N1427A
Registered owner: ANDROMEDA LEASING I LLC, NY (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
AFTER PUSH BACK IN KSCK RIGHT ADI WAS COLLAPSED AND AFTER TOTAL RESET ON DE-ENERGIZING THE PLANE STILL PERSISTED THE PROBLEM AC RETURNED TO THE GATE (BTB) AND MTX GROUNDED A/C MTX DEFERRED R IRU IAW ABX MEL 34-21-1-1-2B MX ACTIONS COMPLIED WITH, PLACARD INSTALLED MBCB 06-22-2026 MUST BE REINSPECTED EACH FLIGHT DAY. A/C DOWNGRADED TO CAT 3A. AND RETURNED A/C TO SERVICE.
DURING TAXI OUT UNABLE TO START RIGHT ENG. INDICATES ZERO ROTATION & VALVE LIGHT STAYS ON. APU DUCT PRESS VALUES BETWEEN 10 & 20 PSI. A/C RETURNED TO THE GATE (BTB) AND MTX GROUNDED A/C . MTX REMOVED AND REPLACED RH STARTER IAW B767 AMM 80-11-01. OPS CHECKED GOOD A/C RELEASED ETOPS 180. RETURNED A/C TO SERVICE
DURING CREW PREFLIGHT, MN CARGO LOOP 2 STATUS MESSAGE DISPLAYED. MTC PERFORMED OPS CHECK OF THE MAIN CARGO COMPARTMENT SMOKE DETECTION SYSTEM IAW B767 AMM 26-14-00 NO DEFECTS NOTED AIRCRAFT RELEASED ETOPS 180. ACFT RETURNED TO SERVICE.
WHILE SITTING ON THE RAMP & LOADING IN KSCK MAIN CARGO LOOP 1, FIRE ALARM & BELL CAME ON. THEN EXTINGUISHED AFTER A FEW SECONDS, MTX VERIFIED NO FIRE IN MAIN CARGO. PERFORMED OPS TEST I.A.W AMM 26-14-00. OPS CHECK GOOD A/C RELEASED ETOPS 180 AND RETURNED A/C TO SERVICE.
AFTER BLOCK OUT AND LT & RT ENGINES STARTED, RUDDER RATIO EICAS CAUTION MESSAGE APPEARED. ACFT RETURNED TO GATE AND MTX GROUNDED ACFT . MTX RESET LT & RR RUDDER RATIO MODULE AND PERFORMED ENGINE RUNS AND NO RUDDER RATIO FAULT IAW FIM 27-09 FT 814 AND AMM 71-00-00 OPS CHECK GOOD ACFT RELEASED ETOPS 180. AND RETURNED ACFT TO SERVICE.
DURING APPROACH, GEAR NOT DOWN EICAS WARNING RECIEVED AT FL190 DESCENDING AT IDLE THRUST ON ARRIVAL. DEFERRED L RAD ALT PER MEL 34-33-1-2A-1 PLACARD INSTALLED MBCB 04/20/2026. A/C RETURNED TO SERVICE.
DURING MAINTENANCE PRE-FLIGHT, EICAS FWD CARGO DET 2 MSG. MAINTENANCE DEFERRED PER B767 MEL 26-16-1-2, MAINTEMANCE PROCEDURES COMPLIED WITH, PLACARDS INSTALLED AND MBCB 04/16/2026, AIRCRAFT REMAINS ETOPS 180. A/C RETURNED TO SERVICE.
AFTER LANDING, STATUS MSG: FWD CARGO DETECTOR 2. Â MTX GROUNDED ACFT AND PERFORMED FIM 26-16 FT832, MSG CLEARED, BITE TESTED GOOD. ACFT REMAINS ETOPS 180. RETURNED TO SERVICE .
