N1321A

ATA 2130

AIRPLANE DOES NOT HOLD PRESSURE AT 350 PRES. DIFF VARIES BETWEEN 7.8 - 8.6. CABIN ALT VARIES 5400 - 8000 FEET RATE VARIES BETWEEN & AND - 500 FT. REMOVED AND REPLACED CABIN PRESSURE SELECTOR IAW AMM 23-31-01. OPS CHECK OK. C/W A/C PRESSURIZATION IAW AMM 05-51-24. NO DEFECTS NOTED. A/C REMAINS E180. A/C RETURNED TO SERVICE.

ATA 2421

L AC BUS OFF AT TOP OF CLIMB OUT FROM CVG BOUND FOR MHT. CREW RAN THROUGH THE QRH AND RESET EVERYTHNING. THEY DECLARED AN EMERGENCY (EDC) AND RETURNED TO CVG WITHOUT INCIDENT. (ATB). MAINTENANCE REMOVED AND REPLACED GCU IAW AMM 24-22-02. OPS CHECK GOOD AC REMAINS ETOPS 180. AIRCRAFT RETURNED TO SERVICE.

ATA 2610

DURING TAXI OUT, AFTER ENG START CHECKLIST R STRUT DCT LEAK & L STRUT DCT LEAK EICAS MESSAGE. MAINTENANCE REMOVED AND REPLACED DUCT LEAK DETECT CARD IAW B767 AMM 26-10-01. OPS CHECK GOOD. A/C REMAINS NO ETOPS. A/C RETURNED TO SERVICE.

ATA 2760

ON PUSHBACK, LOST ALL "C" HYD SYSTEM FLUID. VERY LARGE LEAK FROM LEFT WING OBSERVED (#3 SPOILER PCA PACKING). AIRCRAFT RETURNED TO BLOCKS (BTB). MAINTENANCE FOUND PACKING LEAKING ON SPOILER ACTUATOR. REMOVED & REPLACED PACKING IAW B767 AMM 27-61-02 & SERVICE "C" HYD IAW AMM 12-12-01. OPS CHECK GOOD & NO LEAK NOTED IAW AMM 29-11-00. AIRCRAFT RETURNED TO SERVICE.

ATA 2910

DURING CRUISE, C HYD QTY DROPPED TO NEAR ZERO CAUSING A C HYD PRESS TO DROP TO ZERO. AIRCRAFT RETURNED TO RFD (ATB). FOUND LEAK AT INBD SPOILER ACTUATOR ASSY FILTER CAP SEAL. REPLACED ORING AT INBD SPOILER LEFT WING IAW AMM 27-61-02. OPS CHECK GOOD. NO LEAKS NOTED AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.

ATA 3610

R ENG BLEED OFF MESSAGE APPEARED INTERMITTENT WHILE TAXIING AND AFTER TAKING THE RUNWAY FOR IDLE UP DEICE RUN-UP. AIRCRAFT RETURNED TO BLOCKS (BTB). ACCOMPLISHED THUMB TEST OF RT HPSOV IAW AMM 36-11-07 NO FAULTS PRESENT CYCLED PRV AND PRSOV NO ISSUES NOTED BOTH VALVES CYCLE SMOOTH. SWAPPED LT & RT BLEED CARDS REF B767 AMM 36-11-12 ACCOMPLISHED ENGINE RUNS AT IDLE IAW AMM NO MESSAGES OR LIGHTS PRESENT AT IDLE OR AT START RETURNED BLEED CARDS TO ORIGINAL POSITIONS NO ABNORMAL FAULTS PRESENT AT THIS TIME ACFT REMAINS NO ETOPS. AIRCRAFT RETURNED TO SERVICE.

ATA 2822

DURING TAXI OUT, RT AFT FUEL PUMP LOW PRESSURE LIGHT AND EICAS MESSAGE CAME ON, ACFT RETURNED TO THE GATE (BTB) AND MTX GROUNDED A/C , MTX DEFERRED RT AFT FUEL PUMP IAW MEL 28-22-1. AND RETURNED A/C TO SERVICE.

ATA 7933

ON TAXI OUT,  RT ENGINE OIL TEMP INDICATION BLANKED AFTER ENGINE START, ACFT RETURNED TO THE GATE AND MTX GROUNDED ACFT , TROUBLESHOT AND FOUND NR 2 ENGINE OIL TEMP SENSOR DAMAGED. REMOVED AND REPLACED THE SENSOR IAW AMM 79-34-01. OPS CHECKED GOOD, ALL INDICATIONS GOOD .ACFT REMAINS NO ETOPS .MTX RETURNED ACFT TO SERVICE.

ATA 5730

DURING C-CHECK AT AMES (TPA) CORROSION WAS OBSERVED ON THE RIGHT-WING UPPER SURFACE SKIN PANEL NUMBER 1 ON STA WS 616 , THE DAMAGE WAS REMOVED BY BLENDING AFFECTED AREA PER SRM 51-10-02 WITH MEASURED MATERIAL REMAINING OF 0.133¿ INCHES FROM INITIAL THICKNESS OF 0.170¿, INCH (UT MEASURED) WITH MATERIAL LOSS OF 0.037 INCH (23.5%), FOUND TO BE OUT OF LIMITS PER SRM 57-20-01, ALLOWABLEDAMAGE 1, TABLE I OF 0.030 INCHES. AMES CONTACTED FLIGHT VEHICLES CONSULTING INC. REQUESTING FURTHER EVALUATION AND REPAIR APPROVAL. .COMPLIED WITH IAW ABX-REA-5725-65599-00.

ATA 5730

DURING C-CHECK AT AMES (TPA) CORROSION WAS OBSERVED ON THE LEFT-WING UPPER SURFACE SKIN PANEL NUMBER 1 AT WS 434 OVER UPPER RIB FLANGE P/N 113T1545-7, THE DAMAGE WAS REMOVED BY BLENDING AFFECTED AREA PER SRM 51-10-02 WITH MEASURED MATERIAL REMAINING OF 0.145¿ INCHES FROM INITIAL THICKNESS OF 0.200¿, INCH (UT MEASURED) WITH MATERIAL LOSS OF 0.055 INCH (27.5%), FOUND TO BE OUT OF LIMITS PER SRM 57-20-01, ALLOWABLE DAMAGE 1, TABLE I OF 0.035 INCHES. AMES CONTACTED FLIGHT VEHICLES CONSULTING INC. REQUESTING FURTHER EVALUATION AND REPAIR APPROVAL. COMPLIED WITH REA ABX-REA-5725-65598-00.

ATA 7600

DURING DESCENT, ON THE ARRIVAL TO MIA, L & R ENG CONTROL STATUS MESSAGES. RIGHT ENGINE WOULD NOT ACCELERATE FROM IDLE. DECLARED EMERGENCY AT APPROX. 1930Z AND LANDED AT MIA. AFTER LANDING L & R ENGINE CONTROL EICAS MESSAGES APPEARED. MIA FIRE DEPARTMENT CHECKED A/C, EVERYTHING LOOKED NORMAL. REMOVED AND REPLACED M644EEC DISCRETE PRINTED CIRCUIT CARD, PER B767-300 AMM 73-21-11 AND REMOVED & REPLACED RIGHT ENG HMU IN REF WITH B767 AMM 73-21-14. OPS CHECK OK. NO LEAKS. A/C REMAINS NO ETOPS AND RETURNED AC TO SERVICE.

ATA 2697

DURING CRUSE FLIGHT L STRUT DUCT LEAK MSG IN-FLIGHT. DID NOT CLEAR AFTER PACK "OFF" & BLEEDS REMOVED, AC THEN DIVERTED TO CLT.BECAUSE OF ICE CONDITIONS AT CVG. AFTER LANDING MTX GROUNDED AC AND TROUBLESHOT TIGHTNED WIRES ON L STRUT TS236. RUNG WIRES PIN 1 & PIN 20 ON C/P D10224, READ 4¿. PERFORMED UPSTREAM LEAK CHECK FROM PRSOV, NO PNEUMATIC LEAKS NOTED. SWAPPED BLEED AIR CONTROL CARDS M859 & M860 FOR T/S. PERFORMED AIR/GROUND TEST. NO DEFECTS FOUND. SYSTEM OPS CHECK GOOD AT THIS TIME. WORK DONE IAW B767 AMM 26-18-00, 20-10-01, 36-11-09, AND B767 WDM 26-18-12. AIRCRAFT REMAINS NO ETOPS.AND RETURNED AC TO SERVICE .

ATA 7532

ON TAXI OUT, R ENG BLEED EICAS MSG ILLUMINATED. AIRCRAFT RETURNED TO BLOCKS. (BTB). MAINTENANCE REPLACED RT ENGINE PRSOV IAW AMM 36-11-09, RAN RT ENGINE AS PER AMM 71-00-00 AND ABX B767-10A. OPS CK NORMAL PER B AMM 36-11-09. AIRCRAFT REMAINS NO ETOPS. AIRCRAFT RETURNED TO SERVICE.

ATA 2210

AUTOPILOT EICAS MESSAGE ON BLOCK OUT. AIRCRAFT RETURNED TO BLOCKS. (BTB). MAINTENANCE DEFERRED RALM STATUS TO CAT 1 MBCB C-CK, PLACARD INSTALLED. PERFORMED MCDP TEST 30/40 IAW B767 AMM 22-00-02. NO FAULTS NOTED AT THIS TIME. PLACARD REMOVED. DI CLEARED. NO REACTIVATION PROCEDURES REQUIRED. RALM PLACARD REFLECTS CURRENT STATUS. A/C RELEASED CAT III B. A/C RETURNED TO SERVICE.

ATA 2230

LOW SPEED ABORT DUE TO AUTOTHROTTLES NOT ENGAGING AT 50 KTS AFTER A/C ABORTED T/O , THEY RETURNED TO THE GATE AND MTX GROUNDED A/C AND DEFERRED THE AUTO- THROTTLE IAW MEL ABX-22-30-1. AND RETURNED A/C TO SERVICE .

ATA 2210

DURING TAXI AUTOPILOT DESCRETE LIGHT STAYS ILLUMINATED AC RETURNED TO GATE (BTB) AND MTX GROUNDED AC . MTX PERFORMED FIM 22-02 F/T 801 MESSAGE CLEARED. A/C REMAINS CAT I.AND REURNED AC TO SERVICE

ATA 3150

ON PUSH GOT A/P EICAS & DISCREET LIGHT. TRIED RESETTING AND BOTH REMAINED.AC TRTURNED TO GATE (BTB)AND MTX GROUNDED AC T/S AS PER FIM 22-03-00 NO FAULTS NOTED PERFORMED MCDP GND TEST 30 NO FAULTS PERFORMED TEST 40 TEST NO FAULTS. PERFORMED 22-03 FT 818. 819 A/C DOWNGRADED TO CATI. AC RETURNED TO SERVICE

ATA 7830

WHILE TAXIING R REV ISLN VAL MSG AFTER ENG START,AC RETURNED TOGATE (BTB) AND MTX GROUNDED AC , MTX DEFERRED RH T/R FOR DEPARTURE IAW MEL ABX-78-31-1, AND RETURNED AC TO SERVICE . AND AC DEPARTED

ATA 8000

DURING TAXI #2 ENG START SELECTOR, SELECTED TO " GROUND" "VALVE" LIGHT DID NOT APPEAR ON THE SINGLE + BOTH POSITION. AC RETURNED TO THE GATE AND WAS GROUNDED BY MTX. MTX THEN DEFERRED THE RH ENGINE START CONTROL IAW MEL ABX-80-00-2-1 RETURNED AC TO SERVICE ,AND THE AC DEPARTED .

ATA 3340

AFTER  ENG START AND PUSH BACK , TURNED ON WING AND TAXI LIGHT AND STARTED LH PACK, COCKPIT FILLED WITH ACIDIC/ SMOKEY SMELL. TAXIED OUT BUT RETURNED TO GATE, SMELL DID NOT GO AWAY.(<P>PER CONVERSATION WITH CREW AND DVI OF LIGHT CONTROL PANELS, FOUND RUNWAY TURNOFF SWITCH BURNT AND ARCHING. R/R LIGHTING CONTROL PANEL ASSY PER AMM 33-13-00, OPS CHECK GOOD. NO FURTHER OVERHEATING/ ARCHING</P>)

ATA 3397

STRONG SMELL OF BURNING WIRE AFTER TURNING ON LIGHTS AT FL180. LASTED ONLY A FEW SECONDS. NO SMOKE PERCEIVED(<P>FOUND BURNT TERMINAL ON LH POSITION LIGHT C/B. R/R TERMINAL IAW SWPM 20-30-11. OPS CHECKS GOOD AT THIS TIME. PERFORMED CHAPTER 5 INSPECTION OF FUMES IN THE CABIN IAW AMM 05-51-56. INSPECTION IS GOOD AT THIS TIME. R/R LH POSITION LIGHT C/B IAW B767 WDM 33-43-11-6.1. C/B CHECKS GOOD AT THIS TIME</P>)

ATA 3310

BURNING SMELL DETECTED IN COCKPIT DURING LANDING FOR 10 - 20 SECONDS(<P>REMOVED AND REPLACED BURNT OUT KORRY SWITCH MODULE ASSY FOR TAT AND AUTO SPEEDBRAKES ANNUNCIATOR LIGHTS IAW SWPM 20-84-18. ALLOWED LIGHTS TO WARM UP, MEASURED TEMPS, TEMPS MEASURED SIGNIFICANTLY LOWER. NO BURNING SMELL WAS PRESENT. MCC NOTIFIED. PICTURES SENT TO MCC.</P>)

ATA 2700

LEFT ELEVATOR, BETWEEN ELEVATOR INBOARD AND OUTBOARD, IN FRONT SPAR HSBL 113.30 WITH FOD.(<P>LEFT ELEVATOR, BETWEEN ELEVATOR INBOARD AND OUTBOARD, IN FRONT SPAR HSBL 113.30 WITH FOD WAS REMOVED AND CLEANED IAW AMM 12-17-02-103-057.</P>)

ATA 3200

RH NEW MAIN LANDING GEAR, DUE SHOCK STRUT, ELECTRICAL CONDUIT P/ N: 287T6104-74 AND S/N: 6512, CRUSHED, IS NECESSARY TO CHECK THE INTERNAL ELECTRICAL WIRING(<P>RH NEW MAIN LANDING GEAR, CHECK THE INTERNAL ELECTRICAL WIRING CONTINUITY BETWEEN J2-J4. SATISFACTORY TEST IAW WDM 27-62-11 AND 32-09-12.</P>)

ATA 5310

FUSELAGE EXTERIOR SURFACES, STA 196.5 APROX. WITH LIGHTNING STRIKES.(<P>FUSELAGE EXTERIOR SURFACES, STA 196.5 APROX LIGHTNING STRIKES WERE REPAIRED PER SRM&NBSP;<SPAN>SRM 53-00-01-2R-8 (</SPAN>MAJOR REPAIR)</P> / <P>&NBSP;</P>)

ATA 2800

LH WING, LOWER SURFACE, BODY SPLICE PLATE, STRINGER L-6 AREA WITH FUEL LEAK(<P><SPAN>LH WING LOWER SURFACE BODY&NBSP;</SPAN><SPAN>SPLICE PLATE STRINGER L-6 AREA WITH FUEL&NBSP;</SPAN><SPAN>LEAK WAS REPAIRED AND THE TEST WAS SATISFACTORY.</SPAN></P>)

ATA 2800

WING LEFT ACCES PANEL 531BB BEETWEN RIB 3/RIB 4 LINE BROKEN(<P><SPAN>THE LINE BROKEN IN ACCESS PANEL&NBSP;</SPAN><SPAN>531BB BEETWEN RIB 3 / RIB 4 WAS REPLACED&NBSP;</SPAN><SPAN>I.A.W AMM 28-22-07</SPAN></P>)

ATA 2800

RH WING, LOWER SURFACE, BODY SPLICE PLATE, STRINGER L-10 AREA WITH FUEL LEAK(<P>RH WING LOWER SURFACE BODY SPLICE PLATE STGR 10 FUEL LEAK WAS REPAIRED AND THE TEST WAS SATISFACTORY IAW AMM 28-11-00-308-013</P>)

ATA 2800

LH WING LOWER SKIN ON L-6 BETWEEN WS375.8 AND WS404.4 WITH FUEL LEAKAGE(<P>LH WING LOWER SKIN ON L-6 BETWEEN WS375.8 AND WS404.4 FUEL LEAK WAS REPAIRED AND THE TEST WAS SATISFACTORY IAW AMM 28-11-00-308-013</P>)

ATA 2700

DERIVED FROM TASK CARD 27-076-00-01, RUDDER FREEPLAY. UPPER RUDDER PCA OUT OF LIMITS(<P>PCA WAS REPLACED IAW AMM 27-21-02-422-038. OPS CHECK GOOD</P>)

ATA 2800

LH WING LOWER SKIN NEAR OF REAR SPAR BETWEEN WS404.4 AND WS433.1 WITH FUEL LEAKAGE(<P>LH WING LOWER SKIN NEAR OF REAR SPAR BETWEEN WS 404.4 AND WS 433.1 FUEL LEAK WAS REPAIRED AND THE TEST WAS SATISFACTORY IAW AMM 28-11-00-308-013</P>)

ATA 5100

DAMAGED HARNESS #12, WHICH IT IS LOCATED UNDER LH FAN COWL, ENGINE #1(<P>ELECTRICAL WIRE WAS REPAIRED I.A.W SWPM 20-10-13. NO FURTHER DEFECTS NOTED</P>)

ATA 2700

LH HORIZONTAL STABILIZER, ELEVATOR OUTBOARD PCA WITH FREE PLAY(<P>LH HORIZONTAL STABILIZER, ELEVATOR OUTBOARD PCA WAS REPLACED IAW AMM 27-31-05-424-027. OPS CHECK GOOD</P>)

ATA 5700

RH MAIN LANDING GEAR, SUPPORT AFT BEAM, BUSHING AFT FACE WITH CORROSION.(<P>RH MLG, SUPPORT BEAM AFT TRUNNION BUSHINGS WERE REPLACED AND CORROSION WAS REMOVED PER CMM 57-54-33 / MXA EO TRE6757192. NO FURTHER DEFECTS NOTED</P>)

