT. MSG CAUSED BY FAULTY L EICAS COMPUTER. REF ITEM #3 FOR REPLACEMENT OF EICAS COMPUTER, RAN RT ENGINE IAW AMM 71-00-00. OPS CHECK GOOD. RT STARTER CUTOUT MSG DID NOT RETURN. ITEM 3: REMOVED AND REPLACED L EICAS COMPUTER IAW 31-41-02 AND UPLOADED CORRECT SOFTWARE IAW 31-41-02-201. OPS CHK GOOD.

Part: SHUTOFF VALVE — MALFUNCTIONED (RIGHT) · airframe 91,872 hrs · 17,822 cycles

UPON ENG START, "R ENG BLEED OFF" CAUTION MSG APPEARED AND REMAINED ILLUMINATED TRANSFERRED TO MDDR # 133090 PER MEL 36-11-01-02A, CAT C, DUE 29AUG20. PLACARD INSTALLED. LP 1279625 ITEMS 7,8,9: REMOVED RH PRSOV IAW AMM 36-11-09. PRSOV IN PYLON BUT NOT INSTALLED. REQ E-SEALS, CLAMP INSTALLATION, PNEUMATIC LINE INSTALLATION, ON UP TO STEP #6 FORWARD. SEE ITEM #8 FOR CONTINUATION. ITEM 8: COMPLETED INSTALL OF RH PRSOV UP TO STEP G OF AMM 36-11-09. NO DEFECTS. TEST AND OPS CHK REQ. REF ITEM M9 FOR OPS CHK. ITEM 9: PERFORMED OPS CHK AND LEAK CHK IAW AMM 36-11-09. OPS CHKS GOOD. LP 1279626 ITEM 12:REF LP 1279625 ITEM M7-M9 FOR CORRECTIVE ACTION. THIS CLEARS DMI #133090. MCC NOTIFIED PLACARDS REMOVED.

Part: WARNING MESSAGE — ILLUMINATED (ENGINE BLEED) · airframe 91,868 hrs · 17,821 cycles

AFTER ENG START ENGINE BLEED OFF EICAS MESSAGE REMAINED AND OFF LT REMAINED ILLUMINATED. PERFORMED AIR SUPPLY BITE TEST IAW AMM 36-23-0 AND PERFORMED ENGINE RUN UP IAW AMM 71-00-00.

Part: WARNING MESSAGE — INTERMITTENT (RT ENGINE) · airframe 91,852 hrs · 17,817 cycles

INTERMITTENT R ENG BLEED OFF EICAS MSG DURING FLIGHT PERFORMED FIM 36-10 FAULT TREE 837 AND PERFORMED ENG RUN. IAW AMM 71-00-00. OPS CHECK GOOD.

Part: PITOT TUBE — WARNING MESSAGE (LEFT) · airframe 91,864 hrs · 17,820 cycles

L AUX PITOT MSG AFTER STARTING RT ENG ON PUSH BACK. REMOVED AND REPLACED L AUX PITOT PROBE IAW AMM 34-11-01 OPS CHECK GOOD

Part: WARNING MESSAGE — FALSE ACTIVATION (WX RADAR SYS) · airframe 91,810 hrs · 17,807 cycles

WINDSHEAR SYS EICAS MSG(<P>BITE CHK LEFT AND RIGHT WEATHER RADAR RECEIVERS IAW 34-43 FT 805. INPUT OK AND RADAR OK ON BOTH SIDES. OPS CHECKED IAW 34-43-00, NO FAULTS NOTED. FLT CREW RECEIVED FAULT ON R TRANSCEIVER, PLACED PN 066-50008-0408 ON ORDER AS PRECAUTIONARY.<BR /></P>)

Part: CONTROL PANEL — INOPERATIVE (APU) · airframe 91,705 hrs · 17,777 cycles

APU INOPERATIVE. OPERATIONS NOT ALLOWED. REMOVED AND REPLACED APU CONTROL PANEL ASSY IAW AMM 49-11-81, OPS CHECKED NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 91,694 hrs · 17,775 cycles

HI FLOW INHIBIT DISPLAYED DURING CLIMB. FAULT COULD NOT BE DUPLICATED AT THIS TIME, SYS CKS NORMAL IAW REF FIM 21-51-875. PERFORMED T/S SYSTEM IAW FIM 21-51 FT 813. NO FAULTS NOTED. CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT WX RADAR SYS) · airframe 91,666 hrs · 17,765 cycles

RECEIVED A WINDSHEAR SYS EICAS AND WXR FAIL MESSAGE DURING TAXI OUT, WITH RT RADAR ON, SWITCHED TO LT, SYSTEM AND MESSAGE CLEARED. COMPLIED WITH A WEATHER RADAR TEST IAW AMM 33-43-00. NO EICAS MESSAGE PRESENT.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT EEC) · airframe 91,666 hrs · 17,765 cycles

LEFT ENG EEC C1 STATUS MESSAGE. COMPLIED WITH ENG RUNS IAW AMM 72-00-00. NO STATUS MESSAGE PRESENT. COMPLIED WITH A BITE OF THE LT PIMU IAW FIM 73-21 FT 885. NO MESSAGES PRESENT.

Part: DUCT — TORN (APU BLEED) · airframe 91,666 hrs · 17,765 cycles

DURING APU INSPECTION, FOUND AIR SURGE DUCT TORN BEFORE SURGE VALVE. REMOVED AND REPLACED AIR SURGE DUCT BEFORE SURGE VALVE IAW AMM 49-53-01. OPS CHECKED NORMAL. NO LEAKS DETECTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (A/C PACKS) · airframe 91,660 hrs · 17,763 cycles

HI FLOW INHIBIT STATUS MESSAGE. PERFORMED FIM 21-51, FT 813, SHUTDOWN LT AND RT PACKS FOR 15 SECONDS, SWITCHED THEM TO ON POSITION, VERIFIED MESSAGE DOES NOT COME BACK, SYSTEM CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT A/C PACK) · airframe 91,653 hrs · 17,761 cycles

HIGH FLOW INHIBIT MESSAGE ON EICAS. BITE TESTED LT PACK CONTROLLER IAW AMM 21-51-00. NO FAULTS NOTED. RESET LT PACK CONTROLLER. MESSAGE CLEARED.

Part: STATUS MESSAGE — FALSE ACTIVATION · airframe 91,636 hrs · 17,757 cycles

STATUS MESSAGES: AIR/GRD DISAGREE, CABIN ALTITUDE AUTO 2, LANDING GEAR MONITOR. PERFORMED GROUND TEST IAW AMM 32-90-01, TEST PASSED, PERFORMED GROUND TEST IAW 21-31-00, TEST PASSED. PERFORMED GROUND TEST IAW AMM 32-61-00, MESSAGE CLEARED. OK FOR RETURN TO SERVICE.

Part: OXYGEN MASK — MALFUNCTIONED (FIRST OFFICER'S) · airframe 91,636 hrs · 17,757 cycles

FIRST OFFICER`S OXYGEN MASK WOULD NOT TEST DURING PRE-FLIGHT. PULLED THE MASK OUT AND AFTER 1-2 MINUTES OF TESTING IT STARTED WORKING. REMOVED AND REPACKED THE OXYGEN MASK IN STORAGE BOX. OPS CHECKED GOOD IAW MM 35-11-00.

Part: CONTROL UNIT — UNKNOWN (COCKPIT TEMP) · airframe 91,563 hrs · 17,732 cycles

UNABLE TO CHANGE COCKPIT TEMP TO WARM THE AREA IN EITHER AND IN FULL ROTATION TO 'W' OR MANUAL IN FULL INCREASE. PERFORMED ZONE TEMP CONTROLLER BITE IAW AMM 216099/101. NO FAULTS NOTED. PERFORMED FLIGHT DECK TEMP CONTROL AND OPS TESTED IAW AMM 21-61-07. NO FAULTS NOTED, OPS CHECKED OK.

Part: STATUS MESSAGE — FALSE ACTIVATION (HIGH FLOW) · airframe 91,563 hrs · 17,732 cycles

HI FLOW INHIBIT STATUS MESSAGE. PERFORMED FIM PROCEDURE 21-51, FAULT TREE 813 IAW FIM. NO DEFECTS NOTED. EICAS MESSAGE CLEARED.

Part: STATUS MESSAGE — FALSE ACTIVATION (HIGH FLOW) · airframe 91,538 hrs · 17,724 cycles

HI FLOW INHIBIT STATUS MESSAGE IN FLIGHT. PERFORMED FIM 21-51 FT 813 WITH L & R PACK ON OFF POSITION, NO MESSAGE NOTED.

Part: FILTER — DIRTY (TEMP CONTROL) · airframe 91,523 hrs · 17,719 cycles

FLIGHT DECK ZONE TEMP CONTROLLER UNABLE TO CONTROL. CLEANED FLT DECK ZONE TEMP CONTROL FILTER AND SCREEN, OPS CHECKED IAW AMM 21-61-00 AND AMM 21-61-03. OK FOR SERVICE.

Part: CONTROL SYSTEM — MALFUNCTIONED (MAIN DECK TEMP) · airframe 91,542 hrs · 17,725 cycles

UNABLE TO CONTROL MAIN DECK CARGO TEMP, FWD TEMP MX + 9* , AFT TEMP MAX +13* , FLIGHT DECK FROM VALVE FULL OPEN TO MAINTAIN ADEQUATE TEMP. PERFORMED FIM 21-60 FT 804, NO FAULTS NOTED ON ZONE TEMP CONTROLLER. PERF OPS CHECK ON TEMP CONTROL VALVES, SYSTEM OPERATES NORMAL IAW AMM 21-61-06.

Part: CONTROLLER — MALFUNCTIONED (TEMP CONTROL) · airframe 91,527 hrs · 17,721 cycles

FLIGHT DECK ZONE TEMPERATURE CONTROLLER UNABLE TO CONTROL TEMPERATURE. PERFORMED OPS CHECK OF TEMP CONTROL VALVE INDICATION IAW AMM 21-64-06. OPS CHECKED NORMAL.

