N1997A

Part: CONTROLLER — FAULTED (FIRE DETECTION) · airframe 107,872 hrs · 23,636 cycles

ON APPROACH, RECEIVED WHEEL WELL FIRE EICAS MESSAGE. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. INSPECTED AND FOUND NO EVIDENCE OF FIRE. REPLACED DETECTION CONTROL CARD.

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 107,578 hrs · 23,475 cycles

DURING SERVICE CHECK, L1 DOOR EMERGENCY LIGHT FAILED TO ILLUMINATE. REPLACED BATTERY ASSEMBLY.

Part: PSEU — MALFUNCTIONED (FLAP SYS) · airframe 107,041 hrs · 23,204 cycles

AS FLAPS MOVED FROM 1 TO UP ON CLIMB OUT; FLAP (RED). EICAS STATUS MSG: NOSE A/G DISAGREE ALSO F/O HAD SPEED LIM ON HIS SPEED TAPE(<P>TROUBLESHOT &AMP; FOUND PSEU CARD MSG 002 AND TARGET MSG 266, TARGET MSG 266, FOUND RH MSG 002, SENSOR HARNESS 266, R/R PER AMM 32-09-08/201. CARD MSG 002, PSEU REMOVED AND REPLACED PER AMM 32-09-04-201. LANDING GEAR SWING PERFORMED PER AMM 32-32-001/S01, OPERATIONAL CHECK SATISFACTORY. NO MESSAGE NOTED.</P>)

Part: WEDGE — DAMAGED (NR 8 SLAT) · airframe 107,041 hrs · 23,204 cycles

8028 - EA-1957A155 PART(3) REV(0) WINGS - LEADING EDGE DEVICES - RH WING #8 LEADING EDGE SLAT (PN 114T4105-58 /SN 000598) TRAILING EDGE WEDGE EXISTING REPAIR DELAMINATION - TIME LIMITED REPAIR(<P>PERMANENT REPAIR WAS PERFORMED IAW EA 1957A155. NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — SCRATCHED (ZONE) · airframe 107,041 hrs · 23,204 cycles

TRAFFIC ALERT &AMP; COLLISION AVOIDANCE SYS HEALTH CHECK, ON TCAS UPPER ANTENNA WITH SCRATCHES ON FUSELAGE SKIN(<P>THE TCAS UPPER ANTENNA DOUBLER WAS BLEND OUT AND INSPECTION WERE PERFORMED IAW TRE 6753708. NO FURTHER DEFECTS NOTED.</P>)

Part: BEAR STRAP — CRACKED (ZONE 200) · airframe 107,041 hrs · 23,204 cycles

LH FWD DOOR, AFT LOWER CORNER WITH CRACK INDICATION AT SECOND LOWER HOLE ON BEAR STRAP APPROX. 10 O'CLOCK.(<P>CRACK WAS REPAIRED IAW EA 6753A937. NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — DEBONDED (ZONE 600 AILERON) · airframe 107,041 hrs · 23,204 cycles

RH WING, INBOARD AILERON, LEADING EDGE DISBONDED BTW RIB 1 AND 2.(<P>RH WING, INBOARD AILERON, L/E BETWEEN RIB 1 AND 2 WAS REPAIRED AS PER B767-300 SRM 57-60-01-2R-1 FIG. 201, SHEET 4, PAG. 1-10 AND B767-300 SRM 51-70-17-0G-0 PAR. 4G, FIG. 15, PAG. 16, 17,42. REV. 126 15 AUG 2024. SN: 000552 &AMP; PN: 113T6100-8A. NO FURTHER DEFECTS NOTED</P>)

Part: WEB — CORRODED (ZONE 100) · airframe 107,041 hrs · 23,204 cycles

AFT CARGO, BTW STA 1263 AND DOOR FRAME, BTW STRG 32R AND 32R, CORROSION ON WEB.(<P>CLIP P/N 146T8081-13 SMALL AUTHORIZATION IAW CONSECUTIVE NUMBER M675498 &AMP; SRM 51-40-02-0G-0. NO FURTHER DEFECTS NOTED.CORROSION REMOVED</P>)

Part: BEARING — COKED (NR 1 ENGINE) · airframe 107,041 hrs · 23,204 cycles

ENGINE 1, BEARING #5, LH/RH SUMP PIPES WITH LEAK EVIDENCE.(<P>DURING VISUAL EXAMINATION, OIL COKE BUILD-UP WAS FOUND, COKING WAS REMOVED AND NO OIL LEAK WAS FOUND IN LH/RH SUMP PIPES IAW AMM SUBTASK 72- 50-00-216-032-H00 REV. 143 DATE: 22 AUG 2024. C/W IDLE LEAK CHECK TEST TRANSFER TO 8007 ITEM NUMBER 34. NO FURTHER DEFECTS NOTED</P>)

Part: SKATE ANGLE — CRACKED (ZONE 400) · airframe 107,041 hrs · 23,204 cycles

CRACK ON LH SKATE ANGLE ON STRUT #2 (FOUND DURING SEALANT REMOVAL)(<P>A SEGMENT OF THE SKATE WITH CRACK WAS REMOVED, AND THE NEW SEGMENT WAS MANUFACTURED AND INSTALLED IAW FVCI CONTROL EO 24190-2. NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — CRACKED (ZONE 800) · airframe 107,041 hrs · 23,204 cycles

RH FWD DOOR, AFT LOWER CORNER WITH CRACK INDICATION AT THIRD HOLE ON SKIN APPROX 1 O'CLOCK, AND VISUAL CRACK (CONFIRMED WITH HFEC) AT FOURTH HOLE ON SKIN AND BEAR STRAP APPROX. 2 O'CLOCK AND CONTINUE TO APPROX 7 O'CLOCK.<BR>(<P>&NBSP;IT WAS REPAIRED IAW EA 6753A937 REV: 1 DATE: 17MAY24. NO FURTHER DEFECTS NOTED</P>)

Part: FRAME — CORRODED (ZONE 100) · airframe 107,041 hrs · 23,204 cycles

BULK CARGO COMPARTMENT AT STA 1480 BTW STGR 31R-32R FRAME WITH CORROSION(<P>FRAME WAS MANUFACTURED AND REPLACED WITH THE NEW ONE. NO FURTHER DEFECTS NOTED</P>)

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 107,041 hrs · 23,204 cycles

FRAME AT STA 1480 BETWEEN STGR 27R / 29R WITH CORROSION (BULK CARGO COMPARTMENT AREA)(<P>FRAME N/P 146T1519-3 WAS MANUFACTURED IN ACCORDANCE SMAL AUTHORIZATION BY BOEING MESSAGE CMA-TLS-24-0222-01B (MXA ENGINEERING TASK CARD M6753499 ISSUED DATE NOVEMBER 19, 2024). THE FRAME WAS REPLACED IAW SRM 51-40-02-0G-0 REV 126 15AUG24 AND SRM 51-10-02-0G-0 REV 126 15AUG24. NO FURTHER DEFECTS NOTED</P>)

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 107,041 hrs · 23,204 cycles

BULK CARGO COMPARTMENT, STA 1480 BTW STGR 28R-29R FRAME WITH CORROSION(<P>SHEAR TIE WAS REPLACED IAW DWG 146T1519. NO FURTHER DEFECTS NOTED</P>)

Part: SPLICE — CORRODED (ZONE 100) · airframe 107,041 hrs · 23,204 cycles

BULK CARGO COMPARTMENT AT STA 1502 BTW STGR 31R-32R SPLICE WITH CORROSION.(<P>A NEW SPLICE WEB WAS MANUFACTURED AND INSTALLED IAW SRM 51-10-02-0G-0. NO FURTHER DEFECTS NOTED.</P>)

Part: SUPPORT BEAM — CORRODED (ZONE 100) · airframe 107,041 hrs · 23,204 cycles

BULK CARGO DOOR, INTERNAL STRUCTURE, CORROSION BTW BEAMS 2 AND 4.(<P>THE AREA WAS CLEANED, NEW SUPPORT WAS DRILLED, SUPPORT BEAM WAS INSTALLED. THE BEAM SUPPORT WAS REPLACED IAW SRM 51-10-02-0G-0. NO FURTHER DEFECTS NOTED</P>)

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 107,041 hrs · 23,204 cycles

BULK CARGO, FLOOR LEVEL AT FRAME 1540, SHEAR TIE WITH CORROSION BTW STRG 39R AND 38R.(<P>THE SHEAR TIE WITH CORROSION WAS REMOVED. THE AREA WAS CLEANED. THE NEW SHEAR TIE WAS DRILLED AND INSTALLED CORRECTLY IAW SRM 51-40-02-0G-0. NO FURTHER DEFECTS NOTED</P>)

Part: LIGHT — BROKEN (CABIN) · airframe 106,417 hrs · 22,925 cycles

EMERGENCY EXIT LIGHT BY L1 BOOR BROKEN(<P>RESECURED EMERGRNCY EXIT SIGN LENSE IAW 33-51-01. NO FURTHER DEFECTS NOTED</P>)

Part: HOSE — UNKNOWN (UNKNOWN) · airframe 104,591 hrs · 22,296 cycles

O2 DISCHARGED COMPLETELY THROUGH FO'S REGULATOR IN MASSIVE AND SUDDEN LEAK(<P>FOUND FO'S OXYGEN MASK BOX CONNECTION HOSE BLOWN OFF AND MASSIVELY LEAKING. REMOVED AND REPLACED CONNECTION HOSE ASSY IAW AMM 20-11-00, OPS AND LEAK CHECHED GOOD IAW AMM 35-11-00.&NBSP;</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 103,933 hrs · 22,049 cycles

FWD E/E CREW OXYGEN NEED SERVICE TO FULL.(<P>SERVICED FWD E&AMP;E CREW OXYGEN AS PER B767 AMM CH 12-15-08, AC 43.18-1B PAR 9-46 THRU&NBSP;9-51 PGS 9-448 THRU&NBSP; 9-455. OPS CHECK GOOD. NO LEAKS FOUND.</P> / <P>PN: 801307-00 SN ST298851 DUE DATE 31 JUL 25 MFG DATE 31 JAN 14</P>)

Part: CONTROLLER — UNKNOWN (UNKNOWN) · airframe 103,933 hrs · 22,049 cycles

CABIN COMPT TEMP CONTROL SYS INOP.(<P>R/R CABIN COMPT TEMP CONTROLLER M195 &AMP; ZONE TEMP CONTR. 1 SYS. OPS TEST GOOD PER AMM 21-61-03. MDDR 182947 CLEARED UP</P>)

Part: LEAD — UNKNOWN (UNKNOWN) · airframe 103,933 hrs · 22,049 cycles

ENG #1 LOWER HIGH TENSION LEAD DAMAGED.(<P>REMOVED &AMP; REPLACED ENG #1 LOWER HIGH TENSION LEAD IAW 767-300 AMM 74-21-02. PERFORMED AUDIBLE TEST FOR ENG #1, AUDIBLE TEST OK IAW AMM 74-00-00</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 103,933 hrs · 22,049 cycles

ECM 2023P-168 N1997A ENG #1 ESN #702928 IS EXPERIENCING HIGH FAN VIBRATION. A TRIM BALANCE IS REQUIRED TSLV 10,240 CSLV 3,348.(<P>PERFORMED LH ENG RUN UP PER AMM 71-00-00. INCREASED N2 POWER TO 99% &AMP; FAN VIB DID NOT EXCEED 0.9. NO DISCREPANCY NOTED. OPS CHECK GOOD.&NBSP;</P>)

Part: PIMU — UNKNOWN (UNKNOWN) · airframe 103,933 hrs · 22,049 cycles

RH PIMU FAULT MESSAGE.(<P>R/R RH PIMU &AMP; OPS CHECK OK PER AMM 77-35-02.</P>)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 103,316 hrs · 21,850 cycles

EMERGENCY LIGHT AT L1 DOOR INOPERATIVE. REPLACED THE LAMPS, OPS CHECKED NORMAL IAW AMM 33-51-00.

Part: PCA — LEAKING · airframe 102,413 hrs

WITH LEFT AND CENTER HYD SYS DEPRESSURIZED LEFT INBOARD AILERON FLOATS UP DURING LEVEL FLIGHT RESULTING IN HARD LEFT ROLL. FOUND LEFT INBOARD AILERON INBOARD & OUTBOARD PCA'S LEAKING AT SCRAPPER SEALS. REMOVED AND REPLACED O/B PCA IAW B767 AMM 27-11-48. STEPS K1-M5 NEED C/W. REF LP 1506539, ITEM 17 FOR OPS/LEAK CHECK. LOGPAGE 1506539, ITEM 17: PERFORMED OPS, LEAKS AND RIG CHECKS OF THE L/H I/B AILERON IAW B767-300 AMM 27-11-48. ALL CHECKS GOOD.

Part: PCA — ERRATIC · airframe 102,413 hrs

AIRPLANE WAS HAVING PROBLEMS MAINTAINING VNAV PTH ON THE ARRIVAL ROUTE. AFTER DISCONNECTING AUTOPILOT I FELT HEAVY RESISTANCE WITH AILERON FLIGHT CONTROLS. BOTH LEFT AND RIGHT AILERON INPUT AT AIRSPEEDS ABOVE 200 KTS. AILERON TRIM SHOWED ZERO WITH LEVEL CONTROL YOKE. VERY HEAVY RESISTANCE. PERFORMED AILERON RESPONSE TEST IAW AMM 27-11-00, NO FAULTS NOTED, OPS CHECK GOOD, NO HEAVY RESISTANCE FOUND. PERFORMED TEST 30 40 IAW 22-00-02 NO FAULTS NOTED, OPS CHECK GOOD, PERFORMED GVI OF LEFT & RIGHT AILERON CONTROL CABLES IAW AMM 20-20-02. NO DEFECTS NOTED. PERF AIL TENSION CHECK IAW AMM 27-11-00-835-429, ALL LOCATIONS WITHING LIMITS. INSPECTED AILERON FEEL, CENTERING AND TRIM MECHANISM PER FIM 27-11 FT 808, NO FINDINGS, SYS OK. PER AMM 27-11-00 PAR 3(M) INSP PCA'S, NO ABNORMAL TEMP WHEN COMPARED TO OTHER PCA. PERF FIM 27-09 FT 807, SYS NORMAL NO DEFECTS AT THIS TIME.</P>)

Part: TRANSDUCER — NONE · airframe 102,178 hrs · 21,482 cycles

SUPERNUMERARY O2 INDICATION IS ERRATIC(<P>TRANSFERRED TO MMDR 164289 IAW MEL 35-11-03-02A, CAT C.</P> / <P>LOGPAGE 1504123 - ITEM #4: REMOVED AND REPLACED PAX O2 TRANSDUCER PER AMM 35-11-04. THIS CLEARS MDDR 164289.</P>)

Part: FITTING — NONE · corrosion level 2 · airframe 102,148 hrs · 21,474 cycles

CORROSION IN THE AFT CARGO COMPARTMENT HORIZONTAL ATTACH FITTING BETWEEN STR,23L AND STR.24L JUST AFT OF THE BS.1065 BULKHEAD(<P>REMOVED AND REPLACED THE LH HORIZ. FITTING AT STA 1065-1109 STR. 23L-24L IAW B767 SRM 51-40-02. (CORROSION LEVEL 2)</P>)

Part: BOTTLE — LOW PRESSURE · airframe 102,165 hrs

CREW O2 LOW AT DEPARTURE CREW O2 READ 1600 ON ARRIVAL 1220(<P>REMOVED AND REPLACED CREW O2 BOTTLE IAW AMM 12-15-08 &AMP; LEAKED CHECKED OKAY PER GMM 3.25.3. NO DEFECTS NOTED AT THIS TIME .&NBSP;</P>)

Part: NONE — NONE · corrosion level 2 · airframe 102,148 hrs · 21,474 cycles

CORROSION AROUND FASTENER HOLE AND UNDER ROLLER TRAY IN THE AFT CARGO COMPARTMENT FLOOR BEAM UPPER CHORD LOWER SURFACE BS.1241 LBL.43.(<P>REMOVED, FABRICATED NEW, AND INSTALLED NEW&NBSP;<SPAN>AFT CARGO COMPARTMENT FLOOR BEAM UPPER CHORD AT STA 1241 IAW B767 SRM 53-00-07, 51-40-02, 51-40-05, AND DWG:</SPAN><SPAN>146T1208 REV: E</SPAN></P>)

Part: NONE — NONE · corrosion level 2 · airframe 102,148 hrs · 21,474 cycles

CORROSION IN THE AFT CARGO COMPARTMENT HORIZONTAL ATTACH FITTING BETWEEN STR,23R AND STR.24R JUST AFT OF THE BS.1065 BULKHEAD. DOT 129-097(<P><SPAN>REMOVED AND REPLACE THE RH HORIZ. FITTING, 2EA. ATTACH BRACKETS AND 1 EA. WEB AT STA. 1065-1109 STR. 23R-24R IAW B767 SRM 51-40-02</SPAN></P>)

Part: NONE — NONE · corrosion level 2 · airframe 10,215 hrs · 21,474 cycles

RH WING UPPER SIDE BODY SPLICE CENTER WING WBL.95 BTWN. 1, 2 STRINGERS U 10, U7 SKIN FOUND CORRODED AREA DOT 11/ 0013(<P>REMOVED CORROSION FROM RH WING UPPER SIDE BODY SPLICE CENTER WING WBL.95 BTWN. 1, 2 STRINGERS U 10, U7 SKIN. ORIGINAL MATERIAL .200" REMAINING MATERIAL .156" MATERIAL LOSS .044" FOUND TO BE OUT OF LIMITS IAW B767 SRM 57-20-01. REPAIRED AREA IAW EA 22005 REV:IR. (CORROSION LEVEL 2)</P>)

Part: FITTING — NONE · airframe 102,148 hrs · 21,474 cycles

RH PYLON OB SIDE AFT STA 280 APPROX LWR FITTING CRACKED AT LWR END.(<P>REMOVED AND REPLACED&NBSP;<SPAN>RH PYLON OB SIDE AFT LWR FITTING&NBSP;</SPAN><SPAN>STA 280 IAW B767 SRM 51-40-02, 51-40-05.</SPAN></P>)

Part: NONE — NONE · airframe 101,869 hrs

GEAR DISAGREE EICAS AFTER SELECTING GEAR DOWN. RAN QRH PROCEDURES(<P>ON WALK AROUND FOUND TAIL SKID RETRACTED. PERFORMED FIM 32-30 FT 305. ON PSEU BITE TEST FOUND MSG '248' TAIL SKID RETRACT. PERFORMED TAIL SKID EXTEND OPS TEST PER AMM 32-71-00-715-001 OPS GOOD. STATUS MSG CLEARED. ALSO PERFORMED TAIL SKID INSPECTION PER AMM 05-51-32-202-038. NO DAMAGE FOUND AT THIS TIME</P>)

Part: SWITCH — NONE · airframe 101,761 hrs · 21,357 cycles

EMERGENCY LIGHT KORRY SWITCH INOP(<P>REMOVED AND REPLACED EMERGENCY LIGHT KORRY SWITCH IAW AMM 33-13-00. OPS TEST GOOD.</P>)

Part: ELEVATOR SYSTEM — FAILED · airframe 101,566 hrs · 21,304 cycles

ELEVATOR NOT RETURNING TO CENTER POSITION WHEN DOING FLIGHT CONTROL CHECK.(<P>PERFORMED ELEVATOR POSITION INDICATING SYSTEM OPS TEST IAW AMM 27-38-00. OPS CHECK GOOD AT THIS TIME. AC OK FOR SERVICE.</P>)

Part: NONE — NONE

FWD EQPT VAL EICAS MSG MOMENTARILY APPEARED DURING ROTATION. REPEAT WRITE UP.(<P>REF ITEM M9 LP 1431441 FOR CORRECTIVE ACTION. EQ COOLING GROUND VALVE POSITION FROM N2 SPEED CARD PER AMM 21-58-00. PERFORMED VALVE OPERATIONAL CHECK IAW AMM 21-58-00 VALVE HEALTH CHECK OPS CHECK GOOD.</P>)

Part: NONE — NONE

L ENG SPEED CARD EICAS MSG.(<P>FOUND CANNON PLUG D4978P WITH BROKEN WIRE PIN 38 TO N2 SPEED CARD. RETERMINATED IAW SWPM 70-60-02 AND WDM77-12-12. PERFORMED IDLE RUN IAW AMM 7100-00 ALL OPS CHECK GOOD.</P>)

Part: NONE — NONE

REPEAT WRITE UP LEFT ENG SPEED CARD STATUS MESSAGE AFTER ENG START(<P>PERFORMED ENG N2 SPEED CARD TEST AS PER B767 AMM TASK 73-21-54-705-005-H00 TEST OK.</P>)

Part: NONE — NONE

DURING TAXI OUT CAPTS PFD &AMP; UPPER EICAS SCREENS WENT BLANK.(<P>CAPT'S ADI AND UPPER EICAS CAME BACK AFTER SHUTDOWN. SUPPLIED AIR FOR HOT/HUMID WEATHER CONDITIONS IAW B767AMM 21-00-00-862-068.</P>)

Part: NONE — NONE

L ENG SPEED CARD STATUS MSG REPEAT WRITE UP.(<P>R/R N2 SPEED CARD ON L/H ENG. FAULT CLEARED. FOUND CONNECTOR ON D10064 TO HAVE DAMAGED THREADED INSERTS CAUSING SPEED CARD NOT TO STAY SECURED. SEE LP 1440560 ITEM 6 FOR CORRECTION REF B767 73-21-54. N2 SPEED CARD OPS CK GOOD.</P>)

Part: NONE — NONE · airframe 101,370 hrs · 21,248 cycles

L. ENG SPEED CARD STATUS MESSAGE AFTER START(<P><SPAN>T/S PER B767 AMM 73-21-54-705-005-HOO AND B767 FIM 73-21 FAULT TREE 871. TEST PASSED NORMAL. MESSAGE CLEARED. COULD NOT DUPLICATE ON GROUND AT THIS TIME. MCC ADVISED</SPAN></P>)

Part: NONE — NONE · 21,256 cycles

L ENG SPEED CARD STATUS MESSAGE AFTER START ...REPEAT WRITE UP(<P>PERFORMED FIM 73-21 TASK TT#871 BLOCK #21 FOUND L END SPEED CARD DISPLAYED. REMOVED/REPLACED M1083 N2 SPEED CARD, PERFORMED ADJUSTMENT/TEST IAW AMM 73-21-54-705-005-H00, MESSAGE CLEARED OPS TEST PASSED GOOD.</P>)

Part: NONE — NONE

LEFT / #1 ENGINE "VIB" INDICATION BETWEEN 1 AND 4 ON STATUS PAGE DURING DEPARTURE. FLUCTUATIONS WERE ALSO SLIGHTLY FELT.(<P>RAN #1 ENGINE HIGH POWER RUN VIBRATION SURVEY PER B767 AMM 71-00-00-735-370-H03. AT IDLE. VIBE 0.7, EGT 319, FF 1.3 AT MAX POWER SETTING: VIB 1.5, EGT 730, FF 16.9. VIBRATION WITHIN LIMITS. NO DEFECTS NOTED AT THIS TIME.</P>)

Part: RADOME — DAMAGED

BIRD STRIKE ON RADOME. INSPECTED NOSE RADOME FOUND DAMAGE ON THE EXTERNAL SIDE SURFACE WAS OUT OF LIMITS IAW AMM 05-51-18 & SRM 53-10-72.LP 1401419, ITEM M6: REMOVED AND REPLACED NOSE RADOME IAW AMM 53-12-01, ADJUSTED AND SAFETIED NOSE RADOME IAW AMM 53-12-01-822-013. OPS CHECK GOOD.

