N1427A

Part: FIRE LOOP — WARNING MESSAGE (ZONE 200) · airframe 93,061 hrs · 21,523 cycles

MAIN DECK CARGO LOOP 2 STATUS MSG ILLUM AFTER LANDING MTX, GROUNDED A/C AND DEFERRED MAIN DECK LOOP2 FOR DEPARTURE IAW MEL ABX-26-16-2-1 .AND RETURNED A/C TO SERVICE

Part: FIRE WARNING — FALSE ACTIVATION (ZONE 100) · airframe 93,049 hrs · 21,518 cycles

AFTER OPENING MCD, MAIN CARGO FIRE (RED) MESSAGE MAIN DECK LOOP 1 MESSAGE (WHITE), AND HORN, INTERMITTENT DURING OFF LOAD. EXECUTED OPS CHECK AFTER A/C RESET OF MDC FIRE DETECTION SYSTEM IAW B767 AMM 26-14-00. OPS CHECK GOOD AT THIS TIME. A/C RELEASED NO-ETOPS. AIRCRAFT RETURNED TO SERVICE.

Part: MODULE — FAULTED (ZONE 300) · airframe 93,027 hrs · 21,509 cycles

DURING TAXI OUT, RUDDR RATIO ANNUNCIATOR LIGHT ILLUMINATED. AIRCRAFT RETURNED TO BLOCKS (BTB). MAINTENANCE RESET RUDDER RATIO CHANGER MODULE IAW B767 FIM 27-21 FAULT TREE 804. NO FURTHER DEFECTS NOTED AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.

Part: SOLENOID — FAULTED (ZONE 700) · airframe 93,023 hrs · 21,508 cycles

DURING T/O, LANDING GEAR LEVER WOULD NOT MOVE PAST OFF POSITION WHILE RETRACTING GEAR PUSHED LOCK OVERRIDE SWITCH TO RAISE GEAR FOUND CIRCUIT BREAKER PULLED AND TIED.AFTER A/C LANDED MTX GROUNDED A/C . MTX DEFERRED LANDING GEAR LATCH SOLENOID IAW MEL 32-31-1 MX PROCEDURES COMPLIED WITH MBCB 12-23-25. RETURNED A/C TO SERVICE .

Part: APU — FAULTED (ZONE 100) · airframe 92,611 hrs · 21,358 cycles

ON PUSHBACK APU SHUTDOWN, ACFT RETURNED TO THE GATE (BTB) AND MTX GROUNDED ACFT . MTX PERFORMED APU START, 1ST ATTEMPT APU START CHECKS GOOD IAW AMM 49-11-00. ACFT REMAINS NO ETOPS. AND RETURNED AC TO SERVICE.

Part: MODULE — DEFECTIVE (ZONE 100) · airframe 92,467 hrs · 21,300 cycles

DURING TAXI OUT, STAB TRIM EICAS MSG APPEARED , AC RETURNED TO GATE (BTB) AND MTX GROUNDED AC . MTX DEFERRED STAB TRIM FOR DEPARTURE IAW MEL ABX-27-41-2 MTX RETURNED AC TO SERVICE AND AC DEPARTED. REMOVED AND REPLACED STAB TRIM MODULE IAW AMM 27-09-00. DI 65934 CLEARED. AIRCRAFT REUTRNED TO SERVICE.

Part: WARNING MESSAGE — ACTIVATED (STAB TRIM) · airframe 92,397 hrs · 21,275 cycles

DURING TAXI, STAB TRIM MESSAGE BEFORE TAKE-OFF. AIRCRAFT RETURNED TO BLOCKS (BTB). DEFERRED IAW MEL 27-41-2. MTX PROCEDURES CW. PLACARD INSTALLED. SEE LP 39094-01/2 FOR RALM DOWNGRADE. AIRCRAFT RETURNED TO SERVICE.

Part: PRESSURE SWITCH — FAILED (ZONE 700) · airframe 92,388 hrs · 21,270 cycles

AFTER PUSHBACK, STAB TRIM EICAS MSG APPEARED. AIRCRAFT RETURNED TO BLOCKS. (BTB). MAINTENANCE REMOVED AND REPLACED RH STCM BRAKE PRESS SWITCH IAW AMM 27-41-07 OPS AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: DOOR — TORN (ZONE 800) · airframe 92,040 hrs · 21,139 cycles

WHILE TAXING INTO THE GATE, GROUND FOUND THE LH PACK BAY DOOR RIPPED OFF THE A/C. AIRCRAFT IS CURRENTLY IN WORK AT CVG. STILL UNDER INVESTIGATION. AN AMENDED SDR REPORT WILL BE FILED ONCE COMPLETED. AMENDED: REMOVED AND REPLACED LH PACK BAY DOOR REF SRM 51-40-02. WORK COMPLETED IN ABX WO# 14758493, NR 135.

Part: BLEED VALVE — WARNING MESSAGE (APU) · airframe 92,004 hrs · 21,125 cycles

ON TAXI OUT, APU BLEED VALVE EICAS MSG ILLUMINATED. AIRCRAFT RETURNED TO BLOCKS (BTB). MAINTENANCE DEFERRED APU IAW MEL ABX-49-11-1A. PLACARD INSTALLED. MX PROCEDURES C/W. NO ETOPS. AIRCRAFT RETURNED TO SERVICE.

Part: PSU — FAULTED (ZONE 100) · airframe 91,582 hrs · 20,967 cycles

DURING TAXI THE WARN ELEX STATUS MSGAPPEARED AND WON'T CLEAR, A/C RETURNED TO THE GATE AND MTX GROUNDED A/C AFETER TROUBLE SHOOTING WARN FLEX MSG IAW B767 FIM 31-51 FT 806 FOUND WARN FLEX PSU B FAULTING REMOVED AND REPLACED WARN FLEX PSU B IAW B767 AMM 31-51-04 WEU CARD MODULE TEST GOOD.AND RETURNED A/C TO SERVICE.

Part: START VALVE — FAULTED (RT ENGINE) · airframe 91,223 hrs · 20,820 cycles

DURING TAXI OUT RH ENGINE START VALVE WOULD NOT OPEN FOR ENGINE START . AC RETURNED TO GATE (BTB)AND MTX GROUNDED AC AND DEFERRED THE START VALVE FOR DEPARTURE IAW MEL ABX-80-00-2-1 . RETURNED AC TO SERVICE AND AC DEPARTED .

Part: TARGET — MISSING (ZONE 600) · airframe 90,977 hrs · 20,724 cycles

AC DURING APPROACH DURING LANDING CHECKLIST EICAS "MSG LE SLAT ASYM " CREW CALLED FOR A GO-AROUND AND MISSED APPROACH, AFTER GO AROUND RECEIVED " STICK SHAKER " ADJUSTED SPEED AND FLAP SETTING FOR LANDING . CAPTAIN DECLARED EMERGENCY AND LANDED . MTX GROUNDED ACRAFT AND BEGAN TROUBLE SHOOTING INBOUND DISCREPANCY "LE SLAT ASYM" MTX FOUND #10 SLAT PROX SENSOR TARGET HARDWARE AND TRACK MISSING , INSTALLED NEW BEARING AND HARDWARE. IAW B 767 AMM 27-81-02-434-115 AND PERFORMED OPS CHECKS IAW B767 AMM 27-81-00-862 NO FAULTS OR MESSAGE AT THIS TIME . MTX REURNED AC TO SERVICE .

Part: PCB — FAULTED (ZONE 100) · airframe 90,919 hrs · 20,703 cycles

AT GATE: MAIN CARGO DECK FIRE INDICATED FOR 10 SECONDS. EICAS, DISCRETE LIGHTS, AURAL WARNING , CREW PERFORMED QRH AND PULLED EVERYONE FROM AC AND CALLED ARFF THEY CLEARED FOR REENTRY AND WAS SUSPECTED FALSE WARNING .AFTER LOADING RESUMED A SECOND FULL FIRE WARNING OCCURED =. AC WAS GROUNDED AT THIS POINT FOR EVAUATION MTX . REMOVED PRINTED CIRCUIT CARD M10427 (P/N:285N0028-136, S/N:D19762) AND INSTALLED AT POSITION M2026,IAW AMM 26-10-01. PREVIOUS FIRE/OUHT LOGIC TEST CARD M2026 (P/N:285N0028-136, S/N:D19502) WAS REMOVED. INSTALLED CIRCUIT CARD M10247 (P/N:285N0028-21, S/N:D02850) REF AMM 26-10-01. C/W AFOLTS CARD INSTALLATION TEST REF AMM 26-10-01. NO FAULTS NOTED. THEN CHEKED GROUND INTEGRITY AT MODULES TEST/ALARM INTERFACE MODULES M12276, M12277, M12278,M12279, M12284, & M12285 PINS 1,RD 26 RESPECTIVELY NO ISSUES NOTED. THEN GRND AT CONNECTOR D7990 PIN 5U (A7 P54 PANL) & CONNECTOR D 10106 PIN FAULTS OBSERVED. THEN C/W MC COMPLY SMOKE DET SYS TEST REF AMM 76-14-00, WITH SMOKE DET 1C2B (D31452) & 2C2B (D31424) DISCONNECTED GREEN LIGHTS ON A M12277 & M12279 RESPECTIVELY, TIGHTENED CONNECTORS, D31520 & D31424, NEW INDICATIONS WORKING PROPERLY. UNABLE TO DUPLICATE ON GROUND, SYSTEM OVERIDING OK. REF 56M 26-16-03. DEFERRED MDE COMPT SMOKE DET SYS PER MEL 26-16-2. PLACARD INSTALLED MB2B 10-22-24. A/C REMAINS NO ETOPS.RETURENED AC TO SERVICE

Part: PCB — FAILED (ZONE 100) · airframe 90,919 hrs · 20,703 cycles

AT GATE: MAIN CARGO DECK FIRE INDICATED FOR 10 SECONDS. EICAS, DISCRETE LIGHTS, AURAL WARNING , CREW PERFORMED QRH AND PULLED EVERYONE FROM AC AND CALLED ARFF THEY CLEARED FOR REENTRY AND WAS SUSPECTED FALSE WARNING .AFTER LOADING RESUMED A SECOND FULL FIRE WARNING OCCURED =. AC WAS GROUNDED AT THIS POINT FOR EVAUATION MTX . REMOVED PRINTED CIRCUIT CARD M10427 (P/N:285N0028-136, S/N:D19762) AND INSTALLED AT POSITION M2026,IAW AMM 26-10-01. PREVIOUS FIRE/OUHT LOGIC TEST CARD M2026 (P/N:285N0028-136, S/N:D19502) WAS REMOVED. INSTALLED CIRCUIT CARD M10247 (P/N:285N0028-21, S/N:D02850) REF AMM 26-10-01. C/W AFOLTS CARD INSTALLATION TEST REF AMM 26-10-01. NO FAULTS NOTED. THEN CHEKED GROUND INTEGRITY AT MODULES TEST/ALARM INTERFACE MODULES M12276, M12277, M12278,M12279, M12284, & M12285 PINS 1,RD 26 RESPECTIVELY NO ISSUES NOTED. THEN GRND AT CONNECTOR D7990 PIN 5U (A7 P54 PANL) & CONNECTOR D 10106 PIN FAULTS OBSERVED. THEN C/W MC COMPLY SMOKE DET SYS TEST REF AMM 76-14-00, WITH SMOKE DET 1C2B (D31452) & 2C2B (D31424) DISCONNECTED GREEN LIGHTS ON A M12277 & M12279 RESPECTIVELY, TIGHTENED CONNECTORS, D31520 & D31424, NEW INDICATIONS WORKING PROPERLY. UNABLE TO DUPLICATE ON GROUND, SYSTEM OVERIDING OK. REF 56M 26-16-03. DEFERRED MDE COMPT SMOKE DET SYS PER MEL 26-16-2. PLACARD INSTALLED MB2B 10-22-24. A/C REMAINS NO ETOPS.RETURNED AC TO SERVICE .

Part: IRU — FAULTED (RIGHT) · airframe 90,857 hrs · 20,678 cycles

DURING TAXI OUT EICAS MESSAGE R IRS FAULT AND DESCRETE CAME ON AC RETURNED TO THE GATE AND MTX GROUNDED AC .MTX DEFERRED THE R IRU IAW MEL ABX-34-21-1-1-2A. AND RETURNED AC TO SERVICE AND AC DEPARTED .

Part: PIN — OUT OF POSITION (ZONE 300) · airframe 90,830 hrs · 20,668 cycles

STAB TRIM EICAS MESSAGE AND DESCRETE LIGHT AFTER ENGINE START WHILE TAXI OUT ,AC RETURNED TO GATE AND MTX GROUNDED AC. MTX FOUND PINS 2&3 SWAPPED ON PRESSURE SWITCH 527. CONNECTED PINS. REF BOEING SWM 20-61. STAB TRIM FUNCTIONS & INDICATIONS CORRECT REF B7676 AMM 27-41-00 AIRCRAFT RALM "CAT I" PENDING MCDP 30/40 TESTS. MTX RETURNED AC TO SERVICE

Part: WARNING MESSAGE — FALSE INDICATION (STAB TRIM) · airframe 90,501 hrs · 20,551 cycles

DURING TAXI STAB TRIM EICAS MESSAGE APPEARED IN ONT. A/C RETURNED TO THE GATE AND MTX GROUNDED A/C, AND DEFERRED STAB TRIM MEASEAGE IAW MEL ABX-27-41-2. AND RETURNED AC TO SERVICE AND A/C DEPARTED . MTX PERFORMED STAB TRIM OPS CHECK IAW B767 AMM 27-41-00 OPS CHECK NORMAL AT THIS TIME THIS CLEAR D.I 53889 PLACARD REMOVED MX PROCEDURES C/W A/C REMAINS CAT III A REF LP 39015-03/1 RETURNED A/C TO SERVICE .

Part: DRIVE ASSY — MALFUNCTIONED (WX RADAR SYSTEM) · airframe 90,417 hrs · 20,519 cycles

ON TAXI OUT, WX RADAR FAIL AND STAB LIGHTS AND WXR SYS STATUS MESSAGE, RETURNED TO BLOCKS. AND MTX GROUNDED A/C L/H SYSTEM TEST OK R/H SYS TEST OK. OPERATED WXR L/H SYS FAILED, R/H SYS INTERMITTENT. REMOVED CONTROL PWL CONNECTOR. NO DEFECTS NOTED. REINSTALLED PNL IAW AMM 34-43-02. REPLACED DRIVE UNIT OPS CHECK OF L+R SYSTEMS NORMAL IAW AMM 34-43-00. A/C REMAINS NO ETOPS AND MTX RETURNED A/C TO SERVICE

Part: MODULE — MALFUNCTIONED (PROX SWITCH) · airframe 90,415 hrs · 20,518 cycles

AFTER TAKEOFF  AT V1 THE FIRE BELL SOUNDED WITH NO OTHER INDICATION INDICATING A FIRE WAS UNABLE TO SILENCE THE BELL. A/C PRFORMED ATR AND RETURNED TO THE GATE WHERE MTX GROUNDED A/C .  PERF AFOLTS TEST PER AMM 26-10-00.  NO DEFECTS NOTED.  PERF BACU BITE CK 24-22-00.  NO DEFECTS NOTED.  PERF PSEU BITE CK PER FIM 32-09 FT803.  MULTIPLE PROX FAILURES, INCLUDING INTERNAL CARD FAILURE (D12 CARD). REMOVED AND REPLACED PSEU PER AMM 32-09-044, OPS CK GOOD.  ALL FAULTS CLEARED.  DURING INSPECTION OF M1000 BELL/CHIME MODULE FOUND SHORTED/DAMAGED COMPONENTS.  REMOVED AND REPLACED BELL CHIME MODULE PER AMM 31-31-04.  OPS CK GOOD.  PERFORMED LANDING/TO CONFIG, LEFT/RIGHT SIREN MODULE AND MASTER CAUTION AND WARNING MODULE.  OPS CHECKS PER AMM 31-31-04.  NO DEFECTS NOTED.  A/C REMAINS NO ETOPS.

Part: WARNING MESSAGE — FALSE ACTIVATION (STAB TRIM) · airframe 90,286 hrs · 20,468 cycles

REJECTED T/O IN MIA, LOW SPEED, DUE TO T/O CONFIG WARNING FOR STAB TRIM. STAB TRIM WAS SET PROPERLY AND SUBSEQUENT T/O WAS SUCCESSFUL.(<P>NOTED BY MX AS PRECAUTIONARY. PERFORMED TAKE OFF CONFIGURATION WARNING TEST PER AMM 31-51-00. OPS CHECK GOOD.</P>)

Part: SERVO — FAULTED (ELEVATOR SYS) · airframe 90,261 hrs · 20,456 cycles

AIRCRAFT DID NOT ACCELERATE THROUGH 10000 FT IN VNAV (ATB)(<P>PERFORMED MCDP TEST 30 &AMP; 40, FAULTING NO INFC. FCC C ELEV SRVO CMD REF AMM 22-00-02. REF LOGPAGE 1742397 ITEMS M7 &AMP; M8 FOR CTR AUTOPILOT ELEVATOR SERVO REPLACEMENT. REMOVED AND REPLACED FCC CENTER ELEVATOR SERVO IAW AMM 22-12-01, OPS CHECK GOOD. PERF MCDP TEST 30/40 IAW AMM 22-10-00, NO FAULTS NOTED. VERIFIED PART EFFECTIVE IAW AIPC 22-12-01-01.</P>)

Part: OXYGEN MASK — FAULTED (CAPTAIN'S) · airframe 89,951 hrs · 20,353 cycles

AT DEPARTURE CREW NOTIFIED FO'S MIC STUCK ON.(<P>R/R FO'S O2 MASK IAW AMM 35-11-51. OPS CHECK GOOD, LEAK CHECK GOOD.</P>)

Part: PCA — LEAKING (LT ELEVATOR) · airframe 89,811 hrs · 20,293 cycles

LH ELEVATOR, OUTBOARD PCA WITH HYDRAULIC LEAK.(<P>LH ELEVATOR OUTBOARD PCA WAS REPLACED PER AMM 27-31-05-424-027 REV. 140 AUG 22, 2023. OPS CHK GOOD.</P>)

Part: SERVO — LEAKING (AUTOPILOT SERVO) · airframe 89,811 hrs · 20,293 cycles

CENTER ELEVATOR AUTO PILOT SERVO (M272) WITH HYDRAULIC LEAK.(<P>CENTER ELEVATOR AUTOPILOT SERVO WAS REPLACED PER AMM 22-12-01-424-019, REV 140 AUG 22, 2023.</P>)

Part: PCA — LEAKING (RT ELEVATOR) · airframe 89,811 hrs · 20,293 cycles

RH ELEVATOR, OUTBOARD PCA WITH HYDRAULIC LEAK(<P>RH ELEVATOR OUTBOARD PCA, WAS REPLACED PER AMM 27-31-05-024-001, 20-11-00-910-802. OPS CHK GOOD.&NBSP;</P>)

Part: FEEL UNIT — LEAKING (ELEVATOR) · airframe 89,811 hrs · 20,293 cycles

ELEVATOR FEEL UNIT (M1139) WITH HYDRAULIC LEAK.(<P>ELEVATOR FEEL UNIT WAS REPLACED PER AMM 27-31-17-424-021, REV 140 AUG 22, 2023. OPS CHK GOOD.</P>)

Part: SWITCH — NO TEST (MICROPHONE) · airframe 89,811 hrs · 20,293 cycles

TRIGGER LH/RH POSITION DON'T PUSH PTT SWITCH ON MIKE MODE AND FAIL TEST IAW EO 6723A218.(<P>TRIGGER LH/RH POSITION WERE REWORKED PUSH PTT SWITCH ON MIKE MODE PER SRM 51-10-02 PAR 6 REV 48. NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 89,811 hrs · 20,293 cycles

RH WING INB AFT FLAP UPPER SKIN OUTBOARD INTERNAL DOUBLER WITH CORROSION(<P>PART WAS REPAIRED PER CMA-TLS 24-0110-04C. NO FURTHER DEFECTS NOTED.</P>)

Part: SUPPORT — BROKEN (BS 544 RBL 33.1) · airframe 89,833 hrs · 20,303 cycles

FWD CARGO, STA 544 BTW 33.15 RBL CEILING BEAM SUPPORT BROKEN(<P>PART WAS REPAIRED PER BOEING REF CMA -TLS 24-0118-03B. NO FURTHER DEFECTS NOTED.</P>)

Part: SERVO — LEAKING (RUDDER YAW) · airframe 89,811 hrs · 20,293 cycles

RUDDER - YAW DAMPER SERVO ASSY LH AND RH WITH LEAK(<P>&NBSP;LH AND RH RUDDER WERE REPLACED PER AMM 27-21-00. OPS CHK GOOD.&NBSP;</P>)

Part: ACTUATOR — LEAKING (THRUST REVERSER) · airframe 89,811 hrs · 20,293 cycles

ENG 2, LH T/REVERSER HYD ACTUATOR WITH LEAK EVIDENCE.(<P>ENG 2, LH T/REVERSER HYD ACTUATOR WAS REPLACED PER AMM 78-31-06-404-006-H00 REV 140, AUG 22-2023</P>)

Part: PCA — LEAKING (RT ELEVATOR) · airframe 89,811 hrs · 20,293 cycles

RH ELEVATOR, MIDDLE PCA WITH HYDRAULIC LEAK(<P>MIDDLE PCA WAS REPLACED PER AMM 27-31-05-424-027, REV 140, AUG 22, 2023. OPS CHK GOOD.</P>)

Part: RELAY — UNKNOWN · airframe 88,210 hrs · 19,748 cycles

AFT CARGO DOOR EICAS MSG IMMEDIATELY AFTER TAKEOFF (APPROX 100' AGL)REMAINED ON AT LEAST THRU 5000' ON DESCENDING, FOR RETURN TO PDX(<P>INSPECTED AND FOUND CARGO DOOR INDICATION INTERMITTENT. TRANSFER TO MDDR 184404, CAT C DUE 04MAY23. MX ACTIONS COMPLIED WITH. PLACARDS INSTALLED. DISPATCH JT 0153Z IAW MEL 52-71-01-01. LOG PG 1749659 REMOVED AND REPLACED GROUND HANDLING RELAY PER B767 SWPM 20-81. OPS CHECKS GOOD PER AMM 52-35-00-912. NO FURTHER DEFECTS FOUND. THIS CLEARS DMI 184404&NBSP;</P>)

Part: NONE — NONE · airframe 86,965 hrs

FOUND LEFT AND RIAGHT OVERHEAD EMERGENCY LIGHTS IN COCKPIT INOP.(<P><SPAN>RELAMPED LIGHTS , OPS CHECKS NORMAL IAW AMM 33-51-11.</SPAN></P>)

Part: HYDRAULIC LINE — LEAKING · airframe 86,471 hrs · 19,217 cycles

AREA AFT OF PRESS BULK HEAD TO BS 1725.5, ELEVATOR FEEL COMPUTER, EVIDENCE OF LEAK ON LOWER HYD TUBES. (BTW STA 1702.2 AND 1725.5, LH SIDE).(THE ELEVATOR FEEL COMPUTER WAS INSTALLED CORRECTLY AS PER AMM 27-31-19-424-015, REV 136</P>)

Part: LOCKOUT — LEAKING · airframe 86,471 hrs · 19,217 cycles

DURING THE DEVELOPMENT OF THE TASK CARD HYDRAULIC POWER LEAK CHECK, RH WING, WAS FOUND LEAK EVIDENCE AT THE O/B AILERON LOCKOUT MECHANISM. LEAK TEST WAS PERFORMED ON O/B RH AILERON LOCKOUT MECHANISM AND NO LEAKS FOUND. TEST PERFORMED IAW 29-11-00-796-053, REV 135</P>)

Part: FUEL TANK — LEAKING · airframe 86,471 hrs · 19,217 cycles

WING CENTER TANK, RH SIDE, FROM L-11 TO L-1C AND BBL 97.42, FUEL LEAK ON JOINS (AUXILIAR CENTER TANK, RH SIDE, ROOT OF FUEL LEAK AT RBBL 97.42 AND STGR L-6 WAS REPAIRED IAW AMM 28-11-00</P>)

Part: PCA — LEAKING · airframe 86,471 hrs · 19,217 cycles

DURING THE DEVELOPMENT OF THE TASK CARD HYDRAULIC POWER LEAK CHECK, RH WING, WAS FOUND WITH INTERNAL LEAK EVIDENCE AT THE O/B AILERON PCA(LEAK TEST WAS PERFORMED ON RH OUTBOARD AILERON PCA´S, NO LEAKS WERE FOUN. TEST PEFORMED IAW AMM 29-11-00-796-053, REV 135 /

Part: ECS — INOPERATIVE · airframe 86,471 hrs · 19,217 cycles

DURING RUN TEST, ONE INDICATION OF AIR TEMPERATURE OF ECS IN EICAS, IS MISSING. PACK OUTLET TEMPERATURE BULB AND COMPRESOR OUTLET SENSOR WAS INSTALLED AS PER AMM 21-51-06-404-011 AND AMM 21-52-06-404-010, REV 136</P>)

Part: ACOUSTIC PANEL — DAMAGED · airframe 86,471 hrs · 19,217 cycles

LH INLET COWL INNER BARREL ACOUSTIC PANEL (LATERAL AND LOWER SEGMENT)(ENGINE # INLET COWL, INNER BARREL, AND ACOUSTIC PANELS WERE REPAIRED IAW SRM 54-15-01, REPAIR 3 &AMP; TRE6754160</P>)

Part: SPOILER — LEAKING · airframe 86,471 hrs · 19,217 cycles

DURING DEVELOPMENT OF TASK CARD HYDRAULIC POWER LEAK CHECK, RH WING, WAS FOUND LEAK EVIDENCE AT THE SPOILER NO. 9. LEAK TEST WAS PERFORMED ON THE RH WINGS, SPOILER ACTUATOR #9 AND NO EVIDENCE OF LEAKS FOUND. TEST REFERENCE AMM 29-11-00-786-053 REV 135</P>)

Part: ACOUSTIC PANEL — DAMAGED · airframe 86,471 hrs · 19,217 cycles

LH INLET COWL INNER BARREL ACOUSTIC PANEL (LATERAL AND LOWER SEGMENT)(ENGINE # INLET COWL, INNER BARREL, AND ACOUSTIC PANELS WERE REPAIRED IAW SRM 54-15-01, REPAIR 3 & TRE6754160</P>)

Part: BEARING — COKED · airframe 86,471 hrs · 19,217 cycles

ENG 2, CORE SECTION BEARING NO.6 PRESSURE AND RETURN PIPES WITH OIL LEAK EVIDENCE (OIL COKE BUILD UP WAS REMOVED AND THE NUTS WERE RE-TORQUED PER AMM 72-50-00-216-032 AND 72-53-04-434-020, REV. 135</P>)

Part: LCCA — LEAKING · airframe 86,471 hrs · 19,217 cycles

LEFT WING, WELL WHEEL ZONE LEFT TOP LCCA WITH LEAK EVIDENCE. LEAK TEST WAS PERFORMED ON LEFT TOP LCCA AND NO LEAK FOUND. REF. AMM 29-11-00-796-053, REV. 135</P>)