ATA 2761

AT 10500' WHILE ON DESENT, SPOILERS WERE EXTENDED AND AILERONS WENT TO 2 UNITS RIGHT IN ORDER TO MAINTAIN STRAIGHT AND LEVEL FLIGHT. EICAS SPOILER MESSAGE SHOWED. RAN QRH CHECKLIST. USED FLAPS 20 FOR LANDING AND SPEED 170 FOR WIND ADDITIVE.(<P>FOUND # 6 SPOILER ACTUATOR VALVE STUCK IN OPEN POSITION. REPLACED SPOILER PCA IAW B-767 AMM 27-61-02-424-023.OPERATIONAL CHECK COMPLETED PER AMM 27-61-00/001, NO ISSUES FOUND. SPOILER RIGGED COMPLETED PER B-767 AMM 27-61-02-424-23, ALL CHECKS GOOD. BITE CHECKED SPOILER CTRL MODULE, NO ISSUES FOUND. REF FIM 27-09 FT 808.</P>)

ATA 7100

ABNORMAL VIBRATION IN LEFT ENGINE. VIBE GAUGE FLUCTUATED 1.1 - 1.9 AND CAN FEEL IT IN FLIGHT DECK VIBRATION.(<P>PERFORMED IDLE RUN OF LEFT ENG IAW AMM 71-00-00 FAN VIB AT PEAK. HIGHEST VIB WAS .4 N2 MOMENTARILY, .2 N2 NORMALLY. NO JUMPING INDICATIONS. ALL INDICATION NORMAL AT THIS TIME. PERFORMED AIRFRAME VIB CONDITIONAL INSPECTION IAW B767 AMM 05-51-38 ITEM 2. LOWER RH T/REV V-BAND CLAMP DISCOVERED TO BE EXTREMELY LOOSE. ADJUSTED T/REV V-BAND LATCH TO CORRECT TENSION PER B767 AMM 78-31-02. PERFORMED GVI OF POWERPLANT AND COMPONENTS PER AMM 71-00-00, NO FURTHER DEFECTS FOUND.</P>)

ATA 5100

NLG FWD CUTOUT SEAL RETAINER EVIDENCE OF CORROSION.(<P>AT NLG FWD CUTOUT, REMOVED SEAL AND CLEANED LIGHT SURFACE CORROSION. NO DAMAGE NOTED, REF. SOPM 30-20-03 AREA TREATED AND PRIMED, REF. B767 AMM 51-21-04, RE-INSTALLED SEAL, REF. 51-31-51-302-001.</P>)

ATA 2100

EICAS MESSAGE,"L PACK TEMP", "FWD EQPT OVHT, &AMP; "CABIN ALTITUDE" RECEIVED IN CRUISE.(<P>DUE TO L PACK TEMP REACHING OVER 35 DEG. IN COCKPIT, CREW RECEIVED FWD EQPT/OVHT. CREW WENT TO OVERIDE TO DUMP HEAT THEN BACK TO AUTO AND MESSAGE WENT AWAY. PERFORMED BITE CHECK, NO DEFECT NOTED IAW FIM 21-58 TASK 803.</P> / <P>AS A RESULT OF GOING OVERIDE FOR EQUIPMENT COOLING AND ONLY RUNNING ONE PACK, CABIN ALTITUDE MSG WAS A RESULT. ONCE EQUIPMENT COOLING WAS PUT TO AUTO, CABIN ALTITUDE STABILIZED. OVERIDE OPENS THE AVIONICS OVERFLOW DOOR. SYSTEM OPERATED AS NORMAL, NO DEFECT NOTED IAW AMM 21-53-00.</P> / <P>TRANSFERED TO MEL 154997 IAW 21-51-01-01. CAT C. COMPLIED WITH MX PROCEDURES. PLACARD INSTALLED. EXP 22OCT21. DC @ 0655Z.</P> / <P>LP 1440132: ITEM M5: REMOVED AND REPLACED LH PACK RAM AIR EXHAUST DOOR ACTUATOR IAW AMM 21-53-02. ALL CHECKS GOOD. THIS CLEARS MDDR 154997. PLACARD REMOVED. LH PACK RE ACTIVATED. DC @ 1017Z</P> / <P>&NBSP;</P>)

ATA 3610

L BLD DUCT LEAK. TURNED LT PACK ON AND OFF, MESSSAGE CLEARED, PERFORMED OPS CHECK PER AMM 21-51-00, OPS CHECKED GOOD.

ATA 3510

FIRST OFFICERS OXYGEN MASK FRAYED ON RIGHT SIDE. REMOVED AND REPLACED F/O O2 MASK IAW B767 AMM 35-11-51 OPS AND LEAK CHECK GOOD AT THIS TIME.

ATA 4990

APU OIL LEAK(<P>TRANSFERRED TO MDDR 151204 IAW MEL 49-11-01A, CAT C.</P> / <P>LP 1369335 ITEM 2. REMOVED AND REPLACED CAP AND ADAPTER ASSEMBLY IAW CMM 49-22-11 AS PER ECM 2021P-245. OPS AND LEAKS CHECKS GOOD. THIS CLEARS MDDR 151204.</P>)

ATA 2150

AFTER LANDING FWD EQPT VAL CAUTION MESSAGE DISPLAYED. THE QRH DID NOT CLEAR THE EICAS MESSAGE. PERFORMED FIM TASK 21-58 F/T 985, FOUND TO BE SHORT TERM POWER INTERRUPTION. MSG DISTINGUISHED. NO OTHER DEFECTS NOTED AT THIS TIME.

ATA 4990

APU OIL QTY EICAS MESSAGE DISPLAYED(<P>UPON FURTHER INVESTIGATION FOUND APU OIL CAP NOT SECURED.. SERVICED APU IAW B767AMM 12-13-04</P>)

ATA 4990

APU OIL SHOWS 50%(<P>SERVICED APU 1 QUART, SHOWS FULL, PERFORMED INSPECTION AT APU, NO LEAKS NOTED I/A/W AMM 49-05-03 AND 12-13-04. TRANSFERRED TO MDDR # 150932, CAT C, PER DDG 49-11-01A.</P> / <P>LP 1369331 ITEM 7: T/S APU OIL LEAK PER B767 FIM 49-11, FAULT TREE 972. PROCEEDED TO REMOVE AND REPLACE APU SHUTOFF VALVE ASSY IAW B767 AMM 49-27-11. VALVE AND APU CHKS OK. NO LEAKS NOTED AT THIS TIME. THIS CLEARS DMI# 150932. MEL AND PLAC REMOVED.</P>)

ATA 3610

RT ENG BLEED VALVE LIGHT INOP.(<P>TRANSFERRED TO MDDR 150803 IAW DDG 36-22-01-02 CAT C DUE 06AUG21</P> / <P>REF LOGPAGE 1390844.ITEM 4... R/R RH ENGINE HIGH PRESSURE CONTROLLER IAW AMM 36-11-08. OPS CHECK GOOD. THIS CLEARS DMI 150803</P>)

ATA 4997

APU FAULT INDICATED ON START ATTEMPT. STATUS SCREEN SHOWS ADD OIL(<P>SERVICED APU OIL IAW 49-27-00. SUSPECT OIL LEAKING PAST OIL FILL CAP. REMOVED AND REPLACE OIL FILL CAP IAW AMM 20-11-00. OPS CKS GOOD.</P>)

ATA 4950

NO APU DUCT PRESSURE(<P>TRANSFERRED TO DMI # 150428 IAW MEL 49-11-01-01 CAT C. MCC NOTIFIED. PLACARDS INTALLED. DP 1425Z.</P> / <P>22JUL21 - LP 1370369 - ITEM# 5 - CVG - REMOVED AND REPLACED APU BLEED VLV.&NBSP; IAW B767 AMM 36-11-10. OPS CHECK OK. THIS CLEARS MDDR 150428. PLACARD REMOVED. DISP: YK @ 1343Z</P>)

ATA 4900

APU INOP ( AUXILIARY POWER UNIT (APU), ER OPERATIONS NOT ALLOWED (NOTIFY DISPATCH) R60 )(<P>TRANSFERRED TO MDDR 150385 IAW MEL 49-11-01A, CAT C.</P> / <P>LP 1486189: PERFORMED FIM. 49-11 FT 988. NO DEFECTS NOFECTS NOTED. APU OPS CHECK GOOD. THIS CLEARS DMI 150385. MCC NOTIFIED. PLACARDS REMOVED.</P>)

ATA 5610

ON TAKEOFF CLIMB FIRST OFFICERS R2 WINDOW OPENED. RETURNED BACK TO RFD FOR A NORMAL LANDING(<P>CHECKED R2 WINDOW, RIGGING, TRACK AND LATCH WORKING PROPERLY. VISUALLY INSP INSIDE AND OUTSIDE NO ABNORMAL SIGN IAW AMM 56-11-02. WINDOW CLOSED AND LATCHED</P>)

ATA 3150

EICAS MESSAGE L ENG PRV CLEARED AT 1500FT, STATUS MSG L ENG PRV(<P>T/S PER FIM 36-10 FT 847. NO FAULTS NOTED.</P>)

ATA 8012

LEFT ENG START VALVE FAILED TO OPEN.(<P>.ITEM TRANSFERRED TO MDDR 149390 PER MEL 80-00-02-01 CAT C DUE DATE 09JUL21. DC @ 07:09Z.</P> / <P>01JUL21 - 1480181 - ITEM# 3 - ONT - R/R # 1 ENG START VALVE IAW AMM 80-11-00. OPS CHECK GOOF, LEAK CHECK GOOD. THIS CLEARS MDDR # 149390, PLACARD REMOVED, MCC NOTIFIED. SP @ 0043Z</P>)

ATA 3150

"FWD EQUIP VAL" ILLUMINATED DURING APPROACH, EXTINGUISHED AFTER TOUCH DOWN.(<P>PERF OPS CHECK FWD EQP COOLING PER AMM 21-58-00. ALL MODES OPERATE NORMAL, NO FAULTS NOTED.</P>)

ATA 2150

UNABLE TO CONTROL FLT DK TEMP IN AUTO OR MANUAL TEMP CONTROL GAGE SAID FULL COLD BUT TEMP RISING. SAME CONDITION IN STBY MODE. ABLE TO CONTROL TEMP BY SHUTTING OFF (C) PACK(<P>REPACKED AND PERF BITE OF TEMP CONTROLLER IAW AMM 21-51-00. NO FAULTS NOTED. TESTED LH/RH PACKS ALONE AND BOTH TOGETHER. TEMP RISE AND FALL NORMAL. NO DEFECTS NOTED.</P>)

ATA 3150

LEFT PRV EICAS MSG.(<P>PERFORMED BITE TEST. TESTED NORMAL REF AMM 36-23-00.&NBSP;</P>)

ATA 3350

EMERGENCY LIGHTS SWITCH WIRE GUARD MISSING FROM SWITCH. LOCATED IN FLIGHT DECK.(<P>ADJUSTED WIRE GUARD ON TOGGLE SWITCH PER SWPM 20-83-11. OPS CHECK GOOD PER AMM 33-51-08.</P>)

ATA 2150

AFT EQ EXH FAN2 STATUS MSG(<P>RESET C/B ON PANEL P11, ROW B, COL 10 IAW 767 AMM 20-60-01-862-001. FAN TEST GOOD IAW AMM 21-26-01-400-002. NO DEFECTS NOTED AT THIS TIME.</P>)

ATA 4920

APU BURN WAS EXCESSIVE. IN 1.5 HOUR APU BURNED 1,000 LBS.(<P>PERFORMED OPS CHECK OF APU IAW 49-11-00-802-002. OPS &AMP; LEAK CHECK GOOD. IAW 49-21-00-206-001<BR /></P>)

ATA 5320

LEFT (CAPT) SIDE EVAS HOOK AND LOOP PULLING UP FROM GLARE SHIELD DEFERRED TO MDDR # 144481 MEL 25-63-06 CAT D. DUE 26JUL21. LP 1254963: RESECURED CAPT SIDE EVAS HOOK AND LOOP FROM GLARESHIELD IAW SRM 51-30-10. NO FURTHER DEFECTS NOTED. THIS CLEARS MDDR 144481. MCC NOTIFIED, PLAC REMOVED.

ATA 7200

LH ENGINE @ CLIMB POWER 104.2 N1 A VIB 3.5(<P>ENGINE VIB WITHIN LIMITS IAW AMM 71-00-00. TEST 6. ALSO PERFORMED GVI INSPECTION IAW AMM 72-00-00</P>)

ATA 3610

ON INITIAL CLIMB "L ENG BLEED OFF" EICAS MESSAGE. RAN QRH PROCEDURE, NO RESOLUTION.(<P>TRANSFERRED TO MDDR 144109 PER DDG 36-11-02-02, CAT C, DUE 30MAR21.</P><P>LP&NBSP;<SPAN>1480687:&NBSP;</SPAN><SPAN>REMOVED AND REPLACED LT PRSOV IAW B767 AMM 36-11-09. COMPLETED UP TO SUBTASK 36-11-090-722-085-001. PERFORMED IDLE ENGINE RUN IAW AMM 71-00-00. PERFORMED LEAK CHECK AND TEST OF PRSOV IAW AMM TASK 36-11-09. OPS CHECK OK. NO LEAKS NOTED. THIS CLEARS MDDR 144109.</SPAN></P>)

ATA 2432

MAIN BAT CHARGER EICAS MESSAGE(<P>T/S FIM 24-31-F/T 803. MAIN BATT. CHARGER TEST OK AMM 24-31-02/714</P>)

ATA 3240

AUTO BRAKES DISARMED IN FLIGHT, COULD NOT BE RESET(<P>T/S FIM 32-42 F/T 803; ANTI / SKID AUTOBRAKE LTL UNIT BITE, NO FAULT INDICATED</P><P>A/E MODULE&NBSP; M239 INSPECTED FOR LEAK OK;&NBSP; MODULE COMPONENTS VISUAL&NBSP; &AMP; CLEANED INSP.&NBSP; OK AMM&NBSP;&NBSP;</P><P>32-42-09. AUTO BRAKE SYS TEST CONTROL OK AMM 32-42-00/705.</P>)

ATA 2561

COCKPIT 1ST OBS SEAT LIFE VEST POUCH VELCRO LOOSE(<P>REMOVED CLEANED AND INSTALLED&NBSP; NEW VELCRO AT COCKPIT 1ST OBS SEAT PER&NBSP; B767-300</P><P>AMM&NBSP; 20-30-01-992-001</P>)

ATA 2562

COCKPIT ELT AUTO RELEASE SEAL DAMAGE(<P>REMOVED &AMP; REPLACED COCKPIT&NBSP; ELT AS REQUIRED PER AMM&NBSP; 25-64-00.</P><P>AEX CODE&NBSP; ADCC06849600401</P>)

ATA 5610

COCKPIT R2 WINDOW NOT CLOSING PROPERLY. DIFFICULT TO CLOSE &AMP; LOCK(<P>ADJUSTED #2 R/H WINDOW IAW AMM 56-11-02, OPS CHECK OK.&NBSP; NO DEFECTS NOTED&NBSP; AT THIS TIME. PENDING PRESSURIZATION CHECK. PERFORMED CABIN PRESSURE WINDOW LEAK CHECK&NBSP; 05-51-24 NO LEAKS NOTED</P>)

ATA 3510

FWD EE CREW OXYGEN NEED SERVICE TO FULL(<P>REMOVED AND REINISTALLED ORIGINAL CYL. PER&NBSP; M/M 12-15-08-603-001. ACCOMPLISHED LEAK CHECK PER&NBSP; M/M 12-15-08-793-039. ACOMPLISHED MASK AND REGULATOR PER 35-11-00. ORIGINAL BOTTLE REINTALLED&NBSP; P/N&NBSP; 801307-00&NBSP; &NBSP;S/N&NBSP; 792582</P>)

ATA 2560

COCKPIT FIRST AID AND KITS AREA MISSING PLACARDS. P/N&NBSP; 767INT-1094(<P>INSTALLED REQUIRED PLACARDS AS PER B767-300 AMM 25-60-00</P>)

ATA 5230

MD CARGO DOOR AFT MID SEAL DEPRESSOR DAMAGED(<P>REMOVED DAMAGED SEAL DEPRESSOR, LOCATED NEW SEAL DEPRESSOR DRILLED AND TRANSFER NUT PLATE, PREPARED CLEANED AND INSTALLED NEW SEAL DEPRESSOR AND PAINTED AT M/D CARGO AFT MID PER B767-300 IAW AMM 20-11-00-910-802.</P>)

ATA 3610

AFTER ENGINE START HAD R ENGINE BLEED OFF EICAS MSG WITH 0 PRESSURE SHOWN ON GAUGE. ADVANCED THROTTLE TO 35% N1 WITH NO PRESSURE SHOWING.(<P>REMOVED FAULTING PRVC AS INDICATED BY AIR SUPPLY MODULE AND INSTALLED NEW PRVC IAW B767 AMM 36-11-19. OPS CHECK GOOD. BLEED LIGHT OFF, GOOD ENGINE PNEUMATIC PRESSURE.

ATA 3150

FWD EQPT VAL EICAS DURING ROLL OUT, PERFORMED QRH STEP AND LIGHT WENT OUT.(<P>PERFORMED CYCLED OVERRIDE SWITCH PER AMM 21-58-20, OPS CHK GOOD.

ATA 7510

BTB RT ENG A/I VALVE WOULD NOT OPEN. PERFORMED FIM 30-21TASK 806. FOUND A/I CONTROL TO CHECK OK. VERIFIED A/I VALVE POSITION OF NR 2 ENGINE AND PERFORMED VALVE OPS CHECK IAW AMM 30-21-03 AND 36-11-09. OPS CHECK GOOD AT THIS TIME.

ATA 2150

FWD EQPT VAL EICAS AND VALVE ANNUNCIATOR ON EQUIP COOLING PANEL ILLUMINATED AFTER LANDING. THEY DID NOT EXTINGUISH UNTIL SHUTOFF DOWN. PERFORMED OPS TEST PER AMM 21-58-00 OPS CHK GOOD.