Part: VALVE — FAULTED (APU PNEUMATIC) · 21,104 cycles

APU PNEUMATICS INOP ( AUXILIARY POWER UNIT, PNEUMATIC FUNCTION )(<P>TRANSCRIBED TO MEL LIST MDDR 152437 DMI # 49-11-01-01 DUE 03SEP21, CAT C. MAINT ACTIONS C/W PER 152437. PLACARDS APPLIED.</P> / <P>25AUG21 - 1397821 - ITEM# 5 - CVG - REMOVED FLOW SENSING MODULE &AMP; INSTALLED SERVICEABLE MODULE PER AMM 49-53-08 PT SENSOR FAULT GONE. PNEUMATIC OPS CK FAILED SEE ITEM M7 FOR NEXT MX ACTIVITY. S/N OFF - 9110. P/N OFF - 3885081-1.</P> / <P>25AUG21 - 1397822 - ITEM# 7 - CVG - REMOVED APU AIR BLEED VALVE &AMP; INSTALLED SERVICEABLE VALVE PER 36-11-10. VALVE FAILED TO ACTUATE SEE ITEM 8 FOR NEXT MX ACTION. S/N OFF - 24509. P/N OFF - 2780540-101.</P> / <P>25AUG21 - 1397822 - ITEM# 8 - CVG - REMOVED APU SURGE VALVE CONTROL &AMP; INSTALLED SERVICEABLE VALVE PER 49-53-01. OPS GOOD. DMI 152437 CLEARED.&NBSP;</P>)

Part: CONTROL VALVE — FAULTED (CABIN TEMP)

AFT CABIN COMPARTMENT SHOWS 7D EVENT THOUGH AFT CABIN TEMPERATURE CONTROLLER IS SET TO WARM DURING CRUISE FLIGHT(<P>PERFORMED BITE CHECK ON DECK SYSTEM IAW FIM. REMOVED AND REPLACED LEFT PACK TEMP CTRL VALVE IAW AMM 21-51-12. OPS CK GOOD AT THIS TIME.</P>)

Part: DISPLAY — DIM (CAPTS WX RADAR)

CAPTAIN'S WEATHER DISPLAY IS UNACCEPTABLY DIM DURING DAY LIGHT(<P>REMOVED AND REPLACED CAPTAIN EHSI INDICATOR ASSY IAW AMM 34-22-04. ALL INDICATIONS NORMAL. ACCOMPLISHED WXR SYSTEM AND OPERATIONAL TEST IAW AMM 34-43-00. OPS CHECK GOOD. NO FURTHER MX REQUIRED.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN TEMP)

RIGHT AFT CABIN TEMP DISPLAY 9 DEGREES WITH TEMPERATURE KNOB IN THE 2 OCLOCK POSITION.(<P>CYCLED ZONE TEMP INDICATION C/B IAW AMM 21-65-01. NO EICAS MESSAGES FOUND. ALL INDICATION NORMAL. NO FURTHER MX NEEDED.</P>)

Part: CHECK VALVE — MALFUNCTIONED (LT A/C PACK) · 20,937 cycles

LEFT AC COMPT CHECK VALVE (BELOW ISO VALVE) MISFUNCTIONING(<P>REMOVED AND REPLACD LEFT AC CHECK VALVE IAW B767 36-11-05. OPS CK GOOD.</P>)

Part: ACTUATOR — FAULTED (APU AIR INTAKE) · airframe 100,438 hrs · 20,934 cycles

APU WILL NOT START 2 ATTEMPTS(<P>REMOVED AND REPLACED ECU DUE TO HARD FAULT ECU. OPS CHECK GOOD. REF: AMM 49-61-05. S/N OFF - 53-1057. P/N OFF - 2117342-20. REMOVED AND REPLACED APU AIR INTAKE ACTUATOR DUE TO APU ECU HARD FAULT. OPS CHECK GOOD. REF: AMM 49-15-06.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 100,386 hrs

DURING HIGH SPEED LATE DESCENT(ATC INSTRUCTIONS) ENCOUNTERED LIGHT TURBULENCE AND OVERSPEED WARNING CAME ON FOR A FEW SECONDS, 2 KNOTS ABOVE FOR 5 SECONDS.(<P>PER MX CTRL ACCOMPLISHED INSPECTION IAW B767 AMM 05-51-04-212-01, STEP 2C/2E. NO DEFECTS NOTED AT THIS TIME. MC CNTL ADVISED, ACFT SAT FOR CONTINUED SERVICE.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT A/C PACK) · airframe 100,351 hrs · 20,906 cycles

RIGHT PACK TEMP EICAS MESSAGE CAME ON IN FLIGHT. WE DID QRH PROCEDURE AND LIGHT WENT OUT.(<P>PERFORMED BITE TEST OF THE PACK SYSTEM, NO FAULT FOUND IAW B767 AMM 21-51-00-700-805-006 AND OPERATIONAL TEST IAW B767-300 AMM 21-51-00-700-806-006, NO FAULTS AT THIS TIME.</P>)

Part: SWITCH — FAILED (APU) · airframe 100,300 hrs · 20,891 cycles

APU SWITCH SHOWS INCORRECT CONFIGURATION "OFF" WHEN IT SHOULD BE "VALVE". REMOVED AND REPLACED APU BLEED KORRY SWITCH IAW SWPM 20-84-13. OPS CHECK GOOD. VALVE INDICATION PRESENT.

Part: AUTOTHROTTLE SYS — FAULTED · airframe 100,265 hrs · 20,880 cycles

AUTOTHROTTLE CONSISTENTLY UP TO 20 KTS SLOWER THAN MCP SELECTED SPEED(<P>PERFORMED FIM 22-30 FAULT TREE 810 MCDP GROUND TEST 10, NO FAULTS AT THIS TIME. PERFORMED FIM 22-03 FAULT TREE 812 MCDP TEST 12. NO FAULTS AT THIS TIME. PERFORMED FIM 22-03 FAULT TREE 820 TEST 40 NO FAULTS AT THIS TIME.</P>)

Part: INDICATOR — DIM (COCKPIT) · airframe 100,054 hrs · 20,824 cycles

STANDBY ENGINE INSTRUMENTS VERY DIM AND HARD TO READ WHEN TURNED ON(<P>REMOVED AND REPLACED ENGINE STANDBY INDICATOR IAW AMM 77-41-01. OPS CHECK GOOD AT THIS TIME<BR /></P>)

Part: ENGINE — NOT REPORTED (NR 2) · airframe 99,950 hrs · 20,789 cycles

R GENERATOR OFF EICAS MESSAGE DISPLAY. TRANSFERED TO DMI # 145249, CAT B, DUE DATE 16 APR 21 IAW DDG 24-00-01-01. LOG PAGE 1465065: REMOVED AND REPLACED #2 ENGINE IAW AMM 71-00-00. OPS CK GOOD. THIS CLEARS MDDR 145249.

Part: START VALVE — MALFUNCTIONED (LT ENGINE) · airframe 99,890 hrs · 20,771 cycles

DURING LEFT ENGINE START, LEFT ENGINE START VALVE DISCRETE LIGHT CYCLED AN AND OFF WHEN "GRD" WAS SELECTED. EICAS L ENG STARTER MSG WAS NOT DISPLAYED(<P>TRANSFERRED TO MDDR 144784 IAW MEL 80-00-01-01, CAT C, 3 APR 21</P>)

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 99,822 hrs · 20,749 cycles

AUTO PRESSURIZATION CNTRL 2 STARTED GETTING LARGE SWINGS IN CABIN RATE APPROACHING MAX DIFF THEN BACK DOWN(<P>RAN FIM 21-31 FT 803. RECEIVED CONTROLLER FAILURE ON CABIN AUTO 2. REMOVED AND REPLACED CONTROLLER IAW AMM 21-31-02. OPS CHECK NORMAL. STATUS MSG CLEARED.<BR /></P>)

Part: MANIFOLD — DEFECTIVE (ENG FUEL SYS) · airframe 99,732 hrs · 20,721 cycles

UNSCHEDULED ENGINE CHANGE REQUIRED DUE TO DEFECT FOUND WITH FUEL MANIFOLD DURING EO 1972A725(<P ><SPAN>REMOVED AND REPLACED ENGINE PER WORK ORDER 78316.</SPAN></P>)

Part: AILERON — DAMAGED (LH OTBD WING) · airframe 99,732 hrs · 20,721 cycles

LH OTBD AILERON HAS STATIC DISCHARGE EVIDENCE ON OTBD TRAILING EDGE UPPER CORNER(<P ><SPAN>LH OTBD AILERON HAS BEEN / INSPECTED AND REPAIRED IAW B767 SRM 57-60-0201-1, 57-60-02-1A-1, 57-60-02-2R1, / 51-70-17</SPAN></P>)

Part: PLENUM — DAMAGED (LT ACM) · airframe 99,668 hrs · 20,696 cycles

APPROX 50 MIN INTO FLIGHT, SLIGHT VIBRATION FELT IN AIRFRAME. VIBRATION FELT EVERY 5 TO 6 MINS. LASTING APPROX.15 SECONDS. NO EICAS OR STATUS MESSAGES ASSCOCIATED. NO HIGH VIB INDICATION ON ENGINE. THE OUTFLOW VALVE APPEARS TO BE MOVING AND SEEMS TO COINCIDE WITH THE VIBRATION. VIBRATION WAS THE SAME @ FL400, FL380 AND FL360. DURING ILS APP. NO AUTOLAND DISPLAYED ON ASA. FOUND FWD CARGO BAY HEAT DISTRIBUTION DUCT DISCONNECTED, RECONNECTED DUCT, REPLACED ALL SCRIVETS AND CLAMPS. PERFORMED FLOW TEST AS PER AMM 21-00-00, PERFORMED FUNCTIONAL CHECK OF OUTFLOW VALVE, ALL CHECKS GOOD AS PER AMM 21-30-00.LP 1232590, ITEM M8: REMOVED L/H ACM IAW AMM 21-51-03. INSTALLED L/H ACM IAW AMM 21-51-03, OPS CHECK GOOD. S.N OFF: 15-3128, P/N OFF: 680640-4.ITEM M9: L/H PLENUM REMOVED AND NEW L/H PLENUM INSTALLED REF AMM 21-51-02.LP 1232591, ITEM M10: SECURED LOOSE DUCTS, INSTALLED NEW CLAMPS AND SCRIVETS AS PER AMM 21-40-00.

Part: WIRE — DAMAGED (CABIN PRESSURE) · airframe 99,652 hrs · 20,688 cycles

REF AP-19149 NUMBER 1 AUTO PRESS CONTROL INOP. (AUTO CABIN PRESSURE CONTROL SYSTEMS, ONE INOPERATIVE ) (TRANSFER TO MDDR 142736, CAT C. DUE DATE 03MAR21, MEL NR 21-31-01A. PLACARD INSTALLED. 23 FEB21- LP 1068689 ITEM 4 - TPA - AP 19149 ACCOMPLISHED. REPLACED WIRES FROM CONN D 46988 PINS 5, 6, 8, 9, TO D704 IAW MM 21-31-21. OPS CHECKS OK PER AMM 21-31-00. DMI 142736 CLEARED. PLACARD REMOVED.)

Part: RELAY — MALFUNCTIONED (CABIN PRESSURE) · airframe 99,617 hrs · 20,674 cycles

OUTFLOW VALVE CYCLES OPEN THEN CLOSES DURING CRUISE FLT EVERY 9 MIN IN AUTO NR 2 AND EVERY 2 TO 3 MIN IN AUTO NR 1. PERFORMED BITE TEST OF THE CABIN PRESSURE CONTROLLER. NO FAULTS ON NR 2. NR 1 FAULTS WITH AC POWER OFF. PERFORMED ENGINE RUN TO ENSURE PRSOV IS NOT CAUSING PRESSURIZATION ISSUES BY MEANS OF BLEED AIR. FOUND BLEED AIR PRESSURE TO BE STABLE WITH VARYING CABIN PRESSURE. LOG PAGE 1303786:THEN PERFORMED THE OPERATION OF THE OUTFLOW VALVE (WITHOUT PRESSURIZING). FOUND THE DOOR TO BE OPERATING SMOOTHLY. THEN PERFORMED BITE OF CABIN PRESSURIZATION MODULE. AC POWER FAIL ON AUTO 1. AUTO 2 NORMAL. OG PAGE 1303787: REMOVED AND REPLACED RELAYS K211 AND K716 PER ACTION PLAN 19115 (OFF PART: PN BACR13CE2, NSN). PERFORMED OPS CHECK OF OUTFLOW VALVE REF AMM 21-31-05. OPS CHK GOOD. ALSO PERFORMED BITE TEST OF AUTO CABIN PRESSURE CONTROLLERS 1 AND 2. NO FAULTS NOTED REF AMM 21-31-01. REMOVED AND REPLACED CABIN PRESSURE SELECTOR PANEL IAW AMM 21-31-01. OPS CK GOOD.

Part: CONTROLLER — FLUCTUATES (CABIN PRESSURE) · airframe 99,592 hrs · 20,666 cycles

AT CRUISE AND ON DESCENT OBSERVED OUTFLOW VALVE FLUCTUATING. AUDIBLE FLUCTUATIONS IN PRESSURE AIR FLOW CHANGES. EAR POPPING. VALVE MOVED FROM 3/4 CLOSED TICK TO 1/2 TICK EACH TIME.(<P>REMOVED AND REPLACED #1 AUTO PRESSURE CONTROLLER IAW AMM 21-31-02. OPS CHECK SAT AT THIS TIME. NO FAULTS PRESENT.</P>)

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 99,587 hrs · 20,664 cycles

AT FL 400 CREW GOT A VIBRATION AND NOTICED RATE INDICATOR ON PRESS PANEL FLUCTUATING UP AND DOWN(<P>REF AP-19049, REPLACED OUTFLOW VALVE ASSY IAW AMM 21-31-03, OPS CK GD. REMOVED AND REPLACED #2 AUTO PRESSURE CONTROLLER IAW AMM 21-31-02 OPS CK GD.</P><P>VALVE S/N OFF 99-1097&NBSP; P/N OFF 606832-21</P>)

Part: ANTI-ICE VALVE — INOPERATIVE (LT ENGINE) · airframe 99,584 hrs · 20,662 cycles

LEFT ENG ANTI-ICE VALVE REQUIRED COMPLETION OF QRH TO OPEN FOLLOWING ENGINE START. PERFORMED OPS TEST IAW AMM 30-21-00. OPS CHECK GOOD.

Part: OUTFLOW VALVE — FLUCTUATES (CABIN) · airframe 99,584 hrs · 20,662 cycles

OUTFLOW VALVE FLUCTUATES CABIN RATE +/- 100FPM EVERY 10-15 MINUTES. PERFORMED BITE TEST WITH NO FAULTS FOUND AND PERFORMED MANUAL MODE CONTROL TEST WITH NO DEFECTS FOUND IAW AMM 21-31-00.

Part: TERMINAL — DAMAGED (FIRE DETECTOR) · airframe 91,490 hrs · 26,553 cycles

"L ENG FIRE LP 1" EICAS MESSAGE. TRANSFERRED TO DMI 141760, PER DDG 26-11-01-01 CAT "C" DUE ON 11 FEB 21. REMOVED AND REPLACED LOWER AFT FIRE LOOP AND REPLACED TERMINAL END ON WIRE W5334-001R-16 WDM 26-11-11, IAW SWPM 20-10-13 AND AMM 26-11-02.

Part: CONTROLLER — INOPERATIVE (CABIN) · airframe 99,580 hrs · 20,660 cycles

CABIN AUTO INOPERATIVE CAUTION MSG. PERFORMED CABIN PRESSURE CONTROLLER BITE PROCEDURE IAW FIM 21-31 FAULT TREE 803. NO FAULTS FOUND. OPS CHECK GOOD.

Part: PUMP — SLOW (RT FWD FUEL PUMP) · airframe 99,568 hrs · 20,657 cycles

RIGHT FWD FUEL PUMP IS SLOW TO MOVE FUEL. R &R RT FWD FUEL PUMP IAW AMM 28-22-03. OPS CHECK AND LEAK CHECK GOOD AT THIS TIME.

Part: PUMP — SLOW (RT AFT BOOST) · airframe 99,568 hrs · 20,657 cycles

RIGHT AFT FUEL PUMP IS SLOW TO MOVE FUEL. R & R RT AFT BOOST PUMP. OPS CHECK GOOD. NO LEAKS NOTED. REF AMM 28-22-03.

Part: WARNING MESSAGE — ACTIVATION ERROR (LT FUEL PUMP) · airframe 99,554 hrs · 20,652 cycles

TRIED TO CROSSFEED FUEL FROM RIGHT TANK TO LEFT ENGINE. AFTER LEFT TANK PUMPS OFF GOT FUEL PRESSURE WARNING AND BEEPER FOR ALL LT PUMPS. OPERATIONAL CHECK ACCOMPLISHED, PER AMM 28-22-00-215-715 -001. ALL VALVES OPERATED NORMALLY.

Part: PUMP — FAILED (RT FUEL BOOST) · airframe 99,493 hrs · 20,633 cycles

ON LANDING, THE FUEL INDICATION SHOWS L: 8.3 C: 0.0 R: 10.7. FMC TOTALIZER AND CALCULATED FUEL ARE BOTH 19.0. SUSPECTED DISCREPANCY IN LEFT FUEL TANK MEASURING SYSTEM, THIS IS A REPEAT WRITE UP. REFERENCE LOG PAGE NR`S: 1349472, 1349467, 1246268, 1349452, 1349456. R & R RT AFT MAIN FUEL BOOST PUMP, IAW AMM 28-22-03. LEAK AND OPERATIONS CHECK GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT FIRE LOOP) · airframe 99,493 hrs · 20,633 cycles

LT ENGINE FIRE LP 1 EICAS MESSAGE. ITEM TRANSFERRED TO MDDR 140963, PER MEL 26-11-01-01 CAT "C". ACCOMPLISHED WITH FIM 26-11 F/T 804 EICAS INDICATION FIRE LOOP L-1 LEFT ENGINE WIRE CHECK. ALL SYSTEM OPERATIONS CHECKED NORMAL. PERFORMED VISUAL INSPECTION, ALL SYSTEM NORMAL AT THIS TIME, REMAINS OPEN. PRESSED AND HELD ENG/APU FIRE/OVHT TEST SWICH FOR 3 SECONDS, AFTER TEST BUTTON RELEASED, STATUS MESSAGE CLEARS. NO DEFECTS NOTED, SYSTEM IS NORMAL, REF AMM 26-11 FAULT TREE 804. THIS CLEARS DMI 140963, STICKERS REMOVED.

Part: SKIN — DENTED (NR 1 ENG INLET) · airframe 99,493 hrs · 20,633 cycles

NR 1 ENGINE INLET HAS SEVERAL DENTS ON INNER BARREL SLEEVE. REMOVED AND REPLACED NR 1 ENGINE INLET COWL ASSEMBLY, IAW B767 AMM 72-33-02.

Part: EEC — MALFUNCTIONED (RT ENGINE) · airframe 99,426 hrs · 20,606 cycles

R ENG EEC EICAS MESSAGE ( ELECTRONIC ENGINE CONTROL (EEC) SYSTEMS, EEC NORM MODE (CF6 FADEC) )(<P>TRANSFERRED TO MDDR 140560 CAT C DUE DATE 16 JAN 21 MEL 73-21-01-03 CAT 3 RESTRICTED</P><P>DATE 7 JAN - LP 1246285 ITEM 3 - ONT- TROUBLESHOT PER FIM 73-21 FT 874 PERF PIMU BITE 71-01 FT 810 FAULTING L ADC CHAN FAIL . PERF FIM 71-01 TASK A 37 WIRING CHECK FROM R/H EEC TO LADC PER WDM 73-21-14 &AMP; 34-12-61. FOUND GOOD CONTINUITY ON ALL CONNECTIONS PER FIM. IF FAULT CONTINUES REPLACE R/H EEC. EEC (P/N 1519M8931) ON ORDER W/MCC DMI REMAINS OPEN.</P><P>LOGPAGE 1349480: REMOVED AND REPLACED NBT 2 ENG EEC IAW B767-200 AMM 73-21-15. OPS CHECK GOOD AT THIS TIME. THIS CLEARS DMI #140560. MCC NOTIFIED. PLACARDS REMOVED. C/W W/O 75897.</P><P><BR /></P><P><BR /></P>)

Part: FIRE LOOP — OUT OF POSITION (LT ENGINE) · airframe 99,393 hrs · 20,593 cycles

LT ENGINE FIRE LP 1 MESSAGE. TRANSFERRED TO MDDR 140263, IAW MEL 26-11-01-01 CAT C DUE DATE 09JAN21. INSPECTED NR 1 ENGINE FIRE LOOPS, FOUND DETECTOR ELEMENT OUT OF GROMMET AT CLAMP AT O7:00 POSITION. REINSTALLED ELEMENT INTO GROMMET, IAW AMM 26-11-02. PERFORMED OPERATIONS TEST OF ENGINE FIRE DETECTION SYSTEM, IAW AMM 26-11-00. NO DEFECT NOTED.THIS CLEARS DMI NR 140263.