Part: CONTROLLER — UNKNOWN (CABIN TEMP) · airframe 91,499 hrs · 17,713 cycles

FWD, AFT & FLIGHT DECK CABIN TEMP CONTROLLERS NOT MAINTAINING SELECTED TEMP. PERFORMED FIM 21-61- TASK 801 . CABIN TEMP CONTROL NORMAL . NO FAULTS FOUND

Part: STATUS MESSAGE — FALSE ACTIVATION (HIGH FLOW) · airframe 91,429 hrs · 17,689 cycles

HIGH FLOW INHIBIT STATUS MESSAGE. PERFORMED BITE CHECK OF LEFT AND RIGHT PACK CONTROLLER IAW AMM 21-51-14. OPERATED GOOD, NO FAULTS FOUND. PERFORMED HI FLOW INHIBIT OPERATIONAL CHECK IAW AMM 21-51-00. NO FAULTS.

Part: APU — UNKNOWN · airframe 91,431 hrs · 17,690 cycles

APU DID NOT START AFTER LANDING 2 ATTEMPTS. PERFORMED BITE TEST PER FIM 49-11 FT 958. TESTED OK. STARTED APU 1ST ATTEMPT.

Part: CIRCUIT CARD — FAULTED (FIRE LOOP) · airframe 91,412 hrs · 17,684 cycles

STATUS MSG R ENGINE FIRE LP 1. REMOVED AND REPLACED THE FIRE DETECTION CIRCUIT CARD IAW FIM FT 26-11 FT 804 & AMM 26-11-02.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 91,354 hrs · 17,666 cycles

HIGH FLOW INHIBIT STATUS MSG DISPLAYED. PERFORMED FIM 21-51 FAULT TREE 813. MSG CLEARED, NO FAULTS NOTED AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT A/C PACK) · airframe 91,336 hrs · 17,659 cycles

HI FLOW INHIBIT DISPLAY IN FLIGHT. PERFORMED FIM 21-51 FT 854, NO FAULT FOUND, RIGHT PACK SYSTEM OPS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 91,323 hrs · 17,654 cycles

STATUS MSG T ALT HIGH FLOW INHIBIT. PERFORMED OPERATIONAL TEST OF AIR CONDITIONER SYSTEM AND NO DEFECTS NOTED AT THIS TIME IAW AMM 21-00-00 AND AMM 21-25-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (A/C PACKS) · airframe 91,238 hrs · 17,627 cycles

STATUS MSG HI FLOW INHIBIT. OPERATED BOTH LEFT AND RIGHT PACKS AND REF FIM 21-51 FAULT TREE 813. OPS CHECK GOOD. NO MSG REPEATED. OK FOR RTS.

Part: TRU — MALFUNCTIONED (APU) · airframe 91,185 hrs · 17,610 cycles

APU TRU INOPERATIVE.(<P>TRANSFERRED TO&NBSP;MDDR 128522 IAW MEL 24-32-01B, CAT 'D'.</P><P> LP 1150932-3 - (20MAY20) - REMOVED AND REPLACED APU TRU IAW AMM 24-32-04. OPS CHECK NORMAL AT THIS TIME. THIS CLEARS MDDR 128522 . MCC ADVISED.</P>)

Part: START VALVE — MALFUNCTIONED (RT ENGINE) · airframe 91,164 hrs · 17,603 cycles

R STARTER CUTOUT MESSAGE MOMENTARILY AFTER ENGINE START.(<P>TRANSFER TO MDDR #128457 IAW DDG 80-11-02, CAT 'C', DUE DATE 27-MAY-2020.</P><P>LP 1150928: REMOVED AND REPLACED RIGHT ENGINE START VALVE OPS CHECK GOOD AMM 80-11-00. THIS CLEARS MDDR 128457.<BR /></P>)

Part: START VALVE — MALFUNCTIONED (NR 2 ENGINE) · airframe 91,133 hrs · 17,595 cycles

EICAS MSG R STARTER CUTOUT ACCOMPANIED WITH R ENGINE STARTER MSG.(<P>REMOVED AND REPLACED #2 ENGINE STARTER VALVE IAW AMM 80-11-02.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 91,125 hrs · 17,593 cycles

HI FLOW INHIBIT STATUS MESSAGE.(<P>PERFORMED FIM 21-51 FAULT TREE 813. HI FLOW INHIBIT MESSAGE CLEARED. NO OTHER FAULTS NOTED.</P>)

Part: CONNECTOR — LOOSE (START VALVE) · airframe 91,115 hrs · 17,588 cycles

RIGHT STARTER CUTOUT (IN FLIGHT) INTERMITTENT WARNING.(<P>FOUND CONNECTOR P94 AND D10970 LOOSE AT START VALVE. SECURED CONNECTORS. OPS CHECK START VALVE NORMAL. NO DEFECTS NOTED IAW AMM 80-11-02 AND 71-00-00.</P>)

Part: PSEU — SHORTED (DOOR) · airframe 90,969 hrs · 17,543 cycles

EMERGENCY DOORS ANNUNCIATOR LT FLASHING ON OVERHEAD PANEL.(<P>LP 1071486-10 - SLAVED IN SERVICEABLE ANNUNCIATOR PANEL (M10394) IAW WDM 33-16-17 NO HELP. RETURNED TO ORIGINAL CONFIG. REF SWPM 20-60-06.&NBSP;</P><P>LP 1071486-11 - T/S PER AMM 32-09-04. PSEU FAULTED S174 "FAR". FOUND TB101 FA195 &AMP; FC195 TO BE SHORTING DUE TO IMPROPER INSTALLATION PER IAW WDM 52-71-15. CLEANED &AMP; PROPERLY INSTALLED PER IAW WDM 52-71-15 AND SWPM 20-90-11. OPS TEST GOOD PER AMM 32-09-04 NO FURTHER DEFECTS NOTED @ THIS TIME.</P>)

Part: CIRCUIT CARD — FAULTY (E&E BAY) · airframe 90,953 hrs · 17,537 cycles

FWD EQ EXH FAN EICAS MESSAGE(<P>T/S PER FIM 21-58-FT 905, FAULTED ECS FAN CONTROL CARD M990. REPLACED CARD IAW AMM 21-26-05, OPS CKS GOOD.</P>)

Part: SENSOR — DEFECTIVE (CABIN TEMP) · airframe 90,937 hrs · 17,533 cycles

STATUS CARGO A/C TEMP(<P>REMOVED AND REPLACED FWD DUCT TEMP SENSOR&NBSP; IAW AMM 21-61-01. OPS CHECK GOOD.</P>)

Part: FIRE LOOP — UNKNOWN (LT ENGINE) · airframe 90,928 hrs · 17,529 cycles

LEFT ENGINE FIRE LOOP 1 INOPERATIVE. PERFORMED SYSTEM TEST OK IAW AMM 26-11-00.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 90,928 hrs · 17,529 cycles

L ENG FIRE LP1 AS DEBRIEFED CREW STATED MSG APPEARED DURING FINAL INTO CVG.(<P>PERFORMED FIM 26-11 F/T 805, MSG NO LONGER IN VIEW. FIRE OVERHEAT TEST IAW 767 AMM 26-11-00, OPS CHECKS GOOD.<BR /></P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 90,911 hrs · 17,523 cycles

L ENG FIRE LP 1 MESSAGE.(<P>TRANSFERRED TO MDDR 126865 AS PER MEL 26-11-01-01, CAT "C".</P><P><SPAN>LP 1189807: T/S PER FIM 26-11 FT 804 TO STEP SHEET 5 BLOCK 110. PER FIM SYSTEM IS OK, THIS CLOSES MDDR #126865, MCC NOTIFIED. PLACARDS REMOVED.</SPAN><BR /></P>)

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 90,873 hrs · 17,511 cycles

APU TOOK 3 ATTEMPTS TO START(<P>PERFORMED APU STARTING AND OPERATIONAL CHECK&NBSP; IAW AMM 49-11-00. NO DEFECTS NOTED. OPS CHECK NORMAL.</P>)

Part: OXYGEN MASK — INOPERATIVE (COCKPIT) · airframe 90,855 hrs · 17,504 cycles

F/O'S O2 MASK WILL NOT INFLATE.(<P>SWAPPED O2 MASK FROM #3 PASSENGER SEAT IAW AMM 35-11-00. MASK OPERATED NORMAL (DEFECTIVE O2 MASK PN&NBSP;MC10-25-104, SN&NBSP;11227). NOW&NBSP;PASSENGER #3 SEAT O2 MASK WILL NOT INFLATE.&NBSP;TRANSFERRED TO MDDR 126495 IAW AMM 25-25-03, CAT D, DUE DATE 29-JUL-20.</P><P>LP 1149897: REMOVED AND REPLACED OXYGEN MASK IAW AMM 35-11-51. THIS CLEARS MDDR 126495.<BR /></P><P><BR DATA-TEMP="1" /></P>)

Part: START VALVE — STUCK (NR 1 ENGINE) · airframe 90,684 hrs · 17,454 cycles

#1 ENG START VALVE STUCK IN THE OPEN POSITION.(<P>REMOVED AND REPLACED START VALVE IAW AMM 80-11-02. OPS CHECKS GOOD IAW AMM 71-00-00. PERFORMED 3 SUCCESSFUL STARTS OF THE LH ENGINE IAW AMM 71-00-00.</P>)

Part: SURGE VALVE — FAULTY (APU) · airframe 90,675 hrs · 17,450 cycles

APU FAULT REVERSE FLOW APU INOP.(<P>TRANSFERRED TO DMI 125491 PER MEL 49-11-01A, CAT 'C'.</P><P>LP 1208396 ITEM M9: REMOVED AND REPLACED APU SURGE CONTROL VALVE IAW AMM 49-53-01, OPS CHK AND LEAK CHK GOOD. THIS CLEARS DMI 125491.</P><P>LP 1208395:&NBSP;WHEN DOING TROUBLESHOOTING APU SHOT OF VISUAL INSP BITE BOX FOUND REVERSE FLOW VALVE GASKET BROKEN. REPLACED REVERSE FLOW VALVE GASKET IAW 49-53-08 (OFF PART:&NBSP;<SPAN>PN&NBSP;3876415-4, NSN</SPAN><SPAN>).</SPAN></P><P>LP 1208396 ITEM M10: INSTALLED NEW BOLT ON APU REVERSE FLOW VALVE IAW AMM 49-53-08. OPS CHECK AND LEAK CHECK GOOD AT THIS TIME.</P>)