DURING CREW PREFLIGHT, MAIN CARGO FIRE LOOP WARNING 1 & 2 SEVERAL TIME. FALSE INDICATION. MAINTENANCE VERIFIED NO FIRE IN MAIN CARGO. PERFORMED OPS TEST IAW AMM 26-14-00. OPS CHECK GOOD. A/C REMAINS NO ETOPS. AIRCRAFT DOWNGRADED TO NO ETOPS DUE TO NON-QUALIFIED TECHNICIAN. MAIN CARGO FIRE DETECTION SYSTEM. PERFORMED SYSTEM TEST PER 767 AMM 26-14-00. TEST GOOD NO FAULTS NOTED. AIRCRAFT RELEASED 180 ETOPS STATUS ANNUNCIATOR UPDATED. AIRCRAFT RETURNED TO SERVICE.
DURING LOADING, MAIN CARGO FIRE MESSAGE. VERIFIED NO FIRE PERFORMED OPS TEST IAW 26-14-00, FIRE DEPT. SCANNED A/C FOR FIRES, NO FIRE CONFIRMED. A/C REMAINS ETOPS 180. A/C RETURNED TO SERVICE.
DURING MAINT INSP, EMERGENCY LIGHTS UNARMED LIGHT INDICATION IS HALFWAY BURNED OUT. REMOVED AND REPLACED LIGHT BULBS IAW AMM 33-16-02. OPS CHECK GOOD. REF. LP 38676-39/2. AIRCRAFT RETURNED TO SERVICE.
MAIN CARGO FIRE EICAS MESSAGE/WARNING. LOOP 1. DEFERRED MAIN CARGO LOOP 1 IAW ABX MEL 26-16-2-1. MX MUST RE-INSPECT PRIOR TO EACH DEPARTURE. MX PROCEDUE C/W. PLACARDS INSTALLED. A/C REMAINS NO ETOPS. AIRCRAFT RETURNED TO SERVICE.
MAIN DECK CARGO LOOP 2 STATUS MSG ILLUM AFTER LANDINGÂ MTX, GROUNDED A/C AND DEFERRED MAIN DECK LOOP2 FOR DEPARTURE IAW MEL ABX-26-16-2-1 .AND RETURNED A/C TO SERVICE
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.
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.
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 .
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.
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.
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.
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.
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.
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.
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.
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 .
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 .
AT GATE: MAIN CARGO DECK FIRE INDICATED FOR 10 SECONDS. EICAS, DISCRETE LIGHTS, AURAL WARNINGÂ , 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 .
AT GATE: MAIN CARGO DECK FIRE INDICATED FOR 10 SECONDS. EICAS, DISCRETE LIGHTS, AURAL WARNINGÂ , 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
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 .
STAB TRIM EICAS MESSAGE AND DESCRETE LIGHT AFTER ENGINE STARTÂ 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
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 .
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
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.
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>)
AIRCRAFT DID NOT ACCELERATE THROUGH 10000 FT IN VNAV (ATB)(<P>PERFORMED MCDP TEST 30 & 40, FAULTING NO INFC. FCC C ELEV SRVO CMD REF AMM 22-00-02. REF LOGPAGE 1742397 ITEMS M7 & 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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
FOUND LEFT AND RIAGHT OVERHEAD EMERGENCY LIGHTS IN COCKPIT INOP.(<P><SPAN>RELAMPED LIGHTS , OPS CHECKS NORMAL IAW AMM 33-51-11.</SPAN></P>)
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 PCAôS, NO LEAKS WERE FOUN. TEST PEFORMED IAW AMM 29-11-00-796-053, REV 135 /
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>)
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>)
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>)
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>)
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>)
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>)
LEFT WING, IN ACCESS PANELS 551TB AND 551UB WITH EWIS CONTAMINATED OF HYDRAULIC(EWIS WAS CLEANED PER SWPM 20-10-04, REV 80</P>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
"R ENG BLD OVHT" ON DEPARTURE. PERFORMED QRH 2.27 & 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>)
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 & 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 & 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>)
APU FAULT DURING START ATTEMPT AFTER LANDING(<P>APU STARTED 1ST ATTEMPT BY MX PER AMM 49-41-00/001. APU CHECKS OK.</P>)
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>)
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>)
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>)
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>)
"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>)
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.
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>)
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.
WEATHER RADAR DOESN'T PAINT WEATHER MULTIPLE THUNDERSTORM SYSEMS ACROSS THE US AFTER APPEARED ONSCREEN(<P>PERFORMED OPS TEST WXR LT & RT IAW AMM 34-43-00. OPS TEST GOOD AT THIS TIME.</P>)
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>)
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>)
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>)
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>)
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>)
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.