Part: PIMU — MALFUNCTIONED (RIGHT) · airframe 99,363 hrs · 20,582 cycles

AFTER RT ENGINE START, RT ENGINE EEC IN ALT MODE. TRANSFERRED TO DMI 140096, IAW DDG/MEL 73-21-01-03. CAT C DUE 06JAN21. MCC NOTIFIED. PLACARD INSTALLED. A/C CAT III RESTRICTED. REMOVED AND REPLACED L ADC (OFF PART: PN 4040800-906, SN 93103896, PER FIM TASK 71-01 TASK A 39 REF B767 AMM 34-12-01, FOR REMOVAL AND INSTALLATION. OPERATIONS CHECK GOOD. REMAINS IN WORK. REMOVED AND REPLACED R (PIMU) UNIT AT M1414. OPERATIONS CHECK NORMAL AT THIS TIME, IAW AMM 77-35-02-404-006-H00.

Part: SHUTOFF VALVE — LEAKING (FUEL SYSTEM) · airframe 99,334 hrs · 20,570 cycles

FUEL LEAK FOUND ON APU FUEL SHUT-OFF VALVE(V96). REPLACED APU SHUT OFF VALVE, IAW AMM 28-25-02. REMOVED & INSTALLED APU SHUT OFF VALVE ACTUATOR, PER AMM 28-25-02, S/N OFF: 67-862072, P/N OFF: AV-31-1. APU SHUT OFF VALVE LEAK CHECKS GOOD, IAW AMM 28-25-02. OK FOR SERVICE.

Part: INDICATOR — INACCURATE (COCKPIT TEMP) · airframe 99,202 hrs · 20,532 cycles

FLIGHT DECK TEMP VALVE INDICATES MAX COLD NO MATTER SELECTION. OPERATIONS CHECKED F/D VALVE POSITION INDICATOR 21-64-1. OPERATIONS CHECKS GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT FUEL PUMP) · airframe 99,175 hrs · 20,521 cycles

EICAS RT FWD FUEL PUMP. TRANSFER TO MDDR 138467 MEL 28-22-01 CAT C. PULLED & COLLARED P-61 G:18 C/B MX ACTION C/W. MCC NOTIFIED PLACARD INSTALLED. ITEM 2 RESET GFI, IAW AMM RIGHT AUX FUEL SYSTEM 28-22-00/001. THIS CLEARS MDDR 138467. C/B RESET, MCC NOTIFIED, PLACARD REMOVED.

Part: DOOR — OUT OF LIMITS (A/C EXHAUST DOOR) · airframe 99,175 hrs · 20,521 cycles

REPEAT WRITE UP IN CRUISE & DESCENT, LOUD RUMBLE OCCURS EVERY 5 MINUTES, SOUNDS LIKE IT IS ORIGINATING AFT OF FLIGHT DECK, GOES AWAY AFTER 1 MINUTE. C/W AP 18181, IAW 32-22-00 AND AMM 21-33-02, NO DEFECTS NOTED. ON VISUAL INSPECTION OF NOSE GEAR DOORS, NOSE GEAR DOOR SEAL PUT AIRPLANE INTO AIR MODE AND CHECKED LEFT AND RIGHT PACK EXHAUST DOOR, IAW 32-09-02. RT PACK EXHAUST DOOR FOUND OUT OF LIMITS BY .290 ADJUSTED AND TESTED, IAW 21-51-00. OPERATIONS NORMAL, NO FURTHER DEFECTS NOTED.

Part: UNKNOWN — VIBRATION (NOT REPORTED) · airframe 99,172 hrs · 20,520 cycles

DURING CRUISE AND DESCENT TO FL 2000 VIBE AND NOISE EVERY 5-6 MINUTES. PERFORMED ZONAL GVI OF MEC 05-41-01. PRESSURIZED AIRCRAFT, IAW 05-51-24. COULD NOT DUPLICATE, NO DEFECTS NOTED.

Part: CONNECTOR — DAMAGED (NR 1 FIRE LOOP) · airframe 99,123 hrs · 20,507 cycles

NR 1 ENGINE FIRE LOOP 2 STATUS MESSAGE. FOUND PUSHED PIN ON CONNECTOR D4154B. RESEATED PIN 2. OPERATIONS CHECK GOOD, IAW AMM 26-11-01.

Part: FIRE DETECTOR — MALFUNCTIONED (NR 1 ENGINE) · airframe 99,115 hrs · 20,505 cycles

NR 1 ENGINE FIRE LOOP 2 STATUS MESSAGE. ITEM M5, FOUND PUSHED PIN ON CONNECTOR D4154B, RESEATED PIN 2. OPERATIONS CHECK IS GOOD AT THIS TIME, IAW WDM 26-11-11 AND AMM OPERATIONS CHECK 26-11-01. REMOVED AND REPLACED FIRE LOOP LOWER FWD, IAW B767 AMM 26-11-02 AS PRECAUTIONARY MEASURE, OPERATIONS CHECK GOOD. P/N OFF 7882, S/N OFF 1979 17NOV20. REMOVED AND REPLACED FIRE LOOP LOWER AFT, IAW B767 AMM 26-11-02 AS PRECAUTIONARY MEASURE. OPERATIONS CHECK GOOD.

Part: DUCT — BLOWN (RT BLEED SYS) · airframe 99,086 hrs · 20,496 cycles

AFTER RIGHT ENGINE START, RT ENGINE BLEED EICAS MESSAGE. ON INITIAL CLIMB STARTING AT APPROXIMATELY 500' AGL UNTIL 7000' MESSAGE RT ENGINE DUCT PRESS INDICATION WAS 0 PSI. PERFORMED FIM TASK 36-10-FT837 AND VISUAL INSPECTION OF PRSOV, PER AMM 36-11-09. FOUND AIR LEAK DOWNSTREAM OF PRSOV AIR FEED DUCT WHEN MANUALLY SUPPLIED WITH PRESSURE. SUSPECT BLOWN SEAL AND COUPLER BETWEEN PYLON AND ENGINE DUCT CONNECTION. UPON INSPECTION OF NR 2 ENGINE BLEED ISSUE FOUND PRSOV FEED LINE LEAKING DOWN STREAM INTO ENGINE COMPARTMENT. FOUND LOOSE DUCT BELOW PRSOV. REINSTALLED DOUCT COUPLING, IAW AMM 36-11-01. LEAK CHECK GOOD. PERFORMED ENGINE RUN AT POWER, IAW AMM 71-00-00. ALL BLEED SYSTEMS WORK AS SHOULD.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 99,086 hrs · 20,496 cycles

AFTER LEFT ENGINE START LT ENGINE ANTI ICE EICAS MESSAGE WITH SWITCH ON. PERFORMED ENGINE ANTI ICE SYSTEM TEST, IAW AMM 30-21-00. PERFORMED ENGINE RUN, IAW AMM 71-00-00, OPS CK GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT A/C PACK) · airframe 99,086 hrs · 20,496 cycles

EICAS MESSAGE: RT PACK OFF, RT ENGINE BLEED OFF. PERFORMED ENGINE RUN AND OPERATIONAL TEST OF PRSOV (RT ENGINE), IAW AMM 71-00-00 AND AMM 36-11-09. OPERATIONS CHECK GOOD.

Part: CONTROLLER — MALFUNCTIONED (HIGH PRESSURE) · airframe 99,086 hrs · 20,496 cycles

"RT ENGINE HPSOV" EICAS DISPLAYED IN CRUISE AT FL350 AND 90 PERCENT N1. RT ENGINE HPSOV STATUS MESSAGE REMAINS AFTER QRH PROCEDURE COMPLETED. PERFORMED CONTINUITY, LIR AND DAR TESTS, PER B767 WDM 36-11-62 & 36-23-21 AND AMM 20-10-39 OF WIRING AT CONNECTORS D1876 (28,31 & 58), D2378A (A1,A5 & D6) AND D2378B (A5, A8 & A11) TO THEIR RESPECTIVE COMPONENTS V347FM7191. ALSO CHECKED GROUND AT GDX3 - DC TO SM1 AND SM2 AND TO U347, M7191, V348, TS101 AND V352. NO FINDINGS AT THIS TIME. CUSTOMER REQ RAR HPC (M7191) STILL REQUIRED. REMOVED AND REPLACED HIGH PRESSURE CONTROLLER, IAW B767 AMM 36-11-08. OPERATIONS CHECK GOOD, LEAK CHECK GOOD, BITE TEST GOOD.

Part: FIRE LOOP — MALFUNCTIONED (LEFT ENGINE) · airframe 99,054 hrs · 20,485 cycles

LT ENGINE FIRE LP 2" STATUS MESSAGE. LT ENGINE FIRE LP 2 PC CARD M682. REMOVED AND RESEATED PC CARD, FAULT STILL EXISTS. REMOVED LT ENGINE FIRE LOOP 2 PC CARD AND SWAPPED WITH RT ENGINE FIRE LP 2 PC CARD, IAW B767 AMM 26-10-01. FAULT STILL REMAINS, SWAPPED LT AND RT ENGINE FIRE LP 2 PC CARDS BACK TO ORIG POSITIONS, FAULT REMAINS. OPENED LT ENGINE COWLS. TRANSFERRED TO MDDR 137015, IAW MEL 26-11-01-01, CAT C. REMOVED AND REPLACED AFT UPPER FIRE LOOP ASSEMBLY, IAW AMM 26-11-02. OPERATIONS CHECK GOOD.

Part: LANYARD — DAMAGED (PORTABLE ELT) · airframe 99,034 hrs · 20,476 cycles

EMERGENCY ELT CORD UNRAVELLED (PORTABLE). REMOVED AND REPLACED PORTABLE EMERGENCY ELT, IAW AMM 25-64-00. OPERATIONS NORMAL AT THIS TIME.

Part: ACTUATOR — MALFUNCTIONED (OUTFLOW VALVE) · airframe 98,919 hrs · 20,438 cycles

DURING CRUISE OUTFLOW VALVE BRIEFLY OPENED AND CLOSED, CREATING A RUBBLE/SHUDDER. PER T/S REMOVED AND REPLACED AUTO 1 CABIN PRESSURE CONT UNIT, IAW AMM 21-31-02. OPERATIONS CHECK GOOD. OFF PART: PN 21173888, SN 62-A0346. REMOVED AND REPLACED AUTO 2 CABIN PRESSURE CONTROLLER UNIT, IAW AMM 21-31-02. OPERATIONS CHECK GOOD. OFF PART: PN 2117388-8, SN 62-A0276. REMOVED AND REPLACED CABIN PRESSURE OUTFLOW VALVE ACTUATOR, IAW AMM 21-31-04. PERFORMED WIRE RESISTANCE CHECKS, IAW AMM 21-31-11 AND WDM 21-31-21. NO DEFECTS NOTED AT THIS TIME.

Part: SELECTOR PANEL — MALFUNCTIONED (CABIN PRESSURE) · airframe 98,919 hrs · 20,438 cycles

OUTFLOW VALVE POSITION INDICATOR BACKLIGHTING INOPERABLE. REMOVED AND REPLACED CABIN PRESSURE SELECTOR PANEL ASSEMBLY, IAW AMM 21-31-01. OPERATIONS CHECK GOOD AT THIS TIME.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 98,919 hrs · 20,438 cycles

INFO ONLY: DURING CRUISE AT 390FL AT ABOUT 6 MIN INTERVALS, THE OUTFLOW VALVE WOUD MOVE FROM A QUARTER POSTION TO HALF POSITION CAUSING THE A/C TO SHUDDER. IT HAPPENED CONTINUOUSLY. PERFORMED CABIN PESS TEST, IAW AMM 05-51-24, SYSTEM TEST OK. PERFORMED MANUAL MODE CONTACT TEST, IAW AMM 21-31-00, TEST OK. PERFORMED BITE TEST ON CABIN PRESSURE CONTROLLERS, NO FAULTS FOUND. A/C OK FOR SERVICE.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 98,916 hrs · 20,436 cycles

WHILE CRUISE AT FL 390 CRUISE VALVE OPENED AND RUMBLE MULTIPLE TIMES. REMOVED AND REPLACED OUTFLOW VALVE ASSEMBLY, IAW AMM 21-31-01-004. OPERATIONAL TEST OK. REMOVED AND REPLACED CABIN PRESS SELECTOR PANEL ASSEMBLY, IAW AMM 21-31-04. OPERATIONS CHECK GOOD (OFF PART: PN 130502-7, SN 42-A0009).

Part: CONTROLLER — FAULTED (SHUTOFF VALVE) · airframe 98,906 hrs · 20,433 cycles

RT ENGINE HPSOV CAUTION MESSAGE IN CLIMBOUT, ASSOCIATED STATUS MESSAGE REMAINED AFTER CAUTION SELF CLEARED. REPEAT WRITE -UP. TRANSFERRED TO MDDR 135784 PER DDG 36-11-02 CAT C DUE 19OCT20 MX ACTION C/W. DISP NOTIFIED 1414 EH. REMOVED AND REPLACED NO 2 ENGINE HIGH PRESSURE CONTROLLER IAW AMM 36-11-08-004-006-007. OPERATIONS CHECK REQUIRED, REF M9 FOR OPERATIONS CHECK. PERFORMED OPERATIONS TEST NR 2 HPC, IAW AMM 36-11-08, OPERATIONS TEST GOOD. MDDR 135784 CLEARED. PLACARDS REMOVED. T/S PER WDM, CHECKED WIRING FROM HP CONTROLLER TO BITE MODULE AND FROM HPSOV TO MODULE, PER WDM 36-11-62. FOUND INTERMITTENT GROUND AT TERM 2 OF HPSOV, SECURED LOOSE CONN D4210P. PERFORMED OPERATIONS CHECK, IAW AMM 36-11-07, PLACARDS REMOVED. MCC NOTIFIED.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 98,906 hrs · 20,433 cycles

IN CRUISE, A/C PRESSURIZATION REPEATEDLY CYCLED TO A DESCENT THEN CLIMB BEFORE STABILIZING. NOTED ON GAUGES AND PRESSURE ON PILOT EARS. PERFORMED CONTROLLER BITE CHECK, NO FAULTS AND A/C PRESSURIZATION TO 4 PSI, IAW AMM 21-31-01. NO DEFECTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (SHUTOFF VALVE) · airframe 98,904 hrs · 20,432 cycles

DURING DESCENT & APPROACH RT ENGINE HPSOV STATUS MESSAGE APPEARED SEVERAL TIMES. PERFORMED BITE TEST OF AIR SUPPLY MODULE, PER AMM 36-23-00-715-001. BITE SUCCESSFUL, NO FAULTS NOTED AT THIS TIME.

Part: SWITCH — MALFUNCTIONED (LT A/C PACK OVRH) · airframe 98,906 hrs · 20,433 cycles

FOUND LEFT HAND PACK INOPERABLE. T/S, IAW FIM M 21-51-18. REMOVED AND REPLACED LEFT PACK OVERHEAT CONNECTOR, NO HELP. NEED TO REPLACE SENSOR S555, PART ON ORDER. REMOVED AND REPLACED LT PACK OVERHEAT SWITCH, IAW AMM 21-51-18. OPERATIONS TEST AND LEAK CHECK OK.

Part: SHIELD — MISSING (FLASHLIGHT) · airframe 98,879 hrs · 20,420 cycles

EMERGENCY FLASHLIGHT NEAR L1 ENTRY MISSING SECURITY SHIELD. DEFERRED ITEM PER MEL 25-63-04B REF MDDR 135322, CAT C, DUE 11OCT20. T AND I TJ 2051Z, PER MCC ANTHONY P/N A1-18-1030. INSTALLED NEW SECURITY SHIELD ON EMERGENCY FLASHLIGHT NEAR L1 DOOR ENTRY, IAW B767 AMM 25-00-00. THIS CLEARS DMI 135322. PLACARD REMOVED MCC NOTIFIED.

Part: SHUTOFF VALVE — MALFUNCTIONED (RT ENGINE) · airframe 98,838 hrs · 20,406 cycles

STATUS MESSAGE RT ENGINE HPSOV. TRANSFERRED TO MDDR 135117, AS PER MEL 36-11-02-02, CAT C DUE DATE 08OCT20. MIA MX, 05OCT20. REMOVED AND REPLACED RT ENGINE HPSOV, IAW AMM 36-11-07. OPERATIONS CHECK AND LEAK CHECK GOOD. PERFORMED ENGINE RUN UP, OPERATIONS CHECK HPSOV AND T/R NORMAL, IAW AMM 71-00-00 AND 78-31-00. THIS CLEARS MDDR 125117. FOUND LEAK AT T-FITTING OF PRECOOLER, REPLACED PACKING. LEAK CHECK GOOD, IAW AMM 36-00-21. THIS CLEARS MDDR 135117, PLACARDS REMOVED. S/N OFF: NSN, P/N OFF: BACP11K6.

Part: FITTING — UNSECURE (SHUTOFF VALVE) · airframe 98,863 hrs · 20,414 cycles

RT ENGINE HPSOV, QRH COMPLETE LIGHT DID NOT EXTINGUISH. PERFORMED AIR SUPPLY MODULE BITE PROCEDURE, PER AMM 36-20 FT 804 TIGHTEND HPSOV LOOSE HPSOV SENSE LINE FITTINGS, IAW AMM 36-11-07. PERFORMED ENGINE RUN, PER AMM 71-00-00. NO FAULTS FOUND.

Part: WARNING LIGHT — ILLUMINATED (WX RADAR SYSTEM) · airframe 98,802 hrs · 20,396 cycles

DURING CRUISE FLIGHT NOTICED A LOUD GRINDING NOISE, THEN GOT A WX FAIL LIGHT. NO MESSAGE FOUND ON ARRIVAL. PERFORMED OPERATIONAL CHECK, IAW AMM 354-43-00-715-001-001. ALL CHECKS FOUND OK.

Part: WARNING LIGHT — INOPERATIVE (RT ENG OVERHEAT) · airframe 98,785 hrs · 20,390 cycles

RT ENG OVHT DISCREET LIGHT ON THE CENTER CONSOLE IS INOP. FOUND DURING PRE-FLIGHT. PERFORMED FIRE TEST SYSTEM, OPERATE NORMAL, AS PER AMM 26-21-04.

Part: TUBE — DAMAGED (RT ENGINE) · airframe 98,739 hrs · 20,375 cycles

EICAS MESSAGE RT ENG HPSOV AT 03.57Z AT FL250 N1 106.5 DURING CLIMB OUT. MESSAGE APPEARED AND SELF CORRECTED BEFORE WE RAN QRH. TRANSFER TO DMI NR 134451, IAW MEL 36-11-02-02, CAT C, DUE DATE 25SEP20. PLACARD INSTALLED. ACTIVATED HPSOV, CHECKED FOR LOOSE LINES, OPERATED HPSOV, ACTIVATED T/R. OPERATION CHECKED NORMAL, IAW TASK CARD & FIM 36-11-00-815-843-001. THIS CLEARS MDDR 134451. TIME & INITIAL - TS 0712Z. PLACARDS REMOVED. MCC NOTIFIED. RT ENGINE HPSOV FAULT FOUND. RE-OPENED MDDR 134451, IAW DDG 36-11-02-02, CAT C, DUE DATE SEP-25-2020. PLACARD INSTALLED. C/W DDG PROCEDURES. REMOVED AND REPLACED PRESSURE LINE AND ELBOW JOINT TO HPSOV, IAW AMM 20-11-00. HPSOV OPS CK GOOD, PER AMM 36-11-07. THIS CLEARS DMI 134451, MCC NOTIFIED, PLACARDS REMOVED. DDG PROCEDURES REVERTED TO NORMAL CONFIG.

Part: SHUTOFF VALVE — MALFUNCTIONED (RT ENGINE) · airframe 98,735 hrs · 20,373 cycles

STATUS MSG RT ENG HPSOV, TRANSFERRED TO MDDR 134368 MEL 36-11-02-02, CAT C, DUE 23SEP20. REMOVED AND REPLACED NR 2 ENG VALVE HIGH PRESSURE SHUT OFF, IAW AMM 36-11-07. OPS TEST OK AND CLEARED DMI 134368. PLACARD REMOVED. DISPATCH D.L. 0418Z.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 98,705 hrs · 20,364 cycles

ENTRY DOOR EMERGENCY FLASH LIGHT INOP. TRANSFERRED TO MDDR 134104 IAW MEL 25-63-04B, CAT C. REMOVED AND REPLACED ENTRY DOOR FLASHLIGHT BATTERY, IAW AMM 25-60-00, NO OTHER DEFECTS NOTED. THIS CLEARS DMI NR 134104, PLACARD REMOVED, DISPATCH: DC1304Z.

Part: UNKNOWN — SPARKS (RADAR UNIT) · airframe 98,694 hrs · 20,361 cycles

RADAR SPARKING ON LEFT SIDE. PERFORMED OPERATIONAL TEST, AS PER AMM 34-43-00-715-001-001, TEST PASS.

Part: ECU — MALFUNCTIONED (APU) · airframe 98,667 hrs · 20,350 cycles

APU AUTO SHUT DOWN FAULT LIGHT ILLUMINATED. ITEM TRANSFERRED TO MDDR #133942, IAW MEL 49-11-01A, CAT C. REMOVED AND REPLACED APU ECU, IAW AMM 49-61-05/401. OPS CHECK GOOD, IAW AMM 49-11-00-802. THIS CLEARS MDDR #133942, MCC NOTIFIED, PLACARDS REMOVED.

Part: CONNECTOR — LOOSE (WINDOW HEAT) · airframe 98,664 hrs · 20,348 cycles

"R FWD WINDOW" EICAS MESSAGE, RESET PER QRH, SAME MESSAGE CAME UP 3-4 MINS LATER, TURNED R FWD WINDOW HEAT OFF PER QRH.TROUBLESHOT AND PERFORMED FIM TASK 30-41 TASK 802. FOUND RESISTANCE TO BE OUT OF RANGE. REMOVED WIRES FROM SENSOR TO SPARE SENSOR IAW AMM 30-41-02. RESISTANCE CHECK GOOD AND OPS CHECK GOOD. SECURED SENSOR WIRE TO CORRECT MAIN SENSOR POSITION IAW FIM 30-41-FT 804. OPS CHECKED GOOD IAW AMM 30-41-00. FOUND CONNECTOR J1 LOOSE. TORQUED IAW AMM 56-11-01, PERFORMED WINDOW HEAT TEST IAW AMM 30-41-00. OPS CHECK GOOD. ALSO SECURED SENSOR CIRCUIT TO CORRECT MAIN SENSOR POSITION IAW FIM 30-41 FT 804. OPS CHECK GOOD. NON-MEL 132921 CLOSED.