Part: ACTUATOR — LEAKING · airframe 86,471 hrs · 19,217 cycles

RH WING, INBOARD FLAP, OUTBOARD ACTUATOR, LEAK EVIDENCE(<P>LEAK TEST WAS PERFORMED ON RH INBOARD FLAP AND NO LEAKS FOUND. TEST PERFORMED IAW AMM 29-11-00-796-053 REV 125</P>)

Part: ACTUATOR — LEAKING · airframe 86,471 hrs · 19,217 cycles

RH WING, INBOARD AILERON, ACTUATORS, LEAK EVIDENCE (LEAK CHECK HAS BEEN PERFORMED ON THE RH INBOARD AILERON ACTUATORS AND NO LEAKS WERE FOUND. TEST PERFORMED IN ACCORDANCE WITH AMM 29-11-00-796-053, REV 135</P>)

Part: LCCA — LEAKING · airframe 86,471 hrs · 19,217 cycles

LEFT WING, WELL WHEEL ZONE LEFT BOTTOM LCCA WITH LEAK EVIDENCE. LEAK TEST WAS PERFORMED ON THE LH BOTTOM LCCA, NO LEAKS FOUND. REF. 29-11-00-796-053</P>)

Part: ACCESS PANEL — CONTAMINATED · airframe 86,471 hrs · 19,217 cycles

LEFT WING, IN ACCESS PANELS 551TB AND 551UB WITH EWIS CONTAMINATED OF HYDRAULIC(EWIS WAS CLEANED PER SWPM 20-10-04, REV 80</P>)

Part: TAB — MISSING · airframe 85,873 hrs · 19,020 cycles

CA O2 MASK LEFT DOOR RETENTION TAB BROKEN AND MISSING.(<P>REMOVED AND REPLACED BOX ASSY, EQIP IAW AMM 35-11-51. OPS GOOD, LEAK CHECK GOOD.</P>)

Part: NONE — NONE · airframe 84,906 hrs · 18,734 cycles

UPON TURNING ON FUEL PUMPS NOTED RT AFT PRESS AND RT AFT FUEL PUMP EICAS MESSAGE AND ASSOCIATED CIRCUIT BREAKER POPPED.(<P>PLACED ITEM ON DMI 156581 IAW MEL 28-22-01 MX ACTION C/W CB PULLED CAT C DUE DATE 21NOV21.</P> / <P>&NBSP;</P> / <P>REMOVED AND REPLACED RIGHT WING AFT FUEL BOOST PUMP IAW AMM 28-22-03. OPS CHECK AND LEAK CHECK GOOD. THIS CLEARS MDDR 156581. PLACARDS REMOVED.&NBSP;</P>)

Part: SWITCH — NONE

LH AFT FUEL PUMP OVERHEAD SWITH INOP / ( FUEL PUMP LOW PRESS LIGHTS, -200/-300 )(<P>TRANSFERRED TO MDDR 156172 PER DDG 28-42-01-01 CAT C DUE 13NOV21. C/W MAINTENANCE ACTION. PLACARD INSTALLED.</P> / <P>LOG PAGE 1373312: REMOVED AND REPLACED (L) AFT MAIN PUMP LIGHTED PUSH BUTTON SWITCH ASSY IAW AMM 33-13-00. PERFORMED MAIN TANK FUEL BOOST PUMP OPS CHECK PER AMM 28-22-00. OPS CHECK GOOD. THIS CLEARS MDDR# 156172.</P>)

Part: NONE — NONE

ATB RH BLEED OFF MSG DISPLAYED DURING CLIMB OUT. RH PACK OFF LIGHT ON.(<P>FOUND PRSOV TO PRECOOLER PNUEMATIC DUCT SLEEVE MISALIGNED, REPLACED DUCT PER AMM 36-11-01. REMOVED/REPLACED PRSOV PER AMM 36-11-09. REMOVED AND REPLACED FAN AIR TEMP SENSOR PER AMM 36-11-17. ENG RUN / LEAK CK PER 71-00-00 OK.</P>)

Part: VALVE — NONE

"R ENG BLD OVHT" ON DEPARTURE. PERFORMED QRH 2.27 &AMP; MESSAGE EXTINGUISHED.(<P>BITE CK'D AIR SUPPLY BITE MODULE PER FIM TASK 36-10. INDICATED RT FAN AIR VALVE INOP. REMOVED AND REPLACED RT ENG FAN AIR VALVE PER AMM 36-11-16</P>)

Part: CARD — NONE · 18,713 cycles

ON CLIMB OUT AT AROUND 7000' THEN AGAIN THROUGH 17,000' EICAS MESSAGE R ENG BLEED OFF DISPLAYED. ACCOMPLISHED ASSOCIATED NON-NORMAL.(<P>PERFORMED AIR SUPPLY BITE CHECK IAW FIM 36-20 FT 804. NO FAULTS. SYS TEST OK. ACCOMPLISHED LEAK CHECK &AMP; GVI OF BLEED SYS IAW AMM 36-11-00. NO LEAKS OR DEFECTS NOTED PER F/C 36-90-87-42, FOLLOWED FIM 36-10 FT 836. CHECKED CONTINUITY ON PR60V IN OPEN POSITION, FROM PIN 1 TO PIN 2, PER BLOCK 2 OF FIM. PRSOV CHECK OK. NEXT STEP REMOVED AND REPLACED BLEED AIR CONTROL CARD (M860) IAW AMM 36-11-12. RAN ENGINE IAW AMM 72-00-00.CYCLED L &AMP; R PACKS ENG BLEED ON/OFF. NO EICAS MSGS NOTED. BLEED PRESSURE REMAINED STABLE. OPS CHECK GOOD. REF LP 1425157 ITEM 01 FOR REPLACEMENT OF BLEED AIR CONTROL CARD (M860) IAW AMM 36-11-12.</P>)

Part: NONE — NONE

APU FAULT DURING START ATTEMPT AFTER LANDING(<P>APU STARTED 1ST ATTEMPT BY MX PER AMM 49-41-00/001. APU CHECKS OK.</P>)

Part: PANEL — NONE · airframe 84,683 hrs

CABIN ALT AUTO 1 EICAS MESSAGE DISPLAYED(<P>TRANSFERRED TO MDDR 154556 IAW MEL 21-31-01A, CAT 'A'.</P> / <P>04OCT21 - LP 1441429 - ITEM# 4 - ONT - REMOVED AND REPLACED CABIN PRESSURE SELECTOR IAW AMM 21-31-01. OPS CHECK GOOD. PERF CABIN PRESSURE CONTROLLER BITE IAW FIM 21-31 FT 803. NO FAULTS NOTED. THIS CLEARS DMI 154556. PLACARD REMOVED. MCC NOTIFIED.</P>)

Part: CHARGER — FAULTED · 18,655 cycles

APU FAULT UPON ARRIVAL.(<P>PERFORMED APU BITE IAW FIM 49-11 FT 987. FOUND APU BATTERY CHARGER AT FAULT. R/R APU BATTERY CHARGER IAW AMM 24-31-05. OPS CHECK GOOD.&NBSP;</P>)

Part: GASKET — DAMAGED

APU REQ MEL PER ATLAS ENGINEERING DUE TO START FAULT.(<P>TRANSFERED TO MDDR 153687 PER DDG 49-11-01A CAT C DUE 27SEP21.</P> / <P>18SEP21 - LP 1440869 - ITEM 3 - SCK - C/W ECM# 2021P-337 STEPS 1-3 NO FAULTS FOUND AT THIS POINT ECM# 2021P-337 STEPS 4-7 REMAIN OPEN. DMI# 153687 REMAINS OPEN.</P> / <P>18SEP21 - LP 1440869 - ITEM 4 - SCK - PERFORMED AMM 49-21-00 APU EXTERNAL INSPECTION FOUND FLOW SENSING MODULE GASKET DAMAGE. PARTS ON ORDER MCC NOTIFIED. GASKET P/N 3876244-1 FLOW SENSING MODULE P/N 3885081-1 DMI# 153687 REMAINS OPEN.</P> / <P>19SEP21 - LP 1440872 - ITEM 3 - ONT - R/R SENSING MODULE IAW B767AMM 49-53-08. STARTED APU MULTIPLE TIMES IAW B767AMM 49-11-00. NO DEFECTS NOTED AT THIS TIME. THIS WILL CLOSE MDDR 153687 MCC NOTIFED. PLACARD REMOVED R/R GASKET P/N 3876415-4.</P> / <P>&NBSP;</P>)

Part: ECU — FAULTY

APU FAULT 2 TIMES ON LANDING.(<P>PERFORMED APU BITE PROCEDURE REF AMM 49-61-05. FOUND MINIFLAG #34. RESET APU ECU AND STARTED APU ON FIRST ATTEMPT. APU OPS CHECK NORMAL AT THIS TIME.</P>)

Part: IGNITION LEAD — FAULTY

"APU FAULT" EICAS ON FIRST START AFTER LANDING. 2ND ATTEMPT OK.(<P>TRANSFERRED TO MDDR #153504 IAW MEL 49-11-01A CAT "C" DUE 24SEP21.</P> / <P>15SEP21 - LP 1397862 ITEM 4 - ONT - R/R APU EXCITER IAW AMM 49-41-03. OPS CHECK APU PER AMM 49-00-00. OPS CHECKS GOOD. NO FAULTS IN VIEW. R/R IGNITER PLUG PER AMM 49-41-02 P/N30576E-1. R/R IGNITER LEAD PER AMM 49-41-04. OPS CHECKS GOOD. THIS CLEARS DMI 133507. PLACARD REMOVED.</P>)

Part: INDICATOR — NO INDICATION (RT START VALVE) · airframe 84,534 hrs · 18,613 cycles

R START VALVE LIGHT INOP DURING ENG START(<P><SPAN>PERFORMED DRY MOTOR RUN OF RH ENG TWICE IAW AMM 71-00-00. OPS CHECK GOOD., RH START VALVE LIGHT OPS CHECK GOOD.

Part: FAULT MESSAGE — FALSE ACTIVATION (APU)

APU FAULT EICAS MSG 1ST START ON GROUND @ TPA. STARTED 2ND ATTEMPT. RECURRANCE OF PREVIOUS LEGS.(<P>TRANSFERRED TO MDDR 153154 PER DDG 49-11-01A. CAT C. DUE 17SEP21 ZH 1707.</P> / <P>REF LOGPAGE 1386720 ITEM 4 RFD: C/W BITE AND OPS CK IAW 49-00-00. OPS CKS GOOD, NO FAULTS .THIS CLEARS MDDR 153154, PLAC REMOVED. MCC NOTIFIED.</P>)

Part: INDICATOR — FAULTED (ENGINE)

COULD NOT PUT STANDBY ENG INDICATOR INTO TEST MODE(<P>REMOVED AND REPLACED STANDBY ENGINE INDICATOR ASSY IAW AMM 77-41-01. OPS CHECK GOOD AND BITE CHECK GOOD.

Part: RADAR — MALFUNCTIONED (WX SYS)

WEATHER RADAR DOESN'T PAINT WEATHER MULTIPLE THUNDERSTORM SYSEMS ACROSS THE US AFTER APPEARED ONSCREEN(<P>PERFORMED OPS TEST WXR LT &AMP; RT IAW AMM 34-43-00. OPS TEST GOOD AT THIS TIME.</P>)

Part: CONTROL VALVE — FAULTED (RT PACK TEMP)

R PACK TEMP EICAS MOMENTARILY DISPLAYED DURING DESCENT(<P>REMOVED AND REPLACED RH PACK TEMP CONTROL VALVE IAW AMM 21-61-12. OPS CHECK GOOD, LEAK CHECK GOOD.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (APU)

APU FAULT EICAS AFTER LANDING DURING FIRST APU START ATTEMPT(<P>PERFORMED BIT CHECK IAW FIM 49-11 FAULT TREE 987. OPS CHECK IAW AMM 49-11-00, OPS CHECK GOOD.</P>)

Part: UNKNOWN — VIBRATION (RT ENGINE)

INFO ONLY, ON INITIAL CLIMB OUT RUGHT ENGINE VIB INDICATION CYCLED FROM FAN-LPT-N2 REPEATEDLY. NO LIMITATIONS EXCEEDED(<P><SPAN>NOTED BY MX. PER B767 AMM 77-31-00/701 DESCRIPTION AND OPERATION OF AIRBORNE VIBRATION MONITORING SYSTEM, SYSTEM OPERATION IS NORMAL.&NBSP;</SPAN></P>)

Part: IGNITION UNIT — INOPERATIVE (APU) · 18,510 cycles

APU FAULT ON ARRIVAL(<P>PERF APU BITE PER AMM 49-61-05, IGN UNIT LRU FAULT SHOWN, FOLLOWED FIM 49-11 FT 819. REMOVED AND REPLACED IGNITION UNIT IAW AMM 49-41-03, PERFORMED MULITIPLE APU START UPS. ALL ATTEMPTS SUCCESSFUL, NO FURTHER DEFECTS NOTED</P>)

Part: MODULE — FAULTED (AIR SUPPLY) · 18,472 cycles

R ENG BLEED VALVE WOULD NOT OPEN, EVEN AT 75% N2(<P>REMOVED AND REPLACED ENG PRESSURE REGULATING VALVE IAW AMM 36-11-18. S/N OFF - NSN P/N OFF-792755-15 - VALVE.</P> / <P>14JUL21 - 1390662 - ITEM# 5 - CVG - REMOVED AND REPLACED AIR SUPPLY BITE MODULE IAW AMM 36-21-01. NO FAULTS PRESENT AT THIS TIME.</P>)

Part: VALVE — INOPERATIVE (APU)

APU BLEED NOT SUPPLYING DUCT PRESSURE AND BLEED VALVE NOT INDICATING OPEN.FOUND GROUNDED SHIELD AT ECU, REPAIRED WIRING. REMOVED AND REPLACED APU BLEED AIR VALVE IAW AMM 36-11-00. OPS CK GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (APU) · airframe 83,990 hrs · 18,455 cycles

APU BLEED VALVE EICAS ON BLOCK IN.(<P>CYCLED APU BLEED VALVE PER AMM 36-11-10. OPS CHECK GOOD AT THIS TIME.</P>)

Part: VALVE — FAILED (APU PNEUMATIC) · airframe 83,986 hrs

APU PNEUMATICS INOP(<P>TRANSFERRED TO MDDR 149618 IAW MEL 49-11-01-01, CAT C.</P> / <P>LP 1361901 - ON A/C ARRIVAL WE ACTIVATED PNEUMATICS ON APU, WE HAD 30 PSI OF DUCT PRESSURE WITH PACKS OFF, WITH BOTH PACKS RUNNING WE HAVE 20-25 PSI OF DUCT PRESSURE, RAN&NBSP; APU PNEUMATICS WITH HIGH DEMAND FOR APPROX 4HRS AND NEVER LOST PNEUMATICS. WE COULD NOT DUPLICATE FAULT ON GROUND, SUSPECT FAULT ONLY OCCURS AT LANDING WHEN MOISTURE IS PRESENT ON APU LINES AND VLV. DMI REMAINS OPEN&NBSP; FOR CONTINUED T/S.</P> / <P>LP 1363575 - REMOVED AND REPLACED APU BLEED SHUTOFF VLV IAW 36-11-00. OPS CKS NORMAL AT THIS TIME. THIS CLEARS MDDR 149618.</P>)

Part: MODULE — FAULTED (FLOW SENSING) · airframe 83,959 hrs · 18,445 cycles

APU BLEED INOP ( AUXILIARY POWER UNIT, PNEUMATIC FUNCTION )(<P>TRANSFERRED TO MDDR 149488, DUE 10JUL21, CAT C, IAW ATLAS DDG 49-11-01-01. MX ACTION COMPLIED WITH.</P> / <P><SPAN>LP 1363567: REPLACED FLOW SENSING MODULE. PERFORMED ENGINE RUN. OPS CHECK GOOD IAW AMM 49-53-08. THIS CLOSES MDDR# 149488. PLACARD REMOVED.</SPAN></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT A/C PACK) · airframe 83,920 hrs · 18,431 cycles

R PACK TEMP ADVISORY MESSAGE IN DESCENT PROX 10000 FT. CAME ON TWICE- EXTINGUISHING BOTH TIMES(<P>PACK RESET &AMP; BIT CHECK IAW FIM TASK 21-51- TF 844, OPS CHECK GOOD &AMP; BITE CHECK GOOD, NO ACTIVE MESSAGES</P>)

Part: SENSOR — FAULTED (APU) · airframe 83,785 hrs · 18,389 cycles

APU INOP(<P>TRANSFERRED TO MDDR # 148142 IAW MEL 49-11-01A CAT C DUE 16 JUN 21</P><P>CVG- 07 JUN- LP 1122138- ITEM 4-&NBSP;FOUND MINI FLAG 14, PT SENSOR ON BITE, CLEARED ECU, PERF OPS CHECK IAW AMM 49-11-00, OPS CK GOOD, NO FURTHER DEFECTS NOTED, CLEARED DMI 148142, PLACARD REMOVED. CLEARED FOR ETOPS.</P>)

Part: GENERATOR — INOPERATIVE (APU) · airframe 83,622 hrs · 18,339 cycles

APU GENERATOR NOT SUPPLYING POWER.(<P>REMOVED AND REPLACED APU GENERATOR IAW AMM 24-21-01, OPS CHECK GOOD. PER FIM 24-20 TASK 805. REMOVED AND REPLACED APU GCU IAW AMM 24-22-02 OPS CHECK GOOD. (GCU P/N OFF 734284F S/N OFF 2232)</P>)

Part: GENERATOR — INOPERATIVE (APU) · airframe 83,666 hrs · 18,353 cycles

APU GENERATOR INOP WONT PICKUP POWER WHEN APU SELECTED.(<P>PERFORMED APU SYSTEM CK, APU GEN CHK GOOD. ACCOMPLISHED APU GEN OPS TEST IAW B767 AMM 24-21-00. NO DEFECTS NOTED, OPS TEST GOOD.</P>)

Part: OXYGEN MASK — INOPERATIVE (CAPTAIN'S) · airframe 83,622 hrs · 18,339 cycles

CAPT'S 02 MASK WILL NOT INFLATE, NOR FLOW ANY OXYGEN TO THE MASK. IT IS COMPLETELY DEAD. SWAPPED O2 STOWAGE MASK BOXES FROM FIRST OBSERVER'S TO CAPT'S. DEFERRED FIRST OBSERVER'S SEAT.(<P>REMOVED AND REPLACED CAPT'S O2 MASK PER AMM 35-11-51. NO HELP, REPLACED OLD CAPT O2 MASK PER AMM 35-11-51. SWAPPED CAPT O2 STOWAGE BOX WITH OBSERVERS #1 O2 STOWAGE BOX PER AMM 35-11-51. OPS CHECK NORMAL, LEAK CHECK GOOD.&NBSP;</P><P>DEFERRED FIRST OBSERVER'S SEAT DUE TO O2 STOWAGE BOX INOP PER MEL 25-11-02-01A, DMI&NBSP;<SPAN>147274,</SPAN><SPAN>&NBSP;CAT A. DUE DATE: 22MAY. DISP: BA @ 20:46Z.</SPAN></P><P>RIV MX, 21MAY, LP 1485750, ITEM M7: REMOVED CAPT 02 STOWAGE BOX AND INSTALLED INTO ORIGINAL POS AT FRST OBS, IAW AMM 35-11-51. OPS CHECK NORMAL, LEAK CHECK GOOD, INSTALLED NEW O2 STOWAGE BOX IN CAPT POSITION, OPS NORMAL, LEAK CHECK GOOD IAW AMM 35-11-51. THIS CLEARS MDDR 147274, PLACARD REMOVED. DIS- GTC 1842Z</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 83,582 hrs · 18,328 cycles

STATUS MSG CABIN ALT AUTO 1(<P>PERF CABIN PRESS CONT BITE IAW FIM 21-31 FT 803. MESSAGE CLEARED. NO FAULTS NOTED AT THIS TIME.</P>)

Part: OIL SYSTEM — OVERSERVICED (APU) · airframe 83,523 hrs · 18,310 cycles

APU SHUTDOWN PRIOR TO DISCONNECTING GPU(<P>TRANSFERRED TO MDDR 146280 IAW MEL&NBSP;49-11-01A, CAT C.</P><P>LP 1481047: PERFORMED FIM 49-11 FAULT TREE 987 APU BITE. FOUND NO CURRENT FAULTS. INSPECTED APU AND FOUND OIL TO BE OVERSERVICED. TOOK EXCESS OIL OUT AND SERVICED TO PROPER LEVELS. PERFORMED APU RUN IAW AMM 49-11-01. APU OPS CHECKS NORMAL. THIS CLEARS DMI 146280.&NBSP;</P>)

Part: CLAMP — UNSECURE (APU BLEED) · airframe 83,353 hrs · 18,255 cycles

APU BLEED FAIL TRANSFERRED TO MEL 49-11-01-01 CAT C, FOUND DUCT CLAMP BETWEEN CATALYTIC OZONE CONVERTER AND LT FLOW CONTROL AND SHUTOFF VALVE LEAKING. REMOVED, REPOSITIONED, AND TORQUED CLAMP TO 55 INCH POUNDS IAW AMM 21-51-01. LEAK CHECK GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (VALVES) · airframe 83,333 hrs · 18,247 cycles

AFTER EXT START OF NBR 2 A CROSSBLEED START WAS ATTEMPTED BOTH APU VALVE AND RT ENG VALVE EXTINGUISHED UNTIL LEFT ENG WENT TO START THEN BOTH VALVES CLOSED AND HAD ZERO PRESSURE(<P>TRANSFER TO DMI 145350 PER MEL 80-00-02-01 CAT "C".</P><P>17APR21 - LP 1444115 - ITEM M11 - AFW - PERFORMED ENGINE STARTING OPERATIONAL TEST IAW AMM 80-11-00 OPS CHECK GOOD. THIS CLEARS MDDR# 145350.</P>)

Part: MODULE — MALFUNCTIONED (FLOW SENSING) · airframe 83,319 hrs · 18,242 cycles

NO AIR FROM APU.(<P>TRANSFER TO DMI 145336 PER MEL 48-11-01-01, CAT C.</P><P>19APR, CVG MX, LP 1444125, ITEM M6: REMOVED AND REPLACED FLOW SENSING MODULE IAW AMM 49-53-08, OPS CK GOOD. DMI 145336 CLEARED. PLACARDS REMOVED. ST 1821Z.

Part: FIRE LOOP — FAILED (LT ENGINE) · airframe 83,241 hrs · 18,218 cycles

L ENG FIRE LOOP 2 EICAS MESSAGE. REMOVED AND REPLACED L ENG FIRE LOOP 2 IAW AMM 26-11-02. OPS CHECK GOOD, NO MSG'S NOTED. THIS CLEARS MDDR 144793. PLACARD REMOVED.

Part: OXYGEN MASK — MISSING (PORTABLE O2) · airframe 83,241 hrs · 18,218 cycles

LAV PORTABLE OXYGEN MASK MISSING MASK P/N 289-601212 POUCH P/N 80189-01.(<P>INSTALLED LAV PORTABLE OXYGEN MASK &AMP; POUCH AS REQUIRED PER AMM 35-31-01. CK'D OK&NBSP;&NBSP;</P>)

Part: BOTTLE — LOW PRESSURE (CREW OXYGEN) · airframe 83,241 hrs · 18,218 cycles

FWD E/E CREW OXYGEN NEED SERVICE TO FULL.(<P>SERVICED CREW OXYGEN CYLINDER AT LOWER E/E COMPARTMENT AS PER B767-300 AMM 12-15-08-603-001, AMM 35-00-00-012-006, AMM 35-11-00-206-228, AMM 35-11-00-206-233. ADVISORY CIRCULAR: AC&NBSP; 43.13- 1B&NBSP;</P><P>PAR 9-46 THRUGH 9-51. PGS 9-448 THRUGH 9-455. LEAK CHECK GOOD.</P><P>PN&NBSP;801307-00</P><P>SN&NBSP;ST276</P>)

Part: BATTERY — NO TEST (APU) · airframe 83,241 hrs · 18,218 cycles

APU BATTERY HEALTH CHECK FAIL.(<P>REMOVED AND REPLACED APU BATTERY PER AMM 24-31-04-404-005. BATTERY CHECK GOOD .</P>)

Part: CYLINDER — DAMAGED (PORTABLE O2) · airframe 83,241 hrs · 18,218 cycles

COCKPIT SUPERNUMERARY PORTABLE OXYGEN CYLINDER TRANFER TUBE DAMAGE. P/N 9800 201A-BF23A&NBSP; S/N ST58846.(<P>REMOVED AND REPLACED SUPERNUMERARY PORTABLE OXYGEN CYLINDER AS REQUIRED PER AMM 35-31-01. LEAK AND OPS CHK OK.</P>)

Part: SEAL — BROKEN (CONTAINMENT BAG) · airframe 83,241 hrs · 18,218 cycles

COCKPIT AVSAX CONTAINMENT BAG VACUUM SEAL IS BROKEN P/N AS-002-1(<P>REMOVED AND REPLACED COCKPIT AVSAX CONTAINMENT BAG AS REQUIRED PER AMM 25-64-00. OPS CHK&NBSP; OK.</P>)

Part: BATTERY — NOT REPORTED (FLASHLIGHT) · airframe 83,241 hrs · 18,218 cycles

COCKPIT FLASH LIGHT BATTERIES DUE FOR O/H 2EA P/N P4-01-0021.(<P>REMOVED AND REPLACED FLASHLIGHTS BATTERIES AS REQUIRED PER AMM 25-64-00. OPS CHK OK 2EA.</P>)

Part: SUPPORT BRACKET — MISSING (ELT) · airframe 83,241 hrs · 18,218 cycles

COCKPIT ELT NEXT TO LAV ANTENNA SUPPORT BRACKET MISSING P/N 1151321-1(<P>REMOVED AND REPLACED COCKPIT ELT PER AMM 25-63-03. OPS CHK OK.</P><P>HEX CODE&NBSP; ADCC068EA44.</P>)

Part: BOLT — UNSAFETIED (IDG) · airframe 83,241 hrs · 18,218 cycles

#2 ENG IDG QUAD-RING BOLT NOT SAFETIED PROPERLY.(<P>INSTALLED SAFETY WIRE PROPERLY ON ENG #2 IDG QUAD-RING BOLT IAW AMM 20-10-23.</P>)

Part: BLADE — DENTED (NR 2 ENG FAN) · airframe 83,241 hrs · 18,218 cycles

#2 ENG HAS ONE FAN BLADE WITH A DENT ON THE LEADING EDGE.(<P STYLE="MARGIN: 0IN; MARGIN-BOTTOM: .0001PT;">CLEANED DENTED&NBSP;AREA&NBSP;OF # 2 ENG FAN BLADE FOUND&NBSP;WITHIN LIMITS AT LEADING EDGE&NBSP;PER B767-300&NBSP;AMM 72-31-02-226-012-H00. PERFORMED&NBSP;NDT SPOT FLOURESCENT&NBSP;PENETRANT INSPECTION. NO&NBSP;CRACK INDICATION&NBSP;NOTED&NBSP;REF AMM 70-11-06</P>)