APU BLEED VALVE EICAS ON BLOCK IN.(<P>CYCLED APU BLEED VALVE PER AMM 36-11-10. OPS CHECK GOOD AT THIS TIME.</P>)
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>)
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>)
R PACK TEMP ADVISORY MESSAGE IN DESCENT PROX 10000 FT. CAME ON TWICE- EXTINGUISHING BOTH TIMES(<P>PACK RESET & BIT CHECK IAW FIM TASK 21-51- TF 844, OPS CHECK GOOD & BITE CHECK GOOD, NO ACTIVE MESSAGES</P>)
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>)
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>)
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>)
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>)
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>)
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>)
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.
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>)
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.
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>)
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.
#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>)
#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>)
#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>)
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>)
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>)
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>)
LAV PORTABLE OXYGEN MASK MISSING MASK P/N 289-601212 POUCH P/N 80189-01.(<P>INSTALLED LAV PORTABLE OXYGEN MASK & POUCH AS REQUIRED PER AMM 35-31-01. CK'D OK&NBSP;&NBSP;</P>)
APU BATTERY HEALTH CHECK FAIL.(<P>REMOVED AND REPLACED APU BATTERY PER AMM 24-31-04-404-005. BATTERY CHECK GOOD .</P>)
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>)
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>)
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>)
FWD EQPT SUP FAN 1 STATUS MSG.(<P>RESET EQUIPMENT FOR 1 BREAKER. OPS TEST SYSTEM PER AMM 21-58-06. OPS NORMAL.</P>)
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>)
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, & WXR CONFIG TESTED, NO FAULTS NOTED.</P>)
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.
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>)
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>)
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>)
L PACK TEMP EICAS. QRH COMPLETE, FAULT REMAINS. RAN FAULT TREE FIM 21-51 TREE 844. NO FAULTS FOUND. OPS CKS GOOD.
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.
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.
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.)
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.
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>)
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>)
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>)
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>)
R GEN DRIVE EICAS MESSAGE. RAN QRH & 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>)
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.
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.
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.
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>)
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.
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.
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.
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.
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.
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.
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.
T-R UNIT DISPLAYED ON EICAS. CYCLED POWER TO A/C, PER FIM 24-32 FAULT TREE 803. MESSAGE CLEARED.
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.
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.
LEFT RADAR INOP(<P>PERFORMED WX TEST IAW AMM 34-43-00. TEST PASSED. MESSAGE CLEARED.<BR /></P>)
AFT EQ EXH FAN 2 STATUS MESSAGE AFTER ENGINE START. PERFORMED FIM 21-26 FT 806. MSG CLEARED. NO FURTHER DEFECTS NOTED.
AFT EQUIPMENT EXHAUST FAN NR 2 STATUS MESSAGE. PERFORMED A TEST IAW 21-58-49. STATUS MESSAGE CLEARED. OK FOR SERVICE.
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.
STATUS MESSAGE FOR WX SYS. CYCLED THE RT WXR SYS CIRCUIT BREAKER IAW FIM 34-43, TASK 801. MESSAGE CLEARED. OPS CHECKED GOOD.
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.
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.
AFT EQUIPMENT EXHAUST FAN 2 STATUS MESSAGE.
FWD EQUIPMENT VALVE EICAS AFTER ENGINE START, MOVED SWITCH TO STANDBY, MESSAGE DID NOT CLEAR.
AFT EQUIP EX FAN 2 STATUS MESSAGE. REMOVED AND REPLACED OVERBOARD EXHAUST VALVE IAW AMM 21-58-05.
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.
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.
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.
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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 & OPS CK GOOD.</P>)
APU FAULT EICAS MSG. REMOVED AND REPLACED APU OIL QTY TRANSMITTER IAW MM 49-94-04/401.
