N1709A

Part: UNKNOWN — VIBRATION (ZONE 700) · airframe 104,357 hrs · 25,623 cycles

ON TAXI OUT, RIGHT GEAR SHAKING. ABORTED TAKE-OFF. (ATO). PERFORMED AIRCRAFT TAXI WITH FLIGHT CREW ASSISTANCE. NO ABNORMAL VIBRATIONS NOTED PER AMM 71-00-00 AND 09-21-00. A/C OK FOR SERVICE.

Part: LINK — DAMAGED (ZONE 700) · airframe 104,357 hrs · 25,623 cycles

DURING TAXI, AIRCRAFT VIOLENTLY SHAKING FROM RT MAIN LANDING GEAR STRUT. A/C RETURNED TO BLOCKS. (BTB). T/S LED TO RMLG UPPER AND LOWER TORSION LINKS. REMOVED OLD, THEN INSTALLED NEW LOWER AND UPPER R MLG TORSION LINKS PER AMM 32-11-22, REF LP 39269-53/3. AFTER REPLACEMENT, CONDUCTED TAXI PER ABX ERU/TAXI CHECK LIST AND AMM 71-00-00, NO SHAKING IN AIRFRAME OR TILLER. NO FURTHER ACTION REQUIRED. AIRCRAFT RETURNED TO SERVICE. (MLG TORSION LINK ASSY'S) PARTS: LWR PN: 161T1140-7, SN: BFG5195HSM UPR PN: 161T1140-7, SN: BFG1974HSM

Part: SEQUENCE VALVE — INOPERATIVE (ZONE 700) · airframe 104,006 hrs · 25,491 cycles

GEAR DOOR S EICAS MESSAGE AFTER TAKEOFF ,WHEN GEAR LEVER WAS MOVE FROM UP TO OFF. LIGHT WENT BLUE AFTER ACCOMPLISH (GEAR DISSAGREE ) QRH NNC.14.17. FINISHED FLIGHT AND LANDED WITH NO OTHER COMPLICATIONS.MTX GROUNDED A/C . PERFORMED ADJUST OF RT MLG UPLOCK RELEASE IAW 32-35-00. UPLOCK RELEASE CRANK, UPLOCK HOOK GAP CLEARANCE ADJ. FROM .200" TO .245". REPLACED RT MLG DOOR LATCH ACTR IAW AMM 32-32-13. TESTED GOOD. PERFORMED GEAR SWINGS IAW AMM 32-32-00, 10 X. SUCCESSFUL WITH PROPER INDICS. NO FAULTS NOTED. DURING EVAL FLT WHEN GEAR HANDLE FROM UP TO OFF RT MLG FELL OUT OF WHEEL WELL. REPLACED RT MLG OPS SEQUENCING VALVE IAW AMM 32-32-08, GEAR SWING GOOD. EVAL FLT SATISFACTORY. ACFT RETURNED TO SERVICE.

Part: PANEL — DEPARTED (ZONE 100) · airframe 103,602 hrs · 25,332 cycles

ON MAINTENANCE POST FLIGHT INSP, FOUND ON RT WING TO FUSELAGE PANEL MISSING 196CR. MAINTENANCE INSTALLED RT WING TO FUSELAGE PANEL 196CR IAW AMM 20-11-00. AIRCRAFT RETURNED TO SERVICE.

Part: LOCK — BROKEN (ZONE 800) · airframe 103,510 hrs · 25,298 cycles

DURING TAXI OUT, MAIN CARGO DOOR SILL"L" LOCK SPRING BROKEN. 2ND FROM AFT TO FWD. P/N 57963-101 AT STA 588 LBL 88.50. POSITION A3L RESTRICTED TO 6595 LBS. AIRCRAFT RETURNED TO BLOCKS (BTB). MAINTENANCE DEFERRED IAW ABX-25-58-1A AND RETURNED AIRCRAFT TO SERVICE.

Part: START VALVE — MALFUNCTIONED · airframe 103,002 hrs · 25,108 cycles

DURING TAXI WHILRE STARTING #2 ENG. IT FAILED TO START. A/C RETURNED TO THE GATE(BTB0 AND MTX GROUNDED A/C MTX DEFERRED RH START VALVE IAW MEL ABX-80-00-2-1. FOR DEPARTURE AND RETURNED A/C TO SERVICE.

Part: TRANSCEIVER — MALFUNCTIONED (ZONE 100) · airframe 102,727 hrs · 25,006 cycles

"DURING TAXI CREW REPORTED LEFT COMM INOP , A/C RETURNED TO GATE (BTB) AND MTX GROUNDED A/C , MTX TROUBLESHOT AND REMOVED & REPLACED LH VHF COMM XCVR IAW B767 AMM 23-12-01. OPS CHECK GOOD. TOWER READS LH VHF COMM 5X5.AND RETURNED A/C TO SERVICE .

Part: WARNING MESSAGE — FALSE ACTIVATION (ZONE 300) · airframe 102,636 hrs · 24,971 cycles

DURING TAXI OUT RUDDER RATIO MSG ON AFTER ENGINE START, AC RETURNED TO THE GATE (BTB) AND MTX GROUNDED AC , MTX B767 FIM 27-09 FT 803. MESSAGE EXTINGUISHED OK FOR SERVICE. AIRCRAFT REMAINS NO ETOPS.AND RETURNED AC TO SERVICE

Part: PITOT HEAD — MALFUNCTIONED (ZONE 100) · airframe 102,487 hrs · 24,911 cycles

"DURING CLIMBOUT ABOUT 4000' WE GOT AN A/S DISAGREE EICAS MSG WITH A 6-7 HT DIFFERENCE BETWEEN CAPT + STBY. FO + STBY AGREED, THEN AROUND 13000-14000 WE GOT AN ALT DISAGREE MSG, I SWITCHED AIRDATA SW TO ALT AND EVERYTHING WENT BACK TO NORMAL, TILL 17500, CONTINUED CLIMB TO 370 AND THE DIFFERENCE BETWEEN ALTIMETERS TO 800' AND A/S 20KTS. DURING CLIMB TO 370 STARTED GETTING INTERMITTENT AILERON LOCKOUT + RUDDER RATIO EICAS . (ATB)AC RETURNED TO FIELD AND LANDED ,MTX GROUNDED AC REMOVED AND REPLACED RIGHT LOWER PITOT PROBE, REF B767 AMM 34-11-01. LEAK & HEAT CHECKS, GOOD. IARCRAFT REMAINS RYSM COMPLIANT.LP: 39041-27/1 MTX RETURNED AC TO SERVICE. "

Part: BEAR STRAP — CRACKED (ZONE 200) · airframe 102,454 hrs · 24,897 cycles

FORWARD SERVICE DOOR CUTOUT AFT LOWER CORNER WITH THREE CRACK INDICATIONS AT RIGHT SIDE IN HOLE #5 ON THE SKIN AND BEAR STRAP, REPAIR IA W TASK CARD 6753A937, PART 2, STEP 8, SRM 53-10-01-2R-1.(<P>FORWARD SERVICE DOOR CUTOUT AFT LOWER CORNER WITH THREE CRACK INDICATIONS AT RIGHT SIDE IN HOLE #5 ON THE SKIN AND BEAR STRAP, CRACK WAS REPAIRED IAW EO 6753A937, PART 2, STEP 8 REV. 1 17MAY24 AND SRM 53-10-01-2R-1 FIG. 201, REV. 126 15AUG24.</P>)

Part: FUEL TANK — LEAKING (ZONE 100) · airframe 102,454 hrs · 24,897 cycles

FUEL LEAK CENTER TANK AT LBL 60 AND STGR L-11(<P>FUEL LEAK CENTER TANK AT LBL 60 AND STGR L-11, THE SEALANT WAS REMOVED WHERE THE FUEL LEAK WAS FOUND, IT WAS CLEANED PROPERLY, THE SEALANT WAS APPLIED CORRECTLY. THE FUEL LEAK WAS REPAIRED. THE FUEL LEAK TEST WAS SATISFACTORY.</P>)

Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 102,454 hrs · 24,897 cycles

RH WING LOWER SKIN, CORROSION ON SKIN AT REAR SPAR LOWER CHORD BTWN W. STA 879.2 AND 906.2.(<P>RH WING LOWER SKIN, CORROSION ON SKIN AT REAR SPAR LOWER CHORD BT WN W. STA 879.2 AND 906.2. REPAIR BY LOWER SKIN CORROSION BETWEEN REAR SPAR AND WSTA 906 AT RH WING IAW CMA-TLS-24-0186 &AMP; TRE6757264 REV 1 ISSUED DATE AUG 22,2024. FAA FORM 8100-9 AUGUST 27, 2024. CORROSION LEVEL 2.</P>)

Part: SKIN — CRACKED (ZONE 200) · airframe 102,454 hrs · 24,897 cycles

FORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER WITH A CRACK INDICATION AT LEFT SIDE IN HOLE #4 ON THE SKIN, TWO CRACK INDICATIONS AT LEFT SIDE IN HOLE #5 ON THE SKIN AND BEAR STRAP, REPAIR IAW TASK CARD 6753A937, PART 1, STEP 8, SRM 53-10-01-2R-1.(<P>FORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER WITH A CRACK INDICATION AT LEFT SIDE IN HOLE #4 ON THE SKIN, TWO CRACK INDICATIONS AT LEFT SIDE IN HOLE #5 ON THE SKIN AND BEAR STRAP, CRACKS WERE REPAIRED IAW EO 6753A937, PART 1, STEP 8 REV. 1 17MAY24 AND SRM 53-10-01-2R-1 FIG. 201 REV. 126 15 AUG 24.</P>)

Part: FUEL CELL — LEAKING (ZONE 100) · airframe 102,454 hrs · 24,897 cycles

RH AND LH WING DRY BAY, FUEL LEAK BETWEEN BAY BARRIER AND RIB 8 W.STA 375.8.(<P>FUEL LEAK WAS REPAIRED &AMP; THE SEALANT WAS APPLIED CORRECTLY IAW AMM 28-11-00-308-013. NO FURTHER DEFECTS NOTED</P>)

Part: ELT — NO TEST (ZONE 200) · airframe 102,454 hrs · 24,897 cycles

FIXED EMERGENCY LOCATOR TRANSMITTER TEST FAIL.(<P>FIXED EMERGENCY LOCATOR TRANSMITTER WAS REPLACED IAW AMM 23-24-01-020-801. OPERATIONAL TEST RESULT WAS SUCCESSFULLY.</P>)

Part: KEELBEAM — CORRODED (ZONE 100) · airframe 102,454 hrs · 24,897 cycles

KEEL BEAM, BETWEEN STA 1021 TO 1065 BEAM, RH SIDE WITH CORROSION(<P>KEEL BEAM, BETWEEN STA 1021 TO 1065 BEAM, RH SIDE WITH CORROSION. THE CORROSION WAS REWORKED AND EVALUATED AND IT WAS FOUND TO BE WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 53-50-12-1A-1</P>)

Part: FUEL TANK — LEAKING (ZONE 100) · airframe 102,454 hrs · 24,897 cycles

FUEL LEAK RH TANK, BETWEEN WS 404.4 AND 433.1 AT STGR L-10(<P>FUEL LEAK RH TANK, BETWEEN WS 404.4 AND 433.1 AT STGR L-10, THE SEALANT WAS REMOVED WHERE THE FUEL LEAK WAS FOUND, IT WAS CLEANED PROPERLY, THE SEALANT WAS APPLIED CORRECTLY. THE FUEL LEAK WAS REPAIRED IAW AMM 28-11-00-308-013. THE FUEL LEAK TEST WAS SATISFACTORY</P>)

Part: FIRE SEAL — MISSING (THRUST REVERSER) · airframe 102,454 hrs · 24,897 cycles

ENG 1, OUTBOARD THRUST REVERSE, NAC STA 195.50 + 7", LOWER BIFURCATION, COVER FIRE SEAL MISSING.(<P>ENG 1, OUTBOARD THRUST REVERSE, NAC STA 195.50 + 7", LOWER BIFURCATION, COVER FIRE SEAL MISSING. THE DAMAGED SEAL PART WAS REMOVED AND THE SE AL WAS REPAIRED IAW AMM 78-00-00-308-H00. NO FURTHER DEFECTS NOTED</P>)

Part: ACCESS PANEL — LEAKING (ZONE 600) · airframe 102,454 hrs · 24,897 cycles

RH WING LOWER SURFACE. FUEL LEAK ON FUEL ACCESS PANEL BTWN RIB 11 AND 12.(<P>&NBSP;FUEL STICK WAS REPLACED IAW AMM 28-44-01-404-033. NO FURTHER DEFECTS NOTED</P>)

Part: SMOKE DETECTOR — DIRTY (ZONE 100) · airframe 102,454 hrs · 24,897 cycles

ZONE 100, LOWER HALF FUSELAGE, FWD AND AFT CARGO COMPARTMENTS VERY DIRTY ALL CARGO SMOKE DET AIR SAMPLING ORIFICES.(<P>LOWER HALF FUSELAGE, FWD AND AFT CARGO COMPARTMENTS, THE SMOKE DET AIR SAMPLING ORIFICES WERE CLEANED IAW AMM 26-16-00-100-804-001 &AMP; TLS 654, REV 142, APR 22, 2024</P>)

Part: SPLICE — LEAKING (ZONE 100) · airframe 102,454 hrs · 24,897 cycles

RH WING, LOWER SIDE OF BODY SPLICE PLATES, AT RBL 97.95 AND BETWEEN STRINGER L-14 AND L-16 WITH EVIDENCE OF FUEL LEAKAGE(<P>RH WING, LOWER SIDE OF BODY SPLICE PLATES, AT RBL 97.95 AND BETWEEN STRINGER L-14 AND L-16 WITH EVIDENCE OF FUEL LEAKAGE. THE SEALANT WAS REMOVED WHERE THE FUEL LEAK WAS FOUND, IT WAS</P> / <P>CLEANED PROPERLY, THE SEALANT WAS APPLIED CORRECTLY. THE FUEL LEAK WAS REPAIRED. THE FUEL LEAK TEST WAS SATISFACTORY IAW AMM 28-11-00-308-013 REV 143 22AUG24.</P>)

Part: FUEL — LEAKING (ZONE 600) · airframe 102,454 hrs · 24,897 cycles

RH WING LOWER SKIN, FUEL LEAK AT STG L-10 BTWN W.STA 284.7 AND 375.8. (RIB 5-8)(<P>RH WING LOWER SKIN, FUEL LEAK AT STG L-10 BTWN W.STA 284.7 AND 375.8. (RIB 5-8). SEALANT WAS REMOVED WHERE THE FUEL LEAK WAS, THE AREA WAS CLEANED AND THE FUEL LEAK WAS REPAIRED. THE FUEL LEAK</P> / <P>TEST WAS SATISFACTORY IAW AMM 28-11-00-308-013 REV 143 22AUG24.</P>)

Part: SCREW — MISSING (ZONE 100) · airframe 102,454 hrs · 24,897 cycles

ZONE 100, LOWER HALF FUSELAGE, MID E/E, MISSING SCREW AND WASHER ON SMOKE DETECTOR.(<P>ZONE 100, LOWER HALF FUSELAGE, MID E/E, ON SMOKE DETECTOR. ZONE 100, LOWER HALF FUSELAGE, MID E/E, SCREW AND WASHER WERE INSTALLED CORRECTLY IAW AMM 26-16-01-400-801-001 REV. 142 DATE 22 APR 24. GOOD FOR SERVICE. PN: NAS602-10P &AMP; NAS1149DN832J</P>)

Part: BOLT — MISSING (ZONE 400) · airframe 102,454 hrs · 24,897 cycles

ENGINE 1, NEAR TO FORWARD ENGINE MOUNT, LH SIDE, FIREWALL PROTECTION, MISING BOLTS.(<P>ENG 1, NEAR TO FORWARD ENGINE MOUNT, LH SIDE, FIREWALL PROTECTION, BOLTS WERE INSTALLED CORRECTLY IAW AMM 54-54-03-404-002</P>)

Part: INDICATOR — FAULTED (HYD PRESSURE) · airframe 102,290 hrs · 24,829 cycles

CENTER HYD SYSTEM PRESSURE EICAS. CENTER HYD QUANTITY DROPPED .04. PERFORMED ALTN GEAR EXTENSION(<P>REMOVED &AMP; REPLACED HYDRAULIC PRESSURE INDICATOR ASSY FOR CENTER HYDRAULIC IPC REF. 29-11-17-01.&NBSP; OPS CHECK GOOD.&NBSP; NO LEAKS NOTED AS PER B767-300 AMM 29-11-18-004-001.</P>)

Part: LIGHT — NO TEST (SWITCH) · airframe 101,933 hrs · 24,695 cycles

OVERHEAD LIGHT EMERGENCY ANNUNCIATOR KORRY SWITCH LIGHT INOP(<P>REMOVED AND REPLACED OVERHEAD EMERGENCY LIGHT "UNARMED" ANNUNCIATOR KORRY LIGHT ASSY IAW SWPM 20-84-00. OPS CHECK GOOD AT THIS TIME. NO DEFECTS NOTED.</P>)

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 101,725 hrs · 24,611 cycles

L1 DOOR EMERGENCY FLASHLIGHT INOP.(<P>REMOVED AND REPLACED L1 DOOR FLASHLIGHT IAW ATLAS EO 6725A129. OPS CHECK GOOD. THIS CLEARS MDDR 205093, PLACARD REMOVED.</P>)

Part: PUMP — UNKNOWN (UNKNOWN) · airframe 101,390 hrs · 24,497 cycles

AT 80 KNOTS " LH FUEL SYS PRESS" EICAS MSG. REJECTED T/O AT 90 KNOTS. QRH PERFORMED.(<P>PERFORMED FIM 28-22-826 NO DEFECT NOTED. SYSTEM OPS CHECKS GOOD. R/R LH AUX TANK OVERRIDE PUMP IAW AMM 28-22-05, OPS CHECK IS GOOD AT THIS TIME. LEAK CHECK GOOD. R/R LH FUEL OVERRIDE PRESS SW AS PRECAUTIONARY IAW B767 AMM 28-42-01, OPS CHECK GOOD. NO DEFECTS NOTED, LEAK CHECK GOOD. R/R RELAY K329 LEFT FUEL OVERRIDE PUMP CONT. PER B767 WDM 28-22-12, OPS CHECK GOOD.</P>)

Part: ELT — UNKNOWN (UNKNOWN) · airframe 101,322 hrs · 24,471 cycles

FOUND PORTABLE ELT NEAR LAV HOLD DOWN TAPE TO BE TORN TO THE POINT OF ALMOST DEPLOYING.(<P>REMOVED AND REPLACED ELT PORTABLE ASSY IAW AMM 25-64-00.&NBSP; VERIFIED PART EFFECTIVITY IAW EEL.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 100,220 hrs · 24,059 cycles

CORROSION DAMAGE ON THE SECTION 41, SHEAR PANEL, BETWEEN STA 266.5 / STA 287.5 AND LBL 54.75 / RBL 54(<P>REWORKED AREA ON THE SECTION 41, SHEAR PANEL, BETWEEN STA 266.5 / STA 287.5 AND LBL 54.75 / RBL 54 PER MXA EOS TRE6753607 (FVCI REF. 23109-4), TRE6753608 (FVCI REF. 23109-5),&NBSP;<SPAN>TRE6753609 (FVCI REF. 23109-6),&NBSP;</SPAN><SPAN>TRE6753610 (FVCI REF. 23109-7),&NBSP;</SPAN><SPAN>TRE6753611 (FVCI REF. 23109-8) AND&NBSP;</SPAN><SPAN>TRE6753612 (FVCI REF. 23109-9)</SPAN></P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 100,220 hrs · 24,059 cycles

LEFT ATC SYSTEM WITH FAIL "SYS REPLY TIMING"(<P>LEFT ATC WAS REPLACED IN ACCORDANCE WITH AMM 34-53-01/401</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 100,220 hrs · 24,059 cycles

CARGO COMPARTMENT FORWARD, BETWEEN STA 654-88 & STA 654-66 AND STGR 34L OF ROLLER TRAY & PALLET LOCK WITH CORROSION.(<P>CORROSION LEVEL 2 CARGO COMPARTMENT FORWARD, BETWEEN STA 654-88 &AMP; STA 654-66 AND STGR 34L OF ROLLER TRAY WAS REPAIRED IAW SRM 53-00-53-2R-1 FIG201 DETAIL IV REV 122 15APR2023&NBSP;</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 100,220 hrs · 24,059 cycles

CORROSION DAMAGE ON THE SECTION 41, SHEAR PANEL, BETWEEN STA 368 / STA 390 AND LBL 54.75 / LBL 76.80(<P>REWORKED AREA ON THE SECTION 41, SHEAR PANEL, BETWEEN STA 368 / STA 390 AND LBL 54.75 / LBL 76.80 PER MXA EO TRE6753605 - FVCI REF. 23109-2 (APPROVED BY FAA FORM 8110-3)</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 100,220 hrs · 24,059 cycles

CORROSION DAMAGE ON THE SECTION 43, SHEAR PANEL, BETWEEN STA 566 / STA 610 AND RBL 73.80 / RBL 88.50(<P>REWORKED AREA ON THE SECTION 43, SHEAR PANEL, BETWEEN STA 566 / STA 610 AND RBL 73.80 / RBL 88.50 PER MXA EO TRE6753606 - FVCI REF. 23109-3 (APPROVED BY FAA FORM 8110-3)</P>)

Part: PCA — UNKNOWN (UNKNOWN) · airframe 100,220 hrs · 24,059 cycles

RUDDER, MID, AND UPPER PCA'S OUT OF LIMITS.(<P>RUDDER, MID, AND UPPER PCA'S WERE REPLACED IAW AMM REQUIREMENTS AMM 27-21-02-422-038</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 100,220 hrs · 24,059 cycles

CORROSION DAMAGE ON THE SECTION 41, SHEAR PANEL, BETWEEN STA 368 / STA 390 AND LBL 76.80 / LBL 88.50(<P>REWORKED AREA ON THE SECTION 41, SHEAR PANEL, BETWEEN STA 368 / STA 390 AND LBL 76.80 / LBL 88.50 PER MXA EO TRE6753604 - FVCI REF. 23109-1 (APPROVED BY FAA FORM 8110-3)</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 100,220 hrs · 24,059 cycles

RH AND LH WING LOWER REAR SPAR SPLICE FITTING WITH LEAK FUEL(<P>RH AND LH WING LOWER REAR SPAR SPLICE FITTING LEAK FUEL WAS REPAIRED AND TEST WAS SATISFACTORY IAW AMM 28-11-00-308-013</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 100,220 hrs · 24,059 cycles

SEVERAL AIR SAMPLING ORIFICES FROM AFT AND BULK CARGO COMPARTMENT SMOKE DET. SYSTEM WERE FOUND TO HAVE BLOCKAGE(<P>&NBSP;</P> / <P>AIR SAMPLING ORIFICES FROM AFT AND BULK CARGO COMPARTMENT SMOKE DET. SYSTEM WERE CLEANED IAW AMM 26-16-00</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 100,220 hrs · 24,059 cycles

CARGO COMPARTMENT FORWARD, BETWEEN STA 654-88 & STA 654-66 AND STGR 34L OF ROLLER TRAY & PALLET LOCK WITH CORROSION.(<P>CORROSION LEVEL 2 CARGO COMPARTMENT FORWARD, BETWEEN STA 654-88 &AMP; STA 654-66 AND STGR 34L OF ROLLER TRAY WAS REPAIRED IAW SRM 53-00-53-2R-1 FIG201 DETAIL IV REV 122 15APR2023&NBSP;</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 100,220 hrs · 24,059 cycles

FUEL LEAK ON EXTERIOR LOWER SURFACE OF THE 642AB ACCES PANNEL(<P>642AB ACCES PANNEL WAS INSTALLED CORRECTLY IN THE EXTERIOR LOWER SURFACE IAW AMM 28-11-00-796-111. LEAK TESTS WERE PERFORMED WITHOUT LEAKS AFTER THAT.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 100,220 hrs · 24,059 cycles

LH WING DRY BAY WITH LEAK FUEL(<P>LH WING DRY BAY LEAK FUEL WAS REPAIRED AND TEST WAS SATISFACTORY IAW AMM 28-11-00-308-013</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 100,220 hrs · 24,059 cycles

LH WING TRAILING EDGE FITTING SUPPORT OF MLG BEAM WITH HOLE (UNDER ACCESS PANEL 551 UB)(<P>LH WING TRAILING EDGE FITTING SUPPORT OF MLG BEAM (UNDER ACCESS PANEL 551 UB) HOLE WAS REPAIRED IAW TRE 6757207 ISSUED DATE JUL,05,2023 , FAA FORM 8100-9 (2-02) DATE JULY,08,2023</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 100,220 hrs · 24,059 cycles

MAIN DECK CARGO, ZONE A, OBSTRUCTION FROM SMOKE DET. SYSTEM(<P>MAIN DECK CARGO, ZONE A, SMOKE DET. SYSTEM WAS CLEANED AND INSTALLED CORRECTLY IAW AMM 26-16-00</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 100,220 hrs · 24,059 cycles

CRACK INDICATION ON STRINGERS 10, 12, 13, 18, 22, 23, AND 25 BETWEEN STA 654+22 AND 654+44.(<P>STRINGERS REPAIRED BY IAI DOCUMENT CS-24086-025 (MXA EO TRE6753603 R1)</P>)

Part: SMOKE GOGGLES — UNKNOWN (UNKNOWN) · airframe 100,279 hrs · 24,078 cycles

SMOKE GOGGLES FOUND CRUSHED(<P>R/R CREW FO SMOKE GOGGLES IAW B767 AMM 25-60-00. NO FURTHER DEFECTS NOTED</P>)

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 100,108 hrs · 24,009 cycles

EMERGENCY FLASHLIGHT INOP..(<P>REMOVED AND REPLACED ENTRY DOOR FLASHLIGHT BATTERY IAW 767-300 SF/BCF EMERGENCY EQUIPMENT LIST</P>)

Part: LAMP — NONE · airframe 99,782 hrs · 23,888 cycles

EMERGENCY LIGHT BY L 1 DOOR INOP.(<P>RELAMPED OPS CHECK NORMAL IAW AMM 33-51-00</P>)