Part: SEAL — LEAKING (PRVC) · airframe 83,241 hrs · 18,218 cycles

#2 ENG PRVC LOCATIONS E AND K FOUND TO HAVE LEAKS(<P>REMOVED AND REPLACED SEALS AT BOTH LOCATION "E AND K". ACCOMPLISHED RECHECK FOR LEAKS PER TALLY ENG PNEU LEAK CHECK. NO LEAK NOTED AMM 36-11-19.</P>)

Part: VALVE — FAULTED (ECS) · airframe 83,239 hrs · 18,217 cycles

AFTER STARTING THE SECOND ENG GOT FWD EQUIP VALVE EICAS, VALVE LIGHT STAYED ILLUMINATED, RETURNED TO PARKING.(<P>TRANSFERRED TO MDDR# 144449, MEL 21-58-08-01-01. PLACARD INSTALLED AND MCC NOTIFIED. CAT C.</P><P>CVG, 28MAR, LP 1334570, ITEM M3: REMOVED AND REPLACED EQUIPMENT INBOARD SUPPLY VALVE IAW AMM 21-58-07 (OFF PART: PN&NBSP;398774-6, SN&NBSP;3273). OPS CHECK GOOD, DMI 14449 CLEARED, PLACARD REMOVED. NO FURTHER DEFECT NOTED BY MCC NOTIFIED. DISP RS @ 1508Z</P><P>LP&NBSP;1491892: FWD EQ VALVE EICAS. DMI 144449 RE-OPENED.</P><P>LP 1491897: REMOVED AND REPLACED THE EQUIPMENT COOLING INDICATION CARD IAW B767 AMM 21-58-24. OPS TEST GOOD. PERFORMED ENGINE RUN IAW AMM 72-00-00. DMI REMAINS OPEN. P/N 285T0095-8 S/N D00137.<BR DATA-MCE-BOGUS="1" /></P><P>LP 1491899: T/S PER FIM 21-58 TASK 805. FOUND EQUIP COOLING 3 WAY SHUTOFF VALVE TO BE STICKING AND MAKING GRINDING NOISES. REMOVED AND REPLACED 3 WAY VALE IAW AMM 21-58-01. PERFORMED FWD EQ COOLING OPS CHECK IAW AMM 21-58-00. NO FAULTS NOTED. THIS CLEARS MDDR 14449.<BR DATA-MCE-BOGUS="1" /></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 83,239 hrs · 18,217 cycles

FWD EQUIP VALVE EICAS MESSAGE AFTER TOUCHDOWN, WENT AWAY AFTER ENGINE SHUTDOWN(<P>PERFORMED FIM TASK 21-58 FAULT TREE 985 AND RAN BOTH ENGINES IAW AMM 71-00-00. OPS CHECKS GOOD. NO FURTHER DEFECTS FOUND AT THIS TIME.</P>)

Part: STATUS MESSAGE — FALSE INDICATION (EQUIP SUPLY FAN) · airframe 83,214 hrs · 18,210 cycles

FWD EQPT SUP FAN 1 STATUS MSG.(<P>RESET EQUIPMENT FOR 1 BREAKER. OPS TEST SYSTEM PER AMM 21-58-06. OPS NORMAL.</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 83,153 hrs · 18,193 cycles

STATUS MSG CABIN ALT AUTO 1(<P>TRANSFERRED TO MDDR # 144050 PER MEL 21-31-01A, CAT C.</P><P>LOG 1186992 ITEM #4: C/W FIM 21-31 F/T 809. CABIN ALT AUTO 1 BITE TEST IS OK PER BLOCK 2. REF AMM 21-31-00-705-001. THIS CLEARS DMI 144050, PLACARD REMOVED.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (WX RADAR SYSTEM) · airframe 83,123 hrs · 18,180 cycles

STATUS MESSAGE (WXR SYS).(<P>PER FIM 34-43 TASK 801. WXR SYS ERASED, NO FURTHER REQ'D. OPS TEST OF WXR SYS IAW B767 AMM 34-43-00, &AMP; WXR CONFIG TESTED, NO FAULTS NOTED.</P>)

Part: CHECK VALVE — STUCK (LT A/C PACK) · airframe 83,133 hrs · 18,185 cycles

L PACK TEMP. CLEARED AFTER QRH, LEFT IN N POSITION PER PROCEDURE. PERFORMED PACK TEMPATURE CONTROLLER BITE TEST IAW AMM 21-51-14. BITE TEST GOOD. PERFORMED OPS CHECK OF COOLING PACK IAW AMM 21-51-00, OPS CHECK GOOD NO DEFECTS NOTED AT THIS TIME. DUE TO HISTORY TRANSFER TO MDDR 143784 IAW MEL 21-51-03-01 CATC. REMOVED AND REPLACED LT PACK FLOW CONTROL AND S/O VALVE IAW AMM 21-51-01. DURING OPS CHECK FOUND TRIM AIR CHECK VALVE STUCK OPEN. INSPECTED AND CLEANED CHECK VALVE. OPS CHECK NORMAL IAW AMM 21-61-05. LT PACK OPS CHECK NORMAL IAW AMM 21-51-00.

Part: MODULE — MALFUNCTIONED (FLOW SENSING) · airframe 83,090 hrs · 18,173 cycles

APU PNEUMATICS INOP ( AUXILIARY POWER UNIT, PNEUMATIC FUNCTION )(<P>TRANSFERRED TO MDDR 143579 IAW MEL 49-11-01-01, CAT C.</P><P>LP 1312385: REPLACED FLOW SENSING MODULE IAW 49-53-08. OPS CHECK GOOD. THIS CLOSES MDDR #143579. PLACARD REMOVED. TI: YK 1815Z.<BR /></P>)

Part: A/C PACK — MALFUNCTIONED (LEFT) · airframe 83,090 hrs · 18,173 cycles

LEFT PACK INOP AND LEFT PACK TEMP EICAS MSG(<P>PERFORMED PACK RESET AND BITE CHECK IAW FIM 21-51-803. NO FAULTS NOTED. OPS CHECK GOOD.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT A/C PACK) · airframe 83,027 hrs · 18,156 cycles

L PACK TEMP EICAS. QRH COMPLETE, FAULT REMAINS. RAN FAULT TREE FIM 21-51 TREE 844. NO FAULTS FOUND. OPS CKS GOOD.

Part: CONTROL VALVE — MALFUNCTIONED (ACM TEMP) · airframe 83,027 hrs · 18,156 cycles

LEFT PACK INOP IN AUTO ( PACK TEMPERATURE CONTROL SYSTEMS (-200/-300) , AUTO MODE )(<P>TRANSFER TO DMI 143251 IAW MEL 21-51-03-01, CAT C, DUE DATE 13MAR21. </P><P>ACCOMPLISHED ACTION PLAN 19320 PER MCS 8001 REV 0. REMOVED AND REPLACED ACM TEMP CONTROL VALVE PER ACTION PLAN. PACK OPS NORMAL AT THIS TIME. THIS CLEARS MDDR 143251. MCC NOTIFIED. PLAC REMOVED.</P>)

Part: ACTUATOR — FAILED (LT A/C INLET DR) · airframe 83,031 hrs · 18,157 cycles

L PACK TEMP EICAS MSG REMOVED AND REPLACED;LH PACK INLET DOOR ACTUATOR IAW B767 AMM 21-53-03. OPS CHECK/ BITE TEST GOOD IAW 767 AMM 32-09-02. REMOVED AND REPLACED LH PACK LOW LIMIT VALVE IAW AMM 21-51-11 PN: 3289696-1 SN: 3182. OPS AND LEAK CHECKS GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT PACK TEMP) · airframe 82,971 hrs · 18,140 cycles

LEFT PACK TEMP EICAS IN THE DESCENT, QRH COULD NOT CLEAR IT(PERFORMED TS IAW FIM 21-51 FAULT TREE 847. NO FAULT NOTED. C/W PACK BITE W/ MIX MAN SENSOR LIGHT. TRANSFER TO DMI 142739 PER MEL 21-51-03-01, CAT C, DUE 03MAR21. REQ FURTHER TS WITH TECH SUPPORT. DATE 22FEB21- LP 1491841 ITEM 3 - CVG - PERFORMED SYSTEM TEST PER BOEING 767 FIM 21-51 FAULT TREE 844. SYSTEM OPERATIONAL TEST GOOD. NO DEFECTS NOTED AT THIS TIME. THIS ACTION CLEARS DMI 142739. PLACARD REMOVED. MCC NOTIFIED.)

Part: WARNING MESSAGE — FALSE ACTIVATION (A/C PACK) · airframe 82,982 hrs · 18,143 cycles

AFTER LANDING "FWD EQPT VAL" ON EICAS, RUN QRH MESSAGE DID NOT CLEAR. PERFORMED FIM 21-58 FT 985. COULD NOT DUPLICATE THE FAULT AT THIS TIME. OPS TEST GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT A/C PACK) · airframe 82,920 hrs · 18,124 cycles

DURING DESCENT (15000) EICAS "L PACK TEMP" CAME ON FOLLOWED QRH. TURNED OFF PACK. PERFORMED OPS CHECK OF LT PACK TEMP. NO DEFECTS NOTED IAW AMM 21-61-00. LT PACK TEMP CONTROLLER HAD LT MIX MANIFOLD TEMP SENSOR LIGHT TOOK 3 TIMES TO CLEAR FAULT. RAN PACK, NO FAULTS AT THIS TIME.

Part: SENSOR — FALSE INDICATION (LT A/C PACK TEMP) · airframe 82,920 hrs · 18,124 cycles

EICAS LEFT PACK TEMP(<P>PERF FIM 21-51 FT 877, VERIFIED FLOW CONT VALVE OPERATE NORMAL. NO SIGN OF ANY UNUSUAL DEFECTS ON ECS MAINT PAGE. C/W LPACK BITE IAW FIM 21-51 FT 844. FOUND NO PREVIOUS OR CURRENT FAULT PER FIM 21-51 FT 877 SUSPECT TEMP SENSOR 515198 ON ORDER WITH MCC P/N 624014-2. REMOVED AND REPLACED L PACK TEMP SENSOR TS198 IAW AMM 21-51-08. SYSTEM OPERATING NORMAL, NO FAULTS IN VIEW.<BR /></P>)

Part: SENSOR — FALSE INDICATION (LT A/C PACK) · airframe 82,896 hrs · 18,117 cycles

EICAS LEFT PACK TEMP(<P>TRANSFERRED TO MDDR 142348 IAW MEL 21-51-03-01, CAT C.</P><P>13FEB21 / LP 1017445 / ITEM# 3 / ONT - PER FIM TASK 21-51 FT803 REMOVED AND REPLACED MIX MANIFOLD TEMPERATURE SENSOR IAW AMM 21-61-03. RE-PERFORMED FIM TASK 21-51 FT. 803. NO DEFECTS NOTED, FAULT CLEARED. THIS CLEARS DMI# 142348, PLACARDS REMOVED, MCC NOTIFIED.</P>)

Part: IDG — FAILED (RIGHT) · airframe 82,890 hrs · 18,115 cycles

ITEM 1: RIGHT GEN OFF. ITEM 2: R GEN DRIVE(<P>REMOVED AND REPLACED RT ENG IDG ASSY PER AMM 24-11-01. OPERATIONAL CHK POWER PLANT TEST REF AMM 71-00-00. LEAK AND OPERATIONAL CHK GOOD. ENG C/W.</P>)

Part: OXYGEN MASK — NOT REPORTED (CAIBN) · airframe 82,890 hrs · 18,115 cycles

O2 MASKS IN SUPERNUMRARY SEATS #2#3#4 INOP. MOVED #3 O2 MASK TO F/O P/N MC10-25-104&NBSP; S/N B126S41 F/O OLD MASK MOVED TO # 3 POS P/N MC10-08-109 S/N 121011(<P>ITEM TRANSFERRED TO MDDR 142132 PER MEL 25-25-03 DUE DATE 08JUN21. </P><P>REF LP1017426 ITEM 1: REMOVED AND REPLACED SUPERNUMERARY O2 MASK P/N MC10-08-109 S/N 121011 IAW AMM 35-11-51. OPS CK ALL SUPERNUMERARY O2 MASKS IAW AMM 35-11-00. ALL OPS NORMAL. THIS CLEARS DMI # 142132. PLACARD REMOVED, MCC NOTIFIED.</P>)

Part: GCU — DISCONNECTED (RIGHT) · airframe 82,856 hrs · 18,104 cycles

R GEN DRIVE EICAS MESSAGE. RAN QRH &AMP; DISCONNECTED DRIVE SWITCH.(<P>THIS BECOMES DMI 141960, CAT B, MEL 24-00-01-01. DUE 08FEB21. PLACARD INSTALLED. MCC NOTIFIED. ETOPS 180 RESTRICTED. </P><P>LOG 1017409 ITEM #8: REMOVED AND REPLACED R GCU IAW AMM 24-22-02, OPS CHECK OF IDG REQ, REF LP 1017409 ITEM #9 FOR CORRECTIVE ACTION. </P><P>ITEM #9: ENG RUN COMPLIED WITH #2 ENG GCU- GCU OPERATES NORMAL AT THIS TIME IAW 767 M/M 24-11-00. THIS CLEARS DMI 141960.</P>)

Part: RELAY — FAULTY (EQUIP VAL EICAS) · airframe 82,849 hrs · 18,102 cycles

UPON LANDING WE GOT FWD EQUIPMENT VALVE EICAS MSG, RAN QRH, SELECTED EQUIP COOLING TO STANBY, AFTER 30 SEC LIGHT DID NOT GO OUT. UPON ENGINE SHUTDOWN, LIGHT WENT OUT. PERFORMED FIM TASK 21-58 FT 986, R & R AIR GROUND RELAY, K200 PER SWPM 20-81. PERFORMED OPS CHECK IAW AMM 21-58-00. OPS CHECK GOOD, NO DEFECTS NOTED.

Part: A/C PACK — FAULT MESSAGE (CABIN) · airframe 82,844 hrs · 18,101 cycles

ON APPROACH WITH LT PACK TURNED OFF, LT PACK TEMP CAUTION. TEMP GOT QUITE WARM, COMPLIED WITH QRH ON GROUND. PACK DID NOT RESET. PERFORMED PACK RESET AND CHECK. OPS CHECK GOOD IAW AMM 21-00-00-662.

Part: EXHAUST FAN — FAULT MESSAGE (EQUIPMENT BAY) · airframe 82,839 hrs · 18,100 cycles

AFT EQ EXH FAN 2 STATUS MESSAGE. PUT EQUIPMENT COOLING TO STAND BY AND ERASED MSG IAW 21-26 FT 806. MSG CLEARED. PLACED SELECTOR BACK INTO AUTO. OPS NORMAL. NO FURTHER DEFECTS NOTED.

Part: CONTROLLER — FAULTY (COCKPIT) · airframe 82,839 hrs · 18,100 cycles

FD TEMP REMAINED AT 33C THROUGHOUT FLT EVEN WITH FD TEMP CONTROLLER AT THE FULL COLD POS 7 O'CLOCK(<P>PERFORMED RH PACK OPERATION OF PC OK AS PER AMM 21-51/501.<BR /></P>)

Part: EICAS — FALSE INDICATION (FWD EQUIP BAY) · airframe 82,834 hrs · 18,098 cycles

FORWARD EQUIP VAL EICAS MSG AFTER LANDING. PERFORMED SYS AND OPS TEST ON EQUIP COOLING VALVE IAH AMM 21-58-00. OPS CKS GOOD SYS OPERATES NORMAL.

Part: CONTROL CARD — INTERMITTENT (PACK TEMP EICAS) · airframe 82,828 hrs · 18,095 cycles

LEFT PACK TEMP EICAS MESSAGE @ 4000 FEET. DEFERRED PER MEL 21-51-01-01, MDDR 141737, CAT C, DUE 10FEB21. MAINTENANCE ACTIONS C/W. PACK FLOW CONTROL SHUTOFF VALVE CLOSED. DP @ 18:43.1209080 - M1: OPS CHECKED PACK IAW 21-51-00, FLOW CONTROL VALVE OPERATED NORMAL. NO FAULTS ON LT PACK BITE IAW FIM 21-51 FT844, SUSPECTED INTERMITTENT PACK CONTROL CARD. R & R LEFT PC CARD IAW WDM 21-51-11. OPS TEST NORMAL. 1209081 - M4:&NBSP; FLIGHT DECK TEMP REMAINED @29C THROUGHOUT FLIGHT. DUE TO ITEM NR1 LP 1209080 SUSPECT MECHANICAL FAILURE OF FLOW CONTROL AND SHUT OFF VALVE. R & R IAW AMM 21-51-01 OFF PART: PN 396496-1, SN 7070. REF LP 1209082 ITEM 8 FOR OPS CHECK. LP 1209082 - M8: PERFORMED ENG RUN IAW AMM 71-00-00, OPS CHECK OF LT PACK NORMAL AT THIS TIME. THIS CLEARS DMI 141737. ALL PLACARDS REMOVED.

Part: SWITCH — FAILED (APU BAY) · airframe 82,828 hrs · 18,095 cycles

APU FAULT ON TAXI IN. DEFERRED PER MEL 49-11-01A MDDR 141738 CAT C 10FEB21 DUE DATE. DP @ 18:43 02FEB21 LOG PG 1209084 ITM 15 RIV. R & R APU LOW OIL PRESSURE SWITCH PER AMM 49-94-02. OPS TEST OF APU NORMAL. NO DEFECTS NOTED. THIS CLEARS DMI 141738. PLACARDS REMOVED.

Part: ECU — MALFUNCTIONED (APU) · airframe 82,814 hrs · 18,088 cycles

APU BLEED AIR INOPERABLE WHILE APU RUNNING. REMOVED AND REINSTALLED APU ECU UNIT, IAW B767 AMM 20-10-01. PERFORMED OPERATIONS CHECK ON APU SYSTEM, IAW B767 AMM 49-11-00. CHECKS GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: MOTOR — FAILED (STARTER) · airframe 82,804 hrs · 18,085 cycles

APU SHUTDOWN (AUTO) ON GROUND IN CVG AFTER INITIAL START. MINI FLAG 35 SHOOTED ECU NOTED. REMOVED AND REPLACED ECU, IAW AMM 49-61-05. CLEARED MINI FLAG BUT NOW POINTING TO APU STARTER. REF LP 1253076 FOR STARTER CHANGE ITEM NR 4. S/N OFF 94-A0068 P/N OFF 2117342-20. REMOVED AND REPLACED APU STARTER MOTOR, IAW AMM 49-41-01. OPERATIONS CHECK GOOD.

Part: CONDENSER — INOPERATIVE (RT A/C PACK) · airframe 82,578 hrs · 18,012 cycles

RT PACK INOPERABLE (AIR CONDITIONING PACKS - 200/300 (NOTIFY DISPATCH). ER RESTRICTED R-60. TRANSFERRED TO MDDR 138732, IAW MEL 21-51-01-01, CAT C. REMOVED AND REPLACED RT PACK CONDENSER, IAW AMM 21-51-10. OPERATIONS AND LEAK CHECK GOOD. NO FAULTS AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 82,474 hrs · 17,975 cycles

FWD EQUIPMENT VALVE ON EICAS AFTER LANDING, COMPLETED QRH CHECKLIST. PERFORMED FIM TASK 21-58 FT 985, NO MESSAGE OR OTHER FAULTS AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION (T/R UNIT) · airframe 82,046 hrs · 17,848 cycles

T-R UNIT DISPLAYED ON EICAS. CYCLED POWER TO A/C, PER FIM 24-32 FAULT TREE 803. MESSAGE CLEARED.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 81,906 hrs · 17,805 cycles

LEFT AOA INOPERABLE. REMOVED AND REPLACED CAPTAINS ANGLE OF ATTACK KORRY LIGHT ASSEMBLY IAW AMM 33-13-00 AND OPERATIONS CHECKED GOOD IAW AMM 30-32-00.

Part: CONNECTOR — DIRTY (PRESS INDICATOR) · airframe 81,791 hrs · 17,768 cycles

PNEUMATIC PRESSURE READS APPROXIMATELY 22 PSI LOWER ON RIGHT SIDE COMPARED TO LEFT PNEUMATIC INDICATOR BAD FROM STOCK R/H INDICATOR READS INCORRECTLY REMOVED AND REPLACED DUCT PRESSURE INDICATOR IAW AMM 36-21-02, OPS CHECK GOOD. REINSTALLED PNEUMATIC INDICATOR IAW AMM 36-21-02.LP 1134898 ITEM 2: PERFORMED TROUBLESHOOTING AS PER FIM 36-20 FAULT TREE 803 AND CLEANED THE CONNECTOR AT THE BACK OF INDICATOR. PERFORMED OPS CHECK AND THE INDICATOR WORKING GOOD.

Part: RADAR — MALFUNCTIONED (LEFT) · airframe 81,737 hrs · 17,749 cycles

LEFT RADAR INOP(<P>PERFORMED WX TEST IAW AMM 34-43-00. TEST PASSED. MESSAGE CLEARED.<BR /></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (FAN) · airframe 81,684 hrs · 17,734 cycles

AFT EQ EXH FAN 2 STATUS MESSAGE AFTER ENGINE START. PERFORMED FIM 21-26 FT 806. MSG CLEARED. NO FURTHER DEFECTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (EXHAUST FAN) · airframe 81,648 hrs · 17,722 cycles

AFT EQUIPMENT EXHAUST FAN NR 2 STATUS MESSAGE. PERFORMED A TEST IAW 21-58-49. STATUS MESSAGE CLEARED. OK FOR SERVICE.

Part: CONTROL VALVE — FAILED (APU) · airframe 81,646 hrs · 17,721 cycles

APU AIR PRESSURE DROPS TO 10 PSI AND STAYS AT 10 PSI DURING START. REMOVED AND REPLACED APU SURGE CONTROL VALVE IAW AMM 49-53-01, OPS AND LEAK CHECKED GOOD.

Part: CIRCUIT CARD — FAILED (EQUIP COOLING) · airframe 81,636 hrs · 17,717 cycles

AFTER BLOCK OUT FWD EQPT OVHT EICAS MSG. AFTER QRH CHECKLIST ACCOMPLISHED, MSG STAYED EXTINGUISHED. T/S FIM 2158 FAULT TREE 999 FOUND VALVE ASSY AIR MODULATION INOP. REMOVED AND REPLACED VALVE ASSY AIR MODULATION IAW AMM 21-58-07. OPS TESTED OK. BOTH PACKS RUNNING ON GRD ALL TIME. PERFORMED FIM 21-58 TFT 986. VERIFIED V90 VALVE MOVED TO POS C-B IN OVRD & A-B IN AUTO. AFTER 30 SEC LIGHT STAYED ON STBY. REMOVED AND REPLACED M867 CARD COOLING IAW AMM 21-58-24. PERFORMED EQPT COOLING OPERATIONAL CHECK IAW AMM 21-58-00. SYSTEM CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (WEATHER RADAR) · airframe 81,641 hrs · 17,719 cycles

STATUS MESSAGE FOR WX SYS. CYCLED THE RT WXR SYS CIRCUIT BREAKER IAW FIM 34-43, TASK 801. MESSAGE CLEARED. OPS CHECKED GOOD.

Part: FUEL FILTER — WARNING MESSAGE · airframe 81,608 hrs · 17,709 cycles

RIGHT ENGINE FUEL FILTER EICAS MESSAGE DISPLAYED TWICE DURING CLIMB. MESSAGE LASTED A FEW SECONDS THEN BECAME A STATUS MESSAGE. REMOVED AND REPLACED THE RT FUEL FILTER. NO FUEL FILTER STATUS, OPS AND LEAK CHECKED OK IAW AMM 73-11-02.

Part: WARNING MESSAGE — ILLUMINATED (EQUIPMENT COOLIN) · airframe 81,589 hrs · 17,703 cycles

FWD EQUIPMENT VALVE EICAS AFTER ENGINE START, MOVED SWITCH TO STANDBY, MESSAGE DID NOT CLEAR.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 81,589 hrs · 17,703 cycles

AFT EQUIP EX FAN 2 STATUS MESSAGE. REMOVED AND REPLACED OVERBOARD EXHAUST VALVE IAW AMM 21-58-05.

Part: STATUS MESSAGE — ILLUMINATED (EQUIP COOLING) · airframe 81,589 hrs · 17,703 cycles

AFT EQUIPMENT EXHAUST FAN 2 STATUS MESSAGE.

Part: VALVE — WARNING MESSAGE · airframe 81,589 hrs · 17,703 cycles

FWD EQUIP VALVE EICAS AFTER ENGINE START, MOVED SWITCH TO STAND BY MSG DID NOT CLEAR. REMOVED AND REPLACED OVERBOARD EXHAUST VALVE IAW AMM 21-58-05.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 81,571 hrs · 17,697 cycles

ON LANDING FWD EQUIP VLV EICAS MESSAGE DISPLAYED. PERFORMED OPS CHECK MANIFOLD INTERCONNECT VALVE AND OVERRIDE VALVE. REF AMM 21-58-00-705-161-008 REV 130, OPS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 81,401 hrs · 17,632 cycles

WHEN SELECTING APU BLEED VALVE FROM OFF TO ON FOR START, A MOMENTARY APU BLEED VALVE MESSAGE DISPLAYED, LASTED APPROXIMATELY TWO SECONDS AND CLEARED. PERFORMED TEST OF APU PNEUMATICS IAW AMM 36-00-00-862. PRESSURE NORMAL NO FAULTS NOTED AT THIS TIME.