Part: CONTROLLER — MALFUNCTIONED (WINDOW HEAT) · airframe 98,650 hrs · 20,342 cycles

R FWD WINDOW CAUTION MESSAGE.(<P>REPLACED R FWD AND L SIDE WINDOW HEAT CONTROLLER IAW AMM 30-41-01. OPS CKS GOOD.</P>)

Part: RADAR — MALFUNCTIONED (WEATHER) · airframe 98,643 hrs · 20,339 cycles

RADAR INOP APPROX 2 HR 30 MIN INTO FLIGHT. HEARD GRINDING NOISE WXR RADAR FAIL MESSAGE ON BOTH MFDS.(<P>COULD NOT DUPLICATE. PERFORMED OPS CK PER AMM 34-43-00. OPS CK NORMAL.</P>)

Part: CIRCUIT CARD — MALFUNCTIONED (SMOKE DETECTION) · airframe 98,611 hrs · 20,326 cycles

AFT CARGO DECK SMOKE DET 2 INOP. TROUBLE SHOOT AFT CARGO DET IAW FIM 26-10 FT 803 AND FIM 26-16 FT 806 BLK 1 AND 50. REMOVED AND REPLACED CARGO FIRE CIRCUIT CARD M10427 IAW AMM 26-10-01. CHECKS GOOD,

Part: CIRCUIT CARD — FAILED (FIRE DETECTION) · airframe 98,611 hrs · 20,326 cycles

AFT CARGO DECK SMOKE DETECTOR NR 2 WAS INOPERATIVE. TROUBLESHOT THE AFT CARGO SMOKE DETECTOR IAW FIM 26-10, FT 803, AND FIM 26-16, FT 806, BLK 1, AND 50. REMOVED AND REPLACED THE CARGO FIRE CIRCUIT CARD M10427 IAW AMM 26-10-01. CHECKED GOOD,

Part: FAULT MESSAGE — FALSE ACTIVATION (EXHAUST FAN) · airframe 98,581 hrs · 20,314 cycles

STATUS MESSAGE AFT EQ EXHAUST FAN 2. FIM FAULT TREE 21-26, FAULT TREE 808 CARRIED OOUT FOR AFT EQ EXHAUST FAN 2 AND MESSAGE CLEARED. NO FURTHER FAULTS NOTED AT THIS TIME.

Part: GENERATOR — INOPERATIVE (APU) · airframe 98,583 hrs · 20,315 cycles

APU GENERATOR INOPERATIVE. TROUBLESHOT APU GENERATOR SVST TEST IAW AMM 24-21-00. CONFIRM APU GENERATOR INOPERATIVE.

Part: GENERATOR — INOPERATIVE (APU) · airframe 98,583 hrs · 20,315 cycles

APU GENERATOR INOPERATIVE. REMOVED AND REPLACED THE APU GENERATOR UNIT IAW AMM 24-21-01. OPS AND LEAK CHECKED GOOD.

Part: ANTI-ICE VALVE — UNSECURE (RT ENGINE) · airframe 98,563 hrs · 20,308 cycles

AFTER ENGINE START, RT ENGINE BLEED OFF LIGHT ILLUMINATED. RT ENG BLEED OFF EICAS MESSAGE. ON GVI OF PNEUMATIC VALVES ON RT ENG FOUND ANTI-ICE VALVE TO BE LOOSE. SECURED THE ANTI-ICE VALVE. RAN NR 2 ENG. PERFORMED RT ENG BLEED VALVE OPS CHECK. CHECKED GOOD IAW AMM 36-11-09.

Part: VALVE — INOPERATIVE (COCKPIT TEMP) · airframe 98,525 hrs · 20,295 cycles

FLIGHT DECK COMP AUTO TEMP CONTROL INOPERATIVE. REMOVED AND REPLACED FLIGHT DECK TRIM AIR MOD VALVE IAW AMM 21-61-07. OPS CHECKED NORMAL.

Part: CONNECTOR — UNSECURE (MODULATION VALVE) · airframe 98,529 hrs · 20,296 cycles

FLT DECK TEMP EICAS MESSAGE ALONG WITH OVHD TEMP CONTROL INOPERATIVE. TROUBLESHOT IAW FIM 21-60 FT 805 AND FT 805. TRIM VALVE FLIGHT DECK LIGHT WAS ON. ON THE ZONE TEMP CONTROLLER IAW AMM 21-61-07-004-006. FOUND LOOSE CONNECTOR PLUG ON TRIM AIR MODULATING VALVE. REMOVED AND CLEANED THE CONNECTOR PLUG, OPS CHECKED NORMAL.

Part: STARTER — MALFUNCTIONED (RT ENGINE) · airframe 98,412 hrs · 20,259 cycles

RT STARTER CUTOUT ON ENG START. START VALVE CLOSED AFTER SELECTING START SWITCH FROM END TO AUTO. PERFORMED R ENG RUN PER AMM 71-00-00. NORMAL START. NO MESSAGES OR FAULTS INDICATED.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENG N2) · airframe 98,109 hrs · 20,164 cycles

RIGHT ENGINE ANALOG N2 STATUS MSG. PERFORMED FIM 77-12- FT 809. NO DEFECTS NOTED. MESSAGE CLEARED.

Part: SHUTOFF VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 97,946 hrs · 20,115 cycles

AFTER ENG START EICAS L ENG BLEED(<P>REPLACED L PRSOV IAW AMM 36-11-09. CHECKS GOOD.</P>)

Part: SENSOR — FAULTY (RT ENGINE) · airframe 97,946 hrs · 20,115 cycles

R ENG ANALOG N2 STATUS(<P>REPLACED N2 SPEED SENSOR AND PERFORMED POWER PLANT TEST 4 . CHKS GOOD PER AMM 71-00-00-795-034-M03.</P>)

Part: IGNITER — DEFECTIVE (APU) · airframe 97,922 hrs · 20,104 cycles

APU INOP.(<P>TRANSFER TO MDDR #127587 IAW DDG 49-11-01A, CAT C, DUE DATE 05/06/20.</P><P>LOG PAGE 1138319: REMOVED AND REPLACED APU IGNITOR PLUG IAW AMM 49-41-02. OPS CHECK GOOD. THIS CLEARS DMI #127587.</P>)

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 97,869 hrs · 20,081 cycles

CARGO FIRE DET 1A INOP.(<P>TRANSFER TO MDDR #127023 IAW DDG 26-16-02-02.</P><P>LP 1167027: RESET MAIN DECK SMOKE DETECTORS AND OPS CHECKED GOOD IAW AMM 26-19-01. THIS CLEARS MDDR 127023. PLACARD REMOVED.</P>)

Part: RESTRAINT — DEFECTIVE (AC BAY) · airframe 97,861 hrs · 20,077 cycles

LEFT PACK INOP(<P>TRANSFER TO MDDR 126988 IAW DDG 21-51-01-01, CAT 'C', DUE DATE 22-APR-2020.</P><P>LP 1167020 - M2:&NBSP; REMOVED AND REPLACED RESTRAIN FLEXIBLE PER AMM 21-51-01. TEST OK, THIS CLEARS MDDR 126988.</P>)

Part: DRIVE UNIT — MALFUNCTIONED (WEATHER RADAR) · airframe 97,861 hrs · 20,077 cycles

WXR RADAR IS INOP ON NAV MODE.(<P>LP 1167016 - 1: REMOVED AND REPLACED&NBSP; NOSE RADOME IAW AMM 53-12-01. OPS TEST OK (PN OFF 284T052-28 S/N OFF 000952).</P><P>LP1167017 - M6: REMOVED AND REPLACED ANTENNA DRIVE IAW AMM 34-43-05 TEST OK.</P><P>LP 1167018 - M7: REMOVED&NBSP; AND REPLACED TRANCEIVER IAW AMM 34-43-01. TEST OK (PN OFF 622-5132-106 S/N OFF 6022).</P>)

Part: CONTROL PANEL — MALFUNCTIONED (WEATHER RADAR) · airframe 97,852 hrs · 20,073 cycles

WEATHER RADAR SYSTEM INOP(<P>TRANSFERRED TO MDDR #126873 IAW DDG 34-43-02, CAT 'C'.</P><P>REF LP 1167014: REPLACED WX RADAR CONTROL PANEL IAW AMM 34-43-02. CKS GOOD. CLOSED MDDR 126873.<BR /></P>)

Part: TRANSCEIVER — MALFUNCTIONED (WEATHER RADAR) · airframe 97,829 hrs · 20,065 cycles

WEATHER RADAR WOULD NOT DISPLAY ANY RETURNS IN ANY MODE AT ANY GAIN SETTING DURING DESCENT.(<P>REMOVED AND REPLACED WXR TRANCEIVER PER AMM 34-43-01. OPS CHK OK AT THIS TIME.</P>)

Part: IGNITER — DEFECTIVE (NR 2 ENGINE) · airframe 97,810 hrs · 20,059 cycles

INFO ONLY #2 ENGINE 1ST START ATTEMPT UNSUCCESSFUL, 2ND START ATTEMPT SUCCESSFUL WITH IGNITER IN BOTH THEN BACK TO SINGLE AFTER #2 ENGINE STABILIZED.(<P>TRANSFERRED SINGLE IGNITION SYSTEM #2 ENGINE TO MDDR 126428, EXP 31MAR20, PER MEL 74-00-01A, CAT "A".</P><P>LP 1138341: REMOVED AND REPLACED #2 ENG UPPER AND LOWER IGNITER IAW AMM 74-21-00. OPS CK GOOD. THIS CLEARS DMI 126428, PLACARD REMOVED.<BR /></P>)

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 97,806 hrs · 20,057 cycles

R ENG START VALVE DID NOT ILLUMINATE.(<P>FWD TO MDDR 126373 PER MEL 80-00-01-01.</P><P>LP&NBSP; 1138325-M7: REMOVED AND REPLACED RH ENGINE START VALVE INDICATION LIGHT IAW SWPM 20-84-18. PERFORMED ENGINE START&NBSP; IAW AMM 80-11-00. LIGHT OPS TEST NORMAL. THIS CLEARS MDDR 126373.</P>)

Part: TRANSCEIVER — MALFUNCTIONED (WEATHER RADAR) · airframe 97,769 hrs · 20,046 cycles

WEATHER RADAR INOP WXR WEAK MESSAGE DISPLAYED.(<P>PERFORMED FIM WXR BITE IAW FIM 34-43-FT805. REMOVED AND REPLACED WXR TRANSCEIVER IAW AMM 34-43-01. OPS CHECK BAD. REINSTALLED ORIGINAL PART. OPS CHECK NORMAL AT THIS TIME. PERFORMED WXR BITE IAW FIM 34-43-FT805. OPS CHECK GOOD AT THIS TIME.</P>)

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 97,755 hrs · 20,043 cycles

WXR WEAK DISPLAYED ON EHSI WHEN REACHING CRUISE ALT FL 300.(<P>PERFORMED OPERATIONAL TEST ON WEATHER RADAR SYSTEM, REF AMM 34-43-00. OPERATIONAL TEST NORMAL, COULD NOT DUPLICATE FAULT AT THIS TIME.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 97,635 hrs · 20,006 cycles

ON TAKEOFF, R CENTER FUEL PUMP LOW PRESSURE EICAS WITH ABOUT 4000 LBS IN CENTER TANK.(<P>PERFORMED OPS CHECK ON R CENTER FUEL PUMP IAW B767 AMM 28-22-00. OPS CHK NORMAL, NO MESSAGES DISPLAYED.&NBSP;</P>)

Part: ANTI-ICE VALVE — MALFUNCTIONED (RIGHT ENGINE) · airframe 97,482 hrs · 19,961 cycles

RIGHT ENGINE ANTI-ICE VALVE DID NOT CLOSE AFTER IT WAS OPENED.(<P>ACTIVATED VALVE MANUALLY. PERFORMED SYSTEM TEST IAW B767 AMM 30-21-00. SYSTEM TESTS SATISFACTORY AT THIS TIME.<BR /></P>)

Part: WARNING LIGHT — FALSE ACTIVATION (ANTI-ICE SYSTEM) · airframe 97,515 hrs · 19,969 cycles

R ENG ANTI-ICE CAUTION MSG IN FLIGHT.(<P>PERFORMED SYSTEM TEST IAW B767 AMM 30-21-00. OPS CHECK GOOD. NO DEFECTS AT THIS TIME.</P>)

Part: ANTI-ICE VALVE — FAILED (RT ENGINE) · airframe 97,467 hrs · 19,954 cycles

INFLIGHT AFTER TAKEOFF EICAS R ENG ANTI ICE.(<P>C/W FIM 30-21 FAULT TREE 805. FOUND THE R ENG ANTI ICE VALVE TO WORK NORMAL. OPS CHECK GOOD.<BR /></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (WEATHER RADAR) · airframe 97,445 hrs · 19,946 cycles

WXR WEAK MESSAGE DISPLAYED ON HSI.(<P>C/W TEST PER AMM 34-43-00. OPS CHECK OK AT THIS TIME. NO FAULTS NOTED.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (WEATHER RADAR) · airframe 97,436 hrs · 19,943 cycles

INTERMITTENT WXR WEAK MSG ON MFD.(<P>COMPLETED TEST OF WXR IAW B767 AMM 34-43-00. OPS CHECK GOOD AT THIS TIME.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT FUEL VALVE) · airframe 97,422 hrs · 19,936 cycles

L ENG FUEL VALVE EICAS MESSAGE. L ENG VALVE ILLUMINATED DURING ENG START, QRH COMPLETE.(<P>PERFORMED FIM 76-11 FT 812, UNTIL STEP 2. OPERATES NORMALLY. PERFORMED ENG RUN (#1 ENG ONLY) IAW AMM 71-00-00. NO EICAS OR ANNUNCIATOR MESSAGES. NO FAULTS NOTED AT THIS TIME.</P>)

Part: LATCH — OUT OF ADJUST (THRUST REVERSER) · airframe 97,378 hrs · 19,924 cycles

RIGHT ENG HIGH VIBRATION (3.0) DURING CLIMB ABOVE FL180. T/S PER FIM 71-05 FT 852. FOUND INBD T/R HALF NOT LATCHED FULLY AND FAN COWL NOT ADJUSTED CORRECTLY. ADJUSTED LATCHES IAW AMM 71-11-05 AND 78-31-04. PERFORMED TEST 6 VIB SURVEY IAW AMM 71-00-00-735-320-403, ENG VIB PARAMETERS WITHIN LIMITS.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT BLEED SYSTEM) · airframe 97,309 hrs · 19,901 cycles

L ENG BLEED OFF EICAS MESSAGE AFTER START. PERFORMED NR 1 AND 2 ENG RUNS IAW AMM 71-00-00. LT BLEED OPS CHECKED IAW AMM 36-11-00, ALL OPS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 97,264 hrs · 19,890 cycles

LEFT ENG VALVE FAULT ON POWER UP OF PLANE.(<P>PERFORMED RUN OF LEFT ENGINE IAW B767 AMM&NBSP;<SPAN>71-00-00.&NBSP;</SPAN><SPAN>OPS CHECK GOOD, NO FAULT LIGHT OR INDICATIONS AT THIS TIME.</SPAN></P>)

Part: UNKNOWN — MALFUNCTIONED (BLEED AIR SYS) · airframe 97,177 hrs · 19,866 cycles

ON TAXI OUT, LH DUCT PRESSURE LOW, READING 5 PSI UNTIL LARGE ADVANCEMENT OF THRUST INCREASED DUCT PRESSURE TO NORMAL.(<P>PERFORMED OPERATIONAL TEST OF AIR SUPPLY SYS PRESS INDICATING SYS IAW AMM 36-21-00. OPS CHK GOOD.</P>)

Part: PRESSURE SWITCH — MALFUNCTIONED (LT ENGINE FUEL) · airframe 97,175 hrs · 19,865 cycles

LEFT ENGINE FUEL FILTER STATUS MESSAGE. REMOVED AND REPLACED FUEL FILTER DIFFERENTIAL PRESSURE SWITCH IAW AMM 73-34-01. OPS CHECKED NORMAL. NO LEAKS OR DEFECTS NOTED.

Part: DUCT — DAMAGED (APU AIR SURGE) · airframe 97,149 hrs · 19,854 cycles

FWD APU AIR SURGE DUCT FOUND TO HAVE HOLE IN DUCT. REMOVED AND REPLACED FWD APU AIR SURGE DUCT IAW AMM 49-53-01. LEAK CHECK GOOD AT THIS TIME.

Part: EXHAUST FAN — FAILED (FWD E/E BAY) · airframe 97,122 hrs · 19,842 cycles

FWD EQUIPMENT EXH FAN STATUS MSG IN CRUISE.(<P>TRANSFERRED TO MDDR #122295 CAT 'C', DUE 29DEC19, PER MEL 21-58-04-02-01.</P><P>LP 1221208: T/S IAW FIM 21-58 FAULT TREE 905. FOUND FWD EQUIPMENT EXH FAN AT FAULT. REMOVED AND REPLACED FWD EQUIPMENT EXHAUST FAN IAW AMM 21-58-06. OPS CK GOOD. THIS CLEARS DMI 122295.&NBSP;</P>)

Part: OXYGEN MASK — DAMAGED (PILOT'S) · airframe 97,002 hrs · 19,807 cycles

PILOT NOTIFIED OF FRAYED OXYGEN MASK ON FIRST OFFICER SEAT.(<P>REMOVED AND REPLACED OXYGEN MASK IAW 35-11-51, OPS CHECK NORMAL.<BR /></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI ICE SYS) · airframe 96,977 hrs · 19,802 cycles

CLIMBING THRU ~ 10,000 FT, OBSERVED R ENG ANTI-ICE ON EICAS. R ENGINE ANTI-ICE SW "VALVE" DISAGREEMENT LIGHT.&NBSP;(<P>PERFORMED RIGHT ENGINE ANTI-ICE THERMAL VALVE OPERATIONAL TEST IAW AMM 30-21-00, OPS CHECK NORMAL. CYCLED ANTI-ICE VALVE LIGHT, EXTINGUISHED AS COMMANDED. NO DEFECTS NOTED AT THIS TIME.&NBSP;</P>)

Part: TRANSCEIVER — MALFUNCTIONED (WX RADAR SYS) · airframe 96,855 hrs · 19,764 cycles

WEATHER RADAR RETURNING A LINE OF RED WITH NO WEATHER IN THE AREA IN THE 10 O'CLOCK POSITION, FROM THE AIRCRAFT DIAGRAM TO THE EDGE OF THE COMPASS ROSE ON THE HSI. THIS OCCURRED FL 210 -FL 370. NO TERRAIN IN THE AREA AND THE GAIN WAS CHANGED FROM CAL TO MIN, TO MAX, WITH NO CHANGES. (<P>REMOVED AND REPLACED WX RADAR TRANSCEIVER IAW AMM 34-43-01-004 AND AMM 34-43-01-404. OPS CHECK GOOD, NO FAULTS NOTED AT THIS TIME.&NBSP;</P>)

Part: OXYGEN MASK — INOPERATIVE (OBSERVER'S) · airframe 96,850 hrs · 19,763 cycles

FIRST OBSERVERS SEAT INOP.&NBSP;(<P>TRANSFERRED TO MDDR 120257 PER MEL 25-11-02-01A, CAT 'A'.&NBSP;</P><P>LP 1231530 - M6: REMOVED AND REPLACED 1ST OBSERVERS O2 MASK ASSY REF AMM 35-11-51. THIS CLEARS DMI 120257 AND COMPLETES W/O 58890.&NBSP;&NBSP;</P>)

Part: GUARD — FAILED (LIGHT SWITCH) · airframe 96,855 hrs · 19,764 cycles

EMERGENCY LIGHT SWITCH GUARD DOES NOT SPRING BACK.(<P>REMOVED AND REPLACED EMERGENCY LIGHT/PASS OXYGEN PANEL IAW AMM 33-51-08. OPS TEST OK AT THIS TIME, NO FURTHER DEFECTS NOTED AT THIS TIME.<BR /></P>)

Part: ACTUATOR — FAILED (LT PACK DOOR) · airframe 96,695 hrs · 19,715 cycles

LT PACK EXH DOOR DOES NOT ACTUATE.(<P>TRANSFERRED TO DMI #119370 PER MEL 21-53-01B, CAT 'C'.</P><P>LP 1075896 - M4: LEFT PACK INOP DUE TO DMI 119370. TRANSFERRED L PACK TO DMI 119371 PER MEL 21-51-01-01.</P><P>LP 1075901 - M5: REMOVED AND REPLACED ACTUATOR ASSY DOOR IAW AMM 21-53-04. PERFORMED LEFT HAND PACK BITE TEST IAW AMM 21-51-14, TEST RESULT OK. THIS ACTION CLEARS DMI 119370. PLACARD REMOVED.&NBSP;</P><P>LP 1075901 - M6: REF DMI 119370 CLOSE OUT ON ITEM #5. THIS ALSO CLEARS DMI 119371, PLACARDS REMOVED.</P>)

Part: SWITCH — MALFUNCTIONED (FIRE) · airframe 96,590 hrs · 19,679 cycles

LEFT ENGINE FUEL VALVE LIGHT WITH EICAS MESSAGE ILLUMINATED. T/S PER FIM 76-11 FT 812 AND WDM 76-11-11. RESET S37, LEFT ENGINE FIRE SWITCH ON P8. LIGHT (ENG FUEL VALVE) WENT OFF. CREW RAN ENGINE PER AMM 71-00-00, NO FAULTS NOTED. MCC NOTIFIED.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (SMOKE DETECTOR) · airframe 69,565 hrs · 19,672 cycles

MAIN DECK SMOKE DETECTOR FAILED, AMBER A1. TROUBLESHOOTED MAIN DECK SMOKE DETECTOR A1 IAW FIM 26-16-816. NO DEFECTS FOUND DURING OPS CHECK. NOTIFIED MCC. DMI 118610 REMAINS OPEN FOR FURTHER INVESTIGATION.</P><P>LP 1223520 - M5: COMPLIED WITH SYSTEM OPERATIONAL TEST. OPS CHECK GOOD AT THIS TIME IAW M.M CH 26-19-00.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 96,537 hrs · 19,661 cycles

WXR SYS STATUS MSG.(<P>PERFORMED WX RADAR SYSTEM TEST IAW AMM 34-43-00. OPS CHECK NORMAL AT THIS TIME, MSG CLEARED.&NBSP;</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 96,513 hrs · 19,652 cycles

STATUS MSG WXR SYS. PERFORMED FIM 34-43 TASK 801, MESSAGE CLEARED. WXR SYSTEM OPS CHECKS NORMAL PER AMM 34-43-00/501.