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 & 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>)
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>)
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>)
R FWD WINDOW EICAS MSG AFTER LDG.(<P>C/W FIM FT CH. 30-41 FAULT TREE 803, CKS GOOD AT THIS TIME.</P>)
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>)
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>)
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>)
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>)
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 & CHECK HARNESS, PERFORMED OPERATIONAL TEST, FOUND OK IAW AMM 30-41-00. THIS CLEARS MDDR 126512.</SPAN><BR DATA-MCE-BOGUS="1" /></P>)
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>)
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 & 71-00-00. OPS CHECK GOOD. NO DEFECTS NOTED. THIS CLEARS MDDR #126081.</P>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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.
"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>)
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>)
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>)
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>)
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>)
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>)
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>)
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 & CYCLED ANTI-ICE SEVERAL TIMES, NO DEFECTS NOTED. OPERATIONAL CHECK GOOD.</P>)
DURING DESCENT, "L ENG BLEED OFF" CAUTION MESSAGE. REMOVED AND REPLACED HIGH PRESSURE SHUT OFF VALVE IAW AMM 36-11-07.
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>)
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.
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>)
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.
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.
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'.
STATUS MESSAGE AFT EQUIPMENT EXH FAN 2.(<P>PERFORMED FIM 21-26 TASK 806. NO FAULTS FOUND.</P>)
HI FLOW INHIBIT STATUS MESSAGE.(<P>PERFORMED FIM 21-51 FAULT TREE 854. NO FAULTS NOTED.&NBSP;</P>)
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>)
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.
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.
STATUS MESSAGE FOR AFT EQUIP EXHAUST FAN NR 2. ACCOMPLISHED FIM TASK 21-26 FT 806. MESSAGE CLEARED. OPS CHECKED NORMAL.
STATUS MSG AFT EQUIPMENT EXH FAN 2(<P>PERFORMED FIM 21-26 FT 806, MSG ERASED. OPS CHK NORMAL AT THIS TIME.</P>)
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>)
"R BLEED OFF" MSG DISPLAYED & 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>)
FOUND SURGE VALVE DUCT DAMAGED.(<P>REMOVED AND REPLACED DUCT IAW B767 AMM 49-53-01, OPS CHECK GOOD.&NBSP;<BR /></P>)
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>)
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.
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>)
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.
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.
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>)
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>)
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>)
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 & L ENGINES ENSURING DUCT PRESSURE IS WITHIN REQUIRED LIMITS. THIS CLEARS DMI #119894. PLACARD REMOVED FROM FLT DECK AND MCC NOTIFIED.</P>)
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>)
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>)
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>)
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.
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)
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.
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.
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.
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.
RIGHT FWD WINDOW EICAS MESSAGE DURING APU START ATTEMPT. PERFORMED OPS CHECK IAW AMM 30-41-00, OPS CHECKS GOOD AT THIS TIME.
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.
RT FWD WINDOW EICAS MESSAGE UPON LANDING. PERFORMED OPS CHECK IAW AMM 30-41-00. OPS CHECKED GOOD AT THIS TIME.
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.
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.
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>)
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.
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.
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.
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>)
RECEIVED "RIGHT FWD WINDOW" EICAS AFTER LANDING. REMOVED AND REPLACED RIGHT WINDOW HEAT CONTROLLER IAW AMM 30-41-01. OPS CHECK GOOD.
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.
RH PACK CONTROLLER REQUIRES REPLACEMENT. REMOVED AND REPLACED RH PACK CONTROLLER IAW AMM 21-51-24. OPS CHECK GOOD AT THIS TIME.
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.
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.
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.
R FWD WINDOW EICAS MESSAGE. PERFORMED OPS CHECK OF RT FWD WINDOW HEAT, OPS CHECK GOOD AT THIS TIME IAW AMM 30-41-01.
APU INOP. PERFORMED OPERATIONAL CHECK OF APU IAW AMM 49-11-00, OPS CHECK GOOD.
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.
FWD RIGHT WINDOW HEAT INOP. PERFORMED BITE CHECK OF WINDOW HEAT CONTROLLERS PER AMM 30-41-00. NO FAULTS NOTED, MESSAGE CLEARED.
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
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.
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.