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 81,222 hrs · 17,571 cycles

WEATHER RADAR NOT SHOWING RED WHEN SHOULD BE EVEN WITH MAX GAIN(<P>OPS CHECK GOOD IAW FIM 34-43 FT 805 FULL COLOR PATTERN SHOWS ON BOTH EHSI. NO FAULTS SHOWN AT THIS TIME.</P>)

Part: TRU — MALFUNCTIONED (APU) · airframe 81,198 hrs · 17,562 cycles

APU FAULT WHEN STARTING ON GROUND.(<P>TRANSFERRED APU TO MDDR #127810, CAT 'C', REF MEL 49-11-01A. DUE 11MAY.</P><P>LP 1232313 ITEM 4: T/S APU IAW FIM 49-11 FT 989. TRU DEFERRED, SEE MDDR 127847. THIS CLEARS MDDR 127810. PLACARD REMOVED.</P><P><SPAN>LP 1232313&NBSP;</SPAN>ITEM 5: OPENED MDDR 127847 TRU INOP IAW MEL&NBSP;24-32-01B, CAT 'D'.</P><P>LP 1232322:&NBSP;<SPAN>REPLACED APU TRU IAW 24-32-04, OPS CHECK GOOD. THIS CLEARS MDDR 127847. PLACARD REMOVED.</SPAN><BR DATA-MCE-BOGUS="1" /></P>)

Part: CONTROL UNIT — MALFUNCTIONED (APU) · airframe 81,185 hrs · 17,556 cycles

APU FAILED TO START UPON LANDING IN MIA, 2 ATTEMPTS MADE.(<P>RESET APU CONTROL UNIT AND PERFORMED BITE TEST, TEST OK IAW MM 49-61-05. APU STARTED NORMALLY.</P>)

Part: CONTROL UNIT — MALFUNCTIONED (WINDOW HEAT) · airframe 81,185 hrs · 17,556 cycles

R FWD WINDOW MESSAGE WINDOW HEAT INOP LIGHT ON.(<P>REMOVED AND REPLACED WINDOW HEAT CONTROL AND FAIL TEST, NO HELP, IAW AMM 30-41-01 AND REINSTALLED ORIGINAL UNIT. REMOVED AND REPLACED M191 L FWD WINDOW HEAT CONTROL UNIT IAW 30-40-101 AMM OPS NORMAL AT THIS TIME, NO FAULT INDICATED.</P>)

Part: UNKNOWN — UNKNOWN (COCKPIT) · airframe 81,183 hrs · 17,555 cycles

RIGHT FWD WINDOW(<P>PERFORMED FIM 30-41-00. BITE PROCEDURES COMPLETED. OPS CHECK GOOD. TASK 802. PERFORMED NO WIRING DAMAGE FOUND. WINDOW SENSOR RESISTANCE CHECK PERFORMED. RESISTANCE WITHIN LIMITS. WINDOW HEAT OPS CHECK GOOD.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 81,183 hrs · 17,555 cycles

APU FAULT&NBSP;(<P>BEGAN APU BITE PROCEDURE. PERFORMED TWO SUCCESSFUL STARTS DURING OPS CHECK IAW AMM 49-11-00. OPS CHECK WAS GOOD.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 81,180 hrs · 17,554 cycles

EICAS RIGHT FWD WINDOW ON. RESET PER QRH, OPS NORMAL.(<P>NOTED BY MAINTENANCE. MCC NOTIFIED. OPS CHECK NORMAL PER AMM 30-41-0 AT THIS TIME.</P>)

Part: FILTER ELEMENT — FAULTED (LT ENGINE) · airframe 81,165 hrs · 17,550 cycles

L. ENG FUEL FILTER ADVISORY AND STATUS MESSAGE DISPLAYED IN FLIGHT. NO ERRATIC ENGINE OPERATION NOTED.(<P>REMOVED AND REPLACED LEFT ENG FUEL FILTER ELEMENT PER AMM 73-11-02. LEAK AND OPS CK PERFORMED PER AMM 71-00-00-712-168-H03. ALL LEAK &AMP; OPS CK GOOD.</P>)

Part: TRANSMITTER — FAILED (APU OIL SYSTEM) · airframe 81,136 hrs · 17,544 cycles

APU FAULT EICAS MSG. REMOVED AND REPLACED APU OIL QTY TRANSMITTER IAW MM 49-94-04/401.

Part: CONNECTOR — DIRTY (APU) · airframe 81,081 hrs · 17,528 cycles

APU WILL NOT START, 3 ATTEMPTS.(<P>TRANSFER TO MDDR 127112 PER MEL 49-11-01A CAT C DUE 25APR20. PLACARD INSTALLED. SD @21:42Z</P><P>17APR: LP 1150290, ITEM M5: PERF APU BITE IAW FIM 49-11 FT 987. FOUND MINI FLAG 34 &AMP; LRU FAULT. A/C START CIRCUIT PERF FIM 49-11 FT 991. EXAMINE CONNECTOR 408B FROM ECU TO STARTER M893 FOUND M893 POSITIVE CONNECTOR BUILT UP EXCESSIVELY DIRT. CLEANED CONNECTOR. CLEARED ECU, PERF MULTIPLE APU STARTS, SUCCESSFUL. THIS CLEARS DMI 127112. PLACARD REMOVED. DI: YK@ 16:26Z</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 81,060 hrs · 17,519 cycles

STATUS MESSAGE AFT EQ EXH FAN 2.(<P>AFT EQ EXH FAN 2 TEST PROCEDURED RUN PER AMM 21-58-41. STATUS MSG CLEARED. OK FOR SERVICE, TESTED OK.</P>)

Part: ECU — MALFUNCTIONED (APU) · airframe 81,058 hrs · 17,518 cycles

APU INOP. THREE START ATTEMPTS AFTER LANDING.(<P>TRANSFERRED TO MDDR 126965 IAW MEL&NBSP;49-11-01A , CAT 'C'.&NBSP;</P><P>REF LOG PAGE 1150271 ITEM 4: REMOVED AND REPLACED APU ECU IAW AMM 49-61-05, OPS CHECK GOOD. THIS CLEARS MDDR 126965.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 81,037 hrs · 17,511 cycles

R FWD WINDOW EICAS MSG AFTER LDG.(<P>C/W FIM FT CH. 30-41 FAULT TREE 803, CKS GOOD AT THIS TIME.</P>)

Part: RELAY — FAILED (APU) · airframe 81,024 hrs · 17,507 cycles

APU WOULD NOT START. REACHED 17% AND WOULD SHUT DOWN.(<P>PERFORMED APU BITE PROCEDURE IAW FIM 49-11-00. FOUND FAULT "AC START CIRCUIT". FOLLOWED TS FIM TO BOX 23. REMOVED AND REPLACED RELAY K197 PER WDM 49-41-11. OPS CHECKED GOOD. APU OPERATIONAL.</P>)

Part: CONTROLLER — MALFUNCTIONED (WINDOW HEAT) · airframe 81,014 hrs · 17,504 cycles

ON TAXI IN EICAS R FWD WINDOW(<P>REMOVED AND REPLACED M192 R FWD WINDOW HEAT CONTROLLER IAW AMM 30-41-01. OPS CHECK GOOD, MESSAGE EXTINGUISHED.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 81,009 hrs · 17,502 cycles

ON LANDING RIGHT FWD WINDOW EICAS MESSAGE INOP LIGHT.(<P>PERFORMED GROUND OPS CHECK OF WINDOW HEAT, REF AMM 30-41-00/501, NO FAULTS. OPS CHECK NORMAL.</P>)

Part: BLEED AIR SYS — MALFUNCTIONED (APU) · airframe 81,009 hrs · 17,502 cycles

DURING ENGINE START, APU WOULD ONLY MAKE 21 PSI DUCT PRESSURE. START WAS NORMAL.(<P>PERFORMED #1 AND #2 ENGINE RUNS (INDEPENDENT) WITH APU, BOTH ENGINE STARTS NORMAL. NO FAULTS, APU PRESSURE +30 PSI, REF AMM 71-00-00/501. OPS CHECK GOOD.</P>)

Part: UNKNOWN — MALFUNCTIONED (WINDOW HEAT) · airframe 81,000 hrs · 17,499 cycles

L2 WINDOW HEAT INOP(<P>CONFIRMED L2 WINDOW HEAT INOP AND COMPLIED WITH DDG 30-41-01-02, PLACED ON DMI 126512, CAT 'C'. MX ACTIONS COMPLIED WITH.</P><P><SPAN>LP 1190013: PERFORMED CHECK WIRING &AMP; CHECK HARNESS, PERFORMED OPERATIONAL TEST, FOUND OK IAW AMM 30-41-00. THIS CLEARS MDDR 126512.</SPAN><BR DATA-MCE-BOGUS="1" /></P>)

Part: CHARGER — FAILED (PAU BATTERY) · airframe 80,974 hrs · 17,490 cycles

APU FAULT(<P>TRANSFERRED TO MDDR #126389 IAW MEL 49-11-01A, CAT "C" EXP: 7APR2020. INITIALS L.U.C. AT 2307Z.</P><P>29MAR20, CVG, LP 1071438, ITEM M2: REMOVED AND REPLACED APU BATTERY CHARGER IAW B767 AMM 24-31-05. OPS CHECK GOOD AT THIS TIME. THIS CLEARS DMI #126389. MCC NOTIFIED, PLACARDS REMOVED. T/I: DP @ 15:17Z.</P>)

Part: ANTI-ICE VALVE — FAILED (LT ENGINE) · airframe 80,967 hrs · 17,487 cycles

L ENG ANTI ICE VALVE EICAS.(<P>PERFORMED REMOVAL AND REPLACEMENT OF LH ENGINE ANTI ICE AUTO RELAY K2105 IN THE P36 PANEL, NO FIX IAW WDM 30-21-11. P/N OFF: W26F4AM11, S/N: OFF: NSN.</P><P>ITEM M3: SECURED LH ANTI ICE VALVE (ENGINE) OPEN IAW DDG 30-21-01-04-02. TRANSFERRED TO MDDR #126081 IAW MEL 30-21-01-04-02, CAT C, DUE DATE 31MAR20.</P><P>LOGPAGE 1071428 ITEM #2: ACCOMPLISHED TAI VALVE TEST IAW AMM 30-21-03. OPS CK FAIL AT STEP E13(1). VALVE FAILED TO CLOSE WHEN COMMANDED. TAI DEACTIVATED PER DDG 30-21-01-04. DMI 126081 REMAINS.</P><P>LOGPAGE 1071428 ITEM #3: REMOVED AND REPLACED L ENG ANTI ICE VALVE IAW B767 30-21-03 AMM &AMP; 71-00-00. OPS CHECK GOOD. NO DEFECTS NOTED. THIS CLEARS MDDR #126081.</P>)

Part: OIL SYSTEM — LOW (APU) · airframe 80,955 hrs · 17,483 cycles

APU FAULT ON GROUND.(<P>SERVICED APU OIL TO FULL, NO LEAKS NOTED. PERFORMED&NBSP; BITE&NBSP; TEST&NBSP; ON&NBSP; ECU,&NBSP; NO FAULT&NBSP; FOUND. APU STARTED. OPS CK GOOD. REF AMM 49-11-00.&NBSP; OK&NBSP; TO&NBSP; CONTINUE&NBSP; AT&NBSP; THIS&NBSP; TIME.<BR /></P>)

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 80,931 hrs · 17,476 cycles

APU FAULT LIGHT ON ATTEMPTED 2 STARTS, BOTH FAILED.(<P>PERFORMED FIM 49-11-04, NO DEFECTS NOTED AT THIS TIME. APU STARTED AS REQUIRED ON GROUND.</P>)

Part: UNKNOWN — MALFUNCTIONED (WINDOW HEAT) · airframe 80,955 hrs · 17,483 cycles

FWD R WINDOW HEAT.(<P>PERFORMED&NBSP; BIT&NBSP; TEST&NBSP; ON&NBSP; WINDOW&NBSP; HEAT&NBSP; CONTROL&NBSP; UNIT.&NBSP; NO&NBSP; FAULTS&NBSP; FOUND.&NBSP; OPS&NBSP; CK&NBSP; GOOD.&NBSP; REF&NBSP; AMM 30-41-00.&NBSP; OK&NBSP; TO&NBSP; CONTINUE&NBSP; AT&NBSP; THIS TIME.<BR /></P>)

Part: OXYGEN MASK — FRAYED (COCKPIT) · airframe 80,871 hrs · 17,460 cycles

CAPT'S O2 MASK SUPPLY HAS FRAYED COVER.(<P>REMOVED AND REPLACED CAPT'S O2 MASK ASSY IAW AMM 35-11-04. OPS CHECK GOOD.</P>)

Part: UNKNOWN — MALFUNCTIONED (VIBRATION SYS) · airframe 80,864 hrs · 17,458 cycles

AT T/O AND CLIMB, POWER L ENGINE VIB 3.8 EVENT RECORDED.(<P>PERFORMED INSPECTION FOR ENGINE #1 IAW FIM 71-05 FT 853. NO DEFECTS NOTED AT THIS TIME PER FIM. THERE IS NO VIBRATION LIMITS DURING TRANSIENT (CHANGING ENGINE SPEEDS).</P>)

Part: CONTROL UNIT — MALFUNCTIONED (WINDOW HEAT) · airframe 80,850 hrs · 17,453 cycles

R FWD WINDOW EICAS MESSAGE.(<P>PERFORMED FIM 30-41 F/T 804 UP TO BLOCK 3, MOVED TO FIM 30-41-00/201 TASK 802 TO STEP E. PER TABLE 102 OF 30-41 FOUND&NBSP;RESISTANCE OK. PER STEP 2 OF TABLE 102. REPLACED RT WHCU IAW AMM 30-41-01. OPS NORMAL AT THIS TIME.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 80,834 hrs · 17,448 cycles

UPON LANDING, R WINDOW HEAT EICAS MSG DISPLAYED AND THEN EXTINGUISHED.(<P>TROUBLESHOOT R WINDOW HEAT ISSUE I.A.W B767 FIM 30-41 FT 803/804. NO FAULTS NOTED AT THIS TIME, OPS CHECK GOOD.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 80,840 hrs · 17,451 cycles

RIGHT FWD WINDOW EICAS MESSAGE AT TOUCHDOWN.(<P>PERFORMED R/H FWD WINDOW BITE TEST I.A.W FIM 30-41 FAULT TREE 804. TEST SUCCESSFUL.<BR /></P>)

Part: DOOR — OPEN (A/C PACKS) · airframe 80,789 hrs · 17,432 cycles

ON CLIMB OUT PASSING 10,000 FT, A/C DEVELOPED LOUD AIR FRAME NOISE AND VIBRATION ON ACCELERATION TO 310 KNOTS. RETURN TO AIRPORT UNEVENTFUL, ON ARRIVAL FOUND RIGHT A/C PACK DOOR OPEN, LANDING UNEVENTFUL.(<P>REMOVED AND REPLACED PACK DOOR AND HARDWARE IAW 52-48-07. OPS CHECKED GOOD.<BR /></P>)

Part: APU — SHUTDOWN · airframe 80,765 hrs · 17,426 cycles

APU SHUTDOWN DURING USE.(<P>TRANSFERRED TO MDDR #124907 I.A.W MEL 49-11-01A, CAT 'C'.</P><P>LP 1190973, ITEM M10: REMOVED AND REPLACED AUXILIARY POWER UNIT IAW B767 AMM 49-11-01-004-001. OPS CHECK AND LEAK CHECK GOOD. THIS CLEARS MDDR 124907, MCC NOTIFIED. PLACARDS REMOVED.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT WINDOW HEAT) · airframe 80,761 hrs · 17,423 cycles

"RT FWD WINDOW HEAT" EICAS ON APP AND LDG REMAINED ON.(<P>PERFORMED OPS TEST OF RT FWD WINDOW HEAT AFTER RESETTING SYSTEM, IAW AMM 30-41-00. NO DEFECTS NOTED AT THIS TIME.<BR /></P>)

Part: SURGE VALVE — MALFUNCTIONED (APU) · airframe 80,746 hrs · 17,418 cycles

APU AUTO SHUT DOWN WHEN PACK TURNED ON.(<P>REMOVED AND REPLACED APU SURGE CONTROL VALVE IAW AMM 49-53-01. OPS CHECK GOOD AT THIS TIME.&NBSP;</P>)

Part: SENSOR — FAILED (BLEED SYS) · airframe 80,690 hrs · 17,398 cycles

IN FLIGHT, LEFT BLEED PRESS 19, RIGHT BLEED PRESS 35. BOTH BLEED PRESS AT 20 ON GROUND.(<P>DEFERRED PER MEL 36-12-02-01, MDDR 124463, CAT 'C', DUE 19FEB20. LEFT ENG FAN AIR VALVE LOCKED AT INTERMEDIATE POSITION AS PER AMM 36-00-00/901.</P><P>LP 1169718 - ITEM M5: REMOVED AND REPLACED LH ENG FAN AIR TEMP SENSOR IAW B767 AMM 36-11-17. OPS CHK GOOD, LEAK CHECK GOOD. FATS REPLACED AFTER FAULT WAS DISCOVERED ON AIR SUPPLY BITE MODULE. FURTHER MONITORING AND OPERATIONAL CHECK REQUIRED IN ORDER TO CLEAR DMI.</P><P>LP 1169727 - ITEM M6:&NBSP;REACTIVATED LT ENG BLEED VLV PER DDG 36-12-02-01 AND PERFORMED BITE CHECK OF AIR SUPPLY CONTROL SYS IAW AMM 36-23-00, TEST GOOD. THIS CLEARS MDDR 124463, PLACARDS REMOVED. MCC NOTIFIED.</P>)

Part: CONTROLLER — FAILED (LT ENGINE A/I) · airframe 80,687 hrs · 17,397 cycles

WITH LEFT ENGINE ANTI-ICE ON, COMPLETE LOSS OF LEFT AIR SYSTEM PRESSURE (I.E. PACK AND BLEED AIR EICAS IN CRUISE, L DUCT PRESS 18 PSI).(<P>AS PER FIM 36-10 FAULT TREE 837, REMOVED AND REPLACED PRV CONTROLLER ON LEFT ENGINE PER AMM 36-11-19. OPS CHECK LEFT ENGINE IDLE RUN OK.</P>)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 80,696 hrs · 17,401 cycles

BOTH DOME LIGHTS IN AFT COCKPIT INOP.(<P>RELAMPED 2 EA EMERGENCY LIGHT LAMPS IAW B767 AMM 33-51-41. OPS CK GOOD.<BR /></P>)

Part: VALVE — FAILED (FAN AIR) · airframe 80,685 hrs · 17,396 cycles

L DUCT PRESSURE FLUCTUATES TO 0 DURING CLIMB, ACCOMPANIED WITH "L ENG BLEED OFF" (INTERMITTENT). NOTE: DURING CRUISE, RIGHT DUCT PRESSURE AT 35 AND LEFT AT 17.(<P>RAN FIM 36-10 FAULT TREE 837, REMOVED AND REPLACED FAN AIR VALVE PER AMM 36-11-16. RAN ENGINE, OPS CHECKS GOOD.</P>)

Part: SHUTOFF VALVE — MALFUNCTIONED (ENGINE BLEED) · airframe 80,652 hrs · 17,382 cycles

DURING CLIMB AND DESCENT, L DUCT INTERMITTENTLY ZERO. ACCOMPANIED W/ L PACK OFF EICAS L ENG BLD OFF EICAS.(<P>LOG PAGE 1196915: REMOVED AND REPLACED L/H PRSOV IAW AMM 36-11-09, OPS AND LEAK CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.&NBSP;<BR /></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (DUCT PRESSURE) · airframe 80,646 hrs · 17,378 cycles

L DUCT PRESS DROPS TO 10 PSI WHEN L ENG ANT-ICE SELECTED.(<P>PERFORMED AIR SUPPLY BITE IAW 36-23-00, NO DEFECTS NOTED. PERFORMED VISUAL INSPECTION OF TAI AND ANTI-ICE DUCTING IAW 30-11-02, NO DEFECTS NOTED. PERFORMED ENGINE RUN &AMP; CYCLED ANTI-ICE SEVERAL TIMES, NO DEFECTS NOTED. OPERATIONAL CHECK GOOD.</P>)

Part: SHUTOFF VALVE — FAILED (LT ENGINE) · airframe 80,638 hrs · 17,375 cycles

DURING DESCENT, "L WING ANTI-ICE" CAUTION MESSAGE. NOTED BY MX, CAUTION MSG IS ASSOCIATED WITH LT ENG HPSOV FAILURE, REMOVED AND REPLACED HIGH PRESSURE SHUT OFF VALVE IAW AMM 36-11-07.

Part: WIRE — LOOSE (ANTI-ICE SYS) · airframe 80,638 hrs · 17,375 cycles

LEFT ENG BLEED EICAS MSG DISPLAYED WHEN LEFT ENG ANTI-ICE SELECTED.(<P>PERFORMED BITE CHECK FOR FAMV, FOUND L FAV, FAS LIGHT ON. OPENED T/R ON LEFT ENG AND FOUND TWO LOOSE WIRES. TIGHTENED WIRES, RAN ENG, NO MESSAGES PRESENT AT THIS TIME. VERIFIED BITE ON FAMV, NO MESSAGES STORED IAW B767-300 AMM 36-11-16 AND AMM 71-00-00. OPS CHK GOOD.</P>)

Part: SHUTOFF VALVE — FAILED (LT ENGINE) · airframe 80,638 hrs · 17,375 cycles

DURING DESCENT, "L ENG BLEED OFF" CAUTION MESSAGE. REMOVED AND REPLACED HIGH PRESSURE SHUT OFF VALVE IAW AMM 36-11-07.

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI-ICE VALVE) · airframe 80,638 hrs · 17,375 cycles

LEFT ANTI-ICE VALVE EICAS MSG WHEN SELECTED ENG ANTI-ICE FROM ON TO AUTO.(<P>PERFORMED ANTI-ICE VALVE OPS CHK IAW 30-21-00. NO PROBLEMS NOTED.</P>)

Part: CIRCUIT CARD — MALFUNCTIONED (LT BLEED) · airframe 80,623 hrs · 17,370 cycles

LEFT ENGINE BLEED OFF CAUTION MESSAGE ON EICAS. BITE PROCEDURE PERFORMED, FOUND FAS AND FAU FAULTS. REMOVED AND REPLACED LEFT ENGINE AIR SUPPLY CONTROL IAW AMM 36-11-03. FAULTS CLEARED. MCC NOTIFIED.

Part: SEAL — LEAKING (SHUTOFF VALVE) · airframe 80,612 hrs · 17,366 cycles

AFTER BOTH ENGINES WERE STARTED AND WITH AIRCRAFT CONFIGURED NORMALLY, THE LEFT DUCT PRESSURE WOULD OSCILLATE BETWEEN 10 AND 40 PSI WHILE RIGHT DUCT PRESSURE WAS STEADY AT 35 PSI. THE OSCILLATION TOOK APPROX 20 SECONDS FROM 10 TO 40 PSI THEN REMAINED AT 40 FOR 20 SECONDS, THEN DROPPED BACK TO 10 PSI FOR 20 SECONDS AND REPEATED, FROM AFTER PACKS WERE TURNED ON TO TOP OF CLIMB. IN CRUISE, THE LEFT DUCT PRESS REMAINED EVEN WITH THE RIGHT DUCT PRESSURE AT 35 PSI. FOUND SEALS ON #1 ENGINE HPSOV WORN AND CAUSING LEAKS. REMOVED AND REPLACED SEALS IAW 767 AMM 36-11-07. RAN #1 ENGINE, NO FLUX NOTED. BITE BOX NO FAULTS AT THIS TIME.

Part: PUMP — MALFUNCTIONED (HYDRAULIC SYS) · airframe 80,591 hrs · 17,359 cycles

DURING T/O, CENTER HYD DEM PUMP EICAS MSG, C HYD SYS PRESS, GEAR DISAGREE AT APPROX 2000FT. AFTER GEAR RETRACTED, ONLY C HYD DEM PUMP REMAINED ON. QRH COMPLETED CALLING FOR PUMP TO BE TURNED OFF. T/S TO CENTER HYD DEMAND PUMP. TRANSFER TO MDDR 123516 IAW MEL 29-11-03, CAT 'C'.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 80,541 hrs · 17,337 cycles

STATUS MESSAGE AFT EQUIPMENT EXH FAN 2.(<P>PERFORMED FIM 21-26 TASK 806. NO FAULTS FOUND.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 80,541 hrs · 17,337 cycles

HI FLOW INHIBIT STATUS MESSAGE.(<P>PERFORMED FIM 21-51 FAULT TREE 854. NO FAULTS NOTED.&NBSP;</P>)

Part: START VALVE — MALFUNCTIONED (LT ENGINE) · airframe 80,520 hrs · 17,328 cycles

APU INSUFFICIENT DUCT PRESSURE(<P>ITEM TRANSFERRED TO MDDR 123039 IAW DDG 49-11-01-01, CAT&NBSP;'C'.</P><P>REF LOG PAGE 1178031: FOUND INSUFFICIENT AIR FLOW IN LH STARTER, REMOVED AND REPLACED LEFT ENG STARTER (OFF PART: P/N 3505448-5-1, S/N GRTA0349) AND START VALVE WITH DIFFERENT MODELS, PER AMM 80-11-01/80-11-02, OPS CHK GOOD. THIS CLEARS MDDR 123039.</P>)

Part: ACOUSTIC LINER — DAMAGED (RT ENGINE) · airframe 80,440 hrs · 17,304 cycles

ON WALKAROUND FOUND RT ENG ACOUSTIC PANEL AT APPROX. 07 O'CLOCK POSITION AFT OF N1 FAN, TOP COAT MISSING. REMOVED AND REPLACED NR 2 ENGINE ACOUSTIC LINER PANEL AT 7 O'CLOCK IAW AMM 72-33-01.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENGINE) · airframe 80,429 hrs · 17,300 cycles

LEFT ENGINE ANTI-ICE EICAS MESSAGE ILLUMINATED DURING DESCENT. CYCLED THE SWITCH AND THE MESSAGE WENT AWAY. PERFORMED ENGINE INLET TAI TEST IAW AMM 30-21-00. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (EXHAUST FAN) · airframe 80,423 hrs · 17,297 cycles

STATUS MESSAGE FOR AFT EQUIP EXHAUST FAN NR 2. ACCOMPLISHED FIM TASK 21-26 FT 806. MESSAGE CLEARED. OPS CHECKED NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (EXHAUST FAN) · airframe 80,410 hrs · 17,292 cycles

STATUS MSG AFT EQUIPMENT EXH FAN 2(<P>PERFORMED FIM 21-26 FT 806, MSG ERASED. OPS CHK NORMAL AT THIS TIME.</P>)

Part: SENSOR — FAILED (RT PACK TEMP) · airframe 80,404 hrs · 17,290 cycles

RH PACK PRIMARY HEAT EXCHANGER IN TEMP INDICATOR IS BLANK.(<P>REMOVED AND REPLACED BULB ASSY IAW AMM 21-61-02. OPS CHK NORMAL.</P>)

Part: DUCT — DAMAGED (SURGE VALVE) · airframe 80,364 hrs · 17,278 cycles

FOUND SURGE VALVE DUCT DAMAGED.(<P>REMOVED AND REPLACED DUCT IAW B767 AMM 49-53-01, OPS CHECK GOOD.&NBSP;<BR /></P>)

Part: WARNING MESSAGE — ILLUMINATED (ENGINE VIBRATION) · airframe 80,369 hrs · 17,279 cycles

ON THE CLIMB, L/H ENG DISPLAYED 3.5 VIB FAN AT CLIMB POWER (104.1). EVENT RECORD WAS PUSHED.&NBSP;(<P>PERFORMED FIM 71-05 FT 853 UP TO BLOCK 56. CONTINUE THE ENGINE TO SERVICE, MONITOR THE ENG VIB ON SUBSEQUENT FLIGHTS. MCC NOTIFIED.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT BLEED) · airframe 80,362 hrs · 17,277 cycles

"R BLEED OFF" MSG DISPLAYED &AMP; CLEARED NUMEROUS TIMES DURING FLIGHT.(<P>PERFORMED AIR SUPPLY MODULE BITE TEST, NO FAULT FOUND PER FIM 36-10 FT 836. IDLE ENG RUN UP IAW 71-00-00-862-002-600, OPS CHECK NORMAL.</P>)

Part: MODULE — FAILED (FLOW SENSING) · airframe 80,283 hrs · 17,245 cycles

APU NOT PROVIDING ENOUGH AIR PRESSURE TO START RIGHT ENGINE. REMOVED AND REPLACED FLOW SENSING MODULE IAW B767 AMM 49-53-08. OPS CHECKED GOOD.