ATA 2612

R ENG FIRE LOOP 2 ILLUMINATED INTERMITTENTLY IN FLIGHT(<P>DEFERRED IAW MEL 26-11-01-01 MDDR 142435, CAT C, DUE 24 FEB 21. MCC NOTIFIED.</P><P>LP 1233212: REMOVED AND REPLACED #2 ENGINE UPPER AFT FIRE LOOP IAW AMM 26-11-02. OPS CHECKS GOOD. THIS CLOSES DMI 142435.</P>)

ATA 2612

RH ENG FIRE LOOP EICAS MSG(<P>REMOVED AND REPLACED&NBSP;RH ENG LWR AFT FIRE DET ASSY IAW AMM 26-11-02. OPS CHECK GOOD W/ IDLE ENG RUN IAW AMM 77-35-02. NO MSGS NOTED AT THIS TIME. OPS CHECK GOOD.<BR /></P>)

ATA 2612

R ENG FIRE LP 2 STATUS MSG / FIRE OVERHEAT SYS EICAS AFTER PUSHBACK.(<P>TRANSFERRED TO MDDR&NBSP;142292 IAW MEL 26-11-01-01, CAT C.</P><P>LP&NBSP;<SPAN>1342774:&NBSP;</SPAN><SPAN>OPENED #2 ENG. FOUND SEVERAL KINKS IN LOOPS 1&AMP;2 AND AREAS WERE LOOP WAS CLOSE TO METAL. ALSO FOUND LOOSE TERMMINAL ON LOOP 2 IAW AMM 26-11-00. STRAIGHENED AND ADJUSTED LOOPS. NO PRESENT MESSAGES OPS NORMAL AT THIS TIME. THIS CLEARS MDDR 142292.</SPAN></P>)

ATA 2410

AFTER ENGINE START LT GEN CONTROL TRIPPED. RESET PER QRH, TRIPPED AGAIN, RETURNED TO GATE PER MX CONT. TRANSFERRED TO MDDR 141784 PER MEL 24-00-01-01, CAT B, DUE 25FEB21. LP 1482158: R & R LT GEN IDG. REF AMM 24-11-01 401. OPS CHECKS GOOD. THIS CLEARS DMI 141284. STICKERS REMOVED T & TS 05:04Z.

ATA 7500

DURING RECENT APPROACH LT ENGINE BLEED EICAS FLASHED NUMEROUS TIMES. PERFORMED AIR SUPPLY BITE, REF FIM TASK 36-20-00-815-804. FOUND FAULT BALL ON HPC. PERFORMED HP SOV AND HPC TEST, REF AMM 36-11-07/501. SYSTEM CHECK GOOD. NO FAULTS FOUND. OK TO CONTINUE.

ATA 7261

HIGH OIL CONSUMPTION #2 ENGINE. RH ENG CHANGE COMPLETE IAW W/CARD A-71-999-04-02 ENG. RUN COMPLETED

ATA 3150

FWD EQUIPMENT VALVE EICAS. PERFORMED FIM TASK 21-58 TASK 805. NO EICAS, NO FAULTS AT THIS TIME.

ATA 3610

LT ENGINE BLEED OFF EICAS MESSAGE DISPLAYED INTERMITTANTLY DURING CRUISE FLT. PERFORMED BITE OF AIR SUPPLY, IAW 36-20 FT 804 FAULTED LT HPC-WIRE FAULT T/S, PER W/D 36-11-61. REMOVED AND REPLACED LT BLEED AIR CONT CARD, IAW AMM 36-11-12. OPERATIONS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

ATA 7261

NR 2 ENGINE REQUIRES DRAIN LINES TO BE CAPPED DUE TO HIGH OIL CONSUMPTION. CAPPED THE NR 2 ENGINE STARTER, IDG, HYD PUMP/ FUEL PUMP AND HMU DRAIN LINES, PER AMM 71-71-00 AND PER MM 2020P-525. TRANSFERRED TO NON-MEL 140508, MCC NOTIFIED. DUE IN 10 FLT CYCLES. REMOVED NR 2 IDG, RESEALED AND REINSTALLED NR 2 IDG LEAK AND OPERATIONS CHECK GOOD, IAW 24-11-01. UNCAPPED NR 2 ENGINE STARTER, IDG, HYD PUMP, FUEL PUMP AND HMU DRAIN LINES, IAW 71-71-00. REINSTALLED IDG LINE AND RESTORED A/C BACK TO NORMAL CONDITION, THIS CLEARS MDDR NR 140508.

ATA 2150

AIRCRAFT PACKS EXCESSIVELY LOUD, W/BOTH PACKS ON THEY HAVE A LOUD WHISTLE. DURING DEPARTURE EVEN WITH VOLUME ALL THE WAY UP. ATC COULD BARELY BE UNDERSTOOD AND PILOTS HAD TO YELL AT EACH OTHER. CONT-WHISTLE WHENT AWAY AS WE CLIMBED THROUGH FL250, WHICH DROPPED NOISE LEVEL GREATLY. PERFORMED ENGINE RUN, IAW 767 M/M 71-00-00 & OPERATION OF BOTH PACKS IAW 767 M/M 21-00-00 & FOUND BOTH PACKS TO OPERATE NORMAL WITH NO WHISTLE. TALKED IN A NORMAL VOICE USING RADIO'S, NO DEFECTS NOTED AT THIS TIME.

ATA 7500

ON DESCENT, "LT ENGINE BLEED OFF" EICAS. RAN QRH AND TURNED WING ANTI-ICE LT PACK OFF. PERFORMED ENGINE RUN OF LT ENGINE, FOUND ENGINE TO OPERATE NORMAL AT THIS TIME, IAW 767 M/M 71-00-00.

ATA 7320

RT ENGINE SPEED CARD STATUS MESSAGE AFTER ENGINE START. PERFORMED FIM 73-21 F/T 871, SYSTEM IS OK. NO FURTHER FAULTS NOTED.

ATA 7700

AFTER ENGINE STARTED, RECEIVED PROBE HEAT EICAS CAUTION MESSAGE. MULTIPLE DISCREET LIGHTS, "CAPT PITOT", "R AUX PITOT" "L AOA". REMOVED AND REPLACED RT N2 SPEED CARD, IAW AMM 73-21-54. RAN BOTH ENGINES, IAW 71-00-00, NO FAULTS MESSAGE NOTED. OPERATIONS NORMAL AT THIS TIME.

ATA 2612

MAIN CARGO LOOP 1 STAUS MESSAGE. TRANSFERRED TO MDDR 138670, PER MEL 26-16-02-01. DUE DATE 09 DEC 2020. T/S PER FIM 26-14-FT809. NO FAULTS NOTED AT THIS TIME. THIS CLEARS MDDR 138670.

ATA 3610

INTERMITTENT EICAS LT ENGINE BLEED OFF IN DECENT. PERFORMED T/S, IAW FIM 3-10 F/T838 AND PERFORMED IDLE POWER ENGINE RUN, IAW AMM 71-00-00. OPERATIONS CHECK GOOD AT THIS TIME.

ATA 2150

INFLIGHT (BOTH ENGINES ON) AND BOTH PACKS OPERATING, UNUSUALLY LOUD MAKING INTERCOM AND ATC EXTREMELY DIFFICULT, NOISE REDUCTION SIGNIFICANTLY REDUCED WHEN 1 PACK SELECTED OFF. SQUEALS NOTED W/ BOTH PACKS. PERFORMED ENGINE RUN, PACK OPERATION TO DETERMINE NOISE, PACK OPERATIONAL TEST SATISFACTORY WITH NO ISSUES NOTED, IAW B767 AMM 21-00-00. PERFORMED PNEUMATIC SYSTEMS OPERATIONAL TEST, PER AMM 36-00-00. DUCT PRESSURE NORMAL. COULD NOT DUPLICATE DISCREPANCY. OPERATIONS/LEAK CHECK GOOD AT THIS TIME.

ATA 2150

OPERATING LEFT PACK UNUSUALLY LOUD WITH NORMAL DUCT PRESSURES OBSERVED. LOUD SQUEELING INTERMITTENT, COMMUNICATIONS BETWEEN PILOTS AND ATC AFFECTED, SELECTED LEFT PACK OFF. PERFORMED LT PACK INSPECTION, IAW AMM 21-51-00. NO LEAKS OR DEFECTS NOTED. PERFORMED OPERATIONS CHECK ON LT PACK, IAW AMM 21-00-00. FOUND GASPER MAKING LOUD NOISE IN SUPERNUMERARY SEATS, READJUSTED GASPER, IAW AMM 21-22-00. NO NOISE WITH LT PACK NOTED. OPERATIONS CHECK NORMAL.

ATA 5100

IMMEDIATELY AFTER TAKEOFF A DEAFENING ROAR MADE COMMUNICATIONS BETWEEN PILOTS AND BETWEEN PILOTS AND ATC ALMOST IMPOSSIBLE. UNABLE TO DETERMINE WHERE THE NOISE CAME FROM. ONCE THE CABIN DIFF PRESSURE REACHED 6.0 THE NOISE SLOWLY ABATED. GENERAL VISUAL OF AIRCRAFT NO DEFECTS NOTED. PRESSURIZED AIRCRAFT TO 4.0 DIFFERENTIAL. NO NOISES OR SQUEALS NOTED AT THIS TIME, IAW B767 AMM 21-31-00.

ATA 7500

EICAS MESSAGE: LT ENGINE BLEED OFF AND LT ENGINE BLEED OFF LIGHT ILLUMINATED. FOUND LT ENGINE BLEED CNT POPPED AND HP CONT FAULT ON AIR SUPPLY MODULE BITE. RESET MODULE AND BREAKER PERFORMED IDLE ENGINE RUN, NO FAULTS NOTED, IAW AMM 36-23-01 AND 71-00-00.

ATA 7421

STATUS MESSAGE: LT ENGINE IGNITOR 1. NO LIGHT OFF OF FIRST ATTEMPT, LEFT ENGINE NORMAL START 2ND ATTEMPT W/ENGINE START BOTH. PERFORMED AUDIBLE TEST OF LT ENGINE IGNITER 1. NO FAULTS NOTED, STATUS MESSAGE CLEARED, NO FAULTS NOTED AT THIS TIME. PERFORMED AUDIBLE TEST, IAW AMM 74-00-00-705-104-H03. TRANSFERRED LT ENGINE IGNITOR 1 TO DMI NR 136674, IAW MEL 74-00-01A, CAT A, DUE 25OCT20. MCC NOTIFIED. PLACARDS INSTALLED. DISPATCH- ZH AT 1540Z. REMOVED AND REPLACED LEFT ENGINE IGNITOR 1 PLUG, IAW AMM 74-21-02. PERFORMED ENGINE RUN, IAW AMM 71-00-00, TWICE BOTH CHANNELS OF EEC OPERATIONS NORMAL. THIS CLEARS DMI 136674. ALL PLACARDS REMOVED. ZH 1812Z. P/N OFF: CH31772A, NSN. DUE TO REPLACEMENT OF LT ENGINE IGNITOR 1, ALSO REMOVED AND REPLACED LT ENGINE IGNITOR 2 FOR MX CONVENIENCE, PER AMM 74-21-02. PERFORMED ENGINE RUN, IAW AMM 71-00-00. OPERATIONS GOOD, NO FURTHER DEFECT NOTED.

ATA 3510

F/O MASK FAILED THE PREFLIGHT TEST. SWAPPED F/O'S CREW O2 MASK WITH RT SUPER NUMERARY OBSERVER POSITION. PLACED ON MEL 35-11-02-03A. TRANSFERED TO MDDR 136525. T.J. 12:25 22OCT20. R & R RT SUPERNUMERARY OXYGEN MASK, IAW AMM 35-11-51. OPERATIONS CHECK GOOD. THIS CLEARS DMI 136525. MCC NOTIFIED, PLACARDS REMOVED. WO 72350 C/W DISPATCH: DP@1504Z.

ATA 7311

DURING WALK AROUND FOUND NR 1 ENGINE FUEL LEAK. FOUND FUEL OIL COOLER LINE BROKEN. R & R LINE, IAW AMM 24-11-10. LEAK CHECK PENDING. PERFORMED ENGINE WET MOTOR AND ENGINE RUN UP, NO LEAKS NOTED. OPERATIONS CHECK NORMAL, IAW 71-00-00 REF LEAK CHECK ONLY. P/N OFF: 1326M91G01, NSN. FOUND FUEL LEAK FROM MAIN PUMP STRAINER COVER. REMOVED AND REPLACED PACKING, ENGINE WET MOTOR AND RUN UP OPERATIONS CHECK GOOD. NO LEAKS NOTED, IAW AMM 73-11-01 AND 71-00-00.

ATA 3610

L ENGINE BLEED OFF ADVISORY MESSAGE AND L ENG HPSOV STATUS MESSAGE AFTER ENGINE START.(<P>TRANSFERRED TO DDG MDDR #135084 IAW 36-11-02-02, CAT C. T.I. # 1429Z.</P><P>01OCT, LP 121215, ITEM M5: FOUND HPC FAULTING ON AIR SUPPLY MODULE IAW 36-10 FT 833. REMOVED AND REPLACED HPC IAW 36-11-08, LEAK CHECK GOOD, REF ITEM #6 FOR R&AMP;R HPSOV AND OPS CHECK. S/N OFF: 960316, P/N OFF: 773289-15.</P><P>ITEM M6: DUE TO HISTORY REMOVED AND REPLACED HPSOV IAW 36-11-07, LEAK CHECK GOOD, NO FAULTS ON AIR SUPPLY BITE. PER MCC RAN ENGINES HIGH POWER IAW 71-00-00, NO FAULTS NOTED, SYSTEM NORMAL.

ATA 7421

STATUS MSG "LT ENG IGNITOR 1". PERFORMED LT PIMO BITE, IAW FIM F/T 810. 2 FAULTS 350-18 A/B TMC & 35120-8 LT IGN 1 FAIL. CLEARED FAULTS, STATUS MSG CLEARS. PERFORMED ENGINE RUN NR 1 IN BOTH SINGLE AND BOTH IGNITORS POSITIONS. ALL PARAMETERS NORMAL, PER 72-00-00 AND BITE TEST PERFORMED, NO FAULTS.

ATA 7400

NO LIGHT OFF ON THE NR 1 ENGINE ON FIRST ATTEMPT. DISCONTINUED START AFTER 25 SECONDS, IAW COMPANY POLICY. GROUND CREW REPORTED SEEING SOME SMOKE COMING FROM THE NR 1 ENGINE DESPITE NO INDICATION OF LIGHT OFF OR EGT RISE IN COCKPIT. ATTEMPTED 2ND START WITH IGNITION SELECTED TO "BOTH". SECOND ATTEMPT SUCCESSFUL. REPEAT WRITE-UP. PERFORMED AUDIBLE IGNITION SYS TEST. VERIFIED BOTH IGNITORS ARE FIRING INDEPENDENTLY. OPS CK GOOD, NO FURTHER DEFECTS NOTED, REF B767 AMM 74-00-00. VERIFIED BOTH IGNITORS ARE FIRING INDEPENDENTLY. OPS CK GOOD, REF B767 AMM 74-00-00.

ATA 5340

DURING PRE-FLIGHT WALK AROUND, FOUND PANEL P40 (APU REMOTE PANEL) DROOPING. REMOVED AND REPLACED 4 MOUNTING CLIPS ON PANEL P40, REF AMM 26-15-01. OPS CK GOOD, OK FOR SERVICE.

ATA 2197

LT BLD DUCT LEAK EICAS MESSAGE AND ASSOCIATED DUCT LEAK ANNUNCIATOR ON OVER HEAD WHILE AT THE GATE. DEFERRED LEFT PACK, MDDR 133999 PER MEL 21-51-02, CAT C, DUE 16 SEP 20. PERFORMED BITE OF PACK TEMP CONTROLLER, IAW FIM 21-51 FT 844, NO FAULTS NOTED. PERFORMED DVI OF LT PACK AREA, FOUND CANNON PLUG LOOSE, RESECURED IAW AMM 20-00-00. CHECKED DUCTS FOR LEAKS, NONE NOTED. LT PACK OPS NORMAL AT THIS TIME, THIS CLEARS MDDR # 133999. PLACARD REMOVED, DISP: EH@1150Z.

ATA 4900

APU TRU START CONT C/B OPENED ON FLT. PERFORMED OPS CHK OF APU TRU IAW 24-32-04, OPS CHK NORMAL, C/B REMAINED SET.

ATA 4920

APU AUTO SHUTDOWN AUXILIARY POWER UNIT (APU), ER OPERATIONS NOT ALLOWED (NOTIFY DISPATCH) R60. TRANSFERRED TO MDDR #133793 PER MEL 49-11-01A, CAT C, EXP 12 SEP 20. PLACARDS INSTALLED. DISPATCH DP 1707Z. REMOVED AND REPLACED APU IGV GUIDE VANE ACTUATOR IAW AMM 49-52-02. OPERATIONS CHECK GOOD IAW AMM 49-11-00. THIS CLEARS MDDR 133793.

ATA 2150

AFTER LANDING, RECEIVED A FWD EQUIP VALVE ADVISORY MESSAGE. PERFORMED BITE TEST OF EQUIPMENT COOLING SYSTEM CONTROLLER. NO FAULTS NOTED IAW AMM 21-58-00.

ATA 7740

STANDBY ENGINE INDICATOR GAUGE IS SO DIM IT'S NEARLY IMPOSSIBLE TO READ.(<P>REMOVED AND REPLACED STANDBY ENG IND IAW B767 AMM 77-41-01. OPS CHECKS GOOD AT THIS TIME.<BR /></P>)

ATA 7230

DURING WALK AROUND FOUND NICKS ON NR 2 ENG FAN BLADES, 5 BLADES WITH NICKS. PERFORMED FAN ROTOR BLADE INSPECTION IAW AMM 72-31-02. REPAIRED THE ROTOR FAN BLADES IAW AMM 72-31-02.

ATA 2150

DURING DAILY CHK NOTICED ODOR COMING FROM A/C DUCTS, UPON INSP FOUND L/H PACK CONDENSER HEAT EXCHANGER CRACKED. REMOVED AND REPLACED L/H PACK HEAT EXCHANGER CONDENSER ASSY IAW AMM 21-51-10. OPS CHECK NORMAL. NO LEAKS NOTED.

ATA 3350

SPRING ON EMERGENCY LIGHT INOPERATIVE. REPOSITIONED THE EMERGENCY LIGHT TOGGLE SWITCH ARMING ARM, IAW MM 33-51-08. OPS CHECKED GOOD IAW 33-51-00.

ATA 2560

BOTH EVAS SYSTEM INOPERTIVE, COCKPIT SMOKE VISION SYSTEM. REPLACED EVAS HOOK AND LOOP ON CA AND FO DASH.

ATA 4997

APU OIL QTY INDICATION INOP. RE-SEATED CONNECTOR D4024. OPS CHKS GOOD. CLOSED MDDR 127547.