Part: IGNITER — DEFECTIVE (RT ENGINE) · airframe 90,675 hrs · 17,450 cycles

RH ENG REQUIRED 2 START ATTEMPTS. AFTER START, R ENG IGNITOR 1 STATUS MESSAGE.(<P>PERFORMED PIMU BITE TEST,&NBSP;VISUAL INSPECTION OF IGNITOR SHOWS BAD. REMOVED AND REPLACED RH ENG #2 IGNITOR IAW AMM 74-21-02. OPS CHKS GOOD IAW AMM 74-00-00.<BR /></P>)

Part: VALVE — FAULTY (CABIN TEMP) · airframe 90,623 hrs · 17,431 cycles

FWD/AFT CABIN TEMP EICAS MSG(<P>DEFERRED CABIN TEMP CONTROL SYS IAW MEL 21-61-01-02, DMI 125198, CAT 'C'.</P><P>LP 1208383 - M5: REMOVED AND REPLACED FWD TRIM VALVE IAW AMM 21-61-07.</P><P>LP 1208398 - M16: OPS SYSTEM TEST OK IAW AMM 21-61-01, CLEARED MDDR 125198.</P>)

Part: IGNITER — FAILED (NR 2 ENGINE) · airframe 90,552 hrs · 17,411 cycles

ATTEMPTED 2 STARTS ON RIGHT ENGINE. GOOD DUCT PRESSURE ROTATION, FUEL FLOWING IN SINGLE AND BOTH HAD NO LIGHT OFF.(<P>PERFORMED ENGINE RUN IAW AMM 71-00-00. ENGINE RUN GOOD. FAULTED RIGHT ENGINE IGNITION 2. TRANSFERRED TO MDDR 124867 IAW MEL 74-00-01A, CAT "A". </P><P>LP 1190679: REMOVED AND REPLACED #2 ENG IGNITER IAW AMM 74-21-02 AND OPS CHECKED GOOD IAW AMM 71-00-00/801. THIS CLEARS MDDR 124867.</P><P><BR /></P>)

Part: CONTROL VALVE — FAILED (CARGO HEAT) · airframe 90,409 hrs · 17,367 cycles

CARGO A/C TEMP EICAS MESSAGES (FORWARD CARGO AIR CONDITIONING SYSTEM / (NOTIGY DISPATCH))&NBSP; &NBSP;&NBSP;(<P>TRANSFERRED TO MDDR 124223 IAW MEL 21-28-01, CAT 'D'.</P><P>LP 1070867: REMOVED AND REPLACED FWD CARGO HEAT CONTROL VALVE IAW AMM 21-43-02. OPS CHECK NORMAL AT THIS TIME. THIS CLEARS MDDR 124223. PLACARDS REMOVED. MCC NOTIFIED.</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (CARGO TEMP) · airframe 90,409 hrs · 17,367 cycles

CARGO A/C TEMP STATUS MSG.(<P>PERFORMED OPERATION TEST ON CARGO A/C TEMP REF 21-28 FAULT TREE 804. SYS OK.<BR /></P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (CARGO TEMP) · airframe 79,475 hrs · 10,930 cycles

CARGO A/C TEMP STATUS MESSAGE. PERFORMED AN OPS CHECK IAW AMM 21-28-00/705, OPS CHECKED GOOD.

Part: STATUS MESSAGE — FALSE ACTIVATION (CARGO TEMP) · airframe 90,409 hrs · 17,367 cycles

CARGO A/C TEMP STATUS MSG.(<P>PERFORMED BITE CHECK OF PACK TEMP CONTROLLER PER 21-51-00. NO FAULTS NOTED, STATUS MSG CLEARED.<BR /></P>)

Part: INDICATION SYS — MALFUNCTIONED (RT ENG OIL PRESS) · airframe 90,297 hrs · 17,331 cycles

RIGHT ENGINE OIL PRESSURE INDICATION WENT TO ZERO AFTER LANDING. PERFORMED RIGHT ENGINE IDLE RUN PER AMM 72-00-00. OIL PRESSURE WAS NORMAL DURING ENGINE RUN. NO DEFECTS NOTED AT THIS TIME. A/C OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 90,206 hrs · 17,294 cycles

DURING CLIMB OUT MAIN DECK CARGO DOOR LIGHT ILLUMINATED.(<P>PLACED MAIN DECK CARGO INDICATION ON MEL 52-71-01-02, MDDR 122924, C/W DDG, OBSERVED LOCK SECTORS ENGAGING LATCH CAMS, VENT DOORS FAIRED, NO DAMAGE NOTED ON MECHANISMS.</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (CARGO TEMP) · airframe 90,107 hrs · 17,260 cycles

CARGO A/C TEMP STATUS MSG.(<P>PERFORMED OPS CHECK ON A/C TEMP SYSTEM. OPS CHECK NORMAL. NO DEFECT NOTED IAW AMM 21-61-00.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (A/C PACK) · airframe 90,018 hrs · 17,225 cycles

STATUS MESSAGE "HI FLOW INHIBIT".(<P>RECYCLED PACK CONTROL SWITCH, AND "HI FLOW INHIBIT" STATUS MSG ERASED AS PER FIM 21-51 TASK 875.</P>)

Part: SWITCH — INOPERATIVE (AIR TRIM) · airframe 90,008 hrs · 17,221 cycles

"ON" INDICATOR LIGHT ON TRIM AIR ON/OFF SWITCH INOPERATIVE. REMOVED AND REPLACED TRIM AIR ON SWITCH IAW SWPM 20-84-00. OPS CHECKED GOOD IAW MM 21-51-00.

Part: SWITCH — FALSE INDICATION (FWD CARGO) · airframe 90,016 hrs · 17,224 cycles

FWD CARGO A/C EICAS MESSAGE(<P>TRANSFERRED TO DMI 121519 IAW MEL 21-28-01, CAT 'D'.</P><P>LP 1025893 - M4: PERFORMED&NBSP; ACTION PLAN-16140, REPLACED&NBSP; SWITCH&NBSP; ASSY&NBSP; OVHT&NBSP; IAW B767 AMM 21-61-01, OPS CHECK GOOD, PERFORMED FIM 21-58 FT 810, NO FAULTS FOUND. THIS CLEARS DMI 121519, PLACARDS REMOVED, MCC NOTIFIED.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (HIGH FLOW) · airframe 89,997 hrs · 17,217 cycles

HI FLOW INHIBIT STATUS MESSAGE.(<P>PERFORMED FIM 21-51 FAULT TREE 813. NO DEFECTS FOUND AT THIS TIME, CHECK OK.</P>)

Part: WARNING LIGHT — ILLUMINATED (IDLE DISAGREE) · airframe 89,918 hrs · 17,194 cycles

ON APPROACH, IDLE DISAGREE DISPLAYED ON EICAS SEVERAL TIMES, THEN EXTINGUISHED.(<P>PERFORMED TROUBLESHOOTING PER FIM 71-05 FAULT TREE 846, AND NO DEFECTS FOUND ON BOTH ENGINES' IDLE READING AT THIS TIME.</P><P>NOTE: LP 1113292 - M5:&NBSP;NO IDLE DISAGREE FAULTS ON LAST FLIGHT, NOTED BY PILOTS.</P>)

Part: NONE — NONE (NONE) · airframe 89,859 hrs · 17,175 cycles

BIRD STRIKE RIGHT ENGINE(<P>PERFORMED&NBSP; #2&NBSP; ENGINE&NBSP; BOROSCOPE&NBSP; INSPECTION&NBSP; PER&NBSP; B767&NBSP; AMM 72-00-00/601.&NBSP; NO&NBSP; DAMAGE&NBSP; OR&NBSP; DEFECTS&NBSP; NOTED. C/W&NBSP; FIM&NBSP; 71-05 FT 822&NBSP; AND&NBSP; AMM 05-51-18.</P><P>LP 1110215 - M2: INSTALLED BOROSCOPE&NBSP; MOTERIM&NBSP; COVER&NBSP; PAD AND&NBSP; SEAL,&NBSP; REF&NBSP; AMM&NBSP; 71-00-00-995.&NBSP; NO&NBSP; LEAKS NOTED.<BR /></P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (HIGH FLOW) · airframe 89,851 hrs · 17,172 cycles

STATUS MSG 'HI FLOW INHIBIT' IN CRUISE AT 38,000 FT(<P>PERFORMED FIM 21-51 FAULT TREE 813, MSG CLEARED. A/C SATISFACTORY AT THIS TIME.<BR /></P>)

Part: BULB — INOPERATIVE (INDICATOR) · airframe 89,818 hrs · 17,157 cycles

R BUS TIE ISLN "AUTO" LIGHT INOP.(<P>TRANSFERRED TO MEL 24-27-04, DMI #120272 ASSIGNED, MCC NOTIFIED.</P><P>LP 1110212 - M3: RELAMPED R/H BUS TIE AUTO INDICATOR IAW B767 AMM REF 33-13-00, OPS CHECK GOOD. THIS CLEARS DMI #120272. PLACARD REMOVED.</P>)

Part: DIODE — DEFECTIVE (EXTINGUISH SYS) · airframe 89,782 hrs · 17,144 cycles

LOWER CARGO FIRE BOTTLE DISCHARGE LIGHT WON'T TEST.(<P>TRANSFERRED TO MEL 26-23-01-03A, MDDR 120039 ASSIGNED, CAT 'C', MBCR 12NOV19.&NBSP;</P><P>LP 1098343 - ITEM 3: REMOVED AND REPLACED KORRY SWITCH (OFF PART: P/N&NBSP;S231T290-5060, SN: NSN)&NBSP;AND DIODE IAW SWPM 20-84-15 FOR LWR CARGO FIRE DISCHARGE LIGHT. LIGHT TEST GOOD IAW AMM 33-13-00. THIS CLEARS DMI 120039. PLACARDS REMOVED.&NBSP;</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 89,673 hrs · 17,110 cycles

SHORTLY AFTER TAKEOFF, RECEIVED "FWD CGO BACKUP" EICAS MESSAGE, BRIEFLY FOLLOWED BY "CARGO A/C TEMP" STATUS MESSAGE.(<P>PERFORMED SATISFACTORY BITE OF THE ZONE TEMP CONTROLLER IAW FIM 21-60 FAULT TREE 804. NO FAULTS NOTED AT THIS TIME.<BR /></P>)

Part: RADAR — FALSE INDICATION (WEATHER) · airframe 89,553 hrs · 17,070 cycles

WINDSHEAR SYSTEM MESSAGE ON SHORT FINAL. PERFORMED WEATHER RADAR OPERATIONAL TEST FOR CAPT AND FO'S IAW AMM 34-43-00. NO FAULTS OR MESSAGE NOTED AT THIS TIME.