Part: O-RING — DAMAGED (OIL FILLER CAP) · airframe 80,280 hrs · 17,244 cycles

DURING MAINTENANCE ON APU, EVIDENCE OF OIL LEAK FROM FILLER CAP. FOUND FILLER CAP "O" RING DAMAGED.(<P>REMOVED AND REPLACED FILLER CAP "O" RING IAW AMM 20-10-19. RAN APU AND CHECKED FOR OIL LEAKS, NO LEAKS NOTED AT THIS TIME.</P>)

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 80,245 hrs · 17,231 cycles

UNCOMMANDED CHANGES IN THE NR 1 ENGINE N1, N2 FUEL FLOW DURING POWER SURGES FROM BAD CPU. NO THRUST LEVER MOVEMENT. PERFORMED PIMU BITE PROCEDURE AND GROUND TEST ON BOTH ENGINES BY PLACING EEC MAINT (L/R) ENGINES POWER SWITCH ON P61 PANEL TO TEST PER FIM 71-01 FT 810. NO FAULTS FOUND AT THIS TIME.

Part: SENSOR — FAULTED (INLET TEMP) · airframe 80,221 hrs · 17,223 cycles

APU AUTO SHUTDOWN. SERVICED APU OIL (1.5 QT) IAW AMM 12-13-04. OPS CHECK AND LEAK CHECK NORMAL, NO FAULTS NOTED. APU AUTO SHUTDOWN AGAIN. REMOVED AND REPLACED INLET TEMP SENSOR ON APU PER AMM 49-61-03. RAN APU, PERFORMED OPERATIONAL CHECK, OPS CHECK GOOD.

Part: NONE — NONE (NONE) · airframe 80,201 hrs · 17,216 cycles

RADAR GROUND CLUTTER SUPPRESSION (GCS) SWITCH DOES NOT LOCK DOWN IN THE GROUND CLUTTER SUPPRESSION MODE. ALL MODES APPEAR TO OPERATE ON THE RADAR DISPLAY.(<P>THIS IS NON-LATCHING COMPONENT IAW S/B 34-45-32, PN 622-5130-005. PERFORMED OPS CHECK OF THE WX RADAR SYSTEM IAW AMM 34-43-00-501. OPS CHECK NORMAL, A/C OK FOR SERVICE.</P>)

Part: PUMP — WARNING MESSAGE (LT FUEL BOOST) · airframe 80,150 hrs · 17,194 cycles

L FWD FUEL PUMP EICAS MESSAGE.(<P>PLACED ON DMI 120572 IAW MEL 28-22-01, CAT 'C', DUE DATE: 23-NOV-19.</P><P>REF LOG PAGE 1232423 ITEM M3: REMOVED AND REPLACED LEFT FWD BOOST PUMP IAW B767 AMM 28-22-03. OPS CHECK GOOD. THIS CLEARS MDDR 120572. PLACARDS REMOVED.&NBSP;</P>)

Part: OXYGEN MASK — DAMAGED · airframe 80,121 hrs · 17,185 cycles

PORTABLE MASK RUBBER CRACKED.(<P>REMOVED AND REPLACED&NBSP;PORTABLE O2 MASK IAW LOPA DRAWING #B767F 25-EEL REV 11. OPS CHK NORMAL AT THIS TIME.&NBSP;</P>)

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 80,069 hrs · 17,167 cycles

APU INOP; LOW DUCT PRESSURE.(<P>TRANSFERRED TO MDDR 119894 IAW MEL 49-11-01A, CAT 'C', DUE DATE 09-NOV-19.</P><P>LP 1075747 - M9: PERFORMED APU BITE TEST IAW AMM 49-61-05. NO FAULTS DISPLAYED ON ANY OF THE LEGS. PERFORMED AIR SUPPLY BITE IAW 36-23-01, NO FAULTS DISPLAYED. PERFORMED DRY RUN ON BOTH R &AMP; L ENGINES ENSURING DUCT PRESSURE IS WITHIN REQUIRED LIMITS. THIS CLEARS DMI #119894. PLACARD REMOVED FROM FLT DECK AND MCC NOTIFIED.</P>)

Part: APU — UNKNOWN · airframe 80,017 hrs · 17,151 cycles

APU SHUTDOWN WHEN SWITCHING FROM EXT PWR TO APU GEN.(<P>PERFORMED APU BITE IAW B767 FIM 49-11 FT 987. NO FAULTS OR ABNORMAL SHUTDOWN ECU. STARTED APU IAW B767 AMM 49-11-00. PERFORMED POWER TRANSFER AND OPS CHK OF APU GENERATOR IAW B767 AMM 24-21-00, OPS CHECK OK.<BR /></P>)

Part: SENSE LINE — UNSECURE (LT ENGINE) · airframe 79,996 hrs · 17,143 cycles

LEFT ENGINE BLEED OFF INTERMITTENT.(<P>SECURED PRSOV SENSE LINES AND EXERCISED PRSOV VALVE. NO DEFECTS NOTED AT THIS TIME PER FIM 36-11-07.&NBSP;</P>)

Part: CIRCUIT BREAKER — TRIPPED (BOOST PUMP) · airframe 79,846 hrs · 17,095 cycles

L FWD FUEL BOOST PUMP CIRCUIT BREAKER POPPED AFTER TURNING FUEL PUMPS ON&NBSP;(<P>RESET CIRCUIT BREAKER AND OPS CHECKED FUEL PUMP I.A.W AMM 28-21-00 NO FAULTS AT THIS TIME&NBSP;</P>)

Part: FIRE WARNING — FALSE ACTIVATION (MAIN CARGO) · airframe 79,851 hrs · 17,096 cycles

MAIN CARGO FIRE EICAS MESSAGE WITH FIRE WARMING LIGHT, AND MASTER CAUTION LIGHT AND CARGO FIRE ARM SWITCH LIGHT DEPRESSED MAIN CARGO FIRE ARM SWITCH AND INCORRECTLY DISCHARGED APU FIRE BOTTLE. REMOVED AND REPLACED APU FIRE EXTINGUISHER IAW AMM 26-22-02.

Part: CONTROL VALVE — MALFUNCTIONED (APU) · airframe 79,740 hrs · 17,061 cycles

VERY LOW DUCT PRESSURE DURING FIRST ENGINE START (RIGHT ENGINE), LONGER THAN NORMAL START PROCESS. TRANSFERRED TO MDDR 117914 IAW MEL 49-11-01-01, CAT "C", DUE 28-SEP-2019. MAINT ACTION C/W. LP 1210156 - M6: REMOVED AND REPLACED THE APU AIR SUPPLY SHUTOFF VALVE IAW AMM 36-11-10. OPS CHECK GOOD AND LEAK CHECK GOOD AT THIS TIME. DMI 117914 REMAINS OPEN DUE TO ENGINE RUN REQUIRED. COULD NOT RUN ENGINE DUE TO GROUND TIME. MCC NOTIFIED. LP 1210161 - M1: C/W DG 49-11-01-01. LOCKED OUT APU BLEED. LP 1210166 - M3: REMOVED AND REPLACED SURGE CONTROL VALVE ON APU IAW AMM 49-53-01. INSTALLED A SERVICEABLE FLOW CONTROL GASKET IAW AMM 49-53-08. OPS CHECK GOOD, COMPLIED WITH MX PROCEDURE. LP 1210168 - M7: PERFORMED ENGINE RUNS AND WATCHED PNEUMATICS DURING ENGINE START WITH ADP OPERATING IN AUTO POSITION IAW AMM 71-00-00. PNEUMATICS PARAMETERS ARE NORMAL. THIS CLEARS MDDR #117914. PLACARDS REMOVED AND MCC NOTIFIED. GASKET OFF PART (PN: 3876179-2, SN: NSN)

Part: PUMP — MALFUNCTIONED (APU) · airframe 79,717 hrs · 17,049 cycles

DURING R ENG START, APU DUCT PRESSURE STARTED FLUCTUATING BETWEEN 15 - 30%. R ENG STARTER MESSAGE DISPLAYED @ APPROX 5% N2. TRANSFERRED TO MDDR # 117639 IAW MEL 49-11-01A, CAT C. DUE 22SEP19. DISP: ZH 10:45Z. LP 1086521 - M1: PRESSURIZED PNEU SYS IAW AMM 36-00-00. CHECKED FOR LEAKS ON ALL DUCTS AND CONNECTIONS. NO LEAKS NOTED. PERFORMED BITE TEST ON ALL 3 TEMP CONTROLLERS AND AIR SUPPLY CONTROLLER IAW FIM 21-61 F/T 912 AND FIM 36-20 F/T 804. NO FAULTS FOUND. PERFORMED ENG RUNS IAW AMM 71-00-00 ALL OPS GOOD. ENG PARAMETERS ALL WITHIN LIMITS. DMI REMAINS OPEN. LP 1086526 - M5: PERFORMED FIM 36-10 F/T 840, BLOCK 1-4. FOUND RT PRSOV FAULTED. REMOVED AND REPLACED RT ENG PRSOV IAW AMM 36-11-09. OPS CHECKS GOOD AT THIS TIME. OFF PART (PN: 799801-4, SN: 9811013) LP 1086526 - M6: FOUND ADP TO BE AT FAULT FOR PNEUMATIC DROP ON ENGINE START. ADP PUT ON DEFERRAL (REF LP 1086527 - ITEM 1). PERFORMED OPS TEST OF APU IAW 49-11-00. ALL OPS CHECK GOOD AT THIS TIME. THIS CLEARS DMI #117639. PLACARDS REMOVED AND MCC NOTIFIED.

Part: FIRE DETECTOR — FAULTY (RT ENGINE) · airframe 79,717 hrs · 17,049 cycles

RIGHT ENG #2 FIRE LOOP EICAS MSG. TRANSFERRED TO MDDR #117634 IAW MEL 26-11-01-01, CAT "C", DUE 22-SEP-19. DISPATCH: DL @ 09:36Z LP 1210141- M4: REMOVED AND REPLACED LOWER AFT FIRE DETECTOR ON RT ENGINE IAW AMM 26-11-02, OPS CHECK GOOD. THIS CLEARS DMI #117634. PLACARD REMOVED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 79,652 hrs · 17,028 cycles

RIGHT FWD WINDOW EICAS MESSAGE DURING APU START ATTEMPT. PERFORMED OPS CHECK IAW AMM 30-41-00, OPS CHECKS GOOD AT THIS TIME.

Part: TRU — FAULTY (APU) · airframe 79,652 hrs · 17,028 cycles

APU FAILED TO START, APU FAULT MESSAGE. TRANSFERRED TO MDDR 117125 IAW MEL 49-11-01A, CAT 'C', DUE 10-SEP-19. LP 1073215 - M2: T/S PER FIM TASK 49-11 FAULT TREE 991, FOUND FAULTY APU TRU. REMOVED AND REPLACED APU TRU IAW AMM 24-32-04. OPS CHECK GOOD, NO FAULTS AT THIS TIME. THIS CLEARS MDDR 117125. MCC NOTIFIED AND ALL PLACARDS REMOVED.

Part: VALVE — MISINSTALLED (AC BAY) · airframe 79,652 hrs · 17,028 cycles

DURING APPROACH, LEFT PACK TEMP EICAS MESSAGE. PACK OPERATED IN STANDBY MODE AFTER PACK RESET. TRANSFERRED TO MDDR 117124 PER MEL 21-51-03-01, CAT C, DUE 10-SEP-19. PLACARDS INSTALLED AND MCC NOTIFIED. LP 1073215 - M3: T/S PACK CONTROL SYSTEM AND FOUND TRIM AIR SUPPLY VALVE INSTALLED BACKWARDS. REMOVED AND RE-INSTALLED TRIM AIR SUPPLY VALVE IAW AMM 21-61-05. OPS CHECKS GOOD, NO FAULTS AT THIS TIME. THIS CLEARS MDDR 117124. MCC NOTIFIED AND PLACARDS REMOVED.

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 79,648 hrs · 17,027 cycles

APU FAILED TO START UPON LANDING AT RFD. SECOND ATTEMPT FAILED AS WELL WITH "APU FAULT" EICAS MESSAGE. PERFORMED BITE TEST IAW FIM 49-11 FAULT TREE 958. NO FAULTS FOUND AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 79,648 hrs · 17,027 cycles

RT FWD WINDOW EICAS MESSAGE UPON LANDING. PERFORMED OPS CHECK IAW AMM 30-41-00. OPS CHECKED GOOD AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT A/C PACK) · airframe 79,643 hrs · 17,025 cycles

LEFT PACK TEMP EICAS MESSAGE IN FLIGHT. PERFORMED LEFT PACK SYSTEM BITE AND PACK SYSTEM TEST IAW AMM 21-51-00, NO FAULTS FOUND. RECYCLED LEFT PACK SWITCH, OPS CHECK GOOD.

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 79,645 hrs · 17,026 cycles

APU FAILED TO START ONCE A/C LANDED IN ONT. PERFORMED FIM 49-11 FT 987 APU BITE, FLAG 34 FAULT. CLEARED FAULT AND PERFORMED OPS CHECK. OPS CHECK NORMAL AT THIS TIME IAW AMM 49-11-00.

Part: WIRE — DISCONNECTED (WINDOW HEAT) · airframe 79,637 hrs · 17,024 cycles

RT FWD WINDOW HEAT EICAS MESSAGE AND INOP LIGHT ON OVERHEAD PANEL CAME ON AFTER LANDING. DURING TROUBLESHOOTING, FOUND 2 SHIELDED WIRES FROM TERMINAL BOARD T234, FA2 AND FC2 NOT CONNECTED FOR WIRES W624-203B AND W624-202R. RESOLDERED IAW SWPM 20-10-15. PERFORMED ENGINE RUNS IAW AMM 71-00-00. TURNED OFF APU AND RESTARTED TWICE, NO ISSUES WERE FOUND. OK FOR SERVICE.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT WINDOW) · airframe 79,636 hrs · 17,023 cycles

RIGHT FWD WINDOW EICAS MESSAGE CAME ON AFTER LANDING. RESET RIGHT FWD WINDOW HEAT PBSW, FAULT CLEARED. PERFORMED FIM 30-41 FT 804, NO FAULT NOTED.

Part: STATUS MESSAGE — FALSE INDICATION (NR 2 FIRE LOOP) · airframe 79,634 hrs · 17,022 cycles

DURING PRE-FLIGHT CHECK, FOUND STATUS MESSAGE: R ENG FIRE LP 2. T/S PER FIM 26-11. CHECKED AND CLEANED ALL CONNECTORS, NO FAULTS NOTED. ALL CHECKED OK, TESTED FIRE DETECTOR LOOPS AND ALL CHECK OK PER AMM 26-11-00.

Part: CONTROLLER — NOT REPORTED (RT A/C PACK) · airframe 79,634 hrs · 17,022 cycles

RH PACK CONTROLLER REQUIRES REPLACEMENT. REMOVED AND REPLACED RH PACK CONTROLLER IAW AMM 21-51-24. OPS CHECK GOOD AT THIS TIME.

Part: WIRE — SHORTED (SENSOR) · airframe 79,634 hrs · 17,022 cycles

EICAS MESSAGE FOR RT FWD WINDOW. RAN QRH 3.15. PERFORMED FIM 30-41 FT 802. CHECKED SENSOR 1 SENSOR 2 OHMS GOOD. CHECKED WINDOW HEAT ELEMENT RESISTANCE AT 10.2 OHMS GOOD, FOUND SHORT TO GROUND ON WIRE W624-202B-24 W624-203B-24, W624-215B-24. ITEM 3. ITEM 3, REPLACED SOLDER SPLICES ON WIRE W624-202B-24, W624-202R-24, W624-203B-24, W624-203-24, W624-215B-24, W624-215R-24, TO SHIELD TO GROUND AT TB324. OPS CHECK GOOD IAW SWPM 20-30-12, AMM 30-41-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (WINDOW HEAT) · airframe 79,628 hrs · 17,019 cycles

RT FWD WINDOW EICAS MSG. PERFORMED FWD WINDOW HEAT OPERATIONAL CHECK IAW AMM 30-41-00. FOUND NO DISCREPANCY AT THIS TIME, OPS CHECK IAW FIM 30-41-00 FAULT TREE 804.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT A./C PACK) · airframe 79,634 hrs · 17,022 cycles

DURING DESCENT RECEIVED AN EICAS MESSAGE, LT PACK TEMP. RAN THE QRH TO SBY N. PERFORMED SYSTEM TEST OF LT PACK COOLING SYSTEM IAW B767 AMM 21-51-00. FOUND NO MESSAGES OR FAULTS ON LT PACK CONTROLLER AT THIS TIME. AIRCRAFT OK FOR SERVICE.

Part: CONTROLLER — MALFUNCTIONED (WINDOW HEAT) · airframe 79,632 hrs · 17,021 cycles

RECEIVED "RIGHT FWD WINDOW" EICAS AFTER LANDING. REMOVED AND REPLACED RIGHT WINDOW HEAT CONTROLLER IAW AMM 30-41-01. OPS CHECK GOOD.

Part: CONTROLLER — NO TEST (WINDOW HEAT) · airframe 79,634 hrs · 17,022 cycles

R FWD AND L AFT WINDOW HEAT CONTROLLER REQUIRES REPLACEMENT, WILL NOT TEST CONSISTENTLY. REMOVED AND INSTALLED. SERVICEABLE WINDOW HEAT CONTROLLER IAW B767 AMM 30-41-01. OPS CHECK GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (WINDOW HEAT) · airframe 79,628 hrs · 17,019 cycles

EICAS MESSAGE: RIGHT FWD WINDOW. PERFORMED OPS CHECK OF THE RIGHT FWD WINDOW HEAT IAW AMM 30-41-00. OPS CHECK GOOD AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION (WINDOW HEAT) · airframe 79,623 hrs · 17,017 cycles

DURING DESCENT, RECEIVED EICAS ADVISORY "R FWD WINDOW". RAN QRH AND COMPLIED, MSG EXTINGUISHED. PERFORMED WINDOW HEAT CONTROL UNIT BITE. NO FAULTS AND NO EICAS MESSAGES AT THIS TIME. PERFORMED BITE PER AMM 30-41-01-861-001. OPS CHECK TESTED OK.

Part: WARNING MESSAGE — FALSE ACTIVATION (WINDOW HEAT) · airframe 79,627 hrs · 17,018 cycles

R FWD WINDOW EICAS MESSAGE. PERFORMED OPS CHECK OF RT FWD WINDOW HEAT, OPS CHECK GOOD AT THIS TIME IAW AMM 30-41-01.

Part: APU — INOPERATIVE · airframe 79,627 hrs · 17,018 cycles

APU INOP. PERFORMED OPERATIONAL CHECK OF APU IAW AMM 49-11-00, OPS CHECK GOOD.

Part: UNKNOWN — MALFUNCTIONED (WINDOW HEAT) · airframe 79,614 hrs · 17,014 cycles

FWD RIGHT WINDOW HEAT INOP. PERFORMED BITE CHECK OF WINDOW HEAT CONTROLLERS PER AMM 30-41-00. NO FAULTS NOTED, MESSAGE CLEARED.

Part: HOOK AND LOOP — MISSING (EVAS) · airframe 79,614 hrs · 17,014 cycles

EVAS SYSTEM: HOOK AND LOOP STRIP FOR IVU ON THE TOP GLARE SHIELD NOT INSTALLED ON CA/FO SIDES. INSTALLED LOOP SIDE OF FASTENER FOR COCKPIT SMOKE VISION SYSTEM IAW EO 6725A222.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT A/C PACK TEMP) · airframe 79,599 hrs · 17,011 cycles

LEFT PACK TEMP CAUTION MESSAGE. PERFORMED LEFT PACK TEMPERATURE CAUTION B9 TE TEST PROCEDURES IAW B767 300 FIM 21-51 FT 844. RE SAT THE INITIAL BITE TEST OK EVERYTHING WORKING GOOD AT THIS TIME

Part: CONNECTOR — DAMAGED (WX RADAR) · airframe 79,599 hrs · 17,011 cycles

RIGHT SYS RADAR DISPLAYS ATT DISAGREE LEFT SYS ON OK. PERFORMED R WXR TEST IAW FIM 34-43 F/T 805. WXR FAIL ATT. SWAPPED WX RADAR RT PER AMM 34-43-01. NO HELP. WXR ATT FAULT WHEN USING RT WXR. INSPECTED WXR ANTENNA PER AMM 34-43-00. NO DEFECTS. FOUND D4769 PIN CONNECTOR PIN 44 GROUNDING BUS 3 OF IRU RIGHT. IAW WDM 34-21-27 PIN 44 IS UNUSED. DE-PINNED AND STOWED WIRE W9003-902B-24 PER SWPM 20-61-00. RIGHT WEATHER RADAR OPS CHECKS GOOD PER AMM 34-43-00.

Part: LEAD — DAMAGED (IGNITION) · airframe 79,597 hrs · 17,009 cycles

#2 ENGINE INBD LOWER IGNITION LEAD HAS ARC DAMAGE.(<P>REMOVED &AMP; REPLACED #2 ENG #1 SYSTEM IGNITOR LEAD IAW AMM 74-21-01. ASSET # 0019077, 0019114, 0018917 OPS CHECK ACCOMPLISHED ON TASK # T2031.</P>)

Part: TRANSDUCER — MALFUNCTIONED (THRUST REVERSER) · airframe 79,597 hrs · 17,009 cycles

WHILE PERFORMING ENGINE RUN, RT EFC CHAN 2 MESSAGE SHOWS ON EICAS DISPLAY. REMOVED AND REPLACED NR 2 ENGINE OUTBD THRUST REVERSER TRANSDUCER IAW AMM 78-36-03. PERFORMED SATISFACTORY OPS CHECK IAW AMM 71-00-00, NO DEFECTS NOTED, EICAS MESSAGE DID NOT COME BACK.

Part: BLADE — DAMAGED (NR 2 ENGINE FAN) · airframe 79,597 hrs · 17,009 cycles

#2 ENG LE FAN BLADE DENT MARKED WITH DOT.(<P>UPON FURTHER EVALUATION, FOUND DAMAGE TO BE NICK IN AREA "D" OF BLADE WITH ALLOWABLE DAMAGE TO 0.060". MEASURED 0.040". ASSET # 0017552 WITHIN ALLOWABLE LIMITS IAW AMM 72-31-02. NO ACTION REQUIRED.</P>)

Part: CONNECTOR — NOT SEATED (HP CONTROLLER) · airframe 79,597 hrs · 17,009 cycles

NR 1 ENGINE, DURING START, N2 RISING UP TO 20% ONLY AND PRESSURE MANIFOLD FLUCTUATES AROUND 15-20 PSI. SEATED THE CONNECTOR PLUGS ON NR 1 HP CONTROLLER AND PERFORMED SATISFACTORY NR 1 ENGINE START WITH NO FLUCTUATING IN MANIFOLD PRESSURE IAW AMM 71-00-00.

Part: WIRE HARNESS — MALFUNCTIONED (FUEL QTY) · airframe 79,597 hrs · 17,009 cycles

A/C HAS A HISTORY OF LEFT WING FUEL QTY INDICATIONS ISSUES. REPLACED L/W FQIS WIRE HARNESS, PERFORMED BITE CHECK, BITE CHECK FAILED IAW AMM 28-41-09.

Part: MONITOR — MALFUNCTIONED (ENGINE VIBRATION) · airframe 79,597 hrs · 17,009 cycles

WHILE PERFORMING ENGINE RUNS, ENGINE VIBE BITE MSG SHOWS ON EICAS.(<P>REMOVED AND REPLACED ENG AVM IAW AMM 77-31-03. PERFORMED SATISFACTORY ENG AMM OPS CHK IAW AMM 77-31-00.</P>)

Part: PLENUM — DAMAGED (LT ACM) · airframe 79,597 hrs · 17,009 cycles

L/H A/C PACK PLENUM ON AFT SIDE OF AIR CYCLE MACHINE HAS LARGE HOLE TOP FWD SIDE AND SMALL 1 SQ IN HOLE BOTTOM FWD SIDE.(<P>REMOVED AND REPLACED THE L/H A/C PACK PLENUM IAW AMM 21-51-02. PERFORMED SATISFACTORY LEAK CHECK IAW AMM 21-51-02 WITH NO LEAKS NOTED AT THIS TIME. ASSET # 0019077 0019118.</P>)

Part: HEAT EXCHANGER — CRACKED (RT A/C PACK) · airframe 79,597 hrs · 17,009 cycles

RIGHT AIR CONDITIONING MAIN HEAT EXCHANGER CRACKED. REMOVED & REPLACED THE RT SECONDARY HEAT EXCHANGER IAW AMM 21-51-02. PERFORMED SATISFACTORY LEAK CHECKED IAW AMM 21-51-02.

Part: TUBE — CRACKED (NR 1 COOLING) · airframe 79,597 hrs · 17,009 cycles

#1 ENGINE TURBINE COOLING AIR TUBE CRACKED AT 8:30 POSITION.(<P>REMOVED AND REPLACED #1 ENG TURBINE COOLING AIR MANIFOLD @ 8:30 POSITION IAW AMM 75-24-03. AS# 0018938, AS# 0013164, AS# 0019069.</P>)

Part: CONNECTOR — DISCONNECTED (SMOKE DETECTOR) · airframe 79,597 hrs · 17,009 cycles

MAIN CARGO LOOP 1 MESSAGE SHOWS ON LOWER EICAS DISPLAY. CONNECTED THE SMOKE DETECTOR M12213 1A2D ELECTRICAL PLUG IAW SWPM 20-60-06 SHT. PERFORMED SATISFACTORY MAIN CARGO SMOKE DET OPS CHECK IAW SMPM 26-14-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (APU) · airframe 79,597 hrs · 17,009 cycles

APU BITE MESSAGE SHOWS ON LOWER EICAS DISPLAY.(<P>PERFORMED SATISFACTORY T/S AT LOWER EICAS DISPLAY IAW FIM 49-11 FAULT TREE 987. APU MESSAGE ISN'T SHOWING ON DISPLAY.</P>)

Part: ECU — UNKNOWN (APU) · airframe 79,597 hrs · 17,009 cycles

APU BITE MESSAGE ON EICAS DURING APU RUN. NO FAULTS ON ECU. REMOVED AND REPLACED APU ECU IAW AMM 49-61-05.</P>)

Part: ISOLATION VALVE — MALFUNCTIONED (NR 1 ENGINE) · airframe 79,597 hrs · 17,009 cycles

N1 ENGINE FAILS TO SPOOL ABOVE 20% N2. REMOVED AND REPLACE RT ISOLATION VALVE IAW AMM 36-11-04. ACCOMPLISHED SATISFACTORY OPERATIONAL AND LEAK TEST IAW AMM 71-00-00, 36-11-04. NR 1 ENGINE SPOOL UP WAS 26% N2 IAW AMM 71-00-00. NO DEFECTS NOTED.