ATA 2150

AFTER LANDING FWD EQUIP VAC EICAS MSG.(<P>PERFORMED FIM TASK 21-58 F/T 985 MSG CLEARED.<BR /></P>)

ATA 2150

MSG HI FLOW INHIBIT(<P>BITE CHK LH &AMP; RH PACK CONTROLLERS IAW AMM 21-51-814, OPS CHKS NORMAL.</P>)

ATA 7310

R ENG FUEL FILTER EICAS ON INITIAL CLIMBOUT(<P>REMOVED AND REPLACED R ENGINE FUEL FILTER PER AMM 73-11-03. PERFORMED ENGINE LEAK CHECK, FOUND OK.</P>)

ATA 4910

APU DOOR INOP(<P>PLACED ON MDDR 126819 PER MEL 49-15-01-01B, CAT 'C'.</P><P>REF LP 1126379 - M2: REMOVED AND REPLACED APU INLET ACTUATOR PER AMM 49-15-06/401. OPS CHECKS GOOD. MCC GLEN DISPATCH T.I. 2310Z. THIS CLEARS DMI #126819.</P>)

ATA 7740

STANDBY ENGINE INDICATOR DOES NOT SHOW INDICATIONS WITH SWITCH IN ON POSITION.(<P>FOUND SCREW OVERTIGHTENED. TIGHTENED SCREWS IAW B767 AMM 77-41-01-434-008-H00. THEN PERFORMED SEI BITE PER AMM 77-41-00-745-001-H00. OPS CHECK TESTED OK.<BR /></P>)

ATA 2150

FWD EQUIP VALVE EICAS MSG ON LANDING.(<P>PERFORMED FIM TASK 21-58 FT 805. NO DEFECTS NOTED AT THIS TIME.</P>)

ATA 3150

FWD EQUIPMENT VALVE EICAS MESSAGE AFTER LANDING.(<P>PERFORMED FIM TASK 21-58 FAULT TREE 986. MESSAGE NO LONGER PRESENT.<BR /></P>)

ATA 3442

STATUS MSG WX RADAR SYSTEM(<P>MESSAGE CLEARED AFTER OPS CHK PER AMM 34-43-00, OK FOR RTS.</P>)

ATA 3697

STATUS MESSAGE FOR LT ENG HPSOV, INTERMITTENT EICAS MSG L ENG HPSOV. TROUBLESHOOTING PER AMM 36-11-06 AND WDM 36-11-03 AMM 36-11-04 FOUND WIRE CONNECTOR BLK 2 WAS LOOSE AS WELL AS BLK 1 AND BLK 3. SECURED THE TERMINAL WIRE IAW SWPM. NO LEAK OR FAULTS FOUND. OPERATIONAL CHECK NORMAL AT THIS TIME. AMM 71-00-00 FOR ENGINE RUNS.

ATA 2822

CTR R FUEL PUMP EICAS MESSAGE AFTER PUSHBACK. CHECKED RT CTR FUEL BOOST PUMP ELECTRICAL CONNECTOR IAW SWPM 20-13-06. NO DEFECTS NOTED. TRANSFERRED FUEL INTO CTR TANK AND BACK OUT USING RT CTR BOOST PUMP IAW AMM 28-22-00. OPS CHECK NORMAL.

ATA 2121

FWD EQUIPMENT EXHAUST FAN EICAS DISPLAYED MSG. REMOVED AND REPLACED FWD SUPPLY/EXHAUST FAN CURRENT SENSOR IAW AMM 21-58-11. OPS CHECKED NORMAL.

ATA 3197

OVERHEAD CLUSTER TAT LIGHT INOP, WORKS DURING TEST.&NBSP;(<P>PERFORMED TROUBLESHOOTING,&NBSP; DISCOVERED 2&NBSP;BROKEN WIRES ON K00644 PIN D3 AND K00126 PIN C3. RE-PINNED WIRES IAW SWPM 20-81-12. PERFORMED TAT PROBE TEST IAW AMM 30-33-00. OPS CHECK GOOD.&NBSP;</P>)

ATA 3150

UPON LANDING, "FWD EQUIP VALVE" EICAS CAME ON. QRH PROCEDURE ACCOMPLISHED, LIGHT STAYED ON.&NBSP;(<P>PERFORMED FIM TASK 21-58 FAULT TREE 986, SYSTEM CHECKS OK.<BR /></P>)

ATA 2121

FWD EQUIPMENT EXHAUST FAN STATUS MESSAGE. REACTIVATED EQUIPMENT COOLING SYSTEM, CHECKED IAW AMM 21-58-00. OPS CHECK NORMAL.

ATA 7310

DURING RIGHT ENGINE START, "R ENG FUEL VAL" EICAS MESSAGE DISPLAYED.(<P>COMPLIED WITH&NBSP;ENGINE RUN PER AMM 71-00-00, NO FURTHER DEFECTS NOTED AT THIS TIME. MCC NOTIFIED.</P>)

ATA 3442

MOMENTARY WX FAIL AFTER BIRD STRIKE.(<P>ACCOMPLISHED WX RADAR TEST IAW B767 AMM 34-43-00/501, TEST OPS CHECKS NORMAL. NO FAULTS AT THIS TIME.</P>)

ATA 3110

STDBY ENGINE INDICATOR INSTRUNMENTS INOP.(<P>PERFORMED BITE TEST OF STDBY ENGINE INDICATOR INSTRUMENTS IAW B767 AMM 77-41-00-745-001-H00, OPS CHECK NORMAL.&NBSP;<BR /></P>)

ATA 3610

UPON PDSC IDG CHECK, FOUND LOOSE BOLT IN ENGINE COWLING OF #1 ENGINE.(<P>DETERMINED BOLT TO BE FROM PRE-COOLER ATTACHMENT BRACKET. INSTALLED NEW BOLT (P/N BACB30PN6C25), WASHER (P/N BACW10BP6ACU), WASHER (PN AN960C616L), NUT (P/N NAS1805-6P) IAW AMM 36-11-15. FOUND NO LEAKS IN PRE-COOLER, NO FURTHER DEFECTS NOTED.&NBSP; &NBSP;</P>)

ATA 3097

F/O'S SLIDING WINDOW HEAT INOPERATIVE. ACCOMPLISHED M PROCEDURE PER DDG. REMOVED AND REPLACED R2 WINDSHIELD CONNECTOR J8 IAW SWPM 20-30-12. OPS CHECKED GOOD.

ATA 4970

MAINT MSG, APU DOOR. IMPROPER APU SHUTDOWN. CLOSED APU DOOR, APU START NORMAL IAW AMM 49-11-00.

ATA 3610

DURING CLIMB TO FL 380, AT ABOUT FL 360, L ENG BLEED OFF EICAS. PERFORMED QRH. REMOVED AND REPLACED THE LEFT PRSOV IAW AMM 36-11-09. OPS AND LEAK CHECKED GOOD.

ATA 2613

SHORTLY AFTER LEVEL OFF AT FL 380, "L BLD DUCT LEAK" EICAS MSG ANNUNCIATED. FOLLOWED FIM 26-18 FAULT TREE 804. PERFORMED LEAK CHECK, NO OBVIOUS LEAK NOTED. REMOVED AND REPLACED WHEEL WELL OVERHEAT CARD IAW AMM 26-10-01. OPS CHECK NORMAL.

ATA 3150

AFTER LANDING, EICAS IDLE DISAGREE. IAW FAULT ISOLATION MANUAL 71-05-4384A, MESSAGE CLEARED.

ATA 2160

LEFT PACK TEMP CAUTION MESSAGE. REMOVED AND REPLACED L PACK TEMP SENSOR IAW AMM 21-61-02. PERFORMED OPS CHECK, NO MESSAGES NOTED, OPS NORMAL.

ATA 2121

STATUS MESSAGE, AFT EQ EXH FAN 1 DISPLAYED. (<P>DURING POWER TRANSFER, MESSAGE CLEARED. PERFORMED OPERATIONAL TEST IAW AMM 21-58-00. SYSTEM OPS CHECKS NORMAL.</P>)

ATA 2421

RT ENGINE GEN OFF EICAS MESSAGE DISPLAYED WITH GEN CONTROL LIGHT ILLUMINATED. GEN CONTROL LIGHT WOULD NOT RESET. (<P>PERFORMED BITE IAW FIM 24-20 FT 801. PLACED RT IDG ON DEFERRAL DDG 24-00-04-01, CAT 'B', DMI 115342. PLACARDS INSTALLED.&NBSP;&NBSP;</P><P>LP 1086197 - M4:&NBSP; REMOVED AND REPLACED #2 ENG IDG IAW AMM 24-11-01. OPS CHECK GOOD IAW AMM 24-11-00. THIS ACTION CLOSES DMI 115342. PLACARDS REMOVED. ETOPS STATUS REINSTATED.</P>)

ATA 3442

WEATHER RADAR INOP. &NBSP;(<P>C/W OPS TEST OF WEATHER RADAR IAW AMM 34-43-00. OPS CHECK GOOD AT THIS TIME, NO FAULTS NOTED.&NBSP;</P>)

ATA 3442

RADAR NOT PAINTING KNOWN PRECIPITATION.(<P>PERFORMED SYS TEST OF WX SYS, NO FAULTS FOUND. OPS CHK GOOD IAW AMM 34-43-00.</P>)

ATA 7200

HIGH ENGINE VIBRATIONS NOTED ON TAKEOFF / CIMB OUT / HIGH THRUST SETTINGS ON LEFT ENGINE. EVENT RECORD SNAPSHOT. TAKEN 0440Z ON CLIMB OUT. LEFT VIB 3.2 FAN, RIGHT VIB 0.7 FAN.(<P><SPAN>FOLLOWED FIM 71-05 TREE 853 PERFORMED INCET EXAUST INSPECTION FOUND OK ALL CHIP DETECTORS FOUN NORMAL NO OBVIOUS DEFECTS NOTED DUE TRANSIT MODE OF VIBRATION A/C OK TO CONTINUE SERVICE. MCC RON</SPAN><BR DATA-MCE-BOGUS="1" /></P>)

ATA 2822

L FWD FUEL PUMP INOPERATIVE. LIGHT STAYS ILLUMINATED DURING PUMP OPERATION. REMOVED AND REPLACED RELAYS K512 + K505 AT P37 PANEL, NO FIX, REF B767 SWPM 20-81-22. TROUBLESHOT IAW FIM 28-25 FT 808 AND WDM 28-25-11-1 PAGE 1. REMOVED AND REPLACED RELAY K513 IAW SWPM 20-81-11. OPS CHECKS GOOD.

ATA 2560

DESCENT DEVICE IN POSITION 'G' IS MISSING. INSTALLED MISSING DESCENT DEVICE IN POSITION 'G' IAW AMM 25-61-05. NO FURTHER DEFECTS NOTED AT THIS TIME.

ATA 4930

REMOVED AND REPLACED APU FUEL FLOW DIVIDER IAW B767 AMM 49-31-03-404-017. OPERATIONAL CHECK GOOD. LEAK CHECK GOOD.&NBSP;</P>)

ATA 2432

APU BATTERY CHARGER FAILS TEST IAW EO 6749A003 PART 1. REMOVED AND REPLACED APU BATTERY CHARGER IAW B767 AMM 24-31-05. OPS CHECK GOOD.&NBSP;</P>)

ATA 4920

APU NO DUCT PRESSURE. REMOVED AND REPLACED APU ECU IAW B767 AMM TASK 49-11-01. OPS AND BITE CHECK GOOD. NO DISCREPANCIES NOTED AT THIS TIME.&NBSP;</P><P>LOG PAGE 1024426: PERFORMED OPS CHECK OF APU IAW AMM TASK 49-11-00, OPS CHECK GOOD. GOOD DUCT PRESSURE. NO FAULT NOTED AT THIS TIME.

ATA 4900

APU NO DUCT PRESSURE.(<P>TRANSFERRED TO MDDR# 112450 MEL 49-11-01A CAT C. DUE 10JAN19.</P>)

ATA 7200

AMBER OIL PRESSURE INDICATION (22 PSI) ZERO OIL QUANTITY ENG # 1.(<P>LP 1024421 - M4: PERFORMED MAG CHIP INSPECTION PER AMM 79-35-00, CHIP DETECTORS CLEAN AND SCREEN CLEAN, NO FINDINGS.</P><P>LP 1024421 - M5: BOROSCOPE COMPLETED, FINDINGS AND PICTURES SENT TO MCC AND POWERPLANT ENGINEERING.&NBSP;</P><P>LP 1024420 - M2:&NBSP;REMOVED AND REPLACED ENG #1 IAW WC A-71999-04-02. ALL OPS CHK AND LEAK CHECKS NORMAL REF AMM 71-00-02-004-002-H03 REV 127-22-APR-19.</P><P>LP 1024423 - M11:&NBSP;VERIFICATION FLIGHT LEFT ENGINE OPS OK , MDDR 112412 CLOSED.&NBSP;</P>)

ATA 2910

FAIRLY SUBSTANTIAL LEAK FOUND COMING FROM TAILSKID AREA AT BLOCK IN. INSPECTION REVEALED A DAMAGED FLEX HOSE COMING FROM STABILIZER TRIM CONTROL UNIT.(<P>UNIT REQUIRES P/N A5154A06RR0146B. INSTALLED TEMPORARY HOSE A5115-04C0360 IAW B767 AMM 20-10-10 AND GMM 3.24.1. TRANSFERRED ITEM TO NON MEL # 112206. NON MEL ITEM LIST UPDATED. MCC NOTIFIED. LEAK CHECK AND OPS CHECK OF STAB TRIM CONTROL UNIT GOOD IAW 27-41-16. </P><P>LP 1050610 -&NBSP; ITEM 1: REMOVED TEMP LINE AND INSTALLED PERMANENT&NBSP;HYD LINE BETWEEN STAB TRIM CONTROL MOD. AND JACK SCREW ACTUATOR IAW B767 AMM TASK 20-11-00 AND 27-41-00. OPS CHECK AND LEAK CHECK GOOD. THIS CLEARS DMI 112206.<BR /></P>)

ATA 3442

WXR SYS STATUS MESSAGE. (<P>RESET L &AMP; R RADAR CB'S. PERFORMED WX RADAR OPERATIONAL TEST. NO DEFECTS AT THIS TIME PER AMM 34-43-00.</P>)

ATA 7261

CW W/O #51764. #1 ENGINE EXPERIENCING HIGH OIL CONSUMPTION. FOUND OIL ON STARTER, DURING INSPECTION ON AND AROUND V CLAMP.(<P>REMOVED AND REPLACED OUTER #1 STARTER CARBON SEAL IAW TASK AMM 72-64-02. PERFORMED 2 MIN DRY MOTOR RUN IAW AMM 72-10-00. NO NEW OIL FOUND TO HAVE LEAKED.</P>)

ATA 2150

LEFT PACK INOP AFTER ENGINE START.(<P>PLACED ON MEL 21-51-01-01 AND TRANSFERRED TO MDDR #111344.</P><P>LP 1078472 - M5:&NBSP;R AND R LEFT PACK FLOW CONTROL CARD IAW WDM 21-51-11 AND AMM 21-51-24. PACK OFF INDICATION STILL INTERMITTENT. INSTALLED ORIGINAL CARD BACK IAW 21-51-11 AND 21-51-24.</P><P>LP 1078476 - M4:&NBSP;T/S LT PACK PER AMM 21-51-00. PACK CONTROL WORKS AS DESCRIBED. OFF, EICAS MSG. ON, MSG CLEARED. LIGHTS WORK WITH SWITCH. BITE TEST PERFORMED IRW 25-51 FT 844. OPS CK NORMAL AT THIS TIME. DMI REMAINS OPEN. MCC UPDATED WITH PART NUMBER REQUESTED.</P><P>LP 1078477 - M2:&NBSP;T/S L PACK PER AMM 21-51-00. PACK CONTROL WORKS AS DESCRIBED. OFF EICAS MSG ON MSG CLEARED LIGHT WORKS WITH SWITCH BITE TEST IAW 25-51 FT 844 OPS GOOD. DMI REMAINS OPEN.</P><P>LP 1078478 - M2: PERFORMED FIM 21-51 FT 844. R&AMP;R LT PACK FLOW CONTROL VALVE ASSY AMM 21-51-01. OPS CHECK GOOD . LEAK CHECK GOOD. MCC NOTIFIED. THIS CLEARS DMI 111344. MX ACTION REVERSED.&NBSP;</P>)

ATA 8012

BTB WHILE TAXING AIRCRAFT AFTER ENGINE START, L STARTER CUT OUT AND L ENG STARTER EICAS MESSAGE CAME ON NUMEROUS TIMES(<P>REMOVED AND REPLACED NR 1 ENGINE STARTER VALVE IAW AMM 80-11-02-004. PERFORMED RUNUP OPS CHECK GOOD AT THIS TIME.</P>)

ATA 2433

APU DOOR STATUS MESSAGE DISPLAYED(<P>APU PLACED ON MEL PER MEL 49-11-01A</P><P>LP 1058363-M5 FOUND APU TRU CB POPPING ALSO. REPLACED TRU. OPS CKS GOOD IAW AMM 24-32-04&NBSP; CLOSED MDDR</P>)

ATA 2150

LT PACK SWITCH "PACK OFF" LIGHT NOT ILLUMINATED.(<P>CYCLED LT PACK SWITCH IAW AMM 21-51-00-501. OPS CHECK NORMAL AT THIS TIME.</P>)

ATA 4940

APU WON'T START. PERFORMED APU AIR INTAKE SYSTEM TEST IAW AMM 49-15-00. AIR INTAKE CB POPS OUT. NOTICED WHEN THE INTAKE OPENS WITHOUT POPPING BREAKERS THE LT FWD FUEL PUMP LIGHT ILLUMINATED AND EXTINGUISHED CORRECTLY WITH EICAS MSGS. PER WDM 49-15-11 PAGE 1 OPERATIONS BEYOND RELAY TO APU INLET ACTUATOR IS INTERMITTENT. SUSPECT RELAY BAD. PERFORMED T/S, REMOVED AND REPLACED INLET DOOR ACTUATOR CIRCUIT BREAKER IAW SWPM 20-30-00 AND NO FIX. FOUND TRU FAN NOT RUNNING AND SUSPECT THAT IT IS THE PROBLEM. SWAPPED RELAY K176 W/ K616 FOR T/S. INLET DOOR OPS CORRECTLY W/ LT FWD FUEL LOW PRESSURE LIGHT. RETURNED RELAYS TO ORIGINAL POSITION. REMOVED AND REPLACED RELAY K176 IAW WDM 49-15-11. OPS CHECK APU IAW AMM 49-11-00; OPS CHECKED NORMAL AT THIS TIME.