Part: ELT — INOPERATIVE (CABIN) · airframe 99,699 hrs · 23,857 cycles

PORTABLE ELT INOP ( EMERGENCY LOCATOR TRANSMITTER (ELT), SURVIVAL TYPE ELTS )(<P>R/R PORTABLE ELT IAW 25-63-04</P>)

Part: LIGHT — FAULTED (CABIN) · airframe 99,224 hrs · 23,717 cycles

EMERGENCY LIGHT AT L1 DOOR INOP(<P>RELAMPED LIGHT OPS CHECK NORMAL I/A/W 33-51-00</P>)

Part: ANNUNCIATOR — DAMAGED · airframe 98,512 hrs · 23,499 cycles

EMERGENCY LIGHT ANNUNCIATOR BURNT OUT. LAMP INOP UPON INVESTIGATION FOUND ANNUNCIATOR TABS BROKEN, REMOVED AND REPLACED LIGHT ANNUNCIATOR IAW B767 AMM 33-18-02, OPS CHECK GOOD.</P>)

Part: FITTING — NONE · airframe 97,466 hrs · 23,161 cycles

#2 PYLON FAN COWL SUPPORT FITTING IS CRACKED ON I/B SIDE LOWER RADIUS(<P>REMOVED AND REPLACED #2 PYLON FAN COWL SUPPORT FITTING IAW B767 51-40-02-0G-0</P>)

Part: NONE — NONE · airframe 97,466 hrs · 23,161 cycles

CORROSION OF LEFT ENGINE FAN CASE AT FORWARD SIDE OF KEVLAR FAN SHIELD FROM 4 OCLOCK TO 7 OCLOCK POSITION.(<P>CLEANED THE AREA AND UPON FURTHER EVALUATION THE CORROSION ON THE #1 ENGINE FAN CASE AT FWD SIDE OF KEVLAR FAN SHIELD FRON 4 TO 7 O'CLOCK POSITION IS WITHIN LIMITS IAW B767 AMM 72-00-00-206-167-H00 PAGE 2</P>)

Part: DOUBLER — NONE · airframe 97,466 hrs · 23,161 cycles

UPON REOMOVAL OF EXISTING DOUBLER #2 PYLON FOUND ELONGATED HOLE ON THE PYLON WEB BOTTOM(<P>REMOVED AND REPLACED DOUBLER,FILLER,AND 2EA. ANGLES ON #2 PYLON STRUT FWD UPPER SPAR WEB. REPAIRED ELONGATED HOLE IAW B767 FAS 21091 REV:IR SRM 51-40-02, 51-40-05, 51-20-07, 51-20-01</P>)

Part: NONE — NONE · corrosion level 2 · airframe 97,466 hrs · 23,161 cycles

MAIN CABIN CENTER WING UPPER SURFACE HAS AREA OF CORROSION AT BS 954 RBL 75. DOT 024(<P>REPAIRED CORROSION AT MAIN CABIN CENTER WING SKIN UPPER SURFACE STA 954 RBL 75 IAW FVCI EO: 21194 REV:IR</P>)

Part: NONE — NONE · airframe 97,466 hrs · 23,161 cycles

LT WING INBD MAIN FLAP LOWER SURFACE LOWER SKIN PANEL HAS SEVERAL BULGING AREAS , APPROX 33" FROM THE INBD END DOT 129-054(<P>BLENDED THE CORROSION&NBSP; ON THE "T" CHORD IAW B767-300 SRM 51-10-02. UPON THE EVALUATION THE LOWEST REMAINING MATERIAL IS 0.062"&NBSP; AND WAS OUT OUF LIMITS IAW B767-300-SRM 57-53-02. REMOVED AND REPLACED THE CORRODED "T" CHORD ON THE LH WING MAIN IB FLAP IAW B767-300 SRM 51-40-02-0G-0</P>)

Part: FITTING — NONE · airframe 97,466 hrs · 23,161 cycles

#1 PYLON FAN COWL SUPPORT FITTING IS CRACKED ON O/B SIDE LOWER RADIUS.(<P>REMOVED AND REPLACED #1 PYLON FAN COWL SUPPORT FITTING IAW B767 SRM 51-40-02, 51-40-05,AMM 54-51-01, 20-11-00</P>)

Part: NONE — NONE · 23,160 cycles

"L PACK TEMP" EICAS DURING PREFLIGHT ON GROUND(<P>RESET LEFT PACK IAW AMM 21-51-00 AND PERFORMED BIT CHECK ON TEMP CONTROLLER IAW AMM 21-51-01, NO FAULTS NOTED.</P>)

Part: SENSOR — NONE

EICAS MESSAGE: L PACK TEMP, AND LEFT PACK RESET INOP LIGHT CAME ON.(<P>TRANSFERRED TO MEL # 21-51-01-01 MDDR # 155538.</P> / <P>22OCT-ONTMX: LP 1401921, ITEM M3: PERF. L PACK CONT BITE PER FIM 21-51-FT 844, FAULTED MIX MANIFOLD SENSOR MULTIPLE ATTEMPTS. R/R SENSOR TS200 PER AMM 21-61-02. OPS CHECK GOOD. NO FAULTS NOTED. THIS CLEARS DMI 155538.</P>)

Part: BATTERY — NONE · airframe 97,453 hrs

APU INOP.(<P>FOUND MAIN BATT DISCHARGED. SWAPPED APU BATTERY WITH MAIN BATTERY. TRANSFERRED TO MDDR 155522 MEL 49-11-01A CAT C.</P> / <P>REF LOG 1387369 ITEM 3:&NBSP; REMOVED AND REPLACED APU BATT. OPS CHECK OK. THIS CLEARS MDDR 155522.</P>)

Part: SENSOR — NONE · airframe 97,431 hrs

L PACK TEMP CAUITON MSG COMPLIED WITH QRH L TEMP CONTROLLER WORKS IN STANDBY MODE.(<P>R&AMP;R CABIN AIR SENSOR ASSY IAW AMM 21-61-02 STILL REQ'S OPS CHECK.&NBSP;</P> / <P>LP 1387359, ITEM M11: PERFORMED OPS CHECK AND LEAK CHECK FOR CABIN AIR SENSOR ASSY. IAW AMM 21-61-02. OPS CHECK GOOD AND LEAK CHECK GOOD.</P>)

Part: CONTROLLER — NONE · airframe 97,400 hrs · 23,141 cycles

R PACK TEMP EICAS AFTER LANDING. MESSAGE EXTINGUISHED IN STBY -N PER QRH.(<P>TRANSFERRED TO MDDR 155053 IAW MEL 21-51-01-01, CAT C.</P> / <P>14OCT21 - LP 1372006 - ITEM# 4 - ONT - REMOVED AND REPLACED PACK CONTROLLER PER AMM 21-51-04 OPS CHECKS GOOD. MDDR 155053 CLOSED. PLACARD REMOVED. MCC NOTIFIED.&NBSP;</P>)

Part: NONE — NONE

R PACK TEMP EICAS ON CLIMBOUT OPERATED IN STBY NORMALLY.(<P>PERFORMED BITE PROCEDURE 21-51 TREE 803. NO FAULTS NOTED, NO RECENT HISTORY(R) PACK CONTROLLER. OK TO CONTINUE.</P>)

Part: NONE — NONE

L PACK TEMP EICAS DURING PUSH BACK. RAN NON-NORMAL PROC. LIGHT &AMP; MSG EXTINGUISHED.(<P>PERFORMED PACK TEMPERATURE TEST. NO FAULTS FOUND IAW B767-300 AMM 21-51-00.</P>)

Part: APU — NONE

APU DUCT PRESS SURGING WHEN PNEUMATIC LOAD APPLIED TO APU(<P>PERFORMED FIM 49-11 FT. 976 TO BLOCK 8. ISSUE STILL REMAINS. TRANSFERRED TO DMI 154796 IAW DDG 36-11-04. PLACARD INSTALLED AND MX ACTIONS ACCOMPLISHED.</P> / <P>18OCT- CVG MX: LP 1387361, ITEM M15: REMOVED AND REPLACED APU IAW AMM 49-11-01, OPS CHECK OK.</P>)

Part: NONE — NONE

CAPTS O2 MASK MIC INOP(<P>SWAPPED CAPTS AND FIRST OFFICERS O2 BOX ASSY. CAPTS PNO MXP147 SNO 3875. FIRSTS OBS PNO MXP147 SNO 53357. OPS CHK NORMAL. REF AMM 35-11-51. TRANSFERRED TO MDDR 154761.</P> / <P>ONT MX-16OCT, LP 1371987: REMOVED AND REPLACED OBS OXY MASK BOX &AMP; O2 LINE(OXYGEN SUPPLY) IAW AMM 35-11-51. FOUND #2 PIN NOT SECURED, RESECURED PIN 2 IAW SWPM 20-60 &AMP; WDM 23-71-11. OPS CHECK GOOD. THIS CLEARS MDDR 154761. MCC NOTIFIED. JT 0852Z.</P>)

Part: GENERATOR — NONE · airframe 97,338 hrs · 23,119 cycles

APU GEN TRIPPED OFF 2X(<P>ITEM TRANSFERED TO MDDR 154611 CAT C DUE 15OCT21 PER MEL 49-11-01A</P> / <P>REF LOG 1373475 ITEM 3: REMOVED AND REPLACED APU GENERATOR IAW AMM 24-21-01. OPS CKS NML. DMI 154611 CLEARED.</P> / <P>&NBSP;</P>)

Part: NONE — NONE

APU RELIABILITY COLD START ACCOMPLISHED AT FL380, -56 DEGREES C ON FIRST ATTEMPT, FOLLOWED BY APU GEN OFF MESSAGE. GEN RESET WITH QRH PROCEDURE.(<P>PERFORMED BITE PROCEDURE ON ECU PER FIM 49-11 FT958. NO FAULTS NOTED. SYSTEM OK.</P> / <P>LP 1373456, ITEM M2: PERFORMED APU ECU BITE TEST PER FIM 4911 F/T 958, NO FAULTS NOTED. PERFORMED BPCU BITE TEST PER FIM 24-20 F/T 801, SYSTEM CHECK OK, OPS CHECK APU, OPS CHECK NORMAL IAW AMM 49-11-00.</P>)

Part: NONE — NONE

LT PACK INOP EICAS MSG(<P>RESET LT PACK PER AMM 21-00-10. OPS CHECK GOOD.</P>)

Part: NONE — NONE

L PACK INOP LIGHT ILLUMINATED AFTER SELECTING PACK TO ON(<P><SPAN>PERFORMED OPS CHECK ON L PACK SYSTEM IAW B767 AMM 21-51-00. OPS CHECKS GOOD AT THIS TIME.</SPAN></P>)

Part: VALVE — NONE

APU SHUTS DOWN WITH GENERATOR/ PACK ON(<P>APU IS DEFERRED MEL # 49-11-01A. ITEM TRANSFERRED TO MDDR # 154509. PLACARD INSTALLED.</P> / <P>LP 1382352 - ITEM # 5 - CVG - REMOVED AND REPLACED APU SURGE CONTROL VALVE IAW B767 AMM 49-53-01. OPS CHECK GOOD. DMI #154509 CLEARED. PLACARDS REMOVED.</P>)

Part: TRANSCEIVER — LOOSE · 23,094 cycles

REPEAT WRITE UP "WXR FAIL" ON BOTH CAPT. AND F/O HSI'S - WENT ON/OFF SEVERAL TIMES THROUGHOUT FLIGHT.PERFORMED WEATHER RADAR SYSTEM TEST NO FAULTS AT THIS TIME IAW B767-300 AMM 34-43-00. FOUND L WX RADAR TRANSCEIVER LOOSE IN RACK. RESECURED TRANSCEIVER IAW B767-300 AMM 34-43-01. NO FAULTS AT THIS TIME.

Part: FIRE WARNING — FALSE ACTIVATION (RT ENGINE)

R ENG FIRE LP 1 STATUS MESSAGE INFLIGHT(<P>T/S REF B767 AMM 26-11-00 AND FIM 26-11 FAULT TREE 806. NO MESSAGE PRESENT AT THIS TIME. COULD NOT DUPLICATE ON GROUND.</P>)

Part: ENVIRON SYS — CONTAMINATED (A/C PACKS)

EXTREME ODOR ON FLIGHT DECK. SMELL OF "WET SOCKS" OR MOLD. REPEAT WRITE UP.(<P>LP 1431030, ITEM M15: PERFORMED "SMOKE OR FUEMES IN CABIN" CONDITIONAL INSPECTION IAW AMM 05-51-56. NO EVIDENCE OF OIL OR WATER CONTAMINATION IN PACK SYSTEM OR DUCTING. ALSO PERFORMED REMOVAL OF CONTAMINATION FROM A/C AND PNEUMATIC SYSTEM PER AMM 21-00-21-102-130. NO ODOR PRESENT.</P> / <P>LP 1431031, ITEM M16: PERFORMED VISUAL INSPECTION OF MIX MANIFOLD DUCTING PER AMM 21-21-00. NO EVIDENCE OF ODOR CAUSING CONTAMINATION.</P>)

Part: ENVIRON SYS — CONTAMINATED (A/C PACKS)

STRONG ODOR WHEN LEFT AND RIGHT PACKS ON. SMELLS LIKE "WET SOCKS" OR WET PAINT.(<P>PERFORMED FUMES IN THE CABIN CONDITIONAL INSPECTION IAW AMM 05-51-56 TASK 05-51-56-202-201. REMOVED OIL CONTAMINATION FROM AIR CONDITIONING SYSTEM IAW AMM 21-00-21-102-C80. NO SMOKE OR ODOR DETECTED AT THIS TIME. OPS CHECK IS GOOD AT THIS TIME.</P>)

Part: FIRE LOOP — OUT OF POSITION (NR 2) · airframe 97,226 hrs · 23,080 cycles

LT ENGINE FIRE LP 2 STATUS MSG.(<P>PERF FIM 26-11 F/T 804 AND F/T 805. NO CURRENT FAULTS ON EICAS UPON VISUAL INSPECTION. FOUND TS681 LOOP 2 ELEMENT RUBBING ON METAL BRACKET. FIXED INSTALLATION PER AMM 26-11-02. NO FAULT NOTED AT THIS TIME. RESISTANCE CHECKS OKAY AT THIS TIME PER WDM 26-11-11. REF LP 1407706 TRANSFERRED TO MDDR 153518 IAW ATLAS DDG 26-11-01-01 CAT C DUE 24SEP21. PLACARDS INSTALLED.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT FIRE LOOP)

INTERMITTENT "L ENG FIRE LP 2" STATUS MESSAGE(<P>PERFORMED FIM 26-11 FT.805 &AMP; 26-11 FT. 804. NO DEFECTS NOTED. VISUAL INSPECTED L ENG FIRE LP2 AND NO DEFECTS NOTED AT THIS TIME. OPS TEST GOOD. RUN L/H ENG IAW AMM 71-00-00. NO FAULTS NOTED AT THIS TIME. OPS CHECK GOOD. ENG RUN C/W.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT FUEL PUMP) · airframe 97,158 hrs · 23,057 cycles

DURING CLIMBOUT PASSING FL340, "L FWD FUEL PUMP" EICAS ILLUMINATED FOR APPROX 1 MIN. THEN EXTINGUISHED.(<P>PERFORMED OPS TEST OF L FWD PUMP IAW AMM 28-22-00. OPS TEST OK AT THIS TIME.</P>)

Part: VALVE — FAULTED (CABIN TEMP) · 23,056 cycles

AFT CABIN TEMP CONTROL SYSTEM INOP ( CABIN COMPT TEMP CONTROL SYSTEM / ALL CARGO CONFIGURATION )(<P>TRANSFERRED TO MEL 21-61-01-02, CAT C, DUE DATE 17 SEP21. MDDR 153159. MCC NOTIFIED. PLACARD INSTALLED. LP 1407696: T/S PER FIM 21-60 FT 804 TO STEP 52 SHEET 5, " TRIM VALVE "&NBSP; MSG ON ZONE TEMP BITE, TABLE B SHEET 2. PERF CONT CHECK FROM CONNECTOR D770B PINS C13,C15 TO PINS 2.1 CONNECTOR D700 CHECK GOOD, SWAPPED FWD AND AFT TRIM AIR VALVES IAW AMM 21-61-02. REMOVED AND INSTALLED FWD AND AFT TRIM VALVES TO ORIG POSITIONS. IAW AMM 21-61-07. REMOVED AND REPLACED AFT TRIM CONTROL VALVE IAW AMM 21-61-07. OPS CHECK GOOD. THIS CLEARS DMI 153159. MCC NOTIFIED. PLAC REMOVED.

Part: CIRCUIT CARD — FAULTED (FIRE DETECTION) · airframe 97,117 hrs · 23,043 cycles

L ENG FIRE LP 2 EICAS STATUS MSG IN-FLIGHT..(<P>TRANSFERRED TO MDDR 152473 PER MEL 26-11-01-01, CAT C, DUE DATE: 04SEP21. DISP: DP @ 1611Z.</P> / <P>LOG PAGE 1208209: REMOVED &AMP; REPLACED L/H ENG FIRE LOOP #2 CARD IAW AMM 26-11-02. OPS CHECK NORMAL AT THIS TIME. THIS CLEARS MDDR 152473.</P>)

Part: BOOT — DAMAGED (DUCT)

APU INOP DUE TO DUCT - AIR SURGE BOOT DAMAGED.(<P>TRANSFERRED TO MDDR 152086 IAW MEL 49-11-01A, CAT C.&NBSP;</P> / <P>REMOVED AND REPLACED SLEEVE ON APU SURGE AIR DUCT ASSEMBLY REF. B767 AMM 46-53-013. OPS CHECK NORMAL. NO LEAKS NOTED AT THIS TIME. THIS CLEARS MDDR # 152086. PLACARD REMOVED.</P>)

Part: APU — SHUTDOWN

DURING PUSHBACK, WHEN APU AIR SELECTED OFF FOR ENGINE START, APU SHUTDOWN(<P>PERFORMED FIM TASK ATLAS 767 FIM 49-11- FAULT TREE 958. APU BITE PROCEDURE. RE-STARTED APU. NO FAULT FOUND.</P>)

Part: PNEUMATIC SYSTEM — MALFUNCTIONED · 23,007 cycles

APU FAULT DUE TO PNEUMATICS SURGING(<P>FWD TO MEL AND PLAC 49-11-01A, CAT C, DUE 21AUG21. MDDR 151717.</P> / <P>REF LOGPAGE 1439202&NBSP; ITEM 5: T/S PER FIM 49-11 F/T 976 TO BLOCK 28. NO SURGING OR FLUCUATION NOTED . 3 SUCCESSFUL APU STARTS ACCOMPLISHED AND LOAD PLACED ON APU . NO FAULTS NOTED , APU OPS NML AT THIS TIME. THIS CLEARS MDDR 151717, PLAC REMOVED.</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (LT FIRE LOOP)

STATUS MSG: L ENG FIRE LOOP 2(<P>PERFORMED OPS CHECK PER B767AMM 26-11-02 OPS CK GOOD AT THIS TIME. NO MESSAGE DISPLAYED</P>)

Part: CIRCUIT CARD — FAULTED (NR 2 FIRE LOOP) · airframe 96,886 hrs

L ENG FIRE LOOP 2 STATUS MSG(<P>PERF ENG FIRE TEST BITE PER FIM 26-11 FT 804. FOUND L ENG FIRE LOOP 2 CARD M682 AT FAULT. REMOVED AND REPLACED M682 PER AMM 26-10-01. OPS CHECK GOOD, NO FAULTS IN VIEW.</P>)

Part: FIRE WARNING — FALSE ACTIVATION (RT ENGINE)

R ENG. FIRE LP 1 STATUS MESSAGE APPEARED DURING DESCENT(<P>PERFORMED ENGINE DETECTION SYSTEM BITE PROCEDURE REF. B767 26-11 F/T 804. COULD NOT DUPLICATE FAULT ON GROUND. NO FAULTS NOTED AT THIS TIME.</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (FIRE LOOP)

STATUS MESSAGE L ENG. FIRE LOOP 1(<P>PERFORMED FIRE LOOP BITE PROCEDURE PER 767 FIM 26-11 F/T 805. NO FAULTS NOTED AT THIS TIME AND MESSAGE NO LONGER APPEARS.</P>)

Part: DETECTOR LOOP — OUT OF POSITION (A/C PACK BAY) · airframe 96,738 hrs · 22,932 cycles

L BLEED DUCT LEAK MSG (ISOLATED TO LEFT PACK FAULT)(<P>TRANSFERRED TO MDDR 150009 IAW MEL # 21-51-01-01, CAT C, DUE DATE: 21JUL21. DISPATCH: LUC 2249Z. MX ACTION C/W. INSPECTED FOR LEAKS IAW AMM 26-18-00 AND FOUND LOOP TOUCHING FRAME, ADJUSTED LOOP. OPS CHECK GOOD AFTER 1 HOUR OF OPERATION. MEL 150009 CLEARED. MCC NOTIFIED. PLACARD REMOVED.

Part: FIRE WARNING — FALSE ACTIVATION (APU BAY)

STATUS MSG: APU FIRE LP1(<P>MESSAGE CLEARED BEFORE LANDING. PERFORMED STEPS IN FIM 26-15-804. OPERATIONAL NORMAL.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT WINDOW) · 22,934 cycles

R SIDE WINDOW EICAS(<P>RESET RT SIDE WINDOW HEAT SWITCH TO ON POSITION. NO DEFECT NOTED. OK FOR SVC. PER AMM 30-41-00.

Part: LAMP — INOPERATIVE (INDICATOR)

L AUX PITOT HEAT ON OVERHEAD, WILL NOT ILLUMINATE DISCRETE. PROBE HEAT LIGHTS EXCEPT CAPT AND F/O PITOT(<P>ITEM PLACED ON DMI 149728 IAW MEL 30-31-02 .</P> / <P>07JUL21 - LP1363846 - ITEM# 3 - CVG - RELAMPED LT AUX PITOT HEAT LIGHT IAW 33-16-02, PERF OPS CK IAW AMM 30-31-00, OPS CHECK GOOD, CLEARED DMI 149728, PLACARD REMOVED.</P>)

Part: INDICATION SYS — MALFUNCTIONED (FUEL) · airframe 96,663 hrs

FUEL CONFIG EICAS ON CLIMB. FUEL INDICATION IN LEFT TANK DROPPED TO 12,000LBS MOMENTARILY THEN RETURNED TO NORMAL INDICATION. NO IRREGULAR PITCH ALTITUDE OR BANK ANGLES WERE MADE DURING DEPARTURE(<P>PERFORMED FIM 28-41 FT 852 AND OPS TEST IAW AMM 28-22-00. OPS CHECK GOOD. COULD NOT DUPLICATE SYS OK.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PUMP) · airframe 96,663 hrs

LEFT FWD FUEL PUMP EICAS MSG RETURNED JUST AFTER LEVEL OFF FOR CRUISE. MSG EXTEINGUISED ON ITS OWN BEFORE QRH CHECKLIST WAS ACCOMPLISHED.(<P>PERFORMED FIM 28-41 FT 852 AND OPS CHECK IAW AMM 28-22-00. OPS CHECK GOOD. COULD NOT DUPLICATE. SYS OK</P>)

Part: RADAR — FAULTED (RT WX SYSTEM) · airframe 96,319 hrs · 22,797 cycles

R WX RADAR INOP. OPS CK WRX-R IAW B767 AMM 34-43-01, CK WRK-R IN 4 MODES AND WRK-L IN 4 MODES, ALL 8 MODES CK GD. SWEEOS AND CONTRAST WITHIN OPERATIONAL PARAMETERS. NO DEFECTS AT THIS TIME.

Part: APU — MALFUNCTIONED · airframe 96,180 hrs · 22,754 cycles

APU INOP. PERFORMED APU BITE PROCEDURE, CLEARED FAULT. APU STARTED ON FIRST ATTEMPT. IAW AMM 49-11-01. NO DEFECTS NOTED.

Part: FAULT LIGHT — FALSE ACTIVATION (APU) · airframe 96,187 hrs · 22,757 cycles

WITH APU RUNNING WE DISCONNECTED ELECTRICAL POWER AND WE GOT APU FAULT LIGHT(<P>RESTARTED APU, TRANSFERED POWER FROM GROUND TO APU TWO TIMES NO FAULTS AT THIS TIME IAW AMM 49-11-01.</P>)

Part: CONTROL VALVE — FAULTED (FLOW) · airframe 96,170 hrs · 22,751 cycles

PACK OFF LIGHT ON L PACK. PERFORMED FIM 21-51 FT 803. REMOVED AND REPLACED CABIN AIR SENSOR IAW AMM 71-51-08 NO FIX. FUTHER TROUBLESHOOTING REQ. THIS DMI REMAINS OPEN. REMOVED AND REPLACED LT FLOW CONTROL VALVE ASSY IAW AMM 21-51-01, OPS CHECK GOOD, NO DEFECTS NOTED AT THIS TIME. CLEARED DMI 145663, PLACARD REMOVED MCC NOTIFIED.