Part: RELAY — FAILED (FUEL SYSTEM) · airframe 96,503 hrs · 19,648 cycles

CTR R FUEL PUMP EICAS MESSAGE AFTER ENGINE START WITH CENTER TANK FUEL. REMOVED AND REPLACED K10692, RT RELAY IAW SWPM 20-81-11. OPS CHECK OK PER AMM 28-22-00.

Part: CONNECTOR — DAMAGED (ELT) · airframe 96,490 hrs · 19,642 cycles

FIXED ELT INOPERATIVE. FOUND DURING TROUBLESHOOTING ON P5 PANEL, ELT CONTROL PANEL CIRCULAR CONNECTOR PIN G RECESSED GROUND PIN ON CIRCULAR CONNECTOR IAW SWPM 20-62-00. PERFORMED OPS CHECK OF FIXED ELT IAW IAW TM A06V2 DOCUMENT, DL 241-1472-00 REV 1. OPS CHECK FAILED. PERFORMED TEST FROM COCKPIT AND AT ELT, BOTH FAILED TO GET ANY RESPONSE FROM BOTH LOCATIONS. PERFORMED GROUND TEST PROCEDURE OF FIXED ELT IAW CEIS TM A06V2, D6241-17472-00 REV 1. TEST FAILED, NO PIN RESPONSE FROM ELT ON FREQS. OPS CHECKED FIXED ELT IAW CMM 23-24-04, OPS CHECK NORMAL.

Part: TRANSCEIVER — MALFUNCTIONED (WEATHER RADAR) · airframe 96,473 hrs · 19,634 cycles

WEATHER RADAR WILL NOT TEST, MESSAGE: WEATHER FAIL RIGHT. WORKS NORMAL IN FLIGHT. RE-RACKED WEATHER RADAR TRANSCEIVER AND PERFORMED OPS TEST OF WEATHER RADAR SYSTEM IAW AMM 34-43-00. NO DEFECTS NOTED AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 96,406 hrs · 19,607 cycles

AFTER T/O, WX FAIL APPEARED ON HSI. WX RADAR WAS RECYCLED AND WORKED NORMALLY. AFTER BLOCK IN, WXR SYS STATUS MSG REMAINED. NO DEFECTS NOTED AT THIS TIME, ACKNOWLEDGED BY MAINTENANCE. PERFORMED WEATHER RADAR SYSTEM TEST IAW AMM 34-43-00.

Part: PRESSURE SWITCH — MALFUNCTIONED (FUEL PUMP) · airframe 96,370 hrs · 19,595 cycles

CTR R FUEL PUMP EICAS MESSAGE WITH 2,300 LBS IN CTR TANK. PERFORMED POWER WIRE CHECK, NO POWER A1, B1, C1 K330 RELAY. REMOVED AND REPLACED K330 RELAY PER WDM 28-22-13, NO HELP. REMOVED AND REPLACED RIGHT CENTER OVERRIDE PRESSURE SWITCH IAW AMM 28-42-01. OPS CHECK NORMAL AND NO LEAKS NOTED.

Part: IGNITER — MALFUNCTIONED (NR 2 ENGINE) · airframe 96,283 hrs · 19,564 cycles

R ENG IGNITER ON EICAS - #2 ENG WOULD NOT START SINGLE SETTING. NORMAL START ON BOTH. R & R NR 1 AND 2 IGNITER AND SWAP IGINITION BOXES ON NR 1 AND 2 TO ORIGINAL POSITION IAW AMM 74-21-02-74-11-01, OPS CHECKS OK

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENGINE) · airframe 96,263 hrs · 19,558 cycles

RIGHT ENGINE NR 1 IGNITER STATUS MESSAGE. PERFORMED FIM 74-00 FT P11 FOR THE NR 1 IGNITER. MESSAGE CLEARED, NO FAULTS NOTED AT THIS TIME.

Part: WARNING LIGHT — NO INDICATION · airframe 96,232 hrs · 19,548 cycles

RT "ENG VALVE" LIGHT DID NOT ILLUMINATE ON SHUTDOWN. ENGINE SHUTS DOWN IMMEDIATELY ON SELECTION OF "CUT OFF".(<P>REPLACED RELAY K1252 PER FIM 76-11 FT 808, NO HELP. CYCLED INDICATOR LIGHT AND LIGHT TEST NORMAL. OPERATED SWITCH WITH ENG OFF, LIGHT OPS NORMAL. STARTED ENGINE, LIGHT OPERATIONAL. PERFORMED OPS CHECK OF THE RIGHT ENGINE SPAR VALVE IAW AMM 28-22-01. OPS CHECKS GOOD. NO DEFECTS NOTED.

Part: COVER — MISSING (WEATHER RADAR) · airframe 96,133 hrs · 19,516 cycles

WXR CONTROL PANEL MISSING UNUSED SWITCH COVERS. (<P>REMOVED AND REPLACED WXR CONTROL PANEL IAW AMM 34-43-02. PANEL&NBSP;OPS CHECK NORMAL AT THIS TIME.</P>)

Part: SWITCH — BROKEN (RADAR CONTROL) · airframe 96,095 hrs · 19,503 cycles

RADAR GAIN SWITCH BROKEN / CRACKED.&NBSP;(<P>REMOVED AND REPLACED WEATHER RADAR CONTROL PANEL IAW AMM 34-43-00. OPS CHECK GOOD.&NBSP;</P>)

Part: PUMP — MALFUNCTIONED (FUEL SYSTEM) · airframe 96,073 hrs · 19,497 cycles

CENTER RT FUEL PUMP EICAS.(<P>TRANSFERRED TO MDDR 114716 PER MEL 28-22-02A, CAT C, DUE DATE 24-JUL-19.</P><P>LP 1099299 - M2: REMOVED AND REPLACED RIGHT AUX TANK FUEL OVRD&NBSP;PUMP PRESSURE SWITCH IAW AMM 28-42-01, NO HELP. OFF PART (PN: 21C1-3-21, S/N W033388)</P><P>LP 1099299 - M3: REMOVED AND REPLACED RIGHT CENTER FUEL PUMP IAW AMM 28-22-05. PERFORMED OPS CHECK, OPS CHECK GOOD. THIS CLEARS MDDR 114716. MCC NOTIFIED AND PLACARD REMOVED.</P>)

Part: SMOKE DETECTOR — FAILED (CARGO BAY) · airframe 96,012 hrs · 19,484 cycles

#3A CARGO SMOKE DETECTOR SHOWS FAILED (INOP).(<P>TRANSFERRED TO MDDR #114489 PER MEL 26-16-02-02 CAT "C" DUE DATE 20-JUL-19.</P><P><SPAN>REPLACED SMOKE DETECTOR IAW AMM 26-19-01 OPS CHECKED GOOD THIS CLEARS MDDR 114489 PLACARD REMOVED</SPAN><BR DATA-MCE-BOGUS="1" /></P>)

Part: BATTERY — INOPERATIVE (APU) · airframe 95,914 hrs · 19,457 cycles

STATUS MSG - APU BATT CHGR. PERFORMED FIM 24-31 F/T 805 BLOCK 22. REMOVED AND REPLACED APU BATTERY CURRENT MONITOR IAW 24-31-02, OPS CHECK FAILED. PERFORMED FIM 24-31 FT 805 BLOCK 23. REMOVED AND REPLACED RELAY K788 IAW WDM 24-31-41. NO HELP, REMOVED AND REPLACED APU BATTERY IAW AMM 24-31-04. OPS CHECK GOOD.

Part: PRESSURE SWITCH — FAILED (FUEL SYSTEM) · airframe 95,908 hrs · 19,456 cycles

AFTER ENGINE START, CENTER RIGHT FUEL PUMP EICAS MESSAGE. REMAINED ON WITH 5000 LBS OF CENTER TANK FUEL. T/S DMI #113803 TO R/H CENTER AUX TANK OVERRIDE PRESSURE SWITCH IAW FIM 28-22 FT 805, BLOCK 50. REMOVED AND REPLACED THE RT CENTER AUX PRESSURE SWITCH IAW AMM 28-42-01. PERFORMED OPS CHECK OF PUMP. NO PRESSURE LIGHT, NO MESSAGES, OPS NORMAL AT THIS TIME.

Part: APU — FAULTED · airframe 95,868 hrs · 19,446 cycles

APU FAULT, DID NOT START AFTER 2 ATTEMPTS. PERFORM BITE CHECK OF ECU PER AMM 49-61-05, NO FAULTS FOUND. APU START SUCCESSFUL OF 1ST ATTEMPT BY MAINT, OPS CHECKED GOOD.

Part: SENSOR — FAULTY (AC BAY) · airframe 95,682 hrs · 19,388 cycles

LT PACK INOP IN AUTO, OK IN STBY (<P>TRANSFERRED TO DMI # 112307 MEL 21-51-03-01 CAT C DUE 07 JUN19&NBSP; - PLACARDS INSTALLED&NBSP;</P><P>LP 1078848-M3: REMOVED AND INSTALLED COMPRESSOR OUTLET SENSOR ON LEFT PACK IAW AMM 21-51-06-404. EFFECTIVITY CHECK GOOD. A/C EFFECTIVITY CODE 997. THIS CLEARS DMI 112307. PLACARDS REMOVED.&NBSP;&NBSP;</P><P>LP 1078849 - M4:&NBSP;RESET CBS N-10 AND N-25 IAW AMM 21-51-06-404; OPS CHECK GOOD AT THIS TIME.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 95,699 hrs · 19,394 cycles

LT PACK TEMP EICAS MSG. (<P>PERFORM PACK TEMP CONTROLLER BITE, NO CURRENT FLIGHT FAULTS NOTED PER FIM 21-51 FT 803. PERFORM OPS CHECK, NO DEFECTS NOTED. PLACED P/N 625928-2 ON ORDER WITH MCC DUE TO PREVIOUS FLT FAULT COMPRESSOR SENSOR PACK.<BR /></P>)

Part: SWITCH — BROKEN (COCKPIT) · airframe 95,642 hrs · 19,376 cycles

F/O WXR SWITCH BROKEN.(<P><SPAN>REMOVED AND REPLACED&NBSP;FO EFIS CONTROL PANEL IAW AMM 31-11-00. OPS CHECK GOOD AT THIS TIME.</SPAN><BR /></P>)

Part: RELAY — FAILED (APU) · airframe 95,617 hrs · 19,367 cycles

APU COULD NOT START "START ABORTED" ON BITE&NBSP;(<P>TRANSFERRED TO MDDR 111830 IAW DDG 49-11-01A CAT "C".</P><P>LP 1074463 - M7:&NBSP;R&AMP;R APU BATTERY IAW AMM 24-31-04. NO HELP. MDDR REMAINS. BATTERY OFF PART (P/N: 4579, S/N: 113363)</P><P>LP 1074463 - M8:&NBSP;R&AMP;R APU BATTERY CHARGER IAW AMM 24-31-05. NO HELP.&NBSP; CHARGER OFF PART (P/N: 4-254-04, S/N: 2872).&NBSP;<BR /></P><P>LP 1074468 - M2:&NBSP;REMOVED AND REPLACED APU BATTERY IAW AMM 34-31-04-004-001. BATTERY OFF PART (P/N: 018550-000, S/N: 090520006BE0D)</P><P>LP 1074468 - M3: REMOVED AND REPLACED APU CRANK CONTACTOR RELAY&NBSP;IAW SWPM 20-81-21. OPS CHECK GOOD. THIS CLEARS MDDR 111830. MCC NOTIFIED. PLACARDS REMOVED.</P>)

Part: BATTERY — DISCHARGED (MAIN) · airframe 95,617 hrs · 19,367 cycles

MAIN SHIP BATTERY LOW.&NBSP;(<P>REMOVED AND REPLACED MAIN SHIP BATTERY IAW AMM 24-31-01. CHARGER GOOD OPS GOOD.&NBSP;</P>)

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 95,566 hrs · 19,349 cycles

WX TL SW&NBSP; INOP.(<P>PERFORMED OPERATIONAL CHECK OF WX RADAR MODE CONTROL PANEL IAW AMM 34-43-00 AND ALL CHECK GOOD AT THIS TIME.&NBSP;</P>)

Part: PRESSURE SWITCH — MALFUNCTIONED (FUEL SYSTEM) · airframe 95,560 hrs · 19,347 cycles

CTR R FUEL PUMP EICAS MSG(<P>FUEL PUMP PLACED ON MEL 28-22-00 AND TRANSFERRED TO MDDR 111302 (RE-OPENED).</P><P>LOG PAGE 1054057: REMOVED AND REPLACED CENTER FUEL PUMP PRESSURE SWITCH. OPS CHECKED NORMAL IAW AMM 28-42-01.</P><P><BR /></P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 95,550 hrs · 19,344 cycles

CTR R FUEL PUMP EICAS MESSAGE(<P>TRANSFERRED TO DMI #111302 CAT 'C' DUE DATE 17MAY19 IAW MEL 28-22-02A.</P><P>LOG PAGE&NBSP;<SPAN>1058308:&NBSP;</SPAN><SPAN>PERFORMED FIM 28-22 TASK 805. CTR RIGHT FUEL PUMP OPERATED PROPERLY WITH NO DEFECTS. THIS CLEARS DMI #111302. MCC NOTIFIED.</SPAN></P>)

Part: PUMP — FAILED (FUEL BOOST) · airframe 95,437 hrs · 19,318 cycles

CTR LEFT FUEL PUMP EICAS MESSAGE WHILE TAXING.(<P>REMOVED AND REPLACED LEFT CENTER FUEL PUMP. OPS CHECKS NORM AT THIS TIME IAW AMM 28-22-05.</P>)

Part: PUMP — MALFUNCTIONED (RT FUEL) · airframe 95,413 hrs · 19,308 cycles

RT CTR FUEL PUMP INOP.(<P>TRANSFERRED TO MDDR # 110272.<BR /></P><P>LP 1053688 - M1:&NBSP;CENTER TANK CONFIRMED EMPTY REF MEL #28-22-02B, MDDR#110272 REMAINS OPEN.</P><P>LP 1050362 - M11:&NBSP;AMENDMENT&NBSP;DDG 28-22-02B AS PER MCC TO DDG 28-22-02A CAT C. DUE DATE 25APR19 MX ACTION C/W DISPATCH LC@0123Z.&NBSP;</P><P>LP 1053689 -&NBSP;PERFORMED FIM TASK 28-22 FT 805 UP TO AND INCLUDING SHEET 2 BLOCK 24, 25, 45, 46. FOUND 28VDC AT X2, 115VAC AT B1/C1/A1. REMOVED AND REPLACED GROUND ENABLE RELAY K633 IAW WDM 91-02-71. RELAY R&AMP;R DID NOT FIX PROBLEM. RELAY MS27418-213 ON ORDER. MCC NOTIFIED. T/S REQUIRED. DMI 110272 REMAINS OPEN.</P><P>LP 1050365 - 1:&NBSP;PERFORMED FIM 28-22 F/T 805. BLOCK 25 FOUND 28V DC ACROSS X2 PIN ON RELAY RELAY K330. PROCEED TO BLOCK 46. DUE TO PREVIOUS CHANGING OF K633 RELAY SUSPECT K330 RELAY BAD. PER WDM 28-22-12 ALSO FOUND 115V AC AT PINS A2, B2, AND C2 ON K330 RELAY. THIS CONFIRMS BAD RELAY. DMI 110272 REMAINS OPEN.</P><P>LP 1050372 - M3:&NBSP;REMOVED AND REPLACED RELAY K330 IN P37 PANEL IAW WDM 28-22-10. UNABLE TO OPS CHECK DUE TI TIME. DMI REMAINS OPEN.&NBSP;</P><P>LP 1050375 - M2:&NBSP;OPS CHECKED RT CENTER FUEL PUMP IAW 28-22-00. OPS CHECK FAIL. BOOST PUMP PRESSURE LIGHT ILLUMINATED WITH "RT CENTER" FUEL EICAS MSG. CIRCUIT BREAKER RE-COLLARED IAW 28-22-02A. DMI 110272 REMAINS OPEN.</P><P>LP 1050379 - M3: T/S AND FOUND PUSHED BACK PIN ON K10690 D31184 PIN 6. INSTALLED THE PIN BACK PROPERLY AND OPS CHECK GOOD IAW WDM 28-22-12 AND AMM 28-22-00. THIS CLEARS MDDR 110272. MCC NOTIFIED AND STICKER REMOVED.</P>)

Part: SMOKE DETECTOR — INOPERATIVE (MAIN CARGO) · airframe 95,366 hrs · 19,293 cycles

MAIN CARGO DECK #B2 SMOKE DETECTOR LOOP INOP. VERIFIED CARGO COMPARTMENT SMOKE DETECTION SYSTEM. OPS CHECKS GOOD PER AMM 26-19-00. PERFORMED FIM 26-19 FT 802 AND ALSO DID A WIRE SHAKEDOWN ON LOOP 2B. NO FAULTS NOTED. R & R NR 2B SMOKE DETECTOR IAW AMM 26-19-01. PERFORMED OPS CHECK, OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: SMOKE DETECTOR — FAILED (CARGO BAY) · airframe 95,339 hrs · 19,286 cycles

CARGO SMOKE DETECTOR FAILED LIGHT ILLUMINATED IN POS A2.(<P>PLACED ZONE A2 ON DEFERRAL IAW MEL 26-16-02-02 CAT C MDDR # 109819.</P><P><BR /></P><P>LP 1054109 - M2: REMOVED &AMP; REPLACED LOOP 2 CHANNEL A "A-2" SMOKE DETECTOR ASSEMBLY IAW AMM 26-16-01. OPS CHECK GOOD. THIS&NBSP;CLEARS DMI 109819. MCC NOTIFIED. PLACARDS REMOVED. THIS COMPLETES&NBSP;WO # 49992.</P>)

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 95,329 hrs · 19,284 cycles

"L ENG ANTI-ICE" EICAS MSG WHEN SELECTED ENG ANTI-ICE OFF. AFTER RECYCLING, MSG CLEARED.(<P>PERFORMED OPERATIONAL CHECK OF THE LT ENG ANTI ICE VALVE IAW AMM 30-21-00. OPS CHECK NORMAL AT THIS TIME. OK FOR SERVICE.</P>)

Part: BPCU — FAULTED · airframe 95,354 hrs · 19,291 cycles

UPON ARRIVAL AIRCRAFT WOULD NOT CONNECT TO GROUND POWER.(<P>BITE BPCU IAW FIM 21-20 TASK 801. REPLACE BPCU FAULT CODE 41 PER FIM 24-20 TASK 803 TABLE 101. FOUND INTERLOCK FUSE BLOWN, R&AMP;R IAW AMM 20-00-00. DID NOT HELP, REMOVED &AMP; REPLACED BPCU IAW AMM 24-22-02. OPS CHECK NORMAL, GROUND POWER CONNECTS AND NO DEFECTS NOTED AT THIS TIME.</P>)

Part: SWITCH — NOT SEATED (WX SYSTEM) · airframe 95,280 hrs · 19,268 cycles

F/O WX SWITCH ON AISLE STAND INOPERATIVE. RESEATED THE F/O WXR SWITCH OPS CHECK GOOD IAW AMM 34-43-00.

Part: TRANSCEIVER — MALFUNCTIONED (WX RADAR SYSTEM) · airframe 95,280 hrs · 19,268 cycles

WEATHER STATUS MESSAGE ON ARRIVAL. PERFORMED BITE TEST AND RESET WEATHER RADAR TRANSCEIVER PER AMM 34-43-01, GROUND OPS CHECK GOOD, NO MESSAGE.

Part: STATUS MESSAGE — FALSE ACTIVATION (WEATHER RADAR) · airframe 95,275 hrs · 19,267 cycles

AFTER BLOCK IN STATUS MESSAGE WXR SYS. PERFORM BITE TEST AND RESET OF WXR TRANSCEIVER IAW AMM 34-43-01 OPS CHECKED GOOD.