ATA 3240

IN FLIGHT, CFL 410, RECEIVED EICAS ADVISORY MSG "PARKING BRAKE ". NOT ASSOCIATED W/MEL 32-44-01- 03C. ALREADY IN USED COMPLIED WITH QRH, PLANNED ARRIVAL INTO PHX WITH AUTO BRAKES AND ANTI SKID INOP.&NBSP;&NBSP;(<P>AMENDED TO MEL 32-44-01 PARKING BRAKE VALVE INOP. COMPLIED WITH MAINTENANCE PROCEDURES CAT C DUE DATE&NBSP; 05-MAY-19. MDDR 110744 REMAIN OPEN.&NBSP;</P><P>LP 1058388-2:&NBSP;T/S PER FIM 32-44 FT 805 AND FOUND PARKING BRAKE VALVE (V41) BAD. REMOVED AND REPLACED V41. OPS CHECK GOOD IAW AMM 32-44-04 THIS CLEARS MDDR # 110744, MCC NOTIFIED AND STICKER REMOVED.&NBSP;</P>)

ATA 2820

LT FWD FUEL LOW PRESS LIGHT INOP.(<P>TRANSFERRED TO DMI 110717. PERFORMED MX PROCEDURES PER DDG 28-42-01-01, SYS OPS NORMAL AT THIS TIME PER DDG.</P><P>LP 1058397 - M7:&NBSP;PERFORMED FIM 28-25 FT807. PASSES STEP 1 . BUT SUSPECT PROBLEM WITH RELAY K176 PER WDM 49-15-11. MCC NOTIFIED . DMI REMAINS OPEN.</P><P>LP 1058344 - 1:&NBSP;PERFORMED MAINTENANCE ACTIONS FOR LEFT FWD FUEL BOOST PUMP EICAS MESSAGE FOR PRESSURE LIGHT ILLUMINATION PER MEL # 28-42-01-01.&NBSP; OPS CHECK GOOD. DMI # 110717 REMAINS OPEN.&NBSP;</P><P>LP 1058346 - M7:&NBSP;PERFORMED TROUBLESHOOTING ON DMI 110717 LT FWD FUEL PUMP PSI LIGHT STAYS ILLUMINATED DURING APU START&NBSP;IAW FIM 28-25 FAULT TREE 807 AND SUSPECT BOOST PUMP PSI SWITCH S70.&NBSP;REF LP 1058344/M3</P><P>LP 1058356 - M4:&NBSP;REMOVED AND REPLACED RELAY K176 IAW WDM 49-15-11. OPS CHECK IAW AMM 28-22-00, NORMAL AT THIS TIME. THIS CLOSES DMI 110717. PLACARDS REMOVED.&NBSP;</P>)

ATA 5247

APU DOOR FAULT ON EICAS(<P>APU TRANSFERRED TO MDDR 110656 CAT C.</P><P>LP 1058379 - M5 - T/S PER WDM 49-15-11. REMOVED AND REPLACED INLET DOOR OPEN RELAY (K547). OPS CHECKS GOOD IAW 49-11-00. THIS CLEARS DMI 110656. REMOVED PLACARD AND MCC ADVISED. DISPATCH DF@0520Z.<BR /></P>)

ATA 2121

AFT EQ EXH FAN 2 STATUS MSG.(<P>PERFORMED OPERATIONAL TEST ON AFT EQ EXH FAN REF AMM 21-26-00. OPS CHECKED NORMAL.</P><P>MSG CLEARED.&NBSP;</P>)

ATA 3150

EICAS OVERSPEED FLASHED BRIEFLY ON #2 ENGINE START(<P>PERFORMED PIMU BITE IAW 71-01 FT 810, NO FAULTS FOUND. PERFORMED UNUSUAL CONDITION INSPECTION IAW AMM 72-00-00-206-096-H00&NBSP; FAN SPEED WAS BELOW 65PCT AT START. RAN ENG FOR 05 MIN. IDLE, NO MESSAGES ON START UP.</P>)

ATA 5247

APU INOP. FOUND C/B POPPING WHEN TRYING TO OPERATE APU, PER FIM 49-11 FT 988. REMOVED AND REPLACED APU INLET DOOR ACTUATOR IAW AMM 49-15-06-004. OPS CHECK GOOD.

ATA 2150

WHILE CLIMBING THROUGH 24,000, SMELLED AND SAW SMOKE IN COCKPIT. COMPLIED WITH QRH. AFTER GALLEY POWER REMOVED, SMOKE SEEMED TO DISSIPATE. EMERGENCY RETURN TO CVG. RECEIVED NO MAIN DECK ALERTS.(<P>PERFORMED A SMOKE INSPECTION IAW AMM 21-00-21. DURING INSPECTION FOUND THE LT PACK DOOR ACTUATOR MALFUNCTIONED IN THE CLOSED POSITION. THIS CAUSED AN OVERHEAT SITUATION OF THE LT PACK SYSTEM. R&AMP;R THE LT PACK DOOR ACTUATOR IAW AMM 21-53-01. OPS CHECK LT SYSTEM WITH NO FAULTS NOTED AT THIS TIME. </P><P>LT PACK CONTROLLER WAS FOUND TO BE INOP, REMOVED AND REPLACED LT PACK TEMP CONTROLLER IAW AMM 21-61-03 OPS CHECK GOOD. OFF PART (S/N:&NBSP;<SPAN>099C-1110, P/N:&NBSP;</SPAN><SPAN>625946-10).</SPAN></P><P>LP 1073441: HIGH POWER ENG RUN COMPLETE AND OIL CONTAMINATION INSPECTION COMPLETE WITH NO NOTED DEFECTS, FUMES, SMOKE, OR SMELL I.A.W. 21-00-21.</P>)

ATA 8011

RT ENG START SELECTOR REMAINS IN GND AFTER, MX CONFIRMED BY ENG STARTS OK IN MANUAL MODE / ( STARTER SWITCH HOLDING/CUTOUT SYSTEMS )(<P>TRANSFERRED TO MDDR # 108631.</P><P>LOG PAGE 1073447: REMOVED AND REPLACED NR 2 ENG START SELECTOR SW IAW SWPM 20-74-12. OPS TEST GOOD IAW AMM 71-00-00. MDDR # 108631 CLOSED.</P>)

ATA 3350

EMERGENCY LIGHT GUARD SPRING BROKEN AND CATCHES SWITCH, MOVES SWITCH TO OFF WHEN CLOSED/GUARDED.(<TABLE CLASS="MSONORMALTABLE" BORDER="0" CELLSPACING="0" CELLPADDING="0" WIDTH="1040" STYLE="MARGIN-LEFT: -0.15PT;" DATA-LEFT="1.8125"> / <TBODY><TR STYLE="HEIGHT: 75PX;"> / <TD WIDTH="146" VALIGN="TOP"> / <P><SPAN>ADJUSTED EMERGENCY LIGHTS GUARD IAW AMM 20-11-00. OPS CHEKC GOOD / IAW AMM 33-50-00</SPAN></P> / </TD> / </TR> / </TBODY></TABLE>)

ATA 2810

EVIDENCE OF FUEL LEAK ON #1 PYLON AFT SKIRT FAIRING AT AFT SPAR.(<P>SEALED 8 EA FASTENERS ON INBOARD NR 1 PYLON AFT SKIRT FAIRING, PERFORMED SATISFACTORY LEAK CHECK, NO LEAKS NOTED IAW AMM 28-11-00.&NBSP;</P>)

ATA 3510

INFORMED BY CA, O2 MASK DAMAGED.(<P>REPLACED O2 MASK IAW 35-11-51.<BR /></P>)

ATA 4997

NO DUCT PRESSURE DURING APU OPERATION.(<P>ITEM TRANSFERRED TO MDDR# 107913 PER DDG 49-11-01-01 (APU PNEUMATIC INOP).</P><P>NOTE PERFORMED INITIAL TS BITE ECU SHOWING P2 SENSOR FAULY. TS SHOWING WIRE TO P2 SENSOR PIN 1 OPEN. NEED FURTHER TS AND REPAIR BROKEN WIRE TO P2 SENSOR. TROUBLESHOOT SYSTEM, FOUND APU WIRING HARNESS BAD, REMOVED, REPLACED AND PERFORMED&NBSP; GOOD OP'S CHECK IAW MM 49-11-00.<BR /></P>)

ATA 4950

APU INOP. NO DUCT PRESSURE.(<P>TRANSFERED TO MDDR 107846. LP 1015204, WO 48189 COMPLIED WITH T/S PER B767 AMM 24-21-00 OPS TEST APU GENERATOR OK. AMM 36-23-00 AIR SUPPLY CONTROL SYSTEM BITE TEST OK,AMM AIR SUPPLY PRESSURE IND SYSTEM OPS TEST. LEFT DUCT PSI 31 RIGHT DUCT PSI 32 NORMAL.REMOVED AND REPLACED APU FLOW SENSING MODULE IAW AMM 49-53-08.PERFORMED APU SELF TEST AND RAN UNDER LOADS AND OPS CHECK AND TEST GOOD IAW 49-61-05.REMOVED PLACARDS.<BR /></P>)

ATA 4990

APU RUNNING AFTER COLD SOAK START, AT APPROX 1000 AGL "APU FAULT" LIGHT CAME ON, FOLLOWED BY "APU GEN OFF" LIGHT.(<P>PERFORMED BITE CK OF APU ECU &AMP; FOUND MINI FLAGS 15EL16, UPON INSPECTION OF APU, FOUND A LOOSE OIL PRESSURE LINE. TIGHTEN OIL PRESSURE LINE&AMP; OPS CKD APU IAW AMM 49-11-01, DELTA P &AMP; CHIP DETECTORS ALSO GOOD. OPS CHK GOOD.</P>)

ATA 2421

" APU GEN OFF" EICAS MSG AND "APU FAULT " EICAS MESSAGE(<P>PERFORMED BITE TEST AND RESET, STARTED APU, OPS CHECK NORMAL ON APU GENERATOR&NBSP;IAW B767 AMM 49-11-00-815.</P>)

ATA 4950

APU PNEUMATIC FUNCTION INOPERATIVE. REMOVED AND REPLACED THE APU SHUTOFF VALVE IAW AMM 36-11-10. OPS CHECKED IAW AMM 36-11-10.

ATA 4920

DURING ENGINE START, W/ START VALVE OPEN BARELY REACHED 21 PSI. N2 AT 30 SEC, ONLY 18 AND ONLY REACHED 21 AT 45 SEC. SLIGHTLY SLOW TO ACCELERATE. R&R SURGE VALVE IAW AMM 49-53-01. NO FIX. REQUIRES MORE T/S. DMI REMAINS OPEN. SURGE VALVE OBSERVED NOT FULLY CLOSING. REMOVED AND REPLACED APU ASSY PER AMM 49-01-01/401 BUT IT WILL NOT START ECM SHOW ON LRU SUMMARY AP SENSOR P2 P1.

ATA 2611

INTERMITTENT STATUS MSG AFT CARGO DET 2. PERFORMED AFT CARGO SMOKE DET TEST PER AMM 26-16-00, TEST OK. PERFORMED FIM 26-10 FT 803, AFOLTS CARDS OK. NO RED LIGHTS NOTED, NO YELLOW LIGHTS, RAN FIM 26-10 FT 832, SYSTEM OK. MSG CLEARED. ORDERED SMOKE DET P/N 2156-55 WITH MCC AS PRECAUTION- SYSTEM OPS OK. FOUND DETECTOR 2A2C FAULTING, REMOVED AND REPLACED DETECTORS 2A2C, 2A2A, 2A2B, 2A2D IAW AMM 26-14-01. SN OFF: 30736B, PN OFF 2153-55.

ATA 7810

RT ENGINE EXHAUST PLUG, TAIL RING HAS A CRACK(<P>TEMP REPAIRED PER EO 6778A052. ITEM TRANSFERRED TO NON MEL 107005, PART #1 C/W, DVI EVRY 5 FC.&NBSP;</P><P>LP 1031080: REMOVED AND REPLACED RH ENG EXHAUST PLUG IAW B767 AMM 78-11-02. THIS ACTION CLOSES MDDR 107005.&NBSP;&NBSP;</P><P><BR DATA-MCE-BOGUS="1" /></P>)

ATA 4950

ON START APU DUCT PRESSURE 21PSI DOES NOT REACH MAX MOTORING N2 AT 30 SECONDS NEEDS 50 SECONDS TO REACH MAX MOTERING.(<P>PERFORMED DRY MOTOR OF ENG #1 AND ENG #2 FOUND ALL VALUES TO BE WITHIN LIMITS PER B767 AMM 71-00-01-862-053-H03, NO FURTHER DEFECTS NOTED.<BR /></P>)

ATA 2432

APU BATT. LOW WILL NOT START APU(<P>REMOVED AND REPLACED APU BATTERY, INSTALLATION CHECK GOOD PER B767 AMM 24-31-00<BR /></P>)

ATA 4960

INFO ONLY:&NBSP; APU ONLY PUTS OUT 25PSI ON START. VERY SLOW TO START&NBSP;(<P>PERFORMED BITE TEST ON APU CONTROLLER NO FAULTS NOTED. OPS CHECK OK&NBSP; CREW WILL NOTE APU PERFORMANCE NEXT LEG - REF AMM 49-61-05</P>)

ATA 2820

LT AFT MAIN BOOST PUMP INOP(<P>OPENED MDDR 106484</P><P>LP 1023891-M5 REMOVED AND REPLACED&NBSP; FUEL FEED ASSY IAW AMM 28-22-01 OPS CHECK&NBSP; GOOD AT THIS TIME THIS CLEARED DMI 106484 PLACARD REMOVED&NBSP;</P>)

ATA 7200

SIGNIFICANT VIBRATION FELT FROM LEFT ENGINE DURING CLIMB AND DECENT WITH MODERATE POWER SETTINGS. N2 VIBRATION INDICATES 3.9. FOLLOWED FIM 71-05 TASK 841, NO DEFECTS NOTED AT THIS TIME. ACFT OK TO CONTINUE.

ATA 2822

L AFT FUEL PUMP EICAS MSG ON TAKEOFF&NBSP; PAST ROTATION RUN NNL AT 10,000 ML TURNED LEFT AFT FUEL PUMP SWITCH OFF CONTINUES NORMAL OPS.(<P>RESET C/B G-15 ON THE P-6 PANEL IAW AMM 20-60-01 OPS CHECK OF LEFT AFT BOSST PUMP CHECK GOOD AT THIS TIME IAW AMM 28-22-03</P>)

ATA 4950

INTERMITTENT LOW \APU BLEED PRESSURE 21 PSI IS REQUIRED. OCCURED ON THE SECOND ENGINE START.(<P>REMOVED AND INSPECTED CLEANED SURGE VALVE FILTER ELEMENT IAW AMM 49-53-06, 26PSI. NO PACKS MINIMUM ENGINE START 25 PSI OK FOR SERVICE.<BR /></P>)

ATA 8012

RT ENGINE START VALVE LIGHT INDICATION INOP(<DIV>TRANSFERRED TO MDDR 105584 IAW MEL 80-00-01-01 CAT C - DUE DATE 17JAN19&NBSP;&NBSP;</DIV><DIV>LP 1023826 -M2 REMOVED AND REPLACED ENGINE START VALVE ASSY IAW AMM 80-11-02 PERFORMED OPS CHECK&NBSP; NORMAL IAW AMM 71-00-00 CLEARED MDDR 105584</DIV>)

ATA 2612

AFT CARGO DET 2 STATUS MESSAGE(<P>LP 1022369- (TS) PFMD FIM 26-10 FAULT TREE 803. RE-RACKED CARDS M10224, M10274, M10400 AND M10427. AFT CARGO DET 2 MSG CLEARS FROM THE STATUS PAGE. PERFORMED FIM 26-10 FAULT TREE 832 SYSTEM TEST OK. PERFORMED AFT CARGO SMOKE DETECTION TEST PER AMM 26-16-00-735-352-003.NO FAULTS WERE NOTED.<BR /></P><P>LP 1023811 - AFTER TS - ITEM TRANSFERRED TO MDDR 105643 IAW DDG 26-16-01-01-01 CAT C - DETECTOR INOP.&NBSP;NOTE: PROBLEM RETURNED DURING MX PRE-FLIGHT. REPLACED CARD M10427 FIRE OVHT.</P>)

ATA 4950

APU INOP(<P>TRANSFERRED TO MDDR 105583 IAW MEL 49-11-01A CAT "C" DUE DATE 17JAN19. </P><P>LP 1023816 - M3: REMOVED AND REPLACED SURGE VALVE IAW AMM 49-53-01. OPS CHECK GOOD AT THIS TIME. THIS ACTION CLEARS DMI #105583. MCC NOTIFIED AND PLACARDS REMOVED.&NBSP;<BR /></P>)

ATA 2610

AFT CARGO DET 2 STATUS MSG.(<P>C/W FIM 26-16-01 OPS CHECKS NORMAL.<BR /></P>)

ATA 2613

STATUS AFT CARGO DET 2(<P>FIRE AND OVERHEAT TEST CARRIED OUT IAW AMM 26-10-00 AND STATUS MESSAGE CLEARED, OPERATION AS EXPECTED. MCC NOTIFIED.</P>)

ATA 8011

BOTH ENGINES&NBSP; SLOW&NBSP; TO START&NBSP; N2 SLOW TO RISE(<P>INSPECTED PENUMATIC FUNCTION FROM APU AND PRESS STAY&NBSP; NO LEAKS FOUND IAW&NBSP; FIM 80-11 FT 805 REPLACED #2 ENG STARTER OPS CHECK NORMAL IAW AMM 80-11-01</P>)

ATA 4960

FOR BOTH ENGINE STARTS DUCT PRESS WAS AT MIN 21 PSI MAX MOTOR N2 LOWER THAN NORMAL STARTS OK.(<P>PERFORMED APU ECU MINIFLAG BITE PROCEDURES NO FAULT NOTED OPS NORMAL IAW AMM 49-61-05.</P>)

ATA 7320

LEFT EEC INOP. RR / LH EEC CONT KORRY SW MASTER MODULE IAW AMM 33-13-00 OPS CKD NML.

ATA 7200

SLOW N2 ON START FOR BOTH ENGINES. C/W IDLE ENGINE RUN. ENGINES BOTH WITHIN NORMAL STARTUP PARAMETERS IAW B767 AMM 71-00-00.