Part: FILTER — FAULTED (RT ENG FUEL SYS) · 22,712 cycles

RT ENGINE FUEL FILTER ILLUMINATED IN CLIMBOUT WITH FF ABOVE 10KPPH. EXTINGUISHED ON POWER REDUCTION.(<P>R/R R/H ENG FUEL FILTER IAW AMM 73-11-02. LEAK CHECKS GOOD. OPS CHECKS NORMAL, NO DEFECTS NOTED</P>)

Part: FILTER — WARNING MESSAGE (RT ENGINE) · airframe 96,051 hrs

RT ENG FUEL FILTER ILLUMINATED IN CLIMBOUT W/FF ABOVE 10K PPH EXTINGUISHED ON POWER REDUCTION(<P>REMOVED AND REPLACED&NBSP;RH ENG FUEL FILTER IAW AMM 73-11-02. LEAK CHECKS GOOD. OPS CHECKS NORMAL. NO DEFECTS NOTED.</P>)

Part: CONNECTOR — LOOSE (ACCELEROMETER) · airframe 95,993 hrs · 22,692 cycles

DURING CLIMB L ENG VIBE INDICATED FAN 4.1 AT 104.7 AT PEAK. HELD STEADY AT 3.8-3.6 ABOVE 104.7(<P>CREW REPORTED NO VIBRATIONS FELT, INDICATION ONLY. PERFORMED GVI OF ENG, AFT ACCELEROMETER AND MOUNTING BRACKET. NO DEFECTS NOTED. FOUND MAIN #1 BEARING ACCELEROMETER CONNECTOR D10994 LOOSE. CLEANED AND RESECURED PER FIM TASK 77-31 FT808 AND AMM 77-31-02. PERFORMED AMM BITE PER AMM 77-31-00<BR /></P><P>LP&NBSP;1276157:&NBSP;PERF LH ENG IDLE RUN IAW AMM 71-00-00. ENG VIB READINGS 0.6-0.8. NO OTHER ENG RELATED ISSUES NOTED AT THIS TIME.</P>)

Part: SKIN — SCRATCHED (CROWN) · airframe 95,932 hrs · 22,670 cycles

MAINTENANCE DISCOVERED SCRATCHES ON THE FUSELAGE SKIN CROWN AREA BETWEEN DOOR STA 923 AND STA 1540 BETWEEN STR 2L AND STR 3L AS RECORD IN NRC NO. 76226-NR-0055. THE AFFECTED AREA ARE LOCATED AROUND THE ELT ANTENNA.(<DIV>&NBSP;MAINTENANCE REMOVED THE SCRATCHES TO A SMOOTH CONTOUR PER B767-300 SRM 51-10-02 AND RESTORED THE SURFACE FINISH.</DIV><P STYLE="MARGIN: 0IN 0IN 0.0001PT;">PERFORMED A HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION AND FOUND NO CRACKS. PERFORMED AN OPEN HOLE HFEC INSPECTION AT ALL OPEN HOLES, NO DEFECTS FOUND. ALL WORK ACCOMPLISHED PER ATLAS AIR EO 6753A926 REV 0 DATED 19MAR21.</P>)

Part: CONTROL PANEL — MALFUNCTIONED (WX RADAR SYS) · airframe 95,929 hrs · 22,669 cycles

BOTH WX RADARS FAILED. WILL NOT TEST EITHER.(<P>TRANSFER TO MDDR# 144120, CAT C, MEL- 34-43-01-02. DUE DATE 30MAR21. PLACARD INSTALLED.</P><P>DATE 20 MAR21 - LP 1342642 ITEM 8 - TPA - REMOVED AND REPLACED THE WXR CONTROL PANEL IAW AMM 34-43-02. OPS CHECK GOOD. THIS CLEARS MDDR 144120.</P>)

Part: APU — FALSE INDICATION · airframe 95,846 hrs · 22,646 cycles

APU FAIL. PERFORMED OPS CHECK OF APU IAW 49-11-02-201. OPS NORMAL NO DEFECTS NOTED.

Part: APU — FAULTED · airframe 95,827 hrs · 22,639 cycles

APU FAULT SHUTDOWN, NOTED TWICE DURING PREFLIGHT.(<P>TRANSFERRED TO MDDR 143224 PER MEL 49-11-01A, CAT C, DUE DATE 12MAR21. DI: JT@ 19:26Z</P><P>&NBSP;LP 1491954, ITEM M5: PERFORMED APU BITE PER FIM 49-11 F/T 958, NO FAULTS CURRENT OR PREVIOUS. PERFORMED VISUAL INSP APU, NO DEFECTS NOTED, OPERATED APU WITH APU GEN, BLEED AND PACKS FOR 3 HOURS, NO AUTO SHUTDOWN, OPS TEST GOOD IAW AMM 49-11-00. PLACARD REMOVED/DMI 143224 CLEARED. T.I.: 0533/JD

Part: SURGE VALVE — FAILED (APU) · airframe 95,776 hrs · 22,625 cycles

APU INOP. SURGE WITH BOTH PACKS ON(<P>TRANSFER TO MDDR 142909 IAW MEL 49-11-01A CAT C DUE 06MAR21</P><P>LP:1329164 PERFORM BIT OF APU IAW FIM 49-11 FT 965 FOUND LEAK-TORN DUCT- SURGE VALVE. REMOVED AND REPLACED DUCT IAW AMM 49-53-01 PERFORMED OPS CHK FAILED DUCT PRESSURE FLUCTUATING.</P><P>LP:1329167 REMOVED AND REPLACED APU SURGE CONT. VALVE IAW B767 AMM 49-53-01. OPS CHK GOOD AND LEAK GOOD THIS CLEARS DMI 142909&NBSP;</P>)

Part: DISPLAY — FAILED (WX RADAR SYS) · airframe 95,776 hrs · 22,625 cycles

WX FAIL BOTH DISPLAYS. (PERFORMED FIM 34-43-00. OPS TEST OK AT THIS TIME.)

Part: STATUS MESSAGE — FALSE ACTIVATION (RT FIRE LOOP) · airframe 95,718 hrs · 22,603 cycles

STATUS MSG R ENG FIRE LP 1(<P>PERFORMED OPERATIONAL TEST OF ENG FIRE DETECTION SYSTEM&NBSP; REF 26-11-00. OPERATIONAL TEST OKAY. MSG CLEARED.<BR /></P>)

Part: ENGINE — VIBRATION (AIRFRAME) · airframe 95,675 hrs · 22,586 cycles

ABOVE FL 250 KIAS AIRFRAME VIBRATION WITH LOW TONE HUMMING, OCCURS CONTINUOUSLY THROUGHOUT THE FLIGHT DURING CLIMB. N1 (R) AT 1.4 UNITS VIBRATION.(C/W AIRFRAME VIBRATION CONDITIONAL INSPECTION PART 2 77-31-02 FOR ENG 2. LOCKS AND RING SECURE. PERFORMED VISUAL INSPECTION 71-00-00-216, NO DEFECTS NOTED.

Part: STATUS MESSAGE — FALSE INDICATION (RT FIRE LOOP) · airframe 95,645 hrs · 22,577 cycles

STATUS MESSAGE "RT ENG FIRE LP 1". PERFORMED OPS CHECK OF RT H ENG FIRE LOOP IAW AMM 26-11-00 WITH NO DEFECTS NOTED. OPS CHECK GOOD.

Part: CONTROLLER — FAILED (WINDSHEILD HEAT) · airframe 95,569 hrs · 22,553 cycles

AFTER T/O RT WINDSHIELD SPARKED THEN CRACKED. REMOVED AND REPLACED RIGHT WINDOW HEAT CONTROLLER, IAW AMM 30-41-01. REMOVED AND REPLACED R1 WINDOW, PER AMM 56-11-01. WINDOW P/N OFF 141T4081-50 S/N OFF 06063R9259.

Part: FILTER — WARNING MESSAGE (LT ENG FUEL) · airframe 95,457 hrs · 22,517 cycles

STATUS MESSAGE LT ENGINE FUEL FILTER. REMOVED AND REPLACED FUEL FILTER ELEMENT OF ENGINE NR 1, IAW AMM 73-11-02. NO LEAKS THEN PERFORMED WET MOTER, THEN RAN ENGINE NR 1, PER AMM 71-00-00. THIS CLEARS STATUSS MESSAGE LT ENGINE, FUEL FILTER OPERATIONS CHECKS OK.

Part: APU — MALFUNCTIONED · airframe 95,450 hrs · 22,515 cycles

APU WILL NOT START. TRANSFERRED TO MDDR NR 140596, IAW MEL 49-11-01A CAT C DUE DATE 17JAN 21 MX ACTION C/W. PERFORMED APU BITE, IAW B767 FIM 49-11 FT 958, NO DEFAULTS. THEN STARTED THE APU. APU STARTED IN THE FIRST ATTEMPT. ENGINE RPM & EGT PARAMETERS NORMAL. THIS CLEARS DMI NR 140596.

Part: APU — MALFUNCTIONED · airframe 95,423 hrs · 22,506 cycles

UNABLE TO START APU. TRANSFER TO MDDR NR 140208, CAT C, DUE DATE 08JAN2021, AS PER MEL 49-11-01-A. MCC NOTIFIED. PERFORMED SUCCESSFUL APU START, IAW AMM 49-11-00, NO FAULTS NOTED. THIS CLEARS MDDR 140208, PLACARD REMOVED, MCC NOTIFIED.

Part: WARNING MESSAGE — FALSE ACTIVATION (BLEED AIR SYS) · airframe 95,392 hrs · 22,495 cycles

BLEED AIR UNAVAILABLE. AFTER DEICING ACCOMPLISHED POST DE-ICE CHECKLISTS, PER FCOM VOL 1. ENGINE RUN REQUIRED DUE TO ENTRY M1. PERFORMED BITE ON AIR SUPPLY CONTROL SYSTEM, IAW B767 AMM 36-23-00 AND FOUND NO FAULTS. SEE ENTRY M3 FOR ENGINE RUN. M3: PERFORMED IDLE ENGINE RUN, IAW B767 AMM 71-00-00. BLEED LIGHT REMAINED EXTINGUISHED. OPERATIONS CHECKS GOOD.

Part: APU — UNKNOWN (APU BAY) · airframe 95,353 hrs · 22,482 cycles

LARGE QUANTITY OF OIL DISCOVERED ON UNDER SIDE OF TAILCONE NEAR APU. INSPECTED APU, PER B767 AMM 49-05-03-202-011. NO FAULTS NOTED. C/W WO NR 74452, IAW WORK CARD INSTRUCTIONS. APU REMOVED & REPLACED, IAW AMM 49-11-01.

Part: CONTROL VALVE — MALFUNCTIONED (APU SURGE) · airframe 95,300 hrs · 22,464 cycles

NO DUCT PRESS FOR ENGINE START. TRANSFER TO MDDR 138842, IAW MEL 49-11-01-01. MCC NOTIFIED PLACARD INSTALLED. REMOVED AND REPLACED APU SURGE CONTROL VALVE, IAW AMM 49-53-01. OPERATIONS CHECK GOOD. THIS CLEARS DMI 138842.

Part: FIRE DETECTOR — FALSE ACTIVATION (APU BAY) · airframe 95,250 hrs · 22,447 cycles

NOTED APU FIRE LOOP 1 EICAS MESSAGE AFTER BLOCK IN. PERFORMED FIM 26-15 FT 803 MESSAGE CLEARED. NO FAULTS NOTED AT THIS TIME.

Part: STATUS MESSAGE — ILLUMINATED (FUEL PUMP) · airframe 95,231 hrs · 22,442 cycles

RT CENTER OVERRIDE FUEL PUMP STS MESSAGE CENTER TANK FUEL PUMPS, ONE INOPERATIVE, CENTER TANK FUEL USED (NOTIFY DISPATCH). TRANSFERED TO DMI 138002, IAW MEL 28-22-02A CAT C DUE DATE 27NOV20. M PROCEEDURES C/W. TEST OF RT C OVERRHEAD PUMP AND PRESSURE SWITCHES, IAW B767 AMM 28-22-00-715-001 STEP I. NO DEFECTS NOTED. SYSTEM OPERATIONAL.

Part: CONTROL VALVE — LOW PRESSURE (APU) · airframe 95,179 hrs · 22,427 cycles

APU PNEUMATIC FUNCTION INOPERABLE LOW PRESSURE. RT ENGINE STARTER EICAS DURING START. N2 ROTATION MINIMAL PULLED BACK INTO GATE, NO FLY. APU BLEED LOW PRESS, REMOVED AND REPLACED APU SURGE CONTROL VALVE, IAW B767 AMM 49-53-01. OPERATIONS CHECK SATISFACTORY. BLEED PRESSURE AT 35 PSI.

Part: TRANSMITTER — DAMAGED (ELT) · airframe 95,145 hrs · 22,417 cycles

PORTABLE ELT ROPE RETENSION TORN. TRANSFERRED TO MDDR 137443 DUE 08MAR21, IAW DDG 25-63-10-01. PLACARD INSTALLED. MCC NOTIFIED. TS 0730Z 09NOV20. REMOVED AND REPLACED ELT TRANSMITTER, IAW AMM 25-63-03. OPERATIONS CHECK NORMAL AT THIS TIME. THIS CLEARS MDDR 137443. MCC NOTIFIED. PLACARDS REMOVED. DISP: GTC AT 0636Z.

Part: CARBON SEAL — LEAKING (ENGINE OIL) · airframe 95,037 hrs · 22,390 cycles

NR 1 ENGINE OIL LINES CAPPED FOR 10 FLT CYCLES (HIGH OIL CONSUMPTION), REF NON-MEL 136533. UNCAPPED NR 1 ENGINE OIL LINES, PER 71-71-00 RECONNECTED HMV AND FUEL PUMP DRAIN LINES, PER 71-71-00. FOUND IDG WITH 2 OZ OIL AND STARTER EDP WITH 1/8TH OZ OIL. NMEL REMAINS OPEN. DRAIN LINES RECAPPED, PER 71-71-00 AND ECM 2020P-464. TRACKED UNDER NMEL 136533 ITEM NR 8. NMEL 136533 REMAINS OPEN. REMOVED AND REPLACED NR 1 ENGINE CARBON SEAL AND HYD PUMP, IAW MM72-64-04 AND 29-11-05. PERFORMED OPERATIONS CHECK AND ENGINE RUN, ALL OPERATIONS NORMAL, IAW 71-00-00. THIS CLEARS DMI 136533. (OFF PART: P/N 1347MG08 AND SN 1347MG09).

Part: WARNING LIGHT — FALSE INDICATION (LT FUEL PUMP) · airframe 94,897 hrs · 22,343 cycles

LEFT FWD FUEL PUMP PRESSURE LIGHT CAME ON MULTIPLE TIMES DURING CLIMB. PERFORMED ENGINE FUEL FEED/SYSTEM OPERATIONAL TEST, OPS OK. PERFORMED INSPECTION OF THE PRESSURE/SWITCH, NO DAMAGE NOTED, REF AMM 28-22-00-715-001.

Part: RADAR — MALFUNCTIONED (WX SYSTEM) · airframe 94,804 hrs · 22,311 cycles

WX RADAR WILL NOT PAINT WX IN ANY MODE/GAIN. RANDOM RETURNS NOT CONSISTENT WITH ACTUAL WX/TERRAIN. THIS OCCURS ON BOTH LEFT AND RIGHT SYSTEM. PERFORMED FIM 34-43 FAULT TREE 805, NO DEFECT OR FAULT DETECTED ON BOTH LEFT & RIGHT SYSTEMS (EHSI). PERFORMED OPERATIONS TEST FOR ANTENNA FUNCTION, AS PER AMM 34-43-00, FOUND OK.

Part: CONTROL VALVE — MALFUNCTIONED (APU SURGE) · airframe 94,745 hrs · 22,292 cycles

APU PNEUMATIC PRESSURE INSUFFICIENT TO START ENGINES. ISSUED MDDR 134719, IAW MEL 49-11-01A, CAT C, DUE 30SEP20 DISPATCH 1457Z ST. ITEM M4: R & R APU SURGE CONTROL VALVE, IAW AMM 49-53-01. OPS CHECK GOOD. THIS CLEARS DMI 134719. PLACARD REMOVED. MCC NOTIFIED. T/I: EH AT 13:48Z.

Part: RADAR — MALFUNCTIONED (LT WEATHER) · airframe 94,700 hrs · 22,276 cycles

LEFT WX RADAR FAIL. PERFORMED OPS TEST OF WXR SYS. NO FAULT DISPLAYED. OPS TEST OKAY, IAW AMM 34-43-00.

Part: RADAR — MALFUNCTIONED (RT WEATHER) · airframe 94,700 hrs · 22,276 cycles

RIGHT WX RADAR RETURNS IN STREAKS COULD NOT DUPLICATE DISCREPANCY. OPS TEST OKAY, WXR DISPLAYS NORMALLY, IAW AMM 34-43-00.

Part: TRANSDUCER — FAILED (APU) · airframe 94,653 hrs · 22,259 cycles

APU INOP, TRANSFERRED TO MEL 49-11-01A, MDDR 133954, CAT C. REMOVED AND REPLACED TRANSDUCER, DIFF PRESSURE SURGE, IAW B767 AMM 49-53-04. OPS CHECK GOOD AT THIS TIME. THIS CLEARS DMI #133954. MCC NOTIFIED. ALL PLACARDS REMOVED.

Part: IDG — MALFUNCTIONED (RIGHT) · airframe 94,580 hrs · 22,236 cycles

R GEN DRIVE CAUTION LIGHT ON T/O ROLL BRIEFLY, CLEARED ITSELF. ALSO SWITCH LIGHT DRIVE FLICKERED FOR THE 1ST 15 MIN OF FLIGHT. SERVICED R IDG TO SERVICE LIMITS IAW AMM 12-13-03-613-027. OPERATED R ENG AT IDLE PACE IAW AMM 71-00-00-862 FOR LEAK CHECK. LEAK CHECKED GOOD.

Part: FEEDER CABLE — FAILED · airframe 94,423 hrs · 22,181 cycles

RT GEN INOPERATIVE AT ROTATION, RESET OK FOR 15SEC THEN TRIPPED AGAIN. REMAINED OFF FOR DURATION OF FLT. PERFORMED LOW INSULATION RESISTANCE TEST ON RT IDG FEEDER CABLES TO RT GCB IAW AMM 30-10-39. FOUND BREAK IN CABLE T2 JUST AFT OF ENGINE FIREWALL. REPAIR/REPLACEMENT REQUIRED, REPLACED T2 AND T3 FEEDER CABLES IAW SWPM 20-10-11 AND WD 24-21-21 SWPM 20-30-13, ACCOMPLISHED OPERATIONAL CHECKS IAW AMM 24-11-00 AND 24-11-01. OPS CHECK GOOD.</P>)

Part: IDG — MALFUNCTIONED (RT GENERATOR) · airframe 94,407 hrs · 22,176 cycles

REJECTED TAKEOFF FOR R GEN OFF STATUS AND SCREENS FLASHING AND GOING BLANK(<P>TRANSFERRED TO MDDR 131975 MEL 24-00-01-01. CAT B.<BR /></P><P>LP 1296050: PERFORMED T/S IAW FIM 24-20 FAULT TREE 801. REMOVED AND REPLACED R/H GCU (OFF PART: PN&NBSP;734284F, SN&NBSP;5695). CKD GOOD. THIS CLEARS MDDR 131975.</P><P>29JUL, IAH, LP&NBSP;1291252:&NBSP;REJECTED TAKEOFF FOR GEN OFF ON T/O ROLL. EICAS AND NAVIGATION SCREENS CYCLED OFF AND ON. RE-OPENED MDDR 131975.</P><P>29JUL, BWI. LP 1291257 ITEM M4: REMOVED AND REPLACED R/H ENG IDG IAW AMM 24-11-00. OPS CHECK GOOD. ENG RUN PERFORMED IAW AMM 71-00-00 AND SUPERVISED BY MARK AUSMUS. THIS CLEARS MDDR # 131975. MCC NOTIFIED. PLACARD REMOVED.<BR /></P>)

Part: RADAR — UNKNOWN · airframe 94,407 hrs · 22,176 cycles

RADAR HAD EXCESSIVE SPIKING ON BOTH LT AND RT RADARS. PERFORMED TEST IAW AMM 34-43-00. SYSTEM DISPLAY TEST OK.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT FUEL PUMP) · airframe 94,420 hrs · 22,180 cycles

LEFT FWD FUEL PUMP EICAS CAME ON BRIEFLY ,LESS THAN ONE MINUTE DURING CLIMB. PERFORMED TROUBLESHOOTING PER FIM 28-22 FAULT TREE 827, SYSTEM TEST OKAY. PERFORMED OPS TEST, PERFORM 28-22-00 L/H FWD FUEL PUMP. TEST GOOD. NO FAULTS FOUND.

Part: GCU — FAILED (RT GENERATOR) · airframe 94,351 hrs · 22,154 cycles

AFTER SETTING TAKE OFF THRUST, RT ENG OFF G UTIL BUSS OFF, RT UTIL BUSS OFF, EICAS MESSAGES ILLUMINATED, COMPLIED WITH CHECKLIST. RT GEN INOPERATIVE. REMOVED & REPLACED THE GCU IAW AMM 24-22-02. OPS CHECKED NORMAL, PERFORMED ENGINE RUNS IAW AMM 71-00-00. OPS CHECKED GOOD.

Part: IDG — UNDERSERVICED (RIGHT) · airframe 94,351 hrs · 22,154 cycles

RIGHT GENERATOR OFF EICAS MESSAGE, FL 360, TWO HOURS 20 MIN AFTER TAKE OFF WITH ASSOCIATED GENERATOR OFF LIGHT IN SWITCH. PERFORMED BPCU BITE IAW FIM 24-20 FT 801. RT GENERATOR OP TRIP MESSAGE RESET BPCU AND RT GEN CONT SWITCH, FOUND IDG UNDERSERVICED, SERVICED IDG IAW AMM 12-13-03, RAN ENG IAW AMM 71-00-00. 5 MINS. ALL IDG OUTPUT NORMAL, NO ASSOCIATED MESSAGES, NO FAULTS NOTED.

Part: UNKNOWN — MALFUNCTIONED · airframe 94,173 hrs · 22,094 cycles

RT GEN OFF EICAS PERFORMED BITE OF BPCU IAW FIM 24-20 F/T 801 FLUCTUATING F/T DP TRIP; GEN/ FDR PER TABLE 102. CHECKED IDG WINDING READS PROPER RESISTANCE PER TABLE 102. CHECKED GCU AND PERFORMED ENG RUN IAW 71-00-00. OPS NORMAL. RESECURED GCU PER 24-27-02.

Part: LENS — MISSING (OXYGEN BOTTLE) · airframe 94,166 hrs · 22,092 cycles

LENS MISSING ON LAVATORY OXYGEN BOTTLE. REMOVED AND REPLACED O2 BOTTLE IAW AMM 35-31-00. OPS GOOD.

Part: CONNECTOR — BROKEN (WINDOW HEAT) · airframe 94,107 hrs · 22,072 cycles

L/H SIDE FWD WINDOW HEAT INOPERATIVE. IAW FIM 70-41 TASK 801, BITE BOX AND FAULTED ITSELF. TROUBLESHOT IAW WDM 30-11-11, FOUND CONNECTOR D2916B BROKEN, WINDOW CIRCUITS INTERNALLY CHECKED GOOD. A SIDE OF CB C391 CHECKED BAD. IAW FIM 30-41 PG 801. SWAPPED WIRES TO C SIDE, CONFIRMED GOOD BITE CHECK. SEE ITEM M3 AND M4. L1 WINDOW CHECKED GOOD. DOES NOT NEED REPLACED. DURING TROUBLESHOOTING FOUND CONNECTOR D2916B REQUIRES REPLACEMENT. REMOVE AND REPLACED CONNECTOR D2916B IAW SWPM 20-71-11 AND WDM 30-41-11. ALSO REMOVED AND REPLACED C371 WINDOWS HEAT ICE/RAIN CIRCUIT BREAKER, IAW SWPM 20-30-00, WDM 30-41-11, OPS CHECKED GOOD IAW FIM 30-41 FT 803.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 94,076 hrs · 22,062 cycles

LT FWD WINDOW EICAS IN FLIGHT, REPEAT WRITE UP. PERFORMED FC WH ANTI-ICE OPS TEST AND WH ELEMENT LOOP RESISTANCE TEST IAW AMM 30-41-00-715-001 AND 30-41-00-765-046. OPS TEST NORMAL. PERFORMED FIM 30-41 TASK 801, NO DEFECTS FOUND AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 94,076 hrs · 22,062 cycles

L FWD FUEL PUMP EICAS MESSAGE. PERFORMED OPS CHECK IAW AMM 28-22-00/501. NO FAULTS NOTED. ALL OPS NORMAL.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 94,071 hrs · 22,060 cycles

HI FLOW INHIBIT STATUS MESSAGE TRANSFERRED TO MDDR #129339 IAW MEL 21-51-02-02. PLACARDS INSTALLED. MCC NOTIFIED. PERFORMED FIM 21-51 FT 813 - PERFORMED SYSTEM FAULT RESET AND OPERATED BOTH PACKS, ALL NORMAL. NO FAULTS PRESENT. THIS CLOSES MDDR 129339. PLACARDS REMOVED. MCC ADVISED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 94,076 hrs · 22,062 cycles

LT FORWARD WINDOW HEAT EICAS MSG. PERFORMED BITE TEST OF LT WINDOW HEAT. NO DEFECTS NOTED AT THIS TIME PER FIM 30-41-00.

Part: UNKNOWN — MALFUNCTIONED (THRUST LEVER) · airframe 94,065 hrs · 22,058 cycles

THRUST LEVER MOVEMENT STICKY. NOT SMOOTH. INSPECTED AND WORKED BOTH THRUST LEVERS, NO DISCREPANCY NOTED. LOAD TEST LESS THEN 6LBS IAW AMM 76-11-00-735-100-600.

Part: COUPLER — LEAKING (IDG) · airframe 94,038 hrs · 22,050 cycles

UPON PDSC IDG OIL LEVEL CHECK FOUND OVERFLOW SERVICE COUPLER LEAKING. TIGHTENED OVERFLOW SERVICE COUPLER IAW AMM 20-11-00/201. PERFORMED ENGINE RUN IAW AMM 71-00-00 AND LEAK CHECKED IAW AMM 71-71-00 AND 24-11-01. NO LEAKS NOTED AT THIS TIME.

Part: ISOLATION VALVE — FAULTY (BLEED AIR SYS) · airframe 94,008 hrs · 22,043 cycles

DURING START, RIGHT ISOLATION VALVE DID NOT OPEN. TRANSFERRED TO MDDR 128880 AS PER MEL 36-11-06, CAT 'C'. DISP: GTC 09:27Z, ITEM M1: REMOVED AND REPLACED RIGHT ISO VALVE IAW AMM 36-11-04, OPS CHECK NORMAL. PLACARDS REMOVED. THIS CLEARS MDDR 128880.

Part: SEAL — MISSING (STARTER SHAFT) · airframe 93,999 hrs · 22,040 cycles

OIL QTY WENT TO ZERO AFTER LEVEL OFF. OIL PRESSURE STEADY DROPPED FROM 30PSI TO 12PSI AT LANDING. PERFORMED TEST OF THE NR 3 IDLE LEAK TEST IAW AMM 71-00-00-795. NR 3 FOUND LEAK FROM STARTER WITNESS CHAMBER. REMOVED STARTER IAW AMM 80-11-04. FOUND STARTER SHAFT SEAL MISSING. INSTALLED STARTER SHAFT SEAL AND STARTER IAW AMM 80-11-04. PERFORMED LEAK IDLE TEST PER AMM 71-00-00. NO FURTHER LEAKS NOTED.