Part: LATCH — BROKEN (NR 2 COWLING) · airframe 95,211 hrs · 19,249 cycles

NR 2 ENG OB CORE COWL PRESS RELIEF DOOR LWR BROKEN. (<P>R/R LATCH ON THE NR 2 ENG O/B CORE COWL PRESS RELIEF DOOR IAW SRM 51-40-02</P>)

Part: SEAL — OUT OF POSITION (NR 1 ENGINE) · airframe 95,211 hrs · 19,249 cycles

NR 1 ENG AFT EDGE OF FAN CASE I/B T/R SEAL OUT OF RETAINER&NBSP;(<P>REINSTALLED SEAL IN RETAINING ON NR 1 ENG AFT EDGE OF FAN CASE I/B T/R IAW SOPM 20-50-02</P>)

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 95,211 hrs · 19,249 cycles

UPON PERFORMING OUTFLOW VALVE INSTALLATION TEST HARD TO RESET C/B P-15 IN ORDER FOR AUTO MODE &AMP; AUTO MODE 2 TO FUNCTION.(<P>POST INSTALLATION TEST CARRIED OUT IAW AMM 21-31-03-862-114, TEST GOOD, NO DEFECTS NOTED.</P>)

Part: BEARING — WORN (NR 2 ENGINE) · airframe 95,211 hrs · 19,249 cycles

NR 2 ENG COMPRESSOR SECTION 8:30 POS JUST ABOVE AND FWD OF MAN ACCESSORY GEARBOX LWR PNEUMATIC SUPT ROD HAS WORN BEARING. (<P>REMOVED AND REPLACED BEARING IAW&NBSP; AMM 20-11-00</P>)

Part: WIRE — CONTAMINATED (NR 1 ENGINE) · airframe 65,211 hrs · 19,249 cycles

NR 1 ENG LT SIDE POWER FEEDER CABLE HAS OIL CONTAMINATION TOP TO BOTTOM. (<P>REMOVED OIL CONTAMINATION FROM NR 1 ENG POWER FEEDER CABLES IAW SWPM&NBSP; 20-10--14 STEP B</P>)

Part: OUTFLOW VALVE — UNSERVICEABLE (CABIN PRESSURE) · airframe 95,211 hrs · 19,249 cycles

AFT OF&NBSP; BULK CARGO COMP LT SIDE CABIN PRESS OUTFLOW VALVE EA PUSHROD ATTACH HARDWARE HAS OXIDATION. (<P>REMOVED AND INSTALLED SERVICEABLE OUTFLOW VALVE IAW AMM 21-1-03. PERFORMED OPS CK IAW AMM 21-31-03 TASK 6 WITH NO DEFECTS NOTED AT THIS TIME.</P>)

Part: HINGE — LOOSE (NR 2 COWLING) · airframe 95,211 hrs · 19,249 cycles

NR 2 ENG RT CORE COWL PRESS RELIEF DOOR FITS LOOSE WHEN FULLY CLOSED (<P>REPLACED UPPER AND LOWER HINGES ON PREE RELIEF DOOR IAW SRM 51-40-02</P>)

Part: LINE — LEAKING (NR 1 ENGINE) · airframe 95,211 hrs · 19,249 cycles

NR 1 ENG LT AFT SIDE OIL LINE LEAKING (<P>CLEANED AREA AND FOUND LINE LEAKING FROM CONTACT WITH CLAMP HARDWARE IAW AMM 72-00-00. FOUND AND REPLACED OIL LINE IAW AMM 20-11-00 AND SRM 51-40-02, LEAK CK ACCOMPLISHED ON THE T/E T2031 ITEM 2. ADJUSTED CLAMP DURING INSTALLATION OF LINE.</P>)

Part: SEAL — TORN (NR 1 ENGINE) · airframe 95,211 hrs · 19,249 cycles

NR 1 ENG I/B FAN COWL, LOWER SEAL TORN. (<P>R/R AND REPLACED SEAL IAW AMM 20-10-23.</P>)

Part: PLENUM — DAMAGED (HEAT EXCHANGER) · airframe 95,211 hrs · 19,249 cycles

LT HEAT EXCHANGER PLENUM HAS ELONGATED HOLES (<P>R/R LT HEAT EXCHANGER PLENUM IAW AMM 21-51-02</P>)

Part: LATCH — CRACKED (NR 1 COWLING) · airframe 95,211 hrs · 19,249 cycles

NR 1 ENG I/B CORE COWL FWD LATCH HAS A CRACK (<P>REPAIRE FWD LATCH ON THE NR 1 ENG CORE COWL IAW SRM 54-42-01-2R-7</P>)

Part: RECEPTACLE — BROKEN (APU BAY) · airframe 95,211 hrs · 19,249 cycles

APU FIREWALL RECEPTACLE D40305 HAS BROKEN LOCK AT PIN 3 (<P>REMOVED AND REPLACED RECEPTACLE D 40305 IAW SWPM 20-31-14</P>)

Part: TUBE — CHAFED (NR 1 ENGINE) · airframe 95,211 hrs · 19,249 cycles

NR 1 ENG BLEED AIR TUBE LH SIDE 7 O'CLOCK POS CHAFFED FORM CORE COWL.(<P>R/R NR 1 ENG BLEED AIR TUBE LT SIDE 7 O'CLOCK POSITION IAW AMM 75-24-03.</P>)

Part: CLAMP — BROKEN (NR 2 ENGINE) · airframe 95,211 hrs · 19,249 cycles

NR 2 ENG COMPRESSOR SECTION 3:30 POS ABOVE AIR/OIL HEAT EXCHANGER LINE HAS 1 EA BROKEN CLAMP.(<P>REMOVED AND REPLACED NR 2 ENG PNEUMATIC LINE CLAMP ABOVE AIR COOLER IAW AMM 70-00-00-00</P>)

Part: WIRE — CONTAMINATED (NR 1 ENGINE) · airframe 95,211 hrs · 19,249 cycles

NR 1 ENG LT&NBSP; SIDE WIRE BUNDLES HAVE OIL CONTAMINATION (<P>CLEANED OIL CONTAMINATION FORM WIRE BUNDLES ON LT SIDE OF NR 1 ENG IAW SWPM 20-10-14.</P>)

Part: PRESSURE SWITCH — FAILED (FUEL SYSTEM) · airframe 95,211 hrs · 19,249 cycles

NR 1 ENG FUEL FILTER DIFFERENTIAL PRESS SWITCH FAILED TO OPS CK ON TASK CARD A-73-306-01-1(<P>R/R FUEL FILTER DIFFERENTIAL PRESS SWITCH THEN RETEST, TROUBLESHOOT AS REQUIRED IAW AMM 73-34-01.</P>)

Part: CEILING PANEL — OUT OF POSITION (CARGO BAY) · airframe 95,211 hrs · 19,249 cycles

SMOKE DETECTOR TUBE NOT PROTRUDING FROM CEILING ORIFICE IN FWD CARGO COMPARTMENT AT STA 500.(<P>REMOVED AND REINSTALLED FWD CARGO CEILNG PANEL AT STA 500 IAW AMM 25-52-02. SMOKE DETECTOR CONFIGURED CORRECTLY THROUGH CEILING PANEL.</P>)

Part: NOSE COWL — DENTED (NR 2 ENGINE) · airframe 95,211 hrs · 19,249 cycles

NR 2 NOSE COWL HAS INTERNAL DENTS 5-7 O'CLOCK (<P>REPAIRED NR 2 NOSE COWL (6 DENST) AT INTERNAL POSITION 5-7 IAW AMM SRM 54-15-01-2R REP 3 PAR 3</P>)

Part: BEARING — WORN (NR 2 COWLING) · airframe 95,211 hrs · 19,249 cycles

NR 2 ENG LT CORE COWL HOLD OPEN ROD ATTACH BEARING WORN. (<P>REPLACED NR 2 ENG LT CORE COWL HOLD OPEN ROD END BEARING IAW SRM 51-40-02. NO ADJUSTMENT DISTURBED.</P>)

Part: BEARING — WORN (NR 2 ENGINE) · airframe 95,211 hrs · 19,249 cycles

NR 2 ENG BEARING RT CORE COWL HOLD OPEN ROD ATTACH BEARING WORN. (<P>REPLACED NR 2 ENG CORE COWL HOLD OPEN ROD END BEARING IAW AMM 51-40-02. NO ADJUSTMENTS DISTURBED.</P>)

Part: START VALVE — OUT OF ALIGNMENT · airframe 95,211 hrs · 19,249 cycles

CARRY OUT BOTH ENG'S STARTER VALVE MANUAL OVERRIDE BUTTON ALIGN WITH C-DUCT MANUAL GUIDE TUBE. (<P>ADJUSTED BOTH ENGINES START VALVE TO ALINE THE MANUAL OVERRIDE BUTON AND C-DUCT GUIDE TUBE IAW AMM 80-11-62-404-017-H00</P>)

Part: LINE — LEAKING (NR 1 ENGINE) · airframe 95,211 hrs · 19,249 cycles

NR 1 ENG LT AF SIDE OIL LINE LEAKING. (<P>CLEANED AND FOUND OIL LINE LEAKING FROM CONTACT WITH CLAMP HARDWARE IAW AMM 72-00-00. REMOVED OIL LINE IAW AMM 20-11-00 AND SRM 51-40-02. LEAK CK ACCOMPLISHED ON T/E T2031 ITEM 2. ADJUSTED CLAMP USING INSTALLATION OF LINE.</P>)

Part: HEAT EXCHANGER — NOT REPORTED (AC BAY) · airframe 95,211 hrs · 19,249 cycles

REPLACED THE PRIMARY AND SECONDARY COOLING PACK HEAT EXCHANGERS(<P>R/R BOTH LT &AMP; RT PRIMARY AND SECONDARY HEAT EXCHANGERS IAW AMM 21-51-02 (VENDOR TO CLAEN)</P>)

Part: WIRE — CHAFED (NR 2 ENGINE) · airframe 95,211 hrs · 19,249 cycles

NR 2 ENG TRANSFER ANGLE GEARBOX 6:00 POS SEVERAL WIRE BUNDLES CHAFFING ON SHAFT. (<P>REPAIRED AND REPOSITIONED WIRE BUNDLES IAW SWPM 20-10-11.</P>)

Part: ELT — LOOSE · airframe 95,211 hrs · 19,249 cycles

CONTROL CABIN CORD FOR SECURING ELT TO RAFT IS TORN LOOSE FORM ELT LT SIDE OF CABIN. (<P>REMOVED AND REPLACED CONTROL ELT IAW AMM 25-63-03.</P>)

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 95,211 hrs · 19,249 cycles

ETOPS VERIFICATION FLIGHT ACCOMPLISHED, WXR RADAR FAIL.(<P>OPS CHECKED WXR SYSTEM IAW AMM 34-43-00. OPS CHECK GOOD AT THIS TIME.</P>)

Part: SMOKE DETECTOR — OUT OF ADJUST (CARGO BAY) · airframe 95,211 hrs · 19,249 cycles

SMOKE DETECTOR TUBE NOT PROTRUDING FORM CEILING ORIFICE IN FWD CARGO COMP STA 654 + 50 (<P>ADJUSTED SMOKE DETETCTOR IN FWD CARGO COMPARTMENT AT STAT 645 + 50 IAW AMM 26-05-03.</P>)

Part: BEARING — WORN (NR 2 ENGINE) · airframe 95,211 hrs · 19,249 cycles

NR 2 ENG COMPRESSOR SECTION 3:00 POS I/B AND ABOVE AIR/OIL HEAT EXCHANGER 1" SMALL&NBSP; ATTACH LINK HAS 2' WORN ROD END(<P>R/R NR 2 ENG HEAT EXCHANGER ATTACHE LINK ROD BEARING IAW AMM 51-40-02. NO ADJUSTMENT DISTURBED.</P>)

Part: ROD END — WORN (NR 2 ENGINE) · airframe 95,211 hrs · 19,249 cycles

NR 2 ENG COMPRESSOR SECTION 3:00 POS I/B OF AIR OIL HEAT EXCHANGER PNEUMATIC DUCT SUP ROD HAS WORN ROD ENDS.(<P>REPLACED ROD ENDS</P>)

Part: PLENUM — DAMAGED (HEAT EXCHANGER) · airframe 95,211 hrs · 19,249 cycles

AFTER REMOVAL OF LT HEAT EXCHANGER ASSEMBLY FOUND FOUR EACH ELONGATED MOUNT HOLES ON UPPER PART OF PLENUM(<P>R/R LT PLENUM IAW AMM 21-51-02.</P>)

Part: TUBE — CHAFED (NR 1 ENGINE) · airframe 95,211 hrs · 19,249 cycles

NR 1 ENG BLEED AIT TUBE LT SIDE 7 O'CLOCK POS CHAFED FROM CORE COWL (<P>REMOVED AND REPLACED NR 1 ENG BLEED AIR TUBE LT SIDE 7 O'CLOCK POSITION IAW AMM 72-24-03</P>)

Part: WIRE — DAMAGED (IGNITOR) · airframe 95,211 hrs · 19,249 cycles

"R ENG IGNITOR 2" STATUS MESSAGE.(<P>TRANSFERRED TO DMI 109050, MEL 74-00-01B. CAT: C, DUE 31MAR19. MCC NOTIFIED &AMP; PLACARD INSTALLED. DISP. JL @ 16:35Z.</P><P>REPINNED WIRE W66-62P-22 @ TB104 PIN XC2 IAW SWPM 20-90-11 $ WDM 74-31-21. PERFORMED ENGINE RUN IAW AMM 71-00-00 NO FAULTS NOTED. THIS CLEARS DMI 109050. PLACARDS REMOVED. MCC NOTIFIED DPI ST@0032Z. RT ENG IGNITOR OPS NORMAL.<BR /></P>)

Part: HF COMM — MALFUNCTIONED (RIGHT) · airframe 95,191 hrs · 19,242 cycles

AIR RETURN DUE TO HF RIGHT DID NOT TRANSMIT AND SAT DATALINK FAILED ON T/O, DATALINK LOST EICAS CAUTION MESSAGE.(<P><SPAN>PERFORMED&NBSP;</SPAN><SPAN>HF RADIO OPS TEST IAW FIM 23-11 F/T 804 AND AMM 23-11-00. HF RADIO TEST GOOD WAS ABLE TO TRANSMIT AND RECEIVE TO SFO GROUND 8.843. FOR DATA LINK,&NBSP;</SPAN>PERFORMED OPS CHECK IAW ASG AMM 23-25-00. OPS NORMAL NO DEFECTS NOTED AT THIS TIME.<BR /></P>)

Part: PUMP — INOPERATIVE (FUEL BOOST) · airframe 95,166 hrs · 19,234 cycles

RIGHT FWD FUEL PUMP INOP ETOPS 120 MINUTES RESTRICTED.(<P>TRANSFERRED TO MDDR 107257.<BR /></P><P>REF LOG PAGE 1053745 ITEM M4; REMOVED AND REPLACED RIGHT FWD BOOST PUMP IAW B767 AMM 28-22-03 AND PERFORMED OPS CHECK IAW B767 28-22-01/501. THIS CLEARS MDDR 107257.&NBSP;</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENGINE A/I) · airframe 95,162 hrs · 19,232 cycles

R ENG ANTI ICE EICAS, WITH SWITCH OFF.&NBSP;(<P>PERFORMED FIM 30-21 FT 805 MSG CLEARED, COULD NOT DUPLICATE FAULT. NO FURTHER ACTION NEEDED.&NBSP;</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 95,137 hrs · 19,224 cycles

STATUS MESSAGE CABIN ALT AUTO 2(<P>PERFORMED FIM 21-31 FT 810 BITE #2 CABIN PRESSURE CONTROLLER IAW AMM 21-31-00 NO FAULTS ARE DETECTED&NBSP;</P>)

Part: INDICATOR — INOPERATIVE (BLEED AIR SYS) · airframe 95,150 hrs · 19,228 cycles

LT BLEED AIR DUCT INDICATION INOP. REMOVED AND REPLACED DUAL DUCT INDICATOR ASSY IAW AMM 36-21-02-004 AND 36-21-02-404 OPS CHECK GOOD AT THIS TIME.

Part: UNKNOWN — UNKNOWN (COOLING SYSTEM) · airframe 95,069 hrs · 19,202 cycles

UNABLE TO COOL COCKPIT WITH BOTH PACK RUNNING&NBSP;(<P>PERFORMED ZONE CONTROL SYSTEM TEST IAW AMM 20-51-00 OPS CHECK GOOD</P>)

Part: EEC — INOPERATIVE (LT ENGINE) · airframe 95,081 hrs · 19,206 cycles

L ENG CONTROL EICAS AFTER LEFT ENGINE START(<P>REMOVED AND REPLACED LH EEC IAW 73-21-15 OPS CHECKS GOOD IAW AMM 71-00-00</P>)

Part: IDG — MALFUNCTIONED (LEFT) · airframe 95,057 hrs · 19,198 cycles

EICAS MESSAGE LEFT GEN OFF AFTER BLOCK OUT AND ENGINE START(<P>TRANSFER TO MDDR 106580 IAW MEL 24-00-01-01</P><P>LOG PAGE 1045563 ITEM M7; REMOVED AND REPLACED LEFT ENGINE IDG IAW AMM 24-11-01-004-001-024, OPS/LEAK CHECK IAW AMM 24-11-00-715-005. OPS CHECK GOOD,

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 95,029 hrs · 19,190 cycles

LEFT ENGINE CONTROL MESSAGE(<P>T/S IAW FIM 73 -21 F/T 878 NO FAULTS NOTED AT THIS TIME.<BR /></P>)

Part: UNKNOWN — MALFUNCTIONED (COCKPIT) · airframe 95,021 hrs · 19,187 cycles

APU COLD SOAK TEST FAIL APU FAULT EICAS 1345Z FL 380 SAT -52 MAX N1 376 EGT800*(<P>REFERENCE LOG PAGE 1045533 ITEM M4; PERFORMED APU BITE PROCEDURE PER FIM 49-11-00 FAULT TREE 958. NO FAULT FOUND. OPS CHECKED APU SEVERAL TIMES, NO DEFECTS NOTED. TRANSFERRED TO MDDR 106361 PER DDG 25-AP-01 CAT N&NBSP;</P>)

Part: UNKNOWN — MALFUNCTIONED (AC BAY) · airframe 95,016 hrs · 19,185 cycles

L PACK OFF &AMP; L PACK TEMP(<P>PERFIM 21-51 FT 803, NO FAULTS FOUND. PERFORMED FIM 21-51 FT 804, NO FAULTS FOUND, UNABLE TO DUPLICATE, OPS CKD GOOD</P>)

Part: A/C PACK — TRIPPED (AC BAY) · airframe 94,997 hrs · 19,179 cycles

LEFT PACK TRIPPED W/LEFT PACK TEMP EICAS MESSAGE&NBSP;(<P>PERFORMED LEFT PACK CONTROLLER BITE TEST REF. FIM 21-51 FT 872. ALL TEST PASS. NO FAULTS RECORDER , OK FOR SERVICE</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 94,976 hrs · 19,174 cycles

EICAS MSG L PACK TEMP(<P>PERFORMED FIM 21-51-TASK 877 AND NO FAULTS WERE FOUND. SYSTEM CHECK IS GOOD.<BR /></P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 94,959 hrs · 19,169 cycles

L PACK TEMP EICAS MSG DISPLAYED INTERMITTENTY(<P>PERFORMED FIM 21-51 FT 812 PACK CONTROLLER BITE PROC ( GND ) FIG 106 NO FAULTS OPS CHECK GOOD SYSTEM OK&NBSP;</P>)

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 94,779 hrs · 19,112 cycles

RADAR TILT NOT AGREEING WITH ITS TILT. OPS TEST GOOD IAW AMM 34-43-00-715-001-001.

Part: SWITCH — MALFUNCTIONED (COCKPIT) · airframe 94,748 hrs · 19,099 cycles

RT GENERATOR DRIVE LIGHT INOP. EXERCISED LEFT GENERATOR DISCONNECT SWITCH AND PERFORMED ENGINE RUNS. OPS CHECK GOOD IAW AMM 24-22-01. NO DEFECTS NOTED AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 94,736 hrs · 19,094 cycles

EICAS MESSAGE RT ENG HPSOV DISPLAYED. PERFORMED FIM 36-20 FT 804, CLEARED MESSAGE. RAN ENGINE AT IDLE FOR 5 MINS IAW AMM 71-00-00, COULD NOT DUPLICATE FAULT.

Part: SMOKE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 94,601 hrs · 19,047 cycles

AFT CARGO DET 1 STATUS MSG ON EICAS. MSG NOT ACTIVE AT BLOCK IN 26NOV18, TESTED CARGO AFT SMOKE DETECTOR IAW AMM 26-19-00. TEST OK, NO MSG, THIS CLEARS MDDR.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 94,572 hrs · 19,036 cycles

LEFT PACK TEMP EICAS PRIOR TO PUSH BACK. REMOVED AND REPLACED LT AIR CYCLE MACHINE IAW AMM 21-15-03. OPS CHECK GOOD AT THIS TIME.

Part: CONNECTOR — DIRTY (BLEED AIR SYS) · airframe 94,359 hrs · 18,958 cycles

DURING CLIMB OUT EICAS MSG RT ENG HPSOV ILLUMINATED FOR 30 SECONDS THEN STATUS MSG. RT ENG HPSOV ILLUMINATED REST OF FLIGHT. VERIFIED ELECTRICAL CONTINUITY OF RT HPSOV SYSTEM IAW WDM 36-11-62. NO FAULTS FOUND, CLEANED LIGHT DIRT FROM CONECTOR D17066P. AS PRECAUTIONARY CHANGED RT ENG AIR SUPPLY CONTROL CARD IAW AMM 36-11-12. BITE CHECK GOOD ITEM REMAINS OPEN PENDING OPERATIONAL TEST.

Part: SHUTOFF VALVE — NOT REPORTED (BLEED AIR SYS) · airframe 94,317 hrs · 18,945 cycles

REMOVED AND REPLACED HPSOV IAW AMM 36-11-07-024-001-001. LEAK CK GOOD AT THIS TIME.

Part: SHUTOFF VALVE — INOPERATIVE (BLEED AIR SYS) · airframe 94,317 hrs · 18,945 cycles

RT ENGINE HPSOV INOP. TRANSFERRED TO MDD 100176 IAW MEL 36-11-02-02.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 94,317 hrs · 18,945 cycles

STATUS MESSAGE APU FIRE LOOP 1. PERFORMED GROUND TEST FIRE DETECTION IAW AMM 26-11-00. MESSAGE ERASED, TEST PASS.

Part: CONNECTOR — UNSECURE (HMU) · airframe 94,303 hrs · 18,940 cycles

DURING PRE DEPARTURE LEFT ENG VALVE LIGHT ILLUMINATED. CYCLED LEFT ENG VALVE BREAKER AND SECURED CONNECTOR ON HMU IAW 73-00-00. OPS GOOD.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 94,217 hrs · 18,904 cycles

WXR SYS STATUS MSG. PERFORMED OPERATIONAL TEST OF WXR SYSTEM GOOD IAW AMM 34-43-00, NO DEFECT NOTED AT THIS TIME.

Part: DUCT — DAMAGED (CARGO BAY) · airframe 94,205 hrs · 18,899 cycles

AFT CARGO HEAT DUCT DAMAGE. REMOVED AND REPLACED AFT CARGO HEAT DUCT AT STA 1198 IAW AMM 21-40-01. OPS CHECK GOOD.

Part: SWITCH — DEFECTIVE (RT MLG) · airframe 94,063 hrs · 18,845 cycles

RIGHT GEAR INDICATOR INOP IN NORMAL POSITION IN FLIGHT. BITE PSEU REF AMM 32-09-04 NO FAULTS NOTED. REPLACED RT GEAR SWITCH REF AMM 23-11-60. WIRE REPAIR AND REPIN REF AMM 20-90-15 & WDM 33-16-15, OPS CHECK NORMAL.