#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>)
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>)
#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>)
#2 ENGINE INBD LOWER IGNITION LEAD HAS ARC DAMAGE.(<P>REMOVED & REPLACED #2 ENG #1 SYSTEM IGNITOR LEAD IAW AMM 74-21-01. ASSET # 0019077, 0019114, 0018917 OPS CHECK ACCOMPLISHED ON TASK # T2031.</P>)
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>)
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>)
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.
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.
APU BITE MESSAGE ON EICAS DURING APU RUN. NO FAULTS ON ECU. REMOVED AND REPLACED APU ECU IAW AMM 49-61-05.</P>)
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.
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.
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.
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>)
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>)
APU SHUTDOWN - 0 OIL QUANTITY&NBSP;(<P>SERVICED APU OIL IAW AMM 12-10-00. APU OPS CHECK GOOD. NO DEFECTS NOTED&NBSP;</P>)
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>)
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&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>)
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>)
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.
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>)
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.
AFTER START, GOT "R GEN OFF". RECYCLED AND OPERATED NORMALLY. PERFORMED BITE TEST OK PER FIM 24-20. NO FAULTS NOTED AT THIS TIME.
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.
"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>)
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.
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>)
"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>)
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>)
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&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>)
LEFT SIDE WINDOW CAUTION MESSAGE IN FLIGHT(<P>PERFORMED BITE CHECK IAW FIM 30-41 F/T 804 OPS CHECK GOOD</P>)
LEFT PACK EXHAUST DOOR DOES NOT OPEN(<P>REMOVED AND REPLACED EXHAUST DOOR ACTUATOR IAW AMM 21-53-04 OPS CHECK NORMAL</P>)
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>)
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.
LEFT SIDE WINDOW EICAS MSG. REMOVED AND REPLACED THE LT SIDE WINDOW HEAT CONTROL UNIT IAW AMM 30-41-01. OPS CHECKED GOOD.
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>)
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&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 & 804, RES CHECK NORMAL AND WINDOW HEAT CONTROLLER, NO FAULTS. WINDOW HEAT OPERATION IS NORMAL. THIS CLEARS MDDR 110216. LC @ 23:25.</P>)
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.
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>)
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.
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>)
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.
TWO AIR COOLING DUCTS TORN ON APU.(<P>R/R BOTH AIR DUCTS COOLING DUCTS IAW AMM 49-51-00. NO LEAKS NOTED.</P>)
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>)
EMERGENCY GLOVES MISSING(<P>INSTALLED FIRE GLOVES PER LOPA FT 25-EEL REV 11.<BR /></P>)
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.
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>)
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>)
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>)
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>)
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>)
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.
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>)
STATUS MESSAGE AFT EQUIP EXHAUST FAN(<P>PERFORM FIM 21-58-PERFORMED OPS CHECK TEST OK PER AMM 21-26-00</P>)
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>)
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>)
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>)
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&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>)
&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>)
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 & 72-10-00</SPAN></P>)
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>)
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>)
RIGHT GENERATOR FAILED IN FLT. R & R THE RT ENGINE IDG IAW AMM 24-11-01,OPS CHECKED GOOD.
CREW OXYGEN PRESSURE INDICATOR INOPERATIVE. R & R THE CREW OXYGEN AVERAGE UNIT IAW 35-11-06. OPS CHECKED GOOD.
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.
CREW OXYGEN INDICATION INOPERATIVE. PERFORMED AN INSPECTION OF THE OXYGEN BOTTLE IAW AMM 35-11-00, OPS CHECKED GOOD.
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.
MAIN AIRCRAFT BATTERY NEEDS REPLACEMENT. R&R AIRCRAFT MAIN BATTERY IAW 24-31-01. OPS CHECK NORMAL.
RT ENGINE AFT FIRE LOOP TERMINAL BROKEN. R&R RT ENG FIRE LOOP IAW AMM 26-11-02. OPS CHECK NORMAL.
RT ENG FIRE LOOP TEMP REPAIR. INSTALLED TEFLON TUBING ON EXPOSED PORTIONS OF WIRE W5324-455R16 IAW AMM 26-11-21.
APU INOP. REMOVED AND REPLACED APU ECU IAW AMM 49-61-05 OPERATIONAL CHECK NORMAL.