Part: BULB — WRONG PART · airframe 89,544 hrs · 17,067 cycles

GEN DRIVE LIGHTS, BUSS TIE ISOLATION, AND WINDOW HEAT LIGHTS ILLUMINATED IN FLIGHT, OVERRIDE ON. NO ASSOCIATED EICAS MESSAGES. FOUND WRONG LIGHT BULBS INSTALLED. REPLACED WITH CORRECT BULBS, OPS CHECKED NORMAL IAW AMM 33-13-00.&NBSP;</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 89,430 hrs · 17,024 cycles

AFTER LANDING WE RECEIVED LEFT ENGINE BLEED OFF ADVISORY MESSAGE. PERFORMED ENGINE RUN IAW AMM 71-00-00. LEFT ENGINE BLEED CHECK GOOD IAW AMM 36-11-00. NO RELATED AND AIR SUPPLY BITE CHECK GOOD.

Part: IGNITER — DEFECTIVE (RT ENGINE) · airframe 89,428 hrs · 17,023 cycles

DURING RIGHT ENG STARTUP, NO EGT RISE AFTER FUEL SELECTOR TO RUN. N2 REMAINED 25.2, FUEL CUTOFF. SWITCHED IGNITER FROM SINGLE TO BOTH, ENGINE START NORMAL, RT ENG IGNITER 2 STATUS. PERFORMED T/S AS PER FIM 74-00 FT 811, CLEARED FAULTS IN BOTH PIMUS. ALSO VERIFIED GND AND VOLTAGE AT BOTH IGN BOXES ON RT ENGINE AS PER WDM 74-31-21 IGN SCHEMATIC, NO ISSUES NOTED. LP 1109658 - M5: REMOVED AND REPLACED RT ENG NR 1 IGNITER, OPS CHECK GOOD IAW AMM 74-21-02. LP 1109659 - M6: REMOVED AND REPLACED RT ENG NR 2 IGNITER, OPS CHECK GOOD IAW AMM 74-21-02.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENGINE BLEED) · airframe 89,372 hrs · 17,002 cycles

"LEFT ENG BLEED OFF", ACCELERATED ENGINE BUT MESSAGE REMAINED. FOLLOWED QRH PROCEDURES AND CONTACTED MX CONTROL. PERFORMED AIR SUPPLY CHECK IAW FIM 36-20-00/101 FIG 104. PERFORMED ENG RUN IAW AMM 71-00-00. OPS CHECK NORMAL

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENG BLEED) · airframe 89,343 hrs · 16,993 cycles

LEFT ENG BLEED OFF EICAS MESSAGE INTERMITTENTLY DURING FLIGHT WITH LOW POWER SETTINGS. THE LEFT DUCT PRESSURE WAS HALF THE PRESSURE OF THE RIGHT. PERFORMED B767 FIM 21-51-FT 803, OPS CHECKS GOOD. ACFT RETURNED TO NORMAL CONFIGURATION.

Part: WARNING MESSAGE — FALSE ACTIVATION (CARGO TEMP) · airframe 89,297 hrs · 16,979 cycles

"CARGO A/C TEMP" STATUS MSG.(<P>T/S PER B767 FIM 21-28 FT 809. NO FAULT NOTED AT THIS TIME.</P>)

Part: INDICATOR — FAILED (EHSI) · airframe 89,287 hrs · 16,976 cycles

ON GROUND BEFORE PUSH THE EHSI ON CAPTS SIDE FAILED. SMOKE WAS PRESENT. REMOVED AND REPLACED CAPTS EHSI IAW AMM 34-22-04. OPS CKS GOOD</P>)

Part: RELAY — FAILED (FWD CARGO) · airframe 89,194 hrs · 16,946 cycles

FWD CARGO OVHT LIGHT ILLUMINATED. REMOVED AND REPLACED RELAY K231 IN P37 IAW SWPM 20-81-14. OPS CHECK GOOD AS PER AMM 21-43-00.

Part: SWITCH — FAILED (CARGO OVERHEAT) · airframe 89,169 hrs · 16,937 cycles

CGO FLOOR OVERHEAT EICAS MSG WITH ASSOCIATED FWD CGO OVERHEAT INDICATION ON OVERHEAD PANEL. FWD CARGO HEAT INOP.(<P>TRANSFERRED TO MDDR #115609 IAW MEL 21-40-01-01, CAT 'C', DUE 11AUG19. C/W MAINTENANCE PROCEDURES PER DDG 21-40-01-01, DEACTIVATED VALVE V89.</P><P>LP 1073603 - M3: REMOVED AND REPLACED FWD CARGO OVHT TEMP SWITCH IAW B767 AMM 21-43-05. OPS CHECK GOOD. THIS ACTION CLEARS DMI 115609, PLACARD REMOVED. A/C DE-CONFIGURED FROM DDG 21-40-01-01.&NBSP;</P>)

Part: TERMINAL — BROKEN · airframe 89,169 hrs · 16,937 cycles

L ENG HPSOV EICAS MSG FOUND BROKEN CONNECTOR OF WIRES AT TERMINAL 1 OF HPSOV TERMINAL BLOCK V347 WDM 36-11-61-1. REPAIRED TERMINAL CONNECTOR IAW SWPM 20-30-22. PERFORMED OPS CHECK IAW AMM 36-11-07-705-130. NO FAULTS NOTED. PERFORMED ENGINE RUN AND BITE CHECK OF AIR SUPPLY CONTROL SYSTEM, NO DEFECTS NOTED AT THIS TIME. OPS NORMAL, BITE PERFORMED IAW AMM 36-23-00.

Part: RELAY — MALFUNCTIONED (CARGO HEAT) · airframe 89,163 hrs · 16,935 cycles

FWD CARGO HEAT INOP. PERFORMED FIM 21-43 FT 806, BLOCK 50. REMOVED AND REPLACED K2085 ANNUNCIATOR DISCONNECT RELAY. PERFORMED FWD CARGO HEATING SYSTEM OPERATIONAL TEST, NO FURTHER DEFECTS NOTED PER AMM 21-43-00.

Part: SHUTOFF VALVE — DISCONNECTED (CARGO BAY) · airframe 89,161 hrs · 16,934 cycles

PRIOR TO DEPARTURE, STATUS MSG COND CARGO VALVE.&NBSP;(<P>ON T/S, FOUND FWD CARGO A/C SHUTOFF VALVE V381 DISCONNECTED, RECONNECTED VALVE. FWD CARGO A/C SYSTEM OPERATIONAL TEST NORMAL IAW AMM 21-28-00, NO ACTIVE MSG.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 89,157 hrs · 16,932 cycles

"FWD CGO BACK UP " EICAS MSG. (<P>TROUBLESHOOT PER FIM FT 21-61 TR 803, NO FAULTS FOUND AT THIS TIME. A/C OK FOR SERVICE.</P>)

Part: VALVE — MALFUNCTIONED (CARGO HEAT) · airframe 89,161 hrs · 16,934 cycles

"CGO FLOOR OVHT" EICAS MSG. (<P>TRANSFER TO MDDR 115336 IAW DDG 21-40-01-01.</P><P>LP 1073583 - M2: REMOVED AND REPLACED VALVE ASSY - CARGO HEAT (V-89) IAW AMM 21-43-01. OPS TEST OK, FWD CARGO HEAT SHUTOFF VALVE (V-89). CLEARED MDDR #115336. PLACARD REMOVED AND MCC NOTIFIED.</P>)

Part: BATTERY — LOW VOLTAGE (APU) · airframe 89,138 hrs · 16,925 cycles

APU WILL NOT START DUE TO LOW BATT. VOLTAGE. (<P>REMOVED AND REPLACED&NBSP;APU BATTERY IAW AMM 24-31-05. OPS CHECKS GOOD.<BR /></P>)

Part: CIRCUIT BREAKER — TRIPPED (COCKPIT) · airframe 89,124 hrs · 16,921 cycles

AFT EQ EXH FAN 2 STATUS MSG. (<P>RESET EQ EXH 2 BRKR PER AMM 21-58-00, MESSAGE CLEARED.<BR /></P>)

Part: GASKET — RUPTURED (APU) · airframe 89,102 hrs · 16,915 cycles

APU DOES'T START. (<P>TRANSFER TO MDDR #114547 IAW MEL 49-11-01A CAT "C" DUE DATE 21-JUL-19 PLACARD INSTALLED. </P><P>LP 1050740 - M5:&NBSP;TS APU IAW FIM TASK 49-11 FAULT TREE 989, FOUND BOLT ON INLET GUIDE VANE ACTUATOR COVER IMPROPERLY INSTALLED. NEEDS BOLT, PN M512180-37, MDDR 114547 REMAINS OPEN.</P><P>LP 1050742 - M3:&NBSP;&NBSP;UPON FURTHER T/S, FOUND FLOW SENSING MODULE PACK GASKET RUPTURED. PLACED P/N 3876415-4 ON ORDER WITH MCC, DMI 114547 REMAINS OPEN. </P><P>LP 1050744 - M4:&NBSP; REPLACED TOTAL PRESSURE FLOW SENSOR GASKET IAW AMM 49-53-03. APU STARTS GOOD. MDDR REMAINS OPEN FOR BOLT, ON IGV COVER</P><P>LP 1050745 - M7:&NBSP; INSTALLED IGV COVER BOLT IAW AMM 49-52-03 STEP D. THIS CLEARS MDDR 114547.&NBSP;</P><P><BR /></P><P>NOTE - OPENED MDDR 114798 - FOR APU COLD SOAK START VERIFICATION (25-AP-01)&NBSP;</P>)

Part: GCU — FAILED (LEFT) · airframe 89,004 hrs · 16,886 cycles

DURING PERIODIC BUSS POWER CONTROL UNIT TEST, RECEIVED "LEFT GEN CT LOOP GROUND DISCONNECT TRIP". REMOVED AND REPLACED L GCU. PERFORMED SATISFACTORY OPS CHECK IAW AMM 24-22-02.