Part: VALVE — FAULTY (TEMP SYSTEM) · airframe 94,034 hrs · 18,833 cycles

FLIGHT DECK TRIM AIR VALVE POSITION INDICATOR STICKS AT COLD. PERFORMED FLIGHT DECK VALVE POSITION INDICATOR TROUBLE SHOOTINGS PROCEDURES, VERIFIED NO COCKPIT OVERHEAD PANEL OR EICAS INDICATION OF VALVE MOVEMENT, VERIFIED VALVE OPERATION AND FULL TEMPERATURE SURGE IN COCKPIT PER FIM 21-64 FT 821. R&R FLT TRIM AIR VALVE IAW AMM 21-61-07, OPS CHECK GOOD AT THIS TIME. NO DEFECTS ON INDICATOR.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 93,950 hrs · 18,801 cycles

LT ENG BLEED OFF MESSAGE APPEARED AND WENT OUT ON DESCENT WITH POWER ON AND ON FINAL APPROACH. PERFORMED FIM TASK 36-20 FAULT TREE 804. NO FAULTS NOTED AT THIS TIME CHECKS GOOD AT THIS TIME.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 93,875 hrs · 18,773 cycles

STATUS MESSAGE CABIN ALT AUTO 2. PERORMED FIM 21-31 FAULT TREE 810 SHEET 1, NO FAULT FOUND.

Part: ROD — DAMAGED (NR 1 COWLING) · airframe 93,752 hrs · 18,728 cycles

NR 1 ENGINE COWLING FWD ROD DAMAGED. REMOVED AND REPLACED NR 1 ENGINE FAN COWL HOLD OPEN ROD IAW AMM 71-11-04.

Part: CLAMP — LOOSE (BLEED AIR SYS) · airframe 93,752 hrs · 18,728 cycles

PNEUMATIC CENTER ISOLATION VALVE LEAKING. FOUND LOOSE CLAMP. TIGHTENED LEAK CHECKED. NO LEAKS IAW AMM 36-11-01.

Part: UNKNOWN — MALFUNCTIONED (COCKPIT) · airframe 93,752 hrs · 18,728 cycles

RT PACK DID NOT SWITCH TO HIDE MODE WHILE PERFORMING TEST. RESET THE M864 IAW FIM 21-51 TASK 875. OPS CK NORMAL.

Part: GUARD — MISSING (COCKPIT) · airframe 93,752 hrs · 18,728 cycles

BATTERY SWITCH ON THE OVERHEAD PANEL, GUARD MISSING. REMOVED AND REPLACED BATTERY SWITCH GUARD IAW AMM 20-84-14.

Part: INDICATOR — BROKEN (COCKPIT) · airframe 93,752 hrs · 18,728 cycles

STAND BY ENGINE INDICATOR BITE SCREW BROKEN. REMOVED AND REPLACED STAND BY INDICATOR IAW AMM 77-41-01.

Part: CONTROL UNIT — FAULTY (APU) · airframe 93,750 hrs · 18,727 cycles

APU FAULT MSG, TWO ATTEMPTS, NO START. REMOVED AND REPLACED APU CONTROL UNIT IAW AMM 49-61-05-404-008.

Part: ECU — MALFUNCTIONED (APU) · airframe 93,750 hrs · 18,727 cycles

APU FAULT, EICAS AND APU FAULT LIGHT DURING ATTEMPTED START, APU WOULD NOT START. PERFORMED BIT TEST AND RE-SET ECU BOX - NO FAULT FOUND. PERFORMED THREE SUCCESSFUL STARTS IAW AMM 49-11-00, OPS CHECK GOOD AT THIS TIME.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 93,720 hrs · 18,716 cycles

AFTER LANDING/TAXI IN APU WOULD NOT START, APU FAULT EICAS, 2 ATTEMPTS. PERFORMED OPERATION TEST OF THE APU, OPS CHECK GOOD, NO DEFECTS NOTED AT THIS TIME PER AMM 49-11-00-802.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 93,690 hrs · 18,703 cycles

APU FAULT. PERFORMED APU BITE TEST. APU OPS CHECK SATISFACTORY NO APU FAULT PER AMM 49-05-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 93,653 hrs · 18,691 cycles

AFTER LANDING 2 ATTEMPTS TO START APU. GOT APU FAULT. RESTARTED APU AND OPS CK GOOD REF AMM 49-41-00.

Part: RADAR — MALFUNCTIONED (WEATHER SYSTEM) · airframe 93,642 hrs · 18,687 cycles

WEATHER RADAR HAS A DEAD SPOT, T/-5* OF CENTER, DOES NOT PAINT WEATHER OR GROUND. PERFORMED AN OPS CHECK OF THE RADAR SYSTEM. OPS CHECKED GOOD IAW AMM 34-43-00.

Part: ECU — MALFUNCTIONED (APU) · airframe 93,624 hrs · 18,680 cycles

ON LANDING, THE APU WOULD NOT START. REMOVED AND REPLACED THE ECU IAW IAW AMM 49-61-05, PERFORMED A BITE OF THE ECU IAW AMM 49-11 FT 958, NO MESSAGES OR FAULTS NOTED.

Part: CONTROL BOX — MALFUNCTIONED (APU) · airframe 93,640 hrs · 18,686 cycles

APU FAULTED ON START. RESET THE APU CONTROL BOX,. APU STARTED NORMAL IAW 49-41-10.

Part: APU — UNKNOWN · airframe 93,594 hrs · 18,671 cycles

APU WOULD NOT START AFTER LANDING. TWO ATTEMPTS, FAULT ON BOTH. PERFORMED A BITE TEST IAW FIM 49-11 FT 958. RAN APU THREE COMPLETED CYCLES WITH LOADS IAW AMM 49-11-01. NO FAULTS NOTED.

Part: APU — FAULTED · airframe 93,579 hrs · 18,666 cycles

APU FAULT ON LANDING. WOULD NOT START. ACCOMPLISHED AN APU BITE PROCEDURE IAW FIM 49-11 FT 958. NO FAULTS NOTED. CHECKED OK.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 93,538 hrs · 18,646 cycles

CABIN ALT AUTO 1 STATUS MESSAGE. PERFORMED AUTOMATIC CABIN PRESSURE CONTROLLER BITE TEST IAW AMM 21-31-00-705-001. NO FAULTS NOTED AT THIS TIME.

Part: MODULE — MALFUNCTIONED (APU) · airframe 93,538 hrs · 18,646 cycles

APU INOP ( ER OPERATIONS NOT ALLOWED ). REMOVED AND REPLACED FLOW SENSE MODULE ASSY IAW AMM 49-53-08. LEAK CHECK AND OPS CHECK GOOD DUCT PRESSURE INDICATION 25-30 PSI.

Part: FILTER — WARNING MESSAGE (LT ENGINE) · airframe 93,475 hrs · 18,620 cycles

LEFT ENGINE FUEL FILTER EICAS MESSAGE FOR 5 MINUTES DURING CLIMB OUT. NO SECONDARY INDICATIONS, STATUS MESSAGE REMAINED. REMOVED AND REPLACED THE LT ENGINE FUEL FILTER ELEMENT IAW AMM 73-11-02, OPS & LEAK CHECKED GOOD.

Part: FILTER — FAILED (RT ENGINE) · airframe 93,442 hrs · 18,607 cycles

RIGHT FUEL FILTER STATUS MESSAGE. REMOVED AND REPLACED THE RIGHT ENGINE FUEL FILTER IAW AMM 73-11-02. LEAK CHECKED OK. STATUS MESSAGE NO LONGER PRESENT.

Part: PNEUMATIC SYSTEM — INOPERATIVE (APU) · airframe 93,426 hrs · 18,602 cycles

APU NOT SUPPLYING PNEUMATICS.

Part: MODULE — MALFUNCTIONED (APU) · airframe 93,408 hrs · 18,593 cycles

APU FAULT MESSAGE DISPLAYED. INSPECTED APU INLET SCREEN, NO FINDINGS, CHECKED PRESSURE SUPPLY TUBE FOR THE SURGE CONTROL VALVE, NO FINDINGS IAW AMM 49-00-00, REMOVED AND REPLACED THE APU FLOW SENSING MODULE IAW AMM 49-53-08, OPS CHECKED GOOD.

Part: TRANSDUCER — MALFUNCTIONED (APU DUCT PRESS) · airframe 93,402 hrs · 18,590 cycles

APU INOPERATIVE. APU DUCT PRESSURE DROPPED OFF. IAW DDG 49-11-01A CAT LOG PAGE 947614 COMPLIED WITH ECM 2018P-529, AND REMOVED AND REPLACED TOTAL PRESSURE TRANSDUCER IAW AMM 49-56-02. APU OPS CHECKED IAW AMM 49-11-00. OPS CHECKED NORMAL.

Part: OIL SYSTEM — LOW (APU) · airframe 93,402 hrs · 18,590 cycles

APU FAULT ON EICAS. ADDED 1.5 QTS OF OIL TO APU IAW AMM 12-13-04. CLEARED APU CONTROL UNIT IAW AMM 49-61-05. RAN APU IAW AMM 49-11-00, OPS CHECKED GOOD, NO OIL LEAKS NOTED. APU FAULT CLEARED.

Part: INLET — CONTAMINATED (APU) · airframe 93,352 hrs · 18,573 cycles

DURING TAXI IN, APU WOULD NOT START AFTER 3 ATTEMPTS EICAS MESSAGE FOR APU FAULT WAS PRESENT. PERFORMED APU ECU BITE TEST ECU BITE SHOWED APU INLET DOOR START ONE ABORTED START 2 AND 3 FOUND DEICING FLUID IN APU INLET DOOR CLEANED S506 INLET DOOR OPEN SW STARTED APU 49-11-00 OPS CKS GOOD SEVERAL TIMES</P>)

Part: ISOLATION VALVE — MALFUNCTIONED (APU BLEED AIR) · airframe 93,350 hrs · 18,572 cycles

NO APU AIR PRESURE WITH APU RUNNING. RESEATING THE CIRCUIT BREAKER CLEARED THE MESSAGE. REACTIVATED CENTER ISOLATION VALVE IAW AMM 36-11-11. PNEUMATIC PRESSURE READS NORMAL.

Part: TRANSMITTER — MALFUNCTIONED (APU OIL QTY) · airframe 93,348 hrs · 18,571 cycles

APU OIL QUANTITY INDICATION INOPERATIVE. REMOVED AND REPLACED THE OIL QTY TRANSMITTER IAW AMM 49-94-04. OPS CHECKED GOOD.

Part: SENSOR — MALFUNCTIONED (LT A/C PACK) · airframe 93,348 hrs · 18,571 cycles

EICAS MESSAGE ON LANDING, LEFT PACK TEMP. REMOVED AND REPLACED THE LT COMPRESSOR OUTLET SENSOR IAW AMM 21-51-06, BITE CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT A/C PACK) · airframe 93,320 hrs · 18,562 cycles

LEFT PACK OVERHEAT MESSAGE ON FINAL DESCENT. PERFORMED A PACK TEMP CONTROLLER BITE TEST IAW 21-51-14, FOUND THE COMPRESSOR SENSOR FAULTED, CLEARED FAULT, RAN THE BITE TEST AGAIN, NO DEFECTS NOTED. GOOD FOR SERVICE.

Part: SENSOR — FAILED (LT A/C PACK) · airframe 93,323 hrs · 18,563 cycles

LEFT PACK TEMP EICAS. NO FOLLOW ON MESSAGE WHEN SWITCHED TO MANUAL, MESSAGE DISAPEARED. REMOVED AND REPLACED THE LEFT PACK COMPRESSOR OUTLET TEMP SENSOR IAW AMM 21-51-06, BITE TESTED GOOD IAW FIM 21-51, FT 803.

Part: CIRCUIT CARD — FAILED · airframe 93,323 hrs · 18,563 cycles

STATUS MESSAGE AFT EQUIPMENT EXHAUST FAN 2. REMOVED AND REPLACED AFT ECS CARD IAW SWPM 20-81-11. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (EXHAUST FAN) · airframe 93,320 hrs · 18,562 cycles

STATUS MESSAGE FOR AFT EQ EXHAUST FAN 2. PERFORMED FIM 21-26 F/T 808, BLOCK 1, MESSAGE CLEARED, NO FAULTS REMAIN. OPS CHECKED NORMAL.

Part: EXCITER — INOPERATIVE (LT ENGINE) · airframe 93,284 hrs · 18,550 cycles

DURING FIRST ATTEMPT, THE LEFT ENGINE START HAD NO EGT RISE, SECOND ATTEMPT SUCCESSFUL. NR 2 IGNITION ON THE LT ENGINE WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE LT NR 2 IGNITION EXCITER IAW AMM 74-11-01 AND REMOVED AND REPLACED THE LT NR 2 IGNITER IAW AMM 74-21-01 & OPS CHECKED GOOD.

Part: APU — INOPERATIVE (APU BAY) · airframe 93,280 hrs · 18,547 cycles

APU INOPERATIVE. REMOVED & REPLACED THE APU IAW AMM 49-11-01. OPS CHECKED GOOD. NO LEAKS DETECTED.

Part: APU — MALFUNCTIONED · airframe 93,273 hrs · 18,544 cycles

DURING TAXI, IN ATTEMPTED APU START, THE APU FAULT EICAS MESSAGE AND APU SHUTDOWN. PERFORMED AN APU ECU BITE TEST IAW 49-61-05. OPS CHECKED GOOD. NO FAULTS NOTED.

Part: SENSOR — MALFUNCTIONED (RT ENGINE) · airframe 93,231 hrs · 18,526 cycles

AT 4000 FT, AFTER DESCENT, WHEN POWER WAS COMING UP. THE RT ENGINE MADE BANGING SOUNDS WITH VIBRATION OFF THE SCALE. PERFORMED A BORESCOPE, NO DEFECTS NOTED AND PERFORMED FIM 71-05 FT 849. NO DEFECTS NOTED. PERFORMED A MAX POWER ASSURANCE TEST IAW MM 71-00-00, NO DEFECTS NOTED. OPS CHECKED GOOD. THE RIGHT ENGINE CIT SENSOR REMOVED AND REPLACED IAW AMM 73-21-02. ALL TESTED OK.

Part: WARNING MESSAGE — FALSE ACTIVATION (APU) · airframe 93,231 hrs · 18,526 cycles

APU FAULT. PERFORMED APU BITE TEST, NO FAULTS NOTED. APU OPS CHECK COMPLIED WITH, NO FAULTS NOTED. OPS GOOD IAW AMM 49-05-00

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 93,222 hrs · 18,522 cycles

UPON LANDING APU FAULTED TWICE AFTER START ATTEMPTS APU FAULT EICAS. PERFORMED APU BITE NO FAULTS NOTED, RAN APU NO FAULTS DETECTED REF AMM 49-05-00.

Part: MODULATING VALVE — FAULTY (CABIN TEMP) · airframe 93,190 hrs · 18,511 cycles

IN FLIGHT ADJUSTED FWD CABIN TEMPERATURE TO WARM. FWD CABIN TEMPERATURE EICAS. REMOVED AND REPLACED FWD CABIN TRIM AIR MODULATING IAW AMM 21-61-07. RESET CIRCUIT BREAKERS R24, R25, R27 OPS CHECK GOOD.

Part: CONTROLLER — MALFUNCTIONED (CABIN TEMP) · airframe 93,190 hrs · 18,511 cycles

FWD CABIN CLIMATE CONTROL INOPERATIVE. PERFORMED BITE CHECK ON ZONE CONTROLLER IAW FIM 21-61 FT 803, NO FAULTS FOUND. ZONE TEMP VALVE WORK NORMAL FOLLOWS SELECT SWITCH POSITION. CHECKED ON ECS PAGE IAW AMM 21-50-00,

Part: LIGHT — NO INDICATION · airframe 93,178 hrs · 18,506 cycles

AFTER MOVEMENT OF IGNITION SWITCH FROM AUTO TO GROUND, DID NOT OBSERVE VALVE LIGHT ILLUMINATE. ENGINE STARTED NORMAL. PERFORMED ENGINE MOTORING, IAW AMM 71-00-00, ALL INDICATIONS AND LIGHTS OPS CHECKED NORMAL, NO FAULTS FOUND.

Part: WARNING LIGHT — NO INDICATION · airframe 93,180 hrs · 18,508 cycles

AFTER MOVEMENT OF IGNITION SWITCH FROM AUTO TO GROUND, DID NOT OBSERVE A VALVE LIGHT ILLUMINATE, ENGINE START WAS NORMAL. PERFORMED MOTORING OF BOTH ENGINES IAW AMM 71-00-00. ALL INDICATIONS AND LIGHTS OPS CHECKED NORMAL. NO FAULTS FOUND.

Part: CONNECTOR — BROKEN (LT PACK VALVE) · airframe 93,178 hrs · 18,506 cycles

LEFT PACK VALVE CONNECTOR BACKSHELL CLAMP BROKEN. REPLACED THE BACKSHELL IAW AMM 20-00-09.

Part: SHUTOFF VALVE — MALFUNCTIONED (RT ENGINE) · airframe 93,178 hrs · 18,506 cycles

RIGHT ENGINE PRSOV DOES NOT FULLY OPEN. REMOVED AND REPLACED THE PRSOV, OPS CHECKED NORMAL IAW AMM 36-11-09.

Part: CONNECTOR — DAMAGED (TEMP CONTROL) · airframe 93,178 hrs · 18,506 cycles

LEFT PACK TEMP CONTROL VALVE BACKSHELL LOOSE. SECURED THE BACKSHELL IAW AMM 20-60-09.

Part: EXTRACTOR — CRACKED (RT A/C PACK) · airframe 93,178 hrs · 18,506 cycles

RIGHT PACK WATER EXTRACTOR IS CRACKED. REMOVED AND REPLACED THE WATER EXTRACTOR, OPS CHECKED OK IAW AMM 21-51-04.

Part: MODULE — ERRATIC (AIR SUPPLY) · airframe 93,178 hrs · 18,506 cycles

AIR SUPPLY BITE BOX GIVING ERRATIC INDICATIONS. REMOVED AND REPLACED THE AIR SUPPLY BITE MODULE, OPS CHECKED NORMAL IAW 36-23-04.

Part: SENSOR — FAILED (LT ENGINE) · airframe 93,178 hrs · 18,506 cycles

LEFT ENGINE FATS FAIL ASM CHECK. REMOVED AND REPLACED FAN AIR TEMP SENSOR IAW AMM 36-11-17.

Part: SWITCH — FAILED (SHUTOFF VALVE) · airframe 93,178 hrs · 18,506 cycles

RIGHT ENGINE HPSOV SWITCH BROKEN. REMOVED AND REPLACED THE HPSOV SWITCH IAW AMM 36-11-07.

Part: PRESSURE SWITCH — FAILED (BOOST PUMP) · airframe 93,019 hrs · 18,451 cycles

RIGHT WING AFT BOOST PUMP PRESSURE SWITCH LIGHT WAS INOPERATIVE. REPLACED THE FUEL BOOST PUMP PRESSURE SWITCH IAW AMM 28-42-01. OPS CHECK NORMAL.

Part: RADAR — MALFUNCTIONED (WX SYSTEM) · airframe 92,984 hrs · 18,439 cycles

WEATHER RADAR PANEL TILT SET TO +4, DISPLAYS TILT OF 0 ON NAVIGATIONAL DISPLAY. SECURED THE SWITCH. NORMAL OPS IAW AMM 27-50-00.

Part: SWITCH — UNSECURE (EMERGENCY LIGHTS) · airframe 92,984 hrs · 18,439 cycles

EMERGENCY LIGHT SWITCH ON OVERHEAD PANEL NOT SECURE. SECURED THE SWITCH, NORMAL OPS IAW AMM 27-50-10.

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 92,954 hrs · 18,426 cycles

CABIN ALTITUDE AUTO 2 STATUS MESSAGE DISPLAYED AFTER LANDING. PERFORMED TROUBLESHOOTING IAW FIM 21-31 F/T 810, SYSTEM CHECKED GOOD, MESSAGE CLEARED. OK FOR SERVICE.

Part: SHUTOFF VALVE — FAILED (LT ENGINE) · airframe 92,883 hrs · 18,396 cycles

L ENG HPSOV FAILED.(<DIV>PERFORMED FIM 36-10-00 FT 833 AND WIRE CHECKS IAW WDM 36-11-61. NO FAULTS NOTED AT THIS TIME.</DIV>)

Part: WIRE — DAMAGED (BLEED LIGHT) · airframe 92,883 hrs · 18,396 cycles

L ENG BLEED LIGHT ON.(<DIV>REMOVED AND REPLACED WIRE W5310-20-18 IAW WDM 36-11-61 AND SWPM 20-10-11, 20-30-11 AND 20-61-11. OPS CHECK GOOD IAW AMM 36-11-07.</DIV>)

Part: SHUTOFF VALVE — FAILED (LT ENGINE) · airframe 92,883 hrs · 18,396 cycles

L ENG HPSOV CAUTION EICAS INTERMITTENT ON AT REPEAT TAKEOFF LEVEL OFF DESCENT , L ENG HPSOV STATUS MSG ON AFTER TAKEOFF&NBSP;(<P>REMOVED AND REPLACED L ENG HPSOV REF AMM 36-11-07 , PERFORMED AIR SUPPLY CONTROL SYS. BITE CHECK REF AMM 36-23-00 BITE OK PASSED. LEAK CHECK OK</P>)

Part: CONTROL CARD — MALFUNCTIONED (LT ENGINE) · airframe 92,877 hrs · 18,393 cycles

L ENG HPSOV STATUS MSG ALSO L ENG HPSOV CAUTION MSG FOR 5 SECONDS AFTER TAKE OFF.(<P>RE-RACKED L ENGINE BLEED CONTROL CARD M859, OPS CHECK GOOD IAW B767 AMM 36-11-12 AND SWPM 20-82-13</P>)

Part: CIRCUIT CARD — MALFUNCTIONED (BLEED AIR) · airframe 92,857 hrs · 18,385 cycles

L ENG HPSOV EICAS&NBSP; MESSAGE AFTER TAKEOFF QRH PROCEDURE COMPLIED WITH. REMOVED AND REPLACED LH BLEED AIR CARD (M859) IAW AMM 36-11-12 PERFORMED OPS CHECKS ALL GOOD.

Part: FAN — FAILED (EQUIP COOLING) · airframe 92,857 hrs · 18,385 cycles

STATUS MESSAGE AFT EQ EXH FAN2. REPLACED #2 EXHAUST FAN PER AMM 21-58-41.