Part: PNEUMATIC SYSTEM — INOPERATIVE (APU) · airframe 93,987 hrs · 22,035 cycles

DURING L ENG START WHEN STARTER MOVED TO "GND" DUCT PRESS DROPPED TO ALMOST NOTHING, N2 NEVER SPOOLED UP TO MORE THAN 15%. DUCT PRESS WAS 30 PSI PRIOR TO THIS.(<P>SWAPPED ECU WITH KNOWN GOOD PART, OPS CHECK BAD. RETURNED AIRCRAFT TO ORIGINAL CONFIG. TRANSFERRED TO MDDR #128556, CAT 'C', DUE 29MAY20. MCC NOTIFIED. PLACARDS INSTALLED. DDG 49-11-01-01. YK @ 13:46. APU PNEUMATICS INOP.</P>)

Part: STARTER — FAILED (ENGINE) · airframe 93,987 hrs · 22,035 cycles

DURING L ENG START WHEN STARTER MOVED TO "GND" DUCT PRESS DROPPED TO ALMOST NOTHING, N2 NEVER SPOOLED UP TO MORE THAN 15%. DUCT PRESS WAS 30 PSI PRIOR TO THIS.(<P>SWAPPED ECU WITH KNOWN GOOD PART, OPS CHECK BAD. RETURNED AIRCRAFT TO ORIGINAL CONFIG. TRANSFERRED TO MDDR #128556, CAT 'C', DUE 29MAY20. MCC NOTIFIED. PLACARDS INSTALLED. DDG 49-11-01-01. YK @ 13:46. APU PNEUMATICS INOP. </P><P>LP 1189517: REMOVED AND REPLACED BOTH ENGINE STARTERS (STARTER OFF PART: PN&NBSP;<SPAN>3505448-5, SN&NBSP;</SPAN><SPAN>AEX02712C</SPAN><SPAN>) AND BOTH ENGINE START VALVES (OFF PARTS: PN&NBSP;</SPAN><SPAN>3291172-3, SN 410C; PN&NBSP;3291172-3, SN 1683C</SPAN><SPAN>) IAW B767 AMM REF 80-11-01 AND 80-11-02. BOTH ENGINE STARTERS AND APU OPS CHECKED GOOD IAW AMM 71-00-00. THIS CLEARS MDDR 128556.</SPAN></P>)

Part: SKIN — CORRODED (LT HORIZ STAB) · airframe 93,984 hrs · 22,034 cycles

CORROSION WAS FOUND ON THE LH HORIZONTAL STABILIZER TOP SKIN, BETWEEN FRONT SPAR AND RIB 3.(<P ><SPAN>CORROSION WAS REWORKED AND / THE SKIN WAS REPAIRED IN ACCORDANCE WITH MEXICANA MRO TRE6755032.</SPAN></P>)

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 93,984 hrs · 22,034 cycles

PREVIOUS REWORK WITH CORROSION DAMAGE WAS FOUND AROUND STATIC PORT BETWEEN STA 1285 / STA 1307 AND STRINGERS S-28L / S-29L.(<P ><SPAN>DAMAGE WAS REPAIRED IN ACCORDANCE / WITH MEXICANA MRO TRE6753350 AND IAI CS-24086-015</SPAN></P><P ><SPAN></SPAN></P>)

Part: SKIN — DENTED (TAILCONE) · airframe 93,984 hrs · 22,034 cycles

DENT WITH CREASE WAS FOUND ON FUSELAGE TAIL CONE SKIN BETWEEN STA 1832 / STA 1843 RH SIDE(<P ><SPAN>DAMAGE REPAIRED IN / ACCORDANCE WITH MEXICANA MRO TRE6753348.</SPAN></P>)

Part: SKIN — GOUGED (BS 1417-1430) · airframe 93,984 hrs · 22,034 cycles

GOUGE DAMAGE WAS FOUND ON FUSELAGE SKIN BETWEEN STA 1417 / STA 1430 AND STRINGERS S-19L / S-20L. DAMAGE REPAIRED IN ACCORDANCE WITH B767-300 SRM 53-00-01-2R-14.

Part: SPLICE PLATE — CORRODED (FUSELAGE) · airframe 93,984 hrs · 22,034 cycles

CORROSION DAMAGE WAS FOUND ON THE SPLICE PLATE AT STA 977 AND STRINGER S-23L(<P ><SPAN>CORROSION DAMAGE WAS REMOVED / AND REPAIRED IN ACCORDANCE WITH MEXICANA MRO TRE6753347</SPAN></P>)

Part: SUPPORT BEAM — CORRODED (RT WING) · corrosion level 2 · airframe 93,984 hrs · 22,034 cycles

CORROSION WAS FOUND ON THE RH WING FIXED TRAILING EDGE SUPPORT BEAM BETWEEN AT BL 97.42, BETWEEN STA 957.80 / STA 1000.10.(<P ><SPAN>DAMAGE WAS REPAIRED IN / ACCORDANCE WITH MEXICANA MRO TRE6757157.</SPAN></P>)

Part: SKIN — CORRODED (RT HORIZ STAB) · corrosion level 2 · airframe 93,984 hrs · 22,034 cycles

CORROSION OVER PREVIOUS REWORKS WAS FOUND ON THE RH HORIZONTAL STABILIZER TOP SKIN AT REAR SPAR AND BETWEEN RS STA 128.605 - RS STA 251.105(<P ><SPAN>DAMAGES REPAIRED IN / ACCORDANCE WITH MEXICANA MRO TRE6755033.</SPAN></P>)

Part: STRAP — CRACKED (FUSELAGE) · airframe 93,984 hrs · 22,034 cycles

CRACK INDICATION WAS FOUND ON THE LH &AMP; RH FAIL SAFE STRAPS DURING ACCOMPLISHMENT OF EO 6753A070 PARTS 1 AND 2(<P ><SPAN>CRACK DAMAGES WERE REPAIRED / IN ACCORDANCE WITH EO 6753A070 PARTS 3 AND 4</SPAN></P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (BLEED AIR SYS) · airframe 93,937 hrs · 22,017 cycles

L ENGINE BLEED DISCREET LIGHT ILLUMINATED BETWEEN 8000-15000 WITH 102.0 N2 AND 103.6 N1 RESPECTIVELY.(<P>PERFORMED AIR SUPPLY CONTROL SYSTEM BITE TEST&NBSP; IAW B767AMM TASK 36-23-00 715-001. NO FAULTS NOTED.</P>)

Part: BLEED AIR SYS — MALFUNCTIONED (APU) · airframe 93,915 hrs · 22,008 cycles

DUCT PRESSURE FOR BOTH ENGINE STARTS WAS 15 PSI, MAX MOTORING TO BOTH STARTS WAS 18% N2, BOTH ENGINE STARTS NORMAL BUT TOOK LONGER THAN USUAL.(<P>DEFERRED APU BLEED AIR SYSTEM IAW ATLAS DDG 49-11-01-01, MDDR 126571, CAT "C".</P>)

Part: OXYGEN BOTTLE — UNSERVICEABLE (CABIN) · airframe 93,881 hrs · 21,996 cycles

GALLEY PORTABLE O2 BOTTLE PRESSURE OUT OF LIMITS.(<P>TRANSFERRED TO MDDR 126397, MEL 35-31-01, CAT 'D', DUE DATE: 27JUL20, TI: TS @ 0247Z. 2 SERVICEABLE PORTABLE O2 BOTTLES STILL ON BOARD, STOWED UNSERVICEABLE BOTTLE IN OVERHEAD BIN PER AMM 35-00-00.</P><P>30MAR, IAH LP 1186536, ITEM M4: INSTALLED PORTABLE O2 BOTTLE AS PER AMM 35-31-00. THIS CLEARS DMI 126297. SD @ 18:54Z.</P>)

Part: OIL SYSTEM — LOW (APU) · airframe 93,870 hrs · 21,992 cycles

APU OIL QUANTITY LOW, APU SHUT DOWN ON DESCENT.(<P>SERVICED APU OIL I/A/W AMM 12-13-04, APU OPS CHECK NORMAL.</P>)

Part: ECU — FAULTY (APU) · airframe 93,870 hrs · 21,992 cycles

APU AUTO SHUTDOWN AFTER MINUTES, ECU WON'T TEST.(<P>REMOVED AND REPLACED ECU IAW AMM 49-61-05, OPS CHECK NORMAL.</P>)

Part: FUEL FILTER — FAULTED (LT ENGINE) · airframe 93,846 hrs · 21,984 cycles

L ENG FUEL FILT ADVISORY SG AND STATUS MSG ILLUMINATED IN FLIGHT. NO ABNORMAL ENGINE INDICATIONS NOTED.(<P>REMOVED AND REPLACED L ENG FUEL FILTER IAW AMM 73-11-02. LEAK CHECK GOOD.<BR /></P>)

Part: UNKNOWN — MALFUNCTIONED (BLEED AIR SYS) · airframe 93,827 hrs · 21,975 cycles

DURING ENGINE START, APU AIR DROPPED TO 15 PSI, FLUCTUATING 2-3 PSI. MAX MOTORING ACHIEVED WAS 16% N2 ON RIGHT ENGINE.(<P>PERFORMED T/S PER FIM 36-10 FAULT TREE 840 AND BITE AIR SUPPLY MODULE PERFORMED AND FOUND NO FAULTS AT THIS TIME.</P>)

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 93,827 hrs · 21,975 cycles

DURING DAILY CHK FOUND EMERGENCY FLASH LIGHT INOP.(<P>REMOVED AND REPLACED EMER FLASH LIGHT BATTERY, OPS CHK GOOD IAW 25-64-00.<BR /></P>)

Part: ELT — INOPERATIVE (GALLEY) · airframe 93,807 hrs · 21,971 cycles

PORTABLE ELT INOP IN GALLEY. ONE SERVICEABLE UNIT REMAINS (EMERGENCY LOCATOR TRANSMITTER (ELT), SURVIVAL TYPE ELTS).(<P>TRANSFERRED TO MDDR 125108, CAT 'D', MEL 25-63-10-01, DUE DATE 25JUN20. NOTIFIED MCC.</P><P>LP 1197029 - ITEM M6: REMOVED &AMP; REPLACED PORTABLE ELT IN GALLEY IAW AMM 25-13-03. THIS CLEARS DMI #125108.</P>)

Part: FILTER — DIRTY (BLEED AIR SYS) · airframe 93,827 hrs · 21,975 cycles

INFO &AMP; DUCT PRESSURE BELOW OPTIMUM 21 PSI UNTIL START VALVE OPEN DURING RIGHT ENGINE START.(<P>PERFORMED DRY MOTORIZED R/H ENG IAW AMM 71-00-00, VERIFIED PNEUMATIC PRESS I.A.W. AMM 36-11-00 PRESSURE WITHIN LIMITS, 30 PSI. SEE LOG PAGE #1197014.<BR /></P><P>LP 1197014: PERFORMED CHECK R/H ENG PRSOV CONTROL PRESSURE FILTER I.A.W. F.I.M. 36-10 FAULT TREE 840, PROCEED TO CLEAN FILTER I.A.W. AMM 36-11-09. OPS TEST OK. PNEUMATIC PRESSURE 30 PSI.<BR DATA-MCE-BOGUS="1" /></P><P><BR DATA-TEMP="1" /></P>)

Part: ECU — MALFUNCTIONED (APU) · airframe 93,767 hrs · 21,954 cycles

ON INITIAL ENGINE START (R-CVG) (L-DEN), APU BLEED AIR PRESSURE IS FLUCTUATING BETWEEN 15 AND 25 PSI, RESULTING IN MAX MOTORING OF 19.5 N2 ONLY.(<P>TRANSFERRED TO DMI 124990, CAT C, DUE 04MAR20 IAW MEL 49-11-01-01.</P><P>LP 1196990: PERFORMED APU BITE IAW FIM 49-11 FT 958, MINI FLAG 36 PRESENT. REMOVED AND REPLACED ECU IAW AMM 49-61-05. OPS CHECK GOOD IN PACK ECS AND IDLE MODES PER AMM 36-00-21. THIS CLEARS DMI 124990. PLACARD REMOVED.</P>)

Part: EEC — MALFUNCTIONED (LT ENGINE) · airframe 93,754 hrs · 21,949 cycles

LEFT ENGINE CONTROL ON EICAS AND STATUS MESSAGE.(<P>PERFORMED FIM 73-21 FAULT TREE 878 AND 71-01 TASK 936. REMOVED AND REPLACED LEFT ENGINE EEC, TESTED AND FOUND OK AS PER AMM 73-21-15. PERFORMED ENGINE RUN UP AS PER AMM 71-00-00. NO FAULT FOUND AT THIS TIME.</P>)

Part: SENSOR — INOPERATIVE (APU) · airframe 93,675 hrs · 21,924 cycles

APU PNEUMATICS INOP (AUXILIARY POWER UNIT, PNEUMATIC FUNCTION)(C/W DDG PROCEDURE 36-11-04)(<P>TRANSFERRED TO MDDR #124303 IAW DDG 49-11-01-01. MX ACTION C/W, CAT 'C', DUE 14FEB20. MCC GLEN&NBSP; NOTIFIED. PLACARDS INSTALLED.</P><P>LOG PAGE 1190476: REMOVED AND REPLACED APU FLOW SENSING MODULE I.A.W AMM 49-53-08. NO DEFECT NOTED. OPS CHECK OK.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,675 hrs · 21,924 cycles

REPEAT WRITE UP (1ST WRITE UP ON LP #1182887), ON BOTH ENGINE STARTS DUCT PRESSURE DROPPED TO AROUND 20 PSI AND N2 MAX MOTORED TO 12%-19% N2 BEFORE RUN SWITCHES ENGAGED (BOTH PACKS OFF).(<P>PERFORMED BITE TEST OF APU CONT. UNIT, NO FAULTS. APU DUCT PRESS NORMAL, ALL MODES. REF AMM FIM 49-11 FT 982.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (DUCT PRESSURE) · airframe 93,650 hrs · 21,918 cycles

ON BOTH ENG STARTS, DUCT PRESS DROPPED TO AROUND 20 PSI AND N2 MAXED AT 19% BEFORE RUN SWITCHES ENGAGED.(<P>PERFORMED FAULT ISOLATION MANUAL 49-11 FAULT TREE 982 FOR LOW DUCT PRESSURE IN MAIN ENGINE START MODE ONLY. FOUND NO LOW PRESSURE OR SURGING. FOUND NO FAULTS DURING BITE PROCEDURE. DUCT PRESSURE NORMAL AND NO FAULTS NOTED DURING DRY MOTOR RUNS ON BOTH ENGINES, SYSTEM OPS CHECK NORMAL AT THIS TIME.</P>)

Part: CAP — UNSECURE (ENGINE OIL TANK) · airframe 93,618 hrs · 21,910 cycles

1000 FT PRIOR TO LEVEL OFF AT FL 370, WE NOTICED R ENG OIL PRESS INDICATION AMBER AT 28. IT REMAINED AMBER FOR DURATION OF FLIGHT. ALL OTHER INDICATIONS NORMAL. AFTER FURTHER INSPECTION, FOUND OIL TANK FILLER CAP NOT SECURED. SERVICED ENG OIL TO PROPER LEVEL AND CLEANED FAN COWLINGS, SECURED OIL FILLER CAP, OPERATED ENG, AND FOUND NO DEFECTS AT THIS TIME IAW AMM 12-13-01 AND 71-00-00.

Part: UNKNOWN — UNKNOWN (RT GENERATOR) · airframe 93,597 hrs · 21,904 cycles

RIGHT ENG GENERATOR INOPERATIVE. RT IDG DISCONNECTED. PERFORMED ENGINE IDLE RUNS TWICE IAW AMM 71-00-00 AND COMPLETED OPERATIONAL TESTS OF RT IDG IAW AMM 24-11-00, NO DEFECTS NOTED. IDG OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT BLEED SYSTEM) · airframe 93,600 hrs · 21,905 cycles

ON INITIAL CLIMB, LEFT BLEED LIGHT ILLUMINATED FOR SEVERAL SECONDS, NO EICAS MSG. REPEAT WRITE UP.(<P>PERFORMED BITE TEST ON AIR SUPPLY CONTROL UNIT IAW AMM 36-23-00. OPS TEST OK, NO FAULTS NOTED.</P>)

Part: RELAY — FAILED (FUEL SYSTEM) · airframe 93,578 hrs · 21,896 cycles

LEFT FUEL OVERRIDE PUMP CB FOUND POPPED. TRANSFERRED TO MDDR 123426 IAW MEL 28-22-02A, CAT 'C', DUE 25JAN2020. PERFORMED FIM 28-22 FT 812, TO STEP 21, R&R RELAY K329 L FUEL OVERRIDE PUMP CONT. RELAY IAW WDM 28-22-12. OPS CHECK OF L CTR PUMP GOOD AT THIS TIME. THIS CLEARS DMI 123426, MCC NOTIFIED. ZH @ 24:22Z. PLACARDS REMOVED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 93,566 hrs · 21,893 cycles

ON CLIMB OUT, LEFT BLEED LIGHT ILLUMINATED. NO EICAS MSG. LIGHT STAYED ON FOR SEVERAL MINUTES, NO EICAS MSG, THEN IT WENT OUT. WRITTEN UP BEFORE. PERFORMED AIR SUPPLY BITE TEST, NO FAULTS, REF AMM 36-20 FT 805 AND 36-23-00. REMOVED AND RE-RACKED AIR SUPPLY CONTROLLER, REF AMM 36-11-02. PERFORMED AIR SUPPLY PRESSURE IND. CHECKS, REF AMM 36-21-00. OPS CHECKS GOOD. ACFT RELEASED FOR FLIGHT.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 93,555 hrs · 21,889 cycles

ON CLIMB OUT, THE LEFT BLEED WAS ILLUMINATED MOMENTARILY.(<P>PERFORMED PUSH TO TEST, OPS CHECK GOOD ON LIGHT. PERFORMED BITE TEST TO AIR SUPPLY CONTROL. NO FAULTS NOTED ON BOX. PERFORMED AIR SUPPLY PRESSURE INDICATION TEST IAW AMM 36-21-00. OPS CHECK GOOD. NO PRESSURE LOSS. NO LEFT BLEED ILLUMINATION NOTED.</P>)

Part: SENSOR — FAULTY (LT ENGINE) · airframe 93,545 hrs · 21,885 cycles

MX MSG L ENG EEC C2, PER THE COMPANY REQUEST REPLACE #1 ENG CIT SENSOR T2.5.(<P>REMOVED AND REPLACED #1 ENGINE CIT SENSOR I.A.W AMM 73-21-02 AND ECM 20-20D-018. OPS CHECK GOOD.</P>)

Part: UNKNOWN — MALFUNCTIONED (COCKPIT) · airframe 93,560 hrs · 21,891 cycles

DURING PRE-FLIGHT FMC PROMPT ON UPPER EICAS STAYS DISPLAYED WITH IRU'S ALIGNED AND ALL FMC DATA ENTERED.(<P>CYCLED APU POWER I.A.W AMM 49-11-00. FMC MESSAGE WENT AWAY. OPS CHECK GOOD.</P>)

Part: PROCESSING UNIT — MALFUNCTIONED (FUEL BALANCE) · airframe 93,508 hrs · 21,869 cycles

SUSPECT FUEL LEAK LT ENG. FUEL IMBALANCE AS MUCH AS 1.0K AND TOTALIZER /CALCULATED TO DIFF AS MUCH AS 2.5K. FUEL WAS BALANCED 2HR INTO FLIGHT, ALSO FUEL XFEED VALVE CHECKED SUCCESSFUL. PERFORMED A BIT PROCEDURES IAW AMM 28-41-00, WAS FAULTING PROCESSOR. REPLACED FUEL QTY PROCESSOR IAW AMM 28-41-08. PERFORMED BIT PROCEDURE WITH NEW PROCESSOR UNIT, GAVE FAULT CODE D2. RESET CIRCUIT BREAKERS FOR FQIS PROCESSOR UNIT AND RESET UNIT, PERFORMED OPS TEST OF FQIS, SUCCESSFUL IAW 28-41-00.

Part: CONTROLLER — MALFUNCTIONED (LT BLEED) · airframe 93,508 hrs · 21,869 cycles

LT BLEED LIGHT CAME ON DURING CLIMBOUT FROM 7,000 TO 15,000, NO BLEED EICAS MSG PRESENT. LIGHT EXTINGUISHED AFTER LEVEL OFF @15,000 AND BEFORE QRH WAS ACCOMPLISHED. PERFORMED AIR SUPPLY BITE TEST, FAULTING HIGH PRESSURE CONTROLLER ON LEFT SIDE, IAW AMM 36-23-00. REMOVED AND REPLACED LEFT ENGINE HIGH PRESSURE CONTROLLER IAW AMM 36-11-08. AIR SUPPLY BITE TEST AND LEAK CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PUMP) · airframe 93,452 hrs · 21,853 cycles

"CTR R FUEL PUMP" EICAS MSG PRIOR TO ADVANCING THRUST LEVERS FOR TAKEOFF. 4000 LBS FUEL IN CTR TANK. CYCLED FUEL PUMP SWITCH PER MX CONTROL, OPERATED NORMALLY.(<P>C/W OPERATIONAL TEST OF CTR R BOOST PUMP IAW B767 AMM 28-22-00, PUMP OPS CHECK NORMAL.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (BOOST PUMPS) · airframe 93,443 hrs · 21,849 cycles

IN FLIGHT, CTR LEFT FUEL AND CENTER RIGHT FUEL PUMP EICAS MESSAGES DO NOT DISPLAY WHEN CTR TANK QTY REACHES ZERO.(<P>PERFORMED TEST OF BOOST PUMPS, ALL OK IAW B767 AMM 28-00-00. FOUND SYSTEM TO OPERATE NORMAL AT THIS TIME.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PUMP) · airframe 93,439 hrs · 21,848 cycles

CENTER R FUEL PUMP AND CENTER L FUEL PUMP EICAS MESSAGES. DOES NOT DISPLAY WHEN CENTER FUEL TANK QUANTITY REACHES ZERO.(<P>PERFORMED OPERATIONAL TEST OF THE CENTER L/R FUEL PUMPS ON EICAS, OPS CHECK GOOD IAW AMM 28-42-00, AMM 28-42-01, AND AMM 28-22-01.&NBSP;</P>)

Part: RELAY — FAILED (GFI) · airframe 93,390 hrs · 21,830 cycles

AFTER START, R FWD FUEL PUMP EICAS ILLUMINATED. PERFORMED FIM 28-22 ON GROUND POWER, APU POWER, AND ENGINE BLEED PRESSURE SENSE LINE RT IAW FIM IAW AMM 28-42-01. OPS CHECKED GOOD. MX PROCEDURE COMPLIED WITH. REMOVED AND REPLACED RELAY K10704 IAW WDM 28-22-11 AND SWPM 20-81-22. PERFORMED OPS CHECK OF THE FWD RT FUEL PUMP IAW AMM 28-22-00.