Part: BOWL — DAMAGED (OIL SCAV FILTER) · airframe 89,004 hrs · 16,886 cycles

NR 1 ENGINE OIL SCAVENGE FILTER BOWL WAS DAMAGED. REMOVED, INSPECTED, AND INSTALLED THE NR 1 ENGINE OIL SCAVENGE FILTER BOWL IAW AMM 79-21-04 AND 79-21-08. NO DAMAGE NOTED. LEAK CHECK ACCOMPLISHED ON T/C T2031.

Part: ECU — NO TEST (APU) · airframe 89,004 hrs · 16,886 cycles

APU ECU FAILS OPS CHECK WITH "ECU" MINI FLAG. REMOVED AND REPLACED ECU IAW B767 AMM 49-61-05.

Part: TERMINAL — BROKEN (LT PRV) · airframe 89,004 hrs · 16,886 cycles

DURING ENGINE RUN PNEUMATIC CHECKS, LH PRV NOT OPENING. TROUBLESHOOT PER FIM 36-10 848. FOUND BROKEN TERMINAL LUG AT PIN 3 Y347. REPAIRED BROKEN TERMINAL LUG AT PIN 3 Y347 IAW SWPM 20-30-11. PERFORMED SATISFACTORY OPS CHECK IAW AMM 36-11-18.</P>)

Part: MOUNT — WORN (FWD CARGO) · airframe 89,004 hrs · 16,886 cycles

FWD CARGO L/H SIDE AIR COOLING FAN AFT MOUNT IS WORN.(<P>REMOVED AND REPLACED FWD CARGO L/H SIDE AIR COOLING FAN AFT MOUNT IAW B767 AMM 21-58-06. PERFORMED A SATISFACTORY POST FAN INSTALLATION CHECK. NO LEAKS NOTED IAW B767 AMM 21-58-06.</P>)

Part: RADAR — MALFUNCTIONED (WX SYSTEM) · airframe 88,983 hrs · 16,876 cycles

BOTH WX RADARS SHOWING ERRONEOUS RETURNS FROM 10-11:30 POSITION IN FLIGHT. T/S PER AMM 34-43-00. NO FAULTS NOTED FOR LEFT OR RIGHT SYS. OK FOR SERVICE.

Part: FAN — FAILED (EQUIP COOLING) · airframe 88,970 hrs · 16,872 cycles

FWD EQUIPMENT SUPPLY FAN 1 EICAS MSG DURING PRE-FLIGHT. REMOVED AND REPLACED FWD COOLING SUPPLY FAN IAW AMM 21-58-06. W/O 52344 C/W. OPS CHECK NORMAL.

Part: TRANSCEIVER — FAULTY (WEATHER RADAR) · airframe 88,939 hrs · 16,859 cycles

WINDSHEAR SYSTEM EICAS MESSAGE ON FINAL APPROACH WITH RIGHT RADAR SYSTEM SELECTED.(<P>IAW 34-43-01 AMM, ACCOMPLISHED WIRE CHECKS &AMP; RAN FIM IAW WDM 34-46-11 &AMP; 34-43-11 &AMP; FIM 34-46 FAULT TREE 815. NO DEFECTS NOTED. FOUND INTERNAL FAULT ON WEATHER RADAR TRANSCEIVER.&NBSP;REMOVED AND REPLACED WEATHER RADAR TRANSCEIVER. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.<BR /></P>)

Part: CIRCUIT BREAKER — TRIPPED (COCKPIT) · airframe 88,931 hrs · 16,857 cycles

RT RADAR CIRCUIT BREAKER OPENED IN FLIGHT. (<P>T/S PER AMM 34-43-00-735-007-001. NO FAULTS NOTED AT THIS TIME. (R) WEATHER RADAR SYSTEM.</P>)

Part: LATCH — UNSECURE (THRUST REVERSER) · airframe 88,927 hrs · 16,856 cycles

IN THE CLIMB, RT ENGINE VIBRATION FAN REACHED 4.8 @ 107.4&NBSP; N1 - CONSTANT POWER SETTING.(<P>T/S PER FIM 71-05 FT 852, FOUND INBD TR UPPER LATCH NOT CLASPING. RE-SECURED UPPER CLASP. PERFORMED VIBRATION SURVEY PER AMM 71-00-00/501, ALL VIBES BELOW 2.5 IPS. RH ENG MAX VIBE @ 1.2.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,931 hrs · 16,857 cycles

WINDSHEAR SYS EICAS MESSAGE APPEARED ON APPROACH AND REMAINED ON TILL ENGINE SHUT DOWN. REPEAT WRITE UP, 5TH WRITE UP.(<P>DEFERRED IAW MEL 34-43-01-07A. MDDR # 112230. CAT 'B' DUE 29 MAY 19 DISPATCH NOTIFIED S.K. 0921Z.</P><P><SPAN>LP 1050701 - M6: TROUBLESHOT IAW FIMS 34-46 FT 806, FIM 34-46-FT 814, AND FT 804, NO FAULTS NOTED. OPS CHECK GOOD AT THIS TIME. THIS CLOSES MDDR 112230. PLACARDS REMOVED AND MCC ADVISED</SPAN></P><P><SPAN>DI : SK@0315Z/28</SPAN></P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,931 hrs · 16,857 cycles

WINDSHEAR SYS EICAS MESSAGE APPEARS DURING APPROACH. (<P>PERFORMED MCDP BITE TEST IAW AMM 22-00-02. NO FAULTS NOTED CHECKED PREVIOUS FLT FAULTS - "NO LAST FLT FAULTS". PERFORMED GPWS OPS TEST IAW AMM 34-46-00. OPS CHK GOOD.</P>)

Part: COMPUTER — MALFUNCTIONED (EICAS) · airframe 88,887 hrs · 16,843 cycles

WINDSHEAR SYS EICAS MESSAGE AFTER SELECTING FLAPS 25, UNTIL RIGHT ENGINE SHUTDOWN DURING TAXI. (REPEAT WRITE UP)(<P>PERFORMED TROUBLESHOOTING, FOUND L EICAS COMPUTER INOP PER EICAS TEST 025, 523, FAIL CODES TRANSFER TO DMI 112088 PER MEL 31-41-01-02 CAT 'A' MBCB 24MAY19, MPCW C/B COLLAR. PLACARD INSTALLED. DISPATCH DF 0725.</P><P>LP 1045937 - M2: REMOVED AND REPLACED LT EICAS COMPUTER ASSY WITH NEW. REF AMM 31-41-02. OPS CHECK GOOD. NO DEFECTS NOTED. THIS CLEARS DMI # 112088. </P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,881 hrs · 16,841 cycles

WINDSHEAR SYS CAUTION MESSAGE HAPPENED DURING APPROACH PHASE. REMAINED ILLUMINATED THROUGH AIRCRAFT SHUT DOWN.(<P><SPAN>PERFORMED GPWS TEST IAW AMM 34-46-00. OPS CHECK GOOD AT THIS TIME.</SPAN><BR /></P>)

Part: RELAY — FAULTY (MAIN BATTERY) · airframe 88,826 hrs · 16,822 cycles

DURING PRE-FLIGHT, FOUND MAIN BATTERY CHARGER STATUS MESSAGE.&NBSP;&NBSP;(<P>REMOVED AND REPLACED MAIN BATTERY CHARGER IAW AMM 24-31-02. CHARGE OFF PART (P/N: 4-254-02, S/N: 0324)</P><P>LOG PAGE 1084171 ITEM M2; REMOVED AND REPLACED MAIN BATTERY IAW AMM 24-31-01. BATTERY OFF PART (S/N 0905200223249, P/N 018550-000).&NBSP;</P><P>LOG PAGE 1084172 ITEM M3: MAIN BATTERY CHARGE STS MSG. RAN FIM 24-31 FT 803. REMOVED AND REPLACED BATTERY CHARGER IAW AMM 24-31-02. (S/N 2973, P/N S282T002-6)</P><P>LOG PAGE 1084172 ITEM M4: PERFORMED FIM 24-31 FT 803. REMOVED AND REPLACED RELAY K115 IAW WDM 24-31-11.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,830 hrs · 16,823 cycles

DURING APPROACH AT 2000' AND AFTER TAXI TO THE GATE, ADVISORY MESSAGE "WINDSHEAR SYS"(<P><SPAN>T/S PER FIM 34-43 FT 805. NO FAULTS NOTED AT THIS TIME.</SPAN></P>)

Part: APU — SHUTDOWN · airframe 88,812 hrs · 16,818 cycles

APU AUTO SHUTDOWN UPON ENGINE SHUTDOWN.(<P>PERFORMED APU OPS CK IAW AMM 49-11-00. NO DEFECTS NOTED AT THIS TIME. APU PERFORMED SATISFACTORY.</P>)