STATUS MESSAGE AFT EQ EXH FAN NR 2. PERFORMED FIM 21-26-FT 8069 NO FAULTS NOTED AT THIS TIME.
APU INOP. REMOVED AND REPLACED TRANSDUCER MOTIONAL MONOPOLE, APU OPS CHECK NORMAL IAW AMM 49-61-02.
LT ENG OIL PRESSURE LIGHT NOT ILLUMINATED. RELAMPED PER AMM 33-16-02.
"WXR DSPY" MESSAGE ON CA HSI INTERMITTENTLY THROUGHOUT FLIGHT. REPEAT WRITE-UP. R&R HSI.
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.
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.
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.
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.
APU INOP. R&R APU ECU IAW 49-61-05 OPS GOOD.
STATUS MESSAGE RT ENG OH LP 2. PERFORMED OPERATIONS TEST FOUND NO FAULTS. CLEARED MESSAGE AND OPS CHECKED GOOD IAW AMM 26-15-00.
AFT EQ EXH FAN 2 STATUS MESSAGE DISPLAYED. RECYCLED AFT EQ EXH FAN 2 BREAKER MESSAGE CLEARED IAW AMM 21-58-41.
APU INOP. REMOVED AND REPLACED APU FUEL SOLENOID PER AMM 4931-03. PERFORMED LEAK & OPS CHECK.
UPON INSPECTION FOUND LEFT ENG OIL PRESSURE LIGHT INOP. REMOVED AND REPLACED OIL PRESS TRANSMITTER. OPS AND LEAK CHECK NORMAL AMM 79-32-01.
INTERMITTENT R FIRE LOOP 2 STATUS MSG. REMOVED AND REPLACED DETECTOR ASSY UPPER AFT IAW AMM 26-11-02 OPS CHECK NORMAL.
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.
APU GEN INOP. REMOVED AND REPLACED APU GENERATOR IAW AMM 24-21-01. OPS CHECK GOOD.
RT STARTER INOP. REMOVED AND REPLACED START VALVE IAW AMM 80-11-02 OPS AND LEAK CHECK GOOD.
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.
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.
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.
APU LOW OIL SHUTDOWN. REMOVED AND REPLACED APU GENERATOR IAW AMM 24-21-01. OPS CHECK GOOD.
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.
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.
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.
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.
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.
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.
RIGHT ENGINE FIRE LOOP 2 STAUS MESSAGE. TRANSFERED TO MDDR 97917 IAW MEL 26-11-01-01 CAT C PLACARD INSTALLED.
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.
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.
LT STARTER WOULD NOT CUT OUT. R&R LT ENGINE STARTER IAW AMM 80-11-01. OPS GOOD.
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.
RIGHT ENGINE FIRE LOOP 2 STATUS MSG. PERFORMED FIM TASK 26-11 FAULT TREE 806, NO FAULT NOTED. OK FOR SERVICES.
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.
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.
APU STARTER MOTOR BRUSH WEAR INDICATOR IS WORN. REMOVED AND REPLACED STARTER IAW AMM 49-41-11.
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.
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.
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.
APU INOP. REMOVED AND REPLACED APU IAW AMM 49-11-01.
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
AFT EQ EXH FAN 2 STATUS DISPLAYED. PERFORMED AFT EQ FAN TEST REF AMM 21-58-41. NO DEFECTS NOTED. NO EICAS MESSAGE SHOWING.
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.
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.
APU SHUTDOWN, WOULD NOT RESTART, WENT TO 48% AND SHUTDOWN. REMOVED AND REPLACED IGV ACTUATOR BRACKET IAW AMM 49-52-02. OPS CHECKED NORMAL,
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.
STATUS MESSAGE FOR THE LEFT ENGINE HP SOV. PERFORMED FIM 36-20-FT 804, NO FAULTS INDICATED. MESSAGE CLEARED, NO HISTORY NOTED.
APU INOPERATIVE. REMOVED AND REPLACED APU CONTROL UNIT IAW AMM 49-61-05, OPS CHECKED GOOD.
APU FAILED TO START AFTER LANDING. REMOVED AND REPLACED SCAVENGE FILTER IAW AMM 49-27-03 OPS AND LEAK CHECKED GOOD.