Part: FIRE WARNING — FALSE ACTIVATION · airframe 93,380 hrs · 21,827 cycles

EICAS MSG ON SHORT FINAL, FIRE/OVERHEAT SYSTEM.(<P>PERFORMED SYSTEM TEST OF THE FIRE/OVERHEAT SYSTEM IAW AMM 26-10-00, COULD NOT DUPLICATE. OPS CHECKS OKAY AND NO FURTHER FAULTS NOTED.</P>)

Part: CIRCUIT CARD — MALFUNCTIONED (APU FIRE LOOP) · airframe 93,376 hrs · 21,825 cycles

DURING CREW PRE-FLIGHT, STATUS MESSAGE "APU FIRE LOOP 1".&NBSP;(<P>TRANSFERRED TO DMI 121097 IAW MEL 26-15-01-01, CAT 'C',&NBSP; DUE DATE: 04-DEC-19.</P><P>LP 1223654 - M6: REMOVED AND REPLACED APU LOOP 1 PRINTED CIRCUIT CARD 685T, OPS CHECK GOOD. THIS CLEARS DMI 121097 IAW AMM 26-10-01. PLACARDS REMOVED AND MCC NOTIFIED.</P>)

Part: OVERHEAT LOOP — OUT OF ADJUST · airframe 93,373 hrs · 21,824 cycles

EICAS FIRE/OVHT SYS.(<P>PERFORMED ADJUSTMENT TEST OF FIRE OVHT SYS IAW AMM 26-11-00, OPERATIONAL TEST NORMAL.</P>)

Part: PIN — BROKEN (F/O OXYGEN MASK) · airframe 93,373 hrs · 21,824 cycles

FO'S O2 MASK PIN ON DOOR BROKEN.(<P>FOUND FO'S O2 MASK SERVICEABLE. RE-ALIGNED DOOR PIN AND STOWED MASK IAW AMM 35-11-51. OPS TEST NORMAL AND LEAK CHECK GOOD.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (FIRE DETECTION) · airframe 93,348 hrs · 21,813 cycles

FIRE/OVERHEAT SYSTEM EICAS ILLUMINATED ON APPROACH.&NBSP;(<P>PERFORMED AFOLTS TEST, NO DEFECT FOUND AT THIS TIME PER FIM 26-10 FAULTS TREE 803.</P>)

Part: CIRCUIT BREAKER — OPEN (FUEL OVERIDE) · airframe 93,295 hrs · 21,792 cycles

ON PRE-FLIGHT, L FUEL OVERRIDE CIRCUIT BREAKER OPEN.(<P>RESET L FUEL OVERRIDE PUMP CIRCUIT BREAKER IAW AMM 20-60-05. OPS CHECKED GOOD AT THIS TIME IAW AMM 28-22-00.</P>)

Part: CONNECTOR — DAMAGED (FIRE LOOP) · airframe 93,293 hrs · 21,791 cycles

DURING POST-FLIGHT INSPECTION, DISCOVERED "APU FIRE LP 1" STATUS MESSAGE.&NBSP;(<P>TRANSFERRED TO&NBSP;DMI #120417 PER MEL CH 26-15-01-01, CAT "C".</P><P>LP 0994698 - M9: PERFORMED RESISTANCE CHECK 3.2 OHMS. NO TIME TO CHECK UPPER LOOPS, MDDR #120417 REMAINS OPEN PER FIM 26-15 FT 805.</P><P>LP 1233178 - M4: REMOVED AND REPLACED UPPER LOOP 1 CONNECTOR ON CABLE (W260453R) IAW SWPM 20-62-16. OPS CHECK OK IAW AMM 26-15-00. THIS ACTION CLEARS DMI 120417. PLACARDS REMOVED AND MCC NOTIFIED.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (APU FIRE LOOP) · airframe 93,273 hrs · 21,786 cycles

APU FIRE LOOP 1.&NBSP;(<P>PERFORMED APU FIRE DETECTION SYSTEM OPS TEST TWICE, NO DEFECTS NOTED AT THIS TIME. APU FIRE LP 1 REMAINS EXTINGUISHED, NO MESSAGES DISPLAYED REF B767 AMM 26-15-00.</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 93,242 hrs · 21,776 cycles

APU FIRE LP 1 STATUS MSG.(<P>RESET POWER AND CONDUCTED FIRE LOOP TEST, TEST OK IAW AMM 26-15-00.</P>)

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 93,247 hrs · 21,778 cycles

STATUS MSG: APU FIRE LP 1.(<P>PERFORMED FIM 26-15 FAULT TREE 804, SYSTEM OPERATES NORMALLY, COULD NOT DUPLICATE.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 93,236 hrs · 21,773 cycles

WXR FAIL ON EADI.(<P>CYCLED C/B AND ACCOMPLISHED TEST REF AMM 34-43-00, ALL CHECKS OK.</P>)

Part: LANYARD — TORN (ENTRY DOOR) · airframe 93,228 hrs · 21,771 cycles

ON ARRIVAL, FOUND MAIN ENTRY DOOR ELT LANYARD TORN.(<P>REMOVED AND REPLACED MAIN ENTRY DOOR ELT, REFERENCE AMM 25-63-03.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (OVERHEAT SYS) · airframe 93,208 hrs · 21,763 cycles

FIRE/OVERHEAT SYSTEM EICAS ON FINAL.(<P>PERFORMED FIRE/OVERHEAT SYSTEM TEST PER AMM 26-11-01, OPS CHECK GOOD.</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (APU FIRE LOOP) · airframe 93,206 hrs · 21,762 cycles

STATUS MSG APU FIRE LOOP 1.&NBSP;(<P>TRANSFERRED TO MDDR #119805 IAW MEL 26-15-01-01, CAT C, DUE DATE: 07-NOV-2019. PLACARDS INSTALLED AND MCC NOTIFIED.&NBSP;</P><P>LP 1212659 - M11: PERFORMED TEST AND OPS CHECK OF APU LOOP IAW B767 AMM 26-11-01, OPS CHECK GOOD. PERFORMED VISUAL INSPECTION OF APU FIRE LOOP, NO DEFECTS NOTED. THIS CLEARS MDDR 119805.&NBSP;MCC NOTIFIED AND PLACARDS REMOVED.</P>)

Part: PRESSURE SWITCH — MALFUNCTIONED (FUEL SYSTEM) · airframe 93,206 hrs · 21,762 cycles

R FWD FUEL PUMP EICAS.(<P>TRANSFERRED TO MDDR #119797 PER DDG 28-22-01, CAT 'C', DUE DATE: 07-NOV-19. MTX PROC C/W, MCC NOTIFIED AND PLACARDS INSTALLED. RESTRICTED TO 120 MIN.&NBSP;</P><P>LP 1212657 - M6: REMOVED AND REPLACED R/H FWD BOOST PUMP IAW AMM 28-22-03. OPS CHECK &AMP; LEAK&NBSP; CHECK GOOD, NO DEFECTS NOTED AT THIS TIME. OFF PART (PN: 5006003D, SN: 2024).</P><P>LP 1212659 - M12: ADDITIONAL TROUBLESHOOTING NEEDED, MDDR 119797 RE-OPENED.&NBSP;</P><P>LP 1212575 - M2: REMOVED AND REPLACED LEFT FWD BOOST PUMP PRESSURE SWITCH IAW AMM 28-42-01, OPS AND LEAK CHECK GOOD.</P><P>LP 1212575 - M3: RESET GFI RELAY IN P141. R FWD BOOST PUMP OPS CHECK GOOD PER AMM 28-22-00. THIS CLEARS MDDR 119797. PLACARDS REMOVED AND MCC NOTIFIED.</P>)

Part: CONTROL VALVE — LEAKING (APU OIL COOLER) · airframe 93,160 hrs · 21,744 cycles

APU OIL COOLER TEMP CONTROL VALVE LEAKING.&NBSP;&NBSP;(<P>DEFERRED APU IAW MEL 49-11-01A, TRANSFERRED TO DMI #119428. MCC NOTIFIED AND ALL PLACARDS INSTALLED.</P><P>LP 1116578 - M18: REMOVED AND REPLACED APU OIL COOLER TEMP CONTROL VALVE IAW B767 AMM 49-27-10. OPS CHECK GOOD, NO LEAKS NOTED. THIS CLEARS MDDR #119428. PLACARDS REMOVED AND MCC NOTIFIED.</P>)

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 93,160 hrs · 21,744 cycles

CABIN AUTO PRESSURE 2 CONTROLLER EICAS MSG.(<P>REMOVED AND REPLACED AUTO PRESSURE CONTROLLER IAW AMM 21-31-02, OPS CHECK GOOD.</P>)

Part: TRANSMITTER — FLUCTUATES (APU OIL QTY) · airframe 93,160 hrs · 21,744 cycles

APU OIL QUANTITY INDICATION FLUCTUATING ON EICAS BETWEEN .50 AND FULL.(<P>REMOVED AND REPLACED OIL QUANTITY TRANSMITTER IAW AMM 49-94-04. OPS CHECK AND LEAK CHECK GOOD.</P>)

Part: FIRE WARNING — FALSE ACTIVATION · airframe 93,160 hrs · 21,744 cycles

FIRE/OVERHEAT SYSTEM ILLUMINATED ON SHORT FINAL.(<P>PERFORMED AUTOMATIC FIRE/OVERHEAT TEST, TEST GOOD PER B767 AMM 26-10-00.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (APU FIRE LOOP) · airframe 93,141 hrs · 21,737 cycles

APU FIRE LOOP 1 STATUS MESSAGE. TROUBLESHOOT IAW FIM 26-15 FAULT TREE 804, STEPS 1 AND 2. SYSTEM OPS CHECK NORMAL AT THIS TIME.

Part: STATUS MESSAGE — FALSE ACTIVATION · airframe 93,114 hrs · 21,728 cycles

STATUS - CABIN ALTITUDE AUTO 2. PERFORMED AUTO PRESSURE CONTROLLER BITE CHECK, NO FAULTS FOUND. RESET BOX, MESSAGE STAYS EXTINGUISHED REF B767 AMM 21-31-00.

Part: CONTROL VALVE — FAILED (LT A/C PACK) · airframe 93,114 hrs · 21,728 cycles

LEFT PACK OFF. REMOVED AND REPLACED FLOW CONTROL VALVE IAW B767 AMM 21-51-01. LEAK CHECK AND OPS CHECK GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT FUEL PUMP) · airframe 93,070 hrs · 21,715 cycles

"L FWD FUEL PUMP" EICAS MSG DURING CLIMB UNTIL CRUISE. RAN QRH, MSG DISAPPEARED PRIOR TO QRH COMPLETION. COMPLIED WITH FIM 28-22 F/T 819, COULD NOT DUPLICATE FAULT. THE FUEL PUMP OPS NORMAL . ACFT OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT FUEL PUMP) · airframe 93,064 hrs · 21,712 cycles

"LEFT FWD FUEL PUMP" EICAS MESSAGE CAME ON TWICE, FOR 1 - 2 MINUTES, JUST PRIOR TO REACHING CRUISE ALT. COMPLIED WITH FIM 28-22 FT 819, COULD NOT DUPLICATE. FUEL PUMP OPS CHECKED NORMAL. ACFT OK FOR SERVICE.

Part: STATUS MESSAGE — FALSE INDICATION (APU FIRE LOOP) · airframe 93,050 hrs · 21,705 cycles

PRIOR TO ENG START, APU FIRE LP 1 STATUS MSG. C/W OPS TEST OF APU FIRE DETECTOR LOOP IAW AMM 26-15-02. ALSO, INSPECTED ELECTRICAL CONNECTOR AND PIN. FOUND NO ISSUES, OPS CHECK GOOD.

Part: START VALVE — NOT REPORTED (LT ENGINE) · airframe 93,041 hrs · 21,699 cycles

PER POWERPLANT ENGINEERING, CHANGE L/H ENGINE STARTER VALVE.&NBSP;(<P>REMOVED AND REPLACED L/H ENGINE STARTER VALVE IAW B767 AMM 80-11-02.&NBSP;OPS AND LEAK CHECK GOOD AT THIS TIME.&NBSP;</P>)

Part: PUMP — MALFUNCTIONED (FUEL SYSTEM) · airframe 93,033 hrs · 21,696 cycles

DURING TAXI OUT CENTER LEFT FUEL PUMP EICAS MESSAGE DISPLAYED WITH APPROX 33.1 LBS OF FUEL IN CENTER TANK. REMOVED AND REPLACED LEFT OVERRIDE PUMP IAW AMM 28-22-05. OPS AND LEAK CHECK GOOD AT THIS TIME.

Part: SURGE VALVE — INOPERATIVE (APU) · airframe 93,015 hrs · 21,689 cycles

APU PNEUMATIC FUNCTION INOPERATIVE. REMOVED AND REPLACED APU SURGE VALVE IAW AMM 49-53-01, OPS CHECKED GOOD. PERFORMED OPS TEST OF APU IAW AMM 49-05-00, OPS CHECKED GOOD.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 92,978 hrs · 21,677 cycles

STATUS MSG AFT EQ EXH FAN 2. AFT EQ EXHAUST FAN 2 PLACED ON MEL 21-58-05, DMI #118029, DUE 01-OCT-19. NO MX ACTION REQUIRED. LP 1211040 - M6; NO EICAS STATUS MESSAGE IN VIEW. #2 AFT EQUIPMENT EXHAUST FAN OPS CHECK NORMAL IAW AMM 21-26-00. THIS CLEARS MDDR 118029. PLACARDS REMOVED.

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 92,965 hrs · 21,673 cycles

WX RADAR INOP. PERFORMED OPERATIONAL TEST OF WEATHER RADAR SYSTEM. CHECKED NORMAL ON GROUND, NO FAULTS NOTED REF AMM 34-43-00.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 92,958 hrs · 21,671 cycles

STATUS MSG "R ENG SPEED CARD" AFTER TAKEOFF. PERFORMED TEST AS PER FIM 73-21 FAULT TREE 871. SYSTEM OPS CHECK NORMAL.

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 92,958 hrs · 21,671 cycles

L & R RADAR PRODUCING SPOKE ARTIFACTS, MAKING RADAR UNUSABLE. PERFORMED TEST IAW AMM 34-43-00, OPS CHECK NORMAL.

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 92,957 hrs · 21,670 cycles

APU GENERATING INSUFFUCUENT PSI FOR ENGINE START. LESS THAN 15 PSI, ADP WAS IN OFF POSITION. TRANSFERRED TO MDDR 117929 IAW DDG 49-11-01A, CAT 'C', DUE 29SEP19. MCC NOTIFIED AND PLACARDS INSTALLED. LP 1211031 - M1: AMENDED DDG 49-11-01A TO NEW DDG. REF 49-11-01-01. APU PNUMATIC FUNCTION ONLY INOP. APU ELECTRICAL WORKS NORMAL. LP 1211040 - M4: APU PNEUMATIC OPS CHECK NORMAL PER AMM 36-10-00. ACCOMPLISHED APU BITE PER FIM 49-11-00 TASK 958. NO FAULTS NOTED. ACCOMPLISHED ENG RUN UP PER AMM 71-00-00. THIS CLEARS MDDR 117929. PLACARD REMOVED. CONFIRMED ADP SYS OFF. NO LEAKS. GOOD PNEUMATIC PRESSURE DURING RUN.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 92,957 hrs · 21,670 cycles

STATUS MSG, RT ENG SPEED CARD. PERFORMED FIM 73-21 FAULT TREE 871. PERFORMED ERASE PROCEDURE AND MSG DID NOT RETURN. SYSTEM CHECKS GOOD AT THIS TIME.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 92,920 hrs · 21,657 cycles

AFT EQ EXH FAN 2 STATUS MESSAGE. PERFORMED FIM TASK 21-26 FAULT TREE 808 PERFORMED MESSAGE ERASE PROCEDURE PER AMM 31-41-00 MESSAGE REMAINS EXTINGUISHED.

Part: UNKNOWN — ODOR · airframe 92,918 hrs · 21,656 cycles

STRONG SMELL AT ALTITUDE WHEN PACK TEMP WAS SELECTED AFTER. PERFORMED OPS CHECK OF LT PACK NO SMELL PRESENT IAW AMM 21-00-00.

Part: CONTROL VALVE — MALFUNCTIONED (AC BAY) · airframe 92,918 hrs · 21,656 cycles

R PACK INOP. TRANSFERRED TO MDDR #117481 PER DDG 21-51-01-01 CAT C DUE 18-SEP-19 MX ACTION C/W. R/R FLOW CONTROL VALVE IAW AMM 21-51-01. OPS CK NORMAL DMI CLOSED.

Part: PIN — STUCK (OXYGEN MASK) · airframe 92,918 hrs · 21,656 cycles

F/O OXYGEN MASK "RESET TEST" PIN IS STUCK IN. RESET AND SEATED PIN ON F/O'S OXYGEN MASK BOX. OPS CHECK IS GOOD. REF AMM 35-11-51.

Part: MODULATING VALVE — MALFUNCTIONED (APU) · airframe 92,898 hrs · 21,649 cycles

DURING RIGHT ENGINE START, DUCT PRESSURE OSCILLATED BETWEEN 16 TO 18 PSI. N2 MAX MOTORING WAS 18.3%. TRANSFERRED TO MDDR 117406 IAW MEL 49-11-01-01, CAT "C". LP 1116286 - M3: PERFORMED THE PUSH AND PULL TEST ON IGV IAW AMM 49-52-02 (TEST GOOD), PERFORMED CHIP DETECTED INSPECTION IAW AMM 49-27-04. (NO METAL FOUND) LP 1116293 M1: REOPENED MDDR 117406 PER MEL 49-11-01-01. LP 1210811 - M2: TROUBLESHOOT APU BLEED DUCT. PRESSURE HOLD 30+ WITHOUT ADP. WHEN ADP BUTTON ON AUTO, WILL DROP DOWN TO 16. TESTED THE VOLTAGE D488 ON MODULATING PINS 2 AND 3. BOTH SHOW 28V. ADP MODULATING VALVE NEEDS REPLACEMENT. IAW FIM 29-11 FLT TREE 839. DMI REMAINS OPEN. LP 1210813 - M5: DEFERRED ADP AUTO FUNCTION. APU BLEED OPS CHECKS NORMAL IAW AMM 49-11-00. THIS CLEARS MDDR #117406. MCC NOTIFIED AND PLACARD REMOVED.

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 92,918 hrs · 21,656 cycles

APU DUCT PRESSURE EXTREMELY WEAK DURING ENG 2 ENG START. PERFORMED ENGINE RUN IAW AMM 71-00-00. APU DUCT PRESSURE HOLD 30% DURING ENG START. NORMAL OPERATION OBSERVED. NO DISCREPANCY FOUND.

Part: CONTROL VALVE — FAILED (RT A/C PACK) · airframe 92,870 hrs · 21,638 cycles

RIGHT PACK TEMP EICAS MESSAGE DURING DESCENT, FOLLOWED QRH. PERFORMED BITE TEST OF THE PACK TEMP CONTROLLER IAW FIM 21-51 FT 803. FOUND TEMP CONTROL VALVE ON TEMP CONTROLLER. REMOVED AND REPLACED THE RT PACK TEMP CONTROL VALVE IAW AMM 21-51-12. OPS AND LEAK CHECKED GOOD.

Part: MODULE — MALFUNCTIONED (APU) · airframe 92,863 hrs · 21,635 cycles

DURING ENGINE START, APU DUCT PRESSURE NO HIGHER THAN 15 PSI. IMPENDING HOT START ON #2 ENGINE, STOPPED START, RESTART SUCCESSFUL. NO EXCEEDANCES. REMOVED AND REPLACED FLOW SENSING MODULE IAW B767 AMM 49-53-08. OPS CHECK GOOD AT THIS TIME.

Part: SENSOR — MALFUNCTIONED (RT A/C PACK) · airframe 92,859 hrs · 21,633 cycles

EICAS RIGHT PACK TEMP. FOUND APU BLEED DUCT PRESSURE TO BE 8 PSI ON LEFT AND 10 PSI ON RIGHT. BITE CHECK OF APU ECU MINI FLAG 3 & 6. FAULTY APU SURGE CONTROL VALVE. REMOVED AND REPLACED APU SURGE CONTROL VALVE AND REMOVED AND REPLACED BELLOW SEAL, AFT OF APU SURGE CONTROL VALVE. REMOVED AND REPLACED RIGHT PACK TEMP SENSOR IAW AMM 49-53-01 AND AMM 21-51-18-402. PACK TEMP TEST, OPS CHECK GOOD IAW AMM 21-51-18-702. APU BLEED PRESSURE GOOD. NO FAULTS NOTED AT THIS TIME.

Part: INDICATION SYS — FALSE INDICATION (APU) · airframe 92,855 hrs · 21,632 cycles

DURING ENGINE START, APU DUCT PRESSURE FALLS FROM 25 PSI TO LESS 15 PSI. N2 GETS TO NO MORE THAN 18% N2. NO START LIMITATIONS EXCEEDED. NOTED BY MX. PERFORMED APU BITE IAW AMM 49-11-00/958, OPS NORMAL, NO FAULTS NOTED. PERFORMED ENGINE RUN IAW AMM 71-00-00, APU MES, OPS NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT A/C PACK) · airframe 92,848 hrs · 21,630 cycles

RIGHT PACK OUT CAUTION MESSAGE. TURNING BASE, TURNED PACK OFF. PERFORMED FIM 21-51 FT 803, NO DEFECTS NOTED. OPS TEST GOOD. NO EICAS MSG OR PACK CONTROLLER FAULTS.

Part: HOSE — TORN (OXYGEN MASK) · airframe 92,829 hrs · 21,620 cycles

HOSE BETWEEN PORTABLE O2 BOTTLE AND MASK IS TORN. PORTABLE O2 BOTTLE ON WALL NEXT TO CARGO ACCESS DOOR.&NBSP;(<P>REMOVED AND REPLACED PORTABLE O2 BOTTLE HOSE AND MASK IAW B767 AMM 35-31-01. NO DEFECTS NOTED AT THIS TIME.&NBSP;</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT A/C PACK) · airframe 92,815 hrs · 21,616 cycles

"RIGHT PACK TEMP" EICAS MESSAGE DISPLAYED IN FLIGHT. AFTER SWITCHING TO STANDBY-N, THE MESSAGE DISAPPEARED. T/S PER B767 FIM 21-51 FT 807. NO FAULTS NOTED, CAN NOT DUPLICATE ON GROUND.&NBSP;</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT A/C PACK) · airframe 92,760 hrs · 21,597 cycles

ON DESCENT BELOW 10000 FT, WITH LEFT PACK OFF, RECEIVED RIGHT PACK TEMP ADVISORY. MESSAGE CLEARED AND SWITCHED TO LEFT PACK. PERFORMED PACK TEMP CONTROLLER BITE IAW FIM 21-51 FT 803. NO FAULTS, EICAS MESSAGE CLEARED. NO DEFECTS NOTED.

Part: CONTROLLER — FAILED (NR 2) · airframe 92,764 hrs · 21,598 cycles

NR 2 PRESSURE CONTROL SYS STATUS MESSAGE CABIN ALTITUDE SHOWING. REMOVED AND REPLACED THE NR 2 CABIN PRESSURE CONTROLLER IAW AMM 21-31-02, OPS CHECKED GOOD.

Part: INDICATOR — MALFUNCTIONED (CABIN PRESSURE) · airframe 92,548 hrs · 21,518 cycles

CABIN ALTITUDE INDICATOR FLUCTUATES CONSTANTLY, EVEN ON GROUND. CONFIRMED ALT RATE INDICATOR HAS MINOR VIBRATION, BUT STILL OPERATIONAL. REMOVED AND REPLACED CABIN PRESSURE CONTROL PANEL IAW 21-33-01. OPS CHECKED GOOD.

Part: SCREW — LOOSE (APU GENERATOR) · airframe 92,520 hrs · 21,512 cycles

STATUS MESSAGE FOR APU OIL QTY. PERFORMED APU EXTERNAL INSPECTION IAW AMM 49-21-00-206-001. FOUND APU GENERATOR HOUSING SCREWS LOOSE AND LEAKING. SECURED GENERATOR HOUSING SCREWS IAW AMM 20-11-00. REPLENISHED APU OIL IAW AMM 12-15-04. LEAK CHECKED OK AT THIS TIME.

Part: ECU — MALFUNCTIONED (APU) · airframe 92,442 hrs · 21,483 cycles

APU FAULT AND SHUTDOWN ON GROUND. REMOVED AND REPLACED APU ECU IAW AMM 49-61-03. OPS CK NORMAL.

Part: MICROPHONE — NO TEST (OXYGEN MASK) · airframe 92,442 hrs · 21,483 cycles

F/O OXYGEN MASK MICROPHONE FAILS TEST.&NBSP;(<P>REMOVED AND REPLACED F/O OXYGEN MASK IAW AMM 35-11-04. </P><P>LP 1088341 - M2: SWAPPED OBSERVER AUDIO SELECTOR PANEL WITH F/O IAW AMM 23-40-00. OPS CHECK GOOD.&NBSP;</P>)

Part: APU — SHUTDOWN · airframe 92,417 hrs · 21,474 cycles

APU DIED JUST PRIOR TO ENGINE START. RESTART SATISFACTORY. (<P>OPERATIONAL CHECK OF APU PERFORMED PER AMM 49-11-00. OPS NORMAL AT THIS TIME.</P>)

Part: INDICATOR — DEFECTIVE (COCKPIT) · airframe 92,331 hrs · 21,443 cycles

RT ENG VALVE DID NOT CYCLE ON ENGINE START.&NBSP;(<P>TRANSFERRED TO MDDR 111540 IAW MEL 73-21-03-01 CAT "C". MAINTENANCE ACTION C/W.</P><P>LP 1079618 - M5:&NBSP;<STRONG></STRONG>PERFORMED OPS CHECK OF R ENG VALVE LIGHT IAW AMM 71-00-00.&NBSP; NO FAULTS NOTED AT THIS TIME. DMI REMAINS OPEN FOR OBSERVATION PER MCC.&NBSP;</P><P>LP 1079619 - M2: REMOVED AND REPLACED RT ENG VALVE IND LIGHT ASSY IAW SWPM 20-84-14 OPS CHECK IS NORMAL AT THIS TIME. PERFORMED ENGINE RUN BOTH L&AMP;R ENG IAW AMM 81-11-00 OPS CHECK IS NORMAL AT THIS TIME. THIS CLOSED DMI 111540 PLACARD REMOVED MCC RA 02257.</P>)

Part: LIGHT — DEFECTIVE (COCKPIT) · airframe 92,309 hrs · 21,436 cycles

"FO PITOT" DISCREET LIGHT IN OVERHEAD PANEL WILL NOT STAY SEATED IN SOCKET.(<P>DEFERRED PITOT LIGHT IAW MEL 30-31-05 DMI #111349 CAT "B". ITEM DUE DAT 11MAY19. PLACARD INSTALLED. MCC NOTIFIED.&NBSP;</P><P>LP 1079679-M3: REMOVED AND REPLACED&NBSP;F/O PITOT KORRY SWITCH LIGHT IAW SWPM 20-84-18. OPS GOOD. THIS CLEARS MDDR 111349. PLACARD REMOVED AND MCC NOTIFIED.&NBSP;</P>)

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 92,290 hrs · 21,429 cycles

WX RADAR FAIL(<P>PERFORMED T/S, RESET C/B BOTH RADAR R/T UNITS IAW AMM 34-43-00. OPS RESET SATISFACTORY</P>)

Part: IDG — LOW (RT ENGINE) · airframe 92,272 hrs · 21,420 cycles

HAD MULTIPLE INTERMITTENT RIGHT GENERATOR DRIVE EICAS MESSAGE&NBSP;(<P>FOUND RIGHT ENGINE IDG OIL LEVEL LOW - SERVICED IDG IAW AMM 12-13-03. PERFORMED ENGINE RUN - RIGHT GENERATOR TEST GOOD IAW AMM 24-11-00</P>)

Part: IDG — INOPERATIVE (RT ENGINE) · airframe 92,275 hrs · 21,421 cycles

R GEN DRIVE EICAS IN FLIGHT, FOLLOWED QRH AND DISCONNECTED RT GEN. SEE PREV PAGES 1057066, 1057056. REPEAT WRITE UP.(<P>RT IDG INOP, OIL IS DRAINED OUT. MDDR #111171 MEL 24-00-01-01 CAT B DUE DATE 07MAY19. DISPATCH TJ 14:28Z.&NBSP;&NBSP;</P><P>REF LOG PAGE 1057079 ITEM M4; REMOVED AND REPLACED RIGHT ENGINE IDG IAW AMM 24-11-01. OPS CHECK GOOD AND LEAK CHECK GOOD. THIS CLEARS MDDR 111171. PLACARD REMOVED AND MCC NOTIFIED.</P>)

Part: PAINT — DETERIORATED (NR 2 ENGINE) · airframe 92,270 hrs · 21,419 cycles

NR 2 ENGINE INLET CASE PAINT IS DAMAGED /DETERIORATED IN SEVERAL AREAS.(<P>PREPARED CLEANED MASKED PRIMED AND PAINTED NR 2 ENGINE INLET CASE WHITE PER SRM 51-20-01-0G-0</P>)

Part: SMOKE DETECTOR — MALFUNCTIONED (E&E BAY) · airframe 92,270 hrs · 21,419 cycles

E&AMP;E EQUIP COOLING TEST FAILED.(<P>REMOVED AND REPLACED E&AMP;E SMOKE DETECTOR TS 164 AMM 21-58-19 OPS CHECK NORMAL.AMM 21-58-00.</P>)

Part: SLIDING WINDOW — DEFECTIVE (COCKPIT) · airframe 92,270 hrs · 21,419 cycles

NR 2 RIGHT SLIDING WINDOW HAS SIGN OF BUBBLES.(<P>REMOVED AND REPLACED NR 2 RT WINDOW. AMM 56-11-02 OPS AND LEAK CHECK NORMAL.</P>)

Part: BATTERY — DISCHARGED (APU) · airframe 92,253 hrs · 21,413 cycles

APU BATTERY BELOW REQUIRED VOLTAGE. APU INOP. REMOVED AND REPLACED APU BATTERY IAW AMM 24-31-04-004-001 AND AMM 24-31-04-404-005. OPS CHECK GOOD. THIS CLEARS MDDR 110806. PLACARDS REMOVED AND MCC NOTIFIED.</P>)

Part: RADAR — FAILED (WEATHER SYS) · airframe 92,253 hrs · 21,413 cycles

WEATHER RADAR FAIL, ANNUNCIATION ON EHSI (BOTH).&NBSP;(<P>PERFORMED B767 FIM 34-43&NBSP; FT 810 &AMP; 801, OPS CHECK GOOD. SYSTEM OPS NOTED NORMAL. PERFORMED BITE CHECK IAW FIM 34-43 FT 805, NO FAULTS FOUND.&NBSP;</P>)

Part: WARNING LIGHT — FALSE ACTIVATION (RT IDG) · airframe 92,245 hrs · 21,410 cycles

INTERMITTENT RIGHT GEN DRIVE EICAS MSG AND OH. DRIVE LIGHT LASTING 10-20 SECONDS, EVENT RECORDED AT 1930Z.(<P>SERVICED RIGHT IDG IAW B767 AMM 12-13-00. PERFORMED RT ENG RUN, OPS CHECKED GOOD.</P>)

Part: PRESSURE SWITCH — MALFUNCTIONED (FUEL SYSTEM) · airframe 92,243 hrs · 21,409 cycles

L FWD FUEL PUMP EICAS ON IN CLIMB OUT. PERFORMED BITE TEST PROCEDURES OF FUEL QT CONTROL BOX AND RESET. PERFORMED FIM FAULT TREE 807, TASK 28-25. REMOVED AND REPLACED BOOST PUMP FUEL PRESS SWITCH IAW AMM 28-285-03-04. OPS CHECK GOOD AT THIS TIME.