Part: TERMINAL — LOOSE (L FIRE LOOP) · airframe 88,565 hrs · 16,732 cycles

L ENG FIRE LP 2 MESSAGE. PERFORMED OPERATIONAL CHECK OF FIRE DETECTION SYS INSPECTED CIRCUIT CARDS AND #2 FIRE LOOP NO DEFECTS NOTED NO MSG REMAINS IAW AMM 26-11-00. OPS CHECK GOOD. L ENG FIRE LP2. DEFERRED PER DDG 26-11-01-01. REMOVED AND REPLACED PER MCC REQUEST OF LEFT ENGINE #2 FIRE LOOP DETECTION CARD (M682) IAW AMM 26-11-02-012-001, OPS CHECK FAILED, REMAINS OPEN. PERFORMED INSPECTION OF THE FIRE LOOP 2 PER B767 AMM 26-11-00, THEN CHECKED CONNECTORS PER B767 WDM 26-11-11. FOUND LH ENGINE OUTBOARD AFT LOWER FIRE DETECTOR, DETECTOR RESPONDER TERMINALS WERE LOOSE, TIGHTENED IT. NO LOOP 2 MSG. REMAINS OPEN FOR MONITORING. T/S PER WDM 26-11-11 FOUND HIGH RES AT LOWER AFT DETECTOR LOOP 2. R/R LOWER AFT FIRE LOOP 2 PER AMM 26-11-02. OPS CHECK OK. DMI 109496 CLEARED AND PLCD REMOVED.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT FIRE LOOP) · airframe 88,577 hrs · 16,736 cycles

INTERMITTENT STATUS MESSAGE LT ENG FIRE LOOP 2(<P>PERFORMED OPERATIONAL TEST OF ENGINE FIRE DETECTION SYSTEM. OPS TEAT GOOD STATUS MESSAGE CLEARED.<BR /></P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,542 hrs · 16,724 cycles

L ENG C1 STATUS MESSAGE.(<P>OPS CHECK NORMAL. NO DEFECTS NOTED IAW FIM 71-01 FT 810 SEE LP 1024042 ITEM M11.<BR /></P>)

Part: UNKNOWN — VIBRATION (NR 1 ENGINE) · airframe 88,542 hrs · 16,724 cycles

INFO TO MX, DURING PERIODS OF HIGH THRUST LEFT ENG FAN VIB INDICATED A VALUE OF 3.4 ABD A/C HAD NOTICABLE AIRFRAME VIBRATION.(<P>ACCOMPLISHED INSPECTION OF #1 ENGINE. NO DEFECTS NOTED AT THIS TIME IAW AMM 71-00-00-935-230.<BR /></P>)

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 88,542 hrs · 16,724 cycles

STATUS MSG L ENG FIRE LP 1.(<P>PERFORMED ENGINE FIRE LOOP TEST PER AMM 26-11-00. TEST OK MSG CLEARED.<BR /></P>)

Part: FIRE LOOP — FALSE ACTIVATION (LT ENGINE) · airframe 88,510 hrs · 16,716 cycles

LEFT ENGINE FIRE LOOP 1 STATUS MSG. REPLACED LOWER AFT FIRE LP 1 PER AMM 26-11-02. CKS GOOD.

Part: CHARGER — INOPERATIVE (MAIN BATTERY) · airframe 88,449 hrs · 16,698 cycles

L, C, R IRS'S DC FAIL EICAS &AMP; LOCAL LIGHT(<P>IRU'S FAILED DUE TO LOSS OF BATTERY CHARGER. REMOVED &AMP; REPLACED MAIN SHIP BATTERY &AMP; MAIN CHARGER IAW AMM 24-31-01 &AMP; 24-31-02. OPS CHECKED NORMAL..</P><P><BR DATA-MCE-BOGUS="1" /></P><P>CHARGER OFF PART: (S/N:<SPAN>0776, P/N:&NBSP;</SPAN><SPAN>S282T002-6)</SPAN></P>)

Part: FIRE LOOP — MALFUNCTIONED (LT ENGINE) · airframe 85,995 hrs · 18,380 cycles

L ENG FIRE LP 1 STATUS MSG(<P>TRANSFERRED&NBSP;TO MDDR 108571 (RE-OPENED) DDG 26-11-01-01 CAT C DUE 03/22/16 PLACARD INSTALLED.</P><P>LP 1085938:&NBSP;PERFORMED FIRE/OVHT TEST REF DDG 26-11-61-01. NO FURTHER MESSAGES NOTED&NBSP; AND TEST PASS. MDDR 108571 REMAINS OPEN.&NBSP;</P><P>LP 1074074 - M4:&NBSP;REMOVED &AMP; REPLACED NR 1 ENG UPPER AFT FIRE LOOP IAW AMM 26-11-02. POST INSTALLATION TEST PERFORMED. OPS CHECK GOOD AT THIS TIME. THIS CLEARS DMI # 108571. MCC NOTIFIED. PLACARDS REMOVED.&NBSP;<BR /></P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,435 hrs · 16,693 cycles

MAIN BATTERY CHARGER STATUS MESSAGE.&NBSP;(<P>PERFORMED FIM TASK&NBSP;24-3583-803 BATTERY RESISTANCE CHECK GOOD AND NO ACTIVE FAULTS AT THIS TIME. MESSAGE CLEARED.</P>)

Part: CIRCUIT CARD — DEFECTIVE (FIRE WARNING) · airframe 88,430 hrs · 16,690 cycles

NR 1 ENGINE LOOP 1 INOP ER RESTRICTED 120 / ( ENGINE FIRE DETECTION SYSTEMS, DETECTION LOOPS (ER RESTRICTED 120) )(<P>PLACED ON MDDR 108571 PER MEL 26-11-01-01</P><P>LP 1015488 - M6:&NBSP;RE-SEATED LOOP 1 DETECT LEFT (M681) CARD ON P54 CARD FILE CABINET. PER AMM 26-10-01, THEN PERFORMED ENGINE FIRE TEST PER AMM 26-11-00 MSG WENT AWAY. DMI REMAINS OPEN FOR MONTERING PER MCC.</P><P>LP 1015499 - M9:&NBSP;TROUBLESHOT IAW FIM 26-11 FAULT TREE 804 AND FAILED INSULATION RESISTANCE TEST AT BLOCK 3 FROM M681 CARD FILE D2832 PIN 19 TO GND FOUND 32.12KZ AND PIN 20 TO GND FOUND 25.83 KZ WHICH IS OUT OF LIIMITS IAW TABLE 3. NEEDS FURTHER T/S MDDR 108571 REMAINS OPEN.</P><P>LP 1085916 - M4: REMOVED AND REPLACED SERVICEABLE FIRE CARD M681 IAW AMM 26-11-01. OPS CHECK GOOD AND MDDR 108571 CLOSED. PLACARDS REMOVED AND MCC NOTIFIED.&NBSP;</P>)

Part: STOWAGE BOX — DEFECTIVE (COCKPIT) · airframe 88,406 hrs · 16,682 cycles

CENTER SUPERNUMERARY SEAT 02 MASK INOP.(<DIV>NO LEAK FOUND AT CENTER SUPERNUMERARY OXYGEN MASK . CENTER MASK INOP TRANSFERRED TO MDDR 108504 IAW DDG 35-11-03-02A CAT C DUE 21MAR19. CENTER SEAT CANNOT BE OCCUPIED. LEAK TEST IAW GMM 3-25-3. MCC INIT ST 0124Z.</DIV><DIV>LP 1015493-M5: PART RECEIVED WAS BAD FROM STOCK. DMI 108504 REMAINS OPEN. NEW PART ON ORDER.&NBSP;</DIV><DIV>LP 1085913-M7: REMOVED AND REPLACED CREW O2 MASK STOWAGE BOX AT CENTER SUPERNUMERARY SEAT IAW&NBSP; AMM 35-11-51. OPS AND LEAK CHECK GOOD. THIS CLEARS MDDR 108504.</DIV>)

Part: PIMU — MALFUNCTIONED · airframe 88,386 hrs · 16,677 cycles

BOTH L &AMP; R EEC EICAS MESSAGE " R EEC MODE" " L ENGINE EEC MODE" INDICATED.(<P>TRANSFERRED TO MDDR# 108417 IAW DDG 73-21-01-03 CAT C DUE 19MAR19.</P><P>LP 1015472-M7&NBSP;REMOVED AND REPLACED L PIMU IAW AMM 77-35-02 PERFORMED ENGINE RUN&NBSP; AND PERFORMED PIMU BITE TEST IAW FIM 71-01 FT 810 OPS CHECK OK.</P>)

Part: OIL FILTER — UNSERVICEABLE (OIL SYSTEM) · airframe 88,386 hrs · 16,677 cycles

R OIL FILTER MASTER CAUTION AFTER START. MESSAGE CLEARED AFTER 90 SECONDS. STATUS MESSAGE REMAINS.(<P>R/R SCAVENGE OIL FILTER IAW AMM 79-21-04. PERFORMED ENGINE RUN IAW 71-00-00. MSG CLEARED, LEAK CHECK GOOD.</P>)

Part: CONTROLLER — MALFUNCTIONED (CARGO TEMP) · airframe 88,371 hrs · 16,672 cycles

EICAS MSG "CGO CARGO FLOOR OVHEAT" STATUS MESSAGE: CARGO TRIM AIR(<P>REMOVED &AMP; REPLACED AUX ZONE TEMP CONTROL IAW AMM 21-61-12, &AMP; 21-43-05&NBSP; OPS CKD SUCCESSFUL, DMI #107996&NBSP; CLOSED.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,366 hrs · 16,670 cycles

STATUS MSG IN FLIGHT " L ENG FIRE LP 1". LATER IN FLT MSG CLEAR ON ITS OWN.(<P>T/S PER B767 26-11 FT 805. NO FAULTS FOUND AT THIS TIME PER FIM OK.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (CARGO TEMP) · airframe 88,287 hrs · 16,646 cycles

"CARGO A/C TEMP STATUS MSG"(<P>PERFORMED BITE TEST ON TEMP CONTROLLER AUX ZONE, NO FAULT SHOWN, STATUS MSG NO LONGER SHOWING. IAW FIM 21-61-00/101.</P>)

Part: BRUSHES — WORN (STARTER) · airframe 88,198 hrs · 16,618 cycles

APU STARTER MOTOR BRUSHES ARE WORN.(<P>REMOVED AND REPLACED APU STARTER IAW AMM 49-41-01. OPS CHECK GOOD.&NBSP;</P><P><BR DATA-MCE-BOGUS="1" /></P><P ><SPAN></SPAN></P>)