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.
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.
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.
COLD WARM GAUGE FOR TEMP CONTROL FLUCTUATES ERRADICALLY. PERFORMED AN OPS CHECK OF THE PACKS. OPS CHECKS GOOD IAW AMM 21-61-00.
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.
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.
RIGHT ENGINE WILL NOT INDICATE RUNNING ON ASM PROGRAM. REPAIRED A BROKEN WIRE IAW WDM 36-11-52.
LEFT PACK TEMP ILLUMINATED ON APPROACH. REMOVED AND REPLACED THE LT PACK TEMP VALVE IAW AMM 21-51-12, OPS CHECKED OK.
APU FAULT. REMOVED AND REPLACED THE APU TRU IAW AMM 24-32-04, OPS CHECKED NORMAL.
STRANGE ODOR APPEARED, LIKE BURNING. PERFORMED AMM 05-61-66, INSPECTION OF SMOKE OR FUMES IN THE COCKPIT, NO DETECTION OF SMOKE NOTED.
STATUS MESSAGE RT ENG FIRE LOOP. ACCOMPLISHED ENGINE FIRE DETECTION SYSTEM OPS TEST IAW AMM 26-11-00 NO FAULTS NOTED AT THIS TIME.
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.
L2 WINDOW HEAT INOPERATIVE. CAME BACK AFTER CONTROLLER REPLACED.
LEFT SIDE WINDOW HEAT INOPERATIVE. REMOVED AND REPLACED THE L2 WINDOW HEAT CONTROLLER, OPS CHECKED GOOD IAW AMM 30-41-01.
LEFT EEC NORMAL LIGHT INOPERATIVE. REPLACED THE SWITCH, OPS CHECKED GOOD.
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.
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.
DURING CLIMB, THE RIGHT ENGINE PRV EICAS. AFTER CLIMB, WENT AWAY. PERFORMED FIM 36-10 F/T 847, NO FAULTS FOUND. OPS CHECKED GOOD.
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.
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.
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.
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.
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.
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.
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.
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.
CORROSION FOUND ON LT SKIN STIFFENER BS 955. REPAIRED IAW EO 6753A070, REV 11. CHECKED NORMAL.
FOUND THE LT UPPER WING BETWEEN FILL PORT ADAPTER AND WING UPPER SKIN CORRODED. REPAIRED IAW EI T2017A57M-2414, REV 2. CHECKED NORMAL.
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.
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.
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.
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.
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.
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.
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.
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.
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.
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.
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.
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.
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.
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.
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.
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.
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>)
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>)
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.
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.
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.
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.
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.
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.
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.
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.
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.
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.
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.
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.
NR 1 ENGINE EXHAUST FWD 11 O'CLOCK SPRING SEAL WORN. REPLACED THE SPRING SEAL IAW AMM 70-50-00-912-001, REV 123.
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.
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.
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.
RIGHT WING INBOARD AFT FLAP UPPER SURFACE, IFS 257.485 CORRODED. REPAIRED THE AREA IAW EI T2017A57M-2363, REV 2.
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.
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.
2R THRUST REVERSER FORWARD INNER TORQUE BOX RIVET WORN. REMOVED AND REPLACED THE DAMAGED RIVETS IAW SRM 51-40-02-0G-0, REV 105.
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.
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.
FOUND PAX WINDOW FRAME CORRODED, BS 775. REMOVED AND REPLACED IAW SRM 51-40-02, REV 106, AND DWG 143T3351, SH5, REV A.
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.
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.
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.
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.
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.
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.
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.
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.
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.
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.
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.
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.
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.
ORD - FIRST OFFICER WINDSHIELD CRACKED AND ARCING. REPLACED FIRST OFFICER WINDSHIELD IN ACCORDANCE WITH MM 56-11-00-4. SYSTEM GROUND CHECKED NORMAL OPERATION.
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)
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
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.
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)
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)
TUL - FOUND STRINGER NR 68 CRACKED APPROXIMATELY STATION 4000. INSTALLED NEW STRINGER AND SPLICE PAGE SRM 51-70-0L. (M)
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)
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)