Part: COOLING FAN — INOPERATIVE (AFT EQUIPMENT) · airframe 92,148 hrs · 21,379 cycles

STATUS MESSAGE AFT EQUIPMENT EXHAUST FAN 1&NBSP;&NBSP;(<P>TRANSFERRED TO MDDR 109784 AS PER DDG 21-58-05 CAT "C".</P><P>LP 1050271 - M4:&NBSP;PERFORMED FIM 21-26 FT 805, PUT P/N 4101487, AFT EQUIP COOLING FAN, 1 ON ORDER WITH MCC MDDR # 109784 REMAINS OPEN.</P><P>LP 1050279: REMOVED AND REPLACED AFT EQUIPMENT COOLING FAN I.A.W. AMM 21-58-41. THIS CLOSES MDDR 109784.</P>)

Part: A/C PACK — CONTAMINATED · airframe 92,144 hrs · 21,377 cycles

ACRID SMELL THROUGH PACKS CONTINUES. NO SMELL EN-ROUTE, NOTICED AGAIN IN DESCENT THROUGH 14000.(<P>PERFORMED REMOVAL OF OIL CONTAMINATION FROM AIR CONDITIONING AND PNEUMATIC SYSTEM IAW AMM 21-00-21-102-030.<BR /></P>)

Part: UNKNOWN — ODOR (CABIN) · airframe 92,144 hrs · 21,377 cycles

A/C HAS INCREDIBLY BAD SMELL COMING FROM PACKS.(<P>T/S PER FIM FT 807. FOUND SYSTEM TO BE WORKING NORMAL AT THIS TIME, COULD NOT DUPLICATE ANY FAULTS.<BR /></P>)

Part: SEAL — LEAKING (APU) · airframe 92,128 hrs · 21,373 cycles

WHILE SERVICING OIL, FOUND OIL LEAKING FROM THE APU BEARING SEAL AREA DRAIN. REMOVED AND REPLACED APU IAW W/O 49976. OPS CHECKED GOOD. INSTALLED APU GENERATOR IAW 24-21-01. OPS CHECKED GOOD. APU COLD SOAK START VERIFICATION ACCOMPLISHED SATISFACTORY.

Part: IDG — LEAKING (NR 1) · airframe 92,144 hrs · 21,377 cycles

DURING ACCOMPLISHMENT OF W/O 49455, #1 ENGINE, DISCOVERED #1 IDG LEAKING FROM RESET RODCOVER PLATE (BROKEN).(<P>REMOVED AND REPLACED #1 IDG PER AMM 24-11-01. REQUIRES A LEAK AND OPS CHECK. OPS AND LEAK CHK NORMAL PER AMM 71-00-00.

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 92,010 hrs · 21,331 cycles

RIGHT ENGINE SPAR VALVE LIGHT DID NOT ILLUMINATED ON ENGINE START LIGHT TEST OK(<P>TRANSFERRED TO DMI 108785 PER MEL 28-40-02 CAT C&NBSP;</P><P>LP 1053656-M7 PERFORMED OPS CHECK OF RT ENG SPAR VALVE LIGHT INSP IAW AMM 28-00-00. OPS CHECK GOOD AT THIS TIME. THIS ACTION CLEARED DMI 108785.&NBSP;</P>)

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 92,005 hrs · 21,329 cycles

"INFO ONLY": APU FAILED TO START ON TWO ATTEMPTS. FL 390, TEMP -42 @ 1150Z. APU STARTED OKAY ON THE GROUND.(<P>NOTED BY MAINTENANCE- INSPECTED FOR CODES ECU STATUS "START ABORTED"- NO CODES PRESENT. OPS CHECKS GOOD PER AMM 49-11-00</P>)

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 92,002 hrs · 21,328 cycles

WEATHER RADAR FAIL BOTH SIDE&NBSP;(<P>PREFORMED FIM 34-43-815. NO FAULT NOTED AT THIS TIME. BOTH LEFT AND RIGHT SYSTEM DETECT AND SCAN, SUSPET WEATHER CONFIG WAS NOT SET UP PROPERLY. OPS CHECK GOOD.&NBSP;&NBSP;</P>)

Part: UNKNOWN — MALFUNCTIONED (WINDOW HEAT) · airframe 91,960 hrs · 21,315 cycles

L2 WINDOW HEATING INOP, ACCUMULATED ICE IN DESCENT WITH ALL OTHER WINDOW CLEAR(<P>PERFORMED WINDOW HEAT CONTROLLER BITE TEST IAW AMM 30-41-01 TEST OK</P>)

Part: IDG — MALFUNCTIONED (RT ENGINE) · airframe 91,932 hrs · 21,307 cycles

EICAS MSG R GEN DRIVE AND R GEN OFF AFTER ENG START. AIRCRAFT RETURNED TO THE GATE.(<P>RESET IDG AND C/W WITH ENGINE RUN, ALL OPS CHECK OK IAW AMM 24-11-01</P>)

Part: MOTOR — FAILED (FUEL SYSTEM) · airframe 91,925 hrs · 21,304 cycles

SPAR VALVE OPS CHECK FAILED ON 2 ENGINE START.(<P>COMPLIED WITH MAINTENANCE PROCEDURES 28-40-02 STEP 1 AND TRANSFERRED TO MDDR 108246 PER DDG 28-40-02 CAT "C". REMOVED AND REPLACED VALVE SPAR MOTOR IAW AMM 28-22-11 AND OPS CHECKED GOOD AT THIS TIME THIS CLEARS DMI 108246 STICKER REMOVED.&NBSP;</P>)

Part: OIL SYSTEM — LEAKING (APU) · airframe 91,934 hrs · 21,308 cycles

FO FOUND APU AREA (TAIL) SOAKED WITH OIL ON WALKAROUND PREFLIGHT.(<P>PERFORMED A VISUAL LEAKAGE CHECK OF APU AREA AND DETERMINED OIL CAME FROM OIL NECK OVERFILL POSSIBLY COOULD NOT SEE ANY OIL LEAKS AT THIS TIME IAW AMM 49-16-00 AND 12-13-04. FILLED WITH OIL IAW 12-13-04.<BR /></P>)

Part: IDG — MALFUNCTIONED (NR 2 ENGINE) · airframe 91,919 hrs · 21,303 cycles

R GEN DRIVE EICAS MSG MOMENTARY AFTER ENGINE START(<P>PLACED IDG ON MEL 24-00 / MDDR 108199.</P><P>LP 1053276-M6: REMOVED AND REPLACED NR 2 IDG IAW AMM 24-11-01. OPS CHECK OK. THIS CLOSES MDDR&NBSP; 108199.</P>)

Part: UNKNOWN — ODOR (CABIN) · airframe 91,919 hrs · 21,303 cycles

LEFT AND RIGHT PACKS SMELL.(<P>INSPECTED VENT SYSTEM AND INLET FOR BOTH LT &AMP; RT PACK\S FOR CONTAMINANTS. NONE FOUND OPERATED SYSTEM AND OPERATES NORMAL IAW AMM 21-26-00.<BR /></P><P><BR DATA-MCE-BOGUS="1" /></P>)

Part: IDG — LOW (RT IDG) · airframe 91,900 hrs · 21,297 cycles

R GEN DRIVE MOMENTARY EICAS AFTER START.(<P>BITE BPCU, FOUND R GEN LOW OIL PRESS, SERVICED IDG IAW AMM 12-15-03 , RAN ENG IAW AMM 71-00-00 OPS CKD GOOD.</P>)

Part: LENS — CRACKED (PORT O2 BOTTLE) · airframe 91,860 hrs · 21,284 cycles

GALLEY PORTABLE OXYGEN BOTTLE GAUGE LENS CRACKED. REMOVED AND REPLACED THE PORTABLE OXYGEN BOTTLE IAW AMM 35-31-01.

Part: IDG — LOW (RIGHT) · airframe 91,848 hrs · 21,279 cycles

R GEN DRIVE EICAS AND LIGHT CAME ON MOMENTARILY.(<P>SERVICED&NBSP;R IDG OIL WITH&NBSP; 1 QRT IAW 12-13-03. PERFORMED R ENG RUN IAW 71-00-00, NO MSG NOTED.<BR /></P>)

Part: OXYGEN MASK — INOPERATIVE · airframe 91,824 hrs · 21,270 cycles

R/H SUPERNUMERATY O2 MASK INOP.(<P>TRANSFERRED TO MDDR 107504.<BR /></P><P>LP 1047746: TEST SW ASSEMBLY SCREW FOUND LOOSE. ADJUSTED IAW SRM 51-42-01 AND 35-11-51 OPS TEST OK. MDDR 107504 IS CLOSED.&NBSP;<BR /></P>)

Part: RADAR — MALFUNCTIONED (WEATHER SYSTEM) · airframe 91,721 hrs · 21,235 cycles

LEFT AND RIGHT WEATHER RADAR FAILED " WEATHER FAIL " WHILE IN CRUSE&NBSP;(<P>FOUND ON CONTROL PANEL TO BE SELECTED BETWEEN LEFT AND RIGHT SELECT EITHER LEFT AND RIGHT BOTH WEATHER RADAR SYSTEM OPS CHECK NORMAL IAW AMM 34-43-00.</P>)

Part: INDICATOR — FAULTY (E&E COOLING) · airframe 91,700 hrs · 21,228 cycles

E&E COOLING MONITOR INDICATOR L-VOR FLOW BALL WILL NOT COME UP.(<P>REMOVED AND REPLACED E/E COOLING MONITOR INDICATOR .OPS CHECK NORMAL IAW AMM 21-58-07.</P>)

Part: ADC — MALFUNCTIONED (COCKPIT) · airframe 91,676 hrs · 21,216 cycles

TOTAL AIR TEMPERATURE INDICATIONS MISSING&NBSP;(<P>CYCLED ADC C/B OPS CHECK NORMAL AS PER AMM 34-12-02</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 91,663 hrs · 21,209 cycles

WX RADAR FAIL FROM LEVEL OFF AND DURATION OF FLIGHT(<P>PERFORMED WX RADAR OPERATION CHECK IAW AMM 34-43-00 OPS CHECK GOOD</P>)

Part: TUBE — UNSECURE (APU) · airframe 91,614 hrs · 21,189 cycles

APU INOP.(<P>DEFERRED TO MDDR 105650.RE-SECURED FLOW DIVIDER TUBE AT FUEL FILTER BY PASS VALVE AT APU IAW AMM 49-31-05 OPS AND LEAK CHECK GOOD NO LEAKS NOTED.<BR /></P>)

Part: MONOPOLE — WARPED (APU) · airframe 91,570 hrs · 21,173 cycles

FOUND MONOPOLE TS8 TO BE WARPED. (<P>R&AMP;R MONOPOLE TS8 IAW AMM 49-61-02 OPS CHECK GOOD.<BR /></P>)

Part: SENSOR — SHORTED (APU) · airframe 91,556 hrs · 21,169 cycles

APU FAILED TO START NO APU FAULT EICAS&NBSP;(<P>TRANSFERRED TO MDDR 105126 AS PER MEL 49-11-01A CAT C.</P><P>PERFORMED APU WIRE BUNDLE ALL WIRING CHECK FOUND OK. FOUND MONOPOLE SENSOR SHORTED. REMOVED AND REPLACED SENSOR TS9 IAW AMM 49-51-02</P>)

Part: CONTROLLER — MALFUNCTIONED (RT A/C PACK) · airframe 91,511 hrs · 21,148 cycles

R PACK TEMP(<P>PERFORMED BITE TEST ON RH PACK TEMP CONTROLLER IAW AMM 21-51-14, DISPLAYED CONTROLLER, R/R RH PACK CONTROLLER IAW AMM 21-51-14, PERFORMED BITE TEST, NO FAULTS DISPLAYED.</P>)

Part: ECU — MALFUNCTIONED (APU) · airframe 91,502 hrs · 21,145 cycles

APU WOULD NOT START AFTER LANDING. CHECKED WIRING FROM ECU TO MANIFOLD T58 &T59. ALL OK CHECKED WIRES FOR APU AT FIREWALL, RERACKED ECU PER AMM 49-61-05 APU STARTED NORMAL. HOLDS ELECT AND PNEUMATIC LOADS 25% N2 ON ENG MOTORING.

Part: ECU — MALFUNCTIONED (APU) · airframe 91,481 hrs · 21,139 cycles

APU FAULT LIGHT UPON LANDING(<P>TRANSFER TO MDDR 104658 IAW MEL49-11-01A CATC PLACARD INSTALLED</P><TABLE WIDTH="721" CLASS="MCE-ITEM-TABLE" STYLE="HEIGHT: 57PX; BORDER-COLLAPSE: COLLAPSE;" BORDER="0" CELLSPACING="0" CELLPADDING="0" DATA-LEFT="2" DATA-MCE-SELECTED="1"><TBODY><TR STYLE="HEIGHT: 76PX;"><TD HEIGHT="75" DIR="LTR">REPLACED APU ECU IAW B767 AMM REF 49-61-05. OPS CKS GOOD. DMI # 104658 CLEARED. PLACARD REMOVED.</TD></TR></TBODY></TABLE><P><BR /></P><P><BR /></P><DIV ID="MCERESIZEHANDLENW" DATA-MCE-BOGUS="ALL" CLASS="MCE-RESIZEHANDLE" UNSELECTABLE="TRUE" STYLE="CURSOR: NW-RESIZE; MARGIN: 0PX; PADDING: 0PX; LEFT: -2.5PX; TOP: 11.5PX;"></DIV><DIV ID="MCERESIZEHANDLENE" DATA-MCE-BOGUS="ALL" CLASS="MCE-RESIZEHANDLE" UNSELECTABLE="TRUE" STYLE="CURSOR: NE-RESIZE; MARGIN: 0PX; PADDING: 0PX; LEFT: 717.5PX; TOP: 11.5PX;"></DIV><DIV ID="MCERESIZEHANDLESE" DATA-MCE-BOGUS="ALL" CLASS="MCE-RESIZEHANDLE" UNSELECTABLE="TRUE" STYLE="CURSOR: SE-RESIZE; MARGIN: 0PX; PADDING: 0PX; LEFT: 717.5PX; TOP: 88.1667PX;"></DIV><DIV ID="MCERESIZEHANDLESW" DATA-MCE-BOGUS="ALL" CLASS="MCE-RESIZEHANDLE" UNSELECTABLE="TRUE" STYLE="CURSOR: SW-RESIZE; MARGIN: 0PX; PADDING: 0PX; LEFT: -2.5PX; TOP: 88.1667PX;"></DIV>)

Part: CONNECTOR — LOOSE (AC BAY) · airframe 91,507 hrs · 21,147 cycles

REPEAT WRITE UP R PACK TEMP CAUTION MSG FOLLOWED QRH PACK PS NORMAL IN STBY-N MODE. FOUND LOOSE CONNECTOR ON R PACK OUTLET TEMP SENS & RESEATED CONNECTOR PER AMM 21-51-00, OPS CHECK NORMAL.

Part: ECS — CONTAMINATED · airframe 91,515 hrs · 21,149 cycles

REPEAT WRITE UO, OIL/MUSTY SMELL FROM PACKS AFTER ENGINE START REF LOG PAGE #1031376 SMELL STRONGEST ON GROUND.(<P>FOUND DEICE FLUID INSIDE ECS BAY. CLEANED RESIDUAL FLUID RAN PAC SYSTEM FOR APPROX 1 HR SYS TEST &AMP; INSP GOOD REF B767 AMM 05-51-56. <BR /></P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 91,477 hrs · 21,137 cycles

BEFORE TAKE OFF " RT PACK TEMP" EICAS MSG, SELECTED "N" PACK OPERATED NORMAL. PERFORMED BITE CHECK OF RT PACK CONTROLLER IAW AMM 21-62-00, NO DEFECTS NOTED.

Part: NOT REPORTED — MALFUNCTIONED (APU) · airframe 91,507 hrs · 21,147 cycles

APU FAULT AFTER LANDING WOULD NOT START. OPS CHECKED IAW FIM AD AMM 49-11-00. OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (AC SYSTEM) · airframe 91,487 hrs · 21,142 cycles

VERY AGRESSIVE BAD MUSTY SMELL COMING FROM AC SYSTEM. C/W FIM 21-00-21 NO ODOR PRESENT FROM A/C SYSTEM. OPS NORMAL.

Part: UNKNOWN — MALFUNCTIONED (AC BAY) · airframe 91,473 hrs · 21,135 cycles

RIGHT AUTO PACK CONTROLLER INOP PRIOR TO PACK OPERATION IN MANUAL. PERFORMED GROUND TEST OF BOTH PACKS IN AUTO AND MANUAL MODES REF AMM 21-51-03. NO DEFECTS NOTED AT THIS TIME, OPS CHECK NORMAL.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 91,410 hrs · 21,115 cycles

RT PACK TEMP EICAS AFTER START ACCOMPLISHED QRH PROCEDURE, SELECTED N FOR REMAINDER OF FLIGHT. MESSAGE NOT INDICATED AFTER LANDING, PERFORMED BITE IAW FIM 21-51 FT 803 PREVIOUS FAULTS SHOWED RAM OUTLET ACTR BIT AND VERIFY NORMAL, PERFORMED OPS CHECK IAW AMM 21-51-00 OPS CHECK NORM AT THIS TIME.

Part: IDG — MALFUNCTIONED (LT ENGINE) · airframe 91,369 hrs · 21,099 cycles

WHILE OPENING UP A/C FOUND LT ENG GEN DRIVE LIGHT OUT. RAI LT IDG IAW 24-11-01. OPS AND LEAK CHECKS GOOD AT THIS TIME.

Part: FAN — FAILED (AFT CARGO) · airframe 91,362 hrs · 21,097 cycles

MAINTENANCE MESSAGE AFT DETECTOR FAN&NBSP;(<P>REMOVED AND REPLACED #1 AFT CARGO SMOKE DETECTOR BLOWER FAN IAW AMM 26-16-02 AND FIM 26-16 FT 812. OPS CHECK GOOD AT THIS TIME&NBSP;</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (LT ENG FIRE LOOP) · airframe 91,344 hrs · 21,091 cycles

STATUS MESSAGE L ENG FIRE LOOP 2(<P>PERFORMED ENG FIRE LOOP TEST L ENG FIRE LOOP 2 OPS TEST NORMAL PER AMM 26-11-00</P>)

Part: WARNING LIGHT — FALSE ACTIVATION (RT ENG VALVE) · airframe 91,250 hrs · 21,059 cycles

RH ENG VALVE LIGHT ON(<P>C/W FIM 76-11 F/T 808 NO FAULTS NOTED AT THIS TIME <BR /></P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 91,237 hrs · 21,054 cycles

LT FWD FUEL PUMP LOW PRESSURE LITE ILLUMINATED IN FLT, LT MAIN TANK FUEL QTY WAS 12.6LBS. PERFORMED OPERATIONAL TEST OF ENGINE FUEL FEED SYSTEM TEST OF ENGINE FUEL FEED PASSED NO DEFECTS NOTED AT THIS TIME AS PER AMM 28-22-00.

Part: PIN — MALFUNCTIONED (OXYGEN MASK) · airframe 91,181 hrs · 21,036 cycles

FO OXYGEN MASK RESET / TEST LEVER INOP. PIN WILL NOT ENGAGE WITH O2 MASK. RESET PIN, PERFORMED OPS CHECK PIN & MASK IN OK CONDITION IAW AMM 35-11-52.

Part: CONTROLLER — NOT REPORTED (BLEED AIR SYS) · airframe 91,127 hrs · 21,017 cycles

RT ENG PRESSURE CONTROLLER. REMOVED AND REPLACED RIGHT ENGINE PRESSURE CONTROLLER IAW AMM 36-11-19. OPS CHECK GOOD NO DEFECT NOTES.

Part: RELIEF VALVE — FAULTY (BLEED AIR SYS) · airframe 91,124 hrs · 21,016 cycles

EICAS MSG RT ENGINE PRV. REMOVED AND REPLACED PRV AND CONTROLLER IAW AMM 36-11-18 & 36-11-19. OPS CK NORMAL.

Part: VALVE — MALFUNCTIONED (APU) · airframe 91,124 hrs · 21,016 cycles

APU INOP REVERSE FLOW. REMOVED AND REPLACED APU SURGE CONTROL VALVE IAW AMM 49-53-01. OPS TEST GOOD.

Part: RELIEF VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 91,127 hrs · 21,017 cycles

EICAS MSG RT ENG PRV. REMOVED AND REPLACED RT ENG PRV IAW AMM 36-11-18. OPS CHECK NO DEFECTS NOTED AT THIS TIME.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 91,127 hrs · 21,017 cycles

APU INOP REVERSE FLOW FAULT. TRANSFER TO MDDR 101485 IAW MEL 49-11-01A CAT C DUE DATE&NBSP; 31 OCT -18.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 91,133 hrs · 21,021 cycles

STATUS MSG: RT ENG PRV. PERFORMED FIM 36-10 FLT 878- N0 DEFECTS NOTED, ALL SUPPLY BITE NO FAULTS EICAS MSG CLEARED.

Part: EXCITER — MALFUNCTIONED (APU) · airframe 91,100 hrs · 21,008 cycles

APU FAULT. APU INOP. PERFORMED OPS CHECK OF APU IAW AMMM 49-11-00. NO LIGHT OFF (NO EGT RISE) BITE CHECK OF ECU IAW FIM 49-11-FT958, ECU BITE SAID IGN UNIT. R&R APU EXCITER BOX IAW AMM 49-41-03. REMOVED AND REPLACED APU IGNITION LEAD IAW AMM 49-41-04, P/N 3888076-3, NSN. REMOVED AND REPLACED APU IGNITION PLUG IAW AMM 49-41-02. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 91,087 hrs · 21,005 cycles

APU BLEED FLOW BAR INOP. RELAMPED BLEED SWITCH IAW AMM 33-10-01. OPS CK OK.

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 91,087 hrs · 21,005 cycles

ON INITIAL CLIMBOUT WXR FAILED, BUT CAME BACK. PERFORMED OPERATIONAL TEST ON WXR SYSTEM IAW AMM 34-43-00-715, OPS CKD GOOD AT THIS TIME.

Part: WIRE — SHORTED (APU) · airframe 91,078 hrs · 21,002 cycles

APU (FISHPOLE HLST PROCEDURE) (ETOPS) APU OFF: P-1672/ APU ON: P-2300. COMPLIED WITH TASK CARD A-49-999-00-01. REMOVED AND REPLACED APU GENERATOR IAW AMM 24-21-01 FAILED OPS CHECK. T/B APU GENE PMG FAULT FOUND WIRE W 242-30R-18 SHORTED. REPAIRED WIRE IAW SWPM 20-10-13 PS CHECK GOOD NO FURTHER ACTION REQUIRED.

Part: WIRE — SHORTED (APU) · airframe 91,078 hrs · 21,002 cycles

APU GENERATOR INOP. R&R APU GENERATOR IAW AMM 24-21-01 FAILED PS CHECK. T/S APU GEN PMG FAULT & FOUND WIRE 242-301R-18 SHORTED. REPLACED WIRE IAW IAW SWPM 20-10-13. PERFORMED GOOD OPS CHECK OF APU GEN IAW AMM 24-21-00 NO FURTHER ACTION REQUIRED.

Part: WIRE — MISSING (BLEED AIR SYS) · airframe 91,078 hrs · 21,002 cycles

DURING ENG RUN NR 2 BLEED LIGHT ILLUMINATED. TROUBLESHOOT ENG NR 2 BLEED IAW FIM 36-10-00 TREE 847 FOUND WIRE MISSING, SAME INSTALLED IAW WDM 36-11-62 OF THE P37. OPS CHECK CARRIED OUT IAW AMM 71-00-00, OPS CHECK SATISFACTORY.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 91,076 hrs · 21,000 cycles

EMERGENCY LIGHTS FAIL OPS CHECK. REMOVED AND REPLACED NEW BATTERY PACK IAW AMM 33-51-07. PERFORMED SATISFACTORY OPS CHECK IAW AMM 33-51-07 STEP E.