Part: GENERATOR — NO TEST · airframe 88,198 hrs · 16,618 cycles

WHILE PERFORMING HMG OPS CHECK, HMG DID NOT DEVELOP A HIGH ENOUGH FREQUENCY, WORKING AT 391 CYCLES. SHOULD BE A MIN OF 395 CYCLES.&NBSP;(<P>REPLACED HMG CONTROL GENERATOR MOTOR IAW AMM 24-25-02. OPS CHECK NORMAL, 399 FREQUENCY.&NBSP;</P>)

Part: RELAY — MALFUNCTIONED (FUEL QTY) · airframe 88,198 hrs · 16,618 cycles

BACK LIGHT ON INDICATOR PANEL FOR MAIN FUEL QTY TURNS ON AND OFF INTERMITTENTLY.&NBSP;&NBSP;(<P>REMOVED AND REPLACED K2169 RELAY IAW SWPM 20-81-22 AND OPS CHECK OK IAW AMM 33-13-00.</P>)

Part: IGNITER — WORN (APU) · airframe 88,198 hrs · 16,618 cycles

APU IGNITER PLUG AND IGNITION LEAD ARE WORN.(<P>REMOVED AND REPLACED APU IGNITER PLUG IAW AMM 49-41-02 AND IGNITION LEAD IAW AMM 49-41-02. BOTH OPS CHECK NORMAL.&NBSP;</P>)

Part: INDICATOR — MALFUNCTIONED (LOW FLOW) · airframe 88,198 hrs · 16,618 cycles

E/E COOLING LOW FLOW PANEL LEVER DOES NOT SPRING BACK TO CLOSE.&NBSP;(<P>R/R E/E COOLING MONITOR INDICATOR IAW B767 AMM 21-58-34. OPS CHECK NORMAL.&NBSP;</P>)

Part: TRU — MALFUNCTIONED · airframe 88,172 hrs · 16,608 cycles

APU FAILED TO START. REMOVED AND REPLACED TRU UNIT IAW AMM 24-32-04. OPS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,078 hrs · 16,576 cycles

RIGHT OIL FILTER&NBSP; STATUS MESSAGE.(<P>CHECKED CHIP DETECTOR. FOUND ALL CLEANED, CHECK AND CLEAN OIL FILTER DIFFERENTIAL PRESSURE SWITCH CONNECTOR, MESSAGE CLEARED- REF: AMM FIM 79-35 F/T 802/803. PERFORMED NR 2 ENG RUN REF AMM 71-00-00. NO MESSAGE RETURN OPS CHECK NORMAL</P>)

Part: PIN — RECESSED (FUEL SYSTEM) · airframe 88,038 hrs · 16,564 cycles

AFTER START CAUTION " R AFT FUEL PUMP" MSG DISPLAYED(<P>APPLIED DEF'L MEL 28-22-06</P><P><BR DATA-MCE-BOGUS="1" /></P><P>TROUBLE SHOOT IAW FIM 28-22 FT 820, FOUND PIN 1 ON RIGHT AFT BOOST PUMP CONNECTOR RECESSED. RESET PIN IAW&NBSP; SWPM 20-61-00 OPS CHECK GOOD IAW AMM 28-22-00</P>)

Part: TUBE — DISCONNECTED (COMPRESS DISCHAR) · airframe 87,836 hrs · 16,495 cycles

APU DUCT PRESSURE TOO LOW FOR START(<P>TRANSFERRED TO DMI #104853 IAW DDG 49-11-01A&NBSP;<BR /></P><P>LP 1037857-M2&NBSP;PERFORMED 49-11 FT A06 AND FIM 49-11 FT 986, NO FAULTS NOTED, CHECK SURGE VALVE FILTER ELEMENT PER AMM 49-53-06, AND FOUND THE COMPRESSOR DISCHARGE TUBE DISCONNCETED, RETIGHTEN, PERFORMED OPS CHECKS.

Part: ANTI-ICE VALVE — MALFUNCTIONED (LT WING) · airframe 87,710 hrs · 16,456 cycles

LEFT WING ANTI ICE EICAS MESSAGE. REMOVED AND REPLACED LEFT THERMAL ANTI ICE VALVE IAW 30-11-02 OPS CKS.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 87,729 hrs · 16,460 cycles

WITH WING ANTI ICE EICAS MSG ATTEMPTED TO CYCLE W/SAME RESULT. PERFORMED OPS CHK OF WING ANTI-ICE VALVES IAW AMM 30-11-02. OPS CHK GOOD AT THIS TIME.

Part: WARNING SYSTEM — INTERMITTENT (COCKPIT) · airframe 87,729 hrs · 16,460 cycles

DURING DESCENT RT ENG BLEED EICAS INTERMMITTENT. PERFORMED CHECK ON EICAS MX PAGE NO MSG FOR RT ENG BLEED, NO FAULT DISPLAYED.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT WING) · airframe 87,686 hrs · 16,447 cycles

LEFT WING ANTI EICAS MSG WHEN SWITCH COMMANDED TO ON.(<P>ACCOMPLISHED SYSTEM TEST ON GROUND NO FAULTS NOTED, IAW FIM 30-11 FAULT TREE 801 &AMP; 802.</P>)

Part: TRANSCEIVER — NOT SEATED (RADAR) · airframe 87,657 hrs · 16,437 cycles

RIGHT RADAR INOP(<P>RE-RACKED R/H RCVR /TRANCEIVER OPS CHECKED NORMAL IAW AMM 34-43-00</P>)

Part: SCREEN — NOT REPORTED (THRUST REVERSER) · airframe 87,566 hrs · 16,407 cycles

NO.2 ENG O/B T/R 1 OCLOCK POSITION WIRE MESH NEEDS REPAIR.(<P>ACCOMPLISHED NO.2 ENG WIRE MESH REPAIR IAW EO NO.6778A019.</P>)

Part: IGNITER — FAULTED (APU) · airframe 87,566 hrs · 16,407 cycles

APU ECU FAULT.(<P>R/R IGNITER PLUG IAW AMM 49-41-02.</P>)

Part: LAMP — INOPERATIVE (INDICATOR LIGHT) · airframe 87,566 hrs · 16,407 cycles

REFUELING PANEL SERVICE LIGHT INOP.(<P>RELAMPED FUEL PANEL SERVICING LIGHT IAW AMM 33-31-00.</P>)

Part: DUCT — LEAKING (PNUMATIC SYSTEM) · airframe 87,566 hrs · 16,407 cycles

PNEUMATIC LEAK BY CENTER ISOLATION VALVE (LEFT WHEEL WELL).(<P>REMOVED AND REPLACED PNEUMATIC DUCT BEHIND ISOLATION VALVE OPS'S CK,LEAK CK NORMAL IAW&NBSP;</P><P>36-11-02.</P><P><BR DATA-MCE-BOGUS="1" /></P>)

Part: SKIN — DENTED (RT NACELLE) · airframe 87,566 hrs · 16,407 cycles

RIGHT ENG O/B COWL DENT.(<P>ACCOMPLISHED RIGHT ENG DENT REPAIR IAW E.O. 1971A187.</P>)

Part: CIRCUIT BREAKER — TRIPPED (WX RADAR) · airframe 87,536 hrs · 16,396 cycles

LEFT WEATHER RADAR FAILED. FOUND THE CIRCUIT BREAKER TRIPPED. RESET THE CIRCUIT BREAKER. OPS CHECKED GOOD IAW AMM 20-60-01. PERFORMED A WEAHTER RADAR CHECK OK IAW AMM 34-43-00.

Part: CIRCUIT BREAKER — TRIPPED (NR 1 IGNITOR) · airframe 87,536 hrs · 16,396 cycles

RIGHT ENGINE IGNITOR NR 1 STATUS MESSAGE. FOUND THE CIRCUIT BREAKER M1 TRIPPED FOR THE RT IGNITOR NR 1. RESET THE CIRCUIT BREAKER AND CLEARED THE MESSAGE. PERFORMED AN AUDIBLE IGNITION TEST ON THE RT ENGINE AND OPS TESTED GOOD IAW AMM 74-00-00.

Part: TRANSMITTER — MALFUNCTIONED (OIL PRESSURE) · airframe 87,510 hrs · 16,386 cycles

STATUS MESSAGE EICAS DISAGREE, R & R THE NR 2 ENG OIL PRESSURE TRANSMITTER IAW AMM 79-32-01. OPS CHECKED GOOD IAW AMM 71-00-00.

Part: VALVE — FAULTY (CABIN TEMP) · airframe 87,341 hrs · 16,324 cycles

AFT CABIN TEMP CONTROL INOP. R&R AFT CABIN TRIM VALVE IAW AMM 21-61-07. OPS CHECK GOOD AT THIS TIME.

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 87,188 hrs · 16,269 cycles

RIGHT WXR SYSTEM DISPLAYS MANUAL AND AUTO INTERMITTENTLY WHILE IN AUTO ON FO'S HSI. C/W OPERATIONAL TEST COULD NOT DUPLICATE FAULT IAW AMM 34-43-00-115-001-001.

Part: TRANSCEIVER — MALFUNCTIONED (WEATHER RADAR) · airframe 87,184 hrs · 16,268 cycles

RT WEATHER RADAR SYSTEM INOP. REMOVED AND REPLACED RT WX RADAR TRANSCEIVER IAW AMM 34-43-01. OPS CHECK GOOD.

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 87,168 hrs · 16,262 cycles

WXR RADAR DID NOT WORK WITH RIGHT SIDE TRANSMITTER SELECTED. WORKED WITH SWITCH IN LEFT POSITION. ACCOMPLISHED WX RADAR SYSTEM OPERATIONAL CHECK IAW AMM 34-43-000-715-001-001. NO FAULTS NOTED AT THIS TIME.

Part: TEST PANEL — FAULTY (COCKPIT) · airframe 87,120 hrs · 16,244 cycles

LOWER FWD CARGO FIRE BOTTLE SQUIB-1 TEST INOP. REMOVED AND REPLACED FIRE OVERHEAT TEST PNL IAW MM 26-22-03. TEST PNL OPERATES NORMAL AT THIS TIME.