Part: UNKNOWN — MALFUNCTIONED · airframe 79,582 hrs · 17,002 cycles

UNABLE TO START RIGHT ENGINE VIA AIR START, DUCT PRESSURE APPROX 10 PSI. LEFT ENGINE STARTED NORMALLY WITH PROPER DUCT PRESSURE, FOLLOWED BY CROSS BLEED TO START RIGHT ENGINE.(<P>PERFORMED SYS TEST OF CTR ISO VALVE SYSTEM IAW 36-11-00, NO FAULTS NOTED. PERFORMED RT ENGINE START IAW AMM 71-00-00, ENGINE START NORMAL, DUCT PRESSURE 30 PSI.</P>)

Part: SENSOR — FAULTY (APU) · airframe 79,572 hrs · 16,999 cycles

APU AUTO SHUTDOWN ON GROUND BEFORE BLOCK-OUT.(<P>TRANSFERRED TO MDDR 114872 IAW DDG 49-11-01A, CATC, DUE DATE 26-JUL-19.</P><P>LP&NBSP;1058751&NBSP; - ITEM 1: REMOVED AND REPLACED APU INLET TEMP SENSOR IAW AMM 49-61-03. OPERATIONAL CHECK SATISFACTORY. MDDR 114872 CLOSED.&NBSP;</P>)

Part: OIL SYSTEM — LOW (APU) · airframe 79,507 hrs · 16,976 cycles

APU SHUTDOWN - 0 OIL QUANTITY&NBSP;(<P>SERVICED APU OIL IAW AMM 12-10-00. APU OPS CHECK GOOD. NO DEFECTS NOTED&NBSP;</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 79,489 hrs · 16,969 cycles

AFT EQ COOLING FAN 2 STATUS MSG (<P>AFT EQ EXH FAN 2 DEFERRED PER MEL 21-58-05. THIS BECOMES DMI 114127, CAT 'C', DUE 12JUL19.&NBSP;<BR /></P><P>LP 1080455 - M6: C/W FIM TASK 21-26 FAULT TREE 809. FIM TEST PAST, NO DEFECTS NOTED. THIS CLEARS DMI #114127. MCC NOTIFIED. ALL PLACARDS REMOVED.</P><P>TI: ZH @ 15:03Z</P>)

Part: ECU — MALFUNCTIONED (APU) · airframe 79,465 hrs · 16,962 cycles

APU PRODUCED 21 PSI FOR #2 ENGINE START AND ONLY 10 PSI FOR #1 ENGINE START. CROSS START REQUIRED. (<P>TRANSFERRED TO MDDR 114030 IAW MEL 49-11-01-01. PNEUMATIC FUNCTION OF APU INOP. CAT 'C', DUE 11-JUL-19.&NBSP;R&AMP;R&NBSP; APU SURGE BLEED OPS&NBSP; CHECK GOOD IAW AMM 49-53-01 AND 49-53-01. ALSO REMOVED AND REPLACED APU ECU IAW AMM 49-61-05 OPS CHECK GOOD. THIS CLEARS MDDR-114030 AND PLACARD REMOVED.</P><P><BR DATA-MCE-BOGUS="1" /></P>)

Part: ISOLATION VALVE — CLOSED (APU) · airframe 79,462 hrs · 16,961 cycles

APU ONLY PRODUCED 10 PSI FOR #1 ENGINE START. CROSS START REQUIRED TO START ENGINE 1.(<P>FOUND RT ISOLATION VALVE CLOSED. VALVE RESET, CYCLED, OPERATE OK REF 36-15-00.</P>)

Part: IDG — MALFUNCTIONED (RT GENERATOR) · airframe 79,342 hrs · 16,919 cycles

AFTER RIGHT ENGINE START, R GEN OFF EICAS MESSAGE DISPLAYED. FOLLOWED QRH PROCEDURE AND OPERATED NORMALLY.(<P>TRANSFERRED TO MDDR # 112777 PER MEL 24-30-01-01, CAT B. DUE DATE 09JUN19. ER 120 MNS RESTRICTED. DISPATCH YK @ 13:02Z. REMOVED AND REPLACED #2 IDG IAW AMM 24-11-01. OPS CHECK GOOD.

Part: GENERATOR — MALFUNCTIONED (RIGHT) · airframe 79,352 hrs · 16,921 cycles

AFTER RIGHT ENG. START, R GEN OFF EICAS APPEARED. PERFORMED QRH PROCEDURE AND CONTINUED FLIGHT. PERFORMED BITE TEST IAW FIM 24-20. NO FAULTS NOTED AT THIS TIME.

Part: IDG — OVERSERVICED (RT GENERATOR) · airframe 79,337 hrs · 16,918 cycles

AFTER RIGHT ENGINE START, R GEN OFF EICAS MSG. PERFORMED QRH PROCEDURE AND CONTINUED WITH FLIGHT.(<P>T/S IAW FIM 24-20 F/T 801 AND FIM 24-20 F/T 804 TABLE 102. RESET BPCU AND RE-SERVICED IDG REF 12-15-02. AFTER FINDING IT TO BE OVER-SERVICED BY 3/4 OF QT,&NBSP; RESET IDG PER AMM 24-11-01. PERFORMED ENGINE RUN PER 72-00-00. RESET R GEN CONT SWITCH. R GEN CONT LIGHT EXTINGUISHED.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT GENERATOR) · airframe 79,332 hrs · 16,917 cycles

AFTER START, GOT "R GEN OFF". RECYCLED AND OPERATED NORMALLY. PERFORMED BITE TEST OK PER FIM 24-20. NO FAULTS NOTED AT THIS TIME.

Part: GCU — FAILED (RT GENERATOR) · airframe 79,321 hrs · 16,913 cycles

"R GEN OFF" ADVISORY AFTER R ENGINE START. RAN QRH AND CONTINUED NORMAL OPS. REMOVED AND REPLACED RH GCU IAW AMM 24-22-01. OPS&NBSP;CHECK GOOD AT THIS TIME.</P>)

Part: APU — MALFUNCTIONED · airframe 79,321 hrs · 16,913 cycles

WHEN STARTING RIGHT ENGINE, APU DUCT PRESSURE WENT FROM 30 PSI TO 10 PSI. ENGINE START W/IN PARAMETERS. PERFORMED OPS CHECK IAW AMM 71-00-00. OPS CHECK GOOD AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION (ISOLATION VALVE) · airframe 79,323 hrs · 16,914 cycles

RIGHT BLEED ISOLATION VALVE EICAS MESSAGE OCCURS WHEN THE VALVE IS PRESSED OUT. CYCLED RIGHT BLEED ISOLATION VALVE MULTIPLE TIMES PER AMM REF 36-11-00. NO FAULTS NOTED.

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 79,211 hrs · 16,878 cycles

LEFT MAIN FUEL PUMP INOP.(<P>TRANSFERRED TO MDDR 111871.</P><P>LP 1015740 - M4: LH MAIN FUEL PUMP OPS CHECK GOOD IAW AMM 28-22-00.&NBSP; THIS CLEARS DMI # 111871.&NBSP; MCC NOTIFIED.&NBSP; DISPATCH DP1540Z. </P>)

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 79,199 hrs · 16,874 cycles

"GCS" BUTTON ON WX RADAR WILL NOT STAY PRESS.(<P>TRANSFER TO MDDR 111815 IAW DDG 34-43-01 DUE DATE 15 SEP-19.</P><P>LP 1015739 - M3:&NBSP;REMOVED AND REPLACED WXR CONTROL PANEL WITH REPAIRED UNIT.&NBSP; OPS CHECK IS GOOD. REF 767 AMM 34-43-02.&NBSP; THIS CLEARS DMI# 111815.&NBSP; PLACARDS REMOVED. DISPATCH DP1540Z.</P>)

Part: UNKNOWN — MALFUNCTIONED (LT ENGINE) · airframe 79,157 hrs · 16,858 cycles

L ENGINE IN FLIGHT GOES TO GROUND IDLE, INSTEAD OF STAYING IN FLIGHT IDLE. EICAS MESSAGE IDLE DISAGREE.(<P>PERFORMED FIM TASK TREE 71-05 FAULT TREE&NBSP;846. RAN ENGINE&NBSP;BOTH ENGINES AND NO FAULTS NOTED AT THIS TIME. OPS CHECK NORMAL. NO FLIGHT IDLE IDLE MESSAGE AT THIS TIME. ENG RUN AMM REF 71-00-00.</P>)

Part: WINDOW — DEFECTIVE (COCKPIT) · airframe 79,123 hrs · 16,849 cycles

LEFT SIDE WINDOW EICAS&NBSP;(<P>REF LOG PAGE 1024257 ITEM 02: NO MESSAGE PRESENT AT THIS GROUND TIME. C/W BITE CHECK OF BOTH CONTROLLERS. NO FAULTS NOTED. LEFT SIDE WINDOW HEAT OPS GOOD AT THIS TIME REF FIM 30-41-00 FT 804.&NBSP;</P><P>REF LOG PAGE 1024259 ITEM M7: TRANSFERRED TO MDDR 111253 AS PER DDG 30-41-01-02 CAT "C"&NBSP;</P><P>LP 1015721 - M8: R&AMP;R L2 WINDOW IAW AMM 56-11-02. PERFORMED OPERATIONAL AND ANTI-ICE TEST IAW AMM 56-11-02-715-145 AMM 30-41-00. NO FAULTS NOTED AT THIS TIME. THIS ACTION CLEARS DMI 111253. MCC NOTIFIED AND PLACARDS REMOVED. WINDOW ASSY OFF PART (S/N: DL1, P/N: 141T4835-45)</P><P>LP 1015722: RE-OPENED MDDR 111253.</P><P>REF LP 1015727: R/R L2 WINDOW HARNESS PIGTAIL OPS CK GOOD.&NBSP;</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 79,121 hrs · 16,848 cycles

LEFT SIDE WINDOW CAUTION MESSAGE IN FLIGHT(<P>PERFORMED BITE CHECK IAW FIM 30-41 F/T 804 OPS CHECK GOOD</P>)

Part: ACTUATOR — MALFUNCTIONED (AC BAY) · airframe 79,111 hrs · 16,845 cycles

LEFT PACK EXHAUST DOOR DOES NOT OPEN(<P>REMOVED AND REPLACED EXHAUST DOOR ACTUATOR IAW AMM 21-53-04 OPS CHECK NORMAL</P>)

Part: IDG — MALFUNCTIONED (RT ENGINE) · airframe 79,099 hrs · 16,841 cycles

EICAS MSG "RT GEN DRIVE".(<P>RT GENERATOR DEFERRED PER MEL 24-11-01, REF MDDR 110882.</P><P>REMOVED AND REPLACED&NBSP;RT IDG IAW AMM 24-11-01 OPS AND LEAK CHECK REQUIRED. OPS AND LEAKED CHECKED OK ON ENG RUN REF AMM 71-00-001. THIS CLOSES MDDR 110882. PLACARD REMOVED AND MCC ADVISED.<BR /></P>)

Part: CONTROLLER — FAILED (WINDOW HEAT) · airframe 79,044 hrs · 16,825 cycles

L SIDE WINDOW" EICAS MESSAGE 2 HOURS INTO FLIGHT. QRH CHECKLIST CYCLES WINDOW HEAT SWITCH. EICAS MESSAGE EXTINGUISHED. L2 WINDOW HEAT INOP.(<P>PERFORMED FLIGHT COMPARTMENT WINDOW ANTI ICE TEST PER AMM 30-41-00. OPS CHECK GOOD. T/S PER WDM 30-41-12. PERFORMED CONTINUITY CHK ON D5872 PIN 1 TO J8C, PIN 2 TO J8D. NO FAULTS. PIN 3 TO J6A, PIN 4 TO J6B. NO FAULTS. PIN 5 TO J7A, PIN 6 TO J7B. NO FAULTS. CONTINUITY CHK FM D5872 TO D4294 PIN 1 TO PIN 11. NO FAULTS. PIN 6 TO PIN 14. NO FAULTS. PIN 5 TO PIN 13 NO FAULTS. PERFORMED WIRE INTEGRITY CHK W/ MEGGAR. NO FAULTS NOTED. T/S L2 WINDOW IAW FIM 30-41-00 ALL CONNECTIONS CLEAN AND SECURE. WINDOW HEAT ELEMENT LOOP RESISTANCE 17.3 RANGE 17.43-23.59 WINDOW CONNECTORS D1920 CD SENSOR D1918. 325 RANGE 165-375 OHMS. R & R WHCU IAW AMM 30-41-01, OPS CHECKED GOOD.

Part: CONTROL UNIT — INOPERATIVE (WINDOW HEAT) · airframe 83,361 hrs · 12,096 cycles

LEFT SIDE WINDOW EICAS MSG. REMOVED AND REPLACED THE LT SIDE WINDOW HEAT CONTROL UNIT IAW AMM 30-41-01. OPS CHECKED GOOD.

Part: FILTER — UNKNOWN (FUEL SYSTEM) · airframe 79,003 hrs · 16,811 cycles

R ENG FUEL FILT EICAS MESSAGE INTERMITTENT(<P>REMOVED AND REPLACED RH ENGINE FUEL FILTER IAW B767 AMM 73-11-03. PERFORMED LEAK CHECK AND WET MOTOR IAW AMM 71-00-00. OPS CHECK GOOD.</P>)

Part: HEATER — INOPERATIVE (L2 WINDOW) · airframe 78,979 hrs · 16,805 cycles

L-2 WINDOW HEAT INOP.(<P>TRANSFERRED TO MDDR #110216.<BR /></P><P>LP 1015670 - M6:&NBSP;PER WDM 30-41-12 SHEET 1-2, REMOVED CONNECTOR D5872P. MEASURED VOLTAGE B/W PINS 2&AMP;1 SHOWS 2.3 V AC. WHEN THE CONNECTOR WAS CONNECTED BACK THE INOP LIGHT EXTINGUISHES. MCC NOTIFIED. DMI REMAINS OPEN FOR MONITORING PER MCC.</P><P>LP 1015674: ACCOMPLISHED FIM 30-41 FT 802 &AMP; 804, RES CHECK NORMAL AND WINDOW HEAT CONTROLLER, NO FAULTS. WINDOW HEAT OPERATION IS NORMAL. THIS CLEARS MDDR 110216. LC @ 23:25.</P>)

Part: CONNECTOR — DIRTY (L2 WINDOW HEAT) · airframe 78,952 hrs · 16,797 cycles

L2 WINDOW HEAT INOP. FOUND LOOSE CONNECTION AT C/P D5872P. CLEANED AND SECURED REF WDM 30-41-02. PERFORMED OPS TEST IAW AMM 30-41-00-715-001, OPS TEST GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT WINDOW) · airframe 78,940 hrs · 16,794 cycles

L SIDE WINDOW ANNUNCIATED IN FLIGHT.&NBSP;(<P>PERFORMED OPERATIONAL TEST I.A.W BITE TEST IN WINDOW HEAT CONTROL UNIT. FOUND GOOD I.A.W AMM 30-41-00.</P>)

Part: WARNING LIGHT — FALSE ACTIVATION (WINDOW HEAT) · airframe 78,923 hrs · 16,788 cycles

RH WINDOW HEAT INOP. PERFORMED WINDOW DE-ICE OPS TEST REF AMM 30-41-00, OPS CKD GOOD. ALSO PERFORMED FIM 30-41 FT 804 & 805. NO DEFECTS, OPS CKD GOOD.

Part: ANTI-ICE SYSTEM — FAILED (RT WINDOW) · airframe 78,919 hrs · 16,787 cycles

R/H WINDOW HEAT INOP(<P>PERFORMED WINDOW DE-ICE TEST I.A.W. AMM 30-41-00 AND BITE TEST OF R/H FWD AND R/H SIDE WINDOWS IAW AMM FIM 30-41 F/T 804. NO DEFECTS NOTED, OPS CHECK GOOD.</P>)

Part: WINDOW — FAILED (LT COCKPIT) · airframe 78,883 hrs · 16,778 cycles

L-3 WINDOW HEAT INOP. PERFORMED BITE CHECK OF RIGHT FORWARD/ LEFT SIDE WINDOW HEAT CONTROL UNIT AND FOUND IT TO BE FAULTING 'L3 WINDOW SENSOR' REF AMM 30-41-01. T/S PER FIM TASK 30-41 FAULT. MAIN AND SPARE SENSE OHMED GOOD @ 293.7. CHECKED J9-J12 AT L3 WINDOW. SUSPECT BAD WINDOW SWAPPED. DMI REMAINS OPEN. ;REMOVED L3 WINDOW. INSPECTED WINDOW FRAME, NO DEFECTS NOTED. INSTALLED SERVICEABLE WINDOW ASSY PER AMM 56-11-10. WINDOW HEAT OPS NORMAL IAW AMM 30-41-00.

Part: WINDOW — DAMAGED (L3) · airframe 78,856 hrs · 16,770 cycles

LH ## WINDOW HAS BUBBLES.(<P>R/R LH #3 WINDOW IAW AMM 56-11-10. WINDOW HEAT TEST OK IAW AMM 30-41-00.</P>)

Part: DUCT — TORN (COOLING) · airframe 78,856 hrs · 16,770 cycles

TWO AIR COOLING DUCTS TORN ON APU.(<P>R/R BOTH AIR DUCTS COOLING DUCTS IAW AMM 49-51-00. NO LEAKS NOTED.</P>)

Part: SAFETY EQUIP — MISSING · airframe 78,795 hrs · 16,751 cycles

EMERGENCY GLOVES MISSING(<P>INSTALLED FIRE GLOVES PER LOPA FT 25-EEL REV 11.<BR /></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (APU GENERATOR) · airframe 78,579 hrs · 16,685 cycles

AFTER PUSHBACK RECEIVED AN APU GEN OFF MESSAGE, ONE RESET ATTEMPT AFTER 5 MINUTES, RECEIVED THE MESSAGE AGAIN. TROUBLESHOT IAW FIM 49-11 F/T 987. RESET THE APU GENERATOR, RAN APU AND APPLIED A LOAD TO THE SYSTEM, NO MESSAGE OR FAULTS NOTED.

Part: OIL SYSTEM — LOW (IDG) · airframe 78,515 hrs · 16,662 cycles

AFTER ENGINE START R GEN DRIVE EICAS WITH R GEN DRIVE DISC LIGHT ILLUMINATED ON OVERHEAD PANEL. LIGHT REMAINED ON APPROXIMATELY 45 SEC THEN WENT OUT.(<P>PERFORMED FIM TASK 24-20 FT 801, FOUND IDG LOW IOL PRESSURE. SERVICED IDG PER 12-13-03-613-027 AND PERFORMED OPERATIONAL TEST OF THE RIGHT IDG PER AMM 24-11-00-715-006 NO FURTHER FAULTS NOTED.</P>)

Part: IDG — OVERSERVICED (RT GENERATOR) · airframe 78,485 hrs · 16,653 cycles

AFTER ENGINE START RIGHT GENERATOR DRIVE EICAS WITH DRIVE LIGHT ILLUMINATED ON OVERHEAD PANEL. REMAIN ON FOR OVER 1 MINUTE THEN WENT OUT.&NBSP;(<P>FOUND IDG TO BE OVER SERVICED, PERFORMED IDG OPERATIONAL TEST IAW AMM 24-11-00-715-006. TEST PASS NO FURTHER DEFECTS NOTED AT THIS TIME.&NBSP;</P>)

Part: FIRE LOOP — ABNORMAL (RT ENGINE) · airframe 78,454 hrs · 16,643 cycles

R ENG FIRE LP 2 STATUS MESSAGE(<P>TRANSFER TO MDDR 106994 IAW&NBSP; DDG 26-11-01-01</P><P>LP 1040431: R/R R/H ENGINE UPPER AFT FIRE LOOP IAW AMM 26-11-02, ENGINE FIRE TEST IAW AMM 26-11-00, NO FAULTS NOTED, NO MSG NOTED @ THIS TIME. THIS ACTION CLOSES MDDR 106994 AND PLACARDS REMOVED.&NBSP;</P>)

Part: APU — MALFUNCTIONED · airframe 78,438 hrs · 16,637 cycles

APU FAULT.(<P>SUSPECT APU COLD SOAKED ALLOWED SUFFICENT GROUND TIME PERFORMED 3 SUCCESSFUL STARTS NO FAULTS OK FOR SERVICE IAW AMM 49-11-00.<BR /></P><P><BR /></P>)

Part: WIRE — MISSING (SWITCH COVER) · airframe 78,443 hrs · 16,639 cycles

PRE-FLIGHT INSP FOUND R IDG SWITCH COVER SHEER WIRE MISSING , ALSO FOUNF R GEN FIELD LIGHT(<P>RECONNECTED R IDG PER AMM 24-11-01 OPS TEST OK FIELD LIGHT OUT&NBSP;</P>)

Part: START VALVE — FAULTY (LT ENGINE) · airframe 78,371 hrs · 16,615 cycles

IN FLT L STARTER CUTOUT AND L ENGINE STARTER MESSAGE DISPLAY NOTE LEFT ENGINE VALVE LIGHT DOES NOT DISPLAY IN ADDITION LEFT ENGINE BLEED VALVE EICAS DISPLAYED TWICE BUT CLEARED STARTER MESSAGE DID NOT CLEAR. REMOVED AND REPLACED LEFT ENGINE START VALVE IAW AMM 80-11-02 OPS CHECK NORMAL.

Part: FUEL FILTER — DEFECTIVE (LT ENGINE) · airframe 78,358 hrs · 16,611 cycles

LT ENG FUEL FILTER STATUS MESSAGE. NO ABNORMAL ENG INDICATIONS OBSERVED.(<P>R/R FUEL FILTER PER FIM 73-11 FT 803. RAN ENGINE LEAK CHECK GOOD. OPS CHECKS GOOD MSG CLEARED.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 78,276 hrs · 16,581 cycles

STATUS MESSAGE AFT EQUIP EXHAUST FAN(<P>PERFORM FIM 21-58-PERFORMED OPS CHECK TEST OK PER AMM 21-26-00</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 78,221 hrs · 16,561 cycles

RT ENGINE FIRE LOOP 2 EICAS MESSAGE(<P>TRANSFER TO MDDR 105598 IAW MEL 26-11-01-01</P><P>LP 1047887-M3 PERFORMED OPERATIONAL TEST&NBSP; FIRE LOOP SYSTEM IAW AMM 26-11-00 NO FAULTS FOUND&NBSP; OPS CHECK GOOD CLEARED MDDR 105598 PLACARD REMOVED&NBSP;</P>)

Part: OXYGEN MASK — INOPERATIVE (COCKPIT) · airframe 78,237 hrs · 16,566 cycles

SUPERNUMERARY SEAT RIGHT O2 MASK INOP.(<P>DEFERRED. MDDR 105634. SECURED O2 MASK AND PERFORMED OPS CHECK IAW AMM 35-11-51, OPS NORMAL, MDDR CLOSED.<BR /></P>)

Part: CIRCUIT CARD — MALFUNCTIONED (RT ENG FIRE LOOP) · airframe 78,123 hrs · 16,524 cycles

RT ENG FIRE LOOP 2 EICAS MSG(<P>TRANSFER TO MEL 26-11-01-01 CAT C DUE 29DEC18 MMDR# 104772.</P><P>PERFORMED VISUAL INSPECTION OF RH ENGINE FIRE LOOP, NO DEFECTS NOTED R/R R ENGINE FIRE LOOP CARD (M684) IAW AMM 26-10-01 OPS CHECK GOOD, THIS CLEARS NDDR 104772.</P>)

Part: SWITCH — UNKNOWN (FUEL PUMP) · airframe 78,133 hrs · 16,527 cycles

RH CTR FUEL PUMP MESSAGE ON EICAS.(<P>TRANSFERRED TO MDDR# 104786 DUE 29DEC18, CAT "C" MXCTRL RA OPENED CB'S @ P6F21 "RIGHTFUEL OTBD PUMP" PER MEL 28-22-02A. PLACARD INSTALLED.<BR /></P><P><BR DATA-MCE-BOGUS="1" /></P><P>R&AMP;R FUEL PRESSURE SWITCH IAW AMM 28-42-01, OPS CHECKS IS GOOD AT THIS TIME, NO FURTHER DEFECTS AT THIS TIME THIS CLEARS DMI PLACARDS REMOVED.</P>)

Part: GCU — MALFUNCTIONED (APU) · airframe 77,985 hrs · 16,472 cycles

&NBSP;APU WILL NOT SUPPLY ELECTRICAL POWER.(<P>PLACED ON MDDR 103295,REMOVED&NBSP; AND REPLACED APU GCU IAW AMM 24-22-02 OPS CHECK NORMAL ,THIS CLEARS MDDR 103295.</P>)

Part: DUCT — UNKNOWN · airframe 77,969 hrs · 16,466 cycles

BEFOREE ENG START DUCT PRESSURE WAS 15 PSI. AS #2 ENG WAS STARTING DUCT PRESSURE CLIMBED TO 30 PSI(<P><SPAN>RAN / BOTH ENG'S TO OPS CHECK DUCT PRESSURE. OPS CHECK GOOD AT THIS TIME IAW AMM / 36-21-00 &AMP; 72-10-00</SPAN></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (DUCT PRESSURE) · airframe 77,960 hrs · 16,463 cycles

PRIOR TO ENGINE START BOTH DUCT PRESSURES FLUCTUATE BETWEEN 15 AND 20 PSI&NBSP;(<P>PERFORMED OPS CHECK OF PNEUMATIC SYS IAW AMM 49-52-00 OPS CHECKED GOOD 35 PSI STEADY&NBSP; WITH NO PACKS RUNNING OPS CK GOOD&NBSP;</P>)

Part: IDG — FAILED (RIGHT) · airframe 77,905 hrs · 16,442 cycles

RIGHT GENERATOR FAILED IN FLT. R & R THE RT ENGINE IDG IAW AMM 24-11-01,OPS CHECKED GOOD.

Part: APU — UNKNOWN · airframe 77,905 hrs · 16,442 cycles

ON STARTING FIRST ENGINE(#2), APU VERY SLOW TO INCREASE PRESSURE TO START MINIMUM.(<P>PERFORMED DRY MOTOR RUN ON NO.2 ENG. PRESSURE HELD NORMAL AT 30 PSI, OPS CKS. OK IAW 71-00-00.</P>)

Part: CONTROL UNIT — INOPERATIVE (OXYGEN PRESSURE) · airframe 77,874 hrs · 16,430 cycles

CREW OXYGEN PRESSURE INDICATOR INOPERATIVE. R & R THE CREW OXYGEN AVERAGE UNIT IAW 35-11-06. OPS CHECKED GOOD.

Part: ADC — MALFUNCTIONED (RIGHT) · airframe 77,801 hrs · 16,403 cycles

DURING TAXI OUT, RECEIVED A LEFT EEC ENGINE MODE AND RT EEC MODE ADVISORY MESSAGE. REMOVED AND REPLACED RIGHT ADC IAW AMM 34-12-01. OPS CHECKED GOOD.

Part: INDICATION SYS — INOPERATIVE (CREW OXYGEN) · airframe 77,825 hrs · 16,412 cycles

CREW OXYGEN INDICATION INOPERATIVE. PERFORMED AN INSPECTION OF THE OXYGEN BOTTLE IAW AMM 35-11-00, OPS CHECKED GOOD.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 77,737 hrs · 16,381 cycles

CABIN ALT AUTO 1 STATUS MESSAGE APPEARS AFTER AC TRANSFER DURING ENGINE START. ACCOMPLISHED CABIN CONTROLLER BITE PER FIM 21-31-809, FAULTED SELECTOR, NO FAULT INDICATED WHEN SELECTED VERIFY. FAULT CLEARED. TRANSFERED POWER SEVERAL TIMES 24-22-00 NO FAULTS NOTED.