Part: DUCT — LEAKING (AC BAY) · airframe 91,076 hrs · 21,000 cycles

LT EACAS BAY DUCT LEAKING FWD 1/B SIDE. REMOVED AND REPLACED LT EACAS BAY DUCT 1/B GASKET IAW AMM 21-51-04 AND PERFORMED LEAK CHECK IAW AMM 21-51-04 NO LEAK NOTED.

Part: CONTROLLER — NOT REPORTED (AC BAY) · airframe 91,076 hrs · 21,000 cycles

STAND BY PACK CONTROLLER FAILS REQUIRES REPLACEMENT. REMOVED AND REPLACED STANDBY PACK CONTROLLER IAW AMM 21-51-14-400. PERFORMED SATISFACTORY OS CHECK IAW AMM 21-51-06-700.

Part: SEAL — NOT REPORTED (BLEED AIR SYS) · airframe 91,076 hrs · 21,000 cycles

RT EACAS BAY AFT DUCT LEAKING. REMOVE AND REPLACED SEAL A7 RT BODY CROSSOVER DUCT O/B OF CHECK VALVE IAW AMM 36-11-01. PERFORMED GOOD LEAK CHECK IAW AMM 36-11-01 NO LEAKS NOTED.

Part: CONNECTOR — LOOSE (AC BAY) · airframe 91,076 hrs · 21,000 cycles

LT EACAS BAY O/B SIDE, PNEUMATIC DUCT TEMP SENSOR CONNECTOR HAS LOOSE BACKSHELL JUST AFT OF LT FLOW CONTROL VALVE. REMOVE AND REPLACE CONNECTOR ON 02152 IAW SWPM 20-61-00, PERFORM SATISFACTORY OPS CHECK ON SENSOR IAW AMM 21-52-08 STEP F.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 91,068 hrs · 20,994 cycles

LT ENGINE BLEED LIGHT ILLUMINATED IN CLIMB OUT WITH NO EICAS MSG. NO FAULTS NOTED AT THIS TIME REF FIM 36-20-00. OPS CHECK GOOD IAW AMM 36-11-00-715-149.

Part: CIRCUIT CARD — NOT SEATED (BLEED AIR SYS) · airframe 91,062 hrs · 20,990 cycles

LEFT ENG BLEED LIGHT ON DURING TAKEOFF AND INITIAL CLIMB. EXTINGUISHED APPROX 7 MIN AFTER TAKE OFF. NO EICAS MSG. NO FAULTS NOTED ON AIR SUPPLY BITE PER FIM 36-20-00. RERACKED LEFT BLEED AIR CONTROL CARD REF AMM 36-11-12. NO DEFECTS NOTED AT THIS TIME.

Part: CIRCUIT CARD — DIRTY (BLEED AIR SYS) · airframe 91,060 hrs · 20,989 cycles

LT ENG BLEED LIGHT ON, ON TAKEOFF ROLL NO EICAS MSG LIGHT GOES OUT AFTER FIRST POWER REDUCTION ALL PARAMETERS NORMAL. CLEANED PINS ON M859 LT BLEED AIR CONTROL CARD AT P50 PANEL. RE-RACKED. ALL OPS OK PER AMM 36-11-12. NO FAULTS ON BITE.

Part: WARNING SYSTEM — FALSE ACTIVATION (BLEED AIR SYS) · airframe 91,054 hrs · 20,986 cycles

OVERHEAD LEFT ENGINE BLEED LIGHT ILLUMINATED ON INTIAL CLIMB FOR A FEW MINUTES, NO EICAS MESSAGE. PERFORMED FIM 36-20 TREE 804, PERFORMED BITE OF AIR SUPPLY MODULE LT ENGINE NO FAULTS NOTED.

Part: CONTROLLER — MALFUNCTIONED (BLEED AIR SYS) · airframe 91,058 hrs · 20,988 cycles

OVERHEAD LEFT ENGINE BLEED LIGHT ILLUMINATED ON CLIMB OUT. NO EICAS MSG, REPLACED LT ENG HP CONTROLLER IAW AMM 36-11-08. OPS & LEAK CHECK OK.

Part: WARNING LIGHT — FALSE INDICATION (COCKPIT) · airframe 91,043 hrs · 20,983 cycles

LT ENG BLEED DISCRETE LT ON OVERHEAD PANEL ILLUMINATED DURING INITIAL CLIMB. NO EICAS MSG. LT WENT OUT AFTER 2-3 MINS. RECURRING WRITE-UP. PERFORMED BITE TEST PROCEDURE IAW FIM 36-20-00 FAULT TREE 804. NO FAULTS FOUND.

Part: TERMINAL — BROKEN (FIRE LOOP) · airframe 91,031 hrs · 20,979 cycles

LT ENG FIRE LP 1 STATUS MSG. T/S ENGINE 1 FIRE LOOP 1. RANG OUT WIRES AT ENGINE PYLON TO FIRE DETECTOR ELEMENTS, FOUND TO BROKEN TERMINALS ON UPPER AFT AND LOWER AFT ELEMENTS. REPLACED 2 TERMINALS FOR UPPER AND LOWER ELEMENTS IAW SWPM 20-30-11. OPS CHECK TEST OK IAW AMM 26-11-00.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 91,026 hrs · 20,977 cycles

LT ENG FIRE LP1 STATUS MSG. STATUS MESSAGE NOT CURRENTLY SHOWN. PERFORMED ENGINE FIRE DETECTION OPS CHECK IAW 26-11-00. NO DEFECTS NOTED. GOOD FOR SERVICE.

Part: VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 91,058 hrs · 20,988 cycles

LT ENGINE BLEED OFF MSG, FAMV FAULT. REMOVED AND REPLACED FAN AIR VALVE IAW AMM 36-11-16. PERFORMED TEST OK.

Part: MODULATING VALVE — FAULTY (BLEED AIR SYS) · airframe 91,026 hrs · 20,977 cycles

LEFT ENGINE BLEED INOP / (FAN AIR (PRECOOLER) CONTROL SYSTEMS. REMOVED AND REPLACED FAN AIR MODULATING VALVE IAW AMM 36-11-16 , PERFORMED OPERATIONAL TEST AND FAN AIR VALVE BITE TEST IAW AMM 36-11-16 NO FAULTS NOTED, THE SYSTEM WORKS NORMAL AT THIS TIME.

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 91,031 hrs · 20,979 cycles

FIRE / OVHT SYS EICAS ILLUMINATED ON SHORT FINAL. PERFORMED FIRE DETECTION BITE PROCEDURE IAW FIM 26-15 FT 804 FAULT CLEARED.

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 91,031 hrs · 20,979 cycles

APU FIRE LP 1 STATUS MSG. PERFORMED FIRE DETECTION BITE PROCEDURE IAW FIM 26-15 TASK 804, FAULT CLEARED.

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 91,058 hrs · 20,988 cycles

LT ENG FIRE LP1 STATUS MSG. STATUS MESSAGE NOT CURRENTLY SHOWN. PERFORMED ENGINE FIRE DETECTION, OPS CHECK IAW 26-11-00. NO DEFECTS NOTED. GOOD FOR SERVICE.

Part: WARNING SYSTEM — INTERMITTENT (COCKPIT) · airframe 91,016 hrs · 20,974 cycles

LEFT BLEED LIGHT ILLUMINATED INTERMITTENTLY DURING CLIMB. NO ASSOCIATED EICAS OR CAUTION. PER FIM 36-20-43 804 PERFORMED BITE CHECK ON AIR SUPPLY MODULE NO DEFECTS NOTED AT THIS TIME A/C OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 91,016 hrs · 20,974 cycles

DURING CLIMB OUT, LT ENG BLEED LIGHT ILLUMINATED, BUT NO EICAS MSG, WENT AWAY. FOLLOWED FIM 36-20 FAULT TREE 804, PERFORMED BITE TEST ON AIR SUPPLY, NO DEFECTS NOTED AT THIS TIME. HPSOV PLACE ON ORDER AS PRECAUTIONARY. P/N 802170-12. VISUALLY INSP HPSOV, NO DEFECT NOTED AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 90,998 hrs · 20,969 cycles

LT ENGINE BLEED LIGHT ON OVERHEAD PANEL ILLUMINATED DURING INITIAL CLIMB. LIGHT EXTINGUISHED AFTER APPROXIMATELY 1 MIN. NO EICAS. THIS IS A REPEAT WRITE UP. PERFORMED AIR SUPPLY BITE TEST IAW AMM 36-23-00-715-001. OPS CHECK GOOD, NO FAULTS NOTED AT THIS TIME.

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 91,006 hrs · 20,971 cycles

WEATHER RADAR SEEMED TO NOT DEPICT HEAVY WEEATHER VISIBLE TO FLIGHT CREW. ON APPROACH, WX RADAR DEPICTED MOD/HEAVY RAIN BUT WE ONLY ENCOUNTERED LT RAIN. GROUND OPERATIONAL CHECKS GOOD IAW 34-43-00/501.

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 90,978 hrs · 20,963 cycles

WEATHER RADAR NO DEFIC HEAVY WEATHER VISIBLE TO FLIGHT CREW ON APPROACH WX RADAR MOD/HEAVY RAIN BUT WE ONLY ENCOUNTERED LT RAIN. GROUND OPERATIONAL CHECK GOOD IAW AMM 34-43-00.

Part: SMOKE DETECTOR — INOPERATIVE · airframe 90,952 hrs · 20,954 cycles

SMOKE DETECTOR POS A2 INOP.REMOVED AND REPLACED A2 SMOKE DETECTOR IAW AMM 26-19-01.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 90,950 hrs · 20,953 cycles

LEFT BLEED LIGHT ON OVERHEAD PANEL ILLUMINATED BRIEFLY IN FLIGHT. INTERROGATED M-129 BLEED AIR SUPPLY MODULE AND RESET ACOMPLISHED LT ENG RUN AND BLEED AIR CHECK PER AMM 36-11-00 BITE TEST OF M-129 AIR SUPPLY MOD SHOWS NO FAULTS NO SUBSEQUENT BLEED OFF LIGHTS OR EICAS MSG NOTED.

Part: NOT REPORTED — MALFUNCTIONED (FUEL SYSTEM) · airframe 90,950 hrs · 20,953 cycles

MAIN TANK IN FLIGHT FUEL IMBALANCE OF 1200LBS (LEFT LOW/RIGHT HIGH). BITE TEST OF M-121 FUEL QTY PROCESSOR SHOWS NO FAULTS FUEL CONFIG LIGHT DID NOT ILLUMINATE AND NO ASSOCIATED EICAS MSG IN VIEW SUSPECT 1200LB APU FUEL BURN DUE TO 4 PLUS HOUR DELAY INBD. NOTE LT ENG FUEL FLOW DEFERRED.

Part: B-NUT — LOOSE (CLEED AIR SYS) · airframe 90,950 hrs · 20,953 cycles

DURING CRUISE LEFT DUCT PRESSURE 10 PSI THE BLEED DISCRET LIGHT ON OVERHEAD PANEL CAME ON FOR SEVERAL SECONDS. REF LOG PAGE 0965172 ITEM 3. T/S BLEED SYSTEM AND FOUND LOOSE B NUT ON PRV SUPPLY PRESSURE LINE, TIGHTEN B NUT OPS CK WITH ENGINE RUNNING GOOD IAW FIM 36-10 FT 838 AND AMM 36-11-00.

Part: SEAL — DAMAGED (BLEED AIR SYS) · airframe 90,948 hrs · 20,952 cycles

LEFT DUCT SHOWING 5 PSI IN FLIGHT AT CRUISE. RECONNECTED SEPARATED LT ENGINE PNEUMATIC SUPPY DUCT, AND REPLACED SEAL UPSTREAM OF LOW AND HIGH PRESSURE "Y" MANIFOLD PER MM CH 36-11-01. LK & OPS-CK GOOD ON ENGINE MX RUN IAW MM CH 71-00-00 AND CH 36-00-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 90,944 hrs · 20,950 cycles

CARGO FIRE SMOKE DETECTOR A2 LIGHT ILLUMINATED. PERFORMED OPERATIONAL TEST OF CARGO DETECTION SYSTEM WITH NO FAULTS PER FIM 26-19F/T 809.

Part: CONNECTOR — DEFECTIVE (BLEED AIR SYS) · airframe 90,950 hrs · 20,953 cycles

DURING CRUISE LEFT DUCT PRESSURE 10 PSI. THE BLEED DISCRETE LIGHT ON OVERHEAD PANEL CAME ON FOR SEVERAL SECONDS. REPLACED ELECTRICAL CONNECTOR D4156P, WHICH IS DAMAGED IAW SWPM 20-35-11. SECURED CONNECTOR ON STRUT DISCONNECT PANEL. OPS CK REQUIRED.

Part: WIRE HARNESS — DEFECTIVE (NR 1 ENGINE) · airframe 90,944 hrs · 20,950 cycles

LEFT FUEL FLOW INDICATION INOP. (NO CALCULATED FUEL ON FMS). REPLACED W13 HARNESS ON NR 1 ENG IAW AMM 73-21-18. FUEL FLOW CHECK DURING ENGINE RUNS IAW AMM 71-00-00.

Part: NOT REPORTED — MALFUNCTIONED (LT ENGINE) · airframe 90,946 hrs · 20,951 cycles

LEFT ENGINE N1, DURING CLIMB COULD NOT ALIGN THE COMMANDED N1, DUE TO HIGH N2. LEFT N2 IN CLIMB WAS 109.2. PERFORMED ENG RUNS PER IAW 71-00 ALL PARAMETERS NORMAL.

Part: DUCT — SEPARATED (BLEED AIR SYS) · airframe 90,950 hrs · 20,953 cycles

LEFT ENG BLEED OFF EICAS MESSAGE DURING FLIGHT. RECONNECTED SUPPLY DUCT, PERFORMED ENG RUNS IAW 36-11-00 AND 71-00. ALL OPS NORMAL.

Part: IDG — LOW (LT ENGINE) · airframe 90,948 hrs · 20,952 cycles

LEFT IDG VALVE STATUS MESSAGE. SERVICED LEFT IDG IAW MM CH 12-13-03. SYSTEM CK'S GOOD DURING ENGINE MX RUN PER MM CH 24-11-00.

Part: CONTROL VALVE — INOPERATIVE (NR 1 ENGINE) · airframe 90,948 hrs · 20,952 cycles

NR 1 ENG STARTER CONTROL VALVE INOP. REMOVED AND REPLACED NR 1 ENG STARTER CONTROL VALVE IAW AMM 80-11-02. OPS CK GOOD.

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 90,938 hrs · 20,947 cycles

WXR FAIL. PERFORMED OPS CHECK ON LEFT AND RIGHT WX SYS IAW AMM 34-00-715-001-001, BOTH PASSED OPS NORMAL.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 90,936 hrs · 20,945 cycles

"WXR FAIL". PERFORMED OPS CHECK ON LEFT AND RIGHT WX SYSTEM IAW AMM 34-43-00-715-001-001. BOTH PASSED, OPS NORMAL.

Part: COVER — LOOSE (FUEL SYSTEM) · airframe 90,931 hrs · 20,940 cycles

RT AFT FUEL PUMP INOP. RESECURED SWITCH ASSEMBLY. SWITCH COVER WAS LOOSE. IAW 28-21-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 90,905 hrs · 20,918 cycles

WEATHER RADAR FAILED IN FLIGHT. PERFORMED OPS AND SYSTEM TEST OF LT AND RT WEATHER RADAR REF AMM 34-43-00 NO FAULTS NOTED AT THIS TIME, OK FOR SERVICE.

Part: ACTUATOR — FAILED (APU) · airframe 90,896 hrs · 20,908 cycles

APU WOULD NOT START AFTER TWO ATTEMPTS, FAULT LIGHT ILLUMINATED ON BOTH ATTEMPTS. R&R INLET GUIDE VANE ACTUATOR IAW AMM 49-52-02. OPS CHECK OK.

Part: CONTROL PANEL — UNSECURE (COCKPIT) · airframe 90,877 hrs · 20,888 cycles

"WX FAIL" MSG DISPLAYED. CLEANED AND RESECURES WX CONTROL PANEL AND PERFORMED OPS TEST IAW AMM 34-43-00-715-001-001. NO FAULTS NOTED AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 90,877 hrs · 20,888 cycles

EICAS MSG "TAT PROB". PERFORMED OPERATIONAL TEST OF TAT IAW AMM 30-33-00-715-010. NO FAULTS NOTED AT THIS TIME.

Part: ACTUATOR — INOPERATIVE (FUEL SYSTEM) · airframe 90,860 hrs · 20,873 cycles

RIGHT DEFUEL VALVE ACT UNABLE TO TRANSFER FUEL. REMOVED AND REPLACED ACTUATOR OPS CHECK NORMAL IAW AMM 28-26-11.

Part: UNKNOWN — MALFUNCTIONED (AC BAY) · airframe 90,860 hrs · 20,873 cycles

RT PACK EXHAUST DOOR DID NOT CLOSE IN FLT MODE. PERFORMED ACTUATOR CHECK OPS CHECKS NORMAL IAW AMM 21-53-01.

Part: ACTUATOR — MALFUNCTIONED (AC BAY) · airframe 90,860 hrs · 20,873 cycles

RIGHT RAM AIR INLET DOOR ACTUATOR. R&R RIGHT HAND RAM AIR DOOR ACTUATOR OPS CHECK GOOD IAW AMM 21-53-01.

Part: DETECTOR — INOPERATIVE (NR 2 ENGINE) · airframe 90,860 hrs · 20,873 cycles

NR 2 ENG FIRE LOOP NR 1 INOP "EICAS MSG". REPLACED AFT LOWER DETECTOR ASSY, ENGINE 2 IAW AMM 26-11-02 OPS CHECK NORMAL.

Part: FIRE DETECTOR — FAILED (RT ENGINE) · airframe 90,839 hrs · 20,866 cycles

RIGHT ENGINE FIRE LOOP NR 2 STATUS MESSAGE DISPLAYED. R & R THE UPPER AFT FIRE DETECTOR ASSY IAW AMM 26-11-02. OPS CHECKED WITH NO ISSUES NOTED.

Part: CIRCUIT BREAKER — TRIPPED · airframe 90,813 hrs · 20,855 cycles

EICAS MESSAGE FOR THE CENTER LT FUEL PUMP. COMPLIED WITH QRH, TURNED THE PUMP OFF. MESSAGE CLEARED. FOUND C369 CIRCUIT BREAKER TRIPPED AT THE P6. RESET THE CIRCUIT BREAKER IAW AMM 20-60-01. ACCOMPLISHED FIM 28-22 TASK 812. LEFT CENTER FUEL PUMP OPS CHECKED GOOD. NO FAULTS.

Part: WARNING MESSAGE — FALSE ACTIVATION (TAT PROBE) · airframe 90,750 hrs · 20,832 cycles

TAT PROBE EICAS MESSAGE AFTER LANDING. PERFORMED AN OPS TEST OF THE TAT PROBE HEAT SYSTEM IAW AMM 30-33-00, OPS CHECKED GOOD, NO DEFECTS NOTED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 90,745 hrs · 20,831 cycles

TAT PROBE MESSAGE ON EICAS. BITE MODULE, NO FAULTS FOUND IAW FIM 30-33 FAULT TREE 803. SYSTEM NORMAL.

Part: RADAR — INTERMITTENT (WX SYSTEM) · airframe 90,797 hrs · 20,849 cycles

WEATHER RADAR FAILED ON TAKEOFF, RESUMED OPERATION AT FL 350. ACCOMPLISHED A BITE TEST OF THE WEATHER RADAR, NO FAULTS FOUND. OPS CHECKED GOOD IAW FIM 34-43-00, AND AMM 34-43-00.

Part: SENSOR — INTERMITTENT (NR 1 FAN SPEED) · airframe 90,521 hrs · 20,750 cycles

DURING CRUISE FLIGHT, N1 INDICATION FLUCTUATED INTERMITTENTLY, FOR THE NR 1 ENGINE. REMOVED AND REPLACED THE NR 1 ENG N1 FAN SPEED SENSOR IAW AMM 77-12-01. OPS CHECKED NORMAL IAW AMM 71-00-00.

Part: BATTERY — DISCHARGED (APU) · airframe 90,470 hrs · 20,733 cycles

APU BATTERY DISCHARGED, CONSIDERED APU INOPERATIVE. REMOVED AND REPLACED THE APU BATTERY IAW AMM 24-31-04.

Part: RADAR — MALFUNCTIONED (WX SYSTEM) · airframe 90,450 hrs · 20,719 cycles

LEFT AND RIGHT RADAR SHOWING SPIKES ON ALL RANGES WELL AS TILT SETTINGS. PERFORMED AN OPERATIONAL CHECK OF THE LEFT AND RIGHT WEATHER RADAR SYSTEM , OPS TESTED GOOD IAW AMM 34-43-00.

Part: PUMP — INTERMITTENT (FUEL) · airframe 90,436 hrs · 20,715 cycles

DURING CRUISE, LEFT FWD FUEL PUMP PRESSURE INTERMITTANT. OPS CHECKED THE FUEL PUMP IAW AMM 28-22-00, OPS CHECKED GOOD. OK FOR SERVICE

Part: CONNECTOR — DAMAGED (PRESSURE SWITCH) · airframe 90,406 hrs · 20,705 cycles

WITH FUEL IN CENTER TANK AND AFTER SELECTING CENTER PUMPS ON, THE LEFT CENTER PUMP DID NOT LOD SHED , RIGHT INDICATED NORMAL OPERATION. REPLACED THE CONNECTOR AT LT OVERRIDE PRESSURE SWITCH IAW SWPM 20-61-11. REMOVED AND REPLACED THE LEFT OVERRIDE PRESSURE SWITCH IAW AMM 28-42-01, OPS CHECKED OK.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 90,349 hrs · 20,687 cycles

PRIOR TO PUSH CREW NOTED NO EGT, FUEL FLOW AND OIL TEMP INDICATION. PERFORMED AN ENGINE START IAW AMM 71-00-00-862-053-H03, ENGINE OPS NORMAL, ALL INDICATION NORMAL.

Part: PRESSURE SWITCH — MALFUNCTIONED (FUEL SYSTEM) · airframe 90,333 hrs · 20,682 cycles

AT LEVEL OFF AT FL 360, THE LT FWD FUEL PUMP EICAS MESSAGE CAME ON , AND THE LT FWD FUEL PUMP PRESSURE SWITCH LIGHT ILLUMINATED EICAS MESSAGES AND PRESSURE LIGHT, WENT OUT REPLACED LT FWD BOOST PUMP PRESSURE SWITCH; SYSTEM CHECKED GOOD IAW AMM 28-42-01.

Part: CONTROL PANEL — MALFUNCTIONED (CABIN PRESSURE) · airframe 90,342 hrs · 20,685 cycles

PRE DEPARTURE, CABIN ALTITUDE AUTO 1 STATUS MESSAGE. REMOVED AND REPLACED THE CABIN PRESSURE SELECT PANEL. OPS NORMAL IAW AMM 21-31-01.

Part: SELECTOR PANEL — MALFUNCTIONED (CABIN PRESSURE) · airframe 90,333 hrs · 20,682 cycles

DURING PRE DEPARTURE, THE CABIN ALTITUDE AUTO 1 STATUS MESSAGE. REMOVED AND REPLACED THE CABIN PRESSURE SELECTOR PANEL. OPS CHECKED GOOD IAW AMM 21-31-01.

Part: SWITCH — INOPERATIVE (BUSS) · airframe 90,333 hrs · 20,682 cycles

RIGHT UTILITY BUSS ON LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE RT UTILITY BUSS SWITCH IAW AMM 36-16-02.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 90,250 hrs · 20,656 cycles

EICAS STATUS MESSAGE "CABIN ALT AUTO 1" NOTE: BITE ON BOX FAULTS SELECTED. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER, OPS CHECKS OK.

Part: FEEDER CABLE — DAMAGED (LT IDG) · airframe 90,237 hrs · 20,652 cycles

LEFT ENGINE POWER FEEDER CABLE HEAT SHRINK FOR THE IDG DAMAGED. INSTALLED THE HEAT SHRINK IAW SWPM 20-10-14.

Part: SEAL — LEAKING (HEAT EXCHANGER) · airframe 90,237 hrs · 20,652 cycles

NR 1 PACK SECONDARY HEAT EXCHANGER LEAKING AT COUPLING. REMOVED AND REPLACED THE COUPLING SEALS IAW AMM 21-57-01.

Part: UNKNOWN — VIBRATION (THRUST REVERSER) · airframe 90,224 hrs · 20,647 cycles

DURING INITIAL CLIMB, AS FLAPS WERE RETRACTING 5 TO 1, AN AMBER REVERSER MESSAGE APPEARED FOR THE LEFT ENGINE. DECLARED AN EMERGENCY, PERFORMED QRH PROCEDURE, RETURNED TO DEPARTURE. RUMBLE & VIBRATION NOTED ABOVE 120 KIAS. PERFORMED UNUSUAL CONDITION INSPECTION IAW AMM 72-00-00-206-096--H00, AND ENGINE POST WINDMILLING INSPECTION, OPS CHECKED NORMAL.

Part: LINER — DAMAGED (NR 1 ENGINE) · airframe 90,237 hrs · 20,652 cycles

NR 1 ENGINE MID OUTER LINER IN THE 2 POSITION, HAS SEVERAL HOLES. REMOVED AND REPLACED THE LINER IAW AMM 72-33-01.

Part: FEEDER CABLE — DAMAGED (RT IDG) · airframe 90,237 hrs · 20,652 cycles

RIGHT ENGINE POWER FEEDER CABLE HEAT SHRINK FOR IDG DAMAGED. INSTALLED HEAT SHRINK IAW SWPM 20-10-14.

Part: COUPLING — LEAKING (HEAT EXCHANGER) · airframe 90,237 hrs · 20,652 cycles

NR 2 PACK SECONDARY HEAT EXCHANGER LEAKING AT COUPLING. REMOVED AND REPLACED THE COUPLING IAW IAW AMM 21-51-02.

Part: SWITCH — DAMAGED (TRIM AIR) · airframe 90,237 hrs · 20,652 cycles

TEMPERATURE CONTROL PANEL, TRIM AIR SWITCH BINDING. REMOVED AND REPLACED THE TRIM AIR SWITCH IAW SPM 20-84-13.

Part: PRESSURE SWITCH — FAILED (BOOST PUMP) · airframe 90,205 hrs · 20,639 cycles

RIGHT AFT FUEL PUMP PRESSURE LIGHT IS NOT ILLUMINATED WITH PUMP TURNED OFF. R & R THE RT AFT BOOST PUMP PRESSURE SWITCH IAW AMM 28-42-01, LEAK AND OPS CHECKED OK.