ATA 4950

APU HAS INSUFFICIENT DUCT PRESSURE FOR ENGINE START. PERFORMED OPS CKS PER APU AMM 49-11-02, OPS CKD GOOD.

ATA 2610

AFT CARGO DETECTOR NR 2 INOP. REMOVED AND REPLACED ALARM/TEST INTERFACE MODULE M12275 AS PER AMM 26-14-04. TEST GOOD PER AMM 26-14-00.

ATA 2422

MAJOR ELECTRICAL EVENT OCCURRED WHEN APP SWITCHED PUSHED. RESULT WAS TEMPORARY LOSS OF POWER TO FLIGHT DECK INSTRUMENTS AND DISENGAGE OF AUTOPILOT. POWER RESTORE WITHIN SECONDS... UPON POWER RESTORATION CAPTAIN SIDE INSTRUMENTS REMAINED NON FUNCTIONAL 5 TO 10 SECOND BEFORE RESTORING. WHEEL WELL FIRE EICAS AND WARNING BELL WERE PRESENT MOMENTARILY CENTER AUTOPILOT WAS SELECTED, ENTIRE EVENT. REPEATED AS DESCRIBED. AFTER ALL EICAS MESSAGE SELF CLEARED, REMAINING STATUS MESSAGE WERE STANDBY INVERTER AND CAPTAINS STANDBY INDICATOR&NBSP;(<P>REMOVED AND REPLACED BUS POWER CONTROL UNIT IAW AMM 24-41-03. OPS CHECK GOOD IAW AMM 24-41-03. REMOVED AND REPLACED CB C841 PER SWPM AND WDM 24-33-11.&NBSP;</P><P>REFERENCE LOG PAGE 885269 ITEM M6; REMOVED AND REPLACED STATIC INVERTER ASSY PER AMM 24-33-03, OPS CHECK GOOD. P/N OFF 707760-4&NBSP; &NBSP;S/N 1034.&NBSP;</P><P>REFERENCE LOG PAGE 885270 ITEM M7; T/S FOUND C/B BATTERY TRANSFER RESET C/B POPPED PER MCC REQUEST REMOVED AND REPLACED RELAY K106 PER AMM SWPM 20-81-16 CHECK OK.&NBSP; P/N OFF 931-8506&NBSP; &NBSP;S/N TL520135.&NBSP; ITEM M8, T/S FOUND C/BB BATTERY TRANSFER CONTROL C/B POPPED PER MCC REQUEST REMOVED AND REPLACED RELAY K104 AMM SWPM 20-81-16. P/N OFF 10-61445-21&NBSP; S/N 217571.&NBSP; ITEM M9,&NBSP; PER MCC REQUEST REMOVED AND REPLACED RELAY K701 PER AMM 20-81-16 CHECK OK P/N OFF BACR13C62A&NBSP; S/N NSN.&NBSP;&NBSP;</P>)

ATA 2822

FOUND L/H AFT FUEL PUMP SWITCH DAMAGED.(<P>REMOVED AND REPLACED LEFT AFT FUEL PRESSURE KORRY SWITCH IAW AMM 20-34-15 OPS CHECK GOOD.</P>)

ATA 7930

RT ENGINE OIL PRESSURE INDICATION LIGHT WAS INOPERATIVE. REMOVED & REPLACED THE LIGHT ASSY IAW AMM 33-13-00, CHECKED NORMAL.

ATA 3697

FOUND THE LT ENGINE PRV TERMINAL LUGS DAMAGED AND CHAFED TO GROUND. REMOVED AND REPLACED THE TERMINAL LUGS IAW SWPM 20-30-11.

ATA 3610

DURING PNEUMATIC LEAK CHECK FOUND LEAK AT PRV MUSCLE LINE AT UNION AND FITTING. REMOVED AND REPLACED SEAL AT PRV MUSCLE LINE IAW AMM 36-11-18 NO LEAKS DETECTED.

ATA 3610

LEFT ENGINE BLEED EICAS AT LEVEL OFF. REMOVED AND REPLACED THE LT ENGINE PRSOV IAW AMM 36-11-09, RAN THE ENGINE IAW AMM 71-00-00, ENGINE BLEED SYS NORMAL.

ATA 2610

LEFT STRUT DUCT LEAK EICAS MESSAGE AT LEVEL OFF. REPLACED THE TS 232 WING - STRUT DUCT LEAK DETECTION SYS, TESTED IAW AMM 26-18-00. PERFORMED A HIGH POWER ENGINE RUN IAW AMM 71-00-00. NO DUCT LEAK MESSAGE OR LIGHT. NO LEAK FOUND IN THE STRUT.

ATA 3610

DURING CLIMB, THE LT ENGINE BLEED OFF EICAS MESSAGE. QRH 2.16 COMPLIED WITH. ACCOMPLISHED FIM 56-10/ 857, NO FAULTS NOTED ON AIR SUPPLY BITE. REPLACED THE BLEED AIR CARD M-859 IAW AMM 36-11-12. RAN ENGINES IAW AMM 71-00-00. OPS CHECKED GOOD.

ATA 7500

LEFT ENGINE BLEED EICAS, DURING FLT. QRH COMPLETED. REMOVED AND REPLACED PRV EXIT PRESSURE SENSOR. OPS CHECKED GOOD, ACFT OK FOR SERVICE IAW AMM 36-21-08. PERFORMED POWER ASSURANCE TEST IAW 71-00-00-735-394-H03. ALL INDICATIONS SATISFACTORY AND NO FAULTS NOTED.

ATA 3610

LEFT ENG BLEED EICAS DURING CLIMB. ACCOMPLISHED FIM 36-10/837. NO FAULTS NOTED ON BITE TEST.

ATA 2610

LEFT STRUT DUCT LEAK EICAS, PERFORMED QRH. PERFORMED FIM 26-18 FT 804 AND AMM 26-18-00, NO DEFECTS NOTED. PRESSURE CHECKED THE LT PACK AREA AND L/E DUCT LEFT SIDE PRSOV. NO LEAKS NOTED. PERFORMED A DUCT LEAK AND WHEEL WELL FIRE CARD IAW AMM 26-10-00 CHECKED GOOD.

ATA 3620

ON CLIMB OUT "LT ENG BLEED OFF" EICAS. PERFORMED BITE TEST OF AIR SUPPLY MONITOR UNIT PASSED NO FAULTS OR EICAS MSG AT THIS TIME AMM 36-11-0.

ATA 3610

EICAS: " L STRUT DUCT LEAK" FL 390, QRH ACCOMPLISHED L DUCT PRESS 5 PSI RT DUCT PRESS 31 PSI. FOUND LOOSE V-BAND CLAMP IN PYLON JUST FWD OF PRSOV RE-TORQUED V-BAND CLAMP AND RAN ENGINE, NO DUCT LEAK NOTED AT THIS TIME. REF AMM 70-50-00 AND 71-00-00.

ATA 2150

LT AC PACK RAM AIR EXHAUST DOOR HOUSING HAS 8 SQ IN DISBONDED. LAYER LOOKING FWD THRU OPEN DOOR .REPAIRED LT A/C PACK RAM AIR EXHAUST DOOR HOUSING IAW AMM 21-23-07. PERFORMED LEAK AND OPERATION CHECK IAW AMM 21-53-02. LEAK AND OPERATIONAL GOOD. (SUP DD 10/27)

ATA 2133

MISSING MATERIAL OF THE BUTYL SEAL OF THE FLAPPER DOOR AFT ASSEMBLY. REMOVED AND REPLACED SEAL ON FLAPPER DOOR AFT ASSY (OUTFLOW VALVE TOP DOOR SEAL) IAW AMM 51-31-01. (SUP DD 10/27)

ATA 2150

LT A/C PACK RAM AIR INLET DOOR WORN 2ND FROM FWD HINGE RT SIDE. REMOVED AND REPLACED LT A/C PACK RAM AIR AFT HINGE ON DOOR IAW SRM 51-40-02. (SUP DD 10/27)

ATA 2150

LT A/C PACK RAM AIR INLET DOOR FWD HINGE HAS MIGRATED PIN. RESEATED LG A/C PACK TAM AIR INLET DOOR FWD HINGE IAW AMM 21-53-01. (SUP DD 10/27)

ATA 2121

EQUIPMENT COOLING EXH FAN C/B IS POPING OUT. REMOVED AND REPLACED EQUIPMENT COOLING FWD EXH FAN IAW AMM 21-58-06. PERFORMED INSTALLATION TEST IAW AMM 21-58-06. (SUP DD 10/27)

ATA 2121

EQUIPMENT COOLING FAN MOUNTING LUG BROKEN OFF FROM ASSY. REMOVED AND REPLACED EQUIPMENT COOLING FAN IAW AMM 21-58-06. OPS CHECK GOOD, NO LEAK NOTED. (SUP DD 10/27)

ATA 7220

LOOSE FIBERGLASS MESH ON ACOUSTICAL PANEL NR 2 ENGINE FAN CASE AT 5 OCLOCK POSITION IAW SRM 54-12-01 REPAIR 6. REPAIRED MESH ON ACOUSTICAL PANEL NR 2 ENGINE FAN CASE AT 5 OCLOCK POSITION IAW SRM 54-12-01 REPAIR 6. (SUP DD 10/27)

ATA 2150

RT PRIM HX IN INDICATION IS MISSING ON EICAS. REMOVED AND REPLACED RT TEMP BULB SENSOR, PERFORMED INSTALLATION TEST IN RT TEMP BULB SENSOR WITH NO FAULTS IAW AMM 21-52-08 RT PRIM HX IN EICAS. (SUP DD 10/27)

ATA 7261

NR 1 ENG, OIL TANK LEAKING AT FILL AND DRAIN PLUGS. CLEANED NR 1 ENG OIL TANK, AREA AROUND FILL AND DRAIL PLUGS IAW SOPM 20-30-03 PERFORMED. SATISFACTORY CHECK OF NR 1 ENG OIL TANK AND (NO LEAKS NOTED) IAW AMM 71-00-00. (SUP DD 10/27)

ATA 7313

NR 1 ENG TCC DUCT AFT OF FUEL NOZZLES HAS 2 EA ATTACH LINKS WITH WORN RODEND BEARINGS. REMOVED AND REPLACED 2 EA ATTACH LINKS AFT OF FUEL NOZZLES ON NR 1 ENG I/B SIDE IAW AMM 70-50-00. (SUP DD 10/27)

ATA 2150

RT A/C PACK AFT EXHAUST DOOR RT ATTACH BEARING HAS MIGRATED LINER. REMOVED AND REPLACED RT A/C PACK AFT EXHAUST DOOR RT ATTACH BEARING IAW S20-50-03.

ATA 2120

DURING E&E COOLING LOW FLOW MONITOR SYSTEM TEST E5 FLOW BALL INTERMITTENT. T/S FOUND LOOSE HOSE CLAMP ON E&E COOLING LOW FLOW MONITOR. RE-SECURED HOSE CLAMP AND PERFORMED SATISFACTORY OPS CHECK IAW AMM 21-58-34.

ATA 7110

NR 2 ENG RT CORE COWL BLOW OUT DOOR FITS LOOSE WHEN FULLY CLOSED. REMOVED AND REPLACED UPPER AND LWR HINGES ON BLOW OUT DOOR IN NR 2 ENG RT CORE COWL IAW SRM 51-40-02. (SUP DD 10/27)

ATA 2613

EICAS MSG L STRUT DUCT LEAK. PERFORMED WING AND BODY DUCT LEAK DETECTION BITE PROCEDURE IAW FIM 26-18 FAULT TREE 804 AND FOUND NO DEFECTS AT THIS TIME.

ATA 2310

DURING COAST OUT HF RADIO L/R BOTH UNREADABLE NO COMM ESTABLISHED, NO SELCAL, RADIO COULD HEAR US BUT WE COULD NOT HEAR THEM. TRANSFER TO MDDR 98961 IAW MEL 23-11-01-02A CAT D DUE 01 JAN 18 PLACARDS INSTALLED.

ATA 3620

"LT ENG BLEED OFF" EICAS MESSAGE IN FLIGHT. REMOVED AND REPLACED LEFT FAN AIR TEMP SENSOR IAW AMM 36-11-17. LEAK AND BITE TEST OK.

ATA 2150

"LT PACK OFF" EICAS MESSAGE IN FLIGHT. PERFORMED ADJUSTMENT OF LT PACK SYSTEM. OPS CHECKS GOOD AT THIS TIME IAW AMM 21-51-00.

ATA 2613

ON LANDING LEFT STRUT DUCT LEAK EICAS MESSAGE. PERFORMED FIM 26-18 FT 804, NO FAULTS NOTED AT THIS TIME. DUCT LEAK OPS CK OK.

ATA 4920

AT CRUISE, APPROX 5 MIN AFTER APU START A STRONG ODOR WAS DETECTED. AFTER APU SHUTDOWN THE ODOR DISSIPATED. IT CAME BACK DURING DESCENT AT APPROX 60,000, WITH L PACK OFF THE ODOR WAS LESS NOTICEABLE. PERFORMED FIM 21-00-21 LEFT PACK. FOUND NO TRACES OF OIL IN LT PACK DUCTING. FOUND OIL RESIDUE IN APU PLENUM DURING APU VISUAL INSPECTION. REF LBP 99475, ITEM 6 FOR CORRECTIVE ACTION OF PLENUM.

ATA 4990

APU INOP. WHILE SEARCHING FOR SOURCE OF SMELL PERFORMED GVI OF LEFT PACK AS PER AMM 21-51-00 FOUND EVIDENCE OF OIL AT DUCT FWD OF AC BEFORE TRIM AIR VALVE, LT PACK CLEAN OIL ON AN DIN DUCTS AS PER AMM 21-00-21, CLEANED RESIDUAL OIL IN MIXING MANIFOLD AS PER AMM 20-30-02 , TOOK AIRCRAFT OUT FOR HIGH POWER RUNS WITH NO ODOR DETECTED.

ATA 4920

APU INOP. THIS ITEM DEFERRED UNDER 49-11-01A, CAT "C". DUE DATE: 20JUL18.

ATA 2120

STRANGE OFFENSIVE ODOR EMANATING FROM THE AIRCRAFT VENTILATING SYSTEM WHEN THE PACKS ARE RUNNING. PERFORMED INSPECTION FOR SMOKE AND FUMES FROM AIRCRAFT VENTILATION SYSTEM IAW AMM 05-51-56, NO OFFENSIVE ODOR OR SMOKE DETECTED AT THIS TIME.

ATA 3610

AFTER ENGINE START LEFT BLEED OFF EICAS MSG WITH BLEED SW ON LT ENGINE DUCT PRESSURE ZERO (REPEATED ITEM). DUE HISTORY - PERFORMED TROUBLE SHOOTING AS FOLLOWS: R&R BLEED AIR CONTROL CARD PN 285T1115-15 SN OFF D01731 SN ON D01066 -AMM36-11-12. R&R HPSOV PN 802170-12 SN OFF 9905070 SN ON 900583 AMM 36-11-07. ALSO REPLACED CONNECTOR D11116 (PRV CONTROLLER CONNECTOR) DUE BACKSHELL STRIPPED. R&R PRSOV PN 799801-4 SN OFF 9910044 SN ON 2009041355 AMM 36-11-09. PERFORMED ENG RUN UP PER AMM 71-00-00, CHECK OK.

ATA 2120

PACKS HAVE EXTREMELY BAD ODOR EMANATING FROM THEM. LEFT FLIGHT WITH HEADACHE. BAD SOCK? RAN PACKS IAW 21-00-00-862-024 AMM FOR ONE HOUR NO DEFECTS NOTED AT THIS TIME.

ATA 3610

L ENG BLEED STATUS MSG. R&R PRV CONTROLLER IAW 36-11-19. TEST OK.

ATA 3610

L ENGINE BLEED EICAS AFTER START. REMOVED AND REPLACED NR 1 ENGINE FAN AIR VALVE IAW AMM 36-11-16. PERFORMED OPS AND BITE TEST OPS NORMAL.

ATA 3442

LAND R WX RADAR INOP. "WX FAIL" APPEARS ON BOTH CA & FO EHDI. "WX SYS" STATUS MESSAGE. PERFORMED OPS CHECKS ON THE L+R WX RADAR PER AMM 34-43-00, OPS CHECKS GOOD & RAN FIM 34-45 TASK 805 BOTH SYSTEM OK.

ATA 2150

ODOR EMANATED FROM THE A/C PACKS. PERFORMED AN OPS CHECK IAW AMM 21-63-01, SYSTEM TESTED OK. COULD NOT DUPLICATE THE ODOR.

ATA 2120

BAD ODOR EMANATING FROM THE A/C PACKS. PERFORMED AN OPS CHECK IAW AMM 21-63-01. RAN BOTH PACKS HOT FOR FIVE MINUTES THEN RAN BOTH PACKS COLD FOR FIVE MINUTES, COULD NOT DUPLICATE THE ODOR.

ATA 2150

LEFT PACK TEMP ON CLIMBOUT. AFTER STBY N AND 5 MINS, PACK RESET PUSH INOP LIGHT STAYS EXTINGUISHED. REMOVED AND REPLACED LT PACK ACM IAW MM21-51-03.

ATA 2150

AFTER TAKE OFF, AN EICAS MESSAGE FOR THE LT PACK TEMP ILLUMINATED. OPERATED THE LEFT PACK IN STBY N MODE IAW QRH 2.33 PROCEDURES.

ATA 2150

LEFT PACK TEMP MESSAGE. ACCOMPLISHED A PACK TEMP BITE, NO FAULTS NOTED IAW FIM 21-51 FT 844 , OPERATED PACK FOR OVER AN HOUR, OPS CHECKED GOOD IAW AMM 21-51-00,

ATA 7300

FOUND A LEAKING PRESSURE TRANSMITTER ON THE NR 2 ENGINE. DEACTIVATED THE PRESSURE TRANSMITTER IAW AMM 73-33-01. REMOVED AND REPLACED, AND REACTIVATED THE NR 2 ENGINE FUEL PUMP PRESSURE TRANSMITTER IAW AMM 73-33-01-402-033-H00. OPS & LEAK CHECKED GOOD.