Part: FIRE LOOP — BROKEN (RT ENGINE) · airframe 77,769 hrs · 16,392 cycles

RT ENGINE AFT FIRE LOOP TERMINAL BROKEN. R&R RT ENG FIRE LOOP IAW AMM 26-11-02. OPS CHECK NORMAL.

Part: FIRE LOOP — DAMAGED (RT ENGINE) · airframe 77,769 hrs · 16,392 cycles

RT ENG FIRE LOOP TEMP REPAIR. INSTALLED TEFLON TUBING ON EXPOSED PORTIONS OF WIRE W5324-455R16 IAW AMM 26-11-21.

Part: BATTERY — NOT REPORTED (MAIN) · airframe 77,769 hrs · 16,392 cycles

MAIN AIRCRAFT BATTERY NEEDS REPLACEMENT. R&R AIRCRAFT MAIN BATTERY IAW 24-31-01. OPS CHECK NORMAL.

Part: ECU — MALFUNCTIONED (APU) · airframe 77,671 hrs · 16,357 cycles

APU INOP. REMOVED AND REPLACED APU ECU IAW AMM 49-61-05 OPERATIONAL CHECK NORMAL.

Part: TRANSDUCER — FAULTY (APU) · airframe 77,718 hrs · 16,374 cycles

APU INOP. REMOVED AND REPLACED TRANSDUCER MOTIONAL MONOPOLE, APU OPS CHECK NORMAL IAW AMM 49-61-02.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 77,682 hrs · 16,361 cycles

STATUS MESSAGE AFT EQ EXH FAN NR 2. PERFORMED FIM 21-26-FT 8069 NO FAULTS NOTED AT THIS TIME.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 77,657 hrs · 16,352 cycles

LT ENG OIL PRESSURE LIGHT NOT ILLUMINATED. RELAMPED PER AMM 33-16-02.

Part: HSI — MALFUNCTIONED (COCKPIT) · airframe 77,657 hrs · 16,352 cycles

"WXR DSPY" MESSAGE ON CA HSI INTERMITTENTLY THROUGHOUT FLIGHT. REPEAT WRITE-UP. R&R HSI.

Part: DISPLAY — INTERMITTENT (COCKPIT) · airframe 77,657 hrs · 16,352 cycles

WX DISPLAY ( WXR DSPY) INTERMITTENT ON PIC HSI (+TERR DISY+TCAS). PERFORMED FIM TASK 34-22 FT 804, NO FURTHER DEFECTS NOTED. NO MX PROCEDURE NECESSARY FOR INTERMITTENT FAILURE.

Part: GENERATOR — FAULTY (COCKPIT) · airframe 77,657 hrs · 16,352 cycles

WEATHER DISPLAY (WXR DSPY) INTERMITTENT ON CAPT'S HSI. R&R GENERATOR ASSY-ELECTRONIC FLT IAW AMM 34-22-01, PERFORMED OPS CK, OPS CHECK SATISFACTORY.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 77,657 hrs · 16,352 cycles

YELLOW " WXR DSPY" MESSAGE DISPLAYED ON CAPT'S EHSI NUMEROUS TIMES, BUT INTERMITTENTLY. PERFORMED TEST OF WEATHER RADAR SYSTEM IAW AMM 34-43-00, OPS TEST GOOD AT THIS TIME.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 77,633 hrs · 16,344 cycles

AFT EQ EXH FAN STATUS. COMPLIED WITH SYSTEM CK, IAW AMM CH 21-58-41 NO FAULTS NOTED ERASE PROCEDURE IAW MM 31-41-00.

Part: ECU — FAULTY (APU) · airframe 77,608 hrs · 16,333 cycles

APU INOP. R&R APU ECU IAW 49-61-05 OPS GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 77,514 hrs · 16,299 cycles

STATUS MESSAGE RT ENG OH LP 2. PERFORMED OPERATIONS TEST FOUND NO FAULTS. CLEARED MESSAGE AND OPS CHECKED GOOD IAW AMM 26-15-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 77,496 hrs · 16,294 cycles

AFT EQ EXH FAN 2 STATUS MESSAGE DISPLAYED. RECYCLED AFT EQ EXH FAN 2 BREAKER MESSAGE CLEARED IAW AMM 21-58-41.

Part: SOLENOID — FAILED (APU) · airframe 77,482 hrs · 16,289 cycles

APU INOP. REMOVED AND REPLACED APU FUEL SOLENOID PER AMM 4931-03. PERFORMED LEAK & OPS CHECK.

Part: TRANSMITTER — FAULTY (LT ENGINE) · airframe 77,445 hrs · 16,276 cycles

UPON INSPECTION FOUND LEFT ENG OIL PRESSURE LIGHT INOP. REMOVED AND REPLACED OIL PRESS TRANSMITTER. OPS AND LEAK CHECK NORMAL AMM 79-32-01.

Part: DETECTOR — DEFECTIVE (RT ENGINE) · airframe 77,440 hrs · 16,274 cycles

INTERMITTENT R FIRE LOOP 2 STATUS MSG. REMOVED AND REPLACED DETECTOR ASSY UPPER AFT IAW AMM 26-11-02 OPS CHECK NORMAL.

Part: BLEED AIR SYS — FLUCTUATES (APU) · airframe 77,407 hrs · 16,263 cycles

APU DUCT PRESSURE BEFORE ENGINE START FLUCUATES BETWEEN 15-T0 22 PSI. PERFORMED AIR SUPPLY DISTRIBUTION OPS TEST IAW AMM 36-11-00 NO DEFECTS NOTED NO FLUCTUATION NOTED AT THIS TIME.

Part: GENERATOR — INOPERATIVE (APU) · airframe 77,397 hrs · 16,260 cycles

APU GEN INOP. REMOVED AND REPLACED APU GENERATOR IAW AMM 24-21-01. OPS CHECK GOOD.

Part: START VALVE — FAULTY (RT ENGINE) · airframe 77,397 hrs · 16,260 cycles

RT STARTER INOP. REMOVED AND REPLACED START VALVE IAW AMM 80-11-02 OPS AND LEAK CHECK GOOD.

Part: UNKNOWN — MALFUNCTIONED (COCKPIT) · airframe 77,402 hrs · 16,261 cycles

LT ENG OIL PRESS INDICATOR LIGHT NOT ILLUMINATED W/ ENGINE SHUTDOWN. PERFORMED ENGINE ILDE RUNS IAW AMM 71-00-00. OPS CHECK GOOD AT THIS TIME.

Part: WIRE — DAMAGED (FIRE LOOP) · airframe 77,365 hrs · 16,248 cycles

RT ENG FIRE LOOP 2 INTERMITTENTLY DISPLAYED(STATUS MESSAGE). REMOVED AND REPLACED WIRE W5306-455R-16 AT RT ENG REPLACED WITH NEW BMS513-67 WIRE MATERIAL, RE CLAMPED & RETERMINATED WIRE TO ENG LOOP 2 TS682% A & TS683 A IAW WDM 26-11-21, SWPM 20-10-12 & 20-10-15. OPS CHECK GOOD IAW WDM 26-11-00. NO FAULTS NOTED AT THIS TIME.

Part: FIRE LOOP — DAMAGED (RT ENGINE) · airframe 77,397 hrs · 16,260 cycles

RIGHT ENGINE FIRE LOOP2 PERMANENT REPAIR. C/W HIGH TEMP TAPE IAW SWP 20-10-13, WIRE W-5324-455R-16 TO BE REPLACED DURING THE NEXT A CHECK.

Part: GENERATOR — FAULTY (APU) · airframe 77,361 hrs · 16,247 cycles

APU LOW OIL SHUTDOWN. REMOVED AND REPLACED APU GENERATOR IAW AMM 24-21-01. OPS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 77,351 hrs · 16,243 cycles

RIGHT ENGINE FIRE LOOP 2 STATUS MESSAGE DISPLAYED AFTER NR 2 ENGINE START. NO CURRENT FAULTS, PERFORMED FIRE/OVERHEAT TEST IAW AMM 26-11-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 77,310 hrs · 16,230 cycles

RT ENG NR 2 FIRE LOOP STATUS MESSAGES, INTERMITTENT DURING FLIGHT. PERFORMED FIRE DETECT OPS CHECK IAW AMM 26-11-00, RT ENG LOOPS. NO DEFECTS NOTED.

Part: SENSOR — FAULTY (APU) · airframe 77,306 hrs · 16,228 cycles

APU AUTO SHUT DOWN. BITE CODE "REVERSE FLOW". T/S IAW FIM 49-11 FT 987. R&R LC TT SENSOR IAW AMM 49-61-03. APU OPS CHK GOOD PER 49-00-00. ERASED ECU PER FIM 49-11 FT 987. NO DEFECTS AT THIS TIME.

Part: CIRCUIT CARD — FAULTY (FIRE WARNING) · airframe 77,300 hrs · 16,225 cycles

ONBOARD FLIGHT CREW REPORTED RT ENGINE FIRE LP 2 STATUS MESSAGE DURING NR 2 ENGINE START. MSG CLEARED SHORTLY AFTER. REMOVED AND REPLACED NR 2 ENGINE LOOP 2 CONTROL/FIRE OVERHEAT CARD, PRECAUTIONARY OPERATIONAL CHECKOF ENG/APU CARGO FIRE/OVERHEAT TESTED GOOD NO DEFECTS NOTED PER AMM 26-11-03 -012-001.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 77,296 hrs · 16,223 cycles

RT ENGINE FIRE LOOP 1 STATUS MESSAGE DISPLAYED AFTER ENGINE START, MESSAGE EXTINGQUISHED. FLIGHT PERFORMED SYSTEM TEST FIRE DETECTION SYSTEM IAW AMM 26-11-00, OPS CHECK GOOD.

Part: FIRE LOOP — DEFECTIVE (RT ENGINE) · airframe 77,274 hrs · 16,216 cycles

RT ENG FIRE LOOP 2 INOP. INSPECTED AND RESISTANCE CHECK OF RT ENG LOWER AFT DETECTOR FAILING WHEN SHAKING/NOT WITHIN LIMITS. REPLACEDLOWER AFT DETECTOR IAW AMM 26-11-02. OPS CHECK IAW AMM 26-22-00, TEST OK.

Part: STATUS MESSAGE — ACTIVATED (COCKPIT) · airframe 77,258 hrs · 16,211 cycles

RIGHT ENGINE FIRE LOOP 2 STAUS MESSAGE. TRANSFERED TO MDDR 97917 IAW MEL 26-11-01-01 CAT C PLACARD INSTALLED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 77,248 hrs · 16,207 cycles

STATUS MESSAGE RT ENG FIRE LOOP 2 AFTER ENGINE START, MSG GOES AWAY AFTER TAKE OFF. C/W FIM 26-11 FAULT TREE 806 NO FAULTS AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 77,258 hrs · 16,211 cycles

RT ENG FIRE LOOP NR 2 WAS INTERMITTENT DURING ALL PHASES OF A/C OPERATION AFTER ENG START. T/S IAW FIM 26-11 FT 804 & WDM 26-11-21. LOOP 2 RT ENG RESISTANCE VALVE FALLS IN RANGE PER FIG 104 SHEET II. INSULATION CHECK IS WITHIN RANGE PER FIG SHEET II. NO DEFECTS NOTED AT THIS TIME.

Part: STARTER — MALFUNCTIONED (LT ENGINE) · airframe 77,258 hrs · 16,211 cycles

LT STARTER WOULD NOT CUT OUT. R&R LT ENGINE STARTER IAW AMM 80-11-01. OPS GOOD.

Part: CIRCUIT CARD — FAULTY (FIRE WARNING) · airframe 77,211 hrs · 16,194 cycles

RT ENG FIRE LP2 STATUS MSG ON PUSHBACK. REMOVED AND REPLACED AFOLT CARD M10274, P/N 285N0027-136 IAW 26-10-01. OPS CHECK GOOD AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 77,190 hrs · 16,186 cycles

RIGHT ENGINE FIRE LOOP 2 STATUS MSG. PERFORMED FIM TASK 26-11 FAULT TREE 806, NO FAULT NOTED. OK FOR SERVICES.

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 77,174 hrs · 16,180 cycles

RADAR WX DEPLICTION VERY WEAK NEED FULL GAIN ON SYSTEMS 1 AND 2. PERFORMED BITE TEST AS PER FIM 34-43 FAULT TREE 205 TEST PASS NO FAULTS FOUND.

Part: STARTER — WORN (APU) · airframe 77,080 hrs · 16,148 cycles

APU STARTER MOTOR BRUSH WEAR INDICATOR IS WORN. REMOVED AND REPLACED STARTER IAW AMM 49-41-11.

Part: FEEDER CABLE — DAMAGED (IDG) · airframe 77,080 hrs · 16,148 cycles

LEFT AND RIGHT IDG'S POWER FEEDERS INSULATION DAMAGED. REMOVED AND REPLACED LEFT AND RIGHT IDG'S POWER FEEDER INSULATION IAW AMM 20-30-14.

Part: STATUS MESSAGE — INTERMITTENT (COCKPIT) · airframe 77,075 hrs · 16,145 cycles

RT ENG FIRE LOOP 2 STATUS INTERMITTENT. TROUBLESHOOT PER FIM 26-11 FAULT TREE 806. NO DEFECTS NOTED AT THIS TIME. OPS CHECKS GOOD. A/C OK FOR SERVICE.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 77,018 hrs · 16,124 cycles

AFTER BLOCK OUT FIRST ENGINE START, RT ENGINE FIRE LOOP STATUS MESSAGE, WENT OUT AFTER T/O. TROUBLE SHOT NR 2 ENGINE FIRE LOOP IAW FIM 26-11 F/T 806, NO DEFECTS NOTED. OPS CHECK GOOD AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 77,016 hrs · 16,122 cycles

AFTER ENGINE START STATUS MSG, RT ENG FIRE LP 2 DISPLAYED ON LOWER EICAS. PERFORMED OPS CHECK OF RIGHT ENGINE FIRE LOOP IAW AMM 26-11-00. OPS CHECK GOOD AT THIS TIME, A/C OK FOR CONTINUED SERVICE.

Part: APU — INOPERATIVE (APU BAY) · airframe 76,983 hrs · 16,110 cycles

APU INOP. REMOVED AND REPLACED APU IAW AMM 49-11-01.

Part: FILTER — DEFECTIVE (APU) · airframe 76,961 hrs · 16,099 cycles

AFTER 30 MINS APU AUTO SHUTDOWN ON RAMP. REMOVED AIR FROM IGV ACTUATOR (LOCKED) AND REINSTALLED ALSO REPLACED APU FUEL FILTER OK PERFORMED APU OPS CHECK OK

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 76,948 hrs · 16,094 cycles

LEFT PACK TEMP EICAS MESSAGE DISPLAYED WHEN LEFT PACK IS PLACED IN AUTO. PERFORMED BITE TEST OF PACK TEMP CONTROLLER. NO DEFECTS NOTED. PERFORMED OPS TEST OF L PACK IN AUTO. NO DEFECTS NOTED. NO EICAS MESSAGE SHOWING REF AMM 21-51-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 76,948 hrs · 16,094 cycles

AFT EQ EXH FAN 2 STATUS DISPLAYED. PERFORMED AFT EQ FAN TEST REF AMM 21-58-41. NO DEFECTS NOTED. NO EICAS MESSAGE SHOWING.

Part: FILTER — DEFECTIVE (RT ENGINE) · airframe 76,960 hrs · 16,097 cycles

RECD RT ENG FUEL F2LT EICAS MOMENTARILY THEN R ENG FUEL F2LT STATUS MSG THAT REMAINED. PER FIM 73-11 FT 803 R&R RT L ENG FUEL FILTER IAW AMM 73-11-03 & DIFF PRESS SWITCH IAW AMM 73-34-01 OPS CKD. LEAK CKD GOOD.

Part: BRACKET — NOT REPORTED (IGV) · airframe 76,911 hrs · 16,083 cycles

APU SHUTDOWN, WOULD NOT RESTART, WENT TO 48% AND SHUTDOWN. REMOVED AND REPLACED IGV ACTUATOR BRACKET IAW AMM 49-52-02. OPS CHECKED NORMAL,

Part: CONTROLLER — MALFUNCTIONED (LT ENGINE) · airframe 76,881 hrs · 16,069 cycles

STATUS MESSAGE FOR THE LEFT ENGINE HPSOV. CONFIRMED THE FAULT ON THE LT HPC IAW FIM 36-10 FT 833. REMOVED AND REPLACED THE LEFT ENGINE HPSOV CONTROLLER IAW AMM 36-11-08. OPS CHECKED GOOD.

Part: STATUS MESSAGE — FALSE ACTIVATION (LT ENGINE) · airframe 76,866 hrs · 16,064 cycles

STATUS MESSAGE FOR THE LEFT ENGINE HP SOV. PERFORMED FIM 36-20-FT 804, NO FAULTS INDICATED. MESSAGE CLEARED, NO HISTORY NOTED.

Part: CONTROL UNIT — MALFUNCTIONED (APU) · airframe 76,815 hrs · 16,050 cycles

APU INOPERATIVE. REMOVED AND REPLACED APU CONTROL UNIT IAW AMM 49-61-05, OPS CHECKED GOOD.

Part: FILTER — NOT REPORTED (APU OIL SYS) · airframe 76,813 hrs · 16,047 cycles

APU FAILED TO START AFTER LANDING. REMOVED AND REPLACED SCAVENGE FILTER IAW AMM 49-27-03 OPS AND LEAK CHECKED GOOD.

Part: APU — MALFUNCTIONED · airframe 76,765 hrs · 16,031 cycles

APU INOPERATIVE. INSPECTED APU AND CLEARED THE MESSAGE ON EICAS, PERFORMED BITE ON ECU, NO FAULTS FOUND. STARTED APU 3 TIMES, ALSO RAN PACKS AND APPLIED ELECTRICAL LOAD, ALL OPS NORMAL IAW AMM 49-11-00.

Part: FILTER — FAULTY (LT ENGINE) · airframe 76,758 hrs · 16,029 cycles

LT ENG FUEL FILTER STATUS. R&R LT ENG FUEL FILTER ELEMENT UNIT IAW AMM 73-11-03. MESSAGE CLEARED. NO LEAKS NOTED AT THIS TIME.

Part: CLUTCH — MALFUNCTIONED (APU) · airframe 76,745 hrs · 16,025 cycles

APU INOP ER OPERATIONS NOT ALLOWED. REMOVED AND REPLACED CLUTCH ASSY IAW 49-41-06. 49-41-01. OPS CHECKED NUMEROUS TIME. NO FAULTS NOTED.

Part: VALVE — INOPERATIVE (A/C PACK) · airframe 76,670 hrs · 16,000 cycles

ZONE TRIM AIR MODULATING VALVE GAUGE FLUCTUATES ERRATICALLY EVERY TIME VALVE MOVES. OPS CHECKED THE A/C PACKS IAW AMM 21-61-00. FOUND ZONE TRIM VALVE TO BE INOPERATIVE.

Part: GAUGE — ERRATIC (CABIN TEMP) · airframe 76,670 hrs · 16,000 cycles

COLD WARM GAUGE FOR TEMP CONTROL FLUCTUATES ERRADICALLY. PERFORMED AN OPS CHECK OF THE PACKS. OPS CHECKS GOOD IAW AMM 21-61-00.

Part: SWITCH — FAILED (FUEL PUMP) · airframe 76,629 hrs · 15,987 cycles

LEFT AFT FUEL PUMP ON SHUTTER DOES NOT CLOSE WHEN SELECTED. REMOVED AND REPLACED THE PUMP SELECTOR PANEL LEFT AFT SWITCH IAW SWPM 20-84-15. OPS CHECKED NORMAL.

Part: WIRE — BROKEN (ASM) · airframe 76,591 hrs · 15,977 cycles

RIGHT ENGINE WILL NOT INDICATE RUNNING ON ASM PROGRAM. REPAIRED A BROKEN WIRE IAW WDM 36-11-52.

Part: VALVE — FAILED (LT PACK TEMP) · airframe 76,573 hrs · 15,972 cycles

LEFT PACK TEMP ILLUMINATED ON APPROACH. REMOVED AND REPLACED THE LT PACK TEMP VALVE IAW AMM 21-51-12, OPS CHECKED OK.

Part: TRU — MALFUNCTIONED (APU) · airframe 76,560 hrs · 15,969 cycles

APU FAULT. REMOVED AND REPLACED THE APU TRU IAW AMM 24-32-04, OPS CHECKED NORMAL.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 76,545 hrs · 15,965 cycles

STRANGE ODOR APPEARED, LIKE BURNING. PERFORMED AMM 05-61-66, INSPECTION OF SMOKE OR FUMES IN THE COCKPIT, NO DETECTION OF SMOKE NOTED.

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 76,537 hrs · 15,963 cycles

STATUS MESSAGE RT ENG FIRE LOOP. ACCOMPLISHED ENGINE FIRE DETECTION SYSTEM OPS TEST IAW AMM 26-11-00 NO FAULTS NOTED AT THIS TIME.

Part: WIRE HARNESS — DEFECTIVE (WINDOW HEAT) · airframe 76,522 hrs · 15,959 cycles

LEFT SIDE WINDOW EICAS MESSAGE IN FLIGHT COMPLIED WITH QRH PROCEDURES AND EICAS MESSAGE DID NOT CLEAR. LEFT SIDE WINDOW INOP NOT EXTINGUISH. REMOVED AND REPLACED WINDOW HEAT WIRE HARNESS W1158 L2 WINDOW IAW AMM 56-11-02, ACCOMPLISHED FLIGHT COMPARTMENT WINDOW ANTI-ICING SYSTEM OPS CHECK IAW AMM 30-41-00 NO FAULTS NOTED AT THIS TIME.

Part: CONTROLLER — MALFUNCTIONED (WINDOW HEAT) · airframe 76,526 hrs · 15,960 cycles

L2 WINDOW HEAT INOPERATIVE. CAME BACK AFTER CONTROLLER REPLACED.

Part: CONTROLLER — INOPERATIVE (WINDOW HEAT) · airframe 76,495 hrs · 15,952 cycles

LEFT SIDE WINDOW HEAT INOPERATIVE. REMOVED AND REPLACED THE L2 WINDOW HEAT CONTROLLER, OPS CHECKED GOOD IAW AMM 30-41-01.

Part: SWITCH — INOPERATIVE (EEC LIGHT) · airframe 76,495 hrs · 15,952 cycles

LEFT EEC NORMAL LIGHT INOPERATIVE. REPLACED THE SWITCH, OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT WINDOW) · airframe 76,495 hrs · 15,952 cycles

EICAS FOR THE LT SIDE WINDOW. PERFORMED FIM 30-41 FT 804. LT SIDE WINDOW ANTI-ICING BITE PROCEDURE. OPS CHECKED GOOD. COULD NOT DUPLICATE.

Part: WARNING LIGHT — FALSE ACTIVATION (RT ENGINE) · airframe 76,495 hrs · 15,952 cycles

DURING CLIMB, THE RIGHT ENGINE PRV EICAS. AFTER CLIMB, WENT AWAY. PERFORMED FIM 36-10 F/T 847, NO FAULTS FOUND. OPS CHECKED GOOD.

Part: COUPLING — LEAKING (APU FUEL) · airframe 76,526 hrs · 15,960 cycles

FUEL MIGRATES FROM LT WING TANK TO CENTER WING TANK AT A HIGH RATE. REMOVED & REPLACED SCALSON APU FUEL FEED LINE COUPLING FOUND LEAKING IAW AMM 28-22-07, LEAK CHECKED APU LINE COUPLING IAW AMM 28-21-00, NO LEAKS NOTED.

Part: ENGINE — MALFUNCTIONED (APU) · airframe 76,495 hrs · 15,952 cycles

APU START PRESSURE LOW RT ENGINE. 22 PSI. ACCOMPLISHED APU GROUND TEST OF THE APU, GROUND START SYSTEM ENGINE START NORMAL. IAW AMM 71-00-00.

Part: FAIRING — WORN (THRUST REVERSER) · airframe 76,471 hrs · 15,947 cycles

2L T/R INNER DUCT FWD UPPER FAIRING, 22 RIVET WORN AND FWD LOWER FAIRING 1 EA RIVET WORN. REMOVED THE DAMAGE RIVETS IAW SRM 51-40-02, REV 106. INSTALLED NEW RIVETS SRM 51-40-02 REV 106. OPS CHECKED GOOD.

Part: WINDOW FRAME — CORRODED (BS 1340) · airframe 76,471 hrs · 15,947 cycles

FOUND PAX WINDOW FRAME CORRODED BS 1340. CORROSION REMOVED IAW SRM 51-10-02, REV 105. FOUND OUT OF LIMITS IAW SRM 56-20-02-1A-1, REV 105 3.

Part: CLAMP — FAILED (ANTI-ICE VALVE) · airframe 76,471 hrs · 15,947 cycles

FOUND LOCK FUNCTION FAILED ON THE CLAMP OF THE LT WING THERMAL ANTI-ICE VALVE IAW AMM 30-11-02-004-001, AND 30-11-02-404-012, REV 123. REPLACED THE CLAMP IAW AMM 30-11-02-404-012, REV 123. LEAK CHECKED GOOD.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 76,471 hrs · 15,947 cycles

FOUND THE LT UPPER WING BETWEEN FILL PORT ADAPTER AND WING UPPER SKIN CORRODED. REPAIRED IAW EI T2017A57M-2414, REV 2. CHECKED NORMAL.

Part: SEAL — WORN (EXHAUST PIPE) · airframe 76,471 hrs · 15,947 cycles

NR 1 ENGINE EXHAUST FWD 11 O'CLOCK SPRING SEAL WORN. REPLACED THE SPRING SEAL IAW AMM 70-50-00-912-001, REV 123.

Part: WINDOW FRAME — CORRODED (BS 775) · airframe 76,471 hrs · 15,947 cycles

FOUND PAX WINDOW FRAME CORRODED BS 775. CORROSION REMOVED IAW SRM 51-10-02, REV 105. PERFORMED PROTECTIVE TREATMENT ON REWORKED AREA IAW SRM 51-20-01, REV 105.

Part: SEAL — DAMAGED (THRUST REVERSER) · airframe 76,471 hrs · 15,947 cycles

FOUND DAMAGED ON THE P-SEAL OF THE 2R THRUST REVERSER, CLOSE TO THE NR 4 BLOCKER DOOR. REPLACED THE P-SEAL IAW AMM 78-31-26-004-001, AND 78-31-26-404-002 REV 123.

Part: SEAL — DAMAGED · airframe 76,471 hrs · 15,947 cycles

L2 CORE COWL SPRING SEAL UPPER AND AFT SIDE DAMAGED. REMOVED IAW SRM 51-40-02 REV 105. INSTALLED NEW IAW SRM 51-40-02, REV 105, AND CMM 71-13-23, FIGURE 3, REV 040. CHECKED NORMAL.

Part: BEARING — WORN (THRUST REVERSER) · airframe 76,471 hrs · 15,947 cycles

NR 1 PYLON LT THRUST REVERSER OPEN ACTUATOR BRACKET BEARING WORN. REPLACED THE BEARING IAW AMM 78-31-46-004-001, REV 122, 78-31-404-006, REV 123, SRM 51-40-22, REV 105, SRM 51-40-02-0G-0, REV 106, AND AWI 311T2671, REV B. CHECKED NORMAL.