Part: CIRCUIT CARD — FAILED (RT ENGINE SPEED) · airframe 90,196 hrs · 20,636 cycles

RIGHT ENGINE SPEED CARD MESSAGE DISPLAYED. REMOVED & REPLACED THE NR 2 ENGINE N2 SPEED CARD IAW AMM 73-21-54. OPS CHECKED OK.

Part: APU — UNKNOWN · airframe 90,192 hrs · 20,635 cycles

APU INOPERATIVE. PERFORMED AN APU OPS TEST IAW AMM 49-11-00, OPS TESTED OK.

Part: SWITCH — BROKEN (FUEL PUMP) · airframe 84,465 hrs · 17,936 cycles

RIGHT AFT FUEL PUMP SWITCH BROKEN. REMOVED AND REPLACED CONTROL PANEL ASSY IAW AMM 28-22-17.

Part: DUCT — RUPTURED (APU BLEED) · airframe 90,114 hrs · 20,605 cycles

APU BLEED DUCT COUPLING IS RUPTURED&NBSP;(<P>REMOVED AND REPLACED BLEED DUCT AS PER 49-53-01 OPS CHECK GOOD,LEAK CHECK GOOD , NO DEFECTS NOTED AT THIS TIME&NBSP;</P>)

Part: CONTROL PANEL — MALFUNCTIONED (RT GENERATOR) · airframe 90,114 hrs · 20,605 cycles

R GEN LIGHT INOP&NBSP;(<P>REMOVED AND REPLACED SERVICEABLE GEN CONTROL PANEL AS PER AMM 24-22-01 OPS CHECK GOOD&NBSP;</P>)

Part: SWITCH — MALFUNCTIONED (ENGINE VALVE) · airframe 90,114 hrs · 20,605 cycles

RIGHT ENG VALVE LIGHT DID NOT ILLUMINATE ON START OR SHUTDOWN&NBSP;(<P>TRANSFERRED TO MDDR # 86908 AS PER MEL 73-21-03-01 CAT C&NBSP;</P><P>LOG PAGE 944350 REMOVED AND REPLACED RH ENG VALVE KORRY SWITCH AS PER AMM 33-13-00 OPS CHECK NORMAL MDDR # 86908 CLOSED&NBSP;</P>)

Part: CONTROL PANEL — INOPERATIVE (WEATHER RADAR) · airframe 90,052 hrs · 20,578 cycles

WEATHER RADAR FAILED ON BOTH ND WITH RR/T BUTTON SELECTED. REMOVED AND REPLACED THE WEATHER RADAR CONTROL PANEL IAW AMM 34-43-02. OPS CHECKED GOOD.

Part: CONTROL PANEL — MALFUNCTIONED (WX RADAR SYS) · airframe 89,994 hrs · 20,554 cycles

WEATHER RADAR WILL ONLY TILT 11 DEGREES DOWN. REPLACED THE WEATHER RADAR PANEL IAW AMM 34-43-02, OPS CHECKED GOOD.

Part: SWITCH — UNSECURE (BOOST PUMP) · airframe 89,988 hrs · 20,551 cycles

LEFT CENTER PUMP SWITCH FALLING OUT OF IT`S SOCKET. REMOVED AND REPLACED THE BOOST PUMP SWITCH IAW SWDM 20-83-00, OPS CHECKED GOOD.

Part: CONTROLLER — FAILED (RT ENGINE PRV) · airframe 89,981 hrs · 20,547 cycles

RIGHT ENGINE PRV EICAS MESSAGE ANNUNCIATED DURING CLIMB AT APPROXIMATELY 10000 FT. REPLACED THE NR 2 ENGINE PRV CONTROLLER IAW AMM 36-11-19, OPS CHECKED OK.

Part: IDG — FAILED · airframe 89,954 hrs · 20,536 cycles

AFTER ENGINE START, LT GEN OFF LIGHT ILLUMINATED, LT GEN DRIVE EICAS MESSAGE CAME ON, ATTEMPTED RESET IAW QRH PROCEDURE UNSUCCESSFUL. REPLACED THE LT GCU IAW MM 24-22-02, GCU REMAINS OPEN. IDG REPLACED, LEAK AND OPS CHECKED NORMAL.

Part: STATUS MESSAGE — FALSE INDICATION (COCKPIT) · airframe 89,963 hrs · 20,540 cycles

STATUS MESSAGE R ENG PRV. STATUS MESSAGE CLEARED IAW AMM REF 36-00-00.

Part: RADAR — UNKNOWN (WX SYSTEM) · airframe 89,931 hrs · 20,525 cycles

BOTH WEATHER RADARS INOPERATIVE. PERFORMED AN OPS CHECK OF THE WEATHER RADAR SYSTEM, OPS CHECKED GOOD IAW AMM 34-45-00.

Part: BLEED VALVE — INOPERATIVE (APU) · airframe 89,844 hrs · 20,491 cycles

APU AUTOSHUTDOWN WHEN TURNING THE LT PACK OFF, RIGHT PACK WAS ALREADY OFF. PERFORMED A BITE CHECK IAW FIM 49-11, FT 958. BITE REVERSE FLOW, MINI FLAG, NO FAULTS. REMOVED AND REPLACED THE SURGE BLEED VALVE, CHECKED OK IAW 49-53-01.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 89,833 hrs · 20,486 cycles

STATUS MESSAGE FOR THE RT ENGINE PRV. PERFORMED AIR SUPPLY BITE TEST IAW FIM 36-20-11. NO FAULTS NOTED, PRV BITE IAW FIM 36-11-18, ITEM 1. NO FAULT FOUND. VERIFIED SYSTEM FOR LOOSE CONNECTORS ,SENSE LINE AND LEAK ,NONE NOTED. RAN RIGHT ENGINE FOR 5 MINUTES, MESSAGE DID NOT PRESENT. OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (N1) · airframe 89,833 hrs · 20,486 cycles

DURING PREFLIGHT, COCKPIT SETUP N1 INDICATED 55 PERCENT N2, INDICATED 50 PERCENT. CYCLED EEC MAINT SWITCH ON MAINTENANCE PANEL. MESSAGE CLEARED, ALL READINGS AT CERO IAW AMM 77-35-00.

Part: TRANSCEIVER — FAILED (WX RADAR SYS) · airframe 89,822 hrs · 20,481 cycles

FIRST OFFICER RADAR TILT INOPERATIVE. REMOVED AND REPLACED WEATHER RADAR TRANCEIVER IAW AMM 34-43-01. PERFORMED A RADAR TEST IAW AMM 34-43-00, FIRST OFFICER TILT OPERATED NORMAL.

Part: ENGINE — UNKNOWN (RIGHT) · airframe 89,800 hrs · 20,470 cycles

WHILE STARTING RIGHT ENGINE, NO SPAR LIGHT ILLUMINATED. ENGINE STARTED, THEN SHUT DOWN . MX REQUESTED A SECOND START ATTEMPT . ON SECOND START, NO SPAR LIGHT ILLUMINATED , BUT ENGINE VALVE LIGHT DID ILLUMINATE WITH NO START. PERFORMED AN OPS CHECK OF BOTH ENGINES . BOTH START NORMAL . CHECKED IAW AMM. 80-11-00.

Part: CIRCUIT CARD — MALFUNCTIONED (RT ENGINE PRV) · airframe 89,794 hrs · 20,466 cycles

STATUS MESSAGE FOR THE RT ENGINE PRV. R & R THE RT BLEED AIR CIRCUIT CARD AND RT FAN AIR TEMP SENSOR IAW AMM 36-11-12, AND AMM 36-11-17. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENGINE PRV) · airframe 89,792 hrs · 20,465 cycles

STATUS MESSAGE FOR THE RT ENGINE PRV, BITE BOX IAW AMM 36-23-00 NO ISSUES NOTED. MESSAGE CLEARED.

Part: SOLENOID VALVE — FAILED (ENGINE FUEL) · airframe 89,789 hrs · 20,464 cycles

AFTER START, THE RT ENGINE FUEL VALVE EICAS MESSAGE ALONG WITH ENGINE VALVE LIGHT APPEARED . FLAMED OUT. REMOVED AND REPLACED THE RELAY K1251 IAW SWPM 20-81-11, OPS CHECKED OK . ENGINE RUNS COMPLETE, NO MESSAGES. OK FOR SERVICE. REMOVED AND REPLACED FUEL SHUTOFF SOLENOID VALVE IAW AMM 73-21-20, OPS CHECKED GOOD AFTER REPLACING RELAY.

Part: CONTROLLER — INOPERATIVE (SHUTOFF VALVE) · airframe 89,789 hrs · 20,464 cycles

RT ENGINE HPSOV INOPERATIVE. R & R THE NR 2 ENGINE HPSOV CONTROLLER IAW AMM 36-11-08 & RT BLEED AIR CIRCUIT CARD IAW AMM 36-11-012,

Part: WARNING LIGHT — FALSE ACTIVATION (RT ENGINE BLEED) · airframe 89,777 hrs · 20,457 cycles

EICAS RT ENG BLEED STAYED ON FOR 4 MINUTES THEN IT CLEARED. OPS CHECKED OK, RAN LEFT AND RIGHT ENGINE, OPERATED BLEED, ALL OPS CHECKED OK IAW AMM 71-00-00.

Part: MODULE — MALFUNCTIONED (APU) · airframe 89,775 hrs · 20,453 cycles

APU AUTO SHUT DOWN. R & R FLOW SENSING MODULE IAW AMM 49-53-03, OPS CHECKED NORMAL.

Part: O-RING — LEAKING (FUEL SYSTEM) · airframe 89,775 hrs · 20,453 cycles

AFTER FUEL FILTER CHANGE FOUND FUEL PRESSURE SWITCH TO HAVE LEAK AT O-RING. REMOVED AND REPLACED O-RING ON FUEL PRESSURE SWITCH IAW AMM 73-34-01. LEAK CHECK GOOD FOR PRESSURE SWITCH. OPS CHECK GOOD LEAK CHECK GOOD FOR FUEL FILTER CHANGE LOG PAGE 894584 ITEM M5 IAW AMM 73-11-02.

Part: RADAR — MALFUNCTIONED (WX SYSTEM) · airframe 89,767 hrs · 20,442 cycles

RADAR INOPERATIVE ON CAPTAIN`S AND FIRST OFFICER`S SIDES. INSTALLED EFIS SOFTWARE ON LEFT AND CENTER COMPUTERS IAW AMM 34-22-00. PERFORMED OPERATION CHECK OF WEATHER RADAR IAW AMM 34-43-00. OPS CHECKED GOOD.

Part: RADAR — MALFUNCTIONED (WX SYS) · airframe 89,766 hrs · 20,441 cycles

CAPTAIN'S RADAR NOT PAINTING ANYTHING, FIRST OFFICER`S RADAR ONLY PAINT A BAND. ACCOMPLISHED AN OPS CHECK OF THE WEATHER RADAR SYSTEM IAW AMM 34-43-00, OPS CHECKED NORMAL.

Part: O-RING — FAILED (FLOW SENSOR) · airframe 89,764 hrs · 20,439 cycles

STARTING RT ENGINE, APU SHUTDOWN. FOUND BAD O-RING ON FLOW PT SENSOR , REMOVED AND REPLACED THE O-RING IAW AMM 49-53-08, OPS CHECKED GOOD.

Part: SHUTOFF VALVE — FAILED (NR 2 ENGINE FUEL) · airframe 89,760 hrs · 20,433 cycles

RIGHT ENGINE SPAR VALVE LIGHT INOPERATIVE DURING ENGINE START AND SHUT DOWN. REMOVED AND REPLACED THE NR 2 ENGINE FUEL SHUTOFF VALVE IAW AMM 28-22-11-004-019, AND AMM 28-22-11-404-008, OPS CHECKED GOOD.

Part: PITOT TUBE — FAILED · airframe 89,766 hrs · 20,441 cycles

CAPTAIN`S PITOT EICAS AFTER ENGINE START. REMOVED AND REPLACED THE PITOT PROBE IAW AMM 34-11-01. SYSTEM TESTED GOOD.

Part: VALVE — FAILED (APU SURGE) · airframe 89,760 hrs · 20,433 cycles

APU AUTO SHUT DOWN AFTER PACKS TURNED OFF. REMOVED AND REPLACED APU SURGE VALVE IAW AMM 49-53 01. OPS CHECKED GOOD.

Part: SHUTOFF VALVE — MALFUNCTIONED (RT ENGINE) · airframe 89,760 hrs · 20,433 cycles

RIGHT ENGINE BLEED OFF LIGHT IS NOT ILLUMINATED WITH RIGHT ENGINE SHUT DOWN. REMOVED AND REPLACED THE PRSOV IAW 36-11-09. OPS CHECKED NORMAL.

Part: BLEED VALVE — MALFUNCTIONED (LT ENGINE) · airframe 89,760 hrs · 20,433 cycles

AFTER ENGINE START, THE LT ENGINE BLEED OFF ADVISORY MESSAGE DISPLAYED. ASSOCIATED OFF LIGHT IN LT ENGINE BLEED SWITCH WAS NOT ILLUMINATED, AND LEFT ENG BLEED VALVE WAS VERIFIED TO BE OPEN. COMPLIED WITH FIM. ACCOMPLISHED A PRSOV TEST IAW AMM 36-11-09. OPS CHECKED GOOD.

Part: CONTROL PANEL — FAULTED (IGNITION SYS) · airframe 89,747 hrs · 20,428 cycles

RAT DEPLOYED UNLOCK LT NO PRESS LT ON POST FLIGHT INSPECTION, ONLY PARTIAL DEPLOYMENT. FOUND ENG IGN START PANEL FAULTY. REMOVED AND ROUTED FOR REPAIR RECEIVED WITH 8130-3 RE-INSTALLED OPS CHECK GOOD.

Part: SEALANT — MISSING (NOSE COWL) · airframe 89,745 hrs · 20,427 cycles

NR 1 ENGINE NOSE COWL INLET L/E AT ALL 4 POINTS MISSING SEALANT. REMOVED REMAINING SEALANT AND APPLIED NEW SEALANT PER AMM 51-31-01-392-039 7A-B11.

Part: CONNECTOR — DISCONNECTED (FIRE BOTTLE) · airframe 89,745 hrs · 20,425 cycles

NR 2 ENGINE SQUIB TEST INOP FOR SYSTEM NR 1 AND NR 2. FOUND BOTH NR 1 AND NR 2 SQUIB CANNON PLUG DISCONNECTED FOR NR 2 ENG FIRE BOTTLE. CONNECTED NR 1 AND NR 2 SQUIB CANNON PLUG PER AMM 26-21-03-404-111 STEPS F(8) TO (12) OP CHECK NORMAL PER AMM 26-21-03-404-111 STEP G.

Part: FUEL LINE — DENTED (FUEL SYSTEM) · airframe 89,745 hrs · 20,427 cycles

NR 2 PYLON FWD SECTION FUEL LINE HAVE SEVERAL DENTS. REMOVED AND REPLACED FUEL LINE OPS CHECK GOOD PER WP 000646 AND AMM 28-22-07.

Part: SEAL — DETERIORATED (LT WING) · airframe 89,745 hrs · 20,427 cycles

LEFT WING L/E BULLNOSE SEAL TORN/DETERIORATED(<P>REMOVED AND REPLACED SEAL ON LEFT WING NR 1 ENGINE PYLON L/E FIXED BULLNOSE IAW AMM 20-00-00.

Part: SEAL — DAMAGED (EXHAUST CONE) · airframe 89,745 hrs · 20,427 cycles

NR 1 ENGINE AFT EXHAUST CONE L/E FINGER SEALS BROKEN, CRACKED AND CHAFED. REMOVED AND REPLACED THE NR 1 ENGINE AFT EXHAUST CONE L/E FINGER SEALS IAW SRM 51-40-02 AND AMM 20-11-00,

Part: DUCT — WORN (ANTI-ICE SYSTEM) · airframe 89,745 hrs · 20,427 cycles

ANTI-ICE DUCT CROSSOVER BETWEEN SLATS 8-9 HAS WEAR MARK (CROSSOVER DUCT). REMOVED AND REPLACED DUCT AND SEAL PER WP000646 OPS 21016 AND AMM 30-11-06.

Part: PRECOOLER — WORN (NR 2) · airframe 89,745 hrs · 20,427 cycles

NR 2 PRECOOLER WORN AT THE FAN AIR MODULATING VALVE COOLING FINS AT SEVERAL PLACES. REMOVED AND REPLACED THE PRE-COOLER .

Part: BLADE — NICKED (NR1 ENGINE) · airframe 89,745 hrs · 20,427 cycles

NR 1 ENGINE FAN BLADE L/E NICKED. BLADE NR 3 REWORKED IAW AMM 72-31-02 E2 THROUGH E4. BLADE IS WITHIN LIMITS.

Part: PACKING — DAMAGED (FUEL SYSTEM) · airframe 89,745 hrs · 20,427 cycles

APU FUEL SUPPLY LINE SHROUD FAILED LEAK CHECK. REMOVED AND REPLACED FUEL SHROUD FUEL SUPPLY LINE PACKINGS PER AMM 28-25-05. LEAK TEST GOOD PER AMM 28-25-00 3D 1 THROUGH 9.

Part: BLADE — NICKED (NR 1 ENGINE) · airframe 89,745 hrs · 20,427 cycles

NR 1 ENGINE FAN BLADE NR 9 L/E NICKED. REWORKED THE FAN BLADE IAW AMM 72-31-02.

Part: BLADE — NICKED (NR 1 ENGINE) · airframe 89,745 hrs · 20,427 cycles

NR 1 ENGINE FAN BLADE L/E HAVE NICKS. BLADE NR 8 REWORKED IAW AMM 72-31-02 E2 THROUGH E4, BLADE IS WITHIN LIMITS.

Part: CLAMP — CRACKED (NR 1 ENGINE) · airframe 89,745 hrs · 20,427 cycles

NR 1 ENG RT BRACKET SUPPORT CLAMP IS CRACKED AT 9 O'CLOCK POSITION. INSTALLED NEW CLAMP ON ENGINE NR 1 ON 9 O'CLOCK POSITION IAW 70-00-00 TASK 70-00-00-912-001-H00 2A(4)(H).

Part: BLADE — NICKED (NR 1 ENGINE FAN) · airframe 89,745 hrs · 20,427 cycles

NR 1 ENGINE FAN BLADE L/E HAVE NICKS BLADE NR 6. REWORKED FAN BLADE IAW AMM 72-31-02.

Part: IGNITER — CORRODED (APU) · airframe 89,745 hrs · 20,427 cycles

APU IGNITER TIP CORRODED. REMOVED AND REPLACED APU IGNITER IAW AMM 49-41-02-404-006. PERFORMED AN OPS TESTED IAW AMM 49-11-00-802-002.

Part: PLATE — BROKEN (NR 1 COWLING) · airframe 89,745 hrs · 20,427 cycles

NR 1 ENGINE I/B CORE COWL HAS BROKEN CHAFE PLATE AT TRAILING EDGE. REMOVED AND REPLACED I/B CORE COWL PER AMM 71-11-06.

Part: BATTERY — DISCHARGED (APU) · airframe 89,745 hrs · 20,427 cycles

APU DID NOT CRANK, APU DOOR FAULT ON LOWER EICAS. TROUBLESHOT THE SYSTEM AND FOUND THAT APU DOOR ACTUATOR WAS NOT EQUIPPED WITH PROPER VOLTAGE TO OPERATE. CHARGED THE APU BATTERY WITH APU BATTERY CHARGER IAW AMM 24-31-05-424-007, STEP E. APU OPS CHECKED GOOD IAW AMM 49-11-00-802-002.

Part: DUCT — DENTED (BLEED AIR SYS) · airframe 89,745 hrs · 20,427 cycles

NR 1 POS HAS BLEED AIR DUCT UIN HOT SECTION 9 O'CLOCK WITH DENT. REMOVED FAN DISCHARGED AIR DUCT PER AMM 75-23-01 PART 2(C) 5,6. INSTALLED FAN DISCHARGED AIR PER AMM 75-23-01-404-007-H00 PART 3(D) 4 (B,E) AND 8 WITH T98583-1.

Part: SEAL — TORN (NR 1 COWLING) · airframe 89,745 hrs · 20,427 cycles

NR 2 ENGINE I/B FAN COWL HAS TORN SEAL BOTTOM OF TRAILING EDGE. NR 2 ENGINE I/B FAN COWL SEAL BOTTOM ON TRAILING EDGE WAS REMOVED AND REPLACED IAW AMM 20-11-00.

Part: PLUG — ERODED (APU) · airframe 89,745 hrs · 20,427 cycles

APU TIP ERRODED. REMOVED AND REPLACED IGNITOR PLUG PER EO 6479A003-CS OPS CHECK GOOD.

Part: BLADE — NICKED (NR 2 ENGINE) · airframe 89,745 hrs · 20,427 cycles

NR 2 ENGINE FAN BLADE L.E. HAS NICKS. REWORKED THE BLADE IAW AMM 72-31-02, 6.2 THROUGH 6.4, BLADE IS WITHIN LIMITS.

Part: PRECOOLER — DAMAGED (BLEED AIR SYS) · airframe 89,745 hrs · 20,427 cycles

NR 2 PRE-COOLER NOZZLE INLET COOLING FINS WORN. RECEIVED SERVICEABLE PRE-COOLER PN 792930-5 SN 890915.

Part: SUPPORT — BROKEN (PRECOOLER) · airframe 89,745 hrs · 20,427 cycles

NR 1 PRECOOLER INLET HAD THE INSIDE SUPPORTS TO THE FINS BROKEN AND MISSING PIECES. REMOVED AND REPLACED THE PRECOOLER IAW WP 000646 OPS 2518.

Part: COWLING — DAMAGED (NR 1 ENGINE) · airframe 89,745 hrs · 20,427 cycles

NR 1 ENGINE I/B CORE COWL HAS DAMAGED TRAILING EDGE CORNER. REMOVED AND REPLACED NR 1 ENG I/B CORE COWL PER AMM.

Part: CHARGER — INOPERATIVE (APU BATTERY) · airframe 89,745 hrs · 20,427 cycles

REPLACED THE APU BATTERY IAW RESULTS STEP 4. REFERENCE EO 6749A003-CS. REMOVED AND REPLACED THE BATTERY CHARGER IAW EO 6749A003-CS OPS 4062.

Part: SEAL — DAMAGED (NR 2 COWLING) · airframe 89,745 hrs · 20,427 cycles

NR 2 ENGINE O/B FAN COWL HAS A DAMAGED SEAL AT TRAILING EDGE. REMOVED AND REPLACED DAMAGED SEAL AT NR 2 ENGINE O/B FAN COWL T/E SRM 51-40-02.

Part: BLADE — NICKED (NR 1 FAN) · airframe 89,745 hrs · 20,427 cycles

NR 1 ENGINE FAN BLADE HAVE NICKS ON L/E BLADE NR 7. REWORKED ENGINE FAN BLADE IAW AMM 72-31-02.

Part: ISOLATION VALVE — BROKEN (BLEED AIR SYS) · airframe 89,745 hrs · 20,427 cycles

LEFT ISOLATION VALVE BYPASS CHECK VALVE SPRING BROKEN. REMOVED AND REPLACED LEFT ISOLATION BY PASS VALVE. OPERATIONAL CHECKS COMPLIED WITH AND GOOD PER AMM.

Part: ACOUSTIC LINER — DENTED (NOSE COWL) · airframe 89,745 hrs · 20,427 cycles

NR 1 ENGINE NOSE COWL INLET ACOUSTIC HAVE MULTIPLE DENTS IN SEVERAL PLACES. REPAIRED NR 1 ENGINE NOSE COWL INLET ACOUSTIC IAW SRM 54-12-01 REPAIR 3 7.11 FIG 201.

Part: IGNITION LEAD — ERODED (APU) · airframe 89,745 hrs · 20,427 cycles

APU IGNITION LEAD TIP IS ERODED. REMOVED AND REPLACED APU IGNITOR LEAD. PERFORMED APU NORMAL OPERATION START TEST. APU TEST CHECKED GOOD IAW AMM 49-11-00.

Part: CONNECTOR — NOT SEATED (CARGO BAY) · airframe 89,745 hrs · 20,427 cycles

CARGO FIRE BOTTLE DISCHARGED LIGHT ILLUMINATED. SEATED CONNECTORS PER AMM 26-2302 OPS CHECK GOOD PER AMM 26-23-02.

Part: STARTER — DEFECTIVE (APU) · airframe 89,745 hrs · 20,427 cycles

APU STARTER BRUSH INDICATOR IS RECESSED BELOW TOP OF PROTECTIVE GUARD. REMOVED AND REPLACED STARTER PER AMM 49-00-00 OPS CHECK GOOD.

Part: FASTENER — WORN (THRUST REVERSER) · airframe 89,745 hrs · 20,427 cycles

LT T/R HAS EXCESSIVE MOVEMENT IN NR 7 BLOCKER DOOR FORM THE TOP. REMOVED AND REPLACED WORN HARDWARE ON NR 7 BLOCKER DOOR ON NR 2 LT T/R INSTALLED BLOCKER DOOR IAW AMM 78-31-14-864-009. OPS CHECK GOOD PER AMM 78-31-14-206-001.

Part: BLADE — NICKED (ENGINE) · airframe 89,745 hrs · 20,427 cycles

NR 1 ENGINE FAN BLADE HAVE SEVERAL NICKS ON L/E BLADE NR 4. REWORKED THE FAN BLADE IAW AMM 72-31-02 E2 THROUGH E4 BLADE IS WITHIN LIMITS.

Part: BLADE — NICKED (NR 1 ENGINE) · airframe 89,745 hrs · 20,427 cycles

NR 1 ENGINE FAN BLADE NICKED. REWORKED THE NR 5 BLADE IAW AMM 72-31-02, E2 THROUGH E4 BLADE IS WITHIN LIMITS.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 89,745 hrs · 20,427 cycles

LT AND RT PIMU DISPLAY ON ECS MESSAGE. PERFORMED OPS CHECK OF THE NR 1 AND 2 PIMU FAULT MESSAGES IAW TASK A77-305-01. OPS CHECKED GOOD, NO DEFECTS NOTED.