Part: MODULE — MALFUNCTIONED (APU) · airframe 92,855 hrs · 18,384 cycles

APU SURGING. REMOVED AND REPLACED SENSING MODULE IAW 49-53-08. ALSO FOUND GASKET FROM FLOW SENSOR DETERIORATED. INSTALLED NEW GASKET, PERFORMED OPS CHECK APU OK AND NO MORE SURGING.

Part: LINE — LOOSE (SHUTOFF VALVE) · airframe 92,852 hrs · 18,383 cycles

DURING CLIMB OUT, HAD A LEFT ENGINE HPSOV EICAS MESSAGE. PERFORMED FIM 36-10 ,FAULT TREE 833, BLOCK 1, 20, 40, ALSO PERFORMED REVERSE FLOW CHECK IAW AMM 36-11-00. FOUND AIR LINE AT HPSOV LOOSE. TIGHTEN FITTING. LEAK CHECKED OK. RAN LEFT ENGINE IAW AMM 71-00-00. HPSOV OPS CHECKED NORMAL.

Part: CONTROLLER — MALFUNCTIONED (SHUTOFF VALVE) · airframe 92,862 hrs · 18,387 cycles

REPEAT WRITE UP. AFTER T/O L ENG. HPSOV EICAS MSG, C/W QRH MSG REMAINED(<P>REMOVED AND REPLACED LH HPSOV CONTROLLER IAW AMM36-11-08.<BR /></P>)

Part: SHUTOFF VALVE — MALFUNCTIONED (LEFT ENGINE) · airframe 92,847 hrs · 18,382 cycles

DURING CLIMB, THE LT ENG HPSOV MESSAGE ILLUMINATED, MESSAGE WAS PRESENT ONLY DURING CLIMB THRUST. AFTER QRH, THE LT ENGINE BLEED OFF, LT ENGINE HPSOV CONTINUED TO DISPLAY DURING HIGH THRUST SETTINGS, CLEARED AT CRUISE THRUST. REMOVED AND REPLACED THE LT HPSOV IAW AMM 36-11-07. OPS & LEAK CHECKED.

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN ALTITUDE) · airframe 92,842 hrs · 18,380 cycles

STATUS MESSAGE FOR CABIN ALTITUDE AUTO 1. PERFORMED FIM 21-31 FT 803, NO FAULTS NOTED AT THIS TIME, STATUS MESSAGE CLEARED.

Part: WARNING MESSAGE — FALSE INDICATION (EXHAUST FAN) · airframe 92,825 hrs · 18,370 cycles

STATUS MESSAGE FOR THE AFT EQUIPMENT EXHAUST FAN NR 2. RESET THE CIRCUIT BREAKERS, OPS CHECKED GOOD AMM 20-60-01.

Part: CONTROL UNIT — MALFUNCTIONED (APU) · airframe 92,829 hrs · 18,373 cycles

APU CONTROL UNIT RPM LOW MALFUNCTIONED. REMOVED & REPLACED APU CONTROL UNIT IAW 49-61-05, OPS CHECKED GOOD

Part: FUEL CONTROL — MALFUNCTIONED (APU) · airframe 92,811 hrs · 18,361 cycles

APU INOP, SINGLE PACK SURGING LT OR RT. REMOVED AND INSTALLED NEW FUEL CONTROL UNIT APU IAW AMM 49-31-01. PERFORMED OPS CHECK. OPS CHECK GOOD AT THIS TIME. NO LEAKS AT THIS TIME.

Part: SHUTOFF VALVE — MALFUNCTIONED (LT ENGINE) · airframe 92,881 hrs · 18,395 cycles

L ENG HPSOV CAUTION EICAS INTERMITTENT ON AT REPEAT TAKEOFF LEVEL OFF DESCENT L ENG HPSOV STATUS MSG ON AFTER TAKEOFF(<DIV>REMOVED AND REPLACED&NBSP; L .ENG HPSOV REF AMM 36-11-07 PERFORMED AIRSUPPLY CONTROL SYSTEM BITE CHECK OK REF AMM 36-23-00 BITE OK PASSED LECK CHECK OK</DIV>)

Part: PIN — OUT OF POSITION (SHUTOFF VALVE) · airframe 92,741 hrs · 18,329 cycles

STATUS MESSAGE FOR THE LEFT ENGINE BLEED OFF. FOUND PRSOV LOCK OUT PIN NOT IN THE STOWED POSITION. STOWED THE PIN IN PRSOV IAW AMM 36-00-21, OPS CHECKED IAW AMM 36-11-07. PERFORMED ENGINE RUN IAW AMM 71-00-00.

Part: COUPLING — UNSECURE (PRECOOLER) · airframe 92,741 hrs · 18,329 cycles

DURING AN OPS CHECK OF THE FAN AIR VALVE FOUND BLEED LEAK ON THE NR 1 ENGINE. TROUBLESHOOTING AND FOUND THE PNEUMATIC DUCT BETWEEN THE PRECOOLER AND PRSOV LOOSE AT THE FLANGE COUPLING ABOVE THE PRECOOLER. SECURED THE FLANGE COUPLING IAW IAW AMM 36-11-01. OPS AND LEAK CHECKED GOOD.

Part: VALVE — FAILED (LT ENG BLEED) · airframe 92,741 hrs · 18,329 cycles

EICAS ILLUMINATED FOR THE LEFT ENGINE BLEED OVERHEAT. REMOVED AND REPLACED FAN AIR VALVE IAW AMM 36-11-16. OPS CHECKED GOOD.

Part: DUCT — LOOSE (BLEED) · airframe 92,739 hrs · 18,327 cycles

EICAS LEFT PACK OFF, LEFT ENGINE BLEED OFF, LEFT ENGINE BLEED OVERHEAT. ACCOMPLISHED THE CHECK LIST. SECURED A LOOSE DUCT ON LEFT ENGINE FAN AIR VALVE. NO OTHER LEAKS NOTED IAW AMM 36-11-15 AND 36-11-16.

Part: COUPLING — BACKED OUT (CHECK VALVE) · airframe 92,696 hrs · 18,308 cycles

APU SURGES WITH ONE PACK ON. PERFORMED FIM 36-10-00, AND 49-17-00. FOUND A LARGE AIR LEAK AT THE FWD PNEUMATIC GROUND AIR CONNECTOR CHECK VALVE. COUPLING HAD BACKED OFF AND THE CHECK VALVE HAD ROTATED FROM ALIGNMENT SLOTS. REINSTALLED THE CHECK VALVE AND COUPLING IAW AMM 36-11-03, LEAK AND OPS CHECKED OK.

Part: WARNING MESSAGE — FALSE ACTIVATION (COOLING FAN) · airframe 92,672 hrs · 18,299 cycles

AFT EQUIPMENT EXHAUST FAN NR 2 STATUS MESSAGE. PERFORMED AN OPS CHECK IAW AMM 21-58-00, MESSAGE CLEARED, OPS CHECKED NORMAL.

Part: CONTROL VALVE — MALFUNCTIONED (APU) · airframe 92,678 hrs · 18,301 cycles

BLEED DUCT PRESS SURGES FROM 0-20 PSI WITH APU SUPPLYING BLEED AND ONE PACK ON. REMOVED AND REPLACED SURGE CONTROL VALVE IAW AMM 49-50-30, LEAK CHECKED , NO LEAKS NOTED.

Part: SKIN — DAMAGED (BS 355-368) · airframe 92,575 hrs · 18,265 cycles

LOWER FUSELAGE SKIN DENTED AND GOUGED BETWEEN BS 355 - 368, STRINGERS 37 AND 38R. REPAIRED IAW SRM 53-00-01-2R-14.

Part: EXCITER — MALFUNCTIONED (NR 1) · airframe 92,467 hrs · 18,232 cycles

NO ENGINE START ON SINGLE IGNITER, LEFT ENGINE SWITCHED TO BOTH AND STARTED FINE. REMOVED AND REPLACED NR 1 ENGINE SYSTEM NR 1 EXCITER IGNITION BOX IAW AMM 74-11-01, OPS CHECKED GOOD IAW AMM 74-00-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT EEC) · airframe 92,370 hrs · 18,202 cycles

IN FLIGHT STATUS MESSAGE FOR THE RT ENGINE EEC C1. PERFORMED A NR 2 ENGINE RUN AND PERFORMED PIMU TEST IAW AMM 77-35-00. NO DEFECTS NOTED. OPS CHECKED GOOD.

Part: STATOR — DAMAGED (ALTERNATOR) · airframe 92,349 hrs · 18,196 cycles

STATUS MESSAGE RIGHT ENGINE EEC C1. REMOVED AND REPLACED THE RT ENG CONTROL ALTERNATOR STATOR AS PER AMM 73-21-08, RAN ENGINE OPS AND LEAK CHECKS OK. NO MESSAGES THIS CLEARS MEL 73-21-01&NBSP;</SPAN><BR DATA-MCE-BOGUS="1" /></P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 92,325 hrs · 18,188 cycles

STATUS MESSAGE RT ENGINE EEC C1. RAN RT ENGINE FOR TEN MINUTES COULD NOT DUPLICATE MESSAGE. PERFORMED BITE TEST ON RT ENGINE PIMU NO DEFECTS NOTED ON CH 1 OR CH 2 SWAPPED CHANNELS DURING RUN NO DEFECTS NOTED IAW AMM 71-00-00.

Part: FILTER — DIRTY (NR 1 IDG) · airframe 92,292 hrs · 18,175 cycles

NR 1 ENGINE IDG FILTER DIFFERENTAL PRESSURE INDICATOR POPPED. REMOVED AND REPLACED SCAVENGE FILTER AND PERFORMED LEAK CHECK IAW AMM 24-11-02. OPS CHECKED OK.

Part: FAN — FAILED (NR 2 EXHAUST) · airframe 92,271 hrs · 18,168 cycles

STATUS MESSAGE FOR THE AFT EQUIPMENT EXHAUST FAN NR 2. REMOVED AND REPLACED THE NR 2 AFT EQUIPMENT COOLING FAN IAW AMM 21-26-01. OPS CHECKED GOOD, LEAK CHECKED GOOD.

Part: CHARGER — FAILED (APU BATTERY) · airframe 92,250 hrs · 18,161 cycles

EICAS MESSAGE FOR AN APU FAULT APPEARED ON START ATTEMPT AFTER LANDING. REMOVED AND REPLACED APU BATTERY IAW AMM 24-31-04 AND BATTERY CHARGER IAW AMM 24-31-05.

Part: PANEL — INOPERATIVE (WINDOW HEAT) · airframe 92,241 hrs · 18,158 cycles

WINDOW HEAT SWITCH LIGHT INOPERATIVE. REPLACED THE RT WINDOW HEAT PANEL ASSY IAW AMM 30-41-00, OPS CHECKED GOOD.

Part: WARNING LIGHT — ILLUMINATED · airframe 92,241 hrs · 18,158 cycles

APU FAULT LIGHT ILLUMINATED WHEN START ATTEMPTED APU DID NOT START. DID BITE CHECK OF ECU AND STARTED APU NORMALLY IAW AMM 49-11-00 FAULT TREE 958 FIM OPS CHECKED GOOD.

Part: FAULT LIGHT — FALSE ACTIVATION (APU) · airframe 92,107 hrs · 18,110 cycles

AFTER APU START, A FAULT ILLUMINATED LANDING. NO FAULTS FOUND AFTER OPS CHECK IAW AMM 49-11-00

Part: ECU — FAULTED (APU) · airframe 92,069 hrs · 18,096 cycles

APU FAULT ANNUNCIATED. R & R THE ECU IAW 49-61-05. OPERATIONAL CHECKED NORMAL.

Part: APU — UNDERSERVICED · airframe 92,046 hrs · 18,089 cycles

APU DID NOT START AFTER LANDING. SERVICED THE APU IAW AMM 12-13-04, APU OPS CHECKED NORMAL IAW AMM 49-11-00.

Part: UNKNOWN — VIBRATION (NR 2 ENGINE) · airframe 91,862 hrs · 18,024 cycles

NR 2 ENGINE VIBRATION FAN REACHED 3.0 IN STABLE CLIMB. NO EICAS MESSAGE NOTED. INSPECTED THE FAN BLADES, INTAKE, AND EXHAUST. NO DEFECTS NOTED .OPENED ENGINE AND INSPECTED. NO DEFECTS NOTED IAW 77-31-00, AND 71-00-00.

Part: CONTROLLER — FAILED (NR 2) · airframe 91,728 hrs · 17,981 cycles

STATUS MESSAGE FOR CABIN ALTITUDE AUTO 2. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER NR 2 IAW AMM 21-31-02.

Part: ACTUATOR — INOPERATIVE (OUTFLOW VALVE) · airframe 91,715 hrs · 17,976 cycles

CABIN AUTO INOPERATIVE EICAS. FOLLOWED FIM 21-31 FT 806 TO BLOCK 42, R & I OUTFLOW VALVE ACTUATOR IAW AMM 21-31-04, OPS CHECKED AND BITE CHECKED GOOD.

Part: STATUS MESSAGE — FALSE INDICATION (CABIN PRESSURE) · airframe 91,706 hrs · 17,974 cycles

CABIN ALT AUTO 1 STATUS MESSAGE DISPLAYED, PERFORMED BITE ON NR 1 CABIN PRESSURE CONTROLLER. NO FAULTS PRESENT. RESET CONTROLLER. OPS CHECK NORMAL, MESSAGE CLEARED REF AMM 21-31-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 91,677 hrs · 17,968 cycles

CABIN ALTITUDE 1 STATUS MESSAGE. PERFORMED BITE TEST ON THE NR 1 CABIN PRESSURE CONTROLLER, NO FAULTS. PERFORMED AN OPERATIONAL TEST, OK IAW AMM 21-31-00199.

Part: WARNING LIGHT — FALSE ACTIVATION (FIRE DETECTOR) · airframe 91,533 hrs · 17,927 cycles

MAIN DECK CARGO FIRE DETECTOR B3 ILLUMINATED AMBER (FAILED). PERFORMED OPS CHECK IAW MM 26-14-00. INDICATION CLEARED, OPS CHECKED NORMAL.

Part: START VALVE — FAILED (RIGHT) · airframe 91,471 hrs · 17,908 cycles

RIGHT START VALVE FAILED TO OPEN DURING START, MANUALLY OPENED START VALVE. REMOVED AND REPLACED THE START VALVE IAW AMM 80-11-02. OPS CHECKED NORMAL, NO FAULTS NOTED.

Part: CLAMP — BROKEN (NR 1 OIL SUMP) · airframe 91,248 hrs · 17,843 cycles

NR 1 ENGINE OIL SUMP TUBE HAS A BROKEN CLAMP. REPLACED THE CLAMP IAW AMM 79-21-09-400-801-H00.

Part: ELT — DAMAGED (COCKPIT) · airframe 91,248 hrs · 17,843 cycles

COCKPIT ELT DAMAGED. REMOVED AND REPLACED THE ELT IAW AMM 25-03-00.

Part: TAPE — MISSING (OIL SUMP) · airframe 91,248 hrs · 17,843 cycles

ENGINE OIL SUMP TUBE WITH TAPE MISSING BY THE CLAMP. REPLACED THE TAPE IAW AMM 79-21-09. OK FOR SERVICE.

Part: IGNITER — INOPERATIVE (LT ENGINE) · airframe 91,160 hrs · 17,816 cycles

LEFT ENGINE DID NOT START ON 2 ATTEMPTS, LT ENGINE IGNITOR 2/1 STATUS MESSAGE. REPLACED TWO. IGNITORS IAW AMM 74-21-02, OPS CHECKED NORMAL.

Part: RELAY — FAILED (IGNITION) · airframe 91,160 hrs · 17,816 cycles

LEFT ENGINE IGNITOR 1 STATUS MESSAGE. REPLACED RELAYS K158 AND K159 IAW WDM 74-31-01. OPS CHECKED NORMAL.

Part: IGNITION SYS — MALFUNCTIONED (LT ENGINE) · airframe 91,142 hrs · 17,811 cycles

LEFT ENGINE DID NOT START, ATTEMPTED TWICE. STATUS MESSAGE DISPLAYED LEFT ENGINE IGNITION SYS 2 AND 1. RESET IGNITION CIRCUIT BREAKER, OPS CHECK NORMAL IAW AMM 74-11-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENGINE) · airframe 91,089 hrs · 17,795 cycles

LEFT ENGINE EXPERIENCED HUNG START STATUS MESSAGE L ENGINE IGNITOR 2 COMPLIED WITH QRH PROCEDURE , NORMAL START CLEARED STATUS MESSAGE, NO MESSAGES PRESENT AFTER ARRIVAL , NO FAULTS ON L PIMU, NO FAULTS ON GROUND TEST OF PIMU IAW AMM 77-35-00 , PERFORMED OPS CHECK OF IGNITION CONTROL SYSTEM AND IGNITERS IAW AMM 74-00-00, NO FAULTS .

Part: ANTI-ICE VALVE — FAULTY (RT ENGINE) · airframe 91,101 hrs · 17,799 cycles

RIGHT ENGINE ANTI ICE VALVE FAIL EICAS MESSAGE. REMOVED AND REPLACED SERVICEABLE ANTI ICE VALVE PER AMM 30-21-03.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT A/C PACK) · airframe 91,018 hrs · 17,773 cycles

RT PACK OFF EICAS AFTER SELECTING APP MODE. PERFORMED RT PACK TEMP CONTROL BITE TEST IAW AMM 21-51-14, ALL SYSTEM GO, OPS NML.

Part: WARNING LIGHT — FALSE ACTIVATION (RT A/C PACK) · airframe 91,028 hrs · 17,776 cycles

RIGHT PACK OFF EICAS AFTER SELECTING APPROACH MODE AND PASSING 1500'AGL. PERFORMED BITE TEST ON PACK CONT, NO FAULTS PRESSENT MCDP SHOWS NO FAULTS, TEST 30-40 CHECK NORMAL. NO FAULTS PRESENT IAW AMM 21-51-00 AND 22-00-02.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 90,945 hrs · 17,751 cycles

EICAS STATUS MESSAGE FOR CABIN ALT AUTO 2. REMOVED AND REPLACED CABIN PRESSURE CONTROLER.

Part: WARNING SYSTEM — ACTIVATED · airframe 90,947 hrs · 17,752 cycles

DURING APPROACH AT 3000FT, WHEN APP MODE SELECTED, A PWR TRANSFER,LOAD SHED EVENT OCCURS. EICAS RT PACK OFF, AUDIBLE ALARM HEARD, BEEPING FOR A COUPLE SECONDS. PERFORMED A BITE TEST ON PACK CONTROLLER, NO FAULTS PRESENT, MCDP SHOWS NO FAULTS, TEST 30/40 CHECKED NORMAL. NO FAULTS PRESENT IAW AMM 21-51-00-22-00-02.

Part: A/C PACK — MALFUNCTIONED (RIGHT) · airframe 90,894 hrs · 17,736 cycles

RT PACK CYCLED OFF & ON DURING APPROACH AT 4000 FT, EICAS RT PACK OFF. PERFORM A PACK TEMP CONTROL BITE TEST, NO FAULTS FOUND. RT PACK OPS NORMAL IAW AMM 21-51-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 90,760 hrs · 17,697 cycles

STATUS MESSAGE FOR CABIN ALT AUTO 1. PERFORMED FIM PROCEDURE 21-31 FAULT TREE 809 RESET FAULT OPS CHECK OK.

Part: CIRCUIT BREAKER — MALFUNCTIONED (APU AIR) · airframe 90,751 hrs · 17,694 cycles

NO APU PNEUMATIC AIR OUTPUT. CYCLED THE CIRCUIT BREAKER AND PERFORMED BITE TEST OPS CHECK NORMAL IAW 49-11-00 FAULT TREE 958, NO FAULTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 90,753 hrs · 17,695 cycles

EICAS MESSAGE CABIN AUTO INOPERATIVE , COMPLIED WITH QRH PROCEDURE AND ACCOMPLISHED FIM PROCEDURE FIM TASK 21-31 FT 803 SYSTEM OK , NO FAULTS NOTED.

Part: SWITCH — DAMAGED (STARTER) · airframe 90,734 hrs · 17,689 cycles

LEFT STARTER SWITCH WILL NOT AUTOMATICALLY CUTOUT BACK TO AUTO AFTER ENGINE START. REMOVED AND REPLACED LEFT START SWITCH IAW AMM 80-11-51, OPS CHECKED OK.

Part: AOA — MALFUNCTIONED · airframe 90,450 hrs · 17,604 cycles

UPON START UP EICAS " L AOA PROBE " SHUT ENGINES DOWN. RESET CIRCUIT BREAKER LEFT AOA IAW MM 30-32-00, OPS CHECKED NORMAL.

Part: INDICATOR — INOPERATIVE (AIR VALVE) · airframe 90,349 hrs · 17,573 cycles

FLIGHT DECK TRIM AIR VALVE POSITION INDICATOR BACK LIGHT INOPERATIVE. REMOVED AND REPLACED TRIM AIR VALVE INDICATOR. OPS CHECKED GOOD IAW 21-61-00.

Part: SENSOR — MALFUNCTIONED (N2 SPEED) · airframe 90,527 hrs · 17,627 cycles

LEFT N2 ERRATIC BELOW 20% AT START. REMOVED AND REPLACED THE NR 1 ENGINE N2 SPEED SENSOR IAW AMM 77-12-02. OPS CHECKED NORMAL.

Part: BLOWER — DEFECTIVE (CARGO BAY) · airframe 89,962 hrs · 17,468 cycles

AFT CARGO FAN EICAS MESSAGE MAINTENANCE. R & R AFT CARGO NR 1 BLOWER, M718, IAW AMM 26-16-02. OPS CK NORMAL.

Part: VALVE — MALFUNCTIONED (APU) · airframe 89,855 hrs · 17,442 cycles

WITH PACKS ON APU SURGES. R & R APU SURGE VALVE IAW AMM 49-53-01. OPS CHECK NORMAL.

Part: FILTER — MALFUNCTIONED (SURGE VALVE) · airframe 89,814 hrs · 17,432 cycles

FOUND APU BLEED PRESSURE DUCT PRESSURE SURGES. REMOVED AND REPLACED SURGE VALVE FILTER. OPS CHECKED NORMAL IAW AMM 49-53-06.

Part: MODULE — INOPERATIVE (APU) · airframe 89,743 hrs · 17,415 cycles

INTERMITTENT , NO DUCT PRESSURE FROM APU. REPLACED FLOW SENSING MODULE IAW AMM 49-53-08. OPS CHECKED NORMAL.