ATA 7532

AFTER DE-ICING, THE LT ENGINE BLEED OFF EICAS MESSAGE AND LT ENGINE BLEED SWITCH OFF LIGHT ILLUMINATED AND WILL NOT EXTINGUISH. RAN THE ENGINE IAW AMM 71-00-00, CYCLED LEFT BLEED SWITCH AND CIRCUIT BREAKER. LEFT ENGINE BLEED OK. REMOVED AND REPLACED THE NR 1 ENGINE HIGH PRESSURE CONTROLLER IAW AMM 36-11-08, OPS & LEAK CHECKED GOOD. REMOVED AND REPLACED THE NR 1 ENGINE HPV IAW AMM 36-11-07, LEAK AND OPS CHECKED SATISFACTORY.

ATA 7330

R ENG FUEL VAL EICAS MESSAGE ON ENGINE START. DEFERRED PER MEL 73-21-03-01 CAT C PLACARD INSTALLED MDDR 91252.

ATA 7100

NR 1 ENGINE COOLING AIR DUCT TURBINE SECTION LT SIDE ONE LINK ROD MISSING. INSTALLED A NEW ROD IAW AMM 75-24-03.

ATA 2100

OVER PRESSURE RELIEF VALVE NEEDS TO BE RESET ON THE LT FUSELAGE. ACCOMPLISHED RESET IAW AMM 21-32-00.

ATA 3610

RT FATS DOES NOT COMMAND FAN AIR VALVE. REMOVED AND REPLACED THE RT ENGINE FAN AIR VALVE TEMP SENSOR IAW AMM 36-11-17.

ATA 4950

APU INOPERATIVE. ACCOMPLISHED AN APU BITE IAW FIM 49-11/ 958, FOUND REVERSE FLOW FAULT. ACCOMPLISHED 49-11 FAULT TREE 965. REMOVED AND REPLACED APU SURGE VALVE IAW AMM 49-53-01, OPS CHECKED NORMAL.

ATA 3610

LEFT ENGINE FAN AIR VALVE SWITCH DISAGREE. FOUND THE LEFT ENGINE FAN AIR VALVE FAULTING. REMOVED AND REPLACED FAN AIR VALVE IAW AMM 36-11-16, OP CHECKED OK.

ATA 2400

EICAS MESSAGE FOR THE STANBY BUSS OFF ILLUMINATED. REMOVED AND REPLACED THE K104 RELAY IAW AMM 24-33-02 AND STANDBY POWER PANEL IAW AMM 24-33-04. OPS CHECKED NORMAL IAW AMM 24-33-00.

ATA 2130

AT FL 370 CABIN ALTITUDE BEGAN A SLOW CLIMB, WITH OUTFLOW VALVE FULLY CLOSED. DESCENDING TO FL 300 AND CABIN ALT STABILIZED AT 9000FT. PERFORMED A BITE CHECK OR THE PRESSURE CONTROLLERS IAW AMM 21-31-00. OPS CHECKED GOOD.

ATA 4920

APU FAILED AND FAILED TO RESTART. ACCOMPLISHED AN APU BITE IAW FIM 49-11 FT 958. FOUND REVERSE FLOW FAULT, ACCOMPLISHED FIM 49-11 FAULT TREE 965, REMOVED AND REPLACED THE APU SURGE CONTROL VALVE IAW AMM 49-53-01. OPS CHECKED GOOD.

ATA 2121

STATUS MESSAGE AFT EQ EXHAUST FAN 2. OPS CHECKED GOOD IAW AMM 21-58-11.

ATA 7320

DURING APPROACH, IDLE DISAGREE. REMOVED AND REPLACED THE LEFT ADC IAW AMM 34-12-01. OPS CHECKED GOOD, PERFORMED TEST 30 OF MCDP IAW AMM 22-02-00. OPS CHECKED GOOD.

ATA 4990

APU AUTO SHUTDOWN. REMOVED AND REPLACED THE GENERATOR OIL FILTER DIFFERENTIAL PRESSURE SWITCH IAW AMM 49-27-15.

ATA 7310

LEFT ENGINE FUEL FILTER BY-PASS EICAS AND STATUS MESSAGE. REMOVED AND REPLACED THE NR 1 FUEL FILTER IAW AMM 73-11-02

ATA 4920

DURING APU START ON GROUND, AN APU FAULT EICAS MESSAGE DISPLAYED, SECOND START SUCCESSFUL, DURING SECOND APU START, THE APU BATTERY DISCHARGE MESSAGE DISPLAYED. TROUBLESHOT IAW FIM 24-90-04, STARTED APU SEVERAL TIMES. NO FAULTS NOTED, OK FOR SERVICE.

ATA 7320

DURING DESCENT, IDLE DISAGREE EICAS MESSAGE DISPLAYED. REMOVED AND REPLACED THE RT EEC IAW AMM 73-21-05, CHECKED NORMAL.

ATA 2822

R CTR FUEL PUMP LOW PRESSURE LIGHT, PERFORMED OPERATIONAL TEST OF FUEL PUMP. OPS CHECK GOOD, NO FAULT IAW 28-22-00.

ATA 7261

EVIDENCE OF THE NR 1 ENGINE OIL CAP LEAKING. REMOVED AND REPLACED THE OIL CAP O-RING IAW AMM 79-11-03, RAN ENGINE AT IDLE AND PERFORMED LEAK CHECK IAW AMM 71-00-00. LEAK CHECKED GOOD.

ATA 3442

WEATHER RADAR CONTROL PANEL MODE SELECT KNOB BROKEN. REPLACED THE CONTROL PANEL ASSY IAW AMM 34-43-02.

ATA 3150

IDLE DISAGREE EICAS MESSAGE DURING DESCENT AND APPROACH. RAN BOTH ENGINES AT IDLE AND APPROACH IDLE IAW AMM 71-00-00 TEST 4. TRANSITION FROM GROUND IDLE TO APPROACH IDLE NORMAL. OK FOR SERVICE.</P>)

ATA 7200

RIGHT ENGINE IN GROUND IDLE ECAS MESSAGE IN FLIGHT. PERFORMED A BITE - PIMU CHECK, MESSAGE CLEARED IAW FIM 71-05-00.

ATA 7200

IDLE DISAGREE EICAS MESSAGE DURING DESCENT, WHEN THROTTLES AT IDLE. PERFORMED FIM 71-05, FT 846, CHECKED RESISTANCES AT THE EEC LEFT AND RIGHT CONNECTORS. RESISTANCES LESS THAN 15 OHMS FOR BOTH ENGINES. PERFORMED PSEU BITE CHECK, NO FAULTS NOTED. EICAS MESSAGE CLEARED, AND RETURNED ACFT FROM AIR MODE TO GROUND MODE IAW AMM 23-09-02.

ATA 4950

APU BLEED PRESSURE SURGING. PERFORMED A BITE TEST OF THE APU ECU. NO DEFECTS NOTED IAW AMM 49-61-05. PERFORMED AN OPS TEST OF THE APU. NO DEFECTS NOTED.

ATA 4950

APU SURGE BLEED DUCT TORN. REMOVED AND REPLACED THE DUCT IAW AMM 49-53-01, NO LEAKS DETECTED.

ATA 7510

LEFT ENGINE TAI VALVE STATUS MESSAGE. REMOVED & REPLACED THE ANTI ICE VALVE IAW AMM 30-20-08, OPS CHECKED NORMAL.

ATA 2121

AFT EQUIPMENT EXHAUST FAN NR 2 STATUS MESSAGE. OPS CHECKED IAW AMM 21-58-41 NO FAULTS NOTED , OK FOR SERVICE.

ATA 4900

APU BLEED PRESSURE SURGED. REMOVED AND REPLACED APU BATTERY CHARGER IAW FIM 49-11, FAULT TREE IAW AMM 24-31-04. OPS CHECKED GOOD.

ATA 2150

RT PACK OFF EICAS MESSAGE DURING CRUISE WHILE LEVELED OFF AT FL 40.0 PACK SWITCH DISPLAYED PACK OFF(<P>FOUND R/H PACK RAM EXHAUST DOOR ACTUATOR FAULTY. REMOVED AND REPLACED ACTUATOR IAW AMM 21-53-04 OPS CHECK GOOD</P>)

ATA 2150

R PACK OFF DURING CLIMB AND CRUISE.(<P>PERFORMED OPS CHECK OF PNUEMATICS IAW B767 AMM 36-00-00. NO DEFECTS NOTED. PERFORMED B767 FIM TASK 21-51 FAULT TREE 803, NO DEFECTS NOTED.</P>)

ATA 2150

R PACK OH EICAS MESSAGE DURING CRUISE WHILE LEVELED OFF AT FL 350.PACK SWITCH DESELECTED "PACK OFF". R & R THE CIRCUIT CARD IAW AMM 20-10-01 & 21--61-03.

ATA 3442

RADAR INOP, STATUS MSG WRX SYS AND C/B OPENED IN FLT ON OVERHEAD PANEL.(<P>PUSHED IN THE C/B PERFORMED OP'S CHECKS AT THE WX RADAR. OP'S CHECKED GOOD AT THIS TIME IAW AMM 34-43-00 AND C/B 20-60-01.</P>)

ATA 4940

APU FAILED PRIOR TO ENGINE START. REMOVED AND REPLACED INLET GUIDE VANE ACTUATOR PER AMM 49-52-02 NO HELP. REPLACED ECU PER FIM 49-11FT 815 NO HELP. REMOVED AND REPLACED APU PER AMM 49-52-02. OPS CHECK NORMAL.

ATA 2121

STATUS MSG AFT EQ EXH FAN 2(<DIV>T/SHOOTING REF FIM 21-26 TASK 806 CLEARED MESSAGE NO FURTHER FAULT NOTED OK FOR SERVICES&NBSP;</DIV>)

ATA 2150

RIGHT PACK CONDENSER LEAKING AT THE FWD LEFT BOTTOM CORNER. REMOVED AND REPLACED THE RT PACK HEAT CONDENSER IAW AMM 21-51-10. OPS CHECKED NORMAL.

ATA 4997

APU LEAD BURNED AND APU IGNITER PLUG WORN. REMOVED AND REPLACED APU IGNITER PLUG AND LEAD IAW AMM 49-41-04.

ATA 3442

WEATHER RADAR DISPLAY SHOWED A CONSTANT RED BAND FROM APPROXIMATELY 20-40 MILES IN ALL TILT, GAIN AND MODE SETTINGS ON BOTH L AND R SYSTEMS. PERFORMED WEATHER RADAR SYSTEM TEST. WEATHER RAD SYSTEM TEST PASSED IAW AMM 34-43-00.

ATA 4930

APU QUIT DURING PUSHBACK. APU WAS RESTARTED AND USED FOR 2 NORMAL ENGINE STARTS. REMOVED AND REPLACED THE APU FUEL CONTROL UNIT IAW 49-31-01. OPS CHECKED NORMAL.

ATA 2800

ON SHUT DOWN, THE RT SPAR VALVE DID NOT CLOSE, RT ENGINE SPAR VALVE INOPERATIVE. REMOVED AND REPLACED THE SPAR VALVE LIGHT SWITCH IAW WDM 28-22-21 OPS CHECKED OK.

ATA 2820

DURING START OF L ENGINE SPAR VALVE LIGHT DID NOT ILLUMINATE. PERFORMED OPS CHECK OF L ENGINE SPAR VALVE PER AMM 28-22-11. OPS CHECK GOOD.

ATA 3150

APU BATTERY DISCHARGE LIGHT INOPERATIVE. RESET CIRCUIT BREAKER U12. PERFORMED STANDBY POWER TEST IAW 24-33-00. APU BATTERY DISCHARGE LIGHT CAME ON AND APU DISCHARGE EICAS INDICATED. OPS CHECKED NORMAL.

ATA 3442

WHEN WEATHER RADAR WAS SELECTED, CPT SHOWS ONLY WX. FO SHOW WX & T, OPS CHECKED GOOD IAW AMM 34-43-00 BOTH SIDES SHOW WX & T.

ATA 4900

APU SHUTDOWN WHEN PACK SELECTED. REMOVED AND REPLACED APU SURGE VALVE IAW AMM 49-53-01. OPS CHECKED NORMAL.

ATA 2150

RIGHT PACK TEMP EICAS MESSAGE DURING CLIMB, PERFORMED QRH PRCEDURES, OPS CHECKED GOOD. REMOVED AND REPLACED RAM DOOR ACTUATOR IAW AMM 21-53-03-004. OPS CHECKED GOOD.

ATA 4920

DURING PREFLIGHT, THE APU QUIT, APU FAULT LIGHT ILLUMINATED, AND APU FAULT EICAS MESSAGE. OPS CHECKED GOOD IAW AMM 49-11-06.

ATA 2150

RIGHT PACK TEMP EICAS MESSAGE AND RT PACK INOPERATIVE LIGHT ILLUMINATED. PERFORMED QRH, OPS NORMAL. RT PACK TEMP CONTROLLER SHOWED NO FAULTS. PERFORMED AN OPS CHECK IAW AMM 21-51-00, SYSTEM OK FOR SERVICE. AFTER QRH PROCEDURES THE RT PACK OPERATED NORMAL.

ATA 4920

APU INOPERATIVE. PERFORMED BITE TEST OF ECU, FOUND REVERSE FLOW. PERFORMED TROUBLESHOOTING IAW FIM 49-11FT 994, NO FAULTS FOUND, APU OPERATIONAL TESTED OK.

ATA 2150

RIGHT PACK INOPERATIVE. REMOVED AND REPLACED THE RT PACK WATER EXTRACTOR IAW AMM 21-51-01, OPS TESTED NORMAL.

ATA 4900

CHECK VALVE WORN ON APU. REMOVED AND REPLACED APU CHECK VALVE IAW AMM 36-11-11. CHECK VALVE OPERATES AS DESIGNED.

ATA 7933

LEFT ENGINE OIL PRESSURE LIGHT NOT ILLUMINATED WITH LEFT ENGINE SHUT DOWN. : REMOVED AND REPLACED THE LT ENGINE LOW OIL PRESSURE SWITCH IAW AMM 79-33-01, LEAK CHECKED GOOD.

ATA 2820

LEFT ENGINE SPAR VALVE DID NOT ILLUMINATE ON ENGINE START. REMOVED AND REPLACED FUEL CONTROL MODULE. OPS CHECKED NORMAL IAW AMM 76-11-09.

ATA 2820

LEFT SPAR VALVE DOES NOT SHOW CORRECT POSITION. VISUALLY CHECKED SPAR VALVE, SPAR VALVE DOES WORK IAW 28-40-02. REPLACED LIGHT IAW AMM 33-13-00, SPAR VALVE, OPS NORMAL.

ATA 2800

RT ENGINE FUEL VALVE LIGHT INOPERATIVE. REPLACED THE FUEL VALVE SWITCH IAW AMM 33-13-00, OPS NORMAL.

ATA 4950

APU REVERSE FLOW SHUTDOWN. REMOVED AND REPLACED APU SURGE CONTROL VALVE IAW AMM 59-53-01. NO DEFECTS NOTED AT THIS TIME. OPS CHECKED GOOD.

ATA 7320

DURING SHUTDOWN, RT ENGINE FUEL VALVE FAILED TO CYCLE ON & OFF.

ATA 2150

RIGHT PACK OFF EICAS MESSAGE, THE RIGHT DUCT PRESSURE WAS AT 40-60 PSI , LEFT DUCT PRESSURE STABLE AT 30 PSI. REMOVED AND REPLACED RIGHT PACK TEMP CONTROLLER IAW AMM 21-51-13, OPS CHECKED GOOD.

ATA 2150

LEFT PACK INOPERATIVE IN AUTO. PERFORMED BITE ON LEFT PACK TEMPERATURE CONTROL. RAM AIR ACTUATOR FAULT. REMOVED AND REPLACED RAM AIR ACTUATOR IAW AMM 21-53-03-404 OPS TESTED NORMAL.

ATA 2150

LEFT PACK TRIPPED IN AUTO MODE.

ATA 2820

DURING LEFT ENGINE START THE SPAR VALVE LIGHT DID NOT ILLUMINATE. CYCLED FUEL VALVE AND PERFORMED OPERATIONAL CHECK OF SPAR VALVE IAW AMM 28-22-00. VALVE INDICATES NORMAL. ENGINE RUN PERFORMED BY FLIGHT CREW WITH NO DISCREPANCIES IAW AMM 71-00-00.

ATA 3610

LEFT PNEUMATIC DUCT PRESSURE FLUCTUATES BETWEEN 15-50 PSI RAPIDLY DURING CLIMB OUT. REMOVED AND REPLACED THE LT ENGINE PRSOV IAW AMM 36-11-09. OPS & LEAK CHECKED OK.

ATA 2130

CABIN RATE OF CLIMB INDICATOR FLUCTUATES . NO CHANGE IN CABIN PRESSURE. REMOVED AND REPLACED THE CONTROL PANEL ASSY IAW AMM 21-33-01. OPS CHECKED GOOD.

ATA 7500

LEFT BLEED PRESSURE OSCILLATES DURING CLIMB THRU 10000 FT, 15-50 PSI RANGE. STOPS AT 10000 FT BUT REMAINS LOUDER THAN RIGHT BLEED. NO BLEED SPLIT AT 410. PACK OPS NORMAL. NO EICAS STATUS. COMPLIED WITH FIM 36-10-01, FAULT TREE 803. INSPECTED BOX AND FOUND LEFT HIGH PRESSURE CONTROLLER FAULTED. INSPECTED VALVE AND FOUND A LOOSE LINE, TIGHTENED THE LINE AND PERFORMED A BITE. NO FAULTS INDICATED IAW FIM 36-10-01.

ATA 2752

CORRODED NR 3 TE FLAP ROTARY ACTUATOR ON LT TE FLAP. REMOVED AND REPLACED IAW 8017-TALLY 1113, AND ENGINEERING ORDER 6727A007_CS.

ATA 2752

CORRODED POSITION NR 4 TE FLAP ROTARY ACTUATOR ON LEFT TE FLAP. REMOVED AND REPLACED IAW 8017-TALLY 1113, AND ENGINEERING ORDER 6727A007_CS.

ATA 2752

CORRODED NR 5 TE FLAP ROTARY ACTUATOR ON RT TE FLAP. REMOVED AND REPLACED IAW 8017-TALLY 1113, AND ENGINEERING ORDER 6727A007_CS.

ATA 7712

LEFT ENGINE N2 INDICATION FOUND ERRATIC ON EICAS DISPLAY DURING ENGINE RUN. THE LT ENGINE N2 SENSOR WAS REMOVED AND REPLACED IAW AMM 77-12-02, REV 121.

ATA 4930

APU DRAINMAST, FOUND HOLDING BRACKET CRACKED AND LINE MISSING. THE BRACKET REPLACED AND DRAIN LINE WERE REPLACED IAW AMM 49-16-00, REV 121. LEAK CHECKED IAW AMM 49-11-00, REV 121. FOUND NO LEAKD FOUND.