Part: MODULATING VALVE — FAULTY (CABIN TEMP) · airframe 87,088 hrs · 16,231 cycles

AFT CAB TEMP EICAS MESSAGE ON TAXI IN. REMOVED AND REPLACED AFT CABIN TRIM OUR MODULATING VALVE IAW AMM 21-61-01-004-006 AND 21-61-404-041 OPS CHECKS GOOD.

Part: PACKING — DAMAGED (FUEL SYSTEM) · airframe 86,924 hrs · 16,168 cycles

FUEL IS LEAKING FROM LT WING BOOST PUMP PANEL 532AB. R&R MOTIVE FUEL SCREEN PACKING LT FWD BOOST PUMP, PERFORMED SAT LEAK CK IAW AMM 28-11-03.

Part: SHUTOFF VALVE — FAULTY (AC SYSTEM) · airframe 86,924 hrs · 16,168 cycles

FWD CARGO AIR CONDITIONING EICAS MESSAGE. R&R CARGO A/C SOV IAW AMM 21-28-01-404-92.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 86,898 hrs · 16,159 cycles

STATUS MESSAGE BLOCK: RT ICE DETECTOR, LT ICE DETECTOR. REF FIM 30-81, FT 803, MESSAGE CLEARED WITH NO OTHER FAULTS NOTED AT THIS TIME.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 86,876 hrs · 16,151 cycles

FWD CARGO A/C EICAS MSG AND COND CARGO VALVE STATUS MESSAGE DISPLAYED. TRANSFERRED TO MDDR 96902 AS PER MEL 21-28-01 CAT D.

Part: SHUTOFF VALVE — MALFUNCTIONED (AC SYSTEM) · airframe 86,807 hrs · 16,122 cycles

FWD CARGO A/C EICAS MESSAGE DISPLAYED. DEACTIVATED FWD CARGO A/C SHUTOFF VALVE PER ACTION PLAN 14302 PERFORMED WIRING CHECK.

Part: RELAY — FAULTY (AC SYSTEM) · airframe 86,795 hrs · 16,118 cycles

FWD CARGO A/C EICAS MSG DISPLAYED ON PUSHBACK. REPLACED FWD CARGO AC VALVE PER AMM 21-28-01. OPS NO GOOD. REMOVED AND REPLACED RELAY K01212 IAW SWOM 20-61-00 SHOW NO FAULTS. P/N BACR13CF2A.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 86,786 hrs · 16,111 cycles

LT BLEED DUCT LEAK CAUTION MESSAGE. RESET BLEED SYSTEM IAW AMM 21-51-00, OPS GOOD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 86,776 hrs · 16,106 cycles

ON START OF RIGHT ENG- NO SPAR VALVE "LIGHT". DISPATCH NOTIFIED.

Part: SHUTOFF VALVE — FAULTY (FUEL SYSTEM) · airframe 86,772 hrs · 16,104 cycles

ON START AT RIGHT ENG NO SPAR VALVE LIGHT. R&R SPAR FUEL SHUTOFF VALVE IAW AMM 28-21-02. OPS CHECKED GOOD.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 86,649 hrs · 16,059 cycles

COND CARGO VALVE STATUS MSG ON PARKING. PERFORMED OPERATIONAL CHECK IAW FIM 21-28- FT 811 MSG CLEAR.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 86,649 hrs · 16,059 cycles

FWD CARGO A/C EICAS MSG ON LANDING. PERFORMED OPERATIONAL CHECK IAW FIM 21-28- FT 811 MSG CLEAR.

Part: VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 86,649 hrs · 16,059 cycles

REPEAT. AFTER L ENG START "L ENG PRV" EICAS MSG DISAPPEARED AND BECAME "L ENG PRV" STATUS MSG. R&R L ENG PRV IAW AMM 36-11-18 OPS CHECKED GOOD AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 86,649 hrs · 16,059 cycles

L ENG PRV STATUS MSG. PREFORMED FIM 36-20 FAULT TREE 804 NO DEFECTS NOTED AT THIS TIME, STATUS MSG CLEARED OK FOR SERVICE.

Part: WIRE — BROKEN (HPSOV) · airframe 86,604 hrs · 16,043 cycles

'L ENG HPSOV" IN CRUISE AT FL280. FOUND WIRE BROKEN AWAY FROM TERMINAL RESECURED WIRE TO TERMINAL IAW SWPRM 20-20-00 PERFORMED FIM36-20 FT 804 NO FAULTS NOTED AT THIS TIME OPS CHECK GOOD.

Part: WIRE — BROKEN (HPSOV) · airframe 86,604 hrs · 16,043 cycles

L ENG HPSOV IN CRUISE AT FL280. LT ENG HPSOV DEFERRED. PROCEDURES C/W, FOUND WIRE BROKEN AWAY FROM TERMINAL. RESECURED WIRE TO TERMINAL IAW SWPM 20-20-00. PERFORMED FIM 36-20 FT 804 NO FAULTS NOTED AT THIS TIME. OPS CHECK GOOD.

Part: DUCT — TORN · airframe 86,570 hrs · 16,031 cycles

TWO SURGE DUCTS WERE FOUND TORN. R & R THE DUCTS IAW AMM 49-50-00, OPS AND LEAK CHECKED NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (CARGO) · airframe 86,570 hrs · 16,031 cycles

FOWARD CARGO A/C ILLUMINATED ON EICAS, DURING FINAL AT 3000 FT, RESET NORMAL. PERFORMED FIM 21-81 FAULT TREE 810 MESSAGE CLEARED, OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (A/C PACK) · airframe 86,570 hrs · 16,031 cycles

HIGH FLOW INHIBIT STATUS REMAINED AT ALL TIMES. TROUBLESHOT IAW FIM 21-51 FT 816, SEATED M0864 FLOW CONTROL CARD, HIGH FLOW INHIBIT STATUS MESSAGE CLEARED IAW AMM 20-41-01, OPS CHECKED GOOD.

Part: PUMP — MALFUNCTIONED (LT OVER RIDE) · airframe 86,570 hrs · 16,031 cycles

LEFT CENTER OVER RIDE PUMP INOPERATIVE. RESET THE LEFT CENTER OVER RIDE PUMP GFI, OPS CHECKED GOOD IAW AMM 28-22-00.

Part: ISOLATION VALVE — MALFUNCTIONED (RIGHT) · airframe 86,477 hrs · 15,999 cycles

PRIOR TO BLOCKOUT, RT BLEED ISOLANTION VALVE EICAS MESSAGE COUPLED WITH A VALVE DISAGREEMENT LIGHT ON THE RT ISOLATION SWITCH. CLEANED THE RT BLEED VALVE. EXERCIZED THE VALVE MANUALLY. OPS CHECKED NORMAL IAW AMM 36-11-04.

Part: CONTROLLER — MALFUNCTIONED (R2 WINDOW) · airframe 86,391 hrs · 15,960 cycles

R2 WINDOW HEAT INOPERATIVE. REMOVED AND REPLACED WINDOW HEAT CONTROLLER IAW AMM 30-41-01. OPS CHECKED OK.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT WINDOW) · airframe 86,385 hrs · 15,958 cycles

RIGHT SIDE WINDOW MESSAGE ON EICAS, FOLLOWED QRH PROCEDURE IN FLIGHT AND EICAS MESSAGE DID NOT CLEAR. CARRIED OUT RIGHT SIDE WINDOW ANTI ICEING BITE PROCEDURE IAW FIM 30-41, TASK 801, AND FIM 30-41-00/201, TASK 801. SYSTEM IS OK, MESSAGE CLEARED.

Part: HEAT EXCHANGER — LEAKING (NR 1 ENGINE) · airframe 86,372 hrs · 15,954 cycles

FOUND FUEL LEAKING FROM FUEL - OIL COOLER ON THE NR 1 ENGINE. REMOVED AND REPLACED THE FUEL- OIL HEAT EXCHANGER GASKET IAW AMM 79-21-01, LEAK CHECKED GOOD, FUEL - OIL HEAT EXCHANGER TESTED GOOD.

Part: CHARGER — INOPERATIVE (APU BATTERY) · airframe 86,345 hrs · 15,942 cycles

APU BATTERY DISCHARGE EICAS MESSAGE DURING APU START. REMOVED AND REPLACED THE BATTERY CHARGER IAW AMM 24-31-05.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENGINE EEC) · airframe 86,345 hrs · 15,942 cycles

LEFT ENGINE EEC EICAS MESSAGE DURING APPROACH. RAN THE LT ENGINE IAW FIM 73-21 F/T 874, NO MESSAGE. COMPLIED WITH A BITE PROCEDURES ON LP1MV. NO FAULT CODES. OPS CHECKED NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (APU) · airframe 86,341 hrs · 15,940 cycles

EICAS MESSAGE FOR THE LEFT ENGINE EEC MODE. RAN THE LEFT ENGINE, PERFORMED FIM 73-21 FAULT TREE 874, NO MESSAGE. COMPLIED WITH A BITE PROCEDURE ON THE LEFT PIMU, NO FAULTS, SYSTEM TESTED NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (APU BATTERY) · airframe 86,341 hrs · 15,940 cycles

AFTER LANDING, WHEN STARTING APU, AN EICAS MESSAGE FOR THE APU BATTERY DISCHARGED. APPLIED ELECTRICAL POWER TO ACFT IAW AMM 24-22-00 1201. NO FAULTS PRESENT, NO STATUS MESSAGE CHARGING SYSTEM TESTED NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (APU CHARGER) · airframe 86,345 hrs · 15,942 cycles

APU BATTERY DISCHARGE EICAS MESSAGE. PERFORMED AN OPS TEST OF APU BATTERY CHARGER IAW AMM 24-31-05. OPS CHECKED GOOD.

Part: CONNECTOR — FAILED (R2 WINDOW HEAT) · airframe 86,331 hrs · 15,934 cycles

R2 WINDOW HEAT INOPERATIVE. R & R CONNECTOR D1904 IAW AMM 30-41-00. OPS CHECKED NORMAL.