Part: RUB STRIP — MISSING (THRUST REVERSER) · airframe 76,471 hrs · 15,947 cycles

NR 1 ENGINE RT THRUST REVERSER BLOCKER DOOR NR 3. AFT WEAR STRIP MISSING IAW AMM 78-31-14-004-001, REV 122. REMOVED BLOCKER DOOR. REPAIRED IAW AMM 78-31-14-404-008, REV 123, AND INSTALLED IAW AMM 7831-00-725-005-1100, REV 123. OPS TESTED NORMAL.

Part: IGNITION SYS — NO TEST (NR 1 ENGINE) · airframe 76,471 hrs · 15,947 cycles

FOUND THE NR 1 ENGINE IGNITION SYSTEM FAILED TO TEST IAW SWPM 20-61-11, REV 67, RECONNECTED IAW AMM 74-00-00-705-157, REV 123. OPS TESTED NORMAL.

Part: FITTING — WORN (THRUST REVERSER) · airframe 76,471 hrs · 15,947 cycles

2L THRUST REVERSER OPEN ACTUATOR FITTING WORN. . BUSHING HOLES REPAIRED IAW AMM 78-31-06-004-001, REV 122, 78-31-06-404-006, REV 123, CMM 78-33-02, REPAIR 020, REV 54, SPM 70-32-03, REV 106, AND SPWPS-PA003, REV 07.

Part: WINDOW FRAME — CORRODED (BS 775) · corrosion level 2 · airframe 76,471 hrs · 15,947 cycles

FOUND PAX WINDOW FRAME CORRODED, BS 775. REMOVED AND REPLACED IAW SRM 51-40-02, REV 106, AND DWG 143T3351, SH5, REV A.

Part: BRACKET — CRACKED (THRUST REVERSER) · airframe 76,471 hrs · 15,947 cycles

CRACK - 2L T/R FWD TORQUE BOX DISCINNECT&NBSP;BRACKET CRACK NEAT 3RD LOCK(<P>REMOVED DAMAGE PARTS IAW SRM 51-40-02 REV106 INSTALLED NEW PARTS IAW MRAS IPC 78-32-21 FIG 65 REV79 AND SRM 51-40-02 REV106. OPS CHECK GOOD&NBSP;</P>)

Part: ISOLATION VALVE — MALFUNCTIONED (THRUST REVERSER) · airframe 76,471 hrs · 15,947 cycles

FOUND THE NR 2 THRUST REVERSER ISOLATION VALVE LIGHT DID NOT COME ON. DURING MOVEMENT OF THE NR 2 THRUST REVERSE LEVER REAPPEARED IN THE REVESE IDLE DETENT IAW SWPM 20-84-17, REV.66. REPLACED THE ISOLATION VALVE, OPS CHECKED GOOD IAW AMM 78-36-00-725-001-M00, REV 123. PILOT VALVE PRESSURE SWITCH CHECKED NORMAL.

Part: WINDOW FRAME — CORRODED (BS 1197) · airframe 76,471 hrs · 15,947 cycles

FOUND PAX WINDOW FRAME CORRODED BS 1197+11. CORROSION REMOVED IAW SRM 51-10-02, REV 105. PERFORMED PROTECTIVE TREATMENT ON REWORKED AREA IAW SRM 51-20-01, REV 105.

Part: VALVE — MALFUNCTIONED (APU) · airframe 76,471 hrs · 15,947 cycles

PNEMATIC DUCT PRESSURE LOW DURING ON THE LT ENGINE START. REPLACED THE APU SURGE VALVE IAW AMM 49-53-01-004-001, AND 49-53-01-404-010, REV 123. OPS CHECKED NORMAL.

Part: BLOCKER DOOR — DAMAGED (THRUST REVERSER) · airframe 76,471 hrs · 15,947 cycles

NR 2 THRUST REVERSER NR 1 BLOCKER DOOR WIRE MESH PEELED OFF IAW AMM 78-31-14-004-001, REV 122. REMOVED THE BLOCKER DOOR. COMPLETED THE WIRE MESH REPAIR IAW AMM 78-31-14-404-008, REV 123. INSTALLED THE THE BLOCKER DOOR IAW AMM 78-31-00-725-005-1100 REV 123. ENGINE THRUST REVERSER OPS CHECKED NORMAL.

Part: BRACKET — CHAFED (NACELLE) · airframe 76,471 hrs · 15,947 cycles

R2 CORE COWL INNER FACE, NR 2 FRAME. CORE COWL HOLD OPEN ROD SUPPORT BRACKET AND LAST LATCH COVER CHAFED. REMOVED IAW SRM 51-40-02, REV 105. INSTALLED A NEW PART IAW SRM 51-40-02, REV 105, CMM 71-13-24, FIG 1, REV 043, 71-13-24, FIG 2, REV 043. CHECKED NORMAL.

Part: WINDOW FRAME — CORRODED (BS 555) · airframe 76,471 hrs · 15,947 cycles

FOUND PAX WINDOW FRAMES CORROSION LT BS 555. CORROSION REMOVED IAW SRM 51-10-02, REV 105. FOUND OUT OF ALLOWABLE LIMITS IAW SRM 56-20-02-1A-1 REV 105. PERFORMED PROTECTIVE TREATMENT ON REWORKED AREA IAW SRM 51-20-01 REV 105.

Part: SHEAR WEB — CORRODED (BS 1373-1395) · corrosion level 2 · airframe 76,471 hrs · 15,947 cycles

FOUND A SHEAR WEB CORRODED AT WL200, BS 1373 - 1395. . REMOVED IAW STM 51-40-02, REV 106. FABRICATED A NEW PART IAW EI T2018P53M-992, REV 0. INSTALLED IAW SRM 51-40-02, REV 106, AND DWG 146T8511, SHT 4, REV E. CHECKED NORMAL.

Part: HINGE FITTING — WORN (NR 1 PYLON) · airframe 76,471 hrs · 15,947 cycles

NR 1 PYLON LT CORE COWL FWD HINGE FITTING AND BOLT WORN. IAW AMM 71-11-06-714-014, REV 122, 71-11-06-714-013, REV 123, 71-11-07-825-008, REV 123, AND DWG 311T2561 ID:0001, REV 2 REPLACED THE BUSHINGS AND BOLT.

Part: BLOWOUT DOOR — CHAFED (THRUST REVERSER) · airframe 76,471 hrs · 15,947 cycles

NR 1 ENGINE RT THRUST REVERSER BLOW OUT DOOR CHAFED. REMOVED THE DOOR IAW SRM 57-40-02, REV 106. REPAIRED THE DAMAGED AREA IAW CMM 78-32-09, REV 54, AND INSTALLED IAW SRM 51-40-02, REV 106 AND 78-31-51-03, REV 33.

Part: RIVET — WORN (THRUST REVERSER) · airframe 76,471 hrs · 15,947 cycles

2L THRUST REVERSER AFT EDGE NR 3, 4, & 5 WEAR STRIP RIVETS WORN. REMOVED AND REPLACED THE DAMAGED RIVETS IAW SRM 51-40-02-0G-0, REV 105.

Part: BRACKET — WORN (NR 1 NACELLE) · airframe 76,471 hrs · 15,947 cycles

WORN NR 1 ENGINE RT FAN COWL INNER FWD SUPPORT ROD BRACKET. REPLACED THE BRACKET IAW AMM 70-50-00-912-001 AND 70-40-00-912-025 REV 122. CHECKED NORMAL.

Part: WINDOW FRAME — CORRODED (BS 1428) · corrosion level 2 · airframe 76,471 hrs · 15,947 cycles

FOUND PAX WINDOW FRAME CORRODED BS 1428. REMOVE IAW SRM 51-40-02, REV 106. INSTALL NEW IAW SRM 51-40-02, REV 106, AND DWG 146T3330, SHT 11, REV A. CHECKED NORMAL.

Part: WINDOW FRAME — CORRODED (BS 1384) · airframe 76,471 hrs · 15,947 cycles

FOUND PAX WINDOW FRAME CORRODED, BS 1384(<P>1. CORROSION REMOVED IAW SRM 51-10-02, REV 105 2. &NBSP;3. PERFORMED PROTECTIVE ON REWORKED AREA IAW SRM 51-20-01 REV 105.

Part: LATCH — WORN (ACCESS DOOR) · airframe 76,471 hrs · 15,947 cycles

WORN SR FAN COWL OIL TANK ACCESS DOOR FWD LATCH ASSY. REMOVED THE LATCH IAW SRM 51-40-02, REV 105. INSTALLED A NEW LATCH IAW SRM 51-40-02, REV 105, AND CMM 71-13-22, FIGURE 4, REV 043. CHECKED NORMAL.

Part: WINDOW FRAME — CORRODED (BS 1065) · airframe 76,471 hrs · 15,947 cycles

FOUND PAX WINDOW FRAME CORRODED BS 1065. CORROSION REMOVED IAW SRM 51-10-02, REV 105. REWORKED AREA, AND WITHIN ALLOWABLE LIMIT IAW SRM 56-20-02-1A-1, REV 105 3.

Part: COUPLING — DAMAGED (FUEL LINE) · airframe 76,471 hrs · 15,947 cycles

DAMAGED NR 1 PYLON FUEL LINE COUPLING. REPLACED THE FUEL LINE IAW AMM 28-22-07-404-104, 28-22-07-404-126, AND 71-00-00-795-034. NO LEAK WAS FOUND AND OPS CHECKED NORMAL.

Part: WINDOW FRAME — CORRODED (BS 1065) · airframe 76,471 hrs · 15,947 cycles

FOUND PAX WINDOW FRAMES CORRODED, LT BS 1065. THE CORROSION WAS REMOVED IAW SRM 51-10-02, REV 105. AREA NOT FOUND WITHIN ALLOWABLE LIMITS IAW SRM 56-20-02-1A-1, REV 105. PERFORMED PROTECTIVE TREATMENT ON REWORKED AREA IAW SRM 51-20-01, REV 105.

Part: WINDOW FRAME — CORRODED (BS 1098) · airframe 76,471 hrs · 15,947 cycles

FOUND PAX WINDOW FRAMES CORRODED, LT BS 1098. CORROSION REMOVED IAW SRM 51-10-02, REV 105. AREA WAS NOT FOUND WITHIN ALLOWABLE LIMITS IAW SRM 51-20-01, REV 105.

Part: SKIN — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 76,471 hrs · 15,947 cycles

RIGHT WING INBOARD AFT FLAP UPPER SURFACE, IFS 257.485 CORRODED. REPAIRED THE AREA IAW EI T2017A57M-2363, REV 2.

Part: VALVE — DAMAGED (NR 1 ENGINE) · airframe 76,471 hrs · 15,947 cycles

FOUND THREAD DAMAGE IN THE PRVC SUPPLY PRESSURE PORT OF THE NR 1 ENGINE IAW AMM 36-11-19-004-001-002, REV 123, & AMM 36-11-19-404-014-002, REV 123. REPLACED THE NR 1 ENGINE PRVC IAW AMM 36-11-19-404-014-002, REV 123. TESTED NORMAL.

Part: JUMPER — DETERIORATED (NR 2 PYLON) · airframe 76,471 hrs · 15,947 cycles

DETERIORATED NR 2 PYLON PRSOV JUMPER WIRE. REPLACED THE JUMPER WIRE IAW AMM 20-10-21-964-001, REV 122, AND SWPM 20-20-00 AND 20-20-10, REV 66, CHECKED NORMAL.

Part: WINDOW FRAME — CORRODED (BS 1296) · airframe 76,471 hrs · 15,947 cycles

FOUND PAX WINDOW FRAME CORRODED. BS 1296. CORROSION REMOVED IAW SRM 51-10-02, REV 105 2. PERFORMED PROTECTIVE TREATMENT IAW SRM 51-20-01 REV.105.

Part: BRACKET — WORN (NACELLE) · airframe 76,471 hrs · 15,947 cycles

2L CORE COWL HOLD OPEN ROD FWD SUPPORT BRACKET WORN. REMOVED THE BRACKET IAW SRM 51-40-02, REV 105. INSTALLED A NEW BRACKET IAW SRM 51-40-02, REV 105. AND CMM 71-13-23, FIGURE 2, REV 040. CHECKED NORMAL.

Part: ADAPTER — WORN (NR 2 NACELLE) · airframe 76,471 hrs · 15,947 cycles

WORN NR 2 ENGINE CORE COWL HOLD OPEN ROD SUPPORT ADAPTER. REPLACED THE ADAPTER IAW AMM 70-50-00-912-001 REV 122. CHECKED NORMAL.

Part: STIFFENER — CORRODED (BS 955) · corrosion level 2 · airframe 76,471 hrs · 15,947 cycles

CORROSION FOUND ON LT SKIN STIFFENER BS 955. REPAIRED IAW EO 6753A070, REV 11. CHECKED NORMAL.

Part: WINDOW FRAME — CORRODED (BS 687) · airframe 76,471 hrs · 15,947 cycles

FOUND PAX WINDOW FRAMES CORRODED, LT BS 687. THE CORROSION WAS REMOVED IAW SRM 51-10-02, REV 105. AREA NOT FOUND WITHIN LIMITS IAW SRM 56-20-02-1A-1, REV 105. PERFORMED PROTECTIVE TREATMENT ON REWORKED AREA IAW SRM 51-20-01, REV 105.

Part: FLOOR SUPPORT — CORRODED (BS 1461-1540) · corrosion level 2 · airframe 76,471 hrs · 15,947 cycles

BULK CARGO FLOOR SUPPORT BETWEEN BS 1461.98 AND 1540, LBL 44 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, REV 106, AND DWG 146T5002, SH1, REV E, SH3, REV G, SH 4, REV C.

Part: RELAY — FAILED (THRUST REVERSER) · airframe 76,471 hrs · 15,947 cycles

NO VOME ON AND THE LT THRUST REVERSER ISOLATION VALVE MESSAGE. NO SHOW OF THE NR 1 THRUST REVERSER SYS. DURING MOVE, THE NR 1 THRUST REVERSER, LEVER REARWARD, IN THE REVERSE IDLE DETENT IAW WDM 78-36-11, REV 14. REPLACED THE M10440 RELAY AND CONDITION CHECKED NORMAL IAW AMM 78-36-00-725-001-H00, REV 123. DIRECTIONAL PILOT VALVE PRESSURE SWITCH TESTED GOOD.

Part: WINDOW FRAME — CORRODED (BS 533) · airframe 76,471 hrs · 15,947 cycles

FOUND PAX WINDOW FRAME CORRODED BS 533. CORROSION REMOVED IAW SRM 51-10-02, REV 105. PERFORMED PROTECTIVE TREATMENT ON REWORKED AREA IAW SRM 51-20-01, REV 105.

Part: WINDOW FRAME — CORRODED (BS 731) · corrosion level 2 · airframe 76,471 hrs · 15,947 cycles

FOUND PAX WINDOW FRAME CORRODED BS 731. REMOVED IAW SRM 51-40-02, REV 106. INSTALL NEW IAW SRM 51-40-02, REV 106, AND DWG 143T3351, SH5, REV A. CHECKED NORMAL.

Part: WINDOW FRAME — CORRODED (BS 1406) · airframe 76,471 hrs · 15,947 cycles

FOUND PAX WINDOW FRAME CORRODED BS 1406. CORROSION REMOVED IAW SRM 51-10-02, REV 105, FOUND TO BE OUT OF LIMITS IAW SRM 56-20-02-1A-1, REV 105 3.

Part: WINDOW FRAME — CORRODED (BS 1318) · airframe 76,471 hrs · 15,947 cycles

FOUND PAX WINDOW FRAME CORRODED BS 1318 CORROSION REMOVED IAW SRM 51-10-02, REV 105. PERFORMED PROTECTIVE TREATMENT ON REWORKED AREA IAW SRM 51-20-01 REV 105.

Part: TUBE — NICKED (NR 2 ENGINE) · airframe 76,471 hrs · 15,947 cycles

FOUND THREE NICKS ON THE TUBE ASSY ATTACHING ON THE PRSOV OF THE NR 2 ENGINE IAW AMM 36-11-09-002-033, 36-11-09-402-058, AND 20-11-00-910-802, REV 123. REPLACED THE TUBE IAW AMM 36-11-09-402-058-001, REV 123. LEAK CHECKED OK.

Part: PIN — CRACKED (NR 2 NACELLE) · airframe 76,471 hrs · 15,947 cycles

CRACK NR 2 PYLON FAN COWL SUPPORT BEAM PIN CRACKED. REPLACED THE PIN IAW AMM 71-11-04-712-011 REV 122 AND AMM 71-11-04-712-012 REV 122, CHECKED NORMAL.

Part: LATCH — WORN (NACELLE) · airframe 76,471 hrs · 15,947 cycles

R2 CORE COWL PRESSURE RELIEF DOOR UPPER LATCH WORN. REMOVED IAW SRM 51-40-02, REV 105. INSTALLED NEW IAW SRM 51-40-02, REV 105, AND CMM 71-13-24, REV 043. CHECKED NORMAL.

Part: BRACKET — WORN (NR 2 NACELLE) · airframe 76,471 hrs · 15,947 cycles

NR 2 PYLON AFT FAIRING STRUT FORWARD LT AND RT FASTENER BRACKET WORN. REMOVED IAW SRM 51-40-02, REV 105. FABRICATED A NEW PART IAW EI T2017 P54M 2339, REV 0 AND T2017P54M-2340 REV 0. INSTALLED IAW SRM 51-40-02, REV 105, AND DRAWING 313T2380, SHEET 10, REV 1 CHECKED NORMAL.

Part: WINDOW FRAME — CORRODED (BS 1428) · corrosion level 2 · airframe 76,471 hrs · 15,947 cycles

FOUND PAX WINDOW FRAMES CORROSION LOCATED AT RT BS 1428. REMOVED DAMAGED PART IAW SRM 51-40-02 REV. 106 2. INSTALL A NEW PART IAW STM 51-40-02, REV 106 AND DWG 146T3330, SH 11, REV A.

Part: SEAL — DAMAGED (THRUST REVERSER) · airframe 76,471 hrs · 15,947 cycles

DAMAGE ON THE P-SEAL OF THE THRUST REVERSER, CLOSE TO NR 5 BLOCKER DOOR. REPLACED THE P-SEAL IAW AM 78-31-26-004-001 AND 78-31-26-404-002-1-100 REV 123.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 76,471 hrs · 15,947 cycles

FOUND THE RT WING UPPER BETWEEN THE WING UPPER SKIN AND THE FILL PORT ADAPTER CORRODED. ACCOMPLISHED DAMAGE AREA IAW EI NO: T2017A57M-2414 REV.2&NBSP; &NBSP;2. ORIGINAL EI ATTACHMENT NRC 266 3. CONDITION CHECKED NORMAL.

Part: SCREW — MISSING (NR 1 NACELLE) · airframe 76,471 hrs · 15,947 cycles

MISSING NR 1 ENGINE COWL EXTERNAL LOWER SIDE ANTI-ICE AIR EXIT FAIRING SCREW. INSTALLED A NEW SCREW IAW AMM 70-50-00-912-001 REV 122, CHECKED NORMAL.

Part: RIVET — WORN (THRUST REVERSER) · airframe 76,471 hrs · 15,947 cycles

2R THRUST REVERSER FORWARD INNER TORQUE BOX RIVET WORN. REMOVED AND REPLACED THE DAMAGED RIVETS IAW SRM 51-40-02-0G-0, REV 105.

Part: TORQUE BOX — WORN (THRUST REVERSER) · airframe 76,471 hrs · 15,947 cycles

2L T/R FWD TORQUE BOX RIVET WORN AT THE 12 O'CLOCK POSITION. REMOVED DAMAGE RIVETS IAW SRM 51-40-02-0G-0 REV 105. INSTALL NEW RIVETS IAW SRM 51-40-02-0G-0 REV 105 AND MARS CF6-80C2. OPS CHECKED GOOD.

Part: RUB STRIP — CHAFED (NACELLE) · airframe 76,471 hrs · 15,947 cycles

R2 CORE COWL FWD WEAR STRIP NR 2, & 3 CHAFED. REMOVED IAW SRM 51-40-02 REV 105. INSTALLED NEW IAW SRM 51-40-02, REV 105, AND CMM 71-13-24, FIGURE 1, REV 043. CHECKED NORMAL.

Part: RUB STRIP — CHAFED (THRUST REVERSER) · airframe 76,471 hrs · 15,947 cycles

2R THRUST REVERSER AFT EDGE WEAR STRIP CHAFED ON UPPER SIDE. REMOVED THE PART IAW SRM 51-40-02 REV 105. AND INSTALLED A NEW IAW SRM 51-40-02, REV 105.

Part: LINK — LOOSE (START DUCT) · airframe 76,471 hrs · 15,947 cycles

FOUND THE NR 1 START DUCT LINK LOOSE. TORQUED THE NR 1 ENGINE START DUCT LINK IAW AMM 70-50-00-912-001, REV 123. CHECKED SATISFACTORY.

Part: FITTING — WORN (THRUST REVERSER) · airframe 76,471 hrs · 15,947 cycles

2R THRUST REVERSER OPEN ACTUATOR FITTING BOLT HOLE WORN. WORN BUSHING HOLES REPAIRED IAW AMM 78-31-06-004-001 REV 122, 78-31-06-404-006 REV 123, CMM 78-32-02, REPAIR 020, REV 54, SPM 70-32-03, REV 106, AND SPWPS PA-003, REV 07.

Part: RUB STRIP — BROKEN (THRUST REVERSER) · airframe 76,471 hrs · 15,947 cycles

BROKEN - 2L T/R TRANSLATING COWL TRACK WEAR STRIP BROKEN(<P>IAW AMM 78-31-10-004-001-H00 REV122 REMOVED THE 2L T/R TRANSLATING COWL IAW AMM 70-50-00-912-001-H00 REV122 REPAIRED THE 2L T/R TRANSLATING COWL WEAR STRIP WITH SERVICEABLE PARTS. IAW AMM 78-31-01-404-012 REV122 INSTALLED THE 2L TRANSLATING COWL. IAW AMM 78-31-00-825-001-H00 REV123 ADJUSTMENT THE 2L T/R ACTUATION SYSTEM AND CONDETION&NBSP;CHECK NORMAL. IAW AMM 78-31-00-725-005-H00 REV 123 DO THE #2 ENG T/R OPERATIONAL TEST NORMAL&NBSP;</P>)

Part: WINDOW FRAME — CORRODED (BS 731) · airframe 76,471 hrs · 15,947 cycles

FOUND PAX WINDOW FRAME CORRODED BS 731. CORROSION REMOVED IAW SRM 51-10-02 REV 105. PERFORMED PROTECTIVE TREATMENT ON REWORKED AREA IAW SRM 51-20-01 REV 105.

Part: SLEEVE — DENTED (EXHAUST) · airframe 76,471 hrs · 15,947 cycles

NR 1 ENGINE EXHAUST SLEEVE MID SECTION FWD AND MID AREA DENTED AT THE 9 AND 10 O`CLOCK POSITIONS. REPLACED OF THE EXHAUST SLEEVE IAW SRM 54-42-30-1A-1, REV 106, AMM 78-11-01-004-001, REV 123, AND AMM 78-11-01-404-009, REV 123.

Part: WINDSHIELD — CRACKED (COCKPIT)

ORD - FIRST OFFICER WINDSHIELD CRACKED AND ARCING. REPLACED FIRST OFFICER WINDSHIELD IN ACCORDANCE WITH MM 56-11-00-4. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ENGINE — VIBRATION (NR 1)

DURING LEVEL FLT AT 31,000 FT, AIRSPEED 270 KNTS, ON SELECTING 250 KNTS, NR 1 ENG INDICATED HIGH VIB ON MFDU ACCOMPANIED BY AUDIBLE NOISE & VIBRATION FELT THROUGH A/C. ATTEMPTED ICE CLEARING PROCEDURES WITH NO SUCCESS. ADVANCING THROTTLE ABOVE 1.14 EPR CAUSED AN IMMEDIATE & SUSTAINED VIB WITH ASOCIATED IND ON MFDU. N1 IND HIGH VIB ON BOTH VIB CHANNELS. N2 SLIGHTLY HIGHER THAN IND ON NR 2 ENG, ALL OTHER ENG IND APPEARED NORM. NR 1 ENG LEFT AT IDLE FOR LAST 390 MINUTES OF FLT. SINGLE ENG PROCEDURES FLOWN WITH NO ADVERSE RESULTS. LANDED DFW WITHOUT INCIDENT. ALL CHECKS GOOD, VIB .4 AT TAKEOFF, AS EPR ENGINEERING. NO FURTHER MAINTENANCE REQUIRED. A/C RETURNED TO SERVICE. SYS GRND CHECKED NORM. (M)

Part: MANIFOLD — FAILED (RUDDER)

DFW - FLT 551 - AFTER TAKEOFF, BOTH STAB TRIM FAULTED, BOTH YAW DAMPER AND NR 2 RUDDER SYSTEM FAULTED. STAB TRIM AND YAW DAMPER WERE RESET. LANDED DFW WITHOUT INCIDENT. REPLACED RUDDER MANIFOLD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M0

Part: RUDDER — FAULTY (COCKPIT)

AFTER TAKEOFF BOTH STABILIZER TRIM FAULTED, BOTH YAW DAMPER AND NR 2 RUDDER SYSTEM FAULTED. STABILIZER TRIM AND YAW DAMPER WERE RESET. LANDED WITHOUT INCIDENT. REPLACED RUDDER LIMITER MONITOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONTROLLER — DEFECTIVE (CABIN)

DFW - FLT 890 - EN ROUTE DFW-MEM, FLIGHT ATTENDANT REPORTED ELECTRICAL SMELL AND SMOKE IN CABIN. DECLARED EMERGENCY, RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. REPLACED CABIN SKIN SENSOR. REPLACED NR 1 SIDE AND NR 2 SIDE CABIN TEMPERATURE CONTROLLERS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FITTING — LEAKING (NR 2 ENGINE)

DFW - FLT 581 - ON APPROACH ORD, HYDRAULIC SYSTEM ONE QTY LOW. MANUALLY EXTEND GEAR AND LANDED ORD WITHOUT INCIDENT. REPLACED NR 2 ENGINE NR 1 QUICK DISCONNECT FITTING. SERVICED NR 1 HYDRAULIC SYSTEM. ACCOMPLISHED LEAK CHECK. GROUND CHECKED NORMAL OPERATION. (M)

Part: STRINGER — CRACKED (BS 4000)

TUL - FOUND STRINGER NR 68 CRACKED APPROXIMATELY STATION 4000. INSTALLED NEW STRINGER AND SPLICE PAGE SRM 51-70-0L. (M)

Part: LIGHT STRIP — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY HAD ONE BULB INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BY FORWARD GALLEY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: PSU — DEFECTIVE (CABIN)

DFW - FLT 1738 - EN ROUTE DTW/DFW DURING CRUISE, ODOR SIMILAR TO HOT PLASTIC NOTED IN CABIN. NO OTHER ABNORMAL INDICATIONS AND AIRCRAFT PROCEEDED TO DFW LANDING WITHOUT INCIDENT. REPLACED PASSENGER SERVICE UNIT PANEL AT SEAT 5DE DUE TO RELAY FOUND HOT AND MELTING. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)