ATA 7330

LEFT ENGINE FUEL PRESSURE SHOWS 200 PSI ON EICAS DISPLAY DURING ENGINE RUN. THE PRESSURE SWITCH WAS REMOVED AND REPLACED IAW AMM 73-33-01, REV 121. POWER PLANT TEST 2 IDLE LEAK CHECK CARRIED OUT IAW AMM 71-00-00, REV 121.

ATA 2752

FLIGHT CONTROLS, TRAILING EDGE FLAP SYSTEM , TE FLAP ROTARY ACTUATOR AND REACTION RING INSPECTION, REWORKED AND REPLACEED IAW SB 767-27A0229 R1, AND AD 2014-22-09

ATA 5710

RIGHT OVERWING REFUELING PORT ACCESS CUTOUT FOUND CORRODED. REPAIRED IAW EN 1098-17 REV .

ATA 2120

RIGHT AIR CONDITIONING BAY AFT ISOLATION BYPASS CHECK VALVE MOUNTING CLAMP FOUND LEAKING. THE CLAMP WAS REMOVED, REPLACED AND LEAK CHECKED IAW AMM 36-11-05, REV 121. FOUND SATISFACTORY.

ATA 2120

LEFT AIR CONDITIONING BAY LT TRIM AIR CHECK VALVE MOUNTING CLAMP FOUND LEAKING. THE CHECK VALVE MOUNTING CLAMP WAS REMOVED AND REPLACED IAW AMM 21-61-05, REV 121, AND LEAK CHECKED IAW AMM 21-61-05, REV 121. FOUND SATISFACTORY.

ATA 2820

NR 2 PYLON TOP FRONT SPAR FUEL LINE FOUND DENTED. THE FUEL LINE WAS REMOVED AND REPLACED IAW AMM 28-22-07, REV 120, BONDING RESISTANCE TEST CARRIED OUT IAW AMM28-22-07, REV 120. FOUND GOOD, LEAK CHECKED IAW AMM 28-22-07, REV 121. FOUND NO LEAKAGE.

ATA 2160

RIGHT AIR CONDITIONING TRIM AIR SUPPLY CHECK VALVE FOUND FLAPPER LOOSE AND INTERNAL HOUSING WITH CHAFED. THE CHECK VALVE WAS REMOVED, REPLACED AND LEAK CHECKED IAW AMM 21-61-05, REV 121. FOUND SATISFACTORY.

ATA 5420

NR 1 ENGINE, RT CORE COWL HOLD OPEN ROD BRACKET FOUND LOOSE. THE BRACKET WAS REMOVED AND REPLACED IAW AMM 70-50-00, REV 121.

ATA 5420

NR 2 ENGINE, RT CORE COWL HOLD OPEN ROD, ROD END FOUND WORN. THE ROD END WAS REMOVED AND REPLACED IAW AMM 70-50-00, REV 120.

ATA 2160

LEFT AIR CONDITIONING TRIM AIR SUPPLY, CHECK VALVE FOUND FLAPPER LOOSE AND INTERNAL HOUSING CHAFED. THE CHECK VALVE WAS REMOVED, REPLACED AND LEAK CHECKED IAW AMM 21-61-05, REV 121. FOUND SATISFACTORY.

ATA 3610

LEFT PNEUMATIC CROSSOVER DUCT ISOLATION BYPASS CHECK VALVE FOUND FLAPPER LOOSE AND INTERNAL HOUSING WITH A CHAFE. THE CROSSOVER DUCT ISOLATION BYPASS CHECK VALVE WAS REMOVED, REPLACED, AND TESTED IAW AMM 36-11-05, REV 121. FOUND SATISFACTORY.

ATA 4990

APU LUBE FILTER ASSEMBLY, DIFFERENTIAL PRESSURE INDICATOR FOUND POPPED OUT. REPLACED IAW AMM 49-27-03, REV 121.

ATA 2150

LEFT PACK COMPRESSOR OUTLET TEMP INDICATION INVALID. LT PACK COMPRESSOR OUT TEMP SENSOR REMOVED & REPLACED IAW AMM 21-52-01, REV 121. FOUND SATISFACTORY.

ATA 2150

RIGHT PACK COMPRESSOR OUTLET TEMP INDICATION INVALID. RT PACK COMPRESSOR OUTLET TEMP SENOR REMOVED & REPLACED IAW AMM 21-52-01, REV 121. FOUND SATISFACTORY.

ATA 2752

FLIGHT CONTROLS, TRAILING EDGE FLAP SYSTEM, TE FLAP NR 6 ROTARY ACTUATOR CORRODED. REMOVED AND REPLACED IAW 8017-TALLY 1113, ENGINEERING ORDER 6727A007_CS.

ATA 2150

LEFT PACK PRIMARY TEMP INDICATION INVALID. LEFT PACK TEMP SENSOR REMOVED & REPLACED IAW AMM 21-52-08, REV 121. FOUND SATISFACTORY.

ATA 2140

FWD CARGO HEAT INOPERATIVE. FWD CARGO HEAT SHUTOFF VALVE REMOVED AND REPLACED IAW AMM 21-43-01, REV 121. OPS TEST PERFORMED IAW AMM 21-43-01, REV 121, FOUND SATISFACTORY.

ATA 5320

MID CABIN-LOWER STRAPS COMMON TO SATCOM, INTERCOSTAL FOUND CORRODED AT BS 977 TO 1043, STRINGER 1L TO 1R. REMOVED, FABRICATED, AND INSTALLED IAW EO 6753A451.

ATA 4940

APU FAILED TO START. APU EXCITER REMOVED AND REPLACED IAW AMM 49-41-03, REV 121. APU CONTROL UNIT BITE TEST AND APU STARTING AND OPERATION CARRIED OUT IAW AMM 49-61-05 AND & AMM 49-11-00, REV 121. FOUND SATISFACTORY.

ATA 5414

NR 2 ENGINE, LT CORE COWL FAIRING SKIN INTERIOR AREA FOUND WORN LOCATED AT UPPER AFT CUT-OUT. THE FAIRING SKIN WAS REPAIRED IAW SRM 54-45-01-2R-11, REPAIR 11, REV 103.

ATA 5411

NR 2 ENGINE, LT CORE COWL UPPER AFT LONGERON FOUND CRACKED. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5410

NR 2 ENGINE, LT CORE COWL UPPER AFT SPRING SEAL FOUND CRACKED. THE SPRING SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5420

NR 1 ENGINE, LT CORE COWL HOLD OPEN ROD STOW BRACKET AND ADAPTER FOUND WORN. THE BRACKET AND ADAPTER WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.

ATA 5410

NR 1 ENGINE, RT CORE COWL RELIEF DOOR FOUND TWO STRIKER PLATES WORN. THE STRIKER PLATES WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5410

NR 1 ENGINE, LT CORE COWL EXTERIOR UPPER FWD AREA FOUND RIVET LOOSE. THE RIVETS WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5420

NR 1 ENGINE, LT CORE COWL INTERIOR AFT UPPER RUB STRIP FOUND WORN. THE RUB STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5420

NR 2 ENGINE, LT CORE COWL UPPER AFT RUBSTRIP FOUND WORN. THE RUBSTRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5410

NR 2 ENGINE, RT CORE COWL PRESSURE RELIEF DOOR FOUND TWO STRIKER PLATES WORN. THE STRIKER PLATES WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5410

NR 1 ENGINE, LT CORE COWL FLIPPER DOOR SEAL FOUND WORN. THE DOOR SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5410

NR 1 ENGINE, LT CORE COWL INTERIOR AFT UPPER AREA ANGLE FOUND CRACKED. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5420

NR 2 ENGINE, LT CORE COWL HOLD OPEN ROD STOW BRACKET AND ADPATER FOUND WORN. THE BRACKETS AND ADAPTER WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5410

NR 1 ENGINE, LT CORE COWL FWD UPPER SEAL FOUND WORN. SEAL REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5410

NR 2 ENGINE RT CORE COWL UPPER AFT AREA FOUND RUB STRIP WITH LOOSE RIVET. THE RUB STRIP RIVETS REPLACED IAW SRM 51-40-02, REV 104.

ATA 3610

NR 2 ENGINE RT CORE COWL PRECOOLER EXIT DUCT FOUND RIVET LOOSE. DUCT RIVET REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5400

NR 2 ENGINE RT CORE COWL UPPER SUPPORT PLATE FOUND RIVET LOOSE. SUPPORT PLATE REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5414

NR 1 ENGINE LT CORE COWL EXTERIOR SKIN FOUND SCRATCHED. SCRATCHES BLENDED OUT AND FOUND WITHIN LIMIT IAW SRM 54-42-01-1A-1, FIG 101, NOTE B, DETAIL III, REV 104.

ATA 5410

NR 2 ENGINE LT CORE COWL INTERIOR AREA 5TH AND 6TH SUPPORT FRAME, SUPPORT PLATE FOUND WORN. THE SUPPORT PLATE WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5320

BS 933, STRINGER 18L FOUND INTERCOSTAL CORRODED. CORROSION BLENDED OUT AND FOUND OUT OF LIMITS IAW SRM 53-00-04-1A-1, FIG 101, ALLOWABLE DAMAGE 1, REV 104. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5311

BS 1329 FRAME FOUND CORRODED BETWEEN STRINGER 19 - 20R, RBL 90, WL 205. BLENDED OUT AND FOUND OUT OF LIMITS IAW SRM 53-00-07-1A-1, FIG 101, ALLOWABLE DAMAGE 1, REV 104. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-02, REV 104.

ATA 5410

NR 1 ENGINE RT CORE COWL LOWER AFT HAT FRAME FOUND CHAFED. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5410

NR 1 ENGINE LT CORE COWL FWD UPPER BRACKET FOUND WORN. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 2750

LEFT WING INBD FLAP TORQUE TUBE AT BETWEEN IFS 92 - 124.5, FOUND TO HAVE LIGHT WEAR. REWORK CARRIED OUT IAW SB 767-57A0066, FIG 9, REV 4 IAW EO 6757A038, REV 3.

ATA 5410

NR 2 ENGINE LT CORE COWL HOLD OPEN ROD , ROD END FOUND LOOSE. THE ROD END WAS REMOVED AND REPLACED IAW AMM 70-50-00, REV 120.

ATA 5420

NR 2 ENGINE RT CORE COWL HOLD OPEN ROD, BRACKET FOUND WORN. THE BRACKET WAS REMOVED AND REPLACED IAW AMM 70-50-00, REV 120.

ATA 5410

NR 1 ENGINE LT CORE COWL HOLD OPEN ROD, ROD END FOUND LOOSE. THE ROD END WAS REMOVED AND REPLACED IAW SRM 70-50-00, REV 120.

ATA 5410

NR 1 ENGINE RT CORE COWL HOLD OPEN ROD, ROD END FOUND WORN. THE ROD END WAS REMOVED AND REPLACED IAW AMM 70-50-00, REV 120.

ATA 5410

NR 2 ENGINE LT CORE COWL UPPER AFT RUB STRIP FOUND CRACKED. THE RUB STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5410

NR 1 ENGINE L/H CORE COWL EXTERIOR FWD RUB STRIP FOUND WORN. THE RUB STRIPS WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5410

NR 2 ENGINE L/H CORE COWL EXTERIOR AREA RUB STRIP FOUND WORN. THE RUB STRIPS WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5410

NR 1 ENGINE RT CORE COWL EXTERIOR AREA RUB STRIP FOUND WORN. THE RUB STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5411

NR 1 ENGINE LT CORE COWL AFT HAT FRAME FOUND EXISTING REPAIRS WORN. THE HAT FRAME REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5311

AFT CARGO BAY, BS 1197+22, BL 0 - RBL 11 FRAME FOUND DEFORMED. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-02, REV 104.

ATA 5230

BULK CARGO DOOR INTERNAL FRAME LOWER, MID SECTION FOUND WORN. A NEW LOWER FRAME WAS FABRICATED IAW DRAWING 146T6322, SHEET 1, REV A, THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 7110

NR 1 ENGINE RT CORE COWL UPPER SUPPORT PLATE FOUND RIVET LOOSE AS MARKED. NR 1 ENG RT CORE COWL UPPER SUPPORT PLATE ATTACH LOOSE RIVET REMOVED AND REPLACED AS PER SRM 51-40-02, REV 103.

ATA 7110

NR 1 ENGINE RT CORE COWL HOLD OPEN ROD STOW ADAPTER FOUND WORN AS MARKED. NR 1 ENGINE RT CORE COWL HOLD OPEN ROD STOW ADAPTER REMOVED AND REPLACED IAW AMM 70-50-00, REV 120.

ATA 4950

APU COOLING DUCT BELLOWS AFT OF COOLING FAN FOUND DETERIORATED. APU COOLING DUCT BELLOWS AFT OF COOLING FAN REMOVED AND REPLACED AS PER AMM 49-51-01, REV 120.

ATA 5753

RT INBOARD AFT FLAP UPPER SURFACE TRAILING EDGE. FOUND GOUGE ON UPPER SURFACE AS INDICATED. RT INBOARD AFT FLAP UPPER SURFACE TRAILING EDGE REPAIRED AS PER SRM 51-70-10 REV 104.

ATA 2750

RT I/B FLAP, TORQUE TUBE AT IFS 92 - IFS 124.5 FOUND LIGHT WEAR AS MARKED. LIGHT WEAR REWORK CARRIED OUT AS PER SB 767-57A0066, FIG 9, REV 4 IN ACCORDANCE WITH EO 6757A038, REV 3.

ATA 7110

NR 2 ENGINE RT CORE COWL FWD UPPER EXTERIOR AREA WEAR STRIP FOUND WORN AS MARKED. NR 2 ENG RT CORE COWL REMOVED AND REPLACED AS PER AMM 71-11-06, REV 121.

ATA 7110

NR 2 ENGINE RT CORE COWL FLIPPER DOOR FOUND SEAL CRACK AS MARKED. NR 2 ENG RT CORE COWL REMOVED AND REPLACED AS PER AMM 71-11-06, REV 121.

ATA 7110

NR 2 ENGINE RT CORE COWL SKIN FOUND CRACK LOCATED AT AFT UPPER CUTOUT AREA AS MARKED. NR 2 ENG RT CORE COWL REMOVED AND REPLACED AS PER AMM 71-11-06, REV 121. REFER TO NRC 0688 FOR CORE COWL REPLACEMENT DETAILS.

ATA 7110

NR 2 ENGINE RT CORE COWL PRECOOLER EXIT DUCT LIP FOUND WORN AS MARKED. NR 2 ENG RT CORE COWL REMOVED AND REPLACED AS PER AMM 71-11-06, REV 121.

ATA 7110

NR 1 ENGINE LT CORE COWL 2ND ZEE FRAME COUNT FROM FWD FOUND EXISTING REPAIR WORN AS MARKED. NR 1 ENG LT CORE COWL 2ND FROM FWD DAMAGED ZEE FRAME REMOVED AND REPLACED AS PER SRM 51-40-02, REV 104.

ATA 5730

LT OVERWING REFUELING PORT ACCESS CUTOUT FOUND CORROSION. LT OVERWING CORROSION AROUND FUEL FILL PORT WAS LOCALLY BLENDED TO CREATE TWO FLAT SURFACE WITH CONSTANT THICKNESS OF 0.210" AND 0.250" TO ALLOW FLAT SEATING OF TWO CUSTOM FILLERS. THE MIN THK WAS 0.207". EXTERNAL REPAIR DOUBLER INSTALLED AS PER EN1089-17, REV-.

ATA 7110

NR 2 ENGINE RT CORE COWL HOLD OPEN ROD SUPPORT BRACKET AT BASE SIDE FOUND WORN AS MARKED. NR 2 ENG RT CORE COWL REMOVED AND REPLACED AS PER AMM 71-11-06, REV 121.

ATA 7110

NR 2 ENGINE RT CORE COWL HOLD OPEN ROD STOW PIN BRACKET AND ADAPTER FOUND WORN AS MARKED. NR 2 ENG RT CORE COWL REMOVED AND REPLACED AS PER AMM 71-11-06, REV 121.

ATA 7110

NR 1 ENGINE RT CORE COWL EXTERIOR AREA PRECOOLER EXIT DUCT CUT-OUT AREA FOUND CRACK AS MARKED. NR 1 ENG RT CORE COWL SKIN PRECOOLER EXIT DUCT ASSY CUT-OUT BELOW NAC STA.281.12 LOWER SECTION CRACK AREA. EXTERNAL PATCH REPAIR CARRIED OUT AS PER SRM 54-42-01-2R-3, REPAIR 3, REV 104.

ATA 4910

APU AIR INTAKE ACTUATOR FOUND 02EA BONDING FRAYED. ITEM REPLACED IAW AMM 49-15-06 REV 121.

ATA 2750

CORRODED NR 2 TE FLAP REACTION RING ON THE LT TE FLAP. REMOVED AND REPLACED IAW 8017-TALLY 1113, AND ENGINEERING ORDER 6727A007_CS.

ATA 2750

CORRODED NR 4 TE FLAP REACTION RING ON THE LT TE FLAP. REMOVED AND REPLACED IAW 8017-TALLY 1113, AND ENGINEERING ORDER 6727A007_CS.

ATA 2750

CORRODED POSITION NR 5 TE FLAP REACTION RING ON THE RT TE FLAP. REMOVED AND REPLACED IAW 8017-TALLY 1113, AND ENGINEERING ORDER 6727A007_CS.

ATA 2750

CORRODED POSITION NR 6 TE FLAP REACTION RING ON THE RT TE FLAP. REMOVED AND REPLACED IAW 8017-TALLY 1113, AND ENGINEERING ORDER 6727A007_CS.

ATA 2750

CORRODED POSITION NR 7 TE FLAP REACTION RING ON RT TE FLAP. REMOVED AND REPLACED IAW 8017-TALLY 1113, AND ENGINEERING ORDER 6727A007_CS.

ATA 2752

CORRODED NR 2 TE FLAP ROTARY ACTUATOR ON LT TE FLAP. REMOVED AND REPLACED IAW 8017-TALLY 1113, AND ENGINEERING ORDER 6727A007_CS.

ATA 4990

APU LEAKING OIL FROM OIL FILL CAP. REMOVED AND REPLACE OIL FILLER CAP O-RING IAW AMM 79-11-03. NO OTHER LEAKS FOUND.